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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  7534.74
   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 
   ------------------------------------------------------------------------
   202/21:41:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              225.3  
   000/00:00:00.000           0.0               0.0              223.0  
   
   205/03:28:03.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              225.8  
   000/00:00:00.000           0.0               0.0              223.0  
   
 
 
    Coasting Arc #1 (Orbit 1664)
    ---------------------------------------
 
    Vector Time (GMT): 2014/202/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1681923.61                 A    =         6793910.53  meter
     Y    =       -5177928.15  meter          E    =           .0001977
     Z    =       -4066343.41                 I    =           51.30480
     XDOT =       4797.957237                 Wp   =          143.61989
     YDOT =      -4572.214500  meter/sec      RA   =          288.75185  deg
     ZDOT =       3836.952574                 TA   =          166.31976
                                              MA   =          166.31440
                                              Ha   =            225.228  n.mi
                                              Hp   =            222.995
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5518122.08                 X    =        -1604144.99
     Y    =      -16987953.24  feet           Y    =        -5196301.27  meter
     Z    =      -13341021.68                 Z    =        -4074325.42
     XDOT =      15741.329518                 XDOT =        4830.089650
     YDOT =     -15000.703741  feet/sec       YDOT =       -4518.381316  meter/sec
     ZDOT =      12588.427081                 ZDOT =        3860.337861
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12371247.61                 X    =        -3770756.27
     Y    =       12849625.49  feet           Y    =         3916565.85  meter
     Z    =      -13373946.44                 Z    =        -4076378.87
     XDOT =     -19700.629022                 XDOT =       -6004.751726
     YDOT =      -5758.955158  feet/sec       YDOT =       -1755.329532  meter/sec
     ZDOT =      12688.457106                 ZDOT =        3867.441726
  
  
    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   14202.50894293  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6479 289.4639 0005751 277.0816  82.9675 15.50150073 16656
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14202.50894293   =   yrday.fracday
    Element set:     900
    Inclination:       51.6479  deg
    RA of node:       289.4639  deg
    Eccentricity:     .0005751     
    Arg of perigee:   277.0816  deg
    Mean anomaly:      82.9675  deg
    Mean motion:   15.50150073  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1665
    Checksum:              326
 
 
    Coasting Arc #2 (Orbit 1671)
    ---------------------------------------
 
    Vector Time (GMT): 2014/202/21:41:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 884340.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4260627.69                 A    =         6794926.62  meter
     Y    =       -3736357.74  meter          E    =           .0005865
     Z    =        3744254.83                 I    =           51.30280
     XDOT =       1680.798166                 Wp   =           89.99840
     YDOT =       6162.796451  meter/sec      RA   =          286.79335  deg
     ZDOT =       4231.431596                 TA   =          314.93894
                                              MA   =          314.98650
                                              Ha   =            225.347  n.mi
                                              Hp   =            223.036
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13978437.31                 X    =         4283903.61
     Y    =      -12258391.54  feet           Y    =        -3688582.85  meter
     Z    =       12284300.61                 Z    =         3765008.39
     XDOT =       5514.429677                 XDOT =        1591.204685
     YDOT =      20219.148460  feet/sec       YDOT =        6181.090898  meter/sec
     ZDOT =      13882.649593                 ZDOT =        4239.379539
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10769310.88                 X    =         3282485.96
     Y    =       15083081.99  feet           Y    =         4597323.39  meter
     Z    =       12373014.79                 Z    =         3771294.91
     XDOT =     -19569.961151                 XDOT =       -5964.924159
     YDOT =       2542.507413  feet/sec       YDOT =         774.956259  meter/sec
     ZDOT =      13915.255324                 ZDOT =        4241.369823
  
  
    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   14202.96021934  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6465 287.2289 0005755 283.1809  76.8699 15.50146672 16728
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14202.96021934   =   yrday.fracday
    Element set:     901
    Inclination:       51.6465  deg
    RA of node:       287.2289  deg
    Eccentricity:     .0005755     
    Arg of perigee:   283.1809  deg
    Mean anomaly:      76.8699  deg
    Mean motion:   15.50146672  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1672
    Checksum:              333
 
 
    Coasting Arc #3 (Orbit 1686)
    ---------------------------------------
 
    Vector Time (GMT): 2014/203/21:41:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 884340.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4058075.96                 A    =         6794022.45  meter
     Y    =        3689289.19  meter          E    =           .0004203
     Z    =       -4014086.31                 I    =           51.29210
     XDOT =      -1875.670823                 Wp   =           17.40952
     YDOT =      -6314.069646  meter/sec      RA   =          281.81386  deg
     ZDOT =      -3904.074518                 TA   =          211.77908
                                              MA   =          211.80445
                                              Ha   =            225.707  n.mi
                                              Hp   =            222.910
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13313897.50                 X    =        -4079529.91
     Y    =       12103967.16  feet           Y    =         3643789.59  meter
     Z    =      -13169574.51                 Z    =        -4033851.42
     XDOT =      -6153.775666                 XDOT =       -1785.961524
     YDOT =     -20715.451593  feet/sec       YDOT =       -6334.542646  meter/sec
     ZDOT =     -12808.643432                 ZDOT =       -3912.968856
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10930373.00                 X    =        -3331577.69
     Y    =      -14214772.19  feet           Y    =        -4332662.56  meter
     Z    =      -13254085.33                 Z    =        -4039845.21
     XDOT =      20122.477611                 XDOT =        6133.331176
     YDOT =      -3487.228502  feet/sec       YDOT =       -1062.907247  meter/sec
     ZDOT =     -12845.247315                 ZDOT =       -3915.231382
  
  
    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   14203.92723531  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6468 282.4372 0005756 288.5205  71.5320 15.50155850 16878
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14203.92723531   =   yrday.fracday
    Element set:     902
    Inclination:       51.6468  deg
    RA of node:       282.4372  deg
    Eccentricity:     .0005756     
    Arg of perigee:   288.5205  deg
    Mean anomaly:      71.5320  deg
    Mean motion:   15.50155850  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1687
    Checksum:              303
 
 
    Coasting Arc #4 (Orbit 1702)
    ---------------------------------------
 
    Vector Time (GMT): 2014/204/21:41:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 884340.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3869070.18                 A    =         6793150.98  meter
     Y    =       -3610299.58  meter          E    =           .0004157
     Z    =        4256376.67                 I    =           51.28369
     XDOT =       2100.554052                 Wp   =          100.39718
     YDOT =       6451.965211  meter/sec      RA   =          276.83385  deg
     ZDOT =       3559.490810                 TA   =          313.04551
                                              MA   =          313.08031
                                              Ha   =            225.692  n.mi
                                              Hp   =            222.966
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12693799.81                 X    =         3888478.01
     Y    =      -11844814.90  feet           Y    =        -3566925.02  meter
     Z    =       13964490.40                 Z    =         4275218.61
     XDOT =       6891.581534                 XDOT =        2010.959970
     YDOT =      21167.864866  feet/sec       YDOT =        6474.953680  meter/sec
     ZDOT =      11678.119457                 ZDOT =        3569.477843
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10957236.10                 X    =         3339765.56
     Y    =       13383355.53  feet           Y    =         4079246.77  meter
     Z    =       14045068.79                 Z    =         4280936.97
     XDOT =     -20608.291092                 XDOT =       -6281.407125
     YDOT =       4560.946874  feet/sec       YDOT =        1390.176607  meter/sec
     ZDOT =      11719.347360                 ZDOT =        3572.057075
  
  
    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   14204.95871226  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6467 277.3265 0005780 291.6654  68.3881 15.50160953 17036
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14204.95871226   =   yrday.fracday
    Element set:     903
    Inclination:       51.6467  deg
    RA of node:       277.3265  deg
    Eccentricity:     .0005780     
    Arg of perigee:   291.6654  deg
    Mean anomaly:      68.3881  deg
    Mean motion:   15.50160953  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1703
    Checksum:              321
 
 
    Coasting Arc #5 (Orbit 1705)
    ---------------------------------------
 
    Vector Time (GMT): 2014/205/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2379361.03                 A    =         6795400.38  meter
     Y    =       -5253522.44  meter          E    =           .0001495
     Z    =       -3592387.78                 I    =           51.28863
     XDOT =       4011.598683                 Wp   =          351.98440
     YDOT =      -4822.137309  meter/sec      RA   =          275.58345  deg
     ZDOT =       4396.125317                 TA   =          325.36127
                                              MA   =          325.37101
                                              Ha   =            225.760  n.mi
                                              Hp   =            222.978
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7806302.59                 X    =        -2302987.70
     Y    =      -17235966.02  feet           Y    =        -5279702.63  meter
     Z    =      -11786049.16                 Z    =        -3603761.19
     XDOT =      13161.413001                 XDOT =        4043.868136
     YDOT =     -15820.660461  feet/sec       YDOT =       -4777.097002  meter/sec
     ZDOT =      14422.983322                 ZDOT =        4415.690744
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5563716.18                 X    =        -1695820.69
     Y    =      -18053923.54  feet           Y    =        -5502835.90  meter
     Z    =      -11833374.25                 Z    =        -3606812.47
     XDOT =      13592.269919                 XDOT =        4142.923871
     YDOT =     -13694.577716  feet/sec       YDOT =       -4174.107288  meter/sec
     ZDOT =      14506.844793                 ZDOT =        4421.686293
  
  
    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   14205.15211193  .00016717  00000-0  10270-3 0  9046
    2 25544  51.6451 276.3662 0005939 291.6709  68.3809 15.50159815 17064
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14205.15211193   =   yrday.fracday
    Element set:     904
    Inclination:       51.6451  deg
    RA of node:       276.3662  deg
    Eccentricity:     .0005939     
    Arg of perigee:   291.6709  deg
    Mean anomaly:      68.3809  deg
    Mean motion:   15.50159815  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1706
    Checksum:              314
 
 
    Coasting Arc #6 (Orbit 1721)
    ---------------------------------------
 
    Vector Time (GMT): 2014/206/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2574721.60                 A    =         6796196.47  meter
     Y    =        5362514.88  meter          E    =           .0007446
     Z    =        3282994.30                 I    =           51.28969
     XDOT =      -3809.517559                 Wp   =           72.54893
     YDOT =       4707.761820  meter/sec      RA   =          270.60439  deg
     ZDOT =      -4691.076214                 TA   =           69.19159
                                              MA   =           69.11184
                                              Ha   =            225.993  n.mi
                                              Hp   =            222.951
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8447249.35                 X    =         2498617.93
     Y    =       17593552.76  feet           Y    =         5390881.28  meter
     Z    =       10770978.68                 Z    =         3295317.32
     XDOT =     -12498.417189                 XDOT =       -3839.090365
     YDOT =      15445.412796  feet/sec       YDOT =        4664.996381  meter/sec
     ZDOT =     -15390.669992                 ZDOT =       -4709.653423
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6479500.28                 X    =         1974951.69
     Y    =       18379238.70  feet           Y    =         5601991.96  meter
     Z    =       10822327.06                 Z    =         3298645.29
     XDOT =     -12618.913239                 XDOT =       -3846.244755
     YDOT =      13579.393154  feet/sec       YDOT =        4138.999033  meter/sec
     ZDOT =     -15470.313866                 ZDOT =       -4715.351666
  
  
    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   14206.18358074  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6453 271.2553 0006133 296.0944  63.9576 15.50195759 17223
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14206.18358074   =   yrday.fracday
    Element set:     905
    Inclination:       51.6453  deg
    RA of node:       271.2553  deg
    Eccentricity:     .0006133     
    Arg of perigee:   296.0944  deg
    Mean anomaly:      63.9576  deg
    Mean motion:   15.50195759  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1722
    Checksum:              318
 
 
    Coasting Arc #7 (Orbit 1736)
    ---------------------------------------
 
    Vector Time (GMT): 2014/207/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2800159.44                 A    =         6797092.50  meter
     Y    =       -5433174.98  meter          E    =           .0004598
     Z    =       -2966644.45                 I    =           51.29154
     XDOT =       3632.593689                 Wp   =          348.63624
     YDOT =      -4576.202642  meter/sec      RA   =          265.62412  deg
     ZDOT =       4955.324563                 TA   =          337.33863
                                              MA   =          337.35893
                                              Ha   =            226.064  n.mi
                                              Hp   =            222.782
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9186874.82                 X    =        -2724785.61
     Y    =      -17825377.21  feet           Y    =        -5464066.51  meter
     Z    =       -9733085.45                 Z    =        -2980064.27
     XDOT =      11917.958297                 XDOT =        3659.424957
     YDOT =     -15013.788194  feet/sec       YDOT =       -4535.430968  meter/sec
     ZDOT =      16257.626520                 ZDOT =        4973.035690
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7517472.88                 X    =        -2291325.73
     Y    =      -18561708.07  feet           Y    =        -5657608.62  meter
     Z    =       -9789090.31                 Z    =        -2983714.73
     XDOT =      11740.130656                 XDOT =        3578.391824
     YDOT =     -13363.406881  feet/sec       YDOT =       -4073.166417  meter/sec
     ZDOT =      16333.567228                 ZDOT =        4978.471291
  
  
    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   14207.15058006  .00016717  00000-0  10270-3 0  9062
    2 25544  51.6438 266.4624 0005867 299.0333  61.0229 15.50173107 17372
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14207.15058006   =   yrday.fracday
    Element set:     906
    Inclination:       51.6438  deg
    RA of node:       266.4624  deg
    Eccentricity:     .0005867     
    Arg of perigee:   299.0333  deg
    Mean anomaly:      61.0229  deg
    Mean motion:   15.50173107  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1737
    Checksum:              298
 
 
    Coasting Arc #8 (Orbit 1752)
    ---------------------------------------
 
    Vector Time (GMT): 2014/208/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3028562.66                 A    =         6797818.44  meter
     Y    =        5492054.76  meter          E    =           .0008142
     Z    =        2615545.30                 I    =           51.29751
     XDOT =      -3494.723565                 Wp   =           87.61484
     YDOT =       4409.647826  meter/sec      RA   =          260.64587  deg
     ZDOT =      -5198.282615                 TA   =           62.83312
                                              MA   =           62.75013
                                              Ha   =            226.291  n.mi
                                              Hp   =            222.688
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9936229.20                 X    =         2954218.94
     Y    =       18018552.36  feet           Y    =         5525506.27  meter
     Z    =        8581185.36                 Z    =         2630077.06
     XDOT =     -11465.628493                 XDOT =       -3518.522463
     YDOT =      14467.348511  feet/sec       YDOT =        4370.434798  meter/sec
     ZDOT =     -17054.732989                 ZDOT =       -5215.316697
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8576593.94                 X    =         2614145.83
     Y    =       18676000.00  feet           Y    =         5692444.80  meter
     Z    =        8641914.27                 Z    =         2634055.47
     XDOT =     -10995.543239                 XDOT =       -3351.441579
     YDOT =      12996.719636  feet/sec       YDOT =        3961.400145  meter/sec
     ZDOT =     -17127.766230                 ZDOT =       -5220.543147
  
  
    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   14208.18203730  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6437 261.3512 0006084 303.3231  56.7336 15.50209850 17532
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14208.18203730   =   yrday.fracday
    Element set:     907
    Inclination:       51.6437  deg
    RA of node:       261.3512  deg
    Eccentricity:     .0006084     
    Arg of perigee:   303.3231  deg
    Mean anomaly:      56.7336  deg
    Mean motion:   15.50209850  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1753
    Checksum:              279
 
 
    Coasting Arc #9 (Orbit 1767)
    ---------------------------------------
 
    Vector Time (GMT): 2014/209/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3277631.30                 A    =         6798605.99  meter
     Y    =       -5503468.37  meter          E    =           .0007674
     Z    =       -2263638.46                 I    =           51.30513
     XDOT =       3388.318488                 Wp   =          356.31331
     YDOT =      -4239.979775  meter/sec      RA   =          255.66697  deg
     ZDOT =       5408.824150                 TA   =          338.41535
                                              MA   =          338.44768
                                              Ha   =            226.350  n.mi
                                              Hp   =            222.518
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10753383.53                 X    =        -3204850.86
     Y    =      -18055998.60  feet           Y    =        -5539713.93  meter
     Z    =       -7426635.36                 Z    =        -2279383.84
     XDOT =      11116.530472                 XDOT =        3409.205303
     YDOT =     -13910.694799  feet/sec       YDOT =       -4201.972842  meter/sec
     ZDOT =      17745.486057                 ZDOT =        5425.334348
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9717762.83                 X    =        -2961974.11
     Y    =      -18607427.46  feet           Y    =        -5671543.89  meter
     Z    =       -7492528.57                 Z    =        -2283722.71
     XDOT =      10381.467637                 XDOT =        3164.271336
     YDOT =     -12587.199605  feet/sec       YDOT =       -3836.578440  meter/sec
     ZDOT =      17816.261370                 ZDOT =        5430.396466
  
  
    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   14209.14902607  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6429 256.5582 0005758 306.6325  53.4296 15.50187551 17681
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14209.14902607   =   yrday.fracday
    Element set:     908
    Inclination:       51.6429  deg
    RA of node:       256.5582  deg
    Eccentricity:     .0005758     
    Arg of perigee:   306.6325  deg
    Mean anomaly:      53.4296  deg
    Mean motion:   15.50187551  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1768
    Checksum:              325
 
 
    Coasting Arc #10 (Orbit 1783)
    ---------------------------------------
 
    Vector Time (GMT): 2014/210/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3520579.62                 A    =         6799180.40  meter
     Y    =        5501731.51  meter          E    =           .0008423
     Z    =        1877376.44                 I    =           51.31564
     XDOT =      -3326.803590                 Wp   =          100.82188
     YDOT =       4043.463261  meter/sec      RA   =          250.69005  deg
     ZDOT =      -5591.005340                 TA   =           58.45324
                                              MA   =           58.37101
                                              Ha   =            226.567  n.mi
                                              Hp   =            222.369
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11550458.07                 X    =         3449676.83
     Y    =       18050300.23  feet           Y    =         5540704.42  meter
     Z    =        6159371.53                 Z    =         1894306.50
     XDOT =     -10914.709940                 XDOT =       -3344.612492
     YDOT =      13265.955582  feet/sec       YDOT =        4006.161355  meter/sec
     ZDOT =     -18343.193372                 ZDOT =       -5607.209329
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10841095.09                 X    =         3304365.78
     Y    =       18461261.93  feet           Y    =         5626992.64  meter
     Z    =        6230308.39                 Z    =         1898998.00
     XDOT =      -9932.573354                 XDOT =       -3027.448358
     YDOT =      12068.426249  feet/sec       YDOT =        3678.456321  meter/sec
     ZDOT =     -18412.630678                 ZDOT =       -5612.169831
  
  
    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   14210.18047195  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6426 251.4465 0005974 310.8571  49.2061 15.50224472 17847
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14210.18047195   =   yrday.fracday
    Element set:     909
    Inclination:       51.6426  deg
    RA of node:       251.4465  deg
    Eccentricity:     .0005974     
    Arg of perigee:   310.8571  deg
    Mean anomaly:      49.2061  deg
    Mean motion:   15.50224472  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1784
    Checksum:              300
 
 
    Coasting Arc #11 (Orbit 1798)
    ---------------------------------------
 
    Vector Time (GMT): 2014/211/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3772527.46                 A    =         6799783.28  meter
     Y    =       -5447367.66  meter          E    =           .0010503
     Z    =       -1497082.17                 I    =           51.32901
     XDOT =       3299.329228                 Wp   =            5.61118
     YDOT =      -3858.899924  meter/sec      RA   =          245.71337  deg
     ZDOT =       5740.838089                 TA   =          337.99314
                                              MA   =          338.03820
                                              Ha   =            226.622  n.mi
                                              Hp   =            222.217
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12377058.60                 X    =        -3704061.15
     Y    =      -17871941.15  feet           Y    =        -5489171.66  meter
     Z    =       -4911686.91                 Z    =        -1515242.01
     XDOT =      10824.570959                 XDOT =        3314.348457
     YDOT =     -12660.432823  feet/sec       YDOT =       -3821.920776  meter/sec
     ZDOT =      18834.770634                 ZDOT =        5756.901930
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11994803.03                 X    =        -3656015.96
     Y    =      -18109898.16  feet           Y    =        -5519896.96  meter
     Z    =       -4987866.97                 Z    =        -1520301.85
     XDOT =       9630.304234                 XDOT =        2935.316730
     YDOT =     -11572.776241  feet/sec       YDOT =       -3527.382198  meter/sec
     ZDOT =      18903.577864                 ZDOT =        5761.810533
  
  
    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   14211.14745002  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6430 246.6536 0005652 314.5089  45.5599 15.50204464 17995
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14211.14745002   =   yrday.fracday
    Element set:     910
    Inclination:       51.6430  deg
    RA of node:       246.6536  deg
    Eccentricity:     .0005652     
    Arg of perigee:   314.5089  deg
    Mean anomaly:      45.5599  deg
    Mean motion:   15.50204464  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1799
    Checksum:              299
 
 
    Coasting Arc #12 (Orbit 1814)
    ---------------------------------------
 
    Vector Time (GMT): 2014/212/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4008696.12                 A    =         6800140.24  meter
     Y    =        5381065.86  meter          E    =           .0008132
     Z    =        1083790.71                 I    =           51.34364
     XDOT =      -3318.573334                 Wp   =          111.94645
     YDOT =       3657.918137  meter/sec      RA   =          240.73844  deg
     ZDOT =      -5854.592062                 TA   =           56.27173
                                              MA   =           56.19426
                                              Ha   =            226.827  n.mi
                                              Hp   =            222.033
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13151890.14                 X    =         3942961.24
     Y    =       17654415.56  feet           Y    =         5425526.14  meter
     Z    =        3555743.79                 Z    =         1103104.44
     XDOT =     -10887.707790                 XDOT =       -3330.791058
     YDOT =      12001.043756  feet/sec       YDOT =        3620.739396  meter/sec
     ZDOT =     -19207.979206                 ZDOT =       -5870.742665
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13088387.32                 X    =         3989340.46
     Y    =       17685061.08  feet           Y    =         5390406.62  meter
     Z    =        3636845.99                 Z    =         1108510.66
     XDOT =      -9504.811485                 XDOT =       -2897.066541
     YDOT =      11020.000875  feet/sec       YDOT =        3358.896267  meter/sec
     ZDOT =     -19277.118352                 ZDOT =       -5875.665674
  
  
    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   14212.17888484  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6424 241.5416 0005849 318.6880  41.3827 15.50238648 18159
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14212.17888484   =   yrday.fracday
    Element set:     911
    Inclination:       51.6424  deg
    RA of node:       241.5416  deg
    Eccentricity:     .0005849     
    Arg of perigee:   318.6880  deg
    Mean anomaly:      41.3827  deg
    Mean motion:   15.50238648  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1815
    Checksum:              320
 
 
    Coasting Arc #13 (Orbit 1829)
    ---------------------------------------
 
    Vector Time (GMT): 2014/213/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4241142.62                 A    =         6800491.56  meter
     Y    =       -5261416.11  meter          E    =           .0012894
     Z    =        -683360.88                 I    =           51.36203
     XDOT =       3370.786513                 Wp   =           15.38694
     YDOT =      -3483.403460  meter/sec      RA   =          235.76470  deg
     ZDOT =       5937.740017                 TA   =          337.21280
                                              MA   =          337.26998
                                              Ha   =            226.883  n.mi
                                              Hp   =            221.906
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13914509.90                 X    =        -4178673.54
     Y    =      -17261863.89  feet           Y    =        -5308494.02  meter
     Z    =       -2241997.64                 Z    =         -703811.77
     XDOT =      11059.010871                 XDOT =        3380.644901
     YDOT =     -11428.489043  feet/sec       YDOT =       -3445.654005  meter/sec
     ZDOT =      19480.774333                 ZDOT =        5954.138596
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14155592.54                 X    =        -4314624.61
     Y    =      -17053207.71  feet           Y    =        -5197817.71  meter
     Z    =       -2327958.55                 Z    =         -709561.77
     XDOT =       9521.401799                 XDOT =        2902.123268
     YDOT =     -10556.096644  feet/sec       YDOT =       -3217.498257  meter/sec
     ZDOT =      19550.935905                 ZDOT =        5959.125264
  
  
    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   14213.14585196  .00016717  00000-0  10270-3 0  9120
    2 25544  51.6438 236.7492 0005593 322.4534  37.6225 15.50223878 18305
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14213.14585196   =   yrday.fracday
    Element set:     912
    Inclination:       51.6438  deg
    RA of node:       236.7492  deg
    Eccentricity:     .0005593     
    Arg of perigee:   322.4534  deg
    Mean anomaly:      37.6225  deg
    Mean motion:   15.50223878  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1830
    Checksum:              309
 
 
    Coasting Arc #14 (Orbit 1845)
    ---------------------------------------
 
    Vector Time (GMT): 2014/214/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4448659.46                 A    =         6800584.54  meter
     Y    =        5133953.68  meter          E    =           .0007157
     Z    =         252556.83                 I    =           51.38030
     XDOT =      -3466.638346                 Wp   =          120.30925
     YDOT =       3304.012891  meter/sec      RA   =          230.79241  deg
     ZDOT =      -5976.990551                 TA   =           56.96524
                                              MA   =           56.89651
                                              Ha   =            227.072  n.mi
                                              Hp   =            221.708
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14595339.45                 X    =         4389692.95
     Y    =       16843680.04  feet           Y    =         5183371.75  meter
     Z    =         828598.54                 Z    =          274024.38
     XDOT =     -11373.485386                 XDOT =       -3474.292870
     YDOT =      10839.937306  feet/sec       YDOT =        3265.203894  meter/sec
     ZDOT =     -19609.549051                 ZDOT =       -5993.849450
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15122764.41                 X    =         4609418.59
     Y    =       16366968.95  feet           Y    =         4988652.13  meter
     Z    =         918907.29                 Z    =          280082.94
     XDOT =      -9702.894468                 XDOT =       -2957.442234
     YDOT =      10090.829790  feet/sec       YDOT =        3075.684920  meter/sec
     ZDOT =     -19681.635813                 ZDOT =       -5998.962596
  
  
    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   14214.17727582  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6432 231.6371 0005760 326.5490  33.5296 15.50251996 18463
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14214.17727582   =   yrday.fracday
    Element set:     913
    Inclination:       51.6432  deg
    RA of node:       231.6371  deg
    Eccentricity:     .0005760     
    Arg of perigee:   326.5490  deg
    Mean anomaly:      33.5296  deg
    Mean motion:   15.50251996  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1846
    Checksum:              309
 
 
    Coasting Arc #15 (Orbit 1861)
    ---------------------------------------
 
    Vector Time (GMT): 2014/215/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4639907.53                 A    =         6800639.15  meter
     Y    =       -4956854.00  meter          E    =           .0014677
     Z    =         158793.90                 I    =           51.40239
     XDOT =       3591.279531                 Wp   =           25.33576
     YDOT =      -3163.631825  meter/sec      RA   =          225.82189  deg
     ZDOT =       5988.678244                 TA   =          336.37860
                                              MA   =          336.44592
                                              Ha   =            227.139  n.mi
                                              Hp   =            221.593
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15222793.75                 X    =        -4584905.37
     Y    =      -16262644.37  feet           Y    =        -5008432.91  meter
     Z    =         520977.36                 Z    =          136387.58
     XDOT =      11782.413159                 XDOT =        3597.298178
     YDOT =     -10379.369503  feet/sec       YDOT =       -3123.438206  meter/sec
     ZDOT =      19647.894502                 ZDOT =        6006.138668
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16008582.71                 X    =        -4879416.01
     Y    =      -15492634.49  feet           Y    =        -4722154.99  meter
     Z    =         426643.62                 Z    =          130040.98
     XDOT =      10003.367920                 XDOT =        3049.026542
     YDOT =      -9772.134974  feet/sec       YDOT =       -2978.546740  meter/sec
     ZDOT =      19722.514466                 ZDOT =        6011.422409
  
  
    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   14215.20869511  .00016717  00000-0  10270-3 0  9147
    2 25544  51.6448 226.5256 0005600 330.5304  29.5530 15.50245101 18622
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14215.20869511   =   yrday.fracday
    Element set:     914
    Inclination:       51.6448  deg
    RA of node:       226.5256  deg
    Eccentricity:     .0005600     
    Arg of perigee:   330.5304  deg
    Mean anomaly:      29.5530  deg
    Mean motion:   15.50245101  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1862
    Checksum:              273
 
 
    Coasting Arc #16 (Orbit 1876)
    ---------------------------------------
 
    Vector Time (GMT): 2014/216/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4798776.31                 A    =         6800441.87  meter
     Y    =        4778980.38  meter          E    =           .0005532
     Z    =        -596571.07                 I    =           51.42372
     XDOT =      -3751.227813                 Wp   =          123.39001
     YDOT =       3029.475399  meter/sec      RA   =          220.85269  deg
     ZDOT =      -5949.279206                 TA   =           63.05449
                                              MA   =           62.99799
                                              Ha   =            227.301  n.mi
                                              Hp   =            221.404
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15744016.76                 X    =         4747877.93
     Y    =       15679069.50  feet           Y    =         4832358.82  meter
     Z    =       -1957254.18                 Z    =         -573382.95
     XDOT =     -12307.177863                 XDOT =       -3755.925765
     YDOT =       9939.223749  feet/sec       YDOT =        2987.500595  meter/sec
     ZDOT =     -19518.632567                 ZDOT =       -5967.513403
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16762997.99                 X    =         5109361.79
     Y    =       14597330.56  feet           Y    =         4449266.35  meter
     Z    =       -1859561.02                 Z    =         -566794.20
     XDOT =     -10432.480482                 XDOT =       -3179.820051
     YDOT =       9502.765848  feet/sec       YDOT =        2896.443030  meter/sec
     ZDOT =     -19596.520492                 ZDOT =       -5973.019446
  
  
    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   14216.17564436  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6442 221.7334 0005726 334.2510  25.8355 15.50265233 18777
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14216.17564436   =   yrday.fracday
    Element set:     915
    Inclination:       51.6442  deg
    RA of node:       221.7334  deg
    Eccentricity:     .0005726     
    Arg of perigee:   334.2510  deg
    Mean anomaly:      25.8355  deg
    Mean motion:   15.50265233  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1877
    Checksum:              294
 
 
    Coasting Arc #17 (Orbit 1892)
    ---------------------------------------
 
    Vector Time (GMT): 2014/217/03:28:03.000
    Vector Time (MET): N/A
    Weight (LBS)     : 898773.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4930201.26                 A    =         6800183.59  meter
     Y    =       -4559136.20  meter          E    =           .0015725
     Z    =        1008735.43                 I    =           51.44818
     XDOT =       3933.444461                 Wp   =           35.39696
     YDOT =      -2943.830220  meter/sec      RA   =          215.88523  deg
     ZDOT =       5886.098249                 TA   =          335.55312
                                              MA   =          335.62761
                                              Ha   =            227.396  n.mi
                                              Hp   =            221.273
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16175200.98                 X    =        -4883753.61
     Y    =      -14957795.94  feet           Y    =        -4614009.22  meter
     Z    =        3309499.45                 Z    =          984898.01
     XDOT =      12905.001511                 XDOT =        3937.478097
     YDOT =      -9658.235629  feet/sec       YDOT =       -2899.821553  meter/sec
     ZDOT =      19311.345960                 ZDOT =        5905.215955
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17389445.74                 X    =        -5300303.06
     Y    =      -13551201.39  feet           Y    =        -4130406.19  meter
     Z    =        3209001.43                 Z    =          978103.64
     XDOT =      10943.079752                 XDOT =        3335.450708
     YDOT =      -9423.357189  feet/sec       YDOT =       -2872.239271  meter/sec
     ZDOT =      19392.977931                 ZDOT =        5910.979673
  
  
    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   14217.20705128  .00016717  00000-0  10270-3 0  9164
    2 25544  51.6454 216.6220 0005660 338.3463  21.7447 15.50265589 18935
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14217.20705128   =   yrday.fracday
    Element set:     916
    Inclination:       51.6454  deg
    RA of node:       216.6220  deg
    Eccentricity:     .0005660     
    Arg of perigee:   338.3463  deg
    Mean anomaly:      21.7447  deg
    Mean motion:   15.50265589  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1893
    Checksum:              303
 
             

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