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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15282.6
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   75.3
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.582
   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 
   ------------------------------------------------------------------------
   348/01:30:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.2  
   000/00:00:00.000           0.0               0.0              215.5  
   
   348/05:14:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.1  
   000/00:00:00.000           0.0               0.0              215.6  
   
   349/15:36:09.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.9  
   000/00:00:00.000           0.0               0.0              215.6  
   
   351/06:36:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.0  
   000/00:00:00.000           0.0               0.0              215.6  
   
   351/07:21:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.9  
   000/00:00:00.000           0.0               0.0              215.7  
   
   351/11:00:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.0  
   000/00:00:00.000           0.0               0.0              215.8  
   
   353/08:43:02.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.0  
   000/00:00:00.000           0.0               0.0              215.7  
   
   361/06:44:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.0  
   000/00:00:00.000           0.0               0.0              215.6  
   
   362/01:04:30.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              220.2  
   000/00:00:00.000           0.0               0.0              215.5  
   
 
 
    Coasting Arc #1 (Orbit 962)
    ---------------------------------------
 
    Vector Time (GMT): 2017/347/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919742.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4959580.49                 A    =         6789265.33  meter
     Y    =       -4629330.37  meter          E    =           .0009144
     Z    =         -46650.96                 I    =           51.39844
     XDOT =       3237.531411                 Wp   =           40.31287
     YDOT =      -3522.163774  meter/sec      RA   =          223.34199  deg
     ZDOT =       5992.039252                 TA   =          319.18301
                                              MA   =          319.25147
                                              Ha   =            220.139  n.mi
                                              Hp   =            215.573
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16271589.54                 X    =        -4907218.86
     Y    =      -15188091.77  feet           Y    =        -4684499.02  meter
     Z    =        -153054.35                 Z    =          -70616.37
     XDOT =      10621.822215                 XDOT =        3247.569909
     YDOT =     -11555.655425  feet/sec       YDOT =       -3485.903676  meter/sec
     ZDOT =      19658.921431                 ZDOT =        6007.790520
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17427611.26                 X    =         5311935.91
     Y    =      -13844767.35  feet           Y    =        -4219885.09  meter
     Z    =        -258778.38                 Z    =          -78875.65
     XDOT =       8865.375630                 XDOT =        2702.166492
     YDOT =      10815.006696  feet/sec       YDOT =        3296.414041  meter/sec
     ZDOT =      19729.345352                 ZDOT =        6013.504463
  
  
    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   17347.50015472  .00016717  00000-0  10270-3 0  9003
    2 25544  51.6413 224.4274 0002950 240.2437 119.8422 15.54148744  9633
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17347.50015472   =   yrday.fracday
    Element set:     900
    Inclination:       51.6413  deg
    RA of node:       224.4274  deg
    Eccentricity:     .0002950     
    Arg of perigee:   240.2437  deg
    Mean anomaly:     119.8422  deg
    Mean motion:   15.54148744  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             963
    Checksum:              290
 
 
    Coasting Arc #2 (Orbit 971)
    ---------------------------------------
 
    Vector Time (GMT): 2017/348/01:30:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 919742.1
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2645142.82                 A    =         6777392.56  meter
     Y    =        3310652.13  meter          E    =           .0012454
     Z    =       -5299939.01                 I    =           51.37117
     XDOT =      -5885.593096                 Wp   =           96.31177
     YDOT =      -4900.239557  meter/sec      RA   =          220.52830  deg
     ZDOT =       -125.136294                 TA   =          172.49924
                                              MA   =          172.48060
                                              Ha   =            220.243  n.mi
                                              Hp   =            215.467
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8678290.10                 X    =        -2656222.07
     Y    =       10861719.59  feet           Y    =         3281010.71  meter
     Z    =      -17388251.36                 Z    =        -5312815.13
     XDOT =     -19309.688636                 XDOT =       -5829.752015
     YDOT =     -16076.901435  feet/sec       YDOT =       -4965.744049  meter/sec
     ZDOT =       -410.552147                 ZDOT =        -153.591642
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12663202.76                 X    =         3859744.20
     Y    =        5561059.97  feet           Y    =         1695011.08  meter
     Z    =      -17445883.89                 Z    =        -5317505.41
     XDOT =     -10306.135281                 XDOT =       -3141.310034
     YDOT =      21802.613039  feet/sec       YDOT =        6645.436454  meter/sec
     ZDOT =       -536.178663                 ZDOT =        -163.427257
  
  
    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   17348.07887164  .00016717  00000-0  10270-3 0  9012
    2 25544  51.6404 221.5409 0002956 236.8315 123.2555 15.54118817  9727
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17348.07887164   =   yrday.fracday
    Element set:     901
    Inclination:       51.6404  deg
    RA of node:       221.5409  deg
    Eccentricity:     .0002956     
    Arg of perigee:   236.8315  deg
    Mean anomaly:     123.2555  deg
    Mean motion:   15.54118817  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             972
    Checksum:              313
 
 
    Coasting Arc #3 (Orbit 974)
    ---------------------------------------
 
    Vector Time (GMT): 2017/348/05:14:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904510.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -100195.00                 A    =         6780050.37  meter
     Y    =       -4924219.74  meter          E    =           .0006881
     Z    =        4657786.86                 I    =           51.38112
     XDOT =       6641.351274                 Wp   =          136.84092
     YDOT =       2566.591636  meter/sec      RA   =          219.76956  deg
     ZDOT =       2848.843128                 TA   =          284.73167
                                              MA   =          284.80791
                                              Ha   =            220.117  n.mi
                                              Hp   =            215.584
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        -328723.75                 X    =          -67749.08
     Y    =      -16155576.58  feet           Y    =        -4925159.07  meter
     Z    =       15281452.95                 Z    =         4657378.63
     XDOT =      21789.210216                 XDOT =        6598.318935
     YDOT =       8420.576234  feet/sec       YDOT =        2640.618976  meter/sec
     ZDOT =       9346.598188                 ZDOT =        2881.000728
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4899952.59                 X    =        -1493505.55
     Y    =       15399194.18  feet           Y    =         4693674.39  meter
     Z    =       15280340.36                 Z    =         4657447.74
     XDOT =     -16633.421860                 XDOT =       -5069.866983
     YDOT =     -14732.611471  feet/sec       YDOT =       -4490.499976  meter/sec
     ZDOT =       9488.994902                 ZDOT =        2892.245646
  
  
    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   17348.27177629  .00016717  00000-0  10270-3 0  9023
    2 25544  51.6374 220.5800 0003001 241.2274 118.8577 15.54154450  9753
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17348.27177629   =   yrday.fracday
    Element set:     902
    Inclination:       51.6374  deg
    RA of node:       220.5800  deg
    Eccentricity:     .0003001     
    Arg of perigee:   241.2274  deg
    Mean anomaly:     118.8577  deg
    Mean motion:   15.54154450  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             975
    Checksum:              300
 
 
    Coasting Arc #4 (Orbit 989)
    ---------------------------------------
 
    Vector Time (GMT): 2017/349/05:14:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904510.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1437799.03                 A    =         6777720.67  meter
     Y    =        4081121.75  meter          E    =           .0011608
     Z    =       -5226926.95                 I    =           51.39945
     XDOT =      -6663.114702                 Wp   =           86.44492
     YDOT =      -3640.805634  meter/sec      RA   =          214.75495  deg
     ZDOT =      -1011.078653                 TA   =          173.83853
                                              MA   =          173.82424
                                              Ha   =            220.129  n.mi
                                              Hp   =            215.535
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4717188.42                 X    =        -1457938.27
     Y    =       13389507.07  feet           Y    =         4064931.12  meter
     Z    =      -17148710.46                 Z    =        -5233959.99
     XDOT =     -21860.612541                 XDOT =       -6616.995646
     YDOT =     -11944.900375  feet/sec       YDOT =       -3715.059189  meter/sec
     ZDOT =      -3317.187183                 ZDOT =       -1043.334600
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8552983.73                 X    =         2606949.44
     Y    =      -11282085.23  feet           Y    =        -3438779.58  meter
     Z    =      -17180513.93                 Z    =        -5236620.64
     XDOT =      16196.231936                 XDOT =        4936.611494
     YDOT =      17540.992140  feet/sec       YDOT =        5346.494404  meter/sec
     ZDOT =      -3459.887364                 ZDOT =       -1054.573668
  
  
    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   17349.23630300  .00016717  00000-0  10270-3 0  9031
    2 25544  51.6379 215.7712 0002848 244.7616 115.3242 15.54129556  9909
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17349.23630300   =   yrday.fracday
    Element set:     903
    Inclination:       51.6379  deg
    RA of node:       215.7712  deg
    Eccentricity:     .0002848     
    Arg of perigee:   244.7616  deg
    Mean anomaly:     115.3242  deg
    Mean motion:   15.54129556  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             990
    Checksum:              304
 
 
    Coasting Arc #5 (Orbit 996)
    ---------------------------------------
 
    Vector Time (GMT): 2017/349/15:36:09.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904510.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6149898.41                 A    =         6787376.62  meter
     Y    =        1990117.30  meter          E    =           .0011849
     Z    =        2048982.73                 I    =           51.44316
     XDOT =        129.196484                 Wp   =          121.27418
     YDOT =       5313.406899  meter/sec      RA   =          212.56655  deg
     ZDOT =      -5530.871849                 TA   =           35.99432
                                              MA   =           35.91458
                                              Ha   =            219.918  n.mi
                                              Hp   =            215.621
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       20176832.04                 X    =         6117234.26
     Y    =        6529256.22  feet           Y    =         2058706.85  meter
     Z    =        6722384.28                 Z    =         2078778.15
     XDOT =        423.872980                 XDOT =          96.637456
     YDOT =      17432.437332  feet/sec       YDOT =        5314.670096  meter/sec
     ZDOT =     -18145.905017                 ZDOT =       -5530.322865
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10479912.64                 X    =         3194277.37
     Y    =       18387898.31  feet           Y    =         5604631.40  meter
     Z    =        6854401.16                 Z    =         2089221.47
     XDOT =      -9999.943080                 XDOT =       -3047.982651
     YDOT =      12484.068959  feet/sec       YDOT =        3805.144219  meter/sec
     ZDOT =     -18144.217203                 ZDOT =       -5530.357403
  
  
    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   17349.68641247  .00016717  00000-0  10270-3 0  9043
    2 25544  51.6371 213.5244 0003113 247.2915 112.7909 15.54164177  9979
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17349.68641247   =   yrday.fracday
    Element set:     904
    Inclination:       51.6371  deg
    RA of node:       213.5244  deg
    Eccentricity:     .0003113     
    Arg of perigee:   247.2915  deg
    Mean anomaly:     112.7909  deg
    Mean motion:   15.54164177  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:             997
    Checksum:              316
 
 
    Coasting Arc #6 (Orbit 1011)
    ---------------------------------------
 
    Vector Time (GMT): 2017/350/15:36:09.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904510.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6141299.71                 A    =         6789200.90  meter
     Y    =       -2857244.98  meter          E    =           .0008559
     Z    =        -390706.51                 I    =           51.47673
     XDOT =       1708.682343                 Wp   =           34.94150
     YDOT =      -4480.843725  meter/sec      RA   =          207.58224  deg
     ZDOT =       5982.594565                 TA   =          320.83734
                                              MA   =          320.89925
                                              Ha   =            220.080  n.mi
                                              Hp   =            215.612
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20148621.10                 X    =        -6106994.92
     Y    =       -9374163.31  feet           Y    =        -2925729.34  meter
     Z    =       -1281845.50                 Z    =         -420456.24
     XDOT =       5605.913198                 XDOT =        1729.600617
     YDOT =     -14700.930856  feet/sec       YDOT =       -4461.619718  meter/sec
     ZDOT =      19627.934926                 ZDOT =        5990.945231
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8920636.26                 X    =        -2719009.93
     Y    =      -20344756.16  feet           Y    =        -6201081.68  meter
     Z    =       -1413557.00                 Z    =         -430852.17
     XDOT =      12340.634266                 XDOT =        3761.425324
     YDOT =      -6762.546037  feet/sec       YDOT =       -2061.224032  meter/sec
     ZDOT =      19665.648526                 ZDOT =        5994.089671
  
  
    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   17350.65093719  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6367 208.7158 0002931 244.4617 115.6233 15.54144599 10126
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17350.65093719   =   yrday.fracday
    Element set:     905
    Inclination:       51.6367  deg
    RA of node:       208.7158  deg
    Eccentricity:     .0002931     
    Arg of perigee:   244.4617  deg
    Mean anomaly:     115.6233  deg
    Mean motion:   15.54144599  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1012
    Checksum:              308
 
 
    Coasting Arc #7 (Orbit 1021)
    ---------------------------------------
 
    Vector Time (GMT): 2017/351/06:36:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904510.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         -30337.41                 A    =         6778205.84  meter
     Y    =        4461137.03  meter          E    =           .0010629
     Z    =       -5112621.71                 I    =           51.45964
     XDOT =      -7246.764127                 Wp   =           78.33863
     YDOT =      -1891.793694  meter/sec      RA   =          204.48102  deg
     ZDOT =      -1608.464522                 TA   =          176.09361
                                              MA   =          176.08531
                                              Ha   =            219.988  n.mi
                                              Hp   =            215.617
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =         -99532.19                 X    =          -55386.03
     Y    =       14636276.35  feet           Y    =         4460658.28  meter
     Z    =      -16773693.26                 Z    =        -5112829.43
     XDOT =     -23775.472858                 XDOT =       -7217.257809
     YDOT =      -6206.672226  feet/sec       YDOT =       -1972.666809  meter/sec
     ZDOT =      -5277.114572                 ZDOT =       -1643.595812
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1086375.72                 X    =         -331127.32
     Y    =      -14594462.58  feet           Y    =        -4448392.19  meter
     Z    =      -16775241.50                 Z    =        -5113093.61
     XDOT =      23067.988280                 XDOT =        7031.122828
     YDOT =       4524.780385  feet/sec       YDOT =        1379.153061  meter/sec
     ZDOT =      -5432.875379                 ZDOT =       -1655.940416
  
  
    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   17351.29395221  .00016717  00000-0  10270-3 0  9063
    2 25544  51.6381 205.5142 0002822 256.0703 104.0136 15.54148171 10229
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17351.29395221   =   yrday.fracday
    Element set:     906
    Inclination:       51.6381  deg
    RA of node:       205.5142  deg
    Eccentricity:     .0002822     
    Arg of perigee:   256.0703  deg
    Mean anomaly:     104.0136  deg
    Mean motion:   15.54148171  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1022
    Checksum:              266
 
 
    Coasting Arc #8 (Orbit 1022)
    ---------------------------------------
 
    Vector Time (GMT): 2017/351/07:21:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904510.4
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        -552379.28                 A    =         6778774.25  meter
     Y    =       -4585970.78  meter          E    =           .0004824
     Z    =        4960691.01                 I    =           51.46314
     XDOT =       7233.025336                 Wp   =          150.17527
     YDOT =       1421.758459  meter/sec      RA   =          204.32950  deg
     ZDOT =       2114.778076                 TA   =          279.15431
                                              MA   =          279.20888
                                              Ha   =            219.921  n.mi
                                              Hp   =            215.656
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1812267.99                 X    =         -525153.42
     Y    =      -15045835.88  feet           Y    =        -4591996.17  meter
     Z    =       16275232.96                 Z    =         4958073.33
     XDOT =      23730.398084                 XDOT =        7206.316662
     YDOT =       4664.561874  feet/sec       YDOT =        1502.493524  meter/sec
     ZDOT =       6938.248282                 ZDOT =        2149.849369
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5868860.00                 X    =         1788828.53
     Y    =       13984825.51  feet           Y    =         4262574.82  meter
     Z    =       16264250.31                 Z    =         4957343.50
     XDOT =     -23049.921035                 XDOT =       -7025.615932
     YDOT =       1404.007737  feet/sec       YDOT =         427.941558  meter/sec
     ZDOT =       7093.809294                 ZDOT =        2162.193073
  
  
    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   17351.35825259  .00016717  00000-0  10270-3 0  9070
    2 25544  51.6386 205.1945 0002985 255.3333 104.7489 15.54171803 10239
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17351.35825259   =   yrday.fracday
    Element set:     907
    Inclination:       51.6386  deg
    RA of node:       205.1945  deg
    Eccentricity:     .0002985     
    Arg of perigee:   255.3333  deg
    Mean anomaly:     104.7489  deg
    Mean motion:   15.54171803  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1023
    Checksum:              313
 
 
    Coasting Arc #9 (Orbit 1024)
    ---------------------------------------
 
    Vector Time (GMT): 2017/351/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925679.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5207178.68                 A    =         6787911.66  meter
     Y    =        3914907.93  meter          E    =           .0006536
     Z    =       -1893292.28                 I    =           51.49871
     XDOT =      -4287.019537                 Wp   =          166.97144
     YDOT =       2995.547500  meter/sec      RA   =          203.57039  deg
     ZDOT =      -5606.606258                 TA   =           33.92006
                                              MA   =           33.87828
                                              Ha   =            220.005  n.mi
                                              Hp   =            215.810
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17083919.54                 X    =         5172210.85
     Y    =       12844186.14  feet           Y    =         3972942.86  meter
     Z    =       -6211588.83                 Z    =        -1868081.77
     XDOT =     -14065.024727                 XDOT =       -4292.963642
     YDOT =       9827.911744  feet/sec       YDOT =        2947.574501  meter/sec
     ZDOT =     -18394.377488                 ZDOT =       -5627.445495
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17844817.26                 X    =        -5439100.30
     Y    =       11822338.97  feet           Y    =         3603448.92  meter
     Z    =       -6100168.72                 Z    =        -1859331.43
     XDOT =      -3716.120212                 XDOT =       -1132.673441
     YDOT =     -15131.131309  feet/sec       YDOT =       -4611.968823  meter/sec
     ZDOT =     -18487.351615                 ZDOT =       -5634.944772
  
  
    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   17351.48685591  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6397 204.5543 0003081 255.6042 104.4769 15.54111157 10252
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17351.48685591   =   yrday.fracday
    Element set:     908
    Inclination:       51.6397  deg
    RA of node:       204.5543  deg
    Eccentricity:     .0003081     
    Arg of perigee:   255.6042  deg
    Mean anomaly:     104.4769  deg
    Mean motion:   15.54111157  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1025
    Checksum:              304
 
 
    Coasting Arc #10 (Orbit 1040)
    ---------------------------------------
 
    Vector Time (GMT): 2017/352/11:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 925679.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4110826.85                 A    =         6784565.33  meter
     Y    =       -4208923.87  meter          E    =           .0009540
     Z    =        3370697.73                 I    =           51.51806
     XDOT =       5794.842740                 Wp   =           90.85686
     YDOT =      -1938.747141  meter/sec      RA   =          198.58314  deg
     ZDOT =       4634.883040                 TA   =          308.56631
                                              MA   =          308.65175
                                              Ha   =            219.943  n.mi
                                              Hp   =            215.778
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13486964.73                 X    =        -4079829.24
     Y    =      -13808805.33  feet           Y    =        -4254721.01  meter
     Z    =       11058719.58                 Z    =         3350803.36
     XDOT =      19011.951247                 XDOT =        5793.577610
     YDOT =      -6360.718965  feet/sec       YDOT =       -1873.952862  meter/sec
     ZDOT =      15206.309186                 ZDOT =        4663.029359
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17414352.54                 X    =         5307894.65
     Y    =       -8441297.73  feet           Y    =        -2572907.55  meter
     Z    =       10970935.21                 Z    =         3343941.05
     XDOT =       -626.900143                 XDOT =        -191.079163
     YDOT =      18682.232260  feet/sec       YDOT =        5694.344393  meter/sec
     ZDOT =      15331.607106                 ZDOT =        4673.073846
  
  
    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   17352.51567756  .00016717  00000-0  10270-3 0  9096
    2 25544  51.6396 199.4247 0003030 264.1255  95.9552 15.54136365 10419
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17352.51567756   =   yrday.fracday
    Element set:     909
    Inclination:       51.6396  deg
    RA of node:       199.4247  deg
    Eccentricity:     .0003030     
    Arg of perigee:   264.1255  deg
    Mean anomaly:      95.9552  deg
    Mean motion:   15.54136365  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1041
    Checksum:              319
 
 
    Coasting Arc #11 (Orbit 1054)
    ---------------------------------------
 
    Vector Time (GMT): 2017/353/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1785074.76                 A    =         6779415.25  meter
     Y    =       -4405370.06  meter          E    =           .0005144
     Z    =        4832455.98                 I    =           51.53009
     XDOT =       7254.081104                 Wp   =          138.31022
     YDOT =       -214.092167  meter/sec      RA   =          194.05928  deg
     ZDOT =       2479.151511                 TA   =          287.27491
                                              MA   =          287.33119
                                              Ha   =            219.977  n.mi
                                              Hp   =            215.681
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5856544.50                 X    =        -1759153.74
     Y    =      -14453313.85  feet           Y    =        -4425187.62  meter
     Z    =       15854514.37                 Z    =         4823847.09
     XDOT =      23799.478688                 XDOT =        7243.893513
     YDOT =       -702.402122  feet/sec       YDOT =        -133.029327  meter/sec
     ZDOT =       8133.699184                 ZDOT =        2514.364793
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13598842.50                 X    =         4144927.19
     Y    =        7711083.59  feet           Y    =         2350338.28  meter
     Z    =       15816880.01                 Z    =         4820985.03
     XDOT =     -17709.082233                 XDOT =       -5397.728265
     YDOT =      14190.426187  feet/sec       YDOT =        4325.241902  meter/sec
     ZDOT =       8290.171033                 ZDOT =        2526.844131
  
  
    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   17353.41589527  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6403 194.9366 0002849 265.1888  94.8939 15.54146019 10559
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17353.41589527   =   yrday.fracday
    Element set:     910
    Inclination:       51.6403  deg
    RA of node:       194.9366  deg
    Eccentricity:     .0002849     
    Arg of perigee:   265.1888  deg
    Mean anomaly:      94.8939  deg
    Mean motion:   15.54146019  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1055
    Checksum:              341
 
 
    Coasting Arc #12 (Orbit 1069)
    ---------------------------------------
 
    Vector Time (GMT): 2017/354/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =           5568.03                 A    =         6777368.45  meter
     Y    =        4251826.36  meter          E    =           .0011740
     Z    =       -5287965.75                 I    =           51.55495
     XDOT =      -7601.580945                 Wp   =           84.10535
     YDOT =       -731.931274  meter/sec      RA   =          189.05487  deg
     ZDOT =       -596.480718                 TA   =          180.18841
                                              MA   =          180.18885
                                              Ha   =            219.853  n.mi
                                              Hp   =            215.655
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =          18267.81                 X    =          -16291.22
     Y    =       13949561.55  feet           Y    =         4251767.00  meter
     Z    =      -17348968.99                 Z    =        -5287991.31
     XDOT =     -24939.570028                 XDOT =       -7589.933930
     YDOT =      -2401.349323  feet/sec       YDOT =        -816.872158  meter/sec
     ZDOT =      -1956.957735                 ZDOT =        -633.378487
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8883885.33                 X    =        -2707808.25
     Y    =      -10753735.79  feet           Y    =        -3277738.67  meter
     Z    =      -17349670.73                 Z    =        -5288179.64
     XDOT =      20094.345607                 XDOT =        6124.756541
     YDOT =     -13178.523827  feet/sec       YDOT =       -4016.814063  meter/sec
     ZDOT =      -2120.808911                 ZDOT =        -646.422556
  
  
    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   17354.38041187  .00016717  00000-0  10270-3 0  9111
    2 25544  51.6396 190.1287 0002936 270.5103  89.5714 15.54171603 10703
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17354.38041187   =   yrday.fracday
    Element set:     911
    Inclination:       51.6396  deg
    RA of node:       190.1287  deg
    Eccentricity:     .0002936     
    Arg of perigee:   270.5103  deg
    Mean anomaly:      89.5714  deg
    Mean motion:   15.54171603  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1070
    Checksum:              298
 
 
    Coasting Arc #13 (Orbit 1085)
    ---------------------------------------
 
    Vector Time (GMT): 2017/355/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1807976.77                 A    =         6777723.29  meter
     Y    =       -3985736.49  meter          E    =           .0002629
     Z    =        5175363.84                 I    =           51.58951
     XDOT =       7379.124980                 Wp   =            8.84553
     YDOT =       1593.818669  meter/sec      RA   =          184.05042  deg
     ZDOT =      -1347.754046                 TA   =           94.13058
                                              MA   =           94.10054
                                              Ha   =            219.698  n.mi
                                              Hp   =            215.704
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        5931682.30                 X    =         1827272.77
     Y    =      -13076563.30  feet           Y    =        -3965411.11  meter
     Z    =       16979540.14                 Z    =         5184192.82
     XDOT =      24209.727626                 XDOT =        7367.300724
     YDOT =       5229.063874  feet/sec       YDOT =        1676.271115  meter/sec
     ZDOT =      -4421.765243                 ZDOT =       -1311.937340
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3946869.44                 X    =         1203005.81
     Y    =       13756849.82  feet           Y    =         4193087.82  meter
     Z    =       17019325.80                 Z    =         5187490.50
     XDOT =     -20924.889320                 XDOT =       -6377.906265
     YDOT =      11287.806135  feet/sec       YDOT =        3440.523310  meter/sec
     ZDOT =      -4262.810442                 ZDOT =       -1299.304623
  
  
    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   17355.40922807  .00016717  00000-0  10270-3 0  9123
    2 25544  51.6402 185.0000 0003118 273.6361  86.4435 15.54191927 10864
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17355.40922807   =   yrday.fracday
    Element set:     912
    Inclination:       51.6402  deg
    RA of node:       185.0000  deg
    Eccentricity:     .0003118     
    Arg of perigee:   273.6361  deg
    Mean anomaly:      86.4435  deg
    Mean motion:   15.54191927  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1086
    Checksum:              291
 
 
    Coasting Arc #14 (Orbit 1100)
    ---------------------------------------
 
    Vector Time (GMT): 2017/356/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3495920.56                 A    =         6780429.95  meter
     Y    =        3645300.49  meter          E    =           .0006858
     Z    =       -4530707.71                 I    =           51.63139
     XDOT =      -6565.696017                 Wp   =          115.78992
     YDOT =      -2384.366337  meter/sec      RA   =          179.05190  deg
     ZDOT =       3148.522413                 TA   =          185.81490
                                              MA   =          185.82286
                                              Ha   =            219.810  n.mi
                                              Hp   =            215.635
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11469555.65                 X    =        -3514415.71
     Y    =       11959647.27  feet           Y    =         3606103.71  meter
     Z    =      -14864526.62                 Z    =        -4547734.26
     XDOT =     -21540.997430                 XDOT =       -6553.839261
     YDOT =      -7822.724203  feet/sec       YDOT =       -2457.722430  meter/sec
     ZDOT =      10329.797944                 ZDOT =        3116.657152
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         740199.07                 X    =          225612.68
     Y    =      -16485310.03  feet           Y    =        -5024722.50  meter
     Z    =      -14940705.47                 Z    =        -4553927.03
     XDOT =      20239.334626                 XDOT =        6168.949194
     YDOT =      -8322.753651  feet/sec       YDOT =       -2536.775313  meter/sec
     ZDOT =      10188.489498                 ZDOT =        3105.451599
  
  
    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   17356.37374297  .00016717  00000-0  10270-3 0  9135
    2 25544  51.6404 180.1911 0003113 279.0945  80.9855 15.54168208 11015
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17356.37374297   =   yrday.fracday
    Element set:     913
    Inclination:       51.6404  deg
    RA of node:       180.1911  deg
    Eccentricity:     .0003113     
    Arg of perigee:   279.0945  deg
    Mean anomaly:      80.9855  deg
    Mean motion:   15.54168208  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1101
    Checksum:              304
 
 
    Coasting Arc #15 (Orbit 1116)
    ---------------------------------------
 
    Vector Time (GMT): 2017/357/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4917722.10                 A    =         6784173.88  meter
     Y    =       -3206890.85  meter          E    =           .0009475
     Z    =        3392222.61                 I    =           51.67665
     XDOT =       5247.562847                 Wp   =           85.08577
     YDOT =       3135.153113  meter/sec      RA   =          174.06558  deg
     ZDOT =      -4631.617737                 TA   =           55.29376
                                              MA   =           55.20454
                                              Ha   =            219.796  n.mi
                                              Hp   =            215.622
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16134258.86                 X    =         4936739.32
     Y    =      -10521295.45  feet           Y    =        -3151791.45  meter
     Z    =       11129339.28                 Z    =         3416157.11
     XDOT =      17216.413541                 XDOT =        5234.612629
     YDOT =      10285.935411  feet/sec       YDOT =        3193.762893  meter/sec
     ZDOT =     -15195.596249                 ZDOT =       -4606.158155
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4904439.73                 X    =        -1494873.23
     Y    =       18562569.35  feet           Y    =         5657871.14  meter
     Z    =       11236175.94                 Z    =         3424786.43
     XDOT =     -18398.303081                 XDOT =       -5607.802779
     YDOT =       4292.287753  feet/sec       YDOT =        1308.289307  meter/sec
     ZDOT =     -15082.844685                 ZDOT =       -4597.251060
  
  
    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   17357.40255608  .00016717  00000-0  10270-3 0  9145
    2 25544  51.6401 175.0622 0003072 285.9391  74.1423 15.54190904 11170
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17357.40255608   =   yrday.fracday
    Element set:     914
    Inclination:       51.6401  deg
    RA of node:       175.0622  deg
    Eccentricity:     .0003072     
    Arg of perigee:   285.9391  deg
    Mean anomaly:      74.1423  deg
    Mean motion:   15.54190904  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1117
    Checksum:              289
 
 
    Coasting Arc #16 (Orbit 1131)
    ---------------------------------------
 
    Vector Time (GMT): 2017/358/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5930598.22                 A    =         6787652.48  meter
     Y    =        2681089.76  meter          E    =           .0006443
     Z    =       -1913797.36                 I    =           51.71975
     XDOT =      -3542.049880                 Wp   =           12.67216
     YDOT =      -3832.190861  meter/sec      RA   =          169.09172  deg
     ZDOT =       5617.432299                 TA   =          326.26616
                                              MA   =          326.30714
                                              Ha   =            219.874  n.mi
                                              Hp   =            215.712
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19457343.24                 X    =        -5950841.91
     Y    =        8796226.24  feet           Y    =         2614656.68  meter
     Z    =       -6278862.75                 Z    =        -1942655.13
     XDOT =     -11620.898557                 XDOT =       -3526.220532
     YDOT =     -12572.804663  feet/sec       YDOT =       -3871.712326  meter/sec
     ZDOT =      18429.895993                 ZDOT =        5600.264476
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        8214995.25                 X    =         2503930.55
     Y    =      -19668333.30  feet           Y    =        -5994907.99  meter
     Z    =       -6407529.77                 Z    =        -1953015.07
     XDOT =      15725.991600                 XDOT =        4793.282240
     YDOT =        599.175697  feet/sec       YDOT =         182.628752  meter/sec
     ZDOT =      18354.088539                 ZDOT =        5594.326187
  
  
    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   17358.36706841  .00016717  00000-0  10270-3 0  9152
    2 25544  51.6396 170.2539 0003191 288.1805  71.9000 15.54147866 11326
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17358.36706841   =   yrday.fracday
    Element set:     915
    Inclination:       51.6396  deg
    RA of node:       170.2539  deg
    Eccentricity:     .0003191     
    Arg of perigee:   288.1805  deg
    Mean anomaly:      71.9000  deg
    Mean motion:   15.54147866  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1132
    Checksum:              312
 
 
    Coasting Arc #17 (Orbit 1147)
    ---------------------------------------
 
    Vector Time (GMT): 2017/359/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6475258.88                 A    =         6789277.02  meter
     Y    =       -2012659.13  meter          E    =           .0009746
     Z    =         209258.52                 I    =           51.75778
     XDOT =       1591.244124                 Wp   =          139.66179
     YDOT =       4478.252602  meter/sec      RA   =          164.12721  deg
     ZDOT =      -6017.781683                 TA   =           38.08742
                                              MA   =           38.01857
                                              Ha   =            219.982  n.mi
                                              Hp   =            215.713
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21244287.66                 X    =         6496267.25
     Y    =       -6603212.38  feet           Y    =        -1940130.90  meter
     Z    =         686543.69                 Z    =          240764.03
     XDOT =       5220.617204                 XDOT =        1570.280067
     YDOT =      14692.429796  feet/sec       YDOT =        4495.930071  meter/sec
     ZDOT =     -19743.378224                 ZDOT =       -6010.102654
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10710090.84                 X    =        -3264435.69
     Y    =       19493683.35  feet           Y    =         5941674.68  meter
     Z    =         826908.76                 Z    =          252041.79
     XDOT =     -12625.749562                 XDOT =       -3848.328466
     YDOT =      -6083.422735  feet/sec       YDOT =       -1854.227250  meter/sec
     ZDOT =     -19709.841637                 ZDOT =       -6007.559731
  
  
    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   17359.39587985  .00016717  00000-0  10270-3 0  9163
    2 25544  51.6404 165.1249 0003136 289.5918  70.4896 15.54137128 11480
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17359.39587985   =   yrday.fracday
    Element set:     916
    Inclination:       51.6404  deg
    RA of node:       165.1249  deg
    Eccentricity:     .0003136     
    Arg of perigee:   289.5918  deg
    Mean anomaly:      70.4896  deg
    Mean motion:   15.54137128  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1148
    Checksum:              347
 
 
    Coasting Arc #18 (Orbit 1163)
    ---------------------------------------
 
    Vector Time (GMT): 2017/360/08:43:02.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6501811.04                 A    =         6788251.39  meter
     Y    =        1213434.29  meter          E    =           .0012211
     Z    =        1496797.95                 I    =           51.78471
     XDOT =        399.098346                 Wp   =           49.67953
     YDOT =      -5023.693714  meter/sec      RA   =          159.16460  deg
     ZDOT =       5782.936867                 TA   =          326.63612
                                              MA   =          326.71302
                                              Ha   =            219.977  n.mi
                                              Hp   =            215.664
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21331401.05                 X    =        -6522167.44
     Y    =        3981083.64  feet           Y    =         1140612.71  meter
     Z    =        4910754.42                 Z    =         1465164.91
     XDOT =       1309.377776                 XDOT =         427.154423
     YDOT =     -16481.934757  feet/sec       YDOT =       -5019.074116  meter/sec
     ZDOT =      18972.889982                 ZDOT =        5784.943469
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12312481.61                 X    =         3752844.39
     Y    =      -17906532.89  feet           Y    =        -5457911.22  meter
     Z    =        4769914.39                 Z    =         1453869.91
     XDOT =       9494.881651                 XDOT =        2894.039927
     YDOT =      11606.158906  feet/sec       YDOT =        3537.557234  meter/sec
     ZDOT =      18982.498063                 ZDOT =        5785.865409
  
  
    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   17360.42468656  .00016717  00000-0  10270-3 0  9173
    2 25544  51.6390 159.9949 0003183 294.3338  65.7482 15.54192183 11642
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17360.42468656   =   yrday.fracday
    Element set:     917
    Inclination:       51.6390  deg
    RA of node:       159.9949  deg
    Eccentricity:     .0003183     
    Arg of perigee:   294.3338  deg
    Mean anomaly:      65.7482  deg
    Mean motion:   15.54192183  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1164
    Checksum:              339
 
 
    Coasting Arc #19 (Orbit 1177)
    ---------------------------------------
 
    Vector Time (GMT): 2017/361/06:44:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 940911.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         659662.79                 A    =         6778771.99  meter
     Y    =       -4608876.99  meter          E    =           .0005691
     Z    =        4926375.02                 I    =           51.78255
     XDOT =       7180.843733                 Wp   =           28.52323
     YDOT =      -1421.507204  meter/sec      RA   =          154.57097  deg
     ZDOT =      -2285.469422                 TA   =           83.80129
                                              MA   =           83.73646
                                              Ha   =            219.959  n.mi
                                              Hp   =            215.566
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2164248.01                 X    =          687221.59
     Y    =      -15120987.50  feet           Y    =        -4601346.33  meter
     Z    =       16162647.69                 Z    =         4929646.16
     XDOT =      23559.198600                 XDOT =        7207.307387
     YDOT =      -4663.737547  feet/sec       YDOT =       -1341.058020  meter/sec
     ZDOT =      -7498.259257                 ZDOT =       -2250.522949
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2209547.52                 X    =          673470.08
     Y    =       15098185.58  feet           Y    =         4601926.97  meter
     Z    =       16177827.56                 Z    =         4931001.84
     XDOT =     -20292.188902                 XDOT =       -6185.059177
     YDOT =      10858.327473  feet/sec       YDOT =        3309.618214  meter/sec
     ZDOT =      -7342.638806                 ZDOT =       -2238.036308
  
  
    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   17361.32489396  .00016717  00000-0  10270-3 0  9188
    2 25544  51.6404 155.5089 0003238 299.1988  60.8841 15.54210671 11783
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17361.32489396   =   yrday.fracday
    Element set:     918
    Inclination:       51.6404  deg
    RA of node:       155.5089  deg
    Eccentricity:     .0003238     
    Arg of perigee:   299.1988  deg
    Mean anomaly:      60.8841  deg
    Mean motion:   15.54210671  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1178
    Checksum:              335
 
 
    Coasting Arc #20 (Orbit 1189)
    ---------------------------------------
 
    Vector Time (GMT): 2017/362/01:04:30.000
    Vector Time (MET): N/A
    Weight (LBS)     : 926477.9
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3860231.67                 A    =         6778461.81  meter
     Y    =       -2382045.02  meter          E    =           .0002741
     Z    =        5035698.03                 I    =           51.80138
     XDOT =       5577.216325                 Wp   =          127.88440
     YDOT =      -4885.348594  meter/sec      RA   =          150.80217  deg
     ZDOT =       1962.050152                 TA   =          303.10481
                                              MA   =          303.13112
                                              Ha   =            220.152  n.mi
                                              Hp   =            215.548
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12664802.05                 X    =        -3857769.06
     Y    =       -7815108.34  feet           Y    =        -2425199.28  meter
     Z    =       16521318.99                 Z    =         5016952.06
     XDOT =      18297.953821                 XDOT =        5621.900415
     YDOT =     -16028.046569  feet/sec       YDOT =       -4822.730609  meter/sec
     ZDOT =       6437.172415                 ZDOT =        1989.250818
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2471498.31                 X    =         -753312.69
     Y    =       14768283.33  feet           Y    =         4501372.76  meter
     Z    =       16438266.76                 Z    =         5010383.71
     XDOT =     -20613.361042                 XDOT =       -6282.952446
     YDOT =     -10758.879638  feet/sec       YDOT =       -3279.306514  meter/sec
     ZDOT =       6558.832114                 ZDOT =        1999.132028
  
  
    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   17362.09649978  .00016717  00000-0  10270-3 0  9198
    2 25544  51.6381 151.6609 0003172 300.6089  59.4751 15.54200791 11909
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      17362.09649978   =   yrday.fracday
    Element set:     919
    Inclination:       51.6381  deg
    RA of node:       151.6609  deg
    Eccentricity:     .0003172     
    Arg of perigee:   300.6089  deg
    Mean anomaly:      59.4751  deg
    Mean motion:   15.54200791  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1190
    Checksum:              321
 
             

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