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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15846.6289
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   84.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.315
   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 
   ------------------------------------------------------------------------
   049/15:01:32.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.9  
   000/00:00:00.000           0.0               0.0              214.9  
   
   051/14:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.7  
   000/00:00:00.000           0.0               0.0              215.3  
   
   052/02:02:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.6  
   000/00:00:00.000           0.0               0.0              215.2  
   
   053/05:58:33.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.3  
   000/00:00:00.000           0.0               0.0              215.5  
   
   055/08:36:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.8  
   000/00:00:00.000           0.0               0.0              215.8  
   
   060/07:22:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              218.8  
   000/00:00:00.000           0.0               0.0              216.5  
   
   061/03:37:23.178          -1.4               2.3              2.3    
   N/A                       -1.6              -0.0              218.9  
   000/00:00:46.356           0.8              -0.0              217.8  
   
 
 
    Coasting Arc #1 (Orbit 314)
    ---------------------------------------
 
    Vector Time (GMT): 2017/048/13:30:01.593
    Vector Time (MET): N/A
    Weight (LBS)     : 886584.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         985820.09                 A    =         6788403.22  meter
     Y    =       -6680572.62  meter          E    =           .0007935
     Z    =         672801.00                 I    =           51.28716
     XDOT =       4678.892136                 Wp   =           74.94014
     YDOT =       1293.561306  meter/sec      RA   =          273.81398  deg
     ZDOT =       5931.953193                 TA   =          292.35934
                                              MA   =          292.44341
                                              Ha   =            221.073  n.mi
                                              Hp   =            214.885
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3234317.88                 X    =         1057182.61
     Y    =      -21917889.16  feet           Y    =        -6669149.44  meter
     Z    =        2207352.36                 Z    =          677763.64
     XDOT =      15350.695984                 XDOT =        4635.265216
     YDOT =       4243.967541  feet/sec       YDOT =        1345.640393  meter/sec
     ZDOT =      19461.788691                 ZDOT =        5954.575507
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7209795.54                 X    =         2197545.68
     Y    =      -20946880.13  feet           Y    =        -6384609.06  meter
     Z    =        2230278.61                 Z    =          679788.92
     XDOT =      12651.094132                 XDOT =        3856.053491
     YDOT =       6456.753600  feet/sec       YDOT =        1968.018497  meter/sec
     ZDOT =      19560.913563                 ZDOT =        5962.166454
  
  
    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   17048.62550062  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6397 274.3297 0006629 205.0053 155.0780 15.54379031  3158
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17048.62550062   =   yrday.fracday
    Element set:     900
    Inclination:       51.6397  deg
    RA of node:       274.3297  deg
    Eccentricity:     .0006629     
    Arg of perigee:   205.0053  deg
    Mean anomaly:     155.0780  deg
    Mean motion:   15.54379031  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             315
    Checksum:              295
 
 
    Coasting Arc #2 (Orbit 329)
    ---------------------------------------
 
    Vector Time (GMT): 2017/049/13:30:01.593
    Vector Time (MET): N/A
    Weight (LBS)     : 886584.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1799212.46                 A    =         6786114.56  meter
     Y    =        6080989.09  meter          E    =           .0009561
     Z    =       -2400372.35                 I    =           51.27772
     XDOT =      -4347.841226                 Wp   =          174.12564
     YDOT =      -3387.546129  meter/sec      RA   =          268.81493  deg
     ZDOT =      -5334.130734                 TA   =           32.85829
                                              MA   =           32.79888
                                              Ha   =            220.848  n.mi
                                              Hp   =            215.033
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5902928.03                 X    =        -1855418.22
     Y    =       19950751.62  feet           Y    =         6060554.65  meter
     Z    =       -7875237.37                 Z    =        -2409249.23
     XDOT =     -14264.570951                 XDOT =       -4283.727328
     YDOT =     -11113.996485  feet/sec       YDOT =       -3435.808527  meter/sec
     ZDOT =     -17500.428917                 ZDOT =       -5355.095026
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9113001.11                 X    =        -2777642.74
     Y    =       18686855.71  feet           Y    =         5695753.62  meter
     Z    =       -7915241.49                 Z    =        -2412565.61
     XDOT =     -10724.152513                 XDOT =       -3268.721686
     YDOT =     -12665.767620  feet/sec       YDOT =       -3860.525970  meter/sec
     ZDOT =     -17591.925958                 ZDOT =       -5362.019032
  
  
    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   17049.58987389  .00016717  00000-0  10270-3 0  9016
    2 25544  51.6390 269.5201 0006508 208.2929 151.7871 15.54384114  3304
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17049.58987389   =   yrday.fracday
    Element set:     901
    Inclination:       51.6390  deg
    RA of node:       269.5201  deg
    Eccentricity:     .0006508     
    Arg of perigee:   208.2929  deg
    Mean anomaly:     151.7871  deg
    Mean motion:   15.54384114  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             330
    Checksum:              324
 
 
    Coasting Arc #3 (Orbit 330)
    ---------------------------------------
 
    Vector Time (GMT): 2017/049/15:01:32.000
    Vector Time (MET): N/A
    Weight (LBS)     : 886584.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1479298.27                 A    =         6786709.31  meter
     Y    =        6291068.94  meter          E    =           .0010912
     Z    =       -2051017.60                 I    =           51.27962
     XDOT =      -4500.676511                 Wp   =          172.63125
     YDOT =      -2852.773059  meter/sec      RA   =          268.49174  deg
     ZDOT =      -5518.067694                 TA   =           30.18098
                                              MA   =           30.11817
                                              Ha   =            220.890  n.mi
                                              Hp   =            214.908
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4853340.79                 X    =        -1539573.95
     Y    =       20639989.97  feet           Y    =         6274189.26  meter
     Z    =       -6729060.35                 Z    =        -2058350.35
     XDOT =     -14765.999051                 XDOT =       -4441.637759
     YDOT =      -9359.491663  feet/sec       YDOT =       -2902.772951  meter/sec
     ZDOT =     -18103.896634                 ZDOT =       -5539.786771
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =          63645.19                 X    =           19399.06
     Y    =       21192247.66  feet           Y    =         6459397.09  meter
     Z    =       -6762317.96                 Z    =        -2061154.52
     XDOT =     -14862.052232                 XDOT =       -4529.953520
     YDOT =      -5748.014192  feet/sec       YDOT =       -1751.994726  meter/sec
     ZDOT =     -18198.798666                 ZDOT =       -5546.993833
  
  
    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   17049.65416595  .00016717  00000-0  10270-3 0  9021
    2 25544  51.6386 269.1972 0006528 206.2614 153.8209 15.54409249  3317
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17049.65416595   =   yrday.fracday
    Element set:     902
    Inclination:       51.6386  deg
    RA of node:       269.1972  deg
    Eccentricity:     .0006528     
    Arg of perigee:   206.2614  deg
    Mean anomaly:     153.8209  deg
    Mean motion:   15.54409249  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             331
    Checksum:              322
 
 
    Coasting Arc #4 (Orbit 346)
    ---------------------------------------
 
    Vector Time (GMT): 2017/050/15:01:32.000
    Vector Time (MET): N/A
    Weight (LBS)     : 886584.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2260643.37                 A    =         6783132.60  meter
     Y    =       -5317083.33  meter          E    =           .0010890
     Z    =        3552420.80                 I    =           51.26818
     XDOT =       4112.996717                 Wp   =          126.90785
     YDOT =       4717.482343  meter/sec      RA   =          263.48583  deg
     ZDOT =       4427.642201                 TA   =          275.26925
                                              MA   =          275.39350
                                              Ha   =            220.903  n.mi
                                              Hp   =            215.043
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7416808.97                 X    =         2302676.63
     Y    =      -17444499.13  feet           Y    =        -5291568.05  meter
     Z    =       11654923.88                 Z    =         3563504.61
     XDOT =      13494.083718                 XDOT =        4038.431836
     YDOT =      15477.304276  feet/sec       YDOT =        4763.060010  meter/sec
     ZDOT =      14526.385175                 ZDOT =        4447.440248
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2813050.76                 X    =          857417.87
     Y    =      -18714931.56  feet           Y    =        -5704311.14  meter
     Z    =       11704483.66                 Z    =         3567526.62
     XDOT =      15437.421102                 XDOT =        4705.325952
     YDOT =      11491.651632  feet/sec       YDOT =        3502.655417  meter/sec
     ZDOT =      14612.550484                 ZDOT =        4453.905387
  
  
    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   17050.68282719  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6374 264.0670 0006822 209.6159 150.4609 15.54404931  3478
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17050.68282719   =   yrday.fracday
    Element set:     903
    Inclination:       51.6374  deg
    RA of node:       264.0670  deg
    Eccentricity:     .0006822     
    Arg of perigee:   209.6159  deg
    Mean anomaly:     150.4609  deg
    Mean motion:   15.54404931  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             347
    Checksum:              308
 
 
    Coasting Arc #5 (Orbit 361)
    ---------------------------------------
 
    Vector Time (GMT): 2017/051/14:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 908298.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1150420.14                 A    =         6788529.51  meter
     Y    =       -6684188.07  meter          E    =           .0006195
     Z    =         231811.39                 I    =           51.29082
     XDOT =       4762.121575                 Wp   =           62.52446
     YDOT =       -608.206679  meter/sec      RA   =          258.66489  deg
     ZDOT =       5975.405848                 TA   =          299.98440
                                              MA   =          300.04588
                                              Ha   =            220.739  n.mi
                                              Hp   =            215.292
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3774344.31                 X    =        -1076716.33
     Y    =      -21929750.88  feet           Y    =        -6696640.73  meter
     Z    =         760536.04                 Z    =          226402.46
     XDOT =      15623.758447                 XDOT =        4739.543536
     YDOT =      -1995.428736  feet/sec       YDOT =        -555.079322  meter/sec
     ZDOT =      19604.349894                 ZDOT =        5998.483668
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3716034.75                 X    =        -1132647.39
     Y    =      -21940480.56  feet           Y    =        -6687458.47  meter
     Z    =         737876.93                 Z    =          224904.89
     XDOT =      13901.572373                 XDOT =        4237.199259
     YDOT =      -1678.080437  feet/sec       YDOT =        -511.478917  meter/sec
     ZDOT =      19705.807458                 ZDOT =        6006.330113
  
  
    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   17051.64719411  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6376 259.2585 0006720 214.2762 145.7958 15.54395363  3629
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17051.64719411   =   yrday.fracday
    Element set:     904
    Inclination:       51.6376  deg
    RA of node:       259.2585  deg
    Eccentricity:     .0006720     
    Arg of perigee:   214.2762  deg
    Mean anomaly:     145.7958  deg
    Mean motion:   15.54395363  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             362
    Checksum:              321
 
 
    Coasting Arc #6 (Orbit 368)
    ---------------------------------------
 
    Vector Time (GMT): 2017/052/02:02:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 908298.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4430349.45                 A    =         6778045.42  meter
     Y    =       -1318152.15  meter          E    =           .0012024
     Z    =       -4967537.56                 I    =           51.26004
     XDOT =       -119.440669                 Wp   =          135.32132
     YDOT =      -7377.452352  meter/sec      RA   =          256.13629  deg
     ZDOT =       2058.805038                 TA   =          154.86364
                                              MA   =          154.80506
                                              Ha   =            220.608  n.mi
                                              Hp   =            215.228
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14535267.21                 X    =        -4391150.72
     Y    =       -4324646.18  feet           Y    =        -1367476.41  meter
     Z    =      -16297695.41                 Z    =        -4988963.26
     XDOT =       -391.865712                 XDOT =         -46.935739
     YDOT =     -24204.240000  feet/sec       YDOT =       -7378.382505  meter/sec
     ZDOT =       6754.609704                 ZDOT =        2058.401348
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14489963.36                 X    =         4416540.83
     Y    =        4116834.22  feet           Y    =         1254811.07  meter
     Z    =      -16391585.38                 Z    =        -4996155.22
     XDOT =       1086.230268                 XDOT =         331.082986
     YDOT =      23138.181557  feet/sec       YDOT =        7052.517739  meter/sec
     ZDOT =       6754.039745                 ZDOT =        2058.631314
  
  
    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   17052.09723046  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6387 257.0177 0006419 215.8077 144.2647 15.54375448  3693
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17052.09723046   =   yrday.fracday
    Element set:     905
    Inclination:       51.6387  deg
    RA of node:       257.0177  deg
    Eccentricity:     .0006419     
    Arg of perigee:   215.8077  deg
    Mean anomaly:     144.2647  deg
    Mean motion:   15.54375448  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             369
    Checksum:              325
 
 
    Coasting Arc #7 (Orbit 384)
    ---------------------------------------
 
    Vector Time (GMT): 2017/053/02:02:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 908298.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4486601.52                 A    =         6781375.47  meter
     Y    =        3044544.39  meter          E    =           .0006554
     Z    =        4065818.76                 I    =           51.27954
     XDOT =       -992.534925                 Wp   =          111.78824
     YDOT =       6575.050799  meter/sec      RA   =          251.11577  deg
     ZDOT =      -3825.657297                 TA   =           17.95317
                                              MA   =           17.93003
                                              Ha   =            220.227  n.mi
                                              Hp   =            215.559
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14719821.27                 X    =         4432473.75
     Y    =        9988662.68  feet           Y    =         3094414.17  meter
     Z    =       13339300.39                 Z    =         4087481.29
     XDOT =      -3256.348180                 XDOT =       -1047.402210
     YDOT =      21571.688973  feet/sec       YDOT =        6563.644607  meter/sec
     ZDOT =     -12551.369086                 ZDOT =       -3830.612279
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14941696.41                 X    =        -4554229.07
     Y    =       -9521439.44  feet           Y    =        -2902134.74  meter
     Z    =       13433962.73                 Z    =         4094671.84
     XDOT =       1795.566286                 XDOT =         547.288604
     YDOT =     -20570.735103  feet/sec       YDOT =       -6269.960060  meter/sec
     ZDOT =     -12574.191739                 ZDOT =       -3832.613642
  
  
    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   17053.12588138  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6380 251.8878 0006380 221.2173 138.8499 15.54415061  3859
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17053.12588138   =   yrday.fracday
    Element set:     906
    Inclination:       51.6380  deg
    RA of node:       251.8878  deg
    Eccentricity:     .0006380     
    Arg of perigee:   221.2173  deg
    Mean anomaly:     138.8499  deg
    Mean motion:   15.54415061  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             385
    Checksum:              318
 
 
    Coasting Arc #8 (Orbit 386)
    ---------------------------------------
 
    Vector Time (GMT): 2017/053/05:58:33.000
    Vector Time (MET): N/A
    Weight (LBS)     : 908298.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3996037.82                 A    =         6785432.96  meter
     Y    =       -4785135.26  meter          E    =           .0001986
     Z    =       -2681613.91                 I    =           51.29648
     XDOT =       2581.346699                 Wp   =          185.59401
     YDOT =      -5046.771816  meter/sec      RA   =          250.29552  deg
     ZDOT =       5156.690778                 TA   =          143.98612
                                              MA   =          143.97274
                                              Ha   =            220.340  n.mi
                                              Hp   =            215.548
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13110360.29                 X    =        -3929206.45
     Y    =      -15699262.68  feet           Y    =        -4829448.13  meter
     Z    =       -8797945.89                 Z    =        -2700862.51
     XDOT =       8468.985232                 XDOT =        2612.540895
     YDOT =     -16557.650314  feet/sec       YDOT =       -5017.730743  meter/sec
     ZDOT =      16918.276832                 ZDOT =        5169.306006
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20052072.68                 X    =         6111871.75
     Y    =       -3844676.75  feet           Y    =        -1171857.47  meter
     Z    =       -8881727.85                 Z    =        -2707150.65
     XDOT =      10178.162231                 XDOT =        3102.303848
     YDOT =      13854.218326  feet/sec       YDOT =        4222.765746  meter/sec
     ZDOT =      16974.499845                 ZDOT =        5173.827553
  
  
    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   17053.25446402  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6398 251.2469 0006317 222.1591 137.9076 15.54399414  3878
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17053.25446402   =   yrday.fracday
    Element set:     907
    Inclination:       51.6398  deg
    RA of node:       251.2469  deg
    Eccentricity:     .0006317     
    Arg of perigee:   222.1591  deg
    Mean anomaly:     137.9076  deg
    Mean motion:   15.54399414  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             387
    Checksum:              319
 
 
    Coasting Arc #9 (Orbit 402)
    ---------------------------------------
 
    Vector Time (GMT): 2017/054/05:58:33.000
    Vector Time (MET): N/A
    Weight (LBS)     : 908298.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3501657.85                 A    =         6788117.60  meter
     Y    =        5720224.76  meter          E    =           .0013768
     Z    =         987623.83                 I    =           51.31766
     XDOT =      -3680.123508                 Wp   =          151.16834
     YDOT =       3272.578361  meter/sec      RA   =          245.29781  deg
     ZDOT =      -5883.979161                 TA   =           18.07577
                                              MA   =           18.02687
                                              Ha   =            220.144  n.mi
                                              Hp   =            215.763
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11488378.77                 X    =         3432635.26
     Y    =       18767141.60  feet           Y    =         5758996.80  meter
     Z    =        3240235.68                 Z    =         1004465.45
     XDOT =     -12073.896025                 XDOT =       -3687.863870
     YDOT =      10736.805646  feet/sec       YDOT =        3231.381063  meter/sec
     ZDOT =     -19304.393574                 ZDOT =       -5901.874739
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21951786.80                 X    =        -6690904.62
     Y    =        1352250.85  feet           Y    =          412166.06  meter
     Z    =        3313314.31                 Z    =         1009898.20
     XDOT =      -3797.841927                 XDOT =       -1157.582219
     YDOT =     -13981.747935  feet/sec       YDOT =       -4261.636771  meter/sec
     ZDOT =     -19383.524547                 ZDOT =       -5908.098282
  
  
    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   17054.28311235  .00016717  00000-0  10270-3 0  9087
    2 25544  51.6402 246.1174 0006362 225.8342 134.2288 15.54397900  4036
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17054.28311235   =   yrday.fracday
    Element set:     908
    Inclination:       51.6402  deg
    RA of node:       246.1174  deg
    Eccentricity:     .0006362     
    Arg of perigee:   225.8342  deg
    Mean anomaly:     134.2288  deg
    Mean motion:   15.54397900  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             403
    Checksum:              287
 
 
    Coasting Arc #10 (Orbit 418)
    ---------------------------------------
 
    Vector Time (GMT): 2017/055/05:58:33.000
    Vector Time (MET): N/A
    Weight (LBS)     : 908298.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2759145.21                 A    =         6788254.94  meter
     Y    =       -6145635.23  meter          E    =           .0007005
     Z    =         809416.98                 I    =           51.33247
     XDOT =       4693.966125                 Wp   =           56.40591
     YDOT =      -1323.971180  meter/sec      RA   =          240.30440  deg
     ZDOT =       5915.104279                 TA   =          312.38260
                                              MA   =          312.44187
                                              Ha   =            219.997  n.mi
                                              Hp   =            215.959
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9052313.69                 X    =        -2694149.73
     Y    =      -20162845.23  feet           Y    =        -6176126.37  meter
     Z    =        2655567.52                 Z    =          796172.55
     XDOT =      15400.151329                 XDOT =        4679.690167
     YDOT =      -4343.737468  feet/sec       YDOT =       -1271.559415  meter/sec
     ZDOT =      19406.510103                 ZDOT =        5937.871075
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       22084024.95                 X    =         6731210.80
     Y    =        1039822.46  feet           Y    =          316937.89  meter
     Z    =        2598338.17                 Z    =          791973.48
     XDOT =      -2966.187356                 XDOT =        -904.093906
     YDOT =      13974.174821  feet/sec       YDOT =        4259.328485  meter/sec
     ZDOT =      19506.736570                 ZDOT =        5945.653306
  
  
    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   17055.31175635  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6401 240.9871 0006346 230.7652 129.2938 15.54406377  4194
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17055.31175635   =   yrday.fracday
    Element set:     909
    Inclination:       51.6401  deg
    RA of node:       240.9871  deg
    Eccentricity:     .0006346     
    Arg of perigee:   230.7652  deg
    Mean anomaly:     129.2938  deg
    Mean motion:   15.54406377  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             419
    Checksum:              313
 
 
    Coasting Arc #11 (Orbit 419)
    ---------------------------------------
 
    Vector Time (GMT): 2017/055/08:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922731.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3095573.60                 A    =         6776744.34  meter
     Y    =        3010935.61  meter          E    =           .0009496
     Z    =       -5230376.53                 I    =           51.29707
     XDOT =      -4450.690412                 Wp   =          103.17222
     YDOT =      -6169.191995  meter/sec      RA   =          239.75748  deg
     ZDOT =       -920.796360                 TA   =          157.99041
                                              MA   =          157.94960
                                              Ha   =            219.822  n.mi
                                              Hp   =            215.849
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10156081.36                 X    =        -3103606.52
     Y    =        9878397.68  feet           Y    =         2976273.46  meter
     Z    =      -17160027.97                 Z    =        -5245433.31
     XDOT =     -14602.002664                 XDOT =       -4376.901441
     YDOT =     -20240.131217  feet/sec       YDOT =       -6218.550119  meter/sec
     ZDOT =      -3020.985434                 ZDOT =        -942.236245
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11824168.08                 X    =        -3604006.43
     Y    =       -7656829.82  feet           Y    =        -2333801.73  meter
     Z    =      -17226644.93                 Z    =        -5250681.37
     XDOT =      16028.059454                 XDOT =        4885.352522
     YDOT =     -17771.087195  feet/sec       YDOT =       -5416.627377  meter/sec
     ZDOT =      -3114.218424                 ZDOT =        -949.213775
  
  
    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   17055.37604442  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6411 240.6672 0006412 231.9395 128.1179 15.54439353  4209
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17055.37604442   =   yrday.fracday
    Element set:     910
    Inclination:       51.6411  deg
    RA of node:       240.6672  deg
    Eccentricity:     .0006412     
    Arg of perigee:   231.9395  deg
    Mean anomaly:     128.1179  deg
    Mean motion:   15.54439353  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             420
    Checksum:              289
 
 
    Coasting Arc #12 (Orbit 435)
    ---------------------------------------
 
    Vector Time (GMT): 2017/056/08:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922731.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4128356.43                 A    =         6776818.06  meter
     Y    =       -1370959.38  meter          E    =           .0002641
     Z    =        5198010.85                 I    =           51.31466
     XDOT =       3618.974919                 Wp   =          234.95149
     YDOT =       6667.107859  meter/sec      RA   =          234.73091  deg
     ZDOT =      -1117.721200                 TA   =          225.80017
                                              MA   =          225.82187
                                              Ha   =            219.611  n.mi
                                              Hp   =            216.133
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13544476.49                 X    =         4118131.17
     Y    =       -4497898.21  feet           Y    =        -1324849.95  meter
     Z    =       17053841.38                 Z    =         5218040.01
     XDOT =      11873.277293                 XDOT =        3549.581850
     YDOT =      21873.713447  feet/sec       YDOT =        6707.189566  meter/sec
     ZDOT =      -3667.064305                 ZDOT =       -1100.310938
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7516730.07                 X    =         2291099.33
     Y    =       12006925.36  feet           Y    =         3659710.85  meter
     Z    =       17142052.09                 Z    =         5224897.48
     XDOT =     -17604.187346                 XDOT =       -5365.756303
     YDOT =      16139.617895  feet/sec       YDOT =        4919.355534  meter/sec
     ZDOT =      -3591.589108                 ZDOT =       -1094.716360
  
  
    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   17056.40468250  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6411 235.5368 0006441 236.1023 123.9517 15.54446536  4368
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17056.40468250   =   yrday.fracday
    Element set:     911
    Inclination:       51.6411  deg
    RA of node:       235.5368  deg
    Eccentricity:     .0006441     
    Arg of perigee:   236.1023  deg
    Mean anomaly:     123.9517  deg
    Mean motion:   15.54446536  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             436
    Checksum:              289
 
 
    Coasting Arc #13 (Orbit 450)
    ---------------------------------------
 
    Vector Time (GMT): 2017/057/08:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922731.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5011344.92                 A    =         6779469.62  meter
     Y    =        -263767.42  meter          E    =           .0007816
     Z    =       -4565185.19                 I    =           51.34175
     XDOT =      -2419.847051                 Wp   =          149.46981
     YDOT =      -6607.227633  meter/sec      RA   =          229.70919  deg
     ZDOT =       3033.777979                 TA   =          151.01720
                                              MA   =          150.97378
                                              Ha   =            219.529  n.mi
                                              Hp   =            216.095
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16441420.34                 X    =        -4985847.95
     Y    =        -865378.66  feet           Y    =         -319665.64  meter
     Z    =      -14977641.69                 Z    =        -4589466.31
     XDOT =      -7939.130745                 XDOT =       -2360.519791
     YDOT =     -21677.256015  feet/sec       YDOT =       -6633.955917  meter/sec
     ZDOT =       9953.339825                 ZDOT =        3022.168225
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3260543.80                 X    =         -993813.75
     Y    =      -16038450.80  feet           Y    =        -4888519.80  meter
     Z    =      -15084292.62                 Z    =        -4597692.39
     XDOT =      17806.243732                 XDOT =        5427.343089
     YDOT =     -12947.303740  feet/sec       YDOT =       -3946.338180  meter/sec
     ZDOT =       9903.321103                 ZDOT =        3018.532272
  
  
    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   17057.36902889  .00016717  00000-0  10270-3 0  9125
    2 25544  51.6398 230.7267 0006407 239.7179 120.3341 15.54439662  4515
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17057.36902889   =   yrday.fracday
    Element set:     912
    Inclination:       51.6398  deg
    RA of node:       230.7267  deg
    Eccentricity:     .0006407     
    Arg of perigee:   239.7179  deg
    Mean anomaly:     120.3341  deg
    Mean motion:   15.54439662  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             451
    Checksum:              324
 
 
    Coasting Arc #14 (Orbit 466)
    ---------------------------------------
 
    Vector Time (GMT): 2017/058/08:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922731.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5606896.94                 A    =         6783343.04  meter
     Y    =        1736031.71  meter          E    =           .0007026
     Z    =        3391965.47                 I    =           51.37803
     XDOT =        907.337532                 Wp   =          112.42167
     YDOT =       6069.587269  meter/sec      RA   =          224.70011  deg
     ZDOT =      -4601.267516                 TA   =           27.75457
                                              MA   =           27.71709
                                              Ha   =            219.103  n.mi
                                              Hp   =            216.384
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18395331.16                 X    =         5570591.23
     Y    =        5695642.09  feet           Y    =         1798529.27  meter
     Z    =       11128495.64                 Z    =         3419113.18
     XDOT =       2976.829173                 XDOT =         861.748734
     YDOT =      19913.344060  feet/sec       YDOT =        6079.478222  meter/sec
     ZDOT =     -15096.022033                 ZDOT =       -4596.971550
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -588778.79                 X    =         -179459.77
     Y    =       19178589.92  feet           Y    =         5845634.21  meter
     Z    =       11247532.64                 Z    =         3428247.95
     XDOT =     -16965.743757                 XDOT =       -5171.158697
     YDOT =       8331.412916  feet/sec       YDOT =        2539.414657  meter/sec
     ZDOT =     -15078.044545                 ZDOT =       -4595.787977
  
  
    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   17058.39765985  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6411 225.5968 0006467 245.3440 114.7040 15.54471844  4679
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17058.39765985   =   yrday.fracday
    Element set:     913
    Inclination:       51.6411  deg
    RA of node:       225.5968  deg
    Eccentricity:     .0006467     
    Arg of perigee:   245.3440  deg
    Mean anomaly:     114.7040  deg
    Mean motion:   15.54471844  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             467
    Checksum:              327
 
 
    Coasting Arc #15 (Orbit 481)
    ---------------------------------------
 
    Vector Time (GMT): 2017/059/08:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922731.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5831228.73                 A    =         6786954.95  meter
     Y    =       -2949120.42  meter          E    =           .0003544
     Z    =       -1824749.12                 I    =           51.41276
     XDOT =        838.220284                 Wp   =          334.68371
     YDOT =      -5139.289943  meter/sec      RA   =          219.70237  deg
     ZDOT =       5626.452268                 TA   =            5.19043
                                              MA   =            5.18676
                                              Ha   =            219.148  n.mi
                                              Hp   =            216.503
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19131327.84                 X    =        -5788953.88
     Y    =       -9675591.94  feet           Y    =        -3014093.04  meter
     Z    =       -5986709.70                 Z    =        -1852971.98
     XDOT =       2750.066548                 XDOT =         868.296646
     YDOT =     -16861.187478  feet/sec       YDOT =       -5129.747452  meter/sec
     ZDOT =      18459.489069                 ZDOT =        5630.597793
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3855945.81                 X    =         1175292.28
     Y    =      -21053772.44  feet           Y    =        -6417189.84  meter
     Z    =       -6110304.87                 Z    =        -1862420.92
     XDOT =      15377.028116                 XDOT =        4686.918170
     YDOT =      -2547.475948  feet/sec       YDOT =        -776.470669  meter/sec
     ZDOT =      18478.459866                 ZDOT =        5632.234567
  
  
    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   17059.36199835  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6403 220.7860 0006490 248.4704 111.5757 15.54438255  4827
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17059.36199835   =   yrday.fracday
    Element set:     914
    Inclination:       51.6403  deg
    RA of node:       220.7860  deg
    Eccentricity:     .0006490     
    Arg of perigee:   248.4704  deg
    Mean anomaly:     111.5757  deg
    Mean motion:   15.54438255  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             482
    Checksum:              319
 
 
    Coasting Arc #16 (Orbit 496)
    ---------------------------------------
 
    Vector Time (GMT): 2017/060/07:22:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 922731.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -577978.12                 A    =         6777589.08  meter
     Y    =        4503428.35  meter          E    =           .0006643
     Z    =       -5037984.51                 I    =           51.40602
     XDOT =      -6819.882808                 Wp   =           79.57726
     YDOT =      -2958.447693  meter/sec      RA   =          214.98923  deg
     ZDOT =      -1863.054479                 TA   =          172.30648
                                              MA   =          172.29629
                                              Ha   =            218.844  n.mi
                                              Hp   =            216.477
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1896253.67                 X    =         -603821.81
     Y    =       14775027.41  feet           Y    =         4496819.82  meter
     Z    =      -16528820.58                 Z    =        -5040855.52
     XDOT =     -22374.943596                 XDOT =       -6777.244080
     YDOT =      -9706.193217  feet/sec       YDOT =       -3034.474080  meter/sec
     ZDOT =      -6112.383461                 ZDOT =       -1896.079111
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14737732.71                 X    =        -4492060.93
     Y    =       -2063379.12  feet           Y    =         -628917.96  meter
     Z    =      -16542092.48                 Z    =        -5042029.79
     XDOT =       9970.467391                 XDOT =        3038.998461
     YDOT =     -21075.365380  feet/sec       YDOT =       -6423.771368  meter/sec
     ZDOT =      -6257.092458                 ZDOT =       -1907.161781
  
  
    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   17060.32633303  .00016717  00000-0  10270-3 0  9150
    2 25544  51.6406 215.9775 0006372 252.3091 107.7366 15.54460319  4978
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17060.32633303   =   yrday.fracday
    Element set:     915
    Inclination:       51.6406  deg
    RA of node:       215.9775  deg
    Eccentricity:     .0006372     
    Arg of perigee:   252.3091  deg
    Mean anomaly:     107.7366  deg
    Mean motion:   15.54460319  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             497
    Checksum:              302
 
 
    Coasting Arc #17 (Orbit 509)
    ---------------------------------------
 
    Vector Time (GMT): 2017/061/03:37:46.356
    Vector Time (MET): N/A
    Weight (LBS)     : 922507.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4763074.16                 A    =         6780481.47  meter
     Y    =        1443339.35  meter          E    =           .0004844
     Z    =       -4608848.16                 I    =           51.43535
     XDOT =      -4518.129548                 Wp   =          154.28351
     YDOT =      -5435.080610  meter/sec      RA   =          210.72951  deg
     ZDOT =       2964.125729                 TA   =          145.37735
                                              MA   =          145.34580
                                              Ha   =            218.865  n.mi
                                              Hp   =            217.792
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15626883.72                 X    =        -4756472.54
     Y    =        4735365.34  feet           Y    =         1390111.75  meter
     Z    =      -15120892.91                 Z    =        -4631969.73
     XDOT =     -14823.259673                 XDOT =       -4471.415470
     YDOT =     -17831.629298  feet/sec       YDOT =       -5485.343805  meter/sec
     ZDOT =       9724.821945                 ZDOT =        2942.292342
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10290177.51                 X    =         3136446.10
     Y    =      -12555695.40  feet           Y    =        -3826975.96  meter
     Z    =      -15222724.52                 Z    =        -4639886.43
     XDOT =      21363.388173                 XDOT =        6511.560715
     YDOT =       5821.224836  feet/sec       YDOT =        1774.309330  meter/sec
     ZDOT =       9629.645828                 ZDOT =        2935.116048
  
  
    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   17061.16208886  .00016717  00000-0  10270-3 0  9168
    2 25544  51.6414 211.8096 0007708 263.8558  96.1717 15.54033939  5108
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17061.16208886   =   yrday.fracday
    Element set:     916
    Inclination:       51.6414  deg
    RA of node:       211.8096  deg
    Eccentricity:     .0007708     
    Arg of perigee:   263.8558  deg
    Mean anomaly:      96.1717  deg
    Mean motion:   15.54033939  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             510
    Checksum:              320
 
 
    Coasting Arc #18 (Orbit 525)
    ---------------------------------------
 
    Vector Time (GMT): 2017/062/03:37:46.356
    Vector Time (MET): N/A
    Weight (LBS)     : 922507.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5763133.02                 A    =         6784160.91  meter
     Y    =        -366170.24  meter          E    =           .0004300
     Z    =        3557078.61                 I    =           51.47612
     XDOT =       3094.023978                 Wp   =           85.66753
     YDOT =       5423.403851  meter/sec      RA   =          205.73035  deg
     ZDOT =      -4449.637107                 TA   =           52.23722
                                              MA   =           52.19827
                                              Ha   =            218.311  n.mi
                                              Hp   =            217.677
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18907916.72                 X    =         5749520.80
     Y    =       -1201345.94  feet           Y    =         -301798.69  meter
     Z    =       11670205.40                 Z    =         3585041.02
     XDOT =      10150.997302                 XDOT =        3054.762214
     YDOT =      17793.319721  feet/sec       YDOT =        5457.783275  meter/sec
     ZDOT =     -14598.546939                 ZDOT =       -4434.703331
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14800143.53                 X    =        -4511083.75
     Y    =       11705689.08  feet           Y    =         3567894.03  meter
     Z    =       11793169.03                 Z    =         3594557.92
     XDOT =     -17697.688180                 XDOT =       -5394.255357
     YDOT =      -7717.605314  feet/sec       YDOT =       -2352.326100  meter/sec
     ZDOT =     -14533.684600                 ZDOT =       -4429.867066
  
  
    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   17062.19098757  .00016717  00000-0  10270-3 0  9177
    2 25544  51.6416 206.6823 0007710 267.6734  92.3536 15.54021982  5260
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17062.19098757   =   yrday.fracday
    Element set:     917
    Inclination:       51.6416  deg
    RA of node:       206.6823  deg
    Eccentricity:     .0007710     
    Arg of perigee:   267.6734  deg
    Mean anomaly:      92.3536  deg
    Mean motion:   15.54021982  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             526
    Checksum:              321
 
 
    Coasting Arc #19 (Orbit 540)
    ---------------------------------------
 
    Vector Time (GMT): 2017/063/03:37:46.356
    Vector Time (MET): N/A
    Weight (LBS)     : 922507.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6406620.03                 A    =         6787521.17  meter
     Y    =        -600967.31  meter          E    =           .0005980
     Z    =       -2147241.41                 I    =           51.51782
     XDOT =      -1355.014062                 Wp   =          324.01328
     YDOT =      -5179.244203  meter/sec      RA   =          200.74151  deg
     ZDOT =       5489.406704                 TA   =           12.13548
                                              MA   =           12.12108
                                              Ha   =            218.276  n.mi
                                              Hp   =            217.584
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21019094.60                 X    =        -6388993.49
     Y    =       -1971677.53  feet           Y    =         -672512.12  meter
     Z    =       -7044755.29                 Z    =        -2178319.83
     XDOT =      -4445.584193                 XDOT =       -1323.662482
     YDOT =     -16992.271008  feet/sec       YDOT =       -5194.221055  meter/sec
     ZDOT =      18009.864514                 ZDOT =        5482.901135
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18186356.72                 X    =         5543201.53
     Y    =      -10630329.37  feet           Y    =        -3240124.39  meter
     Z    =       -7181291.93                 Z    =        -2188857.78
     XDOT =      12840.973627                 XDOT =        3913.928762
     YDOT =       9814.007011  feet/sec       YDOT =        2991.309337  meter/sec
     ZDOT =      17982.008797                 ZDOT =        5480.916281
  
  
    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   17063.15557486  .00016717  00000-0  10270-3 0  9184
    2 25544  51.6422 201.8740 0007726 271.9848  88.0419 15.54051147  5418
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17063.15557486   =   yrday.fracday
    Element set:     918
    Inclination:       51.6422  deg
    RA of node:       201.8740  deg
    Eccentricity:     .0007726     
    Arg of perigee:   271.9848  deg
    Mean anomaly:      88.0419  deg
    Mean motion:   15.54051147  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             541
    Checksum:              316
 
             

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