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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  13813.3262
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   76.4
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.637
   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 
   ------------------------------------------------------------------------
   209/14:48:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.1  
   000/00:00:00.000           0.0               0.0              212.3  
   
   209/15:41:14.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              212.3  
   
   209/20:00:20.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              212.3  
   
   212/23:18:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.1  
   000/00:00:00.000           0.0               0.0              212.1  
   
   214/15:20:50.280          -0.6               0.7              0.7    
   N/A                        0.1              -0.0              223.0  
   000/00:01:40.559           0.1              -0.0              212.6  
   
   216/02:50:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              212.7  
   
 
 
    Coasting Arc #1 (Orbit 2708)
    ---------------------------------------
 
    Vector Time (GMT): 2017/202/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4510652.67                 A    =         6789076.31  meter
     Y    =        5059366.16  meter          E    =           .0013906
     Z    =        -330291.06                 I    =           51.38381
     XDOT =      -3762.330193                 Wp   =          111.34885
     YDOT =       2977.609931  meter/sec      RA   =          226.05091  deg
     ZDOT =      -5978.365194                 TA   =           72.22251
                                              MA   =           72.07082
                                              Ha   =            222.988  n.mi
                                              Hp   =            212.561
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14798729.23                 X    =         4455346.63
     Y    =       16598970.35  feet           Y    =         5109498.15  meter
     Z    =       -1083632.08                 Z    =         -308513.68
     XDOT =     -12343.602994                 XDOT =       -3766.307381
     YDOT =       9769.061455  feet/sec       YDOT =        2935.515492  meter/sec
     ZDOT =     -19614.059034                 ZDOT =       -5996.650505
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2781290.43                 X    =          847737.32
     Y    =      -22067857.30  feet           Y    =        -6726282.91  meter
     Z    =        -988210.26                 Z    =         -301206.49
     XDOT =      13780.173749                 XDOT =        4200.196959
     YDOT =       2585.144798  feet/sec       YDOT =         787.952135  meter/sec
     ZDOT =     -19695.289975                 ZDOT =       -6003.124384
  
  
    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   17202.56626944  .00016717  00000-0  10270-3 0  9001
    2 25544  51.6379 226.9595 0006168  56.5504 303.6238 15.54200987 27091
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17202.56626944   =   yrday.fracday
    Element set:     900
    Inclination:       51.6379  deg
    RA of node:       226.9595  deg
    Eccentricity:     .0006168     
    Arg of perigee:    56.5504  deg
    Mean anomaly:     303.6238  deg
    Mean motion:   15.54200987  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2709
    Checksum:              326
 
 
    Coasting Arc #2 (Orbit 2724)
    ---------------------------------------
 
    Vector Time (GMT): 2017/203/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3685085.18                 A    =         6787407.55  meter
     Y    =       -5325754.73  meter          E    =           .0019923
     Z    =        1998016.58                 I    =           51.40095
     XDOT =       5101.094655                 Wp   =           65.62204
     YDOT =      -1433.510403  meter/sec      RA   =          221.06229  deg
     ZDOT =       5551.638241                 TA   =          316.53867
                                              MA   =          316.69553
                                              Ha   =            222.926  n.mi
                                              Hp   =            212.563
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12090174.49                 X    =        -3634962.52
     Y    =      -17472948.58  feet           Y    =        -5366683.82  meter
     Z    =        6555172.49                 Z    =         1980237.02
     XDOT =      16735.874854                 XDOT =        5089.778762
     YDOT =      -4703.118119  feet/sec       YDOT =       -1376.530399  meter/sec
     ZDOT =      18214.036223                 ZDOT =        5576.389704
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4840516.45                 X    =        -1475389.41
     Y    =       20713735.52  feet           Y    =         6313546.59  meter
     Z    =        6477429.96                 Z    =         1974320.65
     XDOT =     -13113.242522                 XDOT =       -3996.916321
     YDOT =      -8831.381594  feet/sec       YDOT =       -2691.805110  meter/sec
     ZDOT =      18323.606795                 ZDOT =        5585.035351
  
  
    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   17203.59505033  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6372 221.8306 0006027  59.2335 300.9410 15.54223063 27254
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17203.59505033   =   yrday.fracday
    Element set:     901
    Inclination:       51.6372  deg
    RA of node:       221.8306  deg
    Eccentricity:     .0006027     
    Arg of perigee:    59.2335  deg
    Mean anomaly:     300.9410  deg
    Mean motion:   15.54223063  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2725
    Checksum:              269
 
 
    Coasting Arc #3 (Orbit 2739)
    ---------------------------------------
 
    Vector Time (GMT): 2017/204/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2478449.03                 A    =         6783973.65  meter
     Y    =        5262616.88  meter          E    =           .0010974
     Z    =       -3502797.40                 I    =           51.41429
     XDOT =      -6196.249523                 Wp   =           73.85916
     YDOT =        -71.144836  meter/sec      RA   =          216.06667  deg
     ZDOT =      -4499.900647                 TA   =          147.43594
                                              MA   =          147.36820
                                              Ha   =            223.050  n.mi
                                              Hp   =            212.504
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8131394.46                 X    =         2436431.37
     Y    =       17265803.43  feet           Y    =         5290097.98  meter
     Z    =      -11492117.44                 Z    =        -3490859.67
     XDOT =     -20328.902633                 XDOT =       -6173.135606
     YDOT =       -233.414815  feet/sec       YDOT =        -140.305841  meter/sec
     ZDOT =     -14763.453566                 ZDOT =       -4529.943336
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7012423.00                 X    =         2137386.53
     Y    =      -17783280.30  feet           Y    =        -5420343.83  meter
     Z    =      -11440156.14                 Z    =        -3486959.59
     XDOT =      12344.317225                 XDOT =        3762.547890
     YDOT =      14431.950059  feet/sec       YDOT =        4398.858378  meter/sec
     ZDOT =     -14896.191853                 ZDOT =       -4540.359277
  
  
    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   17204.55953080  .00016717  00000-0  10270-3 0  9028
    2 25544  51.6369 217.0210 0006190  62.7094 297.4688 15.54199527 27404
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17204.55953080   =   yrday.fracday
    Element set:     902
    Inclination:       51.6369  deg
    RA of node:       217.0210  deg
    Eccentricity:     .0006190     
    Arg of perigee:    62.7094  deg
    Mean anomaly:     297.4688  deg
    Mean motion:   15.54199527  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2740
    Checksum:              316
 
 
    Coasting Arc #4 (Orbit 2755)
    ---------------------------------------
 
    Vector Time (GMT): 2017/205/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1007917.76                 A    =         6780162.88  meter
     Y    =       -4878726.19  meter          E    =           .0013355
     Z    =        4588117.62                 I    =           51.42756
     XDOT =       6930.953206                 Wp   =           93.94436
     YDOT =       1389.594131  meter/sec      RA   =          211.06333  deg
     ZDOT =       2991.774161                 TA   =          326.11024
                                              MA   =          326.19550
                                              Ha   =            223.031  n.mi
                                              Hp   =            212.457
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3306816.79                 X    =         -975573.95
     Y    =      -16006319.50  feet           Y    =        -4889816.88  meter
     Z    =       15052879.34                 Z    =         4583299.80
     XDOT =      22739.347790                 XDOT =        6900.367043
     YDOT =       4559.035864  feet/sec       YDOT =        1466.929530  meter/sec
     ZDOT =       9815.532025                 ZDOT =        3025.367622
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9137600.02                 X    =        -2785140.49
     Y    =       13574257.53  feet           Y    =         4137433.69  meter
     Z    =       15032307.75                 Z    =         4581847.40
     XDOT =     -11495.372351                 XDOT =       -3503.789493
     YDOT =     -18802.871985  feet/sec       YDOT =       -5731.115381  meter/sec
     ZDOT =       9963.785469                 ZDOT =        3036.961811
  
  
    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   17205.58830587  .00016717  00000-0  10270-3 0  9039
    2 25544  51.6359 211.8918 0006131  64.6780 295.5008 15.54210867 27561
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17205.58830587   =   yrday.fracday
    Element set:     903
    Inclination:       51.6359  deg
    RA of node:       211.8918  deg
    Eccentricity:     .0006131     
    Arg of perigee:    64.6780  deg
    Mean anomaly:     295.5008  deg
    Mean motion:   15.54210867  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2756
    Checksum:              324
 
 
    Coasting Arc #5 (Orbit 2770)
    ---------------------------------------
 
    Vector Time (GMT): 2017/206/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -665666.56                 A    =         6777598.99  meter
     Y    =        4299970.62  meter          E    =           .0020224
     Z    =       -5214300.14                 I    =           51.44766
     XDOT =      -7148.500178                 Wp   =           77.65765
     YDOT =      -2486.018786  meter/sec      RA   =          206.05217  deg
     ZDOT =      -1137.015077                 TA   =          181.38851
                                              MA   =          181.39413
                                              Ha   =            223.071  n.mi
                                              Hp   =            212.339
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2183945.40                 X    =         -688372.54
     Y    =       14107515.16  feet           Y    =         4292399.96  meter
     Z    =      -17107283.92                 Z    =        -5217588.63
     XDOT =     -23453.084575                 XDOT =       -7114.646635
     YDOT =      -8156.229614  feet/sec       YDOT =       -2565.768834  meter/sec
     ZDOT =      -3730.364425                 ZDOT =       -1171.657392
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11435433.03                 X    =         3485519.99
     Y    =       -8514901.69  feet           Y    =        -2595342.04  meter
     Z    =      -17122443.91                 Z    =        -5218920.90
     XDOT =      10188.454333                 XDOT =        3105.440881
     YDOT =      21494.702106  feet/sec       YDOT =        6551.585202  meter/sec
     ZDOT =      -3883.114766                 ZDOT =       -1183.573381
  
  
    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   17206.55278098  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6361 207.0830 0006180  68.8435 291.3378 15.54207199 27716
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17206.55278098   =   yrday.fracday
    Element set:     904
    Inclination:       51.6361  deg
    RA of node:       207.0830  deg
    Eccentricity:     .0006180     
    Arg of perigee:    68.8435  deg
    Mean anomaly:     291.3378  deg
    Mean motion:   15.54207199  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2771
    Checksum:              321
 
 
    Coasting Arc #6 (Orbit 2786)
    ---------------------------------------
 
    Vector Time (GMT): 2017/207/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2382028.79                 A    =         6777271.50  meter
     Y    =       -3558368.71  meter          E    =           .0009281
     Z    =        5246069.68                 I    =           51.47729
     XDOT =       6854.929959                 Wp   =           68.41968
     YDOT =       3349.700223  meter/sec      RA   =          201.03887  deg
     ZDOT =       -835.932177                 TA   =           29.60872
                                              MA   =           29.55621
                                              Ha   =            222.950  n.mi
                                              Hp   =            212.364
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7815055.09                 X    =         2396160.04
     Y    =      -11674438.03  feet           Y    =        -3531652.36  meter
     Z    =       17211514.69                 Z    =         5257674.84
     XDOT =      22489.927688                 XDOT =        6821.023726
     YDOT =      10989.830127  feet/sec       YDOT =        3426.167146  meter/sec
     ZDOT =      -2742.559637                 ZDOT =        -802.715979
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13648509.00                 X    =        -4160065.54
     Y    =        3049534.89  feet           Y    =          929498.24  meter
     Z    =       17263324.31                 Z    =         5261861.25
     XDOT =      -8339.466245                 XDOT =       -2541.869312
     YDOT =     -22542.988395  feet/sec       YDOT =       -6871.102863  meter/sec
     ZDOT =      -2596.216236                 ZDOT =        -791.326709
  
  
    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   17207.58155047  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6367 201.9534 0006102  71.7255 288.4561 15.54224463 27874
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17207.58155047   =   yrday.fracday
    Element set:     905
    Inclination:       51.6367  deg
    RA of node:       201.9534  deg
    Eccentricity:     .0006102     
    Arg of perigee:    71.7255  deg
    Mean anomaly:     288.4561  deg
    Mean motion:   15.54224463  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2787
    Checksum:              312
 
 
    Coasting Arc #7 (Orbit 2801)
    ---------------------------------------
 
    Vector Time (GMT): 2017/208/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3988951.85                 A    =         6779484.19  meter
     Y    =        2776185.10  meter          E    =           .0016652
     Z    =       -4741995.01                 I    =           51.51579
     XDOT =      -5967.761105                 Wp   =           96.99519
     YDOT =      -3956.367468  meter/sec      RA   =          196.03130  deg
     ZDOT =       2710.031205                 TA   =          199.85818
                                              MA   =          199.92308
                                              Ha   =            223.089  n.mi
                                              Hp   =            212.210
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13087112.38                 X    =        -3996665.52
     Y    =        9108218.82  feet           Y    =         2731534.86  meter
     Z    =      -15557726.42                 Z    =        -4761390.49
     XDOT =     -19579.268718                 XDOT =       -5936.240212
     YDOT =     -12980.208229  feet/sec       YDOT =       -4022.926819  meter/sec
     ZDOT =       8891.178495                 ZDOT =        2681.118654
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15707426.67                 X    =         4787623.65
     Y    =        2195739.42  feet           Y    =          669261.38  meter
     Z    =      -15643864.22                 Z    =        -4768249.81
     XDOT =       5669.286430                 XDOT =        1727.998504
     YDOT =      21739.727847  feet/sec       YDOT =        6626.269048  meter/sec
     ZDOT =       8763.927235                 ZDOT =        2671.245021
  
  
    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   17208.54601899  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6371 197.1451 0006196  74.2665 285.9171 15.54208627 28020
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17208.54601899   =   yrday.fracday
    Element set:     906
    Inclination:       51.6371  deg
    RA of node:       197.1451  deg
    Eccentricity:     .0006196     
    Arg of perigee:    74.2665  deg
    Mean anomaly:     285.9171  deg
    Mean motion:   15.54208627  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2802
    Checksum:              327
 
 
    Coasting Arc #8 (Orbit 2817)
    ---------------------------------------
 
    Vector Time (GMT): 2017/209/12:49:52.952
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5346839.85                 A    =         6783131.90  meter
     Y    =       -1936817.38  meter          E    =           .0017761
     Z    =        3684277.64                 I    =           51.55958
     XDOT =       4580.007254                 Wp   =           82.39055
     YDOT =       4386.947031  meter/sec      RA   =          191.03404  deg
     ZDOT =      -4320.398670                 TA   =           53.64689
                                              MA   =           53.48310
                                              Ha   =            222.942  n.mi
                                              Hp   =            212.266
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17542125.49                 X    =         5350204.29
     Y    =       -6354387.72  feet           Y    =        -1877006.61  meter
     Z    =       12087525.06                 Z    =         3710258.74
     XDOT =      15026.270518                 XDOT =        4551.596963
     YDOT =      14392.870836  feet/sec       YDOT =        4438.004980  meter/sec
     ZDOT =     -14174.536318                 ZDOT =       -4298.219660
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17226554.84                 X    =        -5250653.91
     Y    =       -6968027.16  feet           Y    =        -2123854.68  meter
     Z    =       12202666.84                 Z    =         3719372.85
     XDOT =      -2107.959652                 XDOT =        -642.506102
     YDOT =     -19555.758201  feet/sec       YDOT =       -5960.595100  meter/sec
     ZDOT =     -14077.099769                 ZDOT =       -4290.700009
  
  
    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   17209.57478301  .00016717  00000-0  10270-3 0  9078
    2 25544  51.6368 192.0158 0006105  77.4529 282.7306 15.54240445 28184
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17209.57478301   =   yrday.fracday
    Element set:     907
    Inclination:       51.6368  deg
    RA of node:       192.0158  deg
    Eccentricity:     .0006105     
    Arg of perigee:    77.4529  deg
    Mean anomaly:     282.7306  deg
    Mean motion:   15.54240445  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2818
    Checksum:              316
 
 
    Coasting Arc #9 (Orbit 2818)
    ---------------------------------------
 
    Vector Time (GMT): 2017/209/14:48:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3163345.08                 A    =         6780994.14  meter
     Y    =        4125352.02  meter          E    =           .0014806
     Z    =       -4368767.72                 I    =           51.55657
     XDOT =      -6681.367353                 Wp   =           73.27482
     YDOT =       1505.055882  meter/sec      RA   =          190.67424  deg
     ZDOT =      -3422.123972                 TA   =          161.95321
                                              MA   =          161.90059
                                              Ha   =            223.051  n.mi
                                              Hp   =            212.328
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10378428.73                 X    =         3138200.26
     Y    =       13534619.49  feet           Y    =         4160586.15  meter
     Z    =      -14333227.44                 Z    =        -4353462.40
     XDOT =     -21920.496565                 XDOT =       -6681.077928
     YDOT =       4937.847381  feet/sec       YDOT =        1430.341947  meter/sec
     ZDOT =     -11227.440854                 ZDOT =       -3454.578849
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7320196.10                 X    =        -2231195.77
     Y    =      -15467094.36  feet           Y    =        -4714370.36  meter
     Z    =      -14266143.04                 Z    =        -4348320.40
     XDOT =      21269.142362                 XDOT =        6482.834592
     YDOT =        405.444082  feet/sec       YDOT =         123.579356  meter/sec
     ZDOT =     -11371.144363                 ZDOT =       -3465.924802
  
  
    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   17209.63908114  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6386 191.6952 0006155  77.5438 282.6403 15.54245131 28191
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17209.63908114   =   yrday.fracday
    Element set:     908
    Inclination:       51.6386  deg
    RA of node:       191.6952  deg
    Eccentricity:     .0006155     
    Arg of perigee:    77.5438  deg
    Mean anomaly:     282.6403  deg
    Mean motion:   15.54245131  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2819
    Checksum:              321
 
 
    Coasting Arc #10 (Orbit 2819)
    ---------------------------------------
 
    Vector Time (GMT): 2017/209/15:41:14.000
    Vector Time (MET): N/A
    Weight (LBS)     : 887043.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -154485.05                 A    =         6777175.02  meter
     Y    =       -4270533.57  meter          E    =           .0008709
     Z    =        5252650.15                 I    =           51.54583
     XDOT =       7595.491970                 Wp   =           93.31354
     YDOT =        739.548121  meter/sec      RA   =          190.47406  deg
     ZDOT =        822.989615                 TA   =          348.80728
                                              MA   =          348.82664
                                              Ha   =            222.925  n.mi
                                              Hp   =            212.303
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -506840.70                 X    =         -132233.80
     Y    =      -14010936.91  feet           Y    =        -4272136.77  meter
     Z    =       17233104.17                 Z    =         5251953.72
     XDOT =      24919.593079                 XDOT =        7582.660009
     YDOT =       2426.338980  feet/sec       YDOT =         824.414317  meter/sec
     ZDOT =       2700.097163                 ZDOT =         859.854535
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         849241.40                 X    =          258848.78
     Y    =       13997403.87  feet           Y    =         4266408.70  meter
     Z    =       17230629.53                 Z    =         5251895.88
     XDOT =     -23917.108663                 XDOT =       -7289.934720
     YDOT =      -2079.961734  feet/sec       YDOT =        -633.972337  meter/sec
     ZDOT =       2862.981448                 ZDOT =         872.636745
  
  
    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   17209.70337756  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6390 191.3758 0005935  77.8849 282.2969 15.54272239 28205
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17209.70337756   =   yrday.fracday
    Element set:     909
    Inclination:       51.6390  deg
    RA of node:       191.3758  deg
    Eccentricity:     .0005935     
    Arg of perigee:    77.8849  deg
    Mean anomaly:     282.2969  deg
    Mean motion:   15.54272239  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2820
    Checksum:              352
 
 
    Coasting Arc #11 (Orbit 2822)
    ---------------------------------------
 
    Vector Time (GMT): 2017/209/20:00:20.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902274.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6481982.78                 A    =         6788661.00  meter
     Y    =       -1791598.39  meter          E    =           .0018931
     Z    =         867979.57                 I    =           51.59052
     XDOT =       2029.025788                 Wp   =           61.80372
     YDOT =      -4425.020380  meter/sec      RA   =          189.57714  deg
     ZDOT =       5929.076940                 TA   =          307.59812
                                              MA   =          307.76984
                                              Ha   =            222.940  n.mi
                                              Hp   =            212.347
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21266347.70                 X    =        -6465683.07
     Y    =       -5877947.46  feet           Y    =        -1863993.20  meter
     Z    =        2847701.99                 Z    =          836532.05
     XDOT =       6656.908754                 XDOT =        2049.556537
     YDOT =     -14517.783398  feet/sec       YDOT =       -4402.215710  meter/sec
     ZDOT =      19452.352165                 ZDOT =        5938.983012
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14058975.74                 X    =         4285175.81
     Y    =      -17027160.52  feet           Y    =        -5189878.53  meter
     Z    =        2708915.48                 Z    =          825677.44
     XDOT =       9341.264442                 XDOT =        2847.217402
     YDOT =      10863.971961  feet/sec       YDOT =        3311.338654  meter/sec
     ZDOT =      19496.775955                 ZDOT =        5942.617311
  
  
    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   17209.89626931  .00016717  00000-0  10270-3 0  9101
    2 25544  51.6397 190.4142 0005927  78.5958 281.5860 15.54260815 28231
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17209.89626931   =   yrday.fracday
    Element set:     910
    Inclination:       51.6397  deg
    RA of node:       190.4142  deg
    Eccentricity:     .0005927     
    Arg of perigee:    78.5958  deg
    Mean anomaly:     281.5860  deg
    Mean motion:   15.54260815  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2823
    Checksum:              336
 
 
    Coasting Arc #12 (Orbit 2837)
    ---------------------------------------
 
    Vector Time (GMT): 2017/210/20:00:20.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902274.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5773710.33                 A    =         6786350.91  meter
     Y    =        2494002.14  meter          E    =           .0010099
     Z    =       -2553556.24                 I    =           51.61484
     XDOT =      -3993.767253                 Wp   =          105.02860
     YDOT =       3868.375870  meter/sec      RA   =          184.60073  deg
     ZDOT =      -5271.930179                 TA   =          103.65171
                                              MA   =          103.53923
                                              Ha   =            222.987  n.mi
                                              Hp   =            212.453
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18942619.20                 X    =         5757796.43
     Y    =        8182421.71  feet           Y    =         2558478.76  meter
     Z    =       -8377809.17                 Z    =        -2525548.21
     XDOT =     -13102.910935                 XDOT =       -4011.119426
     YDOT =      12691.521882  feet/sec       YDOT =        3823.617926  meter/sec
     ZDOT =     -17296.358855                 ZDOT =       -5291.372550
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14984617.07                 X    =        -4567311.28
     Y    =       14257982.74  feet           Y    =         4345833.14  meter
     Z    =       -8254314.83                 Z    =        -2515915.16
     XDOT =      -5529.913855                 XDOT =       -1685.517743
     YDOT =     -15836.590980  feet/sec       YDOT =       -4826.992931  meter/sec
     ZDOT =     -17382.875263                 ZDOT =       -5298.300380
  
  
    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   17210.86073212  .00016717  00000-0  10270-3 0  9119
    2 25544  51.6398 185.6051 0005808  81.4375 278.7435 15.54228351 28382
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17210.86073212   =   yrday.fracday
    Element set:     911
    Inclination:       51.6398  deg
    RA of node:       185.6051  deg
    Eccentricity:     .0005808     
    Arg of perigee:    81.4375  deg
    Mean anomaly:     278.7435  deg
    Mean motion:   15.54228351  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2838
    Checksum:              315
 
 
    Coasting Arc #13 (Orbit 2853)
    ---------------------------------------
 
    Vector Time (GMT): 2017/211/20:00:20.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902274.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4603745.60                 A    =         6782635.35  meter
     Y    =       -3065935.55  meter          E    =           .0017069
     Z    =        3911767.59                 I    =           51.63404
     XDOT =       5636.924468                 Wp   =           94.13037
     YDOT =      -3256.123629  meter/sec      RA   =          179.61693  deg
     ZDOT =       4065.523577                 TA   =          313.29808
                                              MA   =          313.44031
                                              Ha   =            223.110  n.mi
                                              Hp   =            212.348
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15104152.23                 X    =        -4588120.63
     Y    =      -10058843.68  feet           Y    =        -3117330.51  meter
     Z    =       12833883.17                 Z    =         3889442.07
     XDOT =      18493.846679                 XDOT =        5653.168198
     YDOT =     -10682.820306  feet/sec       YDOT =       -3192.997001  meter/sec
     ZDOT =      13338.331946                 ZDOT =        4092.945148
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15039484.21                 X    =         4584034.79
     Y    =      -10278282.88  feet           Y    =        -3132820.62  meter
     Z    =       12735584.94                 Z    =         3881806.29
     XDOT =       2208.881462                 XDOT =         673.267070
     YDOT =      19977.716548  feet/sec       YDOT =        6089.208004  meter/sec
     ZDOT =      13460.058779                 ZDOT =        4102.625916
  
  
    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   17211.88948846  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6388 180.4750 0005970  84.1007 276.0826 15.54229812 28548
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17211.88948846   =   yrday.fracday
    Element set:     912
    Inclination:       51.6388  deg
    RA of node:       180.4750  deg
    Eccentricity:     .0005970     
    Arg of perigee:    84.1007  deg
    Mean anomaly:     276.0826  deg
    Mean motion:   15.54229812  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2854
    Checksum:              329
 
 
    Coasting Arc #14 (Orbit 2868)
    ---------------------------------------
 
    Vector Time (GMT): 2017/212/20:00:20.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902274.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3045551.75                 A    =         6778959.01  meter
     Y    =        3597525.69  meter          E    =           .0017550
     Z    =       -4888220.24                 I    =           51.65305
     XDOT =      -6817.479655                 Wp   =           78.45841
     YDOT =       2536.314787  meter/sec      RA   =          174.62509  deg
     ZDOT =      -2384.770607                 TA   =          168.15723
                                              MA   =          168.11591
                                              Ha   =            222.971  n.mi
                                              Hp   =            212.383
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9991967.70                 X    =         3028841.31
     Y    =       11802905.80  feet           Y    =         3631489.87  meter
     Z    =      -16037467.97                 Z    =        -4873466.45
     XDOT =     -22367.059237                 XDOT =       -6833.750755
     YDOT =       8321.242740  feet/sec       YDOT =        2459.986213  meter/sec
     ZDOT =      -7824.050547                 ZDOT =       -2417.926974
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14649715.16                 X    =        -4465233.18
     Y    =        5158136.79  feet           Y    =         1572200.09  meter
     Z    =      -15972722.16                 Z    =        -4868485.72
     XDOT =        668.303707                 XDOT =         203.698970
     YDOT =     -22746.030205  feet/sec       YDOT =       -6932.990006  meter/sec
     ZDOT =      -7971.056139                 ZDOT =       -2429.577911
  
  
    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   17212.85394375  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6373 175.6661 0005905  88.9799 271.2030 15.54250213 28696
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17212.85394375   =   yrday.fracday
    Element set:     913
    Inclination:       51.6373  deg
    RA of node:       175.6661  deg
    Eccentricity:     .0005905     
    Arg of perigee:    88.9799  deg
    Mean anomaly:     271.2030  deg
    Mean motion:   15.54250213  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2869
    Checksum:              328
 
 
    Coasting Arc #15 (Orbit 2870)
    ---------------------------------------
 
    Vector Time (GMT): 2017/212/23:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902274.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2666528.08                 A    =         6779389.85  meter
     Y    =        4059848.94  meter          E    =           .0017171
     Z    =       -4745654.89                 I    =           51.65944
     XDOT =      -7010.007113                 Wp   =          103.92736
     YDOT =      -1420.365636  meter/sec      RA   =          173.89710  deg
     ZDOT =       2727.997711                 TA   =          193.07368
                                              MA   =          193.11824
                                              Ha   =            223.058  n.mi
                                              Hp   =            212.141
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8748451.71                 X    =        -2688676.32
     Y    =       13319714.38  feet           Y    =         4029906.37  meter
     Z    =      -15569733.90                 Z    =        -4758661.59
     XDOT =     -22998.711002                 XDOT =       -7006.854384
     YDOT =      -4659.992244  feet/sec       YDOT =       -1498.738782  meter/sec
     ZDOT =       8950.123723                 ZDOT =        2693.953134
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15830628.28                 X    =        -4825175.50
     Y    =       -1236427.14  feet           Y    =         -376862.99  meter
     Z    =      -15627836.33                 Z    =        -4763364.51
     XDOT =      -7007.445203                 XDOT =       -2135.869298
     YDOT =     -21328.419223  feet/sec       YDOT =       -6500.902179  meter/sec
     ZDOT =       8799.746269                 ZDOT =        2682.162663
  
  
    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   17212.98253952  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6375 175.0220 0006168  93.8960 266.2897 15.54248768 28710
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17212.98253952   =   yrday.fracday
    Element set:     914
    Inclination:       51.6375  deg
    RA of node:       175.0220  deg
    Eccentricity:     .0006168     
    Arg of perigee:    93.8960  deg
    Mean anomaly:     266.2897  deg
    Mean motion:   15.54248768  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2871
    Checksum:              342
 
 
    Coasting Arc #16 (Orbit 2886)
    ---------------------------------------
 
    Vector Time (GMT): 2017/213/23:18:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902274.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4240861.24                 A    =         6783170.66  meter
     Y    =       -3791830.10  meter          E    =           .0017750
     Z    =        3679177.95                 I    =           51.70452
     XDOT =       5878.347627                 Wp   =           89.54773
     YDOT =       2342.498290  meter/sec      RA   =          168.90858  deg
     ZDOT =      -4343.320204                 TA   =           46.66755
                                              MA   =           46.51974
                                              Ha   =            222.992  n.mi
                                              Hp   =            212.240
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13913586.76                 X    =         4265075.82
     Y    =      -12440387.47  feet           Y    =        -3744270.70  meter
     Z    =       12070793.79                 Z    =         3699837.18
     XDOT =      19285.917411                 XDOT =        5872.813838
     YDOT =       7685.361845  feet/sec       YDOT =        2408.203244  meter/sec
     ZDOT =     -14249.738203                 ZDOT =       -4314.778583
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17640134.33                 X    =         5376712.94
     Y    =        5911778.29  feet           Y    =         1801910.02  meter
     Z    =       12162719.18                 Z    =         3707196.81
     XDOT =       3289.862160                 XDOT =        1002.749986
     YDOT =      19363.400721  feet/sec       YDOT =        5901.964540  meter/sec
     ZDOT =     -14123.814358                 ZDOT =       -4304.938616
  
  
    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   17214.01128900  .00016717  00000-0  10270-3 0  9159
    2 25544  51.6376 169.8914 0006140  97.8883 262.2967 15.54239517 28873
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17214.01128900   =   yrday.fracday
    Element set:     915
    Inclination:       51.6376  deg
    RA of node:       169.8914  deg
    Eccentricity:     .0006140     
    Arg of perigee:    97.8883  deg
    Mean anomaly:     262.2967  deg
    Mean motion:   15.54239517  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2887
    Checksum:              336
 
 
    Coasting Arc #17 (Orbit 2896)
    ---------------------------------------
 
    Vector Time (GMT): 2017/214/15:21:40.559
    Vector Time (MET): N/A
    Weight (LBS)     : 902208.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -240723.50                 A    =         6777704.99  meter
     Y    =        4324916.67  meter          E    =           .0019728
     Z    =       -5230254.18                 I    =           51.70986
     XDOT =      -7501.533706                 Wp   =           97.82902
     YDOT =        982.033503  meter/sec      RA   =          165.59866  deg
     ZDOT =       1158.431676                 TA   =          183.28297
                                              MA   =          183.29593
                                              Ha   =            222.975  n.mi
                                              Hp   =            212.598
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -789775.25                 X    =         -263662.21
     Y    =       14189359.14  feet           Y    =         4322096.76  meter
     Z    =      -17159626.58                 Z    =        -5231479.01
     XDOT =     -24611.331055                 XDOT =       -7517.584574
     YDOT =       3221.894695  feet/sec       YDOT =         898.056446  meter/sec
     ZDOT =       3800.628859                 ZDOT =        1121.952975
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         438431.75                 X    =          133634.00
     Y    =      -14197265.31  feet           Y    =        -4327326.47  meter
     Z    =      -17165659.83                 Z    =        -5232093.12
     XDOT =      23542.669267                 XDOT =        7175.805592
     YDOT =      -3668.488414  feet/sec       YDOT =       -1118.155269  meter/sec
     ZDOT =       3639.107871                 ZDOT =        1109.200079
  
  
    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   17214.65425443  .00016717  00000-0  10270-3 0  9162
    2 25544  51.6409 166.6910 0005504  94.4224 265.7557 15.54150308 28970
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17214.65425443   =   yrday.fracday
    Element set:     916
    Inclination:       51.6409  deg
    RA of node:       166.6910  deg
    Eccentricity:     .0005504     
    Arg of perigee:    94.4224  deg
    Mean anomaly:     265.7557  deg
    Mean motion:   15.54150308  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2897
    Checksum:              316
 
 
    Coasting Arc #18 (Orbit 2912)
    ---------------------------------------
 
    Vector Time (GMT): 2017/215/15:21:40.559
    Vector Time (MET): N/A
    Weight (LBS)     : 902208.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1970289.66                 A    =         6780091.51  meter
     Y    =       -4550125.28  meter          E    =           .0013263
     Z    =        4614424.36                 I    =           51.74899
     XDOT =       7067.197937                 Wp   =           78.11160
     YDOT =         14.363638  meter/sec      RA   =          160.60889  deg
     ZDOT =      -2993.489698                 TA   =           41.71806
                                              MA   =           41.61699
                                              Ha   =            222.884  n.mi
                                              Hp   =            212.596
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6464204.91                 X    =         1998609.59
     Y    =      -14928232.56  feet           Y    =        -4527934.10  meter
     Z    =       15139187.53                 Z    =         4624063.81
     XDOT =      23186.344938                 XDOT =        7081.052801
     YDOT =         47.124795  feet/sec       YDOT =          93.471494  meter/sec
     ZDOT =      -9821.160428                 ZDOT =       -2959.126201
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5853242.06                 X    =        -1784068.18
     Y    =       15134883.93  feet           Y    =         4613112.62  meter
     Z    =       15182487.20                 Z    =         4627622.10
     XDOT =     -22134.616266                 XDOT =       -6746.631038
     YDOT =       1171.821351  feet/sec       YDOT =         357.171148  meter/sec
     ZDOT =      -9669.116767                 ZDOT =       -2947.146791
  
  
    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   17215.68307736  .00016717  00000-0  10270-3 0  9171
    2 25544  51.6404 161.5627 0005476  97.2660 262.9116 15.54174593 29138
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17215.68307736   =   yrday.fracday
    Element set:     917
    Inclination:       51.6404  deg
    RA of node:       161.5627  deg
    Eccentricity:     .0005476     
    Arg of perigee:    97.2660  deg
    Mean anomaly:     262.9116  deg
    Mean motion:   15.54174593  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2913
    Checksum:              323
 
 
    Coasting Arc #19 (Orbit 2919)
    ---------------------------------------
 
    Vector Time (GMT): 2017/216/02:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902208.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         900147.22                 A    =         6777441.51  meter
     Y    =        4143017.09  meter          E    =           .0020053
     Z    =       -5305016.88                 I    =           51.75384
     XDOT =      -7251.483782                 Wp   =           97.42032
     YDOT =       2368.646693  meter/sec      RA   =          158.24434  deg
     ZDOT =        618.884574                 TA   =          178.49246
                                              MA   =          178.48640
                                              Ha   =            222.932  n.mi
                                              Hp   =            212.733
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2953238.91                 X    =          879520.83
     Y    =       13592575.74  feet           Y    =         4152968.14  meter
     Z    =      -17404911.01                 Z    =        -5300694.15
     XDOT =     -23790.957291                 XDOT =       -7280.437871
     YDOT =       7771.150566  feet/sec       YDOT =        2287.393744  meter/sec
     ZDOT =       2030.461202                 ZDOT =         583.589400
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1750970.97                 X    =          533695.95
     Y    =       13822399.86  feet           Y    =         4213067.48  meter
     Z    =      -17386374.71                 Z    =        -5299367.01
     XDOT =     -23430.828593                 XDOT =       -7141.716555
     YDOT =       5327.394216  feet/sec       YDOT =        1623.789757  meter/sec
     ZDOT =       1873.944260                 ZDOT =         571.178211
  
  
    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   17216.13318632  .00016717  00000-0  10270-3 0  9180
    2 25544  51.6399 159.3162 0005404 103.9654 256.2100 15.54138363 29201
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17216.13318632   =   yrday.fracday
    Element set:     918
    Inclination:       51.6399  deg
    RA of node:       159.3162  deg
    Eccentricity:     .0005404     
    Arg of perigee:   103.9654  deg
    Mean anomaly:     256.2100  deg
    Mean motion:   15.54138363  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2920
    Checksum:              295
 
 
    Coasting Arc #20 (Orbit 2935)
    ---------------------------------------
 
    Vector Time (GMT): 2017/217/02:50:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902208.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         804180.15                 A    =         6779172.33  meter
     Y    =       -4670339.92  meter          E    =           .0011328
     Z    =        4838617.86                 I    =           51.79129
     XDOT =       7121.808748                 Wp   =           80.46149
     YDOT =      -1378.612673  meter/sec      RA   =          153.25514  deg
     ZDOT =      -2507.490111                 TA   =           34.14311
                                              MA   =           34.07030
                                              Ha   =            222.796  n.mi
                                              Hp   =            212.698
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2638386.32                 X    =          832842.10
     Y    =      -15322637.52  feet           Y    =        -4661187.04  meter
     Z    =       15874730.51                 Z    =         4842593.60
     XDOT =      23365.514264                 XDOT =        7148.875414
     YDOT =      -4523.007457  feet/sec       YDOT =       -1298.820287  meter/sec
     ZDOT =      -8226.673592                 ZDOT =       -2472.829466
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3731795.04                 X    =         1137451.13
     Y    =      -15074409.46  feet           Y    =        -4594680.00  meter
     Z    =       15892993.95                 Z    =         4844184.56
     XDOT =      22602.938269                 XDOT =        6889.375584
     YDOT =      -2939.508924  feet/sec       YDOT =        -895.962320  meter/sec
     ZDOT =      -8073.083260                 ZDOT =       -2460.675778
  
  
    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   17217.16200342  .00016717  00000-0  10270-3 0  9193
    2 25544  51.6410 154.1870 0005300 107.5744 252.5988 15.54189748 29362
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17217.16200342   =   yrday.fracday
    Element set:     919
    Inclination:       51.6410  deg
    RA of node:       154.1870  deg
    Eccentricity:     .0005300     
    Arg of perigee:   107.5744  deg
    Mean anomaly:     252.5988  deg
    Mean motion:   15.54189748  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2936
    Checksum:              309
 
             

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