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Date:
July 28th 2010
<B> ISS TRAJECTORY DATA</B>
Lift off time (UTC) : N/A
Area (sq ft) : 8880.23
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 74.8
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.74
ET - UTC (sec) : 66.18
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
There are no maneuvers.
Coasting Arc #1 (Orbit 2979)
Vector Time (GMT): 2010/208/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5593976.34 A = 6734057.59 meter
Y = 646179.01 meter E = .0015774
Z = 3675431.36 I = 51.78783
XDOT = -3477.261292 Wp = 109.99564
YDOT = -5327.330457 meter/sec RA = 24.33098 deg
ZDOT = -4346.054904 TA = 25.92703
MA = 25.84808
Ha = 196.274 n.mi
Hp = 186.497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18352940.75 X = -5618640.45
Y = 2120009.87 feet Y = 583485.61 meter
Z = 12058501.84 Z = 3648196.59
XDOT = -11408.337572 XDOT = -3396.319810
YDOT = -17478.118298 feet/sec YDOT = -5365.762334 meter/sec
ZDOT = -14258.710314 ZDOT = -4362.750903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -588585.71 X = -179400.92
Y = 18536274.98 feet Y = 5649856.61 meter
Z = 11949578.21 Z = 3642231.44
XDOT = -17591.172354 XDOT = -5361.789334
YDOT = 8697.160616 feet/sec YDOT = 2650.894556 meter/sec
ZDOT = -14325.425943 ZDOT = -4366.389827
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 10208.42135606 .00016717 00000-0 10270-3 0 9005
2 25544 51.6461 24.6869 0007109 156.0301 204.1193 15.71318315 29807
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208.42135606 = yrday.fracday
Element set: 900
Inclination: 51.6461 deg
RA of node: 24.6869 deg
Eccentricity: .0007109
Arg of perigee: 156.0301 deg
Mean anomaly: 204.1193 deg
Mean motion: 15.71318315 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 276
Coasting Arc #2 (Orbit 2995)
Vector Time (GMT): 2010/209/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4323530.30 A = 6735628.52 meter
Y = 4113538.89 meter E = .0016416
Z = 3116620.96 I = 51.76403
XDOT = -5559.592175 Wp = 110.12131
YDOT = 2127.643949 meter/sec RA = 19.27540 deg
ZDOT = 4878.099003 TA = 285.98971
MA = 286.17049
Ha = 196.088 n.mi
Hp = 186.653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14184810.69 X = 4262070.96
Y = 13495862.51 feet Y = 4161543.35 meter
Z = 10225134.38 Z = 3137475.22
XDOT = -18240.131807 XDOT = -5606.667103
YDOT = 6980.459149 feet/sec YDOT = 2065.209731 meter/sec
ZDOT = 16004.261820 ZDOT = 4850.976866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15202542.06 X = 4633734.82
Y = -12268588.04 feet Y = -3739465.64 meter
Z = 10308491.39 Z = 3142028.17
XDOT = 3667.337869 XDOT = 1117.804583
YDOT = 17972.248025 feet/sec YDOT = 5477.941198 meter/sec
ZDOT = 15895.776677 ZDOT = 4845.032731
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 10209.43894824 .00016717 00000-0 10270-3 0 9012
2 25544 51.6451 19.4817 0007132 160.5853 199.5582 15.71289510 29969
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209.43894824 = yrday.fracday
Element set: 901
Inclination: 51.6451 deg
RA of node: 19.4817 deg
Eccentricity: .0007132
Arg of perigee: 160.5853 deg
Mean anomaly: 199.5582 deg
Mean motion: 15.71289510 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 325
Coasting Arc #3 (Orbit 3010)
Vector Time (GMT): 2010/210/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3852262.72 A = 6730298.20 meter
Y = -2876537.27 meter E = .0016302
Z = -4725089.92 I = 51.71634
XDOT = 6132.831492 Wp = 129.83370
YDOT = 3750.621062 meter/sec RA = 14.12118 deg
ZDOT = 2712.611111 TA = 166.91581
MA = 166.87347
Ha = 196.032 n.mi
Hp = 186.862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12638657.22 X = 3907095.60
Y = -9437458.24 feet Y = -2833152.13 meter
Z = -15502263.53 Z = -4706242.93
XDOT = 20120.838229 XDOT = 6077.258418
YDOT = 12305.187210 feet/sec YDOT = 3818.891184 meter/sec
ZDOT = 8899.642752 ZDOT = 2742.269086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7957073.02 X = -2425315.86
Y = -13704677.99 feet Y = -4177185.85 meter
Z = -15426867.43 Z = -4702109.19
XDOT = 13470.483680 XDOT = 4105.803426
YDOT = -17987.608328 feet/sec YDOT = -5482.623018 meter/sec
ZDOT = 9018.206619 ZDOT = 2748.749377
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 10210.39293210 .00016717 00000-0 10270-3 0 9022
2 25544 51.6444 14.6014 0007186 164.0441 196.0948 15.71307656 30117
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210.39293210 = yrday.fracday
Element set: 902
Inclination: 51.6444 deg
RA of node: 14.6014 deg
Eccentricity: .0007186
Arg of perigee: 164.0441 deg
Mean anomaly: 196.0948 deg
Mean motion: 15.71307656 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 273
Coasting Arc #4 (Orbit 3026)
Vector Time (GMT): 2010/211/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6149261.14 A = 6738741.61 meter
Y = -2239238.65 meter E = .0014770
Z = -1576435.39 I = 51.71527
XDOT = 2977.419840 Wp = 154.19670
YDOT = -4137.640630 meter/sec RA = 9.04818 deg
ZDOT = -5770.027550 TA = 43.16194
MA = 43.04625
Ha = 195.880 n.mi
Hp = 186.928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20174741.26 X = -6116106.60
Y = -7346583.49 feet Y = -2307817.92 meter
Z = -5172032.11 Z = -1606227.64
XDOT = 9768.437795 XDOT = 3051.495761
YDOT = -13574.936450 feet/sec YDOT = -4103.930913 meter/sec
ZDOT = -18930.536581 ZDOT = -5755.383696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9219001.35 X = -2809951.61
Y = 19358621.18 feet Y = 5900507.74 meter
Z = -5291142.64 Z = -1612740.28
XDOT = -11168.560027 XDOT = -3404.177096
YDOT = -10447.750805 feet/sec YDOT = -3184.474445 meter/sec
ZDOT = -18871.939189 ZDOT = -5752.167065
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 10211.41050696 .00016717 00000-0 10270-3 0 9036
2 25544 51.6443 9.3977 0007166 168.2313 191.9018 15.71300350 30270
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211.41050696 = yrday.fracday
Element set: 903
Inclination: 51.6443 deg
RA of node: 9.3977 deg
Eccentricity: .0007166
Arg of perigee: 168.2313 deg
Mean anomaly: 191.9018 deg
Mean motion: 15.71300350 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 280
Coasting Arc #5 (Orbit 3042)
Vector Time (GMT): 2010/212/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1184044.76 A = 6728017.60 meter
Y = 4063459.05 meter E = .0006664
Z = 5225971.16 I = 51.64887
XDOT = -7568.456691 Wp = 143.90256
YDOT = -1163.824886 meter/sec RA = 3.91381 deg
ZDOT = -814.609073 TA = 313.82223
MA = 313.87731
Ha = 195.858 n.mi
Hp = 187.078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3884661.28 X = -1254781.66
Y = 13331558.55 feet Y = 4049822.62 meter
Z = 17145574.66 Z = 5220047.47
XDOT = -24830.894657 XDOT = -7550.922900
YDOT = -3818.323116 feet/sec YDOT = -1248.361824 meter/sec
ZDOT = -2672.601945 ZDOT = -851.333721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12983383.03 X = 3957335.15
Y = 5006579.44 feet Y = 1526005.41 meter
Z = 17121848.74 Z = 5218739.50
XDOT = -5363.530457 XDOT = -1634.804083
YDOT = 23497.652406 feet/sec YDOT = 7162.084453 meter/sec
ZDOT = -2819.436920 ZDOT = -859.364373
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 10212.42807305 .00016717 00000-0 10270-3 0 9046
2 25544 51.6442 4.1925 0007175 171.9126 188.2153 15.71307487 30433
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212.42807305 = yrday.fracday
Element set: 904
Inclination: 51.6442 deg
RA of node: 4.1925 deg
Eccentricity: .0007175
Arg of perigee: 171.9126 deg
Mean anomaly: 188.2153 deg
Mean motion: 15.71307487 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 283
Coasting Arc #6 (Orbit 3057)
Vector Time (GMT): 2010/213/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6731837.90 A = 6739769.80 meter
Y = -265371.59 meter E = .0009054
Z = -157855.97 I = 51.65758
XDOT = 322.280996 Wp = 80.29205
YDOT = 4763.703897 meter/sec RA = 358.80446 deg
ZDOT = 6029.911767 TA = 277.99649
MA = 278.09922
Ha = 195.703 n.mi
Hp = 187.190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22086082.34 X = 6735071.83
Y = -870641.69 feet Y = -190074.06 meter
Z = -517900.17 Z = -125145.08
XDOT = 1057.352350 XDOT = 239.696414
YDOT = 15628.949793 feet/sec YDOT = 4766.845799 meter/sec
ZDOT = 19783.175087 ZDOT = 6031.277023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 462435.97 X = 140950.48
Y = -22101076.27 feet Y = -6736408.05 meter
Z = -387106.09 Z = -117989.94
XDOT = 14046.203067 XDOT = 4281.282695
YDOT = -30.073606 feet/sec YDOT = -9.166435 meter/sec
ZDOT = 19788.586276 ZDOT = 6031.561097
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 10213.38203262 .00016717 00000-0 10270-3 0 9055
2 25544 51.6433 359.3122 0007151 175.6075 184.5151 15.71330643 30588
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213.38203262 = yrday.fracday
Element set: 905
Inclination: 51.6433 deg
RA of node: 359.3122 deg
Eccentricity: .0007151
Arg of perigee: 175.6075 deg
Mean anomaly: 184.5151 deg
Mean motion: 15.71330643 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 277
Coasting Arc #7 (Orbit 3073)
Vector Time (GMT): 2010/214/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1712233.94 A = 6728046.28 meter
Y = -3946824.50 meter E = .0015346
Z = -5184402.89 I = 51.58777
XDOT = 7403.464701 Wp = 108.94118
YDOT = -1725.985859 meter/sec RA = 353.69868 deg
ZDOT = -1138.770211 TA = 150.20420
MA = 150.11673
Ha = 195.593 n.mi
Hp = 187.195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5617565.44 X = -1642787.79
Y = -12948899.29 feet Y = -3965583.13 meter
Z = -17009195.85 Z = -5192552.44
XDOT = 24289.582354 XDOT = 7427.746662
YDOT = -5662.683266 feet/sec YDOT = -1643.060056 meter/sec
ZDOT = -3736.122739 ZDOT = -1102.745455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13175192.30 X = -4015798.61
Y = 4953504.95 feet Y = 1509828.31 meter
Z = -17041739.17 Z = -5194322.10
XDOT = -4248.484509 XDOT = -1294.938078
YDOT = -23572.005877 feet/sec YDOT = -7184.747391 meter/sec
ZDOT = -3592.068103 ZDOT = -1094.862358
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 10214.39958184 .00016717 00000-0 10270-3 0 9068
2 25544 51.6429 354.1072 0007200 178.3150 181.8037 15.71354547 30749
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214.39958184 = yrday.fracday
Element set: 906
Inclination: 51.6429 deg
RA of node: 354.1072 deg
Eccentricity: .0007200
Arg of perigee: 178.3150 deg
Mean anomaly: 181.8037 deg
Mean motion: 15.71354547 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 301
Coasting Arc #8 (Orbit 3089)
Vector Time (GMT): 2010/215/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5903272.77 A = 6738203.55 meter
Y = 2665364.26 meter E = .0017808
Z = 1817445.51 I = 51.59266
XDOT = -3499.597939 Wp = 135.68222
YDOT = -3873.878546 meter/sec RA = 348.55385 deg
ZDOT = -5665.141610 TA = 24.15040
MA = 24.06701
Ha = 195.343 n.mi
Hp = 187.478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19367692.82 X = -5941467.41
Y = 8744633.38 feet Y = 2599136.64 meter
Z = 5962747.75 Z = 1788674.94
XDOT = -11481.620536 XDOT = -3428.499288
YDOT = -12709.575282 feet/sec YDOT = -3912.615189 meter/sec
ZDOT = -18586.422606 ZDOT = -5681.970187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8239180.98 X = 2511302.36
Y = 19622714.67 feet Y = 5981003.43 meter
Z = 5847688.85 Z = 1782375.56
XDOT = -11569.624076 XDOT = -3526.421418
YDOT = 10437.436060 feet/sec YDOT = 3181.330511 meter/sec
ZDOT = -18653.665050 ZDOT = -5685.637107
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 10215.41712003 .00016717 00000-0 10270-3 0 9071
2 25544 51.6433 348.9021 0006997 184.0724 176.0382 15.71403577 30907
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215.41712003 = yrday.fracday
Element set: 907
Inclination: 51.6433 deg
RA of node: 348.9021 deg
Eccentricity: .0006997
Arg of perigee: 184.0724 deg
Mean anomaly: 176.0382 deg
Mean motion: 15.71403577 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 292
Coasting Arc #9 (Orbit 3105)
Vector Time (GMT): 2010/216/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4222549.98 A = 6730429.50 meter
Y = 2543591.15 meter E = .0012606
Z = 4581813.69 I = 51.53649
XDOT = -5748.476504 Wp = 147.51871
YDOT = 4167.082658 meter/sec RA = 343.47134 deg
ZDOT = 2970.148885 TA = 272.87933
MA = 273.02360
Ha = 195.237 n.mi
Hp = 187.562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13853510.44 X = 4171535.73
Y = 8345115.33 feet Y = 2590524.58 meter
Z = 15032197.15 Z = 4602203.07
XDOT = -18859.831051 XDOT = -5809.074723
YDOT = 13671.531031 feet/sec YDOT = 4102.460665 meter/sec
ZDOT = 9744.582956 ZDOT = 2942.076097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8465173.65 X = 2580184.93
Y = -13691050.62 feet Y = -4173032.23 meter
Z = 15113689.84 Z = 4606652.66
XDOT = 12508.194554 XDOT = 3812.497700
YDOT = 18418.269414 feet/sec YDOT = 5613.888517 meter/sec
ZDOT = 9632.296976 ZDOT = 2935.924118
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 10216.43465247 .00016717 00000-0 10270-3 0 9080
2 25544 51.6426 343.6967 0007157 186.8343 173.2723 15.71385075 31064
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216.43465247 = yrday.fracday
Element set: 908
Inclination: 51.6426 deg
RA of node: 343.6967 deg
Eccentricity: .0007157
Arg of perigee: 186.8343 deg
Mean anomaly: 173.2723 deg
Mean motion: 15.71385075 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3106
Checksum: 318
Coasting Arc #10 (Orbit 3120)
Vector Time (GMT): 2010/217/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3920692.73 A = 6734961.48 meter
Y = -4380230.15 meter E = .0007570
Z = -3296820.05 I = 51.52370
XDOT = 5844.185912 Wp = 151.74716
YDOT = 1693.201433 meter/sec RA = 338.30035 deg
ZDOT = 4698.330260 TA = 169.58441
MA = 169.56872
Ha = 195.249 n.mi
Hp = 187.715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12863165.12 X = 3985397.10
Y = -14370833.81 feet Y = -4336024.49 meter
Z = -10816338.73 Z = -3277616.75
XDOT = 19173.838294 XDOT = 5801.994402
YDOT = 5555.122812 feet/sec YDOT = 1758.318214 meter/sec
ZDOT = 15414.469356 ZDOT = 4726.618804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14480444.91 X = -4413639.61
Y = -12804479.00 feet Y = -3902805.20 meter
Z = -10739511.06 Z = -3273402.97
XDOT = 4459.661443 XDOT = 1359.304808
YDOT = -18072.786406 feet/sec YDOT = -5508.585296 meter/sec
ZDOT = 15527.555388 ZDOT = 4732.798882
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 10217.38858027 .00016717 00000-0 10270-3 0 9098
2 25544 51.6434 338.8166 0007234 188.8703 171.2332 15.71394693 31215
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217.38858027 = yrday.fracday
Element set: 909
Inclination: 51.6434 deg
RA of node: 338.8166 deg
Eccentricity: .0007234
Arg of perigee: 188.8703 deg
Mean anomaly: 171.2332 deg
Mean motion: 15.71394693 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 317
Coasting Arc #11 (Orbit 3136)
Vector Time (GMT): 2010/218/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5716327.37 A = 6733965.97 meter
Y = -276100.67 meter E = .0007238
Z = -3546276.52 I = 51.49356
XDOT = 3023.711564 Wp = 147.81110
YDOT = -5496.799273 meter/sec RA = 333.22671 deg
ZDOT = -4456.218989 TA = 74.49577
MA = 74.41585
Ha = 194.952 n.mi
Hp = 187.729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18754354.89 X = -5695588.15
Y = -905842.10 feet Y = -339907.70 meter
Z = -11634765.47 Z = -3573995.77
XDOT = 9920.313530 XDOT = 3106.600299
YDOT = -18034.118350 feet/sec YDOT = -5462.522366 meter/sec
ZDOT = -14620.141039 ZDOT = -4441.329253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -425874.49 X = -129806.54
Y = 18702240.17 feet Y = 5700442.80 meter
Z = -11745594.42 Z = -3580057.18
XDOT = -16921.941489 XDOT = -5157.807766
YDOT = -9509.022259 feet/sec YDOT = -2898.349985 meter/sec
ZDOT = -14560.547886 ZDOT = -4438.054996
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 10218.40609386 .00016717 00000-0 10270-3 0 9106
2 25544 51.6437 333.6119 0007067 192.6133 167.4853 15.71420869 31370
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218.40609386 = yrday.fracday
Element set: 910
Inclination: 51.6437 deg
RA of node: 333.6119 deg
Eccentricity: .0007067
Arg of perigee: 192.6133 deg
Mean anomaly: 167.4853 deg
Mean motion: 15.71420869 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 310
Coasting Arc #12 (Orbit 3152)
Vector Time (GMT): 2010/219/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1259750.03 A = 6731199.22 meter
Y = 4922980.85 meter E = .0007642
Z = 4406516.97 I = 51.45678
XDOT = -6860.617672 Wp = 117.91068
YDOT = 1189.880333 meter/sec RA = 328.04947 deg
ZDOT = -3289.862997 TA = 5.19906
MA = 5.19113
Ha = 195.006 n.mi
Hp = 188.007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4133038.16 X = -1336111.77
Y = 16151511.99 feet Y = 4908466.14 meter
Z = 14457076.68 Z = 4400212.26
XDOT = -22508.588164 XDOT = -6857.431949
YDOT = 3903.806867 feet/sec YDOT = 1113.178973 meter/sec
ZDOT = -10793.513770 ZDOT = -3323.183448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16318031.61 X = 4973736.03
Y = 3522052.51 feet Y = 1073521.60 meter
Z = 14431819.04 Z = 4398818.44
XDOT = 5119.181452 XDOT = 1560.326507
YDOT = 21066.298842 feet/sec YDOT = 6421.007887 meter/sec
ZDOT = -10926.758020 ZDOT = -3330.475844
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 10219.42359981 .00016717 00000-0 10270-3 0 9113
2 25544 51.6433 328.4063 0007182 196.3063 163.7869 15.71393771 31532
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219.42359981 = yrday.fracday
Element set: 911
Inclination: 51.6433 deg
RA of node: 328.4063 deg
Eccentricity: .0007182
Arg of perigee: 196.3063 deg
Mean anomaly: 163.7869 deg
Mean motion: 15.71393771 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 319
Coasting Arc #13 (Orbit 3168)
Vector Time (GMT): 2010/220/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5940203.61 A = 6737365.17 meter
Y = -2344850.96 meter E = .0010970
Z = 2141388.60 I = 51.45464
XDOT = 134.638995 Wp = 101.16436
YDOT = 5383.033809 meter/sec RA = 322.96383 deg
ZDOT = 5495.129930 TA = 282.81965
MA = 282.94220
Ha = 194.774 n.mi
Hp = 188.032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19488856.98 X = 5955580.42
Y = -7693080.56 feet Y = -2278338.26 meter
Z = 7025553.16 Z = 2170282.62
XDOT = 441.728986 XDOT = 47.741160
YDOT = 17660.872078 feet/sec YDOT = 5384.053058 meter/sec
ZDOT = 18028.641502 ZDOT = 5495.573404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8846993.87 X = -2696563.73
Y = -18949740.66 feet Y = -5775880.95 meter
Z = 7141110.58 Z = 2176610.50
XDOT = 16227.616144 XDOT = 4946.177401
YDOT = -749.995457 feet/sec YDOT = -228.598615 meter/sec
ZDOT = 18030.369416 ZDOT = 5495.656598
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 10220.44109451 .00016717 00000-0 10270-3 0 9123
2 25544 51.6446 323.2014 0007239 200.4868 159.6005 15.71459969 31693
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220.44109451 = yrday.fracday
Element set: 912
Inclination: 51.6446 deg
RA of node: 323.2014 deg
Eccentricity: .0007239
Arg of perigee: 200.4868 deg
Mean anomaly: 159.6005 deg
Mean motion: 15.71459969 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 300
Coasting Arc #14 (Orbit 3183)
Vector Time (GMT): 2010/221/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1418836.85 A = 6728221.07 meter
Y = -4189111.30 meter E = .0014095
Z = -5081508.90 I = 51.40065
XDOT = 6338.354010 Wp = 131.38497
YDOT = -4056.965989 meter/sec RA = 317.80152 deg
ZDOT = 1568.373613 TA = 153.78354
MA = 153.71212
Ha = 194.625 n.mi
Hp = 188.192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4654976.56 X = -1347203.56
Y = -13743803.48 feet Y = -4204576.75 meter
Z = -16671617.12 Z = -5088227.70
XDOT = 20795.124706 XDOT = 6375.629982
YDOT = -13310.255870 feet/sec YDOT = -3985.878397 meter/sec
ZDOT = 5145.582721 ZDOT = 1599.254866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13351452.19 X = -4069522.63
Y = 5603931.44 feet Y = 1708078.30 meter
Z = -16698456.07 Z = -5089689.41
XDOT = -14465.196792 XDOT = -4408.991982
YDOT = -18700.811340 feet/sec YDOT = -5700.007296 meter/sec
ZDOT = 5269.096759 ZDOT = 1606.020692
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 10221.39499044 .00016717 00000-0 10270-3 0 9139
2 25544 51.6450 318.3229 0007091 203.7352 156.3483 15.71456210 31848
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221.39499044 = yrday.fracday
Element set: 913
Inclination: 51.6450 deg
RA of node: 318.3229 deg
Eccentricity: .0007091
Arg of perigee: 203.7352 deg
Mean anomaly: 156.3483 deg
Mean motion: 15.71456210 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3184
Checksum: 291
Coasting Arc #15 (Orbit 3199)
Vector Time (GMT): 2010/222/09:09:47.811
Vector Time (MET): N/A
Weight (LBS) : 828730.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4871358.78 A = 6739227.99 meter
Y = 4607941.10 meter E = .0014927
Z = -572290.44 I = 51.41592
XDOT = -2944.572606 Wp = 165.12510
YDOT = -3850.145630 meter/sec RA = 312.68732 deg
ZDOT = -5984.746134 TA = 21.12026
MA = 21.05869
Ha = 194.364 n.mi
Hp = 188.464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15982148.23 X = -4919743.56
Y = 15117917.00 feet Y = 4553196.14 meter
Z = -1877593.31 Z = -596072.31
XDOT = -9660.671278 XDOT = -2872.228633
YDOT = -12631.711386 feet/sec YDOT = -3882.668940 meter/sec
ZDOT = -19634.993879 ZDOT = -5998.874902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16557438.05 X = 5046707.12
Y = 14472922.23 feet Y = 4411346.70 meter
Z = -1972714.03 Z = -601283.24
XDOT = -10619.974550 XDOT = -3236.968243
YDOT = 9486.237269 feet/sec YDOT = 2891.405120 meter/sec
ZDOT = -19691.473356 ZDOT = -6001.961079
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 10222.41246952 .00016717 00000-0 10270-3 0 9142
2 25544 51.6446 313.1171 0007006 208.4305 151.6476 15.71471886 32003
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222.41246952 = yrday.fracday
Element set: 914
Inclination: 51.6446 deg
RA of node: 313.1171 deg
Eccentricity: .0007006
Arg of perigee: 208.4305 deg
Mean anomaly: 151.6476 deg
Mean motion: 15.71471886 rev/day Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 279
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability. The data normally contains past, current and predicted orbital data. Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics
DOD C-Band Radar Network
Goddard Space Flight Center (GSFC)
NASA Johnson Space Center (JSC)
DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command.
David Cottle
Director Of Engineering
IDB Communications
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