[list_settings.list_name] Current STS TLEs @ 06:30 UTC
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2011/055/21:53:23 980 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 92 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
067/20:00:08
373 16
4 -26
0 26
0
011/22:06:44
393 5
6 0
0 192
1
000/00:00:16
785 19
4 -0
0 171
7
068/15:53:19
622 18
8 -263
4 277
2
012/17:59:55
642 205
1 0
1 193
4
000/00:02:31
283 185
4 -86
2 23
3
Coasting Arc #1 (Orbit 187)
---------------------------------------
Vector Time (GMT): 2011/067/16:23:01
000
Vector Time (MET): 011/18:29:37
020
Weight (LBS) : 213380
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5628087
75 A = 6732013
70 meter
Y = -2708836
94 meter E =
0021822
Z = 2477346
55 I = 51
41093
XDOT = 337
257421 Wp = 59
09133
YDOT = 5578
530805 meter/sec RA = 315
84687 deg
ZDOT = 5310
194406 TA = 329
05221
MA = 329
18063
Ha = 194
326 n
mi
Hp = 182
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18464854
84 X = 5645925
78
Y = -8887260
31 feet Y = -2645800
27 meter
Z = 8127777
38 Z = 2504731
17
XDOT = 1106
487603 XDOT = 249
056407
YDOT = 18302
266422 feet/sec YDOT = 5581
809586 meter/sec
ZDOT = 17421
897658 ZDOT = 5311
618002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4684919
71 X = 1427963
53
Y = -19904166
65 feet Y = -6066790
00 meter
Z = 8238367
70 Z = 2511054
47
XDOT = 13402
407592 XDOT = 4085
053834
YDOT = 10399
220354 feet/sec YDOT = 3169
682364 meter/sec
ZDOT = 17427
486793 ZDOT = 5311
897974
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 37371U 11008A 11067
74116671
00020000 00000-0 20000-3 0 9008
2 37371 51
6372 316
1123 0009402 35
1143 325
0637 15
73098049 1885
Satellite: SHUTTLE
Catalog Number: 37371
Epoch time: 11067
74116671 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 316
1123 deg
Eccentricity:
0009402
Arg of perigee: 35
1143 deg
Mean anomaly: 325
0637 deg
Mean motion: 15
73098049 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 188
Checksum: 265
Coasting Arc #2 (Orbit 189)
---------------------------------------
Vector Time (GMT): 2011/067/20:00:16
765
Vector Time (MET): 011/22:06:52
785
Weight (LBS) : 212835
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3719714
94 A = 6719995
62 meter
Y = 5405651
96 meter E =
0023539
Z = 1498907
54 I = 51
41590
XDOT = -4805
665749 Wp = 30
11914
YDOT = -1693
652339 meter/sec RA = 315
03324 deg
ZDOT = -5758
625461 TA = 133
32888
MA = 133
13242
Ha = 192
115 n
mi
Hp = 171
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12203789
16 X = -3787166
87
Y = 17735078
62 feet Y = 5363678
86 meter
Z = 4917675
66 Z = 1480672
95
XDOT = -15766
619912 XDOT = -4758
395692
YDOT = -5556
602162 feet/sec YDOT = -1747
128458 meter/sec
ZDOT = -18893
128153 ZDOT = -5781
856219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20354324
60 X = 6203998
14
Y = 7063056
28 feet Y = 2152819
55 meter
Z = 4843936
80 Z = 1476431
94
XDOT = -668
825637 XDOT = -203
858054
YDOT = 15084
115733 feet/sec YDOT = 4597
638475 meter/sec
ZDOT = -18986
831474 ZDOT = -5787
186233
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 37371U 11008A 11067
86810177
00020000 00000-0 20000-3 0 9014
2 37371 51
6396 315
4587 0027022 359
1711
9405 15
77952449 1907
Satellite: SHUTTLE
Catalog Number: 37371
Epoch time: 11067
86810177 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 315
4587 deg
Eccentricity:
0027022
Arg of perigee: 359
1711 deg
Mean anomaly:
9405 deg
Mean motion: 15
77952449 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 190
Checksum: 293
Coasting Arc #3 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2011/068/15:54:35
264
Vector Time (MET): 012/18:01:11
283
Weight (LBS) : 207108
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5162469
26 A = 6583488
99 meter
Y = 4014575
22 meter E =
0232056
Z = -1613985
25 I = 51
39572
XDOT = -1906
498476 Wp = 21
50988
YDOT = -4707
039502 meter/sec RA = 310
76544 deg
ZDOT = -5658
091701 TA = 176
34521
MA = 176
17271
Ha = 193
353 n
mi
Hp = 23
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16937235
10 X = -5199136
91
Y = 13171178
55 feet Y = 3956640
21 meter
Z = -5295227
21 Z = -1639153
76
XDOT = -6254
916260 XDOT = -1826
235961
YDOT = -15443
042986 feet/sec YDOT = -4727
910825 meter/sec
ZDOT = -18563
292983 ZDOT = -5667
158059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2694884
14 X = -821400
69
Y = 21260298
69 feet Y = 6480139
04 meter
Z = -5396907
18 Z = -1644977
31
XDOT = -13697
559015 XDOT = -4175
015988
YDOT = -6418
522072 feet/sec YDOT = -1956
365528 meter/sec
ZDOT = -18599
750442 ZDOT = -5669
203935
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 37371U 11008A 11068
68994189
00020000 00000-0 20000-3 0 9022
2 37371 51
6369 311
1960 0029430 200
2406 159
7662 17
03035670 2028
Satellite: SHUTTLE
Catalog Number: 37371
Epoch time: 11068
68994189 = yrday
fracday
Element set: 902
Inclination: 51
6369 deg
RA of node: 311
1960 deg
Eccentricity:
0029430
Arg of perigee: 200
2406 deg
Mean anomaly: 159
7662 deg
Mean motion: 17
03035670 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 202
Checksum: 282
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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