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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  17659.2714
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   76.1
   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 
   ------------------------------------------------------------------------
   237/06:36:20.931           0.4               1.1              1.1    
   N/A                        0.9              -0.0              221.6  
   000/00:02:41.861           0.3               0.0              215.1  
   
   242/05:30:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.0  
   000/00:00:00.000           0.0               0.0              215.7  
   
 
 
    Coasting Arc #1 (Orbit 3112)
    ---------------------------------------
 
    Vector Time (GMT): 2017/228/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3178453.40                 A    =         6780151.48  meter
     Y    =       -3808704.55  meter          E    =           .0010434
     Z    =        4612597.31                 I    =           52.00400
     XDOT =       3137.782321                 Wp   =           93.42065
     YDOT =      -6308.785821  meter/sec      RA   =           96.73572  deg
     ZDOT =      -3041.794277                 TA   =           26.80129
                                              MA   =           26.74741
                                              Ha   =            222.366  n.mi
                                              Hp   =            213.437
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10427996.73                 X    =        -3158032.82
     Y    =      -12495749.85  feet           Y    =        -3844134.10  meter
     Z    =       15133193.27                 Z    =         4597206.99
     XDOT =      10294.561420                 XDOT =        3222.871074
     YDOT =     -20698.116210  feet/sec       YDOT =       -6273.221184  meter/sec
     ZDOT =      -9979.640017                 ZDOT =       -3026.345463
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1231032.11                 X    =          375218.59
     Y    =       16291476.63  feet           Y    =         4965642.08  meter
     Z    =       15065615.42                 Z    =         4591999.58
     XDOT =     -19321.254081                 XDOT =       -5889.118244
     YDOT =      10640.634615  feet/sec       YDOT =        3243.265431  meter/sec
     ZDOT =      -9910.219604                 ZDOT =       -3020.634935
  
  
    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   17228.54286976  .00016717  00000-0  10270-3 0  9004
    2 25544  51.6416  97.4490 0004886 146.9684 213.1774 15.54202015 31130
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17228.54286976   =   yrday.fracday
    Element set:     900
    Inclination:       51.6416  deg
    RA of node:        97.4490  deg
    Eccentricity:     .0004886     
    Arg of perigee:   146.9684  deg
    Mean anomaly:     213.1774  deg
    Mean motion:   15.54202015  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3113
    Checksum:              318
 
 
    Coasting Arc #2 (Orbit 3127)
    ---------------------------------------
 
    Vector Time (GMT): 2017/229/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2594761.72                 A    =         6784015.31  meter
     Y    =        5188985.55  meter          E    =           .0008842
     Z    =       -3527398.46                 I    =           52.01861
     XDOT =      -3699.792088                 Wp   =          122.20252
     YDOT =       4934.391421  meter/sec      RA   =           91.77295  deg
     ZDOT =       4540.889653                 TA   =          196.56550
                                              MA   =          196.59440
                                              Ha   =            222.271  n.mi
                                              Hp   =            213.647
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8512997.77                 X    =         2553678.45
     Y    =       17024230.81  feet           Y    =         5217772.32  meter
     Z    =      -11572829.60                 Z    =        -3514893.70
     XDOT =     -12138.425484                 XDOT =       -3776.751964
     YDOT =      16188.948230  feet/sec       YDOT =        4892.587407  meter/sec
     ZDOT =      14897.931932                 ZDOT =        4522.730601
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2665541.74                 X    =          812457.12
     Y    =      -18879899.77  feet           Y    =        -5754593.45  meter
     Z    =      -11518256.05                 Z    =        -3510764.44
     XDOT =      17911.523832                 XDOT =        5459.432464
     YDOT =      -6503.078519  feet/sec       YDOT =       -1982.138333  meter/sec
     ZDOT =      14816.705731                 ZDOT =        4516.131907
  
  
    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   17229.50738474  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6409  92.6408 0004965 151.0911 209.0517 15.54161015 31285
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17229.50738474   =   yrday.fracday
    Element set:     901
    Inclination:       51.6409  deg
    RA of node:        92.6408  deg
    Eccentricity:     .0004965     
    Arg of perigee:   151.0911  deg
    Mean anomaly:     209.0517  deg
    Mean motion:   15.54161015  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3128
    Checksum:              296
 
 
    Coasting Arc #3 (Orbit 3143)
    ---------------------------------------
 
    Vector Time (GMT): 2017/230/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1936339.78                 A    =         6787442.64  meter
     Y    =       -6166729.16  meter          E    =           .0017803
     Z    =        2039113.76                 I    =           52.03114
     XDOT =       4192.771393                 Wp   =          121.99595
     YDOT =      -3173.582558  meter/sec      RA   =           86.82069  deg
     ZDOT =      -5589.784615                 TA   =           35.56903
                                              MA   =           35.45049
                                              Ha   =            222.198  n.mi
                                              Hp   =            213.662
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6352820.79                 X    =        -1877142.73
     Y    =      -20232051.06  feet           Y    =        -6188051.68  meter
     Z    =        6690005.79                 Z    =         2029851.43
     XDOT =      13755.811657                 XDOT =        4255.099645
     YDOT =     -10412.016265  feet/sec       YDOT =       -3126.347530  meter/sec
     ZDOT =     -18339.188370                 ZDOT =       -5569.266413
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5947301.44                 X    =        -1812737.48
     Y    =       20368064.68  feet           Y    =         6208186.12  meter
     Z    =        6649958.34                 Z    =         2026907.30
     XDOT =     -15838.598863                 XDOT =       -4827.604933
     YDOT =       1361.396403  feet/sec       YDOT =         414.953624  meter/sec
     ZDOT =     -18247.778946                 ZDOT =       -5561.923023
  
  
    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   17230.53619678  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6418  87.5119 0004855 154.3258 205.8136 15.54179596 31447
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17230.53619678   =   yrday.fracday
    Element set:     902
    Inclination:       51.6418  deg
    RA of node:        87.5119  deg
    Eccentricity:     .0004855     
    Arg of perigee:   154.3258  deg
    Mean anomaly:     205.8136  deg
    Mean motion:   15.54179596  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3144
    Checksum:              328
 
 
    Coasting Arc #4 (Orbit 3158)
    ---------------------------------------
 
    Vector Time (GMT): 2017/231/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1244653.56                 A    =         6789172.87  meter
     Y    =        6661496.08  meter          E    =           .0010233
     Z    =        -372395.82                 I    =           52.03244
     XDOT =      -4582.791855                 Wp   =           67.83961
     YDOT =       1185.673602  meter/sec      RA   =           81.87448  deg
     ZDOT =       6028.350515                 TA   =          288.16943
                                              MA   =          288.28082
                                              Ha   =            222.121  n.mi
                                              Hp   =            213.799
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4083509.06                 X    =         1171879.33
     Y    =       21855302.08  feet           Y    =         6675007.73  meter
     Z    =       -1221771.05                 Z    =         -366526.51
     XDOT =     -15035.406350                 XDOT =       -4624.991996
     YDOT =       3890.005256  feet/sec       YDOT =        1134.189726  meter/sec
     ZDOT =      19778.052870                 ZDOT =        6005.986656
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8413300.52                 X    =         2564374.00
     Y    =      -20581689.52  feet           Y    =        -6273298.97  meter
     Z    =       -1196842.01                 Z    =         -364797.44
     XDOT =      13351.043932                 XDOT =        4069.398191
     YDOT =       4339.691689  feet/sec       YDOT =        1322.738027  meter/sec
     ZDOT =      19678.778071                 ZDOT =        5998.091556
  
  
    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   17231.50070569  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6402  82.7028 0004861 158.1485 201.9876 15.54160898 31596
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17231.50070569   =   yrday.fracday
    Element set:     903
    Inclination:       51.6402  deg
    RA of node:        82.7028  deg
    Eccentricity:     .0004861     
    Arg of perigee:   158.1485  deg
    Mean anomaly:     201.9876  deg
    Mean motion:   15.54160898  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3159
    Checksum:              316
 
 
    Coasting Arc #5 (Orbit 3174)
    ---------------------------------------
 
    Vector Time (GMT): 2017/232/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -435986.61                 A    =         6788460.07  meter
     Y    =       -6626765.14  meter          E    =           .0013390
     Z    =       -1375517.60                 I    =           52.02340
     XDOT =       4888.383310                 Wp   =          149.73608
     YDOT =        883.948622  meter/sec      RA   =           76.93110  deg
     ZDOT =      -5843.867925                 TA   =           45.17365
                                              MA   =           45.06490
                                              Ha   =            222.086  n.mi
                                              Hp   =            213.918
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1430402.25                 X    =         -355170.51
     Y    =      -21741355.45  feet           Y    =        -6631188.79  meter
     Z    =       -4512853.01                 Z    =        -1377439.04
     XDOT =      16038.002987                 XDOT =        4906.521510
     YDOT =       2900.093903  feet/sec       YDOT =         938.715164  meter/sec
     ZDOT =     -19172.795029                 ZDOT =       -5820.078126
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10283620.44                 X    =        -3134447.51
     Y    =       19207096.52  feet           Y    =         5854323.02  meter
     Z    =       -4520290.22                 Z    =        -1377784.46
     XDOT =     -10799.247218                 XDOT =       -3291.610552
     YDOT =     -10241.782698  feet/sec       YDOT =       -3121.695366  meter/sec
     ZDOT =     -19067.533910                 ZDOT =       -5811.784336
  
  
    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   17232.52951416  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6393  77.5743 0004939 163.1291 197.0027 15.54150129 31755
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17232.52951416   =   yrday.fracday
    Element set:     904
    Inclination:       51.6393  deg
    RA of node:        77.5743  deg
    Eccentricity:     .0004939     
    Arg of perigee:   163.1291  deg
    Mean anomaly:     197.0027  deg
    Mean motion:   15.54150129  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3175
    Checksum:              308
 
 
    Coasting Arc #6 (Orbit 3190)
    ---------------------------------------
 
    Vector Time (GMT): 2017/233/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -428698.61                 A    =         6785495.81  meter
     Y    =        6097990.51  meter          E    =           .0014411
     Z    =        2936826.04                 I    =           52.00528
     XDOT =      -5053.468739                 Wp   =          101.85718
     YDOT =      -2796.241857  meter/sec      RA   =           71.98013  deg
     ZDOT =       5044.675520                 TA   =          291.47514
                                              MA   =          291.62876
                                              Ha   =            221.900  n.mi
                                              Hp   =            214.016
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1406491.49                 X    =         -511121.46
     Y    =       20006530.54  feet           Y    =         6092735.78  meter
     Z    =        9635256.04                 Z    =         2934543.16
     XDOT =     -16579.621846                 XDOT =       -5046.328898
     YDOT =      -9174.021841  feet/sec       YDOT =       -2852.713054  meter/sec
     ZDOT =      16550.772702                 ZDOT =        5020.145296
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11525789.76                 X    =         3513060.72
     Y    =      -16419793.87  feet           Y    =        -5004753.17  meter
     Z    =        9624145.72                 Z    =         2933439.62
     XDOT =       8421.105860                 XDOT =        2566.753066
     YDOT =      15594.327530  feet/sec       YDOT =        4753.151031  meter/sec
     ZDOT =      16442.542964                 ZDOT =        5011.687095
  
  
    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   17233.55831929  .00016717  00000-0  10270-3 0  9050
    2 25544  51.6390  72.4442 0004937 168.7220 191.4044 15.54193401 31918
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17233.55831929   =   yrday.fracday
    Element set:     905
    Inclination:       51.6390  deg
    RA of node:        72.4442  deg
    Eccentricity:     .0004937     
    Arg of perigee:   168.7220  deg
    Mean anomaly:     191.4044  deg
    Mean motion:   15.54193401  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3191
    Checksum:              302
 
 
    Coasting Arc #7 (Orbit 3205)
    ---------------------------------------
 
    Vector Time (GMT): 2017/234/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1421124.47                 A    =         6781651.09  meter
     Y    =       -5113945.19  meter          E    =           .0008704
     Z    =       -4227150.62                 I    =           51.98016
     XDOT =       5026.334706                 Wp   =          103.54548
     YDOT =       4446.658229  meter/sec      RA   =           67.01877  deg
     ZDOT =      -3698.057737                 TA   =          128.71397
                                              MA   =          128.63612
                                              Ha   =            221.921  n.mi
                                              Hp   =            214.086
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4662481.86                 X    =         1498737.39
     Y    =      -16778035.39  feet           Y    =        -5097619.51  meter
     Z    =      -13868604.41                 Z    =        -4220058.54
     XDOT =      16490.599430                 XDOT =        4994.200453
     YDOT =      14588.773717  feet/sec       YDOT =        4502.686218  meter/sec
     ZDOT =     -12132.735358                 ZDOT =       -3673.720140
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12480588.79                 X    =        -3804083.46
     Y    =       12180719.61  feet           Y    =         3712683.34  meter
     Z    =      -13836342.37                 Z    =        -4217317.15
     XDOT =      -6211.467338                 XDOT =       -1893.255244
     YDOT =     -19993.342133  feet/sec       YDOT =       -6093.970682  meter/sec
     ZDOT =     -12025.634122                 ZDOT =       -3665.413280
  
  
    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   17234.52282373  .00016717  00000-0  10270-3 0  9062
    2 25544  51.6379  67.6345 0004882 169.0676 191.0584 15.54177169 32066
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17234.52282373   =   yrday.fracday
    Element set:     906
    Inclination:       51.6379  deg
    RA of node:        67.6345  deg
    Eccentricity:     .0004882     
    Arg of perigee:   169.0676  deg
    Mean anomaly:     191.0584  deg
    Mean motion:   15.54177169  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3206
    Checksum:              332
 
 
    Coasting Arc #8 (Orbit 3221)
    ---------------------------------------
 
    Vector Time (GMT): 2017/235/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2437068.92                 A    =         6778597.46  meter
     Y    =        3820101.05  meter          E    =           .0009739
     Z    =        5039214.47                 I    =           51.95541
     XDOT =      -4767.410083                 Wp   =          145.78216
     YDOT =      -5671.624459  meter/sec      RA   =           62.04748  deg
     ZDOT =       1984.194549                 TA   =          284.98748
                                              MA   =          285.09526
                                              Ha   =            221.946  n.mi
                                              Hp   =            214.227
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7995632.93                 X    =        -2504082.85
     Y    =       12533139.93  feet           Y    =         3792473.79  meter
     Z    =       16532855.88                 Z    =         5027213.06
     XDOT =     -15641.109197                 XDOT =       -4713.272256
     YDOT =     -18607.691795  feet/sec       YDOT =       -5724.634025  meter/sec
     ZDOT =       6509.824636                 ZDOT =        1961.168234
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13151630.98                 X    =         4008617.12
     Y    =       -7058363.79  feet           Y    =        -2151389.28  meter
     Z    =       16479052.43                 Z    =         5022815.18
     XDOT =       4225.365945                 XDOT =        1287.891540
     YDOT =      22909.944598  feet/sec       YDOT =        6982.951114  meter/sec
     ZDOT =       6408.743791                 ZDOT =        1953.385108
  
  
    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   17235.55162709  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6375  62.5051 0004883 172.7385 187.3840 15.54135756 32226
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17235.55162709   =   yrday.fracday
    Element set:     907
    Inclination:       51.6375  deg
    RA of node:        62.5051  deg
    Eccentricity:     .0004883     
    Arg of perigee:   172.7385  deg
    Mean anomaly:     187.3840  deg
    Mean motion:   15.54135756  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3222
    Checksum:              317
 
 
    Coasting Arc #9 (Orbit 3236)
    ---------------------------------------
 
    Vector Time (GMT): 2017/236/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925218.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3488755.29                 A    =         6777207.12  meter
     Y    =       -2311508.65  meter          E    =           .0016018
     Z    =       -5343765.78                 I    =           51.93482
     XDOT =       4190.190115                 Wp   =          107.93885
     YDOT =       6409.124073  meter/sec      RA   =           57.06779  deg
     ZDOT =        -41.616075                 TA   =          161.69451
                                              MA   =          161.63679
                                              Ha   =            221.796  n.mi
                                              Hp   =            214.345
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11446047.53                 X    =         3540301.02
     Y    =       -7583689.79  feet           Y    =        -2272207.26  meter
     Z    =      -17532039.98                 Z    =        -5326693.28
     XDOT =      13747.342896                 XDOT =        4118.412316
     YDOT =      21027.309951  feet/sec       YDOT =        6455.580295  meter/sec
     ZDOT =       -136.535679                 ZDOT =         -21.436543
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13766463.90                 X    =        -4196018.20
     Y    =        1291765.36  feet           Y    =          393730.08  meter
     Z    =      -17456018.86                 Z    =        -5320594.55
     XDOT =      -2212.576455                 XDOT =        -674.393303
     YDOT =     -24012.774367  feet/sec       YDOT =       -7319.093627  meter/sec
     ZDOT =        -48.201702                 ZDOT =         -14.691879
  
  
    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   17236.51612648  .00016717  00000-0  10270-3 0  9087
    2 25544  51.6374  57.6957 0005039 176.1579 183.9613 15.54180629 32377
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17236.51612648   =   yrday.fracday
    Element set:     908
    Inclination:       51.6374  deg
    RA of node:        57.6957  deg
    Eccentricity:     .0005039     
    Arg of perigee:   176.1579  deg
    Mean anomaly:     183.9613  deg
    Mean motion:   15.54180629  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3237
    Checksum:              338
 
 
    Coasting Arc #10 (Orbit 3248)
    ---------------------------------------
 
    Vector Time (GMT): 2017/237/06:37:41.861
    Vector Time (MET): N/A
    Weight (LBS)     : 925107.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4764109.73                 A    =         6779967.36  meter
     Y    =          45871.53  meter          E    =           .0012858
     Z    =       -4835731.00                 I    =           51.93286
     XDOT =       2542.402033                 Wp   =          128.33506
     YDOT =       6752.591799  meter/sec      RA   =           53.19854  deg
     ZDOT =       2565.657174                 TA   =          166.86734
                                              MA   =          166.83383
                                              Ha   =            221.617  n.mi
                                              Hp   =            215.144
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15630281.26                 X    =         4786732.13
     Y    =         150497.14  feet           Y    =           99273.12  meter
     Z    =      -15865259.18                 Z    =        -4812533.67
     XDOT =       8341.214020                 XDOT =        2454.241198
     YDOT =      22154.172570  feet/sec       YDOT =        6780.529954  meter/sec
     ZDOT =       8417.510412                 ZDOT =        2577.792567
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4930822.47                 X    =         1502914.69
     Y    =      -14942067.26  feet           Y    =        -4554342.10  meter
     Z    =      -15762499.99                 Z    =        -4804410.00
     XDOT =      22536.080026                 XDOT =        6868.997192
     YDOT =      -1509.352033  feet/sec       YDOT =        -460.050500  meter/sec
     ZDOT =       8470.139442                 ZDOT =        2581.698502
  
  
    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   17237.28772544  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6423  53.8527 0004520 190.0459 170.0604 15.53991232 32498
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17237.28772544   =   yrday.fracday
    Element set:     909
    Inclination:       51.6423  deg
    RA of node:        53.8527  deg
    Eccentricity:     .0004520     
    Arg of perigee:   190.0459  deg
    Mean anomaly:     170.0604  deg
    Mean motion:   15.53991232  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3249
    Checksum:              307
 
 
    Coasting Arc #11 (Orbit 3264)
    ---------------------------------------
 
    Vector Time (GMT): 2017/238/06:37:41.861
    Vector Time (MET): N/A
    Weight (LBS)     : 925107.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5363995.13                 A    =         6783417.79  meter
     Y    =       -1436684.89  meter          E    =           .0010642
     Z    =        3884903.21                 I    =           51.92392
     XDOT =      -1306.422675                 Wp   =          104.43021
     YDOT =      -6328.293087  meter/sec      RA   =           48.22963  deg
     ZDOT =      -4137.232237                 TA   =           28.83336
                                              MA   =           28.77460
                                              Ha   =            221.675  n.mi
                                              Hp   =            215.063
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17598409.21                 X    =        -5366401.94
     Y    =       -4713533.11  feet           Y    =        -1496681.89  meter
     Z    =       12745745.44                 Z    =         3858840.98
     XDOT =      -4286.163631                 XDOT =       -1215.464378
     YDOT =     -20762.116426  feet/sec       YDOT =       -6342.394142  meter/sec
     ZDOT =     -13573.596577                 ZDOT =       -4143.356981
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9603901.25                 X    =        -2927269.10
     Y    =       15575945.24  feet           Y    =         4747548.11  meter
     Z    =       12630535.95                 Z    =         3849787.36
     XDOT =     -19956.628452                 XDOT =       -6082.780352
     YDOT =      -1258.578464  feet/sec       YDOT =        -383.614716  meter/sec
     ZDOT =     -13599.657398                 ZDOT =       -4145.175575
  
  
    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   17238.31665041  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6421  48.7252 0004415 192.1859 167.9187 15.53997409 32655
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17238.31665041   =   yrday.fracday
    Element set:     910
    Inclination:       51.6421  deg
    RA of node:        48.7252  deg
    Eccentricity:     .0004415     
    Arg of perigee:   192.1859  deg
    Mean anomaly:     167.9187  deg
    Mean motion:   15.53997409  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3265
    Checksum:              324
 
 
    Coasting Arc #12 (Orbit 3279)
    ---------------------------------------
 
    Vector Time (GMT): 2017/239/06:37:41.861
    Vector Time (MET): N/A
    Weight (LBS)     : 925107.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5714142.83                 A    =         6786963.33  meter
     Y    =        2611816.20  meter          E    =           .0002817
     Z    =       -2570773.58                 I    =           51.91358
     XDOT =       -156.711855                 Wp   =          108.37103
     YDOT =       5543.176660  meter/sec      RA   =           43.26827  deg
     ZDOT =       5287.223300                 TA   =          222.86853
                                              MA   =          222.89049
                                              Ha   =            221.385  n.mi
                                              Hp   =            215.287
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18747187.77                 X    =         5696999.65
     Y    =        8568950.78  feet           Y    =         2675619.61  meter
     Z    =       -8434296.51                 Z    =        -2543057.94
     XDOT =       -514.146507                 XDOT =        -244.368141
     YDOT =      18186.275131  feet/sec       YDOT =        5540.934442  meter/sec
     ZDOT =      17346.533136                 ZDOT =        5286.248768
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13349715.67                 X    =         4068993.34
     Y    =      -15770781.12  feet           Y    =        -4806934.09  meter
     Z    =       -8311972.02                 Z    =        -2533489.07
     XDOT =      16184.604954                 XDOT =        4933.067590
     YDOT =       4567.119349  feet/sec       YDOT =        1392.057977  meter/sec
     ZDOT =      17341.269084                 ZDOT =        5285.618817
  
  
    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   17239.28126549  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6423  43.9176 0004466 197.7916 162.3081 15.54005582 32802
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17239.28126549   =   yrday.fracday
    Element set:     911
    Inclination:       51.6423  deg
    RA of node:        43.9176  deg
    Eccentricity:     .0004466     
    Arg of perigee:   197.7916  deg
    Mean anomaly:     162.3081  deg
    Mean motion:   15.54005582  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3280
    Checksum:              314
 
 
    Coasting Arc #13 (Orbit 3295)
    ---------------------------------------
 
    Vector Time (GMT): 2017/240/06:37:41.861
    Vector Time (MET): N/A
    Weight (LBS)     : 925107.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5705807.40                 A    =         6789436.16  meter
     Y    =       -3529318.60  meter          E    =           .0015279
     Z    =         979755.31                 I    =           51.89750
     XDOT =       1775.250106                 Wp   =          141.29241
     YDOT =      -4527.961314  meter/sec      RA   =           38.31445  deg
     ZDOT =      -5934.096046                 TA   =           28.12626
                                              MA   =           28.04381
                                              Ha   =            221.430  n.mi
                                              Hp   =            215.383
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18719840.54                 X    =        -5670676.71
     Y    =      -11579129.28  feet           Y    =        -3592928.34  meter
     Z    =        3214420.30                 Z    =          952123.85
     XDOT =       5824.311372                 XDOT =        1854.575892
     YDOT =     -14855.516123  feet/sec       YDOT =       -4507.666053  meter/sec
     ZDOT =     -19468.819050                 ZDOT =       -5925.279530
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15972011.21                 X    =        -4868269.02
     Y    =       15171407.92  feet           Y    =         4624245.13  meter
     Z    =        3092636.73                 Z    =          942635.67
     XDOT =     -11743.787391                 XDOT =       -3579.506397
     YDOT =      -8376.435099  feet/sec       YDOT =       -2553.137418  meter/sec
     ZDOT =     -19428.985981                 ZDOT =       -5921.954927
  
  
    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   17240.31018785  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6428  38.7902 0004569 200.6274 159.4695 15.53963723 32965
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17240.31018785   =   yrday.fracday
    Element set:     912
    Inclination:       51.6428  deg
    RA of node:        38.7902  deg
    Eccentricity:     .0004569     
    Arg of perigee:   200.6274  deg
    Mean anomaly:     159.4695  deg
    Mean motion:   15.53963723  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3296
    Checksum:              326
 
 
    Coasting Arc #14 (Orbit 3311)
    ---------------------------------------
 
    Vector Time (GMT): 2017/241/06:37:41.861
    Vector Time (MET): N/A
    Weight (LBS)     : 925107.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5326594.44                 A    =         6789431.44  meter
     Y    =        4148467.03  meter          E    =           .0009472
     Z    =         682580.19                 I    =           51.87175
     XDOT =      -3405.026921                 Wp   =           63.97569
     YDOT =       3378.118613  meter/sec      RA   =           33.36081  deg
     ZDOT =       5980.332094                 TA   =          303.37096
                                              MA   =          303.46156
                                              Ha   =            221.112  n.mi
                                              Hp   =            215.433
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17475703.53                 X    =         5276493.66
     Y    =       13610456.13  feet           Y    =         4207752.54  meter
     Z    =        2239436.31                 Z    =          708333.18
     XDOT =     -11171.348165                 XDOT =       -3471.598312
     YDOT =      11083.066317  feet/sec       YDOT =        3339.669335  meter/sec
     ZDOT =      19620.512121                 ZDOT =        5963.629729
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17377218.93                 X    =         5296576.33
     Y    =      -13717014.41  feet           Y    =        -4180945.99  meter
     Z    =        2352781.93                 Z    =          717127.93
     XDOT =       7074.582856                 XDOT =        2156.332855
     YDOT =      12347.192452  feet/sec       YDOT =        3763.424259  meter/sec
     ZDOT =      19545.945909                 ZDOT =        5957.604313
  
  
    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   17241.33910382  .00016717  00000-0  10270-3 0  9135
    2 25544  51.6426  33.6613 0004408 207.1231 152.9692 15.54018278 33124
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17241.33910382   =   yrday.fracday
    Element set:     913
    Inclination:       51.6426  deg
    RA of node:        33.6613  deg
    Eccentricity:     .0004408     
    Arg of perigee:   207.1231  deg
    Mean anomaly:     152.9692  deg
    Mean motion:   15.54018278  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3312
    Checksum:              283
 
 
    Coasting Arc #15 (Orbit 3325)
    ---------------------------------------
 
    Vector Time (GMT): 2017/242/05:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925107.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4885666.25                 A    =         6781208.98  meter
     Y    =       -1373807.07  meter          E    =           .0009684
     Z    =       -4507118.18                 I    =           51.81709
     XDOT =       4469.972192                 Wp   =          136.48671
     YDOT =       5321.315594  meter/sec      RA   =           28.59476  deg
     ZDOT =       3220.688950                 TA   =          165.86592
                                              MA   =          165.83880
                                              Ha   =            221.032  n.mi
                                              Hp   =            215.688
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16029088.73                 X    =         4922558.69
     Y    =       -4507241.04  feet           Y    =        -1318966.12  meter
     Z    =      -14787133.14                 Z    =        -4483295.56
     XDOT =      14665.263097                 XDOT =        4394.491146
     YDOT =      17458.384496  feet/sec       YDOT =        5370.879952  meter/sec
     ZDOT =      10566.564797                 ZDOT =        3242.219066
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4091014.17                 X    =         1246941.12
     Y    =      -16236590.81  feet           Y    =        -4948912.88  meter
     Z    =      -14681380.59                 Z    =        -4474884.80
     XDOT =      21217.607330                 XDOT =        6467.126714
     YDOT =      -4301.950999  feet/sec       YDOT =       -1311.234665  meter/sec
     ZDOT =      10660.992914                 ZDOT =        3249.470640
  
  
    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   17242.23940701  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6422  29.1747 0004370 210.2574 149.8327 15.54007055 33267
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17242.23940701   =   yrday.fracday
    Element set:     914
    Inclination:       51.6422  deg
    RA of node:        29.1747  deg
    Eccentricity:     .0004370     
    Arg of perigee:   210.2574  deg
    Mean anomaly:     149.8327  deg
    Mean motion:   15.54007055  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3326
    Checksum:              285
 
 
    Coasting Arc #16 (Orbit 3341)
    ---------------------------------------
 
    Vector Time (GMT): 2017/243/05:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925107.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5860354.29                 A    =         6784872.06  meter
     Y    =         347622.92  meter          E    =           .0010824
     Z    =        3388807.02                 I    =           51.80061
     XDOT =      -3008.523576                 Wp   =          110.02574
     YDOT =      -5309.175900  meter/sec      RA   =           23.62118  deg
     ZDOT =      -4649.691417                 TA   =           30.46849
                                              MA   =           30.40564
                                              Ha   =            221.014  n.mi
                                              Hp   =            215.642
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19226884.15                 X    =        -5880267.02
     Y    =        1140495.14  feet           Y    =          281977.23  meter
     Z    =       11118133.27                 Z    =         3360291.02
     XDOT =      -9870.484174                 XDOT =       -2926.345573
     YDOT =     -17418.556102  feet/sec       YDOT =       -5342.359934  meter/sec
     ZDOT =     -15254.893102                 ZDOT =       -4664.106028
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8290149.45                 X    =        -2526837.55
     Y    =       17465421.30  feet           Y    =         5323460.41  meter
     Z    =       10991777.45                 Z    =         3350293.77
     XDOT =     -18698.322728                 XDOT =       -5699.248768
     YDOT =        782.398292  feet/sec       YDOT =         238.474999  meter/sec
     ZDOT =     -15317.801315                 ZDOT =       -4668.865841
  
  
    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   17243.26832188  .00016717  00000-0  10270-3 0  9158
    2 25544  51.6425  24.0471 0004288 214.0883 145.9995 15.54023397 33424
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17243.26832188   =   yrday.fracday
    Element set:     915
    Inclination:       51.6425  deg
    RA of node:        24.0471  deg
    Eccentricity:     .0004288     
    Arg of perigee:   214.0883  deg
    Mean anomaly:     145.9995  deg
    Mean motion:   15.54023397  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3342
    Checksum:              316
 
             

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