SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 1208 48 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 (Orbit 159)
---------------------------------------
Vector Time (GMT): 2006/262/15:51:02
000
Vector Time (MET): 010/00:36:07
028
Weight (LBS) : 209385
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4462720
39 A = 6716228
84 meter
Y = 127147
12 meter E =
0016238
Z = 5017178
92 I = 51
89142
XDOT = -2350
029983 Wp = 19
61642
YDOT = -7088
295890 meter/sec RA = 60
18372 deg
ZDOT = -1893
948820 TA = 88
68250
MA = 88
49648
Ha = 190
518 n
mi
Hp = 179
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14641471
10 X = -4488183
78
Y = 417149
35 feet Y = 77046
92 meter
Z = 16460560
75 Z = 4995437
33
XDOT = -7710
072124 XDOT = -2261
307870
YDOT = -23255
563942 feet/sec YDOT = -7114
106666 meter/sec
ZDOT = -6213
742847 ZDOT = -1905
149530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8012921
71 X = 2442338
54
Y = -12369286
00 feet Y = -3770158
37 meter
Z = 16379578
74 Z = 4992495
60
XDOT = 22604
250892 XDOT = 6889
775672
YDOT = 6285
260330 feet/sec YDOT = 1915
747349 meter/sec
ZDOT = -6256
439708 ZDOT = -1906
962823
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 06262
70479657
00014500 00000-0 95600-4 0 9006
2 29391 51
6341 60
5728 0012064 3
9860 356
1398 15
75785650 1604
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06262
70479657 = yrday
fracday
Element set: 900
Inclination: 51
6341 deg
RA of node: 60
5728 deg
Eccentricity:
0012064
Arg of perigee: 3
9860 deg
Mean anomaly: 356
1398 deg
Mean motion: 15
75785650 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 160
Checksum: 308
Coasting Arc #2 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2006/263/15:51:15
107
Vector Time (MET): 011/00:36:20
136
Weight (LBS) : 209385
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2002345
90 A = 6724821
02 meter
Y = 5986848
41 meter E =
0022048
Z = 2276189
56 I = 51
90540
XDOT = -5426
724451 Wp = 42
63466
YDOT = -273
004532 meter/sec RA = 55
08778 deg
ZDOT = 5477
186261 TA = 342
89612
MA = 342
97031
Ha = 190
552 n
mi
Hp = 179
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6569376
30 X = 1924122
45
Y = 19641891
12 feet Y = 6008825
86 meter
Z = 7467813
53 Z = 2285726
70
XDOT = -17804
214078 XDOT = -5449
871450
YDOT = -895
684159 feet/sec YDOT = -333
883190 meter/sec
ZDOT = 17969
771198 ZDOT = 5450
767127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19980580
70 X = -6090081
00
Y = -5403033
74 feet Y = -1646844
68 meter
Z = 7504162
33 Z = 2287268
68
XDOT = 10238
535461 XDOT = 3120
705609
YDOT = -12974
575503 feet/sec YDOT = -3954
650613 meter/sec
ZDOT = 17871
308862 ZDOT = 5447
174941
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 06263
71948471
00014500 00000-0 95600-4 0 9014
2 29391 51
6342 55
3474 0012064 8
0320 352
1035 15
75786584 1760
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06263
71948471 = yrday
fracday
Element set: 901
Inclination: 51
6342 deg
RA of node: 55
3474 deg
Eccentricity:
0012064
Arg of perigee: 8
0320 deg
Mean anomaly: 352
1035 deg
Mean motion: 15
75786584 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 176
Checksum: 292
Coasting Arc #3 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2006/264/15:51:17
002
Vector Time (MET): 012/00:36:22
030
Weight (LBS) : 209385
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4993294
96 A = 6718355
36 meter
Y = 477583
78 meter E =
0014209
Z = -4474467
01 I = 51
86654
XDOT = 2250
435320 Wp = 53
10180
YDOT = 6614
749440 meter/sec RA = 49
91274 deg
ZDOT = 3232
766542 TA = 249
08783
MA = 249
23999
Ha = 190
678 n
mi
Hp = 178
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16382201
32 X = 5009313
25
Y = 1566875
92 feet Y = 533570
52 meter
Z = -14680009
87 Z = -4450170
68
XDOT = 7383
317980 XDOT = 2160
517714
YDOT = 21701
933859 feet/sec YDOT = 6639
438725 meter/sec
ZDOT = 10606
189441 ZDOT = 3243
480450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10172334
04 X = -3100527
42
Y = 13038652
35 feet Y = 3974181
24 meter
Z = -14589430
24 Z = -4446858
34
XDOT = -21285
710504 XDOT = -6487
884562
YDOT = -4749
825878 feet/sec YDOT = -1447
746928 meter/sec
ZDOT = 10647
006306 ZDOT = 3245
207522
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 06264
67074616
00014500 00000-0 95600-4 0 9022
2 29391 51
6342 50
4495 0012109 11
5375 348
6064 15
75829577 1917
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06264
67074616 = yrday
fracday
Element set: 902
Inclination: 51
6342 deg
RA of node: 50
4495 deg
Eccentricity:
0012109
Arg of perigee: 11
5375 deg
Mean anomaly: 348
6064 deg
Mean motion: 15
75829577 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 191
Checksum: 307
Coasting Arc #4 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2006/265/15:55:59
837
Vector Time (MET): 013/00:41:04
865
Weight (LBS) : 209385
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -79053
15 A = 6718314
57 meter
Y = -5029980
21 meter E =
0019453
Z = -4471554
93 I = 51
84679
XDOT = 6399
266532 Wp = 38
50190
YDOT = 2778
606475 meter/sec RA = 44
80901 deg
ZDOT = -3231
342848 TA = 199
15378
MA = 199
22702
Ha = 190
719 n
mi
Hp = 178
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -259360
72 X = -1019
28
Y = -16502559
75 feet Y = -5030428
62 meter
Z = -14670455
80 Z = -4471749
18
XDOT = 20994
968937 XDOT = 6383
383574
YDOT = 9116
162975 feet/sec YDOT = 2850
153803 meter/sec
ZDOT = -10601
518530 ZDOT = -3200
293759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14330203
71 X = 4367846
09
Y = 8185700
11 feet Y = 2495001
39 meter
Z = -14671864
07 Z = -4471984
17
XDOT = -17909
062544 XDOT = -5458
682263
YDOT = 12514
861636 feet/sec YDOT = 3814
529827 meter/sec
ZDOT = -10485
472327 ZDOT = -3195
971965
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 06265
68540561
00014500 00000-0 95600-4 0 9032
2 29391 51
6339 45
2238 0012148 14
8377 345
3141 15
75822230 2078
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06265
68540561 = yrday
fracday
Element set: 903
Inclination: 51
6339 deg
RA of node: 45
2238 deg
Eccentricity:
0012148
Arg of perigee: 14
8377 deg
Mean anomaly: 345
3141 deg
Mean motion: 15
75822230 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 207
Checksum: 288
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]
If you're still having trouble, please contact the list owner at:
<mailto:list
admin@aus-city
com>
The following physical address is associated with this mailing list:
http://www aus-city com
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
Shuttle TLE list
Privacy Policy:
Private list