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   ISS  TRAJECTORY DATA
 
   Lift off time (UTC)  :  N/A
   Area (sq ft)  :  18298.65
   Drag Coefficient (Cd)  :   2.00
   Monthly MSFC 50% solar flux (F10.7-jansky)  :   127.9
   Monthly MSFC 50% earth geomagnetic index (Kp)  :   2.423
   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 
   ------------------------------------------------------------------------
   239/08:38:29.116          -0.0               1.4              1.4    
   N/A                        1.4              -0.2              228.6  
   000/00:02:58.233          -0.2              -0.0              220.2  
   
 
 
    Coasting Arc #1 (Orbit 2207)
    ---------------------------------------
 
    Vector Time (GMT): 2014/237/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        1164271.35                 A    =         6793313.72  meter
     Y    =        5232824.73  meter          E    =           .0010742
     Z    =       -4181648.53                 I    =           51.96669
     XDOT =      -5200.787555                 Wp   =           87.87654
     YDOT =       4162.264367  meter/sec      RA   =          115.05803  deg
     ZDOT =       3769.282130                 TA   =          220.78325
                                              MA   =          220.86370
                                              Ha   =            228.599  n.mi
                                              Hp   =            219.480
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =        3819787.89                 X    =         1125982.95
     Y    =       17168060.13  feet           Y    =         5245629.95  meter
     Z    =      -13719319.33                 Z    =        -4176086.16
     XDOT =     -17062.951295                 XDOT =       -5265.254089
     YDOT =      13655.722989  feet/sec       YDOT =        4103.745640  meter/sec
     ZDOT =      12366.411188                 ZDOT =        3743.860939
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4359232.38                 X    =         1328694.03
     Y    =      -17057447.28  feet           Y    =        -5199109.93  meter
     Z    =      -13696473.14                 Z    =        -4174685.01
     XDOT =      20240.195574                 XDOT =        6169.211611
     YDOT =      -4646.690302  feet/sec       YDOT =       -1416.311204  meter/sec
     ZDOT =      12257.587372                 ZDOT =        3736.112631
  
  
    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   14237.50923859  .00016717  00000-0  10270-3 0  9005
    2 25544  51.6467 115.9893 0004582  48.8732 311.2813 15.50239461 22085
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14237.50923859   =   yrday.fracday
    Element set:     900
    Inclination:       51.6467  deg
    RA of node:       115.9893  deg
    Eccentricity:     .0004582     
    Arg of perigee:    48.8732  deg
    Mean anomaly:     311.2813  deg
    Mean motion:   15.50239461  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2208
    Checksum:              314
 
 
    Coasting Arc #2 (Orbit 2223)
    ---------------------------------------
 
    Vector Time (GMT): 2014/238/12:00:00.000
    Vector Time (MET): N/A
    Weight (LBS)     : 928977.3
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -1244868.41                 A    =         6794152.17  meter
     Y    =       -5427483.61  meter          E    =           .0015440
     Z    =        3883673.77                 I    =           51.98223
     XDOT =       4961.002475                 Wp   =           72.92613
     YDOT =      -4117.621414  meter/sec      RA   =          110.12385  deg
     ZDOT =      -4146.239396                 TA   =           60.51133
                                              MA   =           60.35741
                                              Ha   =            228.574  n.mi
                                              Hp   =            219.317
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4084213.95                 X    =        -1202949.91
     Y    =      -17806704.77  feet           Y    =        -5441169.81  meter
     Z    =       12741711.84                 Z    =         3877728.76
     XDOT =      16276.254838                 XDOT =        5026.818786
     YDOT =     -13509.256606  feet/sec       YDOT =       -4061.776653  meter/sec
     ZDOT =     -13603.147624                 ZDOT =       -4121.979634
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4115071.90                 X    =        -1254273.92
     Y    =       17817068.44  feet           Y    =         5430642.46  meter
     Z    =       12717272.28                 Z    =         3876224.59
     XDOT =     -19343.557692                 XDOT =       -5895.916385
     YDOT =       5209.944957  feet/sec       YDOT =        1587.991223  meter/sec
     ZDOT =     -13499.264856                 ZDOT =       -4114.575928
  
  
    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   14238.54064915  .00016717  00000-0  10270-3 0  9010
    2 25544  51.6465 110.8775 0004643  51.4187 308.7379 15.50294879 22248
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14238.54064915   =   yrday.fracday
    Element set:     901
    Inclination:       51.6465  deg
    RA of node:       110.8775  deg
    Eccentricity:     .0004643     
    Arg of perigee:    51.4187  deg
    Mean anomaly:     308.7379  deg
    Mean motion:   15.50294879  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2224
    Checksum:              322
 
 
    Coasting Arc #3 (Orbit 2236)
    ---------------------------------------
 
    Vector Time (GMT): 2014/239/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4246381.42                 A    =         6789541.39  meter
     Y    =         244725.04  meter          E    =           .0017672
     Z    =       -5307420.04                 I    =           51.97158
     XDOT =      -1458.805419                 Wp   =           77.26826
     YDOT =       7463.147753  meter/sec      RA   =          105.90701  deg
     ZDOT =       -821.563256                 TA   =          184.88572
                                              MA   =          184.90299
                                              Ha   =            228.616  n.mi
                                              Hp   =            220.162
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13931697.57                 X    =         4269110.72
     Y    =         802903.66  feet           Y    =          292337.38  meter
     Z    =      -17412795.40                 Z    =        -5286736.75
     XDOT =      -4786.107019                 XDOT =       -1538.160785
     YDOT =      24485.392889  feet/sec       YDOT =        7446.390665  meter/sec
     ZDOT =      -2695.417507                 ZDOT =        -828.843333
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2781241.76                 X    =         -847722.49
     Y    =      -13786138.84  feet           Y    =        -4202015.12  meter
     Z    =      -17324819.35                 Z    =        -5280604.94
     XDOT =      23889.349812                 XDOT =        7281.473823
     YDOT =      -1385.647014  feet/sec       YDOT =        -422.345210  meter/sec
     ZDOT =      -2727.584271                 ZDOT =        -831.367686
  
  
    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   14239.37866192  .00016717  00000-0  10270-3 0  9020
    2 25544  51.6453 106.7229 0003662  50.8918 309.2558 15.50032525 22375
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14239.37866192   =   yrday.fracday
    Element set:     902
    Inclination:       51.6453  deg
    RA of node:       106.7229  deg
    Eccentricity:     .0003662     
    Arg of perigee:    50.8918  deg
    Mean anomaly:     309.2558  deg
    Mean motion:   15.50032525  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2237
    Checksum:              309
 
 
    Coasting Arc #4 (Orbit 2252)
    ---------------------------------------
 
    Vector Time (GMT): 2014/240/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4184079.84                 A    =         6789216.83  meter
     Y    =        -323822.02  meter          E    =           .0005469
     Z    =        5332196.82                 I    =           51.97831
     XDOT =       1128.308368                 Wp   =           76.78479
     YDOT =      -7570.954167  meter/sec      RA   =          100.97301  deg
     ZDOT =        426.432595                 TA   =            9.17130
                                              MA   =            9.16132
                                              Ha   =            228.654  n.mi
                                              Hp   =            219.980
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13727296.08                 X    =        -4206049.74
     Y    =       -1062408.22  feet           Y    =         -370733.41  meter
     Z    =       17494084.06                 Z    =         5311817.96
     XDOT =       3701.799107                 XDOT =        1210.813204
     YDOT =     -24839.088476  feet/sec       YDOT =       -7557.875339  meter/sec
     ZDOT =       1399.057069                 ZDOT =         432.114889
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2713073.89                 X    =          826944.92
     Y    =       13609977.47  feet           Y    =         4148321.13  meter
     Z    =       17407414.78                 Z    =         5305780.02
     XDOT =     -23921.421022                 XDOT =       -7291.249127
     YDOT =       2950.285553  feet/sec       YDOT =         899.247037  meter/sec
     ZDOT =       1424.453003                 ZDOT =         434.173275
  
  
    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   14240.41021298  .00016717  00000-0  10270-3 0  9038
    2 25544  51.6449 101.6121 0003506  52.9040 307.2431 15.50080358 22534
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14240.41021298   =   yrday.fracday
    Element set:     903
    Inclination:       51.6449  deg
    RA of node:       101.6121  deg
    Eccentricity:     .0003506     
    Arg of perigee:    52.9040  deg
    Mean anomaly:     307.2431  deg
    Mean motion:   15.50080358  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2253
    Checksum:              256
 
 
    Coasting Arc #5 (Orbit 2267)
    ---------------------------------------
 
    Vector Time (GMT): 2014/241/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4168305.99                 A    =         6789174.14  meter
     Y    =         414552.94  meter          E    =           .0017982
     Z    =       -5358278.98                 I    =           51.98380
     XDOT =       -787.475786                 Wp   =           83.42341
     YDOT =       7607.964909  meter/sec      RA   =           96.03860  deg
     ZDOT =        -22.052242                 TA   =          186.35548
                                              MA   =          186.37832
                                              Ha   =            228.578  n.mi
                                              Hp   =            220.030
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13675544.57                 X    =         4189389.27
     Y    =        1360081.81  feet           Y    =          461282.98  meter
     Z    =      -17579655.45                 Z    =        -5337978.85
     XDOT =      -2583.581976                 XDOT =        -872.384153
     YDOT =      24960.514792  feet/sec       YDOT =        7598.684093  meter/sec
     ZDOT =        -72.349875                 ZDOT =         -26.084668
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2646919.33                 X    =         -806781.01
     Y    =      -13597487.75  feet           Y    =        -4144514.27  meter
     Z    =      -17493335.09                 Z    =        -5331968.54
     XDOT =      23663.058965                 XDOT =        7212.500372
     YDOT =      -4481.352470  feet/sec       YDOT =       -1365.916233  meter/sec
     ZDOT =        -90.743725                 ZDOT =         -27.658687
  
  
    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   14241.37728034  .00016717  00000-0  10270-3 0  9047
    2 25544  51.6455  96.8202 0003633  56.3021 303.8475 15.50079657 22680
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14241.37728034   =   yrday.fracday
    Element set:     904
    Inclination:       51.6455  deg
    RA of node:        96.8202  deg
    Eccentricity:     .0003633     
    Arg of perigee:    56.3021  deg
    Mean anomaly:     303.8475  deg
    Mean motion:   15.50079657  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2268
    Checksum:              301
 
 
    Coasting Arc #6 (Orbit 2283)
    ---------------------------------------
 
    Vector Time (GMT): 2014/242/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4160409.96                 A    =         6789065.80  meter
     Y    =        -526762.13  meter          E    =           .0006074
     Z    =        5334436.29                 I    =           51.98618
     XDOT =        456.647919                 Wp   =           64.24737
     YDOT =      -7642.591635  meter/sec      RA   =           91.10448  deg
     ZDOT =       -395.622433                 TA   =           29.52530
                                              MA   =           29.49101
                                              Ha   =            228.612  n.mi
                                              Hp   =            219.852
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13649638.97                 X    =        -4180123.33
     Y    =       -1728222.22  feet           Y    =         -573396.26  meter
     Z    =       17501431.40                 Z    =         5314177.79
     XDOT =       1498.188710                 XDOT =         543.997005
     YDOT =     -25074.119537  feet/sec       YDOT =       -7636.996742  meter/sec
     ZDOT =      -1297.973860                 ZDOT =        -393.191242
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2521572.24                 X    =          768575.22
     Y    =       13636285.52  feet           Y    =         4156339.83  meter
     Z    =       17415306.14                 Z    =         5308185.31
     XDOT =     -23358.455391                 XDOT =       -7119.657203
     YDOT =       5974.511510  feet/sec       YDOT =        1821.031108  meter/sec
     ZDOT =      -1286.374013                 ZDOT =        -392.086799
  
  
    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   14242.40880122  .00016717  00000-0  10270-3 0  9050
    2 25544  51.6454  91.7090 0003494  58.0802 302.0688 15.50128301 22845
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14242.40880122   =   yrday.fracday
    Element set:     905
    Inclination:       51.6454  deg
    RA of node:        91.7090  deg
    Eccentricity:     .0003494     
    Arg of perigee:    58.0802  deg
    Mean anomaly:     302.0688  deg
    Mean motion:   15.50128301  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2284
    Checksum:              279
 
 
    Coasting Arc #7 (Orbit 2298)
    ---------------------------------------
 
    Vector Time (GMT): 2014/243/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4202109.88                 A    =         6789252.31  meter
     Y    =         635423.94  meter          E    =           .0017534
     Z    =       -5309666.57                 I    =           51.98715
     XDOT =       -127.044527                 Wp   =           89.47822
     YDOT =       7604.712205  meter/sec      RA   =           86.17020  deg
     ZDOT =        812.004661                 TA   =          188.25095
                                              MA   =          188.27982
                                              Ha   =            228.516  n.mi
                                              Hp   =            219.929
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       13786449.74                 X    =         4220484.79
     Y    =        2084724.22  feet           Y    =          682516.97  meter
     Z    =      -17420165.91                 Z    =        -5289208.72
     XDOT =       -416.812752                 XDOT =        -216.017189
     YDOT =      24949.843191  feet/sec       YDOT =        7602.794100  meter/sec
     ZDOT =       2664.057286                 ZDOT =         811.170790
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2461412.64                 X    =         -750238.57
     Y    =      -13833861.95  feet           Y    =        -4216561.12  meter
     Z    =      -17333209.84                 Z    =        -5283162.36
     XDOT =      22774.416813                 XDOT =        6941.642245
     YDOT =      -7373.888727  feet/sec       YDOT =       -2247.561284  meter/sec
     ZDOT =       2659.245869                 ZDOT =         810.538141
  
  
    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   14243.37583998  .00016717  00000-0  10270-3 0  9069
    2 25544  51.6461  86.9170 0003566  60.9910 299.1598 15.50126697 22998
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14243.37583998   =   yrday.fracday
    Element set:     906
    Inclination:       51.6461  deg
    RA of node:        86.9170  deg
    Eccentricity:     .0003566     
    Arg of perigee:    60.9910  deg
    Mean anomaly:     299.1598  deg
    Mean motion:   15.50126697  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2299
    Checksum:              351
 
 
    Coasting Arc #8 (Orbit 2314)
    ---------------------------------------
 
    Vector Time (GMT): 2014/244/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4254716.34                 A    =         6789385.41  meter
     Y    =        -761995.65  meter          E    =           .0007570
     Z    =        5230831.93                 I    =           51.98530
     XDOT =       -181.718717                 Wp   =           58.74296
     YDOT =      -7562.597664  meter/sec      RA   =           81.23587  deg
     ZDOT =      -1244.333332                 TA   =           43.17560
                                              MA   =           43.11627
                                              Ha   =            228.549  n.mi
                                              Hp   =            219.745
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -13959043.12                 X    =        -4271289.03
     Y    =       -2499985.73  feet           Y    =         -809666.97  meter
     Z    =       17161522.08                 Z    =         5210122.90
     XDOT =       -596.190015                 XDOT =         -91.093926
     YDOT =     -24811.672127  feet/sec       YDOT =       -7564.123128  meter/sec
     ZDOT =      -4082.458437                 ZDOT =       -1244.995488
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2365143.91                 X    =          720895.86
     Y    =       14089845.45  feet           Y    =         4294584.89  meter
     Z    =       17073517.60                 Z    =         5204008.16
     XDOT =     -22155.431874                 XDOT =       -6752.975635
     YDOT =       8688.455081  feet/sec       YDOT =        2648.241109  meter/sec
     ZDOT =      -4084.005316                 ZDOT =       -1244.804820
  
  
    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   14244.40733046  .00016717  00000-0  10270-3 0  9076
    2 25544  51.6463  81.8058 0003458  62.6396 297.5106 15.50177727 23152
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14244.40733046   =   yrday.fracday
    Element set:     907
    Inclination:       51.6463  deg
    RA of node:        81.8058  deg
    Eccentricity:     .0003458     
    Arg of perigee:    62.6396  deg
    Mean anomaly:     297.5106  deg
    Mean motion:   15.50177727  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2315
    Checksum:              312
 
 
    Coasting Arc #9 (Orbit 2329)
    ---------------------------------------
 
    Vector Time (GMT): 2014/245/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4355873.20                 A    =         6789814.81  meter
     Y    =         868906.18  meter          E    =           .0016306
     Z    =       -5149821.66                 I    =           51.98127
     XDOT =        477.223808                 Wp   =           95.03729
     YDOT =       7451.265881  meter/sec      RA   =           76.30121  deg
     ZDOT =       1664.009219                 TA   =          190.97335
                                              MA   =          191.00897
                                              Ha   =            228.441  n.mi
                                              Hp   =            219.846
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       14290922.56                 X    =         4370849.30
     Y    =        2850742.05  feet           Y    =          917699.84  meter
     Z    =      -16895740.36                 Z    =        -5128625.13
     XDOT =       1565.694909                 XDOT =         385.783354
     YDOT =      24446.410371  feet/sec       YDOT =        7456.091319  meter/sec
     ZDOT =       5459.347833                 ZDOT =        1666.105016
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2394885.12                 X    =         -729960.99
     Y    =      -14479535.35  feet           Y    =        -4413362.37  meter
     Z    =      -16805678.25                 Z    =        -5122370.73
     XDOT =      21291.499645                 XDOT =        6489.649092
     YDOT =      -9854.823077  feet/sec       YDOT =       -3003.750074  meter/sec
     ZDOT =       5467.000543                 ZDOT =        1666.341765
  
  
    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   14245.37434033  .00016717  00000-0  10270-3 0  9088
    2 25544  51.6466  77.0138 0003477  65.3190 294.8323 15.50173635 23306
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14245.37434033   =   yrday.fracday
    Element set:     908
    Inclination:       51.6466  deg
    RA of node:        77.0138  deg
    Eccentricity:     .0003477     
    Arg of perigee:    65.3190  deg
    Mean anomaly:     294.8323  deg
    Mean motion:   15.50173635  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2330
    Checksum:              298
 
 
    Coasting Arc #10 (Orbit 2345)
    ---------------------------------------
 
    Vector Time (GMT): 2014/246/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4468474.01                 A    =         6790198.53  meter
     Y    =        -989601.52  meter          E    =           .0009531
     Z    =        5010366.93                 I    =           51.97502
     XDOT =       -739.701522                 Wp   =           60.33584
     YDOT =      -7335.729144  meter/sec      RA   =           71.36633  deg
     ZDOT =      -2101.001821                 TA   =           50.06464
                                              MA   =           49.98094
                                              Ha   =            228.470  n.mi
                                              Hp   =            219.657
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -14660347.82                 X    =        -4481414.61
     Y    =       -3246724.16  feet           Y    =        -1039643.02  meter
     Z    =       16438211.72                 Z    =         4988628.42
     XDOT =      -2426.842265                 XDOT =        -647.410782
     YDOT =     -24067.352835  feet/sec       YDOT =       -7343.485030  meter/sec
     ZDOT =      -6893.050594                 ZDOT =       -2104.370680
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2410081.73                 X    =          734592.91
     Y    =       14922671.21  feet           Y    =         4548430.18  meter
     Z    =       16345862.18                 Z    =         4982218.79
     XDOT =     -20417.676061                 XDOT =       -6223.307663
     YDOT =      10889.731489  feet/sec       YDOT =        3319.190158  meter/sec
     ZDOT =      -6906.128946                 ZDOT =       -2104.988103
  
  
    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   14246.40579983  .00016717  00000-0  10270-3 0  9098
    2 25544  51.6468  71.9025 0003402  66.8535 293.2974 15.50227060 23467
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14246.40579983   =   yrday.fracday
    Element set:     909
    Inclination:       51.6468  deg
    RA of node:        71.9025  deg
    Eccentricity:     .0003402     
    Arg of perigee:    66.8535  deg
    Mean anomaly:     293.2974  deg
    Mean motion:   15.50227060  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2346
    Checksum:              319
 
 
    Coasting Arc #11 (Orbit 2360)
    ---------------------------------------
 
    Vector Time (GMT): 2014/247/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4624206.85                 A    =         6790857.61  meter
     Y    =        1075018.44  meter          E    =           .0014373
     Z    =       -4868753.75                 I    =           51.96575
     XDOT =        978.019631                 Wp   =           99.38293
     YDOT =       7159.512014  meter/sec      RA   =           66.43048  deg
     ZDOT =       2513.757990                 TA   =          195.25001
                                              MA   =          195.29338
                                              Ha   =            228.363  n.mi
                                              Hp   =            219.768
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       15171282.33                 X    =         4635492.73
     Y    =        3526963.37  feet           Y    =         1126792.19  meter
     Z    =      -15973601.55                 Z    =        -4846262.81
     XDOT =       3208.725825                 XDOT =         885.676694
     YDOT =      23489.212645  feet/sec       YDOT =        7169.932657  meter/sec
     ZDOT =       8247.237500                 ZDOT =        2518.284416
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -2602453.69                 X    =         -793227.88
     Y    =      -15455664.93  feet           Y    =        -4710886.67  meter
     Z    =      -15878062.89                 Z    =        -4839633.57
     XDOT =      19354.823487                 XDOT =        5899.350199
     YDOT =     -11736.434430  feet/sec       YDOT =       -3577.265214  meter/sec
     ZDOT =       8265.263514                 ZDOT =        2519.252319
  
  
    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   14247.37278022  .00016717  00000-0  10270-3 0  9107
    2 25544  51.6462  67.1100 0003388  69.8781 290.2734 15.50220451 23616
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14247.37278022   =   yrday.fracday
    Element set:     910
    Inclination:       51.6462  deg
    RA of node:        67.1100  deg
    Eccentricity:     .0003388     
    Arg of perigee:    69.8781  deg
    Mean anomaly:     290.2734  deg
    Mean motion:   15.50220451  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2361
    Checksum:              287
 
 
    Coasting Arc #12 (Orbit 2376)
    ---------------------------------------
 
    Vector Time (GMT): 2014/248/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -4789028.96                 A    =         6791476.35  meter
     Y    =       -1170232.92  meter          E    =           .0011614
     Z    =        4664214.11                 I    =           51.95513
     XDOT =      -1170.571434                 Wp   =           66.55027
     YDOT =      -6981.495944  meter/sec      RA   =           61.49440  deg
     ZDOT =      -2943.229912                 TA   =           52.67829
                                              MA   =           52.57251
                                              Ha   =            228.378  n.mi
                                              Hp   =            219.586
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -15712037.26                 X    =        -4798244.22
     Y    =       -3839346.84  feet           Y    =        -1223838.19  meter
     Z    =       15302539.72                 Z    =         4640927.62
     XDOT =      -3840.457462                 XDOT =       -1078.118630
     YDOT =     -22905.170420  feet/sec       YDOT =       -6994.069266  meter/sec
     ZDOT =      -9656.266114                 ZDOT =       -2948.691361
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        2795799.97                 X    =          852159.83
     Y    =       16025278.25  feet           Y    =         4884504.81  meter
     Z    =       15203630.50                 Z    =         4634066.58
     XDOT =     -18321.004894                 XDOT =       -5584.242292
     YDOT =      12410.643235  feet/sec       YDOT =        3782.764058  meter/sec
     ZDOT =      -9678.296071                 ZDOT =       -2949.944643
  
  
    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   14248.40420781  .00016717  00000-0  10270-3 0  9114
    2 25544  51.6463  61.9983 0003324  71.1524 288.9987 15.50275131 23775
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14248.40420781   =   yrday.fracday
    Element set:     911
    Inclination:       51.6463  deg
    RA of node:        61.9983  deg
    Eccentricity:     .0003324     
    Arg of perigee:    71.1524  deg
    Mean anomaly:     288.9987  deg
    Mean motion:   15.50275131  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2377
    Checksum:              313
 
 
    Coasting Arc #13 (Orbit 2391)
    ---------------------------------------
 
    Vector Time (GMT): 2014/249/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        4987418.70                 A    =         6792321.92  meter
     Y    =        1216617.63  meter          E    =           .0011932
     Z    =       -4459015.37                 I    =           51.94097
     XDOT =       1330.840374                 Wp   =          101.01038
     YDOT =       6756.197041  meter/sec      RA   =           56.55671  deg
     ZDOT =       3337.295323                 TA   =          202.59826
                                              MA   =          202.65085
                                              Ha   =            228.289  n.mi
                                              Hp   =            219.686
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       16362922.24                 X    =         4995103.70
     Y    =        3991527.65  feet           Y    =         1272432.79  meter
     Z    =      -14629315.51                 Z    =        -4434768.94
     XDOT =       4366.274192                 XDOT =        1238.980815
     YDOT =      22166.000791  feet/sec       YDOT =        6770.566002  meter/sec
     ZDOT =      10949.131637                 ZDOT =        3343.536629
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -3200991.20                 X    =         -975662.12
     Y    =      -16626298.96  feet           Y    =        -5067695.92  meter
     Z    =      -14526328.78                 Z    =        -4427625.01
     XDOT =      17170.037572                 XDOT =        5233.427452
     YDOT =     -12878.601016  feet/sec       YDOT =       -3925.397590  meter/sec
     ZDOT =      10974.515653                 ZDOT =        3345.032371
  
  
    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   14249.37115785  .00016717  00000-0  10270-3 0  9127
    2 25544  51.6451  57.2050 0003312  75.0745 285.0772 15.50267218 23924
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14249.37115785   =   yrday.fracday
    Element set:     912
    Inclination:       51.6451  deg
    RA of node:        57.2050  deg
    Eccentricity:     .0003312     
    Arg of perigee:    75.0745  deg
    Mean anomaly:     285.0772  deg
    Mean motion:   15.50267218  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2392
    Checksum:              295
 
 
    Coasting Arc #14 (Orbit 2407)
    ---------------------------------------
 
    Vector Time (GMT): 2014/250/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5189459.88                 A    =         6793125.53  meter
     Y    =       -1269758.70  meter          E    =           .0013580
     Z    =        4186655.12                 I    =           51.92648
     XDOT =      -1433.222816                 Wp   =           75.52228
     YDOT =      -6534.198374  meter/sec      RA   =           51.61896  deg
     ZDOT =      -3744.802950                 TA   =           52.89243
                                              MA   =           52.76841
                                              Ha   =            228.272  n.mi
                                              Hp   =            219.529
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -17025786.99                 X    =        -5195212.61
     Y    =       -4165875.01  feet           Y    =        -1327822.34  meter
     Z    =       13735745.14                 Z    =         4161431.95
     XDOT =      -4702.174592                 XDOT =       -1341.858574
     YDOT =     -21437.658706  feet/sec       YDOT =       -6549.715133  meter/sec
     ZDOT =     -12286.098917                 ZDOT =       -3751.542669
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        3612187.81                 X    =         1100994.84
     Y    =       17237042.92  feet           Y    =         5253850.68  meter
     Z    =       13628612.64                 Z    =         4154001.13
     XDOT =     -16098.971427                 XDOT =       -4906.966491
     YDOT =      13144.739348  feet/sec       YDOT =        4006.516553  meter/sec
     ZDOT =     -12313.639415                 ZDOT =       -3753.197294
  
  
    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   14250.40255250  .00016717  00000-0  10270-3 0  9136
    2 25544  51.6454  52.0928 0003228  75.9289 284.2220 15.50322155 24081
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14250.40255250   =   yrday.fracday
    Element set:     913
    Inclination:       51.6454  deg
    RA of node:        52.0928  deg
    Eccentricity:     .0003228     
    Arg of perigee:    75.9289  deg
    Mean anomaly:     284.2220  deg
    Mean motion:   15.50322155  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2408
    Checksum:              281
 
 
    Coasting Arc #15 (Orbit 2422)
    ---------------------------------------
 
    Vector Time (GMT): 2014/251/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =        5412116.67                 A    =         6794085.31  meter
     Y    =        1264000.87  meter          E    =           .0009434
     Z    =       -3916785.49                 I    =           51.90823
     XDOT =       1499.516798                 Wp   =           96.79500
     YDOT =       6282.169151  meter/sec      RA   =           46.67931  deg
     ZDOT =       4106.738263                 TA   =          216.15501
                                              MA   =          216.21883
                                              Ha   =            228.219  n.mi
                                              Hp   =            219.594
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =       17756288.30                 X    =         5416606.36
     Y    =        4146984.49  feet           Y    =         1324547.28  meter
     Z    =      -12850346.11                 Z    =        -3890483.74
     XDOT =       4919.674533                 XDOT =        1409.207687
     YDOT =      20610.791177  feet/sec       YDOT =        6298.433277  meter/sec
     ZDOT =      13473.550731                 ZDOT =        4113.802496
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =       -4248443.08                 X    =        -1294925.45
     Y    =      -17812713.71  feet           Y    =        -5429315.14  meter
     Z    =      -12738626.74                 Z    =        -3882733.43
     XDOT =      14990.174124                 XDOT =        4569.005073
     YDOT =     -13213.953221  feet/sec       YDOT =       -4027.612942  meter/sec
     ZDOT =      13502.512258                 ZDOT =        4115.565736
  
  
    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   14251.36947142  .00016717  00000-0  10270-3 0  9141
    2 25544  51.6441  47.2990 0003263  81.0474 279.1046 15.50314307 24231
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14251.36947142   =   yrday.fracday
    Element set:     914
    Inclination:       51.6441  deg
    RA of node:        47.2990  deg
    Eccentricity:     .0003263     
    Arg of perigee:    81.0474  deg
    Mean anomaly:     279.1046  deg
    Mean motion:   15.50314307  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2423
    Checksum:              286
 
 
    Coasting Arc #16 (Orbit 2438)
    ---------------------------------------
 
    Vector Time (GMT): 2014/252/08:39:58.233
    Vector Time (MET): N/A
    Weight (LBS)     : 928846.8
 
              M50 Cartesian                         M50 Keplerian  
    -----------------------------------       --------------------------------
     X    =       -5630072.61                 A    =         6794983.10  meter
     Y    =       -1263928.65  meter          E    =           .0015241
     Z    =        3576252.06                 I    =           51.89035
     XDOT =      -1497.834353                 Wp   =           86.09395
     YDOT =      -6041.214299  meter/sec      RA   =           41.73993  deg
     ZDOT =      -4475.702210                 TA   =           51.87553
                                              MA   =           51.73823
                                              Ha   =            228.158  n.mi
                                              Hp   =            219.474
 
              M50 Cartesian                         J2K Cartesian  
    -----------------------------------       --------------------------------
     X    =      -18471366.85                 X    =        -5632892.81
     Y    =       -4146747.54  feet           Y    =        -1326903.05  meter
     Z    =       11733110.44                 Z    =         3548895.47
     XDOT =      -4914.154702                 XDOT =       -1408.427395
     YDOT =     -19820.256888  feet/sec       YDOT =       -6057.464758  meter/sec
     ZDOT =     -14684.062369                 ZDOT =       -4482.760446
 
              TDR Cartesian                         TDR Cartesian  
    -----------------------------------       --------------------------------
     X    =        4881114.56                 X    =         1487763.72
     Y    =       18365046.58  feet           Y    =         5597666.20  meter
     Z    =       11616908.96                 Z    =         3540833.85
     XDOT =     -14019.712014                 XDOT =       -4273.208222
     YDOT =      13069.546880  feet/sec       YDOT =        3983.597889  meter/sec
     ZDOT =     -14713.034853                 ZDOT =       -4484.533023
  
  
    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   14252.40083224  .00016717  00000-0  10270-3 0  9150
    2 25544  51.6447  42.1866 0003139  81.4806 278.6700 15.50369890 24393
  
  
    Satellite: ISS
    Catalog Number: 25544
    Epoch time:      14252.40083224   =   yrday.fracday
    Element set:     915
    Inclination:       51.6447  deg
    RA of node:        42.1866  deg
    Eccentricity:     .0003139     
    Arg of perigee:    81.4806  deg
    Mean anomaly:     278.6700  deg
    Mean motion:   15.50369890  rev/day
    Decay rate:    1.67170E-04  rev/day^2
    Epoch rev:            2439
    Checksum:              307
 
             

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