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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  16989.6378
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   68.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.884
   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 
   ------------------------------------------------------------------------
   175/23:10:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.5  
   000/00:00:00.000           0.0               0.0              216.2  
   
   175/23:25:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.3  
   000/00:00:00.000           0.0               0.0              216.3  
   
   176/18:02:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.3  
   000/00:00:00.000           0.0               0.0              216.3  
   
   180/21:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              228.4  
   000/00:00:00.000           0.0               0.0              216.3  
   
 
 
    Coasting Arc #1 (Orbit 1529)
    ---------------------------------------
 
    Vector Time (GMT): 2019/168/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4505386.01                 A    =         6790951.88  meter
     Y    =        3106700.25  meter          E    =           .0017085
     Z    =        4004354.03                 I    =           51.63398
     XDOT =      -5738.275637                 Wp   =           81.90002
     YDOT =       3210.720061  meter/sec      RA   =          359.19172  deg
     ZDOT =       3953.199730                 TA   =          326.96290
                                              MA   =          327.06952
                                              Ha   =            228.183  n.mi
                                              Hp   =            216.758
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14781450.15                 X    =         4450860.20
     Y    =       10192586.12  feet           Y    =         3156776.99  meter
     Z    =       13137644.47                 Z    =         4026107.70
     XDOT =     -18826.363638                 XDOT =       -5792.954809
     YDOT =      10533.858469  feet/sec       YDOT =        3146.244158  meter/sec
     ZDOT =      12969.815386                 ZDOT =        3925.193114
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11538984.24                 X    =         3517082.40
     Y    =      -13661631.64  feet           Y    =        -4164065.32  meter
     Z    =       13235915.01                 Z    =         4034306.89
     XDOT =       7700.282295                 XDOT =        2347.046044
     YDOT =      18984.171806  feet/sec       YDOT =        5786.375566  meter/sec
     ZDOT =      12842.365135                 ZDOT =        3914.352893
  
  
    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   19168.55560996  .00016717  00000-0  10270-3 0  9007
    2 25544  51.6396 359.4756 0007810  55.3822 304.8065 15.51203720 15303
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19168.55560996   =   yrday.fracday
    Element set:     900
    Inclination:       51.6396  deg
    RA of node:       359.4756  deg
    Eccentricity:     .0007810     
    Arg of perigee:    55.3822  deg
    Mean anomaly:     304.8065  deg
    Mean motion:   15.51203720  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1530
    Checksum:              314
 
 
    Coasting Arc #2 (Orbit 1544)
    ---------------------------------------
 
    Vector Time (GMT): 2019/169/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4039044.62                 A    =         6789303.08  meter
     Y    =       -3154022.42  meter          E    =           .0017361
     Z    =       -4471203.77                 I    =           51.59505
     XDOT =       6123.351375                 Wp   =           64.64802
     YDOT =      -3219.383405  meter/sec      RA   =          354.22454  deg
     ZDOT =      -3263.209820                 TA   =          172.38141
                                              MA   =          172.35500
                                              Ha   =            228.353  n.mi
                                              Hp   =            216.511
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13251458.72                 X    =        -3981756.70
     Y    =      -10347842.60  feet           Y    =        -3198868.67  meter
     Z    =      -14669303.70                 Z    =        -4490685.34
     XDOT =      20089.735481                 XDOT =        6174.747147
     YDOT =     -10562.281512  feet/sec       YDOT =       -3150.619802  meter/sec
     ZDOT =     -10706.068964                 ZDOT =       -3233.340755
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11337720.35                 X    =        -3455737.16
     Y    =       12310436.04  feet           Y    =         3752220.90  meter
     Z    =      -14757260.50                 Z    =        -4498013.00
     XDOT =      -8069.936788                 XDOT =       -2459.716733
     YDOT =     -20092.902282  feet/sec       YDOT =       -6124.316615  meter/sec
     ZDOT =     -10570.173589                 ZDOT =       -3221.788910
  
  
    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   19169.52196145  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6394 354.6787 0007943  59.9642 300.2296 15.51212475 15458
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19169.52196145   =   yrday.fracday
    Element set:     901
    Inclination:       51.6394  deg
    RA of node:       354.6787  deg
    Eccentricity:     .0007943     
    Arg of perigee:    59.9642  deg
    Mean anomaly:     300.2296  deg
    Mean motion:   15.51212475  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1545
    Checksum:              329
 
 
    Coasting Arc #3 (Orbit 1560)
    ---------------------------------------
 
    Vector Time (GMT): 2019/170/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3528246.42                 A    =         6787971.10  meter
     Y    =        3218503.56  meter          E    =           .0013252
     Z    =        4812269.89                 I    =           51.55767
     XDOT =      -6457.124426                 Wp   =           89.22167
     YDOT =       3275.727828  meter/sec      RA   =          349.25346  deg
     ZDOT =       2537.498597                 TA   =          335.76922
                                              MA   =          335.83149
                                              Ha   =            228.324  n.mi
                                              Hp   =            216.601
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       11575611.62                 X    =         3468618.80
     Y    =       10559394.88  feet           Y    =         3257624.59  meter
     Z    =       15788287.04                 Z    =         4829264.44
     XDOT =     -21184.791424                 XDOT =       -6505.600315
     YDOT =      10747.138544  feet/sec       YDOT =        3203.248226  meter/sec
     ZDOT =       8325.126632                 ZDOT =        2506.015390
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11233867.53                 X    =         3424082.82
     Y    =      -10810598.38  feet           Y    =        -3295070.39  meter
     Z    =       15864954.93                 Z    =         4835638.26
     XDOT =       8657.014810                 XDOT =        2638.658114
     YDOT =      21031.353624  feet/sec       YDOT =        6410.356585  meter/sec
     ZDOT =       8181.908576                 ZDOT =        2493.845734
  
  
    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   19170.55273396  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6397 349.5620 0007935  63.0841 297.1120 15.51190386 15612
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19170.55273396   =   yrday.fracday
    Element set:     902
    Inclination:       51.6397  deg
    RA of node:       349.5620  deg
    Eccentricity:     .0007935     
    Arg of perigee:    63.0841  deg
    Mean anomaly:     297.1120  deg
    Mean motion:   15.51190386  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1561
    Checksum:              313
 
 
    Coasting Arc #4 (Orbit 1575)
    ---------------------------------------
 
    Vector Time (GMT): 2019/171/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2998958.06                 A    =         6786815.80  meter
     Y    =       -3362683.75  meter          E    =           .0021376
     Z    =       -5094762.71                 I    =           51.52134
     XDOT =       6669.284481                 Wp   =           73.35418
     YDOT =      -3313.213552  meter/sec      RA   =          344.27932  deg
     ZDOT =      -1739.057207                 TA   =          179.75896
                                              MA   =          179.75793
                                              Ha   =            228.474  n.mi
                                              Hp   =            216.324
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9839101.24                 X    =        -2936385.40
     Y    =      -11032426.99  feet           Y    =        -3395869.46  meter
     Z    =      -16715100.75                 Z    =        -5109178.98
     XDOT =      21880.854598                 XDOT =        6714.285400
     YDOT =     -10870.123203  feet/sec       YDOT =       -3238.381028  meter/sec
     ZDOT =      -5705.568266                 ZDOT =       -1706.551903
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11443591.13                 X    =        -3488006.58
     Y    =        9240716.93  feet           Y    =         2816570.52  meter
     Z    =      -16780057.33                 Z    =        -5114561.48
     XDOT =      -9239.323669                 XDOT =       -2816.145854
     YDOT =     -21533.483171  feet/sec       YDOT =       -6563.405671  meter/sec
     ZDOT =      -5557.717932                 ZDOT =       -1693.992426
  
  
    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   19171.51908121  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6396 344.7661 0008086  68.2884 291.9127 15.51213593 15766
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19171.51908121   =   yrday.fracday
    Element set:     903
    Inclination:       51.6396  deg
    RA of node:       344.7661  deg
    Eccentricity:     .0008086     
    Arg of perigee:    68.2884  deg
    Mean anomaly:     291.9127  deg
    Mean motion:   15.51213593  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1576
    Checksum:              326
 
 
    Coasting Arc #5 (Orbit 1591)
    ---------------------------------------
 
    Vector Time (GMT): 2019/172/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2447678.76                 A    =         6786205.00  meter
     Y    =        3534273.28  meter          E    =           .0010579
     Z    =        5241486.73                 I    =           51.48652
     XDOT =      -6832.862177                 Wp   =           84.94434
     YDOT =       3365.234398  meter/sec      RA   =          339.30152  deg
     ZDOT =        920.993730                 TA   =          356.22655
                                              MA   =          356.23453
                                              Ha   =            228.472  n.mi
                                              Hp   =            216.465
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8030442.12                 X    =         2382515.64
     Y    =       11595384.77  feet           Y    =         3561279.78  meter
     Z    =       17196478.77                 Z    =         5253218.78
     XDOT =     -22417.526828                 XDOT =       -6874.458987
     YDOT =      11040.795268  feet/sec       YDOT =        3288.591820  meter/sec
     ZDOT =       3021.632971                 ZDOT =         887.702097
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11798593.70                 X    =         3596211.36
     Y    =       -7610300.31  feet           Y    =        -2319619.53  meter
     Z    =       17249241.91                 Z    =         5257568.93
     XDOT =       9898.441306                 XDOT =        3017.044910
     YDOT =      21856.660509  feet/sec       YDOT =        6661.910123  meter/sec
     ZDOT =       2870.220499                 ZDOT =         874.843208
  
  
    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   19172.54985197  .00016717  00000-0  10270-3 0  9049
    2 25544  51.6390 339.6499 0008053  71.7729 288.4298 15.51175528 15926
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19172.54985197   =   yrday.fracday
    Element set:     904
    Inclination:       51.6390  deg
    RA of node:       339.6499  deg
    Eccentricity:     .0008053     
    Arg of perigee:    71.7729  deg
    Mean anomaly:     288.4298  deg
    Mean motion:   15.51175528  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1592
    Checksum:              359
 
 
    Coasting Arc #6 (Orbit 1606)
    ---------------------------------------
 
    Vector Time (GMT): 2019/173/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1917927.54                 A    =         6785839.05  meter
     Y    =       -3779693.44  meter          E    =           .0022741
     Z    =       -5319021.86                 I    =           51.45684
     XDOT =       6863.936744                 Wp   =           84.37570
     YDOT =      -3369.668773  meter/sec      RA   =          334.32181  deg
     ZDOT =        -78.618875                 TA   =          184.86006
                                              MA   =          184.88218
                                              Ha   =            228.488  n.mi
                                              Hp   =            216.260
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6292413.19                 X    =        -1849682.82
     Y    =      -12400569.04  feet           Y    =        -3800758.74  meter
     Z    =      -17450859.11                 Z    =        -5328173.10
     XDOT =      22519.477507                 XDOT =        6901.489088
     YDOT =     -11055.343743  feet/sec       YDOT =       -3292.701442  meter/sec
     ZDOT =       -257.935943                 ZDOT =         -45.186060
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12455758.43                 X    =        -3796515.17
     Y    =        6065386.04  feet           Y    =         1848729.66  meter
     Z    =      -17491890.53                 Z    =        -5331528.23
     XDOT =     -10413.937904                 XDOT =       -3174.168273
     YDOT =     -21709.072742  feet/sec       YDOT =       -6616.925372  meter/sec
     ZDOT =       -105.895457                 ZDOT =         -32.276935
  
  
    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   19173.51619553  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6409 334.8544 0008050  75.7779 284.4266 15.51222563 16071
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19173.51619553   =   yrday.fracday
    Element set:     905
    Inclination:       51.6409  deg
    RA of node:       334.8544  deg
    Eccentricity:     .0008050     
    Arg of perigee:    75.7779  deg
    Mean anomaly:     284.4266  deg
    Mean motion:   15.51222563  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1607
    Checksum:              323
 
 
    Coasting Arc #7 (Orbit 1622)
    ---------------------------------------
 
    Vector Time (GMT): 2019/174/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1385737.80                 A    =         6786154.64  meter
     Y    =        4051280.53  meter          E    =           .0011300
     Z    =        5255809.07                 I    =           51.42725
     XDOT =      -6858.089317                 Wp   =           73.64011
     YDOT =       3351.379013  meter/sec      RA   =          329.33829  deg
     ZDOT =       -770.614119                 TA   =           23.76755
                                              MA   =           23.71540
                                              Ha   =            228.567  n.mi
                                              Hp   =            216.344
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4546383.87                 X    =         1314802.68
     Y    =       13291602.77  feet           Y    =         4066379.54  meter
     Z    =       17243468.09                 Z    =         5262368.62
     XDOT =     -22500.293035                 XDOT =       -6891.312512
     YDOT =      10995.337969  feet/sec       YDOT =        3274.501383  meter/sec
     ZDOT =      -2528.261546                 ZDOT =        -804.008113
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13255186.16                 X    =         4040180.74
     Y    =       -4541671.00  feet           Y    =        -1384301.32  meter
     Z    =       17272717.41                 Z    =         5264724.27
     XDOT =      10851.980661                 XDOT =        3307.683705
     YDOT =      21423.293605  feet/sec       YDOT =        6529.819891  meter/sec
     ZDOT =      -2680.109522                 ZDOT =        -816.897382
  
  
    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   19174.54696190  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6402 329.7375 0008164  79.5169 280.6902 15.51182114 16230
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19174.54696190   =   yrday.fracday
    Element set:     906
    Inclination:       51.6402  deg
    RA of node:       329.7375  deg
    Eccentricity:     .0008164     
    Arg of perigee:    79.5169  deg
    Mean anomaly:     280.6902  deg
    Mean motion:   15.51182114  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1623
    Checksum:              319
 
 
    Coasting Arc #8 (Orbit 1637)
    ---------------------------------------
 
    Vector Time (GMT): 2019/175/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -914390.04                 A    =         6786722.90  meter
     Y    =       -4377369.19  meter          E    =           .0021260
     Z    =       -5123944.11                 I    =           51.40172
     XDOT =       6730.810845                 Wp   =           94.77085
     YDOT =      -3263.765938  meter/sec      RA   =          324.35591  deg
     ZDOT =       1591.077270                 TA   =          190.64490
                                              MA   =          190.68998
                                              Ha   =            228.525  n.mi
                                              Hp   =            216.232
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2999967.33                 X    =         -840483.99
     Y    =      -14361447.46  feet           Y    =        -4387180.72  meter
     Z    =      -16810840.25                 Z    =        -5128206.83
     XDOT =      22082.712747                 XDOT =        6759.078450
     YDOT =     -10707.893499  feet/sec       YDOT =       -3188.339418  meter/sec
     ZDOT =       5220.069783                 ZDOT =        1623.841086
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14284045.02                 X    =        -4353776.92
     Y    =        3253397.22  feet           Y    =          991635.47  meter
     Z    =      -16829640.27                 Z    =        -5129674.35
     XDOT =     -11030.728011                 XDOT =       -3362.165898
     YDOT =     -20724.434336  feet/sec       YDOT =       -6316.807586  meter/sec
     ZDOT =       5369.034808                 ZDOT =        1636.481809
  
  
    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   19175.51330199  .00016717  00000-0  10270-3 0  9078
    2 25544  51.6406 324.9430 0008086  83.2055 277.0016 15.51222240 16389
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19175.51330199   =   yrday.fracday
    Element set:     907
    Inclination:       51.6406  deg
    RA of node:       324.9430  deg
    Eccentricity:     .0008086     
    Arg of perigee:    83.2055  deg
    Mean anomaly:     277.0016  deg
    Mean motion:   15.51222240  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1638
    Checksum:              291
 
 
    Coasting Arc #9 (Orbit 1645)
    ---------------------------------------
 
    Vector Time (GMT): 2019/175/23:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 931521.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5573158.11                 A    =         6797558.07  meter
     Y    =       -3847611.13  meter          E    =           .0020280
     Z    =         491453.11                 I    =           51.42468
     XDOT =       2355.768056                 Wp   =           62.75588
     YDOT =       4197.460106  meter/sec      RA   =          322.06139  deg
     ZDOT =       5966.485918                 TA   =          302.55614
                                              MA   =          302.75186
                                              Ha   =            228.467  n.mi
                                              Hp   =            216.190
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18284639.45                 X    =         5613381.79
     Y    =      -12623396.09  feet           Y    =        -3785063.32  meter
     Z    =        1612378.97                 Z    =          518622.54
     XDOT =       7728.897821                 XDOT =        2279.674066
     YDOT =      13771.194575  feet/sec       YDOT =        4223.377833  meter/sec
     ZDOT =      19575.085033                 ZDOT =        5977.744936
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9055057.00                 X    =         2759981.37
     Y    =       20279793.94  feet           Y    =         6181281.19  meter
     Z    =        1736040.08                 Z    =          529145.02
     XDOT =     -13454.099228                 XDOT =       -4100.809445
     YDOT =       4280.125842  feet/sec       YDOT =        1304.582357  meter/sec
     ZDOT =      19625.633830                 ZDOT =        5981.893191
  
  
    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   19176.02868124  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6393 322.3888 0008103  83.5231 276.6842 15.51262839 16461
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19176.02868124   =   yrday.fracday
    Element set:     908
    Inclination:       51.6393  deg
    RA of node:       322.3888  deg
    Eccentricity:     .0008103     
    Arg of perigee:    83.5231  deg
    Mean anomaly:     276.6842  deg
    Mean motion:   15.51262839  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1646
    Checksum:              325
 
 
    Coasting Arc #10 (Orbit 1645)
    ---------------------------------------
 
    Vector Time (GMT): 2019/175/23:25:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4579948.67                 A    =         6787762.75  meter
     Y    =        1311341.86  meter          E    =           .0014135
     Z    =        4823876.60                 I    =           51.39178
     XDOT =      -4292.425205                 Wp   =           99.24746
     YDOT =       5857.781862  meter/sec      RA   =          322.02179  deg
     ZDOT =       2474.528344                 TA   =          326.33011
                                              MA   =          326.41983
                                              Ha   =            228.323  n.mi
                                              Hp   =            216.313
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15026078.33                 X    =         4541512.91
     Y    =        4302302.70  feet           Y    =         1362342.62  meter
     Z    =       15826366.81                 Z    =         4846030.95
     XDOT =     -14082.759859                 XDOT =       -4369.629392
     YDOT =      19218.444429  feet/sec       YDOT =        5809.349006  meter/sec
     ZDOT =       8118.531313                 ZDOT =        2453.490598
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6012173.89                 X    =        -1832510.60
     Y    =       14316485.85  feet           Y    =         4363664.89  meter
     Z    =       15926667.04                 Z    =         4854448.11
     XDOT =     -16397.207627                 XDOT =       -4997.868885
     YDOT =     -15841.297265  feet/sec       YDOT =       -4828.427406  meter/sec
     ZDOT =       8022.432533                 ZDOT =        2445.237436
  
  
    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   19176.02868248  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6396 322.3886 0007963  81.7618 278.4436 15.51235575 16460
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19176.02868248   =   yrday.fracday
    Element set:     909
    Inclination:       51.6396  deg
    RA of node:       322.3886  deg
    Eccentricity:     .0007963     
    Arg of perigee:    81.7618  deg
    Mean anomaly:     278.4436  deg
    Mean motion:   15.51235575  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1646
    Checksum:              352
 
 
    Coasting Arc #11 (Orbit 1657)
    ---------------------------------------
 
    Vector Time (GMT): 2019/176/18:02:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3784598.51                 A    =         6786236.46  meter
     Y    =        2174921.59  meter          E    =           .0011311
     Z    =        5186659.47                 I    =           51.36875
     XDOT =      -4954.107624                 Wp   =           97.96117
     YDOT =       5732.464806  meter/sec      RA   =          318.15062  deg
     ZDOT =       1207.314773                 TA   =          340.39576
                                              MA   =          340.43921
                                              Ha   =            228.326  n.mi
                                              Hp   =            216.321
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12416661.78                 X    =         3734802.81
     Y    =        7135569.53  feet           Y    =         2216964.64  meter
     Z    =       17016599.32                 Z    =         5204922.87
     XDOT =     -16253.633936                 XDOT =       -5023.705932
     YDOT =      18807.299231  feet/sec       YDOT =        5676.675221  meter/sec
     ZDOT =       3961.006474                 ZDOT =        1183.081230
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12681158.76                 X    =        -3865217.19
     Y    =       -6439077.88  feet           Y    =        -1962630.94  meter
     Z    =       17099151.54                 Z    =         5211821.39
     XDOT =      14735.388100                 XDOT =        4491.346293
     YDOT =     -18762.042065  feet/sec       YDOT =       -5718.670421  meter/sec
     ZDOT =       3850.443797                 ZDOT =        1173.615269
  
  
    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   19176.80175353  .00016717  00000-0  10270-3 0  9104
    2 25544  51.6417 318.5509 0007915  86.0538 274.1518 15.51234439 16584
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19176.80175353   =   yrday.fracday
    Element set:     910
    Inclination:       51.6417  deg
    RA of node:       318.5509  deg
    Eccentricity:     .0007915     
    Arg of perigee:    86.0538  deg
    Mean anomaly:     274.1518  deg
    Mean motion:   15.51234439  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1658
    Checksum:              322
 
 
    Coasting Arc #12 (Orbit 1672)
    ---------------------------------------
 
    Vector Time (GMT): 2019/177/18:02:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3374092.16                 A    =         6785924.70  meter
     Y    =       -2601452.40  meter          E    =           .0022793
     Z    =       -5301588.97                 I    =           51.34396
     XDOT =       5010.833452                 Wp   =           87.54683
     YDOT =      -5764.865898  meter/sec      RA   =          313.16178  deg
     ZDOT =       -360.661334                 TA   =          178.99280
                                              MA   =          178.98820
                                              Ha   =            228.531  n.mi
                                              Hp   =            216.186
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11069856.17                 X    =        -3318999.04
     Y    =       -8534948.81  feet           Y    =        -2638875.22  meter
     Z    =      -17393664.61                 Z    =        -5317845.53
     XDOT =      16439.742297                 XDOT =        5076.677310
     YDOT =     -18913.602029  feet/sec       YDOT =       -5708.463048  meter/sec
     ZDOT =      -1183.272094                 ZDOT =        -336.161315
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11546446.97                 X    =         3519357.04
     Y    =        7714128.08  feet           Y    =         2351266.24  meter
     Z    =      -17467066.89                 Z    =        -5323961.99
     XDOT =     -14460.774349                 XDOT =       -4407.644022
     YDOT =      19221.469078  feet/sec       YDOT =        5858.703775  meter/sec
     ZDOT =      -1071.511913                 ZDOT =        -326.596831
  
  
    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   19177.76809148  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6424 313.7546 0008002  88.7363 271.4705 15.51205071 16738
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19177.76809148   =   yrday.fracday
    Element set:     911
    Inclination:       51.6424  deg
    RA of node:       313.7546  deg
    Eccentricity:     .0008002     
    Arg of perigee:    88.7363  deg
    Mean anomaly:     271.4705  deg
    Mean motion:   15.51205071  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1673
    Checksum:              309
 
 
    Coasting Arc #13 (Orbit 1688)
    ---------------------------------------
 
    Vector Time (GMT): 2019/178/18:02:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2975634.78                 A    =         6785833.90  meter
     Y    =        3046410.05  meter          E    =           .0010683
     Z    =        5274035.39                 I    =           51.32132
     XDOT =      -5034.270997                 Wp   =           85.53162
     YDOT =       5768.878065  meter/sec      RA   =          308.17200  deg
     ZDOT =       -490.206967                 TA   =            9.17274
                                              MA   =            9.15324
                                              Ha   =            228.386  n.mi
                                              Hp   =            216.241
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9762581.31                 X    =         2915729.41
     Y    =        9994783.64  feet           Y    =         3079350.07  meter
     Z    =       17303265.72                 Z    =         5288344.83
     XDOT =     -16516.637128                 XDOT =       -5096.024927
     YDOT =      18926.765306  feet/sec       YDOT =        5712.236091  meter/sec
     ZDOT =      -1608.290575                 ZDOT =        -514.810886
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10507662.38                 X    =        -3202735.49
     Y    =       -9086012.44  feet           Y    =        -2769416.59  meter
     Z    =       17367789.37                 Z    =         5293702.20
     XDOT =      14070.125937                 XDOT =        4288.574385
     YDOT =     -19570.830990  feet/sec       YDOT =       -5965.189286  meter/sec
     ZDOT =      -1720.509629                 ZDOT =        -524.411335
  
  
    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   19178.79884824  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6416 308.6392 0008072  92.0634 268.1441 15.51246770 16895
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19178.79884824   =   yrday.fracday
    Element set:     912
    Inclination:       51.6416  deg
    RA of node:       308.6392  deg
    Eccentricity:     .0008072     
    Arg of perigee:    92.0634  deg
    Mean anomaly:     268.1441  deg
    Mean motion:   15.51246770  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1689
    Checksum:              335
 
 
    Coasting Arc #14 (Orbit 1703)
    ---------------------------------------
 
    Vector Time (GMT): 2019/179/18:02:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2644201.79                 A    =         6786488.09  meter
     Y    =       -3532101.09  meter          E    =           .0021894
     Z    =       -5175917.36                 I    =           51.30397
     XDOT =       4969.125363                 Wp   =           98.24289
     YDOT =      -5659.505570  meter/sec      RA   =          303.18025  deg
     ZDOT =       1325.307441                 TA   =          184.57681
                                              MA   =          184.59686
                                              Ha   =            228.529  n.mi
                                              Hp   =            216.205
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8675202.71                 X    =        -2579366.49
     Y    =      -11588258.18  feet           Y    =        -3561307.14  meter
     Z    =      -16981356.17                 Z    =        -5188604.99
     XDOT =      16302.904735                 XDOT =        5025.604631
     YDOT =     -18567.931660  feet/sec       YDOT =       -5603.621724  meter/sec
     ZDOT =       4348.121526                 ZDOT =        1349.582029
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9754335.26                 X    =         2973121.39
     Y    =       10604559.01  feet           Y    =         3232269.59  meter
     Z    =      -17038474.08                 Z    =        -5193326.90
     XDOT =     -13415.088594                 XDOT =       -4088.919003
     YDOT =      19494.334469  feet/sec       YDOT =        5941.873146  meter/sec
     ZDOT =       4458.824537                 ZDOT =        1359.049719
  
  
    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   19179.76518338  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6422 303.8429 0008026  95.3549 264.8518 15.51209075 17043
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19179.76518338   =   yrday.fracday
    Element set:     913
    Inclination:       51.6422  deg
    RA of node:       303.8429  deg
    Eccentricity:     .0008026     
    Arg of perigee:    95.3549  deg
    Mean anomaly:     264.8518  deg
    Mean motion:   15.51209075  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1704
    Checksum:              326
 
 
    Coasting Arc #15 (Orbit 1719)
    ---------------------------------------
 
    Vector Time (GMT): 2019/180/18:02:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2334141.94                 A    =         6787288.05  meter
     Y    =        4018830.36  meter          E    =           .0013580
     Z    =        4935635.87                 I    =           51.28937
     XDOT =      -4901.458330                 Wp   =           80.39039
     YDOT =       5496.884166  meter/sec      RA   =          298.18836  deg
     ZDOT =      -2150.548687                 TA   =           30.70113
                                              MA   =           30.62175
                                              Ha   =            228.397  n.mi
                                              Hp   =            216.220
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7657946.00                 X    =         2265054.11
     Y    =       13185138.99  feet           Y    =         4044545.26  meter
     Z    =       16193031.06                 Z    =         4946807.16
     XDOT =     -16080.900033                 XDOT =       -4952.115576
     YDOT =      18034.396871  feet/sec       YDOT =        5441.789740  meter/sec
     ZDOT =      -7055.605929                 ZDOT =       -2174.480330
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9129732.59                 X    =        -2782742.49
     Y    =      -12145449.17  feet           Y    =        -3701932.91  meter
     Z    =       16243224.11                 Z    =         4950934.71
     XDOT =      12781.084532                 XDOT =        3895.674565
     YDOT =     -19221.510620  feet/sec       YDOT =       -5858.716437  meter/sec
     ZDOT =      -7164.727640                 ZDOT =       -2183.808985
  
  
    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   19180.79593677  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6417 298.7271 0008124  98.6214 261.5858 15.51260040 17206
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19180.79593677   =   yrday.fracday
    Element set:     914
    Inclination:       51.6417  deg
    RA of node:       298.7271  deg
    Eccentricity:     .0008124     
    Arg of perigee:    98.6214  deg
    Mean anomaly:     261.5858  deg
    Mean motion:   15.51260040  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1720
    Checksum:              324
 
 
    Coasting Arc #16 (Orbit 1721)
    ---------------------------------------
 
    Vector Time (GMT): 2019/180/21:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4169883.21                 A    =         6786037.31  meter
     Y    =        1081230.43  meter          E    =           .0011173
     Z    =        5234342.11                 I    =           51.28096
     XDOT =      -2908.480013                 Wp   =          104.32494
     YDOT =       7047.408999  meter/sec      RA   =          297.59643  deg
     ZDOT =        857.005379                 TA   =          337.41910
                                              MA   =          337.46822
                                              Ha   =            228.355  n.mi
                                              Hp   =            216.306
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13680719.18                 X    =         4132057.07
     Y    =        3547343.94  feet           Y    =         1127648.60  meter
     Z    =       17173038.41                 Z    =         5254506.21
     XDOT =      -9542.257261                 XDOT =       -2991.232860
     YDOT =      23121.420600  feet/sec       YDOT =        7014.421492  meter/sec
     ZDOT =       2811.697439                 ZDOT =         842.677232
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11182755.99                 X    =        -3408504.03
     Y    =        8458585.73  feet           Y    =         2578176.93  meter
     Z    =       17264335.21                 Z    =         5262169.37
     XDOT =     -11626.964701                 XDOT =       -3543.898841
     YDOT =     -21004.490133  feet/sec       YDOT =       -6402.168592  meter/sec
     ZDOT =       2745.941163                 ZDOT =         836.962866
  
  
    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   19180.92478201  .00016717  00000-0  10270-3 0  9155
    2 25544  51.6397 298.0876 0008036  98.6129 261.5932 15.51226119 17228
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19180.92478201   =   yrday.fracday
    Element set:     915
    Inclination:       51.6397  deg
    RA of node:       298.0876  deg
    Eccentricity:     .0008036     
    Arg of perigee:    98.6129  deg
    Mean anomaly:     261.5932  deg
    Mean motion:   15.51226119  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1722
    Checksum:              327
 
 
    Coasting Arc #17 (Orbit 1736)
    ---------------------------------------
 
    Vector Time (GMT): 2019/181/21:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3928825.90                 A    =         6785839.47  meter
     Y    =       -1635322.50  meter          E    =           .0022803
     Z    =       -5305413.65                 I    =           51.26620
     XDOT =       2938.025652                 Wp   =           93.91440
     YDOT =      -7059.845175  meter/sec      RA   =          292.60191  deg
     ZDOT =         -1.128262                 TA   =          176.08370
                                              MA   =          176.06582
                                              Ha   =            228.503  n.mi
                                              Hp   =            216.154
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12889848.75                 X    =        -3884476.51
     Y    =       -5365231.29  feet           Y    =        -1679008.42  meter
     Z    =      -17406212.75                 Z    =        -5324391.01
     XDOT =       9639.191773                 XDOT =        3016.757982
     YDOT =     -23162.221702  feet/sec       YDOT =       -7026.549893  meter/sec
     ZDOT =         -3.701647                 ZDOT =          13.333478
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12002977.08                 X    =         3658507.41
     Y    =       -6918535.48  feet           Y    =        -2108769.62  meter
     Z    =      -17492071.29                 Z    =        -5331583.33
     XDOT =      12097.859767                 XDOT =        3687.427657
     YDOT =      20817.561041  feet/sec       YDOT =        6345.192605  meter/sec
     ZDOT =         62.652067                 ZDOT =          19.096350
  
  
    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   19181.89111138  .00016717  00000-0  10270-3 0  9166
    2 25544  51.6402 293.2915 0008057 101.4719 258.7337 15.51222450 17374
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19181.89111138   =   yrday.fracday
    Element set:     916
    Inclination:       51.6402  deg
    RA of node:       293.2915  deg
    Eccentricity:     .0008057     
    Arg of perigee:   101.4719  deg
    Mean anomaly:     258.7337  deg
    Mean motion:   15.51222450  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1737
    Checksum:              304
 
 
    Coasting Arc #18 (Orbit 1752)
    ---------------------------------------
 
    Vector Time (GMT): 2019/182/21:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 916289.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3710723.51                 A    =         6786034.58  meter
     Y    =        2190230.21  meter          E    =           .0010609
     Z    =        5233224.32                 I    =           51.25468
     XDOT =      -2948.233981                 Wp   =           91.79571
     YDOT =       7031.756347  meter/sec      RA   =          287.60699  deg
     ZDOT =       -851.282020                 TA   =            6.38994
                                              MA   =            6.37642
                                              Ha   =            228.306  n.mi
                                              Hp   =            216.367
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12174289.73                 X    =         3660535.96
     Y    =        7185794.64  feet           Y    =         2231444.47  meter
     Z    =       17169371.11                 Z    =         5251128.08
     XDOT =      -9672.683665                 XDOT =       -3022.510938
     YDOT =      23070.066755  feet/sec       YDOT =        6998.371988  meter/sec
     ZDOT =      -2792.920012                 ZDOT =        -865.782392
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12927748.88                 X    =        -3940377.86
     Y    =        5471421.65  feet           Y    =         1667689.32  meter
     Z    =       17250308.22                 Z    =         5257893.94
     XDOT =     -12491.515265                 XDOT =       -3807.413853
     YDOT =     -20487.363480  feet/sec       YDOT =       -6244.548389  meter/sec
     ZDOT =      -2859.435277                 ZDOT =        -871.555872
  
  
    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   19182.92186209  .00016717  00000-0  10270-3 0  9173
    2 25544  51.6396 288.1760 0007970 105.0785 255.1249 15.51233196 17533
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19182.92186209   =   yrday.fracday
    Element set:     917
    Inclination:       51.6396  deg
    RA of node:       288.1760  deg
    Eccentricity:     .0007970     
    Arg of perigee:   105.0785  deg
    Mean anomaly:     255.1249  deg
    Mean motion:   15.51233196  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1753
    Checksum:              330
 
             

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