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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  9687.52
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   128.2
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.453
   ET - UTC  (sec) :   67.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   224/13:30:14.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              227.9  
   000/00:00:00.000           0.0               0.0              219.7  
   
   226/17:17:51.104          -2.5               3.7              3.7    
   N/A                        1.8               0.2              228.1  
   000/00:07:42.209          -2.0              -0.3              221.6  
   
 
 
    Coasting Arc #1 (Orbit 1835)
    ---------------------------------------
 
    Vector Time (GMT): 2014/213/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3552994.04                 A    =         6799743.38  meter
     Y    =        5760072.24  meter          E    =           .0003983
     Z    =        -639453.64                 I    =           51.36978
     XDOT =      -4380.828952                 Wp   =          140.53427
     YDOT =       2045.476161  meter/sec      RA   =          234.00196  deg
     ZDOT =      -5939.406320                 TA   =           46.38175
                                              MA   =           46.34872
                                              Ha   =            226.596  n.mi
                                              Hp   =            221.764
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11656804.59                 X    =         3491425.75
     Y    =       18897874.80  feet           Y    =         5799459.86  meter
     Z    =       -2097945.00                 Z    =         -622343.44
     XDOT =     -14372.798400                 XDOT =       -4374.524912
     YDOT =       6710.879794  feet/sec       YDOT =        1996.522130  meter/sec
     ZDOT =     -19486.241207                 ZDOT =       -5960.672248
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7272343.02                 X    =         2216610.15
     Y    =      -20986174.50  feet           Y    =        -6396585.99  meter
     Z    =       -2026239.14                 Z    =         -617597.69
     XDOT =      12674.221995                 XDOT =        3863.102864
     YDOT =       6274.469344  feet/sec       YDOT =        1912.458256  meter/sec
     ZDOT =     -19576.832740                 ZDOT =       -5967.018619
  
  
    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   14213.53105397  .00016717  00000-0  10270-3 0  9001
    2 25544  51.6452 234.8344 0006742 318.6996  41.3644 15.50495980 18360
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14213.53105397   =   yrday.fracday
    Element set:     900
    Inclination:       51.6452  deg
    RA of node:       234.8344  deg
    Eccentricity:     .0006742     
    Arg of perigee:   318.6996  deg
    Mean anomaly:      41.3644  deg
    Mean motion:   15.50495980  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1836
    Checksum:              315
 
 
    Coasting Arc #2 (Orbit 1851)
    ---------------------------------------
 
    Vector Time (GMT): 2014/214/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3662975.48                 A    =         6799349.64  meter
     Y    =       -5602797.99  meter          E    =           .0014765
     Z    =        1136799.61                 I    =           51.38759
     XDOT =       4607.881529                 Wp   =           29.90505
     YDOT =      -1821.143725  meter/sec      RA   =          229.02925  deg
     ZDOT =       5851.456476                 TA   =          342.46771
                                              MA   =          342.51862
                                              Ha   =            226.739  n.mi
                                              Hp   =            221.583
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12017636.10                 X    =        -3605573.64
     Y    =      -18381883.18  feet           Y    =        -5643438.80  meter
     Z    =        3729657.51                 Z    =         1119144.95
     XDOT =      15117.721553                 XDOT =        4599.479224
     YDOT =      -5974.880986  feet/sec       YDOT =       -1769.662403  meter/sec
     ZDOT =      19197.691849                 ZDOT =        5873.820340
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6276514.93                 X    =        -1913081.75
     Y    =       21058714.86  feet           Y    =         6418696.29  meter
     Z    =        3655603.97                 Z    =         1114228.09
     XDOT =     -12703.296724                 XDOT =       -3871.964842
     YDOT =      -7147.092022  feet/sec       YDOT =       -2178.433648  meter/sec
     ZDOT =      19292.911834                 ZDOT =        5880.479527
  
  
    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   14214.56229490  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6452 229.7218 0006850 322.9762  37.0915 15.50509901 18522
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14214.56229490   =   yrday.fracday
    Element set:     901
    Inclination:       51.6452  deg
    RA of node:       229.7218  deg
    Eccentricity:     .0006850     
    Arg of perigee:   322.9762  deg
    Mean anomaly:      37.0915  deg
    Mean motion:   15.50509901  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1852
    Checksum:              303
 
 
    Coasting Arc #3 (Orbit 1866)
    ---------------------------------------
 
    Vector Time (GMT): 2014/215/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3734088.76                 A    =         6798753.78  meter
     Y    =        5438422.77  meter          E    =           .0001229
     Z    =       -1643541.59                 I    =           51.40616
     XDOT =      -4860.055134                 Wp   =          117.96056
     YDOT =       1618.126761  meter/sec      RA   =          224.05695  deg
     ZDOT =      -5691.441434                 TA   =           80.05662
                                              MA   =           80.04275
                                              Ha   =            226.887  n.mi
                                              Hp   =            221.407
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12250947.36                 X    =         3680981.29
     Y    =       17842594.40  feet           Y    =         5479882.84  meter
     Z    =       -5392196.80                 Z    =        -1625530.95
     XDOT =     -15945.062776                 XDOT =       -4850.141150
     YDOT =       5308.814833  feet/sec       YDOT =        1563.833982  meter/sec
     ZDOT =     -18672.708118                 ZDOT =       -5715.026669
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5346792.39                 X    =         1629702.32
     Y    =      -20992029.45  feet           Y    =        -6398370.58  meter
     Z    =       -5316595.09                 Z    =        -1620498.18
     XDOT =      12882.161124                 XDOT =        3926.482710
     YDOT =       8032.540184  feet/sec       YDOT =        2448.318248  meter/sec
     ZDOT =     -18773.086795                 ZDOT =       -5722.036855
  
  
    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   14215.52907645  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6446 224.9281 0006809 326.5114  33.5606 15.50510646 18679
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14215.52907645   =   yrday.fracday
    Element set:     902
    Inclination:       51.6446  deg
    RA of node:       224.9281  deg
    Eccentricity:     .0006809     
    Arg of perigee:   326.5114  deg
    Mean anomaly:      33.5606  deg
    Mean motion:   15.50510646  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1867
    Checksum:              303
 
 
    Coasting Arc #4 (Orbit 1882)
    ---------------------------------------
 
    Vector Time (GMT): 2014/216/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3762631.13                 A    =         6797905.84  meter
     Y    =       -5236803.18  meter          E    =           .0014415
     Z    =        2122155.52                 I    =           51.42638
     XDOT =       5144.703639                 Wp   =           41.79201
     YDOT =      -1465.741457  meter/sec      RA   =          219.08625  deg
     ZDOT =       5493.654468                 TA   =          341.77680
                                              MA   =          341.82841
                                              Ha   =            226.988  n.mi
                                              Hp   =            221.197
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12344590.33                 X    =        -3714101.05
     Y    =      -17181112.81  feet           Y    =        -5278608.06  meter
     Z    =        6962452.49                 Z    =         2103995.03
     XDOT =      16878.948947                 XDOT =        5134.025262
     YDOT =      -4808.863049  feet/sec       YDOT =       -1408.269903  meter/sec
     ZDOT =      18023.800748                 ZDOT =        5518.620612
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4424909.53                 X    =        -1348712.42
     Y    =       20713669.58  feet           Y    =         6313526.49  meter
     Z    =        6886171.70                 Z    =         2098905.14
     XDOT =     -13303.975521                 XDOT =       -4055.051739
     YDOT =      -8881.458611  feet/sec       YDOT =       -2707.068585  meter/sec
     ZDOT =      18130.026568                 ZDOT =        5526.032098
  
  
    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   14216.56030157  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6443 219.8155 0006913 330.0106  30.0648 15.50546130 18839
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14216.56030157   =   yrday.fracday
    Element set:     903
    Inclination:       51.6443  deg
    RA of node:       219.8155  deg
    Eccentricity:     .0006913     
    Arg of perigee:   330.0106  deg
    Mean anomaly:      30.0648  deg
    Mean motion:   15.50546130  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1883
    Checksum:              274
 
 
    Coasting Arc #5 (Orbit 1897)
    ---------------------------------------
 
    Vector Time (GMT): 2014/217/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3748371.17                 A    =         6796997.89  meter
     Y    =        5041790.21  meter          E    =           .0003213
     Z    =       -2599701.89                 I    =           51.44717
     XDOT =      -5433.408411                 Wp   =           18.88656
     YDOT =       1346.140606  meter/sec      RA   =          214.11556  deg
     ZDOT =      -5222.313319                 TA   =          190.38349
                                              MA   =          190.39013
                                              Ha   =            227.166  n.mi
                                              Hp   =            221.029
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12297805.66                 X    =         3704342.56
     Y    =       16541306.47  feet           Y    =         5083460.84  meter
     Z    =       -8529205.68                 Z    =        -2581599.70
     XDOT =     -17826.143082                 XDOT =       -5422.689287
     YDOT =       4416.471803  feet/sec       YDOT =        1285.440866  meter/sec
     ZDOT =     -17133.573880                 ZDOT =       -5248.681793
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3626191.20                 X    =         1105263.08
     Y    =      -20322242.15  feet           Y    =        -6194219.41  meter
     Z    =       -8453129.89                 Z    =        -2576513.99
     XDOT =      13853.760488                 XDOT =        4222.626197
     YDOT =       9647.034563  feet/sec       YDOT =        2940.416135  meter/sec
     ZDOT =     -17245.746351                 ZDOT =       -5256.503488
  
  
    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   14217.52706949  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6435 215.0216 0006931 334.3664  25.7143 15.50533368 18988
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14217.52706949   =   yrday.fracday
    Element set:     904
    Inclination:       51.6435  deg
    RA of node:       215.0216  deg
    Eccentricity:     .0006931     
    Arg of perigee:   334.3664  deg
    Mean anomaly:      25.7143  deg
    Mean motion:   15.50533368  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1898
    Checksum:              310
 
 
    Coasting Arc #6 (Orbit 1913)
    ---------------------------------------
 
    Vector Time (GMT): 2014/218/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3681232.80                 A    =         6795824.71  meter
     Y    =       -4824550.68  meter          E    =           .0012976
     Z    =        3039947.92                 I    =           51.46954
     XDOT =       5743.358129                 Wp   =           52.53245
     YDOT =      -1280.032805  meter/sec      RA   =          209.14656  deg
     ZDOT =       4916.746588                 TA   =          342.39464
                                              MA   =          342.43957
                                              Ha   =            227.235  n.mi
                                              Hp   =            220.814
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12077535.45                 X    =        -3641776.93
     Y    =      -15828578.34  feet           Y    =        -4865496.14  meter
     Z    =        9973582.40                 Z    =         3022160.77
     XDOT =      18843.038480                 XDOT =        5733.361140
     YDOT =      -4199.582695  feet/sec       YDOT =       -1215.863014  meter/sec
     ZDOT =      16131.058361                 ZDOT =        4944.622409
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2911341.13                 X    =         -887376.78
     Y    =       19733752.93  feet           Y    =         6014847.89  meter
     Z    =        9898797.34                 Z    =         3017153.43
     XDOT =     -14621.537916                 XDOT =       -4456.644757
     YDOT =     -10319.361572  feet/sec       YDOT =       -3145.341407  meter/sec
     ZDOT =      16249.635149                 ZDOT =        4952.888794
  
  
    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   14218.55827856  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6430 209.9088 0007008 337.0056  23.0780 15.50577818 19148
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14218.55827856   =   yrday.fracday
    Element set:     905
    Inclination:       51.6430  deg
    RA of node:       209.9088  deg
    Eccentricity:     .0007008     
    Arg of perigee:   337.0056  deg
    Mean anomaly:      23.0780  deg
    Mean motion:   15.50577818  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1914
    Checksum:              316
 
 
    Coasting Arc #7 (Orbit 1928)
    ---------------------------------------
 
    Vector Time (GMT): 2014/219/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3573882.20                 A    =         6794717.09  meter
     Y    =        4629328.70  meter          E    =           .0007349
     Z    =       -3468323.36                 I    =           51.49282
     XDOT =      -6032.520601                 Wp   =           22.26954
     YDOT =       1252.288775  meter/sec      RA   =          204.17721  deg
     ZDOT =      -4541.149053                 TA   =          198.41132
                                              MA   =          198.43793
                                              Ha   =            227.425  n.mi
                                              Hp   =            220.639
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11725335.30                 X    =         3538698.14
     Y    =       15188086.27  feet           Y    =         4669097.61  meter
     Z    =      -11379013.63                 Z    =        -3451047.39
     XDOT =     -19791.734256                 XDOT =       -6024.016488
     YDOT =       4108.558973  feet/sec       YDOT =        1184.877029  meter/sec
     ZDOT =     -14898.782983                 ZDOT =       -4570.433074
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2362535.00                 X    =          720100.67
     Y    =      -19084762.88  feet           Y    =        -5817035.73  meter
     Z    =      -11306354.76                 Z    =        -3446176.93
     XDOT =      15461.001966                 XDOT =        4712.513399
     YDOT =      10821.021176  feet/sec       YDOT =        3298.247254  meter/sec
     ZDOT =     -15023.352010                 ZDOT =       -4579.117693
  
  
    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   14219.52503196  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6425 205.1144 0007066 342.0697  18.0204 15.50560016 19297
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14219.52503196   =   yrday.fracday
    Element set:     906
    Inclination:       51.6425  deg
    RA of node:       205.1144  deg
    Eccentricity:     .0007066     
    Arg of perigee:   342.0697  deg
    Mean anomaly:      18.0204  deg
    Mean motion:   15.50560016  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1929
    Checksum:              282
 
 
    Coasting Arc #8 (Orbit 1944)
    ---------------------------------------
 
    Vector Time (GMT): 2014/220/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3408009.02                 A    =         6793388.09  meter
     Y    =       -4428765.67  meter          E    =           .0010723
     Z    =        3850421.76                 I    =           51.51754
     XDOT =       6330.964031                 Wp   =           60.70557
     YDOT =      -1274.335356  meter/sec      RA   =          199.20982  deg
     ZDOT =       4134.229317                 TA   =          345.74737
                                              MA   =          345.77760
                                              Ha   =            227.475  n.mi
                                              Hp   =            220.425
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11181131.95                 X    =        -3376936.03
     Y    =      -14530071.10  feet           Y    =        -4466702.66  meter
     Z    =       12632617.31                 Z    =         3833941.70
     XDOT =      20770.879367                 XDOT =        6324.661019
     YDOT =      -4180.890277  feet/sec       YDOT =       -1203.573859  meter/sec
     ZDOT =      13563.744478                 ZDOT =        4164.968328
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1963846.39                 X    =         -598580.38
     Y    =       18276506.12  feet           Y    =         5570679.07  meter
     Z    =       12563292.93                 Z    =         3829291.68
     XDOT =     -16468.232964                 XDOT =       -5019.517407
     YDOT =     -11191.252222  feet/sec       YDOT =       -3411.093677  meter/sec
     ZDOT =      13694.514206                 ZDOT =        4174.087930
  
  
    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   14220.55622465  .00016717  00000-0  10270-3 0  9078
    2 25544  51.6424 200.0014 0007113 344.1574  15.9353 15.50605834 19453
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14220.55622465   =   yrday.fracday
    Element set:     907
    Inclination:       51.6424  deg
    RA of node:       200.0014  deg
    Eccentricity:     .0007113     
    Arg of perigee:   344.1574  deg
    Mean anomaly:      15.9353  deg
    Mean motion:   15.50605834  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1945
    Checksum:              275
 
 
    Coasting Arc #9 (Orbit 1959)
    ---------------------------------------
 
    Vector Time (GMT): 2014/221/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3211698.22                 A    =         6792249.46  meter
     Y    =        4265101.77  meter          E    =           .0011395
     Z    =       -4210389.02                 I    =           51.54354
     XDOT =      -6583.261105                 Wp   =           32.23323
     YDOT =       1333.195077  meter/sec      RA   =          194.24208  deg
     ZDOT =      -3666.386625                 TA   =          200.02209
                                              MA   =          200.06684
                                              Ha   =            227.652  n.mi
                                              Hp   =            220.258
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10537067.65                 X    =         3184218.44
     Y    =       13993116.04  feet           Y    =         4300863.50  meter
     Z    =      -13813612.28                 Z    =        -4194854.03
     XDOT =     -21598.625672                 XDOT =       -6579.870182
     YDOT =       4373.999598  feet/sec       YDOT =        1259.595855  meter/sec
     ZDOT =     -12028.827510                 ZDOT =       -3698.358210
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1749591.02                 X    =          533275.34
     Y    =      -17480766.12  feet           Y    =        -5328137.51  meter
     Z    =      -13748262.53                 Z    =        -4190470.42
     XDOT =      17463.376786                 XDOT =        5322.837244
     YDOT =      11327.774984  feet/sec       YDOT =        3452.705815  meter/sec
     ZDOT =     -12164.859459                 ZDOT =       -3707.849163
  
  
    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   14221.52296270  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6426 195.2068 0007191 349.2910  10.8087 15.50587028 19604
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14221.52296270   =   yrday.fracday
    Element set:     908
    Inclination:       51.6426  deg
    RA of node:       195.2068  deg
    Eccentricity:     .0007191     
    Arg of perigee:   349.2910  deg
    Mean anomaly:      10.8087  deg
    Mean motion:   15.50587028  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1960
    Checksum:              306
 
 
    Coasting Arc #10 (Orbit 1975)
    ---------------------------------------
 
    Vector Time (GMT): 2014/222/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2956316.46                 A    =         6790954.60  meter
     Y    =       -4112822.43  meter          E    =           .0008152
     Z    =        4515199.54                 I    =           51.57069
     XDOT =       6833.504272                 Wp   =           62.65719
     YDOT =      -1431.757172  meter/sec      RA   =          189.27672  deg
     ZDOT =       3169.319090                 TA   =          355.49287
                                              MA   =          355.50021
                                              Ha   =            227.692  n.mi
                                              Hp   =            220.042
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9699200.98                 X    =        -2932039.08
     Y    =      -13493511.90  feet           Y    =        -4145746.11  meter
     Z    =       14813646.80                 Z    =         4500897.49
     XDOT =      22419.633437                 XDOT =        6833.611461
     YDOT =      -4697.366050  feet/sec       YDOT =       -1355.339913  meter/sec
     ZDOT =      10398.028510                 ZDOT =        3202.514768
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1733243.34                 X    =         -528292.57
     Y    =       16580821.35  feet           Y    =         5053834.35  meter
     Z    =       14753498.75                 Z    =         4496866.42
     XDOT =     -18557.824122                 XDOT =       -5656.424792
     YDOT =     -11319.855417  feet/sec       YDOT =       -3450.291931  meter/sec
     ZDOT =      10539.291987                 ZDOT =        3212.376198
  
  
    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   14222.55413882  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6432 190.0938 0007214 351.3003   8.8022 15.50632946 19766
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14222.55413882   =   yrday.fracday
    Element set:     909
    Inclination:       51.6432  deg
    RA of node:       190.0938  deg
    Eccentricity:     .0007214     
    Arg of perigee:   351.3003  deg
    Mean anomaly:       8.8022  deg
    Mean motion:   15.50632946  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1976
    Checksum:              293
 
 
    Coasting Arc #11 (Orbit 1990)
    ---------------------------------------
 
    Vector Time (GMT): 2014/223/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2687157.82                 A    =         6789980.55  meter
     Y    =        4009329.39  meter          E    =           .0014777
     Z    =       -4789128.74                 I    =           51.59884
     XDOT =      -7015.531498                 Wp   =           43.22474
     YDOT =       1558.438119  meter/sec      RA   =          184.31133  deg
     ZDOT =      -2625.998995                 TA   =          200.77230
                                              MA   =          200.83241
                                              Ha   =            227.850  n.mi
                                              Hp   =            219.893
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8816134.59                 X    =         2665388.39
     Y    =       13153967.81  feet           Y    =         4039257.07  meter
     Z    =      -15712364.63                 Z    =        -4776128.19
     XDOT =     -23016.835624                 XDOT =       -7019.680932
     YDOT =       5112.985956  feet/sec       YDOT =        1479.962645  meter/sec
     ZDOT =      -8615.482267                 ZDOT =       -2660.088811
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1887823.76                 X    =          575408.68
     Y    =      -15776609.84  feet           Y    =        -4808710.68  meter
     Z    =      -15657720.26                 Z    =        -4772473.14
     XDOT =      19542.446486                 XDOT =        5956.537689
     YDOT =      11051.629403  feet/sec       YDOT =        3368.536642  meter/sec
     ZDOT =      -8760.578097                 ZDOT =       -2670.224204
  
  
    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   14223.52086105  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6438 185.2994 0007297 356.0368   4.0724 15.50613532 19911
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14223.52086105   =   yrday.fracday
    Element set:     910
    Inclination:       51.6438  deg
    RA of node:       185.2994  deg
    Eccentricity:     .0007297     
    Arg of perigee:   356.0368  deg
    Mean anomaly:       4.0724  deg
    Mean motion:   15.50613532  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1991
    Checksum:              302
 
 
    Coasting Arc #12 (Orbit 2006)
    ---------------------------------------
 
    Vector Time (GMT): 2014/224/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900447.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2363113.66                 A    =         6788919.37  meter
     Y    =       -3931722.99  meter          E    =           .0006310
     Z    =        4999149.40                 I    =           51.62775
     XDOT =       7186.135385                 Wp   =           51.62971
     YDOT =      -1708.925419  meter/sec      RA   =          179.34855  deg
     ZDOT =       2054.946173                 TA   =           18.39094
                                              MA   =           18.36814
                                              Ha   =            227.881  n.mi
                                              Hp   =            219.670
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7752997.56                 X    =        -2343256.40
     Y    =      -12899353.63  feet           Y    =        -3958037.59  meter
     Z    =       16401408.80                 Z    =         4987718.36
     XDOT =      23576.559662                 XDOT =        7194.728816
     YDOT =      -5606.710691  feet/sec       YDOT =       -1628.517271  meter/sec
     ZDOT =       6741.949388                 ZDOT =        2089.875690
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2264037.24                 X    =         -690078.55
     Y    =       14931459.14  feet           Y    =         4551108.74  meter
     Z    =       16353414.61                 Z    =         4984520.77
     XDOT =     -20548.738452                 XDOT =       -6263.255480
     YDOT =     -10655.177023  feet/sec       YDOT =       -3247.697957  meter/sec
     ZDOT =       6890.648610                 ZDOT =        2100.269696
  
  
    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   14224.55202037  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6446 180.1867 0007308 358.3849   1.7277 15.50659430 20078
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14224.55202037   =   yrday.fracday
    Element set:     911
    Inclination:       51.6446  deg
    RA of node:       180.1867  deg
    Eccentricity:     .0007308     
    Arg of perigee:   358.3849  deg
    Mean anomaly:       1.7277  deg
    Mean motion:   15.50659430  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2007
    Checksum:              298
 
 
    Coasting Arc #13 (Orbit 2007)
    ---------------------------------------
 
    Vector Time (GMT): 2014/224/13:30:14.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941131.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3450295.51                 A    =         6790543.54  meter
     Y    =       -3590622.96  meter          E    =           .0008560
     Z    =        4608215.06                 I    =           51.63609
     XDOT =       6602.004211                 Wp   =           63.95219
     YDOT =      -2488.159254  meter/sec      RA   =          179.04380  deg
     ZDOT =       3003.717368                 TA   =          356.07197
                                              MA   =          356.07868
                                              Ha   =            227.925  n.mi
                                              Hp   =            219.654
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11319867.15                 X    =        -3432272.71
     Y    =      -11780259.05  feet           Y    =        -3629105.40  meter
     Z    =       15118815.80                 Z    =         4591498.27
     XDOT =      21660.118801                 XDOT =        6614.745885
     YDOT =      -8163.252145  feet/sec       YDOT =       -2414.259998  meter/sec
     ZDOT =       9854.715774                 ZDOT =        3035.819434
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7383545.68                 X    =         2250504.72
     Y    =       14646644.84  feet           Y    =         4464297.35  meter
     Z    =       15048306.71                 Z    =         4586723.89
     XDOT =     -21980.981002                 XDOT =       -6699.803009
     YDOT =        813.112984  feet/sec       YDOT =         247.836838  meter/sec
     ZDOT =       9991.515552                 ZDOT =        3045.413940
  
  
    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   14224.61646785  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6457 179.8675 0007277 359.0382   1.0753 15.50654735 20083
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14224.61646785   =   yrday.fracday
    Element set:     912
    Inclination:       51.6457  deg
    RA of node:       179.8675  deg
    Eccentricity:     .0007277     
    Arg of perigee:   359.0382  deg
    Mean anomaly:       1.0753  deg
    Mean motion:   15.50654735  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2008
    Checksum:              323
 
 
    Coasting Arc #14 (Orbit 2022)
    ---------------------------------------
 
    Vector Time (GMT): 2014/225/13:30:14.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941131.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3152549.40                 A    =         6789534.61  meter
     Y    =        3545650.09  meter          E    =           .0015888
     Z    =       -4870941.09                 I    =           51.66440
     XDOT =      -6752.239660                 Wp   =           46.85346
     YDOT =       2641.204266  meter/sec      RA   =          174.08291  deg
     ZDOT =      -2442.010819                 TA   =          199.10469
                                              MA   =          199.16434
                                              Ha   =            228.026  n.mi
                                              Hp   =            219.500
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10343009.85                 X    =         3136327.95
     Y    =       11632710.27  feet           Y    =         3580812.97  meter
     Z    =      -15980777.85                 Z    =        -4855666.26
     XDOT =     -22153.017258                 XDOT =       -6769.410039
     YDOT =       8665.368326  feet/sec       YDOT =        2565.600228  meter/sec
     ZDOT =      -8011.846519                 ZDOT =       -2474.853621
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6743906.13                 X    =        -2055542.59
     Y    =      -14102181.53  feet           Y    =        -4298344.93  meter
     Z    =      -15916383.64                 Z    =        -4851313.73
     XDOT =      22619.569665                 XDOT =        6894.444834
     YDOT =      -1595.853166  feet/sec       YDOT =        -486.416045  meter/sec
     ZDOT =      -8151.828280                 ZDOT =       -2484.677260
  
  
    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   14225.58317326  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6462 175.0736 0007422   3.3791 356.7409 15.50657575 20230
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14225.58317326   =   yrday.fracday
    Element set:     913
    Inclination:       51.6462  deg
    RA of node:       175.0736  deg
    Eccentricity:     .0007422     
    Arg of perigee:     3.3791  deg
    Mean anomaly:     356.7409  deg
    Mean motion:   15.50657575  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2023
    Checksum:              304
 
 
    Coasting Arc #15 (Orbit 2038)
    ---------------------------------------
 
    Vector Time (GMT): 2014/226/13:30:14.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941131.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2805678.25                 A    =         6788576.82  meter
     Y    =       -3535349.07  meter          E    =           .0006807
     Z    =        5065065.98                 I    =           51.69237
     XDOT =       6887.542861                 Wp   =           53.20627
     YDOT =      -2814.142140  meter/sec      RA   =          169.12372  deg
     ZDOT =       1853.223249                 TA   =           18.86685
                                              MA   =           18.84164
                                              Ha   =            228.080  n.mi
                                              Hp   =            219.296
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9204981.12                 X    =        -2790540.84
     Y    =      -11598914.27  feet           Y    =        -3566639.09  meter
     Z    =       16617670.53                 Z    =         5051473.47
     XDOT =      22596.925396                 XDOT =        6909.497078
     YDOT =      -9232.749802  feet/sec       YDOT =       -2736.998345  meter/sec
     ZDOT =       6080.128769                 ZDOT =        1886.735073
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5901052.57                 X    =         1798640.82
     Y    =       13650769.35  feet           Y    =         4160754.50  meter
     Z    =       16560420.83                 Z    =         5047616.27
     XDOT =     -23203.294966                 XDOT =       -7072.364306
     YDOT =       2490.091622  feet/sec       YDOT =         758.979926  meter/sec
     ZDOT =       6222.992542                 ZDOT =        1896.768127
  
  
    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   14226.61431511  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6461 169.9605 0007328   6.1215 354.0024 15.50684184 20390
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14226.61431511   =   yrday.fracday
    Element set:     914
    Inclination:       51.6461  deg
    RA of node:       169.9605  deg
    Eccentricity:     .0007328     
    Arg of perigee:     6.1215  deg
    Mean anomaly:     354.0024  deg
    Mean motion:   15.50684184  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2039
    Checksum:              283
 
 
    Coasting Arc #16 (Orbit 2040)
    ---------------------------------------
 
    Vector Time (GMT): 2014/226/17:21:42.209
    Vector Time (MET): N/A
    Weight (LBS)     : 940793.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3087609.55                 A    =         6790956.94  meter
     Y    =        3403909.47  meter          E    =           .0013773
     Z    =       -5011629.64                 I    =           51.69871
     XDOT =      -6709.695926                 Wp   =           49.70356
     YDOT =       3046.809256  meter/sec      RA   =          168.32907  deg
     ZDOT =      -2059.424036                 TA   =          200.21077
                                              MA   =          200.26535
                                              Ha   =            228.106  n.mi
                                              Hp   =            221.582
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10129952.59                 X    =         3073661.42
     Y    =       11167681.99  feet           Y    =         3438358.89  meter
     Z    =      -16442354.46                 Z    =        -4996664.66
     XDOT =     -22013.438079                 XDOT =       -6733.263447
     YDOT =       9996.093358  feet/sec       YDOT =        2971.645232  meter/sec
     ZDOT =      -6756.640539                 ZDOT =       -2092.075856
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15091939.99                 X    =        -4600023.31
     Y    =       -1279677.29  feet           Y    =         -390045.64  meter
     Z    =      -16379250.71                 Z    =        -4992395.62
     XDOT =       9293.988451                 XDOT =        2832.807680
     YDOT =     -21136.627789  feet/sec       YDOT =       -6442.444150  meter/sec
     ZDOT =      -6895.885640                 ZDOT =       -2101.865943
  
  
    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   14226.74321207  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6466 169.3217 0005875 343.7600  16.3361 15.49970900 20418
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14226.74321207   =   yrday.fracday
    Element set:     915
    Inclination:       51.6466  deg
    RA of node:       169.3217  deg
    Eccentricity:     .0005875     
    Arg of perigee:   343.7600  deg
    Mean anomaly:      16.3361  deg
    Mean motion:   15.49970900  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2041
    Checksum:              296
 
 
    Coasting Arc #17 (Orbit 2056)
    ---------------------------------------
 
    Vector Time (GMT): 2014/227/17:21:42.209
    Vector Time (MET): N/A
    Weight (LBS)     : 940793.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2994924.82                 A    =         6790536.52  meter
     Y    =       -3314244.44  meter          E    =           .0004160
     Z    =        5111014.91                 I    =           51.72749
     XDOT =       6658.711956                 Wp   =           49.84996
     YDOT =      -3391.229169  meter/sec      RA   =          163.37836  deg
     ZDOT =       1704.490464                 TA   =           23.70411
                                              MA   =           23.68495
                                              Ha   =            228.319  n.mi
                                              Hp   =            221.356
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9825868.83                 X    =        -2982469.06
     Y    =      -10873505.38  feet           Y    =        -3347665.79  meter
     Z    =       16768421.63                 Z    =         5096496.48
     XDOT =      21846.167836                 XDOT =        6687.858766
     YDOT =     -11126.079951  feet/sec       YDOT =       -3316.604122  meter/sec
     ZDOT =       5592.160315                 ZDOT =        1736.908218
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14690108.84                 X    =         4477545.18
     Y    =        1015374.23  feet           Y    =          309486.06  meter
     Z    =       16707199.01                 Z    =         5092354.26
     XDOT =      -8033.770430                 XDOT =       -2448.693227
     YDOT =      22031.636635  feet/sec       YDOT =        6715.242846  meter/sec
     ZDOT =       5730.476943                 ZDOT =        1746.649372
  
  
    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   14227.77481035  .00016717  00000-0  10270-3 0  9165
    2 25544  51.6466 164.2113 0005834 348.5633  11.5384 15.49952948 20572
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14227.77481035   =   yrday.fracday
    Element set:     916
    Inclination:       51.6466  deg
    RA of node:       164.2113  deg
    Eccentricity:     .0005834     
    Arg of perigee:   348.5633  deg
    Mean anomaly:      11.5384  deg
    Mean motion:   15.49952948  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2057
    Checksum:              321
 
             

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