SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/039/09:14:06 981 Area (sq ft) : 5166 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 07 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 07803
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 35)
---------------------------------------
Vector Time (GMT): 2010/041/13:00:12
000
Vector Time (MET): 002/03:46:05
019
Weight (LBS) : 245806
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1859756
17 A = 6717772
72 meter
Y = -4540702
17 meter E =
0010576
Z = 4594267
77 I = 51
74906
XDOT = 7100
261372 Wp = 353
91950
YDOT = -109
439713 meter/sec RA = 159
84677 deg
ZDOT = -2972
650433 TA = 125
58330
MA = 125
48469
Ha = 187
717 n
mi
Hp = 182
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6101562
23 X = 1888101
12
Y = -14897316
82 feet Y = -4519736
35 meter
Z = 15073057
00 Z = 4603370
84
XDOT = 23294
820773 XDOT = 7115
397794
YDOT = -359
054177 feet/sec YDOT = -29
915172 meter/sec
ZDOT = -9752
790136 ZDOT = -2938
121597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11787784
31 X = 3592916
66
Y = -10914320
26 feet Y = -3326684
81 meter
Z = 15109001
02 Z = 4605223
51
XDOT = 20482
539081 XDOT = 6243
077912
YDOT = 8766
433992 feet/sec YDOT = 2672
009081 meter/sec
ZDOT = -9615
771676 ZDOT = -2930
887207
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 36394U 10004A 10041
58425871
00020000 00000-0 20000-3 0 9005
2 36394 51
6458 160
6703 0011114 308
6617 51
3552 15
75820593 363
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041
58425871 = yrday
fracday
Element set: 900
Inclination: 51
6458 deg
RA of node: 160
6703 deg
Eccentricity:
0011114
Arg of perigee: 308
6617 deg
Mean anomaly: 51
3552 deg
Mean motion: 15
75820593 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 36
Checksum: 275
Coasting Arc #2 (Orbit 51)
---------------------------------------
Vector Time (GMT): 2010/042/13:05:13
979
Vector Time (MET): 003/03:51:06
998
Weight (LBS) : 245391
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4857028
02 A = 6718599
14 meter
Y = -1523394
54 meter E =
0004331
Z = 4381956
00 I = 51
78058
XDOT = 4650
752430 Wp = 8
96697
YDOT = -5133
043809 meter/sec RA = 154
73520 deg
ZDOT = 3374
204698 TA = 47
17333
MA = 47
13694
Ha = 187
972 n
mi
Hp = 182
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15935131
29 X = -4860909
28
Y = -4998013
58 feet Y = -1577758
18 meter
Z = 14376496
07 Z = 4358351
82
XDOT = 15258
374115 XDOT = 4691
443518
YDOT = -16840
694911 feet/sec YDOT = -5080
782355 meter/sec
ZDOT = 11070
225386 ZDOT = 3396
896028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12797772
26 X = -3900760
98
Y = -10854129
98 feet Y = -3308338
82 meter
Z = 14282754
49 Z = 4353383
57
XDOT = 19769
775219 XDOT = 6025
827487
YDOT = -8640
886744 feet/sec YDOT = -2633
742280 meter/sec
ZDOT = 11160
077828 ZDOT = 3401
591722
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 36394U 10004A 10042
59890821
00020000 00000-0 20000-3 0 9019
2 36394 51
6463 155
4458 0011195 312
2464 47
7750 15
75868854 527
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10042
59890821 = yrday
fracday
Element set: 901
Inclination: 51
6463 deg
RA of node: 155
4458 deg
Eccentricity:
0011195
Arg of perigee: 312
2464 deg
Mean anomaly: 47
7750 deg
Mean motion: 15
75868854 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 52
Checksum: 303
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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