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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14929.5437
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   75.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.582
   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 
   ------------------------------------------------------------------------
   333/15:51:36.572           0.5               1.2              1.2    
   N/A                       -1.1              -0.1              221.5  
   000/00:03:13.144           0.3              -0.0              214.6  
   
   334/13:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.4  
   000/00:00:00.000           0.0               0.0              214.6  
   
   338/13:10:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.0  
   000/00:00:00.000           0.0               0.0              214.9  
   
   338/19:53:38.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.9  
   000/00:00:00.000           0.0               0.0              215.1  
   
   340/11:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.8  
   000/00:00:00.000           0.0               0.0              215.2  
   
 
 
    Coasting Arc #1 (Orbit 636)
    ---------------------------------------
 
    Vector Time (GMT): 2017/326/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3733843.58                 A    =         6785764.08  meter
     Y    =        4911372.07  meter          E    =           .0016694
     Z    =        2804522.85                 I    =           51.45541
     XDOT =      -5587.266051                 Wp   =          108.21937
     YDOT =      -1330.020529  meter/sec      RA   =          328.47687  deg
     ZDOT =      -5089.709712                 TA   =           39.83558
                                              MA   =           39.71315
                                              Ha   =            222.032  n.mi
                                              Hp   =            213.499
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12250142.97                 X    =        -3802109.57
     Y    =       16113425.42  feet           Y    =         4869235.79  meter
     Z    =        9201190.44                 Z    =         2786219.22
     XDOT =     -18330.925363                 XDOT =       -5547.254425
     YDOT =      -4363.584412  feet/sec       YDOT =       -1392.277084  meter/sec
     ZDOT =     -16698.522678                 ZDOT =       -5116.754279
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8059496.16                 X    =        -2456534.43
     Y    =      -18607968.29  feet           Y    =        -5671708.74  meter
     Z    =        9119124.12                 Z    =         2779509.03
     XDOT =      11343.511824                 XDOT =        3457.502404
     YDOT =     -13187.280325  feet/sec       YDOT =       -4019.483043  meter/sec
     ZDOT =     -16818.240956                 ZDOT =       -5126.199844
  
  
    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   17326.53782513  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6398 328.9242 0003909 138.2726 221.8725 15.54228034  6371
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17326.53782513   =   yrday.fracday
    Element set:     900
    Inclination:       51.6398  deg
    RA of node:       328.9242  deg
    Eccentricity:     .0003909     
    Arg of perigee:   138.2726  deg
    Mean anomaly:     221.8725  deg
    Mean motion:   15.54228034  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             637
    Checksum:              315
 
 
    Coasting Arc #2 (Orbit 651)
    ---------------------------------------
 
    Vector Time (GMT): 2017/327/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4731204.05                 A    =         6788372.21  meter
     Y    =       -4711012.24  meter          E    =           .0009121
     Z    =       -1218641.78                 I    =           51.43649
     XDOT =       4176.539975                 Wp   =           63.72377
     YDOT =       2695.125116  meter/sec      RA   =          323.48965  deg
     ZDOT =       5833.965678                 TA   =          283.00063
                                              MA   =          283.10245
                                              Ha   =            222.006  n.mi
                                              Hp   =            213.460
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15522323.01                 X    =         4789451.86
     Y    =      -15456076.91  feet           Y    =        -4657778.92  meter
     Z    =       -3998168.57                 Z    =        -1195517.57
     XDOT =      13702.558973                 XDOT =        4117.753022
     YDOT =       8842.274001  feet/sec       YDOT =        2741.500954  meter/sec
     ZDOT =      19140.307344                 ZDOT =        5854.111688
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6267780.53                 X    =         1910419.51
     Y    =       21008662.98  feet           Y    =         6403440.48  meter
     Z    =       -3894763.64                 Z    =        -1187123.96
     XDOT =     -12680.242704                 XDOT =       -3864.937976
     YDOT =       7324.245694  feet/sec       YDOT =        2232.430088  meter/sec
     ZDOT =      19229.184024                 ZDOT =        5861.055290
  
  
    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   17327.50230734  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6393 324.1168 0004146 142.3636 217.7808 15.54249930  6522
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17327.50230734   =   yrday.fracday
    Element set:     901
    Inclination:       51.6393  deg
    RA of node:       324.1168  deg
    Eccentricity:     .0004146     
    Arg of perigee:   142.3636  deg
    Mean anomaly:     217.7808  deg
    Mean motion:   15.54249930  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             652
    Checksum:              298
 
 
    Coasting Arc #3 (Orbit 667)
    ---------------------------------------
 
    Vector Time (GMT): 2017/328/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5339464.29                 A    =         6788932.73  meter
     Y    =        4146242.38  meter          E    =           .0014706
     Z    =        -541661.34                 I    =           51.41150
     XDOT =      -2572.556284                 Wp   =          140.32713
     YDOT =      -4078.973275  meter/sec      RA   =          318.50390  deg
     ZDOT =      -5964.767002                 TA   =           45.53756
                                              MA   =           45.41738
                                              Ha   =            221.874  n.mi
                                              Hp   =            213.633
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17517927.46                 X    =        -5382800.69
     Y    =       13603157.41  feet           Y    =         4086290.56  meter
     Z    =       -1777104.15                 Z    =         -567704.12
     XDOT =      -8440.145288                 XDOT =       -2497.778669
     YDOT =     -13382.458252  feet/sec       YDOT =       -4107.322901  meter/sec
     ZDOT =     -19569.445546                 ZDOT =       -5977.082442
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4084447.69                 X    =        -1244939.66
     Y    =      -21790234.12  feet           Y    =        -6641663.36  meter
     Z    =       -1893345.51                 Z    =         -577091.71
     XDOT =      14114.921681                 XDOT =        4302.228128
     YDOT =       -967.634818  feet/sec       YDOT =        -294.935092  meter/sec
     ZDOT =     -19623.348996                 ZDOT =       -5981.196774
  
  
    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   17328.53108418  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6384 318.9869 0003876 145.5281 214.6123 15.54216522  6685
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17328.53108418   =   yrday.fracday
    Element set:     902
    Inclination:       51.6384  deg
    RA of node:       318.9869  deg
    Eccentricity:     .0003876     
    Arg of perigee:   145.5281  deg
    Mean anomaly:     214.6123  deg
    Mean motion:   15.54216522  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             668
    Checksum:              319
 
 
    Coasting Arc #4 (Orbit 683)
    ---------------------------------------
 
    Vector Time (GMT): 2017/329/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5522889.16                 A    =         6786807.29  meter
     Y    =       -3263042.89  meter          E    =           .0015010
     Z    =        2201227.22                 I    =           51.38154
     XDOT =        955.603063                 Wp   =           86.28913
     YDOT =       5313.156623  meter/sec      RA   =          313.51536  deg
     ZDOT =       5447.257077                 TA   =          298.25620
                                              MA   =          298.40763
                                              Ha   =            221.734  n.mi
                                              Hp   =            213.629
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18119715.08                 X    =         5548274.31
     Y    =      -10705521.30  feet           Y    =        -3201140.34  meter
     Z    =        7221874.09                 Z    =         2228117.49
     XDOT =       3135.180654                 XDOT =         869.658525
     YDOT =      17431.616216  feet/sec       YDOT =        5323.362029  meter/sec
     ZDOT =      17871.578335                 ZDOT =        5451.690648
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1609065.29                 X    =          490443.10
     Y    =       20942729.60  feet           Y    =         6383343.98  meter
     Z    =        7341710.43                 Z    =         2237753.34
     XDOT =     -15443.082544                 XDOT =       -4707.051559
     YDOT =      -5120.452187  feet/sec       YDOT =       -1560.713827  meter/sec
     ZDOT =      17890.313835                 ZDOT =        5452.967657
  
  
    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   17329.55985295  .00016717  00000-0  10270-3 0  9030
    2 25544  51.6389 313.8586 0003945 152.6597 207.4763 15.54266996  6844
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17329.55985295   =   yrday.fracday
    Element set:     903
    Inclination:       51.6389  deg
    RA of node:       313.8586  deg
    Eccentricity:     .0003945     
    Arg of perigee:   152.6597  deg
    Mean anomaly:     207.4763  deg
    Mean motion:   15.54266996  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             684
    Checksum:              368
 
 
    Coasting Arc #5 (Orbit 698)
    ---------------------------------------
 
    Vector Time (GMT): 2017/330/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5345485.42                 A    =         6783227.30  meter
     Y    =        2009169.31  meter          E    =           .0007699
     Z    =       -3665143.14                 I    =           51.34731
     XDOT =        591.552720                 Wp   =          106.80560
     YDOT =      -6298.101421  meter/sec      RA   =          308.51538  deg
     ZDOT =      -4325.011269                 TA   =          116.95471
                                              MA   =          116.87605
                                              Ha   =            221.715  n.mi
                                              Hp   =            213.660
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17537681.84                 X    =        -5349751.55
     Y    =        6591762.83  feet           Y    =         1949368.71  meter
     Z    =      -12024747.84                 Z    =        -3691120.42
     XDOT =       1940.789764                 XDOT =         682.944814
     YDOT =     -20663.062406  feet/sec       YDOT =       -6290.975126  meter/sec
     ZDOT =     -14189.669517                 ZDOT =       -4321.915889
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1489813.57                 X    =          454095.18
     Y    =      -18601331.40  feet           Y    =        -5669685.81  meter
     Z    =      -12140309.21                 Z    =        -3700366.25
     XDOT =      16463.720555                 XDOT =        5018.142025
     YDOT =      10549.283817  feet/sec       YDOT =        3215.421708  meter/sec
     ZDOT =     -14174.852134                 ZDOT =       -4320.494930
  
  
    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   17330.52432103  .00016717  00000-0  10270-3 0  9045
    2 25544  51.6387 309.0492 0003778 152.1327 208.0029 15.54230645  6995
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17330.52432103   =   yrday.fracday
    Element set:     904
    Inclination:       51.6387  deg
    RA of node:       309.0492  deg
    Eccentricity:     .0003778     
    Arg of perigee:   152.1327  deg
    Mean anomaly:     208.0029  deg
    Mean motion:   15.54230645  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             699
    Checksum:              294
 
 
    Coasting Arc #6 (Orbit 714)
    ---------------------------------------
 
    Vector Time (GMT): 2017/331/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4858042.51                 A    =         6779448.88  meter
     Y    =        -527725.84  meter          E    =           .0010820
     Z    =        4695103.64                 I    =           51.31469
     XDOT =      -1922.195893                 Wp   =          130.24980
     YDOT =       6897.083136  meter/sec      RA   =          303.50496  deg
     ZDOT =       2753.052878                 TA   =          292.32062
                                              MA   =          292.43528
                                              Ha   =            221.474  n.mi
                                              Hp   =            213.853
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15938459.69                 X    =         4840775.84
     Y    =       -1731383.99  feet           Y    =         -473496.53  meter
     Z    =       15403883.33                 Z    =         4718660.84
     XDOT =      -6306.416972                 XDOT =       -2012.551203
     YDOT =      22628.225512  feet/sec       YDOT =        6875.082561  meter/sec
     ZDOT =       9032.325716                 ZDOT =        2743.496020
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4933894.72                 X    =        -1503851.11
     Y    =       15147819.24  feet           Y    =         4617055.30  meter
     Z    =       15508451.39                 Z    =         4726975.98
     XDOT =     -16906.385758                 XDOT =       -5153.066379
     YDOT =     -14746.408198  feet/sec       YDOT =       -4494.705219  meter/sec
     ZDOT =       8988.761434                 ZDOT =        2739.774485
  
  
    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   17331.55307903  .00016717  00000-0  10270-3 0  9059
    2 25544  51.6380 303.9209 0003699 159.3939 200.7363 15.54263818  7154
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17331.55307903   =   yrday.fracday
    Element set:     905
    Inclination:       51.6380  deg
    RA of node:       303.9209  deg
    Eccentricity:     .0003699     
    Arg of perigee:   159.3939  deg
    Mean anomaly:     200.7363  deg
    Mean motion:   15.54263818  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             715
    Checksum:              317
 
 
    Coasting Arc #7 (Orbit 729)
    ---------------------------------------
 
    Vector Time (GMT): 2017/332/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4156213.09                 A    =         6777256.16  meter
     Y    =       -1148773.70  meter          E    =           .0015736
     Z    =       -5241874.51                 I    =           51.29023
     XDOT =       3009.198081                 Wp   =           96.58690
     YDOT =      -6988.834719  meter/sec      RA   =          298.48216  deg
     ZDOT =       -858.325505                 TA   =          165.17728
                                              MA   =          165.13110
                                              Ha   =            221.583  n.mi
                                              Hp   =            213.777
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13635869.72                 X    =        -4117595.47
     Y    =       -3768942.59  feet           Y    =        -1195035.31  meter
     Z    =      -17197751.03                 Z    =        -5261970.62
     XDOT =       9872.697115                 XDOT =        3091.294838
     YDOT =     -22929.247765  feet/sec       YDOT =       -6954.724765  meter/sec
     ZDOT =      -2816.028560                 ZDOT =        -843.508241
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8809813.56                 X    =         2685231.17
     Y    =      -10929881.80  feet           Y    =        -3331427.97  meter
     Z    =      -17286682.18                 Z    =        -5268980.73
     XDOT =      16353.274624                 XDOT =        4984.478105
     YDOT =      17508.618023  feet/sec       YDOT =        5336.626773  meter/sec
     ZDOT =      -2749.133066                 ZDOT =        -837.935758
  
  
    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   17332.51753578  .00016717  00000-0  10270-3 0  9060
    2 25544  51.6384 299.1113 0003704 161.0893 199.0398 15.54242988  7304
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17332.51753578   =   yrday.fracday
    Element set:     906
    Inclination:       51.6384  deg
    RA of node:       299.1113  deg
    Eccentricity:     .0003704     
    Arg of perigee:   161.0893  deg
    Mean anomaly:     199.0398  deg
    Mean motion:   15.54242988  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             730
    Checksum:              328
 
 
    Coasting Arc #8 (Orbit 745)
    ---------------------------------------
 
    Vector Time (GMT): 2017/333/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933812.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3314627.16                 A    =         6777409.17  meter
     Y    =        2819534.93  meter          E    =           .0004412
     Z    =        5191962.08                 I    =           51.27656
     XDOT =      -3823.815202                 Wp   =          107.10821
     YDOT =       6556.596495  meter/sec      RA   =          293.45635  deg
     ZDOT =      -1119.915210                 TA   =          353.67239
                                              MA   =          353.67796
                                              Ha   =            221.370  n.mi
                                              Hp   =            214.015
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10874761.01                 X    =         3257631.55
     Y    =        9250442.69  feet           Y    =         2856282.59  meter
     Z    =       17033996.33                 Z    =         5207925.42
     XDOT =     -12545.325465                 XDOT =       -3891.408529
     YDOT =      21511.143356  feet/sec       YDOT =        6513.458062  meter/sec
     ZDOT =      -3674.262499                 ZDOT =       -1138.654515
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12644371.58                 X    =        -3854004.46
     Y    =        6445949.82  feet           Y    =         1964725.51  meter
     Z    =       17104319.52                 Z    =         5213396.59
     XDOT =     -14679.292416                 XDOT =       -4474.248328
     YDOT =     -18826.025101  feet/sec       YDOT =       -5738.172451  meter/sec
     ZDOT =      -3758.466159                 ZDOT =       -1145.580485
  
  
    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   17333.54628209  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6388 293.9821 0003607 164.7409 195.3854 15.54255193  7466
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17333.54628209   =   yrday.fracday
    Element set:     907
    Inclination:       51.6388  deg
    RA of node:       293.9821  deg
    Eccentricity:     .0003607     
    Arg of perigee:   164.7409  deg
    Mean anomaly:     195.3854  deg
    Mean motion:   15.54255193  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             746
    Checksum:              337
 
 
    Coasting Arc #9 (Orbit 747)
    ---------------------------------------
 
    Vector Time (GMT): 2017/333/15:53:13.144
    Vector Time (MET): N/A
    Weight (LBS)     : 933686.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2943983.43                 A    =         6778699.16  meter
     Y    =       -3454526.49  meter          E    =           .0014228
     Z    =       -5047702.32                 I    =           51.27966
     XDOT =       4146.983170                 Wp   =          116.36284
     YDOT =      -6178.384123  meter/sec      RA   =          292.64016  deg
     ZDOT =       1807.453448                 TA   =          171.25931
                                              MA   =          171.23451
                                              Ha   =            221.462  n.mi
                                              Hp   =            214.585
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9658738.28                 X    =        -2880615.47
     Y    =      -11333748.33  feet           Y    =        -3487093.72  meter
     Z    =      -16560703.15                 Z    =        -5061849.70
     XDOT =      13605.587827                 XDOT =        4206.983418
     YDOT =     -20270.289119  feet/sec       YDOT =       -6131.674275  meter/sec
     ZDOT =       5929.965380                 ZDOT =        1827.744199
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3517007.97                 X    =         1071984.03
     Y    =      -14398364.70  feet           Y    =        -4388621.56  meter
     Z    =      -16622867.20                 Z    =        -5066649.92
     XDOT =      23320.015990                 XDOT =        7107.940874
     YDOT =      -1263.371842  feet/sec       YDOT =        -385.075737  meter/sec
     ZDOT =       6020.984369                 ZDOT =        1835.196036
  
  
    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   17333.67487486  .00016717  00000-0  10270-3 0  9082
    2 25544  51.6418 293.3417 0003244 180.3515 179.7636 15.54051385  7487
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17333.67487486   =   yrday.fracday
    Element set:     908
    Inclination:       51.6418  deg
    RA of node:       293.3417  deg
    Eccentricity:     .0003244     
    Arg of perigee:   180.3515  deg
    Mean anomaly:     179.7636  deg
    Mean motion:   15.54051385  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             748
    Checksum:              333
 
 
    Coasting Arc #10 (Orbit 761)
    ---------------------------------------
 
    Vector Time (GMT): 2017/334/13:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933686.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4045103.82                 A    =         6777592.22  meter
     Y    =       -1294985.42  meter          E    =           .0015017
     Z    =       -5294406.00                 I    =           51.26306
     XDOT =       2364.935551                 Wp   =          102.15068
     YDOT =      -7283.238059  meter/sec      RA   =          288.16088  deg
     ZDOT =        -28.618318                 TA   =          167.59332
                                              MA   =          167.55631
                                              Ha   =            221.392  n.mi
                                              Hp   =            214.616
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13271338.00                 X    =        -4004604.13
     Y    =       -4248639.83  feet           Y    =        -1339993.92  meter
     Z    =      -17370098.43                 Z    =        -5313957.95
     XDOT =       7758.974906                 XDOT =        2446.341920
     YDOT =     -23895.137990  feet/sec       YDOT =       -7256.336562  meter/sec
     ZDOT =        -93.892118                 ZDOT =         -16.932446
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4252583.22                 X    =         1296187.37
     Y    =      -13156085.10  feet           Y    =        -4009974.74  meter
     Z    =      -17456592.83                 Z    =        -5320769.49
     XDOT =      22934.333999                 XDOT =        6990.385003
     YDOT =       7453.787116  feet/sec       YDOT =        2271.914313  meter/sec
     ZDOT =        -40.859371                 ZDOT =         -12.453936
  
  
    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   17334.57514885  .00016717  00000-0  10270-3 0  9097
    2 25544  51.6395 288.8532 0003230 183.6633 176.4497 15.54047996  7628
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17334.57514885   =   yrday.fracday
    Element set:     909
    Inclination:       51.6395  deg
    RA of node:       288.8532  deg
    Eccentricity:     .0003230     
    Arg of perigee:   183.6633  deg
    Mean anomaly:     176.4497  deg
    Mean motion:   15.54047996  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             762
    Checksum:              349
 
 
    Coasting Arc #11 (Orbit 777)
    ---------------------------------------
 
    Vector Time (GMT): 2017/335/13:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933686.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3448105.26                 A    =         6778699.11  meter
     Y    =        2963146.11  meter          E    =           .0004137
     Z    =        5024424.96                 I    =           51.25829
     XDOT =      -3107.255279                 Wp   =           90.55319
     YDOT =       6763.953513  meter/sec      RA   =          283.13704  deg
     ZDOT =      -1855.330507                 TA   =           17.51798
                                              MA   =           17.50371
                                              Ha   =            221.156  n.mi
                                              Hp   =            214.865
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11312681.29                 X    =         3390307.53
     Y    =        9721607.98  feet           Y    =         3001381.75  meter
     Z    =       16484333.86                 Z    =         5041034.95
     XDOT =     -10194.407083                 XDOT =       -3173.648185
     YDOT =      22191.448533  feet/sec       YDOT =        6728.834934  meter/sec
     ZDOT =      -6087.042346                 ZDOT =       -1870.585846
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9530980.37                 X    =        -2905042.82
     Y    =       11367893.43  feet           Y    =         3464933.92  meter
     Z    =       16557508.70                 Z    =         5046728.65
     XDOT =     -21531.519571                 XDOT =       -6562.807165
     YDOT =      -9080.129567  feet/sec       YDOT =       -2767.623492  meter/sec
     ZDOT =      -6155.811263                 ZDOT =       -1876.291273
  
  
    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   17335.60402762  .00016717  00000-0  10270-3 0  9104
    2 25544  51.6401 283.7258 0003240 188.7762 171.3334 15.54063696  7781
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17335.60402762   =   yrday.fracday
    Element set:     910
    Inclination:       51.6401  deg
    RA of node:       283.7258  deg
    Eccentricity:     .0003240     
    Arg of perigee:   188.7762  deg
    Mean anomaly:     171.3334  deg
    Mean motion:   15.54063696  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             778
    Checksum:              309
 
 
    Coasting Arc #12 (Orbit 792)
    ---------------------------------------
 
    Vector Time (GMT): 2017/336/13:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933686.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2812109.35                 A    =         6781729.61  meter
     Y    =       -4476373.33  meter          E    =           .0009334
     Z    =       -4258134.89                 I    =           51.26287
     XDOT =       3689.595659                 Wp   =          130.01734
     YDOT =      -5696.109659  meter/sec      RA   =          278.11648  deg
     ZDOT =       3550.699754                 TA   =          176.44925
                                              MA   =          176.44262
                                              Ha   =            221.199  n.mi
                                              Hp   =            214.811
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9226080.53                 X    =        -2741159.93
     Y    =      -14686264.21  feet           Y    =        -4507423.22  meter
     Z    =      -13970258.84                 Z    =        -4271623.60
     XDOT =      12104.972634                 XDOT =        3735.768909
     YDOT =     -18688.023815  feet/sec       YDOT =       -5654.592193  meter/sec
     ZDOT =      11649.277409                 ZDOT =        3568.734777
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14366382.90                 X    =         4378873.51
     Y    =       -9631171.25  feet           Y    =        -2935581.00  meter
     Z    =      -14029349.00                 Z    =        -4276145.57
     XDOT =      18385.258517                 XDOT =        5603.826796
     YDOT =      10334.183613  feet/sec       YDOT =        3149.859165  meter/sec
     ZDOT =      11730.194277                 ZDOT =        3575.363216
  
  
    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   17336.56859349  .00016717  00000-0  10270-3 0  9118
    2 25544  51.6409 278.9169 0003206 191.7110 168.3969 15.54080785  7934
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17336.56859349   =   yrday.fracday
    Element set:     911
    Inclination:       51.6409  deg
    RA of node:       278.9169  deg
    Eccentricity:     .0003206     
    Arg of perigee:   191.7110  deg
    Mean anomaly:     168.3969  deg
    Mean motion:   15.54080785  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             793
    Checksum:              346
 
 
    Coasting Arc #13 (Orbit 808)
    ---------------------------------------
 
    Vector Time (GMT): 2017/337/13:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 933686.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2128173.98                 A    =         6785529.64  meter
     Y    =        5675773.64  meter          E    =           .0012979
     Z    =        3033454.93                 I    =           51.27199
     XDOT =      -4162.769734                 Wp   =          110.10102
     YDOT =       4186.593555  meter/sec      RA   =          273.10715  deg
     ZDOT =      -4900.183608                 TA   =           34.89331
                                              MA   =           34.80830
                                              Ha   =            221.066  n.mi
                                              Hp   =            214.955
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6982198.11                 X    =         2049812.46
     Y    =       18621304.59  feet           Y    =         5699133.87  meter
     Z    =        9952279.95                 Z    =         3043603.40
     XDOT =     -13657.381018                 XDOT =       -4185.472800
     YDOT =      13735.543159  feet/sec       YDOT =        4139.916190  meter/sec
     ZDOT =     -16076.717873                 ZDOT =       -4920.460163
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18242054.80                 X    =        -5560178.30
     Y    =        7864603.22  feet           Y    =         2397131.06  meter
     Z    =        9996369.55                 Z    =         3046893.44
     XDOT =     -13839.010640                 XDOT =       -4218.130443
     YDOT =     -11497.362621  feet/sec       YDOT =       -3504.396127  meter/sec
     ZDOT =     -16167.329394                 ZDOT =       -4927.801999
  
  
    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   17337.59745725  .00016717  00000-0  10270-3 0  9125
    2 25544  51.6409 273.7893 0003174 194.9195 165.1864 15.54080922  8093
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17337.59745725   =   yrday.fracday
    Element set:     912
    Inclination:       51.6409  deg
    RA of node:       273.7893  deg
    Eccentricity:     .0003174     
    Arg of perigee:   194.9195  deg
    Mean anomaly:     165.1864  deg
    Mean motion:   15.54080922  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             809
    Checksum:              342
 
 
    Coasting Arc #14 (Orbit 823)
    ---------------------------------------
 
    Vector Time (GMT): 2017/338/13:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919252.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4156363.73                 A    =         6778260.89  meter
     Y    =       -1636721.09  meter          E    =           .0013520
     Z    =       -5110084.26                 I    =           51.24739
     XDOT =       1010.475535                 Wp   =          115.28162
     YDOT =      -7430.254967  meter/sec      RA   =          268.15971  deg
     ZDOT =       1555.537044                 TA   =          169.82918
                                              MA   =          169.80180
                                              Ha   =            220.999  n.mi
                                              Hp   =            214.887
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13636363.94                 X    =        -4112929.93
     Y    =       -5369819.84  feet           Y    =        -1682956.92  meter
     Z    =      -16765368.31                 Z    =        -5130169.58
     XDOT =       3315.208449                 XDOT =        1085.931394
     YDOT =     -24377.476926  feet/sec       YDOT =       -7418.533425  meter/sec
     ZDOT =       5103.467991                 ZDOT =        1560.628081
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5330762.57                 X    =         1624816.43
     Y    =      -13541861.37  feet           Y    =        -4127559.34  meter
     Z    =      -16854195.99                 Z    =        -5137158.94
     XDOT =      23399.260703                 XDOT =        7132.094662
     YDOT =       2819.889586  feet/sec       YDOT =         859.502346  meter/sec
     ZDOT =       5127.245436                 ZDOT =        1562.784409
  
  
    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   17338.56201078  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6413 268.9813 0003172 200.1021 160.0007 15.54096346  8249
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17338.56201078   =   yrday.fracday
    Element set:     913
    Inclination:       51.6413  deg
    RA of node:       268.9813  deg
    Eccentricity:     .0003172     
    Arg of perigee:   200.1021  deg
    Mean anomaly:     160.0007  deg
    Mean motion:   15.54096346  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             824
    Checksum:              275
 
 
    Coasting Arc #15 (Orbit 828)
    ---------------------------------------
 
    Vector Time (GMT): 2017/338/19:53:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919252.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3217457.48                 A    =         6781478.41  meter
     Y    =       -4145281.48  meter          E    =           .0010159
     Z    =        4292661.23                 I    =           51.25492
     XDOT =       3143.262408                 Wp   =          128.09750
     YDOT =       6063.609663  meter/sec      RA   =          266.78868  deg
     ZDOT =       3487.660064                 TA   =          286.17766
                                              MA   =          286.28944
                                              Ha   =            220.928  n.mi
                                              Hp   =            215.062
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10555962.88                 X    =         3242720.11
     Y    =      -13600004.85  feet           Y    =        -4109160.94  meter
     Z    =       14083534.22                 Z    =         4308351.70
     XDOT =      10312.540709                 XDOT =        3058.282335
     YDOT =      19893.732490  feet/sec       YDOT =        6098.284197  meter/sec
     ZDOT =      11442.454279                 ZDOT =        3502.723576
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7580618.57                 X    =         2310572.54
     Y    =      -15392811.35  feet           Y    =        -4691728.90  meter
     Z    =       14153798.13                 Z    =         4314077.67
     XDOT =      12831.595048                 XDOT =        3911.070171
     YDOT =      16936.700765  feet/sec       YDOT =        5162.306393  meter/sec
     ZDOT =      11508.299430                 ZDOT =        3507.729666
  
  
    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   17338.88352558  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6376 267.3749 0003535 201.5803 158.5201 15.54113792  8292
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17338.88352558   =   yrday.fracday
    Element set:     914
    Inclination:       51.6376  deg
    RA of node:       267.3749  deg
    Eccentricity:     .0003535     
    Arg of perigee:   201.5803  deg
    Mean anomaly:     158.5201  deg
    Mean motion:   15.54113792  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             829
    Checksum:              324
 
 
    Coasting Arc #16 (Orbit 843)
    ---------------------------------------
 
    Vector Time (GMT): 2017/339/19:53:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919252.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3734399.16                 A    =         6778407.37  meter
     Y    =        2550067.76  meter          E    =           .0011731
     Z    =       -5059729.08                 I    =           51.24878
     XDOT =      -2440.992333                 Wp   =           90.84427
     YDOT =      -7045.681120  meter/sec      RA   =          261.76818  deg
     ZDOT =      -1753.073375                 TA   =          162.11086
                                              MA   =          162.06953
                                              Ha   =            220.950  n.mi
                                              Hp   =            214.888
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12251965.74                 X    =        -3738059.32
     Y    =        8366364.03  feet           Y    =         2508287.29  meter
     Z    =      -16600161.01                 Z    =        -5077878.33
     XDOT =      -8008.505030                 XDOT =       -2353.508597
     YDOT =     -23115.751707  feet/sec       YDOT =       -7072.488606  meter/sec
     ZDOT =      -5751.553069                 ZDOT =       -1764.719377
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10074011.90                 X    =        -3070558.83
     Y    =       10766984.83  feet           Y    =         3281776.98  meter
     Z    =      -16681078.48                 Z    =        -5084392.72
     XDOT =     -11942.073013                 XDOT =       -3639.943854
     YDOT =     -20143.804818  feet/sec       YDOT =       -6139.831709  meter/sec
     ZDOT =      -5802.100743                 ZDOT =       -1768.480307
  
  
    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   17339.84807112  .00016717  00000-0  10270-3 0  9157
    2 25544  51.6388 262.5672 0003409 200.1173 159.9846 15.54121992  8440
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17339.84807112   =   yrday.fracday
    Element set:     915
    Inclination:       51.6388  deg
    RA of node:       262.5672  deg
    Eccentricity:     .0003409     
    Arg of perigee:   200.1173  deg
    Mean anomaly:     159.9846  deg
    Mean motion:   15.54121992  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             844
    Checksum:              321
 
 
    Coasting Arc #17 (Orbit 853)
    ---------------------------------------
 
    Vector Time (GMT): 2017/340/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940422.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1567437.86                 A    =         6789356.48  meter
     Y    =        6591401.50  meter          E    =           .0013753
     Z    =         291619.30                 I    =           51.28970
     XDOT =      -4610.729970                 Wp   =          144.31187
     YDOT =       1366.680714  meter/sec      RA   =          258.60035  deg
     ZDOT =      -5976.567494                 TA   =           32.52904
                                              MA   =           32.44437
                                              Ha   =            220.808  n.mi
                                              Hp   =            215.154
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5142512.67                 X    =         1492198.00
     Y    =       21625333.02  feet           Y    =         6608508.94  meter
     Z    =         956756.22                 Z    =          299051.42
     XDOT =     -15127.066832                 XDOT =       -4596.638571
     YDOT =       4483.860609  feet/sec       YDOT =        1315.199824  meter/sec
     ZDOT =     -19608.161068                 ZDOT =       -5998.930680
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21245995.86                 X    =        -6475779.54
     Y    =       -6530389.82  feet           Y    =        -1990462.82  meter
     Z    =         988694.03                 Z    =          301353.94
     XDOT =       3259.540858                 XDOT =         993.508054
     YDOT =     -13651.647989  feet/sec       YDOT =       -4161.022307  meter/sec
     ZDOT =     -19707.588993                 ZDOT =       -6006.873125
  
  
    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   17340.49109733  .00016717  00000-0  10270-3 0  9165
    2 25544  51.6400 259.3650 0003101 207.3099 152.7891 15.54106898  8540
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17340.49109733   =   yrday.fracday
    Element set:     916
    Inclination:       51.6400  deg
    RA of node:       259.3650  deg
    Eccentricity:     .0003101     
    Arg of perigee:   207.3099  deg
    Mean anomaly:     152.7891  deg
    Mean motion:   15.54106898  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             854
    Checksum:              309
 
 
    Coasting Arc #18 (Orbit 868)
    ---------------------------------------
 
    Vector Time (GMT): 2017/341/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940422.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -775832.37                 A    =         6788524.19  meter
     Y    =       -6593796.84  meter          E    =           .0011175
     Z    =        1393540.88                 I    =           51.29359
     XDOT =       5008.220572                 Wp   =           68.26764
     YDOT =        637.467302  meter/sec      RA   =          253.60650  deg
     ZDOT =       5771.248669                 TA   =          306.99439
                                              MA   =          307.09662
                                              Ha   =            220.714  n.mi
                                              Hp   =            215.231
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2545381.81                 X    =         -708810.24
     Y    =      -21633191.72  feet           Y    =        -6602098.10  meter
     Z    =        4571984.50                 Z    =         1389934.32
     XDOT =      16431.169857                 XDOT =        4972.686147
     YDOT =       2091.428156  feet/sec       YDOT =         693.273445  meter/sec
     ZDOT =      18934.542878                 ZDOT =        5795.490788
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20102184.56                 X    =         6127145.85
     Y    =        8397196.75  feet           Y    =         2559465.57  meter
     Z    =        4557000.93                 Z    =         1388973.88
     XDOT =      -9229.943520                 XDOT =       -2813.286785
     YDOT =      11702.496719  feet/sec       YDOT =        3566.921000  meter/sec
     ZDOT =      19042.004027                 ZDOT =        5804.002827
  
  
    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   17341.51993356  .00016717  00000-0  10270-3 0  9172
    2 25544  51.6390 254.2370 0003141 212.1356 147.9605 15.54124788  8698
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17341.51993356   =   yrday.fracday
    Element set:     917
    Inclination:       51.6390  deg
    RA of node:       254.2370  deg
    Eccentricity:     .0003141     
    Arg of perigee:   212.1356  deg
    Mean anomaly:     147.9605  deg
    Mean motion:   15.54124788  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             869
    Checksum:              314
 
             

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