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
143/14:34:09
230 0
1 -0
1 0
1
008/20:14:00
275 0
0 0
1 191
4
000/00:00:00
549 -0
1 0
0 183
1
143/16:37:14
664 -2
9 -0
0 3
0
008/22:17:05
709 0
6 -0
0 191
7
000/00:00:11
418 0
5 -3
0 182
8
143/17:05:11
809 1
5 1
5 1
5
008/22:45:02
854 0
0 0
0 192
0
000/00:00:05
707 0
2 -0
0 183
4
Coasting Arc #1 (Orbit 108)
---------------------------------------
Vector Time (GMT): 2010/141/12:58:46
000
Vector Time (MET): 006/18:38:37
045
Weight (LBS) : 214935
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5774800
18 A = 6729292
18 meter
Y = -2551967
88 meter E =
0005726
Z = -2338673
68 I = 51
69974
XDOT = 3890
731064 Wp =
94588
YDOT = -3839
109013 meter/sec RA = 6
83100 deg
ZDOT = -5412
563739 TA = 205
32530
MA = 205
35337
Ha = 191
485 n
mi
Hp = 183
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18946194
83 X = -5734473
52
Y = -8372598
04 feet Y = -2616319
52 meter
Z = -7672813
92 Z = -2366629
98
XDOT = 12764
865694 XDOT = 3959
664863
YDOT = -12595
502012 feet/sec YDOT = -3795
214779 meter/sec
ZDOT = -17757
755048 ZDOT = -5393
495286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13538649
53 X = -4126580
38
Y = 15621860
83 feet Y = 4761543
18 meter
Z = -7784163
60 Z = -2372613
07
XDOT = -7138
034734 XDOT = -2175
672987
YDOT = -15005
507352 feet/sec YDOT = -4573
678641 meter/sec
ZDOT = -17681
795678 ZDOT = -5389
411323
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
56785464
00020000 00000-0 20000-3 0 9005
2 36572 51
6465 7
1796 0010406 338
0113 22
0602 15
74153809 1097
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10141
56785464 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 7
1796 deg
Eccentricity:
0010406
Arg of perigee: 338
0113 deg
Mean anomaly: 22
0602 deg
Mean motion: 15
74153809 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 109
Checksum: 263
Coasting Arc #2 (Orbit 124)
---------------------------------------
Vector Time (GMT): 2010/142/12:59:42
893
Vector Time (MET): 007/18:39:33
938
Weight (LBS) : 214758
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3567383
81 A = 6722768
58 meter
Y = 3474501
61 meter E =
0014217
Z = 4519197
19 I = 51
64809
XDOT = -6528
782610 Wp = 19
31249
YDOT = -2645
037419 meter/sec RA = 1
64868 deg
ZDOT = -3104
180496 TA = 101
71205
MA = 101
55249
Ha = 191
589 n
mi
Hp = 183
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11704015
13 X = -3627924
81
Y = 11399283
48 feet Y = 3434270
24 meter
Z = 14826762
44 Z = 4501719
83
XDOT = -21419
890452 XDOT = -6483
640409
YDOT = -8677
944287 feet/sec YDOT = -2717
793577 meter/sec
ZDOT = -10184
319214 ZDOT = -3135
788096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7759129
91 X = 2364982
80
Y = 14449330
03 feet Y = 4404155
79 meter
Z = 14757143
46 Z = 4497977
33
XDOT = -13111
661159 XDOT = -3996
434321
YDOT = 17624
358715 feet/sec YDOT = 5371
904536 meter/sec
ZDOT = -10310
206749 ZDOT = -3142
551017
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 10142
58357100
00020000 00000-0 20000-3 0 9011
2 36572 51
6467 1
9616 0010481 341
4316 18
6463 15
74217353 1257
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10142
58357100 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 1
9616 deg
Eccentricity:
0010481
Arg of perigee: 341
4316 deg
Mean anomaly: 18
6463 deg
Mean motion: 15
74217353 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 125
Checksum: 259
Coasting Arc #3 (Orbit 140)
---------------------------------------
Vector Time (GMT): 2010/143/13:00:38
620
Vector Time (MET): 008/18:40:29
665
Weight (LBS) : 214758
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5602644
75 A = 6727320
15 meter
Y = 2089694
15 meter E =
0015215
Z = 3060020
86 I = 51
63245
XDOT = -4238
295426 Wp = 42
27211
YDOT = 4156
133530 meter/sec RA = 356
55564 deg
ZDOT = 4918
714982 TA = 353
25085
MA = 353
27132
Ha = 191
526 n
mi
Hp = 183
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18381380
43 X = 5563995
78
Y = 6855951
94 feet Y = 2152129
96 meter
Z = 10039438
53 Z = 3087145
14
XDOT = -13905
168719 XDOT = -4308
349610
YDOT = 13635
608695 feet/sec YDOT = 4108
346371 meter/sec
ZDOT = 16137
516346 ZDOT = 4897
955170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11247379
52 X = 3428201
28
Y = -16006091
61 feet Y = -4878656
72 meter
Z = 10147464
44 Z = 3092947
16
XDOT = 8505
804712 XDOT = 2592
569276
YDOT = 16161
551757 feet/sec YDOT = 4926
040975 meter/sec
ZDOT = 16054
823390 ZDOT = 4893
510169
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 10143
59926895
00020000 00000-0 20000-3 0 9027
2 36572 51
6455 356
7437 0010417 345
0005 15
0848 15
74244072 1414
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143
59926895 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 356
7437 deg
Eccentricity:
0010417
Arg of perigee: 345
0005 deg
Mean anomaly: 15
0848 deg
Mean motion: 15
74244072 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 141
Checksum: 282
Coasting Arc #4 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2010/143/14:34:09
504
Vector Time (MET): 008/20:14:00
549
Weight (LBS) : 214754
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5026499
44 A = 6725536
83 meter
Y = 2561509
16 meter E =
0012610
Z = 3645811
89 I = 51
62311
XDOT = -5097
971727 Wp = 46
59350
YDOT = 3797
065554 meter/sec RA = 356
22083 deg
ZDOT = 4359
954779 TA = 357
22343
MA = 357
23042
Ha = 191
400 n
mi
Hp = 183
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16491139
91 X = 4979771
66
Y = 8403901
45 feet Y = 2617456
96 meter
Z = 11961325
11 Z = 3670117
63
XDOT = -16725
629026 XDOT = -5161
232469
YDOT = 12457
564155 feet/sec YDOT = 3739
702998 meter/sec
ZDOT = 14304
313578 ZDOT = 4335
035076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5773791
34 X = 1759851
60
Y = -17519176
29 feet Y = -5339844
93 meter
Z = 12058123
76 Z = 3675316
12
XDOT = 13621
795254 XDOT = 4151
923193
YDOT = 14268
347697 feet/sec YDOT = 4348
992378 meter/sec
ZDOT = 14205
053530 ZDOT = 4329
700316
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 10143
66274939
00020000 00000-0 20000-3 0 9031
2 36572 51
6439 356
4152 0010063 345
4566 14
6307 15
74265797 1423
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143
66274939 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 356
4152 deg
Eccentricity:
0010063
Arg of perigee: 345
4566 deg
Mean anomaly: 14
6307 deg
Mean motion: 15
74265797 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 142
Checksum: 295
Coasting Arc #5 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2010/143/16:37:20
373
Vector Time (MET): 008/22:17:11
418
Weight (LBS) : 214679
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6530520
37 A = 6731024
69 meter
Y = 1284094
36 meter E =
0010244
Z = 1005717
83 I = 51
63978
XDOT = -1817
778401 Wp = 78
11117
YDOT = -4564
957819 meter/sec RA = 355
74471 deg
ZDOT = -5922
285934 TA = 90
90409
MA = 90
78672
Ha = 191
711 n
mi
Hp = 182
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21425591
76 X = -6549279
64
Y = 4212908
01 feet Y = 1210961
24 meter
Z = 3299599
17 Z = 973946
63
XDOT = -5963
839898 XDOT = -1737
827313
YDOT = -14976
895731 feet/sec YDOT = -4584
837867 meter/sec
ZDOT = -19430
071963 ZDOT = -5930
922934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16950074
30 X = 5166382
65
Y = 13795601
37 feet Y = 4204899
30 meter
Z = 3173057
67 Z = 967147
98
XDOT = -6770
801908 XDOT = -2063
740422
YDOT = 12837
317391 feet/sec YDOT = 3912
814341 meter/sec
ZDOT = -19464
459487 ZDOT = -5932
767252
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 10143
72623494
00020000 00000-0 20000-3 0 9043
2 36572 51
6450 356
0880 0009896 352
9949 7
1074 15
74261533 1433
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143
72623494 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 356
0880 deg
Eccentricity:
0009896
Arg of perigee: 352
9949 deg
Mean anomaly: 7
1074 deg
Mean motion: 15
74261533 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 143
Checksum: 297
Coasting Arc #6 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2010/143/17:05:14
662
Vector Time (MET): 008/22:45:05
707
Weight (LBS) : 214642
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 699032
01 A = 6720427
28 meter
Y = -4195926
06 meter E =
0014600
Z = -5212177
44 I = 51
60225
XDOT = 7637
022394 Wp = 56
11420
YDOT = 146
799215 meter/sec RA = 355
64831 deg
ZDOT = 915
881150 TA = 222
56656
MA = 222
67982
Ha = 192
005 n
mi
Hp = 183
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2293412
11 X = 771219
84
Y = -13766161
60 feet Y = -4187705
08 meter
Z = -17100319
68 Z = -5208606
43
XDOT = 25055
847748 XDOT = 7630
364004
YDOT = 481
624722 feet/sec YDOT = 232
163657 meter/sec
ZDOT = 3004
859416 ZDOT = 952
966176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11178244
25 X = -3407128
85
Y = 8384532
86 feet Y = 2555605
61 meter
Z = -17086086
21 Z = -5207839
08
XDOT = -17291
758097 XDOT = -5270
527868
YDOT = -16694
712155 feet/sec YDOT = -5088
548265 meter/sec
ZDOT = 3152
560970 ZDOT = 960
900584
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 10143
72623568
00020000 00000-0 20000-3 0 9056
2 36572 51
6463 356
0897 0010179 347
1020 12
9881 15
73990257 1438
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143
72623568 = yrday
fracday
Element set: 905
Inclination: 51
6463 deg
RA of node: 356
0897 deg
Eccentricity:
0010179
Arg of perigee: 347
1020 deg
Mean anomaly: 12
9881 deg
Mean motion: 15
73990257 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 143
Checksum: 295
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