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
108/17:31:25
111 17
1 -18
1 18
1
013/07:10:00
155 2
6 0
1 188
3
000/00:00:13
509 -5
4 0
4 171
0
Coasting Arc #1 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2010/108/15:41:23
000
Vector Time (MET): 013/05:19:58
044
Weight (LBS) : 234817
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5372659
82 A = 6722864
71 meter
Y = 2218863
36 meter E =
0007825
Z = -3372877
80 I = 51
67467
XDOT = -4594
621958 Wp = 156
43515
YDOT = 4077
441940 meter/sec RA = 175
13894 deg
ZDOT = -4647
141096 TA = 63
33743
MA = 63
25732
Ha = 188
766 n
mi
Hp = 181
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17626836
69 X = 5363833
81
Y = 7279735
45 feet Y = 2278894
40 meter
Z = -11065872
04 Z = -3346798
47
XDOT = -15074
219021 XDOT = -4617
299923
YDOT = 13377
434187 feet/sec YDOT = 4025
935500 meter/sec
ZDOT = -15246
525906 ZDOT = -4669
516982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9894769
09 X = 3015925
62
Y = -16373138
99 feet Y = -4990532
77 meter
Z = -10962085
03 Z = -3341243
52
XDOT = 9738
975572 XDOT = 2968
439754
YDOT = 16129
041507 feet/sec YDOT = 4916
131851 meter/sec
ZDOT = -15335
368514 ZDOT = -4674
220323
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
67855517
00020000 00000-0 20000-3 0 9008
2 36507 51
6444 176
0240 0007183 193
0952 167
0027 15
75562965 2102
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10108
67855517 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 176
0240 deg
Eccentricity:
0007183
Arg of perigee: 193
0952 deg
Mean anomaly: 167
0027 deg
Mean motion: 15
75562965 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 210
Checksum: 278
Coasting Arc #2 (Orbit 210)
---------------------------------------
Vector Time (GMT): 2010/108/17:31:31
865
Vector Time (MET): 013/07:10:06
909
Weight (LBS) : 234398
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2358245
80 A = 6707997
87 meter
Y = 4050920
96 meter E =
0028009
Z = -4824273
58 I = 51
65748
XDOT = -7179
341858 Wp = 124
97428
YDOT = -1270
070570 meter/sec RA = 174
70061 deg
ZDOT = 2437
203225 TA = 168
89919
MA = 168
83726
Ha = 188
252 n
mi
Hp = 171
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7737026
89 X = -2379932
93
Y = 13290423
10 feet Y = 4024428
56 meter
Z = -15827669
22 Z = -4835782
61
XDOT = -23554
271189 XDOT = -7176
445740
YDOT = -4166
898195 feet/sec YDOT = -1350
338130 meter/sec
ZDOT = 7996
073573 ZDOT = 2402
332576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15045914
44 X = 4585994
72
Y = 2944636
88 feet Y = 897525
32 meter
Z = -15873298
85 Z = -4838181
49
XDOT = 3889
252991 XDOT = 1185
444312
YDOT = 22585
396087 feet/sec YDOT = 6884
028727 meter/sec
ZDOT = 7857
357014 ZDOT = 2394
922418
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
74198266
00020000 00000-0 20000-3 0 9018
2 36507 51
6426 175
6971 0016864 136
8081 223
4411 15
78932083 2112
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10108
74198266 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 175
6971 deg
Eccentricity:
0016864
Arg of perigee: 136
8081 deg
Mean anomaly: 223
4411 deg
Mean motion: 15
78932083 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 211
Checksum: 288
Coasting Arc #3 (Orbit 226)
---------------------------------------
Vector Time (GMT): 2010/109/17:34:45
453
Vector Time (MET): 014/07:13:20
496
Weight (LBS) : 234398
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4409801
65 A = 6710007
47 meter
Y = 2653693
82 meter E =
0021323
Z = -4315345
37 I = 51
69473
XDOT = -5694
122053 Wp = 118
10944
YDOT = 3842
827620 meter/sec RA = 169
56215 deg
ZDOT = -3478
456826 TA = 116
85237
MA = 116
63421
Ha = 188
156 n
mi
Hp = 171
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14467853
17 X = 4400763
12
Y = 8706344
57 feet Y = 2702956
48 meter
Z = -14157957
26 Z = -4293944
27
XDOT = -18681
502799 XDOT = -5719
772213
YDOT = 12607
702164 feet/sec YDOT = 3779
009275 meter/sec
ZDOT = -11412
259928 ZDOT = -3506
181211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3022030
75 X = 921114
97
Y = -16685084
80 feet Y = -5085613
85 meter
Z = -14072748
14 Z = -4289373
63
XDOT = 17139
700039 XDOT = 5224
180572
YDOT = 12759
208014 feet/sec YDOT = 3889
006603 meter/sec
ZDOT = -11522
398718 ZDOT = -3512
027129
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
75461135
00020000 00000-0 20000-3 0 9029
2 36507 51
6425 170
4579 0016847 140
5426 219
6970 15
78977292 2279
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10109
75461135 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 170
4579 deg
Eccentricity:
0016847
Arg of perigee: 140
5426 deg
Mean anomaly: 219
6970 deg
Mean motion: 15
78977292 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 227
Checksum: 306
Coasting Arc #4 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2010/110/17:37:30
166
Vector Time (MET): 015/07:16:05
210
Weight (LBS) : 234398
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6301817
89 A = 6717781
43 meter
Y = -2213437
12 meter E =
0029685
Z = 547909
12 I = 51
75166
XDOT = 2068
881548 Wp = 137
80473
YDOT = 4356
736266 meter/sec RA = 164
35440 deg
ZDOT = -6029
841222 TA = 36
21968
MA = 36
01905
Ha = 187
893 n
mi
Hp = 171
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20675255
55 X = 6323438
93
Y = -7261932
81 feet Y = -2142845
57 meter
Z = 1797602
11 Z = 578575
87
XDOT = 6787
669122 XDOT = 2049
301917
YDOT = 14293
754154 feet/sec YDOT = 4379
762438 meter/sec
ZDOT = -19782
943643 ZDOT = -6019
838001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14559975
70 X = -4437880
59
Y = -16363245
41 feet Y = -4987517
20 meter
Z = 1919515
81 Z = 585068
42
XDOT = 9411
219728 XDOT = 2868
539773
YDOT = -10749
627446 feet/sec YDOT = -3276
486446 meter/sec
ZDOT = -19743
005492 ZDOT = -6017
668074
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 10110
76721854
00020000 00000-0 20000-3 0 9030
2 36507 51
6429 165
2195 0016653 144
2759 215
9525 15
79025351 2438
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10110
76721854 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 165
2195 deg
Eccentricity:
0016653
Arg of perigee: 144
2759 deg
Mean anomaly: 215
9525 deg
Mean motion: 15
79025351 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 243
Checksum: 286
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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