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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  25833.39
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.4
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.378
   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 
   ------------------------------------------------------------------------
   116/10:27:43.751           1.5               1.6              1.6    
   N/A                       -0.4               0.1              226.6  
   000/00:07:27.501          -0.5               0.2              222.1  
   
   119/08:06:35.451           2.1               2.3              2.3    
   N/A                       -0.9               0.1              226.9  
   000/00:11:10.901          -0.4               0.5              223.2  
   
 
 
    Coasting Arc #1 (Orbit 287)
    ---------------------------------------
 
    Vector Time (GMT): 2014/113/17:26:51.399
    Vector Time (MET): N/A
    Weight (LBS)     : 924085.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3755656.55                 A    =         6793116.14  meter
     Y    =       -3887958.49  meter          E    =           .0007093
     Z    =       -4121806.50                 I    =           51.70155
     XDOT =       6312.011084                 Wp   =           38.54694
     YDOT =      -2052.594844  meter/sec      RA   =            8.96751  deg
     ZDOT =      -3813.288397                 TA   =          192.04221
                                              MA   =          192.05917
                                              Ha   =            226.454  n.mi
                                              Hp   =            221.501
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12321707.85                 X    =        -3691878.89
     Y    =      -12755769.33  feet           Y    =        -3929600.30  meter
     Z    =      -13522987.21                 Z    =        -4139895.89
     XDOT =      20708.697783                 XDOT =        6353.018355
     YDOT =      -6734.235053  feet/sec       YDOT =       -1981.780830  meter/sec
     ZDOT =     -12510.788704                 ZDOT =       -3782.525670
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7083919.95                 X    =        -2159178.80
     Y    =       16195545.23  feet           Y    =         4936402.19  meter
     Z    =      -13598812.87                 Z    =        -4144918.16
     XDOT =     -13015.888606                 XDOT =       -3967.242847
     YDOT =     -16093.558524  feet/sec       YDOT =       -4905.316638  meter/sec
     ZDOT =     -12380.308799                 ZDOT =       -3773.518122
  
  
    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   14113.75009039  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6459   9.3723 0004042 318.3209  41.7634 15.50343197  2883
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14113.75009039   =   yrday.fracday
    Element set:     900
    Inclination:       51.6459  deg
    RA of node:         9.3723  deg
    Eccentricity:     .0004042     
    Arg of perigee:   318.3209  deg
    Mean anomaly:      41.7634  deg
    Mean motion:   15.50343197  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             288
    Checksum:              287
 
 
    Coasting Arc #2 (Orbit 303)
    ---------------------------------------
 
    Vector Time (GMT): 2014/114/17:26:51.399
    Vector Time (MET): N/A
    Weight (LBS)     : 924085.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3592354.66                 A    =         6792016.06  meter
     Y    =        3730699.49  meter          E    =           .0006088
     Z    =        4388895.32                 I    =           51.66719
     XDOT =      -6491.273744                 Wp   =           90.61647
     YDOT =       2242.139804  meter/sec      RA   =            4.01190  deg
     ZDOT =       3403.133654                 TA   =          324.88926
                                              MA   =          324.92937
                                              Ha   =            226.324  n.mi
                                              Hp   =            221.513
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11785940.50                 X    =         3529050.14
     Y    =       12239827.72  feet           Y    =         3770517.87  meter
     Z    =       14399262.84                 Z    =         4406192.56
     XDOT =     -21296.829869                 XDOT =       -6532.394862
     YDOT =       7356.101718  feet/sec       YDOT =        2169.320537  meter/sec
     ZDOT =      11165.136659                 ZDOT =        3371.499690
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6547677.25                 X    =         1995732.02
     Y    =      -15612705.97  feet           Y    =        -4758752.78  meter
     Z    =       14471761.52                 Z    =         4410992.91
     XDOT =      14143.607493                 XDOT =        4310.971564
     YDOT =      16168.946804  feet/sec       YDOT =        4928.294986  meter/sec
     ZDOT =      11030.946066                 ZDOT =        3362.232361
  
  
    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   14114.78143299  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6456   4.2593 0004086 318.5061  41.5779 15.50383738  3047
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14114.78143299   =   yrday.fracday
    Element set:     901
    Inclination:       51.6456  deg
    RA of node:         4.2593  deg
    Eccentricity:     .0004086     
    Arg of perigee:   318.5061  deg
    Mean anomaly:      41.5779  deg
    Mean motion:   15.50383738  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             304
    Checksum:              303
 
 
    Coasting Arc #3 (Orbit 318)
    ---------------------------------------
 
    Vector Time (GMT): 2014/115/17:26:51.399
    Vector Time (MET): N/A
    Weight (LBS)     : 924085.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3396259.06                 A    =         6790954.40  meter
     Y    =       -3620613.82  meter          E    =           .0010145
     Z    =       -4643803.08                 I    =           51.63402
     XDOT =       6630.137327                 Wp   =           47.75575
     YDOT =      -2440.176492  meter/sec      RA   =          359.05482  deg
     ZDOT =      -2943.917733                 TA   =          192.85325
                                              MA   =          192.87913
                                              Ha   =            226.491  n.mi
                                              Hp   =            221.197
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11142582.21                 X    =        -3332961.76
     Y    =      -11878654.25  feet           Y    =        -3658239.40  meter
     Z    =      -15235574.41                 Z    =        -4660147.79
     XDOT =      21752.419052                 XDOT =        6671.231932
     YDOT =      -8005.828387  feet/sec       YDOT =       -2365.804487  meter/sec
     ZDOT =      -9658.522747                 ZDOT =       -2911.609099
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6219023.68                 X    =        -1895558.42
     Y    =       14983051.26  feet           Y    =         4566834.02  meter
     Z    =      -15304058.67                 Z    =        -4664677.08
     XDOT =     -15249.820222                 XDOT =       -4648.145204
     YDOT =     -16063.642162  feet/sec       YDOT =       -4896.198131  meter/sec
     ZDOT =      -9521.452832                 ZDOT =       -2902.138823
  
  
    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   14115.74829269  .00016717  00000-0  10270-3 0  9028
    2 25544  51.6466 359.4675 0003973 324.6309  35.4578 15.50424091  3194
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14115.74829269   =   yrday.fracday
    Element set:     902
    Inclination:       51.6466  deg
    RA of node:       359.4675  deg
    Eccentricity:     .0003973     
    Arg of perigee:   324.6309  deg
    Mean anomaly:      35.4578  deg
    Mean motion:   15.50424091  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             319
    Checksum:              326
 
 
    Coasting Arc #4 (Orbit 329)
    ---------------------------------------
 
    Vector Time (GMT): 2014/116/10:31:27.501
    Vector Time (MET): N/A
    Weight (LBS)     : 923924.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2113675.11                 A    =         6789748.99  meter
     Y    =       -3917300.75  meter          E    =           .0011491
     Z    =       -5137085.45                 I    =           51.60860
     XDOT =       7259.777088                 Wp   =           58.50166
     YDOT =      -1830.524792  meter/sec      RA   =          355.52270  deg
     ZDOT =      -1587.956449                 TA   =          196.13004
                                              MA   =          196.16665
                                              Ha   =            226.595  n.mi
                                              Hp   =            222.108
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6934629.62                 X    =        -2044759.20
     Y    =      -12852036.58  feet           Y    =        -3940552.26  meter
     Z    =      -16853954.88                 Z    =        -5147185.85
     XDOT =      23818.166299                 XDOT =        7287.420757
     YDOT =      -6005.658767  feet/sec       YDOT =       -1749.186852  meter/sec
     ZDOT =      -5209.830870                 ZDOT =       -1552.621696
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9232950.37                 X    =        -2814203.27
     Y    =      -11251593.86  feet           Y    =        -3429485.81  meter
     Z    =      -16895975.57                 Z    =        -5149893.35
     XDOT =      21373.906871                 XDOT =        6514.766814
     YDOT =      -9924.843111  feet/sec       YDOT =       -3025.092180  meter/sec
     ZDOT =      -5060.078139                 ZDOT =       -1542.311817
  
  
    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   14116.45730873  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6500 355.9573 0004705 312.3578  47.7174 15.50151030  3308
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14116.45730873   =   yrday.fracday
    Element set:     903
    Inclination:       51.6500  deg
    RA of node:       355.9573  deg
    Eccentricity:     .0004705     
    Arg of perigee:   312.3578  deg
    Mean anomaly:      47.7174  deg
    Mean motion:   15.50151030  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             330
    Checksum:              282
 
 
    Coasting Arc #5 (Orbit 345)
    ---------------------------------------
 
    Vector Time (GMT): 2014/117/10:31:27.501
    Vector Time (MET): N/A
    Weight (LBS)     : 923924.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1966924.20                 A    =         6789259.44  meter
     Y    =        3870421.69  meter          E    =           .0001263
     Z    =        5219647.05                 I    =           51.57621
     XDOT =      -7267.053605                 Wp   =          350.74412
     YDOT =       2136.943126  meter/sec      RA   =          350.56180  deg
     ZDOT =       1155.143227                 TA   =           88.16847
                                              MA   =           88.15400
                                              Ha   =            226.602  n.mi
                                              Hp   =            222.081
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6453163.38                 X    =         1898142.25
     Y    =       12698233.88  feet           Y    =         3892032.83  meter
     Z    =       17124826.28                 Z    =         5229034.96
     XDOT =     -23842.039386                 XDOT =       -7296.020695
     YDOT =       7010.968262  feet/sec       YDOT =        2055.516373  meter/sec
     ZDOT =       3789.839985                 ZDOT =        1119.769780
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8920241.39                 X    =         2718889.58
     Y    =       11044460.25  feet           Y    =         3366351.48  meter
     Z    =       17163837.79                 Z    =         5231537.76
     XDOT =     -21002.616828                 XDOT =       -6401.597609
     YDOT =      11312.894405  feet/sec       YDOT =        3448.170215  meter/sec
     ZDOT =       3639.878840                 ZDOT =        1109.435070
  
  
    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   14117.48878425  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6497 350.8463 0004771 314.7971  45.2791 15.50184535  3462
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14117.48878425   =   yrday.fracday
    Element set:     904
    Inclination:       51.6497  deg
    RA of node:       350.8463  deg
    Eccentricity:     .0004771     
    Arg of perigee:   314.7971  deg
    Mean anomaly:      45.2791  deg
    Mean motion:   15.50184535  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             346
    Checksum:              327
 
 
    Coasting Arc #6 (Orbit 360)
    ---------------------------------------
 
    Vector Time (GMT): 2014/118/10:31:27.501
    Vector Time (MET): N/A
    Weight (LBS)     : 923924.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1819962.12                 A    =         6788871.92  meter
     Y    =       -3866360.58  meter          E    =           .0012370
     Z    =       -5285512.44                 I    =           51.54493
     XDOT =       7222.498806                 Wp   =           65.84481
     YDOT =      -2432.070921  meter/sec      RA   =          345.59819  deg
     ZDOT =       -704.219393                 TA   =          197.38618
                                              MA   =          197.42858
                                              Ha   =            226.685  n.mi
                                              Hp   =            221.854
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5971004.33                 X    =        -1750916.49
     Y    =      -12684910.03  feet           Y    =        -3886326.75  meter
     Z    =      -17340920.09                 Z    =        -5294185.86
     XDOT =      23695.862224                 XDOT =        7252.578918
     YDOT =      -7979.235305  feet/sec       YDOT =       -2351.136147  meter/sec
     ZDOT =      -2310.431079                 ZDOT =        -669.059618
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8635410.61                 X    =        -2632073.15
     Y    =      -10988181.82  feet           Y    =        -3349197.82  meter
     Z    =      -17376906.77                 Z    =        -5296481.18
     XDOT =      20422.740781                 XDOT =        6224.851390
     YDOT =     -12613.035887  feet/sec       YDOT =       -3844.453338  meter/sec
     ZDOT =      -2161.328716                 ZDOT =        -658.772993
  
  
    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   14118.45576842  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6498 346.0547 0004895 318.6572  41.4207 15.50230390  3618
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14118.45576842   =   yrday.fracday
    Element set:     905
    Inclination:       51.6498  deg
    RA of node:       346.0547  deg
    Eccentricity:     .0004895     
    Arg of perigee:   318.6572  deg
    Mean anomaly:      41.4207  deg
    Mean motion:   15.50230390  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             361
    Checksum:              310
 
 
    Coasting Arc #7 (Orbit 374)
    ---------------------------------------
 
    Vector Time (GMT): 2014/119/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1636723.15                 A    =         6789959.36  meter
     Y    =       -3906443.52  meter          E    =           .0010713
     Z    =       -5315847.31                 I    =           51.51639
     XDOT =       7171.803267                 Wp   =           69.35562
     YDOT =      -2662.457413  meter/sec      RA   =          341.11175  deg
     ZDOT =       -248.322807                 TA   =          198.24979
                                              MA   =          198.28827
                                              Ha   =            226.912  n.mi
                                              Hp   =            223.157
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5369826.61                 X    =        -1567095.54
     Y    =      -12816415.75  feet           Y    =        -3924357.25  meter
     Z    =      -17440443.93                 Z    =        -5323629.21
     XDOT =      23529.538277                 XDOT =        7202.248737
     YDOT =      -8735.096500  feet/sec       YDOT =       -2582.087482  meter/sec
     ZDOT =       -814.707372                 ZDOT =        -213.408424
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -422229.29                 X    =         -128695.49
     Y    =      -13848929.14  feet           Y    =        -4221153.60  meter
     Z    =      -17472650.60                 Z    =        -5325663.90
     XDOT =      24092.958569                 XDOT =        7343.533772
     YDOT =        120.058781  feet/sec       YDOT =          36.593916  meter/sec
     ZDOT =       -666.606591                 ZDOT =        -203.181689
  
  
    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   14119.35826836  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6487 341.5820 0005789 304.6852  55.3753 15.49813461  3758
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14119.35826836   =   yrday.fracday
    Element set:     906
    Inclination:       51.6487  deg
    RA of node:       341.5820  deg
    Eccentricity:     .0005789     
    Arg of perigee:   304.6852  deg
    Mean anomaly:      55.3753  deg
    Mean motion:   15.49813461  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             375
    Checksum:              332
 
 
    Coasting Arc #8 (Orbit 390)
    ---------------------------------------
 
    Vector Time (GMT): 2014/120/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1627875.48                 A    =         6789758.51  meter
     Y    =        3903706.94  meter          E    =           .0004505
     Z    =        5313569.48                 I    =           51.48698
     XDOT =      -7030.093143                 Wp   =          328.58076
     YDOT =       3041.363806  meter/sec      RA   =          336.14790  deg
     ZDOT =        -76.904445                 TA   =          122.17625
                                              MA   =          122.13255
                                              Ha   =            226.957  n.mi
                                              Hp   =            223.082
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5340798.80                 X    =         1558290.20
     Y    =       12807437.48  feet           Y    =         3921521.87  meter
     Z    =       17432970.74                 Z    =         5321308.58
     XDOT =     -23064.610049                 XDOT =       -7063.206280
     YDOT =       9978.227711  feet/sec       YDOT =        2962.563645  meter/sec
     ZDOT =       -252.311170                 ZDOT =        -111.136817
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         636086.17                 X    =          193879.06
     Y    =       13821447.95  feet           Y    =         4212777.34  meter
     Z    =       17464994.31                 Z    =         5323330.27
     XDOT =     -24065.059462                 XDOT =       -7335.030124
     YDOT =       1625.368991  feet/sec       YDOT =         495.412468  meter/sec
     ZDOT =       -397.592396                 ZDOT =        -121.186162
  
  
    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   14120.38995938  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6483 336.4724 0005962 307.5047  52.5561 15.49877362  3915
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14120.38995938   =   yrday.fracday
    Element set:     907
    Inclination:       51.6483  deg
    RA of node:       336.4724  deg
    Eccentricity:     .0005962     
    Arg of perigee:   307.5047  deg
    Mean anomaly:      52.5561  deg
    Mean motion:   15.49877362  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             391
    Checksum:              335
 
 
    Coasting Arc #9 (Orbit 405)
    ---------------------------------------
 
    Vector Time (GMT): 2014/121/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1633879.71                 A    =         6789782.68  meter
     Y    =       -3923329.93  meter          E    =           .0010747
     Z    =       -5303928.32                 I    =           51.45978
     XDOT =       6847.135035                 Wp   =           72.95747
     YDOT =      -3396.930675  meter/sec      RA   =          331.18120  deg
     ZDOT =        407.220434                 TA   =          200.92067
                                              MA   =          200.96467
                                              Ha   =            227.099  n.mi
                                              Hp   =            222.826
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5360497.74                 X    =        -1564121.45
     Y    =      -12871817.34  feet           Y    =        -3941210.93  meter
     Z    =      -17401339.63                 Z    =        -5311696.22
     XDOT =      22464.353788                 XDOT =        6882.633200
     YDOT =     -11144.785680  feet/sec       YDOT =       -3320.163139  meter/sec
     ZDOT =       1336.025047                 ZDOT =         440.569676
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -872061.63                 X    =         -265804.39
     Y    =      -13875824.77  feet           Y    =        -4229351.39  meter
     Z    =      -17433480.26                 Z    =        -5313724.78
     XDOT =      23825.264623                 XDOT =        7261.940657
     YDOT =      -3338.345741  feet/sec       YDOT =       -1017.527782  meter/sec
     ZDOT =       1477.633772                 ZDOT =         450.382774
  
  
    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   14121.35714847  .00016717  00000-0  10270-3 0  9083
    2 25544  51.6489 331.6816 0005941 312.0134  48.0511 15.49891639  4060
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14121.35714847   =   yrday.fracday
    Element set:     908
    Inclination:       51.6489  deg
    RA of node:       331.6816  deg
    Eccentricity:     .0005941     
    Arg of perigee:   312.0134  deg
    Mean anomaly:      48.0511  deg
    Mean motion:   15.49891639  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             406
    Checksum:              307
 
 
    Coasting Arc #10 (Orbit 421)
    ---------------------------------------
 
    Vector Time (GMT): 2014/122/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1614812.36                 A    =         6789741.32  meter
     Y    =        3972064.44  meter          E    =           .0006068
     Z    =        5266567.38                 I    =           51.43337
     XDOT =      -6652.362964                 Wp   =          345.19223
     YDOT =       3721.049054  meter/sec      RA   =          326.21243  deg
     ZDOT =       -761.156447                 TA   =          112.14106
                                              MA   =          112.07664
                                              Ha   =            227.156  n.mi
                                              Hp   =            222.713
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5297940.81                 X    =         1544692.12
     Y    =       13031707.49  feet           Y    =         3989730.14  meter
     Z    =       17278764.36                 Z    =         5274241.80
     XDOT =     -21825.337809                 XDOT =       -6689.780642
     YDOT =      12208.166189  feet/sec       YDOT =        3646.448864  meter/sec
     ZDOT =      -2497.232439                 ZDOT =        -793.564020
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1003346.18                 X    =          305819.92
     Y    =       13992466.24  feet           Y    =         4264903.71  meter
     Z    =       17310501.43                 Z    =         5276240.84
     XDOT =     -23460.262502                 XDOT =       -7150.688011
     YDOT =       4964.478187  feet/sec       YDOT =        1513.172951  meter/sec
     ZDOT =      -2634.915974                 ZDOT =        -803.122389
  
  
    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   14122.38878948  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6487 326.5715 0006118 314.9221  45.1432 15.49955229  4228
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14122.38878948   =   yrday.fracday
    Element set:     909
    Inclination:       51.6487  deg
    RA of node:       326.5715  deg
    Eccentricity:     .0006118     
    Arg of perigee:   314.9221  deg
    Mean anomaly:      45.1432  deg
    Mean motion:   15.49955229  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             422
    Checksum:              323
 
 
    Coasting Arc #11 (Orbit 436)
    ---------------------------------------
 
    Vector Time (GMT): 2014/123/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1623196.47                 A    =         6789928.30  meter
     Y    =       -4038498.86  meter          E    =           .0010259
     Z    =       -5219642.43                 I    =           51.40946
     XDOT =       6421.305862                 Wp   =           75.74770
     YDOT =      -4015.152299  meter/sec      RA   =          321.24160  deg
     ZDOT =       1114.001075                 TA   =          204.95797
                                              MA   =          205.00761
                                              Ha   =            227.280  n.mi
                                              Hp   =            222.470
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5325447.74                 X    =        -1552560.75
     Y    =      -13249668.16  feet           Y    =        -4056255.40  meter
     Z    =      -17124811.13                 Z    =        -5227356.33
     XDOT =      21067.276451                 XDOT =        6460.315425
     YDOT =     -13173.071847  feet/sec       YDOT =       -3943.127049  meter/sec
     ZDOT =       3654.859171                 ZDOT =        1145.289937
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1208806.00                 X    =         -368444.07
     Y    =      -14190120.17  feet           Y    =        -4325148.63  meter
     Z    =      -17156705.22                 Z    =        -5229363.75
     XDOT =      22898.296829                 XDOT =        6979.400873
     YDOT =      -6513.279911  feet/sec       YDOT =       -1985.247717  meter/sec
     ZDOT =       3787.862966                 ZDOT =        1154.540632
  
  
    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   14123.35593144  .00016717  00000-0  10270-3 0  9103
    2 25544  51.6493 321.7806 0006145 319.0568  41.0114 15.49969010  4374
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14123.35593144   =   yrday.fracday
    Element set:     910
    Inclination:       51.6493  deg
    RA of node:       321.7806  deg
    Eccentricity:     .0006145     
    Arg of perigee:   319.0568  deg
    Mean anomaly:      41.0114  deg
    Mean motion:   15.49969010  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             437
    Checksum:              291
 
 
    Coasting Arc #12 (Orbit 452)
    ---------------------------------------
 
    Vector Time (GMT): 2014/124/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1611161.95                 A    =         6790075.27  meter
     Y    =        4138053.43  meter          E    =           .0007719
     Z    =        5138455.26                 I    =           51.38704
     XDOT =      -6183.892322                 Wp   =          359.83255
     YDOT =       4268.230915  meter/sec      RA   =          316.26884  deg
     ZDOT =      -1490.730905                 TA   =          104.63167
                                              MA   =          104.54607
                                              Ha   =            227.349  n.mi
                                              Hp   =            222.312
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5285964.40                 X    =         1539808.33
     Y    =       13576290.79  feet           Y    =         4155671.41  meter
     Z    =       16858449.02                 Z    =         5146108.92
     XDOT =     -20288.360638                 XDOT =       -6223.919476
     YDOT =      14003.382266  feet/sec       YDOT =        4198.854889  meter/sec
     ZDOT =      -4890.849427                 ZDOT =       -1520.868832
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1328252.48                 X    =          404851.36
     Y    =       14471542.20  feet           Y    =         4410926.06  meter
     Z    =       16890074.20                 Z    =         5148094.61
     XDOT =     -22226.962793                 XDOT =       -6774.778259
     YDOT =       7926.804375  feet/sec       YDOT =        2416.089973  meter/sec
     ZDOT =      -5019.028491                 ZDOT =       -1529.799884
  
  
    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   14124.38752260  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6494 316.6702 0006316 322.1759  37.8947 15.50033996  4532
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14124.38752260   =   yrday.fracday
    Element set:     911
    Inclination:       51.6494  deg
    RA of node:       316.6702  deg
    Eccentricity:     .0006316     
    Arg of perigee:   322.1759  deg
    Mean anomaly:      37.8947  deg
    Mean motion:   15.50033996  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             453
    Checksum:              310
 
 
    Coasting Arc #13 (Orbit 467)
    ---------------------------------------
 
    Vector Time (GMT): 2014/125/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1637908.37                 A    =         6790451.72  meter
     Y    =       -4246799.51  meter          E    =           .0009254
     Z    =       -5046278.93                 I    =           51.36674
     XDOT =       5918.258796                 Wp   =           76.55430
     YDOT =      -4486.042742  meter/sec      RA   =          311.29439  deg
     ZDOT =       1859.381423                 TA   =          211.53279
                                              MA   =          211.58828
                                              Ha   =            227.456  n.mi
                                              Hp   =            222.089
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5373715.12                 X    =        -1565784.55
     Y    =      -13933069.26  feet           Y    =        -4264712.32  meter
     Z    =      -16556033.23                 Z    =        -5054060.60
     XDOT =      19416.859567                 XDOT =        5958.950525
     YDOT =     -14717.988000  feet/sec       YDOT =       -4419.633477  meter/sec
     ZDOT =       6100.332752                 ZDOT =        1888.230522
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1573459.94                 X    =         -479590.59
     Y    =      -14814378.43  feet           Y    =        -4515422.55  meter
     Z    =      -16588185.10                 Z    =        -5056078.82
     XDOT =      21390.780205                 XDOT =        6519.909807
     YDOT =      -9221.862907  feet/sec       YDOT =       -2810.823814  meter/sec
     ZDOT =       6223.096030                 ZDOT =        1896.799670
  
  
    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   14125.35461761  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6495 311.8791 0006374 325.8676  34.2064 15.50045478  4685
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14125.35461761   =   yrday.fracday
    Element set:     912
    Inclination:       51.6495  deg
    RA of node:       311.8791  deg
    Eccentricity:     .0006374     
    Arg of perigee:   325.8676  deg
    Mean anomaly:      34.2064  deg
    Mean motion:   15.50045478  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             468
    Checksum:              315
 
 
    Coasting Arc #14 (Orbit 483)
    ---------------------------------------
 
    Vector Time (GMT): 2014/126/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1649049.49                 A    =         6790806.17  meter
     Y    =        4390207.62  meter          E    =           .0009355
     Z    =        4912657.97                 I    =           51.34890
     XDOT =      -5653.938293                 Wp   =           13.80293
     YDOT =       4652.937363  meter/sec      RA   =          306.31847  deg
     ZDOT =      -2250.426049                 TA   =           98.34676
                                              MA   =           98.24068
                                              Ha   =            227.533  n.mi
                                              Hp   =            221.890
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5410267.36                 X    =         1575970.33
     Y    =       14403568.32  feet           Y    =         4408239.73  meter
     Z    =       16117644.25                 Z    =         4920491.39
     XDOT =     -18549.666315                 XDOT =       -5694.616342
     YDOT =      15265.542529  feet/sec       YDOT =        4589.483958  meter/sec
     ZDOT =      -7383.287562                 ZDOT =       -2277.991096
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1755068.39                 X    =          534944.84
     Y    =       15251544.67  feet           Y    =         4648670.81  meter
     Z    =       16149995.35                 Z    =         4922518.58
     XDOT =     -20473.901687                 XDOT =       -6240.445234
     YDOT =      10332.520670  feet/sec       YDOT =        3149.352300  meter/sec
     ZDOT =      -7500.644552                 ZDOT =       -2286.196459
  
  
    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   14126.38615844  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6496 306.7686 0006539 329.1953  30.8813 15.50112289  4847
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14126.38615844   =   yrday.fracday
    Element set:     913
    Inclination:       51.6496  deg
    RA of node:       306.7686  deg
    Eccentricity:     .0006539     
    Arg of perigee:   329.1953  deg
    Mean anomaly:      30.8813  deg
    Mean motion:   15.50112289  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             484
    Checksum:              325
 
 
    Coasting Arc #15 (Orbit 498)
    ---------------------------------------
 
    Vector Time (GMT): 2014/127/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1707778.85                 A    =         6791379.35  meter
     Y    =       -4530833.57  meter          E    =           .0007900
     Z    =       -4767721.87                 I    =           51.33263
     XDOT =       5372.369341                 Wp   =           73.03794
     YDOT =      -4781.933615  meter/sec      RA   =          301.34087  deg
     ZDOT =       2625.859852                 TA   =          222.98646
                                              MA   =          223.04822
                                              Ha   =            227.621  n.mi
                                              Hp   =            221.685
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5602948.99                 X    =        -1633826.86
     Y    =      -14864939.54  feet           Y    =        -4549517.59  meter
     Z    =      -15642132.13                 Z    =        -4775838.44
     XDOT =      17625.883666                 XDOT =        5412.687028
     YDOT =     -15688.758578  feet/sec       YDOT =       -4721.630885  meter/sec
     ZDOT =       8615.025762                 ZDOT =        2652.056245
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2106753.57                 X    =         -642138.49
     Y    =      -15712128.23  feet           Y    =        -4789056.69  meter
     Z    =      -15675661.97                 Z    =        -4777941.77
     XDOT =      19441.321539                 XDOT =        5925.714805
     YDOT =     -11293.926692  feet/sec       YDOT =       -3442.388856  meter/sec
     ZDOT =       8726.610839                 ZDOT =        2659.870984
  
  
    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   14127.35320615  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6490 301.9769 0006586 332.5779  27.5023 15.50120893  4998
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14127.35320615   =   yrday.fracday
    Element set:     914
    Inclination:       51.6490  deg
    RA of node:       301.9769  deg
    Eccentricity:     .0006586     
    Arg of perigee:   332.5779  deg
    Mean anomaly:      27.5023  deg
    Mean motion:   15.50120893  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             499
    Checksum:              314
 
 
    Coasting Arc #16 (Orbit 514)
    ---------------------------------------
 
    Vector Time (GMT): 2014/128/08:12:10.901
    Vector Time (MET): N/A
    Weight (LBS)     : 923683.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1755024.60                 A    =         6791940.49  meter
     Y    =        4704840.94  meter          E    =           .0010866
     Z    =        4573780.46                 I    =           51.31986
     XDOT =      -5102.157884                 Wp   =           27.66969
     YDOT =       4850.840206  meter/sec      RA   =          296.36252  deg
     ZDOT =      -3019.721082                 TA   =           92.72158
                                              MA   =           92.59720
                                              Ha   =            227.704  n.mi
                                              Hp   =            221.459
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5757954.74                 X    =         1680065.40
     Y    =       15435829.85  feet           Y    =         4724047.70  meter
     Z    =       15005841.41                 Z    =         4582124.06
     XDOT =     -16739.363138                 XDOT =       -5141.352896
     YDOT =      15914.830073  feet/sec       YDOT =        4793.565402  meter/sec
     ZDOT =      -9907.221399                 ZDOT =       -3044.602163
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2416671.34                 X    =          736601.42
     Y    =       16264778.34  feet           Y    =         4957504.44  meter
     Z    =       15040307.43                 Z    =         4584285.70
     XDOT =     -18370.848244                 XDOT =       -5599.434545
     YDOT =      12026.389966  feet/sec       YDOT =        3665.643662  meter/sec
     ZDOT =     -10013.249026                 ZDOT =       -3052.038303
  
  
    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   14128.38469628  .00016717  00000-0  10270-3 0  9155
    2 25544  51.6490 296.8661 0006758 335.9370  24.1464 15.50188947  5151
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14128.38469628   =   yrday.fracday
    Element set:     915
    Inclination:       51.6490  deg
    RA of node:       296.8661  deg
    Eccentricity:     .0006758     
    Arg of perigee:   335.9370  deg
    Mean anomaly:      24.1464  deg
    Mean motion:   15.50188947  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             515
    Checksum:              340
 
             

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