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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15282.6
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   69.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.031
   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 
   ------------------------------------------------------------------------
   118/11:34:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.0  
   000/00:00:00.000           0.0               0.0              217.5  
   
   120/08:22:21.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.8  
   000/00:00:00.000           0.0               0.0              217.5  
   
   122/11:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              217.4  
   
   128/05:34:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.0  
   000/00:00:00.000           0.0               0.0              217.2  
   
 
 
    Coasting Arc #1 (Orbit 690)
    ---------------------------------------
 
    Vector Time (GMT): 2019/114/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -194688.15                 A    =         6793557.72  meter
     Y    =        6753216.68  meter          E    =           .0010819
     Z    =        -658224.78                 I    =           51.27355
     XDOT =      -4800.139863                 Wp   =          146.09283
     YDOT =       -711.367936  meter/sec      RA   =          267.17033  deg
     ZDOT =      -5934.797548                 TA   =           41.04729
                                              MA   =           40.96593
                                              Ha   =            223.082  n.mi
                                              Hp   =            217.351
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -638740.65                 X    =         -266992.75
     Y    =       22156222.70  feet           Y    =         6750635.28  meter
     Z    =       -2159530.11                 Z    =         -659345.91
     XDOT =     -15748.490363                 XDOT =       -4763.000212
     YDOT =      -2333.884303  feet/sec       YDOT =        -764.838611  meter/sec
     ZDOT =     -19471.120565                 ZDOT =       -5958.024829
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10991679.44                 X    =         3350263.89
     Y    =       19247453.02  feet           Y    =         5866623.68  meter
     Z    =       -2165248.06                 Z    =         -659967.61
     XDOT =     -13149.657214                 XDOT =       -4008.015519
     YDOT =       5327.844276  feet/sec       YDOT =        1623.926935  meter/sec
     ZDOT =     -19576.046209                 ZDOT =       -5966.778885
  
  
    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   19114.53094369  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6379 267.9101 0001239 224.3021 135.8031 15.52611347  6910
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19114.53094369   =   yrday.fracday
    Element set:     900
    Inclination:       51.6379  deg
    RA of node:       267.9101  deg
    Eccentricity:     .0001239     
    Arg of perigee:   224.3021  deg
    Mean anomaly:     135.8031  deg
    Mean motion:   15.52611347  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             691
    Checksum:              286
 
 
    Coasting Arc #2 (Orbit 706)
    ---------------------------------------
 
    Vector Time (GMT): 2019/115/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         572255.36                 A    =         6792344.40  meter
     Y    =       -6515160.31  meter          E    =           .0012602
     Z    =        1812237.59                 I    =           51.27308
     XDOT =       4821.276460                 Wp   =           68.61631
     YDOT =       1993.710647  meter/sec      RA   =          262.18109  deg
     ZDOT =       5618.026139                 TA   =          311.39981
                                              MA   =          311.50806
                                              Ha   =            223.057  n.mi
                                              Hp   =            217.393
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1877478.23                 X    =          636264.32
     Y    =      -21375197.85  feet           Y    =        -6508403.10  meter
     Z    =        5945661.40                 Z    =         1815172.70
     XDOT =      15817.836154                 XDOT =        4771.334513
     YDOT =       6541.045429  feet/sec       YDOT =        2047.346137  meter/sec
     ZDOT =      18431.844287                 ZDOT =        5641.324960
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9878061.01                 X    =        -3010832.99
     Y    =      -19044228.98  feet           Y    =        -5804680.99  meter
     Z    =        5959542.80                 Z    =         1816468.65
     XDOT =      15371.232053                 XDOT =        4685.151530
     YDOT =      -2144.326396  feet/sec       YDOT =        -653.590685  meter/sec
     ZDOT =      18536.981203                 ZDOT =        5650.071871
  
  
    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   19115.56079898  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6387 262.7887 0001478 222.2954 137.8084 15.52613222  7072
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19115.56079898   =   yrday.fracday
    Element set:     901
    Inclination:       51.6387  deg
    RA of node:       262.7887  deg
    Eccentricity:     .0001478     
    Arg of perigee:   222.2954  deg
    Mean anomaly:     137.8084  deg
    Mean motion:   15.52613222  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             707
    Checksum:              333
 
 
    Coasting Arc #3 (Orbit 721)
    ---------------------------------------
 
    Vector Time (GMT): 2019/116/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1012074.28                 A    =         6790193.74  meter
     Y    =        6053199.90  meter          E    =           .0004185
     Z    =       -2904360.40                 I    =           51.27174
     XDOT =      -4841.151634                 Wp   =          132.02093
     YDOT =      -3204.964122  meter/sec      RA   =          257.18806  deg
     ZDOT =      -5000.136195                 TA   =           81.23087
                                              MA   =           81.18348
                                              Ha   =            223.034  n.mi
                                              Hp   =            217.424
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3320453.68                 X    =        -1065579.86
     Y    =       19859579.71  feet           Y    =         6041583.06  meter
     Z    =       -9528741.46                 Z    =        -2909406.53
     XDOT =     -15883.043419                 XDOT =       -4780.665059
     YDOT =     -10514.974152  feet/sec       YDOT =       -3258.762973  meter/sec
     ZDOT =     -16404.646309                 ZDOT =       -5023.505908
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8185867.26                 X    =         2495052.34
     Y    =       18384069.46  feet           Y    =         5603464.37  meter
     Z    =       -9552109.71                 Z    =        -2911483.04
     XDOT =     -17616.002313                 XDOT =       -5369.357505
     YDOT =       -721.904512  feet/sec       YDOT =        -220.036495  meter/sec
     ZDOT =     -16510.004601                 ZDOT =       -5032.249402
  
  
    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   19116.52628668  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6390 257.9866 0001355 230.6680 129.4352 15.52597734  7223
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19116.52628668   =   yrday.fracday
    Element set:     902
    Inclination:       51.6390  deg
    RA of node:       257.9866  deg
    Eccentricity:     .0001355     
    Arg of perigee:   230.6680  deg
    Mean anomaly:     129.4352  deg
    Mean motion:   15.52597734  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             722
    Checksum:              327
 
 
    Coasting Arc #4 (Orbit 737)
    ---------------------------------------
 
    Vector Time (GMT): 2019/117/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1480187.19                 A    =         6787501.63  meter
     Y    =       -5407221.21  meter          E    =           .0010428
     Z    =        3819480.03                 I    =           51.27213
     XDOT =       4852.360304                 Wp   =          102.93642
     YDOT =       4258.643749  meter/sec      RA   =          252.19097  deg
     ZDOT =       4136.609324                 TA   =          303.26156
                                              MA   =          303.36144
                                              Ha   =            222.945  n.mi
                                              Hp   =            217.429
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4856257.18                 X    =         1521989.31
     Y    =      -17740227.07  feet           Y    =        -5390435.02  meter
     Z    =       12531102.46                 Z    =         3826771.73
     XDOT =      15919.817271                 XDOT =        4784.284910
     YDOT =      13971.928310  feet/sec       YDOT =        4312.525575  meter/sec
     ZDOT =      13571.552900                 ZDOT =        4160.015007
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6054386.28                 X    =        -1845376.94
     Y    =      -17343697.74  feet           Y    =        -5286359.07  meter
     Z    =       12564552.30                 Z    =         3829675.54
     XDOT =      19685.257281                 XDOT =        6000.066419
     YDOT =       3064.577176  feet/sec       YDOT =         934.083123  meter/sec
     ZDOT =      13676.994925                 ZDOT =        4168.748053
  
  
    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   19117.55613511  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6397 252.8646 0001363 235.1841 124.9183 15.52622377  7389
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19117.55613511   =   yrday.fracday
    Element set:     903
    Inclination:       51.6397  deg
    RA of node:       252.8646  deg
    Eccentricity:     .0001363     
    Arg of perigee:   235.1841  deg
    Mean anomaly:     124.9183  deg
    Mean motion:   15.52622377  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             738
    Checksum:              309
 
 
    Coasting Arc #5 (Orbit 752)
    ---------------------------------------
 
    Vector Time (GMT): 2019/118/11:34:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4516387.05                 A    =         6788927.71  meter
     Y    =        3773424.89  meter          E    =           .0011401
     Z    =        3373495.42                 I    =           51.28638
     XDOT =      -1511.999843                 Wp   =           94.06316
     YDOT =       5940.429616  meter/sec      RA   =          247.23032  deg
     ZDOT =      -4607.717981                 TA   =           46.34324
                                              MA   =           46.24878
                                              Ha   =            222.976  n.mi
                                              Hp   =            217.455
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14817542.82                 X    =         4457469.27
     Y    =       12380002.91  feet           Y    =         3823600.87  meter
     Z    =       11067898.36                 Z    =         3395291.27
     XDOT =      -4960.629407                 XDOT =       -1555.933250
     YDOT =      19489.598477  feet/sec       YDOT =        5923.275709  meter/sec
     ZDOT =     -15117.184978                 ZDOT =       -4615.169458
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18889976.36                 X    =         5757664.79
     Y    =        3716040.49  feet           Y    =         1132649.14  meter
     Z    =       11166120.98                 Z    =         3403433.67
     XDOT =       5433.156662                 XDOT =        1656.026150
     YDOT =      18033.054249  feet/sec       YDOT =        5496.474935  meter/sec
     ZDOT =     -15151.392386                 ZDOT =       -4618.144399
  
  
    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   19118.52161846  .00016717  00000-0  10270-3 0  9044
    2 25544  51.6384 248.0630 0001284 235.0771 125.0260 15.52580892  7538
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19118.52161846   =   yrday.fracday
    Element set:     904
    Inclination:       51.6384  deg
    RA of node:       248.0630  deg
    Eccentricity:     .0001284     
    Arg of perigee:   235.0771  deg
    Mean anomaly:     125.0260  deg
    Mean motion:   15.52580892  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             753
    Checksum:              296
 
 
    Coasting Arc #6 (Orbit 767)
    ---------------------------------------
 
    Vector Time (GMT): 2019/119/11:34:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4510491.51                 A    =         6791329.00  meter
     Y    =       -4486074.50  meter          E    =           .0004372
     Z    =       -2374404.44                 I    =           51.30966
     XDOT =       2192.368284                 Wp   =           41.63808
     YDOT =      -5030.236829  meter/sec      RA   =          242.23727  deg
     ZDOT =       5348.070424                 TA   =          291.74652
                                              MA   =          291.79304
                                              Ha   =            222.961  n.mi
                                              Hp   =            217.445
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14798200.49                 X    =        -4448458.13
     Y    =      -14718092.19  feet           Y    =        -4536167.16  meter
     Z    =       -7790040.82                 Z    =        -2396164.08
     XDOT =       7192.809332                 XDOT =        2222.476816
     YDOT =     -16503.401671  feet/sec       YDOT =       -5005.551808  meter/sec
     ZDOT =      17546.162807                 ZDOT =        5358.793372
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20118032.79                 X    =        -6131976.39
     Y    =       -5416369.68  feet           Y    =        -1650909.48  meter
     Z    =       -7888054.74                 Z    =        -2404279.09
     XDOT =      -2481.238700                 XDOT =        -756.281556
     YDOT =     -16366.293586  feet/sec       YDOT =       -4988.446285  meter/sec
     ZDOT =      17595.074368                 ZDOT =        5362.978667
  
  
    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   19119.48709702  .00016717  00000-0  10270-3 0  9050
    2 25544  51.6396 243.2613 0001281 245.5208 114.5811 15.52599091  7689
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19119.48709702   =   yrday.fracday
    Element set:     905
    Inclination:       51.6396  deg
    RA of node:       243.2613  deg
    Eccentricity:     .0001281     
    Arg of perigee:   245.5208  deg
    Mean anomaly:     114.5811  deg
    Mean motion:   15.52599091  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             768
    Checksum:              313
 
 
    Coasting Arc #7 (Orbit 781)
    ---------------------------------------
 
    Vector Time (GMT): 2019/120/08:22:21.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5067750.28                 A    =         6788805.84  meter
     Y    =        2985346.76  meter          E    =           .0011097
     Z    =        3380317.68                 I    =           51.31326
     XDOT =       -519.670988                 Wp   =           91.18133
     YDOT =       6110.001028  meter/sec      RA   =          237.90294  deg
     ZDOT =      -4604.086228                 TA   =           49.14910
                                              MA   =           49.05296
                                              Ha   =            222.809  n.mi
                                              Hp   =            217.499
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16626477.29                 X    =         5017570.82
     Y    =        9794444.77  feet           Y    =         3041737.40  meter
     Z    =       11090281.11                 Z    =         3404813.14
     XDOT =      -1704.957310                 XDOT =        -565.591895
     YDOT =      20045.935132  feet/sec       YDOT =        6103.932849  meter/sec
     ZDOT =     -15105.269777                 ZDOT =       -4606.722271
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12889045.90                 X    =         3928581.19
     Y    =       14275143.09  feet           Y    =         4351063.61  meter
     Z    =       11200804.26                 Z    =         3414005.14
     XDOT =      -6452.475007                 XDOT =       -1966.714382
     YDOT =      17720.751542  feet/sec       YDOT =        5401.285070  meter/sec
     ZDOT =     -15117.694339                 ZDOT =       -4607.873234
  
  
    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   19120.38820622  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6373 238.7797 0001321 262.0724  98.0278 15.52612381  7825
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19120.38820622   =   yrday.fracday
    Element set:     906
    Inclination:       51.6373  deg
    RA of node:       238.7797  deg
    Eccentricity:     .0001321     
    Arg of perigee:   262.0724  deg
    Mean anomaly:      98.0278  deg
    Mean motion:   15.52612381  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             782
    Checksum:              306
 
 
    Coasting Arc #8 (Orbit 796)
    ---------------------------------------
 
    Vector Time (GMT): 2019/121/08:22:21.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5177624.58                 A    =         6791254.61  meter
     Y    =       -3692726.36  meter          E    =           .0004688
     Z    =       -2379169.05                 I    =           51.34061
     XDOT =       1341.424669                 Wp   =           40.68519
     YDOT =      -5320.650976  meter/sec      RA   =          232.91132  deg
     ZDOT =       5348.429487                 TA   =          292.65337
                                              MA   =          292.70294
                                              Ha   =            222.968  n.mi
                                              Hp   =            217.357
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16986957.29                 X    =        -5124389.86
     Y    =      -12115243.95  feet           Y    =        -3750328.58  meter
     Z    =       -7805672.75                 Z    =        -2404190.88
     XDOT =       4400.999570                 XDOT =        1374.842048
     YDOT =     -17456.203991  feet/sec       YDOT =       -5305.463257  meter/sec
     ZDOT =      17547.340838                 ZDOT =        5355.026976
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12847724.47                 X    =        -3915986.42
     Y    =      -16385884.35  feet           Y    =        -4994417.55  meter
     Z    =       -7918532.13                 Z    =        -2413568.59
     XDOT =       7820.408650                 XDOT =        2383.660556
     YDOT =     -14611.421977  feet/sec       YDOT =       -4453.561419  meter/sec
     ZDOT =      17577.605921                 ZDOT =        5357.654285
  
  
    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   19121.35367953  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6378 233.9773 0001038 258.5061 101.5974 15.52618095  7977
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19121.35367953   =   yrday.fracday
    Element set:     907
    Inclination:       51.6378  deg
    RA of node:       233.9773  deg
    Eccentricity:     .0001038     
    Arg of perigee:   258.5061  deg
    Mean anomaly:     101.5974  deg
    Mean motion:   15.52618095  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             797
    Checksum:              330
 
 
    Coasting Arc #9 (Orbit 812)
    ---------------------------------------
 
    Vector Time (GMT): 2019/122/08:22:21.000
    Vector Time (MET): N/A
    Weight (LBS)     : 944482.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5150515.94                 A    =         6792990.07  meter
     Y    =        4246665.05  meter          E    =           .0012746
     Z    =        1223038.89                 I    =           51.36676
     XDOT =      -2267.161188                 Wp   =          124.27589
     YDOT =       4438.303679  meter/sec      RA   =          227.92620  deg
     ZDOT =      -5826.692520                 TA   =           42.38576
                                              MA   =           42.28737
                                              Ha   =            222.880  n.mi
                                              Hp   =            217.405
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16898018.17                 X    =         5096704.80
     Y    =       13932628.11  feet           Y    =         4303960.87  meter
     Z    =        4012594.77                 Z    =         1247927.73
     XDOT =      -7438.192875                 XDOT =       -2288.319843
     YDOT =      14561.363775  feet/sec       YDOT =        4412.832287  meter/sec
     ZDOT =     -19116.445276                 ZDOT =       -5837.757157
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12585919.23                 X    =         3836188.18
     Y    =       17898115.47  feet           Y    =         5455345.60  meter
     Z    =        4124822.46                 Z    =         1257245.88
     XDOT =      -9594.707704                 XDOT =       -2924.466908
     YDOT =      11191.056353  feet/sec       YDOT =        3411.033976  meter/sec
     ZDOT =     -19166.837852                 ZDOT =       -5842.052177
  
  
    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   19122.38351273  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6370 228.8554 0001186 269.8322  90.2694 15.52640970  8137
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19122.38351273   =   yrday.fracday
    Element set:     908
    Inclination:       51.6370  deg
    RA of node:       228.8554  deg
    Eccentricity:     .0001186     
    Arg of perigee:   269.8322  deg
    Mean anomaly:      90.2694  deg
    Mean motion:   15.52640970  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             813
    Checksum:              313
 
 
    Coasting Arc #10 (Orbit 814)
    ---------------------------------------
 
    Vector Time (GMT): 2019/122/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         295190.32                 A    =         6784930.66  meter
     Y    =       -5036455.65  meter          E    =           .0007797
     Z    =        4532730.60                 I    =           51.34560
     XDOT =       6264.473114                 Wp   =          118.21428
     YDOT =       3158.732878  meter/sec      RA   =          227.41407  deg
     ZDOT =       3094.102117                 TA   =          300.63485
                                              MA   =          300.71171
                                              Ha   =            222.866  n.mi
                                              Hp   =            217.440
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         968472.17                 X    =          329469.66
     Y    =      -16523804.63  feet           Y    =        -5032962.88  meter
     Z    =       14871163.40                 Z    =         4534247.89
     XDOT =      20552.733314                 XDOT =        6213.656035
     YDOT =      10363.296844  feet/sec       YDOT =        3228.502518  meter/sec
     ZDOT =      10151.253665                 ZDOT =        3124.409524
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5977199.93                 X    =        -1821850.54
     Y    =      -15428258.39  feet           Y    =        -4702533.16  meter
     Z    =       14878423.40                 Z    =         4534943.45
     XDOT =      21807.239857                 XDOT =        6646.846708
     YDOT =       1497.219977  feet/sec       YDOT =         456.352649  meter/sec
     ZDOT =      10288.075224                 ZDOT =        3135.805328
  
  
    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   19122.51224188  .00016717  00000-0  10270-3 0  9092
    2 25544  51.6404 228.2153 0001242 258.3630 101.7383 15.52645740  8157
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19122.51224188   =   yrday.fracday
    Element set:     909
    Inclination:       51.6404  deg
    RA of node:       228.2153  deg
    Eccentricity:     .0001242     
    Arg of perigee:   258.3630  deg
    Mean anomaly:     101.7383  deg
    Mean motion:   15.52645740  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             815
    Checksum:              283
 
 
    Coasting Arc #11 (Orbit 829)
    ---------------------------------------
 
    Vector Time (GMT): 2019/123/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1181777.56                 A    =         6782911.36  meter
     Y    =        4385956.18  meter          E    =           .0011807
     Z    =       -5048090.52                 I    =           51.36302
     XDOT =      -6370.170412                 Wp   =           75.30257
     YDOT =      -3830.402310  meter/sec      RA   =          222.41467  deg
     ZDOT =      -1837.382390                 TA   =          176.81008
                                              MA   =          176.80254
                                              Ha   =            222.908  n.mi
                                              Hp   =            217.423
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3877222.95                 X    =        -1206213.49
     Y    =       14389620.00  feet           Y    =         4372604.07  meter
     Z    =      -16561976.77                 Z    =        -5053890.62
     XDOT =     -20899.509227                 XDOT =       -6317.939179
     YDOT =     -12566.936714  feet/sec       YDOT =       -3901.345980  meter/sec
     ZDOT =      -6028.157447                 ZDOT =       -1868.199952
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2711689.43                 X    =          826522.94
     Y    =       14623944.81  feet           Y    =         4457378.38  meter
     Z    =      -16588552.52                 Z    =        -5056190.81
     XDOT =     -23156.799600                 XDOT =       -7058.192518
     YDOT =      -2699.330726  feet/sec       YDOT =        -822.756005  meter/sec
     ZDOT =      -6167.248689                 ZDOT =       -1879.777400
  
  
    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   19123.47770836  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6414 223.4142 0001239 265.7901  94.3109 15.52623477  8305
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19123.47770836   =   yrday.fracday
    Element set:     910
    Inclination:       51.6414  deg
    RA of node:       223.4142  deg
    Eccentricity:     .0001239     
    Arg of perigee:   265.7901  deg
    Mean anomaly:      94.3109  deg
    Mean motion:   15.52623477  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             830
    Checksum:              295
 
 
    Coasting Arc #12 (Orbit 845)
    ---------------------------------------
 
    Vector Time (GMT): 2019/124/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2119990.57                 A    =         6781688.14  meter
     Y    =       -3688231.71  meter          E    =           .0001698
     Z    =        5280335.13                 I    =           51.38505
     XDOT =       6308.116906                 Wp   =          125.43610
     YDOT =       4330.987794  meter/sec      RA   =          217.41278  deg
     ZDOT =        491.416824                 TA   =          319.85268
                                              MA   =          319.86523
                                              Ha   =            222.764  n.mi
                                              Hp   =            217.398
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6955349.64                 X    =         2135426.42
     Y    =      -12100497.73  feet           Y    =        -3664438.26  meter
     Z    =       17323934.17                 Z    =         5290670.89
     XDOT =      20695.921608                 XDOT =        6256.830656
     YDOT =      14209.277538  feet/sec       YDOT =        4401.242807  meter/sec
     ZDOT =       1612.259921                 ZDOT =         521.935400
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         804567.96                 X    =          245232.31
     Y    =      -13875143.91  feet           Y    =        -4229143.86  meter
     Z    =       17370972.36                 Z    =         5294672.37
     XDOT =      23818.585514                 XDOT =        7259.904865
     YDOT =       3576.448111  feet/sec       YDOT =        1090.101384  meter/sec
     ZDOT =       1749.976106                 ZDOT =         533.392717
  
  
    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   19124.50753313  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6417 218.2918 0001207 274.2526  85.8488 15.52670804  8462
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19124.50753313   =   yrday.fracday
    Element set:     911
    Inclination:       51.6417  deg
    RA of node:       218.2918  deg
    Eccentricity:     .0001207     
    Arg of perigee:   274.2526  deg
    Mean anomaly:      85.8488  deg
    Mean motion:   15.52670804  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             846
    Checksum:              309
 
 
    Coasting Arc #13 (Orbit 860)
    ---------------------------------------
 
    Vector Time (GMT): 2019/125/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3093154.37                 A    =         6781888.06  meter
     Y    =        2998135.38  meter          E    =           .0013383
     Z    =       -5249828.62                 I    =           51.41226
     XDOT =      -6013.659532                 Wp   =           96.55043
     YDOT =      -4655.065746  meter/sec      RA   =          212.41365  deg
     ZDOT =        885.178274                 TA   =          181.95289
                                              MA   =          181.95812
                                              Ha   =            222.915  n.mi
                                              Hp   =            217.258
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10148144.25                 X    =        -3100949.19
     Y    =        9836402.18  feet           Y    =         2963502.18  meter
     Z    =      -17223847.17                 Z    =        -5264873.14
     XDOT =     -19729.854107                 XDOT =       -5965.458107
     YDOT =     -15272.525414  feet/sec       YDOT =       -4722.045218  meter/sec
     ZDOT =       2904.128196                 ZDOT =         856.082458
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4440401.31                 X    =        -1353434.32
     Y    =       13329116.04  feet           Y    =         4062714.57  meter
     Z    =      -17292138.46                 Z    =        -5270643.80
     XDOT =     -23569.491710                 XDOT =       -7183.981073
     YDOT =      -4256.467468  feet/sec       YDOT =       -1297.371284  meter/sec
     ZDOT =       2772.856003                 ZDOT =         845.166510
  
  
    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   19125.47299363  .00016717  00000-0  10270-3 0  9121
    2 25544  51.6412 213.4915 0001114 281.1733  78.9294 15.52654559  8619
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19125.47299363   =   yrday.fracday
    Element set:     912
    Inclination:       51.6412  deg
    RA of node:       213.4915  deg
    Eccentricity:     .0001114     
    Arg of perigee:   281.1733  deg
    Mean anomaly:      78.9294  deg
    Mean motion:   15.52654559  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             861
    Checksum:              314
 
 
    Coasting Arc #14 (Orbit 876)
    ---------------------------------------
 
    Vector Time (GMT): 2019/126/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4041020.43                 A    =         6783211.94  meter
     Y    =       -2325296.23  meter          E    =           .0005671
     Z    =        4924552.48                 I    =           51.44553
     XDOT =       5506.262308                 Wp   =           49.01372
     YDOT =       4851.371999  meter/sec      RA   =          207.41604  deg
     ZDOT =      -2222.299456                 TA   =           62.76870
                                              MA   =           62.71093
                                              Ha   =            222.775  n.mi
                                              Hp   =            217.378
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13257941.04                 X    =         4042800.99
     Y    =       -7628924.63  feet           Y    =        -2280097.04  meter
     Z    =       16156668.26                 Z    =         4944186.84
     XDOT =      18065.165054                 XDOT =        5462.398565
     YDOT =      15916.574800  feet/sec       YDOT =        4912.701751  meter/sec
     ZDOT =      -7291.008713                 ZDOT =       -2195.657801
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7999909.00                 X    =         2438372.26
     Y    =      -12926354.80  feet           Y    =        -3939952.94  meter
     Z    =       16245683.38                 Z    =         4951684.29
     XDOT =      22535.429009                 XDOT =        6868.798762
     YDOT =       4912.761553  feet/sec       YDOT =        1497.409721  meter/sec
     ZDOT =      -7170.837028                 ZDOT =       -2185.671126
  
  
    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   19126.50281446  .00016717  00000-0  10270-3 0  9130
    2 25544  51.6412 208.3690 0001171 286.9898  73.1126 15.52659725  8778
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19126.50281446   =   yrday.fracday
    Element set:     913
    Inclination:       51.6412  deg
    RA of node:       208.3690  deg
    Eccentricity:     .0001171     
    Arg of perigee:   286.9898  deg
    Mean anomaly:      73.1126  deg
    Mean motion:   15.52659725  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             877
    Checksum:              322
 
 
    Coasting Arc #15 (Orbit 891)
    ---------------------------------------
 
    Vector Time (GMT): 2019/127/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4917459.44                 A    =         6785432.25  meter
     Y    =        1720738.59  meter          E    =           .0007746
     Z    =       -4355332.32                 I    =           51.48284
     XDOT =      -4760.265870                 Wp   =          110.76895
     YDOT =      -4920.390635  meter/sec      RA   =          202.42530  deg
     ZDOT =       3432.936282                 TA   =          194.17213
                                              MA   =          194.19387
                                              Ha   =            222.883  n.mi
                                              Hp   =            217.222
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16133397.10                 X    =        -4915179.58
     Y    =        5645467.80  feet           Y    =         1665761.21  meter
     Z    =      -14289148.03                 Z    =        -4379214.25
     XDOT =     -15617.670176                 XDOT =       -4721.566465
     YDOT =     -16143.013894  feet/sec       YDOT =       -4973.407149  meter/sec
     ZDOT =      11262.914311                 ZDOT =        3409.905881
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11264397.87                 X    =        -3433388.47
     Y    =       12734487.67  feet           Y    =         3881471.84  meter
     Z    =      -14397351.30                 Z    =        -4388312.68
     XDOT =     -20635.607190                 XDOT =       -6289.733071
     YDOT =      -5645.525127  feet/sec       YDOT =       -1720.756059  meter/sec
     ZDOT =      11159.070614                 ZDOT =        3401.284723
  
  
    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   19127.46826845  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6409 203.5680 0001158 291.9621  68.1408 15.52670184  8921
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19127.46826845   =   yrday.fracday
    Element set:     914
    Inclination:       51.6409  deg
    RA of node:       203.5680  deg
    Eccentricity:     .0001158     
    Arg of perigee:   291.9621  deg
    Mean anomaly:      68.1408  deg
    Mean motion:   15.52670184  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             892
    Checksum:              320
 
 
    Coasting Arc #16 (Orbit 903)
    ---------------------------------------
 
    Vector Time (GMT): 2019/128/05:34:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5302570.08                 A    =         6786899.71  meter
     Y    =        1535875.72  meter          E    =           .0005924
     Z    =       -3954035.38                 I    =           51.50781
     XDOT =      -4385.877635                 Wp   =          104.75131
     YDOT =      -4834.750428  meter/sec      RA   =          198.56645  deg
     ZDOT =       4007.280379                 TA   =          207.17894
                                              MA   =          207.20996
                                              Ha   =            223.009  n.mi
                                              Hp   =            217.168
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17396883.47                 X    =        -5300143.79
     Y    =        5038962.35  feet           Y    =         1476592.60  meter
     Z    =      -12972557.03                 Z    =        -3979787.64
     XDOT =     -14389.362319                 XDOT =       -4350.953544
     YDOT =     -15862.042085  feet/sec       YDOT =       -4883.601474  meter/sec
     ZDOT =      13147.245339                 ZDOT =        3986.059491
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14696030.46                 X    =        -4479350.08
     Y    =      -10441687.09  feet           Y    =        -3182626.23  meter
     Z    =      -13089224.24                 Z    =        -3989595.55
     XDOT =       2684.633766                 XDOT =         818.276372
     YDOT =     -20124.796590  feet/sec       YDOT =       -6134.038001  meter/sec
     ZDOT =      13051.570461                 ZDOT =        3978.118677
  
  
    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   19128.24063089  .00016717  00000-0  10270-3 0  9156
    2 25544  51.6371 199.7241 0000996 305.8681  54.2378 15.52650070  9046
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19128.24063089   =   yrday.fracday
    Element set:     915
    Inclination:       51.6371  deg
    RA of node:       199.7241  deg
    Eccentricity:     .0000996     
    Arg of perigee:   305.8681  deg
    Mean anomaly:      54.2378  deg
    Mean motion:   15.52650070  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             904
    Checksum:              316
 
 
    Coasting Arc #17 (Orbit 919)
    ---------------------------------------
 
    Vector Time (GMT): 2019/129/05:34:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 964623.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5987430.78                 A    =         6789689.74  meter
     Y    =       -1022260.67  meter          E    =           .0012085
     Z    =        3022587.97                 I    =           51.54748
     XDOT =       3325.208288                 Wp   =           93.88468
     YDOT =       4835.457457  meter/sec      RA   =          193.58658  deg
     ZDOT =      -4935.251392                 TA   =           51.44265
                                              MA   =           51.33442
                                              Ha   =            222.947  n.mi
                                              Hp   =            217.298
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19643801.77                 X    =         5983734.79
     Y    =       -3353873.58  feet           Y    =         -955325.99  meter
     Z    =        9916627.20                 Z    =         3051663.89
     XDOT =      10909.476012                 XDOT =        3294.862644
     YDOT =      15864.361736  feet/sec       YDOT =        4872.473079  meter/sec
     ZDOT =     -16191.769659                 ZDOT =       -4919.171835
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15008852.28                 X    =         4574698.18
     Y    =       13008940.62  feet           Y    =         3965125.10  meter
     Z    =       10048319.66                 Z    =         3062727.83
     XDOT =      -4328.013515                 XDOT =       -1319.178519
     YDOT =      17484.872312  feet/sec       YDOT =        5329.389081  meter/sec
     ZDOT =     -16119.349168                 ZDOT =       -4913.177626
  
  
    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   19129.27044466  .00016717  00000-0  10270-3 0  9169
    2 25544  51.6356 194.6020 0001104 304.8549  55.2499 15.52640179  9204
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19129.27044466   =   yrday.fracday
    Element set:     916
    Inclination:       51.6356  deg
    RA of node:       194.6020  deg
    Eccentricity:     .0001104     
    Arg of perigee:   304.8549  deg
    Mean anomaly:      55.2499  deg
    Mean motion:   15.52640179  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             920
    Checksum:              307
 
             

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