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
662 -2
9 -0
0 3
0
008/22:17:05
707 0
6 -0
0 191
7
000/00:00:11
414 0
5 -3
0 182
8
143/17:05:11
808 1
5 1
5 1
5
008/22:45:02
853 0
0 0
0 192
0
000/00:00:05
705 0
2 -0
0 183
4
Coasting Arc #1 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2010/141/20:07:01
000
Vector Time (MET): 007/01:46:52
045
Weight (LBS) : 214758
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -717806
54 A = 6719533
18 meter
Y = 4115217
58 meter E =
0010016
Z = 5264721
13 I = 51
66005
XDOT = -7637
199375 Wp = 352
99453
YDOT = -940
649143 meter/sec RA = 5
27638 deg
ZDOT = -296
307509 TA = 99
87398
MA = 99
76088
Ha = 191
320 n
mi
Hp = 183
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2355008
34 X = -789345
49
Y = 13501370
02 feet Y = 4106790
34 meter
Z = 17272707
12 Z = 5261060
48
XDOT = -25056
428396 XDOT = -7624
673834
YDOT = -3086
119236 feet/sec YDOT = -1025
982804 meter/sec
ZDOT = -972
137496 ZDOT = -333
378851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2377884
94 X = 724779
33
Y = -13516007
55 feet Y = -4119679
10 meter
Z = 17258118
99 Z = 5260274
67
XDOT = 24082
264144 XDOT = 7340
274111
YDOT = 2766
311354 feet/sec YDOT = 843
171701 meter/sec
ZDOT = -1119
794933 ZDOT = -341
313496
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
88526817
00020000 00000-0 20000-3 0 9005
2 36572 51
6483 5
5448 0009925 338
9424 21
1329 15
74211672 1146
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10141
88526817 = yrday
fracday
Element set: 900
Inclination: 51
6483 deg
RA of node: 5
5448 deg
Eccentricity:
0009925
Arg of perigee: 338
9424 deg
Mean anomaly: 21
1329 deg
Mean motion: 15
74211672 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 114
Checksum: 282
Coasting Arc #2 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2010/142/20:07:47
167
Vector Time (MET): 008/01:47:38
212
Weight (LBS) : 214688
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6672574
17 A = 6731452
35 meter
Y = 499197
29 meter E =
0019356
Z = 609548
58 I = 51
66997
XDOT = -907
973768 Wp = 22
67398
YDOT = 4746
603776 meter/sec RA =
14842 deg
ZDOT = 6006
725392 TA = 343
96709
MA = 344
02826
Ha = 191
474 n
mi
Hp = 183
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21891647
54 X = 6663535
02
Y = 1637786
38 feet Y = 573763
41 meter
Z = 1999831
30 Z = 641942
35
XDOT = -2978
916561 XDOT = -990
163546
YDOT = 15572
847034 feet/sec YDOT = 4735
990379 meter/sec
ZDOT = 19707
104304 ZDOT = 6002
115043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21915096
45 X = -6679721
40
Y = -1059450
46 feet Y = -322920
50 meter
Z = 2128852
66 Z = 648874
29
XDOT = 2605
462512 XDOT = 794
144974
YDOT = -14051
665120 feet/sec YDOT = -4282
947528 meter/sec
ZDOT = 19688
731588 ZDOT = 6001
125388
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
90098002
00020000 00000-0 20000-3 0 9010
2 36572 51
6484
3286 0009985 343
4320 16
6515 15
74195910 1302
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10142
90098002 = yrday
fracday
Element set: 901
Inclination: 51
6484 deg
RA of node:
3286 deg
Eccentricity:
0009985
Arg of perigee: 343
4320 deg
Mean anomaly: 16
6515 deg
Mean motion: 15
74195910 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 130
Checksum: 263
Coasting Arc #3 (Orbit 141)
---------------------------------------
Vector Time (GMT): 2010/143/14:34:09
504
Vector Time (MET): 008/20:14:00
549
Weight (LBS) : 214684
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025782
05 A = 6725531
18 meter
Y = 2561971
08 meter E =
0012633
Z = 3646438
97 I = 51
62290
XDOT = -5098
897557 Wp = 46
68514
YDOT = 3796
693669 meter/sec RA = 356
21959 deg
ZDOT = 4359
231242 TA = 357
14156
MA = 357
14878
Ha = 191
403 n
mi
Hp = 183
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16488786
25 X = 4979046
11
Y = 8405416
94 feet Y = 2617910
82 meter
Z = 11963382
45 Z = 3670741
21
XDOT = -16728
666527 XDOT = -5162
150557
YDOT = 12456
344058 feet/sec YDOT = 3739
320803 meter/sec
ZDOT = 14301
939769 ZDOT = 4334
307060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5775653
53 X = 1760419
20
Y = -17517072
26 feet Y = -5339203
62 meter
Z = 12060167
15 Z = 3675938
95
XDOT = 13621
208778 XDOT = 4151
744435
YDOT = 14271
387429 feet/sec YDOT = 4349
918888 meter/sec
ZDOT = 14202
661885 ZDOT = 4328
971342
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
66274765
00020000 00000-0 20000-3 0 9027
2 36572 51
6437 356
4139 0010058 345
6385 14
4491 15
74267070 1429
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143
66274765 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 356
4139 deg
Eccentricity:
0010058
Arg of perigee: 345
6385 deg
Mean anomaly: 14
4491 deg
Mean motion: 15
74267070 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 142
Checksum: 287
Coasting Arc #4 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2010/143/16:37:20
369
Vector Time (MET): 008/22:17:11
414
Weight (LBS) : 214609
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6530778
40 A = 6731021
85 meter
Y = 1283504
22 meter E =
0010273
Z = 1004763
55 I = 51
63959
XDOT = -1816
531334 Wp = 78
13947
YDOT = -4565
207267 meter/sec RA = 355
74347 deg
ZDOT = -5922
481185 TA = 90
88630
MA = 90
76859
Ha = 191
715 n
mi
Hp = 182
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21426438
34 X = -6549526
42
Y = 4210971
84 feet Y = 1210368
27 meter
Z = 3296468
35 Z = 972991
12
XDOT = -5959
748470 XDOT = -1736
576600
YDOT = -14977
714129 feet/sec YDOT = -4585
073349 meter/sec
ZDOT = -19430
712550 ZDOT = -5931
112118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16949111
19 X = 5166089
09
Y = 13797480
63 feet Y = 4205472
10 meter
Z = 3169921
96 Z = 966192
21
XDOT = -6773
916181 XDOT = -2064
689652
YDOT = 12834
759957 feet/sec YDOT = 3912
034835 meter/sec
ZDOT = -19465
075909 ZDOT = -5932
955137
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
72623314
00020000 00000-0 20000-3 0 9033
2 36572 51
6448 356
0868 0009895 353
1826 6
9201 15
74262816 1436
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143
72623314 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 356
0868 deg
Eccentricity:
0009895
Arg of perigee: 353
1826 deg
Mean anomaly: 6
9201 deg
Mean motion: 15
74262816 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 143
Checksum: 290
Coasting Arc #5 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2010/143/17:05:14
660
Vector Time (MET): 008/22:45:05
705
Weight (LBS) : 214572
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 700139
57 A = 6720424
47 meter
Y = -4195947
19 meter E =
0014626
Z = -5212032
88 I = 51
60205
XDOT = 7636
860108 Wp = 56
17821
YDOT = 147
500282 meter/sec RA = 355
64706 deg
ZDOT = 916
950212 TA = 222
51283
MA = 222
62618
Ha = 192
008 n
mi
Hp = 183
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2297045
83 X = 772326
85
Y = -13766230
94 feet Y = -4187713
84 meter
Z = -17099845
41 Z = -5208456
49
XDOT = 25055
315316 XDOT = 7630
188698
YDOT = 483
924810 feet/sec YDOT = 232
862836 meter/sec
ZDOT = 3008
366838 ZDOT = 954
034419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11180937
01 X = -3407949
60
Y = 8382093
51 feet Y = 2554862
10 meter
Z = -17085590
51 Z = -5207687
99
XDOT = -17289
954435 XDOT = -5269
978112
YDOT = -16695
814231 feet/sec YDOT = -5088
884177 meter/sec
ZDOT = 3156
065122 ZDOT = 961
968649
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
72623388
00020000 00000-0 20000-3 0 9045
2 36572 51
6461 356
0885 0010174 347
2827 12
8079 15
73991511 1436
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10143
72623388 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 356
0885 deg
Eccentricity:
0010174
Arg of perigee: 347
2827 deg
Mean anomaly: 12
8079 deg
Mean motion: 15
73991511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 143
Checksum: 292
Coasting Arc #6 (Orbit 158)
---------------------------------------
Vector Time (GMT): 2010/144/17:05:42
445
Vector Time (MET): 009/22:45:33
490
Weight (LBS) : 214572
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6652890
67 A = 6731684
12 meter
Y = 312400
20 meter E =
0005025
Z = -993422
50 I = 51
60999
XDOT = 652
843751 Wp = 59
85609
YDOT = -4865
915396 meter/sec RA = 350
52454 deg
ZDOT = -5922
016161 TA = 130
99271
MA = 130
94924
Ha = 192
152 n
mi
Hp = 183
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21827069
13 X = -6651063
57
Y = 1024935
04 feet Y = 238013
92 meter
Z = -3259260
18 Z = -1025738
36
XDOT = 2141
875822 XDOT = 735
975369
YDOT = -15964
289357 feet/sec YDOT = -4858
149563 meter/sec
ZDOT = -19429
186879 ZDOT = -5918
643095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16853228
38 X = 5136864
01
Y = 13877485
60 feet Y = 4229857
61 meter
Z = -3387964
31 Z = -1032651
52
XDOT = -11376
295240 XDOT = -3467
494789
YDOT = 9090
913687 feet/sec YDOT = 2770
910492 meter/sec
ZDOT = -19415
736378 ZDOT = -5917
916448
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 10144
74207957
00020000 00000-0 20000-3 0 9059
2 36572 51
6459 350
8711 0010291 350
8750 9
2225 15
74008173 1592
Satellite: SHUTTLE
Catalog Number: 36572
Epoch time: 10144
74207957 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 350
8711 deg
Eccentricity:
0010291
Arg of perigee: 350
8750 deg
Mean anomaly: 9
2225 deg
Mean motion: 15
74008173 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 159
Checksum: 282
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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