Return to Human Space Flight home page

    
   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  21814.1409
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   70.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.049
   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 
   ------------------------------------------------------------------------
   320/18:14:08.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.7  
   000/00:00:00.000           0.0               0.0              213.3  
   
   321/09:01:23.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              213.4  
   
   322/19:30:01.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              213.2  
   
   323/10:20:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.0  
   000/00:00:00.000           0.0               0.0              213.0  
   
   325/21:45:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.9  
   000/00:00:00.000           0.0               0.0              213.1  
   
   331/13:15:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.0  
   000/00:00:00.000           0.0               0.0              212.9  
   
 
 
    Coasting Arc #1 (Orbit 2219)
    ---------------------------------------
 
    Vector Time (GMT): 2018/320/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902349.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5220617.29                 A    =         6782696.72  meter
     Y    =        1466331.39  meter          E    =           .0014568
     Z    =        4061078.25                 I    =           51.50341
     XDOT =      -4403.639115                 Wp   =           86.56746
     YDOT =       4962.754681  meter/sec      RA   =          339.13043  deg
     ZDOT =       3857.986311                 TA   =          323.42134
                                              MA   =          323.52074
                                              Ha   =            222.910  n.mi
                                              Hp   =            213.274
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17128009.50                 X    =         5184105.53
     Y    =        4810798.53  feet           Y    =         1524507.76  meter
     Z    =       13323747.54                 Z    =         4086349.87
     XDOT =     -14447.634893                 XDOT =       -4477.547043
     YDOT =      16282.003546  feet/sec       YDOT =        4913.096829  meter/sec
     ZDOT =      12657.435405                 ZDOT =        3836.415238
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13786524.65                 X    =        -4202132.71
     Y    =       11108967.60  feet           Y    =         3386013.32  meter
     Z    =       13437161.81                 Z    =         4095646.92
     XDOT =      -4056.225372                 XDOT =       -1236.337493
     YDOT =     -20269.551380  feet/sec       YDOT =       -6178.159261  meter/sec
     ZDOT =      12559.737385                 ZDOT =        3828.207955
  
  
    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   18320.55531318  .00016717  00000-0  10270-3 0  9002
    2 25544  51.6400 339.4281 0005316  53.7842 306.3801 15.53958858 22206
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18320.55531318   =   yrday.fracday
    Element set:     900
    Inclination:       51.6400  deg
    RA of node:       339.4281  deg
    Eccentricity:     .0005316     
    Arg of perigee:    53.7842  deg
    Mean anomaly:     306.3801  deg
    Mean motion:   15.53958858  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2220
    Checksum:              292
 
 
    Coasting Arc #2 (Orbit 2223)
    ---------------------------------------
 
    Vector Time (GMT): 2018/320/18:14:08.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902349.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4139764.85                 A    =         6779871.33  meter
     Y    =        2423058.29  meter          E    =           .0010290
     Z    =        4782653.39                 I    =           51.48654
     XDOT =      -5638.209489                 Wp   =           91.80997
     YDOT =       4519.429364  meter/sec      RA   =          337.82909  deg
     ZDOT =       2585.484296                 TA   =          332.66053
                                              MA   =          332.71464
                                              Ha   =            222.736  n.mi
                                              Hp   =            213.344
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13581905.69                 X    =         4089129.94
     Y    =        7949666.30  feet           Y    =         2469068.85  meter
     Z    =       15691120.05                 Z    =         4802640.24
     XDOT =     -18498.062627                 XDOT =       -5700.887053
     YDOT =      14827.524159  feet/sec       YDOT =        4456.028508  meter/sec
     ZDOT =       8482.560027                 ZDOT =        2557.943275
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7317625.64                 X    =         2230412.30
     Y    =       13831142.71  feet           Y    =         4215732.30  meter
     Z    =       15780635.32                 Z    =         4809937.64
     XDOT =     -22563.179008                 XDOT =       -6877.256962
     YDOT =       2382.215588  feet/sec       YDOT =         726.099311  meter/sec
     ZDOT =       8358.087339                 ZDOT =        2547.545021
  
  
    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   18320.81254693  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6403 338.1474 0005053  51.4587 308.7017 15.53998777 22241
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18320.81254693   =   yrday.fracday
    Element set:     901
    Inclination:       51.6403  deg
    RA of node:       338.1474  deg
    Eccentricity:     .0005053     
    Arg of perigee:    51.4587  deg
    Mean anomaly:     308.7017  deg
    Mean motion:   15.53998777  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2224
    Checksum:              315
 
 
    Coasting Arc #3 (Orbit 2232)
    ---------------------------------------
 
    Vector Time (GMT): 2018/321/09:01:23.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902349.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1408804.65                 A    =         6777934.02  meter
     Y    =       -4003915.03  meter          E    =           .0018841
     Z    =       -5300469.24                 I    =           51.46057
     XDOT =       7038.653260                 Wp   =           83.70600
     YDOT =      -2983.154240  meter/sec      RA   =          334.72739  deg
     ZDOT =        385.851926                 TA   =          189.97035
                                              MA   =          190.00779
                                              Ha   =            222.891  n.mi
                                              Hp   =            213.352
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4622062.48                 X    =        -1338179.78
     Y    =      -13136204.15  feet           Y    =        -4019274.35  meter
     Z    =      -17389990.95                 Z    =        -5307141.30
     XDOT =      23092.694421                 XDOT =        7069.614302
     YDOT =      -9787.251442  feet/sec       YDOT =       -2904.270015  meter/sec
     ZDOT =       1265.918392                 ZDOT =         420.118952
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6896515.08                 X    =         2102057.80
     Y    =       12055582.91  feet           Y    =         3674541.67  meter
     Z    =      -17419417.52                 Z    =        -5309438.46
     XDOT =     -19952.050383                 XDOT =       -6081.384957
     YDOT =      13450.976250  feet/sec       YDOT =        4099.857561  meter/sec
     ZDOT =       1420.403180                 ZDOT =         432.938889
  
  
    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   18321.39132369  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6403 335.2616 0004867  55.1622 304.9987 15.53952654 22338
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18321.39132369   =   yrday.fracday
    Element set:     902
    Inclination:       51.6403  deg
    RA of node:       335.2616  deg
    Eccentricity:     .0004867     
    Arg of perigee:    55.1622  deg
    Mean anomaly:     304.9987  deg
    Mean motion:   15.53952654  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2233
    Checksum:              312
 
 
    Coasting Arc #4 (Orbit 2248)
    ---------------------------------------
 
    Vector Time (GMT): 2018/322/09:01:23.000
    Vector Time (MET): N/A
    Weight (LBS)     : 902349.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -202286.21                 A    =         6779412.58  meter
     Y    =        4656938.63  meter          E    =           .0011488
     Z    =        4916363.03                 I    =           51.43705
     XDOT =      -7047.835518                 Wp   =           57.65248
     YDOT =       2057.602623  meter/sec      RA   =          329.71721  deg
     ZDOT =      -2229.167869                 TA   =           54.21191
                                              MA   =           54.10517
                                              Ha   =            222.848  n.mi
                                              Hp   =            213.283
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -663668.68                 X    =         -278227.88
     Y    =       15278670.04  feet           Y    =         4654251.92  meter
     Z    =       16129799.97                 Z    =         4915195.91
     XDOT =     -23122.819940                 XDOT =       -7059.492083
     YDOT =       6750.664775  feet/sec       YDOT =        1978.723646  meter/sec
     ZDOT =      -7313.542877                 ZDOT =       -2263.432724
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2376703.19                 X    =         -724419.13
     Y    =      -15113568.31  feet           Y    =        -4606615.62  meter
     Z    =       16123895.20                 Z    =         4914563.26
     XDOT =      20098.416408                 XDOT =        6125.997321
     YDOT =     -11162.172755  feet/sec       YDOT =       -3402.230256  meter/sec
     ZDOT =      -7467.873051                 ZDOT =       -2276.207706
  
  
    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   18322.42025504  .00016717  00000-0  10270-3 0  9038
    2 25544  51.6408 330.1334 0004892  57.9857 302.1770 15.54009723 22490
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18322.42025504   =   yrday.fracday
    Element set:     903
    Inclination:       51.6408  deg
    RA of node:       330.1334  deg
    Eccentricity:     .0004892     
    Arg of perigee:    57.9857  deg
    Mean anomaly:     302.1770  deg
    Mean motion:   15.54009723  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2249
    Checksum:              292
 
 
    Coasting Arc #5 (Orbit 2255)
    ---------------------------------------
 
    Vector Time (GMT): 2018/322/19:30:01.000
    Vector Time (MET): N/A
    Weight (LBS)     : 917475.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5971982.69                 A    =         6785659.31  meter
     Y    =        -887673.84  meter          E    =           .0017775
     Z    =        3077270.40                 I    =           51.44656
     XDOT =      -1681.974727                 Wp   =           76.79027
     YDOT =       5677.561412  meter/sec      RA   =          327.57923  deg
     ZDOT =       4882.126459                 TA   =          318.70773
                                              MA   =          318.84201
                                              Ha   =            222.918  n.mi
                                              Hp   =            213.199
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       19593119.06                 X    =         5966517.01
     Y    =       -2912315.75  feet           Y    =         -820921.53  meter
     Z    =       10096031.48                 Z    =         3106267.49
     XDOT =      -5518.289786                 XDOT =       -1769.053039
     YDOT =      18627.169987  feet/sec       YDOT =        5658.265533  meter/sec
     ZDOT =      16017.475260                 ZDOT =        4873.744334
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19728019.92                 X    =         6013100.47
     Y    =         724886.53  feet           Y    =          220945.41  meter
     Z    =       10226510.58                 Z    =         3117040.42
     XDOT =      -8898.354801                 XDOT =       -2712.218543
     YDOT =      15839.430623  feet/sec       YDOT =        4827.858454  meter/sec
     ZDOT =      15978.994488                 ZDOT =        4870.397520
  
  
    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   18322.87041443  .00016717  00000-0  10270-3 0  9048
    2 25544  51.6421 327.8914 0005242  57.7622 302.4039 15.53973547 22562
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18322.87041443   =   yrday.fracday
    Element set:     904
    Inclination:       51.6421  deg
    RA of node:       327.8914  deg
    Eccentricity:     .0005242     
    Arg of perigee:    57.7622  deg
    Mean anomaly:     302.4039  deg
    Mean motion:   15.53973547  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2256
    Checksum:              304
 
 
    Coasting Arc #6 (Orbit 2264)
    ---------------------------------------
 
    Vector Time (GMT): 2018/323/10:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3768550.76                 A    =         6778514.29  meter
     Y    =       -2348682.92  meter          E    =           .0018772
     Z    =       -5138344.35                 I    =           51.40472
     XDOT =       5335.228533                 Wp   =           74.06383
     YDOT =      -5279.243869  meter/sec      RA   =          324.47692  deg
     ZDOT =      -1499.391687                 TA   =          181.41781
                                              MA   =          181.42314
                                              Ha   =            223.026  n.mi
                                              Hp   =            213.039
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12364011.69                 X    =        -3717047.15
     Y    =       -7705652.64  feet           Y    =        -2390537.51  meter
     Z    =      -16858085.14                 Z    =        -5156525.95
     XDOT =      17504.030621                 XDOT =        5401.149393
     YDOT =     -17320.353901  feet/sec       YDOT =       -5219.213050  meter/sec
     ZDOT =      -4919.264066                 ZDOT =       -1473.314338
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14473666.28                 X    =         4411573.48
     Y    =         -87675.26  feet           Y    =          -26723.42  meter
     Z    =      -16939486.40                 Z    =        -5163155.45
     XDOT =      -5481.893202                 XDOT =       -1670.881048
     YDOT =      22976.861116  feet/sec       YDOT =        7003.347268  meter/sec
     ZDOT =      -4801.300182                 ZDOT =       -1463.436295
  
  
    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   18323.44918568  .00016717  00000-0  10270-3 0  9054
    2 25544  51.6413 325.0058 0005164  62.7428 297.4250 15.53976215 22658
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18323.44918568   =   yrday.fracday
    Element set:     905
    Inclination:       51.6413  deg
    RA of node:       325.0058  deg
    Eccentricity:     .0005164     
    Arg of perigee:    62.7428  deg
    Mean anomaly:     297.4250  deg
    Mean motion:   15.53976215  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2265
    Checksum:              316
 
 
    Coasting Arc #7 (Orbit 2280)
    ---------------------------------------
 
    Vector Time (GMT): 2018/324/10:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2418591.54                 A    =         6777786.06  meter
     Y    =        3483706.46  meter          E    =           .0007966
     Z    =        5280779.68                 I    =           51.37415
     XDOT =      -6015.631068                 Wp   =           67.93357
     YDOT =       4750.343846  meter/sec      RA   =          319.46131  deg
     ZDOT =       -375.232837                 TA   =           25.67447
                                              MA   =           25.63494
                                              Ha   =            223.001  n.mi
                                              Hp   =            213.051
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7935011.60                 X    =         2353804.14
     Y    =       11429483.13  feet           Y    =         3510390.51  meter
     Z    =       17325392.66                 Z    =         5292371.33
     XDOT =     -19736.322403                 XDOT =       -6066.480916
     YDOT =      15585.117604  feet/sec       YDOT =        4682.788564  meter/sec
     ZDOT =      -1231.078860                 ZDOT =        -404.578844
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12830047.06                 X    =        -3910598.34
     Y    =       -5214987.19  feet           Y    =        -1589528.10  meter
     Z    =       17377011.41                 Z    =         5296513.08
     XDOT =       7466.310681                 XDOT =        2275.731496
     YDOT =     -22949.670907  feet/sec       YDOT =       -6995.059693  meter/sec
     ZDOT =      -1363.649654                 ZDOT =        -415.640414
  
  
    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   18324.47811211  .00016717  00000-0  10270-3 0  9066
    2 25544  51.6394 319.8776 0005321  66.7869 293.3843 15.53995769 22818
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18324.47811211   =   yrday.fracday
    Element set:     906
    Inclination:       51.6394  deg
    RA of node:       319.8776  deg
    Eccentricity:     .0005321     
    Arg of perigee:    66.7869  deg
    Mean anomaly:     293.3843  deg
    Mean motion:   15.53995769  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2281
    Checksum:              348
 
 
    Coasting Arc #8 (Orbit 2295)
    ---------------------------------------
 
    Vector Time (GMT): 2018/325/10:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1062395.20                 A    =         6779474.27  meter
     Y    =       -4546469.20  meter          E    =           .0016624
     Z    =       -4930388.05                 I    =           51.35632
     XDOT =       6241.650958                 Wp   =           95.00174
     YDOT =      -3845.084882  meter/sec      RA   =          314.44542  deg
     ZDOT =       2205.752088                 TA   =          196.61839
                                              MA   =          196.67294
                                              Ha   =            223.059  n.mi
                                              Hp   =            213.067
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3485548.56                 X    =         -987526.49
     Y    =      -14916237.54  feet           Y    =        -4557930.86  meter
     Z    =      -16175813.80                 Z    =        -4935367.24
     XDOT =      20477.857475                 XDOT =        6273.469209
     YDOT =     -12615.107881  feet/sec       YDOT =       -3775.108572  meter/sec
     ZDOT =       7236.719448                 ZDOT =        2236.149829
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11231314.70                 X    =         3423304.72
     Y    =       10382515.33  feet           Y    =         3164590.67  meter
     Z    =      -16197564.29                 Z    =        -4937017.59
     XDOT =      -8937.759254                 XDOT =       -2724.229021
     YDOT =      21146.635750  feet/sec       YDOT =        6445.494576  meter/sec
     ZDOT =       7373.882162                 ZDOT =        2247.559283
  
  
    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   18325.44272689  .00016717  00000-0  10270-3 0  9075
    2 25544  51.6407 315.0702 0005164  68.3634 291.8069 15.53975063 22967
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18325.44272689   =   yrday.fracday
    Element set:     907
    Inclination:       51.6407  deg
    RA of node:       315.0702  deg
    Eccentricity:     .0005164     
    Arg of perigee:    68.3634  deg
    Mean anomaly:     291.8069  deg
    Mean motion:   15.53975063  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2296
    Checksum:              326
 
 
    Coasting Arc #9 (Orbit 2303)
    ---------------------------------------
 
    Vector Time (GMT): 2018/325/21:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4228379.35                 A    =         6778605.88  meter
     Y    =        1406422.16  meter          E    =           .0008735
     Z    =        5100700.14                 I    =           51.34123
     XDOT =      -4022.451591                 Wp   =           95.22654
     YDOT =       6341.401731  meter/sec      RA   =          312.09520  deg
     ZDOT =       1582.886820                 TA   =          339.44087
                                              MA   =          339.47600
                                              Ha   =            222.917  n.mi
                                              Hp   =            213.147
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13872635.66                 X    =         4187560.89
     Y    =        4614245.94  feet           Y    =         1453478.38  meter
     Z    =       16734580.51                 Z    =         5121141.62
     XDOT =     -13197.019657                 XDOT =       -4100.752998
     YDOT =      20805.123791  feet/sec       YDOT =        6295.982001  meter/sec
     ZDOT =       5193.198228                 ZDOT =        1563.156710
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14384502.22                 X    =         4384396.28
     Y    =       -1936595.96  feet           Y    =         -590274.45  meter
     Z    =       16826264.07                 Z    =         5128645.29
     XDOT =      -2823.315994                 XDOT =        -860.546715
     YDOT =      23461.124874  feet/sec       YDOT =        7150.950862  meter/sec
     ZDOT =       5103.641593                 ZDOT =        1555.589958
  
  
    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   18325.95718742  .00016717  00000-0  10270-3 0  9087
    2 25544  51.6394 312.5051 0005124  68.0257 292.1439 15.53969947 23044
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18325.95718742   =   yrday.fracday
    Element set:     908
    Inclination:       51.6394  deg
    RA of node:       312.5051  deg
    Eccentricity:     .0005124     
    Arg of perigee:    68.0257  deg
    Mean anomaly:     292.1439  deg
    Mean motion:   15.53969947  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2304
    Checksum:              325
 
 
    Coasting Arc #10 (Orbit 2318)
    ---------------------------------------
 
    Vector Time (GMT): 2018/326/21:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3181407.38                 A    =         6777748.75  meter
     Y    =       -2821937.07  meter          E    =           .0019708
     Z    =       -5294670.60                 I    =           51.31534
     XDOT =       4796.676634                 Wp   =           87.09931
     YDOT =      -5956.933310  meter/sec      RA   =          307.07410  deg
     ZDOT =        294.660745                 TA   =          185.71638
                                              MA   =          185.73891
                                              Ha   =            223.019  n.mi
                                              Hp   =            212.910
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10437688.25                 X    =        -3123895.82
     Y    =       -9258323.73  feet           Y    =        -2857191.84  meter
     Z    =      -17370966.54                 Z    =        -5309985.71
     XDOT =      15737.128063                 XDOT =        4861.500879
     YDOT =     -19543.744457  feet/sec       YDOT =       -5902.931106  meter/sec
     ZDOT =        966.734728                 ZDOT =         318.119007
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13412590.47                 X    =        -4088157.57
     Y    =       -3518753.40  feet           Y    =        -1072516.04  meter
     Z    =      -17439414.10                 Z    =        -5315533.42
     XDOT =       4802.961392                 XDOT =        1463.942632
     YDOT =     -23594.267254  feet/sec       YDOT =       -7191.532659  meter/sec
     ZDOT =       1072.988694                 ZDOT =         327.046954
  
  
    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   18326.92179673  .00016717  00000-0  10270-3 0  9090
    2 25544  51.6376 307.6962 0005126  72.4574 287.7138 15.54007852 23194
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18326.92179673   =   yrday.fracday
    Element set:     909
    Inclination:       51.6376  deg
    RA of node:       307.6962  deg
    Eccentricity:     .0005126     
    Arg of perigee:    72.4574  deg
    Mean anomaly:     287.7138  deg
    Mean motion:   15.54007852  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2319
    Checksum:              338
 
 
    Coasting Arc #11 (Orbit 2334)
    ---------------------------------------
 
    Vector Time (GMT): 2018/327/21:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2055963.12                 A    =         6779311.67  meter
     Y    =        4162598.89  meter          E    =           .0011178
     Z    =        4932848.23                 I    =           51.30191
     XDOT =      -5260.988515                 Wp   =           65.43934
     YDOT =       5156.348329  meter/sec      RA   =          302.05378  deg
     ZDOT =      -2150.055259                 TA   =           45.64489
                                              MA   =           45.55335
                                              Ha   =            222.926  n.mi
                                              Hp   =            213.093
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6745285.83                 X    =         1985301.20
     Y    =       13656820.52  feet           Y    =         4185194.55  meter
     Z    =       16183885.27                 Z    =         4942664.39
     XDOT =     -17260.461006                 XDOT =       -5307.813139
     YDOT =      16917.153309  feet/sec       YDOT =        5097.254686  meter/sec
     ZDOT =      -7053.987071                 ZDOT =       -2175.725211
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12300622.62                 X    =         3749229.78
     Y    =        8904534.48  feet           Y    =         2714102.11  meter
     Z    =       16227437.22                 Z    =         4946122.86
     XDOT =      -6534.421627                 XDOT =       -1991.691712
     YDOT =      22143.340894  feet/sec       YDOT =        6749.290304  meter/sec
     ZDOT =      -7170.067610                 ZDOT =       -2185.436608
  
  
    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   18327.95071146  .00016717  00000-0  10270-3 0  9102
    2 25544  51.6381 302.5679 0004959  76.3374 283.8330 15.53997690 23359
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18327.95071146   =   yrday.fracday
    Element set:     910
    Inclination:       51.6381  deg
    RA of node:       302.5679  deg
    Eccentricity:     .0004959     
    Arg of perigee:    76.3374  deg
    Mean anomaly:     283.8330  deg
    Mean motion:   15.53997690  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2335
    Checksum:              335
 
 
    Coasting Arc #12 (Orbit 2349)
    ---------------------------------------
 
    Vector Time (GMT): 2018/328/21:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -988084.66                 A    =         6782477.10  meter
     Y    =       -5311719.06  meter          E    =           .0012202
     Z    =       -4111797.28                 I    =           51.29579
     XDOT =       5392.310428                 Wp   =           97.42900
     YDOT =      -3916.800935  meter/sec      RA   =          297.03755  deg
     ZDOT =       3772.129478                 TA   =          211.67157
                                              MA   =          211.74504
                                              Ha   =            223.015  n.mi
                                              Hp   =            212.955
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3241747.59                 X    =         -908640.75
     Y    =      -17426899.82  feet           Y    =        -5322323.87  meter
     Z    =      -13490148.55                 Z    =        -4116404.76
     XDOT =      17691.307178                 XDOT =        5417.385034
     YDOT =     -12850.396770  feet/sec       YDOT =       -3856.360581  meter/sec
     ZDOT =      12375.752882                 ZDOT =        3798.384471
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11245620.58                 X    =        -3427665.15
     Y    =      -13682178.58  feet           Y    =        -4170328.03  meter
     Z    =      -13510139.88                 Z    =        -4117890.64
     XDOT =       8116.008865                 XDOT =        2473.759502
     YDOT =     -18981.646037  feet/sec       YDOT =       -5785.605712  meter/sec
     ZDOT =      12494.292133                 ZDOT =        3808.260242
  
  
    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   18328.91531563  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6380 297.7589 0005089  80.8042 279.3686 15.54016938 23509
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18328.91531563   =   yrday.fracday
    Element set:     911
    Inclination:       51.6380  deg
    RA of node:       297.7589  deg
    Eccentricity:     .0005089     
    Arg of perigee:    80.8042  deg
    Mean anomaly:     279.3686  deg
    Mean motion:   15.54016938  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2350
    Checksum:              337
 
 
    Coasting Arc #13 (Orbit 2365)
    ---------------------------------------
 
    Vector Time (GMT): 2018/329/21:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -38052.15                 A    =         6786183.03  meter
     Y    =        6156013.25  meter          E    =           .0018176
     Z    =        2837722.89                 I    =           51.29422
     XDOT =      -5297.308824                 Wp   =           94.89035
     YDOT =       2306.553981  meter/sec      RA   =          292.03118  deg
     ZDOT =      -5048.296383                 TA   =           52.66769
                                              MA   =           52.50221
                                              Ha   =            222.939  n.mi
                                              Hp   =            212.997
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -124843.02                 X    =         -120671.95
     Y    =       20196893.88  feet           Y    =         6155125.45  meter
     Z    =        9310114.48                 Z    =         2837338.07
     XDOT =     -17379.622127                 XDOT =       -5298.185326
     YDOT =       7567.434320  feet/sec       YDOT =        2247.311467  meter/sec
     ZDOT =     -16562.652176                 ZDOT =       -5074.031124
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9983563.98                 X    =         3042990.30
     Y    =       17558646.40  feet           Y    =         5351875.42  meter
     Z    =        9307562.88                 Z    =         2836945.17
     XDOT =      -9851.499112                 XDOT =       -3002.736929
     YDOT =      14488.516189  feet/sec       YDOT =        4416.099734  meter/sec
     ZDOT =     -16678.636333                 ZDOT =       -5083.648354
  
  
    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   18329.94422111  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6380 292.6304 0004963  83.2201 276.9516 15.54037670 23660
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18329.94422111   =   yrday.fracday
    Element set:     912
    Inclination:       51.6380  deg
    RA of node:       292.6304  deg
    Eccentricity:     .0004963     
    Arg of perigee:    83.2201  deg
    Mean anomaly:     276.9516  deg
    Mean motion:   15.54037670  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2366
    Checksum:              301
 
 
    Coasting Arc #14 (Orbit 2380)
    ---------------------------------------
 
    Vector Time (GMT): 2018/330/21:45:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         907769.58                 A    =         6788899.44  meter
     Y    =       -6592884.29  meter          E    =           .0012718
     Z    =       -1326728.43                 I    =           51.29102
     XDOT =       4998.745631                 Wp   =           56.23903
     YDOT =       -467.979016  meter/sec      RA   =          287.03299  deg
     ZDOT =       5792.802128                 TA   =          289.25120
                                              MA   =          289.38875
                                              Ha   =            223.065  n.mi
                                              Hp   =            212.924
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2978246.67                 X    =          987870.20
     Y    =      -21630197.82  feet           Y    =        -6582284.97  meter
     Z    =       -4352783.57                 Z    =        -1322124.92
     XDOT =      16400.084090                 XDOT =        4975.468545
     YDOT =      -1535.364225  feet/sec       YDOT =        -412.210346  meter/sec
     ZDOT =      19005.256324                 ZDOT =        5817.027945
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8611090.89                 X    =        -2624660.50
     Y    =      -20069174.05  feet           Y    =        -6117084.25  meter
     Z    =       -4331224.13                 Z    =        -1320157.12
     XDOT =      11671.948313                 XDOT =        3557.609846
     YDOT =      -9099.732995  feet/sec       YDOT =       -2773.598617  meter/sec
     ZDOT =      19114.216864                 ZDOT =        5826.013300
  
  
    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   18330.90882021  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6372 287.8228 0005192  89.3802 270.7945 15.54020217 23815
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18330.90882021   =   yrday.fracday
    Element set:     913
    Inclination:       51.6372  deg
    RA of node:       287.8228  deg
    Eccentricity:     .0005192     
    Arg of perigee:    89.3802  deg
    Mean anomaly:     270.7945  deg
    Mean motion:   15.54020217  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2381
    Checksum:              305
 
 
    Coasting Arc #15 (Orbit 2391)
    ---------------------------------------
 
    Vector Time (GMT): 2018/331/13:15:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1692243.84                 A    =         6789613.05  meter
     Y    =       -6568413.34  meter          E    =           .0016514
     Z    =          93406.15                 I    =           51.28961
     XDOT =       4621.590895                 Wp   =           58.31880
     YDOT =       1286.757244  meter/sec      RA   =          283.81478  deg
     ZDOT =       5983.111187                 TA   =          302.69230
                                              MA   =          302.85145
                                              Ha   =            223.027  n.mi
                                              Hp   =            212.923
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5551981.10                 X    =         1765114.18
     Y    =      -21549912.52  feet           Y    =        -6549082.06  meter
     Z    =         306450.62                 Z    =          101802.88
     XDOT =      15162.699786                 XDOT =        4577.795540
     YDOT =       4221.644502  feet/sec       YDOT =        1338.193618  meter/sec
     ZDOT =      19629.629878                 ZDOT =        6005.455179
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       20888661.81                 X    =         6366864.12
     Y    =        7672149.96  feet           Y    =         2338471.31  meter
     Z    =         345048.60                 Z    =          105170.81
     XDOT =      -5142.282281                 XDOT =       -1567.367639
     YDOT =      13012.008969  feet/sec       YDOT =        3966.060334  meter/sec
     ZDOT =      19729.906078                 ZDOT =        6013.675373
  
  
    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   18331.61619003  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6393 284.3009 0005140  88.2842 271.8899 15.54029935 23920
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18331.61619003   =   yrday.fracday
    Element set:     914
    Inclination:       51.6393  deg
    RA of node:       284.3009  deg
    Eccentricity:     .0005140     
    Arg of perigee:    88.2842  deg
    Mean anomaly:     271.8899  deg
    Mean motion:   15.54029935  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2392
    Checksum:              318
 
 
    Coasting Arc #16 (Orbit 2406)
    ---------------------------------------
 
    Vector Time (GMT): 2018/332/13:15:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2386304.36                 A    =         6788236.44  meter
     Y    =        6100522.15  meter          E    =           .0011363
     Z    =       -1774563.02                 I    =           51.27916
     XDOT =      -4072.873339                 Wp   =          120.67351
     YDOT =      -3223.183521  meter/sec      RA   =          278.81942  deg
     ZDOT =      -5636.305484                 TA   =           78.90735
                                              MA   =           78.77959
                                              Ha   =            223.014  n.mi
                                              Hp   =            212.895
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7829082.55                 X    =        -2445724.82
     Y    =       20014836.44  feet           Y    =         6073504.73  meter
     Z    =       -5822057.17                 Z    =        -1786298.76
     XDOT =     -13362.445337                 XDOT =       -4009.149785
     YDOT =     -10574.749086  feet/sec       YDOT =       -3268.372479  meter/sec
     ZDOT =     -18491.815891                 ZDOT =       -5655.935651
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19302168.73                 X    =        -5883301.03
     Y    =       -9417445.79  feet           Y    =        -2870437.48  meter
     Z    =       -5875590.03                 Z    =        -1790879.84
     XDOT =      10947.286883                 XDOT =        3336.733042
     YDOT =     -10912.106562  feet/sec       YDOT =       -3326.010080  meter/sec
     ZDOT =     -18579.654053                 ZDOT =       -5663.078555
  
  
    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   18332.58078083  .00016717  00000-0  10270-3 0  9159
    2 25544  51.6402 279.4927 0005166  90.3970 269.7774 15.54034865 24072
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18332.58078083   =   yrday.fracday
    Element set:     915
    Inclination:       51.6402  deg
    RA of node:       279.4927  deg
    Eccentricity:     .0005166     
    Arg of perigee:    90.3970  deg
    Mean anomaly:     269.7774  deg
    Mean motion:   15.54034865  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2407
    Checksum:              335
 
 
    Coasting Arc #17 (Orbit 2422)
    ---------------------------------------
 
    Vector Time (GMT): 2018/333/13:15:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2938903.88                 A    =         6785133.60  meter
     Y    =       -5186291.73  meter          E    =           .0017919
     Z    =        3224975.25                 I    =           51.26388
     XDOT =       3479.771514                 Wp   =           89.10727
     YDOT =       4931.904640  meter/sec      RA   =          273.81808  deg
     ZDOT =       4737.622903                 TA   =          308.48313
                                              MA   =          308.64373
                                              Ha   =            222.990  n.mi
                                              Hp   =            212.887
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9642073.11                 X    =         2981014.73
     Y    =      -17015392.81  feet           Y    =        -5153191.59  meter
     Z    =       10580627.45                 Z    =         3239353.47
     XDOT =      11416.573209                 XDOT =        3401.349989
     YDOT =      16180.789500  feet/sec       YDOT =        4970.379115  meter/sec
     ZDOT =      15543.382227                 ZDOT =        4754.336298
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16351302.50                 X    =         4983877.00
     Y    =       10665004.55  feet           Y    =         3250693.39  meter
     Z    =       10645911.33                 Z    =         3244873.77
     XDOT =     -16110.326395                 XDOT =       -4910.427485
     YDOT =       9036.437056  feet/sec       YDOT =        2754.306015  meter/sec
     ZDOT =      15617.907534                 ZDOT =        4760.338216
  
  
    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   18333.60967415  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6393 274.3651 0005205  94.2230 265.9517 15.54036057 24231
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18333.60967415   =   yrday.fracday
    Element set:     916
    Inclination:       51.6393  deg
    RA of node:       274.3651  deg
    Eccentricity:     .0005205     
    Arg of perigee:    94.2230  deg
    Mean anomaly:     265.9517  deg
    Mean motion:   15.54036057  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2423
    Checksum:              305
 
 
    Coasting Arc #18 (Orbit 2437)
    ---------------------------------------
 
    Vector Time (GMT): 2018/334/13:15:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 932630.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3448583.02                 A    =         6781264.30  meter
     Y    =        3857910.72  meter          E    =           .0013873
     Z    =       -4396195.84                 I    =           51.25080
     XDOT =      -2805.799510                 Wp   =           79.46457
     YDOT =      -6297.362498  meter/sec      RA   =          268.80608  deg
     ZDOT =      -3331.800800                 TA   =          156.65389
                                              MA   =          156.59083
                                              Ha   =            222.974  n.mi
                                              Hp   =            212.779
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11314248.77                 X    =        -3470112.42
     Y    =       12657187.39  feet           Y    =         3819226.06  meter
     Z    =      -14423214.70                 Z    =        -4413000.11
     XDOT =      -9205.378970                 XDOT =       -2718.987880
     YDOT =     -20660.638117  feet/sec       YDOT =       -6328.253375  meter/sec
     ZDOT =     -10931.104988                 ZDOT =       -3345.219878
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12099389.35                 X    =        -3687893.88
     Y    =      -11816208.51  feet           Y    =        -3601580.35  meter
     Z    =      -14499232.18                 Z    =        -4419365.97
     XDOT =      20216.866835                 XDOT =        6162.101011
     YDOT =      -7241.200289  feet/sec       YDOT =       -2207.117848  meter/sec
     ZDOT =     -10990.669198                 ZDOT =       -3349.955971
  
  
    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   18334.57425848  .00016717  00000-0  10270-3 0  9177
    2 25544  51.6401 269.5572 0005175  97.3424 262.8317 15.54061210 24383
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      18334.57425848   =   yrday.fracday
    Element set:     917
    Inclination:       51.6401  deg
    RA of node:       269.5572  deg
    Eccentricity:     .0005175     
    Arg of perigee:    97.3424  deg
    Mean anomaly:     262.8317  deg
    Mean motion:   15.54061210  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2438
    Checksum:              314
 
             

Curator: Kim Dismukes | Responsible NASA Official: Amiko Kauderer | Updated: 06/08/2009
Privacy Policy and Important Notices