SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/134/18:20:08 955 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 80 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 80 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 71)
---------------------------------------
Vector Time (GMT): 2010/139/04:16:12
000
Vector Time (MET): 004/09:56:03
045
Weight (LBS) : 215706
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4920288
43 A = 6724278
45 meter
Y = 1822266
66 meter E =
0012475
Z = 4208917
03 I = 51
74923
XDOT = -4875
787647 Wp = 22
23585
YDOT = -4708
471164 meter/sec RA = 18
90489 deg
ZDOT = -3646
489007 TA = 104
93925
MA = 104
80110
Ha = 191
181 n
mi
Hp = 184
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16142678
59 X = -4960745
83
Y = 5978565
17 feet Y = 1767018
39 meter
Z = 13808782
90 Z = 4184916
18
XDOT = -15996
678632 XDOT = -4805
060297
YDOT = -15447
740040 feet/sec YDOT = -4762
599260 meter/sec
ZDOT = -11963
546610 ZDOT = -3670
004331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13291524
42 X = -4051256
64
Y = -11058750
15 feet Y = -3370707
05 meter
Z = 13713176
96 Z = 4179776
34
XDOT = 4605
853289 XDOT = 1403
864082
YDOT = -20547
829116 feet/sec YDOT = -6262
978315 meter/sec
ZDOT = -12057
205567 ZDOT = -3675
036257
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 36572U 10019A 10139
21893392
00020000 00000-0 20000-3 0 9004
2 36572 51
6441 19
2404 0010105 330
1112 29
9473 15
74109741 726
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10139
21893392 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 19
2404 deg
Eccentricity:
0010105
Arg of perigee: 330
1112 deg
Mean anomaly: 29
9473 deg
Mean motion: 15
74109741 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 72
Checksum: 251
Coasting Arc #2 (Orbit 87)
---------------------------------------
Vector Time (GMT): 2010/140/04:17:08
652
Vector Time (MET): 005/09:56:59
697
Weight (LBS) : 215706
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4236414
69 A = 6726398
70 meter
Y = 3876471
82 meter E =
0011448
Z = 3488074
51 I = 51
72777
XDOT = -5804
392902 Wp = 41
64697
YDOT = 2259
398061 meter/sec RA = 13
82361 deg
ZDOT = 4538
625833 TA = 359
75096
MA = 359
75153
Ha = 191
162 n
mi
Hp = 184
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13898998
32 X = 4175807
98
Y = 12718083
41 feet Y = 3923506
76 meter
Z = 11443814
00 Z = 3508508
14
XDOT = -19043
283798 XDOT = -5851
274331
YDOT = 7412
723297 feet/sec YDOT = 2194
227359 meter/sec
ZDOT = 14890
504700 ZDOT = 4510
314401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3703960
41 X = -1128967
13
Y = 18421268
28 feet Y = 5614802
57 meter
Z = 11525199
81 Z = 3512880
90
XDOT = -14914
669484 XDOT = -4545
991259
YDOT = -12244
671708 feet/sec YDOT = -3732
175937 meter/sec
ZDOT = 14777
727925 ZDOT = 4504
251471
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 36572U 10019A 10140
23469744
00020000 00000-0 20000-3 0 9019
2 36572 51
6439 14
0238 0010112 333
3225 26
7417 15
74142875 884
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10140
23469744 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 14
0238 deg
Eccentricity:
0010112
Arg of perigee: 333
3225 deg
Mean anomaly: 26
7417 deg
Mean motion: 15
74142875 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 88
Checksum: 264
Coasting Arc #3 (Orbit 102)
---------------------------------------
Vector Time (GMT): 2010/141/04:17:55
554
Vector Time (MET): 006/09:57:46
599
Weight (LBS) : 215706
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5145918
59 A = 6725876
48 meter
Y = -2196111
39 meter E =
0008465
Z = -3727255
83 I = 51
69581
XDOT = 4868
122188 Wp = 12
18440
YDOT = 4159
180532 meter/sec RA = 8
63776 deg
ZDOT = 4280
289700 TA = 302
86381
MA = 302
94526
Ha = 191
557 n
mi
Hp = 183
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16882935
01 X = 5188199
83
Y = -7205089
86 feet Y = -2138330
01 meter
Z = -12228529
64 Z = -3702154
34
XDOT = 15971
529488 XDOT = 4800
458742
YDOT = 13645
605419 feet/sec YDOT = 4213
240162 meter/sec
ZDOT = 14042
945209 ZDOT = 4303
775023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15170859
86 X = 4624078
09
Y = 10451183
81 feet Y = 3185520
83 meter
Z = -12128541
53 Z = -3696779
46
XDOT = -2241
623463 XDOT = -683
246831
YDOT = 19621
337534 feet/sec YDOT = 5980
583680 meter/sec
ZDOT = 14136
484580 ZDOT = 4308
800500
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 36572U 10019A 10141
18696162
00020000 00000-0 20000-3 0 9021
2 36572 51
6438 9
1328 0010218 337
8531 22
2189 15
74121873 1034
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10141
18696162 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 9
1328 deg
Eccentricity:
0010218
Arg of perigee: 337
8531 deg
Mean anomaly: 22
2189 deg
Mean motion: 15
74121873 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 103
Checksum: 266
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