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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  15069.47
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   130.0
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.315
   ET - UTC  (sec) :   67.18
   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 
   ------------------------------------------------------------------------
   087/01:36:05.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              221.0  
   000/00:00:00.000           0.0               0.0              211.3  
   
   092/18:33:27.071          -0.5               1.3              1.3    
   N/A                        1.1              -0.1              220.3  
   000/00:02:54.142           0.5              -0.1              212.4  
   
 
 
    Coasting Arc #1 (Orbit 1532)
    ---------------------------------------
 
    Vector Time (GMT): 2015/086/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 889397.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4470202.36                 A    =         6775278.70  meter
     Y    =        -856358.26  meter          E    =           .0012601
     Z    =        5013865.61                 I    =           51.89840
     XDOT =       3543.951565                 Wp   =          134.93442
     YDOT =      -6494.581746  meter/sec      RA   =          131.09825  deg
     ZDOT =       2038.607860                 TA   =          295.27139
                                              MA   =          295.40192
                                              Ha   =            221.275  n.mi
                                              Hp   =            211.127
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14666018.23                 X    =        -4484649.53
     Y    =       -2809574.33  feet           Y    =         -906427.29  meter
     Z    =       16449690.33                 Z    =         4992115.30
     XDOT =      11627.137681                 XDOT =        3606.409360
     YDOT =     -21307.682893  feet/sec       YDOT =       -6454.601554  meter/sec
     ZDOT =       6688.345997                 ZDOT =        2055.975938
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14922636.96                 X    =        -4548419.74
     Y    =       -1831764.21  feet           Y    =         -558321.73  meter
     Z    =       16356578.39                 Z    =         4985485.09
     XDOT =      10026.138635                 XDOT =        3055.967056
     YDOT =     -20933.910371  feet/sec       YDOT =       -6380.655881  meter/sec
     ZDOT =       6763.845256                 ZDOT =        2061.620034
  
  
    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   15086.55178535  .00016717  00000-0  10270-3 0  9006
    2 25544  51.6435 131.8505 0006760 144.9586 215.2013 15.55324979 15331
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15086.55178535   =   yrday.fracday
    Element set:     900
    Inclination:       51.6435  deg
    RA of node:       131.8505  deg
    Eccentricity:     .0006760     
    Arg of perigee:   144.9586  deg
    Mean anomaly:     215.2013  deg
    Mean motion:   15.55324979  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1533
    Checksum:              311
 
 
    Coasting Arc #2 (Orbit 1541)
    ---------------------------------------
 
    Vector Time (GMT): 2015/087/01:36:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904364.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4493798.83                 A    =         6785740.59  meter
     Y    =        5055381.18  meter          E    =           .0013692
     Z    =         507717.49                 I    =           51.94361
     XDOT =      -3236.128979                 Wp   =           78.27568
     YDOT =      -3493.605157  meter/sec      RA   =          128.26547  deg
     ZDOT =       6009.229627                 TA   =          287.17917
                                              MA   =          287.32901
                                              Ha   =            220.983  n.mi
                                              Hp   =            211.308
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14743434.48                 X    =        -4552461.60
     Y    =       16585896.25  feet           Y    =         5004800.63  meter
     Z    =        1665739.81                 Z    =          485744.61
     XDOT =     -10617.221060                 XDOT =       -3226.012603
     YDOT =     -11461.959177  feet/sec       YDOT =       -3529.736516  meter/sec
     ZDOT =      19715.320300                 ZDOT =        5993.534124
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        5109683.88                 X    =         1557431.65
     Y    =      -21602302.48  feet           Y    =        -6584381.80  meter
     Z    =        1570720.20                 Z    =          478755.52
     XDOT =      13320.055626                 XDOT =        4059.952955
     YDOT =       4613.196892  feet/sec       YDOT =        1406.102413  meter/sec
     ZDOT =      19648.586849                 ZDOT =        5988.889271
  
  
    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   15087.13005705  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6420 128.9608 0006441 147.7739 212.3809 15.55330028 15426
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15087.13005705   =   yrday.fracday
    Element set:     901
    Inclination:       51.6420  deg
    RA of node:       128.9608  deg
    Eccentricity:     .0006441     
    Arg of perigee:   147.7739  deg
    Mean anomaly:     212.3809  deg
    Mean motion:   15.55330028  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1542
    Checksum:              290
 
 
    Coasting Arc #3 (Orbit 1556)
    ---------------------------------------
 
    Vector Time (GMT): 2015/088/01:36:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904364.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4942302.04                 A    =         6783010.66  meter
     Y    =       -3869824.48  meter          E    =           .0011484
     Z    =       -2562478.62                 I    =           51.95339
     XDOT =       1450.219876                 Wp   =          141.48185
     YDOT =       5348.499346  meter/sec      RA   =          123.30774  deg
     ZDOT =      -5301.644839                 TA   =           67.19882
                                              MA   =           67.07755
                                              Ha   =            220.938  n.mi
                                              Hp   =            211.351
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16214901.70                 X    =         4997655.50
     Y    =      -12696274.54  feet           Y    =        -3814247.21  meter
     Z    =       -8407082.10                 Z    =        -2538335.15
     XDOT =       4757.939226                 XDOT =        1416.057163
     YDOT =      17547.570033  feet/sec       YDOT =        5364.525061  meter/sec
     ZDOT =     -17393.847897                 ZDOT =       -5294.683553
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -7962516.58                 X    =        -2426975.05
     Y    =       19038305.67  feet           Y    =         5802875.57  meter
     Z    =       -8302933.23                 Z    =        -2530734.05
     XDOT =     -11450.965992                 XDOT =       -3490.254434
     YDOT =     -12331.220720  feet/sec       YDOT =       -3758.556075  meter/sec
     ZDOT =     -17364.863270                 ZDOT =       -5292.810325
  
  
    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   15088.09382958  .00016717  00000-0  10270-3 0  9025
    2 25544  51.6417 124.1474 0006431 150.6733 209.4782 15.55365683 15575
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15088.09382958   =   yrday.fracday
    Element set:     902
    Inclination:       51.6417  deg
    RA of node:       124.1474  deg
    Eccentricity:     .0006431     
    Arg of perigee:   150.6733  deg
    Mean anomaly:     209.4782  deg
    Mean motion:   15.55365683  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1557
    Checksum:              324
 
 
    Coasting Arc #4 (Orbit 1572)
    ---------------------------------------
 
    Vector Time (GMT): 2015/089/01:36:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904364.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4878315.60                 A    =         6778349.92  meter
     Y    =        2166909.11  meter          E    =           .0015300
     Z    =        4172417.65                 I    =           51.95429
     XDOT =        261.929868                 Wp   =          123.49992
     YDOT =      -6683.024613  meter/sec      RA   =          118.33700  deg
     ZDOT =       3758.890217                 TA   =          287.94439
                                              MA   =          288.11112
                                              Ha   =            220.825  n.mi
                                              Hp   =            211.425
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16004972.45                 X    =        -4922451.85
     Y    =        7109281.86  feet           Y    =         2112110.32  meter
     Z    =       13689034.30                 Z    =         4148612.42
     XDOT =        859.349959                 XDOT =         318.382393
     YDOT =     -21925.933770  feet/sec       YDOT =       -6679.779442  meter/sec
     ZDOT =      12332.316986                 ZDOT =        3760.300542
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       10301579.13                 X    =         3139921.32
     Y    =      -14260870.36  feet           Y    =        -4346713.28  meter
     Z    =       13586601.33                 Z    =         4141196.09
     XDOT =       9353.211987                 XDOT =        2850.859014
     YDOT =      18569.559044  feet/sec       YDOT =        5660.001597  meter/sec
     ZDOT =      12339.452026                 ZDOT =        3761.064978
  
  
    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   15089.12183317  .00016717  00000-0  10270-3 0  9039
    2 25544  51.6413 119.0121 0006455 155.4242 204.7220 15.55400194 15737
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15089.12183317   =   yrday.fracday
    Element set:     903
    Inclination:       51.6413  deg
    RA of node:       119.0121  deg
    Eccentricity:     .0006455     
    Arg of perigee:   155.4242  deg
    Mean anomaly:     204.7220  deg
    Mean motion:   15.55400194  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1573
    Checksum:              270
 
 
    Coasting Arc #5 (Orbit 1587)
    ---------------------------------------
 
    Vector Time (GMT): 2015/090/01:36:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904364.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4408015.32                 A    =         6774408.42  meter
     Y    =         -28866.61  meter          E    =           .0016198
     Z    =       -5156905.80                 I    =           51.95530
     XDOT =      -1793.755187                 Wp   =          101.85775
     YDOT =       7276.758593  meter/sec      RA   =          113.35200  deg
     ZDOT =      -1581.421755                 TA   =          152.98594
                                              MA   =          152.90154
                                              Ha   =            220.750  n.mi
                                              Hp   =            211.484
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14461992.51                 X    =         4433060.69
     Y    =         -94706.74  feet           Y    =           20566.04  meter
     Z    =      -16918982.29                 Z    =        -5135431.79
     XDOT =      -5885.023579                 XDOT =       -1867.310394
     YDOT =      23873.879899  feet/sec       YDOT =        7256.288169  meter/sec
     ZDOT =      -5188.391585                 ZDOT =       -1590.315052
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12398276.97                 X    =        -3778994.82
     Y    =        7651712.34  feet           Y    =         2332241.92  meter
     Z    =      -16826888.75                 Z    =        -5128835.69
     XDOT =      -6845.637485                 XDOT =       -2086.550305
     YDOT =     -22534.600978  feet/sec       YDOT =       -6868.546378  meter/sec
     ZDOT =      -5227.721966                 ZDOT =       -1593.409655
  
  
    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   15090.08556831  .00016717  00000-0  10270-3 0  9042
    2 25544  51.6410 114.1979 0006634 157.0998 203.0452 15.55428970 15883
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15090.08556831   =   yrday.fracday
    Element set:     904
    Inclination:       51.6410  deg
    RA of node:       114.1979  deg
    Eccentricity:     .0006634     
    Arg of perigee:   157.0998  deg
    Mean anomaly:     203.0452  deg
    Mean motion:   15.55428970  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1588
    Checksum:              319
 
 
    Coasting Arc #6 (Orbit 1603)
    ---------------------------------------
 
    Vector Time (GMT): 2015/091/01:36:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904364.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3625143.25                 A    =         6773817.03  meter
     Y    =       -2191973.34  meter          E    =           .0006890
     Z    =        5280758.66                 I    =           51.96455
     XDOT =       3018.103644                 Wp   =          133.00005
     YDOT =      -7006.815197  meter/sec      RA   =          108.35959  deg
     ZDOT =       -840.453791                 TA   =          324.96876
                                              MA   =          325.01406
                                              Ha   =            220.809  n.mi
                                              Hp   =            211.488
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11893514.61                 X    =        -3626014.54
     Y    =       -7191513.58  feet           Y    =        -2232516.18  meter
     Z    =       17325323.69                 Z    =         5263146.66
     XDOT =       9901.914844                 XDOT =        3100.313801
     YDOT =     -22988.238834  feet/sec       YDOT =       -6972.605245  meter/sec
     ZDOT =      -2757.394326                 ZDOT =        -825.591792
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13987893.55                 X    =         4263509.96
     Y    =        -333702.17  feet           Y    =         -101712.42  meter
     Z    =       17250155.80                 Z    =         5257847.49
     XDOT =       3870.335792                 XDOT =        1179.678349
     YDOT =      23712.399734  feet/sec       YDOT =        7227.539439  meter/sec
     ZDOT =      -2692.500444                 ZDOT =        -820.674135
  
  
    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   15091.11353205  .00016717  00000-0  10270-3 0  9058
    2 25544  51.6406 109.0625 0006663 160.7701 199.3705 15.55416046 16042
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15091.11353205   =   yrday.fracday
    Element set:     905
    Inclination:       51.6406  deg
    RA of node:       109.0625  deg
    Eccentricity:     .0006663     
    Arg of perigee:   160.7701  deg
    Mean anomaly:     199.3705  deg
    Mean motion:   15.55416046  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1604
    Checksum:              284
 
 
    Coasting Arc #7 (Orbit 1618)
    ---------------------------------------
 
    Vector Time (GMT): 2015/092/01:36:05.000
    Vector Time (MET): N/A
    Weight (LBS)     : 904364.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2652396.67                 A    =         6776627.25  meter
     Y    =        4266163.48  meter          E    =           .0014867
     Z    =       -4563077.98                 I    =           51.98415
     XDOT =      -3902.277709                 Wp   =          131.88491
     YDOT =       5791.427842  meter/sec      RA   =          103.37146  deg
     ZDOT =       3143.212705                 TA   =          169.52757
                                              MA   =          169.49658
                                              Ha   =            220.511  n.mi
                                              Hp   =            211.563
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8702088.82                 X    =         2626660.02
     Y    =       13996599.34  feet           Y    =         4295679.73  meter
     Z    =      -14970728.29                 Z    =        -4550256.30
     XDOT =     -12802.748388                 XDOT =       -3982.017360
     YDOT =      19000.747513  feet/sec       YDOT =        5747.344638  meter/sec
     ZDOT =      10312.377640                 ZDOT =        3124.061656
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15033135.81                 X    =        -4582099.79
     Y    =       -6874456.48  feet           Y    =        -2095334.33  meter
     Z    =      -14916451.46                 Z    =        -4546534.41
     XDOT =       -168.182279                 XDOT =         -51.261959
     YDOT =     -21850.111969  feet/sec       YDOT =       -6659.914128  meter/sec
     ZDOT =      10229.279947                 ZDOT =        3117.884528
  
  
    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   15092.07722676  .00016717  00000-0  10270-3 0  9067
    2 25544  51.6410 104.2476 0006751 164.0519 196.0848 15.55488175 16190
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15092.07722676   =   yrday.fracday
    Element set:     906
    Inclination:       51.6410  deg
    RA of node:       104.2476  deg
    Eccentricity:     .0006751     
    Arg of perigee:   164.0519  deg
    Mean anomaly:     196.0848  deg
    Mean motion:   15.55488175  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1619
    Checksum:              321
 
 
    Coasting Arc #8 (Orbit 1629)
    ---------------------------------------
 
    Vector Time (GMT): 2015/092/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2651561.84                 A    =         6778110.42  meter
     Y    =        4502971.76  meter          E    =           .0012167
     Z    =       -4329629.82                 I    =           51.99517
     XDOT =      -3787.898641                 Wp   =          135.05571
     YDOT =       5637.339486  meter/sec      RA   =           99.85675  deg
     ZDOT =       3540.925250                 TA   =          170.87893
                                              MA   =          170.85681
                                              Ha   =            220.285  n.mi
                                              Hp   =            212.430
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8699349.87                 X    =         2622043.26
     Y    =       14773529.38  feet           Y    =         4532457.56  meter
     Z    =      -14204822.24                 Z    =        -4316821.38
     XDOT =     -12427.488979                 XDOT =       -3867.855723
     YDOT =      18495.208286  feet/sec       YDOT =        5594.534191  meter/sec
     ZDOT =      11617.208824                 ZDOT =        3522.329273
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11179915.52                 X    =         3407638.25
     Y    =      -13056857.50  feet           Y    =        -3979730.17  meter
     Z    =      -14150646.44                 Z    =        -4313117.03
     XDOT =      20573.201095                 XDOT =        6270.711694
     YDOT =       5104.561918  feet/sec       YDOT =        1555.870473  meter/sec
     ZDOT =      11536.509754                 ZDOT =        3516.328173
  
  
    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   15092.78392496  .00016717  00000-0  10270-3 0  9079
    2 25544  51.6443 100.7214 0005667 173.6583 186.4643 15.55278006 16308
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15092.78392496   =   yrday.fracday
    Element set:     907
    Inclination:       51.6443  deg
    RA of node:       100.7214  deg
    Eccentricity:     .0005667     
    Arg of perigee:   173.6583  deg
    Mean anomaly:     186.4643  deg
    Mean motion:   15.55278006  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1630
    Checksum:              321
 
 
    Coasting Arc #9 (Orbit 1645)
    ---------------------------------------
 
    Vector Time (GMT): 2015/093/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1663288.06                 A    =         6782723.02  meter
     Y    =       -5951972.82  meter          E    =           .0015837
     Z    =        2771917.39                 I    =           52.01489
     XDOT =       4361.526062                 Wp   =          121.29470
     YDOT =      -3632.346159  meter/sec      RA   =           94.88902  deg
     ZDOT =      -5168.724992                 TA   =           27.42411
                                              MA   =           27.34061
                                              Ha   =            220.274  n.mi
                                              Hp   =            212.438
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5456981.83                 X    =        -1610073.10
     Y    =      -19527469.88  feet           Y    =        -5970274.85  meter
     Z    =        9094217.16                 Z    =         2763967.53
     XDOT =      14309.468708                 XDOT =        4426.927558
     YDOT =     -11917.146192  feet/sec       YDOT =       -3583.207801  meter/sec
     ZDOT =     -16957.759159                 ZDOT =       -5147.378022
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16532688.94                 X    =        -5039163.59
     Y    =       11763145.43  feet           Y    =         3585406.73  meter
     Z    =        9061132.50                 Z    =         2761833.19
     XDOT =     -15216.712852                 XDOT =       -4638.054077
     YDOT =      -8360.363272  feet/sec       YDOT =       -2548.238725  meter/sec
     ZDOT =     -16865.590795                 ZDOT =       -5140.632074
  
  
    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   15093.81198882  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6440  95.5873 0005739 176.9964 183.1225 15.55287230 16462
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15093.81198882   =   yrday.fracday
    Element set:     908
    Inclination:       51.6440  deg
    RA of node:        95.5873  deg
    Eccentricity:     .0005739     
    Arg of perigee:   176.9964  deg
    Mean anomaly:     183.1225  deg
    Mean motion:   15.55287230  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1646
    Checksum:              344
 
 
    Coasting Arc #10 (Orbit 1660)
    ---------------------------------------
 
    Vector Time (GMT): 2015/094/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         631191.17                 A    =         6785516.69  meter
     Y    =        6707814.26  meter          E    =           .0006800
     Z    =        -798802.21                 I    =           52.02728
     XDOT =      -4662.660906                 Wp   =           70.42008
     YDOT =       1145.163815  meter/sec      RA   =           89.93414  deg
     ZDOT =       5975.477761                 TA   =          280.99038
                                              MA   =          281.06686
                                              Ha   =            219.980  n.mi
                                              Hp   =            212.547
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        2070837.19                 X    =          560016.21
     Y    =       22007264.64  feet           Y    =         6714474.58  meter
     Z    =       -2620742.15                 Z    =         -795909.78
     XDOT =     -15297.443918                 XDOT =       -4704.146786
     YDOT =       3757.099132  feet/sec       YDOT =        1092.791758  meter/sec
     ZDOT =      19604.585830                 ZDOT =        5952.726312
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19857412.96                 X    =         6052539.47
     Y    =       -9713396.22  feet           Y    =        -2960643.17  meter
     Z    =       -2609489.86                 Z    =         -795372.51
     XDOT =       8246.953139                 XDOT =        2513.671317
     YDOT =      11657.501159  feet/sec       YDOT =        3553.206353  meter/sec
     ZDOT =      19506.813390                 ZDOT =        5945.676721
  
  
    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   15094.77577727  .00016717  00000-0  10270-3 0  9094
    2 25544  51.6447  90.7734 0005657 181.6900 178.4235 15.55346075 16612
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15094.77577727   =   yrday.fracday
    Element set:     909
    Inclination:       51.6447  deg
    RA of node:        90.7734  deg
    Eccentricity:     .0005657     
    Arg of perigee:   181.6900  deg
    Mean anomaly:     178.4235  deg
    Mean motion:   15.55346075  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1661
    Checksum:              340
 
 
    Coasting Arc #11 (Orbit 1676)
    ---------------------------------------
 
    Vector Time (GMT): 2015/095/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         470020.67                 A    =         6785056.90  meter
     Y    =       -6626669.07  meter          E    =           .0013569
     Z    =       -1342046.00                 I    =           52.02516
     XDOT =       4721.459469                 Wp   =          159.47733
     YDOT =       1514.713547  meter/sec      RA   =           84.98438  deg
     ZDOT =      -5855.851340                 TA   =           35.07106
                                              MA   =           34.98180
                                              Ha   =            219.948  n.mi
                                              Hp   =            212.686
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1542062.56                 X    =          550605.96
     Y    =      -21741040.26  feet           Y    =        -6620962.58  meter
     Z    =       -4403038.06                 Z    =        -1339566.14
     XDOT =      15490.352589                 XDOT =        4732.616567
     YDOT =       4969.532636  feet/sec       YDOT =        1567.573646  meter/sec
     ZDOT =     -19212.110697                 ZDOT =       -5832.888210
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -20788829.40                 X    =        -6336435.20
     Y    =        6555840.12  feet           Y    =         1998220.07  meter
     Z    =       -4391248.65                 Z    =        -1338452.59
     XDOT =       -659.521905                 XDOT =        -201.022277
     YDOT =     -14827.786367  feet/sec       YDOT =       -4519.509285  meter/sec
     ZDOT =     -19113.890676                 ZDOT =       -5825.913878
  
  
    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   15095.80379832  .00016717  00000-0  10270-3 0  9108
    2 25544  51.6451  85.6390 0005796 186.1705 173.9378 15.55337324 16777
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15095.80379832   =   yrday.fracday
    Element set:     910
    Inclination:       51.6451  deg
    RA of node:        85.6390  deg
    Eccentricity:     .0005796     
    Arg of perigee:   186.1705  deg
    Mean anomaly:     173.9378  deg
    Mean motion:   15.55337324  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1677
    Checksum:              339
 
 
    Coasting Arc #12 (Orbit 1692)
    ---------------------------------------
 
    Vector Time (GMT): 2015/096/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1563441.58                 A    =         6781225.69  meter
     Y    =        5742732.21  meter          E    =           .0012814
     Z    =        3245015.78                 I    =           52.00936
     XDOT =      -4498.152674                 Wp   =          111.93070
     YDOT =      -3946.471149  meter/sec      RA   =           80.02632  deg
     ZDOT =       4797.123474                 TA   =          285.47058
                                              MA   =          285.61207
                                              Ha   =            219.701  n.mi
                                              Hp   =            212.754
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5129401.52                 X    =        -1643305.27
     Y    =       18840984.93  feet           Y    =         5724802.59  meter
     Z    =       10646377.22                 Z    =         3237226.17
     XDOT =     -14757.718746                 XDOT =       -4476.990943
     YDOT =     -12947.739990  feet/sec       YDOT =       -3996.653591  meter/sec
     ZDOT =      15738.594076                 ZDOT =        4775.323843
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       19391379.54                 X    =         5910492.48
     Y    =       -2449412.35  feet           Y    =         -746580.89  meter
     Z    =       10611955.51                 Z    =         3234524.04
     XDOT =      -6415.145782                 XDOT =       -1955.336434
     YDOT =      17279.601566  feet/sec       YDOT =        5266.822557  meter/sec
     ZDOT =      15645.796509                 ZDOT =        4768.838776
  
  
    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   15096.83179672  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6453  80.5042 0005543 189.2700 170.8352 15.55390070 16939
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15096.83179672   =   yrday.fracday
    Element set:     911
    Inclination:       51.6453  deg
    RA of node:        80.5042  deg
    Eccentricity:     .0005543     
    Arg of perigee:   189.2700  deg
    Mean anomaly:     170.8352  deg
    Mean motion:   15.55390070  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1693
    Checksum:              306
 
 
    Coasting Arc #13 (Orbit 1707)
    ---------------------------------------
 
    Vector Time (GMT): 2015/097/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2668532.46                 A    =         6776343.48  meter
     Y    =       -4136360.40  meter          E    =           .0008630
     Z    =       -4663430.32                 I    =           51.98740
     XDOT =       3952.314916                 Wp   =          102.35789
     YDOT =       5867.551480  meter/sec      RA   =           75.05286  deg
     ZDOT =      -2949.159520                 TA   =          138.44137
                                              MA   =          138.37574
                                              Ha   =            219.503  n.mi
                                              Hp   =            212.918
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        8755027.77                 X    =         2737241.42
     Y    =      -13570736.21  feet           Y    =        -4106135.37  meter
     Z    =      -15299968.25                 Z    =        -4650299.66
     XDOT =      12966.912454                 XDOT =        3900.734934
     YDOT =      19250.496983  feet/sec       YDOT =        5911.460179  meter/sec
     ZDOT =      -9675.720210                 ZDOT =       -2930.085487
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15981013.15                 X    =        -4871012.81
     Y    =       -2676797.30  feet           Y    =         -815887.82  meter
     Z    =      -15242912.97                 Z    =        -4646039.87
     XDOT =      12227.226251                 XDOT =        3726.858561
     YDOT =     -18480.564593  feet/sec       YDOT =       -5632.876088  meter/sec
     ZDOT =      -9594.964741                 ZDOT =       -2924.545253
  
  
    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   15097.79552349  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6456  75.6905 0005583 194.8570 165.2420 15.55445389 17081
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15097.79552349   =   yrday.fracday
    Element set:     912
    Inclination:       51.6456  deg
    RA of node:        75.6905  deg
    Eccentricity:     .0005583     
    Arg of perigee:   194.8570  deg
    Mean anomaly:     165.2420  deg
    Mean motion:   15.55445389  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1708
    Checksum:              341
 
 
    Coasting Arc #14 (Orbit 1723)
    ---------------------------------------
 
    Vector Time (GMT): 2015/098/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3657935.80                 A    =         6773556.00  meter
     Y    =        2085275.05  meter          E    =           .0006657
     Z    =        5305619.08                 I    =           51.96967
     XDOT =      -3066.028195                 Wp   =          171.55404
     YDOT =      -7003.546530  meter/sec      RA   =           70.06556  deg
     ZDOT =        632.240501                 TA   =          272.40199
                                              MA   =          272.47821
                                              Ha   =            219.432  n.mi
                                              Hp   =            212.911
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -12001101.71                 X    =        -3706755.02
     Y    =        6841453.58  feet           Y    =         2044097.06  meter
     Z    =       17406886.75                 Z    =         5287730.57
     XDOT =     -10059.147622                 XDOT =       -2990.556228
     YDOT =     -22977.514861  feet/sec       YDOT =       -7037.410823  meter/sec
     ZDOT =       2074.279860                 ZDOT =         617.529988
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       11262160.00                 X    =         3432706.37
     Y    =        8165406.80  feet           Y    =         2488815.99  meter
     Z    =       17329787.06                 Z    =         5282119.10
     XDOT =     -16106.864109                 XDOT =       -4909.372181
     YDOT =      17898.756591  feet/sec       YDOT =        5455.541009  meter/sec
     ZDOT =       2012.457439                 ZDOT =         613.397027
  
  
    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   15098.82347838  .00016717  00000-0  10270-3 0  9137
    2 25544  51.6460  70.5561 0005626 197.6696 162.4263 15.55474211 17244
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15098.82347838   =   yrday.fracday
    Element set:     913
    Inclination:       51.6460  deg
    RA of node:        70.5561  deg
    Eccentricity:     .0005626     
    Arg of perigee:   197.6696  deg
    Mean anomaly:     162.4263  deg
    Mean motion:   15.55474211  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1724
    Checksum:              325
 
 
    Coasting Arc #15 (Orbit 1738)
    ---------------------------------------
 
    Vector Time (GMT): 2015/099/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4474727.26                 A    =         6774413.56  meter
     Y    =         170265.87  meter          E    =           .0013493
     Z    =       -5094771.90                 I    =           51.96064
     XDOT =       1793.956477                 Wp   =          127.82498
     YDOT =       7224.114939  meter/sec      RA   =           65.07261  deg
     ZDOT =       1812.271001                 TA   =          159.68107
                                              MA   =          159.62732
                                              Ha   =            219.130  n.mi
                                              Hp   =            213.167
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14680863.73                 X    =         4497239.49
     Y    =         558615.06  feet           Y    =          220430.73  meter
     Z    =      -16715130.92                 Z    =        -5072979.65
     XDOT =       5885.683981                 XDOT =        1704.237952
     YDOT =      23701.164498  feet/sec       YDOT =        7243.674605  meter/sec
     ZDOT =       5945.771000                 ZDOT =        1820.767392
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -5880846.00                 X    =        -1792481.86
     Y    =      -13578301.72  feet           Y    =        -4138666.36  meter
     Z    =      -16621696.21                 Z    =        -5066293.00
     XDOT =      17864.672058                 XDOT =        5445.152043
     YDOT =     -15078.047998  feet/sec       YDOT =       -4595.789030  meter/sec
     ZDOT =       5980.887120                 ZDOT =        1822.974394
  
  
    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   15099.78716447  .00016717  00000-0  10270-3 0  9140
    2 25544  51.6454  65.7413 0005630 202.5336 157.5571 15.55519033 17396
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15099.78716447   =   yrday.fracday
    Element set:     914
    Inclination:       51.6454  deg
    RA of node:        65.7413  deg
    Eccentricity:     .0005630     
    Arg of perigee:   202.5336  deg
    Mean anomaly:     157.5571  deg
    Mean motion:   15.55519033  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1739
    Checksum:              320
 
 
    Coasting Arc #16 (Orbit 1754)
    ---------------------------------------
 
    Vector Time (GMT): 2015/100/18:34:54.142
    Vector Time (MET): N/A
    Weight (LBS)     : 904237.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4946070.99                 A    =         6778324.61  meter
     Y    =       -2284991.18  meter          E    =           .0008611
     Z    =        4023364.01                 I    =           51.96050
     XDOT =       -196.772249                 Wp   =          109.19516
     YDOT =      -6566.721920  meter/sec      RA   =           60.08934  deg
     ZDOT =      -3967.205129                 TA   =           21.84484
                                              MA   =           21.80814
                                              Ha   =            218.985  n.mi
                                              Hp   =            213.113
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -16227267.03                 X    =        -4939696.21
     Y    =       -7496690.23  feet           Y    =        -2340265.49  meter
     Z    =       13200013.16                 Z    =         3999352.41
     XDOT =       -645.578246                 XDOT =        -104.055644
     YDOT =     -21544.363256  feet/sec       YDOT =       -6568.404188  meter/sec
     ZDOT =     -13015.764859                 ZDOT =       -3967.935419
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =         588939.74                 X    =          179508.83
     Y    =       17940871.17  feet           Y    =         5468377.53  meter
     Z    =       13097450.09                 Z    =         3992102.79
     XDOT =     -17711.552585                 XDOT =       -5398.481228
     YDOT =      10094.748775  feet/sec       YDOT =        3076.879427  meter/sec
     ZDOT =     -13017.681171                 ZDOT =       -3967.789221
  
  
    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   15100.81507332  .00016717  00000-0  10270-3 0  9159
    2 25544  51.6458  60.6069 0005582 207.6039 152.4819 15.55582926 17551
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15100.81507332   =   yrday.fracday
    Element set:     915
    Inclination:       51.6458  deg
    RA of node:        60.6069  deg
    Eccentricity:     .0005582     
    Arg of perigee:   207.6039  deg
    Mean anomaly:     152.4819  deg
    Mean motion:   15.55582926  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            1755
    Checksum:              314
 
             

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