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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  13813.3262
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   78.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.651
   ET - UTC  (sec) :   68.18
   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 
   ------------------------------------------------------------------------
   152/21:55:46.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.8  
   000/00:00:00.000           0.0               0.0              216.1  
   
   153/10:47:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.7  
   000/00:00:00.000           0.0               0.0              216.2  
   
   153/13:10:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.6  
   000/00:00:00.000           0.0               0.0              216.3  
   
   155/13:34:21.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.3  
   000/00:00:00.000           0.0               0.0              216.4  
   
   156/18:50:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.1  
   000/00:00:00.000           0.0               0.0              216.5  
   
   160/01:48:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.8  
   000/00:00:00.000           0.0               0.0              216.6  
   
 
 
    Coasting Arc #1 (Orbit 1837)
    ---------------------------------------
 
    Vector Time (GMT): 2017/146/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5757854.75                 A    =         6784702.92  meter
     Y    =         606861.32  meter          E    =           .0011752
     Z    =        3532958.62                 I    =           51.84666
     XDOT =       2166.755967                 Wp   =          115.87435
     YDOT =      -5807.917461  meter/sec      RA   =          145.33826  deg
     ZDOT =       4512.259280                 TA   =          285.60926
                                              MA   =          285.73893
                                              Ha   =            221.624  n.mi
                                              Hp   =            215.420
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18890599.56                 X    =        -5781374.56
     Y    =        1991014.84  feet           Y    =          542341.16  meter
     Z    =       11591071.59                 Z    =         3504931.21
     XDOT =       7108.779420                 XDOT =        2209.621870
     YDOT =     -19054.847314  feet/sec       YDOT =       -5783.448198  meter/sec
     ZDOT =      14804.000263                 ZDOT =        4522.888304
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6715306.62                 X    =        -2046825.46
     Y    =       17848719.06  feet           Y    =         5440289.57  meter
     Z    =       11467332.62                 Z    =         3495242.98
     XDOT =     -12591.937799                 XDOT =       -3838.022641
     YDOT =     -14314.894431  feet/sec       YDOT =       -4363.179823  meter/sec
     ZDOT =      14851.792403                 ZDOT =        4526.826324
  
  
    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   17146.55696808  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6360 146.1378 0005009 199.1516 160.9449 15.53939675 18385
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17146.55696808   =   yrday.fracday
    Element set:     900
    Inclination:       51.6360  deg
    RA of node:       146.1378  deg
    Eccentricity:     .0005009     
    Arg of perigee:   199.1516  deg
    Mean anomaly:     160.9449  deg
    Mean motion:   15.53939675  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1838
    Checksum:              342
 
 
    Coasting Arc #2 (Orbit 1852)
    ---------------------------------------
 
    Vector Time (GMT): 2017/147/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4955055.18                 A    =         6781094.76  meter
     Y    =         584068.58  meter          E    =           .0007658
     Z    =       -4598258.17                 I    =           51.86113
     XDOT =      -3550.007049                 Wp   =           98.87439
     YDOT =       6061.268765  meter/sec      RA   =          140.36620  deg
     ZDOT =      -3061.062658                 TA   =          140.62752
                                              MA   =          140.57183
                                              Ha   =            221.578  n.mi
                                              Hp   =            215.588
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16256742.72                 X    =         4970492.04
     Y    =        1916235.51  feet           Y    =          639566.28  meter
     Z    =      -15086148.85                 Z    =        -4574150.20
     XDOT =     -11647.004755                 XDOT =       -3602.652590
     YDOT =      19886.052380  feet/sec       YDOT =        6021.276230  meter/sec
     ZDOT =     -10042.856491                 ZDOT =       -3078.434760
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8800522.52                 X    =         2682399.26
     Y    =      -13917608.68  feet           Y    =        -4242087.12  meter
     Z    =      -14979869.88                 Z    =        -4565864.34
     XDOT =      11904.682875                 XDOT =        3628.547340
     YDOT =      18401.044363  feet/sec       YDOT =        5608.638322  meter/sec
     ZDOT =     -10120.457254                 ZDOT =       -3084.715371
  
  
    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   17147.52162262  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6365 141.3296 0004900 201.2244 158.8706 15.53923580 18535
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17147.52162262   =   yrday.fracday
    Element set:     901
    Inclination:       51.6365  deg
    RA of node:       141.3296  deg
    Eccentricity:     .0004900     
    Arg of perigee:   201.2244  deg
    Mean anomaly:     158.8706  deg
    Mean motion:   15.53923580  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1853
    Checksum:              293
 
 
    Coasting Arc #3 (Orbit 1868)
    ---------------------------------------
 
    Vector Time (GMT): 2017/148/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3934311.79                 A    =         6778560.25  meter
     Y    =       -1851215.70  meter          E    =           .0007004
     Z    =        5200389.88                 I    =           51.87763
     XDOT =       4590.547865                 Wp   =          168.12638
     YDOT =      -5996.346449  meter/sec      RA   =          135.38843  deg
     ZDOT =       1331.383230                 TA   =          269.08337
                                              MA   =          269.16362
                                              Ha   =            221.463  n.mi
                                              Hp   =            215.625
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12907847.08                 X    =        -3938579.70
     Y    =       -6073542.32  feet           Y    =        -1895236.38  meter
     Z    =       17061646.59                 Z    =         5181267.49
     XDOT =      15060.852577                 XDOT =        4650.792158
     YDOT =     -19673.052654  feet/sec       YDOT =       -5944.675163  meter/sec
     ZDOT =       4368.055215                 ZDOT =        1353.828369
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10947393.86                 X    =        -3336765.65
     Y    =        9301476.08  feet           Y    =         2835089.91  meter
     Z    =       16977553.64                 Z    =         5174758.35
     XDOT =     -10934.953481                 XDOT =       -3332.973821
     YDOT =     -21067.375932  feet/sec       YDOT =       -6421.336184  meter/sec
     ZDOT =       4468.052497                 ZDOT =        1361.862401
  
  
    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   17148.55058288  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6369 136.2017 0004829 206.2859 153.8049 15.53924932 18694
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17148.55058288   =   yrday.fracday
    Element set:     902
    Inclination:       51.6369  deg
    RA of node:       136.2017  deg
    Eccentricity:     .0004829     
    Arg of perigee:   206.2859  deg
    Mean anomaly:     153.8049  deg
    Mean motion:   15.53924932  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1869
    Checksum:              339
 
 
    Coasting Arc #4 (Orbit 1883)
    ---------------------------------------
 
    Vector Time (GMT): 2017/149/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2777702.97                 A    =         6778045.59  meter
     Y    =        3170979.34  meter          E    =           .0013345
     Z    =       -5318637.98                 I    =           51.89838
     XDOT =      -5268.590960                 Wp   =          113.07523
     YDOT =       5532.251310  meter/sec      RA   =          130.40803  deg
     ZDOT =        542.760100                 TA   =          162.11512
                                              MA   =          162.06811
                                              Ha   =            221.242  n.mi
                                              Hp   =            215.843
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9113198.73                 X    =         2767873.19
     Y    =       10403475.53  feet           Y    =         3201987.16  meter
     Z    =      -17449599.68                 Z    =        -5305168.23
     XDOT =     -17285.403413                 XDOT =       -5332.698939
     YDOT =      18150.430808  feet/sec       YDOT =        5472.975846  meter/sec
     ZDOT =       1780.708991                 ZDOT =         517.011804
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13230201.69                 X    =         4032565.48
     Y    =       -4277626.32  feet           Y    =        -1303820.50  meter
     Z    =      -17390655.53                 Z    =        -5300671.80
     XDOT =       9372.816934                 XDOT =        2856.834601
     YDOT =      22161.495057  feet/sec       YDOT =        6754.823693  meter/sec
     ZDOT =       1666.186567                 ZDOT =         507.853666
  
  
    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   17149.51523002  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6369 131.3945 0004791 210.0722 150.0156 15.53921794 18848
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17149.51523002   =   yrday.fracday
    Element set:     903
    Inclination:       51.6369  deg
    RA of node:       131.3945  deg
    Eccentricity:     .0004791     
    Arg of perigee:   210.0722  deg
    Mean anomaly:     150.0156  deg
    Mean motion:   15.53921794  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1884
    Checksum:              292
 
 
    Coasting Arc #5 (Orbit 1899)
    ---------------------------------------
 
    Vector Time (GMT): 2017/150/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1598457.32                 A    =         6779664.28  meter
     Y    =       -4389435.09  meter          E    =           .0002980
     Z    =        4910705.50                 I    =           51.92452
     XDOT =       5599.210315                 Wp   =           99.28809
     YDOT =      -4680.363084  meter/sec      RA   =          125.43087  deg
     ZDOT =      -2360.226163                 TA   =           13.72719
                                              MA   =           13.71908
                                              Ha   =            221.127  n.mi
                                              Hp   =            215.868
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5244282.55                 X    =        -1573108.51
     Y    =      -14401033.76  feet           Y    =        -4407168.88  meter
     Z    =       16111238.52                 Z    =         4903001.82
     XDOT =      18370.112582                 XDOT =        5662.596040
     YDOT =     -15355.521928  feet/sec       YDOT =       -4617.394276  meter/sec
     ZDOT =      -7743.524156                 ZDOT =       -2332.873437
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15348839.32                 X    =        -4678326.23
     Y    =        -614270.90  feet           Y    =         -187229.77  meter
     Z    =       16077937.75                 Z    =         4900555.43
     XDOT =      -7114.356982                 XDOT =       -2168.456008
     YDOT =     -21796.701782  feet/sec       YDOT =       -6643.634703  meter/sec
     ZDOT =      -7622.037084                 ZDOT =       -2323.196903
  
  
    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   17150.54418471  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6370 126.2668 0004840 215.2593 144.8240 15.53946216 19003
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17150.54418471   =   yrday.fracday
    Element set:     904
    Inclination:       51.6370  deg
    RA of node:       126.2668  deg
    Eccentricity:     .0004840     
    Arg of perigee:   215.2593  deg
    Mean anomaly:     144.8240  deg
    Mean motion:   15.53946216  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1900
    Checksum:              296
 
 
    Coasting Arc #6 (Orbit 1914)
    ---------------------------------------
 
    Vector Time (GMT): 2017/151/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         470419.41                 A    =         6783002.01  meter
     Y    =        5434765.59  meter          E    =           .0006986
     Z    =       -4038903.20                 I    =           51.95459
     XDOT =      -5600.051660                 Wp   =          147.60213
     YDOT =       3422.816012  meter/sec      RA   =          120.46153  deg
     ZDOT =       3950.923403                 TA   =          163.32065
                                              MA   =          163.29767
                                              Ha   =            220.929  n.mi
                                              Hp   =            216.017
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1543370.76                 X    =          429230.49
     Y    =       17830595.77  feet           Y    =         5439796.17  meter
     Z    =      -13250994.74                 Z    =        -4036717.64
     XDOT =     -18372.872900                 XDOT =       -5657.101931
     YDOT =      11229.711327  feet/sec       YDOT =        3359.873131  meter/sec
     ZDOT =      12962.347124                 ZDOT =        3923.581791
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17169773.95                 X    =         5233347.10
     Y    =        5073792.10  feet           Y    =         1546491.83  meter
     Z    =      -13242224.00                 Z    =        -4036229.88
     XDOT =       3985.707990                 XDOT =        1214.843795
     YDOT =      20048.761937  feet/sec       YDOT =        6110.862638  meter/sec
     ZDOT =      12841.095289                 ZDOT =        3913.965844
  
  
    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   17151.50882605  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6379 121.4594 0004732 218.9063 141.1750 15.53932781 19153
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17151.50882605   =   yrday.fracday
    Element set:     905
    Inclination:       51.6379  deg
    RA of node:       121.4594  deg
    Eccentricity:     .0004732     
    Arg of perigee:   218.9063  deg
    Mean anomaly:     141.1750  deg
    Mean motion:   15.53932781  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1915
    Checksum:              308
 
 
    Coasting Arc #7 (Orbit 1930)
    ---------------------------------------
 
    Vector Time (GMT): 2017/152/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         551050.31                 A    =         6786585.62  meter
     Y    =       -6167621.00  meter          E    =           .0011587
     Z    =        2760532.19                 I    =           51.98233
     XDOT =       5358.336285                 Wp   =          120.62719
     YDOT =      -1840.926657  meter/sec      RA   =          115.50272  deg
     ZDOT =      -5172.318829                 TA   =           28.25216
                                              MA   =           28.18936
                                              Ha   =            220.769  n.mi
                                              Hp   =            216.065
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1807907.86                 X    =          606567.98
     Y    =      -20234977.04  feet           Y    =        -6161148.56  meter
     Z    =        9056864.13                 Z    =         2763343.45
     XDOT =      17579.843455                 XDOT =        5403.648403
     YDOT =      -6039.785619  feet/sec       YDOT =       -1780.752401  meter/sec
     ZDOT =     -16969.549963                 ZDOT =       -5146.179708
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18309752.47                 X    =        -5580812.55
     Y    =       -8788208.88  feet           Y    =        -2678646.07  meter
     Z    =        9070279.13                 Z    =         2764621.08
     XDOT =        -38.956446                 XDOT =         -11.873925
     YDOT =     -17348.540670  feet/sec       YDOT =       -5287.835196  meter/sec
     ZDOT =     -16853.850670                 ZDOT =       -5137.053684
  
  
    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   17152.53777331  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6378 116.3312 0004672 223.7280 136.3503 15.53957509 19316
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17152.53777331   =   yrday.fracday
    Element set:     906
    Inclination:       51.6378  deg
    RA of node:       116.3312  deg
    Eccentricity:     .0004672     
    Arg of perigee:   223.7280  deg
    Mean anomaly:     136.3503  deg
    Mean motion:   15.53957509  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1931
    Checksum:              305
 
 
    Coasting Arc #8 (Orbit 1936)
    ---------------------------------------
 
    Vector Time (GMT): 2017/152/21:55:46.000
    Vector Time (MET): N/A
    Weight (LBS)     : 915838.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1604232.45                 A    =         6781712.78  meter
     Y    =        4924157.09  meter          E    =           .0008471
     Z    =       -4386858.90                 I    =           51.97072
     XDOT =      -4975.174440                 Wp   =          143.65391
     YDOT =       4695.086162  meter/sec      RA   =          113.44563  deg
     ZDOT =       3447.524797                 TA   =          161.20574
                                              MA   =          161.17445
                                              Ha   =            220.831  n.mi
                                              Hp   =            216.111
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5263229.84                 X    =         1570359.28
     Y    =       16155371.04  feet           Y    =         4941907.59  meter
     Z    =      -14392581.68                 Z    =        -4379147.96
     XDOT =     -16322.750787                 XDOT =       -5044.052793
     YDOT =      15403.825991  feet/sec       YDOT =        4639.065046  meter/sec
     ZDOT =      11310.776892                 ZDOT =        3423.189875
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14272848.20                 X    =        -4350364.13
     Y    =       -9270333.61  feet           Y    =        -2825597.68  meter
     Z    =      -14359342.89                 Z    =        -4376727.71
     XDOT =       2508.167244                 XDOT =         764.489376
     YDOT =     -21230.425396  feet/sec       YDOT =       -6471.033661  meter/sec
     ZDOT =      11202.572559                 ZDOT =        3414.544116
  
  
    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   17152.92362774  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6367 114.4048 0004926 221.3045 138.7736 15.53959676 19371
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17152.92362774   =   yrday.fracday
    Element set:     907
    Inclination:       51.6367  deg
    RA of node:       114.4048  deg
    Eccentricity:     .0004926     
    Arg of perigee:   221.3045  deg
    Mean anomaly:     138.7736  deg
    Mean motion:   15.53959676  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1937
    Checksum:              335
 
 
    Coasting Arc #9 (Orbit 1945)
    ---------------------------------------
 
    Vector Time (GMT): 2017/153/10:47:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900606.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4573803.28                 A    =         6780298.84  meter
     Y    =        1562746.01  meter          E    =           .0007641
     Z    =        4755189.05                 I    =           51.97319
     XDOT =        422.056063                 Wp   =          153.95240
     YDOT =      -7146.134679  meter/sec      RA   =          110.83753  deg
     ZDOT =       2746.111572                 TA   =          268.95947
                                              MA   =          269.04701
                                              Ha   =            220.686  n.mi
                                              Hp   =            216.187
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15005916.28                 X    =        -4614036.86
     Y    =        5127119.45  feet           Y    =         1511373.39  meter
     Z    =       15601013.94                 Z    =         4732873.20
     XDOT =       1384.698369                 XDOT =         488.595323
     YDOT =     -23445.323751  feet/sec       YDOT =       -7141.043089  meter/sec
     ZDOT =       9009.552402                 ZDOT =        2748.322972
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5263636.48                 X    =        -1604356.40
     Y    =       15060925.39  feet           Y    =         4590570.06  meter
     Z    =       15502231.15                 Z    =         4725080.05
     XDOT =     -16556.044605                 XDOT =       -5046.282396
     YDOT =     -15099.351537  feet/sec       YDOT =       -4602.282348  meter/sec
     ZDOT =       9020.489680                 ZDOT =        2749.445254
  
  
    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   17153.50240790  .00016717  00000-0  10270-3 0  9089
    2 25544  51.6371 111.5242 0004847 227.5420 132.5323 15.53978450 19462
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17153.50240790   =   yrday.fracday
    Element set:     908
    Inclination:       51.6371  deg
    RA of node:       111.5242  deg
    Eccentricity:     .0004847     
    Arg of perigee:   227.5420  deg
    Mean anomaly:     132.5323  deg
    Mean motion:   15.53978450  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1946
    Checksum:              295
 
 
    Coasting Arc #10 (Orbit 1946)
    ---------------------------------------
 
    Vector Time (GMT): 2017/153/13:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900606.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4299567.34                 A    =         6778289.10  meter
     Y    =         203656.36  meter          E    =           .0010533
     Z    =       -5245025.55                 I    =           51.96916
     XDOT =      -1761.058046                 Wp   =           95.42072
     YDOT =       7364.677590  meter/sec      RA   =          110.33346  deg
     ZDOT =      -1160.620341                 TA   =          163.50704
                                              MA   =          163.47274
                                              Ha   =            220.648  n.mi
                                              Hp   =            216.326
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14106192.06                 X    =         4322448.33
     Y    =         668163.91  feet           Y    =          251865.29  meter
     Z    =      -17208089.07                 Z    =        -5224083.89
     XDOT =      -5777.749494                 XDOT =       -1837.643165
     YDOT =      24162.328050  feet/sec       YDOT =        7344.556104  meter/sec
     ZDOT =      -3807.809517                 ZDOT =       -1169.360619
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1203739.03                 X    =          366899.66
     Y    =      -14182895.15  feet           Y    =        -4322946.44  meter
     Z    =      -17115663.12                 Z    =        -5216854.12
     XDOT =      22892.971840                 XDOT =        6977.777817
     YDOT =       6574.403689  feet/sec       YDOT =        2003.878244  meter/sec
     ZDOT =      -3847.609696                 ZDOT =       -1172.751435
  
  
    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   17153.56671801  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6387 111.2033 0004725 227.8497 132.2255 15.53963408 19475
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17153.56671801   =   yrday.fracday
    Element set:     909
    Inclination:       51.6387  deg
    RA of node:       111.2033  deg
    Eccentricity:     .0004725     
    Arg of perigee:   227.8497  deg
    Mean anomaly:     132.2255  deg
    Mean motion:   15.53963408  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1947
    Checksum:              316
 
 
    Coasting Arc #11 (Orbit 1962)
    ---------------------------------------
 
    Vector Time (GMT): 2017/154/13:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900606.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3784841.33                 A    =         6777933.76  meter
     Y    =       -1873068.02  meter          E    =           .0001858
     Z    =        5302409.19                 I    =           51.97931
     XDOT =       2557.340529                 Wp   =          216.93782
     YDOT =      -7193.280997  meter/sec      RA   =          105.35913  deg
     ZDOT =       -717.169850                 TA   =          239.87134
                                              MA   =          239.88976
                                              Ha   =            220.522  n.mi
                                              Hp   =            216.291
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12417458.42                 X    =        -3789371.60
     Y    =       -6145236.28  feet           Y    =        -1915418.34  meter
     Z    =       17396355.61                 Z    =         5284012.34
     XDOT =       8390.224834                 XDOT =        2641.071304
     YDOT =     -23600.003270  feet/sec       YDOT =       -7164.214870  meter/sec
     ZDOT =      -2352.919454                 ZDOT =        -704.544060
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6400701.11                 X    =        -1950933.70
     Y    =       12401490.79  feet           Y    =         3779974.39  meter
     Z    =       17315439.43                 Z    =         5277745.94
     XDOT =     -22517.591469                 XDOT =       -6863.361880
     YDOT =      -8423.377223  feet/sec       YDOT =       -2567.445378  meter/sec
     ZDOT =      -2295.975984                 ZDOT =        -699.813480
  
  
    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   17154.59565808  .00016717  00000-0  10270-3 0  9102
    2 25544  51.6394 106.0760 0004789 233.4536 126.6176 15.53982864 19633
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17154.59565808   =   yrday.fracday
    Element set:     910
    Inclination:       51.6394  deg
    RA of node:       106.0760  deg
    Eccentricity:     .0004789     
    Arg of perigee:   233.4536  deg
    Mean anomaly:     126.6176  deg
    Mean motion:   15.53982864  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1963
    Checksum:              339
 
 
    Coasting Arc #12 (Orbit 1977)
    ---------------------------------------
 
    Vector Time (GMT): 2017/155/13:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900606.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3216964.32                 A    =         6779884.46  meter
     Y    =        3485419.14  meter          E    =           .0009441
     Z    =       -4853179.77                 I    =           51.99362
     XDOT =      -3200.015124                 Wp   =          130.65924
     YDOT =       6483.276131  meter/sec      RA   =          100.38573  deg
     ZDOT =       2532.193758                 TA   =          164.15900
                                              MA   =          164.12945
                                              Ha   =            220.296  n.mi
                                              Hp   =            216.433
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10554344.88                 X    =         3201324.98
     Y    =       11435102.17  feet           Y    =         3521306.31  meter
     Z    =      -15922505.81                 Z    =        -4837590.33
     XDOT =     -10498.737283                 XDOT =       -3284.575273
     YDOT =      21270.590980  feet/sec       YDOT =        6447.018411  meter/sec
     ZDOT =       8307.722304                 ZDOT =        2516.443978
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11470003.61                 X    =         3496057.10
     Y    =      -10619014.11  feet           Y    =        -3236675.50  meter
     Z    =      -15854258.27                 Z    =        -4832377.92
     XDOT =      20460.829276                 XDOT =        6236.460763
     YDOT =       9788.908911  feet/sec       YDOT =        2983.659436  meter/sec
     ZDOT =       8237.086298                 ZDOT =        2510.663904
  
  
    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   17155.56028628  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6396 101.2676 0004645 236.3230 123.7480 15.53977566 19787
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17155.56028628   =   yrday.fracday
    Element set:     911
    Inclination:       51.6396  deg
    RA of node:       101.2676  deg
    Eccentricity:     .0004645     
    Arg of perigee:   236.3230  deg
    Mean anomaly:     123.7480  deg
    Mean motion:   15.53977566  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1978
    Checksum:              326
 
 
    Coasting Arc #13 (Orbit 1978)
    ---------------------------------------
 
    Vector Time (GMT): 2017/155/13:34:21.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3076852.59                 A    =         6786921.78  meter
     Y    =        5446303.12  meter          E    =           .0009412
     Z    =        2624221.58                 I    =           52.01726
     XDOT =      -3366.036505                 Wp   =           86.97518
     YDOT =      -4445.160146  meter/sec      RA   =          100.34329  deg
     ZDOT =       5263.118474                 TA   =          302.41861
                                              MA   =          302.50962
                                              Ha   =            220.325  n.mi
                                              Hp   =            216.365
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10094660.72                 X    =        -3150273.22
     Y    =       17868448.56  feet           Y    =         5411484.97  meter
     Z    =        8609650.85                 Z    =         2609097.08
     XDOT =     -11043.426853                 XDOT =       -3341.645310
     YDOT =     -14583.858748  feet/sec       YDOT =       -4482.665439  meter/sec
     ZDOT =      17267.449061                 ZDOT =        5246.826063
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18819204.96                 X    =         5736093.67
     Y    =        8257258.95  feet           Y    =         2516812.53  meter
     Z    =        8541950.36                 Z    =         2603586.47
     XDOT =     -12754.314313                 XDOT =       -3887.515003
     YDOT =      11225.503170  feet/sec       YDOT =        3421.533366  meter/sec
     ZDOT =      17196.259350                 ZDOT =        5241.419850
  
  
    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   17155.62459499  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6397 100.9474 0004641 236.5206 123.5503 15.53969023 19795
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17155.62459499   =   yrday.fracday
    Element set:     912
    Inclination:       51.6397  deg
    RA of node:       100.9474  deg
    Eccentricity:     .0004641     
    Arg of perigee:   236.5206  deg
    Mean anomaly:     123.5503  deg
    Mean motion:   15.53969023  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1979
    Checksum:              326
 
 
    Coasting Arc #14 (Orbit 1993)
    ---------------------------------------
 
    Vector Time (GMT): 2017/156/13:34:21.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3495260.65                 A    =         6783217.31  meter
     Y    =       -4274415.17  meter          E    =           .0002307
     Z    =       -3941717.34                 I    =           52.01090
     XDOT =       2643.545198                 Wp   =          101.18874
     YDOT =       5923.957505  meter/sec      RA   =           95.38864  deg
     ZDOT =      -4082.292941                 TA   =          126.30592
                                              MA   =          126.28461
                                              Ha   =            220.210  n.mi
                                              Hp   =            216.465
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11467390.58                 X    =         3561945.68
     Y    =      -14023671.82  feet           Y    =        -4234955.61  meter
     Z    =      -12932143.50                 Z    =        -3924576.62
     XDOT =       8673.048551                 XDOT =        2596.935505
     YDOT =      19435.556119  feet/sec       YDOT =        5953.259150  meter/sec
     ZDOT =     -13393.349544                 ZDOT =       -4069.563966
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15310025.40                 X    =        -4666495.74
     Y    =       -9784590.99  feet           Y    =        -2982343.33  meter
     Z    =      -12855724.61                 Z    =        -3918424.86
     XDOT =      17528.783098                 XDOT =        5342.773088
     YDOT =      -9913.398578  feet/sec       YDOT =       -3021.603886  meter/sec
     ZDOT =     -13338.155728                 ZDOT =       -4065.469866
  
  
    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   17156.58921983  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6406  96.1403 0004633 240.6825 119.3865 15.53992189 19948
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17156.58921983   =   yrday.fracday
    Element set:     913
    Inclination:       51.6406  deg
    RA of node:        96.1403  deg
    Eccentricity:     .0004633     
    Arg of perigee:   240.6825  deg
    Mean anomaly:     119.3865  deg
    Mean motion:   15.53992189  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1994
    Checksum:              338
 
 
    Coasting Arc #15 (Orbit 1997)
    ---------------------------------------
 
    Vector Time (GMT): 2017/156/18:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1532447.34                 A    =         6789003.70  meter
     Y    =        6472525.31  meter          E    =           .0008869
     Z    =        1338033.28                 I    =           52.02805
     XDOT =      -4410.234654                 Wp   =           59.05647
     YDOT =      -2258.735517  meter/sec      RA   =           94.28692  deg
     ZDOT =       5851.060957                 TA   =          315.43118
                                              MA   =          315.50246
                                              Ha   =            220.122  n.mi
                                              Hp   =            216.518
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5027714.38                 X    =        -1611210.52
     Y    =       21235319.25  feet           Y    =         6454947.94  meter
     Z    =        4389872.97                 Z    =         1330398.29
     XDOT =     -14469.273800                 XDOT =       -4413.071054
     YDOT =      -7410.549597  feet/sec       YDOT =       -2308.070119  meter/sec
     ZDOT =      19196.394215                 ZDOT =        5829.630037
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6517015.93                 X    =         1986386.46
     Y    =      -20833860.35  feet           Y    =        -6350160.63  meter
     Z    =        4355048.39                 Z    =         1327418.75
     XDOT =      12526.077670                 XDOT =        3817.948474
     YDOT =       7928.041498  feet/sec       YDOT =        2416.467049  meter/sec
     ZDOT =      19102.148968                 ZDOT =        5822.335006
  
  
    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   17156.84645078  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6378  94.8564 0004930 241.0910 118.9748 15.53983973 19989
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17156.84645078   =   yrday.fracday
    Element set:     914
    Inclination:       51.6378  deg
    RA of node:        94.8564  deg
    Eccentricity:     .0004930     
    Arg of perigee:   241.0910  deg
    Mean anomaly:     118.9748  deg
    Mean motion:   15.53983973  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1998
    Checksum:              357
 
 
    Coasting Arc #16 (Orbit 2012)
    ---------------------------------------
 
    Vector Time (GMT): 2017/157/18:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2183051.30                 A    =         6786233.72  meter
     Y    =       -5740583.97  meter          E    =           .0004113
     Z    =       -2880928.65                 I    =           52.02066
     XDOT =       4022.528938                 Wp   =          183.81990
     YDOT =       4083.207741  meter/sec      RA   =           89.33876  deg
     ZDOT =      -5091.728014                 TA   =           28.78026
                                              MA   =           28.75757
                                              Ha   =            220.012  n.mi
                                              Hp   =            216.567
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7162241.79                 X    =         2261076.09
     Y    =      -18833936.91  feet           Y    =        -5715735.05  meter
     Z    =       -9451865.65                 Z    =        -2870135.00
     XDOT =      13197.273419                 XDOT =        4001.303925
     YDOT =      13396.350856  feet/sec       YDOT =        4128.072237  meter/sec
     ZDOT =     -16705.144402                 ZDOT =       -5072.238676
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8196966.10                 X    =        -2498435.27
     Y    =       18432096.61  feet           Y    =         5618103.05  meter
     Z    =       -9403202.25                 Z    =        -2866096.05
     XDOT =     -11244.791324                 XDOT =       -3427.412396
     YDOT =     -13473.325084  feet/sec       YDOT =       -4106.669485  meter/sec
     ZDOT =     -16619.792794                 ZDOT =       -5065.712844
  
  
    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   17157.81107198  .00016717  00000-0  10270-3 0  9159
    2 25544  51.6381  90.0483 0004837 245.6418 114.4230 15.53994713 20130
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17157.81107198   =   yrday.fracday
    Element set:     915
    Inclination:       51.6381  deg
    RA of node:        90.0483  deg
    Eccentricity:     .0004837     
    Arg of perigee:   245.6418  deg
    Mean anomaly:     114.4230  deg
    Mean motion:   15.53994713  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2013
    Checksum:              303
 
 
    Coasting Arc #17 (Orbit 2028)
    ---------------------------------------
 
    Vector Time (GMT): 2017/158/18:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2785278.72                 A    =         6782545.62  meter
     Y    =        4604995.12  meter          E    =           .0007040
     Z    =        4125978.36                 I    =           52.00706
     XDOT =      -3562.791699                 Wp   =          126.75575
     YDOT =      -5600.840577  meter/sec      RA   =           84.38146  deg
     ZDOT =       3837.376415                 TA   =          283.78065
                                              MA   =          283.85898
                                              Ha   =            219.864  n.mi
                                              Hp   =            216.597
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9138053.53                 X    =        -2856608.21
     Y    =       15108251.70  feet           Y    =         4573448.92  meter
     Z    =       13536674.40                 Z    =         4112275.46
     XDOT =     -11688.949144                 XDOT =       -3518.537169
     YDOT =     -18375.461210  feet/sec       YDOT =       -5640.435145  meter/sec
     ZDOT =      12589.817633                 ZDOT =        3820.176065
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9749518.43                 X    =         2971653.22
     Y    =      -14777237.44  feet           Y    =        -4504101.97  meter
     Z    =       13475347.47                 Z    =         4107285.91
     XDOT =      10042.956506                 XDOT =        3061.093143
     YDOT =      18064.169694  feet/sec       YDOT =        5505.958923  meter/sec
     ZDOT =      12514.849623                 ZDOT =        3814.526165
  
  
    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   17158.83999600  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6381  84.9195 0004941 248.9173 111.1451 15.54001951 20292
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17158.83999600   =   yrday.fracday
    Element set:     916
    Inclination:       51.6381  deg
    RA of node:        84.9195  deg
    Eccentricity:     .0004941     
    Arg of perigee:   248.9173  deg
    Mean anomaly:     111.1451  deg
    Mean motion:   15.54001951  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2029
    Checksum:              316
 
 
    Coasting Arc #18 (Orbit 2043)
    ---------------------------------------
 
    Vector Time (GMT): 2017/159/18:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3372174.45                 A    =         6779289.84  meter
     Y    =       -3140303.69  meter          E    =           .0007729
     Z    =       -4979571.35                 I    =           51.99167
     XDOT =       2998.165166                 Wp   =           76.36198
     YDOT =       6700.337583  meter/sec      RA   =           79.41532  deg
     ZDOT =      -2196.200754                 TA   =          172.31111
                                              MA   =          172.29926
                                              Ha   =            219.861  n.mi
                                              Hp   =            216.628
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11063564.46                 X    =         3431228.11
     Y    =      -10302833.64  feet           Y    =        -3102262.90  meter
     Z    =      -16337176.34                 Z    =        -4963047.17
     XDOT =       9836.499887                 XDOT =        2933.685589
     YDOT =      21982.734854  feet/sec       YDOT =        6733.504863  meter/sec
     ZDOT =      -7205.383051                 ZDOT =       -2181.792147
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11351773.11                 X    =        -3460020.45
     Y    =       10103736.10  feet           Y    =         3079618.76  meter
     Z    =      -16263638.40                 Z    =        -4957156.99
     XDOT =      -8753.540216                 XDOT =       -2668.079058
     YDOT =     -21326.832334  feet/sec       YDOT =       -6500.418495  meter/sec
     ZDOT =      -7142.951926                 ZDOT =       -2177.171747
  
  
    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   17159.80461051  .00016717  00000-0  10270-3 0  9173
    2 25544  51.6377  80.1122 0004701 250.1709 109.8937 15.54002244 20445
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17159.80461051   =   yrday.fracday
    Element set:     917
    Inclination:       51.6377  deg
    RA of node:        80.1122  deg
    Eccentricity:     .0004701     
    Arg of perigee:   250.1709  deg
    Mean anomaly:     109.8937  deg
    Mean motion:   15.54002244  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2044
    Checksum:              282
 
 
    Coasting Arc #19 (Orbit 2048)
    ---------------------------------------
 
    Vector Time (GMT): 2017/160/01:48:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3518509.29                 A    =         6778609.33  meter
     Y    =        2706084.80  meter          E    =           .0004622
     Z    =        5124766.31                 I    =           51.99162
     XDOT =      -2834.072264                 Wp   =          186.46771
     YDOT =      -6917.433595  meter/sec      RA   =           77.97410  deg
     ZDOT =       1702.577101                 TA   =          247.13780
                                              MA   =          247.18661
                                              Ha   =            219.804  n.mi
                                              Hp   =            216.610
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11543665.65                 X    =        -3573401.80
     Y    =        8878230.98  feet           Y    =         2666430.83  meter
     Z    =       16813537.75                 Z    =         5107541.34
     XDOT =      -9298.137350                 XDOT =       -2764.779445
     YDOT =     -22694.992110  feet/sec       YDOT =       -6948.738903  meter/sec
     ZDOT =       5585.882876                 ZDOT =        1688.977264
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11397591.53                 X    =        -3473985.90
     Y    =       -9205577.80  feet           Y    =        -2805860.11  meter
     Z    =       16736979.97                 Z    =         5101431.49
     XDOT =      19150.215507                 XDOT =        5836.985687
     YDOT =     -13635.384516  feet/sec       YDOT =       -4156.065201  meter/sec
     ZDOT =       5527.066452                 ZDOT =        1684.649855
  
  
    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   17160.12614616  .00016717  00000-0  10270-3 0  9188
    2 25544  51.6415  78.5113 0005020 251.0422 109.0187 15.54019416 20499
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17160.12614616   =   yrday.fracday
    Element set:     918
    Inclination:       51.6415  deg
    RA of node:        78.5113  deg
    Eccentricity:     .0005020     
    Arg of perigee:   251.0422  deg
    Mean anomaly:     109.0187  deg
    Mean motion:   15.54019416  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2049
    Checksum:              271
 
 
    Coasting Arc #20 (Orbit 2063)
    ---------------------------------------
 
    Vector Time (GMT): 2017/161/01:48:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 923344.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4054689.62                 A    =         6777770.90  meter
     Y    =       -1024012.36  meter          E    =           .0010141
     Z    =       -5342426.53                 I    =           51.98036
     XDOT =       2102.288319                 Wp   =           99.08916
     YDOT =       7364.701735  meter/sec      RA   =           72.99995  deg
     ZDOT =        182.657335                 TA   =          172.65257
                                              MA   =          172.63770
                                              Ha   =            219.629  n.mi
                                              Hp   =            216.834
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13302787.47                 X    =         4091790.13
     Y    =       -3359620.59  feet           Y    =         -978461.86  meter
     Z    =      -17527646.09                 Z    =        -5322639.98
     XDOT =       6897.271388                 XDOT =        2018.890779
     YDOT =      24162.407266  feet/sec       YDOT =        7387.744616  meter/sec
     ZDOT =        599.269472                 ZDOT =         192.668187
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6666692.50                 X    =         2032007.87
     Y    =       12118938.48  feet           Y    =         3693852.45  meter
     Z    =      -17440072.36                 Z    =        -5315734.05
     XDOT =     -20727.170912                 XDOT =       -6317.641694
     YDOT =      12332.209205  feet/sec       YDOT =        3758.857366  meter/sec
     ZDOT =        642.140600                 ZDOT =         195.724455
  
  
    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   17161.09075509  .00016717  00000-0  10270-3 0  9198
    2 25544  51.6411  73.7041 0004996 255.7990 104.2608 15.53989585 20648
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17161.09075509   =   yrday.fracday
    Element set:     919
    Inclination:       51.6411  deg
    RA of node:        73.7041  deg
    Eccentricity:     .0004996     
    Arg of perigee:   255.7990  deg
    Mean anomaly:     104.2608  deg
    Mean motion:   15.53989585  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2064
    Checksum:              330
 
             

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