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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14248.1882
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   75.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.596
   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 
   ------------------------------------------------------------------------
   270/16:51:48.844          -0.9               1.4              1.4    
   N/A                       -0.9               0.0              220.6  
   000/00:03:37.689          -0.6               0.0              215.8  
   
   274/01:42:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.8  
   000/00:00:00.000           0.0               0.0              215.6  
   
 
 
    Coasting Arc #1 (Orbit 3625)
    ---------------------------------------
 
    Vector Time (GMT): 2017/261/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3397536.81                 A    =         6788442.31  meter
     Y    =        5752783.98  meter          E    =           .0006060
     Z    =       -1182331.90                 I    =           51.31309
     XDOT =      -3666.673571                 Wp   =          160.69671
     YDOT =      -3361.564134  meter/sec      RA   =          292.41889  deg
     ZDOT =      -5833.797795                 TA   =           32.20288
                                              MA   =           32.16589
                                              Ha   =            219.681  n.mi
                                              Hp   =            215.848
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11146774.31                 X    =        -3455870.30
     Y    =       18873963.17  feet           Y    =         5714464.10  meter
     Z    =       -3879041.67                 Z    =        -1198978.36
     XDOT =     -12029.768935                 XDOT =       -3600.473571
     YDOT =     -11028.753720  feet/sec       YDOT =       -3402.197924  meter/sec
     ZDOT =     -19139.756544                 ZDOT =       -5851.448074
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12179115.73                 X    =         3712194.48
     Y    =      -18208848.10  feet           Y    =        -5550056.90  meter
     Z    =       -3953608.28                 Z    =        -1205059.80
     XDOT =       9927.905616                 XDOT =        3026.025632
     YDOT =      10802.998737  feet/sec       YDOT =        3292.754015  meter/sec
     ZDOT =     -19217.329371                 ZDOT =       -5857.441992
  
  
    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   17261.52983304  .00016717  00000-0  10270-3 0  9008
    2 25544  51.6409 293.0091 0003944 292.4893  67.5842 15.54220914 36260
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17261.52983304   =   yrday.fracday
    Element set:     900
    Inclination:       51.6409  deg
    RA of node:       293.0091  deg
    Eccentricity:     .0003944     
    Arg of perigee:   292.4893  deg
    Mean anomaly:      67.5842  deg
    Mean motion:   15.54220914  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3626
    Checksum:              312
 
 
    Coasting Arc #2 (Orbit 3641)
    ---------------------------------------
 
    Vector Time (GMT): 2017/262/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3853729.64                 A    =         6785788.86  meter
     Y    =       -4834912.80  meter          E    =           .0010662
     Z    =        2781929.24                 I    =           51.29059
     XDOT =       2682.994396                 Wp   =           66.97368
     YDOT =       5073.565261  meter/sec      RA   =          287.42039  deg
     ZDOT =       5089.538539                 TA   =          324.75060
                                              MA   =          324.82107
                                              Ha   =            219.797  n.mi
                                              Hp   =            215.770
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12643469.95                 X    =         3893995.28
     Y    =      -15862574.82  feet           Y    =        -4791592.26  meter
     Z    =        9127064.45                 Z    =         2800747.87
     XDOT =       8802.475051                 XDOT =        2601.338596
     YDOT =      16645.555318  feet/sec       YDOT =        5103.112447  meter/sec
     ZDOT =      16697.961087                 ZDOT =        5102.372662
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13205208.26                 X    =        -4024947.48
     Y    =       15347974.52  feet           Y    =         4678062.63  meter
     Z    =        9211084.11                 Z    =         2807538.44
     XDOT =      -6903.561595                 XDOT =       -2104.205574
     YDOT =     -16017.052259  feet/sec       YDOT =       -4881.997528  meter/sec
     ZDOT =      16753.963878                 ZDOT =        5106.608190
  
  
    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   17262.55861103  .00016717  00000-0  10270-3 0  9015
    2 25544  51.6390 287.8798 0003835 298.6407  61.4360 15.54196812 36427
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17262.55861103   =   yrday.fracday
    Element set:     901
    Inclination:       51.6390  deg
    RA of node:       287.8798  deg
    Eccentricity:     .0003835     
    Arg of perigee:   298.6407  deg
    Mean anomaly:      61.4360  deg
    Mean motion:   15.54196812  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3642
    Checksum:              326
 
 
    Coasting Arc #3 (Orbit 3656)
    ---------------------------------------
 
    Vector Time (GMT): 2017/263/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4133078.15                 A    =         6781816.70  meter
     Y    =        3488412.51  meter          E    =           .0005811
     Z    =       -4098060.75                 I    =           51.27009
     XDOT =      -1687.990222                 Wp   =           39.36401
     YDOT =      -6445.751665  meter/sec      RA   =          282.41197  deg
     ZDOT =      -3782.981439                 TA   =          191.36522
                                              MA   =          191.37835
                                              Ha   =            219.864  n.mi
                                              Hp   =            215.643
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13559967.69                 X    =        -4151872.92
     Y    =       11444922.94  feet           Y    =         3442087.94  meter
     Z    =      -13445081.20                 Z    =        -4118184.15
     XDOT =      -5538.025664                 XDOT =       -1597.410746
     YDOT =     -21147.479216  feet/sec       YDOT =       -6464.121997  meter/sec
     ZDOT =     -12411.356426                 ZDOT =       -3790.960275
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13727152.48                 X    =         4184036.07
     Y    =      -11135869.24  feet           Y    =        -3394212.95  meter
     Z    =      -13534655.32                 Z    =        -4125362.94
     XDOT =       4164.245167                 XDOT =        1269.261927
     YDOT =      20265.619656  feet/sec       YDOT =        6176.960871  meter/sec
     ZDOT =     -12445.676118                 ZDOT =       -3793.442081
  
  
    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   17263.52308406  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6402 283.0715 0003968 300.6177  59.4584 15.54233100 36576
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17263.52308406   =   yrday.fracday
    Element set:     902
    Inclination:       51.6402  deg
    RA of node:       283.0715  deg
    Eccentricity:     .0003968     
    Arg of perigee:   300.6177  deg
    Mean anomaly:      59.4584  deg
    Mean motion:   15.54233100  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3657
    Checksum:              296
 
 
    Coasting Arc #4 (Orbit 3672)
    ---------------------------------------
 
    Vector Time (GMT): 2017/264/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4247860.35                 A    =         6778492.88  meter
     Y    =       -1821305.89  meter          E    =           .0002193
     Z    =        4957106.16                 I    =           51.25162
     XDOT =        726.418410                 Wp   =          117.27320
     YDOT =       7347.528234  meter/sec      RA   =          277.39114  deg
     ZDOT =       2075.396282                 TA   =          312.41531
                                              MA   =          312.43386
                                              Ha   =            219.873  n.mi
                                              Hp   =            215.657
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13936549.71                 X    =         4243831.62
     Y    =       -5975413.01  feet           Y    =        -1773825.24  meter
     Z    =       16263471.64                 Z    =         4977731.54
     XDOT =       2383.262499                 XDOT =         634.121082
     YDOT =      24106.063761  feet/sec       YDOT =        7355.135767  meter/sec
     ZDOT =       6809.042921                 ZDOT =        2078.699807
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13861894.53                 X    =        -4225105.45
     Y    =        5898738.81  feet           Y    =         1797935.59  meter
     Z    =       16355006.83                 Z    =         4985006.08
     XDOT =      -1777.216250                 XDOT =        -541.695513
     YDOT =     -23108.164376  feet/sec       YDOT =       -7043.368502  meter/sec
     ZDOT =       6822.552168                 ZDOT =        2079.513901
  
  
    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   17264.55185257  .00016717  00000-0  10270-3 0  9038
    2 25544  51.6389 277.9413 0003926 306.6640  53.4151 15.54227086 36730
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17264.55185257   =   yrday.fracday
    Element set:     903
    Inclination:       51.6389  deg
    RA of node:       277.9413  deg
    Eccentricity:     .0003926     
    Arg of perigee:   306.6640  deg
    Mean anomaly:      53.4151  deg
    Mean motion:   15.54227086  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3673
    Checksum:              322
 
 
    Coasting Arc #5 (Orbit 3687)
    ---------------------------------------
 
    Vector Time (GMT): 2017/265/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4249360.67                 A    =         6777104.87  meter
     Y    =         -15613.23  meter          E    =           .0012029
     Z    =       -5289603.58                 I    =           51.24321
     XDOT =        204.385736                 Wp   =           76.47059
     YDOT =      -7656.141727  meter/sec      RA   =          272.36457  deg
     ZDOT =       -139.096407                 TA   =          192.18055
                                              MA   =          192.20966
                                              Ha   =            220.070  n.mi
                                              Hp   =            215.496
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13941472.03                 X    =        -4223175.70
     Y    =         -51224.51  feet           Y    =          -62986.78  meter
     Z    =      -17354342.44                 Z    =        -5310182.25
     XDOT =        670.556876                 XDOT =         290.659228
     YDOT =     -25118.575219  feet/sec       YDOT =       -7653.373780  meter/sec
     ZDOT =       -456.353041                 ZDOT =        -137.892991
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13827025.18                 X    =         4214477.27
     Y    =        -109971.79  feet           Y    =          -33519.40  meter
     Z    =      -17445393.34                 Z    =        -5317355.89
     XDOT =       -386.090682                 XDOT =        -117.680440
     YDOT =      24116.513697  feet/sec       YDOT =        7350.713375  meter/sec
     ZDOT =       -449.887571                 ZDOT =        -137.125732
  
  
    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   17265.51632000  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6385 273.1335 0004054 308.6693  51.4097 15.54216881 36884
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17265.51632000   =   yrday.fracday
    Element set:     904
    Inclination:       51.6385  deg
    RA of node:       273.1335  deg
    Eccentricity:     .0004054     
    Arg of perigee:   308.6693  deg
    Mean anomaly:      51.4097  deg
    Mean motion:   15.54216881  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3688
    Checksum:              307
 
 
    Coasting Arc #6 (Orbit 3703)
    ---------------------------------------
 
    Vector Time (GMT): 2017/266/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4132896.40                 A    =         6778128.22  meter
     Y    =        1875736.25  meter          E    =           .0006092
     Z    =        5034566.40                 I    =           51.24603
     XDOT =      -1119.026335                 Wp   =           14.58005
     YDOT =       7364.902042  meter/sec      RA   =          267.33578  deg
     ZDOT =      -1819.059263                 TA   =           93.16408
                                              MA   =           93.09437
                                              Ha   =            220.068  n.mi
                                              Hp   =            215.548
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13559371.40                 X    =         4087158.50
     Y    =        6153990.33  feet           Y    =         1921697.98  meter
     Z    =       16517606.30                 Z    =         5054531.66
     XDOT =      -3671.346242                 XDOT =       -1192.463254
     YDOT =      24163.064443  feet/sec       YDOT =        7351.977499  meter/sec
     ZDOT =      -5968.042203                 ZDOT =       -1824.674459
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13623369.32                 X    =        -4152402.97
     Y    =       -5763246.80  feet           Y    =        -1756637.62  meter
     Z    =       16605669.59                 Z    =         5061408.09
     XDOT =       2510.611472                 XDOT =         765.234377
     YDOT =     -23264.190852  feet/sec       YDOT =       -7090.925372  meter/sec
     ZDOT =      -5993.973294                 ZDOT =       -1826.963060
  
  
    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   17266.54508142  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6379 268.0034 0004090 313.1930  46.8881 15.54242051 37047
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17266.54508142   =   yrday.fracday
    Element set:     905
    Inclination:       51.6379  deg
    RA of node:       268.0034  deg
    Eccentricity:     .0004090     
    Arg of perigee:   313.1930  deg
    Mean anomaly:      46.8881  deg
    Mean motion:   15.54242051  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3704
    Checksum:              294
 
 
    Coasting Arc #7 (Orbit 3718)
    ---------------------------------------
 
    Vector Time (GMT): 2017/267/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3916616.96                 A    =         6781324.33  meter
     Y    =       -3558911.93  meter          E    =           .0005075
     Z    =       -4244599.64                 I    =           51.25957
     XDOT =       2017.219603                 Wp   =           87.15069
     YDOT =      -6474.046651  meter/sec      RA   =          262.31456  deg
     ZDOT =       3570.814960                 TA   =          219.51196
                                              MA   =          219.54897
                                              Ha   =            220.303  n.mi
                                              Hp   =            215.349
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12849793.16                 X    =        -3855910.71
     Y    =      -11676220.25  feet           Y    =        -3602371.23  meter
     Z    =      -13925851.83                 Z    =        -4263477.78
     XDOT =       6618.174551                 XDOT =        2072.118691
     YDOT =     -21240.310536  feet/sec       YDOT =       -6451.181394  meter/sec
     ZDOT =      11715.272179                 ZDOT =        3580.748133
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13283495.64                 X    =         4048809.47
     Y    =       11076150.75  feet           Y    =         3376010.75  meter
     Z    =      -14008864.37                 Z    =        -4269901.86
     XDOT =      -4746.369048                 XDOT =       -1446.693286
     YDOT =      20549.937892  feet/sec       YDOT =        6263.621069  meter/sec
     ZDOT =      11760.168980                 ZDOT =        3584.499505
  
  
    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   17267.50954141  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6384 263.1952 0004129 319.1083  40.9759 15.54223704 37195
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17267.50954141   =   yrday.fracday
    Element set:     906
    Inclination:       51.6384  deg
    RA of node:       263.1952  deg
    Eccentricity:     .0004129     
    Arg of perigee:   319.1083  deg
    Mean anomaly:      40.9759  deg
    Mean motion:   15.54223704  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3719
    Checksum:              314
 
 
    Coasting Arc #8 (Orbit 3734)
    ---------------------------------------
 
    Vector Time (GMT): 2017/268/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3556500.99                 A    =         6785114.19  meter
     Y    =        4952908.10  meter          E    =           .0010566
     Z    =        2969426.96                 I    =           51.27686
     XDOT =      -2923.447540                 Wp   =           80.27061
     YDOT =       5075.981005  meter/sec      RA   =          257.30324  deg
     ZDOT =      -4948.297339                 TA   =           65.59108
                                              MA   =           65.48086
                                              Ha   =            220.377  n.mi
                                              Hp   =            215.304
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11668310.34                 X    =         3486427.72
     Y    =       16249698.50  feet           Y    =         4992287.79  meter
     Z    =        9742214.43                 Z    =         2986532.92
     XDOT =      -9591.363321                 XDOT =       -2955.954513
     YDOT =      16653.480989  feet/sec       YDOT =        5043.106815  meter/sec
     ZDOT =     -16234.571321                 ZDOT =       -4962.578141
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12609944.15                 X    =        -3843510.98
     Y    =      -15483053.48  feet           Y    =        -4719234.70  meter
     Z    =        9817192.74                 Z    =         2992280.35
     XDOT =       7282.104347                 XDOT =        2219.585405
     YDOT =     -16299.806624  feet/sec       YDOT =       -4968.181059  meter/sec
     ZDOT =     -16298.496573                 ZDOT =       -4967.781755
  
  
    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   17268.53829413  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6372 258.0655 0004324 322.4085  37.6765 15.54273066 37355
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17268.53829413   =   yrday.fracday
    Element set:     907
    Inclination:       51.6372  deg
    RA of node:       258.0655  deg
    Eccentricity:     .0004324     
    Arg of perigee:   322.4085  deg
    Mean anomaly:      37.6765  deg
    Mean motion:   15.54273066  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3735
    Checksum:              322
 
 
    Coasting Arc #9 (Orbit 3749)
    ---------------------------------------
 
    Vector Time (GMT): 2017/269/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3050595.13                 A    =         6788069.55  meter
     Y    =       -5895356.70  meter          E    =           .0010588
     Z    =       -1390492.28                 I    =           51.29488
     XDOT =       3797.962930                 Wp   =           16.40939
     YDOT =      -3322.719393  meter/sec      RA   =          252.30348  deg
     ZDOT =       5775.964839                 TA   =          328.35845
                                              MA   =          328.42206
                                              Ha   =            220.433  n.mi
                                              Hp   =            215.173
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10008514.21                 X    =        -2977690.54
     Y    =      -19341721.47  feet           Y    =        -5929063.02  meter
     Z    =       -4561982.54                 Z    =        -1405133.75
     XDOT =      12460.508301                 XDOT =        3806.779042
     YDOT =     -10901.310346  feet/sec       YDOT =       -3280.198223  meter/sec
     ZDOT =      18950.015875                 ZDOT =        5794.436068
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11502714.23                 X    =         3506027.30
     Y    =       18476269.76  feet           Y    =         5631567.02  meter
     Z    =       -4625932.55                 Z    =        -1409984.24
     XDOT =     -10071.384810                 XDOT =       -3069.758090
     YDOT =      11018.423586  feet/sec       YDOT =        3358.415509  meter/sec
     ZDOT =      19032.230122                 ZDOT =        5801.023741
  
  
    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   17269.50274804  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6372 253.2575 0004068 326.3116  33.7777 15.54271171 37508
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17269.50274804   =   yrday.fracday
    Element set:     908
    Inclination:       51.6372  deg
    RA of node:       253.2575  deg
    Eccentricity:     .0004068     
    Arg of perigee:   326.3116  deg
    Mean anomaly:      33.7777  deg
    Mean motion:   15.54271171  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3750
    Checksum:              312
 
 
    Coasting Arc #10 (Orbit 3765)
    ---------------------------------------
 
    Vector Time (GMT): 2017/270/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904993.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2337710.69                 A    =         6788848.61  meter
     Y    =        6359836.26  meter          E    =           .0007245
     Z    =        -370409.65                 I    =           51.30930
     XDOT =      -4615.481440                 Wp   =          129.56377
     YDOT =       1353.706451  meter/sec      RA   =          247.30861  deg
     ZDOT =      -5968.950116                 TA   =           54.44634
                                              MA   =           54.37882
                                              Ha   =            220.644  n.mi
                                              Hp   =            215.081
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7669654.48                 X    =         2268218.85
     Y    =       20865604.52  feet           Y    =         6385589.55  meter
     Z    =       -1215254.76                 Z    =         -359222.91
     XDOT =     -15142.655643                 XDOT =       -4601.281373
     YDOT =       4441.294132  feet/sec       YDOT =        1302.171948  meter/sec
     ZDOT =     -19583.169671                 ZDOT =       -5991.336538
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9677608.54                 X    =        -2949735.08
     Y    =      -20016411.48  feet           Y    =        -6101002.22  meter
     Z    =       -1166644.88                 Z    =         -355593.36
     XDOT =      13049.177672                 XDOT =        3977.389354
     YDOT =      -5178.366453  feet/sec       YDOT =       -1578.366095  meter/sec
     ZDOT =     -19682.433253                 ZDOT =       -5999.205656
  
  
    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   17270.53149274  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6381 248.1273 0004313 331.0792  29.0121 15.54274200 37666
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17270.53149274   =   yrday.fracday
    Element set:     909
    Inclination:       51.6381  deg
    RA of node:       248.1273  deg
    Eccentricity:     .0004313     
    Arg of perigee:   331.0792  deg
    Mean anomaly:      29.0121  deg
    Mean motion:   15.54274200  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3766
    Checksum:              288
 
 
    Coasting Arc #11 (Orbit 3768)
    ---------------------------------------
 
    Vector Time (GMT): 2017/270/16:53:37.689
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2414909.08                 A    =         6779728.26  meter
     Y    =        4118633.55  meter          E    =           .0010482
     Z    =       -4823115.34                 I    =           51.28217
     XDOT =      -4613.855354                 Wp   =           49.60011
     YDOT =      -5595.593469  meter/sec      RA   =          246.30426  deg
     ZDOT =      -2465.025178                 TA   =          196.02453
                                              MA   =          196.05771
                                              Ha   =            220.627  n.mi
                                              Hp   =            215.819
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7922930.06                 X    =        -2437356.69
     Y    =       13512577.27  feet           Y    =         4091502.53  meter
     Z    =      -15823869.23                 Z    =        -4834901.16
     XDOT =     -15137.320716                 XDOT =       -4538.967021
     YDOT =     -18358.246291  feet/sec       YDOT =       -5646.770200  meter/sec
     ZDOT =      -8087.352947                 ZDOT =       -2487.255783
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11808588.36                 X    =        -3599257.73
     Y    =      -10210187.66  feet           Y    =        -3112065.20  meter
     Z    =      -15876608.94                 Z    =        -4839190.41
     XDOT =      20113.672520                 XDOT =        6130.647384
     YDOT =     -10519.176098  feet/sec       YDOT =       -3206.244875  meter/sec
     ZDOT =      -8184.949624                 ZDOT =       -2494.772645
  
  
    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   17270.72438389  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6414 247.1670 0004512 316.3499  43.7297 15.54022503 37691
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17270.72438389   =   yrday.fracday
    Element set:     910
    Inclination:       51.6414  deg
    RA of node:       247.1670  deg
    Eccentricity:     .0004512     
    Arg of perigee:   316.3499  deg
    Mean anomaly:      43.7297  deg
    Mean motion:   15.54022503  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3769
    Checksum:              314
 
 
    Coasting Arc #12 (Orbit 3784)
    ---------------------------------------
 
    Vector Time (GMT): 2017/271/16:53:37.689
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3346059.12                 A    =         6777776.02  meter
     Y    =       -2663445.01  meter          E    =           .0002087
     Z    =        5258193.40                 I    =           51.28912
     XDOT =       4116.011594                 Wp   =          352.62227
     YDOT =       6438.402542  meter/sec      RA   =          241.28304  deg
     ZDOT =        644.091281                 TA   =           91.21065
                                              MA   =           91.18675
                                              Ha   =            220.559  n.mi
                                              Hp   =            215.848
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10977884.26                 X    =         3350051.86
     Y    =       -8738336.65  feet           Y    =        -2626004.40  meter
     Z    =       17251290.68                 Z    =         5274457.53
     XDOT =      13503.975047                 XDOT =        4040.581047
     YDOT =      21123.367921  feet/sec       YDOT =        6484.008879  meter/sec
     ZDOT =       2113.160371                 ZDOT =         663.902083
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6759231.63                 X    =         2060213.80
     Y    =       12193587.48  feet           Y    =         3716605.46  meter
     Z    =       17323646.05                 Z    =         5280247.32
     XDOT =     -22222.991123                 XDOT =       -6773.567694
     YDOT =       9202.864599  feet/sec       YDOT =        2805.033130  meter/sec
     ZDOT =       2199.948481                 ZDOT =         670.544297
  
  
    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   17271.75329948  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6407 242.0389 0004511 318.9157  41.1655 15.54032063 37852
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17271.75329948   =   yrday.fracday
    Element set:     911
    Inclination:       51.6407  deg
    RA of node:       242.0389  deg
    Eccentricity:     .0004511     
    Arg of perigee:   318.9157  deg
    Mean anomaly:      41.1655  deg
    Mean motion:   15.54032063  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3785
    Checksum:              310
 
 
    Coasting Arc #13 (Orbit 3799)
    ---------------------------------------
 
    Vector Time (GMT): 2017/272/16:53:37.689
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4230614.05                 A    =         6778134.29  meter
     Y    =        1137902.80  meter          E    =           .0011171
     Z    =       -5181458.50                 I    =           51.30706
     XDOT =      -3337.269112                 Wp   =           83.33539
     YDOT =      -6783.103904  meter/sec      RA   =          236.26106  deg
     ZDOT =       1238.787662                 TA   =          198.60181
                                              MA   =          198.64268
                                              Ha   =            220.755  n.mi
                                              Hp   =            215.613
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13879967.34                 X    =        -4217854.81
     Y    =        3733276.92  feet           Y    =         1090664.14  meter
     Z    =      -16999535.76                 Z    =        -5201978.73
     XDOT =     -10949.045643                 XDOT =       -3267.188065
     YDOT =     -22254.277901  feet/sec       YDOT =       -6820.031584  meter/sec
     ZDOT =       4064.263982                 ZDOT =        1222.746875
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1576944.17                 X    =         -480652.58
     Y    =      -14177529.85  feet           Y    =        -4321311.10  meter
     Z    =      -17090522.54                 Z    =        -5209191.27
     XDOT =      22639.678815                 XDOT =        6900.574103
     YDOT =      -7318.956149  feet/sec       YDOT =       -2230.817834  meter/sec
     ZDOT =       3994.190148                 ZDOT =        1217.429157
  
  
    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   17272.71790526  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6408 237.2317 0004605 322.0763  38.0065 15.54028412 38004
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17272.71790526   =   yrday.fracday
    Element set:     912
    Inclination:       51.6408  deg
    RA of node:       237.2317  deg
    Eccentricity:     .0004605     
    Arg of perigee:   322.0763  deg
    Mean anomaly:      38.0065  deg
    Mean motion:   15.54028412  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3800
    Checksum:              284
 
 
    Coasting Arc #14 (Orbit 3815)
    ---------------------------------------
 
    Vector Time (GMT): 2017/273/16:53:37.689
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4992764.74                 A    =         6780522.38  meter
     Y    =         376036.73  meter          E    =           .0008970
     Z    =        4571687.02                 I    =           51.33495
     XDOT =       2266.528642                 Wp   =           34.44187
     YDOT =       6676.151923  meter/sec      RA   =          231.24374  deg
     ZDOT =      -3014.252148                 TA   =           85.83873
                                              MA   =           85.73623
                                              Ha   =            220.789  n.mi
                                              Hp   =            215.604
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16380461.75                 X    =         4965981.61
     Y    =        1233716.31  feet           Y    =          431719.88  meter
     Z    =       14998973.15                 Z    =         4595875.34
     XDOT =       7436.117591                 XDOT =        2206.347505
     YDOT =      21903.385574  feet/sec       YDOT =        6701.161037  meter/sec
     ZDOT =      -9889.278700                 ZDOT =       -3003.388758
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3442472.45                 X    =        -1049265.60
     Y    =       15961483.05  feet           Y    =         4865060.03  meter
     Z    =       15105999.51                 Z    =         4604308.65
     XDOT =     -21556.561082                 XDOT =       -6570.439818
     YDOT =       4696.763267  feet/sec       YDOT =        1431.573444  meter/sec
     ZDOT =      -9842.089337                 ZDOT =       -2999.868830
  
  
    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   17273.74681093  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6413 232.1034 0004753 326.1221  33.9627 15.54065430 38164
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17273.74681093   =   yrday.fracday
    Element set:     913
    Inclination:       51.6413  deg
    RA of node:       232.1034  deg
    Eccentricity:     .0004753     
    Arg of perigee:   326.1221  deg
    Mean anomaly:      33.9627  deg
    Mean motion:   15.54065430  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3816
    Checksum:              287
 
 
    Coasting Arc #15 (Orbit 3821)
    ---------------------------------------
 
    Vector Time (GMT): 2017/274/01:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3481072.07                 A    =         6788933.03  meter
     Y    =       -5670443.20  meter          E    =           .0014129
     Z    =        1304972.65                 I    =           51.36941
     XDOT =       4758.217037                 Wp   =           42.35171
     YDOT =      -1578.433704  meter/sec      RA   =          229.43673  deg
     ZDOT =       5807.565745                 TA   =          331.91106
                                              MA   =          331.98722
                                              Ha   =            220.847  n.mi
                                              Hp   =            215.622
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11420840.11                 X    =        -3423743.88
     Y    =      -18603816.27  feet           Y    =        -5709050.26  meter
     Z    =        4281406.33                 Z    =         1288202.38
     XDOT =      15610.948285                 XDOT =        4747.303438
     YDOT =      -5178.588269  feet/sec       YDOT =       -1525.284558  meter/sec
     ZDOT =      19053.693388                 ZDOT =        5830.653419
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19990976.04                 X    =        -6093249.50
     Y    =       -8804671.79  feet           Y    =        -2683663.96  meter
     Z    =        4207925.93                 Z    =         1282575.82
     XDOT =       9160.126721                 XDOT =        2792.006624
     YDOT =     -11600.697329  feet/sec       YDOT =       -3535.892546  meter/sec
     ZDOT =      19156.113137                 ZDOT =        5838.783284
  
  
    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   17274.13265078  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6407 230.1751 0004162 325.6916  34.3967 15.54026556 38225
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17274.13265078   =   yrday.fracday
    Element set:     914
    Inclination:       51.6407  deg
    RA of node:       230.1751  deg
    Eccentricity:     .0004162     
    Arg of perigee:   325.6916  deg
    Mean anomaly:      34.3967  deg
    Mean motion:   15.54026556  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3822
    Checksum:              304
 
 
    Coasting Arc #16 (Orbit 3836)
    ---------------------------------------
 
    Vector Time (GMT): 2017/275/01:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2483893.39                 A    =         6786190.02  meter
     Y    =        5633525.22  meter          E    =           .0002310
     Z    =       -2857550.19                 I    =           51.38186
     XDOT =      -5768.284622                 Wp   =           55.82133
     YDOT =        -14.209920  meter/sec      RA   =          224.44487  deg
     ZDOT =      -5043.688297                 TA   =          156.78213
                                              MA   =          156.77170
                                              Ha   =            220.919  n.mi
                                              Hp   =            215.558
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8149256.51                 X    =         2434593.83
     Y    =       18482694.28  feet           Y    =         5661025.84  meter
     Z    =       -9375164.66                 Z    =        -2845604.52
     XDOT =     -18924.818315                 XDOT =       -5743.197144
     YDOT =        -46.620473  feet/sec       YDOT =         -78.575099  meter/sec
     ZDOT =     -16547.533783                 ZDOT =       -5071.648013
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17436036.67                 X    =         5314503.98
     Y    =       10245973.75  feet           Y    =         3122972.80  meter
     Z    =       -9323021.44                 Z    =        -2841656.93
     XDOT =     -14578.645110                 XDOT =       -4443.571030
     YDOT =       9644.540526  feet/sec       YDOT =        2939.655952  meter/sec
     ZDOT =     -16671.319024                 ZDOT =       -5081.418038
  
  
    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   17275.09724436  .00016717  00000-0  10270-3 0  9150
    2 25544  51.6403 225.3679 0004146 327.9114  32.1786 15.54030860 38377
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17275.09724436   =   yrday.fracday
    Element set:     915
    Inclination:       51.6403  deg
    RA of node:       225.3679  deg
    Eccentricity:     .0004146     
    Arg of perigee:   327.9114  deg
    Mean anomaly:      32.1786  deg
    Mean motion:   15.54030860  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3837
    Checksum:              311
 
 
    Coasting Arc #17 (Orbit 3852)
    ---------------------------------------
 
    Vector Time (GMT): 2017/276/01:42:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904844.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1224117.85                 A    =         6782360.67  meter
     Y    =       -5251872.44  meter          E    =           .0008338
     Z    =        4105380.16                 I    =           51.39426
     XDOT =       6514.168785                 Wp   =           81.96774
     YDOT =       1445.174552  meter/sec      RA   =          219.44494  deg
     ZDOT =       3785.659934                 TA   =          328.84947
                                              MA   =          328.89887
                                              Ha   =            220.927  n.mi
                                              Hp   =            215.399
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4016134.67                 X    =        -1185241.07
     Y    =      -17230552.62  feet           Y    =        -5265343.47  meter
     Z    =       13469095.00                 Z    =         4099528.83
     XDOT =      21371.944834                 XDOT =        6479.135323
     YDOT =       4741.386324  feet/sec       YDOT =        1517.825029  meter/sec
     ZDOT =      12420.144139                 ZDOT =        3817.218651
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13566247.08                 X    =        -4134992.11
     Y    =      -11386706.04  feet           Y    =        -3470668.00  meter
     Z    =       13443870.98                 Z    =         4097691.88
     XDOT =      19090.351586                 XDOT =        5818.739163
     YDOT =      -7894.502483  feet/sec       YDOT =       -2406.244357  meter/sec
     ZDOT =      12559.688637                 ZDOT =        3828.193097
  
  
    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   17276.12613752  .00016717  00000-0  10270-3 0  9164
    2 25544  51.6410 220.2396 0004147 331.0161  29.0761 15.54073565 38539
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17276.12613752   =   yrday.fracday
    Element set:     916
    Inclination:       51.6410  deg
    RA of node:       220.2396  deg
    Eccentricity:     .0004147     
    Arg of perigee:   331.0161  deg
    Mean anomaly:      29.0761  deg
    Mean motion:   15.54073565  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3853
    Checksum:              287
 
             

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