[list_settings.list_name] Current STS TLEs @ 06:30 UTC
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2011/189/15:29:03.960 Area (sq ft) : 1208.48 Drag Coefficient (Cd) : 2.00 Monthly MSFC 50% solar flux (F10.7-jansky) : 99.0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1.52 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
There are no maneuvers.
Coasting Arc #1 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2011/201/13:47:30.000
Vector Time (MET): 011/22:18:26.040
Weight (LBS) : 235971.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6188636.73 A = 6759888.26 meter
Y = 1107909.15 meter E = .0016142
Z = 2454442.66 I = 51.60777
XDOT = -2957.673445 Wp = 37.78014
YDOT = 4679.621253 meter/sec RA = 352.13032 deg
ZDOT = 5339.155205 TA = 349.86491
MA = 349.89742
Ha = 207.962 n.mi
Hp = 200.281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20303926.28 X = 6163864.87
Y = 3634872.54 feet Y = 1176975.59 meter
Z = 8052633.39 Z = 2484446.48
XDOT = -9703.653035 XDOT = -3035.718295
YDOT = 15353.088100 feet/sec YDOT = 4646.110034 meter/sec
ZDOT = 17516.913403 ZDOT = 5324.597784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14270989.24 X = -4349797.52
Y = -14826469.26 feet Y = -4519107.83 meter
Z = 8174429.68 Z = 2491566.17
XDOT = 15869.728234 XDOT = 4837.093166
YDOT = -5639.460392 feet/sec YDOT = -1718.907527 meter/sec
ZDOT = 17457.484437 ZDOT = 5321.041257
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 37736U 11031A 11201.63359910 .00020000 00000-0 20000-3 0 9002
2 37736 51.6418 352.3287 0009792 340.2714 19.8063 15.63387558 1897
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11201.63359910 = yrday.fracday
Element set: 900
Inclination: 51.6418 deg
RA of node: 352.3287 deg
Eccentricity: .0009792
Arg of perigee: 340.2714 deg
Mean anomaly: 19.8063 deg
Mean motion: 15.63387558 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 189
Checksum: 305
Coasting Arc #2 (Orbit 203)
---------------------------------------
Vector Time (GMT): 2011/202/13:49:23.897
Vector Time (MET): 012/22:20:19.937
Weight (LBS) : 235971.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1301901.46 A = 6750567.95 meter
Y = -4007171.48 meter E = .0015874
Z = -5285175.85 I = 51.54645
XDOT = 7410.736233 Wp = 49.69455
YDOT = -1968.261556 meter/sec RA = 347.04735 deg
ZDOT = -323.751125 TA = 217.16249
MA = 217.27247
Ha = 208.238 n.mi
Hp = 199.990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4271330.24 X = -1231321.62
Y = -13146888.07 feet Y = -4021335.15 meter
Z = -17339815.77 Z = -5291329.24
XDOT = 24313.439084 XDOT = 7433.767636
YDOT = -6457.551036 feet/sec YDOT = -1885.261392 meter/sec
ZDOT = -1062.175606 ZDOT = -287.694408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4003045.20 X = -1220128.18
Y = 13198565.38 feet Y = 4022922.73 meter
Z = -17364551.25 Z = -5292715.22
XDOT = -22743.691706 XDOT = -6932.277232
YDOT = -8143.246029 feet/sec YDOT = -2482.061390 meter/sec
ZDOT = -915.603375 ZDOT = -279.075909
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 37736U 11031A 11202.59242903 .00020000 00000-0 20000-3 0 9012
2 37736 51.6418 347.4833 0009983 344.2201 15.8644 15.63383039 2045
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11202.59242903 = yrday.fracday
Element set: 901
Inclination: 51.6418 deg
RA of node: 347.4833 deg
Eccentricity: .0009983
Arg of perigee: 344.2201 deg
Mean anomaly: 15.8644 deg
Mean motion: 15.63383039 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 204
Checksum: 283
Coasting Arc #3 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2011/203/13:50:54.831
Vector Time (MET): 013/22:21:50.870
Weight (LBS) : 235971.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4514273.24 A = 6758717.09 meter
Y = 4008946.05 meter E = .0013739
Z = 3038744.63 I = 51.54419
XDOT = -5410.271587 Wp = 53.04666
YDOT = -2345.929918 meter/sec RA = 341.95398 deg
ZDOT = -4918.959642 TA = 91.91554
MA = 91.75818
Ha = 208.427 n.mi
Hp = 199.890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14810607.76 X = -4573528.07
Y = 13152710.15 feet Y = 3958133.16 meter
Z = 9969634.62 Z = 3016670.88
XDOT = -17750.234867 XDOT = -5359.741663
YDOT = -7696.620466 feet/sec YDOT = -2406.147971 meter/sec
ZDOT = -16138.319035 ZDOT = -4945.119922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19639705.77 X = 5986182.32
Y = -2900765.32 feet Y = -884153.27 meter
Z = 9879727.67 Z = 3011340.99
XDOT = 10375.304939 XDOT = 3162.392945
YDOT = 14654.866063 feet/sec YDOT = 4466.803176 meter/sec
ZDOT = -16244.415890 ZDOT = -4951.297963
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 37736U 11031A 11203.61517193 .00020000 00000-0 20000-3 0 9023
2 37736 51.6419 342.3133 0009909 348.1656 11.9267 15.63369760 2209
Satellite: SHUTTLE
Catalog Number: 37736
Epoch time: 11203.61517193 = yrday.fracday
Element set: 902
Inclination: 51.6419 deg
RA of node: 342.3133 deg
Eccentricity: .0009909
Arg of perigee: 348.1656 deg
Mean anomaly: 11.9267 deg
Mean motion: 15.63369760 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 220
Checksum: 288
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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