SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 6944 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 16339
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 (begining on orbit 675)
---------------------------------------
Vector Time (GMT): 2006/254/08:41:24
000
Vector Time (MET): 001/17:26:29
028
Weight (LBS) : 429540
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 146955
96 A = 6725910
99 meter
Y = -6518707
59 meter E =
0007457
Z = 1654081
78 I = 51
95600
XDOT = 4925
547504 Wp = 60
43696
YDOT = -1355
663030 meter/sec RA = 102
74128 deg
ZDOT = -5757
364367 TA = 101
36953
MA = 101
28574
Ha = 188
932 n
mi
Hp = 181
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 482138
96 X = 211880
47
Y = -21386835
94 feet Y = -6516699
11 meter
Z = 5426777
49 Z = 1654953
39
XDOT = 16159
932755 XDOT = 4968
324587
YDOT = -4447
713354 feet/sec YDOT = -1300
284702 meter/sec
ZDOT = -18888
990704 ZDOT = -5733
331963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18773535
72 X = -5722173
69
Y = 10254673
48 feet Y = 3125624
48 meter
Z = 5429102
32 Z = 1654790
39
XDOT = -11205
915923 XDOT = -3415
563173
YDOT = -10522
200705 feet/sec YDOT = -3207
166775 meter/sec
ZDOT = -18799
688220 ZDOT = -5730
144969
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 29391U 06036A 06254
39703308
00014500 00000-0 95600-4 0 9005
2 29391 51
6315 103
3573 0011697 328
2032 31
8425 15
75783339 6766
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06254
39703308 = yrday
fracday
Element set: 900
Inclination: 51
6315 deg
RA of node: 103
3573 deg
Eccentricity:
0011697
Arg of perigee: 328
2032 deg
Mean anomaly: 31
8425 deg
Mean motion: 15
75783339 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 676
Checksum: 299
Coasting Arc #2 (begining on orbit 691)
---------------------------------------
Vector Time (GMT): 2006/255/08:46:13
619
Vector Time (MET): 002/17:31:18
647
Weight (LBS) : 429540
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3951882
10 A = 6714986
26 meter
Y = -1428312
28 meter E =
0012389
Z = 5241547
10 I = 51
92551
XDOT = 1630
374212 Wp = 346
47491
YDOT = -7484
037536 meter/sec RA = 97
60385 deg
ZDOT = -798
751867 TA = 111
16236
MA = 111
02992
Ha = 189
084 n
mi
Hp = 181
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12965492
47 X = -3961061
95
Y = -4686063
92 feet Y = -1472603
02 meter
Z = 17196676
84 Z = 5222326
38
XDOT = 5348
996760 XDOT = 1717
909743
YDOT = -24553
928925 feet/sec YDOT = -7465
296386 meter/sec
ZDOT = -2620
576993 ZDOT = -790
619027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2958845
88 X = 901856
22
Y = 13556252
98 feet Y = 4131945
91 meter
Z = 17124897
68 Z = 5219668
81
XDOT = -22668
852970 XDOT = -6909
466385
YDOT = 8268
780547 feet/sec YDOT = 2520
324311 meter/sec
ZDOT = -2591
335256 ZDOT = -789
838986
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 29391U 06036A 06255
41169131
00014500 00000-0 95600-4 0 9010
2 29391 51
6321 98
1309 0011920 331
6044 28
4469 15
75869666 6927
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06255
41169131 = yrday
fracday
Element set: 901
Inclination: 51
6321 deg
RA of node: 98
1309 deg
Eccentricity:
0011920
Arg of perigee: 331
6044 deg
Mean anomaly: 28
4469 deg
Mean motion: 15
75869666 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 692
Checksum: 305
SPACE SHUTTLE ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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