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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14248.1877
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   90.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.169
   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 
   ------------------------------------------------------------------------
   273/17:05:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              213.5  
   
   278/01:56:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              213.1  
   
   284/02:47:17.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              212.2  
   
   286/10:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.8  
   000/00:00:00.000           0.0               0.0              211.9  
   
 
 
    Coasting Arc #1 (Orbit 2104)
    ---------------------------------------
 
    Vector Time (GMT): 2016/272/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3345827.55                 A    =         6785297.74  meter
     Y    =       -4926537.47  meter          E    =           .0009535
     Z    =       -3249392.80                 I    =           51.27637
     XDOT =       3075.556901                 Wp   =           41.42725
     YDOT =      -5194.901442  meter/sec      RA   =          261.76256  deg
     ZDOT =       4724.362951                 TA   =          280.69843
                                              MA   =          280.80578
                                              Ha   =            222.847  n.mi
                                              Hp   =            213.869
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10977124.49                 X    =        -3274704.91
     Y    =      -16163180.67  feet           Y    =        -4963555.53  meter
     Z    =      -10660737.55                 Z    =        -3265472.59
     XDOT =      10090.409780                 XDOT =        3110.470086
     YDOT =     -17043.639900  feet/sec       YDOT =       -5160.312646  meter/sec
     ZDOT =      15499.878447                 ZDOT =        4739.388754
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12755117.97                 X    =         3887759.96
     Y    =       14750189.34  feet           Y    =         4495857.71  meter
     Z    =      -10730138.70                 Z    =        -3270546.28
     XDOT =      -6813.790213                 XDOT =       -2076.843257
     YDOT =      17180.492242  feet/sec       YDOT =        5236.614035  meter/sec
     ZDOT =      15566.360290                 ZDOT =        4744.626617
  
  
    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   16272.50677776  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6393 262.6469 0006828  14.4091 345.7255 15.53953784 21056
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16272.50677776   =   yrday.fracday
    Element set:     900
    Inclination:       51.6393  deg
    RA of node:       262.6469  deg
    Eccentricity:     .0006828     
    Arg of perigee:    14.4091  deg
    Mean anomaly:     345.7255  deg
    Mean motion:   15.53953784  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2105
    Checksum:              330
 
 
    Coasting Arc #2 (Orbit 2120)
    ---------------------------------------
 
    Vector Time (GMT): 2016/273/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2845225.21                 A    =         6788319.01  meter
     Y    =        5900477.90  meter          E    =           .0014717
     Z    =        1769844.63                 I    =           51.29200
     XDOT =      -3806.775439                 Wp   =           86.65665
     YDOT =       3538.365747  meter/sec      RA   =          256.76100  deg
     ZDOT =      -5635.198364                 TA   =           73.81665
                                              MA   =           73.65474
                                              Ha   =            222.917  n.mi
                                              Hp   =            213.682
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9334728.37                 X    =         2770435.92
     Y    =       19358523.28  feet           Y    =         5931877.20  meter
     Z    =        5806576.86                 Z    =         1783483.56
     XDOT =     -12489.420732                 XDOT =       -3818.685935
     YDOT =      11608.811505  feet/sec       YDOT =        3495.728416  meter/sec
     ZDOT =     -18488.183609                 ZDOT =       -5653.720242
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11845970.23                 X    =        -3610651.73
     Y    =      -17913086.75  feet           Y    =        -5459908.84  meter
     Z    =        5865170.47                 Z    =         1787703.96
     XDOT =       9367.862177                 XDOT =        2855.324392
     YDOT =     -12319.296371  feet/sec       YDOT =       -3754.921534  meter/sec
     ZDOT =     -18569.651156                 ZDOT =       -5660.029672
  
  
    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   16273.53571090  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6387 257.5177 0006970  16.7888 343.3494 15.54010656 21215
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16273.53571090   =   yrday.fracday
    Element set:     901
    Inclination:       51.6387  deg
    RA of node:       257.5177  deg
    Eccentricity:     .0006970     
    Arg of perigee:    16.7888  deg
    Mean anomaly:     343.3494  deg
    Mean motion:   15.54010656  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2121
    Checksum:              316
 
 
    Coasting Arc #3 (Orbit 2123)
    ---------------------------------------
 
    Vector Time (GMT): 2016/273/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3989315.13                 A    =         6777771.80  meter
     Y    =        1508405.84  meter          E    =           .0018429
     Z    =       -5282767.77                 I    =           51.26162
     XDOT =      -2207.427520                 Wp   =           66.12453
     YDOT =      -7318.485872  meter/sec      RA   =          255.72107  deg
     ZDOT =       -416.553946                 TA   =          199.83946
                                              MA   =          199.91122
                                              Ha   =            222.918  n.mi
                                              Hp   =            213.530
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13088304.25                 X    =        -3980224.48
     Y    =        4948838.05  feet           Y    =         1463844.70  meter
     Z    =      -17331915.24                 Z    =        -5302125.09
     XDOT =      -7242.216274                 XDOT =       -2123.402836
     YDOT =     -24010.780421  feet/sec       YDOT =       -7342.701059  meter/sec
     ZDOT =      -1366.646806                 ZDOT =        -427.071969
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3630209.69                 X    =        -1106487.91
     Y    =      -13404111.60  feet           Y    =        -4085573.22  meter
     Z    =      -17416697.79                 Z    =        -5308609.49
     XDOT =      23634.533870                 XDOT =        7203.805924
     YDOT =      -4540.859015  feet/sec       YDOT =       -1384.053828  meter/sec
     ZDOT =      -1411.381535                 ZDOT =        -430.189092
  
  
    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   16273.72863561  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6421 256.5574 0006946  17.5352 342.6039 15.54008315 21241
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16273.72863561   =   yrday.fracday
    Element set:     902
    Inclination:       51.6421  deg
    RA of node:       256.5574  deg
    Eccentricity:     .0006946     
    Arg of perigee:    17.5352  deg
    Mean anomaly:     342.6039  deg
    Mean motion:   15.54008315  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2124
    Checksum:              301
 
 
    Coasting Arc #4 (Orbit 2139)
    ---------------------------------------
 
    Vector Time (GMT): 2016/274/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4430296.91                 A    =         6778264.79  meter
     Y    =         223221.46  meter          E    =           .0010958
     Z    =        5121889.81                 I    =           51.27248
     XDOT =       1342.498626                 Wp   =           33.84759
     YDOT =       7407.776941  meter/sec      RA   =          250.69686  deg
     ZDOT =      -1473.593176                 TA   =           70.46611
                                              MA   =           70.34780
                                              Ha   =            222.745  n.mi
                                              Hp   =            213.551
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14535094.84                 X    =         4402591.37
     Y    =         732353.87  feet           Y    =          272609.86  meter
     Z    =       16804100.44                 Z    =         5143343.94
     XDOT =       4404.523051                 XDOT =        1266.721343
     YDOT =      24303.730120  feet/sec       YDOT =        7422.365746  meter/sec
     ZDOT =      -4834.623280                 ZDOT =       -1467.256751
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1921155.56                 X    =         -585568.21
     Y    =       14316355.11  feet           Y    =         4363625.04  meter
     Z    =       16897758.83                 Z    =         5150436.89
     XDOT =     -23542.385700                 XDOT =       -7175.719161
     YDOT =       2556.235730  feet/sec       YDOT =         779.140651  meter/sec
     ZDOT =      -4808.150515                 ZDOT =       -1465.524277
  
  
    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   16274.75754892  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6419 251.4296 0006852  19.6985 340.4431 15.54058957 21401
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16274.75754892   =   yrday.fracday
    Element set:     903
    Inclination:       51.6419  deg
    RA of node:       251.4296  deg
    Eccentricity:     .0006852     
    Arg of perigee:    19.6985  deg
    Mean anomaly:     340.4431  deg
    Mean motion:   15.54058957  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2140
    Checksum:              332
 
 
    Coasting Arc #5 (Orbit 2154)
    ---------------------------------------
 
    Vector Time (GMT): 2016/275/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4762668.71                 A    =         6780968.69  meter
     Y    =       -1833373.96  meter          E    =           .0012058
     Z    =       -4473678.01                 I    =           51.29427
     XDOT =       -324.285811                 Wp   =           76.02771
     YDOT =      -6950.843235  meter/sec      RA   =          245.67750  deg
     ZDOT =       3203.928494                 TA   =          226.33041
                                              MA   =          226.43042
                                              Ha   =            222.901  n.mi
                                              Hp   =            213.327
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15625553.52                 X    =        -4720082.02
     Y    =       -6015006.44  feet           Y    =        -1886395.85  meter
     Z    =      -14677421.30                 Z    =        -4496710.44
     XDOT =      -1063.929827                 XDOT =        -262.099106
     YDOT =     -22804.603791  feet/sec       YDOT =       -6954.121449  meter/sec
     ZDOT =      10511.576424                 ZDOT =        3202.505222
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7017924.68                 X    =         2139063.44
     Y    =      -15104062.97  feet           Y    =        -4603718.39  meter
     Z    =      -14777717.56                 Z    =        -4504248.31
     XDOT =      21727.511715                 XDOT =        6622.545571
     YDOT =       -151.693048  feet/sec       YDOT =         -46.236041  meter/sec
     ZDOT =      10506.475444                 ZDOT =        3202.373715
  
  
    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   16275.72214034  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6431 246.6218 0006856  23.3039 336.8423 15.54049018 21555
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16275.72214034   =   yrday.fracday
    Element set:     904
    Inclination:       51.6431  deg
    RA of node:       246.6218  deg
    Eccentricity:     .0006856     
    Arg of perigee:    23.3039  deg
    Mean anomaly:     336.8423  deg
    Mean motion:   15.54049018  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2155
    Checksum:              294
 
 
    Coasting Arc #6 (Orbit 2170)
    ---------------------------------------
 
    Vector Time (GMT): 2016/276/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4906467.87                 A    =         6784705.75  meter
     Y    =        3288383.58  meter          E    =           .0016871
     Z    =        3330953.80                 I    =           51.32100
     XDOT =       -874.733965                 Wp   =           69.73222
     YDOT =       6037.655706  meter/sec      RA   =          240.66836  deg
     ZDOT =      -4647.085941                 TA   =           71.27414
                                              MA   =           71.09112
                                              Ha   =            222.998  n.mi
                                              Hp   =            213.189
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16097335.55                 X    =         4853151.08
     Y    =       10788660.04  feet           Y    =         3342953.33  meter
     Z    =       10928326.13                 Z    =         3354658.61
     XDOT =      -2869.862089                 XDOT =        -919.609669
     YDOT =      19808.581711  feet/sec       YDOT =        6027.622302  meter/sec
     ZDOT =     -15246.344950                 ZDOT =       -4651.445056
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11548748.87                 X    =        -3520058.65
     Y    =       15488181.86  feet           Y    =         4720797.83  meter
     Z    =       11031334.07                 Z    =         3362350.62
     XDOT =     -18521.425788                 XDOT =       -5645.330580
     YDOT =      -2879.438176  feet/sec       YDOT =        -877.652756  meter/sec
     ZDOT =     -15266.344122                 ZDOT =       -4653.181688
  
  
    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   16276.75101951  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6430 241.4937 0006921  28.4818 331.6712 15.54071176 21711
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16276.75101951   =   yrday.fracday
    Element set:     905
    Inclination:       51.6430  deg
    RA of node:       241.4937  deg
    Eccentricity:     .0006921     
    Arg of perigee:    28.4818  deg
    Mean anomaly:     331.6712  deg
    Mean motion:   15.54071176  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2171
    Checksum:              298
 
 
    Coasting Arc #7 (Orbit 2185)
    ---------------------------------------
 
    Vector Time (GMT): 2016/277/17:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4819444.83                 A    =         6787813.91  meter
     Y    =       -4384692.56  meter          E    =           .0013782
     Z    =       -1884458.39                 I    =           51.34860
     XDOT =       2164.280479                 Wp   =           35.40691
     YDOT =      -4771.964490  meter/sec      RA   =          235.66987  deg
     ZDOT =       5599.766026                 TA   =          303.75287
                                              MA   =          303.88411
                                              Ha   =            222.926  n.mi
                                              Hp   =            213.089
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15811826.88                 X    =        -4760901.84
     Y    =      -14385474.28  feet           Y    =        -4438259.72  meter
     Z    =       -6182606.26                 Z    =        -1907727.71
     XDOT =       7100.657739                 XDOT =        2190.279222
     YDOT =     -15656.051476  feet/sec       YDOT =       -4747.615998  meter/sec
     ZDOT =      18371.935782                 ZDOT =        5610.343474
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14867407.98                 X    =         4531585.95
     Y    =      -15318536.54  feet           Y    =        -4669089.94  meter
     Z    =       -6283548.20                 Z    =        -1915225.49
     XDOT =      14313.731726                 XDOT =        4362.825430
     YDOT =       6378.755455  feet/sec       YDOT =        1944.244663  meter/sec
     ZDOT =      18418.889668                 ZDOT =        5614.077571
  
  
    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   16277.71557631  .00016717  00000-0  10270-3 0  9061
    2 25544  51.6432 236.6860 0006817  30.8451 329.3101 15.54113158 21867
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16277.71557631   =   yrday.fracday
    Element set:     906
    Inclination:       51.6432  deg
    RA of node:       236.6860  deg
    Eccentricity:     .0006817     
    Arg of perigee:    30.8451  deg
    Mean anomaly:     329.3101  deg
    Mean motion:   15.54113158  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2186
    Checksum:              302
 
 
    Coasting Arc #8 (Orbit 2191)
    ---------------------------------------
 
    Vector Time (GMT): 2016/278/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1302853.86                 A    =         6779823.71  meter
     Y    =        4669530.88  meter          E    =           .0016622
     Z    =       -4755666.57                 I    =           51.32794
     XDOT =      -5757.201848                 Wp   =           58.54135
     YDOT =      -4298.247191  meter/sec      RA   =          233.85731  deg
     ZDOT =      -2641.508055                 TA   =          185.21939
                                              MA   =          185.23674
                                              Ha   =            222.904  n.mi
                                              Hp   =            213.104
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4274454.92                 X    =        -1331871.52
     Y    =       15319983.19  feet           Y    =         4654798.68  meter
     Z    =      -15602580.60                 Z    =        -4762066.65
     XDOT =     -18888.457508                 XDOT =       -5695.878325
     YDOT =     -14101.860864  feet/sec       YDOT =       -4362.285516  meter/sec
     ZDOT =      -8666.365011                 ZDOT =       -2669.326138
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6984780.01                 X    =         2128960.95
     Y    =       14257964.95  feet           Y    =         4345827.72  meter
     Z    =      -15631271.70                 Z    =        -4764411.61
     XDOT =     -22414.575278                 XDOT =       -6831.962545
     YDOT =       1341.083646  feet/sec       YDOT =         408.762295  meter/sec
     ZDOT =      -8787.192998                 ZDOT =       -2678.336426
  
  
    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   16278.10139514  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6428 234.7586 0006286  34.8673 325.2890 15.54099251 21920
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16278.10139514   =   yrday.fracday
    Element set:     907
    Inclination:       51.6428  deg
    RA of node:       234.7586  deg
    Eccentricity:     .0006286     
    Arg of perigee:    34.8673  deg
    Mean anomaly:     325.2890  deg
    Mean motion:   15.54099251  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2192
    Checksum:              326
 
 
    Coasting Arc #9 (Orbit 2207)
    ---------------------------------------
 
    Vector Time (GMT): 2016/279/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2567410.84                 A    =         6777413.28  meter
     Y    =       -3434617.33  meter          E    =           .0007543
     Z    =        5242082.31                 I    =           51.34126
     XDOT =       5484.983545                 Wp   =           63.92609
     YDOT =       5308.625677  meter/sec      RA   =          228.83837  deg
     ZDOT =        794.208251                 TA   =           18.47199
                                              MA   =           18.44462
                                              Ha   =            222.736  n.mi
                                              Hp   =            212.948
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8423263.90                 X    =         2580162.54
     Y    =      -11268429.57  feet           Y    =        -3405834.98  meter
     Z    =       17198432.79                 Z    =         5254585.71
     XDOT =      17995.352838                 XDOT =        5421.355489
     YDOT =      17416.750910  feet/sec       YDOT =        5369.606760  meter/sec
     ZDOT =       2605.670115                 ZDOT =         820.698315
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1441184.26                 X    =         -439272.96
     Y    =      -13926651.84  feet           Y    =        -4244843.48  meter
     Z    =       17253588.80                 Z    =         5258893.87
     XDOT =      24003.813473                 XDOT =        7316.362347
     YDOT =        876.861737  feet/sec       YDOT =         267.267457  meter/sec
     ZDOT =       2720.551889                 ZDOT =         829.224216
  
  
    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   16279.13022761  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6435 229.6297 0006322  38.3914 321.7688 15.54181257 22080
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16279.13022761   =   yrday.fracday
    Element set:     908
    Inclination:       51.6435  deg
    RA of node:       229.6297  deg
    Eccentricity:     .0006322     
    Arg of perigee:    38.3914  deg
    Mean anomaly:     321.7688  deg
    Mean motion:   15.54181257  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2208
    Checksum:              316
 
 
    Coasting Arc #10 (Orbit 2222)
    ---------------------------------------
 
    Vector Time (GMT): 2016/280/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3816906.91                 A    =         6777578.29  meter
     Y    =        2104374.52  meter          E    =           .0018618
     Z    =       -5205791.10                 I    =           51.36361
     XDOT =      -4787.031239                 Wp   =           82.04548
     YDOT =      -5863.138332  meter/sec      RA   =          223.81966  deg
     ZDOT =       1145.824037                 TA   =          198.96687
                                              MA   =          199.03630
                                              Ha   =            222.914  n.mi
                                              Hp   =            212.633
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12522660.45                 X    =        -3814866.93
     Y    =        6904115.89  feet           Y    =         2061702.24  meter
     Z    =      -17079367.12                 Z    =        -5224328.24
     XDOT =     -15705.483069                 XDOT =       -4726.678368
     YDOT =     -19236.018148  feet/sec       YDOT =       -5916.332569  meter/sec
     ZDOT =       3759.265212                 ZDOT =        1122.716547
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4296586.47                 X    =        -1309599.56
     Y    =       13536585.03  feet           Y    =         4125951.12  meter
     Z    =      -17160676.92                 Z    =        -5230574.33
     XDOT =     -23653.171336                 XDOT =       -7209.486623
     YDOT =      -2893.797557  feet/sec       YDOT =        -882.029495  meter/sec
     ZDOT =       3659.231912                 ZDOT =        1115.333887
  
  
    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   16280.09473930  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6432 224.8230 0006477  42.2109 317.9542 15.54193530 22232
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16280.09473930   =   yrday.fracday
    Element set:     909
    Inclination:       51.6432  deg
    RA of node:       224.8230  deg
    Eccentricity:     .0006477     
    Arg of perigee:    42.2109  deg
    Mean anomaly:     317.9542  deg
    Mean motion:   15.54193530  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2223
    Checksum:              294
 
 
    Coasting Arc #11 (Orbit 2238)
    ---------------------------------------
 
    Vector Time (GMT): 2016/281/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4937440.89                 A    =         6780003.55  meter
     Y    =        -724929.32  meter          E    =           .0014611
     Z    =        4582903.36                 I    =           51.39568
     XDOT =       3679.990242                 Wp   =           57.28643
     YDOT =       6029.058192  meter/sec      RA   =          218.80448  deg
     ZDOT =      -2996.266792                 TA   =           62.76901
                                              MA   =           62.62021
                                              Ha   =            222.804  n.mi
                                              Hp   =            212.634
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16198953.06                 X    =         4922918.13
     Y    =       -2378377.04  feet           Y    =         -669796.38  meter
     Z    =       15035772.16                 Z    =         4606853.39
     XDOT =      12073.458799                 XDOT =        3626.853086
     YDOT =      19780.374647  feet/sec       YDOT =        6069.912965  meter/sec
     ZDOT =      -9830.271628                 ZDOT =       -2978.519573
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9864285.60                 X    =         3006634.25
     Y    =      -12945949.33  feet           Y    =        -3945925.36  meter
     Z    =       15140524.02                 Z    =         4614831.72
     XDOT =      21556.143606                 XDOT =        6570.312571
     YDOT =       4961.693762  feet/sec       YDOT =        1512.324259  meter/sec
     ZDOT =      -9753.667838                 ZDOT =       -2972.917957
  
  
    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   16281.12352944  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6428 219.6941 0006441  46.1377 314.0307 15.54224946 22399
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16281.12352944   =   yrday.fracday
    Element set:     910
    Inclination:       51.6428  deg
    RA of node:       219.6941  deg
    Eccentricity:     .0006441     
    Arg of perigee:    46.1377  deg
    Mean anomaly:     314.0307  deg
    Mean motion:   15.54224946  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2239
    Checksum:              299
 
 
    Coasting Arc #12 (Orbit 2253)
    ---------------------------------------
 
    Vector Time (GMT): 2016/282/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5791814.72                 A    =         6783668.13  meter
     Y    =        -520925.10  meter          E    =           .0010568
     Z    =       -3498162.54                 I    =           51.43370
     XDOT =      -2193.186739                 Wp   =           70.19367
     YDOT =      -5794.409290  meter/sec      RA   =          213.80111  deg
     ZDOT =       4508.697774                 TA   =          248.56204
                                              MA   =          248.67480
                                              Ha   =            222.808  n.mi
                                              Hp   =            212.491
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19002016.79                 X    =        -5768566.33
     Y    =       -1709071.86  feet           Y    =         -585563.32  meter
     Z    =      -11476911.22                 Z    =        -3526241.62
     XDOT =      -7195.494549                 XDOT =       -2150.130801
     YDOT =     -19010.529167  feet/sec       YDOT =       -5818.693908  meter/sec
     ZDOT =      14792.315532                 ZDOT =        4498.148669
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14532817.05                 X    =        -4429602.64
     Y    =       12246032.77  feet           Y    =         3732590.79  meter
     Z    =      -11599524.55                 Z    =        -3535535.08
     XDOT =     -17744.662758                 XDOT =       -5408.573209
     YDOT =      -7134.657678  feet/sec       YDOT =       -2174.643660  meter/sec
     ZDOT =      14747.113854                 ZDOT =        4494.920303
  
  
    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   16282.08799773  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6426 214.8867 0006299  49.2648 310.9051 15.54252322 22544
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16282.08799773   =   yrday.fracday
    Element set:     911
    Inclination:       51.6426  deg
    RA of node:       214.8867  deg
    Eccentricity:     .0006299     
    Arg of perigee:    49.2648  deg
    Mean anomaly:     310.9051  deg
    Mean motion:   15.54252322  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2254
    Checksum:              326
 
 
    Coasting Arc #13 (Orbit 2269)
    ---------------------------------------
 
    Vector Time (GMT): 2016/283/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6273163.04                 A    =         6787129.68  meter
     Y    =        1657874.97  meter          E    =           .0018184
     Z    =        1972250.09                 I    =           51.47273
     XDOT =        372.647392                 Wp   =           94.39690
     YDOT =       5263.052365  meter/sec      RA   =          208.80928  deg
     ZDOT =      -5566.423280                 TA   =           63.77977
                                              MA   =           63.59295
                                              Ha   =            222.868  n.mi
                                              Hp   =            212.343
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20581243.58                 X    =         6244577.57
     Y    =        5439222.35  feet           Y    =         1727866.00  meter
     Z    =        6470636.77                 Z    =         2002654.35
     XDOT =       1222.596430                 XDOT =         340.806509
     YDOT =      17267.232170  feet/sec       YDOT =        5267.041128  meter/sec
     ZDOT =     -18262.543569                 ZDOT =       -5564.690745
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18129095.59                 X    =         5525748.34
     Y    =      -11080379.77  feet           Y    =        -3377299.75  meter
     Z    =        6603252.55                 Z    =         2012671.38
     XDOT =      12594.566162                 XDOT =        3838.823766
     YDOT =       9644.795212  feet/sec       YDOT =        2939.733581  meter/sec
     ZDOT =     -18255.778511                 ZDOT =       -5564.361290
  
  
    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   16283.11673597  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6423 209.7574 0006448  53.4507 306.7239 15.54295677 22705
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16283.11673597   =   yrday.fracday
    Element set:     912
    Inclination:       51.6423  deg
    RA of node:       209.7574  deg
    Eccentricity:     .0006448     
    Arg of perigee:    53.4507  deg
    Mean anomaly:     306.7239  deg
    Mean motion:   15.54295677  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2270
    Checksum:              328
 
 
    Coasting Arc #14 (Orbit 2284)
    ---------------------------------------
 
    Vector Time (GMT): 2016/284/01:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6281329.72                 A    =         6788803.68  meter
     Y    =       -2541111.93  meter          E    =           .0017841
     Z    =        -267792.43                 I    =           51.50648
     XDOT =       1582.176230                 Wp   =           48.02695
     YDOT =      -4514.604156  meter/sec      RA   =          203.82687  deg
     ZDOT =       5996.826790                 TA   =          309.08092
                                              MA   =          309.23948
                                              Ha   =            222.894  n.mi
                                              Hp   =            212.343
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20608037.15                 X    =        -6251146.69
     Y    =       -8336981.39  feet           Y    =        -2611185.23  meter
     Z    =        -878584.10                 Z    =         -298232.34
     XDOT =       5190.866895                 XDOT =        1603.411813
     YDOT =     -14811.693424  feet/sec       YDOT =       -4496.791998  meter/sec
     ZDOT =      19674.628576                 ZDOT =        6004.564608
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20106201.47                 X    =        -6128370.21
     Y    =        9470291.52  feet           Y    =         2886544.86  meter
     Z    =       -1011239.29                 Z    =         -308225.73
     XDOT =      -6748.379388                 XDOT =       -2056.906038
     YDOT =     -12304.605954  feet/sec       YDOT =       -3750.443895  meter/sec
     ZDOT =      19709.134644                 ZDOT =        6007.344239
  
  
    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   16284.08115161  .00016717  00000-0  10270-3 0  9135
    2 25544  51.6419 204.9491 0006468  55.8158 304.3607 15.54295625 22857
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16284.08115161   =   yrday.fracday
    Element set:     913
    Inclination:       51.6419  deg
    RA of node:       204.9491  deg
    Eccentricity:     .0006468     
    Arg of perigee:    55.8158  deg
    Mean anomaly:     304.3607  deg
    Mean motion:   15.54295625  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2285
    Checksum:              316
 
 
    Coasting Arc #15 (Orbit 2285)
    ---------------------------------------
 
    Vector Time (GMT): 2016/284/02:47:17.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5460447.89                 A    =         6787746.55  meter
     Y    =        3727677.93  meter          E    =           .0010962
     Z    =       -1536887.64                 I    =           51.50361
     XDOT =      -3856.547017                 Wp   =          106.41608
     YDOT =       3296.759876  meter/sec      RA   =          203.66599  deg
     ZDOT =      -5742.927968                 TA   =           90.39993
                                              MA   =           90.27432
                                              Ha   =            222.911  n.mi
                                              Hp   =            212.242
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17914855.29                 X    =         5425823.82
     Y    =       12229914.45  feet           Y    =         3788546.60  meter
     Z    =       -5042282.29                 Z    =        -1510446.30
     XDOT =     -12652.713311                 XDOT =       -3865.228664
     YDOT =      10816.141326  feet/sec       YDOT =        3253.584389  meter/sec
     ZDOT =     -18841.627192                 ZDOT =       -5761.683627
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19546640.67                 X    =         5957816.08
     Y    =       -9465103.09  feet           Y    =        -2884963.42  meter
     Z    =       -4927283.28                 Z    =        -1501835.94
     XDOT =       2441.062856                 XDOT =         744.035958
     YDOT =      14827.650172  feet/sec       YDOT =        4519.467772  meter/sec
     ZDOT =     -18924.103194                 ZDOT =       -5768.066653
  
  
    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   16284.14544567  .00016717  00000-0  10270-3 0  9149
    2 25544  51.6411 204.6287 0006524  57.2448 302.9333 15.54341679 22862
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16284.14544567   =   yrday.fracday
    Element set:     914
    Inclination:       51.6411  deg
    RA of node:       204.6287  deg
    Eccentricity:     .0006524     
    Arg of perigee:    57.2448  deg
    Mean anomaly:     302.9333  deg
    Mean motion:   15.54341679  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2286
    Checksum:              315
 
 
    Coasting Arc #16 (Orbit 2301)
    ---------------------------------------
 
    Vector Time (GMT): 2016/285/02:47:17.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4400832.22                 A    =         6784561.62  meter
     Y    =       -4101741.16  meter          E    =           .0019096
     Z    =        3115524.20                 I    =           51.52320
     XDOT =       5515.686958                 Wp   =           77.24457
     YDOT =      -2211.463783  meter/sec      RA   =          198.68021  deg
     ZDOT =       4858.685633                 TA   =          318.72965
                                              MA   =          318.87383
                                              Ha   =            222.898  n.mi
                                              Hp   =            212.150
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14438425.92                 X    =        -4369772.42
     Y    =      -13457156.04  feet           Y    =        -4150780.27  meter
     Z    =       10221536.08                 Z    =         3094221.70
     XDOT =      18096.085821                 XDOT =        5516.404575
     YDOT =      -7255.458605  feet/sec       YDOT =       -2149.779214  meter/sec
     ZDOT =      15940.569663                 ZDOT =        4885.481620
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18790739.47                 X    =        -5727417.39
     Y    =        6193034.67  feet           Y    =         1887636.97  meter
     Z    =       10129038.62                 Z    =         3087330.97
     XDOT =       2798.248958                 XDOT =         852.906283
     YDOT =     -17887.082794  feet/sec       YDOT =       -5451.982836  meter/sec
     ZDOT =      16058.033643                 ZDOT =        4894.488655
  
  
    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   16285.17412597  .00016717  00000-0  10270-3 0  9151
    2 25544  51.6412 199.4991 0006449  61.2351 298.9449 15.54377413 23026
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16285.17412597   =   yrday.fracday
    Element set:     915
    Inclination:       51.6412  deg
    RA of node:       199.4991  deg
    Eccentricity:     .0006449     
    Arg of perigee:    61.2351  deg
    Mean anomaly:     298.9449  deg
    Mean motion:   15.54377413  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2302
    Checksum:              331
 
 
    Coasting Arc #17 (Orbit 2316)
    ---------------------------------------
 
    Vector Time (GMT): 2016/286/02:47:17.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2890045.58                 A    =         6780401.16  meter
     Y    =        4295631.46  meter          E    =           .0015334
     Z    =       -4393970.92                 I    =           51.54154
     XDOT =      -6780.032998                 Wp   =           67.82557
     YDOT =       1110.276055  meter/sec      RA   =          193.68531  deg
     ZDOT =      -3377.811360                 TA   =          167.89859
                                              MA   =          167.86171
                                              Ha   =            222.840  n.mi
                                              Hp   =            212.054
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9481776.83                 X    =         2863140.13
     Y    =       14093279.07  feet           Y    =         4327798.98  meter
     Z    =      -14415915.08                 Z    =        -4379997.50
     XDOT =     -22244.202748                 XDOT =       -6775.536390
     YDOT =       3642.637976  feet/sec       YDOT =        1034.481953  meter/sec
     ZDOT =     -11082.058267                 ZDOT =       -3410.736529
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16935065.32                 X    =         5161807.91
     Y    =       -1862038.60  feet           Y    =         -567549.36  meter
     Z    =      -14355472.45                 Z    =        -4375548.00
     XDOT =      -7299.734307                 XDOT =       -2224.959017
     YDOT =      20061.470607  feet/sec       YDOT =        6114.736241  meter/sec
     ZDOT =     -11226.162617                 ZDOT =       -3421.734366
  
  
    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   16286.13848737  .00016717  00000-0  10270-3 0  9168
    2 25544  51.6421 194.6898 0006511  64.6140 295.5687 15.54414768 23170
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16286.13848737   =   yrday.fracday
    Element set:     916
    Inclination:       51.6421  deg
    RA of node:       194.6898  deg
    Eccentricity:     .0006511     
    Arg of perigee:    64.6140  deg
    Mean anomaly:     295.5687  deg
    Mean motion:   15.54414768  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2317
    Checksum:              342
 
 
    Coasting Arc #18 (Orbit 2321)
    ---------------------------------------
 
    Vector Time (GMT): 2016/286/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907704.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6274072.89                 A    =         6785733.50  meter
     Y    =         690970.38  meter          E    =           .0011767
     Z    =       -2489308.32                 I    =           51.56976
     XDOT =      -2631.999863                 Wp   =           57.85816
     YDOT =      -4862.439677  meter/sec      RA   =          191.95046  deg
     ZDOT =       5308.536775                 TA   =          274.21563
                                              MA   =          274.35010
                                              Ha   =            222.775  n.mi
                                              Hp   =            211.914
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20584228.65                 X    =        -6269241.10
     Y    =        2266963.18  feet           Y    =          620836.22  meter
     Z    =       -8167022.05                 Z    =        -2519774.80
     XDOT =      -8635.170155                 XDOT =       -2603.218018
     YDOT =     -15952.886079  feet/sec       YDOT =       -4891.710933  meter/sec
     ZDOT =      17416.459236                 ZDOT =        5295.821531
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20300344.72                 X    =         6187545.07
     Y    =       -3814517.03  feet           Y    =        -1162664.79  meter
     Z    =       -8300319.52                 Z    =        -2529937.39
     XDOT =       9652.456494                 XDOT =        2942.068739
     YDOT =      13762.758134  feet/sec       YDOT =        4194.888679  meter/sec
     ZDOT =      17361.598372                 ZDOT =        5291.815184
  
  
    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   16286.45993591  .00016717  00000-0  10270-3 0  9173
    2 25544  51.6415 193.0881 0006592  63.1273 297.0553 15.54429614 23229
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16286.45993591   =   yrday.fracday
    Element set:     917
    Inclination:       51.6415  deg
    RA of node:       193.0881  deg
    Eccentricity:     .0006592     
    Arg of perigee:    63.1273  deg
    Mean anomaly:     297.0553  deg
    Mean motion:   15.54429614  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2322
    Checksum:              326
 
 
    Coasting Arc #19 (Orbit 2337)
    ---------------------------------------
 
    Vector Time (GMT): 2016/287/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907704.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6739475.47                 A    =         6788096.17  meter
     Y    =         245944.87  meter          E    =           .0017558
     Z    =         724573.88                 I    =           51.61043
     XDOT =        476.658804                 Wp   =          108.59752
     YDOT =       4810.438235  meter/sec      RA   =          186.97315  deg
     ZDOT =      -5953.584079                 TA   =           63.56922
                                              MA   =           63.38915
                                              Ha   =            222.778  n.mi
                                              Hp   =            211.846
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       22111140.00                 X    =         6732704.65
     Y    =         806905.74  feet           Y    =          321272.44  meter
     Z    =        2377210.91                 Z    =          757296.45
     XDOT =       1563.841220                 XDOT =         451.752104
     YDOT =      15782.277674  feet/sec       YDOT =        4815.628531  meter/sec
     ZDOT =     -19532.756164                 ZDOT =       -5951.329675
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22074752.93                 X    =        -6728384.69
     Y    =        1248353.22  feet           Y    =          380498.06  meter
     Z    =        2520245.56                 Z    =          768170.85
     XDOT =      -3057.477431                 XDOT =        -931.919121
     YDOT =     -13945.660797  feet/sec       YDOT =       -4250.637411  meter/sec
     ZDOT =     -19523.616057                 ZDOT =       -5950.798174
  
  
    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   16287.48855162  .00016717  00000-0  10270-3 0  9189
    2 25544  51.6423 187.9583 0006521  67.5582 292.6261 15.54467216 23386
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16287.48855162   =   yrday.fracday
    Element set:     918
    Inclination:       51.6423  deg
    RA of node:       187.9583  deg
    Eccentricity:     .0006521     
    Arg of perigee:    67.5582  deg
    Mean anomaly:     292.6261  deg
    Mean motion:   15.54467216  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2338
    Checksum:              339
 
             

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