SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/095/10:21:24 956 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 05 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 69)
---------------------------------------
Vector Time (GMT): 2010/099/18:07:30
000
Vector Time (MET): 004/07:46:05
044
Weight (LBS) : 215029
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5583350
00 A = 6724850
36 meter
Y = 1056924
18 meter E =
0014483
Z = 3580889
12 I = 51
42400
XDOT = 1677
342031 Wp = 104
09271
YDOT = 6099
648369 meter/sec RA = 220
89258 deg
ZDOT = -4404
314466 TA = 32
91123
MA = 32
82114
Ha = 190
321 n
mi
Hp = 181
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18318077
44 X = 5553721
07
Y = 3467599
01 feet Y = 1119195
10 meter
Z = 11748323
88 Z = 3607940
89
XDOT = 5503
090652 XDOT = 1630
405292
YDOT = 20011
969713 feet/sec YDOT = 6118
142664 meter/sec
ZDOT = -14449
850609 ZDOT = -4396
280398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2655196
53 X = -809303
90
Y = -18384441
53 feet Y = -5603577
78 meter
Z = 11855866
02 Z = 3613667
96
XDOT = 15765
946025 XDOT = 4805
460348
YDOT = -11598
610553 feet/sec YDOT = -3535
256497 meter/sec
ZDOT = -14417
697529 ZDOT = -4394
514207
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 36507U 10012 10099
79461532
00020000 00000-0 20000-3 0 9000
2 36507 51
6451 221
6894 0004829 154
4236 205
7167 15
74575655 700
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10099
79461532 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 221
6894 deg
Eccentricity:
0004829
Arg of perigee: 154
4236 deg
Mean anomaly: 205
7167 deg
Mean motion: 15
74575655 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 70
Checksum: 298
Coasting Arc #2 (Orbit 85)
---------------------------------------
Vector Time (GMT): 2010/100/18:07:42
352
Vector Time (MET): 005/07:46:17
395
Weight (LBS) : 215029
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1631587
28 A = 6723459
09 meter
Y = -5129370
98 meter E =
0014181
Z = 4023107
83 I = 51
44285
XDOT = 6593
147180 Wp = 118
53204
YDOT = 951
038051 meter/sec RA = 215
78882 deg
ZDOT = 3869
451517 TA = 291
42731
MA = 291
57852
Ha = 190
380 n
mi
Hp = 182
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5352976
64 X = -1593652
00
Y = -16828644
94 feet Y = -5147403
94 meter
Z = 13199172
68 Z = 4015274
13
XDOT = 21631
060303 XDOT = 6563
225389
YDOT = 3120
203579 feet/sec YDOT = 1024
599546 meter/sec
ZDOT = 12695
050909 ZDOT = 3901
408262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13953169
17 X = -4252925
96
Y = 10862445
34 feet Y = 3310873
34 meter
Z = 13167845
70 Z = 4013559
37
XDOT = -3653
857807 XDOT = -1113
695860
YDOT = -20304
578608 feet/sec YDOT = -6188
835560 meter/sec
ZDOT = 12822
088993 ZDOT = 3908
172725
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 36507U 10012 10100
81007214
00020000 00000-0 20000-3 0 9010
2 36507 51
6450 216
4702 0004802 156
7301 203
4081 15
74601107 867
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10100
81007214 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 216
4702 deg
Eccentricity:
0004802
Arg of perigee: 156
7301 deg
Mean anomaly: 203
4081 deg
Mean motion: 15
74601107 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 86
Checksum: 225
Coasting Arc #3 (Orbit 100)
---------------------------------------
Vector Time (GMT): 2010/101/18:08:26
642
Vector Time (MET): 006/07:47:01
686
Weight (LBS) : 215029
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5982538
93 A = 6726252
21 meter
Y = -777283
49 meter E =
0006586
Z = -2983314
44 I = 51
47998
XDOT = -1741
569766 Wp = 117
52274
YDOT = -5616
540722 meter/sec RA = 210
58366 deg
ZDOT = 4961
144425 TA = 207
96622
MA = 208
00162
Ha = 190
115 n
mi
Hp = 181
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19627752
41 X = -5958910
11
Y = -2550142
70 feet Y = -844051
93 meter
Z = -9787777
03 Z = -3012320
27
XDOT = -5713
811568 XDOT = -1702
735608
YDOT = -18426
970872 feet/sec YDOT = -5635
798454 meter/sec
ZDOT = 16276
720553 ZDOT = 4952
778631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4694457
26 X = 1430870
57
Y = 19168813
35 feet Y = 5842654
31 meter
Z = -9903087
26 Z = -3018461
00
XDOT = -13683
797662 XDOT = -4170
821527
YDOT = 11733
859058 feet/sec YDOT = 3576
480241 meter/sec
ZDOT = 16243
255676 ZDOT = 4950
944330
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 36507U 10012 10101
76202645
00020000 00000-0 20000-3 0 9021
2 36507 51
6463 211
5779 0004724 160
5518 199
5826 15
74688816 1019
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10101
76202645 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 211
5779 deg
Eccentricity:
0004724
Arg of perigee: 160
5518 deg
Mean anomaly: 199
5826 deg
Mean motion: 15
74688816 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 101
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
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:
https://aus-city com/cgi-bin/dada/mail cgi/u/STSTLE_LIST/example/example com/
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:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- 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