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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14929.5432
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   90.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.169
   ET - UTC  (sec) :   68.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   284/02:47:17.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.3  
   000/00:00:00.000           0.0               0.0              212.5  
   
   286/10:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.3  
   000/00:00:00.000           0.0               0.0              212.2  
   
   287/18:48:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.3  
   000/00:00:00.000           0.0               0.0              212.2  
   
 
 
    Coasting Arc #1 (Orbit 2135)
    ---------------------------------------
 
    Vector Time (GMT): 2016/274/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2241736.96                 A    =         6789635.45  meter
     Y    =       -6396577.11  meter          E    =           .0018157
     Z    =        -159612.94                 I    =           51.30433
     XDOT =       4484.565124                 Wp   =           36.18598
     YDOT =      -1711.965351  meter/sec      RA   =          251.76738  deg
     ZDOT =       5986.121585                 TA   =          322.08550
                                              MA   =          322.21322
                                              Ha   =            222.892  n.mi
                                              Hp   =            213.574
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7354780.06                 X    =        -2169266.86
     Y    =      -20986145.38  feet           Y    =        -6421240.54  meter
     Z    =        -523664.51                 Z    =         -170325.85
     XDOT =      14713.140171                 XDOT =        4474.297222
     YDOT =      -5616.684221  feet/sec       YDOT =       -1661.872458  meter/sec
     ZDOT =      19639.506512                 ZDOT =        6007.881960
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10478809.98                 X    =         3193941.28
     Y    =       19612639.40  feet           Y    =         5977932.49  meter
     Z    =        -569411.44                 Z    =         -173556.61
     XDOT =     -12123.442635                 XDOT =       -3695.225315
     YDOT =       7018.566345  feet/sec       YDOT =        2139.259022  meter/sec
     ZDOT =      19734.815747                 ZDOT =        6015.171840
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16274.50033672  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6383 252.7108 0006713  21.8902 338.2536 15.54019889 21364
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16274.50033672   =   yrday.fracday
    Element set:     900
    Inclination:       51.6383  deg
    RA of node:       252.7108  deg
    Eccentricity:     .0006713     
    Arg of perigee:    21.8902  deg
    Mean anomaly:     338.2536  deg
    Mean motion:   15.54019889  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2136
    Checksum:              301
 
 
    Coasting Arc #2 (Orbit 2151)
    ---------------------------------------
 
    Vector Time (GMT): 2016/275/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1448911.89                 A    =         6788713.03  meter
     Y    =        6457766.44  meter          E    =           .0007901
     Z    =       -1517567.86                 I    =           51.31346
     XDOT =      -5080.079430                 Wp   =           91.89621
     YDOT =       -200.813319  meter/sec      RA   =          246.77378  deg
     ZDOT =      -5730.979747                 TA   =          104.74180
                                              MA   =          104.65422
                                              Ha   =            223.078  n.mi
                                              Hp   =            213.459
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4753647.95                 X    =         1383963.60
     Y    =       21186897.78  feet           Y    =         6473605.78  meter
     Z    =       -4978897.17                 Z    =        -1510688.02
     XDOT =     -16666.927263                 XDOT =       -5049.617367
     YDOT =       -658.836348  feet/sec       YDOT =        -257.452685  meter/sec
     ZDOT =     -18802.426993                 ZDOT =       -5755.583761
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8320636.88                 X    =        -2536130.12
     Y    =      -20063320.44  feet           Y    =        -6115300.07  meter
     Z    =       -4949888.69                 Z    =        -1508726.07
     XDOT =      14952.997403                 XDOT =        4557.673609
     YDOT =      -1557.307904  feet/sec       YDOT =        -474.667449  meter/sec
     ZDOT =     -18909.847805                 ZDOT =       -5763.721611
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16275.52925800  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6397 247.5816 0006920  24.4526 335.6954 15.54006206 21520
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16275.52925800   =   yrday.fracday
    Element set:     901
    Inclination:       51.6397  deg
    RA of node:       247.5816  deg
    Eccentricity:     .0006920     
    Arg of perigee:    24.4526  deg
    Mean anomaly:     335.6954  deg
    Mean motion:   15.54006206  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2152
    Checksum:              304
 
 
    Coasting Arc #3 (Orbit 2167)
    ---------------------------------------
 
    Vector Time (GMT): 2016/276/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -515307.35                 A    =         6785736.61  meter
     Y    =       -6049892.43  meter          E    =           .0017845
     Z    =        3006313.53                 I    =           51.31798
     XDOT =       5541.754545                 Wp   =           65.14476
     YDOT =       1984.034186  meter/sec      RA   =          241.77715  deg
     ZDOT =       4926.918293                 TA   =          329.49475
                                              MA   =          329.59843
                                              Ha   =            222.991  n.mi
                                              Hp   =            213.340
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1690640.91                 X    =         -462221.20
     Y    =      -19848728.43  feet           Y    =        -6055357.70  meter
     Z    =        9863233.35                 Z    =         3003940.03
     XDOT =      18181.609399                 XDOT =        5495.223492
     YDOT =       6509.298512  feet/sec       YDOT =        2045.746309  meter/sec
     ZDOT =      16164.430096                 ZDOT =        4953.725847
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5436297.28                 X    =         1656983.41
     Y    =       19169307.19  feet           Y    =         5842804.83  meter
     Z    =        9853831.39                 Z    =         3003447.81
     XDOT =     -17577.590694                 XDOT =       -5357.649643
     YDOT =      -3410.737148  feet/sec       YDOT =       -1039.592683  meter/sec
     ZDOT =      16281.195118                 ZDOT =        4962.508272
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16276.55816902  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6402 242.4542 0006765  27.7073 332.4439 15.54047924 21689
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16276.55816902   =   yrday.fracday
    Element set:     902
    Inclination:       51.6402  deg
    RA of node:       242.4542  deg
    Eccentricity:     .0006765     
    Arg of perigee:    27.7073  deg
    Mean anomaly:     332.4439  deg
    Mean motion:   15.54047924  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2168
    Checksum:              310
 
 
    Coasting Arc #4 (Orbit 2182)
    ---------------------------------------
 
    Vector Time (GMT): 2016/277/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -592418.05                 A    =         6782036.49  meter
     Y    =        5278565.43  meter          E    =           .0014196
     Z    =       -4232313.55                 I    =           51.32132
     XDOT =      -5759.251122                 Wp   =           52.25488
     YDOT =      -3532.703826  meter/sec      RA   =          236.77094  deg
     ZDOT =      -3599.641208                 TA   =          180.70829
                                              MA   =          180.71030
                                              Ha   =            223.187  n.mi
                                              Hp   =            213.162
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1943628.78                 X    =         -630841.18
     Y    =       17318128.05  feet           Y    =         5271725.25  meter
     Z    =      -13885543.15                 Z    =        -4235285.41
     XDOT =     -18895.180846                 XDOT =       -5701.833681
     YDOT =     -11590.235649  feet/sec       YDOT =       -3596.787047  meter/sec
     ZDOT =     -11809.846483                 ZDOT =       -3627.478772
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1716749.43                 X    =         -523265.23
     Y    =      -17331017.22  feet           Y    =        -5282494.05  meter
     Z    =      -13899358.77                 Z    =        -4236524.55
     XDOT =      19522.934618                 XDOT =        5950.590472
     YDOT =       7635.174536  feet/sec       YDOT =        2327.201199  meter/sec
     ZDOT =     -11930.873653                 ZDOT =       -3636.530290
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16277.52276915  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6400 237.6461 0006973  31.1371 329.0193 15.54027554 21837
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16277.52276915   =   yrday.fracday
    Element set:     903
    Inclination:       51.6400  deg
    RA of node:       237.6461  deg
    Eccentricity:     .0006973     
    Arg of perigee:    31.1371  deg
    Mean anomaly:     329.0193  deg
    Mean motion:   15.54027554  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2183
    Checksum:              301
 
 
    Coasting Arc #5 (Orbit 2198)
    ---------------------------------------
 
    Vector Time (GMT): 2016/278/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1796452.45                 A    =         6778783.24  meter
     Y    =       -4193009.06  meter          E    =           .0008895
     Z    =        5006171.46                 I    =           51.33031
     XDOT =       5710.520034                 Wp   =           74.47389
     YDOT =       4751.041007  meter/sec      RA   =          231.75780  deg
     ZDOT =       1929.588749                 TA   =          356.73876
                                              MA   =          356.74455
                                              Ha   =            223.012  n.mi
                                              Hp   =            213.118
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5893872.88                 X    =         1818887.96
     Y    =      -13756591.41  feet           Y    =        -4172793.92  meter
     Z    =       16424447.06                 Z    =         5014953.30
     XDOT =      18735.301950                 XDOT =        5647.594980
     YDOT =      15587.404878  feet/sec       YDOT =        4814.548254  meter/sec
     ZDOT =       6330.671750                 ZDOT =        1957.176154
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2608314.67                 X    =         -795014.31
     Y    =       14693365.68  feet           Y    =         4478537.86  meter
     Z    =       16463465.78                 Z    =         5018064.37
     XDOT =     -20602.281576                 XDOT =       -6279.575424
     YDOT =     -10886.674850  feet/sec       YDOT =       -3318.258494  meter/sec
     ZDOT =       6450.426283                 ZDOT =        1966.089931
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16278.55166525  .00016717  00000-0  10270-3 0  9040
    2 25544  51.6409 232.5188 0006787  33.5816 326.5765 15.54072319 21992
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16278.55166525   =   yrday.fracday
    Element set:     904
    Inclination:       51.6409  deg
    RA of node:       232.5188  deg
    Eccentricity:     .0006787     
    Arg of perigee:    33.5816  deg
    Mean anomaly:     326.5765  deg
    Mean motion:   15.54072319  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2199
    Checksum:              336
 
 
    Coasting Arc #6 (Orbit 2213)
    ---------------------------------------
 
    Vector Time (GMT): 2016/279/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3044812.95                 A    =         6777601.57  meter
     Y    =        2953142.60  meter          E    =           .0019905
     Z    =       -5302838.87                 I    =           51.34718
     XDOT =      -5276.321729                 Wp   =           73.71664
     YDOT =      -5544.745281  meter/sec      RA   =          226.73810  deg
     ZDOT =        -52.968381                 TA   =          195.74463
                                              MA   =          195.80661
                                              Ha   =            223.239  n.mi
                                              Hp   =            212.867
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9989543.79                 X    =        -3051850.06
     Y    =        9688788.04  feet           Y    =         2919053.58  meter
     Z    =      -17397765.33                 Z    =        -5317647.47
     XDOT =     -17310.766829                 XDOT =       -5213.669523
     YDOT =     -18191.421527  feet/sec       YDOT =       -5603.398346  meter/sec
     ZDOT =       -173.780776                 ZDOT =         -78.447175
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7293549.97                 X    =         2223074.03
     Y    =      -11755700.92  feet           Y    =        -3583137.64  meter
     Z    =      -17462916.77                 Z    =        -5322697.03
     XDOT =      20277.083101                 XDOT =        6180.454929
     YDOT =      13028.393220  feet/sec       YDOT =        3971.054253  meter/sec
     ZDOT =       -284.214170                 ZDOT =         -86.628479
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16279.51624793  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6412 227.7105 0006930  37.4285 322.7349 15.54046756 22144
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16279.51624793   =   yrday.fracday
    Element set:     905
    Inclination:       51.6412  deg
    RA of node:       227.7105  deg
    Eccentricity:     .0006930     
    Arg of perigee:    37.4285  deg
    Mean anomaly:     322.7349  deg
    Mean motion:   15.54046756  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2214
    Checksum:              312
 
 
    Coasting Arc #7 (Orbit 2229)
    ---------------------------------------
 
    Vector Time (GMT): 2016/280/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4239031.61                 A    =         6778635.64  meter
     Y    =       -1608888.92  meter          E    =           .0012376
     Z    =        5033421.62                 I    =           51.37338
     XDOT =       4467.014281                 Wp   =           47.82402
     YDOT =       5959.254196  meter/sec      RA   =          221.72101  deg
     ZDOT =      -1846.112213                 TA   =           60.17460
                                              MA   =           60.05162
                                              Ha   =            223.183  n.mi
                                              Hp   =            212.839
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13907584.02                 X    =         4232256.94
     Y    =       -5278506.95  feet           Y    =        -1561522.67  meter
     Z    =       16513850.45                 Z    =         5053997.81
     XDOT =      14655.558665                 XDOT =        4409.012158
     YDOT =      19551.358910  feet/sec       YDOT =        6008.882878  meter/sec
     ZDOT =      -6056.798599                 ZDOT =       -1824.553592
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12005993.99                 X    =        -3659426.97
     Y    =        8611287.63  feet           Y    =         2624720.47  meter
     Z    =       16603994.07                 Z    =         5060897.39
     XDOT =     -18553.052580                 XDOT =       -5654.970426
     YDOT =     -14298.544794  feet/sec       YDOT =       -4358.196453  meter/sec
     ZDOT =      -5963.540584                 ZDOT =       -1817.687170
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16280.54512568  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6409 222.5831 0007008  41.4121 318.7561 15.54063132 22306
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16280.54512568   =   yrday.fracday
    Element set:     906
    Inclination:       51.6409  deg
    RA of node:       222.5831  deg
    Eccentricity:     .0007008     
    Arg of perigee:    41.4121  deg
    Mean anomaly:     318.7561  deg
    Mean motion:   15.54063132  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2230
    Checksum:              276
 
 
    Coasting Arc #8 (Orbit 2244)
    ---------------------------------------
 
    Vector Time (GMT): 2016/281/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5255036.96                 A    =         6781601.14  meter
     Y    =         344839.21  meter          E    =           .0012974
     Z    =       -4282629.06                 I    =           51.40800
     XDOT =      -3265.333728                 Wp   =           81.70503
     YDOT =      -5957.127195  meter/sec      RA   =          216.71105  deg
     ZDOT =       3538.129986                 TA   =          224.47050
                                              MA   =          224.57473
                                              Ha   =            223.251  n.mi
                                              Hp   =            212.658
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17240934.90                 X    =        -5237698.97
     Y    =        1131362.24  feet           Y    =          286170.48  meter
     Z    =      -14050620.28                 Z    =        -4308115.03
     XDOT =     -10713.037165                 XDOT =       -3215.663908
     YDOT =     -19544.380560  feet/sec       YDOT =       -5993.364357  meter/sec
     ZDOT =      11608.038012                 ZDOT =        3522.388661
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16203036.08                 X    =         4938685.40
     Y    =       -5731344.11  feet           Y    =        -1746913.69  meter
     Z    =      -14162028.92                 Z    =        -4316586.42
     XDOT =      15258.631388                 XDOT =        4650.830847
     YDOT =      14710.842877  feet/sec       YDOT =        4483.864909  meter/sec
     ZDOT =      11540.181514                 ZDOT =        3517.447325
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16281.50968947  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6407 217.7757 0006905  44.5150 315.6556 15.54073099 22457
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16281.50968947   =   yrday.fracday
    Element set:     907
    Inclination:       51.6407  deg
    RA of node:       217.7757  deg
    Eccentricity:     .0006905     
    Arg of perigee:    44.5150  deg
    Mean anomaly:     315.6556  deg
    Mean motion:   15.54073099  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2245
    Checksum:              331
 
 
    Coasting Arc #9 (Orbit 2260)
    ---------------------------------------
 
    Vector Time (GMT): 2016/282/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5997348.51                 A    =         6785352.89  meter
     Y    =         852961.30  meter          E    =           .0018417
     Z    =        3045331.26                 I    =           51.44809
     XDOT =       1702.007338                 Wp   =           79.70105
     YDOT =       5646.358557  meter/sec      RA   =          211.71183  deg
     ZDOT =      -4904.801960                 TA   =           65.24570
                                              MA   =           65.05416
                                              Ha   =            223.240  n.mi
                                              Hp   =            212.589
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19676340.24                 X    =         5972571.63
     Y    =        2798429.45  feet           Y    =          919889.35  meter
     Z    =        9991244.31                 Z    =         3074405.02
     XDOT =       5584.013575                 XDOT =        1662.567553
     YDOT =      18524.798414  feet/sec       YDOT =        5665.170674  meter/sec
     ZDOT =     -16091.869947                 ZDOT =       -4896.630123
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19588761.77                 X    =        -5970654.59
     Y    =        2952591.47  feet           Y    =          899949.88  meter
     Z    =       10118159.49                 Z    =         3084015.01
     XDOT =     -10554.381222                 XDOT =       -3216.975397
     YDOT =     -14680.049975  feet/sec       YDOT =       -4474.479232  meter/sec
     ZDOT =     -16057.029028                 ZDOT =       -4894.182448
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16282.53854548  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6415 212.6470 0006950  47.8428 312.3314 15.54110159 22619
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16282.53854548   =   yrday.fracday
    Element set:     908
    Inclination:       51.6415  deg
    RA of node:       212.6470  deg
    Eccentricity:     .0006950     
    Arg of perigee:    47.8428  deg
    Mean anomaly:     312.3314  deg
    Mean motion:   15.54110159  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2261
    Checksum:              299
 
 
    Coasting Arc #10 (Orbit 2275)
    ---------------------------------------
 
    Vector Time (GMT): 2016/283/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6349341.91                 A    =         6788318.70  meter
     Y    =       -1826361.60  meter          E    =           .0014932
     Z    =       -1538012.07                 I    =           51.48522
     XDOT =         79.988428                 Wp   =           44.53816
     YDOT =      -5078.649386  meter/sec      RA   =          206.72451  deg
     ZDOT =       5744.892243                 TA   =          298.61764
                                              MA   =          298.76777
                                              Ha   =            223.301  n.mi
                                              Hp   =            212.514
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20831174.26                 X    =        -6320976.09
     Y    =       -5992000.01  feet           Y    =        -1897205.71  meter
     Z    =       -5045971.37                 Z    =        -1568786.88
     XDOT =        262.429225                 XDOT =         108.866722
     YDOT =     -16662.235520  feet/sec       YDOT =       -5077.593013  meter/sec
     ZDOT =      18848.071664                 ZDOT =        5745.351325
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21635632.50                 X    =         6594540.79
     Y    =        -607261.67  feet           Y    =         -185093.36  meter
     Z    =       -5180188.37                 Z    =        -1578921.42
     XDOT =       4881.982793                 XDOT =        1488.028355
     YDOT =      14338.522575  feet/sec       YDOT =        4370.381681  meter/sec
     ZDOT =      18850.853846                 ZDOT =        5745.740252
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16283.50308634  .00016717  00000-0  10270-3 0  9095
    2 25544  51.6408 207.8395 0006993  51.4632 308.7147 15.54110916 22768
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16283.50308634   =   yrday.fracday
    Element set:     909
    Inclination:       51.6408  deg
    RA of node:       207.8395  deg
    Eccentricity:     .0006993     
    Arg of perigee:    51.4632  deg
    Mean anomaly:     308.7147  deg
    Mean motion:   15.54110916  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2276
    Checksum:              317
 
 
    Coasting Arc #11 (Orbit 2285)
    ---------------------------------------
 
    Vector Time (GMT): 2016/284/02:47:17.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5668325.55                 A    =         6788708.79  meter
     Y    =        3533879.08  meter          E    =           .0011859
     Z    =       -1208192.01                 I    =           51.50490
     XDOT =      -3453.419236                 Wp   =          107.60207
     YDOT =       3559.280205  meter/sec      RA   =          203.67053  deg
     ZDOT =      -5842.229357                 TA   =           85.54275
                                              MA   =           85.40727
                                              Ha   =            223.310  n.mi
                                              Hp   =            212.485
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18596868.61                 X    =         5634256.46
     Y    =       11594091.48  feet           Y    =         3597075.52  meter
     Z    =       -3963884.56                 Z    =        -1180739.48
     XDOT =     -11330.115603                 XDOT =       -3464.584045
     YDOT =      11677.428494  feet/sec       YDOT =        3520.598872  meter/sec
     ZDOT =     -19167.419150                 ZDOT =       -5859.032756
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19331878.53                 X    =         5892356.58
     Y    =      -10367142.33  feet           Y    =        -3159904.98  meter
     Z    =       -3844436.52                 Z    =        -1171784.25
     XDOT =       3782.132035                 XDOT =        1152.793844
     YDOT =      14124.058740  feet/sec       YDOT =        4305.013104  meter/sec
     ZDOT =     -19241.402418                 ZDOT =       -5864.779457
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16284.14610683  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6412 204.6330 0006783  56.1085 304.0712 15.54139426 22863
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16284.14610683   =   yrday.fracday
    Element set:     910
    Inclination:       51.6412  deg
    RA of node:       204.6330  deg
    Eccentricity:     .0006783     
    Arg of perigee:    56.1085  deg
    Mean anomaly:     304.0712  deg
    Mean motion:   15.54139426  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2286
    Checksum:              285
 
 
    Coasting Arc #12 (Orbit 2301)
    ---------------------------------------
 
    Vector Time (GMT): 2016/285/02:47:17.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4766172.35                 A    =         6786101.14  meter
     Y    =       -3938175.77  meter          E    =           .0019984
     Z    =        2772668.99                 I    =           51.52603
     XDOT =       5111.863191                 Wp   =           73.03943
     YDOT =      -2565.252292  meter/sec      RA   =          198.68770  deg
     ZDOT =       5118.823428                 TA   =          318.47208
                                              MA   =          318.62373
                                              Ha   =            223.363  n.mi
                                              Hp   =            212.433
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15637048.38                 X    =        -4735248.97
     Y    =      -12920524.19  feet           Y    =        -3991301.15  meter
     Z    =        9096683.03                 Z    =         2749591.40
     XDOT =      16771.204694                 XDOT =        5115.303327
     YDOT =      -8416.182060  feet/sec       YDOT =       -2508.068305  meter/sec
     ZDOT =      16794.040118                 ZDOT =        5143.664369
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18896890.83                 X    =        -5759772.33
     Y    =        7495274.77  feet           Y    =         2284559.75  meter
     Z    =        8996401.64                 Z    =         2742103.22
     XDOT =       1234.096948                 XDOT =         376.152750
     YDOT =     -17275.721849  feet/sec       YDOT =       -5265.640020  meter/sec
     ZDOT =      16903.011664                 ZDOT =        5152.037955
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16285.17493067  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6412 199.5043 0006767  59.8963 300.2860 15.54142829 23025
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16285.17493067   =   yrday.fracday
    Element set:     911
    Inclination:       51.6412  deg
    RA of node:       199.5043  deg
    Eccentricity:     .0006767     
    Arg of perigee:    59.8963  deg
    Mean anomaly:     300.2860  deg
    Mean motion:   15.54142829  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2302
    Checksum:              317
 
 
    Coasting Arc #13 (Orbit 2316)
    ---------------------------------------
 
    Vector Time (GMT): 2016/286/02:47:17.000
    Vector Time (MET): N/A
    Weight (LBS)     : 893178.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3433086.30                 A    =         6782190.47  meter
     Y    =        4187286.13  meter          E    =           .0014073
     Z    =       -4099051.38                 I    =           51.54509
     XDOT =      -6449.735532                 Wp   =           67.89261
     YDOT =       1551.994586  meter/sec      RA   =          193.69734  deg
     ZDOT =      -3821.823488                 TA   =          162.52889
                                              MA   =          162.48042
                                              Ha   =            223.340  n.mi
                                              Hp   =            212.359
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11263406.49                 X    =         3405919.43
     Y    =       13737815.38  feet           Y    =         4225524.86  meter
     Z    =      -13448331.29                 Z    =        -4082440.61
     XDOT =     -21160.549646                 XDOT =       -6448.046044
     YDOT =       5091.845753  feet/sec       YDOT =        1479.878348  meter/sec
     ZDOT =     -12538.790972                 ZDOT =       -3853.151008
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17452325.29                 X    =         5319468.75
     Y    =       -3597124.86  feet           Y    =        -1096403.66  meter
     Z    =      -13376342.80                 Z    =        -4077109.28
     XDOT =      -5634.036354                 XDOT =       -1717.254281
     YDOT =      19736.429493  feet/sec       YDOT =        6015.663709  meter/sec
     ZDOT =     -12675.977170                 ZDOT =       -3863.637841
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16286.13944078  .00016717  00000-0  10270-3 0  9129
    2 25544  51.6422 194.6959 0006836  63.2945 296.8907 15.54165829 23177
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16286.13944078   =   yrday.fracday
    Element set:     912
    Inclination:       51.6422  deg
    RA of node:       194.6959  deg
    Eccentricity:     .0006836     
    Arg of perigee:    63.2945  deg
    Mean anomaly:     296.8907  deg
    Mean motion:   15.54165829  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2317
    Checksum:              350
 
 
    Coasting Arc #14 (Orbit 2321)
    ---------------------------------------
 
    Vector Time (GMT): 2016/286/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907704.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6016318.46                 A    =         6785438.52  meter
     Y    =        1108817.46  meter          E    =           .0011444
     Z    =       -2938019.64                 I    =           51.56636
     XDOT =      -3312.875194                 Wp   =           64.88819
     YDOT =      -4762.759434  meter/sec      RA   =          191.95953  deg
     ZDOT =       5006.489628                 TA   =          261.56191
                                              MA   =          261.69164
                                              Ha   =            223.289  n.mi
                                              Hp   =            212.207
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19738577.62                 X    =        -6013998.63
     Y    =        3637852.56  feet           Y    =         1041551.59  meter
     Z    =       -9639172.06                 Z    =        -2967240.15
     XDOT =     -10869.013103                 XDOT =       -3283.690167
     YDOT =     -15625.851162  feet/sec       YDOT =       -4799.642475  meter/sec
     ZDOT =      16425.490907                 ZDOT =        4990.467802
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19343829.10                 X    =         5895999.11
     Y    =       -5116579.30  feet           Y    =        -1559533.37  meter
     Z    =       -9767084.92                 Z    =        -2977007.48
     XDOT =      11753.733346                 XDOT =        3582.537924
     YDOT =      13337.822903  feet/sec       YDOT =        4065.368421  meter/sec
     ZDOT =      16356.159355                 ZDOT =        4985.357372
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16286.46094216  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6416 193.0946 0006919  61.9143 298.2709 15.54172795 23228
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16286.46094216   =   yrday.fracday
    Element set:     913
    Inclination:       51.6416  deg
    RA of node:       193.0946  deg
    Eccentricity:     .0006919     
    Arg of perigee:    61.9143  deg
    Mean anomaly:     298.2709  deg
    Mean motion:   15.54172795  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2322
    Checksum:              328
 
 
    Coasting Arc #15 (Orbit 2337)
    ---------------------------------------
 
    Vector Time (GMT): 2016/287/10:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907704.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6647413.42                 A    =         6788373.65  meter
     Y    =        -243472.00  meter          E    =           .0018736
     Z    =        1324698.86                 I    =           51.60857
     XDOT =       1348.810703                 Wp   =          103.01480
     YDOT =       4810.319230  meter/sec      RA   =          186.98123  deg
     ZDOT =      -5819.063091                 TA   =           62.55563
                                              MA   =           62.36521
                                              Ha   =            223.331  n.mi
                                              Hp   =            212.169
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21809099.16                 X    =         6643207.05
     Y    =        -798792.65  feet           Y    =         -169159.51  meter
     Z    =        4346124.87                 Z    =         1356980.50
     XDOT =       4425.231965                 XDOT =        1323.187061
     YDOT =      15781.887238  feet/sec       YDOT =        4825.258523  meter/sec
     ZDOT =     -19091.414342                 ZDOT =       -5812.573687
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21612225.98                 X    =        -6587406.48
     Y    =        2817705.26  feet           Y    =          858836.56  meter
     Z    =        4487304.58                 Z    =         1367730.44
     XDOT =      -5789.125669                 XDOT =       -1764.525504
     YDOT =     -13713.573530  feet/sec       YDOT =       -4179.897212  meter/sec
     ZDOT =     -19063.757741                 ZDOT =       -5810.633359
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16287.48973748  .00016717  00000-0  10270-3 0  9146
    2 25544  51.6423 187.9660 0006892  66.1018 294.0857 15.54185620 23385
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16287.48973748   =   yrday.fracday
    Element set:     914
    Inclination:       51.6423  deg
    RA of node:       187.9660  deg
    Eccentricity:     .0006892     
    Arg of perigee:    66.1018  deg
    Mean anomaly:     294.0857  deg
    Mean motion:   15.54185620  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2338
    Checksum:              345
 
 
    Coasting Arc #16 (Orbit 2342)
    ---------------------------------------
 
    Vector Time (GMT): 2016/287/18:48:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907704.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5981551.04                 A    =         6787041.80  meter
     Y    =        2324330.63  meter          E    =           .0010815
     Z    =       -2214379.67                 I    =           51.61227
     XDOT =      -3572.224976                 Wp   =          102.36155
     YDOT =       4011.631895  meter/sec      RA   =          185.37009  deg
     ZDOT =      -5463.414878                 TA   =          102.23038
                                              MA   =          102.10924
                                              Ha   =            223.312  n.mi
                                              Hp   =            212.175
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19624511.29                 X    =         5965871.86
     Y    =        7625756.67  feet           Y    =         2391132.39  meter
     Z    =       -7265025.17                 Z    =        -2185360.83
     XDOT =     -11719.898216                 XDOT =       -3590.279323
     YDOT =      13161.521966  feet/sec       YDOT =        3971.583215  meter/sec
     ZDOT =     -17924.589495                 ZDOT =       -5480.812442
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4643427.97                 X    =         1415316.84
     Y    =       20579959.69  feet           Y    =         6272771.71  meter
     Z    =       -7138489.68                 Z    =        -2175811.66
     XDOT =     -15894.142832                 XDOT =       -4844.534735
     YDOT =      -2629.090953  feet/sec       YDOT =        -801.346922  meter/sec
     ZDOT =     -18001.255417                 ZDOT =       -5486.782651
  
  
    The mean element set is posted at the UTC for which position is
    just north of the next ascending node relative to the above
    vector time
 
 
    TWO LINE MEAN ELEMENT SET
  
    ISS
    1 25544U 98067A   16287.81123242  .00016717  00000-0  10270-3 0  9150
    2 25544  51.6397 186.3590 0006823  69.8177 290.3709 15.54222955 23434
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16287.81123242   =   yrday.fracday
    Element set:     915
    Inclination:       51.6397  deg
    RA of node:       186.3590  deg
    Eccentricity:     .0006823     
    Arg of perigee:    69.8177  deg
    Mean anomaly:     290.3709  deg
    Mean motion:   15.54222955  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2343
    Checksum:              328
 
 
    Coasting Arc #17 (Orbit 2358)
    ---------------------------------------
 
    Vector Time (GMT): 2016/288/18:48:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 907704.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4919199.66                 A    =         6783501.65  meter
     Y    =       -2911617.00  meter          E    =           .0018394
     Z    =        3635672.33                 I    =           51.63364
     XDOT =       5284.408324                 Wp   =           87.24319
     YDOT =      -3433.277004  meter/sec      RA   =          180.38932  deg
     ZDOT =       4382.204224                 TA   =          315.95117
                                              MA   =          316.09758
                                              Ha   =            223.315  n.mi
                                              Hp   =            212.145
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16139106.48                 X    =        -4903936.43
     Y    =       -9552549.22  feet           Y    =        -2966540.97  meter
     Z    =       11928058.81                 Z    =         3611813.15
     XDOT =      17337.297651                 XDOT =        5301.120131
     YDOT =     -11264.032164  feet/sec       YDOT =       -3374.089177  meter/sec
     ZDOT =      14377.310445                 ZDOT =        4407.916034
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1440335.33                 X    =         -439014.21
     Y    =      -18764732.58  feet           Y    =        -5719490.49  meter
     Z    =       11824161.16                 Z    =         3604004.32
     XDOT =      17733.220517                 XDOT =        5405.085614
     YDOT =       7807.634211  feet/sec       YDOT =        2379.766908  meter/sec
     ZDOT =      14490.252883                 ZDOT =        4416.629079
  
  
    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   16288.84001224  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6406 181.2299 0006652  74.7338 285.4550 15.54236047 23592
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16288.84001224   =   yrday.fracday
    Element set:     916
    Inclination:       51.6406  deg
    RA of node:       181.2299  deg
    Eccentricity:     .0006652     
    Arg of perigee:    74.7338  deg
    Mean anomaly:     285.4550  deg
    Mean motion:   15.54236047  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2359
    Checksum:              316
 
             

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