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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  16520.4497
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   68.6
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.584
   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 
   ------------------------------------------------------------------------
   317/14:50:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              225.3  
   000/00:00:00.000           0.0               0.0              223.7  
   
 
 
    Coasting Arc #1 (Orbit 3841)
    ---------------------------------------
 
    Vector Time (GMT): 2019/317/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6455088.97                 A    =         6801367.65  meter
     Y    =       -2110598.75  meter          E    =           .0009500
     Z    =         226548.05                 I    =           51.53463
     XDOT =       1290.144558                 Wp   =           18.39208
     YDOT =       4595.627032  meter/sec      RA   =          340.37539  deg
     ZDOT =       5994.069233                 TA   =          344.04833
                                              MA   =          344.07823
                                              Ha   =            225.310  n.mi
                                              Hp   =            223.505
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21178113.41                 X    =         6477110.06
     Y    =       -6924536.60  feet           Y    =        -2038290.28  meter
     Z    =         743267.90                 Z    =          257958.74
     XDOT =       4232.757737                 XDOT =        1209.542326
     YDOT =      15077.516509  feet/sec       YDOT =        4609.603324  meter/sec
     ZDOT =      19665.581472                 ZDOT =        6000.140942
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7789278.08                 X    =        -2374171.96
     Y    =       20869957.40  feet           Y    =         6361163.01  meter
     Z    =         886660.80                 Z    =          270254.21
     XDOT =     -12822.757733                 XDOT =       -3908.376557
     YDOT =      -5629.481808  feet/sec       YDOT =       -1715.866055  meter/sec
     ZDOT =      19692.788562                 ZDOT =        6002.361954
  
  
    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   19317.56395630  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6424 340.6614 0006312 275.7466  84.2964 15.49986245 38420
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19317.56395630   =   yrday.fracday
    Element set:     900
    Inclination:       51.6424  deg
    RA of node:       340.6614  deg
    Eccentricity:     .0006312     
    Arg of perigee:   275.7466  deg
    Mean anomaly:      84.2964  deg
    Mean motion:   15.49986245  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3842
    Checksum:              329
 
 
    Coasting Arc #2 (Orbit 3842)
    ---------------------------------------
 
    Vector Time (GMT): 2019/317/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2099408.24                 A    =         6792847.70  meter
     Y    =       -4612108.85  meter          E    =           .0003711
     Z    =       -4527368.54                 I    =           51.49941
     XDOT =       6981.876401                 Wp   =          134.80285
     YDOT =         91.333169  meter/sec      RA   =          339.76459  deg
     ZDOT =       3143.586192                 TA   =          166.84088
                                              MA   =          166.83120
                                              Ha   =            225.350  n.mi
                                              Hp   =            223.652
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6887822.31                 X    =         2172818.23
     Y    =      -15131590.71  feet           Y    =        -4588221.06  meter
     Z    =      -14853571.33                 Z    =        -4516992.07
     XDOT =      22906.418640                 XDOT =        6965.065938
     YDOT =        299.649505  feet/sec       YDOT =         169.315261  meter/sec
     ZDOT =      10313.602993                 ZDOT =        3177.461691
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15587115.86                 X    =         4750952.91
     Y    =        5904722.69  feet           Y    =         1799759.48  meter
     Z    =      -14805802.38                 Z    =        -4512808.57
     XDOT =       1739.529842                 XDOT =         530.208696
     YDOT =      21664.065189  feet/sec       YDOT =        6603.207069  meter/sec
     ZDOT =      10468.005475                 ZDOT =        3190.648069
  
  
    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   19317.62842942  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6396 340.3423 0006410 276.3276  83.7144 15.49973815 38432
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19317.62842942   =   yrday.fracday
    Element set:     901
    Inclination:       51.6396  deg
    RA of node:       340.3423  deg
    Eccentricity:     .0006410     
    Arg of perigee:   276.3276  deg
    Mean anomaly:      83.7144  deg
    Mean motion:   15.49973815  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3843
    Checksum:              322
 
 
    Coasting Arc #3 (Orbit 3858)
    ---------------------------------------
 
    Vector Time (GMT): 2019/318/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2091092.25                 A    =         6793482.12  meter
     Y    =        4796746.46  meter          E    =           .0004994
     Z    =        4332505.53                 I    =           51.47095
     XDOT =      -6827.906510                 Wp   =           34.55657
     YDOT =        161.199223  meter/sec      RA   =          334.79907  deg
     ZDOT =      -3467.976971                 TA   =           90.83437
                                              MA   =           90.77715
                                              Ha   =            225.499  n.mi
                                              Hp   =            223.651
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6860538.88                 X    =        -2165620.91
     Y    =       15737357.14  feet           Y    =         4772945.33  meter
     Z    =       14214256.99                 Z    =         4322166.87
     XDOT =     -22401.268078                 XDOT =       -6812.355667
     YDOT =        528.868842  feet/sec       YDOT =          84.931974  meter/sec
     ZDOT =     -11377.877201                 ZDOT =       -3501.107483
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16287014.18                 X    =        -4964281.92
     Y    =       -5551205.16  feet           Y    =        -1692007.33  meter
     Z    =       14166643.77                 Z    =         4317993.02
     XDOT =      -2886.155016                 XDOT =        -879.700049
     YDOT =     -21004.219172  feet/sec       YDOT =       -6402.086004  meter/sec
     ZDOT =     -11528.904257                 ZDOT =       -3514.010017
  
  
    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   19318.66000591  .00016717  00000-0  10270-3 0  9028
    2 25544  51.6397 335.2315 0006528 280.1978  79.8437 15.50003835 38594
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19318.66000591   =   yrday.fracday
    Element set:     902
    Inclination:       51.6397  deg
    RA of node:       335.2315  deg
    Eccentricity:     .0006528     
    Arg of perigee:   280.1978  deg
    Mean anomaly:      79.8437  deg
    Mean motion:   15.50003835  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3859
    Checksum:              326
 
 
    Coasting Arc #4 (Orbit 3873)
    ---------------------------------------
 
    Vector Time (GMT): 2019/319/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2048086.70                 A    =         6794279.08  meter
     Y    =       -4994798.46  meter          E    =           .0001076
     Z    =       -4126673.65                 I    =           51.44455
     XDOT =       6653.391541                 Wp   =          134.99398
     YDOT =       -389.159150  meter/sec      RA   =          329.83186  deg
     ZDOT =       3772.993874                 TA   =          174.05518
                                              MA   =          174.05390
                                              Ha   =            225.789  n.mi
                                              Hp   =            223.702
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6719444.55                 X    =         2123833.31
     Y    =      -16387134.06  feet           Y    =        -4971471.41  meter
     Z    =      -13538955.56                 Z    =        -4116541.07
     XDOT =      21828.712404                 XDOT =        6638.921211
     YDOT =      -1276.768866  feet/sec       YDOT =        -314.837485  meter/sec
     ZDOT =      12378.588827                 ZDOT =        3805.279112
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17011008.58                 X    =         5184955.41
     Y    =        5057349.64  feet           Y    =         1541480.17  meter
     Z    =      -13492265.08                 Z    =        -4112442.40
     XDOT =       3914.574642                 XDOT =        1193.162351
     YDOT =      20251.034627  feet/sec       YDOT =        6172.515354  meter/sec
     ZDOT =      12525.782974                 ZDOT =        3817.858650
  
  
    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   19319.62710787  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6406 330.4403 0006481 284.6927  75.3504 15.49981180 38740
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19319.62710787   =   yrday.fracday
    Element set:     903
    Inclination:       51.6406  deg
    RA of node:       330.4403  deg
    Eccentricity:     .0006481     
    Arg of perigee:   284.6927  deg
    Mean anomaly:      75.3504  deg
    Mean motion:   15.49981180  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3874
    Checksum:              325
 
 
    Coasting Arc #5 (Orbit 3889)
    ---------------------------------------
 
    Vector Time (GMT): 2019/320/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1989532.61                 A    =         6794986.59  meter
     Y    =        5199568.08  meter          E    =           .0006229
     Z    =        3894757.90                 I    =           51.41858
     XDOT =      -6463.995603                 Wp   =           51.75791
     YDOT =        580.310127  meter/sec      RA   =          324.86332  deg
     ZDOT =      -4068.460442                 TA   =           81.07840
                                              MA   =           81.00788
                                              Ha   =            226.007  n.mi
                                              Hp   =            223.612
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6527337.97                 X    =        -2066446.74
     Y    =       17058950.39  feet           Y    =         5176889.29  meter
     Z    =       12778077.11                 Z    =         3884907.02
     XDOT =     -21207.334657                 XDOT =       -6450.241706
     YDOT =       1903.904615  feet/sec       YDOT =         508.102464  meter/sec
     ZDOT =     -13347.967331                 ZDOT =       -4099.827215
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17738231.14                 X    =        -5406612.85
     Y    =       -4486403.74  feet           Y    =        -1367455.86  meter
     Z    =       12732655.71                 Z    =         3880913.46
     XDOT =      -4788.026581                 XDOT =       -1459.390502
     YDOT =     -19434.215509  feet/sec       YDOT =       -5923.548887  meter/sec
     ZDOT =     -13490.992282                 ZDOT =       -4112.054448
  
  
    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   19320.65868268  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6404 325.3298 0006558 289.2362  70.8078 15.50006596 38907
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19320.65868268   =   yrday.fracday
    Element set:     904
    Inclination:       51.6404  deg
    RA of node:       325.3298  deg
    Eccentricity:     .0006558     
    Arg of perigee:   289.2362  deg
    Mean anomaly:      70.8078  deg
    Mean motion:   15.50006596  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3890
    Checksum:              336
 
 
    Coasting Arc #6 (Orbit 3904)
    ---------------------------------------
 
    Vector Time (GMT): 2019/321/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1887545.11                 A    =         6795810.39  meter
     Y    =       -5406925.01  meter          E    =           .0001829
     Z    =       -3656447.92                 I    =           51.39431
     XDOT =       6266.904473                 Wp   =          337.58893
     YDOT =       -747.021536  meter/sec      RA   =          319.89347  deg
     ZDOT =       4340.710842                 TA   =          338.88926
                                              MA   =          338.89681
                                              Ha   =            226.230  n.mi
                                              Hp   =            223.611
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6192733.29                 X    =         1965627.86
     Y    =      -17739255.27  feet           Y    =        -5385380.22  meter
     Z    =      -11996220.22                 Z    =        -3647089.66
     XDOT =      20560.710213                 XDOT =        6253.707073
     YDOT =      -2450.858057  feet/sec       YDOT =        -677.014780  meter/sec
     ZDOT =      14241.177303                 ZDOT =        4371.121400
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18439253.42                 X    =         5620284.44
     Y    =        3749584.13  feet           Y    =         1142873.24  meter
     Z    =      -11953032.04                 Z    =        -3643284.16
     XDOT =       5541.160246                 XDOT =        1688.945643
     YDOT =      18581.031890  feet/sec       YDOT =        5663.498520  meter/sec
     ZDOT =      14379.858387                 ZDOT =        4382.980836
  
  
    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   19321.62578469  .00016717  00000-0  10270-3 0  9055
    2 25544  51.6403 320.5390 0006603 292.6354  67.4093 15.49981446 39056
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19321.62578469   =   yrday.fracday
    Element set:     905
    Inclination:       51.6403  deg
    RA of node:       320.5390  deg
    Eccentricity:     .0006603     
    Arg of perigee:   292.6354  deg
    Mean anomaly:      67.4093  deg
    Mean motion:   15.49981446  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3905
    Checksum:              325
 
 
    Coasting Arc #7 (Orbit 3920)
    ---------------------------------------
 
    Vector Time (GMT): 2019/322/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1772325.63                 A    =         6796517.90  meter
     Y    =        5615122.57  meter          E    =           .0007107
     Z    =        3391731.00                 I    =           51.37323
     XDOT =      -6061.645191                 Wp   =           66.23307
     YDOT =        872.069469  meter/sec      RA   =          314.92227  deg
     ZDOT =      -4600.726368                 TA   =           74.05612
                                              MA   =           73.97783
                                              Ha   =            226.398  n.mi
                                              Hp   =            223.452
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5814716.65                 X    =        -1851459.15
     Y    =       18422318.16  feet           Y    =         5594860.45  meter
     Z    =       11127726.37                 Z    =         3382929.86
     XDOT =     -19887.287371                 XDOT =       -6048.598418
     YDOT =       2861.120304  feet/sec       YDOT =         804.357181  meter/sec
     ZDOT =     -15094.246615                 ZDOT =       -4630.140106
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19115851.14                 X    =        -5826511.43
     Y    =       -2946214.03  feet           Y    =         -898006.04  meter
     Z    =       11087068.52                 Z    =         3379338.48
     XDOT =      -6123.882874                 XDOT =       -1866.559500
     YDOT =     -17703.320826  feet/sec       YDOT =       -5395.972188  meter/sec
     ZDOT =     -15228.393510                 ZDOT =       -4641.614342
  
  
    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   19322.65735962  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6414 315.4287 0006647 296.6817  63.3653 15.50008326 39216
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19322.65735962   =   yrday.fracday
    Element set:     906
    Inclination:       51.6414  deg
    RA of node:       315.4287  deg
    Eccentricity:     .0006647     
    Arg of perigee:   296.6817  deg
    Mean anomaly:      63.3653  deg
    Mean motion:   15.50008326  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3921
    Checksum:              323
 
 
    Coasting Arc #8 (Orbit 3935)
    ---------------------------------------
 
    Vector Time (GMT): 2019/323/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1611399.77                 A    =         6797297.91  meter
     Y    =       -5814229.67  meter          E    =           .0004792
     Z    =       -3124012.70                 I    =           51.35286
     XDOT =       5860.801376                 Wp   =          342.65627
     YDOT =       -973.334359  meter/sec      RA   =          309.94956  deg
     ZDOT =       4837.139780                 TA   =          341.27654
                                              MA   =          341.29416
                                              Ha   =            226.615  n.mi
                                              Hp   =            223.357
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5286744.64                 X    =         1691471.26
     Y    =      -19075556.66  feet           Y    =        -5795761.97  meter
     Z    =      -10249385.51                 Z    =        -3115990.91
     XDOT =      19228.350970                 XDOT =        5847.753558
     YDOT =      -3193.354196  feet/sec       YDOT =        -907.867972  meter/sec
     ZDOT =      15869.881169                 ZDOT =        4865.577856
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19714780.12                 X    =         6009064.98
     Y    =        1978212.96  feet           Y    =          602959.31  meter
     Z    =      -10212274.60                 Z    =        -3112701.30
     XDOT =       6593.318056                 XDOT =        2009.643343
     YDOT =      16843.593276  feet/sec       YDOT =        5133.927230  meter/sec
     ZDOT =      15999.586414                 ZDOT =        4876.673939
  
  
    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   19323.62445949  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6414 310.6377 0006702 300.6555  59.3935 15.49989348 39364
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19323.62445949   =   yrday.fracday
    Element set:     907
    Inclination:       51.6414  deg
    RA of node:       310.6377  deg
    Eccentricity:     .0006702     
    Arg of perigee:   300.6555  deg
    Mean anomaly:      59.3935  deg
    Mean motion:   15.49989348  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3936
    Checksum:              343
 
 
    Coasting Arc #9 (Orbit 3951)
    ---------------------------------------
 
    Vector Time (GMT): 2019/324/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1440558.76                 A    =         6797986.25  meter
     Y    =        6008799.76  meter          E    =           .0007862
     Z    =        2829530.44                 I    =           51.33457
     XDOT =      -5659.582434                 Wp   =           78.27283
     YDOT =       1030.898595  meter/sec      RA   =          304.97618  deg
     ZDOT =      -5057.058049                 TA   =           69.50360
                                              MA   =           69.41923
                                              Ha   =            226.806  n.mi
                                              Hp   =            223.134
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4726242.65                 X    =        -1521388.26
     Y    =       19713909.97  feet           Y    =         5992238.36  meter
     Z    =        9283236.34                 Z    =         2822336.57
     XDOT =     -18568.183838                 XDOT =       -5646.124994
     YDOT =       3382.213237  feet/sec       YDOT =         967.684576  meter/sec
     ZDOT =     -16591.397800                 ZDOT =       -5084.517722
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20264995.71                 X    =        -6176770.69
     Y    =        -960971.46  feet           Y    =         -292904.10  meter
     Z    =        9249895.97                 Z    =         2819368.29
     XDOT =      -6891.843298                 XDOT =       -2100.633837
     YDOT =     -16001.057836  feet/sec       YDOT =       -4877.122428  meter/sec
     ZDOT =     -16716.643365                 ZDOT =       -5095.232898
  
  
    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   19324.65603284  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6413 305.5275 0006678 305.3547  54.6978 15.50006780 39523
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19324.65603284   =   yrday.fracday
    Element set:     908
    Inclination:       51.6413  deg
    RA of node:       305.5275  deg
    Eccentricity:     .0006678     
    Arg of perigee:   305.3547  deg
    Mean anomaly:      54.6978  deg
    Mean motion:   15.50006780  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3952
    Checksum:              325
 
 
    Coasting Arc #10 (Orbit 3966)
    ---------------------------------------
 
    Vector Time (GMT): 2019/325/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1222911.27                 A    =         6798677.24  meter
     Y    =       -6182043.78  meter          E    =           .0007626
     Z    =       -2538133.24                 I    =           51.31795
     XDOT =       5474.892592                 Wp   =          350.21677
     YDOT =      -1071.500074  meter/sec      RA   =          300.00167  deg
     ZDOT =       5252.742019                 TA   =          341.19010
                                              MA   =          341.21826
                                              Ha   =            226.939  n.mi
                                              Hp   =            223.044
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4012176.08                 X    =         1304278.79
     Y    =      -20282295.88  feet           Y    =        -6167913.32  meter
     Z    =       -8327208.79                 Z    =        -2531995.23
     XDOT =      17962.246036                 XDOT =        5460.952283
     YDOT =      -3515.420190  feet/sec       YDOT =       -1010.354018  meter/sec
     ZDOT =      17233.405573                 ZDOT =        5279.303451
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20685725.54                 X    =         6305009.14
     Y    =        -210138.98  feet           Y    =          -64050.36  meter
     Z    =       -8298680.00                 Z    =        -2529437.66
     XDOT =       7110.302075                 XDOT =        2167.220072
     YDOT =      15225.838022  feet/sec       YDOT =        4640.835429  meter/sec
     ZDOT =      17354.554595                 ZDOT =        5289.668241
  
  
    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   19325.62313292  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6407 300.7368 0006735 308.1666  51.8877 15.49992365 39677
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19325.62313292   =   yrday.fracday
    Element set:     909
    Inclination:       51.6407  deg
    RA of node:       300.7368  deg
    Eccentricity:     .0006735     
    Arg of perigee:   308.1666  deg
    Mean anomaly:      51.8877  deg
    Mean motion:   15.49992365  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3967
    Checksum:              345
 
 
    Coasting Arc #11 (Orbit 3982)
    ---------------------------------------
 
    Vector Time (GMT): 2019/326/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1000906.95                 A    =         6799273.91  meter
     Y    =        6346073.81  meter          E    =           .0008071
     Z    =        2219278.69                 I    =           51.30543
     XDOT =      -5297.085273                 Wp   =           89.32324
     YDOT =       1068.744251  meter/sec      RA   =          295.02594  deg
     ZDOT =      -5427.828267                 TA   =           65.94718
                                              MA   =           65.86275
                                              Ha   =            227.114  n.mi
                                              Hp   =            222.853
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3283815.44                 X    =        -1082576.41
     Y    =       20820452.14  feet           Y    =         6334424.28  meter
     Z    =        7281098.06                 Z    =         2214218.33
     XDOT =     -17378.888691                 XDOT =       -5282.276769
     YDOT =       3506.378777  feet/sec       YDOT =        1009.591403  meter/sec
     ZDOT =     -17807.835522                 ZDOT =       -5453.523971
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21039242.57                 X    =        -6412761.14
     Y    =        1402967.41  feet           Y    =          427624.47  meter
     Z    =        7257479.91                 Z    =         2212079.88
     XDOT =      -7170.076750                 XDOT =       -2185.439393
     YDOT =     -14504.657023  feet/sec       YDOT =       -4421.019461  meter/sec
     ZDOT =     -17925.032745                 ZDOT =       -5463.549981
  
  
    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   19326.65470538  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6418 295.6261 0006773 312.1429  47.9145 15.50006801 39832
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19326.65470538   =   yrday.fracday
    Element set:     910
    Inclination:       51.6418  deg
    RA of node:       295.6261  deg
    Eccentricity:     .0006773     
    Arg of perigee:   312.1429  deg
    Mean anomaly:      47.9145  deg
    Mean motion:   15.50006801  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3983
    Checksum:              313
 
 
    Coasting Arc #12 (Orbit 3997)
    ---------------------------------------
 
    Vector Time (GMT): 2019/327/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         736876.63                 A    =         6799829.00  meter
     Y    =       -6478057.27  meter          E    =           .0010377
     Z    =       -1907627.53                 I    =           51.29384
     XDOT =       5145.544936                 Wp   =          358.41187
     YDOT =      -1055.280971  meter/sec      RA   =          290.04923  deg
     ZDOT =       5580.659801                 TA   =          340.49703
                                              MA   =          340.53669
                                              Ha   =            227.270  n.mi
                                              Hp   =            222.675
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2417574.25                 X    =          818527.78
     Y    =      -21253468.74  feet           Y    =        -6469360.40  meter
     Z    =       -6258620.51                 Z    =        -1903849.85
     XDOT =      16881.709106                 XDOT =        5129.854647
     YDOT =      -3462.207911  feet/sec       YDOT =        -997.827738  meter/sec
     ZDOT =      18309.251315                 ZDOT =        5605.617319
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21222604.39                 X    =         6468649.82
     Y    =       -2716211.85  feet           Y    =         -827901.37  meter
     Z    =       -6240848.12                 Z    =        -1902210.51
     XDOT =       7186.010885                 XDOT =        2190.296118
     YDOT =      13888.523808  feet/sec       YDOT =        4233.222057  meter/sec
     ZDOT =      18423.078710                 ZDOT =        5615.354391
  
  
    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   19327.62180297  .00016717  00000-0  10270-3 0  9116
    2 25544  51.6415 290.8348 0006818 316.2974  43.7636 15.49999873 39985
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19327.62180297   =   yrday.fracday
    Element set:     911
    Inclination:       51.6415  deg
    RA of node:       290.8348  deg
    Eccentricity:     .0006818     
    Arg of perigee:   316.2974  deg
    Mean anomaly:      43.7636  deg
    Mean motion:   15.49999873  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3998
    Checksum:              365
 
 
    Coasting Arc #13 (Orbit 4013)
    ---------------------------------------
 
    Vector Time (GMT): 2019/328/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -474337.80                 A    =         6800323.67  meter
     Y    =        6597396.65  meter          E    =           .0008062
     Z    =        1568925.06                 I    =           51.28561
     XDOT =      -5007.773066                 Wp   =           98.37370
     YDOT =       1002.918366  meter/sec      RA   =          285.07266  deg
     ZDOT =      -5707.205722                 TA   =           64.42164
                                              MA   =           64.33833
                                              Ha   =            227.449  n.mi
                                              Hp   =            222.487
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1556226.39                 X    =         -555697.71
     Y    =       21645002.13  feet           Y    =         6591637.28  meter
     Z    =        5147391.91                 Z    =         1566423.54
     XDOT =     -16429.701659                 XDOT =       -4990.892699
     YDOT =       3290.414586  feet/sec       YDOT =         947.012562  meter/sec
     ZDOT =     -18724.428223                 ZDOT =       -5731.491146
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21327956.21                 X    =        -6500761.05
     Y    =        4021093.75  feet           Y    =         1225629.38  meter
     Z    =        5135434.78                 Z    =         1565280.52
     XDOT =      -7072.428986                 XDOT =       -2155.676355
     YDOT =     -13356.114834  feet/sec       YDOT =       -4070.943801  meter/sec
     ZDOT =     -18835.186159                 ZDOT =       -5740.964741
  
  
    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   19328.65337423  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6420 285.7244 0006766 320.2199  39.8455 15.49999645 40147
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19328.65337423   =   yrday.fracday
    Element set:     912
    Inclination:       51.6420  deg
    RA of node:       285.7244  deg
    Eccentricity:     .0006766     
    Arg of perigee:   320.2199  deg
    Mean anomaly:      39.8455  deg
    Mean motion:   15.49999645  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4014
    Checksum:              337
 
 
    Coasting Arc #14 (Orbit 4028)
    ---------------------------------------
 
    Vector Time (GMT): 2019/329/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         175463.45                 A    =         6800695.78  meter
     Y    =       -6675382.49  meter          E    =           .0012711
     Z    =       -1243985.14                 I    =           51.27951
     XDOT =       4903.784970                 Wp   =            6.41565
     YDOT =       -951.142102  meter/sec      RA   =          280.09527  deg
     ZDOT =       5813.792530                 TA   =          340.00855
                                              MA   =          340.05831
                                              Ha   =            227.538  n.mi
                                              Hp   =            222.349
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         575667.49                 X    =          256139.22
     Y    =      -21900861.20  feet           Y    =        -6672969.16  meter
     Z    =       -4081316.08                 Z    =        -1242937.31
     XDOT =      16088.533365                 XDOT =        4885.815582
     YDOT =      -3120.544955  feet/sec       YDOT =        -896.405407  meter/sec
     ZDOT =      19074.122473                 ZDOT =        5837.570158
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21231640.19                 X    =         6471403.93
     Y    =       -5407406.99  feet           Y    =        -1648177.65  meter
     Z    =       -4075985.74                 Z    =        -1242360.45
     XDOT =       6969.401369                 XDOT =        2124.273537
     YDOT =      12950.241335  feet/sec       YDOT =        3947.233559  meter/sec
     ZDOT =      19182.562675                 ZDOT =        5846.845103
  
  
    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   19329.62047206  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6422 280.9333 0006869 323.2137  36.8542 15.50003458 40294
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19329.62047206   =   yrday.fracday
    Element set:     913
    Inclination:       51.6422  deg
    RA of node:       280.9333  deg
    Eccentricity:     .0006869     
    Arg of perigee:   323.2137  deg
    Mean anomaly:      36.8542  deg
    Mean motion:   15.50003458  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4029
    Checksum:              300
 
 
    Coasting Arc #15 (Orbit 4044)
    ---------------------------------------
 
    Vector Time (GMT): 2019/330/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         114126.95                 A    =         6801036.04  meter
     Y    =        6739137.18  meter          E    =           .0007486
     Z    =         891578.08                 I    =           51.27687
     XDOT =      -4818.365831                 Wp   =          106.13179
     YDOT =        865.913082  meter/sec      RA   =          275.11824  deg
     ZDOT =      -5889.025632                 TA   =           64.19163
                                              MA   =           64.11443
                                              Ha   =            227.713  n.mi
                                              Hp   =            222.189
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         374432.25                 X    =           34428.58
     Y    =       22110030.13  feet           Y    =         6739967.72  meter
     Z    =        2925124.94                 Z    =          891939.56
     XDOT =     -15808.286848                 XDOT =       -4799.084338
     YDOT =       2840.922184  feet/sec       YDOT =         812.139097  meter/sec
     ZDOT =     -19320.950236                 ZDOT =       -5912.385073
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21057911.90                 X    =        -6418451.55
     Y    =        6749189.93  feet           Y    =         2057153.09  meter
     Z    =        2926220.99                 Z    =          891912.16
     XDOT =      -6770.499468                 XDOT =       -2063.648238
     YDOT =     -12645.358899  feet/sec       YDOT =       -3854.305392  meter/sec
     ZDOT =     -19427.481095                 ZDOT =       -5921.496238
  
  
    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   19330.65204225  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6432 275.8231 0006797 326.7320  33.3403 15.49993999 40459
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19330.65204225   =   yrday.fracday
    Element set:     914
    Inclination:       51.6432  deg
    RA of node:       275.8231  deg
    Eccentricity:     .0006797     
    Arg of perigee:   326.7320  deg
    Mean anomaly:      33.3403  deg
    Mean motion:   15.49993999  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4045
    Checksum:              317
 
 
    Coasting Arc #16 (Orbit 4059)
    ---------------------------------------
 
    Vector Time (GMT): 2019/331/14:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932295.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -430034.68                 A    =         6801189.57  meter
     Y    =       -6755254.51  meter          E    =           .0014765
     Z    =        -556957.89                 I    =           51.27623
     XDOT =       4771.319123                 Wp   =           14.82405
     YDOT =       -790.100736  meter/sec      RA   =          270.14040  deg
     ZDOT =       5948.086248                 TA   =          339.14240
                                              MA   =          339.20258
                                              Ha   =            227.833  n.mi
                                              Hp   =            221.967
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1410874.95                 X    =         -351758.06
     Y    =      -22162908.50  feet           Y    =        -6759625.72  meter
     Z    =       -1827289.66                 Z    =         -558857.55
     XDOT =      15653.934130                 XDOT =        4750.906591
     YDOT =      -2592.194017  feet/sec       YDOT =        -736.859314  meter/sec
     ZDOT =      19514.718660                 ZDOT =        5971.214305
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20669226.23                 X    =         6299980.16
     Y    =       -8120248.87  feet           Y    =        -2475051.85  meter
     Z    =       -1835405.65                 Z    =         -559431.64
     XDOT =       6628.906036                 XDOT =        2020.490560
     YDOT =      12474.687964  feet/sec       YDOT =        3802.284891  meter/sec
     ZDOT =      19620.194610                 ZDOT =        5980.235317
  
  
    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   19331.61913717  .00016717  00000-0  10270-3 0  9155
    2 25544  51.6437 271.0319 0006968 331.0449  29.0314 15.50012877 40609
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19331.61913717   =   yrday.fracday
    Element set:     915
    Inclination:       51.6437  deg
    RA of node:       271.0319  deg
    Eccentricity:     .0006968     
    Arg of perigee:   331.0449  deg
    Mean anomaly:      29.0314  deg
    Mean motion:   15.50012877  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4060
    Checksum:              298
 
             

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