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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  14929.5432
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   88.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.118
   ET - UTC  (sec) :   68.18
   UT1 - UTC (sec) :    0.00
 
 
   Maneuvers contained within the current ephemeris are as follows:
 
 
   IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS) 
   IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
   DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP 
   ------------------------------------------------------------------------
   332/03:10:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.6  
   000/00:00:00.000           0.0               0.0              217.7  
   
   336/14:51:52.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.7  
   000/00:00:00.000           0.0               0.0              217.6  
   
   338/15:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.9  
   000/00:00:00.000           0.0               0.0              217.5  
   
   338/16:38:45.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.9  
   000/00:00:00.000           0.0               0.0              217.5  
   
 
 
    Coasting Arc #1 (Orbit 3006)
    ---------------------------------------
 
    Vector Time (GMT): 2016/330/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -262250.41                 A    =         6779465.10  meter
     Y    =       -4443667.70  meter          E    =           .0008465
     Z    =       -5120661.30                 I    =           51.45901
     XDOT =       7156.916742                 Wp   =          120.79917
     YDOT =      -2237.194819  meter/sec      RA   =          333.02400  deg
     ZDOT =       1572.574817                 TA   =          164.42757
                                              MA   =          164.40152
                                              Ha   =            219.903  n.mi
                                              Hp   =            217.606
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -860401.60                 X    =         -187666.27
     Y    =      -14578962.28  feet           Y    =        -4446183.30  meter
     Z    =      -16800069.87                 Z    =        -5121754.14
     XDOT =      23480.697974                 XDOT =        7173.762679
     YDOT =      -7339.878016  feet/sec       YDOT =       -2157.067188  meter/sec
     ZDOT =       5159.366196                 ZDOT =        1607.382857
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13434737.21                 X    =         4094907.90
     Y    =        5715200.94  feet           Y    =         1741993.25  meter
     Z    =      -16803960.67                 Z    =        -5121847.21
     XDOT =      -3263.082362                 XDOT =        -994.587504
     YDOT =      23311.794255  feet/sec       YDOT =        7105.434889  meter/sec
     ZDOT =       5312.180502                 ZDOT =        1619.152617
  
  
    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   16330.51329439  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6408 333.5634 0006155 255.7021 104.3448 15.53701844 30074
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16330.51329439   =   yrday.fracday
    Element set:     900
    Inclination:       51.6408  deg
    RA of node:       333.5634  deg
    Eccentricity:     .0006155     
    Arg of perigee:   255.7021  deg
    Mean anomaly:     104.3448  deg
    Mean motion:   15.53701844  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3007
    Checksum:              284
 
 
    Coasting Arc #2 (Orbit 3022)
    ---------------------------------------
 
    Vector Time (GMT): 2016/331/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1188936.46                 A    =         6781969.09  meter
     Y    =        4951461.32  meter          E    =           .0003237
     Z    =        4478551.19                 I    =           51.43837
     XDOT =      -6848.341762                 Wp   =           46.24009
     YDOT =       1260.787220  meter/sec      RA   =          328.01950  deg
     ZDOT =      -3208.324646                 TA   =           76.13246
                                              MA   =           76.09645
                                              Ha   =            219.602  n.mi
                                              Hp   =            217.584
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3900710.17                 X    =        -1265971.90
     Y    =       16244951.85  feet           Y    =         4937735.02  meter
     Z    =       14693409.42                 Z    =         4472588.51
     XDOT =     -22468.312868                 XDOT =       -6846.346256
     YDOT =       4136.441010  feet/sec       YDOT =        1184.215684  meter/sec
     ZDOT =     -10525.999496                 ZDOT =       -3241.587960
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13033605.77                 X    =        -3972643.04
     Y    =      -10489735.17  feet           Y    =        -3197271.28  meter
     Z    =       14666317.11                 Z    =         4470293.46
     XDOT =       4957.328822                 XDOT =        1510.993825
     YDOT =     -21097.236009  feet/sec       YDOT =       -6430.437536  meter/sec
     ZDOT =     -10671.848038                 ZDOT =       -3252.779282
  
  
    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   16331.54239316  .00016717  00000-0  10270-3 0  9015
    2 25544  51.6397 328.4362 0006211 260.2317  99.8135 15.53746063 30235
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16331.54239316   =   yrday.fracday
    Element set:     901
    Inclination:       51.6397  deg
    RA of node:       328.4362  deg
    Eccentricity:     .0006211     
    Arg of perigee:   260.2317  deg
    Mean anomaly:      99.8135  deg
    Mean motion:   15.53746063  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3023
    Checksum:              294
 
 
    Coasting Arc #3 (Orbit 3032)
    ---------------------------------------
 
    Vector Time (GMT): 2016/332/03:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4916785.07                 A    =         6781447.89  meter
     Y    =         994753.19  meter          E    =           .0004940
     Z    =        4564392.74                 I    =           51.42216
     XDOT =      -4003.705344                 Wp   =          162.09868
     YDOT =       5783.831015  meter/sec      RA   =          324.90361  deg
     ZDOT =       3046.805445                 TA   =          257.31609
                                              MA   =          257.37131
                                              Ha   =            219.557  n.mi
                                              Hp   =            217.668
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16131184.61                 X    =         4883123.75
     Y    =        3263625.94  feet           Y    =         1049547.63  meter
     Z    =       14975041.81                 Z    =         4588196.01
     XDOT =     -13135.516219                 XDOT =       -4082.884425
     YDOT =      18975.823540  feet/sec       YDOT =        5738.616085  meter/sec
     ZDOT =       9996.080855                 ZDOT =        3027.163904
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3291050.08                 X    =        -1003112.06
     Y    =      -16028416.80  feet           Y    =        -4885461.44  meter
     Z    =       15079028.24                 Z    =         4596087.81
     XDOT =      21466.337531                 XDOT =        6542.939679
     YDOT =       4931.259998  feet/sec       YDOT =        1503.048047  meter/sec
     ZDOT =       9908.951794                 ZDOT =        3020.248507
  
  
    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   16332.18557813  .00016717  00000-0  10270-3 0  9022
    2 25544  51.6421 325.2275 0006387 259.0488 100.9946 15.53760299 30332
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16332.18557813   =   yrday.fracday
    Element set:     902
    Inclination:       51.6421  deg
    RA of node:       325.2275  deg
    Eccentricity:     .0006387     
    Arg of perigee:   259.0488  deg
    Mean anomaly:     100.9946  deg
    Mean motion:   15.53760299  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3033
    Checksum:              318
 
 
    Coasting Arc #4 (Orbit 3047)
    ---------------------------------------
 
    Vector Time (GMT): 2016/333/03:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3850912.76                 A    =         6779058.51  meter
     Y    =       -2142541.62  meter          E    =           .0007714
     Z    =       -5158153.14                 I    =           51.38815
     XDOT =       4991.820436                 Wp   =           76.41287
     YDOT =      -5646.393351  meter/sec      RA   =          319.89611  deg
     ZDOT =      -1381.358558                 TA   =          180.24738
                                              MA   =          180.24776
                                              Ha   =            219.423  n.mi
                                              Hp   =            217.429
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12634228.22                 X    =        -3801611.51
     Y    =       -7029336.04  feet           Y    =        -2185329.22  meter
     Z    =      -16923074.62                 Z    =        -5176740.64
     XDOT =      16377.363636                 XDOT =        5061.299028
     YDOT =     -18524.912570  feet/sec       YDOT =       -5590.182921  meter/sec
     ZDOT =      -4532.016265                 ZDOT =       -1356.940554
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1304364.26                 X    =         -397570.22
     Y    =       14303438.22  feet           Y    =         4359687.97  meter
     Z    =      -17004000.45                 Z    =        -5182819.34
     XDOT =     -22566.582517                 XDOT =       -6878.294351
     YDOT =      -7317.320768  feet/sec       YDOT =       -2230.319370  meter/sec
     ZDOT =      -4424.014060                 ZDOT =       -1348.439485
  
  
    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   16333.15035117  .00016717  00000-0  10270-3 0  9039
    2 25544  51.6421 320.4219 0006240 263.4092  96.6351 15.53749190 30489
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16333.15035117   =   yrday.fracday
    Element set:     903
    Inclination:       51.6421  deg
    RA of node:       320.4219  deg
    Eccentricity:     .0006240     
    Arg of perigee:   263.4092  deg
    Mean anomaly:      96.6351  deg
    Mean motion:   15.53749190  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3048
    Checksum:              282
 
 
    Coasting Arc #5 (Orbit 3063)
    ---------------------------------------
 
    Vector Time (GMT): 2016/334/03:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2669570.16                 A    =         6778464.91  meter
     Y    =        3305875.95  meter          E    =           .0003762
     Z    =        5284565.61                 I    =           51.36210
     XDOT =      -5626.026738                 Wp   =          278.42266
     YDOT =       5190.743713  meter/sec      RA   =          314.88152  deg
     ZDOT =       -404.826440                 TA   =          175.45584
                                              MA   =          175.45242
                                              Ha   =            219.190  n.mi
                                              Hp   =            217.530
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8758432.29                 X    =         2606733.97
     Y    =       10846049.71  feet           Y    =         3335377.22  meter
     Z    =       17337813.69                 Z    =         5297381.54
     XDOT =     -18458.092974                 XDOT =       -5681.686314
     YDOT =      17029.999060  feet/sec       YDOT =        5127.518518  meter/sec
     ZDOT =      -1328.170736                 ZDOT =        -432.291663
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        6159164.01                 X    =         1877313.19
     Y    =      -12429254.76  feet           Y    =        -3788436.85  meter
     Z    =       17393246.94                 Z    =         5301461.67
     XDOT =      22338.846579                 XDOT =        6808.880437
     YDOT =       9040.117309  feet/sec       YDOT =        2755.427756  meter/sec
     ZDOT =      -1449.414054                 ZDOT =        -441.781404
  
  
    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   16334.17943650  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6420 315.2944 0006261 267.3464  92.6972 15.53767722 30648
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16334.17943650   =   yrday.fracday
    Element set:     904
    Inclination:       51.6420  deg
    RA of node:       315.2944  deg
    Eccentricity:     .0006261     
    Arg of perigee:   267.3464  deg
    Mean anomaly:      92.6972  deg
    Mean motion:   15.53767722  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3064
    Checksum:              315
 
 
    Coasting Arc #6 (Orbit 3078)
    ---------------------------------------
 
    Vector Time (GMT): 2016/335/03:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1465459.09                 A    =         6779956.95  meter
     Y    =       -4411337.83  meter          E    =           .0006603
     Z    =       -4941687.90                 I    =           51.34596
     XDOT =       5905.853360                 Wp   =          120.36351
     YDOT =      -4379.716346  meter/sec      RA   =          309.86801  deg
     ZDOT =       2157.180897                 TA   =          170.77325
                                              MA   =          170.76112
                                              Ha   =            219.264  n.mi
                                              Hp   =            217.421
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4807936.64                 X    =        -1392016.47
     Y    =      -14472893.16  feet           Y    =        -4427314.57  meter
     Z    =      -16212886.82                 Z    =        -4948628.80
     XDOT =      19376.159317                 XDOT =        5943.910704
     YDOT =     -14369.148117  feet/sec       YDOT =       -4313.460496  meter/sec
     ZDOT =       7077.365149                 ZDOT =        2185.962647
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10935076.07                 X    =        -3333011.19
     Y    =       10585248.13  feet           Y    =         3226383.63  meter
     Z    =      -16242389.71                 Z    =        -4950680.38
     XDOT =     -20629.556749                 XDOT =       -6287.888897
     YDOT =     -10251.340715  feet/sec       YDOT =       -3124.608650  meter/sec
     ZDOT =       7204.205180                 ZDOT =        2195.841739
  
  
    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   16335.14419947  .00016717  00000-0  10270-3 0  9059
    2 25544  51.6429 310.4890 0006208 270.5579  89.4862 15.53782231 30798
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16335.14419947   =   yrday.fracday
    Element set:     905
    Inclination:       51.6429  deg
    RA of node:       310.4890  deg
    Eccentricity:     .0006208     
    Arg of perigee:   270.5579  deg
    Mean anomaly:      89.4862  deg
    Mean motion:   15.53782231  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3079
    Checksum:              331
 
 
    Coasting Arc #7 (Orbit 3094)
    ---------------------------------------
 
    Vector Time (GMT): 2016/336/03:10:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         310590.07                 A    =         6783137.02  meter
     Y    =        5358371.09  meter          E    =           .0005035
     Z    =        4146206.02                 I    =           51.33656
     XDOT =      -5875.581338                 Wp   =           52.58008
     YDOT =       3225.288901  meter/sec      RA   =          304.85783  deg
     ZDOT =      -3721.958739                 TA   =           75.89117
                                              MA   =           75.83521
                                              Ha   =            219.426  n.mi
                                              Hp   =            217.503
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1018996.28                 X    =          230507.55
     Y    =       17579957.66  feet           Y    =         5361396.21  meter
     Z    =       13603038.11                 Z    =         4147520.74
     XDOT =     -19276.841661                 XDOT =       -5893.130741
     YDOT =      10581.656498  feet/sec       YDOT =        3159.486387  meter/sec
     ZDOT =     -12211.150720                 ZDOT =       -3750.543594
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       15233888.59                 X    =         4643289.24
     Y    =       -8825763.88  feet           Y    =        -2690092.83  meter
     Z    =       13607734.61                 Z    =         4147637.51
     XDOT =      17510.989884                 XDOT =        5337.349717
     YDOT =      11172.964351  feet/sec       YDOT =        3405.519534  meter/sec
     ZDOT =     -12336.897650                 ZDOT =       -3760.286404
  
  
    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   16336.17327443  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6432 305.3617 0006075 274.9054  85.1405 15.53750497 30953
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16336.17327443   =   yrday.fracday
    Element set:     906
    Inclination:       51.6432  deg
    RA of node:       305.3617  deg
    Eccentricity:     .0006075     
    Arg of perigee:   274.9054  deg
    Mean anomaly:      85.1405  deg
    Mean motion:   15.53750497  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3095
    Checksum:              310
 
 
    Coasting Arc #8 (Orbit 3101)
    ---------------------------------------
 
    Vector Time (GMT): 2016/336/14:51:52.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1917055.12                 A    =         6788533.70  meter
     Y    =       -6157752.71  meter          E    =           .0006443
     Z    =       -2105278.95                 I    =           51.34419
     XDOT =       5343.492003                 Wp   =          343.16841
     YDOT =       -214.448983  meter/sec      RA   =          302.42868  deg
     ZDOT =       5494.821593                 TA   =          353.41691
                                              MA   =          353.42537
                                              Ha   =            219.679  n.mi
                                              Hp   =            217.576
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        6289550.93                 X    =         1995996.87
     Y    =      -20202600.77  feet           Y    =        -6135873.35  meter
     Z    =       -6907083.17                 Z    =        -2095775.04
     XDOT =      17531.141741                 XDOT =        5318.801091
     YDOT =       -703.572780  feet/sec       YDOT =        -154.832988  meter/sec
     ZDOT =      18027.629898                 ZDOT =        5520.719263
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21072061.36                 X    =         6422764.30
     Y    =       -2064289.80  feet           Y    =         -629195.53  meter
     Z    =       -6864274.48                 Z    =        -2092230.86
     XDOT =       7300.397169                 XDOT =        2225.161057
     YDOT =      14218.348886  feet/sec       YDOT =        4333.752741  meter/sec
     ZDOT =      18141.022062                 ZDOT =        5529.383524
  
  
    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   16336.62349243  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6415 303.1219 0006228 282.1832  77.8623 15.53763262 31026
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16336.62349243   =   yrday.fracday
    Element set:     907
    Inclination:       51.6415  deg
    RA of node:       303.1219  deg
    Eccentricity:     .0006228     
    Arg of perigee:   282.1832  deg
    Mean anomaly:      77.8623  deg
    Mean motion:   15.53763262  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3102
    Checksum:              296
 
 
    Coasting Arc #9 (Orbit 3117)
    ---------------------------------------
 
    Vector Time (GMT): 2016/337/14:51:52.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2715041.28                 A    =         6790248.41  meter
     Y    =        6193810.13  meter          E    =           .0007741
     Z    =         555450.59                 I    =           51.33436
     XDOT =      -4599.314783                 Wp   =          148.10055
     YDOT =      -1479.381905  meter/sec      RA   =          297.43836  deg
     ZDOT =      -5953.276158                 TA   =           25.88160
                                              MA   =           25.84290
                                              Ha   =            219.841  n.mi
                                              Hp   =            217.567
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8907615.76                 X    =        -2786798.43
     Y    =       20320899.37  feet           Y    =         6163047.45  meter
     Z    =        1822344.45                 Z    =          542087.72
     XDOT =     -15089.615429                 XDOT =       -4553.511426
     YDOT =      -4853.615174  feet/sec       YDOT =       -1530.557925  meter/sec
     ZDOT =     -19531.745926                 ZDOT =       -5975.507546
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -22192023.51                 X    =        -6764128.77
     Y    =         112593.26  feet           Y    =           34318.43  meter
     Z    =        1762646.91                 Z    =          537254.78
     XDOT =      -1638.737918                 XDOT =        -499.487317
     YDOT =     -14025.977284  feet/sec       YDOT =       -4275.117876  meter/sec
     ZDOT =     -19628.762735                 ZDOT =       -5982.846882
  
  
    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   16337.65255980  .00016717  00000-0  10270-3 0  9085
    2 25544  51.6424 297.9955 0006226 285.3418  74.7046 15.53770019 31186
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16337.65255980   =   yrday.fracday
    Element set:     908
    Inclination:       51.6424  deg
    RA of node:       297.9955  deg
    Eccentricity:     .0006226     
    Arg of perigee:   285.3418  deg
    Mean anomaly:      74.7046  deg
    Mean motion:   15.53770019  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3118
    Checksum:              335
 
 
    Coasting Arc #10 (Orbit 3133)
    ---------------------------------------
 
    Vector Time (GMT): 2016/338/14:51:52.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3306814.60                 A    =         6789879.37  meter
     Y    =       -5830633.74  meter          E    =           .0011033
     Z    =        1036512.55                 I    =           51.31922
     XDOT =       3770.050949                 Wp   =           29.13974
     YDOT =       3184.913146  meter/sec      RA   =          292.44814  deg
     ZDOT =       5871.252175                 TA   =          342.14923
                                              MA   =          342.18795
                                              Ha   =            219.988  n.mi
                                              Hp   =            217.504
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       10849129.27                 X    =         3366733.51
     Y    =      -19129375.79  feet           Y    =        -5793319.77  meter
     Z    =        3400631.72                 Z    =         1052721.39
     XDOT =      12368.933559                 XDOT =        3705.636069
     YDOT =      10449.190112  feet/sec       YDOT =        3226.711759  meter/sec
     ZDOT =      19262.638370                 ZDOT =        5889.410035
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       21911638.61                 X    =         6678667.45
     Y    =        1738196.09  feet           Y    =          529802.17  meter
     Z    =        3472706.13                 Z    =         1058480.83
     XDOT =      -4177.735732                 XDOT =       -1273.373851
     YDOT =      13913.563066  feet/sec       YDOT =        4240.854023  meter/sec
     ZDOT =      19341.500872                 ZDOT =        5895.289466
  
  
    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   16338.68162130  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6424 292.8684 0006301 289.8205  70.2268 15.53777034 31345
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16338.68162130   =   yrday.fracday
    Element set:     909
    Inclination:       51.6424  deg
    RA of node:       292.8684  deg
    Eccentricity:     .0006301     
    Arg of perigee:   289.8205  deg
    Mean anomaly:      70.2268  deg
    Mean motion:   15.53777034  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3134
    Checksum:              313
 
 
    Coasting Arc #11 (Orbit 3133)
    ---------------------------------------
 
    Vector Time (GMT): 2016/338/15:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 896210.0
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4563833.84                 A    =         6784731.30  meter
     Y    =       -3488655.39  meter          E    =           .0006097
     Z    =        3603813.36                 I    =           51.30228
     XDOT =       1250.847731                 Wp   =           78.21207
     YDOT =       6167.975128  meter/sec      RA   =          292.43563  deg
     ZDOT =       4381.738522                 TA   =          324.70372
                                              MA   =          324.74407
                                              Ha   =            219.881  n.mi
                                              Hp   =            217.489
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14973208.15                 X    =         4584999.82
     Y    =      -11445719.77  feet           Y    =        -3437501.47  meter
     Z    =       11823534.63                 Z    =         3626034.58
     XDOT =       4103.831138                 XDOT =        1160.498174
     YDOT =      20236.138873  feet/sec       YDOT =        6181.457427  meter/sec
     ZDOT =      14375.782553                 ZDOT =        4387.595899
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       16961744.97                 X    =         5169939.87
     Y    =        8073111.27  feet           Y    =         2460684.32  meter
     Z    =       11921472.92                 Z    =         3633664.95
     XDOT =     -15619.471652                 XDOT =       -4760.814960
     YDOT =      11527.707811  feet/sec       YDOT =        3513.645341  meter/sec
     ZDOT =      14400.228390                 ZDOT =        4389.189613
  
  
    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   16338.68162098  .00016717  00000-0  10270-3 0  9109
    2 25544  51.6426 292.8685 0006258 289.4478  70.5998 15.53784477 31349
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16338.68162098   =   yrday.fracday
    Element set:     910
    Inclination:       51.6426  deg
    RA of node:       292.8685  deg
    Eccentricity:     .0006258     
    Arg of perigee:   289.4478  deg
    Mean anomaly:      70.5998  deg
    Mean motion:   15.53784477  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3134
    Checksum:              362
 
 
    Coasting Arc #12 (Orbit 3134)
    ---------------------------------------
 
    Vector Time (GMT): 2016/338/16:38:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911335.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4616274.99                 A    =         6780180.90  meter
     Y    =       -1010993.17  meter          E    =           .0001432
     Z    =        4862605.72                 I    =           51.28761
     XDOT =       -898.827478                 Wp   =          184.79614
     YDOT =       7239.947237  meter/sec      RA   =          292.08590  deg
     ZDOT =       2357.212940                 TA   =          241.99161
                                              MA   =          242.00610
                                              Ha   =            219.886  n.mi
                                              Hp   =            217.529
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15145259.15                 X    =         4603616.52
     Y    =       -3316906.71  feet           Y    =         -959442.04  meter
     Z    =       15953430.84                 Z    =         4884999.72
     XDOT =      -2948.909047                 XDOT =        -991.170005
     YDOT =      23753.107733  feet/sec       YDOT =        7229.379442  meter/sec
     ZDOT =       7733.638255                 ZDOT =        2352.622916
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13866943.85                 X    =         4226644.49
     Y    =        6704119.02  feet           Y    =         2043415.48  meter
     Z    =       16051646.55                 Z    =         4892541.87
     XDOT =     -16566.944797                 XDOT =       -5049.604774
     YDOT =      15791.699787  feet/sec       YDOT =        4813.310095  meter/sec
     ZDOT =       7712.148833                 ZDOT =        2350.662964
  
  
    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   16338.74593645  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6441 292.5488 0006281 289.5502  70.4972 15.53784082 31353
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16338.74593645   =   yrday.fracday
    Element set:     911
    Inclination:       51.6441  deg
    RA of node:       292.5488  deg
    Eccentricity:     .0006281     
    Arg of perigee:   289.5502  deg
    Mean anomaly:      70.4972  deg
    Mean motion:   15.53784082  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3135
    Checksum:              330
 
 
    Coasting Arc #13 (Orbit 3149)
    ---------------------------------------
 
    Vector Time (GMT): 2016/339/16:38:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911335.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4239019.02                 A    =         6778357.02  meter
     Y    =        -580859.21  meter          E    =           .0009587
     Z    =       -5265313.28                 I    =           51.27008
     XDOT =       1773.011039                 Wp   =           66.73096
     YDOT =      -7428.848616  meter/sec      RA   =          287.06620  deg
     ZDOT =       -605.046835                 TA   =          197.44231
                                              MA   =          197.47527
                                              Ha   =            220.146  n.mi
                                              Hp   =            217.219
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13907542.72                 X    =        -4206631.96
     Y    =       -1905706.08  feet           Y    =         -628081.33  meter
     Z    =      -17274649.86                 Z    =        -5285826.81
     XDOT =       5816.965352                 XDOT =        1858.889621
     YDOT =     -24372.862915  feet/sec       YDOT =       -7408.541399  meter/sec
     ZDOT =      -1985.061794                 ZDOT =        -596.225880
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -9827092.10                 X    =        -2995297.67
     Y    =       -9867789.05  feet           Y    =        -3007702.10  meter
     Z    =      -17364330.92                 Z    =        -5292648.06
     XDOT =      18672.821694                 XDOT =        5691.476052
     YDOT =     -15156.833394  feet/sec       YDOT =       -4619.802818  meter/sec
     ZDOT =      -1945.031487                 ZDOT =        -592.845597
  
  
    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   16339.71067356  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6435 287.7424 0006377 293.9863  66.0622 15.53823722 31502
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16339.71067356   =   yrday.fracday
    Element set:     912
    Inclination:       51.6435  deg
    RA of node:       287.7424  deg
    Eccentricity:     .0006377     
    Arg of perigee:   293.9863  deg
    Mean anomaly:      66.0622  deg
    Mean motion:   15.53823722  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3150
    Checksum:              323
 
 
    Coasting Arc #14 (Orbit 3165)
    ---------------------------------------
 
    Vector Time (GMT): 2016/340/16:38:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911335.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        3776911.29                 A    =         6778689.12  meter
     Y    =        2211244.07  meter          E    =           .0005708
     Z    =        5179471.18                 I    =           51.26202
     XDOT =      -2515.270496                 Wp   =          335.50832
     YDOT =       7139.572031  meter/sec      RA   =          282.04406  deg
     ZDOT =      -1209.279694                 TA   =          126.18623
                                              MA   =          126.13343
                                              Ha   =            220.266  n.mi
                                              Hp   =            217.323
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       12391441.25                 X    =         3726744.20
     Y    =        7254737.75  feet           Y    =         2253199.24  meter
     Z    =       16993015.69                 Z    =         5197696.78
     XDOT =      -8252.199791                 XDOT =       -2589.045911
     YDOT =      23423.792753  feet/sec       YDOT =        7111.032149  meter/sec
     ZDOT =      -3967.453063                 ZDOT =       -1221.677075
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5610645.94                 X    =         1710124.88
     Y    =       13114731.84  feet           Y    =         3997370.26  meter
     Z    =       17072377.67                 Z    =         5203660.71
     XDOT =     -19530.895794                 XDOT =       -5953.017038
     YDOT =      13612.334118  feet/sec       YDOT =        4149.039439  meter/sec
     ZDOT =      -4023.068097                 ZDOT =       -1226.231156
  
  
    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   16340.73972054  .00016717  00000-0  10270-3 0  9132
    2 25544  51.6428 282.6156 0006429 296.9742  63.0754 15.53840281 31666
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16340.73972054   =   yrday.fracday
    Element set:     913
    Inclination:       51.6428  deg
    RA of node:       282.6156  deg
    Eccentricity:     .0006429     
    Arg of perigee:   296.9742  deg
    Mean anomaly:      63.0754  deg
    Mean motion:   15.53840281  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3166
    Checksum:              322
 
 
    Coasting Arc #15 (Orbit 3180)
    ---------------------------------------
 
    Vector Time (GMT): 2016/341/16:38:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911335.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3277955.01                 A    =         6781046.95  meter
     Y    =       -3727344.54  meter          E    =           .0004242
     Z    =       -4623801.30                 I    =           51.26372
     XDOT =       3134.026203                 Wp   =           92.95162
     YDOT =      -6360.754968  meter/sec      RA   =          277.02435  deg
     ZDOT =       2907.834730                 TA   =          206.14243
                                              MA   =          206.16386
                                              Ha   =            220.427  n.mi
                                              Hp   =            217.119
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10754445.57                 X    =        -3213570.77
     Y    =      -12228820.68  feet           Y    =        -3763640.65  meter
     Z    =      -15169951.78                 Z    =        -4639568.60
     XDOT =      10282.238200                 XDOT =        3190.795825
     YDOT =     -20868.618660  feet/sec       YDOT =       -6325.390883  meter/sec
     ZDOT =       9540.140190                 ZDOT =        2923.196710
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1636197.23                 X    =         -498712.92
     Y    =      -16138381.77  feet           Y    =        -4918978.76  meter
     Z    =      -15238276.94                 Z    =        -4644626.81
     XDOT =      19218.002431                 XDOT =        5857.647141
     YDOT =     -11014.604025  feet/sec       YDOT =       -3357.251307  meter/sec
     ZDOT =       9608.572237                 ZDOT =        2928.692818
  
  
    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   16341.70444770  .00016717  00000-0  10270-3 0  9140
    2 25544  51.6425 277.8087 0006488 300.6187  59.4325 15.53833135 31813
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16341.70444770   =   yrday.fracday
    Element set:     914
    Inclination:       51.6425  deg
    RA of node:       277.8087  deg
    Eccentricity:     .0006488     
    Arg of perigee:   300.6187  deg
    Mean anomaly:      59.4325  deg
    Mean motion:   15.53833135  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3181
    Checksum:              317
 
 
    Coasting Arc #16 (Orbit 3196)
    ---------------------------------------
 
    Vector Time (GMT): 2016/342/16:38:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911335.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2733887.00                 A    =         6784452.64  meter
     Y    =        5038447.13  meter          E    =           .0007999
     Z    =        3627607.67                 I    =           51.27284
     XDOT =      -3671.748194                 Wp   =           53.83900
     YDOT =       5133.225954  meter/sec      RA   =          272.01189  deg
     ZDOT =      -4351.096057                 TA   =           82.88951
                                              MA   =           82.79856
                                              Ha   =            220.706  n.mi
                                              Hp   =            216.986
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8969445.54                 X    =         2659721.17
     Y    =       16530338.36  feet           Y    =         5068604.49  meter
     Z    =       11901599.97                 Z    =         3640708.29
     XDOT =     -12046.417959                 XDOT =       -3707.740502
     YDOT =      16841.292500  feet/sec       YDOT =        5091.964889  meter/sec
     ZDOT =     -14275.249532                 ZDOT =       -4369.019838
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1966873.28                 X    =         -599502.98
     Y    =       18667841.26  feet           Y    =         5689958.02  meter
     Z    =       11958019.62                 Z    =         3644804.38
     XDOT =     -18002.007967                 XDOT =       -5487.012028
     YDOT =       7322.210825  feet/sec       YDOT =        2231.809859  meter/sec
     ZDOT =     -14354.657306                 ZDOT =       -4375.299547
  
  
    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   16342.73348079  .00016717  00000-0  10270-3 0  9150
    2 25544  51.6429 272.6810 0006626 305.6297  54.4238 15.53870122 31977
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16342.73348079   =   yrday.fracday
    Element set:     915
    Inclination:       51.6429  deg
    RA of node:       272.6810  deg
    Eccentricity:     .0006626     
    Arg of perigee:   305.6297  deg
    Mean anomaly:      54.4238  deg
    Mean motion:   15.53870122  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3197
    Checksum:              321
 
 
    Coasting Arc #17 (Orbit 3211)
    ---------------------------------------
 
    Vector Time (GMT): 2016/343/16:38:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911335.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2164349.09                 A    =         6787909.26  meter
     Y    =       -6000334.56  meter          E    =           .0008253
     Z    =       -2305471.26                 I    =           51.28199
     XDOT =       4138.131577                 Wp   =          352.69041
     YDOT =      -3560.053378  meter/sec      RA   =          267.00817  deg
     ZDOT =       5386.652670                 TA   =          341.48285
                                              MA   =          341.51286
                                              Ha   =            220.816  n.mi
                                              Hp   =            216.922
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7100882.83                 X    =        -2085891.87
     Y    =      -19686137.01  feet           Y    =        -6024099.02  meter
     Z    =       -7563882.09                 Z    =        -2315794.81
     XDOT =      13576.547169                 XDOT =        4151.467212
     YDOT =     -11679.965150  feet/sec       YDOT =       -3513.703594  meter/sec
     ZDOT =      17672.744981                 ZDOT =        5406.787126
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4916179.36                 X    =         1498451.47
     Y    =      -20325566.49  feet           Y    =        -6195232.67  meter
     Z    =       -7607980.45                 Z    =        -2318912.44
     XDOT =      16180.981371                 XDOT =        4931.963122
     YDOT =      -2727.312482  feet/sec       YDOT =        -831.284844  meter/sec
     ZDOT =      17761.535303                 ZDOT =        5413.715960
  
  
    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   16343.69819516  .00016717  00000-0  10270-3 0  9166
    2 25544  51.6410 267.8735 0006568 308.4488  51.6075 15.53831975 32126
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16343.69819516   =   yrday.fracday
    Element set:     916
    Inclination:       51.6410  deg
    RA of node:       267.8735  deg
    Eccentricity:     .0006568     
    Arg of perigee:   308.4488  deg
    Mean anomaly:      51.6075  deg
    Mean motion:   15.53831975  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3212
    Checksum:              336
 
 
    Coasting Arc #18 (Orbit 3227)
    ---------------------------------------
 
    Vector Time (GMT): 2016/344/16:38:45.000
    Vector Time (MET): N/A
    Weight (LBS)     : 911335.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1528391.57                 A    =         6789908.76  meter
     Y    =        6569939.21  meter          E    =           .0006842
     Z    =         749592.44                 I    =           51.29192
     XDOT =      -4547.593941                 Wp   =          122.24926
     YDOT =       1737.591332  meter/sec      RA   =          262.01323  deg
     ZDOT =      -5920.905944                 TA   =           49.61397
                                              MA   =           49.55427
                                              Ha   =            221.002  n.mi
                                              Hp   =            216.745
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5014408.02                 X    =         1451169.99
     Y    =       21554918.67  feet           Y    =         6586598.91  meter
     Z    =        2459292.79                 Z    =          756829.72
     XDOT =     -14919.927628                 XDOT =       -4537.924623
     YDOT =       5700.758962  feet/sec       YDOT =        1686.791343  meter/sec
     ZDOT =     -19425.544437                 ZDOT =       -5942.973715
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7299903.66                 X    =        -2225010.63
     Y    =       20888257.18  feet           Y    =         6366740.79  meter
     Z    =        2489788.37                 Z    =          758887.49
     XDOT =     -14025.498905                 XDOT =       -4274.972066
     YDOT =      -2560.591431  feet/sec       YDOT =        -780.468268  meter/sec
     ZDOT =     -19522.466006                 ZDOT =       -5950.447639
  
  
    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   16344.72721776  .00016717  00000-0  10270-3 0  9172
    2 25544  51.6415 262.7467 0006496 311.9177  48.1421 15.53844474 32282
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      16344.72721776   =   yrday.fracday
    Element set:     917
    Inclination:       51.6415  deg
    RA of node:       262.7467  deg
    Eccentricity:     .0006496     
    Arg of perigee:   311.9177  deg
    Mean anomaly:      48.1421  deg
    Mean motion:   15.53844474  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3228
    Checksum:              328
 
             

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