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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15140.5164
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   68.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   1.584
   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 
   ------------------------------------------------------------------------
   346/03:16:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.4  
   000/00:00:00.000           0.0               0.0              219.4  
   
   349/11:36:38.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.6  
   000/00:00:00.000           0.0               0.0              219.1  
   
   355/13:08:55.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.9  
   000/00:00:00.000           0.0               0.0              218.5  
   
   356/04:02:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              229.9  
   000/00:00:00.000           0.0               0.0              218.4  
   
   359/09:45:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              230.0  
   000/00:00:00.000           0.0               0.0              218.3  
   
 
 
    Coasting Arc #1 (Orbit 274)
    ---------------------------------------
 
    Vector Time (GMT): 2019/345/11:24:50.319
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6399283.94                 A    =         6798920.68  meter
     Y    =        -602810.93  meter          E    =           .0013218
     Z    =       -2200498.82                 I    =           51.51020
     XDOT =      -1380.382922                 Wp   =           31.27778
     YDOT =      -5193.050920  meter/sec      RA   =          201.17770  deg
     ZDOT =       5462.719944                 TA   =          304.27792
                                              MA   =          304.40301
                                              Ha   =            229.240  n.mi
                                              Hp   =            219.554
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20995026.05                 X    =        -6381378.58
     Y    =       -1977726.16  feet           Y    =         -674271.82  meter
     Z    =       -7219484.33                 Z    =        -2231541.17
     XDOT =      -4528.815362                 XDOT =       -1348.745339
     YDOT =     -17037.568635  feet/sec       YDOT =       -5208.311217  meter/sec
     ZDOT =      17922.309527                 ZDOT =        5456.090572
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8954552.79                 X    =         2729347.69
     Y    =      -19038202.55  feet           Y    =        -5802844.14  meter
     Z    =       -7361134.52                 Z    =        -2243673.80
     XDOT =      16216.206503                 XDOT =        4942.699742
     YDOT =        741.273929  feet/sec       YDOT =         225.940294  meter/sec
     ZDOT =      17892.343173                 ZDOT =        5453.586199
  
  
    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   19345.48004270  .00016717  00000-0  10270-3 0  9004
    2 25544  51.6415 202.3564 0007472  20.6419 339.5032 15.50105232  2751
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19345.48004270   =   yrday.fracday
    Element set:     900
    Inclination:       51.6415  deg
    RA of node:       202.3564  deg
    Eccentricity:     .0007472     
    Arg of perigee:    20.6419  deg
    Mean anomaly:     339.5032  deg
    Mean motion:   15.50105232  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             275
    Checksum:              269
 
 
    Coasting Arc #2 (Orbit 285)
    ---------------------------------------
 
    Vector Time (GMT): 2019/346/03:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1641370.35                 A    =         6791396.06  meter
     Y    =       -4526873.26  meter          E    =           .0010303
     Z    =        4779377.42                 I    =           51.50241
     XDOT =       7208.116440                 Wp   =           72.73258
     YDOT =        147.996477  meter/sec      RA   =          197.93686  deg
     ZDOT =       2613.976319                 TA   =          351.44008
                                              MA   =          351.45764
                                              Ha   =            229.409  n.mi
                                              Hp   =            219.438
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5385073.33                 X    =        -1613843.36
     Y    =      -14851946.41  feet           Y    =        -4545075.04  meter
     Z    =       15680372.10                 Z    =         4771470.33
     XDOT =      23648.675984                 XDOT =        7193.228391
     YDOT =        485.552747  feet/sec       YDOT =         228.519085  meter/sec
     ZDOT =       8576.037791                 ZDOT =        2648.954909
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8169567.64                 X    =        -2490084.22
     Y    =       13563192.39  feet           Y    =         4134061.04  meter
     Z    =       15644531.72                 Z    =         4768453.27
     XDOT =     -13363.771133                 XDOT =       -4073.277441
     YDOT =     -18132.008758  feet/sec       YDOT =       -5526.636269  meter/sec
     ZDOT =       8735.697525                 ZDOT =        2662.640605
  
  
    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   19346.18919882  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6382 198.8411 0007407  25.3533 334.7979 15.50116406  2865
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19346.18919882   =   yrday.fracday
    Element set:     901
    Inclination:       51.6382  deg
    RA of node:       198.8411  deg
    Eccentricity:     .0007407     
    Arg of perigee:    25.3533  deg
    Mean anomaly:     334.7979  deg
    Mean motion:   15.50116406  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             286
    Checksum:              326
 
 
    Coasting Arc #3 (Orbit 300)
    ---------------------------------------
 
    Vector Time (GMT): 2019/347/03:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1571307.75                 A    =         6790802.06  meter
     Y    =        4396333.37  meter          E    =           .0018312
     Z    =       -4948152.08                 I    =           51.53198
     XDOT =      -7319.066685                 Wp   =           57.35471
     YDOT =        119.505889  meter/sec      RA   =          192.97175  deg
     ZDOT =      -2214.369270                 TA   =          190.92112
                                              MA   =          190.96093
                                              Ha   =            229.518  n.mi
                                              Hp   =            219.305
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5155209.15                 X    =         1546065.41
     Y    =       14423665.91  feet           Y    =         4413764.50  meter
     Z    =      -16234094.74                 Z    =        -4940579.81
     XDOT =     -24012.685976                 XDOT =       -7309.102822
     YDOT =        392.079688  feet/sec       YDOT =          37.714983  meter/sec
     ZDOT =      -7264.991043                 ZDOT =       -2249.898571
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7749409.31                 X    =         2362019.96
     Y    =      -13254370.80  feet           Y    =        -4039932.22  meter
     Z    =      -16199767.33                 Z    =        -4937689.08
     XDOT =      14620.116096                 XDOT =        4456.211386
     YDOT =      17640.291386  feet/sec       YDOT =        5376.760814  meter/sec
     ZDOT =      -7427.209154                 ZDOT =       -2263.813350
  
  
    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   19347.15622863  .00016717  00000-0  10270-3 0  9026
    2 25544  51.6376 194.0491 0007510  29.3424 330.8147 15.50106213  3019
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19347.15622863   =   yrday.fracday
    Element set:     902
    Inclination:       51.6376  deg
    RA of node:       194.0491  deg
    Eccentricity:     .0007510     
    Arg of perigee:    29.3424  deg
    Mean anomaly:     330.8147  deg
    Mean motion:   15.50106213  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             301
    Checksum:              279
 
 
    Coasting Arc #4 (Orbit 316)
    ---------------------------------------
 
    Vector Time (GMT): 2019/348/03:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1466564.31                 A    =         6790183.02  meter
     Y    =       -4266788.95  meter          E    =           .0009098
     Z    =        5066213.47                 I    =           51.56256
     XDOT =       7440.388659                 Wp   =           69.80222
     YDOT =       -405.770630  meter/sec      RA   =          188.00938  deg
     ZDOT =       1812.526679                 TA   =            2.63772
                                              MA   =            2.63293
                                              Ha   =            229.547  n.mi
                                              Hp   =            219.198
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4811562.70                 X    =        -1443351.71
     Y    =      -13998651.42  feet           Y    =        -4283060.13  meter
     Z    =       16621435.28                 Z    =         5059145.14
     XDOT =      24410.723946                 XDOT =        7435.568863
     YDOT =      -1331.268470  feet/sec       YDOT =        -322.594188  meter/sec
     ZDOT =       5946.609839                 ZDOT =        1848.657576
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7419639.61                 X    =        -2261506.15
     Y    =       12850154.77  feet           Y    =         3916727.18  meter
     Z    =       16589392.94                 Z    =         5056446.97
     XDOT =     -15938.335166                 XDOT =       -4858.004558
     YDOT =     -17090.951018  feet/sec       YDOT =       -5209.321870  meter/sec
     ZDOT =       6111.621333                 ZDOT =        1862.822182
  
  
    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   19348.18772651  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6372 188.9384 0007460  31.9076 328.2525 15.50121158  3177
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19348.18772651   =   yrday.fracday
    Element set:     903
    Inclination:       51.6372  deg
    RA of node:       188.9384  deg
    Eccentricity:     .0007460     
    Arg of perigee:    31.9076  deg
    Mean anomaly:     328.2525  deg
    Mean motion:   15.50121158  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             317
    Checksum:              313
 
 
    Coasting Arc #5 (Orbit 331)
    ---------------------------------------
 
    Vector Time (GMT): 2019/349/03:16:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1365885.39                 A    =         6789787.22  meter
     Y    =        4188106.91  meter          E    =           .0019868
     Z    =       -5184077.05                 I    =           51.59518
     XDOT =      -7485.243238                 Wp   =           64.48786
     YDOT =        709.035394  meter/sec      RA   =          183.04786  deg
     ZDOT =      -1395.213168                 TA   =          192.02504
                                              MA   =          192.07254
                                              Ha   =            229.620  n.mi
                                              Hp   =            219.102
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        4481251.29                 X    =         1344132.52
     Y    =       13740508.22  feet           Y    =         4203260.35  meter
     Z    =      -17008126.81                 Z    =        -5177494.32
     XDOT =     -24557.884640                 XDOT =       -7485.838417
     YDOT =       2326.231606  feet/sec       YDOT =         625.326998  meter/sec
     ZDOT =      -4577.471025                 ZDOT =       -1431.574885
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7222028.28                 X    =         2201274.22
     Y    =      -12559441.46  feet           Y    =        -3828117.76  meter
     Z    =      -16978288.92                 Z    =        -5174982.46
     XDOT =      17108.239555                 XDOT =        5214.591416
     YDOT =      16268.745917  feet/sec       YDOT =        4958.713755  meter/sec
     ZDOT =      -4743.583557                 ZDOT =       -1445.844268
  
  
    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   19349.15475490  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6380 184.1461 0007489  35.7278 324.4373 15.50109295  3321
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19349.15475490   =   yrday.fracday
    Element set:     904
    Inclination:       51.6380  deg
    RA of node:       184.1461  deg
    Eccentricity:     .0007489     
    Arg of perigee:    35.7278  deg
    Mean anomaly:     324.4373  deg
    Mean motion:   15.50109295  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             332
    Checksum:              317
 
 
    Coasting Arc #6 (Orbit 337)
    ---------------------------------------
 
    Vector Time (GMT): 2019/349/11:36:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5295817.84                 A    =         6796557.36  meter
     Y    =       -2709512.92  meter          E    =           .0018175
     Z    =        3265254.23                 I    =           51.63075
     XDOT =       4799.397472                 Wp   =           68.68417
     YDOT =      -3645.183114  meter/sec      RA   =          181.33755  deg
     ZDOT =       4744.398089                 TA   =          329.17538
                                              MA   =          329.28197
                                              Ha   =            229.588  n.mi
                                              Hp   =            219.142
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17374730.45                 X    =        -5280986.39
     Y    =       -8889478.09  feet           Y    =        -2768652.04  meter
     Z    =       10712776.36                 Z    =         3239564.89
     XDOT =      15746.054699                 XDOT =        4816.756743
     YDOT =     -11959.262186  feet/sec       YDOT =       -3591.416485  meter/sec
     ZDOT =      15565.610529                 ZDOT =        4767.753283
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12558263.83                 X    =         3827758.82
     Y    =      -15023023.88  feet           Y    =        -4579017.68  meter
     Z    =       10595584.91                 Z    =         3229534.28
     XDOT =       7070.690956                 XDOT =        2155.146603
     YDOT =      16998.953516  feet/sec       YDOT =        5181.281032  meter/sec
     ZDOT =      15672.483503                 ZDOT =        4776.972972
  
  
    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   19349.54156356  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6391 182.2292 0007334  34.6572 325.5055 15.50135080  3384
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19349.54156356   =   yrday.fracday
    Element set:     905
    Inclination:       51.6391  deg
    RA of node:       182.2292  deg
    Eccentricity:     .0007334     
    Arg of perigee:    34.6572  deg
    Mean anomaly:     325.5055  deg
    Mean motion:   15.50135080  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             338
    Checksum:              301
 
 
    Coasting Arc #7 (Orbit 352)
    ---------------------------------------
 
    Vector Time (GMT): 2019/350/11:36:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5213253.00                 A    =         6795684.90  meter
     Y    =        2507721.74  meter          E    =           .0011744
     Z    =       -3580369.13                 I    =           51.66039
     XDOT =      -4898.733104                 Wp   =           58.00785
     YDOT =       3836.459437  meter/sec      RA   =          176.38285  deg
     ZDOT =      -4450.460625                 TA   =          164.13323
                                              MA   =          164.09641
                                              Ha   =            229.664  n.mi
                                              Hp   =            219.031
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17103848.44                 X    =         5202214.78
     Y    =        8227433.53  feet           Y    =         2565958.74  meter
     Z    =      -11746617.89                 Z    =        -3555071.80
     XDOT =     -16071.959001                 XDOT =       -4919.651735
     YDOT =      12586.809177  feet/sec       YDOT =        3781.561927  meter/sec
     ZDOT =     -14601.248769                 ZDOT =       -4474.306986
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11595678.94                 X    =        -3534362.94
     Y    =       15115260.76  feet           Y    =         4607131.48  meter
     Z    =      -11631184.29                 Z    =        -3545184.97
     XDOT =      -7916.413385                 XDOT =       -2412.922800
     YDOT =     -17380.803724  feet/sec       YDOT =       -5297.668975  meter/sec
     ZDOT =     -14710.390893                 ZDOT =       -4483.727144
  
  
    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   19350.50858993  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6382 177.4369 0007538  39.2886 320.8810 15.50130234  3530
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19350.50858993   =   yrday.fracday
    Element set:     906
    Inclination:       51.6382  deg
    RA of node:       177.4369  deg
    Eccentricity:     .0007538     
    Arg of perigee:    39.2886  deg
    Mean anomaly:     320.8810  deg
    Mean motion:   15.50130234  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             353
    Checksum:              322
 
 
    Coasting Arc #8 (Orbit 368)
    ---------------------------------------
 
    Vector Time (GMT): 2019/351/11:36:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5100785.15                 A    =         6794846.03  meter
     Y    =       -2298305.05  meter          E    =           .0016798
     Z    =        3838790.78                 I    =           51.69063
     XDOT =       4982.703185                 Wp   =           76.79966
     YDOT =      -4079.717037  meter/sec      RA   =          171.43044  deg
     ZDOT =       4166.610988                 TA   =          329.33993
                                              MA   =          329.43798
                                              Ha   =            229.745  n.mi
                                              Hp   =            218.909
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16734859.42                 X    =        -5093352.30
     Y    =       -7540370.88  feet           Y    =        -2355304.45  meter
     Z    =       12594457.96                 Z    =         3814031.10
     XDOT =      16347.451394                 XDOT =        5007.714530
     YDOT =     -13384.898416  feet/sec       YDOT =       -4023.857492  meter/sec
     ZDOT =      13669.983556                 ZDOT =        4190.875245
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10590461.65                 X    =         3227972.71
     Y    =      -15086039.93  feet           Y    =        -4598224.97  meter
     Z    =       12481450.45                 Z    =         3804346.10
     XDOT =       8961.014489                 XDOT =        2731.317216
     YDOT =      17724.206781  feet/sec       YDOT =        5402.338227  meter/sec
     ZDOT =      13781.061921                 ZDOT =        4200.467674
  
  
    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   19351.54008334  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6378 172.3255 0007343  42.7724 317.3997 15.50134307  3696
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19351.54008334   =   yrday.fracday
    Element set:     907
    Inclination:       51.6378  deg
    RA of node:       172.3255  deg
    Eccentricity:     .0007343     
    Arg of perigee:    42.7724  deg
    Mean anomaly:     317.3997  deg
    Mean motion:   15.50134307  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             369
    Checksum:              310
 
 
    Coasting Arc #9 (Orbit 383)
    ---------------------------------------
 
    Vector Time (GMT): 2019/352/11:36:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4976139.54                 A    =         6793949.85  meter
     Y    =        2143434.30  meter          E    =           .0014427
     Z    =       -4114970.96                 I    =           51.72046
     XDOT =      -5022.327221                 Wp   =           59.74327
     YDOT =       4315.217778  meter/sec      RA   =          166.47945  deg
     ZDOT =      -3828.611715                 TA   =          170.65325
                                              MA   =          170.62638
                                              Ha   =            229.759  n.mi
                                              Hp   =            218.829
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16325917.12                 X    =         4971789.32
     Y    =        7032264.78  feet           Y    =         2199057.01  meter
     Z    =      -13500560.91                 Z    =        -4090809.28
     XDOT =     -16477.451512                 XDOT =       -5051.610820
     YDOT =      14157.538641  feet/sec       YDOT =        4258.891126  meter/sec
     ZDOT =     -12561.062058                 ZDOT =       -3853.078945
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9759340.72                 X    =        -2974647.05
     Y    =       14956925.61  feet           Y    =         4558870.93  meter
     Z    =      -13390261.67                 Z    =        -4081351.76
     XDOT =     -10024.490098                 XDOT =       -3055.464582
     YDOT =     -17877.806570  feet/sec       YDOT =       -5449.155443  meter/sec
     ZDOT =     -12673.093973                 ZDOT =       -3862.759043
  
  
    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   19352.50710908  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6377 167.5335 0007504  47.5482 312.6302 15.50137109  3841
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19352.50710908   =   yrday.fracday
    Element set:     908
    Inclination:       51.6377  deg
    RA of node:       167.5335  deg
    Eccentricity:     .0007504     
    Arg of perigee:    47.5482  deg
    Mean anomaly:     312.6302  deg
    Mean motion:   15.50137109  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             384
    Checksum:              300
 
 
    Coasting Arc #10 (Orbit 399)
    ---------------------------------------
 
    Vector Time (GMT): 2019/353/11:36:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4825879.08                 A    =         6793125.87  meter
     Y    =       -1989642.02  meter          E    =           .0015100
     Z    =        4333284.32                 I    =           51.75044
     XDOT =       5045.930962                 Wp   =           83.79111
     YDOT =      -4595.063920  meter/sec      RA   =          161.53000  deg
     ZDOT =       3500.817611                 TA   =          330.63244
                                              MA   =          330.71721
                                              Ha   =            229.858  n.mi
                                              Hp   =            218.711
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15832936.61                 X    =        -4824320.29
     Y    =       -6527696.90  feet           Y    =        -2043599.98  meter
     Z    =       14216812.08                 Z    =         4309845.72
     XDOT =      16554.891606                 XDOT =        5079.934297
     YDOT =     -15075.669029  feet/sec       YDOT =       -4538.446860  meter/sec
     ZDOT =      11485.622082                 ZDOT =        3525.411080
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8926192.12                 X    =         2720703.36
     Y    =      -14718940.41  feet           Y    =        -4486333.04  meter
     Z    =       14109795.95                 Z    =         4300665.80
     XDOT =      11253.791548                 XDOT =        3430.155664
     YDOT =      17971.185615  feet/sec       YDOT =        5477.617375  meter/sec
     ZDOT =      11598.260153                 ZDOT =        3535.149695
  
  
    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   19353.53859985  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6381 162.4216 0007338  50.5654 309.6145 15.50139283  4003
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19353.53859985   =   yrday.fracday
    Element set:     909
    Inclination:       51.6381  deg
    RA of node:       162.4216  deg
    Eccentricity:     .0007338     
    Arg of perigee:    50.5654  deg
    Mean anomaly:     309.6145  deg
    Mean motion:   15.50139283  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             400
    Checksum:              316
 
 
    Coasting Arc #11 (Orbit 414)
    ---------------------------------------
 
    Vector Time (GMT): 2019/354/11:36:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4675429.66                 A    =         6792297.01  meter
     Y    =        1893569.82  meter          E    =           .0017189
     Z    =       -4565972.39                 I    =           51.77929
     XDOT =      -5015.766674                 Wp   =           63.99161
     YDOT =       4854.004734  meter/sec      RA   =          156.58267  deg
     ZDOT =      -3124.805665                 TA   =          174.67867
                                              MA   =          174.66037
                                              Ha   =            229.896  n.mi
                                              Hp   =            218.600
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15339336.15                 X    =         4676086.72
     Y    =        6212499.40  feet           Y    =         1945857.76  meter
     Z    =      -14980224.39                 Z    =        -4543259.15
     XDOT =     -16455.927409                 XDOT =       -5054.494195
     YDOT =      15925.212383  feet/sec       YDOT =        4797.698558  meter/sec
     ZDOT =     -10251.987090                 ZDOT =       -3149.264155
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8291785.24                 X    =        -2527336.14
     Y    =       14430292.25  feet           Y    =         4398353.08  meter
     Z    =      -14876507.26                 Z    =        -4534359.41
     XDOT =     -12447.319935                 XDOT =       -3793.943116
     YDOT =     -17830.668885  feet/sec       YDOT =       -5434.787876  meter/sec
     ZDOT =     -10364.038674                 ZDOT =       -3158.958988
  
  
    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   19354.50562238  .00016717  00000-0  10270-3 0  9101
    2 25544  51.6383 157.6299 0007641  55.8764 304.3110 15.50143100  4152
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19354.50562238   =   yrday.fracday
    Element set:     910
    Inclination:       51.6383  deg
    RA of node:       157.6299  deg
    Eccentricity:     .0007641     
    Arg of perigee:    55.8764  deg
    Mean anomaly:     304.3110  deg
    Mean motion:   15.50143100  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             415
    Checksum:              287
 
 
    Coasting Arc #12 (Orbit 430)
    ---------------------------------------
 
    Vector Time (GMT): 2019/355/11:36:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 957055.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4506436.94                 A    =         6791572.11  meter
     Y    =       -1803736.02  meter          E    =           .0013429
     Z    =        4738486.32                 I    =           51.80583
     XDOT =       4969.549615                 Wp   =           89.30081
     YDOT =      -5149.936863  meter/sec      RA   =          151.63659  deg
     ZDOT =       2759.238516                 TA   =          333.42435
                                              MA   =          333.49314
                                              Ha   =            229.999  n.mi
                                              Hp   =            218.504
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14784898.11                 X    =        -4508949.15
     Y    =       -5917769.10  feet           Y    =        -1854144.62  meter
     Z    =       15546214.97                 Z    =         4716589.39
     XDOT =      16304.296637                 XDOT =        5013.365454
     YDOT =     -16896.118317  feet/sec       YDOT =       -5094.119079  meter/sec
     ZDOT =       9052.619802                 ZDOT =        2783.484846
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7682831.34                 X    =         2341726.99
     Y    =      -14060105.49  feet           Y    =        -4285520.15  meter
     Z    =       15446214.41                 Z    =         4708006.15
     XDOT =      13770.652972                 XDOT =        4197.295026
     YDOT =      17615.708580  feet/sec       YDOT =        5369.267975  meter/sec
     ZDOT =       9163.737402                 ZDOT =        2793.107160
  
  
    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   19355.53711116  .00016717  00000-0  10270-3 0  9117
    2 25544  51.6370 152.5181 0007430  59.2814 300.9068 15.50138333  4316
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19355.53711116   =   yrday.fracday
    Element set:     911
    Inclination:       51.6370  deg
    RA of node:       152.5181  deg
    Eccentricity:     .0007430     
    Arg of perigee:    59.2814  deg
    Mean anomaly:     300.9068  deg
    Mean motion:   15.50138333  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             431
    Checksum:              277
 
 
    Coasting Arc #13 (Orbit 431)
    ---------------------------------------
 
    Vector Time (GMT): 2019/355/13:08:55.000
    Vector Time (MET): N/A
    Weight (LBS)     : 987055.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4676743.18                 A    =         6791893.78  meter
     Y    =       -1605650.83  meter          E    =           .0013993
     Z    =        4644063.01                 I    =           51.81094
     XDOT =       4746.879913                 Wp   =           89.96979
     YDOT =      -5248.717880  meter/sec      RA   =          151.32047  deg
     ZDOT =       2957.892667                 TA   =          330.60770
                                              MA   =          330.68633
                                              Ha   =            229.933  n.mi
                                              Hp   =            218.498
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15343645.60                 X    =        -4680999.12
     Y    =       -5267883.31  feet           Y    =        -1657973.66  meter
     Z    =       15236427.21                 Z    =         4621334.57
     XDOT =      15573.752996                 XDOT =        4790.851942
     YDOT =     -17220.203020  feet/sec       YDOT =       -5195.389292  meter/sec
     ZDOT =       9704.372267                 ZDOT =        2981.057715
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         762003.81                 X    =          232258.76
     Y    =      -16301843.76  feet           Y    =        -4968801.98  meter
     Z    =       15132614.09                 Z    =         4612420.78
     XDOT =      19665.239630                 XDOT =        5993.965039
     YDOT =      10049.689929  feet/sec       YDOT =        3063.145490  meter/sec
     ZDOT =       9810.553669                 ZDOT =        2990.256758
  
  
    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   19355.60157885  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6389 152.1983 0007293  60.6799 299.5079 15.50157663  4320
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19355.60157885   =   yrday.fracday
    Element set:     912
    Inclination:       51.6389  deg
    RA of node:       152.1983  deg
    Eccentricity:     .0007293     
    Arg of perigee:    60.6799  deg
    Mean anomaly:     299.5079  deg
    Mean motion:   15.50157663  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             432
    Checksum:              347
 
 
    Coasting Arc #14 (Orbit 440)
    ---------------------------------------
 
    Vector Time (GMT): 2019/356/04:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 987055.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         560224.02                 A    =         6789860.30  meter
     Y    =        4412944.26  meter          E    =           .0019811
     Z    =       -5146605.40                 I    =           51.82393
     XDOT =      -6933.341354                 Wp   =           87.18274
     YDOT =       2781.334781  meter/sec      RA   =          148.22349  deg
     ZDOT =       1636.524654                 TA   =          198.57719
                                              MA   =          198.64962
                                              Ha   =            229.949  n.mi
                                              Hp   =            218.447
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1838005.31                 X    =          535835.04
     Y    =       14478163.58  feet           Y    =         4419073.20  meter
     Z    =      -16885188.31                 Z    =        -5143942.84
     XDOT =     -22747.182919                 XDOT =       -6971.877124
     YDOT =       9125.114112  feet/sec       YDOT =        2703.585635  meter/sec
     ZDOT =       5369.175373                 ZDOT =        1602.751546
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5510229.27                 X    =         1679517.88
     Y    =      -13529062.52  feet           Y    =        -4123658.26  meter
     Z    =      -16873260.19                 Z    =        -5142969.71
     XDOT =      23316.434829                 XDOT =        7106.849336
     YDOT =       3019.082744  feet/sec       YDOT =         920.216420  meter/sec
     ZDOT =       5214.619269                 ZDOT =        1589.415953
  
  
    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   19356.18179226  .00016717  00000-0  10270-3 0  9131
    2 25544  51.6408 149.3280 0007638  59.0244 301.1656 15.50130330  4413
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19356.18179226   =   yrday.fracday
    Element set:     913
    Inclination:       51.6408  deg
    RA of node:       149.3280  deg
    Eccentricity:     .0007638     
    Arg of perigee:    59.0244  deg
    Mean anomaly:     301.1656  deg
    Mean motion:   15.50130330  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             441
    Checksum:              288
 
 
    Coasting Arc #15 (Orbit 456)
    ---------------------------------------
 
    Vector Time (GMT): 2019/357/04:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 987055.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -484011.20                 A    =         6790274.64  meter
     Y    =       -4548436.27  meter          E    =           .0013542
     Z    =        5010515.55                 I    =           51.85376
     XDOT =       6745.018515                 Wp   =           59.91502
     YDOT =      -3006.233290  meter/sec      RA   =          143.28028  deg
     ZDOT =      -2066.639255                 TA   =           50.18523
                                              MA   =           50.06611
                                              Ha   =            229.930  n.mi
                                              Hp   =            218.357
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1587963.25                 X    =         -457451.72
     Y    =      -14922691.19  feet           Y    =        -4553700.91  meter
     Z    =       16438699.31                 Z    =         5008228.37
     XDOT =      22129.325837                 XDOT =        6788.172430
     YDOT =      -9862.970112  feet/sec       YDOT =       -2930.564196  meter/sec
     ZDOT =      -6780.312515                 ZDOT =       -2033.769833
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5712866.26                 X    =        -1741281.64
     Y    =       13889083.96  feet           Y    =         4233392.79  meter
     Z    =       16428502.07                 Z    =         5007407.43
     XDOT =     -23168.780674                 XDOT =       -7061.844349
     YDOT =      -1645.873463  feet/sec       YDOT =        -501.662232  meter/sec
     ZDOT =      -6629.849029                 ZDOT =       -2020.777984
  
  
    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   19357.21327804  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6410 144.2171 0007601  61.9986 298.1933 15.50162595  4572
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19357.21327804   =   yrday.fracday
    Element set:     914
    Inclination:       51.6410  deg
    RA of node:       144.2171  deg
    Eccentricity:     .0007601     
    Arg of perigee:    61.9986  deg
    Mean anomaly:     298.1933  deg
    Mean motion:   15.50162595  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             457
    Checksum:              310
 
 
    Coasting Arc #16 (Orbit 471)
    ---------------------------------------
 
    Vector Time (GMT): 2019/358/04:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 987055.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         476730.11                 A    =         6790923.71  meter
     Y    =        4707891.01  meter          E    =           .0018287
     Z    =       -4886809.65                 I    =           51.88291
     XDOT =      -6497.424579                 Wp   =           91.43413
     YDOT =       3200.669454  meter/sec      RA   =          138.33873  deg
     ZDOT =       2457.134794                 TA   =          202.62598
                                              MA   =          202.70670
                                              Ha   =            230.011  n.mi
                                              Hp   =            218.313
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1564075.16                 X    =          447787.14
     Y    =       15445836.65  feet           Y    =         4713060.98  meter
     Z    =      -16032840.07                 Z    =        -4884563.52
     XDOT =     -21317.009775                 XDOT =       -6544.667930
     YDOT =      10500.884037  feet/sec       YDOT =        3127.746170  meter/sec
     ZDOT =       8061.465861                 ZDOT =        2425.458328
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5741204.49                 X    =         1749919.13
     Y    =      -14435341.49  feet           Y    =        -4399892.09  meter
     Z    =      -16022847.71                 Z    =        -4883763.98
     XDOT =      22748.657032                 XDOT =        6933.790663
     YDOT =        287.889967  feet/sec       YDOT =          87.748862  meter/sec
     ZDOT =       7916.418039                 ZDOT =        2412.924218
  
  
    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   19358.18029536  .00016717  00000-0  10270-3 0  9153
    2 25544  51.6420 139.4250 0007689  65.5685 294.6267 15.50138599  4724
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19358.18029536   =   yrday.fracday
    Element set:     915
    Inclination:       51.6420  deg
    RA of node:       139.4250  deg
    Eccentricity:     .0007689     
    Arg of perigee:    65.5685  deg
    Mean anomaly:     294.6267  deg
    Mean motion:   15.50138599  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             472
    Checksum:              341
 
 
    Coasting Arc #17 (Orbit 487)
    ---------------------------------------
 
    Vector Time (GMT): 2019/359/04:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 987055.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -454384.58                 A    =         6791552.69  meter
     Y    =       -4876454.46  meter          E    =           .0015646
     Z    =        4695726.46                 I    =           51.90923
     XDOT =       6269.251386                 Wp   =           66.49013
     YDOT =      -3358.397120  meter/sec      RA   =          133.40007  deg
     ZDOT =      -2867.368366                 TA   =           51.94631
                                              MA   =           51.80523
                                              Ha   =            230.004  n.mi
                                              Hp   =            218.223
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1490763.05                 X    =         -422630.08
     Y    =      -15998866.33  feet           Y    =        -4881358.87  meter
     Z    =       15405926.71                 Z    =         4693595.62
     XDOT =      20568.410060                 XDOT =        6320.268089
     YDOT =     -11018.363255  feet/sec       YDOT =       -3288.004232  meter/sec
     ZDOT =      -9407.376529                 ZDOT =       -2836.791314
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5811295.68                 X    =        -1771282.92
     Y    =       14990194.51  feet           Y    =         4569011.29  meter
     Z    =       15396479.70                 Z    =         4692847.01
     XDOT =     -22291.302340                 XDOT =       -6794.388953
     YDOT =        922.741904  feet/sec       YDOT =         281.251732  meter/sec
     ZDOT =      -9267.318922                 ZDOT =       -2824.678808
  
  
    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   19359.21177914  .00016717  00000-0  10270-3 0  9163
    2 25544  51.6417 134.3145 0007677  68.8854 291.3117 15.50168072  4882
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19359.21177914   =   yrday.fracday
    Element set:     916
    Inclination:       51.6417  deg
    RA of node:       134.3145  deg
    Eccentricity:     .0007677     
    Arg of perigee:    68.8854  deg
    Mean anomaly:     291.3117  deg
    Mean motion:   15.50168072  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             488
    Checksum:              329
 
 
    Coasting Arc #18 (Orbit 491)
    ---------------------------------------
 
    Vector Time (GMT): 2019/359/09:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 987055.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4880055.21                 A    =         6800830.30  meter
     Y    =        4688061.49  meter          E    =           .0020225
     Z    =         588119.38                 I    =           51.94127
     XDOT =      -2901.048715                 Wp   =           59.39688
     YDOT =      -3790.202009  meter/sec      RA   =          132.24786  deg
     ZDOT =       5997.645778                 TA   =          306.91634
                                              MA   =          307.10147
                                              Ha   =            230.023  n.mi
                                              Hp   =            218.280
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16010679.83                 X    =        -4934972.54
     Y    =       15380779.18  feet           Y    =         4633182.11  meter
     Z    =        1929525.53                 Z    =          564281.28
     XDOT =      -9517.876361                 XDOT =       -2887.583128
     YDOT =     -12435.045962  feet/sec       YDOT =       -3822.569222  meter/sec
     ZDOT =      19677.315544                 ZDOT =        5983.585715
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4922276.70                 X    =        -1500309.94
     Y    =      -21658517.03  feet           Y    =        -6601515.99  meter
     Z    =        1820202.65                 Z    =          554797.77
     XDOT =      14049.815265                 XDOT =        4282.383693
     YDOT =      -1502.959077  feet/sec       YDOT =        -458.101927  meter/sec
     ZDOT =      19613.239915                 ZDOT =        5978.115526
  
  
    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   19359.46965046  .00016717  00000-0  10270-3 0  9172
    2 25544  51.6377 133.0319 0007574  73.2246 286.9735 15.50137610  4922
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19359.46965046   =   yrday.fracday
    Element set:     917
    Inclination:       51.6377  deg
    RA of node:       133.0319  deg
    Eccentricity:     .0007574     
    Arg of perigee:    73.2246  deg
    Mean anomaly:     286.9735  deg
    Mean motion:   15.50137610  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             492
    Checksum:              328
 
 
    Coasting Arc #19 (Orbit 506)
    ---------------------------------------
 
    Vector Time (GMT): 2019/360/09:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 987055.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4673667.80                 A    =         6800422.03  meter
     Y    =       -4833465.40  meter          E    =           .0014625
     Z    =       -1005793.75                 I    =           51.96338
     XDOT =       2821.513278                 Wp   =          112.93547
     YDOT =       3945.990985  meter/sec      RA   =          127.31636  deg
     ZDOT =      -5926.089495                 TA   =           77.89139
                                              MA   =           77.72756
                                              Ha   =            229.998  n.mi
                                              Hp   =            218.173
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15333555.79                 X    =         4732255.22
     Y    =      -15857826.13  feet           Y    =        -4780873.40  meter
     Z    =       -3299848.28                 Z    =         -982949.45
     XDOT =       9256.933327                 XDOT =        2805.963802
     YDOT =      12946.164650  feet/sec       YDOT =        3977.457140  meter/sec
     ZDOT =     -19442.550837                 ZDOT =       -5912.420873
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6041457.64                 X    =         1841436.29
     Y    =       21231347.24  feet           Y    =         6471314.64  meter
     Z    =       -3195037.62                 Z    =         -973847.47
     XDOT =     -14357.698605                 XDOT =       -4376.226535
     YDOT =       1206.794408  feet/sec       YDOT =         367.830936  meter/sec
     ZDOT =     -19380.272653                 ZDOT =       -5907.107105
  
  
    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   19360.43666493  .00016717  00000-0  10270-3 0  9186
    2 25544  51.6391 128.2399 0007622  74.8643 285.3350 15.50181162  5078
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      19360.43666493   =   yrday.fracday
    Element set:     918
    Inclination:       51.6391  deg
    RA of node:       128.2399  deg
    Eccentricity:     .0007622     
    Arg of perigee:    74.8643  deg
    Mean anomaly:     285.3350  deg
    Mean motion:   15.50181162  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             507
    Checksum:              318
 
             

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