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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  13813.3257
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   94.1
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.554
   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 
   ------------------------------------------------------------------------
   213/16:38:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.6  
   000/00:00:00.000           0.0               0.0              212.8  
   
   217/02:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.5  
   000/00:00:00.000           0.0               0.0              212.8  
   
   220/05:58:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.6  
   000/00:00:00.000           0.0               0.0              212.7  
   
   223/08:44:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.4  
   000/00:00:00.000           0.0               0.0              212.9  
   
 
 
    Coasting Arc #1 (Orbit 1156)
    ---------------------------------------
 
    Vector Time (GMT): 2016/211/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5607679.79                 A    =         6786537.52  meter
     Y    =       -3657218.31  meter          E    =           .0015300
     Z    =        1069016.01                 I    =           51.49057
     XDOT =       3436.107671                 Wp   =           60.38795
     YDOT =      -3533.996104  meter/sec      RA   =          205.81212  deg
     ZDOT =       5878.503749                 TA   =          311.23707
                                              MA   =          311.36882
                                              Ha   =            220.446  n.mi
                                              Hp   =            212.708
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18397899.57                 X    =        -5571559.84
     Y    =      -11998747.74  feet           Y    =        -3719725.25  meter
     Z    =        3507270.37                 Z    =         1041863.04
     XDOT =      11273.319130                 XDOT =        3446.815377
     YDOT =     -11594.475408  feet/sec       YDOT =       -3495.511806  meter/sec
     ZDOT =      19286.429623                 ZDOT =        5895.221089
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1394702.55                 X    =          425105.34
     Y    =       21939007.02  feet           Y    =         6687009.34  meter
     Z    =        3389450.84                 Z    =         1033104.62
     XDOT =     -14358.118931                 XDOT =       -4376.354650
     YDOT =      -2107.556622  feet/sec       YDOT =        -642.383258  meter/sec
     ZDOT =      19359.926763                 ZDOT =        5900.905677
  
  
    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   16211.56227129  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6387 206.6068 0001954  87.3196 272.8181 15.54934887 11570
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16211.56227129   =   yrday.fracday
    Element set:     900
    Inclination:       51.6387  deg
    RA of node:       206.6068  deg
    Eccentricity:     .0001954     
    Arg of perigee:    87.3196  deg
    Mean anomaly:     272.8181  deg
    Mean motion:   15.54934887  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1157
    Checksum:              326
 
 
    Coasting Arc #2 (Orbit 1171)
    ---------------------------------------
 
    Vector Time (GMT): 2016/212/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4486421.30                 A    =         6783621.40  meter
     Y    =        4178645.00  meter          E    =           .0006442
     Z    =       -2905988.27                 I    =           51.50879
     XDOT =      -5336.138426                 Wp   =          107.18574
     YDOT =       2243.751828  meter/sec      RA   =          200.82367  deg
     ZDOT =      -5022.914314                 TA   =          105.99042
                                              MA   =          105.91945
                                              Ha   =            220.579  n.mi
                                              Hp   =            212.781
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14719229.99                 X    =         4453477.04
     Y    =       13709465.21  feet           Y    =         4228631.17  meter
     Z    =       -9534082.23                 Z    =        -2884274.36
     XDOT =     -17507.015834                 XDOT =       -5336.433222
     YDOT =       7361.390513  feet/sec       YDOT =        2184.078296  meter/sec
     ZDOT =     -16479.377671                 ZDOT =       -5048.836127
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1807062.44                 X    =          550792.63
     Y    =      -20077943.12  feet           Y    =        -6119757.06  meter
     Z    =       -9440053.89                 Z    =        -2877328.43
     XDOT =      15000.242721                 XDOT =        4572.073981
     YDOT =       9134.243427  feet/sec       YDOT =        2784.117397  meter/sec
     ZDOT =     -16592.820660                 ZDOT =       -5057.491737
  
  
    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   16212.52633186  .00016717  00000-0  10270-3 0  9014
    2 25544  51.6378 201.7947 0002043  84.3398 275.7988 15.54883111 11720
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16212.52633186   =   yrday.fracday
    Element set:     901
    Inclination:       51.6378  deg
    RA of node:       201.7947  deg
    Eccentricity:     .0002043     
    Arg of perigee:    84.3398  deg
    Mean anomaly:     275.7988  deg
    Mean motion:   15.54883111  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1172
    Checksum:              318
 
 
    Coasting Arc #3 (Orbit 1187)
    ---------------------------------------
 
    Vector Time (GMT): 2016/213/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2864896.56                 A    =         6779221.09  meter
     Y    =       -4371728.43  meter          E    =           .0011572
     Z    =        4309329.12                 I    =           51.52516
     XDOT =       6760.726830                 Wp   =          104.72447
     YDOT =       -972.475898  meter/sec      RA   =          195.82605  deg
     ZDOT =       3497.315074                 TA   =          309.62222
                                              MA   =          309.72431
                                              Ha   =            220.493  n.mi
                                              Hp   =            212.770
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9399266.93                 X    =        -2836730.35
     Y    =      -14342941.05  feet           Y    =        -4403608.43  meter
     Z    =       14138218.88                 Z    =         4295480.52
     XDOT =      22180.862303                 XDOT =        6754.110690
     YDOT =      -3190.537723  feet/sec       YDOT =        -896.910174  meter/sec
     ZDOT =      11474.130821                 ZDOT =        3530.140265
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5262287.89                 X    =        -1603945.35
     Y    =       16372509.42  feet           Y    =         4990340.87  meter
     Z    =       14078518.09                 Z    =         4291132.31
     XDOT =     -15113.817806                 XDOT =       -4606.691667
     YDOT =     -14877.914678  feet/sec       YDOT =       -4534.788394  meter/sec
     ZDOT =      11617.498283                 ZDOT =        3541.013477
  
  
    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   16213.55465791  .00016717  00000-0  10270-3 0  9024
    2 25544  51.6382 196.6630 0001832  87.8120 272.3243 15.54913888 11881
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16213.55465791   =   yrday.fracday
    Element set:     902
    Inclination:       51.6382  deg
    RA of node:       196.6630  deg
    Eccentricity:     .0001832     
    Arg of perigee:    87.8120  deg
    Mean anomaly:     272.3243  deg
    Mean motion:   15.54913888  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1188
    Checksum:              319
 
 
    Coasting Arc #4 (Orbit 1190)
    ---------------------------------------
 
    Vector Time (GMT): 2016/213/16:38:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2795145.73                 A    =         6779013.46  meter
     Y    =       -4343962.44  meter          E    =           .0011303
     Z    =        4382344.09                 I    =           51.53290
     XDOT =       6820.711651                 Wp   =          105.41773
     YDOT =       -968.536905  meter/sec      RA   =          194.86112  deg
     ZDOT =       3380.112432                 TA   =          310.29844
                                              MA   =          310.39717
                                              Ha   =            220.556  n.mi
                                              Hp   =            212.776
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9170425.63                 X    =        -2767649.85
     Y    =      -14251845.28  feet           Y    =        -4375066.19  meter
     Z    =       14377769.31                 Z    =         4368832.71
     XDOT =      22377.662898                 XDOT =        6814.616329
     YDOT =      -3177.614518  feet/sec       YDOT =        -892.297464  meter/sec
     ZDOT =      11089.607716                 ZDOT =        3413.230251
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13283695.33                 X    =         4048870.34
     Y    =       10603135.23  feet           Y    =         3231835.62  meter
     Z    =       14319532.55                 Z    =         4364593.52
     XDOT =     -19393.142030                 XDOT =       -5911.029691
     YDOT =       9078.569928  feet/sec       YDOT =        2767.148114  meter/sec
     ZDOT =      11234.255283                 ZDOT =        3424.201010
  
  
    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   16213.74747083  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6408 195.7011 0001914  84.8224 275.3148 15.54892111 11912
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16213.74747083   =   yrday.fracday
    Element set:     903
    Inclination:       51.6408  deg
    RA of node:       195.7011  deg
    Eccentricity:     .0001914     
    Arg of perigee:    84.8224  deg
    Mean anomaly:     275.3148  deg
    Mean motion:   15.54892111  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1191
    Checksum:              299
 
 
    Coasting Arc #5 (Orbit 1205)
    ---------------------------------------
 
    Vector Time (GMT): 2016/214/16:38:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         781065.47                 A    =         6775705.55  meter
     Y    =        4311446.20  meter          E    =           .0015855
     Z    =       -5182372.35                 I    =           51.55437
     XDOT =      -7537.296976                 Wp   =           80.61176
     YDOT =       -235.188542  meter/sec      RA   =          189.85203  deg
     ZDOT =      -1332.610302                 TA   =          176.55594
                                              MA   =          176.54501
                                              Ha   =            220.484  n.mi
                                              Hp   =            212.716
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2562550.75                 X    =          757968.92
     Y    =       14145164.69  feet           Y    =         4320051.74  meter
     Z    =      -17002533.97                 Z    =        -5178634.08
     XDOT =     -24728.664619                 XDOT =       -7527.633750
     YDOT =       -771.615951  feet/sec       YDOT =        -319.421527  meter/sec
     ZDOT =      -4372.081044                 ZDOT =       -1369.200347
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7210719.91                 X    =        -2197827.43
     Y    =      -12457466.02  feet           Y    =        -3797035.64  meter
     Z    =      -16986923.52                 Z    =        -5177614.29
     XDOT =      22650.246318                 XDOT =        6903.795078
     YDOT =      -6935.457583  feet/sec       YDOT =       -2113.927471  meter/sec
     ZDOT =      -4531.704557                 ZDOT =       -1381.263549
  
  
    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   16214.71152506  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6417 190.8898 0001972  85.0276 275.1102 15.54913270 12060
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16214.71152506   =   yrday.fracday
    Element set:     904
    Inclination:       51.6417  deg
    RA of node:       190.8898  deg
    Eccentricity:     .0001972     
    Arg of perigee:    85.0276  deg
    Mean anomaly:     275.1102  deg
    Mean motion:   15.54913270  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1206
    Checksum:              296
 
 
    Coasting Arc #6 (Orbit 1221)
    ---------------------------------------
 
    Vector Time (GMT): 2016/215/16:38:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1350450.59                 A    =         6775223.84  meter
     Y    =       -4062138.86  meter          E    =           .0004910
     Z    =        5247776.14                 I    =           51.58486
     XDOT =       7502.645610                 Wp   =           70.56735
     YDOT =       1342.805697  meter/sec      RA   =          184.83991  deg
     ZDOT =       -889.011934                 TA   =           27.94888
                                              MA   =           27.92252
                                              Ha   =            220.325  n.mi
                                              Hp   =            212.753
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4430612.16                 X    =         1370283.25
     Y    =      -13327227.24  feet           Y    =        -4046926.52  meter
     Z    =       17217113.34                 Z    =         5254384.16
     XDOT =      24614.979035                 XDOT =        7491.390744
     YDOT =       4405.530502  feet/sec       YDOT =        1426.642394  meter/sec
     ZDOT =      -2916.705819                 ZDOT =        -852.594104
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         584225.49                 X    =          178071.93
     Y    =       13995981.21  feet           Y    =         4265975.07  meter
     Z    =       17246608.14                 Z    =         5256766.16
     XDOT =     -23607.238168                 XDOT =       -7195.486194
     YDOT =       4393.160376  feet/sec       YDOT =        1339.035283  meter/sec
     ZDOT =      -2757.990132                 ZDOT =        -840.635392
  
  
    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   16215.73984838  .00016717  00000-0  10270-3 0  9057
    2 25544  51.6415 185.7583 0001753  89.1275 271.0079 15.54937360 12225
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16215.73984838   =   yrday.fracday
    Element set:     905
    Inclination:       51.6415  deg
    RA of node:       185.7583  deg
    Eccentricity:     .0001753     
    Arg of perigee:    89.1275  deg
    Mean anomaly:     271.0079  deg
    Mean motion:   15.54937360  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1222
    Checksum:              326
 
 
    Coasting Arc #7 (Orbit 1236)
    ---------------------------------------
 
    Vector Time (GMT): 2016/216/16:38:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3362217.85                 A    =         6777968.28  meter
     Y    =        3665150.63  meter          E    =           .0012045
     Z    =       -4616410.79                 I    =           51.62726
     XDOT =      -6652.369511                 Wp   =          107.61437
     YDOT =      -2345.064758  meter/sec      RA   =          179.83321  deg
     ZDOT =       2986.071991                 TA   =          192.18985
                                              MA   =          192.21902
                                              Ha   =            220.406  n.mi
                                              Hp   =            212.722
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11030898.45                 X    =        -3380528.60
     Y    =       12024772.42  feet           Y    =         3627449.76  meter
     Z    =      -15145704.70                 Z    =        -4632787.64
     XDOT =     -21825.359287                 XDOT =       -6640.156698
     YDOT =      -7693.782015  feet/sec       YDOT =       -2419.387760  meter/sec
     ZDOT =       9796.824119                 ZDOT =        2953.786834
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5809199.87                 X    =         1770644.12
     Y    =      -15176983.18  feet           Y    =        -4625944.47  meter
     Z    =      -15217773.22                 Z    =        -4638377.28
     XDOT =      22080.303087                 XDOT =        6730.076381
     YDOT =      -1221.310432  feet/sec       YDOT =        -372.255420  meter/sec
     ZDOT =       9656.285482                 ZDOT =        2943.235815
  
  
    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   16216.70390204  .00016717  00000-0  10270-3 0  9064
    2 25544  51.6428 180.9470 0001733  91.0098 269.1253 15.54902760 12378
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16216.70390204   =   yrday.fracday
    Element set:     906
    Inclination:       51.6428  deg
    RA of node:       180.9470  deg
    Eccentricity:     .0001733     
    Arg of perigee:    91.0098  deg
    Mean anomaly:     269.1253  deg
    Mean motion:   15.54902760  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1237
    Checksum:              296
 
 
    Coasting Arc #8 (Orbit 1243)
    ---------------------------------------
 
    Vector Time (GMT): 2016/217/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3202206.54                 A    =         6777536.74  meter
     Y    =       -3631200.70  meter          E    =           .0009677
     Z    =        4737270.04                 I    =           51.63901
     XDOT =       6760.738435                 Wp   =          116.12450
     YDOT =      -2406.957548  meter/sec      RA   =          177.83715  deg
     ZDOT =       2716.540315                 TA   =          306.99183
                                              MA   =          307.08036
                                              Ha   =            220.476  n.mi
                                              Hp   =            212.765
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10505926.97                 X    =        -3184374.63
     Y    =      -11913388.12  feet           Y    =        -3666910.24  meter
     Z    =       15542224.55                 Z    =         4721758.17
     XDOT =      22180.900378                 XDOT =        6773.955697
     YDOT =      -7896.842348  feet/sec       YDOT =       -2331.280571  meter/sec
     ZDOT =       8912.533842                 ZDOT =        2749.413613
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8015185.98                 X    =        -2443028.69
     Y    =      -13789205.55  feet           Y    =        -4202949.85  meter
     Z    =       15475098.26                 Z    =         4716809.95
     XDOT =      22248.171774                 XDOT =        6781.242757
     YDOT =      -2737.086947  feet/sec       YDOT =        -834.264101  meter/sec
     ZDOT =       9056.408445                 ZDOT =        2760.393294
  
  
    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   16217.15379138  .00016717  00000-0  10270-3 0  9078
    2 25544  51.6428 178.6973 0001863 109.5095 250.6259 15.54931644 12448
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16217.15379138   =   yrday.fracday
    Element set:     907
    Inclination:       51.6428  deg
    RA of node:       178.6973  deg
    Eccentricity:     .0001863     
    Arg of perigee:   109.5095  deg
    Mean anomaly:     250.6259  deg
    Mean motion:   15.54931644  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1244
    Checksum:              330
 
 
    Coasting Arc #9 (Orbit 1258)
    ---------------------------------------
 
    Vector Time (GMT): 2016/218/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1160210.26                 A    =         6775239.30  meter
     Y    =        4077633.75  meter          E    =           .0016363
     Z    =       -5299123.31                 I    =           51.66326
     XDOT =      -7507.504919                 Wp   =           88.31227
     YDOT =       1397.655112  meter/sec      RA   =          172.83378  deg
     ZDOT =       -569.286853                 TA   =          176.25532
                                              MA   =          176.24305
                                              Ha   =            220.423  n.mi
                                              Hp   =            212.844
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3806464.09                 X    =         1140267.21
     Y    =       13378063.50  feet           Y    =         4090496.43  meter
     Z    =      -17385575.18                 Z    =        -5293535.91
     XDOT =     -24630.921651                 XDOT =       -7519.810590
     YDOT =       4585.482650  feet/sec       YDOT =        1313.632363  meter/sec
     ZDOT =      -1867.739019                 ZDOT =        -605.785562
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1408775.11                 X    =          429394.65
     Y    =       13867301.06  feet           Y    =         4226753.36  meter
     Z    =      -17361834.30                 Z    =        -5291887.09
     XDOT =     -24030.493265                 XDOT =       -7324.494347
     YDOT =        -92.598495  feet/sec       YDOT =         -28.224021  meter/sec
     ZDOT =      -2027.293192                 ZDOT =        -617.918965
  
  
    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   16218.11784273  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6428 173.8873 0001822 109.6175 250.5175 15.54899782 12597
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16218.11784273   =   yrday.fracday
    Element set:     908
    Inclination:       51.6428  deg
    RA of node:       173.8873  deg
    Eccentricity:     .0001822     
    Arg of perigee:   109.6175  deg
    Mean anomaly:     250.5175  deg
    Mean motion:   15.54899782  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1259
    Checksum:              337
 
 
    Coasting Arc #10 (Orbit 1274)
    ---------------------------------------
 
    Vector Time (GMT): 2016/219/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         967326.73                 A    =         6775849.77  meter
     Y    =       -4337669.24  meter          E    =           .0006103
     Z    =        5110358.70                 I    =           51.69789
     XDOT =       7488.483690                 Wp   =           69.83376
     YDOT =       -280.456304  meter/sec      RA   =          167.82882  deg
     ZDOT =      -1651.871185                 TA   =           36.10773
                                              MA   =           36.06653
                                              Ha   =            220.335  n.mi
                                              Hp   =            212.784
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3173644.11                 X    =          990936.28
     Y    =      -14231198.31  feet           Y    =        -4326719.82  meter
     Z    =       16766268.71                 Z    =         5115115.10
     XDOT =      24568.516044                 XDOT =        7499.087198
     YDOT =       -920.132232  feet/sec       YDOT =        -196.655826  meter/sec
     ZDOT =      -5419.524886                 ZDOT =       -1615.468915
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5381666.48                 X    =         1640331.94
     Y    =      -13524672.10  feet           Y    =        -4122320.06  meter
     Z    =       16787724.66                 Z    =         5116898.48
     XDOT =      23429.005761                 XDOT =        7141.160956
     YDOT =       2778.127635  feet/sec       YDOT =         846.773303  meter/sec
     ZDOT =      -5260.553855                 ZDOT =       -1603.416815
  
  
    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   16219.14616206  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6430 168.7552 0001808 112.7154 247.4190 15.54934624 12758
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16219.14616206   =   yrday.fracday
    Element set:     909
    Inclination:       51.6430  deg
    RA of node:       168.7552  deg
    Eccentricity:     .0001808     
    Arg of perigee:   112.7154  deg
    Mean anomaly:     247.4190  deg
    Mean motion:   15.54934624  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1275
    Checksum:              303
 
 
    Coasting Arc #11 (Orbit 1289)
    ---------------------------------------
 
    Vector Time (GMT): 2016/220/02:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2935307.86                 A    =         6779303.16  meter
     Y    =        4408322.10  meter          E    =           .0010079
     Z    =       -4242513.20                 I    =           51.74078
     XDOT =      -6673.753820                 Wp   =          111.70280
     YDOT =       -943.296951  meter/sec      RA   =          162.83423  deg
     ZDOT =       3640.579220                 TA   =          195.52766
                                              MA   =          195.55860
                                              Ha   =            220.356  n.mi
                                              Hp   =            212.729
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9630275.13                 X    =        -2963776.69
     Y    =       14462999.01  feet           Y    =         4375338.22  meter
     Z    =      -13919006.57                 Z    =        -4256841.25
     XDOT =     -21895.517781                 XDOT =       -6680.393726
     YDOT =      -3094.806271  feet/sec       YDOT =       -1017.964346  meter/sec
     ZDOT =      11944.157547                 ZDOT =        3608.144190
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11585583.92                 X    =        -3531285.98
     Y    =       12881370.42  feet           Y    =         3926241.71  meter
     Z    =      -13982268.21                 Z    =        -4261795.35
     XDOT =     -20328.084210                 XDOT =       -6196.000067
     YDOT =      -5483.539474  feet/sec       YDOT =       -1671.382832  meter/sec
     ZDOT =      11802.688019                 ZDOT =        3597.459308
  
  
    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   16220.11021068  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6430 163.9451 0001851 116.0302 244.1042 15.54930656 12901
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16220.11021068   =   yrday.fracday
    Element set:     910
    Inclination:       51.6430  deg
    RA of node:       163.9451  deg
    Eccentricity:     .0001851     
    Arg of perigee:   116.0302  deg
    Mean anomaly:     244.1042  deg
    Mean motion:   15.54930656  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1290
    Checksum:              253
 
 
    Coasting Arc #12 (Orbit 1292)
    ---------------------------------------
 
    Vector Time (GMT): 2016/220/05:58:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4693076.37                 A    =         6778945.76  meter
     Y    =       -2130398.36  meter          E    =           .0011560
     Z    =        4396214.02                 I    =           51.74247
     XDOT =       5221.121727                 Wp   =          108.83940
     YDOT =      -4488.271784  meter/sec      RA   =          162.14644  deg
     ZDOT =       3387.754275                 TA   =          306.89677
                                              MA   =          307.00266
                                              Ha   =            220.604  n.mi
                                              Hp   =            212.728
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15397232.18                 X    =        -4690259.52
     Y    =       -6989495.95  feet           Y    =        -2182863.60  meter
     Z    =       14423274.34                 Z    =         4373423.47
     XDOT =      17129.664458                 XDOT =        5254.466665
     YDOT =     -14725.301130  feet/sec       YDOT =       -4429.699167  meter/sec
     ZDOT =      11114.679380                 ZDOT =        3413.197926
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15911353.24                 X    =        -4849780.47
     Y    =        5967207.99  feet           Y    =         1818804.99  meter
     Z    =       14324102.83                 Z    =         4365986.54
     XDOT =       2147.923825                 XDOT =         654.687182
     YDOT =     -21308.110224  feet/sec       YDOT =       -6494.711996  meter/sec
     ZDOT =      11226.488929                 ZDOT =        3421.833826
  
  
    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   16220.30302032  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6418 162.9838 0002037 105.7521 254.3857 15.54913869 12937
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16220.30302032   =   yrday.fracday
    Element set:     911
    Inclination:       51.6418  deg
    RA of node:       162.9838  deg
    Eccentricity:     .0002037     
    Arg of perigee:   105.7521  deg
    Mean anomaly:     254.3857  deg
    Mean motion:   15.54913869  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1293
    Checksum:              294
 
 
    Coasting Arc #13 (Orbit 1307)
    ---------------------------------------
 
    Vector Time (GMT): 2016/221/05:58:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2973076.00                 A    =         6775731.90  meter
     Y    =        3192244.85  meter          E    =           .0015602
     Z    =       -5198407.60                 I    =           51.76303
     XDOT =      -6475.118958                 Wp   =           83.50973
     YDOT =       3866.168594  meter/sec      RA   =          157.15224  deg
     ZDOT =      -1330.821079                 TA   =          173.71771
                                              MA   =          173.69813
                                              Ha   =            220.461  n.mi
                                              Hp   =            212.866
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9754186.36                 X    =         2962409.87
     Y    =       10473244.26  feet           Y    =         3225431.99  meter
     Z    =      -17055143.03                 Z    =        -5183991.31
     XDOT =     -21243.828601                 XDOT =       -6511.405711
     YDOT =      12684.280164  feet/sec       YDOT =        3793.556556  meter/sec
     ZDOT =      -4366.210890                 ZDOT =       -1362.363455
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14384350.22                 X    =         4384349.95
     Y    =         222460.10  feet           Y    =           67805.84  meter
     Z    =      -16992700.81                 Z    =        -5179375.21
     XDOT =      -5670.532483                 XDOT =       -1728.378301
     YDOT =      23005.696341  feet/sec       YDOT =        7012.136245  meter/sec
     ZDOT =      -4504.565169                 ZDOT =       -1372.991464
  
  
    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   16221.26706662  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6428 158.1731 0001927 109.6277 250.5084 15.54901214 13083
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16221.26706662   =   yrday.fracday
    Element set:     912
    Inclination:       51.6428  deg
    RA of node:       158.1731  deg
    Eccentricity:     .0001927     
    Arg of perigee:   109.6277  deg
    Mean anomaly:     250.5084  deg
    Mean motion:   15.54901214  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1308
    Checksum:              294
 
 
    Coasting Arc #14 (Orbit 1323)
    ---------------------------------------
 
    Vector Time (GMT): 2016/222/05:58:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1040299.44                 A    =         6775281.47  meter
     Y    =       -4134829.14  meter          E    =           .0004875
     Z    =        5261480.03                 I    =           51.78934
     XDOT =       7039.993320                 Wp   =           79.28777
     YDOT =      -2918.028326  meter/sec      RA   =          152.15396  deg
     ZDOT =       -899.647492                 TA   =           19.30239
                                              MA   =           19.28393
                                              Ha   =            220.512  n.mi
                                              Hp   =            212.721
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3413055.91                 X    =        -1019543.18
     Y    =      -13565712.41  feet           Y    =        -4146346.29  meter
     Z    =       17262073.59                 Z    =         5256477.07
     XDOT =      23097.090944                 XDOT =        7076.470282
     YDOT =      -9573.583747  feet/sec       YDOT =       -2839.098480  meter/sec
     ZDOT =      -2951.599382                 ZDOT =        -865.360635
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12301804.04                 X    =        -3749589.87
     Y    =       -6713722.39  feet           Y    =        -2046342.58  meter
     Z    =       17240888.54                 Z    =         5255022.83
     XDOT =       8350.816737                 XDOT =        2545.328941
     YDOT =     -22508.936643  feet/sec       YDOT =       -6860.723889  meter/sec
     ZDOT =      -2801.395382                 ZDOT =        -853.865313
  
  
    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   16222.29538133  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6410 153.0413 0002037 110.9223 249.2148 15.54919986 13243
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16222.29538133   =   yrday.fracday
    Element set:     913
    Inclination:       51.6410  deg
    RA of node:       153.0413  deg
    Eccentricity:     .0002037     
    Arg of perigee:   110.9223  deg
    Mean anomaly:     249.2148  deg
    Mean motion:   15.54919986  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1324
    Checksum:              285
 
 
    Coasting Arc #15 (Orbit 1338)
    ---------------------------------------
 
    Vector Time (GMT): 2016/223/05:58:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -873445.45                 A    =         6778012.88  meter
     Y    =        4889854.71  meter          E    =           .0012157
     Z    =       -4623654.25                 I    =           51.82779
     XDOT =      -6857.859309                 Wp   =          110.65491
     YDOT =       1614.406513  meter/sec      RA   =          147.16159  deg
     ZDOT =       3005.062934                 TA   =          189.27129
                                              MA   =          189.29376
                                              Ha   =            220.413  n.mi
                                              Hp   =            212.816
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2865634.66                 X    =         -905600.59
     Y    =       16042830.40  feet           Y    =         4879907.40  meter
     Z    =      -15169469.32                 Z    =        -4627975.36
     XDOT =     -22499.538415                 XDOT =       -6889.999502
     YDOT =       5296.609295  feet/sec       YDOT =        1537.537682  meter/sec
     ZDOT =       9859.130361                 ZDOT =        2971.671359
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10023736.01                 X    =         3055234.74
     Y    =       12826225.19  feet           Y    =         3909433.44  meter
     Z    =      -15189132.05                 Z    =        -4629647.45
     XDOT =     -10297.495194                 XDOT =       -3138.676535
     YDOT =      19541.380092  feet/sec       YDOT =        5956.212652  meter/sec
     ZDOT =       9713.029114                 ZDOT =        2960.531274
  
  
    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   16223.25942410  .00016717  00000-0  10270-3 0  9143
    2 25544  51.6424 148.2305 0001821 112.5213 247.6133 15.54899461 13398
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16223.25942410   =   yrday.fracday
    Element set:     914
    Inclination:       51.6424  deg
    RA of node:       148.2305  deg
    Eccentricity:     .0001821     
    Arg of perigee:   112.5213  deg
    Mean anomaly:     247.6133  deg
    Mean motion:   15.54899461  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1339
    Checksum:              285
 
 
    Coasting Arc #16 (Orbit 1340)
    ---------------------------------------
 
    Vector Time (GMT): 2016/223/08:44:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5605437.41                 A    =         6780967.47  meter
     Y    =         -95255.82  meter          E    =           .0007624
     Z    =       -3821764.68                 I    =           51.83822
     XDOT =      -2764.701392                 Wp   =           84.90767
     YDOT =       5777.740654  meter/sec      RA   =          146.63457  deg
     ZDOT =      -4205.587313                 TA   =          140.84887
                                              MA   =          140.79368
                                              Ha   =            220.443  n.mi
                                              Hp   =            212.898
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18390542.69                 X    =         5624650.31
     Y    =        -312519.11  feet           Y    =          -32464.70  meter
     Z    =      -12538598.02                 Z    =        -3794488.42
     XDOT =      -9070.542624                 XDOT =       -2808.675306
     YDOT =      18955.842040  feet/sec       YDOT =        5746.577986  meter/sec
     ZDOT =     -13797.858639                 ZDOT =       -4219.124313
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -123396.89                 X    =          -37611.37
     Y    =      -18473445.92  feet           Y    =        -5630706.32  meter
     Z    =      -12419449.99                 Z    =        -3785448.36
     XDOT =      17513.974072                 XDOT =        5338.259297
     YDOT =       9184.913464  feet/sec       YDOT =        2799.561624  meter/sec
     ZDOT =     -13857.917305                 ZDOT =       -4223.893195
  
  
    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   16223.38796391  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6399 147.5883 0001858 110.4645 249.6707 15.54915020 13410
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16223.38796391   =   yrday.fracday
    Element set:     915
    Inclination:       51.6399  deg
    RA of node:       147.5883  deg
    Eccentricity:     .0001858     
    Arg of perigee:   110.4645  deg
    Mean anomaly:     249.6707  deg
    Mean motion:   15.54915020  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1341
    Checksum:              327
 
 
    Coasting Arc #17 (Orbit 1356)
    ---------------------------------------
 
    Vector Time (GMT): 2016/224/08:44:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4464092.84                 A    =         6776859.58  meter
     Y    =       -1379827.02  meter          E    =           .0008511
     Z    =        4903756.52                 I    =           51.85098
     XDOT =       4395.146887                 Wp   =          120.13278
     YDOT =      -5833.219216  meter/sec      RA   =          141.65219  deg
     ZDOT =       2352.511892                 TA   =          306.88250
                                              MA   =          306.96048
                                              Ha   =            220.418  n.mi
                                              Hp   =            212.843
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14645973.87                 X    =        -4472151.63
     Y    =       -4526991.54  feet           Y    =        -1429792.54  meter
     Z    =       16088440.02                 Z    =         4882051.67
     XDOT =      14419.773250                 XDOT =        4448.621364
     YDOT =     -19137.858320  feet/sec       YDOT =       -5783.770745  meter/sec
     ZDOT =       7718.214868                 ZDOT =        2373.992146
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4423612.64                 X    =        -1348317.13
     Y    =       14780538.64  feet           Y    =         4505108.18  meter
     Z    =       15993856.14                 Z    =         4874927.35
     XDOT =     -18158.069726                 XDOT =       -5534.579653
     YDOT =     -13914.568246  feet/sec       YDOT =       -4241.160401  meter/sec
     ZDOT =       7812.992890                 ZDOT =        2381.400233
  
  
    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   16224.41627296  .00016717  00000-0  10270-3 0  9166
    2 25544  51.6397 142.4569 0001656 115.2689 244.8636 15.54942429 13578
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16224.41627296   =   yrday.fracday
    Element set:     916
    Inclination:       51.6397  deg
    RA of node:       142.4569  deg
    Eccentricity:     .0001656     
    Arg of perigee:   115.2689  deg
    Mean anomaly:     244.8636  deg
    Mean motion:   15.54942429  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1357
    Checksum:              338
 
 
    Coasting Arc #18 (Orbit 1371)
    ---------------------------------------
 
    Vector Time (GMT): 2016/225/08:44:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3004679.59                 A    =         6775095.04  meter
     Y    =        2923884.74  meter          E    =           .0016382
     Z    =       -5336196.69                 I    =           51.86943
     XDOT =      -5481.832939                 Wp   =           91.64689
     YDOT =       5344.649643  meter/sec      RA   =          136.66031  deg
     ZDOT =       -159.046725                 TA   =          176.84528
                                              MA   =          176.83493
                                              Ha   =            220.341  n.mi
                                              Hp   =            212.968
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9857872.67                 X    =         2997681.38
     Y    =        9592797.71  feet           Y    =         2957445.99  meter
     Z    =      -17507207.00                 Z    =        -5321617.81
     XDOT =     -17985.016204                 XDOT =       -5540.418169
     YDOT =      17534.939772  feet/sec       YDOT =        5283.020554  meter/sec
     ZDOT =       -521.806841                 ZDOT =        -185.818116
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9348098.55                 X    =         2849300.44
     Y    =      -10199102.36  feet           Y    =        -3108686.40  meter
     Z    =      -17443998.48                 Z    =        -5316930.74
     XDOT =      17219.456482                 XDOT =        5248.490336
     YDOT =      16871.729780  feet/sec       YDOT =        5142.503237  meter/sec
     ZDOT =       -639.637382                 ZDOT =        -194.961474
  
  
    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   16225.38031344  .00016717  00000-0  10270-3 0  9177
    2 25544  51.6396 137.6452 0001701 116.7524 243.3803 15.54910646 13722
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16225.38031344   =   yrday.fracday
    Element set:     917
    Inclination:       51.6396  deg
    RA of node:       137.6452  deg
    Eccentricity:     .0001701     
    Arg of perigee:   116.7524  deg
    Mean anomaly:     243.3803  deg
    Mean motion:   15.54910646  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1372
    Checksum:              293
 
 
    Coasting Arc #19 (Orbit 1387)
    ---------------------------------------
 
    Vector Time (GMT): 2016/226/08:44:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930011.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1399975.58                 A    =         6776376.08  meter
     Y    =       -4336714.93  meter          E    =           .0006820
     Z    =        5010471.92                 I    =           51.89801
     XDOT =       6001.101938                 Wp   =           69.12070
     YDOT =      -4317.796360  meter/sec      RA   =          131.67029  deg
     ZDOT =      -2055.794686                 TA   =           40.80935
                                              MA   =           40.75829
                                              Ha   =            220.343  n.mi
                                              Hp   =            212.897
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4593095.72                 X    =        -1375715.74
     Y    =      -14228067.35  feet           Y    =        -4352234.83  meter
     Z    =       16438556.18                 Z    =         5003730.12
     XDOT =      19688.654652                 XDOT =        6058.924673
     YDOT =     -14165.998558  feet/sec       YDOT =       -4250.364687  meter/sec
     ZDOT =      -6744.733222                 ZDOT =       -2026.502778
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14020379.76                 X    =        -4273411.75
     Y    =        5282740.88  feet           Y    =         1610179.42  meter
     Z    =       16409818.97                 Z    =         5001712.82
     XDOT =     -14584.130684                 XDOT =       -4445.243033
     YDOT =     -18107.607553  feet/sec       YDOT =       -5519.198782  meter/sec
     ZDOT =      -6616.040202                 ZDOT =       -2016.569053
  
  
    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   16226.40861976  .00016717  00000-0  10270-3 0  9184
    2 25544  51.6408 132.5135 0001631 120.4829 239.6485 15.54924596 13880
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16226.40861976   =   yrday.fracday
    Element set:     918
    Inclination:       51.6408  deg
    RA of node:       132.5135  deg
    Eccentricity:     .0001631     
    Arg of perigee:   120.4829  deg
    Mean anomaly:     239.6485  deg
    Mean motion:   15.54924596  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1388
    Checksum:              328
 
             

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