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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)  :   80.2
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.526
   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 
   ------------------------------------------------------------------------
   090/02:35:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.1  
   000/00:00:00.000           0.0               0.0              214.0  
   
   093/14:35:23.666           1.8               2.2              2.2    
   N/A                        0.3              -0.2              222.6  
   000/00:00:43.331          -1.1              -0.0              214.5  
   
   094/02:52:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.4  
   000/00:00:00.000           0.0               0.0              214.6  
   
 
 
    Coasting Arc #1 (Orbit 857)
    ---------------------------------------
 
    Vector Time (GMT): 2017/083/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1359126.13                 A    =         6785193.77  meter
     Y    =       -5944321.72  meter          E    =           .0011003
     Z    =        2974018.40                 I    =           52.01452
     XDOT =       4569.520986                 Wp   =           62.88174
     YDOT =      -3564.597891  meter/sec      RA   =           99.50774  deg
     ZDOT =      -5017.363904                 TA   =           83.32588
                                              MA   =           83.20065
                                              Ha   =            221.427  n.mi
                                              Hp   =            215.157
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4459075.23                 X    =        -1307000.39
     Y    =      -19502367.86  feet           Y    =        -5959228.59  meter
     Z    =        9757278.21                 Z    =         2967543.54
     XDOT =      14991.866752                 XDOT =        4633.413360
     YDOT =     -11694.874972  feet/sec       YDOT =       -3513.141770  meter/sec
     ZDOT =     -16461.167664                 ZDOT =       -4995.011136
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4961258.41                 X    =        -1512191.56
     Y    =      -19394565.05  feet           Y    =        -5911463.43  meter
     Z    =        9729693.92                 Z    =         2965610.71
     XDOT =      13416.862819                 XDOT =        4089.459787
     YDOT =     -11672.078892  feet/sec       YDOT =       -3557.649646  meter/sec
     ZDOT =     -16362.145773                 ZDOT =       -4987.182032
  
  
    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   17083.53823120  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6396 100.2544 0007515 334.1083  25.9693 15.54269521  8583
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17083.53823120   =   yrday.fracday
    Element set:     900
    Inclination:       51.6396  deg
    RA of node:       100.2544  deg
    Eccentricity:     .0007515     
    Arg of perigee:   334.1083  deg
    Mean anomaly:      25.9693  deg
    Mean motion:   15.54269521  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             858
    Checksum:              297
 
 
    Coasting Arc #2 (Orbit 872)
    ---------------------------------------
 
    Vector Time (GMT): 2017/084/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         555331.18                 A    =         6788029.63  meter
     Y    =        6613738.57  meter          E    =           .0013826
     Z    =       -1382718.61                 I    =           52.02907
     XDOT =      -4703.615851                 Wp   =            9.93189
     YDOT =       1612.044149  meter/sec      RA   =           94.55810  deg
     ZDOT =       5843.449292                 TA   =          335.07395
                                              MA   =          335.14066
                                              Ha   =            221.477  n.mi
                                              Hp   =            214.946
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1821952.71                 X    =          488049.90
     Y    =       21698617.34  feet           Y    =         6619572.28  meter
     Z    =       -4536478.37                 Z    =        -1380185.30
     XDOT =     -15431.810534                 XDOT =       -4749.677016
     YDOT =       5288.858758  feet/sec       YDOT =        1559.188377  meter/sec
     ZDOT =      19171.421561                 ZDOT =        5820.488629
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2712485.22                 X    =          826765.50
     Y    =       21607488.09  feet           Y    =         6585962.37  meter
     Z    =       -4526369.89                 Z    =        -1379637.54
     XDOT =     -13758.155796                 XDOT =       -4193.485887
     YDOT =       5706.861077  feet/sec       YDOT =        1739.451256  meter/sec
     ZDOT =      19070.024429                 ZDOT =        5812.543446
  
  
    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   17084.50268653  .00016717  00000-0  10270-3 0  9013
    2 25544  51.6400  95.4461 0007369 336.7804  23.3014 15.54297881  8734
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17084.50268653   =   yrday.fracday
    Element set:     901
    Inclination:       51.6400  deg
    RA of node:        95.4461  deg
    Eccentricity:     .0007369     
    Arg of perigee:   336.7804  deg
    Mean anomaly:      23.3014  deg
    Mean motion:   15.54297881  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             873
    Checksum:              311
 
 
    Coasting Arc #3 (Orbit 888)
    ---------------------------------------
 
    Vector Time (GMT): 2017/085/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         256873.54                 A    =         6788854.92  meter
     Y    =       -6772389.36  meter          E    =           .0005335
     Z    =        -387753.62                 I    =           52.03222
     XDOT =       4705.871846                 Wp   =          102.25739
     YDOT =        519.430640  meter/sec      RA   =           89.61313  deg
     ZDOT =      -6025.595207                 TA   =           81.89763
                                              MA   =           81.83711
                                              Ha   =            221.719  n.mi
                                              Hp   =            214.771
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         842760.96                 X    =          334468.58
     Y    =      -22219125.20  feet           Y    =        -6769083.02  meter
     Z    =       -1272157.55                 Z    =         -386316.36
     XDOT =      15439.212092                 XDOT =        4728.982990
     YDOT =       1704.168768  feet/sec       YDOT =         572.183225  meter/sec
     ZDOT =     -19769.013145                 ZDOT =       -6002.679556
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -415305.51                 X    =         -126585.12
     Y    =      -22231646.54  feet           Y    =        -6776205.87  meter
     Z    =       -1264740.67                 Z    =         -385492.96
     XDOT =      14018.197503                 XDOT =        4272.746599
     YDOT =        843.732042  feet/sec       YDOT =         257.169526  meter/sec
     ZDOT =     -19668.152622                 ZDOT =       -5994.852919
  
  
    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   17085.53143370  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6391  90.3159 0007604 341.7147  18.3732 15.54267871  8893
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17085.53143370   =   yrday.fracday
    Element set:     902
    Inclination:       51.6391  deg
    RA of node:        90.3159  deg
    Eccentricity:     .0007604     
    Arg of perigee:   341.7147  deg
    Mean anomaly:      18.3732  deg
    Mean motion:   15.54267871  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             889
    Checksum:              313
 
 
    Coasting Arc #4 (Orbit 904)
    ---------------------------------------
 
    Vector Time (GMT): 2017/086/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1048154.18                 A    =         6787003.40  meter
     Y    =        6359044.35  meter          E    =           .0016348
     Z    =        2094001.79                 I    =           52.02401
     XDOT =      -4605.107022                 Wp   =           41.87218
     YDOT =      -2595.812142  meter/sec      RA   =           84.66748  deg
     ZDOT =       5564.786160                 TA   =          341.20747
                                              MA   =          341.26775
                                              Ha   =            221.799  n.mi
                                              Hp   =            214.590
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3438826.05                 X    =        -1129356.42
     Y    =       20863006.41  feet           Y    =         6346869.47  meter
     Z    =        6870084.61                 Z    =         2088711.99
     XDOT =     -15108.618839                 XDOT =       -4602.768753
     YDOT =      -8516.444035  feet/sec       YDOT =       -2647.295650  meter/sec
     ZDOT =      18257.172440                 ZDOT =        5542.422026
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1928033.59                 X    =         -587664.64
     Y    =       21064353.25  feet           Y    =         6420414.87  meter
     Z    =        6845752.87                 Z    =         2086585.47
     XDOT =     -14280.266572                 XDOT =       -4352.625251
     YDOT =      -7222.618990  feet/sec       YDOT =       -2201.454268  meter/sec
     ZDOT =      18159.079287                 ZDOT =        5534.887367
  
  
    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   17086.56017484  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6380  85.1867 0007591 344.0161  16.0751 15.54294618  9050
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17086.56017484   =   yrday.fracday
    Element set:     903
    Inclination:       51.6380  deg
    RA of node:        85.1867  deg
    Eccentricity:     .0007591     
    Arg of perigee:   344.0161  deg
    Mean anomaly:      16.0751  deg
    Mean motion:   15.54294618  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             905
    Checksum:              311
 
 
    Coasting Arc #5 (Orbit 919)
    ---------------------------------------
 
    Vector Time (GMT): 2017/087/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1861720.25                 A    =         6783509.44  meter
     Y    =       -5452253.26  meter          E    =           .0008951
     Z    =       -3591860.64                 I    =           52.00785
     XDOT =       4355.776927                 Wp   =           24.51864
     YDOT =       4436.460328  meter/sec      RA   =           79.71271  deg
     ZDOT =      -4472.707819                 TA   =          197.64878
                                              MA   =          197.67990
                                              Ha   =            221.973  n.mi
                                              Hp   =            214.469
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6108006.07                 X    =         1939998.00
     Y    =      -17887970.02  feet           Y    =        -5430997.10  meter
     Z    =      -11784319.69                 Z    =        -3582626.00
     XDOT =      14290.606717                 XDOT =        4327.569897
     YDOT =      14555.316038  feet/sec       YDOT =        4485.011198  meter/sec
     ZDOT =     -14674.238250                 ZDOT =       -4451.617847
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4526687.39                 X    =         1379734.32
     Y    =      -18378639.24  feet           Y    =        -5601809.24  meter
     Z    =      -11742747.59                 Z    =        -3579189.47
     XDOT =      14313.607730                 XDOT =        4362.787636
     YDOT =      12850.722005  feet/sec       YDOT =        3916.900067  meter/sec
     ZDOT =     -14582.066514                 ZDOT =       -4444.613874
  
  
    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   17087.52461885  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6378  80.3771 0007671 348.6510  11.4469 15.54265177  9205
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17087.52461885   =   yrday.fracday
    Element set:     904
    Inclination:       51.6378  deg
    RA of node:        80.3771  deg
    Eccentricity:     .0007671     
    Arg of perigee:   348.6510  deg
    Mean anomaly:      11.4469  deg
    Mean motion:   15.54265177  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             920
    Checksum:              322
 
 
    Coasting Arc #6 (Orbit 935)
    ---------------------------------------
 
    Vector Time (GMT): 2017/088/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2673726.54                 A    =         6779618.17  meter
     Y    =        4102725.07  meter          E    =           .0007392
     Z    =        4681285.53                 I    =           51.98906
     XDOT =      -3960.917513                 Wp   =           55.82408
     YDOT =      -5895.121234  meter/sec      RA   =           74.74757  deg
     ZDOT =       2905.036676                 TA   =            5.46154
                                              MA   =            5.45348
                                              Ha   =            222.167  n.mi
                                              Hp   =            214.212
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8772068.71                 X    =        -2742145.19
     Y    =       13460384.07  feet           Y    =         4072443.73  meter
     Z    =       15358548.34                 Z    =         4668130.53
     XDOT =     -12995.136196                 XDOT =       -3908.813736
     YDOT =     -19340.948930  feet/sec       YDOT =       -5939.123170  meter/sec
     ZDOT =       9530.960224                 ZDOT =        2885.922928
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7361068.81                 X    =        -2243653.77
     Y    =       14343752.61  feet           Y    =         4371975.79  meter
     Z    =       15299920.37                 Z    =         4663415.73
     XDOT =     -14029.715084                 XDOT =       -4276.257158
     YDOT =     -17274.709082  feet/sec       YDOT =       -5265.331328  meter/sec
     ZDOT =       9447.748217                 ZDOT =        2879.673657
  
  
    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   17088.55335160  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6385  75.2476 0007775 351.4476   8.6543 15.54289181  9365
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17088.55335160   =   yrday.fracday
    Element set:     905
    Inclination:       51.6385  deg
    RA of node:        75.2476  deg
    Eccentricity:     .0007775     
    Arg of perigee:   351.4476  deg
    Mean anomaly:       8.6543  deg
    Mean motion:   15.54289181  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             936
    Checksum:              333
 
 
    Coasting Arc #7 (Orbit 950)
    ---------------------------------------
 
    Vector Time (GMT): 2017/089/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3471777.34                 A    =         6777245.01  meter
     Y    =       -2498692.54  meter          E    =           .0016783
     Z    =       -5270022.06                 I    =           51.97173
     XDOT =       3353.011219                 Wp   =           54.43176
     YDOT =       6809.509402  meter/sec      RA   =           69.77255  deg
     ZDOT =      -1012.491635                 TA   =          205.86297
                                              MA   =          205.94696
                                              Ha   =            222.249  n.mi
                                              Hp   =            214.121
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11390345.59                 X    =         3525059.84
     Y    =       -8197810.16  feet           Y    =        -2459571.47  meter
     Z    =      -17290098.61                 Z    =        -5253027.32
     XDOT =      11000.692976                 XDOT =        3281.534558
     YDOT =      22340.910113  feet/sec       YDOT =        6846.605274  meter/sec
     ZDOT =      -3321.822948                 ZDOT =        -996.377946
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10383386.07                 X    =         3164856.07
     Y    =       -9577415.03  feet           Y    =        -2919196.10  meter
     Z    =      -17214818.88                 Z    =        -5247076.80
     XDOT =      13039.030064                 XDOT =        3974.296364
     YDOT =      20024.401757  feet/sec       YDOT =        6103.437655  meter/sec
     ZDOT =      -3251.996127                 ZDOT =        -991.208420
  
  
    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   17089.51778471  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6388  70.4386 0007830 356.0146   4.0943 15.54280580  9517
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17089.51778471   =   yrday.fracday
    Element set:     906
    Inclination:       51.6388  deg
    RA of node:        70.4386  deg
    Eccentricity:     .0007830     
    Arg of perigee:   356.0146  deg
    Mean anomaly:       4.0943  deg
    Mean motion:   15.54280580  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             951
    Checksum:              319
 
 
    Coasting Arc #8 (Orbit 960)
    ---------------------------------------
 
    Vector Time (GMT): 2017/090/02:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2177402.98                 A    =         6779285.78  meter
     Y    =        4322910.43  meter          E    =           .0007489
     Z    =        4739341.48                 I    =           51.97474
     XDOT =      -4684.913667                 Wp   =           59.71035
     YDOT =      -5405.287939  meter/sec      RA   =           66.76611  deg
     ZDOT =       2778.364528                 TA   =            2.92884
                                              MA   =            2.92446
                                              Ha   =            222.141  n.mi
                                              Hp   =            213.981
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7143710.55                 X    =        -2248602.75
     Y    =       14182777.01  feet           Y    =         4298163.62  meter
     Z    =       15549020.62                 Z    =         4728590.82
     XDOT =     -15370.451665                 XDOT =       -4637.618242
     YDOT =     -17733.884315  feet/sec       YDOT =       -5457.413083  meter/sec
     ZDOT =       9115.369185                 ZDOT =        2755.721814
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5316166.56                 X    =        -1620367.57
     Y    =      -15013838.74  feet           Y    =        -4576218.05  meter
     Z    =       15500929.83                 Z    =         4724683.41
     XDOT =      22390.257327                 XDOT =        6824.550433
     YDOT =       1379.611142  feet/sec       YDOT =         420.505476  meter/sec
     ZDOT =       9016.555301                 ZDOT =        2748.246056
  
  
    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   17090.16073726  .00016717  00000-0  10270-3 0  9073
    2 25544  51.6416  67.2292 0007345 356.7956   3.3148 15.54318986  9618
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17090.16073726   =   yrday.fracday
    Element set:     907
    Inclination:       51.6416  deg
    RA of node:        67.2292  deg
    Eccentricity:     .0007345     
    Arg of perigee:   356.7956  deg
    Mean anomaly:       3.3148  deg
    Mean motion:   15.54318986  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             961
    Checksum:              325
 
 
    Coasting Arc #9 (Orbit 975)
    ---------------------------------------
 
    Vector Time (GMT): 2017/091/02:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3184289.77                 A    =         6777077.29  meter
     Y    =       -2820450.59  meter          E    =           .0017039
     Z    =       -5289346.12                 I    =           51.95430
     XDOT =       4179.657065                 Wp   =           57.69720
     YDOT =       6357.080148  meter/sec      RA   =           61.79083  deg
     ZDOT =       -866.745523                 TA   =          203.99908
                                              MA   =          204.07858
                                              Ha   =            222.196  n.mi
                                              Hp   =            213.950
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10447144.92                 X    =         3241285.46
     Y    =       -9253446.81  feet           Y    =        -2784523.45  meter
     Z    =      -17353497.78                 Z    =        -5273738.99
     XDOT =      13712.785646                 XDOT =        4112.470170
     YDOT =      20856.562165  feet/sec       YDOT =        6403.444165  meter/sec
     ZDOT =      -2843.653290                 ZDOT =        -846.605521
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -300822.72                 X    =          -91690.76
     Y    =       14038400.95  feet           Y    =         4278904.61  meter
     Z    =      -17284264.66                 Z    =        -5268243.87
     XDOT =     -23632.549233                 XDOT =       -7203.201006
     YDOT =      -3927.345738  feet/sec       YDOT =       -1197.054981  meter/sec
     ZDOT =      -2756.041329                 ZDOT =        -840.041397
  
  
    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   17091.12516391  .00016717  00000-0  10270-3 0  9081
    2 25544  51.6424  62.4218 0007405    .2379 359.8776 15.54306128  9766
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17091.12516391   =   yrday.fracday
    Element set:     908
    Inclination:       51.6424  deg
    RA of node:        62.4218  deg
    Eccentricity:     .0007405     
    Arg of perigee:      .2379  deg
    Mean anomaly:     359.8776  deg
    Mean motion:   15.54306128  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             976
    Checksum:              311
 
 
    Coasting Arc #10 (Orbit 991)
    ---------------------------------------
 
    Vector Time (GMT): 2017/092/02:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4142755.16                 A    =         6777202.58  meter
     Y    =        1155933.98  meter          E    =           .0010466
     Z    =        5235895.39                 I    =           51.93934
     XDOT =      -3366.289818                 Wp   =           21.35570
     YDOT =      -6795.261429  meter/sec      RA   =           56.80916  deg
     ZDOT =      -1153.064779                 TA   =           79.70988
                                              MA   =           79.59189
                                              Ha   =            222.406  n.mi
                                              Hp   =            213.607
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13591716.41                 X    =        -4180806.84
     Y    =        3792434.32  feet           Y    =         1109394.47  meter
     Z    =       17178134.47                 Z    =         5215678.50
     XDOT =     -11044.257934                 XDOT =       -3284.452176
     YDOT =     -22294.164794  feet/sec       YDOT =       -6832.448052  meter/sec
     ZDOT =      -3783.020929                 ZDOT =       -1169.218088
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6232802.80                 X    =         1899758.29
     Y    =      -12779981.05  feet           Y    =        -3895338.22  meter
     Z    =       17088881.49                 Z    =         5208691.08
     XDOT =      23070.299616                 XDOT =        7031.827323
     YDOT =       6054.269561  feet/sec       YDOT =        1845.341362  meter/sec
     ZDOT =      -3852.982073                 ZDOT =       -1174.388936
  
  
    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   17092.15387847  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6430  57.2916 0007532   4.3686 355.7531 15.54336256  9924
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17092.15387847   =   yrday.fracday
    Element set:     909
    Inclination:       51.6430  deg
    RA of node:        57.2916  deg
    Eccentricity:     .0007532     
    Arg of perigee:     4.3686  deg
    Mean anomaly:     355.7531  deg
    Mean motion:   15.54336256  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             992
    Checksum:              326
 
 
    Coasting Arc #11 (Orbit 1006)
    ---------------------------------------
 
    Vector Time (GMT): 2017/093/02:35:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900777.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4946745.23                 A    =         6779782.49  meter
     Y    =         433766.57  meter          E    =           .0011290
     Z    =       -4623052.41                 I    =           51.92904
     XDOT =       2232.970215                 Wp   =           69.29357
     YDOT =       6675.976267  meter/sec      RA   =           51.83313  deg
     ZDOT =       3025.541817                 TA   =          230.76091
                                              MA   =          230.86116
                                              Ha   =            222.445  n.mi
                                              Hp   =            213.534
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16229479.10                 X    =         4963983.71
     Y    =        1423118.68  feet           Y    =          489180.54  meter
     Z    =      -15167494.77                 Z    =        -4598980.71
     XDOT =       7326.017765                 XDOT =        2143.455088
     YDOT =      21902.809274  feet/sec       YDOT =        6700.446521  meter/sec
     ZDOT =       9926.318296                 ZDOT =        3036.171123
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11682953.54                 X    =        -3560964.24
     Y    =       11494900.35  feet           Y    =         3503645.63  meter
     Z    =      -15061541.06                 Z    =        -4590757.71
     XDOT =     -20535.016393                 XDOT =       -6259.072997
     YDOT =      -7847.500992  feet/sec       YDOT =       -2391.918302  meter/sec
     ZDOT =       9971.956492                 ZDOT =        3039.452339
  
  
    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   17093.11829451  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6427  52.4846 0007490   8.3819 351.7457 15.54340381 10079
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17093.11829451   =   yrday.fracday
    Element set:     910
    Inclination:       51.6427  deg
    RA of node:        52.4846  deg
    Eccentricity:     .0007490     
    Arg of perigee:     8.3819  deg
    Mean anomaly:     351.7457  deg
    Mean motion:   15.54340381  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1007
    Checksum:              302
 
 
    Coasting Arc #12 (Orbit 1014)
    ---------------------------------------
 
    Vector Time (GMT): 2017/093/14:35:45.331
    Vector Time (MET): N/A
    Weight (LBS)     : 900551.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1088474.56                 A    =         6784369.69  meter
     Y    =       -5636130.70  meter          E    =           .0009271
     Z    =       -3627929.85                 I    =           51.92930
     XDOT =       6015.645480                 Wp   =           36.93082
     YDOT =       1689.094604  meter/sec      RA   =           49.39696  deg
     ZDOT =      -4427.580940                 TA   =          185.80622
                                              MA   =          185.81698
                                              Ha   =            222.588  n.mi
                                              Hp   =            214.527
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3571110.77                 X    =        -1007746.24
     Y    =      -18491242.47  feet           Y    =        -5647851.60  meter
     Z    =      -11902656.98                 Z    =        -3633020.91
     XDOT =      19736.369685                 XDOT =        6017.817558
     YDOT =       5541.648964  feet/sec       YDOT =        1756.377496  meter/sec
     ZDOT =     -14526.184185                 ZDOT =       -4398.353559
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16442560.32                 X    =        -5011692.39
     Y    =       -9154815.19  feet           Y    =        -2790387.67  meter
     Z    =      -11924080.35                 Z    =        -3634459.69
     XDOT =      16284.005183                 XDOT =        4963.364780
     YDOT =     -10488.286977  feet/sec       YDOT =       -3196.829870  meter/sec
     ZDOT =     -14397.744233                 ZDOT =       -4388.432442
  
  
    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   17093.63265303  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6417  49.9220 0006563   1.9992 358.1186 15.53912094 10150
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17093.63265303   =   yrday.fracday
    Element set:     911
    Inclination:       51.6417  deg
    RA of node:        49.9220  deg
    Eccentricity:     .0006563     
    Arg of perigee:     1.9992  deg
    Mean anomaly:     358.1186  deg
    Mean motion:   15.53912094  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1015
    Checksum:              301
 
 
    Coasting Arc #13 (Orbit 1022)
    ---------------------------------------
 
    Vector Time (GMT): 2017/094/02:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900551.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2934526.11                 A    =         6787825.76  meter
     Y    =       -5698079.38  meter          E    =           .0004694
     Z    =       -2241872.12                 I    =           51.92967
     XDOT =       5324.672223                 Wp   =           69.07467
     YDOT =       -590.875154  meter/sec      RA   =           46.85064  deg
     ZDOT =      -5475.596969                 TA   =          135.72148
                                              MA   =          135.68392
                                              Ha   =            222.448  n.mi
                                              Hp   =            214.601
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9627710.34                 X    =        -2859700.68
     Y    =      -18694486.15  feet           Y    =        -5730477.01  meter
     Z    =       -7355223.50                 Z    =        -2255945.04
     XDOT =      17469.397058                 XDOT =        5357.481585
     YDOT =      -1938.566777  feet/sec       YDOT =        -531.147973  meter/sec
     ZDOT =     -17964.556986                 ZDOT =       -5449.651622
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20796492.34                 X    =         6338770.87
     Y    =        2963425.47  feet           Y    =          903252.08  meter
     Z    =       -7416194.94                 Z    =        -2260456.22
     XDOT =      -8346.807084                 XDOT =       -2544.106799
     YDOT =      13966.110326  feet/sec       YDOT =        4256.870427  meter/sec
     ZDOT =     -17850.168481                 ZDOT =       -5440.731353
  
  
    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   17094.14714424  .00016717  00000-0  10270-3 0  9128
    2 25544  51.6416  47.3557 0005968   2.6968 357.4222 15.53899626 10230
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17094.14714424   =   yrday.fracday
    Element set:     912
    Inclination:       51.6416  deg
    RA of node:        47.3557  deg
    Eccentricity:     .0005968     
    Arg of perigee:     2.6968  deg
    Mean anomaly:     357.4222  deg
    Mean motion:   15.53899626  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1023
    Checksum:              322
 
 
    Coasting Arc #14 (Orbit 1038)
    ---------------------------------------
 
    Vector Time (GMT): 2017/095/02:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900551.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1836566.77                 A    =         6784364.19  meter
     Y    =        5439151.26  meter          E    =           .0013636
     Z    =        3599449.01                 I    =           51.89638
     XDOT =      -6190.827984                 Wp   =           66.91534
     YDOT =       -861.897459  meter/sec      RA   =           41.89092  deg
     ZDOT =       4453.053881                 TA   =          335.54428
                                              MA   =          335.60891
                                              Ha   =            222.511  n.mi
                                              Hp   =            214.405
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6025481.52                 X    =         1758123.94
     Y    =       17844984.45  feet           Y    =         5459250.67  meter
     Z    =       11809215.93                 Z    =         3608179.52
     XDOT =     -20311.115433                 XDOT =       -6202.360623
     YDOT =      -2827.747568  feet/sec       YDOT =        -931.191623  meter/sec
     ZDOT =      14609.756829                 ZDOT =        4422.952870
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18098635.90                 X    =        -5516464.22
     Y    =       -5128612.57  feet           Y    =        -1563201.11  meter
     Z    =       11846695.32                 Z    =         3610872.73
     XDOT =      13448.323744                 XDOT =        4099.049077
     YDOT =     -13955.480743  feet/sec       YDOT =       -4253.630530  meter/sec
     ZDOT =      14477.326143                 ZDOT =        4412.689008
  
  
    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   17095.17612149  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6424  42.2275 0006066   6.2789 353.8439 15.53932101 10394
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17095.17612149   =   yrday.fracday
    Element set:     913
    Inclination:       51.6424  deg
    RA of node:        42.2275  deg
    Eccentricity:     .0006066     
    Arg of perigee:     6.2789  deg
    Mean anomaly:     353.8439  deg
    Mean motion:   15.53932101  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1039
    Checksum:              302
 
 
    Coasting Arc #15 (Orbit 1053)
    ---------------------------------------
 
    Vector Time (GMT): 2017/096/02:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900551.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -503358.98                 A    =         6780867.12  meter
     Y    =       -4933983.81  meter          E    =           .0014425
     Z    =       -4638140.04                 I    =           51.85877
     XDOT =       6724.093021                 Wp   =           48.09527
     YDOT =       2121.904819  meter/sec      RA   =           36.92120  deg
     ZDOT =      -2983.571838                 TA   =          192.18566
                                              MA   =          192.22059
                                              Ha   =            222.655  n.mi
                                              Hp   =            214.309
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1651440.21                 X    =         -425618.71
     Y    =      -16187610.93  feet           Y    =        -4939178.47  meter
     Z    =      -15216994.89                 Z    =        -4640395.92
     XDOT =      22060.672641                 XDOT =        6714.358278
     YDOT =       6961.629984  feet/sec       YDOT =        2197.043467  meter/sec
     ZDOT =      -9788.621515                 ZDOT =       -2950.932200
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14387044.67                 X    =         4385171.22
     Y    =        7583107.58  feet           Y    =         2311331.19  meter
     Z    =      -15226042.20                 Z    =        -4640897.66
     XDOT =     -17403.736165                 XDOT =       -5304.658783
     YDOT =      13630.142077  feet/sec       YDOT =        4154.467305  meter/sec
     ZDOT =      -9645.241902                 ZDOT =       -2939.869732
  
  
    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   17096.14078385  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6416  37.4210 0006135   9.7626 350.3644 15.53908369 10541
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17096.14078385   =   yrday.fracday
    Element set:     914
    Inclination:       51.6416  deg
    RA of node:        37.4210  deg
    Eccentricity:     .0006135     
    Arg of perigee:     9.7626  deg
    Mean anomaly:     350.3644  deg
    Mean motion:   15.53908369  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1054
    Checksum:              306
 
 
    Coasting Arc #16 (Orbit 1069)
    ---------------------------------------
 
    Vector Time (GMT): 2017/097/02:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900551.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -989064.00                 A    =         6778318.11  meter
     Y    =        4212828.65  meter          E    =           .0006010
     Z    =        5212504.86                 I    =           51.82444
     XDOT =      -6887.339185                 Wp   =           51.20678
     YDOT =      -3146.198059  meter/sec      RA   =           31.94100  deg
     ZDOT =       1238.661255                 TA   =           26.95806
                                              MA   =           26.92686
                                              Ha   =            222.728  n.mi
                                              Hp   =            214.112
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3244960.63                 X    =        -1061419.21
     Y    =       13821616.30  feet           Y    =         4201364.27  meter
     Z    =       17101393.89                 Z    =         5207524.10
     XDOT =     -22596.257169                 XDOT =       -6857.662502
     YDOT =     -10322.172110  feet/sec       YDOT =       -3223.050879  meter/sec
     ZDOT =       4063.849263                 ZDOT =        1205.277157
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9893493.93                 X    =        -3015536.95
     Y    =      -10220638.22  feet           Y    =        -3115250.53  meter
     Z    =       17078695.84                 Z    =         5205586.49
     XDOT =      20063.830586                 XDOT =        6115.455563
     YDOT =     -12890.575239  feet/sec       YDOT =       -3929.047333  meter/sec
     ZDOT =       3917.385174                 ZDOT =        1194.019001
  
  
    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   17097.16974959  .00016717  00000-0  10270-3 0  9157
    2 25544  51.6419  32.2934 0006135  13.2747 346.8566 15.53954881 10705
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17097.16974959   =   yrday.fracday
    Element set:     915
    Inclination:       51.6419  deg
    RA of node:        32.2934  deg
    Eccentricity:     .0006135     
    Arg of perigee:    13.2747  deg
    Mean anomaly:     346.8566  deg
    Mean motion:   15.53954881  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1070
    Checksum:              336
 
 
    Coasting Arc #17 (Orbit 1084)
    ---------------------------------------
 
    Vector Time (GMT): 2017/098/02:52:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900551.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2516419.63                 A    =         6778094.75  meter
     Y    =       -3405686.64  meter          E    =           .0017029
     Z    =       -5306257.04                 I    =           51.79492
     XDOT =       6565.482756                 Wp   =           73.62848
     YDOT =       3889.442953  meter/sec      RA   =           26.95523  deg
     ZDOT =        623.585179                 TA   =          202.28361
                                              MA   =          202.35769
                                              Ha   =            222.833  n.mi
                                              Hp   =            214.097
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8255969.92                 X    =         2580091.13
     Y    =      -11173512.60  feet           Y    =        -3377190.97  meter
     Z    =      -17408979.80                 Z    =        -5293877.98
     XDOT =      21540.297755                 XDOT =        6518.472954
     YDOT =      12760.639608  feet/sec       YDOT =        3962.599853  meter/sec
     ZDOT =       2045.883133                 ZDOT =         655.363661
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5200937.74                 X    =         1585245.82
     Y    =       12956670.14  feet           Y    =         3949193.06  meter
     Z    =      -17353845.28                 Z    =        -5289452.04
     XDOT =     -21141.903016                 XDOT =       -6444.052039
     YDOT =      11385.352667  feet/sec       YDOT =        3470.255493  meter/sec
     ZDOT =       2185.129127                 ZDOT =         666.027358
  
  
    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   17098.13440076  .00016717  00000-0  10270-3 0  9164
    2 25544  51.6416  27.4863 0006251  16.6533 343.4824 15.53925168 10850
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17098.13440076   =   yrday.fracday
    Element set:     916
    Inclination:       51.6416  deg
    RA of node:        27.4863  deg
    Eccentricity:     .0006251     
    Arg of perigee:    16.6533  deg
    Mean anomaly:     343.4824  deg
    Mean motion:   15.53925168  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1085
    Checksum:              308
 
             

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