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
107/11:51:25
413 -0
2 -0
2 0
2
012/01:30:00
457 0
0 -0
1 188
9
000/00:00:00
914 0
1 0
0 182
4
107/14:07:30
709 -1
2 0
0 3
0
012/03:46:05
753 1
7 -0
0 189
3
000/00:00:11
505 -2
1 -3
0 182
4
107/14:35:30
707 -2
1 -3
0 3
0
012/04:14:05
750 1
3 0
0 188
7
000/00:00:11
501 -1
7 -0
0 181
9
108/17:31:24
950 17
8 -19
0 19
0
013/07:09:59
994 3
0 0
0 187
9
000/00:00:13
120 -5
9 -0
0 171
1
Coasting Arc #1 (Orbit 165)
---------------------------------------
Vector Time (GMT): 2010/105/20:57:27
000
Vector Time (MET): 010/10:36:02
044
Weight (LBS) : 216425
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2112263
78 A = 6718366
18 meter
Y = 3787712
15 meter E =
0015570
Z = -5144446
31 I = 51
56935
XDOT = -7236
276129 Wp = 115
09334
YDOT = -2251
807085 meter/sec RA = 189
40318 deg
ZDOT = 1309
808149 TA = 167
48266
MA = 167
44394
Ha = 189
437 n
mi
Hp = 182
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6929999
28 X = -2129470
43
Y = 12426877
14 feet Y = 3763995
23 meter
Z = -16878104
69 Z = -5154749
75
XDOT = -23741
063416 XDOT = -7216
921123
YDOT = -7387
818520 feet/sec YDOT = -2332
619180 meter/sec
ZDOT = 4297
270830 ZDOT = 1274
700754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11066645
01 X = 3373113
40
Y = -8865771
59 feet Y = -2702287
18 meter
Z = -16918925
67 Z = -5156888
54
XDOT = 18482
006051 XDOT = 5633
315444
YDOT = 15114
654816 feet/sec YDOT = 4606
946788 meter/sec
ZDOT = 4157
620393 ZDOT = 1267
242696
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 10105
88697748
00020000 00000-0 20000-3 0 9008
2 36507 51
6453 190
3789 0004103 178
1992 181
9188 15
74796850 1660
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10105
88697748 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 190
3789 deg
Eccentricity:
0004103
Arg of perigee: 178
1992 deg
Mean anomaly: 181
9188 deg
Mean motion: 15
74796850 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 166
Checksum: 326
Coasting Arc #2 (Orbit 181)
---------------------------------------
Vector Time (GMT): 2010/106/20:57:40
793
Vector Time (MET): 011/10:36:15
836
Weight (LBS) : 216399
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6329141
24 A = 6728798
26 meter
Y = 1681105
87 meter E =
0011787
Z = -1520556
91 I = 51
63526
XDOT = -2552
319081 Wp = 155
69550
YDOT = 4400
741309 meter/sec RA = 184
28369 deg
ZDOT = -5784
686897 TA = 41
07060
MA = 40
98192
Ha = 189
311 n
mi
Hp = 182
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20764899
08 X = 6317259
13
Y = 5515439
20 feet Y = 1751815
66 meter
Z = -4988703
77 Z = -1489838
27
XDOT = -8373
750265 XDOT = -2573
237809
YDOT = 14438
127655 feet/sec YDOT = 4372
082803 meter/sec
ZDOT = -18978
631551 ZDOT = -5797
137086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17334298
70 X = -5283494
24
Y = -12740778
28 feet Y = -3883389
22 meter
Z = -4866510
67 Z = -1483312
45
XDOT = 12042
267302 XDOT = 3670
483074
YDOT = -9149
812290 feet/sec YDOT = -2788
862786 meter/sec
ZDOT = -19027
973425 ZDOT = -5799
726300
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 10106
90227472
00020000 00000-0 20000-3 0 9016
2 36507 51
6456 185
1593 0004023 182
1583 177
9564 15
74851347 1824
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10106
90227472 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 185
1593 deg
Eccentricity:
0004023
Arg of perigee: 182
1583 deg
Mean anomaly: 177
9564 deg
Mean motion: 15
74851347 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 182
Checksum: 288
Coasting Arc #3 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2010/107/11:51:25
870
Vector Time (MET): 012/01:30:00
914
Weight (LBS) : 216393
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3210275
39 A = 6719934
83 meter
Y = -3625907
65 meter E =
0006401
Z = 4653047
51 I = 51
62658
XDOT = 6768
811570 Wp = 95
93009
YDOT = 2362
892570 meter/sec RA = 181
05584 deg
ZDOT = -2826
047037 TA = 21
97305
MA = 21
94562
Ha = 188
942 n
mi
Hp = 182
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10532399
57 X = 3227978
31
Y = -11896022
46 feet Y = -3589909
52 meter
Z = 15265903
92 Z = 4668686
23
XDOT = 22207
387042 XDOT = 6755
614851
YDOT = 7752
272210 feet/sec YDOT = 2438
511702 meter/sec
ZDOT = -9271
807863 ZDOT = -2793
195642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5072068
56 X = 1545966
50
Y = -14994080
63 feet Y = -4570195
78 meter
Z = 15327957
47 Z = 4671961
44
XDOT = 22438
094161 XDOT = 6839
131100
YDOT = -1763
377274 feet/sec YDOT = -537
477393 meter/sec
ZDOT = -9141
102582 ZDOT = -2786
208067
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 10107
53681622
00020000 00000-0 20000-3 0 9028
2 36507 51
6468 181
8963 0004298 189
0942 171
0144 15
74957439 1929
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10107
53681622 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 181
8963 deg
Eccentricity:
0004298
Arg of perigee: 189
0942 deg
Mean anomaly: 171
0144 deg
Mean motion: 15
74957439 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 192
Checksum: 305
Coasting Arc #4 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/107/14:07:36
461
Vector Time (MET): 012/03:46:11
505
Weight (LBS) : 216317
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2821349
97 A = 6719500
91 meter
Y = 3774625
38 meter E =
0013624
Z = -4802315
98 I = 51
62683
XDOT = -6983
899819 Wp = 130
38848
YDOT = -2043
624270 meter/sec RA = 180
57213 deg
ZDOT = 2492
694631 TA = 164
04919
MA = 164
00624
Ha = 189
253 n
mi
Hp = 182
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9256397
53 X = -2840019
66
Y = 12383941
53 feet Y = 3742971
06 meter
Z = -15755629
85 Z = -4816067
60
XDOT = -22913
057149 XDOT = -6972
637833
YDOT = -6704
804036 feet/sec YDOT = -2121
659464 meter/sec
ZDOT = 8178
131991 ZDOT = 2458
793632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5325791
21 X = 1623301
16
Y = 14455347
31 feet Y = 4405989
86 meter
Z = -15810175
75 Z = -4818941
57
XDOT = -17148
679744 XDOT = -5226
917586
YDOT = 15129
663251 feet/sec YDOT = 4611
521359 meter/sec
ZDOT = 8043
263230 ZDOT = 2451
586633
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 10107
60027144
00020000 00000-0 20000-3 0 9030
2 36507 51
6461 181
5707 0005223 190
0535 170
0525 15
74910940 1933
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10107
60027144 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 181
5707 deg
Eccentricity:
0005223
Arg of perigee: 190
0535 deg
Mean anomaly: 170
0525 deg
Mean motion: 15
74910940 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 193
Checksum: 251
Coasting Arc #5 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2010/107/14:35:36
457
Vector Time (MET): 012/04:14:11
501
Weight (LBS) : 216242
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4758158
25 A = 6722107
35 meter
Y = -2972696
05 meter E =
0012392
Z = 3701587
84 I = 51
64048
XDOT = 5445
869969 Wp = 130
59595
YDOT = -3348
992042 meter/sec RA = 180
51765 deg
ZDOT = 4293
507425 TA = 274
01706
MA = 274
15870
Ha = 188
699 n
mi
Hp = 181
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15610755
40 X = -4742545
31
Y = -9752939
81 feet Y = -3025817
38 meter
Z = 12144317
05 Z = 3678510
21
XDOT = 17867
027457 XDOT = 5462
056834
YDOT = -10987
506699 feet/sec YDOT = -3288
002652 meter/sec
ZDOT = 14086
310451 ZDOT = 4320
003139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15683694
71 X = -4780390
15
Y = 9749876
77 feet Y = 2971762
44 meter
Z = 12052451
15 Z = 3673587
11
XDOT = -1275
679322 XDOT = -388
827057
YDOT = -19665
781418 feet/sec YDOT = -5994
130176 meter/sec
ZDOT = 14191
544486 ZDOT = 4325
582759
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 10107
66370086
00020000 00000-0 20000-3 0 9043
2 36507 51
6452 181
2444 0007260 199
0546 161
0347 15
75477375 1946
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10107
66370086 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 181
2444 deg
Eccentricity:
0007260
Arg of perigee: 199
0546 deg
Mean anomaly: 161
0347 deg
Mean motion: 15
75477375 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 194
Checksum: 287
Coasting Arc #6 (Orbit 208)
---------------------------------------
Vector Time (GMT): 2010/108/14:40:28
506
Vector Time (MET): 013/04:19:03
550
Weight (LBS) : 216242
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6161025
79 A = 6726244
88 meter
Y = 1970555
61 meter E =
0001994
Z = -1848306
23 I = 51
68654
XDOT = -3050
624147 Wp = 126
86079
YDOT = -4234
649164 meter/sec RA = 175
31187 deg
ZDOT = 5657
034815 TA = 212
64228
MA = 212
65461
Ha = 188
435 n
mi
Hp = 181
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20213339
21 X = -6173624
15
Y = 6465077
45 feet Y = 1901588
97 meter
Z = -6063996
83 Z = -1878267
39
XDOT = -10008
609406 XDOT = -3030
525989
YDOT = -13893
205920 feet/sec YDOT = -4268
650869 meter/sec
ZDOT = 18559
825508 ZDOT = 5642
263386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2318957
10 X = -706818
12
Y = 21060398
28 feet Y = 6419209
40 meter
Z = -6183075
93 Z = -1884601
54
XDOT = -15274
211993 XDOT = -4655
579816
YDOT = 3746
961539 feet/sec YDOT = 1142
073877 meter/sec
ZDOT = 18500
937772 ZDOT = 5639
085833
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 10108
61513782
00020000 00000-0 20000-3 0 9052
2 36507 51
6460 176
3483 0007323 202
9328 157
1510 15
75539959 2097
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10108
61513782 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 176
3483 deg
Eccentricity:
0007323
Arg of perigee: 202
9328 deg
Mean anomaly: 157
1510 deg
Mean motion: 15
75539959 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 209
Checksum: 287
Coasting Arc #7 (Orbit 210)
---------------------------------------
Vector Time (GMT): 2010/108/17:31:31
510
Vector Time (MET): 013/07:10:06
554
Weight (LBS) : 215839
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2345713
51 A = 6707706
00 meter
Y = 4052670
67 meter E =
0027439
Z = -4827887
55 I = 51
65794
XDOT = -7185
299449 Wp = 125
89904
YDOT = -1260
774076 meter/sec RA = 174
69841 deg
ZDOT = 2426
577508 TA = 167
86386
MA = 167
79763
Ha = 187
897 n
mi
Hp = 171
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7695910
47 X = -2367403
59
Y = 13296163
62 feet Y = 4026318
40 meter
Z = -15839526
08 Z = -4839335
70
XDOT = -23573
817091 XDOT = -7182
455225
YDOT = -4136
397886 feet/sec YDOT = -1341
108547 meter/sec
ZDOT = 7961
212298 ZDOT = 2391
677792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15037977
89 X = 4583575
66
Y = 2904192
43 feet Y = 885197
85 meter
Z = -15884913
56 Z = -4841721
65
XDOT = 3920
800059 XDOT = 1195
059858
YDOT = 22594
530940 feet/sec YDOT = 6886
813031 meter/sec
ZDOT = 7822
380457 ZDOT = 2384
261563
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 10108
74199651
00020000 00000-0 20000-3 0 9062
2 36507 51
6431 175
6946 0016389 138
8337 221
4068 15
79028921 2112
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10108
74199651 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 175
6946 deg
Eccentricity:
0016389
Arg of perigee: 138
8337 deg
Mean anomaly: 221
4068 deg
Mean motion: 15
79028921 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 211
Checksum: 302
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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