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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15846.6289
   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 
   ------------------------------------------------------------------------
   348/03:56:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.4  
   000/00:00:00.000           0.0               0.0              213.6  
   
   354/01:40:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.1  
   000/00:00:00.000           0.0               0.0              214.1  
   
   358/04:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.8  
   000/00:00:00.000           0.0               0.0              214.6  
   
   361/02:52:50.495          -1.8               2.2              2.2    
   N/A                        1.0              -0.0              221.4  
   000/00:05:40.991           0.7              -0.0              216.2  
   
   361/09:04:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.4  
   000/00:00:00.000           0.0               0.0              216.2  
   
 
 
    Coasting Arc #1 (Orbit 2625)
    ---------------------------------------
 
    Vector Time (GMT): 2018/346/14:51:13.974
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3956599.57                 A    =         6778987.94  meter
     Y    =       -2362622.92  meter          E    =           .0008313
     Z    =        4964352.13                 I    =           51.43409
     XDOT =       5539.948359                 Wp   =           93.83935
     YDOT =       4882.321895  meter/sec      RA   =          208.35198  deg
     ZDOT =      -2089.289943                 TA   =           16.55101
                                              MA   =           16.52389
                                              Ha   =            222.525  n.mi
                                              Hp   =            213.488
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12980969.71                 X    =         3958610.87
     Y    =       -7751387.53  feet           Y    =        -2318366.71  meter
     Z    =       16287244.53                 Z    =         4983576.53
     XDOT =      18175.683594                 XDOT =        5495.089772
     YDOT =      16018.116452  feet/sec       YDOT =        4944.022829  meter/sec
     ZDOT =      -6854.625797                 ZDOT =       -2062.487342
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13531326.90                 X    =         4124348.44
     Y    =        6531358.21  feet           Y    =         1990757.98  meter
     Z    =       16374018.13                 Z    =         4990800.73
     XDOT =      -2956.940289                 XDOT =        -901.275400
     YDOT =      23029.550156  feet/sec       YDOT =        7019.406888  meter/sec
     ZDOT =      -6734.480890                 ZDOT =       -2052.669775
  
  
    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   18346.66360442  .00016717  00000-0  10270-3 0  9000
    2 25544  51.6355 209.2941 0005017 139.5923 220.5603 15.54043037 26265
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18346.66360442   =   yrday.fracday
    Element set:     900
    Inclination:       51.6355  deg
    RA of node:       209.2941  deg
    Eccentricity:     .0005017     
    Arg of perigee:   139.5923  deg
    Mean anomaly:     220.5603  deg
    Mean motion:   15.54043037  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2626
    Checksum:              289
 
 
    Coasting Arc #2 (Orbit 2640)
    ---------------------------------------
 
    Vector Time (GMT): 2018/347/14:51:13.974
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5207125.09                 A    =         6782112.97  meter
     Y    =        1347022.69  meter          E    =           .0012439
     Z    =       -4145169.65                 I    =           51.47424
     XDOT =      -4302.585707                 Wp   =          123.31917
     YDOT =      -5106.365688  meter/sec      RA   =          203.34637  deg
     ZDOT =       3746.963558                 TA   =          185.39455
                                              MA   =          185.40797
                                              Ha   =            222.604  n.mi
                                              Hp   =            213.353
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17083743.75                 X    =        -5201665.88
     Y    =        4419365.78  feet           Y    =         1288823.86  meter
     Z    =      -13599637.94                 Z    =        -4170450.62
     XDOT =     -14116.094840                 XDOT =       -4263.365845
     YDOT =     -16753.168268  feet/sec       YDOT =       -5154.261209  meter/sec
     ZDOT =      12293.187525                 ZDOT =        3726.157978
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13199158.59                 X    =        -4023103.54
     Y    =      -11578217.12  feet           Y    =        -3529040.58  meter
     Z    =      -13713582.58                 Z    =        -4179899.97
     XDOT =       5042.670135                 XDOT =        1537.005857
     YDOT =     -20193.066740  feet/sec       YDOT =       -6154.846742  meter/sec
     ZDOT =      12200.038775                 ZDOT =        3718.571819
  
  
    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   18347.62817295  .00016717  00000-0  10270-3 0  9011
    2 25544  51.6351 204.4853 0005177 143.0885 217.0625 15.54069006 26410
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18347.62817295   =   yrday.fracday
    Element set:     901
    Inclination:       51.6351  deg
    RA of node:       204.4853  deg
    Eccentricity:     .0005177     
    Arg of perigee:   143.0885  deg
    Mean anomaly:     217.0625  deg
    Mean motion:   15.54069006  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2641
    Checksum:              305
 
 
    Coasting Arc #3 (Orbit 2649)
    ---------------------------------------
 
    Vector Time (GMT): 2018/348/03:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4438073.59                 A    =         6780379.00  meter
     Y    =       -2241507.11  meter          E    =           .0010444
     Z    =        4600768.37                 I    =           51.48578
     XDOT =       5400.530765                 Wp   =           92.87330
     YDOT =       4566.736337  meter/sec      RA   =          200.63062  deg
     ZDOT =      -2979.293677                 TA   =           26.89899
                                              MA   =           26.84488
                                              Ha   =            222.390  n.mi
                                              Hp   =            213.551
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14560608.89                 X    =         4440460.84
     Y    =       -7354025.94  feet           Y    =        -2191864.48  meter
     Z    =       15094384.41                 Z    =         4622332.58
     XDOT =      17718.276787                 XDOT =        5363.534669
     YDOT =      14982.730763  feet/sec       YDOT =        4626.922190  meter/sec
     ZDOT =      -9774.585555                 ZDOT =       -2953.149340
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15858450.95                 X    =        -4833655.85
     Y    =       -3414014.70  feet           Y    =        -1040591.68  meter
     Z    =       15191692.01                 Z    =         4630427.73
     XDOT =      -4599.406397                 XDOT =       -1401.899070
     YDOT =     -21685.901237  feet/sec       YDOT =       -6609.862697  meter/sec
     ZDOT =      -9657.337072                 ZDOT =       -2943.556340
  
  
    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   18348.20691317  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6357 201.6036 0004920 143.6572 216.4916 15.54072253 26506
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18348.20691317   =   yrday.fracday
    Element set:     902
    Inclination:       51.6357  deg
    RA of node:       201.6036  deg
    Eccentricity:     .0004920     
    Arg of perigee:   143.6572  deg
    Mean anomaly:     216.4916  deg
    Mean motion:   15.54072253  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2650
    Checksum:              292
 
 
    Coasting Arc #4 (Orbit 2664)
    ---------------------------------------
 
    Vector Time (GMT): 2018/349/03:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5625484.36                 A    =         6784094.70  meter
     Y    =        1356719.34  meter          E    =           .0009291
     Z    =       -3552297.87                 I    =           51.53042
     XDOT =      -3971.004577                 Wp   =          120.67203
     YDOT =      -4792.914255  meter/sec      RA   =          195.63404  deg
     ZDOT =       4462.082455                 TA   =          197.39986
                                              MA   =          197.43172
                                              Ha   =            222.489  n.mi
                                              Hp   =            213.542
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18456313.53                 X    =        -5622982.30
     Y    =        4451178.95  feet           Y    =         1293825.48  meter
     Z    =      -11654520.57                 Z    =        -3579618.35
     XDOT =     -13028.230241                 XDOT =       -3938.788170
     YDOT =     -15724.784301  feet/sec       YDOT =       -4837.140935  meter/sec
     ZDOT =      14639.378133                 ZDOT =        4442.870645
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17206038.93                 X    =         5244400.67
     Y    =        7843155.87  feet           Y    =         2390593.91  meter
     Z    =      -11777668.83                 Z    =        -3589833.46
     XDOT =       1192.560007                 XDOT =         363.492290
     YDOT =      19217.978939  feet/sec       YDOT =        5857.639981  meter/sec
     ZDOT =      14553.346785                 ZDOT =        4435.860100
  
  
    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   18349.17147849  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6367 196.7957 0004871 145.5805 214.5664 15.54052381 26653
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18349.17147849   =   yrday.fracday
    Element set:     903
    Inclination:       51.6367  deg
    RA of node:       196.7957  deg
    Eccentricity:     .0004871     
    Arg of perigee:   145.5805  deg
    Mean anomaly:     214.5664  deg
    Mean motion:   15.54052381  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2665
    Checksum:              343
 
 
    Coasting Arc #5 (Orbit 2680)
    ---------------------------------------
 
    Vector Time (GMT): 2018/350/03:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6423096.30                 A    =         6787525.41  meter
     Y    =        -493015.89  meter          E    =           .0017841
     Z    =        2106981.53                 I    =           51.57410
     XDOT =       2191.428701                 Wp   =          119.97103
     YDOT =       4864.737157  meter/sec      RA   =          190.64958  deg
     ZDOT =      -5515.971154                 TA   =           36.65014
                                              MA   =           36.52823
                                              Ha   =            222.307  n.mi
                                              Hp   =            213.687
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21073150.59                 X    =         6417897.34
     Y    =       -1617506.21  feet           Y    =         -421217.55  meter
     Z    =        6912669.06                 Z    =         2138170.12
     XDOT =       7189.726710                 XDOT =        2163.660714
     YDOT =      15960.423743  feet/sec       YDOT =        4889.088284  meter/sec
     ZDOT =     -18097.018222                 ZDOT =       -5505.393101
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17739498.40                 X    =        -5406999.11
     Y    =      -11403598.08  feet           Y    =        -3475816.69  meter
     Z    =        7053165.46                 Z    =         2149804.83
     XDOT =       2974.078476                 XDOT =         906.499119
     YDOT =     -15842.606274  feet/sec       YDOT =       -4828.826392  meter/sec
     ZDOT =     -18049.859127                 ZDOT =       -5501.597062
  
  
    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   18350.20034679  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6365 191.6668 0004780 149.4773 210.6659 15.54076199 26812
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18350.20034679   =   yrday.fracday
    Element set:     904
    Inclination:       51.6365  deg
    RA of node:       191.6668  deg
    Eccentricity:     .0004780     
    Arg of perigee:   149.4773  deg
    Mean anomaly:     210.6659  deg
    Mean motion:   15.54076199  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2681
    Checksum:              335
 
 
    Coasting Arc #6 (Orbit 2695)
    ---------------------------------------
 
    Vector Time (GMT): 2018/351/03:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6764029.14                 A    =         6789323.66  meter
     Y    =        -287785.74  meter          E    =           .0010149
     Z    =        -482859.02                 I    =           51.61289
     XDOT =       -216.069756                 Wp   =           68.16842
     YDOT =      -4785.016224  meter/sec      RA   =          185.67536  deg
     ZDOT =       5983.399368                 TA   =          286.62422
                                              MA   =          286.73564
                                              Ha   =            222.299  n.mi
                                              Hp   =            213.795
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22191696.67                 X    =        -6757962.84
     Y    =        -944178.94  feet           Y    =         -363391.87  meter
     Z    =       -1584183.12                 Z    =         -515701.78
     XDOT =       -708.890274                 XDOT =        -191.610653
     YDOT =     -15698.872127  feet/sec       YDOT =       -4787.296052  meter/sec
     ZDOT =      19630.575354                 ZDOT =        5982.408902
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17354173.31                 X    =         5289552.03
     Y    =       13845761.54  feet           Y    =         4220188.12  meter
     Z    =       -1732070.20                 Z    =         -527935.00
     XDOT =      -7571.307211                 XDOT =       -2307.734438
     YDOT =      11905.736588  feet/sec       YDOT =        3628.868512  meter/sec
     ZDOT =      19626.580968                 ZDOT =        5982.181879
  
  
    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   18351.16490984  .00016717  00000-0  10270-3 0  9051
    2 25544  51.6363 186.8593 0004877 153.9098 206.2301 15.54087695 26964
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18351.16490984   =   yrday.fracday
    Element set:     905
    Inclination:       51.6363  deg
    RA of node:       186.8593  deg
    Eccentricity:     .0004877     
    Arg of perigee:   153.9098  deg
    Mean anomaly:     206.2301  deg
    Mean motion:   15.54087695  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2696
    Checksum:              349
 
 
    Coasting Arc #7 (Orbit 2711)
    ---------------------------------------
 
    Vector Time (GMT): 2018/352/03:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6584248.93                 A    =         6788857.27  meter
     Y    =        1058733.96  meter          E    =           .0013762
     Z    =       -1235551.21                 I    =           51.64575
     XDOT =      -1831.241535                 Wp   =          147.79834
     YDOT =       4608.041119  meter/sec      RA   =          180.70465  deg
     ZDOT =      -5851.468373                 TA   =           45.63457
                                              MA   =           45.52191
                                              Ha   =            222.241  n.mi
                                              Hp   =            213.943
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21601866.57                 X    =         6577922.22
     Y    =        3473536.60  feet           Y    =         1132328.32  meter
     Z    =       -4053645.71                 Z    =        -1203582.26
     XDOT =      -6008.010287                 XDOT =       -1854.210273
     YDOT =      15118.245142  feet/sec       YDOT =        4587.434881  meter/sec
     ZDOT =     -19197.730881                 ZDOT =       -5860.419449
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15681968.53                 X    =        -4779864.01
     Y    =      -15294700.00  feet           Y    =        -4661824.56  meter
     Z    =       -3909751.19                 Z    =        -1191692.16
     XDOT =      12397.039547                 XDOT =        3778.617654
     YDOT =      -7829.024503  feet/sec       YDOT =       -2386.286669  meter/sec
     ZDOT =     -19238.498873                 ZDOT =       -5863.894456
  
  
    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   18352.19377451  .00016717  00000-0  10270-3 0  9069
    2 25544  51.6377 181.7301 0004676 157.8540 202.2816 15.54083425 27125
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18352.19377451   =   yrday.fracday
    Element set:     906
    Inclination:       51.6377  deg
    RA of node:       181.7301  deg
    Eccentricity:     .0004676     
    Arg of perigee:   157.8540  deg
    Mean anomaly:     202.2816  deg
    Mean motion:   15.54083425  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2712
    Checksum:              308
 
 
    Coasting Arc #8 (Orbit 2727)
    ---------------------------------------
 
    Vector Time (GMT): 2018/353/03:56:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 966149.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5925402.58                 A    =         6786214.45  meter
     Y    =       -1767035.57  meter          E    =           .0014875
     Z    =        2786527.54                 I    =           51.66947
     XDOT =       3712.992128                 Wp   =           97.91375
     YDOT =      -4336.434988  meter/sec      RA   =          175.73235  deg
     ZDOT =       5120.181140                 TA   =          293.67110
                                              MA   =          293.82714
                                              Ha   =            222.166  n.mi
                                              Hp   =            214.035
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19440297.16                 X    =        -5918738.31
     Y    =       -5797360.78  feet           Y    =        -1833260.52  meter
     Z    =        9142150.72                 Z    =         2757759.74
     XDOT =      12181.732703                 XDOT =        3736.336028
     YDOT =     -14227.148910  feet/sec       YDOT =       -4294.783658  meter/sec
     ZDOT =      16798.494554                 ZDOT =        5138.274056
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12877402.36                 X    =         3925032.24
     Y    =       15749816.28  feet           Y    =         4800544.00  meter
     Z    =        9012727.74                 Z    =         2747079.42
     XDOT =     -16827.858277                 XDOT =       -5129.131203
     YDOT =       4050.725980  feet/sec       YDOT =        1234.661279  meter/sec
     ZDOT =      16880.426967                 ZDOT =        5145.154139
  
  
    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   18353.22263660  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6370 176.6019 0004727 161.4172 198.7154 15.54100796 27288
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18353.22263660   =   yrday.fracday
    Element set:     907
    Inclination:       51.6370  deg
    RA of node:       176.6019  deg
    Eccentricity:     .0004727     
    Arg of perigee:   161.4172  deg
    Mean anomaly:     198.7154  deg
    Mean motion:   15.54100796  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2728
    Checksum:              313
 
 
    Coasting Arc #9 (Orbit 2741)
    ---------------------------------------
 
    Vector Time (GMT): 2018/354/01:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3589711.22                 A    =         6779934.24  meter
     Y    =       -3242259.78  meter          E    =           .0011467
     Z    =        4747330.40                 I    =           51.67675
     XDOT =       6445.256166                 Wp   =          135.57033
     YDOT =      -3158.699612  meter/sec      RA   =          171.21735  deg
     ZDOT =       2704.362220                 TA   =          287.66075
                                              MA   =          287.78593
                                              Ha   =            222.113  n.mi
                                              Hp   =            214.123
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11777267.78                 X    =        -3576248.81
     Y    =      -10637335.24  feet           Y    =        -3282327.68  meter
     Z    =       15575230.97                 Z    =         4729925.00
     XDOT =      21145.853564                 XDOT =        6466.962115
     YDOT =     -10363.187703  feet/sec       YDOT =       -3086.503209  meter/sec
     ZDOT =       8872.579461                 ZDOT =        2735.723715
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5189801.32                 X    =        -1581851.44
     Y    =       15078117.93  feet           Y    =         4595810.34  meter
     Z    =       15497131.32                 Z    =         4723525.63
     XDOT =     -16636.061714                 XDOT =       -5070.671610
     YDOT =     -15031.263785  feet/sec       YDOT =       -4581.529202  meter/sec
     ZDOT =       9014.191481                 ZDOT =        2747.525563
  
  
    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   18354.12289046  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6353 172.1145 0004697 165.9155 194.2129 15.54102937 27424
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18354.12289046   =   yrday.fracday
    Element set:     908
    Inclination:       51.6353  deg
    RA of node:       172.1145  deg
    Eccentricity:     .0004697     
    Arg of perigee:   165.9155  deg
    Mean anomaly:     194.2129  deg
    Mean motion:   15.54102937  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2742
    Checksum:              316
 
 
    Coasting Arc #10 (Orbit 2756)
    ---------------------------------------
 
    Vector Time (GMT): 2018/355/01:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1929409.89                 A    =         6777775.65  meter
     Y    =        3814144.61  meter          E    =           .0015579
     Z    =       -5272883.97                 I    =           51.70258
     XDOT =      -7199.663363                 Wp   =          100.85930
     YDOT =       2462.889703  meter/sec      RA   =          166.22305  deg
     ZDOT =       -857.924604                 TA   =          160.96236
                                              MA   =          160.90407
                                              Ha   =            222.013  n.mi
                                              Hp   =            214.266
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6330084.93                 X    =         1912228.73
     Y    =       12513597.80  feet           Y    =         3835625.25  meter
     Z    =      -17299488.08                 Z    =        -5263552.71
     XDOT =     -23620.942792                 XDOT =       -7222.501615
     YDOT =       8080.346795  feet/sec       YDOT =        2382.250480  meter/sec
     ZDOT =      -2814.713269                 ZDOT =        -892.953483
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8841835.76                 X    =         2694991.54
     Y    =      -10950889.29  feet           Y    =        -3337831.05  meter
     Z    =      -17257820.18                 Z    =        -5260183.59
     XDOT =      16127.865399                 XDOT =        4915.773374
     YDOT =      17680.700247  feet/sec       YDOT =        5389.077435  meter/sec
     ZDOT =      -2972.808151                 ZDOT =        -906.111924
  
  
    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   18355.08744753  .00016717  00000-0  10270-3 0  9096
    2 25544  51.6358 167.3053 0004668 167.9105 192.2161 15.54078082 27571
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18355.08744753   =   yrday.fracday
    Element set:     909
    Inclination:       51.6358  deg
    RA of node:       167.3053  deg
    Eccentricity:     .0004668     
    Arg of perigee:   167.9105  deg
    Mean anomaly:     192.2161  deg
    Mean motion:   15.54078082  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2757
    Checksum:              331
 
 
    Coasting Arc #11 (Orbit 2772)
    ---------------------------------------
 
    Vector Time (GMT): 2018/356/01:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -197986.55                 A    =         6777818.49  meter
     Y    =       -4294725.38  meter          E    =           .0004530
     Z    =        5236138.74                 I    =           51.73530
     XDOT =       7419.665430                 Wp   =          124.85698
     YDOT =      -1635.941181  meter/sec      RA   =          161.22948  deg
     ZDOT =      -1063.142291                 TA   =          335.29782
                                              MA   =          335.31951
                                              Ha   =            221.928  n.mi
                                              Hp   =            214.323
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -649562.16                 X    =         -175381.48
     Y    =      -14090306.38  feet           Y    =        -4296813.80  meter
     Z    =       17178932.87                 Z    =         5235231.25
     XDOT =      24342.734352                 XDOT =        7442.571738
     YDOT =      -5367.261094  feet/sec       YDOT =       -1552.841090  meter/sec
     ZDOT =      -3487.999644                 ZDOT =       -1027.044621
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12467552.13                 X    =        -3800109.89
     Y    =        6606393.38  feet           Y    =         2013628.70  meter
     Z    =       17175276.11                 Z    =         5235024.16
     XDOT =     -14615.773397                 XDOT =       -4454.887731
     YDOT =     -18954.152126  feet/sec       YDOT =       -5777.225568  meter/sec
     ZDOT =      -3325.140678                 ZDOT =       -1013.502879
  
  
    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   18356.11630530  .00016717  00000-0  10270-3 0  9100
    2 25544  51.6362 162.1766 0004550 171.7375 188.3854 15.54082365 27734
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18356.11630530   =   yrday.fracday
    Element set:     910
    Inclination:       51.6362  deg
    RA of node:       162.1766  deg
    Eccentricity:     .0004550     
    Arg of perigee:   171.7375  deg
    Mean anomaly:     188.3854  deg
    Mean motion:   15.54082365  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2773
    Checksum:              308
 
 
    Coasting Arc #12 (Orbit 2787)
    ---------------------------------------
 
    Vector Time (GMT): 2018/357/01:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1490702.58                 A    =         6780178.15  meter
     Y    =        4685136.53  meter          E    =           .0013137
     Z    =       -4681596.42                 I    =           51.77409
     XDOT =      -7066.904960                 Wp   =          128.03686
     YDOT =        632.021328  meter/sec      RA   =          156.24118  deg
     ZDOT =       2880.336215                 TA   =          170.58358
                                              MA   =          170.55892
                                              Ha   =            221.792  n.mi
                                              Hp   =            214.434
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4890756.49                 X    =        -1520241.64
     Y    =       15371182.83  feet           Y    =         4668302.02  meter
     Z    =      -15359568.32                 Z    =        -4688908.74
     XDOT =     -23185.383728                 XDOT =       -7087.438284
     YDOT =       2073.560787  feet/sec       YDOT =         552.879030  meter/sec
     ZDOT =       9449.921965                 ZDOT =        2845.957965
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15921903.41                 X    =         4852996.16
     Y    =       -2378528.38  feet           Y    =         -724975.45  meter
     Z    =      -15393007.97                 Z    =        -4691788.83
     XDOT =      11812.144012                 XDOT =        3600.341495
     YDOT =      18866.773967  feet/sec       YDOT =        5750.592705  meter/sec
     ZDOT =       9294.884602                 ZDOT =        2833.080827
  
  
    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   18357.08085791  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6360 157.3685 0004471 175.9601 184.1588 15.54074441 27888
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18357.08085791   =   yrday.fracday
    Element set:     911
    Inclination:       51.6360  deg
    RA of node:       157.3685  deg
    Eccentricity:     .0004471     
    Arg of perigee:   175.9601  deg
    Mean anomaly:     184.1588  deg
    Mean motion:   15.54074441  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2788
    Checksum:              333
 
 
    Coasting Arc #13 (Orbit 2803)
    ---------------------------------------
 
    Vector Time (GMT): 2018/358/01:40:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2981232.56                 A    =         6783760.01  meter
     Y    =       -4887016.08  meter          E    =           .0012353
     Z    =        3626332.18                 I    =           51.81766
     XDOT =       6253.284746                 Wp   =          107.09235
     YDOT =        531.584339  meter/sec      RA   =          151.26378  deg
     ZDOT =      -4415.632422                 TA   =           30.00222
                                              MA   =           29.93150
                                              Ha   =            221.615  n.mi
                                              Hp   =            214.538
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9780946.70                 X    =         3018044.33
     Y    =      -16033517.33  feet           Y    =        -4853472.57  meter
     Z    =       11897415.30                 Z    =         3640902.54
     XDOT =      20516.026071                 XDOT =        6268.324277
     YDOT =       1744.043108  feet/sec       YDOT =         601.597658  meter/sec
     ZDOT =     -14486.983012                 ZDOT =       -4385.219804
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18684243.13                 X    =        -5694957.31
     Y    =       -1435344.96  feet           Y    =         -437493.14  meter
     Z    =       11963608.61                 Z    =         3646507.90
     XDOT =      -7837.576726                 XDOT =       -2388.893386
     YDOT =     -17823.552551  feet/sec       YDOT =       -5432.618818  meter/sec
     ZDOT =     -14349.915837                 ZDOT =       -4373.854347
  
  
    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   18358.10971308  .00016717  00000-0  10270-3 0  9124
    2 25544  51.6373 152.2398 0004432 180.2127 179.9024 15.54102147 28047
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18358.10971308   =   yrday.fracday
    Element set:     912
    Inclination:       51.6373  deg
    RA of node:       152.2398  deg
    Eccentricity:     .0004432     
    Arg of perigee:   180.2127  deg
    Mean anomaly:     179.9024  deg
    Mean motion:   15.54102147  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2804
    Checksum:              295
 
 
    Coasting Arc #14 (Orbit 2805)
    ---------------------------------------
 
    Vector Time (GMT): 2018/358/04:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4973630.07                 A    =         6781188.02  meter
     Y    =       -1218922.43  meter          E    =           .0011675
     Z    =        4442291.56                 I    =           51.81372
     XDOT =       4305.111656                 Wp   =          131.54366
     YDOT =      -5407.278215  meter/sec      RA   =          150.74556  deg
     ZDOT =       3323.138334                 TA   =          284.93654
                                              MA   =          285.06578
                                              Ha   =            221.787  n.mi
                                              Hp   =            214.582
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16317683.97                 X    =        -4981208.18
     Y    =       -3999089.35  feet           Y    =        -1274584.04  meter
     Z    =       14574447.38                 Z    =         4418113.04
     XDOT =      14124.382072                 XDOT =        4349.115502
     YDOT =     -17740.414091  feet/sec       YDOT =       -5358.889907  meter/sec
     ZDOT =      10902.684822                 ZDOT =        3344.156958
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13725566.04                 X    =         4183552.53
     Y    =        9850409.27  feet           Y    =         3002404.75  meter
     Z    =       14465556.20                 Z    =         4409101.53
     XDOT =     -18950.763428                 XDOT =       -5776.192693
     YDOT =      10191.106940  feet/sec       YDOT =        3106.249395  meter/sec
     ZDOT =      10998.006769                 ZDOT =        3352.192463
  
  
    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   18358.23832037  .00016717  00000-0  10270-3 0  9134
    2 25544  51.6390 151.5996 0004497 180.2116 179.9035 15.54092545 28065
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18358.23832037   =   yrday.fracday
    Element set:     913
    Inclination:       51.6390  deg
    RA of node:       151.5996  deg
    Eccentricity:     .0004497     
    Arg of perigee:   180.2116  deg
    Mean anomaly:     179.9035  deg
    Mean motion:   15.54092545  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2806
    Checksum:              323
 
 
    Coasting Arc #15 (Orbit 2820)
    ---------------------------------------
 
    Vector Time (GMT): 2018/359/04:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3722328.78                 A    =         6778210.78  meter
     Y    =        2368958.19  meter          E    =           .0013093
     Z    =       -5156356.46                 I    =           51.83409
     XDOT =      -5432.691717                 Wp   =           97.14611
     YDOT =       5171.491883  meter/sec      RA   =          145.76360  deg
     ZDOT =      -1550.860387                 TA   =          157.95804
                                              MA   =          157.90169
                                              Ha   =            221.557  n.mi
                                              Hp   =            214.736
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12212364.78                 X    =         3720608.27
     Y    =        7772172.54  feet           Y    =         2410574.89  meter
     Z    =      -16917179.98                 Z    =        -5138278.82
     XDOT =     -17823.791723                 XDOT =       -5482.583871
     YDOT =      16966.836888  feet/sec       YDOT =        5110.460977  meter/sec
     ZDOT =      -5088.124628                 ZDOT =       -1577.370670
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8723229.88                 X    =        -2658840.47
     Y    =      -11670355.09  feet           Y    =        -3557124.23  meter
     Z    =      -16835901.24                 Z    =        -5131582.70
     XDOT =      21835.692893                 XDOT =        6655.519194
     YDOT =      -8831.625140  feet/sec       YDOT =       -2691.879343  meter/sec
     ZDOT =      -5208.204988                 ZDOT =       -1587.460880
  
  
    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   18359.20286868  .00016717  00000-0  10270-3 0  9148
    2 25544  51.6406 146.7915 0004367 183.6239 176.4883 15.54120201 28210
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18359.20286868   =   yrday.fracday
    Element set:     914
    Inclination:       51.6406  deg
    RA of node:       146.7915  deg
    Eccentricity:     .0004367     
    Arg of perigee:   183.6239  deg
    Mean anomaly:     176.4883  deg
    Mean motion:   15.54120201  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2821
    Checksum:              322
 
 
    Coasting Arc #16 (Orbit 2836)
    ---------------------------------------
 
    Vector Time (GMT): 2018/360/04:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950917.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2326146.65                 A    =         6777351.24  meter
     Y    =       -3493593.84  meter          E    =           .0004106
     Z    =        5319594.81                 I    =           51.85806
     XDOT =       6112.590861                 Wp   =          154.53403
     YDOT =      -4619.567162  meter/sec      RA   =          140.77922  deg
     ZDOT =       -364.461397                 TA   =          298.90895
                                              MA   =          298.95013
                                              Ha   =            221.482  n.mi
                                              Hp   =            214.745
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7631714.74                 X    =        -2312746.78
     Y    =      -11461922.06  feet           Y    =        -3519532.04  meter
     Z    =       17452738.87                 Z    =         5308327.58
     XDOT =      20054.431959                 XDOT =        6165.564191
     YDOT =     -15156.060243  feet/sec       YDOT =       -4550.915692  meter/sec
     ZDOT =      -1195.739491                 ZDOT =        -334.640832
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3359590.53                 X    =         1024003.20
     Y    =       13419783.33  feet           Y    =         4090349.96  meter
     Z    =       17402281.11                 Z    =         5304215.28
     XDOT =     -23057.959716                 XDOT =       -7028.066121
     YDOT =       7133.052281  feet/sec       YDOT =        2174.154335  meter/sec
     ZDOT =      -1060.766947                 ZDOT =        -323.321765
  
  
    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   18360.23171854  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6403 141.6635 0004394 189.1246 170.9828 15.54138221 28375
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18360.23171854   =   yrday.fracday
    Element set:     915
    Inclination:       51.6403  deg
    RA of node:       141.6635  deg
    Eccentricity:     .0004394     
    Arg of perigee:   189.1246  deg
    Mean anomaly:     170.9828  deg
    Mean motion:   15.54138221  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2837
    Checksum:              311
 
 
    Coasting Arc #17 (Orbit 2850)
    ---------------------------------------
 
    Vector Time (GMT): 2018/361/02:55:40.991
    Vector Time (MET): N/A
    Weight (LBS)     : 950680.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -395458.29                 A    =         6782404.11  meter
     Y    =        5160984.56  meter          E    =           .0008931
     Z    =       -4391866.94                 I    =           51.89389
     XDOT =      -6403.424809                 Wp   =          139.03923
     YDOT =       2429.837267  meter/sec      RA   =          136.09820  deg
     ZDOT =       3429.321335                 TA   =          165.65325
                                              MA   =          165.62787
                                              Ha   =            221.376  n.mi
                                              Hp   =            216.179
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1297435.35                 X    =         -431807.45
     Y    =       16932364.05  feet           Y    =         5156359.36  meter
     Z    =      -14409012.27                 Z    =        -4393875.81
     XDOT =     -21008.611578                 XDOT =       -6446.777586
     YDOT =       7971.907045  feet/sec       YDOT =        2357.987059  meter/sec
     ZDOT =      11251.054249                 ZDOT =        3398.111099
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12100149.78                 X    =         3688125.65
     Y    =      -11903699.55  feet           Y    =        -3628247.62  meter
     Z    =      -14418607.34                 Z    =        -4394791.52
     XDOT =      20217.710799                 XDOT =        6162.358252
     YDOT =       7083.706350  feet/sec       YDOT =        2159.113696  meter/sec
     ZDOT =      11110.022219                 ZDOT =        3386.334772
  
  
    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   18361.13196358  .00016717  00000-0  10270-3 0  9169
    2 25544  51.6398 137.1754 0004348 214.8936 145.1932 15.53700139 28519
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18361.13196358   =   yrday.fracday
    Element set:     916
    Inclination:       51.6398  deg
    RA of node:       137.1754  deg
    Eccentricity:     .0004348     
    Arg of perigee:   214.8936  deg
    Mean anomaly:     145.1932  deg
    Mean motion:   15.53700139  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2851
    Checksum:              322
 
 
    Coasting Arc #18 (Orbit 2854)
    ---------------------------------------
 
    Vector Time (GMT): 2018/361/09:04:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 950680.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         545187.69                 A    =         6780907.34  meter
     Y    =        4779634.12  meter          E    =           .0010950
     Z    =       -4789081.53                 I    =           51.89164
     XDOT =      -6325.442284                 Wp   =          132.51207
     YDOT =       3396.687452  meter/sec      RA   =          134.82868  deg
     ZDOT =       2666.573848                 TA   =          163.76785
                                              MA   =          163.73275
                                              Ha   =            221.424  n.mi
                                              Hp   =            216.238
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1788673.51                 X    =          514962.43
     Y    =       15681214.31  feet           Y    =         4785562.12  meter
     Z    =      -15712209.73                 Z    =        -4786506.31
     XDOT =     -20752.763400                 XDOT =       -6375.907487
     YDOT =      11143.987703  feet/sec       YDOT =        3325.669602  meter/sec
     ZDOT =       8748.601863                 ZDOT =        2635.725182
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13365654.11                 X    =        -4073851.37
     Y    =       -8414777.77  feet           Y    =        -2564824.27  meter
     Z    =      -15701088.34                 Z    =        -4785691.73
     XDOT =       3854.069564                 XDOT =        1174.720403
     YDOT =     -22205.674668  feet/sec       YDOT =       -6768.289639  meter/sec
     ZDOT =       8609.096395                 ZDOT =        2624.052581
  
  
    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   18361.38924299  .00016717  00000-0  10270-3 0  9170
    2 25544  51.6365 135.8901 0004578 214.4828 145.6028 15.53693734 28550
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18361.38924299   =   yrday.fracday
    Element set:     917
    Inclination:       51.6365  deg
    RA of node:       135.8901  deg
    Eccentricity:     .0004578     
    Arg of perigee:   214.4828  deg
    Mean anomaly:     145.6028  deg
    Mean motion:   15.53693734  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2855
    Checksum:              344
 
             

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