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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14248.1882
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   71.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.118
   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 
   ------------------------------------------------------------------------
   265/17:52:27.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.7  
   000/00:00:00.000           0.0               0.0              215.4  
   
   267/01:30:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.7  
   000/00:00:00.000           0.0               0.0              215.7  
   
   270/11:54:38.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.3  
   000/00:00:00.000           0.0               0.0              216.0  
   
   271/01:02:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.3  
   000/00:00:00.000           0.0               0.0              216.1  
   
   274/09:07:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.8  
   000/00:00:00.000           0.0               0.0              216.3  
   
   277/07:57:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.6  
   000/00:00:00.000           0.0               0.0              216.4  
   
 
 
    Coasting Arc #1 (Orbit 1348)
    ---------------------------------------
 
    Vector Time (GMT): 2018/264/12:03:24.619
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2611787.56                 A    =         6789418.99  meter
     Y    =        6053002.01  meter          E    =           .0015531
     Z    =        1585388.86                 I    =           51.27943
     XDOT =      -3985.690604                 Wp   =          131.38446
     YDOT =       3222.079650  meter/sec      RA   =          257.77713  deg
     ZDOT =      -5709.455164                 TA   =           31.17658
                                              MA   =           31.08453
                                              Ha   =            221.866  n.mi
                                              Hp   =            215.426
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8568856.82                 X    =         2536206.15
     Y    =       19858930.48  feet           Y    =         6081786.37  meter
     Z    =        5201407.01                 Z    =         1597891.86
     XDOT =     -13076.412742                 XDOT =       -3993.691162
     YDOT =      10571.127462  feet/sec       YDOT =        3177.463659  meter/sec
     ZDOT =     -18731.808280                 ZDOT =       -5728.835897
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8635066.37                 X    =        -2631968.23
     Y    =      -19815612.68  feet           Y    =        -6039798.75  meter
     Z    =        5256822.70                 Z    =         1602279.56
     XDOT =      11452.645850                 XDOT =        3490.766455
     YDOT =     -10005.877893  feet/sec       YDOT =       -3049.791582  meter/sec
     ZDOT =     -18819.091228                 ZDOT =       -5736.059006
  
  
    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   18264.53769407  .00016717  00000-0  10270-3 0  9009
    2 25544  51.6363 258.5570 0004017 190.7069 169.3998 15.53724827 13498
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18264.53769407   =   yrday.fracday
    Element set:     900
    Inclination:       51.6363  deg
    RA of node:       258.5570  deg
    Eccentricity:     .0004017     
    Arg of perigee:   190.7069  deg
    Mean anomaly:     169.3998  deg
    Mean motion:   15.53724827  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1349
    Checksum:              341
 
 
    Coasting Arc #2 (Orbit 1363)
    ---------------------------------------
 
    Vector Time (GMT): 2018/265/12:03:24.619
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2043523.60                 A    =         6790383.79  meter
     Y    =       -6472449.76  meter          E    =           .0008689
     Z    =         -45284.96                 I    =           51.29136
     XDOT =       4560.729810                 Wp   =           60.69593
     YDOT =      -1475.672249  meter/sec      RA   =          252.78407  deg
     ZDOT =       5980.981892                 TA   =          298.81420
                                              MA   =          298.90141
                                              Ha   =            221.871  n.mi
                                              Hp   =            215.422
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6704473.77                 X    =        -1970775.02
     Y    =      -21235071.40  feet           Y    =        -6494895.10  meter
     Z    =        -148572.69                 Z    =          -55034.28
     XDOT =      14963.024310                 XDOT =        4547.839854
     YDOT =      -4841.444386  feet/sec       YDOT =       -1424.742452  meter/sec
     ZDOT =      19622.644004                 ZDOT =        6003.105112
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7175015.08                 X    =         2186944.60
     Y    =       21080387.65  feet           Y    =         6425302.16  meter
     Z    =        -191610.75                 Z    =          -58402.96
     XDOT =     -13183.460285                 XDOT =       -4018.318695
     YDOT =       4646.228827  feet/sec       YDOT =        1416.170547  meter/sec
     ZDOT =      19722.036314                 ZDOT =        6011.276669
  
  
    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   18265.50248361  .00016717  00000-0  10270-3 0  9019
    2 25544  51.6365 253.7509 0004301 192.3770 167.7277 15.53763701 13645
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18265.50248361   =   yrday.fracday
    Element set:     901
    Inclination:       51.6365  deg
    RA of node:       253.7509  deg
    Eccentricity:     .0004301     
    Arg of perigee:   192.3770  deg
    Mean anomaly:     167.7277  deg
    Mean motion:   15.53763701  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1364
    Checksum:              308
 
 
    Coasting Arc #3 (Orbit 1367)
    ---------------------------------------
 
    Vector Time (GMT): 2018/265/17:52:27.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4241523.68                 A    =         6778654.20  meter
     Y    =         627631.02  meter          E    =           .0014322
     Z    =       -5262428.74                 I    =           51.25795
     XDOT =      -1909.028233                 Wp   =          110.90184
     YDOT =      -7386.971378  meter/sec      RA   =          251.56571  deg
     ZDOT =        654.091967                 TA   =          165.40609
                                              MA   =          165.36470
                                              Ha   =            221.722  n.mi
                                              Hp   =            215.449
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13915760.11                 X    =        -4222664.74
     Y    =        2059156.87  feet           Y    =          580304.23  meter
     Z    =      -17265186.17                 Z    =        -5282986.80
     XDOT =      -6263.215988                 XDOT =       -1829.460411
     YDOT =     -24235.470401  feet/sec       YDOT =       -7407.874494  meter/sec
     ZDOT =       2145.971019                 ZDOT =         645.012649
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1762658.05                 X    =         -537258.17
     Y    =      -13841477.85  feet           Y    =        -4218882.45  meter
     Z    =      -17357467.76                 Z    =        -5290556.17
     XDOT =      23354.535348                 XDOT =        7118.462374
     YDOT =      -5629.717593  feet/sec       YDOT =       -1715.937922  meter/sec
     ZDOT =       2106.030997                 ZDOT =         641.918248
  
  
    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   18265.75976082  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6403 252.4695 0003990 197.6950 162.4064 15.53730364 13680
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18265.75976082   =   yrday.fracday
    Element set:     902
    Inclination:       51.6403  deg
    RA of node:       252.4695  deg
    Eccentricity:     .0003990     
    Arg of perigee:   197.6950  deg
    Mean anomaly:     162.4064  deg
    Mean motion:   15.53730364  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1368
    Checksum:              329
 
 
    Coasting Arc #4 (Orbit 1383)
    ---------------------------------------
 
    Vector Time (GMT): 2018/266/17:52:27.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4641142.07                 A    =         6780281.76  meter
     Y    =         921211.45  meter          E    =           .0004350
     Z    =        4852455.04                 I    =           51.27492
     XDOT =       1053.885512                 Wp   =           91.37056
     YDOT =       7216.533103  meter/sec      RA   =          246.54604  deg
     ZDOT =      -2376.261908                 TA   =           22.03536
                                              MA   =           22.01666
                                              Ha   =            221.406  n.mi
                                              Hp   =            215.701
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15226844.08                 X    =         4606925.22
     Y    =        3022347.28  feet           Y    =          972921.19  meter
     Z    =       15920128.09                 Z    =         4874916.89
     XDOT =       3457.629632                 XDOT =         984.652539
     YDOT =      23676.289709  feet/sec       YDOT =        7227.930989  meter/sec
     ZDOT =      -7796.134868                 ZDOT =       -2371.311526
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3086362.40                 X    =         -940723.26
     Y    =       15107960.45  feet           Y    =         4604906.35  meter
     Z    =       16020790.87                 Z    =         4883137.06
     XDOT =     -22588.432095                 XDOT =       -6884.954103
     YDOT =       3635.943690  feet/sec       YDOT =        1108.235637  meter/sec
     ZDOT =      -7774.677938                 ZDOT =       -2369.721836
  
  
    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   18266.78886499  .00016717  00000-0  10270-3 0  9032
    2 25544  51.6400 247.3426 0003904 202.7723 157.3257 15.53758719 13842
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18266.78886499   =   yrday.fracday
    Element set:     903
    Inclination:       51.6400  deg
    RA of node:       247.3426  deg
    Eccentricity:     .0003904     
    Arg of perigee:   202.7723  deg
    Mean anomaly:     157.3257  deg
    Mean motion:   15.53758719  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1384
    Checksum:              338
 
 
    Coasting Arc #5 (Orbit 1388)
    ---------------------------------------
 
    Vector Time (GMT): 2018/267/01:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3930788.96                 A    =         6778592.38  meter
     Y    =       -1599581.99  meter          E    =           .0003906
     Z    =        5284816.99                 I    =           51.27058
     XDOT =       3104.625626                 Wp   =          165.22205
     YDOT =       7010.048129  meter/sec      RA   =          244.96685  deg
     ZDOT =       -191.101846                 TA   =          286.58695
                                              MA   =          286.62985
                                              Ha   =            221.685  n.mi
                                              Hp   =            215.717
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12896289.24                 X    =         3922712.89
     Y    =       -5247972.39  feet           Y    =        -1555669.68  meter
     Z    =       17338638.41                 Z    =         5303892.00
     XDOT =      10185.779614                 XDOT =        3026.934852
     YDOT =      22998.845567  feet/sec       YDOT =        7044.331787  meter/sec
     ZDOT =       -626.974562                 ZDOT =        -176.210201
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9460806.77                 X    =         2883653.90
     Y    =      -10068183.83  feet           Y    =        -3068782.43  meter
     Z    =       17424370.34                 Z    =         5310948.08
     XDOT =      18064.544706                 XDOT =        5506.073226
     YDOT =      16024.870380  feet/sec       YDOT =        4884.380492  meter/sec
     ZDOT =       -560.895898                 ZDOT =        -170.961070
  
  
    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   18267.11046221  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6376 245.7349 0004351 199.1875 160.9114 15.53704150 13891
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18267.11046221   =   yrday.fracday
    Element set:     904
    Inclination:       51.6376  deg
    RA of node:       245.7349  deg
    Eccentricity:     .0004351     
    Arg of perigee:   199.1875  deg
    Mean anomaly:     160.9114  deg
    Mean motion:   15.53704150  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1389
    Checksum:              307
 
 
    Coasting Arc #6 (Orbit 1403)
    ---------------------------------------
 
    Vector Time (GMT): 2018/268/01:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4581836.91                 A    =         6779749.15  meter
     Y    =          94841.55  meter          E    =           .0013011
     Z    =       -5007812.60                 I    =           51.29042
     XDOT =      -2276.387671                 Wp   =          124.35773
     YDOT =      -7048.250068  meter/sec      RA   =          239.94769  deg
     ZDOT =       1945.691549                 TA   =          164.66377
                                              MA   =          164.62430
                                              Ha   =            221.660  n.mi
                                              Hp   =            215.629
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15032273.34                 X    =        -4558231.48
     Y    =         311159.93  feet           Y    =           43735.61  meter
     Z    =      -16429831.35                 Z    =        -5030012.37
     XDOT =      -7468.463488                 XDOT =       -2206.854191
     YDOT =     -23124.180012  feet/sec       YDOT =       -7073.317178  meter/sec
     ZDOT =       6383.502458                 ZDOT =        1934.803383
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13341653.71                 X    =        -4066536.05
     Y    =        6692059.93  feet           Y    =         2039739.87  meter
     Z    =      -16529429.23                 Z    =        -5038170.03
     XDOT =     -16230.088783                 XDOT =       -4946.931061
     YDOT =     -16679.975099  feet/sec       YDOT =       -5084.056410  meter/sec
     ZDOT =       6335.369020                 ZDOT =        1931.020477
  
  
    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   18268.07524550  .00016717  00000-0  10270-3 0  9055
    2 25544  51.6383 240.9290 0004445 203.2275 156.8677 15.53732375 14042
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18268.07524550   =   yrday.fracday
    Element set:     905
    Inclination:       51.6383  deg
    RA of node:       240.9290  deg
    Eccentricity:     .0004445     
    Arg of perigee:   203.2275  deg
    Mean anomaly:     156.8677  deg
    Mean motion:   15.53732375  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1404
    Checksum:              311
 
 
    Coasting Arc #7 (Orbit 1419)
    ---------------------------------------
 
    Vector Time (GMT): 2018/269/01:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5097450.12                 A    =         6782703.45  meter
     Y    =        1309641.07  meter          E    =           .0007456
     Z    =        4271466.65                 I    =           51.31879
     XDOT =       1243.754618                 Wp   =           98.02542
     YDOT =       6694.661835  meter/sec      RA   =          234.93384  deg
     ZDOT =      -3532.581904                 TA   =           28.14583
                                              MA   =           28.10555
                                              Ha   =            221.484  n.mi
                                              Hp   =            215.922
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16723917.73                 X    =         5061677.76
     Y    =        4296722.67  feet           Y    =         1366444.82  meter
     Z    =       14013998.20                 Z    =         4296141.48
     XDOT =       4080.559771                 XDOT =        1185.960200
     YDOT =      21964.113632  feet/sec       YDOT =        6708.246768  meter/sec
     ZDOT =     -11589.835643                 ZDOT =       -3526.681336
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16804869.77                 X    =         5122124.31
     Y    =       -3554772.10  feet           Y    =        -1083494.54  meter
     Z    =       14124565.22                 Z    =         4305167.48
     XDOT =      13240.820104                 XDOT =        4035.801968
     YDOT =      16590.848270  feet/sec       YDOT =        5056.890553  meter/sec
     ZDOT =     -11564.027306                 ZDOT =       -3524.715523
  
  
    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   18269.10434642  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6396 235.8012 0004407 206.1875 153.9055 15.53701778 14206
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18269.10434642   =   yrday.fracday
    Element set:     906
    Inclination:       51.6396  deg
    RA of node:       235.8012  deg
    Eccentricity:     .0004407     
    Arg of perigee:   206.1875  deg
    Mean anomaly:     153.9055  deg
    Mean motion:   15.53701778  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1420
    Checksum:              303
 
 
    Coasting Arc #8 (Orbit 1434)
    ---------------------------------------
 
    Vector Time (GMT): 2018/270/01:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 909660.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5442755.13                 A    =         6786196.99  meter
     Y    =       -2534128.95  meter          E    =           .0003595
     Z    =       -3168624.50                 I    =           51.35084
     XDOT =        -11.533151                 Wp   =          141.97722
     YDOT =      -5973.393265  meter/sec      RA   =          229.93101  deg
     ZDOT =       4797.208412                 TA   =          181.32114
                                              MA   =          181.32209
                                              Ha   =            221.444  n.mi
                                              Hp   =            215.969
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17856808.16                 X    =        -5398621.56
     Y    =       -8314071.37  feet           Y    =        -2594747.22  meter
     Z    =      -10395749.68                 Z    =        -3194956.39
     XDOT =        -37.838423                 XDOT =          31.961218
     YDOT =     -19597.746933  feet/sec       YDOT =       -5973.278484  meter/sec
     ZDOT =      15738.872744                 ZDOT =        4797.258727
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19618049.13                 X    =        -5979581.37
     Y    =         810256.42  feet           Y    =          246966.16  meter
     Z    =      -10513639.94                 Z    =        -3204557.46
     XDOT =      -9091.573993                 XDOT =       -2771.111753
     YDOT =     -15898.973708  feet/sec       YDOT =       -4846.007186  meter/sec
     ZDOT =      15739.681205                 ZDOT =        4797.454831
  
  
    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   18270.06912444  .00016717  00000-0  10270-3 0  9072
    2 25544  51.6399 230.9951 0004274 212.0098 148.0796 15.53709750 14353
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18270.06912444   =   yrday.fracday
    Element set:     907
    Inclination:       51.6399  deg
    RA of node:       230.9951  deg
    Eccentricity:     .0004274     
    Arg of perigee:   212.0098  deg
    Mean anomaly:     148.0796  deg
    Mean motion:   15.53709750  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1435
    Checksum:              319
 
 
    Coasting Arc #9 (Orbit 1441)
    ---------------------------------------
 
    Vector Time (GMT): 2018/270/11:54:38.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         399521.86                 A    =         6783242.58  meter
     Y    =        5365315.99  meter          E    =           .0004946
     Z    =       -4134933.71                 I    =           51.34820
     XDOT =      -6233.260003                 Wp   =           97.43171
     YDOT =      -2418.183460  meter/sec      RA   =          227.81385  deg
     ZDOT =      -3744.484351                 TA   =          133.85539
                                              MA   =          133.81451
                                              Ha   =            221.251  n.mi
                                              Hp   =            216.043
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1310767.27                 X    =          359581.35
     Y    =       17602742.75  feet           Y    =         5369559.94  meter
     Z    =      -13566055.47                 Z    =        -4133090.54
     XDOT =     -20450.328095                 XDOT =       -6187.566925
     YDOT =      -7933.672770  feet/sec       YDOT =       -2487.633029  meter/sec
     ZDOT =     -12285.053646                 ZDOT =       -3774.652571
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2626899.90                 X    =         -800679.09
     Y    =      -17460934.74  feet           Y    =        -5322092.91  meter
     Z    =      -13558306.65                 Z    =        -4132571.87
     XDOT =      19599.375869                 XDOT =        5973.889765
     YDOT =       6684.132719  feet/sec       YDOT =        2037.323653  meter/sec
     ZDOT =     -12420.172060                 ZDOT =       -3785.668444
  
  
    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   18270.51935405  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6378 228.7550 0003823 215.8494 144.2402 15.53733689 14428
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18270.51935405   =   yrday.fracday
    Element set:     908
    Inclination:       51.6378  deg
    RA of node:       228.7550  deg
    Eccentricity:     .0003823     
    Arg of perigee:   215.8494  deg
    Mean anomaly:     144.2402  deg
    Mean motion:   15.53733689  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1442
    Checksum:              317
 
 
    Coasting Arc #10 (Orbit 1450)
    ---------------------------------------
 
    Vector Time (GMT): 2018/271/01:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -436902.57                 A    =         6782721.60  meter
     Y    =       -5259159.87  meter          E    =           .0009562
     Z    =        4259007.05                 I    =           51.36109
     XDOT =       6369.470199                 Wp   =          132.74452
     YDOT =       2360.170503  meter/sec      RA   =          225.07382  deg
     ZDOT =       3556.349800                 TA   =          280.77312
                                              MA   =          280.88075
                                              Ha   =            221.309  n.mi
                                              Hp   =            216.080
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1433407.37                 X    =         -398749.06
     Y    =      -17254461.52  feet           Y    =        -5263831.85  meter
     Z    =       13973120.24                 Z    =         4256977.90
     XDOT =      20897.211939                 XDOT =        6325.329561
     YDOT =       7743.341546  feet/sec       YDOT =        2431.151896  meter/sec
     ZDOT =      11667.814305                 ZDOT =        3587.183537
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7746458.47                 X    =        -2361120.54
     Y    =      -15492051.49  feet           Y    =        -4721977.30  meter
     Z    =       13964523.26                 Z    =         4256386.69
     XDOT =      21079.004522                 XDOT =        6424.880578
     YDOT =        135.695764  feet/sec       YDOT =          41.360069  meter/sec
     ZDOT =      11805.931476                 ZDOT =        3598.447914
  
  
    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   18271.09821932  .00016717  00000-0  10270-3 0  9099
    2 25544  51.6399 225.8678 0004404 214.9521 145.1342 15.53760303 14513
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18271.09821932   =   yrday.fracday
    Element set:     909
    Inclination:       51.6399  deg
    RA of node:       225.8678  deg
    Eccentricity:     .0004404     
    Arg of perigee:   214.9521  deg
    Mean anomaly:     145.1342  deg
    Mean motion:   15.53760303  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1451
    Checksum:              306
 
 
    Coasting Arc #11 (Orbit 1465)
    ---------------------------------------
 
    Vector Time (GMT): 2018/272/01:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -871412.36                 A    =         6779838.44  meter
     Y    =        4495456.96  meter          E    =           .0009618
     Z    =       -5008073.91                 I    =           51.37626
     XDOT =      -6548.419710                 Wp   =           90.90100
     YDOT =      -3455.433130  meter/sec      RA   =          220.06596  deg
     ZDOT =      -1965.733758                 TA   =          159.94357
                                              MA   =          159.90574
                                              Ha   =            221.184  n.mi
                                              Hp   =            216.181
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2858964.44                 X    =         -897290.02
     Y    =       14748874.55  feet           Y    =         4485567.12  meter
     Z    =      -16430688.69                 Z    =        -5012370.23
     XDOT =     -21484.316635                 XDOT =       -6499.744731
     YDOT =     -11336.722866  feet/sec       YDOT =       -3528.390106  meter/sec
     ZDOT =      -6449.257736                 ZDOT =       -1997.425771
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3102470.84                 X    =          945633.11
     Y    =       14677520.83  feet           Y    =         4473708.35  meter
     Z    =      -16450397.13                 Z    =        -5014081.05
     XDOT =     -23076.989492                 XDOT =       -7033.866397
     YDOT =      -2496.769183  feet/sec       YDOT =        -761.015247  meter/sec
     ZDOT =      -6591.136247                 ZDOT =       -2008.978328
  
  
    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   18272.06299481  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6407 221.0621 0004340 219.0970 140.9869 15.53733140 14664
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18272.06299481   =   yrday.fracday
    Element set:     910
    Inclination:       51.6407  deg
    RA of node:       221.0621  deg
    Eccentricity:     .0004340     
    Arg of perigee:   219.0970  deg
    Mean anomaly:     140.9869  deg
    Mean motion:   15.53733140  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1466
    Checksum:              295
 
 
    Coasting Arc #12 (Orbit 1481)
    ---------------------------------------
 
    Vector Time (GMT): 2018/273/01:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2229978.93                 A    =         6778385.27  meter
     Y    =       -3598617.49  meter          E    =           .0003627
     Z    =        5294265.18                 I    =           51.39803
     XDOT =       6370.055903                 Wp   =          187.63633
     YDOT =       4263.248687  meter/sec      RA   =          215.05340  deg
     ZDOT =        211.195379                 TA   =          260.32347
                                              MA   =          260.36444
                                              Ha   =            220.951  n.mi
                                              Hp   =            216.240
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7316203.83                 X    =         2244336.73
     Y    =      -11806487.84  feet           Y    =        -3573599.71  meter
     Z    =       17369636.42                 Z    =         5305132.93
     XDOT =      20899.133541                 XDOT =        6320.883740
     YDOT =      13987.036374  feet/sec       YDOT =        4334.208146  meter/sec
     ZDOT =        692.898225                 ZDOT =         242.019742
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1900268.79                 X    =          579201.93
     Y    =      -13696729.86  feet           Y    =        -4174763.26  meter
     Z    =       17418749.45                 Z    =         5309234.83
     XDOT =      23738.276686                 XDOT =        7235.426734
     YDOT =       4364.625636  feet/sec       YDOT =        1330.337894  meter/sec
     ZDOT =        830.824760                 ZDOT =         253.235387
  
  
    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   18273.09208285  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6408 215.9348 0004240 223.4724 136.6094 15.53779625 14826
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18273.09208285   =   yrday.fracday
    Element set:     911
    Inclination:       51.6408  deg
    RA of node:       215.9348  deg
    Eccentricity:     .0004240     
    Arg of perigee:   223.4724  deg
    Mean anomaly:     136.6094  deg
    Mean motion:   15.53779625  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1482
    Checksum:              314
 
 
    Coasting Arc #13 (Orbit 1496)
    ---------------------------------------
 
    Vector Time (GMT): 2018/274/01:02:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3588162.37                 A    =         6779179.67  meter
     Y    =        2641350.21  meter          E    =           .0011817
     Z    =       -5119687.70                 I    =           51.42789
     XDOT =      -5769.860654                 Wp   =          118.96344
     YDOT =      -4785.410259  meter/sec      RA   =          210.04356  deg
     ZDOT =       1572.099722                 TA   =          166.27325
                                              MA   =          166.24109
                                              Ha   =            220.933  n.mi
                                              Hp   =            216.159
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11772186.26                 X    =        -3592562.89
     Y    =        8665847.15  feet           Y    =         2601200.06  meter
     Z    =      -16796875.67                 Z    =        -5137128.82
     XDOT =     -18929.989022                 XDOT =       -5723.556582
     YDOT =     -15700.164891  feet/sec       YDOT =       -4849.673871  meter/sec
     ZDOT =       5157.807486                 ZDOT =        1544.184006
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7024348.06                 X    =        -2141021.29
     Y    =       12715955.62  feet           Y    =         3875823.27  meter
     Z    =      -16875405.63                 Z    =        -5143623.64
     XDOT =     -22836.112555                 XDOT =       -6960.447107
     YDOT =      -5923.142646  feet/sec       YDOT =       -1805.373878  meter/sec
     ZDOT =       5032.963912                 ZDOT =        1534.047400
  
  
    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   18274.05685279  .00016717  00000-0  10270-3 0  9124
    2 25544  51.6403 211.1297 0004158 225.9421 134.1389 15.53770459 14973
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18274.05685279   =   yrday.fracday
    Element set:     912
    Inclination:       51.6403  deg
    RA of node:       211.1297  deg
    Eccentricity:     .0004158     
    Arg of perigee:   225.9421  deg
    Mean anomaly:     134.1389  deg
    Mean motion:   15.53770459  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1497
    Checksum:              321
 
 
    Coasting Arc #14 (Orbit 1502)
    ---------------------------------------
 
    Vector Time (GMT): 2018/274/09:07:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5513248.50                 A    =         6789943.84  meter
     Y    =       -3839826.67  meter          E    =           .0009514
     Z    =         950860.35                 I    =           51.46988
     XDOT =       3446.325605                 Wp   =           58.05470
     YDOT =      -3477.744816  meter/sec      RA   =          208.38540  deg
     ZDOT =       5899.823403                 TA   =          312.26434
                                              MA   =          312.34498
                                              Ha   =            220.845  n.mi
                                              Hp   =            216.286
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18088085.63                 X    =        -5474519.57
     Y    =      -12597856.53  feet           Y    =        -3901263.05  meter
     Z    =        3119620.56                 Z    =          924172.76
     XDOT =      11306.842535                 XDOT =        3456.299955
     YDOT =     -11409.923937  feet/sec       YDOT =       -3439.149604  meter/sec
     ZDOT =      19356.375994                 ZDOT =        5916.589050
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7985930.34                 X    =         2434111.57
     Y    =       20563088.75  feet           Y    =         6267629.45  meter
     Z    =        3000193.49                 Z    =          914458.98
     XDOT =     -14144.173849                 XDOT =       -4311.144189
     YDOT =       2638.745494  feet/sec       YDOT =         804.289627  meter/sec
     ZDOT =      19431.955565                 ZDOT =        5922.860056
  
  
    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   18274.44275797  .00016717  00000-0  10270-3 0  9138
    2 25544  51.6366 209.2095 0003988 228.4583 131.6228 15.53795519 15038
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18274.44275797   =   yrday.fracday
    Element set:     913
    Inclination:       51.6366  deg
    RA of node:       209.2095  deg
    Eccentricity:     .0003988     
    Arg of perigee:   228.4583  deg
    Mean anomaly:     131.6228  deg
    Mean motion:   15.53795519  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1503
    Checksum:              340
 
 
    Coasting Arc #15 (Orbit 1517)
    ---------------------------------------
 
    Vector Time (GMT): 2018/275/09:07:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4734170.32                 A    =         6787901.01  meter
     Y    =        4187441.83  meter          E    =           .0005915
     Z    =       -2466703.00                 I    =           51.49310
     XDOT =      -4945.988901                 Wp   =          171.39555
     YDOT =       2466.020444  meter/sec      RA   =          203.40276  deg
     ZDOT =      -5313.586305                 TA   =           36.28924
                                              MA   =           36.24914
                                              Ha   =            220.777  n.mi
                                              Hp   =            216.427
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15532054.84                 X    =         4698975.38
     Y    =       13738326.20  feet           Y    =         4240185.73  meter
     Z    =       -8092857.60                 Z    =        -2443791.46
     XDOT =     -16226.997708                 XDOT =       -4947.386188
     YDOT =       8090.618254  feet/sec       YDOT =        2410.702963  meter/sec
     ZDOT =     -17433.025935                 ZDOT =       -5337.615909
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5601371.32                 X    =        -1707297.98
     Y    =      -20006472.30  feet           Y    =        -6097972.76  meter
     Z    =       -7990393.24                 Z    =        -2435471.86
     XDOT =      16459.690379                 XDOT =        5016.913628
     YDOT =       2387.614658  feet/sec       YDOT =         727.744948  meter/sec
     ZDOT =     -17541.128539                 ZDOT =       -5346.535979
  
  
    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   18275.40752481  .00016717  00000-0  10270-3 0  9146
    2 25544  51.6374 204.4021 0003783 235.5576 124.5219 15.53754296 15181
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18275.40752481   =   yrday.fracday
    Element set:     914
    Inclination:       51.6374  deg
    RA of node:       204.4021  deg
    Eccentricity:     .0003783     
    Arg of perigee:   235.5576  deg
    Mean anomaly:     124.5219  deg
    Mean motion:   15.53754296  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1518
    Checksum:              311
 
 
    Coasting Arc #16 (Orbit 1533)
    ---------------------------------------
 
    Vector Time (GMT): 2018/276/09:07:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 943739.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3625087.22                 A    =         6784463.22  meter
     Y    =       -4342362.19  meter          E    =           .0008836
     Z    =        3741507.59                 I    =           51.51296
     XDOT =       6200.167797                 Wp   =          111.15555
     YDOT =      -1500.628258  meter/sec      RA   =          198.41620  deg
     ZDOT =       4254.382222                 TA   =          293.65745
                                              MA   =          293.75017
                                              Ha   =            220.612  n.mi
                                              Hp   =            216.460
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11893330.78                 X    =        -3594434.66
     Y    =      -14246595.12  feet           Y    =        -4382728.88  meter
     Z    =       12275287.37                 Z    =         3723972.72
     XDOT =      20341.757863                 XDOT =        6195.821773
     YDOT =      -4923.321056  feet/sec       YDOT =       -1431.317798  meter/sec
     ZDOT =      13957.946922                 ZDOT =        4284.490155
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2612800.62                 X    =          796381.63
     Y    =       18425714.72  feet           Y    =         5616157.85  meter
     Z    =       12196957.80                 Z    =         3717632.74
     XDOT =     -18438.893939                 XDOT =       -5620.174873
     YDOT =      -6738.989027  feet/sec       YDOT =       -2054.043855  meter/sec
     ZDOT =      14093.265060                 ZDOT =        4295.627190
  
  
    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   18276.43660152  .00016717  00000-0  10270-3 0  9154
    2 25544  51.6377 199.2755 0003917 239.7645 120.3120 15.53787714 15345
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18276.43660152   =   yrday.fracday
    Element set:     915
    Inclination:       51.6377  deg
    RA of node:       199.2755  deg
    Eccentricity:     .0003917     
    Arg of perigee:   239.7645  deg
    Mean anomaly:     120.3120  deg
    Mean motion:   15.53787714  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1534
    Checksum:              323
 
 
    Coasting Arc #17 (Orbit 1547)
    ---------------------------------------
 
    Vector Time (GMT): 2018/277/07:57:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928631.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6210762.08                 A    =         6787324.35  meter
     Y    =         663922.01  meter          E    =           .0001300
     Z    =       -2654887.91                 I    =           51.55161
     XDOT =      -2747.149315                 Wp   =           35.44628
     YDOT =      -4913.850353  meter/sec      RA   =          193.62118  deg
     ZDOT =       5200.078072                 TA   =          294.58829
                                              MA   =          294.60183
                                              Ha   =            220.553  n.mi
                                              Hp   =            216.397
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20376516.02                 X    =        -6204828.57
     Y    =        2178221.81  feet           Y    =          594501.98  meter
     Z    =       -8710262.16                 Z    =        -2685043.34
     XDOT =      -9012.957071                 XDOT =       -2717.256408
     YDOT =     -16121.556275  feet/sec       YDOT =       -4944.403432  meter/sec
     ZDOT =      17060.623597                 ZDOT =        5186.806234
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15084191.63                 X    =         4597661.61
     Y    =       13785349.64  feet           Y    =         4201774.57  meter
     Z    =       -8845734.59                 Z    =        -2696179.90
     XDOT =      -5033.575596                 XDOT =       -1534.233842
     YDOT =      16412.479737  feet/sec       YDOT =        5002.523824  meter/sec
     ZDOT =      17001.473032                 ZDOT =        5182.048980
  
  
    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   18277.33704292  .00016717  00000-0  10270-3 0  9169
    2 25544  51.6366 194.7893 0003707 243.0096 117.0679 15.53757861 15488
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18277.33704292   =   yrday.fracday
    Element set:     916
    Inclination:       51.6366  deg
    RA of node:       194.7893  deg
    Eccentricity:     .0003707     
    Arg of perigee:   243.0096  deg
    Mean anomaly:     117.0679  deg
    Mean motion:   15.53757861  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1548
    Checksum:              341
 
 
    Coasting Arc #18 (Orbit 1563)
    ---------------------------------------
 
    Vector Time (GMT): 2018/278/07:57:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928631.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6682531.59                 A    =         6789728.98  meter
     Y    =          86744.74  meter          E    =           .0011820
     Z    =        1158709.64                 I    =           51.59304
     XDOT =        958.633972                 Wp   =          137.08783
     YDOT =       4848.767899  meter/sec      RA   =          188.64419  deg
     ZDOT =      -5864.882500                 TA   =           30.32044
                                              MA   =           30.25211
                                              Ha   =            220.358  n.mi
                                              Hp   =            216.478
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21924316.24                 X    =         6675436.52
     Y    =         284595.61  feet           Y    =          161433.87  meter
     Z    =        3801540.81                 Z    =         1191153.88
     XDOT =       3145.124580                 XDOT =         932.831018
     YDOT =      15908.031165  feet/sec       YDOT =        4859.343258  meter/sec
     ZDOT =     -19241.740487                 ZDOT =       -5860.288846
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14568528.84                 X    =        -4440487.59
     Y    =      -16351929.40  feet           Y    =        -4984068.08  meter
     Z    =        3947242.35                 Z    =         1203119.47
     XDOT =       8336.769281                 XDOT =        2541.047277
     YDOT =     -12087.892101  feet/sec       YDOT =       -3684.389512  meter/sec
     ZDOT =     -19221.544556                 ZDOT =       -5858.726781
  
  
    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   18278.36611453  .00016717  00000-0  10270-3 0  9170
    2 25544  51.6374 189.6615 0003786 249.0913 110.9834 15.53780819 15645
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18278.36611453   =   yrday.fracday
    Element set:     917
    Inclination:       51.6374  deg
    RA of node:       189.6615  deg
    Eccentricity:     .0003786     
    Arg of perigee:   249.0913  deg
    Mean anomaly:     110.9834  deg
    Mean motion:   15.53780819  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1564
    Checksum:              339
 
 
    Coasting Arc #19 (Orbit 1579)
    ---------------------------------------
 
    Vector Time (GMT): 2018/279/07:57:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928631.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6727764.54                 A    =         6790208.12  meter
     Y    =        -770264.42  meter          E    =           .0009319
     Z    =         426319.29                 I    =           51.62839
     XDOT =        921.466526                 Wp   =           41.12594
     YDOT =      -4694.740118  meter/sec      RA   =          183.67415  deg
     ZDOT =       5991.711309                 TA   =          323.47080
                                              MA   =          323.53432
                                              Ha   =            220.304  n.mi
                                              Hp   =            216.529
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22072718.30                 X    =        -6720722.05
     Y    =       -2527114.25  feet           Y    =         -845459.54  meter
     Z    =        1398685.33                 Z    =          393655.22
     XDOT =       3023.184141                 XDOT =         944.791253
     YDOT =     -15402.690677  feet/sec       YDOT =       -4684.304608  meter/sec
     ZDOT =      19657.845501                 ZDOT =        5996.244622
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13345162.92                 X    =         4067605.66
     Y    =       17773197.34  feet           Y    =         5417270.55  meter
     Z    =        1252039.72                 Z    =          381621.71
     XDOT =     -11877.021184                 XDOT =       -3620.116057
     YDOT =       7514.234479  feet/sec       YDOT =        2290.338669  meter/sec
     ZDOT =      19678.623268                 ZDOT =        5998.044372
  
  
    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   18279.39518044  .00016717  00000-0  10270-3 0  9187
    2 25544  51.6381 184.5346 0003818 250.6963 109.3777 15.53805301 15807
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18279.39518044   =   yrday.fracday
    Element set:     918
    Inclination:       51.6381  deg
    RA of node:       184.5346  deg
    Eccentricity:     .0003818     
    Arg of perigee:   250.6963  deg
    Mean anomaly:     109.3777  deg
    Mean motion:   15.53805301  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1580
    Checksum:              328
 
             

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