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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  13813.3257
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   94.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.554
   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 
   ------------------------------------------------------------------------
   217/02:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.4  
   000/00:00:00.000           0.0               0.0              212.7  
   
   220/06:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.5  
   000/00:00:00.000           0.0               0.0              212.7  
   
 
 
    Coasting Arc #1 (Orbit 1093)
    ---------------------------------------
 
    Vector Time (GMT): 2016/207/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4250908.70                 A    =         6776141.49  meter
     Y    =        1459546.01  meter          E    =           .0015096
     Z    =       -5084605.44                 I    =           51.35579
     XDOT =      -4151.423623                 Wp   =           99.13239
     YDOT =      -6209.420731  meter/sec      RA   =          225.81041  deg
     ZDOT =       1690.265431                 TA   =          187.27142
                                              MA   =          187.29334
                                              Ha   =            220.508  n.mi
                                              Hp   =            212.700
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13946550.86                 X    =        -4242215.23
     Y    =        4788536.76  feet           Y    =         1412058.20  meter
     Z    =      -16681776.38                 Z    =        -5105233.92
     XDOT =     -13620.156244                 XDOT =       -4089.890264
     YDOT =     -20372.115260  feet/sec       YDOT =       -6255.500699  meter/sec
     ZDOT =       5545.490260                 ZDOT =        1670.248418
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11516155.60                 X    =         3510124.23
     Y    =        9044211.21  feet           Y    =         2756675.58  meter
     Z    =      -16771953.74                 Z    =        -5112091.50
     XDOT =      -9076.897441                 XDOT =       -2766.638340
     YDOT =      21669.844067  feet/sec       YDOT =        6604.968471  meter/sec
     ZDOT =       5459.276494                 ZDOT =        1663.987475
  
  
    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   16207.51321548  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6423 226.8128 0001897  71.2906 288.8452 15.54860792 10940
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16207.51321548   =   yrday.fracday
    Element set:     900
    Inclination:       51.6423  deg
    RA of node:       226.8128  deg
    Eccentricity:     .0001897     
    Arg of perigee:    71.2906  deg
    Mean anomaly:     288.8452  deg
    Mean motion:   15.54860792  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1094
    Checksum:              316
 
 
    Coasting Arc #2 (Orbit 1109)
    ---------------------------------------
 
    Vector Time (GMT): 2016/208/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5327856.50                 A    =         6779513.27  meter
     Y    =         188184.83  meter          E    =           .0012198
     Z    =        4180092.41                 I    =           51.38899
     XDOT =       2673.898931                 Wp   =           74.60329
     YDOT =       6183.090134  meter/sec      RA   =          220.79122  deg
     ZDOT =      -3674.308324                 TA   =           53.24449
                                              MA   =           53.13256
                                              Ha   =            220.387  n.mi
                                              Hp   =            212.686
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17479844.18                 X    =         5305051.27
     Y    =         617404.30  feet           Y    =          247636.86  meter
     Z    =       13714213.93                 Z    =         4205918.21
     XDOT =       8772.634289                 XDOT =        2622.407396
     YDOT =      20285.728787  feet/sec       YDOT =        6212.703649  meter/sec
     ZDOT =     -12054.817336                 ZDOT =       -3661.444194
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9149999.73                 X    =        -2788919.92
     Y    =      -14802144.01  feet           Y    =        -4511693.49  meter
     Z    =       13826779.89                 Z    =         4214402.51
     XDOT =      10866.476354                 XDOT =        3312.101993
     YDOT =     -17963.132078  feet/sec       YDOT =       -5475.162657  meter/sec
     ZDOT =     -11999.770067                 ZDOT =       -3657.529917
  
  
    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   16208.54154936  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6406 221.6810 0002072  73.9819 286.1562 15.54909039 11100
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16208.54154936   =   yrday.fracday
    Element set:     901
    Inclination:       51.6406  deg
    RA of node:       221.6810  deg
    Eccentricity:     .0002072     
    Arg of perigee:    73.9819  deg
    Mean anomaly:     286.1562  deg
    Mean motion:   15.54909039  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1110
    Checksum:              296
 
 
    Coasting Arc #3 (Orbit 1124)
    ---------------------------------------
 
    Vector Time (GMT): 2016/209/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5991189.31                 A    =         6783829.77  meter
     Y    =       -1632451.66  meter          E    =           .0006730
     Z    =       -2732732.67                 I    =           51.42839
     XDOT =       -803.619146                 Wp   =           65.26334
     YDOT =      -5630.550389  meter/sec      RA   =          215.78745  deg
     ZDOT =       5138.090376                 TA   =          263.72563
                                              MA   =          263.80230
                                              Ha   =            220.489  n.mi
                                              Hp   =            212.645
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19656132.92                 X    =        -5959215.20
     Y    =       -5355812.54  feet           Y    =        -1699270.25  meter
     Z    =       -8965658.36                 Z    =        -2761758.59
     XDOT =      -2636.545753                 XDOT =        -765.555654
     YDOT =     -18472.934346  feet/sec       YDOT =       -5639.324388  meter/sec
     ZDOT =      16857.251889                 ZDOT =        5134.278831
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6767899.87                 X    =         2062855.88
     Y    =       19156287.10  feet           Y    =         5838836.31  meter
     Z    =       -9091947.82                 Z    =        -2771225.70
     XDOT =     -12216.204700                 XDOT =       -3723.499192
     YDOT =      12289.764744  feet/sec       YDOT =        3745.920294  meter/sec
     ZDOT =      16841.573328                 ZDOT =        5133.311550
  
  
    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   16209.50561153  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6406 216.8707 0002055  79.0026 281.1358 15.54898326 11259
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16209.50561153   =   yrday.fracday
    Element set:     902
    Inclination:       51.6406  deg
    RA of node:       216.8707  deg
    Eccentricity:     .0002055     
    Arg of perigee:    79.0026  deg
    Mean anomaly:     281.1358  deg
    Mean motion:   15.54898326  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1125
    Checksum:              296
 
 
    Coasting Arc #4 (Orbit 1140)
    ---------------------------------------
 
    Vector Time (GMT): 2016/210/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6100248.15                 A    =         6786744.03  meter
     Y    =        2828679.57  meter          E    =           .0014998
     Z    =         870614.86                 I    =           51.46389
     XDOT =      -1323.950743                 Wp   =          119.78660
     YDOT =       4697.927329  meter/sec      RA   =          210.79613  deg
     ZDOT =      -5917.817194                 TA   =           50.76532
                                              MA   =           50.63230
                                              Ha   =            220.537  n.mi
                                              Hp   =            212.666
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20013937.49                 X    =         6063934.72
     Y    =        9280444.78  feet           Y    =         2896693.52  meter
     Z    =        2856347.97                 Z    =          900160.10
     XDOT =      -4343.670416                 XDOT =       -1347.639754
     YDOT =      15413.147405  feet/sec       YDOT =        4682.989929  meter/sec
     ZDOT =     -19415.410743                 ZDOT =       -5924.305827
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4142975.96                 X    =        -1262779.07
     Y    =      -21651103.32  feet           Y    =        -6599256.29  meter
     Z    =        2984719.10                 Z    =          909742.38
     XDOT =      13394.927469                 XDOT =        4082.773892
     YDOT =      -5273.677874  feet/sec       YDOT =       -1607.417016  meter/sec
     ZDOT =     -19444.488383                 ZDOT =       -5926.680059
  
  
    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   16210.53394087  .00016717  00000-0  10270-3 0  9039
    2 25544  51.6398 211.7381 0002100  79.0055 281.1335 15.54898221 11411
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16210.53394087   =   yrday.fracday
    Element set:     903
    Inclination:       51.6398  deg
    RA of node:       211.7381  deg
    Eccentricity:     .0002100     
    Arg of perigee:    79.0055  deg
    Mean anomaly:     281.1335  deg
    Mean motion:   15.54898221  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1141
    Checksum:              284
 
 
    Coasting Arc #5 (Orbit 1156)
    ---------------------------------------
 
    Vector Time (GMT): 2016/211/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5605804.45                 A    =         6786517.36  meter
     Y    =       -3659120.77  meter          E    =           .0015312
     Z    =        1072155.46                 I    =           51.49070
     XDOT =       3439.967383                 Wp   =           60.40000
     YDOT =      -3531.468296  meter/sec      RA   =          205.81242  deg
     ZDOT =       5877.792826                 TA   =          311.25967
                                              MA   =          311.39147
                                              Ha   =            220.439  n.mi
                                              Hp   =            212.697
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18391746.89                 X    =        -5569678.62
     Y    =      -12004989.41  feet           Y    =        -3721606.71  meter
     Z    =        3517570.41                 Z    =         1045011.61
     XDOT =      11285.982227                 XDOT =        3450.649989
     YDOT =     -11586.182074  feet/sec       YDOT =       -3492.940977  meter/sec
     ZDOT =      19284.097197                 ZDOT =        5894.528854
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1386061.40                 X    =          422471.51
     Y    =       21937859.53  feet           Y    =         6686659.59  meter
     Z    =        3399790.99                 Z    =         1036256.29
     XDOT =     -14359.134421                 XDOT =       -4376.664172
     YDOT =      -2122.047241  feet/sec       YDOT =        -646.799999  meter/sec
     ZDOT =      19357.675426                 ZDOT =        5900.219470
  
  
    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   16211.56226486  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6389 206.6069 0001960  87.0700 273.0677 15.54940876 11576
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16211.56226486   =   yrday.fracday
    Element set:     904
    Inclination:       51.6389  deg
    RA of node:       206.6069  deg
    Eccentricity:     .0001960     
    Arg of perigee:    87.0700  deg
    Mean anomaly:     273.0677  deg
    Mean motion:   15.54940876  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1157
    Checksum:              321
 
 
    Coasting Arc #6 (Orbit 1171)
    ---------------------------------------
 
    Vector Time (GMT): 2016/212/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4481390.52                 A    =         6783585.46  meter
     Y    =        4180748.08  meter          E    =           .0006443
     Z    =       -2910687.49                 I    =           51.50889
     XDOT =      -5341.509858                 Wp   =          106.96081
     YDOT =       2238.720914  meter/sec      RA   =          200.82393  deg
     ZDOT =      -5019.443164                 TA   =          106.27598
                                              MA   =          106.20510
                                              Ha   =            220.568  n.mi
                                              Hp   =            212.766
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14702724.82                 X    =         4448445.95
     Y    =       13716365.10  feet           Y    =         4230678.00  meter
     Z    =       -9549499.64                 Z    =        -2888998.02
     XDOT =     -17524.638643                 XDOT =       -5341.764860
     YDOT =       7344.884890  feet/sec       YDOT =        2178.987537  meter/sec
     ZDOT =     -16467.989382                 ZDOT =       -5045.390973
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1822553.25                 X    =          555514.23
     Y    =      -20069182.14  feet           Y    =        -6117086.71  meter
     Z    =       -9455578.25                 Z    =        -2882060.25
     XDOT =      14998.645336                 XDOT =        4571.587098
     YDOT =       9157.208413  feet/sec       YDOT =        2791.117124  meter/sec
     ZDOT =     -16581.544938                 ZDOT =       -5054.054897
  
  
    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   16212.52632088  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6380 201.7948 0002048  84.1947 275.9439 15.54891492 11721
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16212.52632088   =   yrday.fracday
    Element set:     905
    Inclination:       51.6380  deg
    RA of node:       201.7948  deg
    Eccentricity:     .0002048     
    Arg of perigee:    84.1947  deg
    Mean anomaly:     275.9439  deg
    Mean motion:   15.54891492  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1172
    Checksum:              323
 
 
    Coasting Arc #7 (Orbit 1187)
    ---------------------------------------
 
    Vector Time (GMT): 2016/213/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2854922.00                 A    =         6779170.96  meter
     Y    =       -4373132.38  meter          E    =           .0011555
     Z    =        4314449.76                 I    =           51.52523
     XDOT =       6766.131694                 Wp   =          104.79246
     YDOT =       -964.210257  meter/sec      RA   =          195.82620  deg
     ZDOT =       3489.192599                 TA   =          309.64971
                                              MA   =          309.75160
                                              Ha   =            220.478  n.mi
                                              Hp   =            212.752
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9366541.98                 X    =        -2826765.70
     Y    =      -14347547.19  feet           Y    =        -4404900.90  meter
     Z    =       14155018.88                 Z    =         4300649.59
     XDOT =      22198.594796                 XDOT =        6759.462179
     YDOT =      -3163.419477  feet/sec       YDOT =        -888.584390  meter/sec
     ZDOT =      11447.482280                 ZDOT =        3522.043916
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5286269.41                 X    =        -1611254.92
     Y    =       16349929.04  feet           Y    =         4983458.37  meter
     Z    =       14095529.61                 Z    =         4296317.42
     XDOT =     -15105.490419                 XDOT =       -4604.153480
     YDOT =     -14907.090830  feet/sec       YDOT =       -4543.681285  meter/sec
     ZDOT =      11590.962367                 ZDOT =        3532.925329
  
  
    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   16213.55464052  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6383 196.6631 0001838  87.7076 272.4287 15.54924568 11884
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16213.55464052   =   yrday.fracday
    Element set:     906
    Inclination:       51.6383  deg
    RA of node:       196.6631  deg
    Eccentricity:     .0001838     
    Arg of perigee:    87.7076  deg
    Mean anomaly:     272.4287  deg
    Mean motion:   15.54924568  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1188
    Checksum:              335
 
 
    Coasting Arc #8 (Orbit 1202)
    ---------------------------------------
 
    Vector Time (GMT): 2016/214/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         850824.53                 A    =         6775866.24  meter
     Y    =        4330678.46  meter          E    =           .0015698
     Z    =       -5155342.49                 I    =           51.54545
     XDOT =      -7513.503767                 Wp   =           80.14518
     YDOT =       -257.270453  meter/sec      RA   =          190.81632  deg
     ZDOT =      -1457.287680                 TA   =          175.79729
                                              MA   =          175.78409
                                              Ha   =            220.524  n.mi
                                              Hp   =            212.721
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2791419.05                 X    =          827376.45
     Y    =       14208262.67  feet           Y    =         4340062.14  meter
     Z    =      -16913853.33                 Z    =        -5151266.19
     XDOT =     -24650.602909                 XDOT =       -7502.989764
     YDOT =       -844.063167  feet/sec       YDOT =        -341.232598  meter/sec
     ZDOT =      -4781.127560                 ZDOT =       -1493.760100
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9083012.01                 X    =         2768502.06
     Y    =      -11302351.77  feet           Y    =        -3444956.82  meter
     Z    =      -16896772.47                 Z    =        -5150136.25
     XDOT =      14242.999008                 XDOT =        4341.266098
     YDOT =      18826.065160  feet/sec       YDOT =        5738.184661  meter/sec
     ZDOT =      -4940.229651                 ZDOT =       -1505.781998
  
  
    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   16214.51868879  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6385 191.8509 0002017  87.3686 272.7698 15.54899235 12039
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16214.51868879   =   yrday.fracday
    Element set:     907
    Inclination:       51.6385  deg
    RA of node:       191.8509  deg
    Eccentricity:     .0002017     
    Arg of perigee:    87.3686  deg
    Mean anomaly:     272.7698  deg
    Mean motion:   15.54899235  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1203
    Checksum:              353
 
 
    Coasting Arc #9 (Orbit 1218)
    ---------------------------------------
 
    Vector Time (GMT): 2016/215/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1282462.16                 A    =         6775262.51  meter
     Y    =       -4065565.87  meter          E    =           .0004859
     Z    =        5262109.85                 I    =           51.57521
     XDOT =       7510.475575                 Wp   =           73.65631
     YDOT =       1374.540842  meter/sec      RA   =          185.80340  deg
     ZDOT =       -766.513368                 TA   =           23.68024
                                              MA   =           23.65789
                                              Ha   =            220.439  n.mi
                                              Hp   =            212.750
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4207553.03                 X    =         1302268.57
     Y    =      -13338470.71  feet           Y    =        -4051113.99  meter
     Z    =       17264139.91                 Z    =         5268387.52
     XDOT =      24640.667896                 XDOT =        7498.270226
     YDOT =       4509.648431  feet/sec       YDOT =        1458.459783  meter/sec
     ZDOT =      -2514.807637                 ZDOT =        -730.059798
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12786065.43                 X    =        -3897192.74
     Y    =        5582597.53  feet           Y    =         1701575.73  meter
     Z    =       17292193.78                 Z    =         5270660.66
     XDOT =     -12237.131082                 XDOT =       -3729.877554
     YDOT =     -20710.104649  feet/sec       YDOT =       -6312.439897  meter/sec
     ZDOT =      -2355.945563                 ZDOT =        -718.092208
  
  
    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   16215.54700408  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6383 186.7191 0001910  90.4058 269.7314 15.54902579 12190
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16215.54700408   =   yrday.fracday
    Element set:     908
    Inclination:       51.6383  deg
    RA of node:       186.7191  deg
    Eccentricity:     .0001910     
    Arg of perigee:    90.4058  deg
    Mean anomaly:     269.7314  deg
    Mean motion:   15.54902579  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1219
    Checksum:              312
 
 
    Coasting Arc #10 (Orbit 1233)
    ---------------------------------------
 
    Vector Time (GMT): 2016/216/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3308587.82                 A    =         6777784.05  meter
     Y    =        3650781.30  meter          E    =           .0012511
     Z    =       -4666494.65                 I    =           51.61686
     XDOT =      -6685.893798                 Wp   =          107.37128
     YDOT =      -2377.078595  meter/sec      RA   =          180.79582  deg
     ZDOT =       2883.416663                 TA   =          191.31639
                                              MA   =          191.34454
                                              Ha   =            220.469  n.mi
                                              Hp   =            212.671
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10854946.92                 X    =        -3326498.60
     Y    =       11977628.93  feet           Y    =         3613682.41  meter
     Z    =      -15310021.82                 Z    =        -4682609.99
     XDOT =     -21935.347107                 XDOT =       -6672.821862
     YDOT =      -7798.814289  feet/sec       YDOT =       -2451.771694  meter/sec
     ZDOT =       9460.028421                 ZDOT =        2850.970736
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16096908.54                 X    =         4906337.72
     Y    =          79253.06  feet           Y    =           24156.33  meter
     Z    =      -15380945.68                 Z    =        -4688112.24
     XDOT =       8795.108091                 XDOT =        2680.748946
     YDOT =      20445.186893  feet/sec       YDOT =        6231.692965  meter/sec
     ZDOT =       9318.797015                 ZDOT =        2840.369330
  
  
    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   16216.51104640  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6393 181.9079 0001886  92.4584 267.6785 15.54898918 12348
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16216.51104640   =   yrday.fracday
    Element set:     909
    Inclination:       51.6393  deg
    RA of node:       181.9079  deg
    Eccentricity:     .0001886     
    Arg of perigee:    92.4584  deg
    Mean anomaly:     267.6785  deg
    Mean motion:   15.54898918  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1234
    Checksum:              345
 
 
    Coasting Arc #11 (Orbit 1243)
    ---------------------------------------
 
    Vector Time (GMT): 2016/217/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3171434.87                 A    =         6777429.00  meter
     Y    =       -3642044.80  meter          E    =           .0009611
     Z    =        4749510.98                 I    =           51.63898
     XDOT =       6779.293099                 Wp   =          116.39108
     YDOT =      -2385.813395  meter/sec      RA   =          177.83681  deg
     ZDOT =       2688.905432                 TA   =          307.02022
                                              MA   =          307.10812
                                              Ha   =            220.445  n.mi
                                              Hp   =            212.733
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10404970.03                 X    =        -3153543.44
     Y    =      -11948965.87  feet           Y    =        -3677409.90  meter
     Z    =       15582385.11                 Z    =         4734148.73
     XDOT =      22241.775258                 XDOT =        6792.406778
     YDOT =      -7827.471769  feet/sec       YDOT =       -2309.929507  meter/sec
     ZDOT =       8821.868216                 ZDOT =        2721.868611
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7909416.45                 X    =        -2410790.13
     Y    =      -13803965.65  feet           Y    =        -4207448.73  meter
     Z    =       15515913.65                 Z    =         4729250.48
     XDOT =      22293.474063                 XDOT =        6795.050895
     YDOT =      -2664.566205  feet/sec       YDOT =        -812.159779  meter/sec
     ZDOT =       8966.131753                 ZDOT =        2732.876958
  
  
    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   16217.15373813  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6430 178.6971 0001868 109.7163 250.4192 15.54951407 12445
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16217.15373813   =   yrday.fracday
    Element set:     910
    Inclination:       51.6430  deg
    RA of node:       178.6971  deg
    Eccentricity:     .0001868     
    Arg of perigee:   109.7163  deg
    Mean anomaly:     250.4192  deg
    Mean motion:   15.54951407  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1244
    Checksum:              305
 
 
    Coasting Arc #12 (Orbit 1258)
    ---------------------------------------
 
    Vector Time (GMT): 2016/218/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1117157.20                 A    =         6775156.61  meter
     Y    =        4085504.65  meter          E    =           .0016392
     Z    =       -5302231.45                 I    =           51.66335
     XDOT =      -7515.836553                 Wp   =           88.61449
     YDOT =       1367.925772  meter/sec      RA   =          172.83313  deg
     ZDOT =       -530.564230                 TA   =          176.32395
                                              MA   =          176.31189
                                              Ha   =            220.388  n.mi
                                              Hp   =            212.806
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3665213.90                 X    =         1097144.43
     Y    =       13403886.64  feet           Y    =         4097885.49  meter
     Z    =      -17395772.47                 Z    =        -5296853.35
     XDOT =     -24658.256407                 XDOT =       -7527.997257
     YDOT =       4487.945447  feet/sec       YDOT =        1283.810664  meter/sec
     ZDOT =      -1740.696293                 ZDOT =        -567.103058
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1265252.33                 X    =          385648.91
     Y    =       13866893.47  feet           Y    =         4226629.13  meter
     Z    =      -17372946.55                 Z    =        -5295274.11
     XDOT =     -24040.385464                 XDOT =       -7327.509490
     YDOT =       -183.160829  feet/sec       YDOT =         -55.827421  meter/sec
     ZDOT =      -1900.420864                 ZDOT =        -579.248279
  
  
    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   16218.11777618  .00016717  00000-0  10270-3 0  9115
    2 25544  51.6430 173.8871 0001827 109.9320 250.2030 15.54922923 12599
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16218.11777618   =   yrday.fracday
    Element set:     911
    Inclination:       51.6430  deg
    RA of node:       173.8871  deg
    Eccentricity:     .0001827     
    Arg of perigee:   109.9320  deg
    Mean anomaly:     250.2030  deg
    Mean motion:   15.54922923  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1259
    Checksum:              298
 
 
    Coasting Arc #13 (Orbit 1274)
    ---------------------------------------
 
    Vector Time (GMT): 2016/219/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1020172.79                 A    =         6775827.37  meter
     Y    =       -4339453.56  meter          E    =           .0006206
     Z    =        5098480.26                 I    =           51.69820
     XDOT =       7479.540250                 Wp   =           69.76017
     YDOT =       -241.247373  meter/sec      RA   =          167.82798  deg
     ZDOT =      -1698.166246                 TA   =           36.64033
                                              MA   =           36.59791
                                              Ha   =            220.295  n.mi
                                              Hp   =            212.745
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3347023.57                 X    =         1043856.07
     Y    =      -14237052.37  feet           Y    =        -4327912.76  meter
     Z    =       16727297.43                 Z    =         5103493.54
     XDOT =      24539.174048                 XDOT =        7489.930855
     YDOT =       -791.494007  feet/sec       YDOT =        -157.548098  meter/sec
     ZDOT =      -5571.411567                 ZDOT =       -1661.807938
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5553862.94                 X    =         1692817.42
     Y    =      -13501666.33  feet           Y    =        -4115307.90  meter
     Z    =       16749875.19                 Z    =         5105361.96
     XDOT =      23381.393887                 XDOT =        7126.648857
     YDOT =       2887.714454  feet/sec       YDOT =         880.175366  meter/sec
     ZDOT =      -5412.638705                 ZDOT =       -1649.772277
  
  
    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   16219.14607955  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6432 168.7549 0001814 113.1521 246.9824 15.54959501 12755
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16219.14607955   =   yrday.fracday
    Element set:     912
    Inclination:       51.6432  deg
    RA of node:       168.7549  deg
    Eccentricity:     .0001814     
    Arg of perigee:   113.1521  deg
    Mean anomaly:     246.9824  deg
    Mean motion:   15.54959501  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1275
    Checksum:              315
 
 
    Coasting Arc #14 (Orbit 1289)
    ---------------------------------------
 
    Vector Time (GMT): 2016/220/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2992263.47                 A    =         6779334.20  meter
     Y    =        4399990.59  meter          E    =           .0009914
     Z    =       -4211105.08                 I    =           51.74129
     XDOT =      -6641.471729                 Wp   =          111.69872
     YDOT =       -991.297031  meter/sec      RA   =          162.83342  deg
     ZDOT =       3686.829932                 TA   =          196.08591
                                              MA   =          196.11741
                                              Ha   =            220.310  n.mi
                                              Hp   =            212.688
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9817137.38                 X    =        -3020787.47
     Y    =       14435664.65  feet           Y    =         4366369.48  meter
     Z    =      -13815961.55                 Z    =        -4225709.94
     XDOT =     -21789.605409                 XDOT =       -6647.801948
     YDOT =      -3252.286847  feet/sec       YDOT =       -1065.601692  meter/sec
     ZDOT =      12095.898727                 ZDOT =        3654.552472
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11766955.59                 X    =        -3586568.07
     Y    =       12826449.23  feet           Y    =         3909501.73  meter
     Z    =      -13880430.47                 Z    =        -4230755.21
     XDOT =     -20204.899265                 XDOT =       -6158.453296
     YDOT =      -5610.416131  feet/sec       YDOT =       -1710.054837  meter/sec
     ZDOT =      11955.124825                 ZDOT =        3643.922047
  
  
    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   16220.11011144  .00016717  00000-0  10270-3 0  9135
    2 25544  51.6432 163.9448 0001851 116.6687 243.4656 15.54958219 12909
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16220.11011144   =   yrday.fracday
    Element set:     913
    Inclination:       51.6432  deg
    RA of node:       163.9448  deg
    Eccentricity:     .0001851     
    Arg of perigee:   116.6687  deg
    Mean anomaly:     243.4656  deg
    Mean motion:   15.54958219  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1290
    Checksum:              298
 
 
    Coasting Arc #15 (Orbit 1292)
    ---------------------------------------
 
    Vector Time (GMT): 2016/220/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3973239.88                 A    =         6777322.34  meter
     Y    =       -2683776.20  meter          E    =           .0009561
     Z    =        4784215.12                 I    =           51.73760
     XDOT =       5936.778859                 Wp   =          116.11625
     YDOT =      -4090.742607  meter/sec      RA   =          162.13523  deg
     ZDOT =       2627.487443                 TA   =          307.98606
                                              MA   =          308.07238
                                              Ha   =            220.539  n.mi
                                              Hp   =            212.680
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13035563.92                 X    =        -3966173.23
     Y    =       -8805040.02  feet           Y    =        -2728167.97  meter
     Z    =       15696243.83                 Z    =         4764931.64
     XDOT =      19477.620927                 XDOT =        5969.318331
     YDOT =     -13421.071544  feet/sec       YDOT =       -4024.171559  meter/sec
     ZDOT =       8620.365627                 ZDOT =        2656.405558
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15495670.49                 X    =        -4723080.37
     Y    =        3156199.81  feet           Y    =          962009.70  meter
     Z    =       15612473.40                 Z    =         4758681.89
     XDOT =       4335.453722                 XDOT =        1321.446295
     YDOT =     -22117.513907  feet/sec       YDOT =       -6741.418239  meter/sec
     ZDOT =       8747.282522                 ZDOT =        2666.171713
  
  
    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   16220.30291737  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6421 162.9835 0002009 106.3969 253.7406 15.54947024 12933
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16220.30291737   =   yrday.fracday
    Element set:     914
    Inclination:       51.6421  deg
    RA of node:       162.9835  deg
    Eccentricity:     .0002009     
    Arg of perigee:   106.3969  deg
    Mean anomaly:     253.7406  deg
    Mean motion:   15.54947024  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1293
    Checksum:              302
 
 
    Coasting Arc #16 (Orbit 1307)
    ---------------------------------------
 
    Vector Time (GMT): 2016/221/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2099089.72                 A    =         6775106.96  meter
     Y    =        3660317.35  meter          E    =           .0016516
     Z    =       -5315019.09                 I    =           51.76143
     XDOT =      -6896.738503                 Wp   =           89.25335
     YDOT =       3296.656136  meter/sec      RA   =          157.13730  deg
     ZDOT =       -454.454544                 TA   =          176.41927
                                              MA   =          176.40743
                                              Ha   =            220.405  n.mi
                                              Hp   =            212.804
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6886777.29                 X    =         2083820.88
     Y    =       12008915.20  feet           Y    =         3683705.25  meter
     Z    =      -17437726.66                 Z    =        -5304859.54
     XDOT =     -22627.094827                 XDOT =       -6930.882449
     YDOT =      10815.800970  feet/sec       YDOT =        3219.341272  meter/sec
     ZDOT =      -1490.992598                 ZDOT =        -488.039797
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13518111.10                 X    =         4120320.26
     Y    =        3229137.42  feet           Y    =          984241.08  meter
     Z    =      -17393947.24                 Z    =        -5301675.12
     XDOT =      -7559.856564                 XDOT =       -2304.244281
     YDOT =      22841.523373  feet/sec       YDOT =        6962.096324  meter/sec
     ZDOT =      -1638.176663                 ZDOT =        -499.316247
  
  
    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   16221.26694495  .00016717  00000-0  10270-3 0  9150
    2 25544  51.6430 158.1727 0001908 110.1563 249.9796 15.54930215 13080
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16221.26694495   =   yrday.fracday
    Element set:     915
    Inclination:       51.6430  deg
    RA of node:       158.1727  deg
    Eccentricity:     .0001908     
    Arg of perigee:   110.1563  deg
    Mean anomaly:     249.9796  deg
    Mean motion:   15.54930215  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1308
    Checksum:              314
 
 
    Coasting Arc #17 (Orbit 1323)
    ---------------------------------------
 
    Vector Time (GMT): 2016/222/06:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -100490.93                 A    =         6775906.77  meter
     Y    =       -4473234.07  meter          E    =           .0006568
     Z    =        5083778.62                 I    =           51.79206
     XDOT =       7136.779586                 Wp   =           70.22472
     YDOT =      -2187.754864  meter/sec      RA   =          152.13910  deg
     ZDOT =      -1779.905216                 TA   =           36.96625
                                              MA   =           36.92101
                                              Ha   =            220.394  n.mi
                                              Hp   =            212.670
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -329694.64                 X    =          -75157.19
     Y    =      -14675964.78  feet           Y    =        -4474216.06  meter
     Z    =       16679063.71                 Z    =         5083352.10
     XDOT =      23414.631188                 XDOT =        7169.359124
     YDOT =      -7177.673437  feet/sec       YDOT =       -2107.764500  meter/sec
     ZDOT =      -5839.584043                 ZDOT =       -1745.157683
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11083171.28                 X    =        -3378150.61
     Y    =       -9627779.68  feet           Y    =        -2934547.25  meter
     Z    =       16677918.93                 Z    =         5083429.69
     XDOT =       9922.051350                 XDOT =        3024.241252
     YDOT =     -21297.124671  feet/sec       YDOT =       -6491.363600  meter/sec
     ZDOT =      -5687.485356                 ZDOT =       -1733.545536
  
  
    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   16222.29523705  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6412 153.0408 0001994 111.8047 248.3319 15.54964736 13247
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16222.29523705   =   yrday.fracday
    Element set:     916
    Inclination:       51.6412  deg
    RA of node:       153.0408  deg
    Eccentricity:     .0001994     
    Arg of perigee:   111.8047  deg
    Mean anomaly:     248.3319  deg
    Mean motion:   15.54964736  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1324
    Checksum:              301
 
             

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