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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15846.6289
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   75.7
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.610
   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 
   ------------------------------------------------------------------------
   294/08:55:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.4  
   000/00:00:00.000           0.0               0.0              213.3  
   
   299/12:05:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.6  
   000/00:00:00.000           0.0               0.0              212.8  
   
   303/19:34:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              222.7  
   000/00:00:00.000           0.0               0.0              212.6  
   
   306/03:16:27.095           0.6               1.1              1.1    
   N/A                        1.0              -0.1              222.6  
   000/00:02:54.191          -0.1               0.0              213.3  
   
 
 
    Coasting Arc #1 (Orbit 92)
    ---------------------------------------
 
    Vector Time (GMT): 2017/291/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5907035.44                 A    =         6785776.16  meter
     Y    =        1721027.12  meter          E    =           .0017086
     Z    =        2839403.06                 I    =           51.87215
     XDOT =        810.531237                 Wp   =           66.76887
     YDOT =      -5672.132466  meter/sec      RA   =          142.51985  deg
     ZDOT =       5106.483340                 TA   =          325.41781
                                              MA   =          325.52883
                                              Ha   =            222.344  n.mi
                                              Hp   =            213.496
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19380037.52                 X    =        -5939634.09
     Y    =        5646414.42  feet           Y    =         1654788.66  meter
     Z    =        9315626.85                 Z    =         2810628.59
     XDOT =       2659.223217                 XDOT =         849.093015
     YDOT =     -18609.358485  feet/sec       YDOT =       -5662.852364  meter/sec
     ZDOT =      16753.554265                 ZDOT =        5110.515029
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14926325.64                 X    =         4549544.05
     Y    =      -13676193.12  feet           Y    =        -4168503.66  meter
     Z    =        9187779.84                 Z    =         2800435.30
     XDOT =       4961.967544                 XDOT =        1512.407708
     YDOT =      16722.864769  feet/sec       YDOT =        5097.129182  meter/sec
     ZDOT =      16772.174737                 ZDOT =        5112.158860
  
  
    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   17291.55862804  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6388 143.3110 0005129  28.8249 331.3187 15.54206883   936
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17291.55862804   =   yrday.fracday
    Element set:     900
    Inclination:       51.6388  deg
    RA of node:       143.3110  deg
    Eccentricity:     .0005129     
    Arg of perigee:    28.8249  deg
    Mean anomaly:     331.3187  deg
    Mean motion:   15.54206883  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:              93
    Checksum:              305
 
 
    Coasting Arc #2 (Orbit 107)
    ---------------------------------------
 
    Vector Time (GMT): 2017/292/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5346439.28                 A    =         6781915.38  meter
     Y    =        -467731.00  meter          E    =           .0011859
     Z    =       -4159327.62                 I    =           51.88355
     XDOT =      -2396.994272                 Wp   =           55.66931
     YDOT =       6212.441587  meter/sec      RA   =          137.55241  deg
     ZDOT =      -3780.904018                 TA   =          175.46362
                                              MA   =          175.45286
                                              Ha   =            222.276  n.mi
                                              Hp   =            213.550
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17540811.29                 X    =         5371476.66
     Y    =       -1534550.52  feet           Y    =         -407803.91  meter
     Z    =      -13646087.99                 Z    =        -4133294.82
     XDOT =      -7864.154436                 XDOT =       -2447.919098
     YDOT =      20382.026204  feet/sec       YDOT =        6185.351627  meter/sec
     ZDOT =     -12404.540741                 ZDOT =       -3792.672480
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14964386.71                 X    =        -4561145.07
     Y    =        9446789.96  feet           Y    =         2879381.58  meter
     Z    =      -13530554.81                 Z    =        -4124113.11
     XDOT =      -1737.606004                 XDOT =        -529.622310
     YDOT =     -20589.783714  feet/sec       YDOT =       -6275.766076  meter/sec
     ZDOT =     -12457.560877                 ZDOT =       -3797.064555
  
  
    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   17292.52311250  .00016717  00000-0  10270-3 0  9018
    2 25544  51.6378 138.5024 0005047  31.8627 328.2830 15.54203870  1088
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17292.52311250   =   yrday.fracday
    Element set:     901
    Inclination:       51.6378  deg
    RA of node:       138.5024  deg
    Eccentricity:     .0005047     
    Arg of perigee:    31.8627  deg
    Mean anomaly:     328.2830  deg
    Mean motion:   15.54203870  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             108
    Checksum:              280
 
 
    Coasting Arc #3 (Orbit 123)
    ---------------------------------------
 
    Vector Time (GMT): 2017/293/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4463278.79                 A    =         6778641.88  meter
     Y    =        -944906.40  meter          E    =           .0008222
     Z    =        5006318.24                 I    =           51.89617
     XDOT =       3681.572764                 Wp   =           84.65875
     YDOT =      -6407.353569  meter/sec      RA   =          132.57525  deg
     ZDOT =       2070.719676                 TA   =          345.27589
                                              MA   =          345.29982
                                              Ha   =            222.561  n.mi
                                              Hp   =            213.325
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14643303.13                 X    =        -4476699.74
     Y    =       -3100086.62  feet           Y    =         -994892.43  meter
     Z    =       16424928.61                 Z    =         4984603.95
     XDOT =      12078.650801                 XDOT =        3742.889078
     YDOT =     -21021.501210  feet/sec       YDOT =       -6365.840682  meter/sec
     ZDOT =       6793.699725                 ZDOT =        2088.753579
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14458958.81                 X    =         4407090.64
     Y    =       -4257485.03  feet           Y    =        -1297681.44  meter
     Z    =       16328731.57                 Z    =         4976997.38
     XDOT =       -952.429055                 XDOT =        -290.300376
     YDOT =      23158.856253  feet/sec       YDOT =        7058.819386  meter/sec
     ZDOT =       6874.555951                 ZDOT =        2095.364654
  
  
    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   17293.55189272  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6381 133.3721 0005157  36.3536 323.7966 15.54181738  1246
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17293.55189272   =   yrday.fracday
    Element set:     902
    Inclination:       51.6381  deg
    RA of node:       133.3721  deg
    Eccentricity:     .0005157     
    Arg of perigee:    36.3536  deg
    Mean anomaly:     323.7966  deg
    Mean motion:   15.54181738  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             124
    Checksum:              310
 
 
    Coasting Arc #4 (Orbit 136)
    ---------------------------------------
 
    Vector Time (GMT): 2017/294/08:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3329340.87                 A    =         6777047.54  meter
     Y    =        2541402.99  meter          E    =           .0018657
     Z    =       -5343477.17                 I    =           51.91227
     XDOT =      -4703.739879                 Wp   =           77.20964
     YDOT =       6039.376170  meter/sec      RA   =          128.23282  deg
     ZDOT =        -54.506396                 TA   =          192.24930
                                              MA   =          192.29473
                                              Ha   =            222.398  n.mi
                                              Hp   =            213.251
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10923034.36                 X    =         3326631.47
     Y    =        8337936.33  feet           Y    =         2578618.41  meter
     Z    =      -17531093.07                 Z    =        -5327310.60
     XDOT =     -15432.217450                 XDOT =       -4770.659428
     YDOT =      19814.226281  feet/sec       YDOT =        5986.401565  meter/sec
     ZDOT =       -178.826758                 ZDOT =         -77.519308
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8094721.44                 X    =        -2467271.09
     Y    =      -11216361.71  feet           Y    =        -3418747.05  meter
     Z    =      -17459719.38                 Z    =        -5321722.47
     XDOT =      19761.857264                 XDOT =        6023.414094
     YDOT =     -13803.565306  feet/sec       YDOT =       -4207.326705  meter/sec
     ZDOT =       -281.739493                 ZDOT =         -85.874197
  
  
    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   17294.38777204  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6402 129.2064 0005225  39.2528 320.9003 15.54236853  1377
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17294.38777204   =   yrday.fracday
    Element set:     903
    Inclination:       51.6402  deg
    RA of node:       129.2064  deg
    Eccentricity:     .0005225     
    Arg of perigee:    39.2528  deg
    Mean anomaly:     320.9003  deg
    Mean motion:   15.54236853  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             137
    Checksum:              292
 
 
    Coasting Arc #5 (Orbit 152)
    ---------------------------------------
 
    Vector Time (GMT): 2017/295/08:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2136137.42                 A    =         6778116.85  meter
     Y    =       -3967052.26  meter          E    =           .0010648
     Z    =        5058855.39                 I    =           51.93536
     XDOT =       5241.567901                 Wp   =           49.33982
     YDOT =      -5268.265271  meter/sec      RA   =          123.25213  deg
     ZDOT =      -1908.592602                 TA   =           59.13042
                                              MA   =           59.02573
                                              Ha   =            222.416  n.mi
                                              Hp   =            213.086
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7008324.86                 X    =        -2116192.12
     Y    =      -13015263.33  feet           Y    =        -3990828.21  meter
     Z    =       16597294.58                 Z    =         5048527.08
     XDOT =      17196.745083                 XDOT =        5309.360741
     YDOT =     -17284.334878  feet/sec       YDOT =       -5209.271534  meter/sec
     ZDOT =      -6261.786753                 ZDOT =       -1882.965043
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3220329.95                 X    =          981556.57
     Y    =       14479087.65  feet           Y    =         4413225.92  meter
     Z    =       16552020.43                 Z    =         5045055.83
     XDOT =     -20306.006233                 XDOT =       -6189.270700
     YDOT =      11579.065152  feet/sec       YDOT =        3529.299058  meter/sec
     ZDOT =      -6147.357367                 ZDOT =       -1873.714525
  
  
    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   17295.41654317  .00016717  00000-0  10270-3 0  9046
    2 25544  51.6399 124.0773 0005128  41.9960 318.1585 15.54264708  1536
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17295.41654317   =   yrday.fracday
    Element set:     904
    Inclination:       51.6399  deg
    RA of node:       124.0773  deg
    Eccentricity:     .0005128     
    Arg of perigee:    41.9960  deg
    Mean anomaly:     318.1585  deg
    Mean motion:   15.54264708  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             153
    Checksum:              316
 
 
    Coasting Arc #6 (Orbit 167)
    ---------------------------------------
 
    Vector Time (GMT): 2017/296/08:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         992355.81                 A    =         6781347.17  meter
     Y    =        5189748.84  meter          E    =           .0011335
     Z    =       -4259930.28                 I    =           51.96332
     XDOT =      -5403.943661                 Wp   =           86.11568
     YDOT =       4020.591869  meter/sec      RA   =          118.27862  deg
     ZDOT =       3648.407071                 TA   =          221.04975
                                              MA   =          221.13510
                                              Ha   =            222.443  n.mi
                                              Hp   =            213.088
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3255760.53                 X    =          954942.09
     Y    =       17026735.03  feet           Y    =         5200636.67  meter
     Z    =      -13976149.22                 Z    =        -4255200.69
     XDOT =     -17729.473953                 XDOT =       -5466.223992
     YDOT =      13190.918206  feet/sec       YDOT =        3959.813201  meter/sec
     ZDOT =      11969.839472                 ZDOT =        3622.004266
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        1218133.77                 X    =          371287.17
     Y    =      -17308714.32  feet           Y    =        -5275696.13  meter
     Z    =      -13955894.38                 Z    =        -4253756.61
     XDOT =      19374.066400                 XDOT =        5905.215439
     YDOT =      -8168.709605  feet/sec       YDOT =       -2489.822688  meter/sec
     ZDOT =      11852.123259                 ZDOT =        3612.527169
  
  
    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   17296.38101475  .00016717  00000-0  10270-3 0  9056
    2 25544  51.6402 119.2683 0005127  44.9260 315.2306 15.54238124  1680
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17296.38101475   =   yrday.fracday
    Element set:     905
    Inclination:       51.6402  deg
    RA of node:       119.2683  deg
    Eccentricity:     .0005127     
    Arg of perigee:    44.9260  deg
    Mean anomaly:     315.2306  deg
    Mean motion:   15.54238124  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             168
    Checksum:              290
 
 
    Coasting Arc #7 (Orbit 183)
    ---------------------------------------
 
    Vector Time (GMT): 2017/297/08:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         108657.46                 A    =         6785209.92  meter
     Y    =       -6098188.76  meter          E    =           .0017094
     Z    =        2960764.63                 I    =           51.99154
     XDOT =       5293.401792                 Wp   =           83.99470
     YDOT =      -2358.565666  meter/sec      RA   =          113.31616  deg
     ZDOT =      -5025.548356                 TA   =           62.34636
                                              MA   =           62.17295
                                              Ha   =            222.481  n.mi
                                              Hp   =            212.922
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         356487.74                 X    =          162458.67
     Y    =      -20007180.99  feet           Y    =        -6096672.77  meter
     Z    =        9713794.72                 Z    =         2961423.33
     XDOT =      17366.803779                 XDOT =        5343.794727
     YDOT =      -7738.076331  feet/sec       YDOT =       -2299.089620  meter/sec
     ZDOT =     -16488.019541                 ZDOT =       -4999.711557
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5179066.64                 X    =        -1578579.51
     Y    =       19326610.90  feet           Y    =         5890751.00  meter
     Z    =        9717590.35                 Z    =         2961921.54
     XDOT =     -17427.868490                 XDOT =       -5312.014316
     YDOT =       3606.076895  feet/sec       YDOT =        1099.132238  meter/sec
     ZDOT =     -16373.033077                 ZDOT =       -4990.500482
  
  
    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   17297.40977831  .00016717  00000-0  10270-3 0  9068
    2 25544  51.6406 114.1384 0005297  47.6784 312.4817 15.54266687  1844
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17297.40977831   =   yrday.fracday
    Element set:     906
    Inclination:       51.6406  deg
    RA of node:       114.1384  deg
    Eccentricity:     .0005297     
    Arg of perigee:    47.6784  deg
    Mean anomaly:     312.4817  deg
    Mean motion:   15.54266687  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             184
    Checksum:              336
 
 
    Coasting Arc #8 (Orbit 198)
    ---------------------------------------
 
    Vector Time (GMT): 2017/298/08:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1037020.99                 A    =         6788217.04  meter
     Y    =        6558716.29  meter          E    =           .0013749
     Z    =       -1385781.04                 I    =           52.01178
     XDOT =      -4951.347085                 Wp   =           42.93364
     YDOT =        441.613212  meter/sec      RA   =          108.36487  deg
     ZDOT =       5839.051418                 TA   =          302.04307
                                              MA   =          302.17655
                                              Ha   =            222.560  n.mi
                                              Hp   =            212.937
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3402299.83                 X    =        -1103553.64
     Y    =       21518098.07  feet           Y    =         6546747.58  meter
     Z    =       -4546525.72                 Z    =        -1390980.43
     XDOT =     -16244.577052                 XDOT =       -4984.281200
     YDOT =       1448.862243  feet/sec       YDOT =         386.059858  meter/sec
     ZDOT =      19156.992841                 ZDOT =        5814.918775
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8188965.18                 X    =         2495996.59
     Y    =      -20182318.54  feet           Y    =        -6151570.69  meter
     Z    =       -4570552.75                 Z    =        -1393104.48
     XDOT =      14797.861210                 XDOT =        4510.388097
     YDOT =       1722.447469  feet/sec       YDOT =         525.001989  meter/sec
     ZDOT =      19049.832774                 ZDOT =        5806.389030
  
  
    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   17298.37424213  .00016717  00000-0  10270-3 0  9077
    2 25544  51.6392 109.3298 0005231  51.2671 308.8949 15.54226620  1996
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17298.37424213   =   yrday.fracday
    Element set:     907
    Inclination:       51.6392  deg
    RA of node:       109.3298  deg
    Eccentricity:     .0005231     
    Arg of perigee:    51.2671  deg
    Mean anomaly:     308.8949  deg
    Mean motion:   15.54226620  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             199
    Checksum:              317
 
 
    Coasting Arc #9 (Orbit 214)
    ---------------------------------------
 
    Vector Time (GMT): 2017/299/08:55:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1868973.70                 A    =         6788995.32  meter
     Y    =       -6511523.47  meter          E    =           .0013045
     Z    =        -392854.96                 I    =           52.02436
     XDOT =       4447.795975                 Wp   =          115.16213
     YDOT =       1630.533309  meter/sec      RA   =          103.42030  deg
     ZDOT =      -6027.122021                 TA   =           69.04967
                                              MA   =           68.91012
                                              Ha   =            222.558  n.mi
                                              Hp   =            212.937
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6131803.49                 X    =         1943556.72
     Y    =      -21363265.98  feet           Y    =        -6490206.32  meter
     Z    =       -1288894.22                 Z    =         -383594.59
     XDOT =      14592.506479                 XDOT =        4458.509723
     YDOT =       5349.518730  feet/sec       YDOT =        1680.331377  meter/sec
     ZDOT =     -19774.022380                 ZDOT =       -6005.489595
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10513317.71                 X    =        -3204459.24
     Y    =       19584814.20  feet           Y    =         5969451.37  meter
     Z    =       -1246835.63                 Z    =         -380035.50
     XDOT =     -11832.394770                 XDOT =       -3606.513926
     YDOT =      -7569.714954  feet/sec       YDOT =       -2307.249118  meter/sec
     ZDOT =     -19678.254898                 ZDOT =       -5997.932093
  
  
    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   17299.40300024  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6399 104.2007 0005053  56.0661 304.0972 15.54221099  2157
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17299.40300024   =   yrday.fracday
    Element set:     908
    Inclination:       51.6399  deg
    RA of node:       104.2007  deg
    Eccentricity:     .0005053     
    Arg of perigee:    56.0661  deg
    Mean anomaly:     304.0972  deg
    Mean motion:   15.54221099  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             215
    Checksum:              277
 
 
    Coasting Arc #10 (Orbit 216)
    ---------------------------------------
 
    Vector Time (GMT): 2017/299/12:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2970068.71                 A    =         6787089.33  meter
     Y    =       -5736523.31  meter          E    =           .0009061
     Z    =       -2085024.52                 I    =           52.01726
     XDOT =       3578.021746                 Wp   =          104.79176
     YDOT =       3866.762654  meter/sec      RA   =          102.77575  deg
     ZDOT =      -5564.186474                 TA   =           98.14449
                                              MA   =           98.04169
                                              Ha   =            222.564  n.mi
                                              Hp   =            212.778
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        9744319.90                 X    =         3044123.52
     Y    =      -18820614.53  feet           Y    =        -5702895.95  meter
     Z    =       -6840631.62                 Z    =        -2070416.57
     XDOT =      11738.916491                 XDOT =        3561.545259
     YDOT =      12686.229180  feet/sec       YDOT =        3906.682292  meter/sec
     ZDOT =     -18255.204966                 ZDOT =       -5546.845319
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2937431.78                 X    =          895329.21
     Y    =       21010308.53  feet           Y    =         6403942.04  meter
     Z    =       -6774951.85                 Z    =        -2065005.32
     XDOT =     -15484.412365                 XDOT =       -4719.648889
     YDOT =      -3673.145248  feet/sec       YDOT =       -1119.574672  meter/sec
     ZDOT =     -18178.812678                 ZDOT =       -5540.902104
  
  
    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   17299.53159478  .00016717  00000-0  10270-3 0  9096
    2 25544  51.6376 103.5550 0005217  59.4684 300.6983 15.54275207  2177
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17299.53159478   =   yrday.fracday
    Element set:     909
    Inclination:       51.6376  deg
    RA of node:       103.5550  deg
    Eccentricity:     .0005217     
    Arg of perigee:    59.4684  deg
    Mean anomaly:     300.6983  deg
    Mean motion:   15.54275207  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             217
    Checksum:              327
 
 
    Coasting Arc #11 (Orbit 232)
    ---------------------------------------
 
    Vector Time (GMT): 2017/300/12:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3435985.73                 A    =         6783632.58  meter
     Y    =        4635453.37  meter          E    =           .0016860
     Z    =        3551047.41                 I    =           52.01196
     XDOT =      -2796.124010                 Wp   =           84.26474
     YDOT =      -5542.590209  meter/sec      RA   =           97.82155  deg
     ZDOT =       4512.957673                 TA   =          317.41872
                                              MA   =          317.54933
                                              Ha   =            222.647  n.mi
                                              Hp   =            212.729
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11272919.07                 X    =        -3504814.78
     Y    =       15208180.34  feet           Y    =         4596645.07  meter
     Z    =       11650418.00                 Z    =         3534188.87
     XDOT =      -9173.635204                 XDOT =       -2755.859583
     YDOT =     -18184.351079  feet/sec       YDOT =       -5573.633130  meter/sec
     ZDOT =      14806.291577                 ZDOT =        4499.472674
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         101615.50                 X    =           30972.40
     Y    =      -18976593.14  feet           Y    =        -5784065.59  meter
     Z    =       11574898.70                 Z    =         3528029.12
     XDOT =      16872.067660                 XDOT =        5142.606223
     YDOT =       9119.147452  feet/sec       YDOT =        2779.516143  meter/sec
     ZDOT =      14747.267732                 ZDOT =        4494.967205
  
  
    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   17300.56034714  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6377  98.4252 0005105  65.1773 294.9911 15.54270419  2332
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17300.56034714   =   yrday.fracday
    Element set:     910
    Inclination:       51.6377  deg
    RA of node:        98.4252  deg
    Eccentricity:     .0005105     
    Arg of perigee:    65.1773  deg
    Mean anomaly:     294.9911  deg
    Mean motion:   15.54270419  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             233
    Checksum:              295
 
 
    Coasting Arc #12 (Orbit 247)
    ---------------------------------------
 
    Vector Time (GMT): 2017/301/12:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3810717.98                 A    =         6779794.54  meter
     Y    =       -3123083.72  meter          E    =           .0015671
     Z    =       -4672563.77                 I    =           52.00287
     XDOT =       1961.693545                 Wp   =           69.65641
     YDOT =       6790.447488  meter/sec      RA   =           92.85849  deg
     ZDOT =      -2941.466393                 TA   =          171.17716
                                              MA   =          171.14959
                                              Ha   =            222.640  n.mi
                                              Hp   =            212.742
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12502355.57                 X    =         3868055.29
     Y    =      -10246337.65  feet           Y    =        -3080149.24  meter
     Z    =      -15329933.61                 Z    =        -4653912.81
     XDOT =       6436.002445                 XDOT =        1899.903576
     YDOT =      22278.371024  feet/sec       YDOT =        6812.038892  meter/sec
     ZDOT =      -9650.480293                 ZDOT =       -2932.087265
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3785066.47                 X    =        -1153688.26
     Y    =       15796055.17  feet           Y    =         4814637.62  meter
     Z    =      -15246675.29                 Z    =        -4647186.63
     XDOT =     -17544.303186                 XDOT =       -5347.503611
     YDOT =     -13471.105344  feet/sec       YDOT =       -4105.992909  meter/sec
     ZDOT =      -9609.876784                 ZDOT =       -2929.090444
  
  
    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   17301.52479968  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6380  93.6175 0005251  68.4946 291.6766 15.54267829  2486
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17301.52479968   =   yrday.fracday
    Element set:     911
    Inclination:       51.6380  deg
    RA of node:        93.6175  deg
    Eccentricity:     .0005251     
    Arg of perigee:    68.4946  deg
    Mean anomaly:     291.6766  deg
    Mean motion:   15.54267829  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             248
    Checksum:              341
 
 
    Coasting Arc #13 (Orbit 263)
    ---------------------------------------
 
    Vector Time (GMT): 2017/302/12:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4056516.68                 A    =         6777314.05  meter
     Y    =        1351432.74  meter          E    =           .0007992
     Z    =        5251549.09                 I    =           51.99538
     XDOT =      -1115.369471                 Wp   =           92.74381
     YDOT =      -7517.581343  meter/sec      RA   =           87.88436  deg
     ZDOT =       1071.242886                 TA   =          347.04300
                                              MA   =          347.06352
                                              Ha   =            222.763  n.mi
                                              Hp   =            212.653
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13308781.76                 X    =        -4096837.12
     Y    =        4433834.45  feet           Y    =         1305844.81  meter
     Z    =       17229491.78                 Z    =         5231745.49
     XDOT =      -3659.348659                 XDOT =       -1036.426625
     YDOT =     -24663.980783  feet/sec       YDOT =       -7529.612716  meter/sec
     ZDOT =       3514.576397                 ZDOT =        1066.016799
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7764515.24                 X    =         2366624.24
     Y    =      -11811999.72  feet           Y    =        -3600297.51  meter
     Z    =       17141380.12                 Z    =         5224692.66
     XDOT =      17342.775283                 XDOT =        5286.077906
     YDOT =      16476.903494  feet/sec       YDOT =        5022.160185  meter/sec
     ZDOT =       3492.528975                 ZDOT =        1064.522832
  
  
    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   17302.55354472  .00016717  00000-0  10270-3 0  9128
    2 25544  51.6381  88.4871 0005116  71.4015 288.7693 15.54267114  2644
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17302.55354472   =   yrday.fracday
    Element set:     912
    Inclination:       51.6381  deg
    RA of node:        88.4871  deg
    Eccentricity:     .0005116     
    Arg of perigee:    71.4015  deg
    Mean anomaly:     288.7693  deg
    Mean motion:   15.54267114  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             264
    Checksum:              306
 
 
    Coasting Arc #14 (Orbit 278)
    ---------------------------------------
 
    Vector Time (GMT): 2017/303/12:05:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4228479.96                 A    =         6777194.91  meter
     Y    =         521340.01  meter          E    =           .0019378
     Z    =       -5287265.32                 I    =           51.99396
     XDOT =        216.744068                 Wp   =           91.29428
     YDOT =       7595.216308  meter/sec      RA   =           82.90795  deg
     ZDOT =        924.746199                 TA   =          187.51091
                                              MA   =          187.53998
                                              Ha   =            222.642  n.mi
                                              Hp   =            212.693
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13872965.76                 X    =         4248019.30
     Y    =        1710433.11  feet           Y    =          568734.68  meter
     Z    =      -17346671.00                 Z    =        -5266676.91
     XDOT =        711.102585                 XDOT =         127.304182
     YDOT =      24918.688675  feet/sec       YDOT =        7597.140059  meter/sec
     ZDOT =       3033.944221                 ZDOT =         925.581366
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11895194.33                 X    =        -3625655.23
     Y    =        7553052.03  feet           Y    =         2302170.26  meter
     Z    =      -17255361.84                 Z    =        -5259434.29
     XDOT =     -15793.737231                 XDOT =       -4813.931108
     YDOT =     -17955.133401  feet/sec       YDOT =       -5472.724661  meter/sec
     ZDOT =       3036.476286                 ZDOT =         925.517972
  
  
    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   17303.51798858  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6392  83.6790 0005227  75.2463 284.9269 15.54282779  2792
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17303.51798858   =   yrday.fracday
    Element set:     913
    Inclination:       51.6392  deg
    RA of node:        83.6790  deg
    Eccentricity:     .0005227     
    Arg of perigee:    75.2463  deg
    Mean anomaly:     284.9269  deg
    Mean motion:   15.54282779  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             279
    Checksum:              352
 
 
    Coasting Arc #15 (Orbit 283)
    ---------------------------------------
 
    Vector Time (GMT): 2017/303/19:34:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2309991.43                 A    =         6782504.58  meter
     Y    =       -5059592.07  meter          E    =           .0011777
     Z    =       -3893995.45                 I    =           52.01242
     XDOT =       4031.761211                 Wp   =           73.92487
     YDOT =       5023.191745  meter/sec      RA   =           81.39561  deg
     ZDOT =      -4142.279196                 TA   =          152.76806
                                              MA   =          152.70626
                                              Ha   =            222.697  n.mi
                                              Hp   =            212.570
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7578712.03                 X    =         2385312.90
     Y    =      -16599711.50  feet           Y    =        -5033339.28  meter
     Z    =      -12775575.63                 Z    =        -3882590.74
     XDOT =      13227.563029                 XDOT =        3995.412400
     YDOT =      16480.287877  feet/sec       YDOT =        5068.074134  meter/sec
     ZDOT =     -13590.154844                 ZDOT =       -4122.782439
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       14546894.13                 X    =         4433893.33
     Y    =      -11076376.21  feet           Y    =        -3376079.47  meter
     Z    =      -12724165.67                 Z    =        -3878325.70
     XDOT =       3236.517849                 XDOT =         986.490641
     YDOT =      19736.731825  feet/sec       YDOT =        6015.755860  meter/sec
     ZDOT =     -13504.390503                 ZDOT =       -4116.138225
  
  
    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   17303.83946790  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6411  82.0792 0005404  73.2928 286.8818 15.54285842  2841
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17303.83946790   =   yrday.fracday
    Element set:     914
    Inclination:       51.6411  deg
    RA of node:        82.0792  deg
    Eccentricity:     .0005404     
    Arg of perigee:    73.2928  deg
    Mean anomaly:     286.8818  deg
    Mean motion:   15.54285842  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             284
    Checksum:              327
 
 
    Coasting Arc #16 (Orbit 299)
    ---------------------------------------
 
    Vector Time (GMT): 2017/304/19:34:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3036163.13                 A    =         6778925.65  meter
     Y    =        3609050.94  meter          E    =           .0011728
     Z    =        4860300.69                 I    =           51.99258
     XDOT =      -3534.779499                 Wp   =          101.09536
     YDOT =      -6340.614374  meter/sec      RA   =           76.42818  deg
     ZDOT =       2492.867537                 TA   =          324.52259
                                              MA   =          324.60053
                                              Ha   =            222.873  n.mi
                                              Hp   =            212.451
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9961165.13                 X    =        -3099904.29
     Y    =       11840718.32  feet           Y    =         3574742.46  meter
     Z    =       15945868.40                 Z    =         4845396.56
     XDOT =     -11597.045601                 XDOT =       -3475.723717
     YDOT =     -20802.540598  feet/sec       YDOT =       -6379.812306  meter/sec
     ZDOT =       8178.699269                 ZDOT =        2475.840238
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14339619.44                 X    =        -4370716.01
     Y    =        5993850.66  feet           Y    =         1826925.68  meter
     Z    =       15879143.82                 Z    =         4839963.04
     XDOT =       -520.036992                 XDOT =        -158.507275
     YDOT =     -22777.343202  feet/sec       YDOT =       -6942.534208  meter/sec
     ZDOT =       8104.113631                 ZDOT =        2470.133835
  
  
    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   17304.86820306  .00016717  00000-0  10270-3 0  9151
    2 25544  51.6391  76.9494 0005525  76.8822 283.2947 15.54280212  3004
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17304.86820306   =   yrday.fracday
    Element set:     915
    Inclination:       51.6391  deg
    RA of node:        76.9494  deg
    Eccentricity:     .0005525     
    Arg of perigee:    76.8822  deg
    Mean anomaly:     283.2947  deg
    Mean motion:   15.54280212  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             300
    Checksum:              309
 
 
    Coasting Arc #17 (Orbit 314)
    ---------------------------------------
 
    Vector Time (GMT): 2017/305/19:34:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 920041.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3752031.44                 A    =         6777044.03  meter
     Y    =       -1911912.91  meter          E    =           .0019998
     Z    =       -5327198.04                 I    =           51.97831
     XDOT =       2831.879040                 Wp   =           84.13495
     YDOT =       7089.423691  meter/sec      RA   =           71.45272  deg
     ZDOT =       -549.615294                 TA   =          180.63379
                                              MA   =          180.63633
                                              Ha   =            222.698  n.mi
                                              Hp   =            212.651
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12309814.42                 X    =         3799009.65
     Y    =       -6272680.16  feet           Y    =        -1869692.84  meter
     Z    =      -17477683.87                 Z    =        -5308857.15
     XDOT =       9290.941731                 XDOT =        2755.062564
     YDOT =      23259.264077  feet/sec       YDOT =        7120.662150  meter/sec
     ZDOT =      -1803.199782                 ZDOT =        -536.045656
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13917160.09                 X    =         4241950.40
     Y    =        -201059.94  feet           Y    =          -61283.07  meter
     Z    =      -17395968.23                 Z    =        -5302291.12
     XDOT =      -1834.667181                 XDOT =        -559.206557
     YDOT =      23969.383721  feet/sec       YDOT =        7305.868158  meter/sec
     ZDOT =      -1744.096065                 ZDOT =        -531.600481
  
  
    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   17305.83263862  .00016717  00000-0  10270-3 0  9168
    2 25544  51.6400  72.1412 0005291  79.9142 280.2607 15.54269850  3153
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17305.83263862   =   yrday.fracday
    Element set:     916
    Inclination:       51.6400  deg
    RA of node:        72.1412  deg
    Eccentricity:     .0005291     
    Arg of perigee:    79.9142  deg
    Mean anomaly:     280.2607  deg
    Mean motion:   15.54269850  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             315
    Checksum:              295
 
 
    Coasting Arc #18 (Orbit 319)
    ---------------------------------------
 
    Vector Time (GMT): 2017/306/03:17:54.191
    Vector Time (MET): N/A
    Weight (LBS)     : 919921.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3780901.11                 A    =         6777501.61  meter
     Y    =       -1817084.36  meter          E    =           .0019081
     Z    =       -5339748.20                 I    =           51.97648
     XDOT =       2894.443378                 Wp   =           84.96687
     YDOT =       7076.882928  meter/sec      RA   =           69.85503  deg
     ZDOT =       -358.232823                 TA   =          181.62402
                                              MA   =          181.63023
                                              Ha   =            222.613  n.mi
                                              Hp   =            213.295
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12404531.18                 X    =         3826877.77
     Y    =       -5961562.87  feet           Y    =        -1774547.04  meter
     Z    =      -17518858.91                 Z    =        -5321269.48
     XDOT =       9496.205309                 XDOT =        2816.832824
     YDOT =      23218.119844  feet/sec       YDOT =        7108.816600  meter/sec
     ZDOT =      -1175.304536                 ZDOT =        -344.361146
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -6007203.14                 X    =        -1830995.52
     Y    =      -12498136.66  feet           Y    =        -3809432.05  meter
     Z    =      -17436545.93                 Z    =        -5314659.20
     XDOT =      22272.929307                 XDOT =        6788.788853
     YDOT =      -9147.629574  feet/sec       YDOT =       -2788.197494  meter/sec
     ZDOT =      -1114.863831                 ZDOT =        -339.810496
  
  
    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   17306.15411765  .00016717  00000-0  10270-3 0  9172
    2 25544  51.6417  70.5389 0004316  77.5146 282.6490 15.54093233  3203
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17306.15411765   =   yrday.fracday
    Element set:     917
    Inclination:       51.6417  deg
    RA of node:        70.5389  deg
    Eccentricity:     .0004316     
    Arg of perigee:    77.5146  deg
    Mean anomaly:     282.6490  deg
    Mean motion:   15.54093233  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             320
    Checksum:              299
 
             

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