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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  24322.132
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   84.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.315
   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 
   ------------------------------------------------------------------------
   027/13:58:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.4  
   000/00:00:00.000           0.0               0.0              212.3  
   
   027/15:30:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.4  
   000/00:00:00.000           0.0               0.0              212.2  
   
   031/14:25:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.0  
   000/00:00:00.000           0.0               0.0              212.6  
   
   033/03:20:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              223.0  
   000/00:00:00.000           0.0               0.0              212.7  
   
 
 
    Coasting Arc #1 (Orbit 3924)
    ---------------------------------------
 
    Vector Time (GMT): 2017/023/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930840.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1622183.31                 A    =         6777686.54  meter
     Y    =        3975887.89  meter          E    =           .0011248
     Z    =        5235755.59                 I    =           51.86081
     XDOT =      -6410.933402                 Wp   =          114.36663
     YDOT =      -4074.976033  meter/sec      RA   =           38.98042  deg
     ZDOT =       1101.751978                 TA   =          325.08144
                                              MA   =          325.15517
                                              Ha   =            223.754  n.mi
                                              Hp   =            212.005
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5322123.71                 X    =        -1691954.64
     Y    =       13044251.62  feet           Y    =         3957357.25  meter
     Z    =       17177675.82                 Z    =         5227706.27
     XDOT =     -21033.246071                 XDOT =       -6370.241218
     YDOT =     -13369.343939  feet/sec       YDOT =       -4146.439921  meter/sec
     ZDOT =       3614.671844                 ZDOT =        1070.708635
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13936584.03                 X    =        -4247870.81
     Y    =        2343056.00  feet           Y    =          714163.47  meter
     Z    =       17141521.57                 Z    =         5224735.77
     XDOT =        282.520974                 XDOT =          86.112393
     YDOT =     -23925.389600  feet/sec       YDOT =       -7292.458750  meter/sec
     ZDOT =       3479.038732                 ZDOT =        1060.411005
  
  
    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   17023.55006902  .00016717  00000-0  10270-3 0  9007
    2 25544  51.6417  39.3548 0007572 110.9042 249.2922 15.54138237 39254
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17023.55006902   =   yrday.fracday
    Element set:     900
    Inclination:       51.6417  deg
    RA of node:        39.3548  deg
    Eccentricity:     .0007572     
    Arg of perigee:   110.9042  deg
    Mean anomaly:     249.2922  deg
    Mean motion:   15.54138237  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3925
    Checksum:              295
 
 
    Coasting Arc #2 (Orbit 3939)
    ---------------------------------------
 
    Vector Time (GMT): 2017/024/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930840.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3116640.05                 A    =         6777659.54  meter
     Y    =       -2910212.17  meter          E    =           .0021660
     Z    =       -5287012.98                 I    =           51.83391
     XDOT =       5909.267905                 Wp   =          102.50486
     YDOT =       4787.642996  meter/sec      RA   =           33.99557  deg
     ZDOT =        846.476865                 TA   =          175.59276
                                              MA   =          175.57365
                                              Ha   =            223.646  n.mi
                                              Hp   =            212.227
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10225197.00                 X    =         3174632.56
     Y    =       -9547940.20  feet           Y    =        -2875035.35  meter
     Z    =      -17345843.10                 Z    =        -5271732.75
     XDOT =      19387.361894                 XDOT =        5851.180339
     YDOT =      15707.490145  feet/sec       YDOT =        4853.399590  meter/sec
     ZDOT =       2777.155070                 ZDOT =         875.041015
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13647762.82                 X    =         4159838.11
     Y    =        3435309.00  feet           Y    =         1047082.18  meter
     Z    =      -17278116.53                 Z    =        -5266369.92
     XDOT =      -2312.900923                 XDOT =        -704.972201
     YDOT =      23810.362368  feet/sec       YDOT =        7257.398450  meter/sec
     ZDOT =       2901.746078                 ZDOT =         884.452205
  
  
    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   17024.51459619  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6411  34.5476 0007434 114.8054 245.3872 15.54115880 39405
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17024.51459619   =   yrday.fracday
    Element set:     901
    Inclination:       51.6411  deg
    RA of node:        34.5476  deg
    Eccentricity:     .0007434     
    Arg of perigee:   114.8054  deg
    Mean anomaly:     245.3872  deg
    Mean motion:   15.54115880  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3940
    Checksum:              301
 
 
    Coasting Arc #3 (Orbit 3955)
    ---------------------------------------
 
    Vector Time (GMT): 2017/025/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930840.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4477586.49                 A    =         6779745.56  meter
     Y    =        1792187.94  meter          E    =           .0013416
     Z    =        4753412.26                 I    =           51.81301
     XDOT =      -4963.335417                 Wp   =           89.17449
     YDOT =      -5191.022215  meter/sec      RA   =           29.01052  deg
     ZDOT =      -2711.366598                 TA   =           27.56326
                                              MA   =           27.49219
                                              Ha   =            223.667  n.mi
                                              Hp   =            212.146
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14690244.39                 X    =        -4520383.81
     Y    =        5879881.68  feet           Y    =         1741877.08  meter
     Z    =       15595184.58                 Z    =         4731557.98
     XDOT =     -16283.908850                 XDOT =       -4891.748895
     YDOT =     -17030.912779  feet/sec       YDOT =       -5246.125210  meter/sec
     ZDOT =      -8895.559704                 ZDOT =       -2735.302900
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13166873.13                 X    =        -4013262.93
     Y    =       -8944670.78  feet           Y    =        -2726335.65  meter
     Z    =       15498786.64                 Z    =         4724030.17
     XDOT =       4343.477026                 XDOT =        1323.891798
     YDOT =     -22026.727010  feet/sec       YDOT =       -6713.746393  meter/sec
     ZDOT =      -8999.727575                 ZDOT =       -2743.116965
  
  
    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   17025.54341961  .00016717  00000-0  10270-3 0  9027
    2 25544  51.6402  29.4183 0007380 118.2539 241.9359 15.54159359 39567
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17025.54341961   =   yrday.fracday
    Element set:     902
    Inclination:       51.6402  deg
    RA of node:        29.4183  deg
    Eccentricity:     .0007380     
    Arg of perigee:   118.2539  deg
    Mean anomaly:     241.9359  deg
    Mean motion:   15.54159359  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3956
    Checksum:              318
 
 
    Coasting Arc #4 (Orbit 3970)
    ---------------------------------------
 
    Vector Time (GMT): 2017/026/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930840.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5608764.42                 A    =         6783441.38  meter
     Y    =        -737388.92  meter          E    =           .0013058
     Z    =       -3758099.67                 I    =           51.79665
     XDOT =       3551.457641                 Wp   =          111.70419
     YDOT =       5266.775317  meter/sec      RA   =           24.03279  deg
     ZDOT =       4274.173814                 TA   =          203.53358
                                              MA   =          203.59338
                                              Ha   =            223.592  n.mi
                                              Hp   =            212.287
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18401458.08                 X    =         5634847.92
     Y    =       -2419254.99  feet           Y    =         -674521.99  meter
     Z    =      -12329723.33                 Z    =        -3730791.20
     XDOT =      11651.763914                 XDOT =        3471.537791
     YDOT =      17279.446578  feet/sec       YDOT =        5306.043129  meter/sec
     ZDOT =      14022.879966                 ZDOT =        4291.231418
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12610038.38                 X    =         3843539.70
     Y    =       13725959.32  feet           Y    =         4183672.40  meter
     Z    =      -12209566.11                 Z    =        -3721475.75
     XDOT =      -6485.821091                 XDOT =       -1976.878268
     YDOT =      18476.674894  feet/sec       YDOT =        5631.690508  meter/sec
     ZDOT =      14096.799652                 ZDOT =        4296.704534
  
  
    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   17026.50793736  .00016717  00000-0  10270-3 0  9036
    2 25544  51.6405  24.6107 0007484 120.4044 239.7849 15.54137761 39713
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17026.50793736   =   yrday.fracday
    Element set:     903
    Inclination:       51.6405  deg
    RA of node:        24.6107  deg
    Eccentricity:     .0007484     
    Arg of perigee:   120.4044  deg
    Mean anomaly:     239.7849  deg
    Mean motion:   15.54137761  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3971
    Checksum:              313
 
 
    Coasting Arc #5 (Orbit 3986)
    ---------------------------------------
 
    Vector Time (GMT): 2017/027/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930840.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6360111.98                 A    =         6786973.78  meter
     Y    =        -261668.50  meter          E    =           .0020935
     Z    =        2323486.27                 I    =           51.77776
     XDOT =      -1780.808096                 Wp   =          112.81008
     YDOT =      -5133.037361  meter/sec      RA   =           19.06227  deg
     ZDOT =      -5421.818743                 TA   =           41.31213
                                              MA   =           41.15395
                                              Ha   =            223.470  n.mi
                                              Hp   =            212.272
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20866509.12                 X    =        -6367999.36
     Y    =        -858492.44  feet           Y    =         -332835.69  meter
     Z    =        7622986.47                 Z    =         2292572.30
     XDOT =      -5842.546247                 XDOT =       -1696.940807
     YDOT =     -16840.673758  feet/sec       YDOT =       -5152.482553  meter/sec
     ZDOT =     -17788.119237                 ZDOT =       -5430.265551
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11629751.65                 X    =        -3544748.30
     Y    =      -17405431.95  feet           Y    =        -5305175.66  meter
     Z    =        7487185.71                 Z    =         2282094.20
     XDOT =       8965.474922                 XDOT =        2732.676756
     YDOT =     -13702.162621  feet/sec       YDOT =       -4176.419167  meter/sec
     ZDOT =     -17824.223153                 ZDOT =       -5432.823217
  
  
    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   17027.53675035  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6394  19.4810 0007276 123.8744 236.3102 15.54180494 39879
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17027.53675035   =   yrday.fracday
    Element set:     904
    Inclination:       51.6394  deg
    RA of node:        19.4810  deg
    Eccentricity:     .0007276     
    Arg of perigee:   123.8744  deg
    Mean anomaly:     236.3102  deg
    Mean motion:   15.54180494  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3987
    Checksum:              315
 
 
    Coasting Arc #6 (Orbit 3987)
    ---------------------------------------
 
    Vector Time (GMT): 2017/027/13:58:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 930840.2
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -388616.18                 A    =         6778075.66  meter
     Y    =       -4414079.92  meter          E    =           .0019399
     Z    =       -5145485.06                 I    =           51.74614
     XDOT =       7395.106506                 Wp   =           93.61104
     YDOT =       1184.829938  meter/sec      RA   =           18.68495  deg
     ZDOT =      -1581.268315                 TA   =          161.17282
                                              MA   =          161.10098
                                              Ha   =            223.441  n.mi
                                              Hp   =            212.289
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1274987.46                 X    =         -314234.20
     Y    =      -14481889.50  feet           Y    =        -4418009.73  meter
     Z    =      -16881512.67                 Z    =        -5147192.19
     XDOT =      24262.160453                 XDOT =        7388.988682
     YDOT =       3887.237330  feet/sec       YDOT =        1267.492815  meter/sec
     ZDOT =      -5187.888174                 ZDOT =       -1545.360778
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4873302.42                 X    =         1485382.58
     Y    =      -13688600.84  feet           Y    =        -4172285.54  meter
     Z    =      -16888141.32                 Z    =        -5147505.47
     XDOT =      19569.844394                 XDOT =        5964.888571
     YDOT =      13147.561335  feet/sec       YDOT =        4007.376695  meter/sec
     ZDOT =      -5030.326049                 ZDOT =       -1533.243380
  
  
    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   17027.60105233  .00016717  00000-0  10270-3 0  9059
    2 25544  51.6402  19.1601 0007260 124.6884 235.4954 15.54148849 39885
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17027.60105233   =   yrday.fracday
    Element set:     905
    Inclination:       51.6402  deg
    RA of node:        19.1601  deg
    Eccentricity:     .0007260     
    Arg of perigee:   124.6884  deg
    Mean anomaly:     235.4954  deg
    Mean motion:   15.54148849  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3988
    Checksum:              308
 
 
    Coasting Arc #7 (Orbit 3988)
    ---------------------------------------
 
    Vector Time (GMT): 2017/027/15:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900114.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -897373.33                 A    =         6778513.84  meter
     Y    =       -4474824.29  meter          E    =           .0018497
     Z    =       -5027620.94                 I    =           51.74694
     XDOT =       7346.967837                 Wp   =           92.21290
     YDOT =        773.108756  meter/sec      RA   =           18.37232  deg
     ZDOT =      -2006.528718                 TA   =          158.32780
                                              MA   =          158.24942
                                              Ha   =            223.418  n.mi
                                              Hp   =            212.240
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2944138.22                 X    =         -822846.79
     Y    =      -14681182.07  feet           Y    =        -4484442.57  meter
     Z    =      -16494819.36                 Z    =        -5031799.05
     XDOT =      24104.225188                 XDOT =        7347.523225
     YDOT =       2536.446050  feet/sec       YDOT =         855.270629  meter/sec
     ZDOT =      -6583.099470                 ZDOT =       -1970.838821
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2513725.79                 X    =         -766183.62
     Y    =      -14741418.73  feet           Y    =        -4493184.43  meter
     Z    =      -16512294.79                 Z    =        -5032947.45
     XDOT =      23010.071018                 XDOT =        7013.469646
     YDOT =       3248.735529  feet/sec       YDOT =         990.214589  meter/sec
     ZDOT =      -6426.412611                 ZDOT =       -1958.770564
  
  
    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   17027.66535323  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6412  18.8400 0007271 124.3879 235.7963 15.54166483 39890
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17027.66535323   =   yrday.fracday
    Element set:     906
    Inclination:       51.6412  deg
    RA of node:        18.8400  deg
    Eccentricity:     .0007271     
    Arg of perigee:   124.3879  deg
    Mean anomaly:     235.7963  deg
    Mean motion:   15.54166483  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3989
    Checksum:              327
 
 
    Coasting Arc #8 (Orbit 4004)
    ---------------------------------------
 
    Vector Time (GMT): 2017/028/15:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900114.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -866270.56                 A    =         6777126.66  meter
     Y    =        4106374.19  meter          E    =           .0009106
     Z    =        5314579.52                 I    =           51.71213
     XDOT =      -7482.877725                 Wp   =          119.73955
     YDOT =      -1704.626504  meter/sec      RA   =           13.38048  deg
     ZDOT =         92.863091                 TA   =          329.35063
                                              MA   =          329.40380
                                              Ha   =            223.265  n.mi
                                              Hp   =            212.390
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2842095.01                 X    =         -937939.76
     Y    =       13472356.28  feet           Y    =         4096286.28  meter
     Z    =       17436284.50                 Z    =         5310197.44
     XDOT =     -24550.123771                 XDOT =       -7463.711087
     YDOT =      -5592.606640  feet/sec       YDOT =       -1788.197918  meter/sec
     ZDOT =        304.668933                 ZDOT =          56.560963
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3019498.97                 X    =         -920343.28
     Y    =       13459714.08  feet           Y    =         4102520.85  meter
     Z    =       17416217.39                 Z    =         5308463.06
     XDOT =     -23543.211022                 XDOT =       -7175.970719
     YDOT =      -5489.117528  feet/sec       YDOT =       -1673.083023  meter/sec
     ZDOT =        145.481668                 ZDOT =          44.342812
  
  
    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   17028.69416011  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6418  13.7123 0007072 129.5627 230.6151 15.54202130 40052
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17028.69416011   =   yrday.fracday
    Element set:     907
    Inclination:       51.6418  deg
    RA of node:        13.7123  deg
    Eccentricity:     .0007072     
    Arg of perigee:   129.5627  deg
    Mean anomaly:     230.6151  deg
    Mean motion:   15.54202130  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4005
    Checksum:              266
 
 
    Coasting Arc #9 (Orbit 4019)
    ---------------------------------------
 
    Vector Time (GMT): 2017/029/15:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900114.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2647975.38                 A    =         6778399.74  meter
     Y    =       -3660211.83  meter          E    =           .0019642
     Z    =       -5071254.88                 I    =           51.68507
     XDOT =       6993.723893                 Wp   =          113.34944
     YDOT =       2503.003890  meter/sec      RA   =            8.38381  deg
     ZDOT =       1843.320183                 TA   =          174.53768
                                              MA   =          174.51622
                                              Ha   =            223.278  n.mi
                                              Hp   =            212.512
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8687583.26                 X    =         2713341.14
     Y    =      -12008569.00  feet           Y    =        -3630235.03  meter
     Z    =      -16637975.34                 Z    =        -5058233.28
     XDOT =      22945.288362                 XDOT =        6956.261125
     YDOT =       8211.955021  feet/sec       YDOT =        2581.003003  meter/sec
     ZDOT =       6047.638396                 ZDOT =        1877.201726
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8645469.59                 X    =         2635139.13
     Y    =      -12118593.12  feet           Y    =        -3693747.18  meter
     Z    =      -16580036.56                 Z    =        -5053595.14
     XDOT =      22122.199304                 XDOT =        6742.846348
     YDOT =       7296.364264  feet/sec       YDOT =        2223.931828  meter/sec
     ZDOT =       6196.024671                 ZDOT =        1888.548320
  
  
    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   17029.65866267  .00016717  00000-0  10270-3 0  9080
    2 25544  51.6427   8.9031 0007158 131.7186 228.4580 15.54178284 40206
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17029.65866267   =   yrday.fracday
    Element set:     908
    Inclination:       51.6427  deg
    RA of node:         8.9031  deg
    Eccentricity:     .0007158     
    Arg of perigee:   131.7186  deg
    Mean anomaly:     228.4580  deg
    Mean motion:   15.54178284  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4020
    Checksum:              320
 
 
    Coasting Arc #10 (Orbit 4035)
    ---------------------------------------
 
    Vector Time (GMT): 2017/030/15:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 900114.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4240299.65                 A    =         6781573.08  meter
     Y    =        3122455.37  meter          E    =           .0014928
     Z    =        4258976.57                 I    =           51.66327
     XDOT =      -5978.675794                 Wp   =           98.51071
     YDOT =      -3202.921976  meter/sec      RA   =            3.39344  deg
     ZDOT =      -3595.646281                 TA   =           28.19494
                                              MA   =           28.11420
                                              Ha   =            223.349  n.mi
                                              Hp   =            212.525
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13911744.27                 X    =        -4295588.21
     Y    =       10244276.16  feet           Y    =         3074728.52  meter
     Z    =       13973020.25                 Z    =         4238244.52
     XDOT =     -19615.078063                 XDOT =       -5924.950016
     YDOT =     -10508.274201  feet/sec       YDOT =       -3269.479305  meter/sec
     ZDOT =     -11796.739767                 ZDOT =       -3624.557627
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13692472.16                 X    =        -4173465.52
     Y    =       10656097.68  feet           Y    =         3247978.57  meter
     Z    =       13881314.98                 Z    =         4231024.81
     XDOT =     -19063.822882                 XDOT =       -5810.653214
     YDOT =      -8927.073230  feet/sec       YDOT =       -2720.971920  meter/sec
     ZDOT =     -11923.142478                 ZDOT =       -3634.173827
  
  
    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   17030.68745925  .00016717  00000-0  10270-3 0  9093
    2 25544  51.6425   3.7755 0007208 135.3129 224.8605 15.54178083 40365
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17030.68745925   =   yrday.fracday
    Element set:     909
    Inclination:       51.6425  deg
    RA of node:         3.7755  deg
    Eccentricity:     .0007208     
    Arg of perigee:   135.3129  deg
    Mean anomaly:     224.8605  deg
    Mean motion:   15.54178083  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4036
    Checksum:              312
 
 
    Coasting Arc #11 (Orbit 4050)
    ---------------------------------------
 
    Vector Time (GMT): 2017/031/14:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2117139.33                 A    =         6778063.94  meter
     Y    =        3965467.33  meter          E    =           .0012262
     Z    =        5067524.01                 I    =           51.62113
     XDOT =      -7290.044714                 Wp   =          133.35777
     YDOT =       1588.325327  meter/sec      RA   =          358.67314  deg
     ZDOT =       1791.804756                 TA   =          299.25068
                                              MA   =          299.37322
                                              Ha   =            222.985  n.mi
                                              Hp   =            212.609
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6945995.17                 X    =         2048023.98
     Y    =       13010063.42  feet           Y    =         3988756.42  meter
     Z    =       16625734.95                 Z    =         5077640.17
     XDOT =     -23917.469533                 XDOT =       -7315.967528
     YDOT =       5211.041099  feet/sec       YDOT =        1506.658280  meter/sec
     ZDOT =       5878.624526                 ZDOT =        1756.329555
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3583884.28                 X    =         1092367.93
     Y    =       14255187.66  feet           Y    =         4344981.20  meter
     Z    =       16669404.91                 Z    =         5080834.62
     XDOT =     -23469.373147                 XDOT =       -7153.464935
     YDOT =       -833.140887  feet/sec       YDOT =        -253.941342  meter/sec
     ZDOT =       5722.453683                 ZDOT =        1744.203882
  
  
    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   17031.65194929  .00016717  00000-0  10270-3 0  9105
    2 25544  51.6422 358.9674 0007090 140.7519 219.4148 15.54229538 40510
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17031.65194929   =   yrday.fracday
    Element set:     910
    Inclination:       51.6422  deg
    RA of node:       358.9674  deg
    Eccentricity:     .0007090     
    Arg of perigee:   140.7519  deg
    Mean anomaly:     219.4148  deg
    Mean motion:   15.54229538  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4051
    Checksum:              319
 
 
    Coasting Arc #12 (Orbit 4065)
    ---------------------------------------
 
    Vector Time (GMT): 2017/032/14:25:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -275122.38                 A    =         6777151.04  meter
     Y    =       -4212719.86  meter          E    =           .0020072
     Z    =       -5318351.49                 I    =           51.58614
     XDOT =       7619.208192                 Wp   =          107.15305
     YDOT =       -713.186966  meter/sec      RA   =          353.66976  deg
     ZDOT =        165.509331                 TA   =          164.45918
                                              MA   =          164.39747
                                              Ha   =            223.048  n.mi
                                              Hp   =            212.677
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -902632.46                 X    =         -202160.62
     Y    =      -13821259.40  feet           Y    =        -4215388.82  meter
     Z    =      -17448659.73                 Z    =        -5319510.48
     XDOT =      24997.402204                 XDOT =        7625.813009
     YDOT =      -2339.852250  feet/sec       YDOT =        -627.946902  meter/sec
     ZDOT =        543.009617                 ZDOT =         202.536654
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2251102.80                 X    =          686136.13
     Y    =      -13661092.74  feet           Y    =        -4163901.07  meter
     Z    =      -17452929.96                 Z    =        -5319653.05
     XDOT =      23904.286934                 XDOT =        7286.026657
     YDOT =       3015.206362  feet/sec       YDOT =         919.034899  meter/sec
     ZDOT =        705.815328                 ZDOT =         215.132512
  
  
    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   17032.61643678  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6431 354.1584 0007083 142.8418 217.3226 15.54205829 40668
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17032.61643678   =   yrday.fracday
    Element set:     911
    Inclination:       51.6431  deg
    RA of node:       354.1584  deg
    Eccentricity:     .0007083     
    Arg of perigee:   142.8418  deg
    Mean anomaly:     217.3226  deg
    Mean motion:   15.54205829  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4066
    Checksum:              305
 
 
    Coasting Arc #13 (Orbit 4074)
    ---------------------------------------
 
    Vector Time (GMT): 2017/033/03:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5224435.51                 A    =         6783008.13  meter
     Y    =        2171426.44  meter          E    =           .0017215
     Z    =        3734639.83                 I    =           51.58986
     XDOT =      -4806.314766                 Wp   =          115.65600
     YDOT =       4185.823042  meter/sec      RA   =          351.01021  deg
     ZDOT =       4267.209988                 TA   =          289.01618
                                              MA   =          289.20261
                                              Ha   =            222.968  n.mi
                                              Hp   =            212.683
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17140536.44                 X    =         5181624.93
     Y    =        7124102.50  feet           Y    =         2229610.44  meter
     Z    =       12252755.35                 Z    =         3759914.12
     XDOT =     -15768.749233                 XDOT =       -4873.492279
     YDOT =      13733.015230  feet/sec       YDOT =        4131.700215  meter/sec
     ZDOT =      14000.032770                 ZDOT =        4243.699282
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17259240.25                 X    =        -5260616.43
     Y    =       -6629234.83  feet           Y    =        -2020590.78  meter
     Z    =       12363361.65                 Z    =         3768352.63
     XDOT =      14972.575639                 XDOT =        4563.641055
     YDOT =     -12928.244007  feet/sec       YDOT =       -3940.528773  meter/sec
     ZDOT =      13895.935687                 ZDOT =        4235.481197
  
  
    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   17033.19512334  .00016717  00000-0  10270-3 0  9122
    2 25544  51.6441 351.2713 0007410 147.8209 212.3397 15.54231834 40757
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17033.19512334   =   yrday.fracday
    Element set:     912
    Inclination:       51.6441  deg
    RA of node:       351.2713  deg
    Eccentricity:     .0007410     
    Arg of perigee:   147.8209  deg
    Mean anomaly:     212.3397  deg
    Mean motion:   15.54231834  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4075
    Checksum:              283
 
 
    Coasting Arc #14 (Orbit 4089)
    ---------------------------------------
 
    Vector Time (GMT): 2017/034/03:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3819109.82                 A    =         6779396.63  meter
     Y    =       -2953344.62  meter          E    =           .0014582
     Z    =       -4770661.88                 I    =           51.54429
     XDOT =       6159.489715                 Wp   =          100.97973
     YDOT =      -3701.864054  meter/sec      RA   =          346.01543  deg
     ZDOT =      -2648.836643                 TA   =          142.86178
                                              MA   =          142.76081
                                              Ha   =            222.969  n.mi
                                              Hp   =            212.799
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12529887.87                 X    =        -3762627.59
     Y    =       -9689450.84  feet           Y    =        -2995736.89  meter
     Z    =      -15651777.83                 Z    =        -4789076.44
     XDOT =      20208.299589                 XDOT =        6213.293767
     YDOT =     -12145.223275  feet/sec       YDOT =       -3632.683776  meter/sec
     ZDOT =      -8690.408934                 ZDOT =       -2618.785164
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12861219.15                 X    =         3920099.60
     Y    =        9107798.91  feet           Y    =         2776057.11  meter
     Z    =      -15732092.61                 Z    =        -4795141.83
     XDOT =     -19018.952800                 XDOT =       -5796.976813
     YDOT =      12129.145555  feet/sec       YDOT =        3696.963565  meter/sec
     ZDOT =      -8557.683363                 ZDOT =       -2608.381889
  
  
    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   17034.15960206  .00016717  00000-0  10270-3 0  9135
    2 25544  51.6428 346.4638 0007367 151.5713 208.5843 15.54197739 40902
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17034.15960206   =   yrday.fracday
    Element set:     913
    Inclination:       51.6428  deg
    RA of node:       346.4638  deg
    Eccentricity:     .0007367     
    Arg of perigee:   151.5713  deg
    Mean anomaly:     208.5843  deg
    Mean motion:   15.54197739  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4090
    Checksum:              321
 
 
    Coasting Arc #15 (Orbit 4105)
    ---------------------------------------
 
    Vector Time (GMT): 2017/035/03:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2190970.95                 A    =         6777164.71  meter
     Y    =        3667322.97  meter          E    =           .0009959
     Z    =        5257034.73                 I    =           51.50635
     XDOT =      -6994.585901                 Wp   =          143.88815
     YDOT =       3057.619073  meter/sec      RA   =          341.00979  deg
     ZDOT =        773.489752                 TA   =          298.66150
                                              MA   =          298.76159
                                              Ha   =            222.753  n.mi
                                              Hp   =            212.968
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7188224.89                 X    =         2124263.26
     Y    =       12031899.50  feet           Y    =         3691451.07  meter
     Z    =       17247489.26                 Z    =         5267515.56
     XDOT =     -22948.116472                 XDOT =       -7032.014343
     YDOT =      10031.558640  feet/sec       YDOT =        2979.191647  meter/sec
     ZDOT =       2537.696037                 ZDOT =         739.421483
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7822968.35                 X    =        -2384440.75
     Y    =      -11561696.72  feet           Y    =        -3524005.16  meter
     Z    =       17292813.64                 Z    =         5270849.60
     XDOT =      21440.408068                 XDOT =        6535.036379
     YDOT =     -10893.996698  feet/sec       YDOT =       -3320.490193  meter/sec
     ZDOT =       2387.460893                 ZDOT =         727.698080
  
  
    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   17035.18837153  .00016717  00000-0  10270-3 0  9144
    2 25544  51.6431 341.3353 0007321 155.5438 204.6064 15.54250861 41068
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17035.18837153   =   yrday.fracday
    Element set:     914
    Inclination:       51.6431  deg
    RA of node:       341.3353  deg
    Eccentricity:     .0007321     
    Arg of perigee:   155.5438  deg
    Mean anomaly:     204.6064  deg
    Mean motion:   15.54250861  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4106
    Checksum:              286
 
 
    Coasting Arc #16 (Orbit 4120)
    ---------------------------------------
 
    Vector Time (GMT): 2017/036/03:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -431336.99                 A    =         6777602.26  meter
     Y    =       -4341682.36  meter          E    =           .0018851
     Z    =       -5202486.17                 I    =           51.47655
     XDOT =       7240.472911                 Wp   =          118.09997
     YDOT =      -2172.061421  meter/sec      RA   =          335.99824  deg
     ZDOT =       1207.025578                 TA   =          163.55786
                                              MA   =          163.49664
                                              Ha   =            222.774  n.mi
                                              Hp   =            213.086
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1415147.61                 X    =         -357484.22
     Y    =      -14244364.69  feet           Y    =        -4346093.00  meter
     Z    =      -17068524.18                 Z    =        -5204402.01
     XDOT =      23754.832385                 XDOT =        7258.360253
     YDOT =      -7126.185763  feet/sec       YDOT =       -2090.993538  meter/sec
     ZDOT =       3960.057670                 ZDOT =        1242.240717
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2445512.60                 X    =          745392.24
     Y    =       14094872.19  feet           Y    =         4296117.04  meter
     Z    =      -17076098.27                 Z    =        -5204794.75
     XDOT =     -22050.834500                 XDOT =       -6721.094356
     YDOT =       8832.671510  feet/sec       YDOT =        2692.198276  meter/sec
     ZDOT =       4115.151291                 ZDOT =        1254.298113
  
  
    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   17036.15283865  .00016717  00000-0  10270-3 0  9158
    2 25544  51.6425 336.5266 0007186 157.9404 202.2059 15.54225375 41215
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17036.15283865   =   yrday.fracday
    Element set:     915
    Inclination:       51.6425  deg
    RA of node:       336.5266  deg
    Eccentricity:     .0007186     
    Arg of perigee:   157.9404  deg
    Mean anomaly:     202.2059  deg
    Mean motion:   15.54225375  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4121
    Checksum:              307
 
 
    Coasting Arc #17 (Orbit 4136)
    ---------------------------------------
 
    Vector Time (GMT): 2017/037/03:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1254505.57                 A    =         6780088.78  meter
     Y    =        4849036.15  meter          E    =           .0010749
     Z    =        4559209.64                 I    =           51.45636
     XDOT =      -6958.486101                 Wp   =          107.69160
     YDOT =       1075.262564  meter/sec      RA   =          330.98947  deg
     ZDOT =      -3055.566348                 TA   =           12.91835
                                              MA   =           12.89084
                                              Ha   =            222.598  n.mi
                                              Hp   =            213.203
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4115831.93                 X    =        -1330781.65
     Y    =       15908911.26  feet           Y    =         4834580.95  meter
     Z    =       14958036.89                 Z    =         4552930.44
     XDOT =     -22829.678810                 XDOT =       -6955.150533
     YDOT =       3527.764317  feet/sec       YDOT =         997.466722  meter/sec
     ZDOT =     -10024.823977                 ZDOT =       -3089.360017
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2640855.83                 X    =          804932.86
     Y    =      -16245357.61  feet           Y    =        -4951585.00  meter
     Z    =       14929522.24                 Z    =         4550518.38
     XDOT =      21126.704577                 XDOT =        6439.419555
     YDOT =      -5923.329349  feet/sec       YDOT =       -1805.430786  meter/sec
     ZDOT =     -10173.457555                 ZDOT =       -3100.869863
  
  
    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   17037.18159565  .00016717  00000-0  10270-3 0  9162
    2 25544  51.6428 331.3977 0007128 161.9043 198.2365 15.54277769 41375
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17037.18159565   =   yrday.fracday
    Element set:     916
    Inclination:       51.6428  deg
    RA of node:       331.3977  deg
    Eccentricity:     .0007128     
    Arg of perigee:   161.9043  deg
    Mean anomaly:     198.2365  deg
    Mean motion:   15.54277769  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4137
    Checksum:              341
 
 
    Coasting Arc #18 (Orbit 4151)
    ---------------------------------------
 
    Vector Time (GMT): 2017/038/03:20:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 885680.5
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2751767.10                 A    =         6783934.89  meter
     Y    =       -5166680.99  meter          E    =           .0009877
     Z    =       -3441751.51                 I    =           51.44030
     XDOT =       6147.319679                 Wp   =          135.26097
     YDOT =        237.075218  meter/sec      RA   =          325.98835  deg
     ZDOT =       4560.174266                 TA   =          184.33555
                                              MA   =          184.34411
                                              Ha   =            222.602  n.mi
                                              Hp   =            213.276
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9028107.30                 X    =         2826055.82
     Y    =      -16951053.12  feet           Y    =        -5135493.50  meter
     Z    =      -11291835.66                 Z    =        -3428204.07
     XDOT =      20168.371650                 XDOT =        6122.061031
     YDOT =        777.805833  feet/sec       YDOT =         305.677455  meter/sec
     ZDOT =      14961.201659                 ZDOT =        4589.974211
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7097654.77                 X    =        -2163365.18
     Y    =       17883811.34  feet           Y    =         5450985.70  meter
     Z    =      -11231342.95                 Z    =        -3423313.33
     XDOT =     -18723.461669                 XDOT =       -5706.911117
     YDOT =       2044.831169  feet/sec       YDOT =         623.264540  meter/sec
     ZDOT =      15092.039997                 ZDOT =        4600.053791
  
  
    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   17038.14605322  .00016717  00000-0  10270-3 0  9177
    2 25544  51.6417 326.5897 0007316 164.0141 196.1244 15.54277268 41526
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17038.14605322   =   yrday.fracday
    Element set:     917
    Inclination:       51.6417  deg
    RA of node:       326.5897  deg
    Eccentricity:     .0007316     
    Arg of perigee:   164.0141  deg
    Mean anomaly:     196.1244  deg
    Mean motion:   15.54277268  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4152
    Checksum:              307
 
             

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