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
107/14:29:31
681 -1
7 -3
2 3
2
012/04:08:06
725 1
7 0
0 189
0
000/00:00:13
450 -2
2 -0
6 181
5
108/17:31:25
418 17
8 -19
0 19
0
013/07:10:00
462 3
0 0
0 188
4
000/00:00:14
055 -5
9 0
0 170
6
Coasting Arc #1 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/107/14:14:45
758
Vector Time (MET): 012/03:53:20
802
Weight (LBS) : 235632
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5365742
33 A = 6725007
59 meter
Y = 2488692
43 meter E =
0006340
Z = -3209010
50 I = 51
64544
XDOT = -4642
256094 Wp = 134
53695
YDOT = -3834
368742 meter/sec RA = 180
54147 deg
ZDOT = 4790
000571 TA = 188
00961
MA = 188
01974
Ha = 189
428 n
mi
Hp = 182
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17604141
51 X = -5377583
50
Y = 8165001
40 feet Y = 2428623
35 meter
Z = -10528249
67 Z = -3235106
41
XDOT = -15230
498995 XDOT = -4622
303793
YDOT = -12579
949940 feet/sec YDOT = -3886
169732 meter/sec
ZDOT = 15715
224972 ZDOT = 4767
496536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2197509
44 X = -669800
88
Y = 19223689
24 feet Y = 5859380
48 meter
Z = -10631924
17 Z = -3240610
49
XDOT = -17327
930839 XDOT = -5281
553320
YDOT = 6658
593986 feet/sec YDOT = 2029
539447 meter/sec
ZDOT = 15625
609440 ZDOT = 4762
685757
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
60027721
00020000 00000-0 20000-3 0 9008
2 36507 51
6459 181
5714 0004979 180
5932 179
5227 15
74914153 1933
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10107
60027721 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 181
5714 deg
Eccentricity:
0004979
Arg of perigee: 180
5932 deg
Mean anomaly: 179
5227 deg
Mean motion: 15
74914153 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 193
Checksum: 289
Coasting Arc #2 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2010/107/14:29:38
406
Vector Time (MET): 012/04:08:13
450
Weight (LBS) : 235544
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6260691
64 A = 6726561
18 meter
Y = -1558178
64 meter E =
0011969
Z = 1896414
02 I = 51
65509
XDOT = 2818
266040 Wp = 97
21695
YDOT = -4429
682215 meter/sec RA = 180
53080 deg
ZDOT = 5632
685777 TA = 283
85709
MA = 283
99022
Ha = 189
002 n
mi
Hp = 181
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20540326
90 X = -6252015
08
Y = -5112134
63 feet Y = -1628140
93 meter
Z = 6221830
76 Z = 1866020
15
XDOT = 9246
279660 XDOT = 2840
227079
YDOT = -14533
078132 feet/sec YDOT = -4398
043992 meter/sec
ZDOT = 18479
940213 ZDOT = 5646
430398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14105089
54 X = -4299231
29
Y = 15829570
55 feet Y = 4824853
10 meter
Z = 6100923
94 Z = 1859561
62
XDOT = -7452
118468 XDOT = -2271
405709
YDOT = -13824
599468 feet/sec YDOT = -4213
737918 meter/sec
ZDOT = 18534
435263 ZDOT = 5649
295868
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
66370799
00020000 00000-0 20000-3 0 9011
2 36507 51
6452 181
2449 0007130 188
9524 171
1514 15
75448211 1945
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10107
66370799 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 181
2449 deg
Eccentricity:
0007130
Arg of perigee: 188
9524 deg
Mean anomaly: 171
1514 deg
Mean motion: 15
75448211 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 194
Checksum: 284
Coasting Arc #3 (Orbit 208)
---------------------------------------
Vector Time (GMT): 2010/108/14:34:36
978
Vector Time (MET): 013/04:13:12
022
Weight (LBS) : 235544
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4620703
34 A = 6722035
01 meter
Y = 3265255
23 meter E =
0009035
Z = -3640167
16 I = 51
67190
XDOT = -5571
982671 Wp = 153
99479
YDOT = -3009
840679 meter/sec RA = 175
32433 deg
ZDOT = 4369
147155 TA = 162
39773
MA = 162
36640
Ha = 188
779 n
mi
Hp = 181
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15159787
87 X = -4639189
10
Y = 10712779
62 feet Y = 3213480
54 meter
Z = -11942805
64 Z = -3662659
60
XDOT = -18280
783042 XDOT = -5559
136748
YDOT = -9874
805378 feet/sec YDOT = -3072
078221 meter/sec
ZDOT = 14334
472292 ZDOT = 4342
109244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3167121
26 X = 965338
56
Y = 18232125
31 feet Y = 5557151
79 meter
Z = -12032139
12 Z = -3667396
00
XDOT = -15493
155183 XDOT = -4722
313700
YDOT = 12088
577532 feet/sec YDOT = 3684
598432 meter/sec
ZDOT = 14226
846517 ZDOT = 4336
342819
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
61515011
00020000 00000-0 20000-3 0 9026
2 36507 51
6460 176
3486 0007183 192
7573 167
3411 15
75509193 2092
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10108
61515011 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 176
3486 deg
Eccentricity:
0007183
Arg of perigee: 192
7573 deg
Mean anomaly: 167
3411 deg
Mean motion: 15
75509193 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 209
Checksum: 276
Coasting Arc #4 (Orbit 210)
---------------------------------------
Vector Time (GMT): 2010/108/17:31:32
445
Vector Time (MET): 013/07:10:07
489
Weight (LBS) : 235105
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2345984
87 A = 6707742
93 meter
Y = 4053231
79 meter E =
0028677
Z = -4828548
29 I = 51
65773
XDOT = -7184
328220 Wp = 125
04707
YDOT = -1260
684520 meter/sec RA = 174
69879 deg
ZDOT = 2426
273775 TA = 168
71519
MA = 168
65074
Ha = 188
359 n
mi
Hp = 170
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7696800
77 X = -2367678
00
Y = 13298004
55 feet Y = 4026876
46 meter
Z = -15841693
85 Z = -4839997
76
XDOT = -23570
630642 XDOT = -7181
483593
YDOT = -4136
104067 feet/sec YDOT = -1341
008128 meter/sec
ZDOT = 7960
215796 ZDOT = 2391
378777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15040201
46 X = 4584253
41
Y = 2903403
29 feet Y = 884957
32 meter
Z = -15887086
58 Z = -4842383
99
XDOT = 3921
605398 XDOT = 1195
305325
YDOT = 22590
999656 feet/sec YDOT = 6885
736695 meter/sec
ZDOT = 7821
402727 ZDOT = 2383
963551
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
74200976
00020000 00000-0 20000-3 0 9032
2 36507 51
6429 175
6951 0017507 136
5431 223
7118 15
79016111 2117
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10108
74200976 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 175
6951 deg
Eccentricity:
0017507
Arg of perigee: 136
5431 deg
Mean anomaly: 223
7118 deg
Mean motion: 15
79016111 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 211
Checksum: 267
Coasting Arc #5 (Orbit 226)
---------------------------------------
Vector Time (GMT): 2010/109/17:34:48
751
Vector Time (MET): 014/07:13:23
794
Weight (LBS) : 235105
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4377151
85 A = 6709694
64 meter
Y = 2675348
32 meter E =
0022017
Z = -4335061
56 I = 51
69479
XDOT = -5726
678574 Wp = 118
33571
YDOT = 3823
242195 meter/sec RA = 169
55937 deg
ZDOT = -3446
222929 TA = 117
00197
MA = 116
77701
Ha = 188
263 n
mi
Hp = 170
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14360734
42 X = 4367969
39
Y = 8777389
50 feet Y = 2724245
06 meter
Z = -14222642
92 Z = -4313819
42
XDOT = -18788
315532 XDOT = -5752
263894
YDOT = 12543
445521 feet/sec YDOT = 3759
060146 meter/sec
ZDOT = -11306
505674 ZDOT = -3474
105319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3122125
30 X = 951623
79
Y = -16610968
49 feet Y = -5063023
19 meter
Z = -14138065
32 Z = -4309282
31
XDOT = 17125
965749 XDOT = 5219
994360
YDOT = 12870
681221 feet/sec YDOT = 3922
983636 meter/sec
ZDOT = -11417
273565 ZDOT = -3479
984983
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 10109
75458439
00020000 00000-0 20000-3 0 9044
2 36507 51
6428 170
4555 0017490 140
2867 219
9583 15
79061237 2274
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10109
75458439 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 170
4555 deg
Eccentricity:
0017490
Arg of perigee: 140
2867 deg
Mean anomaly: 219
9583 deg
Mean motion: 15
79061237 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 227
Checksum: 306
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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