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Date:
May 25th 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 ------------------------------------------------------------------------ 145/15:23:22.259 11.3 -0.1 17.6 010/21:03:13.304 6.7 -0.0 193.9 000/00:00:12.608 11.7 -17.6 181.7
Coasting Arc #1 (Orbit 150)
Vector Time (GMT): 2010/144/05:06:55.000 Vector Time (MET): 009/10:46:46.045 Weight (LBS) : 221081.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739169.20 A = 6722925.08 meter
Y = -3210263.48 meter E = .0016348
Z = -4586272.80 I = 51.59510
XDOT = 6357.177738 Wp = 26.96158
YDOT = -3142.358338 meter/sec RA = 353.10948 deg
ZDOT = -2973.239778 TA = 213.42123
MA = 213.52452
Ha = 192.297 n.mi
Hp = 183.054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12267615.50 X = -3680713.90
Y = -10532360.49 feet Y = -3251749.89 meter
Z = -15046826.78 Z = -4604296.24
XDOT = 20856.882344 XDOT = 6406.287369
YDOT = -10309.574601 feet/sec YDOT = -3070.993772 meter/sec
ZDOT = -9754.723682 ZDOT = -2942.237058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1905214.81 X = -580709.47
Y = -15988436.72 feet Y = -4873275.51 meter
Z = -15118599.51 Z = -4608149.13
XDOT = 21235.882470 XDOT = 6472.696977
YDOT = 6608.172546 feet/sec YDOT = 2014.170992 meter/sec
ZDOT = -9631.239121 ZDOT = -2935.601684
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 10144.23415742 .00020000 00000-0 20000-3 0 9001
2 36572 51.6454 353.4871 0011187 347.7804 12.3086 15.74016213 1519
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10144.23415742 = yrday.fracday
Element set: 900
Inclination: 51.6454 deg
RA of node: 353.4871 deg
Eccentricity: .0011187
Arg of perigee: 347.7804 deg
Mean anomaly: 12.3086 deg
Mean motion: 15.74016213 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 151
Checksum: 261
Coasting Arc #2 (Orbit 166)
Vector Time (GMT): 2010/145/05:07:29.776 Vector Time (MET): 010/10:47:20.821 Weight (LBS) : 221081.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479639.18 A = 6729692.90 meter
Y = 3100864.13 meter E = .0013693
Z = 2378578.25 I = 51.58816
XDOT = -4295.064985 Wp = 58.17708
YDOT = -3441.964680 meter/sec RA = 347.92575 deg
ZDOT = -5377.869431 TA = 95.01376
MA = 94.85743
Ha = 192.466 n.mi
Hp = 182.940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17977818.82 X = -5525461.26
Y = 10173438.73 feet Y = 3039331.09 meter
Z = 7803734.40 Z = 2351846.67
XDOT = -14091.420555 XDOT = -4230.131886
YDOT = -11292.535040 feet/sec YDOT = -3489.631043 meter/sec
ZDOT = -17643.928578 ZDOT = -5398.577879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20261101.26 X = -6175583.66
Y = -4223629.88 feet Y = -1287362.39 meter
Z = 7697260.71 Z = 2346125.06
XDOT = -3387.760093 XDOT = -1032.589276
YDOT = -16233.772562 feet/sec YDOT = -4948.053877 meter/sec
ZDOT = -17726.388959 ZDOT = -5403.003355
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 10145.24997835 .00020000 00000-0 20000-3 0 9012
2 36572 51.6456 348.2709 0011274 351.5455 8.5517 15.74033977 1674
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145.24997835 = yrday.fracday
Element set: 901
Inclination: 51.6456 deg
RA of node: 348.2709 deg
Eccentricity: .0011274
Arg of perigee: 351.5455 deg
Mean anomaly: 8.5517 deg
Mean motion: 15.74033977 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 167
Checksum: 307
Coasting Arc #3 (Orbit 173)
Vector Time (GMT): 2010/145/15:23:28.563 Vector Time (MET): 010/21:03:19.608 Weight (LBS) : 220697.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262066.21 A = 6723050.91 meter
Y = 2599573.09 meter E = .0013333
Z = 4493725.11 I = 51.55255
XDOT = -5764.116617 Wp = 12.07650
YDOT = 4036.590451 meter/sec RA = 345.76578 deg
ZDOT = 3142.990439 TA = 46.59888
MA = 46.48795
Ha = 193.910 n.mi
Hp = 181.696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13983156.86 X = 4210850.42
Y = 8528783.10 feet Y = 2646947.18 meter
Z = 14743192.62 Z = 4514306.52
XDOT = -18911.143757 XDOT = -5824.094464
YDOT = 13243.406991 feet/sec YDOT = 3971.796955 meter/sec
ZDOT = 10311.648421 ZDOT = 3114.842590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2365866.47 X = 721116.10
Y = -16132209.43 feet Y = -4917097.43 meter
Z = 14825148.91 Z = 4518705.39
XDOT = 18469.695762 XDOT = 5629.563268
YDOT = 12048.387081 feet/sec YDOT = 3672.348382 meter/sec
ZDOT = 10199.529579 ZDOT = 3108.816616
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 10145.69440136 .00020000 00000-0 20000-3 0 9029
2 36572 51.6443 345.9838 0017293 342.9630 17.0950 15.74078594 1741
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145.69440136 = yrday.fracday
Element set: 902
Inclination: 51.6443 deg
RA of node: 345.9838 deg
Eccentricity: .0017293
Arg of perigee: 342.9630 deg
Mean anomaly: 17.0950 deg
Mean motion: 15.74078594 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 174
Checksum: 301
Coasting Arc #4 (Orbit 188)
Vector Time (GMT): 2010/146/15:24:03.568 Vector Time (MET): 011/21:03:54.613 Weight (LBS) : 220697.9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880170.62 A = 6729240.37 meter
Y = -3856550.09 meter E = .0020258
Z = -2536322.42 I = 51.54501
XDOT = 4897.378121 Wp = 359.98214
YDOT = 2729.737006 meter/sec RA = 340.57710 deg
ZDOT = 5292.364101 TA = 331.19102
MA = 331.30274
Ha = 194.240 n.mi
Hp = 181.481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16011058.48 X = 4935253.77
Y = -12652723.41 feet Y = -3801668.78 meter
Z = -8321267.79 Z = -2512480.85
XDOT = 16067.513521 XDOT = 4840.779906
YDOT = 8955.830072 feet/sec YDOT = 2784.185215 meter/sec
ZDOT = 17363.399282 ZDOT = 5316.018901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18145749.25 X = -5530824.37
Y = -9420654.50 feet Y = -2871415.49 meter
Z = -8226296.47 Z = -2507375.17
XDOT = 896.621390 XDOT = 273.290200
YDOT = -16913.682960 feet/sec YDOT = -5155.290566 meter/sec
ZDOT = 17457.592792 ZDOT = 5321.074283
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 10146.64670948 .00020000 00000-0 20000-3 0 9032
2 36572 51.6453 341.0938 0017293 347.0084 13.0632 15.74068320 1894
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10146.64670948 = yrday.fracday
Element set: 903
Inclination: 51.6453 deg
RA of node: 341.0938 deg
Eccentricity: .0017293
Arg of perigee: 347.0084 deg
Mean anomaly: 13.0632 deg
Mean motion: 15.74068320 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 189
Checksum: 287
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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