Date:
February 24th 2010
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2010/039/09:14:06 981 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 07 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 07803
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 191)
---------------------------------------
Vector Time (GMT): 2010/051/11:10:46
000
Vector Time (MET): 012/01:56:39
019
Weight (LBS) : 209039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2384032
83 A = 6716752
69 meter
Y = 4237759
19 meter E =
0010200
Z = -4636772
59 I = 51
95081
XDOT = -4353
229867 Wp = 45
97723
YDOT = 5638
761038 meter/sec RA = 108
91550 deg
ZDOT = 2926
152583 TA = 252
81575
MA = 252
92744
Ha = 188
979 n
mi
Hp = 180
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7821630
02 X = 2358968
41
Y = 13903409
42 feet Y = 4264292
14 meter
Z = -15212508
51 Z = -4625252
01
XDOT = -14282
250221 XDOT = -4430
206344
YDOT = 18499
872173 feet/sec YDOT = 5589
625300 meter/sec
ZDOT = 9600
238134 ZDOT = 2904
817725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3641807
68 X = -1110022
98
Y = 15576077
63 feet Y = 4747588
46 meter
Z = -15166612
91 Z = -4622783
62
XDOT = -21954
413239 XDOT = -6691
705155
YDOT = 4097
602082 feet/sec YDOT = 1248
949114 meter/sec
ZDOT = 9515
717450 ZDOT = 2900
390679
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 36394U 10004A 10051
47660669
00020000 00000-0 20000-3 0 9000
2 36394 51
6438 109
7392 0011065 345
6248 14
4600 15
76146754 1923
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
47660669 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 109
7392 deg
Eccentricity:
0011065
Arg of perigee: 345
6248 deg
Mean anomaly: 14
4600 deg
Mean motion: 15
76146754 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 192
Checksum: 290
Coasting Arc #2 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/052/11:15:24
504
Vector Time (MET): 013/02:01:17
523
Weight (LBS) : 209039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4219303
52 A = 6718013
49 meter
Y = -2930639
42 meter E =
0015330
Z = -4342706
64 I = 51
96339
XDOT = 1127
115067 Wp = 23
99785
YDOT = 6774
054430 meter/sec RA = 103
81620 deg
ZDOT = -3466
892248 TA = 211
05311
MA = 211
14381
Ha = 189
097 n
mi
Hp = 179
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13842859
32 X = 4272873
14
Y = -9614958
74 feet Y = -2883132
98 meter
Z = -14247725
20 Z = -4322079
35
XDOT = 3697
884077 XDOT = 1068
085384
YDOT = 22224
588024 feet/sec YDOT = 6786
334701 meter/sec
ZDOT = -11374
318399 ZDOT = -3461
560138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16829694
65 X = 5129690
93
Y = 1777149
16 feet Y = 541675
07 meter
Z = -14165909
01 Z = -4317769
07
XDOT = -11492
084292 XDOT = -3502
787292
YDOT = 18086
735753 feet/sec YDOT = 5512
837057 meter/sec
ZDOT = -11352
917567 ZDOT = -3460
369274
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 36394U 10004A 10052
49106230
00020000 00000-0 20000-3 0 9013
2 36394 51
6437 104
5130 0011086 349
4364 10
6565 15
76131913 2086
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10052
49106230 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 104
5130 deg
Eccentricity:
0011086
Arg of perigee: 349
4364 deg
Mean anomaly: 10
6565 deg
Mean motion: 15
76131913 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 208
Checksum: 256
Coasting Arc #3 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/053/11:20:06
741
Vector Time (MET): 014/02:05:59
760
Weight (LBS) : 209039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 412231
72 A = 6725671
39 meter
Y = -6670931
79 meter E =
0010064
Z = 760863
64 I = 51
99668
XDOT = 4803
292823 Wp = 71
87381
YDOT = -395
379647 meter/sec RA = 98
63941 deg
ZDOT = -6001
439263 TA = 99
87323
MA = 99
75961
Ha = 189
217 n
mi
Hp = 179
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1352466
27 X = 483138
46
Y = -21886259
14 feet Y = -6665922
97 meter
Z = 2496271
77 Z = 763038
34
XDOT = 15758
834720 XDOT = 4836
512522
YDOT = -1297
177320 feet/sec YDOT = -341
453107 meter/sec
ZDOT = -19689
761361 ZDOT = -5978
024475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14667384
62 X = 4470618
83
Y = -16299177
96 feet Y = -4967989
44 meter
Z = 2504696
20 Z = 763431
40
XDOT = 12044
781778 XDOT = 3671
249486
YDOT = 7793
571140 feet/sec YDOT = 2375
480483 meter/sec
ZDOT = -19596
783059 ZDOT = -5973
099476
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 36394U 10004A 10053
50550282
00020000 00000-0 20000-3 0 9027
2 36394 51
6445 99
2870 0011318 353
9357 6
1668 15
76198300 2241
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10053
50550282 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 99
2870 deg
Eccentricity:
0011318
Arg of perigee: 353
9357 deg
Mean anomaly: 6
1668 deg
Mean motion: 15
76198300 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 224
Checksum: 285
Coasting Arc #4 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/054/11:24:41
551
Vector Time (MET): 015/02:10:34
570
Weight (LBS) : 209039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3803932
59 A = 6714903
29 meter
Y = -2302077
61 meter E =
0014996
Z = 5032461
12 I = 51
96371
XDOT = 1897
394789 Wp = 15
63099
YDOT = -7231
830972 meter/sec RA = 93
48748 deg
ZDOT = -1858
563198 TA = 92
29080
MA = 92
11908
Ha = 189
354 n
mi
Hp = 179
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12480093
80 X = -3802340
67
Y = -7552748
07 feet Y = -2344628
32 meter
Z = 16510699
22 Z = 5013985
73
XDOT = 6225
048519 XDOT = 1987
190817
YDOT = -23726
479568 feet/sec YDOT = -7210
100002 meter/sec
ZDOT = -6097
648289 ZDOT = -1849
127897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5652713
96 X = -1722947
21
Y = -13537489
50 feet Y = -4126226
80 meter
Z = 16437248
44 Z = 5010073
33
XDOT = 18119
019713 XDOT = 5522
677209
YDOT = -14985
964381 feet/sec YDOT = -4567
721943 meter/sec
ZDOT = -6060
394082 ZDOT = -1847
208116
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 36394U 10004A 10054
51992696
00020000 00000-0 20000-3 0 9039
2 36394 51
6442 94
0612 0011277 357
5052 2
6054 15
76225556 2403
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10054
51992696 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 94
0612 deg
Eccentricity:
0011277
Arg of perigee: 357
5052 deg
Mean anomaly: 2
6054 deg
Mean motion: 15
76225556 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 240
Checksum: 279
Coasting Arc #5 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/055/11:29:16
873
Vector Time (MET): 016/02:15:09
892
Weight (LBS) : 209039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2734061
36 A = 6720037
97 meter
Y = 4904224
15 meter E =
0016076
Z = 3672632
56 I = 51
98135
XDOT = -3566
170990 Wp = 50
41178
YDOT = -5262
383786 meter/sec RA = 88
38371 deg
ZDOT = 4369
759951 TA = 353
60188
MA = 353
62239
Ha = 189
583 n
mi
Hp = 178
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8970017
60 X = -2806566
39
Y = 16089974
25 feet Y = 4873229
00 meter
Z = 12049319
44 Z = 3659174
80
XDOT = -11700
036056 XDOT = -3528
257911
YDOT = -17265
038669 feet/sec YDOT = -5302
071135 meter/sec
ZDOT = 14336
482779 ZDOT = 4352
527825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16523743
89 X = -5036437
14
Y = 8221693
58 feet Y = 2505972
20 meter
Z = 11996008
86 Z = 3656383
50
XDOT = 563
196885 XDOT = 171
662410
YDOT = -19698
023212 feet/sec YDOT = -6003
957475 meter/sec
ZDOT = 14267
878292 ZDOT = 4348
849304
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 36394U 10004A 10055
53433669
00020000 00000-0 20000-3 0 9043
2 36394 51
6440 88
8347 0011337 2
9662 357
1568 15
76215928 2569
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10055
53433669 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 88
8347 deg
Eccentricity:
0011337
Arg of perigee: 2
9662 deg
Mean anomaly: 357
1568 deg
Mean motion: 15
76215928 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 256
Checksum: 309
Coasting Arc #6 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2010/056/11:33:53
726
Vector Time (MET): 017/02:19:46
745
Weight (LBS) : 209039
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2132259
83 A = 6724361
33 meter
Y = 6112566
39 meter E =
0018132
Z = -1782866
07 I = 51
99518
XDOT = -4133
226700 Wp = 18
76686
YDOT = 3101
289087 meter/sec RA = 83
19693 deg
ZDOT = 5722
260019 TA = 321
54121
MA = 321
67030
Ha = 189
559 n
mi
Hp = 178
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6995603
12 X = 2072375
26
Y = 20054351
66 feet Y = 6136087
73 meter
Z = -5849298
12 Z = -1772653
22
XDOT = -13560
455051 XDOT = -4195
413017
YDOT = 10174
832963 feet/sec YDOT = 3054
697442 meter/sec
ZDOT = 18773
818959 ZDOT = 5702
030325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4692127
76 X = -1430160
54
Y = 20726178
11 feet Y = 6317339
09 meter
Z = -5808549
75 Z = -1770445
97
XDOT = -15475
766250 XDOT = -4717
013553
YDOT = 1705
118314 feet/sec YDOT = 519
720062 meter/sec
ZDOT = 18693
548331 ZDOT = 5697
793531
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 36394U 10004A 10056
48532878
00020000 00000-0 20000-3 0 9051
2 36394 51
6449 83
9356 0011329 6
2889 353
8416 15
76267582 2718
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10056
48532878 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 83
9356 deg
Eccentricity:
0011329
Arg of perigee: 6
2889 deg
Mean anomaly: 353
8416 deg
Mean motion: 15
76267582 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 271
Checksum: 326
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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