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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  19375.04
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.423
   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 
   ------------------------------------------------------------------------
   239/08:38:29.119          -0.0               1.4              1.4    
   N/A                        1.4              -0.2              228.6  
   000/00:02:58.237          -0.2              -0.0              220.2  
   
 
 
    Coasting Arc #1 (Orbit 2131)
    ---------------------------------------
 
    Vector Time (GMT): 2014/232/13:58:55.677
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5840154.34                 A    =         6798413.67  meter
     Y    =       -2371238.52  meter          E    =           .0006513
     Z    =       -2553244.34                 I    =           51.88852
     XDOT =        -65.240829                 Wp   =           87.69972
     YDOT =       5527.844624  meter/sec      RA   =          139.37492  deg
     ZDOT =      -5294.434804                 TA   =          120.80075
                                              MA   =          120.73663
                                              Ha   =            228.603  n.mi
                                              Hp   =            220.071
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19160611.36                 X    =         5878638.68
     Y    =       -7779653.94  feet           Y    =        -2305714.99  meter
     Z    =       -8376785.90                 Z    =        -2524780.61
     XDOT =       -214.044714                 XDOT =        -101.331324
     YDOT =      18135.973177  feet/sec       YDOT =        5526.913215  meter/sec
     ZDOT =     -17370.192926                 ZDOT =       -5294.839443
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19505926.26                 X    =        -5945406.33
     Y    =        7013598.19  feet           Y    =         2137744.73  meter
     Z    =       -8255353.80                 Z    =        -2516231.84
     XDOT =       1334.044188                 XDOT =         406.616668
     YDOT =     -16693.711785  feet/sec       YDOT =       -5088.243352  meter/sec
     ZDOT =     -17372.764651                 ZDOT =       -5295.218666
  
  
    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   14232.60982345  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6469 140.2654 0004463  33.7179 326.4255 15.50092404 21327
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14232.60982345   =   yrday.fracday
    Element set:     900
    Inclination:       51.6469  deg
    RA of node:       140.2654  deg
    Eccentricity:     .0004463     
    Arg of perigee:    33.7179  deg
    Mean anomaly:     326.4255  deg
    Mean motion:   15.50092404  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2132
    Checksum:              287
 
 
    Coasting Arc #2 (Orbit 2147)
    ---------------------------------------
 
    Vector Time (GMT): 2014/233/13:58:55.677
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5615076.17                 A    =         6797599.25  meter
     Y    =        2516846.45  meter          E    =           .0017039
     Z    =        2866771.30                 I    =           51.90913
     XDOT =         37.034921                 Wp   =           69.68667
     YDOT =      -5735.501439  meter/sec      RA   =          134.43777  deg
     ZDOT =       5089.256565                 TA   =          322.76444
                                              MA   =          322.88247
                                              Ha   =            228.738  n.mi
                                              Hp   =            219.846
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18422165.90                 X    =        -5656728.42
     Y    =        8257370.24  feet           Y    =         2453822.21  meter
     Z    =        9405417.65                 Z    =         2839393.30
     XDOT =        121.505646                 XDOT =          76.446309
     YDOT =     -18817.261940  feet/sec       YDOT =       -5734.866833  meter/sec
     ZDOT =      16697.035974                 ZDOT =        5089.532307
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18661328.44                 X    =         5687972.91
     Y    =       -7842167.28  feet           Y    =        -2390292.59  meter
     Z    =        9288566.86                 Z    =         2831155.18
     XDOT =      -1009.698852                 XDOT =        -307.756210
     YDOT =      17449.926271  feet/sec       YDOT =        5318.737527  meter/sec
     ZDOT =      16699.095364                 ZDOT =        5089.884267
  
  
    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   14233.64131297  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6468 135.1538 0004691  36.7208 323.4263 15.50128932 21488
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14233.64131297   =   yrday.fracday
    Element set:     901
    Inclination:       51.6468  deg
    RA of node:       135.1538  deg
    Eccentricity:     .0004691     
    Arg of perigee:    36.7208  deg
    Mean anomaly:     323.4263  deg
    Mean motion:   15.50128932  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2148
    Checksum:              296
 
 
    Coasting Arc #3 (Orbit 2162)
    ---------------------------------------
 
    Vector Time (GMT): 2014/234/13:58:55.677
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5402538.82                 A    =         6796671.52  meter
     Y    =       -2600423.68  meter          E    =           .0007675
     Z    =       -3209930.26                 I    =           51.92719
     XDOT =         -1.672261                 Wp   =           71.19530
     YDOT =       5941.900760  meter/sec      RA   =          129.50222  deg
     ZDOT =      -4823.485718                 TA   =          145.64223
                                              MA   =          145.59257
                                              Ha   =            228.581  n.mi
                                              Hp   =            219.897
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17724864.89                 X    =         5446808.35
     Y    =       -8531573.74  feet           Y    =        -2539761.58  meter
     Z    =      -10531267.27                 Z    =        -3183578.36
     XDOT =         -5.486419                 XDOT =         -44.685320
     YDOT =      19494.425064  feet/sec       YDOT =        5941.641404  meter/sec
     ZDOT =     -15825.084375                 ZDOT =       -4823.598506
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17834908.50                 X    =        -5436080.11
     Y    =        8439889.71  feet           Y    =         2572478.38  meter
     Z    =      -10418756.01                 Z    =        -3175636.83
     XDOT =        622.639496                 XDOT =         189.780518
     YDOT =     -18192.744462  feet/sec       YDOT =       -5545.148512  meter/sec
     ZDOT =     -15826.486117                 ZDOT =       -4823.912969
  
  
    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   14234.60831811  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6466 130.3624 0004446  39.2828 320.8645 15.50148542 21634
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14234.60831811   =   yrday.fracday
    Element set:     902
    Inclination:       51.6466  deg
    RA of node:       130.3624  deg
    Eccentricity:     .0004446     
    Arg of perigee:    39.2828  deg
    Mean anomaly:     320.8645  deg
    Mean motion:   15.50148542  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2163
    Checksum:              289
 
 
    Coasting Arc #4 (Orbit 2178)
    ---------------------------------------
 
    Vector Time (GMT): 2014/235/13:58:55.677
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5166611.35                 A    =         6795754.56  meter
     Y    =        2662585.97  meter          E    =           .0015692
     Z    =        3504854.30                 I    =           51.94323
     XDOT =        -79.807235                 Wp   =           78.45512
     YDOT =      -6168.615141  meter/sec      RA   =          124.56651  deg
     ZDOT =       4554.400042                 TA   =          322.52600
                                              MA   =          322.63530
                                              Ha   =            228.735  n.mi
                                              Hp   =            219.679
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16950824.65                 X    =        -5213026.15
     Y    =        8735518.26  feet           Y    =         2604550.23  meter
     Z    =       11498865.80                 Z    =         3479643.23
     XDOT =       -261.834762                 XDOT =         -32.945833
     YDOT =     -20238.238650  feet/sec       YDOT =       -6169.245363  meter/sec
     ZDOT =      14942.257355                 ZDOT =        4554.126471
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16916766.54                 X    =         5156230.44
     Y    =       -8940218.10  feet           Y    =        -2724978.48  meter
     Z    =       11391187.85                 Z    =         3472034.06
     XDOT =        -53.139063                 XDOT =         -16.196786
     YDOT =      18997.632829  feet/sec       YDOT =        5790.478486  meter/sec
     ZDOT =      14942.054182                 ZDOT =        4554.338115
  
  
    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   14235.63977545  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6463 125.2505 0004621  42.2377 317.9129 15.50174963 21797
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14235.63977545   =   yrday.fracday
    Element set:     903
    Inclination:       51.6463  deg
    RA of node:       125.2505  deg
    Eccentricity:     .0004621     
    Arg of perigee:    42.2377  deg
    Mean anomaly:     317.9129  deg
    Mean motion:   15.50174963  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2179
    Checksum:              312
 
 
    Coasting Arc #5 (Orbit 2193)
    ---------------------------------------
 
    Vector Time (GMT): 2014/236/13:58:55.677
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4955476.43                 A    =         6794706.45  meter
     Y    =       -2664016.44  meter          E    =           .0010034
     Z    =       -3821299.60                 I    =           51.95603
     XDOT =        174.808468                 Wp   =           63.76300
     YDOT =       6378.001245  meter/sec      RA   =          119.63175  deg
     ZDOT =      -4224.010075                 TA   =          161.75219
                                              MA   =          161.71616
                                              Ha   =            228.556  n.mi
                                              Hp   =            219.713
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16258124.77                 X    =         5003460.09
     Y    =       -8740211.41  feet           Y    =        -2608333.05  meter
     Z    =      -12537072.18                 Z    =        -3797110.31
     XDOT =        573.518595                 XDOT =         123.993719
     YDOT =      20925.200935  feet/sec       YDOT =        6379.671676  meter/sec
     ZDOT =     -13858.300771                 ZDOT =       -4223.284724
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16074483.98                 X    =        -4899502.72
     Y    =        9214627.21  feet           Y    =         2808618.37  meter
     Z    =      -12433732.57                 Z    =        -3789801.69
     XDOT =       -599.556877                 XDOT =        -182.744936
     YDOT =     -19723.622481  feet/sec       YDOT =       -6011.760132  meter/sec
     ZDOT =     -13856.212042                 ZDOT =       -4223.373430
  
  
    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   14236.60675013  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6454 120.4586 0004436  45.4343 314.7169 15.50206028 21949
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14236.60675013   =   yrday.fracday
    Element set:     904
    Inclination:       51.6454  deg
    RA of node:       120.4586  deg
    Eccentricity:     .0004436     
    Arg of perigee:    45.4343  deg
    Mean anomaly:     314.7169  deg
    Mean motion:   15.50206028  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2194
    Checksum:              288
 
 
    Coasting Arc #6 (Orbit 2209)
    ---------------------------------------
 
    Vector Time (GMT): 2014/237/13:58:55.677
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4731803.67                 A    =         6793764.85  meter
     Y    =        2639625.10  meter          E    =           .0013838
     Z    =        4086051.86                 I    =           51.96729
     XDOT =       -313.742175                 Wp   =           86.99529
     YDOT =      -6600.711765  meter/sec      RA   =          114.69657  deg
     ZDOT =       3890.163664                 TA   =          322.86054
                                              MA   =          322.95620
                                              Ha   =            228.720  n.mi
                                              Hp   =            219.524
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15524290.26                 X    =        -4780817.30
     Y    =        8660187.34  feet           Y    =         2586437.28  meter
     Z    =       13405681.96                 Z    =         4062946.54
     XDOT =      -1029.337846                 XDOT =        -258.805047
     YDOT =     -21655.878494  feet/sec       YDOT =       -6603.912755  meter/sec
     ZDOT =      12763.004147                 ZDOT =        3888.773529
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15189744.39                 X    =         4629834.09
     Y    =       -9376111.02  feet           Y    =        -2857838.64  meter
     Z    =       13306951.16                 Z    =         4055958.71
     XDOT =       1429.364612                 XDOT =         435.670334
     YDOT =      20472.336584  feet/sec       YDOT =        6239.968191  meter/sec
     ZDOT =      12758.126545                 ZDOT =        3888.676971
  
  
    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   14237.63817544  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6450 115.3464 0004531  48.2900 311.8637 15.50218670 22102
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14237.63817544   =   yrday.fracday
    Element set:     905
    Inclination:       51.6450  deg
    RA of node:       115.3464  deg
    Eccentricity:     .0004531     
    Arg of perigee:    48.2900  deg
    Mean anomaly:     311.8637  deg
    Mean motion:   15.50218670  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2210
    Checksum:              283
 
 
    Coasting Arc #7 (Orbit 2224)
    ---------------------------------------
 
    Vector Time (GMT): 2014/238/13:58:55.677
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4545595.51                 A    =         6792687.62  meter
     Y    =       -2560117.10  meter          E    =           .0012853
     Z    =       -4363606.70                 I    =           51.97493
     XDOT =        467.717317                 Wp   =           63.91690
     YDOT =       6788.114972  meter/sec      RA   =          109.76161  deg
     ZDOT =      -3497.848037                 TA   =          170.61714
                                              MA   =          170.59311
                                              Ha   =            228.536  n.mi
                                              Hp   =            219.527
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14913371.09                 X    =         4595082.21
     Y    =       -8399334.31  feet           Y    =        -2509009.01  meter
     Z    =      -14316294.94                 Z    =        -4341404.69
     XDOT =       1534.505632                 XDOT =         408.767492
     YDOT =      22270.718411  feet/sec       YDOT =        6793.015362  meter/sec
     ZDOT =     -11475.879388                 ZDOT =       -3495.719766
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14438842.60                 X    =        -4400959.22
     Y    =        9337288.38  feet           Y    =         2846005.50  meter
     Z    =      -14221414.32                 Z    =        -4334687.08
     XDOT =      -2338.229956                 XDOT =        -712.692491
     YDOT =     -21069.663847  feet/sec       YDOT =       -6422.033540  meter/sec
     ZDOT =     -11467.896673                 ZDOT =       -3495.414906
  
  
    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   14238.60511990  .00016717  00000-0  10270-3 0  9062
    2 25544  51.6437 110.5537 0004426  52.4893 307.6659 15.50260985 22255
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14238.60511990   =   yrday.fracday
    Element set:     906
    Inclination:       51.6437  deg
    RA of node:       110.5537  deg
    Eccentricity:     .0004426     
    Arg of perigee:    52.4893  deg
    Mean anomaly:     307.6659  deg
    Mean motion:   15.50260985  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2225
    Checksum:              311
 
 
    Coasting Arc #8 (Orbit 2236)
    ---------------------------------------
 
    Vector Time (GMT): 2014/239/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4247159.46                 A    =         6789531.82  meter
     Y    =         240285.72  meter          E    =           .0017601
     Z    =       -5306927.23                 I    =           51.97188
     XDOT =      -1455.437537                 Wp   =           77.27535
     YDOT =       7463.441469  meter/sec      RA   =          105.90459  deg
     ZDOT =       -825.406948                 TA   =          184.84193
                                              MA   =          184.85898
                                              Ha   =            228.584  n.mi
                                              Hp   =            220.181
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13934250.19                 X    =         4269935.95
     Y    =         788338.97  feet           Y    =          287907.03  meter
     Z    =      -17411178.58                 Z    =        -5286240.05
     XDOT =      -4775.057536                 XDOT =       -1534.777766
     YDOT =      24486.356524  feet/sec       YDOT =        7446.722127  meter/sec
     ZDOT =      -2708.028044                 ZDOT =        -832.670627
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2795979.36                 X    =         -852214.51
     Y    =      -13784908.37  feet           Y    =        -4201640.07  meter
     Z    =      -17323185.24                 Z    =        -5280106.86
     XDOT =      23887.551407                 XDOT =        7280.925669
     YDOT =      -1395.589177  feet/sec       YDOT =        -425.375581  meter/sec
     ZDOT =      -2740.125084                 ZDOT =        -835.190126
  
  
    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   14239.37866840  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6456 106.7202 0003596  50.5442 309.6026 15.50036465 22375
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14239.37866840   =   yrday.fracday
    Element set:     907
    Inclination:       51.6456  deg
    RA of node:       106.7202  deg
    Eccentricity:     .0003596     
    Arg of perigee:    50.5442  deg
    Mean anomaly:     309.6026  deg
    Mean motion:   15.50036465  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2237
    Checksum:              304
 
 
    Coasting Arc #9 (Orbit 2252)
    ---------------------------------------
 
    Vector Time (GMT): 2014/240/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4184450.04                 A    =         6789202.25  meter
     Y    =        -321204.12  meter          E    =           .0005398
     Z    =        5332105.32                 I    =           51.97860
     XDOT =       1126.273629                 Wp   =           76.88132
     YDOT =      -7571.089385  meter/sec      RA   =          100.97057  deg
     ZDOT =        428.608718                 TA   =            9.05394
                                              MA   =            9.04421
                                              Ha   =            228.619  n.mi
                                              Hp   =            219.998
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13728510.65                 X    =        -4206448.75
     Y    =       -1053819.30  feet           Y    =         -368119.80  meter
     Z    =       17493783.87                 Z    =         5311724.60
     XDOT =       3695.123455                 XDOT =        1208.769558
     YDOT =     -24839.532102  feet/sec       YDOT =       -7558.033360  meter/sec
     ZDOT =       1406.196582                 ZDOT =         434.281107
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2721675.33                 X    =          829566.64
     Y    =       13608826.19  feet           Y    =         4147970.22  meter
     Z    =       17407106.22                 Z    =         5305685.98
     XDOT =     -23920.116786                 XDOT =       -7290.851596
     YDOT =       2956.256264  feet/sec       YDOT =         901.066909  meter/sec
     ZDOT =       1431.550390                 ZDOT =         436.336559
  
  
    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   14240.41021640  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6452 101.6094 0003439  52.4930 307.6533 15.50085541 22531
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14240.41021640   =   yrday.fracday
    Element set:     908
    Inclination:       51.6452  deg
    RA of node:       101.6094  deg
    Eccentricity:     .0003439     
    Arg of perigee:    52.4930  deg
    Mean anomaly:     307.6533  deg
    Mean motion:   15.50085541  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2253
    Checksum:              269
 
 
    Coasting Arc #10 (Orbit 2267)
    ---------------------------------------
 
    Vector Time (GMT): 2014/241/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4168247.63                 A    =         6789154.78  meter
     Y    =         414449.10  meter          E    =           .0017910
     Z    =       -5358246.53                 I    =           51.98408
     XDOT =       -787.204668                 Wp   =           83.44902
     YDOT =       7608.058786  meter/sec      RA   =           96.03613  deg
     ZDOT =        -21.988402                 TA   =          186.33058
                                              MA   =          186.35324
                                              Ha   =            228.541  n.mi
                                              Hp   =            220.046
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13675353.13                 X    =         4189331.92
     Y    =        1359741.14  feet           Y    =          461178.50  meter
     Z    =      -17579548.97                 Z    =        -5337946.67
     XDOT =      -2582.692479                 XDOT =        -872.114414
     YDOT =      24960.822789  feet/sec       YDOT =        7598.780995  meter/sec
     ZDOT =        -72.140425                 ZDOT =         -26.019514
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2647194.68                 X    =         -806864.94
     Y    =      -13597205.34  feet           Y    =        -4144428.19  meter
     Z    =      -17493229.79                 Z    =        -5331936.44
     XDOT =      23663.118909                 XDOT =        7212.518644
     YDOT =      -4482.278797  feet/sec       YDOT =       -1366.198577  meter/sec
     ZDOT =        -90.528706                 ZDOT =         -27.593150
  
  
    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   14241.37728007  .00016717  00000-0  10270-3 0  9092
    2 25544  51.6459  96.8175 0003565  55.8814 304.2674 15.50086219 22689
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14241.37728007   =   yrday.fracday
    Element set:     909
    Inclination:       51.6459  deg
    RA of node:        96.8175  deg
    Eccentricity:     .0003565     
    Arg of perigee:    55.8814  deg
    Mean anomaly:     304.2674  deg
    Mean motion:   15.50086219  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2268
    Checksum:              325
 
 
    Coasting Arc #11 (Orbit 2283)
    ---------------------------------------
 
    Vector Time (GMT): 2014/242/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4160237.21                 A    =         6789043.48  meter
     Y    =        -529686.71  meter          E    =           .0006006
     Z    =        5334316.47                 I    =           51.98646
     XDOT =        458.469938                 Wp   =           63.99571
     YDOT =      -7642.294747  meter/sec      RA   =           91.10196  deg
     ZDOT =       -398.393635                 TA   =           29.80326
                                              MA   =           29.76907
                                              Ha   =            228.572  n.mi
                                              Hp   =            219.867
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13649072.21                 X    =        -4179917.31
     Y    =       -1737817.30  feet           Y    =         -576318.72  meter
     Z    =       17501038.29                 Z    =         5314058.89
     XDOT =       1504.166464                 XDOT =         545.829030
     YDOT =     -25073.145496  feet/sec       YDOT =       -7636.679423  meter/sec
     ZDOT =      -1307.065730                 ZDOT =        -395.953568
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2512259.36                 X    =          765736.65
     Y    =       13638648.26  feet           Y    =         4157059.99  meter
     Z    =       17414917.42                 Z    =         5308066.83
     XDOT =     -23359.181453                 XDOT =       -7119.878507
     YDOT =       5969.151554  feet/sec       YDOT =        1819.397394  meter/sec
     ZDOT =      -1295.428155                 ZDOT =        -394.846502
  
  
    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   14242.40879614  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6457  91.7063 0003425  57.5822 302.5659 15.50136166 22849
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14242.40879614   =   yrday.fracday
    Element set:     910
    Inclination:       51.6457  deg
    RA of node:        91.7063  deg
    Eccentricity:     .0003425     
    Arg of perigee:    57.5822  deg
    Mean anomaly:     302.5659  deg
    Mean motion:   15.50136166  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2284
    Checksum:              303
 
 
    Coasting Arc #12 (Orbit 2298)
    ---------------------------------------
 
    Vector Time (GMT): 2014/243/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4201949.14                 A    =         6789228.40  meter
     Y    =         641982.26  meter          E    =           .0017452
     Z    =       -5308903.18                 I    =           51.98744
     XDOT =       -131.415117                 Wp   =           89.53086
     YDOT =       7604.074613  meter/sec      RA   =           86.16763  deg
     ZDOT =        817.973061                 TA   =          188.25553
                                              MA   =          188.28428
                                              Ha   =            228.474  n.mi
                                              Hp   =            219.942
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13785922.38                 X    =         4220247.01
     Y    =        2106241.02  feet           Y    =          689073.07  meter
     Z    =      -17417661.34                 Z    =        -5288446.29
     XDOT =       -431.151959                 XDOT =        -220.409317
     YDOT =      24947.751355  feet/sec       YDOT =        7602.107513  meter/sec
     ZDOT =       2683.638652                 ZDOT =         817.117906
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2440852.00                 X    =         -743971.69
     Y    =      -13840214.94  feet           Y    =        -4218497.51  meter
     Z    =      -17330710.48                 Z    =        -5282400.55
     XDOT =      22776.586966                 XDOT =        6942.303707
     YDOT =      -7361.022216  feet/sec       YDOT =       -2243.639571  meter/sec
     ZDOT =       2678.736757                 ZDOT =         816.478963
  
  
    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   14243.37582954  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6464  86.9144 0003497  60.4684 299.6815 15.50135907 22999
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14243.37582954   =   yrday.fracday
    Element set:     911
    Inclination:       51.6464  deg
    RA of node:        86.9144  deg
    Eccentricity:     .0003497     
    Arg of perigee:    60.4684  deg
    Mean anomaly:     299.6815  deg
    Mean motion:   15.50135907  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2299
    Checksum:              339
 
 
    Coasting Arc #13 (Orbit 2314)
    ---------------------------------------
 
    Vector Time (GMT): 2014/244/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4254992.68                 A    =         6789362.24  meter
     Y    =        -772645.54  meter          E    =           .0007524
     Z    =        5229079.10                 I    =           51.98561
     XDOT =       -174.292957                 Wp   =           58.39562
     YDOT =      -7561.149232  meter/sec      RA   =           81.23323  deg
     ZDOT =      -1253.895576                 TA   =           43.61573
                                              MA   =           43.55628
                                              Ha   =            228.504  n.mi
                                              Hp   =            219.757
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13959949.73                 X    =        -4271437.74
     Y    =       -2534926.31  feet           Y    =         -820319.23  meter
     Z    =       17155771.34                 Z    =         5208369.04
     XDOT =       -571.827287                 XDOT =         -83.638465
     YDOT =     -24806.920054  feet/sec       YDOT =       -7562.591491  meter/sec
     ZDOT =      -4113.830630                 ZDOT =       -1254.521587
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2332523.67                 X    =          710953.22
     Y    =       14102386.14  feet           Y    =         4298407.30  meter
     Z    =       17067764.26                 Z    =         5202254.55
     XDOT =     -22158.279488                 XDOT =       -6753.843588
     YDOT =       8666.110746  feet/sec       YDOT =        2641.430555  meter/sec
     ZDOT =      -4115.223920                 ZDOT =       -1254.320251
  
  
    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   14244.40731342  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6466  81.8031 0003389  62.0278 298.1215 15.50188336 23158
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14244.40731342   =   yrday.fracday
    Element set:     912
    Inclination:       51.6466  deg
    RA of node:        81.8031  deg
    Eccentricity:     .0003389     
    Arg of perigee:    62.0278  deg
    Mean anomaly:     298.1215  deg
    Mean motion:   15.50188336  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2315
    Checksum:              291
 
 
    Coasting Arc #14 (Orbit 2329)
    ---------------------------------------
 
    Vector Time (GMT): 2014/245/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4356805.23                 A    =         6789794.63  meter
     Y    =         884092.57  meter          E    =           .0016201
     Z    =       -5146324.93                 I    =           51.98159
     XDOT =        466.201305                 Wp   =           95.10860
     YDOT =       7449.034641  meter/sec      RA   =           76.29849  deg
     ZDOT =       1677.496623                 TA   =          191.03525
                                              MA   =          191.07083
                                              Ha   =            228.394  n.mi
                                              Hp   =            219.856
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14293980.41                 X    =         4371594.46
     Y    =        2900566.18  feet           Y    =          932895.61  meter
     Z    =      -16884268.14                 Z    =        -5125124.33
     XDOT =       1529.531839                 XDOT =         374.721103
     YDOT =      24439.090030  feet/sec       YDOT =        7453.736597  meter/sec
     ZDOT =       5503.597846                 ZDOT =        1679.538778
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2349295.69                 X    =         -716065.33
     Y    =      -14499848.96  feet           Y    =        -4419553.96  meter
     Z    =      -16794191.28                 Z    =        -5118869.50
     XDOT =      21295.979334                 XDOT =        6491.014501
     YDOT =      -9821.467479  feet/sec       YDOT =       -2993.583288  meter/sec
     ZDOT =       5511.022634                 ZDOT =        1679.759699
  
  
    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   14245.37431625  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6469  77.0111 0003408  64.6716 295.4788 15.50185551 23302
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14245.37431625   =   yrday.fracday
    Element set:     913
    Inclination:       51.6469  deg
    RA of node:        77.0111  deg
    Eccentricity:     .0003408     
    Arg of perigee:    64.6716  deg
    Mean anomaly:     295.4788  deg
    Mean motion:   15.50185551  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2330
    Checksum:              304
 
 
    Coasting Arc #15 (Orbit 2345)
    ---------------------------------------
 
    Vector Time (GMT): 2014/246/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4470527.62                 A    =         6790183.87  meter
     Y    =       -1009675.35  meter          E    =           .0009511
     Z    =        5004567.93                 I    =           51.97538
     XDOT =       -724.311365                 Wp   =           60.09070
     YDOT =      -7332.140464  meter/sec      RA   =           71.36352  deg
     ZDOT =      -2118.660881                 TA   =           50.48877
                                              MA   =           50.40472
                                              Ha   =            228.420  n.mi
                                              Hp   =            219.665
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14667085.38                 X    =        -4483215.43
     Y    =       -3312583.16  feet           Y    =        -1059738.40  meter
     Z    =       16419186.12                 Z    =         4982820.05
     XDOT =      -2376.349623                 XDOT =        -631.976116
     YDOT =     -24055.578950  feet/sec       YDOT =       -7339.723999  meter/sec
     ZDOT =      -6950.987143                 ZDOT =       -2121.954870
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2351271.66                 X    =          716667.60
     Y    =       14953039.52  feet           Y    =         4557686.45  meter
     Z    =       16326800.18                 Z    =         4976408.70
     XDOT =     -20423.212022                 XDOT =       -6224.995024
     YDOT =      10842.404957  feet/sec       YDOT =        3304.765031  meter/sec
     ZDOT =      -6963.747453                 ZDOT =       -2122.550224
  
  
    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   14246.40576732  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6471  71.8997 0003333  66.1046 294.0454 15.50240493 23468
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14246.40576732   =   yrday.fracday
    Element set:     914
    Inclination:       51.6471  deg
    RA of node:        71.8997  deg
    Eccentricity:     .0003333     
    Arg of perigee:    66.1046  deg
    Mean anomaly:     294.0454  deg
    Mean motion:   15.50240493  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2346
    Checksum:              305
 
 
    Coasting Arc #16 (Orbit 2360)
    ---------------------------------------
 
    Vector Time (GMT): 2014/247/08:39:58.237
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4627604.06                 A    =         6790850.90  meter
     Y    =        1100219.53  meter          E    =           .0014230
     Z    =       -4859736.57                 I    =           51.96614
     XDOT =        957.594721                 Wp   =           99.42198
     YDOT =       7154.662274  meter/sec      RA   =           66.42759  deg
     ZDOT =       2535.694307                 TA   =          195.44007
                                              MA   =          195.48353
                                              Ha   =            228.312  n.mi
                                              Hp   =            219.774
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15182428.00                 X    =         4638564.07
     Y    =        3609644.13  feet           Y    =         1152029.45  meter
     Z    =      -15944017.62                 Z    =        -4837229.92
     XDOT =       3141.714965                 XDOT =         865.200974
     YDOT =      23473.301423  feet/sec       YDOT =        7164.854229  meter/sec
     ZDOT =       8319.207045                 ZDOT =        2540.121389
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2530304.68                 X    =         -771236.87
     Y    =      -15497503.11  feet           Y    =        -4723638.95  meter
     Z    =      -15848416.46                 Z    =        -4830597.34
     XDOT =      19362.960242                 XDOT =        5901.830282
     YDOT =     -11673.298825  feet/sec       YDOT =       -3558.021482  meter/sec
     ZDOT =       8336.811070                 ZDOT =        2541.060014
  
  
    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   14247.37273893  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6465  67.1072 0003319  69.0977 291.0529 15.50235159 23612
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14247.37273893   =   yrday.fracday
    Element set:     915
    Inclination:       51.6465  deg
    RA of node:        67.1072  deg
    Eccentricity:     .0003319     
    Arg of perigee:    69.0977  deg
    Mean anomaly:     291.0529  deg
    Mean motion:   15.50235159  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2361
    Checksum:              319
 
             

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