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Date:
May 26th 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 ------------------------------------------------------------------------ 145/15:23:22.242 11.4 -0.1 17.6 010/21:03:13.287 6.6 -0.0 194.0 000/00:00:12.574 11.6 -17.6 181.9
Coasting Arc #1 (Orbit 164)
Vector Time (GMT): 2010/145/01:58:36.000 Vector Time (MET): 010/07:38:27.045 Weight (LBS) : 220514.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538637.26 A = 6725164.58 meter
Y = 4013380.82 meter E = .0015595
Z = 4076887.02 I = 51.57439
XDOT = -6442.461626 Wp = 30.11727
YDOT = -1786.561459 meter/sec RA = 348.59334 deg
ZDOT = -3813.611174 TA = 99.20289
MA = 99.02646
Ha = 192.466 n.mi
Hp = 183.276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11609702.31 X = -3603057.76
Y = 13167259.91 feet Y = 3973449.07 meter
Z = 13375613.59 Z = 4059539.92
XDOT = -21136.685124 XDOT = -6403.478973
YDOT = -5861.422108 feet/sec YDOT = -1858.386559 meter/sec
ZDOT = -12511.847685 ZDOT = -3844.814726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13454883.78 X = -4101048.57
Y = -11356575.88 feet Y = -3461484.33 meter
Z = 13306511.45 Z = 4055824.69
XDOT = 4506.902540 XDOT = 1373.703894
YDOT = -20220.931789 feet/sec YDOT = -6163.340009 meter/sec
ZDOT = -12636.113014 ZDOT = -3851.487247
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 10145.12301315 .00020000 00000-0 20000-3 0 9000
2 36572 51.6440 348.9210 0011304 347.3969 12.6910 15.73955012 1651
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145.12301315 = yrday.fracday
Element set: 900
Inclination: 51.6440 deg
RA of node: 348.9210 deg
Eccentricity: .0011304
Arg of perigee: 347.3969 deg
Mean anomaly: 12.6910 deg
Mean motion: 15.73955012 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 165
Checksum: 252
Coasting Arc #2 (Orbit 173)
Vector Time (GMT): 2010/145/15:23:28.529 Vector Time (MET): 010/21:03:19.574 Weight (LBS) : 219942.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4284247.40 A = 6723350.68 meter
Y = 2584512.06 meter E = .0013265
Z = 4482276.08 I = 51.55234
XDOT = -5742.180619 Wp = 9.07042
YDOT = 4049.389236 meter/sec RA = 345.76447 deg
ZDOT = 3165.196910 TA = 49.35717
MA = 49.24191
Ha = 194.030 n.mi
Hp = 181.883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14055929.81 X = 4233254.00
Y = 8479370.28 feet Y = 2632135.44 meter
Z = 14705630.17 Z = 4502965.78
XDOT = -18839.175258 XDOT = -5802.411091
YDOT = 13285.397757 feet/sec YDOT = 3984.839627 meter/sec
ZDOT = 10384.504298 ZDOT = 3137.155016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2291735.14 X = 698520.87
Y = -16179830.67 feet Y = -4931612.39 meter
Z = 14788017.83 Z = 4507387.83
XDOT = 18476.611363 XDOT = 5631.671144
YDOT = 11971.546591 feet/sec YDOT = 3648.927401 meter/sec
ZDOT = 10272.807379 ZDOT = 3131.151689
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 10145.69444688 .00020000 00000-0 20000-3 0 9014
2 36572 51.6440 345.9822 0017583 340.6204 19.4289 15.73989642 1740
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10145.69444688 = yrday.fracday
Element set: 901
Inclination: 51.6440 deg
RA of node: 345.9822 deg
Eccentricity: .0017583
Arg of perigee: 340.6204 deg
Mean anomaly: 19.4289 deg
Mean motion: 15.73989642 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 174
Checksum: 315
Coasting Arc #3 (Orbit 188)
Vector Time (GMT): 2010/146/15:24:07.947 Vector Time (MET): 011/21:03:58.992 Weight (LBS) : 219942.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4859413.54 A = 6729444.61 meter
Y = -3868065.22 meter E = .0020285
Z = -2558488.24 I = 51.54449
XDOT = 4924.838215 Wp = 357.82024
YDOT = 2708.111398 meter/sec RA = 340.57592 deg
ZDOT = 5278.178461 TA = 333.07664
MA = 333.18174
Ha = 194.365 n.mi
Hp = 181.674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15942957.80 X = 4914734.67
Y = -12690502.71 feet Y = -3813414.70 meter
Z = -8393990.30 Z = -2534746.93
XDOT = 16157.605692 XDOT = 4868.548693
YDOT = 8884.879914 feet/sec YDOT = 2762.868410 meter/sec
ZDOT = 17316.858469 ZDOT = 5301.967411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18155278.61 X = -5533728.92
Y = -9337630.91 feet Y = -2846109.90 meter
Z = -8299418.23 Z = -2529662.68
XDOT = 794.954864 XDOT = 242.302243
YDOT = -16966.568591 feet/sec YDOT = -5171.410107 meter/sec
ZDOT = 17411.586358 ZDOT = 5307.051522
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 10146.64680877 .00020000 00000-0 20000-3 0 9023
2 36572 51.6450 341.0926 0017579 344.6561 15.4067 15.73979475 1897
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10146.64680877 = yrday.fracday
Element set: 902
Inclination: 51.6450 deg
RA of node: 341.0926 deg
Eccentricity: .0017579
Arg of perigee: 344.6561 deg
Mean anomaly: 15.4067 deg
Mean motion: 15.73979475 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 189
Checksum: 321
Coasting Arc #4 (Orbit 204)
Vector Time (GMT): 2010/147/15:25:10.509 Vector Time (MET): 012/21:05:01.554 Weight (LBS) : 219942.2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4150549.74 A = 6722138.59 meter
Y = -2288073.62 meter E = .0022289
Z = -4781846.83 I = 51.49224
XDOT = 5521.837894 Wp = 19.75566
YDOT = -4720.940980 meter/sec RA = 335.47069 deg
ZDOT = -2516.702975 TA = 225.42535
MA = 225.60750
Ha = 194.445 n.mi
Hp = 181.261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13617289.19 X = -4101425.91
Y = -7506803.22 feet Y = -2334212.12 meter
Z = -15688473.87 Z = -4801891.56
XDOT = 18116.266056 XDOT = 5586.443784
YDOT = -15488.651510 feet/sec YDOT = -4658.830874 meter/sec
ZDOT = -8256.899524 ZDOT = -2489.721283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -927861.25 X = -282812.11
Y = 15440560.24 feet Y = 4706282.76 meter
Z = -15768292.38 Z = -4806175.52
XDOT = -20690.334280 XDOT = -6306.413889
YDOT = -9623.103333 feet/sec YDOT = -2933.121896 meter/sec
ZDOT = -8149.412873 ZDOT = -2483.941044
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 10147.66264701 .00020000 00000-0 20000-3 0 9031
2 36572 51.6450 335.8768 0017669 348.4819 11.5937 15.74010473 2057
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10147.66264701 = yrday.fracday
Element set: 903
Inclination: 51.6450 deg
RA of node: 335.8768 deg
Eccentricity: .0017669
Arg of perigee: 348.4819 deg
Mean anomaly: 11.5937 deg
Mean motion: 15.74010473 rev/day Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 205
Checksum: 299
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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