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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  17659.2714
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   69.6
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.922
   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 
   ------------------------------------------------------------------------
   016/05:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.8  
   000/00:00:00.000           0.0               0.0              216.2  
   
   018/18:05:10.698           3.0               3.2              3.2    
   N/A                        0.8               0.0              220.9  
   000/00:08:17.397          -0.6              -0.0              218.0  
   
   020/01:03:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.0  
   000/00:00:00.000           0.0               0.0              217.9  
   
   025/12:55:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.6  
   000/00:00:00.000           0.0               0.0              217.5  
   
   026/08:59:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.8  
   000/00:00:00.000           0.0               0.0              217.4  
   
 
 
    Coasting Arc #1 (Orbit 3136)
    ---------------------------------------
 
    Vector Time (GMT): 2019/014/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2829696.45                 A    =         6787626.57  meter
     Y    =       -5628335.52  meter          E    =           .0003091
     Z    =       -2524477.48                 I    =           51.92620
     XDOT =       5505.483972                 Wp   =          146.58238
     YDOT =       -385.072906  meter/sec      RA   =           45.01300  deg
     ZDOT =      -5318.198167                 TA   =           61.61581
                                              MA   =           61.58465
                                              Ha   =            220.719  n.mi
                                              Hp   =            216.074
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9283781.02                 X    =        -2754286.09
     Y    =      -18465667.70  feet           Y    =        -5659557.42  meter
     Z    =       -8282406.43                 Z    =        -2538040.02
     XDOT =      18062.611458                 XDOT =        5535.213467
     YDOT =      -1263.362551  feet/sec       YDOT =        -323.340344  meter/sec
     ZDOT =     -17448.156715                 ZDOT =       -5291.382574
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13452162.09                 X    =         4100219.01
     Y    =      -15658974.03  feet           Y    =        -4772855.28  meter
     Z    =       -8342877.04                 Z    =        -2542908.92
     XDOT =       7063.413020                 XDOT =        2152.928288
     YDOT =      15289.851465  feet/sec       YDOT =        4660.346727  meter/sec
     ZDOT =     -17327.048985                 ZDOT =       -5281.284531
  
  
    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   19014.52708432  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6422  45.5300 0002452 287.2155  72.8729 15.53770861 31374
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19014.52708432   =   yrday.fracday
    Element set:     900
    Inclination:       51.6422  deg
    RA of node:        45.5300  deg
    Eccentricity:     .0002452     
    Arg of perigee:   287.2155  deg
    Mean anomaly:      72.8729  deg
    Mean motion:   15.53770861  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3137
    Checksum:              291
 
 
    Coasting Arc #2 (Orbit 3152)
    ---------------------------------------
 
    Vector Time (GMT): 2019/015/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1735385.68                 A    =         6784308.64  meter
     Y    =        5345456.63  meter          E    =           .0009272
     Z    =        3792576.05                 I    =           51.88865
     XDOT =      -6317.419207                 Wp   =           92.76245
     YDOT =       -964.724541  meter/sec      RA   =           40.05289  deg
     ZDOT =       4241.062848                 TA   =          312.54859
                                              MA   =          312.62682
                                              Ha   =            220.859  n.mi
                                              Hp   =            216.036
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5693522.56                 X    =         1657060.17
     Y    =       17537587.36  feet           Y    =         5364424.80  meter
     Z    =       12442834.81                 Z    =         3800815.88
     XDOT =     -20726.440969                 XDOT =       -6326.762490
     YDOT =      -3165.106762  feet/sec       YDOT =       -1035.422762  meter/sec
     ZDOT =      13914.248189                 ZDOT =        4210.352606
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13789876.04                 X    =        -4203154.22
     Y    =       12203015.80  feet           Y    =         3719479.22  meter
     Z    =       12479304.14                 Z    =         3803691.90
     XDOT =      -4605.049008                 XDOT =       -1403.618938
     YDOT =     -19322.838392  feet/sec       YDOT =       -5889.601142  meter/sec
     ZDOT =      13775.747544                 ZDOT =        4198.847851
  
  
    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   19015.55616275  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6402  40.4028 0002312 294.1684  65.9227 15.53745097 31539
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19015.55616275   =   yrday.fracday
    Element set:     901
    Inclination:       51.6402  deg
    RA of node:        40.4028  deg
    Eccentricity:     .0002312     
    Arg of perigee:   294.1684  deg
    Mean anomaly:      65.9227  deg
    Mean motion:   15.53745097  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3153
    Checksum:              294
 
 
    Coasting Arc #3 (Orbit 3163)
    ---------------------------------------
 
    Vector Time (GMT): 2019/016/05:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5936183.90                 A    =         6787015.53  meter
     Y    =       -1566921.04  meter          E    =           .0010879
     Z    =        2881736.78                 I    =           51.87942
     XDOT =       -975.177622                 Wp   =           98.20537
     YDOT =      -5666.323504  meter/sec      RA   =           36.39803  deg
     ZDOT =      -5074.986258                 TA   =           49.10465
                                              MA   =           49.01047
                                              Ha   =            220.802  n.mi
                                              Hp   =            216.189
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19475668.98                 X    =        -5932218.78
     Y    =       -5140817.07  feet           Y    =        -1633281.59  meter
     Z    =        9454517.00                 Z    =         2852910.69
     XDOT =      -3199.401648                 XDOT =        -887.091372
     YDOT =     -18590.300210  feet/sec       YDOT =       -5676.735795  meter/sec
     ZDOT =     -16650.217381                 ZDOT =       -5079.509679
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20200160.38                 X    =         6157008.88
     Y    =        -350365.99  feet           Y    =         -106791.55  meter
     Z    =        9324609.29                 Z    =         2842140.91
     XDOT =       7988.070137                 XDOT =        2434.763778
     YDOT =      15584.615103  feet/sec       YDOT =        4750.190683  meter/sec
     ZDOT =     -16669.858994                 ZDOT =       -5080.973021
  
  
    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   19016.26365308  .00016717  00000-0  10270-3 0  9029
    2 25544  51.6410  36.8752 0002482 283.3022  76.7854 15.53747168 31644
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19016.26365308   =   yrday.fracday
    Element set:     902
    Inclination:       51.6410  deg
    RA of node:        36.8752  deg
    Eccentricity:     .0002482     
    Arg of perigee:   283.3022  deg
    Mean anomaly:      76.7854  deg
    Mean motion:   15.53747168  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3164
    Checksum:              307
 
 
    Coasting Arc #4 (Orbit 3178)
    ---------------------------------------
 
    Vector Time (GMT): 2019/017/05:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6163261.66                 A    =         6789600.00  meter
     Y    =        2448057.32  meter          E    =           .0008332
     Z    =       -1434397.95                 I    =           51.86204
     XDOT =       -624.072454                 Wp   =           20.10035
     YDOT =       4964.754004  meter/sec      RA   =           31.44094  deg
     ZDOT =       5809.373304                 TA   =          324.30761
                                              MA   =          324.36329
                                              Ha   =            220.841  n.mi
                                              Hp   =            216.138
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20220674.74                 X    =         6142396.20
     Y    =        8031684.12  feet           Y    =         2516862.65  meter
     Z    =       -4706030.02                 Z    =        -1404509.78
     XDOT =      -2047.481803                 XDOT =        -707.761897
     YDOT =      16288.563005  feet/sec       YDOT =        4957.306791  meter/sec
     ZDOT =      19059.623701                 ZDOT =        5806.138942
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21705992.01                 X    =        -6615986.36
     Y    =       -1866025.05  feet           Y    =         -568764.43  meter
     Z    =       -4571456.75                 Z    =        -1393380.02
     XDOT =      -2739.427061                 XDOT =        -834.977368
     YDOT =     -14644.144467  feet/sec       YDOT =       -4463.535234  meter/sec
     ZDOT =      19044.335112                 ZDOT =        5804.713342
  
  
    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   19017.22841008  .00016717  00000-0  10270-3 0  9033
    2 25544  51.6423  32.0688 0002536 292.9444  67.1441 15.53751354 31792
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19017.22841008   =   yrday.fracday
    Element set:     903
    Inclination:       51.6423  deg
    RA of node:        32.0688  deg
    Eccentricity:     .0002536     
    Arg of perigee:   292.9444  deg
    Mean anomaly:      67.1441  deg
    Mean motion:   15.53751354  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3179
    Checksum:              299
 
 
    Coasting Arc #5 (Orbit 3194)
    ---------------------------------------
 
    Vector Time (GMT): 2019/018/05:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928709.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6011679.70                 A    =         6790369.24  meter
     Y    =       -3142412.48  meter          E    =           .0009430
     Z    =        -167195.90                 I    =           51.83495
     XDOT =       2322.870056                 Wp   =          141.26601
     YDOT =      -4133.385208  meter/sec      RA   =           26.48690  deg
     ZDOT =      -6025.324510                 TA   =           40.52991
                                              MA   =           40.45972
                                              Ha   =            220.793  n.mi
                                              Hp   =            216.078
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19723358.59                 X    =        -5975281.42
     Y    =      -10309752.24  feet           Y    =        -3209435.74  meter
     Z    =        -548542.98                 Z    =         -196310.04
     XDOT =       7620.964751                 XDOT =        2398.185518
     YDOT =     -13560.975091  feet/sec       YDOT =       -4106.987556  meter/sec
     ZDOT =     -19768.125034                 ZDOT =       -6013.858450
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21920578.10                 X    =         6681392.20
     Y    =        3824823.40  feet           Y    =         1165806.17  meter
     Z    =        -679519.52                 Z    =         -207117.55
     XDOT =      -2982.363790                 XDOT =        -909.024483
     YDOT =      13679.275511  feet/sec       YDOT =        4169.443176  meter/sec
     ZDOT =     -19715.790181                 ZDOT =       -6009.372847
  
  
    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   19018.25748341  .00016717  00000-0  10270-3 0  9044
    2 25544  51.6414  26.9420 0002471 294.9208  65.1687 15.53764139 31959
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19018.25748341   =   yrday.fracday
    Element set:     904
    Inclination:       51.6414  deg
    RA of node:        26.9420  deg
    Eccentricity:     .0002471     
    Arg of perigee:   294.9208  deg
    Mean anomaly:      65.1687  deg
    Mean motion:   15.53764139  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3195
    Checksum:              317
 
 
    Coasting Arc #6 (Orbit 3202)
    ---------------------------------------
 
    Vector Time (GMT): 2019/018/18:09:19.397
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1978710.32                 A    =         6780178.40  meter
     Y    =       -3711628.21  meter          E    =           .0010205
     Z    =       -5326606.75                 I    =           51.77926
     XDOT =       6910.898202                 Wp   =           86.86691
     YDOT =       3291.485180  meter/sec      RA   =           23.84784  deg
     ZDOT =        274.698500                 TA   =          185.74362
                                              MA   =          185.75534
                                              Ha   =            220.947  n.mi
                                              Hp   =            217.951
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6491831.76                 X    =         2045941.14
     Y    =      -12177257.90  feet           Y    =        -3689124.43  meter
     Z    =      -17475743.95                 Z    =        -5316832.12
     XDOT =      22673.550533                 XDOT =        6872.243943
     YDOT =      10798.835894  feet/sec       YDOT =        3368.551498  meter/sec
     ZDOT =        901.241799                 ZDOT =         308.175143
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        -198942.88                 X    =          -60637.79
     Y    =      -13854538.50  feet           Y    =        -4222863.34  meter
     Z    =      -17431101.53                 Z    =        -5312999.75
     XDOT =      24041.484986                 XDOT =        7327.844624
     YDOT =      -1664.524446  feet/sec       YDOT =        -507.347051  meter/sec
     ZDOT =       1051.886530                 ZDOT =         320.615014
  
  
    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   19018.77202257  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6414  24.3821 0004744 283.7239  76.3385 15.53170510 32034
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19018.77202257   =   yrday.fracday
    Element set:     905
    Inclination:       51.6414  deg
    RA of node:        24.3821  deg
    Eccentricity:     .0004744     
    Arg of perigee:   283.7239  deg
    Mean anomaly:      76.3385  deg
    Mean motion:   15.53170510  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3203
    Checksum:              291
 
 
    Coasting Arc #7 (Orbit 3218)
    ---------------------------------------
 
    Vector Time (GMT): 2019/019/18:09:19.397
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3247629.22                 A    =         6781237.02  meter
     Y    =        3116494.70  meter          E    =           .0004618
     Z    =        5073430.95                 I    =           51.75198
     XDOT =      -6443.508778                 Wp   =          358.22806
     YDOT =      -3727.145510  meter/sec      RA   =           18.86814  deg
     ZDOT =      -1830.686914                 TA   =          109.50062
                                              MA   =          109.45073
                                              Ha   =            221.058  n.mi
                                              Hp   =            217.907
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10654951.51                 X    =        -3306880.86
     Y    =       10224720.15  feet           Y    =         3079845.62  meter
     Z    =       16645114.67                 Z    =         5057511.87
     XDOT =     -21140.120663                 XDOT =       -6392.459589
     YDOT =     -12228.167683  feet/sec       YDOT =       -3798.915683  meter/sec
     ZDOT =      -6006.190662                 ZDOT =       -1861.862946
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4137512.10                 X    =        -1261113.69
     Y    =       14260272.40  feet           Y    =         4346531.03  meter
     Z    =       16572819.95                 Z    =         5051395.52
     XDOT =     -23347.045175                 XDOT =       -7116.179369
     YDOT =        386.241740  feet/sec       YDOT =         117.726482  meter/sec
     ZDOT =      -6146.386608                 ZDOT =       -1873.418638
  
  
    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   19019.80149679  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6413  19.2582 0004951 287.3682  72.6929 15.53193896 32194
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19019.80149679   =   yrday.fracday
    Element set:     906
    Inclination:       51.6413  deg
    RA of node:        19.2582  deg
    Eccentricity:     .0004951     
    Arg of perigee:   287.3682  deg
    Mean anomaly:      72.6929  deg
    Mean motion:   15.53193896  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3219
    Checksum:              345
 
 
    Coasting Arc #8 (Orbit 3222)
    ---------------------------------------
 
    Vector Time (GMT): 2019/020/01:03:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1820716.88                 A    =         6780253.91  meter
     Y    =       -3816708.92  meter          E    =           .0010188
     Z    =       -5308756.95                 I    =           51.73723
     XDOT =       7154.952543                 Wp   =           89.82382
     YDOT =       2683.196869  meter/sec      RA   =           17.44620  deg
     ZDOT =        525.726351                 TA   =          185.18580
                                              MA   =          185.19636
                                              Ha   =            220.985  n.mi
                                              Hp   =            217.886
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5973480.57                 X    =         1889047.58
     Y    =      -12522010.91  feet           Y    =        -3795965.79  meter
     Z    =      -17417181.61                 Z    =        -5299747.20
     XDOT =      23474.253749                 XDOT =        7121.862876
     YDOT =       8803.139334  feet/sec       YDOT =        2763.023459  meter/sec
     ZDOT =       1724.823987                 ZDOT =         560.401693
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13239044.54                 X    =        -4035260.78
     Y    =        4317942.42  feet           Y    =         1316108.85  meter
     Z    =      -17375975.24                 Z    =        -5296197.25
     XDOT =      -9649.252720                 XDOT =       -2941.092229
     YDOT =     -22027.834444  feet/sec       YDOT =       -6714.083939  meter/sec
     ZDOT =       1880.961847                 ZDOT =         573.317171
  
  
    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   19020.05886592  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6391  17.9724 0004596 283.7195  76.3446 15.53170504 32237
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19020.05886592   =   yrday.fracday
    Element set:     907
    Inclination:       51.6391  deg
    RA of node:        17.9724  deg
    Eccentricity:     .0004596     
    Arg of perigee:   283.7195  deg
    Mean anomaly:      76.3446  deg
    Mean motion:   15.53170504  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3223
    Checksum:              320
 
 
    Coasting Arc #9 (Orbit 3238)
    ---------------------------------------
 
    Vector Time (GMT): 2019/021/01:03:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3133093.51                 A    =         6781742.52  meter
     Y    =        3348126.14  meter          E    =           .0004819
     Z    =        4997336.25                 I    =           51.70928
     XDOT =      -6675.471755                 Wp   =           10.30574
     YDOT =      -3149.235811  meter/sec      RA   =           12.46214  deg
     ZDOT =      -2070.332732                 TA   =           99.84792
                                              MA   =           99.79350
                                              Ha   =            221.258  n.mi
                                              Hp   =            217.835
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10279178.18                 X    =        -3194574.03
     Y    =       10984665.80  feet           Y    =         3312745.51  meter
     Z    =       16395460.13                 Z    =         4981968.20
     XDOT =     -21901.154051                 XDOT =       -6629.703706
     YDOT =     -10332.138487  feet/sec       YDOT =       -3223.629498  meter/sec
     ZDOT =      -6792.430223                 ZDOT =       -2102.647995
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15114072.59                 X    =         4606769.33
     Y    =        -417587.45  feet           Y    =         -127280.65  meter
     Z    =       16325621.90                 Z    =         4976049.55
     XDOT =       8110.038362                 XDOT =        2471.939693
     YDOT =      21660.760474  feet/sec       YDOT =        6602.199792  meter/sec
     ZDOT =      -6937.848359                 ZDOT =       -2114.656180
  
  
    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   19021.08833941  .00016717  00000-0  10270-3 0  9084
    2 25544  51.6386  12.8464 0004509 287.8517  72.2143 15.53130165 32398
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19021.08833941   =   yrday.fracday
    Element set:     908
    Inclination:       51.6386  deg
    RA of node:        12.8464  deg
    Eccentricity:     .0004509     
    Arg of perigee:   287.8517  deg
    Mean anomaly:      72.2143  deg
    Mean motion:   15.53130165  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3239
    Checksum:              306
 
 
    Coasting Arc #10 (Orbit 3253)
    ---------------------------------------
 
    Vector Time (GMT): 2019/022/01:03:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4324456.33                 A    =         6784229.01  meter
     Y    =       -2900794.42  meter          E    =           .0003976
     Z    =       -4352625.85                 I    =           51.68592
     XDOT =       5852.664258                 Wp   =          108.79321
     YDOT =       3529.308393  meter/sec      RA   =            7.48243  deg
     ZDOT =       3464.030130                 TA   =          196.38349
                                              MA   =          196.39634
                                              Ha   =            221.253  n.mi
                                              Hp   =            217.885
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14187848.84                 X    =         4377714.47
     Y    =       -9517042.06  feet           Y    =        -2852137.29  meter
     Z    =      -14280268.55                 Z    =        -4331490.68
     XDOT =      19201.654390                 XDOT =        5795.937703
     YDOT =      11579.095779  feet/sec       YDOT =        3594.439579  meter/sec
     ZDOT =      11364.928249                 ZDOT =        3492.321814
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16884341.14                 X    =        -5146347.18
     Y    =       -3084659.83  feet           Y    =         -940204.31  meter
     Z    =      -14184467.29                 Z    =        -4323425.63
     XDOT =      -5926.114396                 XDOT =       -1806.279668
     YDOT =     -20387.472132  feet/sec       YDOT =       -6214.101506  meter/sec
     ZDOT =      11492.130727                 ZDOT =        3502.801445
  
  
    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   19022.05346789  .00016717  00000-0  10270-3 0  9092
    2 25544  51.6394   8.0428 0004585 291.4174  68.6488 15.53161727 32544
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19022.05346789   =   yrday.fracday
    Element set:     909
    Inclination:       51.6394  deg
    RA of node:         8.0428  deg
    Eccentricity:     .0004585     
    Arg of perigee:   291.4174  deg
    Mean anomaly:      68.6488  deg
    Mean motion:   15.53161727  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3254
    Checksum:              330
 
 
    Coasting Arc #11 (Orbit 3269)
    ---------------------------------------
 
    Vector Time (GMT): 2019/023/01:03:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5338626.77                 A    =         6787398.38  meter
     Y    =        2452548.81  meter          E    =           .0008477
     Z    =        3393595.34                 I    =           51.66343
     XDOT =      -4728.357610                 Wp   =           78.08431
     YDOT =      -3871.168335  meter/sec      RA   =            2.50588  deg
     ZDOT =      -4629.215342                 TA   =           62.29682
                                              MA   =           62.21084
                                              Ha   =            221.350  n.mi
                                              Hp   =            217.803
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17515179.68                 X    =        -5382138.81
     Y    =        8046419.98  feet           Y    =         2392605.18  meter
     Z    =       11133842.99                 Z    =         3367557.43
     XDOT =     -15512.984284                 XDOT =       -4662.232189
     YDOT =     -12700.683514  feet/sec       YDOT =       -3923.674269  meter/sec
     ZDOT =     -15187.714378                 ZDOT =       -4652.022775
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       18347077.79                 X    =         5592189.31
     Y    =        6125494.48  feet           Y    =         1867050.72  meter
     Z    =       11015984.17                 Z    =         3357671.97
     XDOT =       3038.838668                 XDOT =         926.238026
     YDOT =      18464.125266  feet/sec       YDOT =        5627.865381  meter/sec
     ZDOT =     -15290.114605                 ZDOT =       -4660.426932
  
  
    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   19023.08293871  .00016717  00000-0  10270-3 0  9101
    2 25544  51.6395   2.9178 0004617 294.2978  65.7692 15.53151143 32703
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19023.08293871   =   yrday.fracday
    Element set:     910
    Inclination:       51.6395  deg
    RA of node:         2.9178  deg
    Eccentricity:     .0004617     
    Arg of perigee:   294.2978  deg
    Mean anomaly:      65.7692  deg
    Mean motion:   15.53151143  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3270
    Checksum:              318
 
 
    Coasting Arc #12 (Orbit 3284)
    ---------------------------------------
 
    Vector Time (GMT): 2019/024/01:03:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6088239.54                 A    =         6790110.59  meter
     Y    =       -2017584.53  meter          E    =           .0006900
     Z    =       -2216023.52                 I    =           51.64120
     XDOT =       3373.938490                 Wp   =             .63998
     YDOT =       4184.843322  meter/sec      RA   =          357.53442  deg
     ZDOT =       5466.265841                 TA   =          334.74862
                                              MA   =          334.78233
                                              Ha   =            221.514  n.mi
                                              Hp   =            217.720
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19974539.17                 X    =         6121112.18
     Y    =       -6619371.80  feet           Y    =        -1949317.78  meter
     Z    =       -7270418.37                 Z    =        -2186370.08
     XDOT =      11069.352000                 XDOT =        3300.340257
     YDOT =      13729.800925  feet/sec       YDOT =        4222.161540  meter/sec
     ZDOT =      17933.943048                 ZDOT =        5482.475985
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19300214.19                 X    =        -5882705.28
     Y    =       -8498943.71  feet           Y    =        -2590478.04  meter
     Z    =       -7136313.45                 Z    =        -2175148.34
     XDOT =        450.035474                 XDOT =         137.170812
     YDOT =     -16122.151433  feet/sec       YDOT =       -4914.031757  meter/sec
     ZDOT =      18006.523706                 ZDOT =        5488.388426
  
  
    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   19024.04806487  .00016717  00000-0  10270-3 0  9112
    2 25544  51.6412 358.1137 0004659 299.7091  60.3597 15.53169889 32853
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19024.04806487   =   yrday.fracday
    Element set:     911
    Inclination:       51.6412  deg
    RA of node:       358.1137  deg
    Eccentricity:     .0004659     
    Arg of perigee:   299.7091  deg
    Mean anomaly:      60.3597  deg
    Mean motion:   15.53169889  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3285
    Checksum:              339
 
 
    Coasting Arc #13 (Orbit 3300)
    ---------------------------------------
 
    Vector Time (GMT): 2019/025/01:03:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928366.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6552033.19                 A    =         6791807.87  meter
     Y    =        1546519.23  meter          E    =           .0008710
     Z    =         865714.30                 I    =           51.61316
     XDOT =      -1848.950872                 Wp   =          127.16501
     YDOT =      -4494.801544  meter/sec      RA   =          352.56636  deg
     ZDOT =      -5927.973487                 TA   =           43.47023
                                              MA   =           43.40160
                                              Ha   =            221.549  n.mi
                                              Hp   =            217.631
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21496171.88                 X    =        -6573044.91
     Y    =        5073881.98  feet           Y    =         1473132.35  meter
     Z    =        2840270.01                 Z    =          833836.64
     XDOT =      -6066.111785                 XDOT =       -1769.757163
     YDOT =     -14746.724226  feet/sec       YDOT =       -4515.035093  meter/sec
     ZDOT =     -19448.731913                 ZDOT =       -5936.762384
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19552596.24                 X    =         5959631.34
     Y    =       10311317.77  feet           Y    =         3142889.66  meter
     Z    =        2696205.38                 Z    =          821803.40
     XDOT =      -4463.623998                 XDOT =       -1360.512595
     YDOT =      13592.238051  feet/sec       YDOT =        4142.914158  meter/sec
     ZDOT =     -19487.779015                 ZDOT =       -5939.875044
  
  
    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   19025.07753157  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6405 352.9896 0004656 303.5351  56.5356 15.53177678 33013
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19025.07753157   =   yrday.fracday
    Element set:     912
    Inclination:       51.6405  deg
    RA of node:       352.9896  deg
    Eccentricity:     .0004656     
    Arg of perigee:   303.5351  deg
    Mean anomaly:      56.5356  deg
    Mean motion:   15.53177678  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3301
    Checksum:              319
 
 
    Coasting Arc #14 (Orbit 3308)
    ---------------------------------------
 
    Vector Time (GMT): 2019/025/12:55:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 913933.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4060136.58                 A    =         6783115.20  meter
     Y    =        2960978.54  meter          E    =           .0003984
     Z    =        4552865.75                 I    =           51.56783
     XDOT =      -6055.953289                 Wp   =           94.17228
     YDOT =       3544.102569  meter/sec      RA   =          350.13646  deg
     ZDOT =       3093.009432                 TA   =          324.82304
                                              MA   =          324.84933
                                              Ha   =            221.599  n.mi
                                              Hp   =            217.517
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13320658.07                 X    =         4004609.48
     Y    =        9714496.52  feet           Y    =         3006071.43  meter
     Z    =       14937223.60                 Z    =         4572453.06
     XDOT =     -19868.613152                 XDOT =       -6110.158171
     YDOT =      11627.633100  feet/sec       YDOT =        3476.077655  meter/sec
     ZDOT =      10147.668739                 ZDOT =        3063.460765
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3193825.03                 X    =          973477.87
     Y    =       16092689.00  feet           Y    =         4905051.61  meter
     Z    =       15025207.66                 Z    =         4579683.29
     XDOT =     -21383.990261                 XDOT =       -6517.840231
     YDOT =      -5113.615911  feet/sec       YDOT =       -1558.630130  meter/sec
     ZDOT =      10013.848294                 ZDOT =        3052.220960
  
  
    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   19025.59226340  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6400 350.4317 0004980 309.1721  50.8988 15.53207744 33096
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19025.59226340   =   yrday.fracday
    Element set:     913
    Inclination:       51.6400  deg
    RA of node:       350.4317  deg
    Eccentricity:     .0004980     
    Arg of perigee:   309.1721  deg
    Mean anomaly:      50.8988  deg
    Mean motion:   15.53207744  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3309
    Checksum:              299
 
 
    Coasting Arc #15 (Orbit 3321)
    ---------------------------------------
 
    Vector Time (GMT): 2019/026/08:59:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 913933.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4592363.79                 A    =         6783957.71  meter
     Y    =        2422975.74  meter          E    =           .0005360
     Z    =        4361162.40                 I    =           51.54198
     XDOT =      -5452.809776                 Wp   =           87.45205
     YDOT =       4165.489121  meter/sec      RA   =          345.97313  deg
     ZDOT =       3424.212794                 TA   =          327.76632
                                              MA   =          327.79906
                                              Ha   =            221.794  n.mi
                                              Hp   =            217.436
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15066810.34                 X    =         4543744.34
     Y    =        7949395.49  feet           Y    =         2474058.98  meter
     Z    =       14308275.59                 Z    =         4383351.88
     XDOT =     -17889.795853                 XDOT =       -5515.616828
     YDOT =      13666.302890  feet/sec       YDOT =        4104.160880  meter/sec
     ZDOT =      11234.293943                 ZDOT =        3397.572928
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10606641.65                 X    =        -3232904.38
     Y    =       13222522.19  feet           Y    =         4030224.76  meter
     Z    =       14408069.70                 Z    =         4391579.64
     XDOT =      -9107.163589                 XDOT =       -2775.863462
     YDOT =     -19427.520206  feet/sec       YDOT =       -5921.508159  meter/sec
     ZDOT =      11113.525881                 ZDOT =        3387.402689
  
  
    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   19026.42870485  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6390 346.2679 0004860 313.5493  46.5255 15.53164039 33223
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19026.42870485   =   yrday.fracday
    Element set:     914
    Inclination:       51.6390  deg
    RA of node:       346.2679  deg
    Eccentricity:     .0004860     
    Arg of perigee:   313.5493  deg
    Mean anomaly:      46.5255  deg
    Mean motion:   15.53164039  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3322
    Checksum:              315
 
 
    Coasting Arc #16 (Orbit 3336)
    ---------------------------------------
 
    Vector Time (GMT): 2019/027/08:59:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 913933.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3453483.88                 A    =         6781419.20  meter
     Y    =       -3019730.07  meter          E    =           .0011479
     Z    =       -5004320.10                 I    =           51.50199
     XDOT =       6298.732230                 Wp   =           53.15425
     YDOT =      -3863.732097  meter/sec      RA   =          340.98049  deg
     ZDOT =      -2011.753922                 TA   =          197.21423
                                              MA   =          197.25319
                                              Ha   =            222.025  n.mi
                                              Hp   =            217.151
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11330327.67                 X    =        -3395151.87
     Y    =       -9907250.89  feet           Y    =        -3058023.21  meter
     Z    =      -16418373.03                 Z    =        -5020953.90
     XDOT =      20665.131989                 XDOT =        6351.241285
     YDOT =     -12676.286408  feet/sec       YDOT =       -3793.001698  meter/sec
     ZDOT =      -6600.242527                 ZDOT =       -1981.029916
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11670180.98                 X    =         3557071.16
     Y    =       -9374447.78  feet           Y    =        -2857331.68  meter
     Z    =      -16493014.37                 Z    =        -5027070.78
     XDOT =       8291.698191                 XDOT =        2527.309609
     YDOT =      21709.967819  feet/sec       YDOT =        6617.198191  meter/sec
     ZDOT =      -6461.100172                 ZDOT =       -1969.343333
  
  
    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   19027.39382636  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6394 341.4639 0004780 318.2479  41.8308 15.53175743 33374
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19027.39382636   =   yrday.fracday
    Element set:     915
    Inclination:       51.6394  deg
    RA of node:       341.4639  deg
    Eccentricity:     .0004780     
    Arg of perigee:   318.2479  deg
    Mean anomaly:      41.8308  deg
    Mean motion:   15.53175743  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3337
    Checksum:              330
 
 
    Coasting Arc #17 (Orbit 3352)
    ---------------------------------------
 
    Vector Time (GMT): 2019/028/08:59:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 913933.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2188289.78                 A    =         6780191.07  meter
     Y    =        3635818.79  meter          E    =           .0003094
     Z    =        5288322.67                 I    =           51.46553
     XDOT =      -6833.149168                 Wp   =          349.22462
     YDOT =       3446.840031  meter/sec      RA   =          335.98074  deg
     ZDOT =        460.791105                 TA   =           96.38658
                                              MA   =           96.35134
                                              Ha   =            222.125  n.mi
                                              Hp   =            217.208
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7179428.40                 X    =         2121782.98
     Y    =       11928539.34  feet           Y    =         3659917.87  meter
     Z    =       17350139.99                 Z    =         5298790.92
     XDOT =     -22418.468399                 XDOT =       -6873.423092
     YDOT =      11308.530287  feet/sec       YDOT =        3370.201805  meter/sec
     ZDOT =       1511.781840                 ZDOT =         427.500859
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12869319.53                 X    =        -3922568.59
     Y    =        5156625.93  feet           Y    =         1571739.58  meter
     Z    =       17396879.73                 Z    =         5302568.94
     XDOT =      -7371.153172                 XDOT =       -2246.727487
     YDOT =     -22954.745743  feet/sec       YDOT =       -6996.606503  meter/sec
     ZDOT =       1361.129030                 ZDOT =         414.872128
  
  
    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   19028.42328729  .00016717  00000-0  10270-3 0  9161
    2 25544  51.6382 336.3390 0004944 321.7154  38.3647 15.53171978 33530
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19028.42328729   =   yrday.fracday
    Element set:     916
    Inclination:       51.6382  deg
    RA of node:       336.3390  deg
    Eccentricity:     .0004944     
    Arg of perigee:   321.7154  deg
    Mean anomaly:      38.3647  deg
    Mean motion:   15.53171978  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3353
    Checksum:              325
 
 
    Coasting Arc #18 (Orbit 3367)
    ---------------------------------------
 
    Vector Time (GMT): 2019/029/08:59:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 913933.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -914478.66                 A    =         6780614.68  meter
     Y    =       -4247390.75  meter          E    =           .0011339
     Z    =       -5215137.31                 I    =           51.43666
     XDOT =       7011.476078                 Wp   =           79.92519
     YDOT =      -2873.526272  meter/sec      RA   =          330.97857  deg
     ZDOT =       1114.847045                 TA   =          200.78033
                                              MA   =          200.82646
                                              Ha   =            222.289  n.mi
                                              Hp   =            217.060
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3000258.08                 X    =         -841583.27
     Y    =      -13935009.03  feet           Y    =        -4257209.39  meter
     Z    =      -17110030.54                 Z    =        -5219402.49
     XDOT =      23003.530441                 XDOT =        7037.672318
     YDOT =      -9427.579631  feet/sec       YDOT =       -2794.972610  meter/sec
     ZDOT =       3657.634661                 ZDOT =        1148.969283
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14199072.00                 X    =         4327877.15
     Y    =        -965912.05  feet           Y    =         -294409.99  meter
     Z    =      -17128705.10                 Z    =        -5220829.32
     XDOT =       6147.930116                 XDOT =        1873.889099
     YDOT =      23010.811451  feet/sec       YDOT =        7013.695330  meter/sec
     ZDOT =       3811.954469                 ZDOT =        1161.883722
  
  
    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   19029.38840601  .00016717  00000-0  10270-3 0  9176
    2 25544  51.6380 331.5353 0004968 325.4799  34.6030 15.53162305 33681
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19029.38840601   =   yrday.fracday
    Element set:     917
    Inclination:       51.6380  deg
    RA of node:       331.5353  deg
    Eccentricity:     .0004968     
    Arg of perigee:   325.4799  deg
    Mean anomaly:      34.6030  deg
    Mean motion:   15.53162305  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3368
    Checksum:              311
 
             

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