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Date:
May 24th 2010
<B> SHUTTLE TRAJECTORY DATA</B>
Lift off time (UTC) : 2010/134/18:20:08.955
Area (sq ft) : 1208.48
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 80.0
Monthly MSFC 50% earth geomagnetic index (Kp) : 0.80
ET - UTC (sec) : 66.18
UT1 - UTC (sec) : 0.0
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 ------------------------------------------------------------------------ 143/14:34:09.230 0.1 -0.1 0.1 008/20:14:00.275 0.0 0.1 191.4 000/00:00:00.549 -0.1 0.0 183.1 143/16:37:14.662 -2.9 -0.0 3.0 008/22:17:05.707 0.6 -0.0 191.7 000/00:00:11.414 0.5 -3.0 182.8 143/17:05:11.808 1.5 1.5 1.5 008/22:45:02.853 0.0 0.0 192.0 000/00:00:05.705 0.2 -0.0 183.4
Coasting Arc #1 (Orbit 113)
Vector Time (GMT): 2010/141/20:07:01.000 Vector Time (MET): 007/01:46:52.045 Weight (LBS) : 214758.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -717806.54 A = 6719533.18 meter
Y = 4115217.58 meter E = .0010016
Z = 5264721.13 I = 51.66005
XDOT = -7637.199375 Wp = 352.99453
YDOT = -940.649143 meter/sec RA = 5.27638 deg
ZDOT = -296.307509 TA = 99.87398
MA = 99.76088
Ha = 191.320 n.mi
Hp = 183.605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2355008.34 X = -789345.49
Y = 13501370.02 feet Y = 4106790.34 meter
Z = 17272707.12 Z = 5261060.48
XDOT = -25056.428396 XDOT = -7624.673834
YDOT = -3086.119236 feet/sec YDOT = -1025.982804 meter/sec
ZDOT = -972.137496 ZDOT = -333.378851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2377884.94 X = 724779.33
Y = -13516007.55 feet Y = -4119679.10 meter
Z = 17258118.99 Z = 5260274.67
XDOT = 24082.264144 XDOT = 7340.274111
YDOT = 2766.311354 feet/sec YDOT = 843.171701 meter/sec
ZDOT = -1119.794933 ZDOT = -341.313496
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
SHUTTLE
1 36572U 10019A 10141.88526817 .00020000 00000-0 20000-3 0 9005
2 36572 51.6483 5.5448 0009925 338.9424 21.1329 15.74211672 1146
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10141.88526817 = yrday.fracday
Element set: 900
Inclination: 51.6483 deg
RA of node: 5.5448 deg
Eccentricity: .0009925
Arg of perigee: 338.9424 deg
Mean anomaly: 21.1329 deg
Mean motion: 15.74211672 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 114
Checksum: 282
Coasting Arc #2 (Orbit 129)
Vector Time (GMT): 2010/142/20:07:47.167 Vector Time (MET): 008/01:47:38.212 Weight (LBS) : 214688.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6672574.17 A = 6731452.35 meter
Y = 499197.29 meter E = .0019356
Z = 609548.58 I = 51.66997
XDOT = -907.973768 Wp = 22.67398
YDOT = 4746.603776 meter/sec RA = .14842 deg
ZDOT = 6006.725392 TA = 343.96709
MA = 344.02826
Ha = 191.474 n.mi
Hp = 183.357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21891647.54 X = 6663535.02
Y = 1637786.38 feet Y = 573763.41 meter
Z = 1999831.30 Z = 641942.35
XDOT = -2978.916561 XDOT = -990.163546
YDOT = 15572.847034 feet/sec YDOT = 4735.990379 meter/sec
ZDOT = 19707.104304 ZDOT = 6002.115043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21915096.45 X = -6679721.40
Y = -1059450.46 feet Y = -322920.50 meter
Z = 2128852.66 Z = 648874.29
XDOT = 2605.462512 XDOT = 794.144974
YDOT = -14051.665120 feet/sec YDOT = -4282.947528 meter/sec
ZDOT = 19688.731588 ZDOT = 6001.125388
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
SHUTTLE
1 36572U 10019A 10142.90098002 .00020000 00000-0 20000-3 0 9010
2 36572 51.6484 .3286 0009985 343.4320 16.6515 15.74195910 1302
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10142.90098002 = yrday.fracday
Element set: 901
Inclination: 51.6484 deg
RA of node: .3286 deg
Eccentricity: .0009985
Arg of perigee: 343.4320 deg
Mean anomaly: 16.6515 deg
Mean motion: 15.74195910 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 130
Checksum: 263
Coasting Arc #3 (Orbit 141)
Vector Time (GMT): 2010/143/14:34:09.504 Vector Time (MET): 008/20:14:00.549 Weight (LBS) : 214684.4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025782.05 A = 6725531.18 meter
Y = 2561971.08 meter E = .0012633
Z = 3646438.97 I = 51.62290
XDOT = -5098.897557 Wp = 46.68514
YDOT = 3796.693669 meter/sec RA = 356.21959 deg
ZDOT = 4359.231242 TA = 357.14156
MA = 357.14878
Ha = 191.403 n.mi
Hp = 183.115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16488786.25 X = 4979046.11
Y = 8405416.94 feet Y = 2617910.82 meter
Z = 11963382.45 Z = 3670741.21
XDOT = -16728.666527 XDOT = -5162.150557
YDOT = 12456.344058 feet/sec YDOT = 3739.320803 meter/sec
ZDOT = 14301.939769 ZDOT = 4334.307060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5775653.53 X = 1760419.20
Y = -17517072.26 feet Y = -5339203.62 meter
Z = 12060167.15 Z = 3675938.95
XDOT = 13621.208778 XDOT = 4151.744435
YDOT = 14271.387429 feet/sec YDOT = 4349.918888 meter/sec
ZDOT = 14202.661885 ZDOT = 4328.971342
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
SHUTTLE
1 36572U 10019A 10143.66274765 .00020000 00000-0 20000-3 0 9027
2 36572 51.6437 356.4139 0010058 345.6385 14.4491 15.74267070 1429
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143.66274765 = yrday.fracday
Element set: 902
Inclination: 51.6437 deg
RA of node: 356.4139 deg
Eccentricity: .0010058
Arg of perigee: 345.6385 deg
Mean anomaly: 14.4491 deg
Mean motion: 15.74267070 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 142
Checksum: 287
Coasting Arc #4 (Orbit 142)
Vector Time (GMT): 2010/143/16:37:20.369 Vector Time (MET): 008/22:17:11.414 Weight (LBS) : 214609.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6530778.40 A = 6731021.85 meter
Y = 1283504.22 meter E = .0010273
Z = 1004763.55 I = 51.63959
XDOT = -1816.531334 Wp = 78.13947
YDOT = -4565.207267 meter/sec RA = 355.74347 deg
ZDOT = -5922.481185 TA = 90.88630
MA = 90.76859
Ha = 191.715 n.mi
Hp = 182.780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21426438.34 X = -6549526.42
Y = 4210971.84 feet Y = 1210368.27 meter
Z = 3296468.35 Z = 972991.12
XDOT = -5959.748470 XDOT = -1736.576600
YDOT = -14977.714129 feet/sec YDOT = -4585.073349 meter/sec
ZDOT = -19430.712550 ZDOT = -5931.112118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16949111.19 X = 5166089.09
Y = 13797480.63 feet Y = 4205472.10 meter
Z = 3169921.96 Z = 966192.21
XDOT = -6773.916181 XDOT = -2064.689652
YDOT = 12834.759957 feet/sec YDOT = 3912.034835 meter/sec
ZDOT = -19465.075909 ZDOT = -5932.955137
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
SHUTTLE
1 36572U 10019A 10143.72623314 .00020000 00000-0 20000-3 0 9033
2 36572 51.6448 356.0868 0009895 353.1826 6.9201 15.74262816 1436
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143.72623314 = yrday.fracday
Element set: 903
Inclination: 51.6448 deg
RA of node: 356.0868 deg
Eccentricity: .0009895
Arg of perigee: 353.1826 deg
Mean anomaly: 6.9201 deg
Mean motion: 15.74262816 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 143
Checksum: 290
Coasting Arc #5 (Orbit 142)
Vector Time (GMT): 2010/143/17:05:14.660 Vector Time (MET): 008/22:45:05.705 Weight (LBS) : 214572.6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 700139.57 A = 6720424.47 meter
Y = -4195947.19 meter E = .0014626
Z = -5212032.88 I = 51.60205
XDOT = 7636.860108 Wp = 56.17821
YDOT = 147.500282 meter/sec RA = 355.64706 deg
ZDOT = 916.950212 TA = 222.51283
MA = 222.62618
Ha = 192.008 n.mi
Hp = 183.434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2297045.83 X = 772326.85
Y = -13766230.94 feet Y = -4187713.84 meter
Z = -17099845.41 Z = -5208456.49
XDOT = 25055.315316 XDOT = 7630.188698
YDOT = 483.924810 feet/sec YDOT = 232.862836 meter/sec
ZDOT = 3008.366838 ZDOT = 954.034419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11180937.01 X = -3407949.60
Y = 8382093.51 feet Y = 2554862.10 meter
Z = -17085590.51 Z = -5207687.99
XDOT = -17289.954435 XDOT = -5269.978112
YDOT = -16695.814231 feet/sec YDOT = -5088.884177 meter/sec
ZDOT = 3156.065122 ZDOT = 961.968649
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
SHUTTLE
1 36572U 10019A 10143.72623388 .00020000 00000-0 20000-3 0 9045
2 36572 51.6461 356.0885 0010174 347.2827 12.8079 15.73991511 1436
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143.72623388 = yrday.fracday
Element set: 904
Inclination: 51.6461 deg
RA of node: 356.0885 deg
Eccentricity: .0010174
Arg of perigee: 347.2827 deg
Mean anomaly: 12.8079 deg
Mean motion: 15.73991511 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 143
Checksum: 292
Coasting Arc #6 (Orbit 158)
Vector Time (GMT): 2010/144/17:05:42.445 Vector Time (MET): 009/22:45:33.490 Weight (LBS) : 214572.6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6652890.67 A = 6731684.12 meter
Y = 312400.20 meter E = .0005025
Z = -993422.50 I = 51.60999
XDOT = 652.843751 Wp = 59.85609
YDOT = -4865.915396 meter/sec RA = 350.52454 deg
ZDOT = -5922.016161 TA = 130.99271
MA = 130.94924
Ha = 192.152 n.mi
Hp = 183.156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21827069.13 X = -6651063.57
Y = 1024935.04 feet Y = 238013.92 meter
Z = -3259260.18 Z = -1025738.36
XDOT = 2141.875822 XDOT = 735.975369
YDOT = -15964.289357 feet/sec YDOT = -4858.149563 meter/sec
ZDOT = -19429.186879 ZDOT = -5918.643095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16853228.38 X = 5136864.01
Y = 13877485.60 feet Y = 4229857.61 meter
Z = -3387964.31 Z = -1032651.52
XDOT = -11376.295240 XDOT = -3467.494789
YDOT = 9090.913687 feet/sec YDOT = 2770.910492 meter/sec
ZDOT = -19415.736378 ZDOT = -5917.916448
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
SHUTTLE
1 36572U 10019A 10144.74207957 .00020000 00000-0 20000-3 0 9059
2 36572 51.6459 350.8711 0010291 350.8750 9.2225 15.74008173 1592
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10144.74207957 = yrday.fracday
Element set: 905
Inclination: 51.6459 deg
RA of node: 350.8711 deg
Eccentricity: .0010291
Arg of perigee: 350.8750 deg
Mean anomaly: 9.2225 deg
Mean motion: 15.74008173 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 159
Checksum: 282
SPACE SHUTTLE 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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