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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  10763.91
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   122.5
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.819
   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 
   ------------------------------------------------------------------------
   245/10:53:00.000           0.0               0.0              0.0    
   N/A                        0.0               0.0              219.4  
   000/00:00:00.000           0.0               0.0              212.8  
   
   250/04:11:18.328           0.8               0.9              0.9    
   N/A                        0.5               0.0              219.0  
   000/00:04:32.655          -0.1               0.0              213.3  
   
 
 
    Coasting Arc #1 (Orbit 3973)
    ---------------------------------------
 
    Vector Time (GMT): 2015/243/08:06:25.568
    Vector Time (MET): N/A
    Weight (LBS)     : 927021.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4571503.45                 A    =         6776016.39  meter
     Y    =       -1185162.13  meter          E    =           .0007036
     Z    =        4854643.02                 I    =           51.97235
     XDOT =       -795.668390                 Wp   =           66.90594
     YDOT =      -7209.648941  meter/sec      RA   =           68.04043  deg
     ZDOT =      -2503.791926                 TA   =           47.59468
                                              MA   =           47.53517
                                              Ha   =            219.415  n.mi
                                              Hp   =            212.735
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14998370.88                 X    =        -4581492.73
     Y    =       -3888327.20  feet           Y    =        -1236338.98  meter
     Z    =       15927306.48                 Z    =         4832411.63
     XDOT =      -2610.460597                 XDOT =        -702.826845
     YDOT =     -23653.703874  feet/sec       YDOT =       -7218.027811  meter/sec
     ZDOT =      -8214.540438                 ZDOT =       -2507.430754
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -1218172.25                 X    =         -371298.90
     Y    =       15544299.50  feet           Y    =         4737902.49  meter
     Z    =       15831617.70                 Z    =         4825477.07
     XDOT =     -21722.637395                 XDOT =       -6621.059878
     YDOT =       6697.347385  feet/sec       YDOT =        2041.351483  meter/sec
     ZDOT =      -8228.912363                 ZDOT =       -2508.172488
  
  
    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   15243.38161185  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6444  68.5781 0000859 163.5486 196.5696 15.55301747 39749
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15243.38161185   =   yrday.fracday
    Element set:     900
    Inclination:       51.6444  deg
    RA of node:        68.5781  deg
    Eccentricity:     .0000859     
    Arg of perigee:   163.5486  deg
    Mean anomaly:     196.5696  deg
    Mean motion:   15.55301747  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3974
    Checksum:              338
 
 
    Coasting Arc #2 (Orbit 3988)
    ---------------------------------------
 
    Vector Time (GMT): 2015/244/08:06:25.568
    Vector Time (MET): N/A
    Weight (LBS)     : 927021.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4787717.65                 A    =         6780457.07  meter
     Y    =        3137214.64  meter          E    =           .0005695
     Z    =       -3640727.84                 I    =           51.97437
     XDOT =       -717.108725                 Wp   =          105.56772
     YDOT =       6219.092995  meter/sec      RA   =           63.06286  deg
     ZDOT =       4420.211385                 TA   =          211.48699
                                              MA   =          211.52109
                                              Ha   =            219.282  n.mi
                                              Hp   =            212.898
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15707735.07                 X    =         4769965.93
     Y    =       10292698.94  feet           Y    =         3190654.38  meter
     Z    =      -11944645.15                 Z    =        -3617513.63
     XDOT =      -2352.718915                 XDOT =        -808.070457
     YDOT =      20403.848410  feet/sec       YDOT =        6210.565713  meter/sec
     ZDOT =      14502.005857                 ZDOT =        4416.506194
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7109141.28                 X    =         2166866.26
     Y    =      -17449963.84  feet           Y    =        -5318748.98  meter
     Z    =      -11845083.90                 Z    =        -3610381.57
     XDOT =      19225.894299                 XDOT =        5860.052582
     YDOT =      -1990.167548  feet/sec       YDOT =        -606.603069  meter/sec
     ZDOT =      14484.868369                 ZDOT =        4414.987879
  
  
    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   15244.34543518  .00016717  00000-0  10270-3 0  9017
    2 25544  51.6446  63.7645 0000812 170.1330 189.9840 15.55278512 39894
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15244.34543518   =   yrday.fracday
    Element set:     901
    Inclination:       51.6446  deg
    RA of node:        63.7645  deg
    Eccentricity:     .0000812     
    Arg of perigee:   170.1330  deg
    Mean anomaly:     189.9840  deg
    Mean motion:   15.55278512  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            3989
    Checksum:              315
 
 
    Coasting Arc #3 (Orbit 4004)
    ---------------------------------------
 
    Vector Time (GMT): 2015/245/08:06:25.568
    Vector Time (MET): N/A
    Weight (LBS)     : 927021.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4580371.44                 A    =         6784612.05  meter
     Y    =       -4647180.76  meter          E    =           .0014536
     Z    =        1832227.59                 I    =           51.97328
     XDOT =       2372.503608                 Wp   =          116.86569
     YDOT =      -4586.984370  meter/sec      RA   =           58.10011  deg
     ZDOT =      -5675.079710                 TA   =           43.06259
                                              MA   =           42.94894
                                              Ha   =            219.337  n.mi
                                              Hp   =            212.805
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15027465.36                 X    =        -4536965.38
     Y    =      -15246656.04  feet           Y    =        -4698158.61  meter
     Z    =        6011245.38                 Z    =         1810082.97
     XDOT =       7783.804487                 XDOT =        2451.187410
     YDOT =     -15049.161319  feet/sec       YDOT =       -4560.014093  meter/sec
     ZDOT =     -18619.027919                 ZDOT =       -5663.362997
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11803873.49                 X    =        -3597820.64
     Y    =       17890859.11  feet           Y    =         5453133.86  meter
     Z    =        5916590.02                 Z    =         1803376.64
     XDOT =     -15054.343047                 XDOT =       -4588.563761
     YDOT =      -3761.001220  feet/sec       YDOT =       -1146.353172  meter/sec
     ZDOT =     -18567.625781                 ZDOT =       -5659.412338
  
  
    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   15245.37350150  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6449  58.6305 0000901 166.3645 193.7533 15.55278067 40055
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15245.37350150   =   yrday.fracday
    Element set:     902
    Inclination:       51.6449  deg
    RA of node:        58.6305  deg
    Eccentricity:     .0000901     
    Arg of perigee:   166.3645  deg
    Mean anomaly:     193.7533  deg
    Mean motion:   15.55278067  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4005
    Checksum:              299
 
 
    Coasting Arc #4 (Orbit 4006)
    ---------------------------------------
 
    Vector Time (GMT): 2015/245/10:53:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941307.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -3389513.31                 A    =         6774056.65  meter
     Y    =        2446505.93  meter          E    =           .0002863
     Z    =        5328292.96                 I    =           51.93260
     XDOT =      -4259.286801                 Wp   =          117.06376
     YDOT =      -6378.300571  meter/sec      RA   =           57.54016  deg
     ZDOT =        217.780804                 TA   =          330.86216
                                              MA   =          330.87813
                                              Ha   =            219.411  n.mi
                                              Hp   =            212.835
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -11120450.49                 X    =        -3442501.63
     Y    =        8026594.26  feet           Y    =         2408306.41  meter
     Z    =       17481276.10                 Z    =         5311698.44
     XDOT =     -13974.038062                 XDOT =       -4188.704436
     YDOT =     -20926.182976  feet/sec       YDOT =       -6425.536049  meter/sec
     ZDOT =        714.503951                 ZDOT =         197.262115
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       13804732.76                 X    =         4207682.55
     Y    =         183299.16  feet           Y    =           55869.58  meter
     Z    =       17409233.28                 Z    =         5306334.30
     XDOT =      -1117.039130                 XDOT =        -340.473527
     YDOT =      24133.315299  feet/sec       YDOT =        7355.834503  meter/sec
     ZDOT =        627.188419                 ZDOT =         191.167030
  
  
    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   15245.50200832  .00016717  00000-0  10270-3 0  9037
    2 25544  51.6415  57.9859 0000934 173.0729 187.0437 15.55262569 40079
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15245.50200832   =   yrday.fracday
    Element set:     903
    Inclination:       51.6415  deg
    RA of node:        57.9859  deg
    Eccentricity:     .0000934     
    Arg of perigee:   173.0729  deg
    Mean anomaly:     187.0437  deg
    Mean motion:   15.55262569  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4007
    Checksum:              310
 
 
    Coasting Arc #5 (Orbit 4021)
    ---------------------------------------
 
    Vector Time (GMT): 2015/246/10:53:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941307.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4566249.87                 A    =         6775422.37  meter
     Y    =        -474914.61  meter          E    =           .0012852
     Z    =       -4994819.48                 I    =           51.91929
     XDOT =       3030.252902                 Wp   =          109.62224
     YDOT =       6704.254072  meter/sec      RA   =           52.54688  deg
     ZDOT =       2133.054107                 TA   =          181.09367
                                              MA   =          181.09648
                                              Ha   =            219.189  n.mi
                                              Hp   =            212.891
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14981134.74                 X    =         4595484.06
     Y    =       -1558118.79  feet           Y    =         -423688.75  meter
     Z    =      -16387203.03                 Z    =        -4972566.50
     XDOT =       9941.774614                 XDOT =        2944.697522
     YDOT =      21995.584227  feet/sec       YDOT =        6737.662162  meter/sec
     ZDOT =       6998.209013                 ZDOT =        2147.566120
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13208929.28                 X    =        -4026081.64
     Y    =       -7451581.69  feet           Y    =        -2271242.10  meter
     Z    =      -16291122.53                 Z    =        -4965534.15
     XDOT =       4102.956206                 XDOT =        1250.581051
     YDOT =     -22705.208328  feet/sec       YDOT =       -6920.547498  meter/sec
     ZDOT =       7059.537852                 ZDOT =        2151.747137
  
  
    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   15246.46580595  .00016717  00000-0  10270-3 0  9041
    2 25544  51.6411  53.1713 0000979 175.3968 184.7194 15.55320028 40227
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15246.46580595   =   yrday.fracday
    Element set:     904
    Inclination:       51.6411  deg
    RA of node:        53.1713  deg
    Eccentricity:     .0000979     
    Arg of perigee:   175.3968  deg
    Mean anomaly:     184.7194  deg
    Mean motion:   15.55320028  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4022
    Checksum:              312
 
 
    Coasting Arc #6 (Orbit 4037)
    ---------------------------------------
 
    Vector Time (GMT): 2015/247/10:53:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941307.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5387263.12                 A    =         6779621.95  meter
     Y    =       -1412894.27  meter          E    =           .0011188
     Z    =        3856726.93                 I    =           51.91363
     XDOT =      -1337.936636                 Wp   =           86.58155
     YDOT =      -6303.155219  meter/sec      RA   =           47.56379  deg
     ZDOT =      -4166.990420                 TA   =           47.08997
                                              MA   =           46.99612
                                              Ha   =            219.208  n.mi
                                              Hp   =            212.842
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17674747.75                 X    =        -5389797.91
     Y    =       -4635479.89  feet           Y    =        -1473152.10  meter
     Z    =       12653303.57                 Z    =         3830550.62
     XDOT =      -4389.555892                 XDOT =       -1247.112133
     YDOT =     -20679.643107  feet/sec       YDOT =       -6317.609364  meter/sec
     ZDOT =     -13671.228412                 ZDOT =       -4173.268811
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12044901.06                 X    =         3671285.84
     Y    =       13843505.16  feet           Y    =         4219500.37  meter
     Z    =       12540661.72                 Z    =         3822393.69
     XDOT =      -7106.196511                 XDOT =       -2165.968697
     YDOT =      18624.065877  feet/sec       YDOT =        5676.615279  meter/sec
     ZDOT =     -13697.104861                 ZDOT =       -4174.877562
  
  
    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   15247.49384482  .00016717  00000-0  10270-3 0  9053
    2 25544  51.6414  48.0372 0000926 188.6730 171.4408 15.55332314 40389
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15247.49384482   =   yrday.fracday
    Element set:     905
    Inclination:       51.6414  deg
    RA of node:        48.0372  deg
    Eccentricity:     .0000926     
    Arg of perigee:   188.6730  deg
    Mean anomaly:     171.4408  deg
    Mean motion:   15.55332314  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4038
    Checksum:              306
 
 
    Coasting Arc #7 (Orbit 4052)
    ---------------------------------------
 
    Vector Time (GMT): 2015/248/10:53:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941307.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5708811.23                 A    =         6783897.34  meter
     Y    =        2977601.15  meter          E    =           .0005736
     Z    =       -2132395.15                 I    =           51.90600
     XDOT =       -683.513455                 Wp   =           47.10417
     YDOT =       5263.221181  meter/sec      RA   =           42.59352  deg
     ZDOT =       5532.681662                 TA   =          289.35006
                                              MA   =          289.41208
                                              Ha   =            219.126  n.mi
                                              Hp   =            212.790
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18729695.65                 X    =         5685449.03
     Y    =        9769032.63  feet           Y    =         3041310.07  meter
     Z    =       -6996047.07                 Z    =        -2104719.86
     XDOT =      -2242.498211                 XDOT =        -769.192882
     YDOT =      17267.786027  feet/sec       YDOT =        5255.098959  meter/sec
     ZDOT =      18151.842723                 ZDOT =        5529.152870
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -10308992.02                 X    =        -3142180.77
     Y    =      -18482650.23  feet           Y    =        -5633511.79  meter
     Z    =       -6877244.81                 Z    =        -2096184.22
     XDOT =      10118.365036                 XDOT =        3084.077663
     YDOT =     -12375.403914  feet/sec       YDOT =       -3772.023113  meter/sec
     ZDOT =      18135.606754                 ZDOT =        5527.732939
  
  
    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   15248.45762071  .00016717  00000-0  10270-3 0  9065
    2 25544  51.6414  43.2230 0000975 181.3159 178.7991 15.55354528 40533
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15248.45762071   =   yrday.fracday
    Element set:     906
    Inclination:       51.6414  deg
    RA of node:        43.2230  deg
    Eccentricity:     .0000975     
    Arg of perigee:   181.3159  deg
    Mean anomaly:     178.7991  deg
    Mean motion:   15.55354528  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4053
    Checksum:              312
 
 
    Coasting Arc #8 (Orbit 4068)
    ---------------------------------------
 
    Vector Time (GMT): 2015/249/10:53:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 941307.7
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5384776.77                 A    =         6785585.31  meter
     Y    =       -4118607.07  meter          E    =           .0012497
     Z    =          33599.34                 I    =           51.88816
     XDOT =       2847.591099                 Wp   =          136.71357
     YDOT =      -3782.992849  meter/sec      RA   =           37.63373  deg
     ZDOT =      -6035.738735                 TA   =           42.92552
                                              MA   =           42.82806
                                              Ha   =            218.930  n.mi
                                              Hp   =            212.709
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17666590.46                 X    =        -5338484.51
     Y    =      -13512490.39  feet           Y    =        -4178564.35  meter
     Z    =         110234.06                 Z    =            7553.98
     XDOT =       9342.490481                 XDOT =        2919.000991
     YDOT =     -12411.393860  feet/sec       YDOT =       -3750.750294  meter/sec
     ZDOT =     -19802.292439                 ZDOT =       -6021.732100
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        7685668.13                 X    =         2342591.65
     Y    =       20871954.15  feet           Y    =         6361771.63  meter
     Z    =          -1311.23                 Z    =            -399.66
     XDOT =     -13121.562288                 XDOT =       -3999.452185
     YDOT =       4853.311156  feet/sec       YDOT =        1479.289240  meter/sec
     ZDOT =     -19741.142486                 ZDOT =       -6017.100230
  
  
    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   15249.48563352  .00016717  00000-0  10270-3 0  9071
    2 25544  51.6413  38.0883 0000679 192.2260 167.8877 15.55417613 40697
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15249.48563352   =   yrday.fracday
    Element set:     907
    Inclination:       51.6413  deg
    RA of node:        38.0883  deg
    Eccentricity:     .0000679     
    Arg of perigee:   192.2260  deg
    Mean anomaly:     167.8877  deg
    Mean motion:   15.55417613  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4069
    Checksum:              332
 
 
    Coasting Arc #9 (Orbit 4079)
    ---------------------------------------
 
    Vector Time (GMT): 2015/250/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        2194052.55                 A    =         6774135.93  meter
     Y    =       -3574816.28  meter          E    =           .0014073
     Z    =       -5331495.55                 I    =           51.83352
     XDOT =       6416.751019                 Wp   =           91.11845
     YDOT =       4180.324487  meter/sec      RA   =           34.04112  deg
     ZDOT =       -162.920089                 TA   =          177.33515
                                              MA   =          177.32765
                                              Ha   =            218.976  n.mi
                                              Hp   =            213.286
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        7198335.14                 X    =         2259762.15
     Y    =      -11728399.86  feet           Y    =        -3549913.87  meter
     Z    =      -17491783.29                 Z    =        -5320677.53
     XDOT =      21052.332738                 XDOT =        6370.320110
     YDOT =      13714.975351  feet/sec       YDOT =        4251.821199  meter/sec
     ZDOT =       -534.514727                 ZDOT =        -131.862043
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3937479.84                 X    =        -1200143.86
     Y    =      -13248476.43  feet           Y    =        -4038135.62  meter
     Z    =      -17444426.03                 Z    =        -5317061.05
     XDOT =      23259.531081                 XDOT =        7089.505074
     YDOT =      -6387.075311  feet/sec       YDOT =       -1946.780555  meter/sec
     ZDOT =       -401.364038                 ZDOT =        -122.335759
  
  
    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   15250.19238771  .00016717  00000-0  10270-3 0  9086
    2 25544  51.6452  34.5628 0001019 232.9039 127.2021 15.55236454 40809
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15250.19238771   =   yrday.fracday
    Element set:     908
    Inclination:       51.6452  deg
    RA of node:        34.5628  deg
    Eccentricity:     .0001019     
    Arg of perigee:   232.9039  deg
    Mean anomaly:     127.2021  deg
    Mean motion:   15.55236454  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4080
    Checksum:              289
 
 
    Coasting Arc #10 (Orbit 4095)
    ---------------------------------------
 
    Vector Time (GMT): 2015/251/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4021066.52                 A    =         6775600.41  meter
     Y    =        2238745.60  meter          E    =           .0005327
     Z    =        4969928.86                 I    =           51.81159
     XDOT =      -5437.965728                 Wp   =           55.35634
     YDOT =      -4962.730057  meter/sec      RA   =           29.04286  deg
     ZDOT =      -2159.644632                 TA   =           55.65442
                                              MA   =           55.60403
                                              Ha   =            218.966  n.mi
                                              Hp   =            213.227
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13192475.47                 X    =        -4069943.67
     Y    =        7344965.89  feet           Y    =         2193506.46  meter
     Z    =       16305540.86                 Z    =         4950276.62
     XDOT =     -17841.094909                 XDOT =       -5371.576481
     YDOT =     -16281.922758  feet/sec       YDOT =       -5023.169919  meter/sec
     ZDOT =      -7085.448268                 ZDOT =       -2185.899331
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3057330.01                 X    =         -931874.19
     Y    =       14879983.71  feet           Y    =         4535419.03  meter
     Z    =       16220339.51                 Z    =         4943959.48
     XDOT =     -22855.207871                 XDOT =       -6966.267359
     YDOT =       3166.640902  feet/sec       YDOT =         965.192147  meter/sec
     ZDOT =      -7197.722613                 ZDOT =       -2193.865853
  
  
    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   15251.22048906  .00016717  00000-0  10270-3 0  9091
    2 25544  51.6449  29.4291 0001075 246.7041 113.3999 15.55276485 40967
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15251.22048906   =   yrday.fracday
    Element set:     909
    Inclination:       51.6449  deg
    RA of node:        29.4291  deg
    Eccentricity:     .0001075     
    Arg of perigee:   246.7041  deg
    Mean anomaly:     113.3999  deg
    Mean motion:   15.55276485  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4096
    Checksum:              322
 
 
    Coasting Arc #11 (Orbit 4110)
    ---------------------------------------
 
    Vector Time (GMT): 2015/252/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5506063.74                 A    =         6779810.05  meter
     Y    =        -872762.95  meter          E    =           .0005314
     Z    =       -3864212.53                 I    =           51.79774
     XDOT =       3741.542837                 Wp   =          109.92503
     YDOT =       5245.865405  meter/sec      RA   =           24.05218  deg
     ZDOT =       4149.317765                 TA   =          203.61110
                                              MA   =          203.63550
                                              Ha   =            218.869  n.mi
                                              Hp   =            213.358
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       18064513.58                 X    =         5534184.64
     Y    =       -2863395.50  feet           Y    =         -811033.61  meter
     Z    =      -12677862.62                 Z    =        -3837397.08
     XDOT =      12275.403009                 XDOT =        3662.448625
     YDOT =      17210.844505  feet/sec       YDOT =        5287.263911  meter/sec
     ZDOT =      13613.247260                 ZDOT =        4167.300682
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        9344195.27                 X    =         2848110.72
     Y    =      -15815662.19  feet           Y    =        -4820613.84  meter
     Z    =      -12562035.24                 Z    =        -3828908.34
     XDOT =      19879.385266                 XDOT =        6059.236629
     YDOT =        879.157406  feet/sec       YDOT =         267.967177  meter/sec
     ZDOT =      13689.784082                 ZDOT =        4172.646188
  
  
    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   15252.18432339  .00016717  00000-0  10270-3 0  9106
    2 25544  51.6455  24.6157 0001061 252.6582 107.4455 15.55264001 41113
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15252.18432339   =   yrday.fracday
    Element set:     910
    Inclination:       51.6455  deg
    RA of node:        24.6157  deg
    Eccentricity:     .0001061     
    Arg of perigee:   252.6582  deg
    Mean anomaly:     107.4455  deg
    Mean motion:   15.55264001  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4111
    Checksum:              273
 
 
    Coasting Arc #12 (Orbit 4126)
    ---------------------------------------
 
    Vector Time (GMT): 2015/253/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -6417271.44                 A    =         6784186.00  meter
     Y    =        -439313.75  meter          E    =           .0013181
     Z    =        2136142.53                 I    =           51.78286
     XDOT =      -1494.498850                 Wp   =          112.61774
     YDOT =      -5115.423497  meter/sec      RA   =           19.07505  deg
     ZDOT =      -5519.548696                 TA   =           43.73225
                                              MA   =           43.62791
                                              Ha   =            218.938  n.mi
                                              Hp   =            213.269
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -21054040.16                 X    =        -6422258.44
     Y    =       -1441318.07  feet           Y    =         -511103.57  meter
     Z    =        7008341.64                 Z    =         2104956.98
     XDOT =      -4903.211450                 XDOT =       -1410.374286
     YDOT =     -16782.885488  feet/sec       YDOT =       -5131.666153  meter/sec
     ZDOT =     -18108.755563                 ZDOT =       -5526.603752
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14278129.28                 X    =        -4351973.81
     Y    =       15599711.07  feet           Y    =         4754791.93  meter
     Z    =        6873928.72                 Z    =         2095173.47
     XDOT =     -14971.308599                 XDOT =       -4563.254861
     YDOT =      -5677.807540  feet/sec       YDOT =       -1730.595738  meter/sec
     ZDOT =     -18138.183604                 ZDOT =       -5528.518363
  
  
    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   15253.21240063  .00016717  00000-0  10270-3 0  9113
    2 25544  51.6455  19.4818 0000977 251.6787 108.4261 15.55258167 41279
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15253.21240063   =   yrday.fracday
    Element set:     911
    Inclination:       51.6455  deg
    RA of node:        19.4818  deg
    Eccentricity:     .0000977     
    Arg of perigee:   251.6787  deg
    Mean anomaly:     108.4261  deg
    Mean motion:   15.55258167  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4127
    Checksum:              306
 
 
    Coasting Arc #13 (Orbit 4141)
    ---------------------------------------
 
    Vector Time (GMT): 2015/254/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        6593662.93                 A    =         6785871.27  meter
     Y    =        1576425.57  meter          E    =           .0011185
     Z    =         -99116.70                 I    =           51.75917
     XDOT =      -1024.041052                 Wp   =           40.81048
     YDOT =       4637.343110  meter/sec      RA   =           14.10615  deg
     ZDOT =       6023.633465                 TA   =          318.12304
                                              MA   =          318.20855
                                              Ha   =            218.739  n.mi
                                              Hp   =            213.195
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       21632752.40                 X    =         6576026.37
     Y    =        5171999.90  feet           Y    =         1650061.63  meter
     Z    =        -325186.03                 Z    =          -67129.33
     XDOT =      -3359.714739                 XDOT =       -1105.081085
     YDOT =      15214.380283  feet/sec       YDOT =        4625.439185  meter/sec
     ZDOT =      19762.576986                 ZDOT =        6018.461553
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17291795.18                 X    =         5270539.17
     Y    =      -13992496.26  feet           Y    =        -4264912.86  meter
     Z    =        -187545.62                 Z    =          -57163.91
     XDOT =       8913.590345                 XDOT =        2716.862337
     YDOT =      10780.604218  feet/sec       YDOT =        3285.928166  meter/sec
     ZDOT =      19739.367271                 ZDOT =        6016.559144
  
  
    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   15254.17620841  .00016717  00000-0  10270-3 0  9126
    2 25544  51.6459  14.6682 0001125 266.1685  93.9340 15.55317921 41420
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15254.17620841   =   yrday.fracday
    Element set:     912
    Inclination:       51.6459  deg
    RA of node:        14.6682  deg
    Eccentricity:     .0001125     
    Arg of perigee:   266.1685  deg
    Mean anomaly:      93.9340  deg
    Mean motion:   15.55317921  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4142
    Checksum:              300
 
 
    Coasting Arc #14 (Orbit 4157)
    ---------------------------------------
 
    Vector Time (GMT): 2015/255/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5962559.90                 A    =         6784202.29  meter
     Y    =       -2547541.82  meter          E    =           .0005975
     Z    =       -1987574.72                 I    =           51.72232
     XDOT =       3522.859203                 Wp   =          148.58565
     YDOT =      -3897.501911  meter/sec      RA   =            9.13658  deg
     ZDOT =      -5585.261641                 TA   =           53.33587
                                              MA   =           53.28097
                                              Ha   =            218.681  n.mi
                                              Hp   =            213.261
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -19562204.39                 X    =        -5923974.71
     Y    =       -8358076.85  feet           Y    =        -2614003.61  meter
     Z    =       -6520914.44                 Z    =        -2016445.39
     XDOT =      11557.937017                 XDOT =        3593.311073
     YDOT =     -12787.079761  feet/sec       YDOT =       -3857.713779  meter/sec
     ZDOT =     -18324.349217                 ZDOT =       -5567.976800
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18346978.10                 X    =        -5592158.92
     Y    =       10690795.46  feet           Y    =         3258554.46  meter
     Z    =       -6644915.48                 Z    =        -2025370.24
     XDOT =      -2529.738267                 XDOT =        -771.064224
     YDOT =     -15659.104138  feet/sec       YDOT =       -4772.894941  meter/sec
     ZDOT =     -18249.052194                 ZDOT =       -5562.311109
  
  
    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   15255.20425854  .00016717  00000-0  10270-3 0  9139
    2 25544  51.6458   9.5345 0001242 268.0037  92.0975 15.55292716 41585
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15255.20425854   =   yrday.fracday
    Element set:     913
    Inclination:       51.6458  deg
    RA of node:         9.5345  deg
    Eccentricity:     .0001242     
    Arg of perigee:   268.0037  deg
    Mean anomaly:      92.0975  deg
    Mean motion:   15.55292716  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4158
    Checksum:              308
 
 
    Coasting Arc #15 (Orbit 4173)
    ---------------------------------------
 
    Vector Time (GMT): 2015/256/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4590223.55                 A    =         6779837.92  meter
     Y    =        3295727.99  meter          E    =           .0010430
     Z    =        3738046.47                 I    =           51.67620
     XDOT =      -5630.818989                 Wp   =           95.03030
     YDOT =       2979.927382  meter/sec      RA   =            4.15297  deg
     ZDOT =       4276.022799                 TA   =          309.65826
                                              MA   =          309.75023
                                              Ha   =            218.648  n.mi
                                              Hp   =            213.180
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15059788.55                 X    =         4534870.83
     Y    =       10812755.88  feet           Y    =         3346749.92  meter
     Z    =       12263931.99                 Z    =         3760209.87
     XDOT =     -18473.815582                 XDOT =       -5684.493977
     YDOT =       9776.664638  feet/sec       YDOT =        2916.660329  meter/sec
     ZDOT =      14028.946190                 ZDOT =        4248.538739
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       17514070.19                 X    =         5338288.59
     Y    =       -5884977.83  feet           Y    =        -1793741.24  meter
     Z    =       12358856.35                 Z    =         3766979.42
     XDOT =      -3286.143127                 XDOT =       -1001.616425
     YDOT =      19508.179907  feet/sec       YDOT =        5946.093236  meter/sec
     ZDOT =      13909.856735                 ZDOT =        4239.724333
  
  
    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   15256.23229526  .00016717  00000-0  10270-3 0  9142
    2 25544  51.6456   4.3997 0001156 286.7997  73.3030 15.55320281 41746
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15256.23229526   =   yrday.fracday
    Element set:     914
    Inclination:       51.6456  deg
    RA of node:         4.3997  deg
    Eccentricity:     .0001156     
    Arg of perigee:   286.7997  deg
    Mean anomaly:      73.3030  deg
    Mean motion:   15.55320281  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4174
    Checksum:              312
 
 
    Coasting Arc #16 (Orbit 4188)
    ---------------------------------------
 
    Vector Time (GMT): 2015/257/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -2624509.14                 A    =         6775394.93  meter
     Y    =       -3858938.35  meter          E    =           .0011248
     Z    =       -4922378.16                 I    =           51.62908
     XDOT =       7064.092017                 Wp   =           69.48888
     YDOT =      -1904.829061  meter/sec      RA   =          359.15189  deg
     ZDOT =      -2273.478329                 TA   =          178.27276
                                              MA   =          178.26887
                                              Ha   =            218.600  n.mi
                                              Hp   =            213.098
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -8610594.30                 X    =        -2557251.46
     Y    =      -12660558.89  feet           Y    =        -3887911.98  meter
     Z    =      -16149534.65                 Z    =        -4934963.58
     XDOT =      23176.154913                 XDOT =        7095.910949
     YDOT =      -6249.439178  feet/sec       YDOT =       -1825.656144  meter/sec
     ZDOT =      -7458.918403                 ZDOT =       -2239.084846
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15253324.07                 X    =        -4649213.18
     Y    =        -192266.22  feet           Y    =          -58602.74  meter
     Z    =      -16203045.82                 Z    =        -4938688.36
     XDOT =       8035.811281                 XDOT =        2449.315279
     YDOT =     -21550.133554  feet/sec       YDOT =       -6568.480707  meter/sec
     ZDOT =      -7310.258747                 ZDOT =       -2228.166866
  
  
    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   15257.19606543  .00016717  00000-0  10270-3 0  9157
    2 25544  51.6448 359.5862 0001311 288.0711  72.0300 15.55366761 41890
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15257.19606543   =   yrday.fracday
    Element set:     915
    Inclination:       51.6448  deg
    RA of node:       359.5862  deg
    Eccentricity:     .0001311     
    Arg of perigee:   288.0711  deg
    Mean anomaly:      72.0300  deg
    Mean motion:   15.55366761  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4189
    Checksum:              311
 
 
    Coasting Arc #17 (Orbit 4204)
    ---------------------------------------
 
    Vector Time (GMT): 2015/258/04:13:34.655
    Vector Time (MET): N/A
    Weight (LBS)     : 941209.6
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =         334561.60                 A    =         6773720.87  meter
     Y    =        4195060.71  meter          E    =           .0001455
     Z    =        5306737.21                 I    =           51.59187
     XDOT =      -7637.976312                 Wp   =           59.15898
     YDOT =        716.886149  meter/sec      RA   =          354.13810  deg
     ZDOT =        -84.428463                 TA   =           31.65007
                                              MA   =           31.64132
                                              Ha   =            218.617  n.mi
                                              Hp   =            213.130
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        1097643.04                 X    =          261848.35
     Y    =       13763322.54  feet           Y    =         4198396.19  meter
     Z    =       17410555.14                 Z    =         5308185.23
     XDOT =     -25058.977402                 XDOT =       -7645.014912
     YDOT =       2351.988678  feet/sec       YDOT =         631.433899  meter/sec
     ZDOT =       -276.996269                 ZDOT =        -121.549535
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       12007064.83                 X    =         3659753.36
     Y    =        6802593.83  feet           Y    =         2073430.60  meter
     Z    =       17415981.43                 Z    =         5308391.14
     XDOT =     -11423.833836                 XDOT =       -3481.984553
     YDOT =      21289.405768  feet/sec       YDOT =        6489.010878  meter/sec
     ZDOT =       -437.170829                 ZDOT =        -133.249669
  
  
    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   15258.22407569  .00016717  00000-0  10270-3 0  9160
    2 25544  51.6450 354.4522 0001249 292.1542  67.9479 15.55375793 42052
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      15258.22407569   =   yrday.fracday
    Element set:     916
    Inclination:       51.6450  deg
    RA of node:       354.4522  deg
    Eccentricity:     .0001249     
    Arg of perigee:   292.1542  deg
    Mean anomaly:      67.9479  deg
    Mean motion:   15.55375793  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            4205
    Checksum:              326
 
             

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