Date:
February 10th 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
041/00:56:42
981 14
3 21
0 21
0
001/15:42:36
000 6
9 -0
0 187
1
000/00:00:15
922 -13
8 0
0 176
6
041/01:30:43
425 0
2 -0
2 0
2
001/16:16:36
445 -0
0 0
0 187
1
000/00:00:00
889 -0
0 -0
0 176
6
041/02:28:31
490 5
5 8
1 8
2
001/17:14:24
509 3
9 -1
2 187
2
000/00:00:13
019 -4
8 0
2 181
3
041/03:45:25
641 2
4 2
5 3
1
001/18:31:18
660 -0
4 0
8 187
7
000/00:00:13
320 -1
8 1
5 182
3
Coasting Arc #1 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2010/040/12:31:30
000
Vector Time (MET): 001/03:17:23
019
Weight (LBS) : 247423
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2395419
26 A = 6698360
15 meter
Y = -3570482
40 meter E =
0031361
Z = 5149557
70 I = 51
71114
XDOT = 7018
141574 Wp = 318
85394
YDOT = -2905
078772 meter/sec RA = 165
14585 deg
ZDOT = 1277
909129 TA = 119
10013
MA = 118
78577
Ha = 186
666 n
mi
Hp = 164
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7858987
09 X = -2380309
98
Y = -11714181
10 feet Y = -3597198
81 meter
Z = 16894874
35 Z = 5137957
53
XDOT = 23025
398866 XDOT = 7043
913464
YDOT = -9531
098332 feet/sec YDOT = -2826
413735 meter/sec
ZDOT = 4192
615254 ZDOT = 1312
064816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -194859
54 X = -59393
19
Y = -14160001
63 feet Y = -4315968
50 meter
Z = 16848705
58 Z = 5135485
46
XDOT = 23415
635026 XDOT = 7137
085556
YDOT = 4719
805350 feet/sec YDOT = 1438
596671 meter/sec
ZDOT = 4328
024997 ZDOT = 1319
182019
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 10040
57147101
00020000 00000-0 20000-3 0 9000
2 36394 51
6455 165
9047 0035529 317
0959 42
7437 15
81857978 201
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10040
57147101 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 165
9047 deg
Eccentricity:
0035529
Arg of perigee: 317
0959 deg
Mean anomaly: 42
7437 deg
Mean motion: 15
81857978 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 20
Checksum: 298
Coasting Arc #2 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2010/041/00:56:50
942
Vector Time (MET): 001/15:42:43
961
Weight (LBS) : 246909
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4708644
35 A = 6717419
98 meter
Y = -3855494
36 meter E =
0011610
Z = 2859801
98 I = 51
75245
XDOT = 5185
049318 Wp = 357
05024
YDOT = 2557
522677 meter/sec RA = 162
43059 deg
ZDOT = -5078
713828 TA = 150
16069
MA = 150
09444
Ha = 187
139 n
mi
Hp = 176
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15448308
23 X = 4737536
82
Y = -12649259
73 feet Y = -3802651
26 meter
Z = 9382552
42 Z = 2882745
91
XDOT = 17011
316660 XDOT = 5180
721204
YDOT = 8390
822431 feet/sec YDOT = 2615
510536 meter/sec
ZDOT = -16662
446942 ZDOT = -5053
535917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19423934
97 X = -5920415
38
Y = 4432933
51 feet Y = 1351158
13 meter
Z = 9473443
91 Z = 2887505
70
XDOT = -11229
617361 XDOT = -3422
787372
YDOT = -13737
618949 feet/sec YDOT = -4187
226256 meter/sec
ZDOT = -16562
436912 ZDOT = -5048
230771
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 10041
07698522
00020000 00000-0 20000-3 0 9015
2 36394 51
6447 163
2845 0019472 314
2417 45
7150 15
77917004 281
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041
07698522 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 163
2845 deg
Eccentricity:
0019472
Arg of perigee: 314
2417 deg
Mean anomaly: 45
7150 deg
Mean motion: 15
77917004 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 28
Checksum: 283
Coasting Arc #3 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2010/041/01:30:43
870
Vector Time (MET): 001/16:16:36
889
Weight (LBS) : 246903
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 44507
54 A = 6709231
75 meter
Y = 4270023
10 meter E =
0011448
Z = -5173488
19 I = 51
72621
XDOT = -7486
661687 Wp = 3
18246
YDOT = 1443
346049 meter/sec RA = 162
32349 deg
ZDOT = 1138
222280 TA = 277
59286
MA = 277
72288
Ha = 187
088 n
mi
Hp = 176
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 146022
10 X = 21862
96
Y = 14009262
13 feet Y = 4270394
67 meter
Z = -16973386
46 Z = -5173326
75
XDOT = -24562
538343 XDOT = -7507
781876
YDOT = 4735
387301 feet/sec YDOT = 1359
464960 meter/sec
ZDOT = 3734
325066 ZDOT = 1101
801852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4109729
58 X = 1252645
58
Y = -13394713
69 feet Y = -4082708
73 meter
Z = -16972576
81 Z = -5173241
41
XDOT = 23864
053886 XDOT = 7273
763624
YDOT = 2820
302360 feet/sec YDOT = 859
628159 meter/sec
ZDOT = 3589
861463 ZDOT = 1094
189774
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 10041
07698533
00020000 00000-0 20000-3 0 9028
2 36394 51
6452 163
2844 0019314 314
5621 45
3967 15
77953453 281
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041
07698533 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 163
2844 deg
Eccentricity:
0019314
Arg of perigee: 314
5621 deg
Mean anomaly: 45
3967 deg
Mean motion: 15
77953453 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 28
Checksum: 296
Coasting Arc #4 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2010/041/02:28:38
000
Vector Time (MET): 001/17:14:31
019
Weight (LBS) : 246702
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4866106
14 A = 6722117
03 meter
Y = -3789686
40 meter E =
0006088
Z = 2678319
05 I = 51
75395
XDOT = 4980
344796 Wp = 29
81331
YDOT = 2706
393622 meter/sec RA = 162
10497 deg
ZDOT = -5208
910684 TA = 119
71093
MA = 119
65032
Ha = 187
216 n
mi
Hp = 181
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15964915
15 X = 4895132
24
Y = -12433354
32 feet Y = -3735080
80 meter
Z = 8787135
99 Z = 2702028
24
XDOT = 16339
713898 XDOT = 4974
998811
YDOT = 8879
244167 feet/sec YDOT = 2762
085498 meter/sec
ZDOT = -17089
601982 ZDOT = -5184
729672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16651673
64 X = -5075430
13
Y = 11424928
05 feet Y = 3482318
07 meter
Z = 8881067
40 Z = 2706949
34
XDOT = -15025
959415 XDOT = -4579
912430
YDOT = -8664
552446 feet/sec YDOT = -2640
955586 meter/sec
ZDOT = -16993
541068 ZDOT = -5179
631317
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 10041
14035887
00020000 00000-0 20000-3 0 9034
2 36394 51
6429 162
9598 0013108 307
5740 52
4233 15
76417169 290
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041
14035887 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 162
9598 deg
Eccentricity:
0013108
Arg of perigee: 307
5740 deg
Mean anomaly: 52
4233 deg
Mean motion: 15
76417169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 291
Coasting Arc #5 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2010/041/03:45:32
301
Vector Time (MET): 001/18:31:25
320
Weight (LBS) : 246615
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -974774
83 A = 6714461
13 meter
Y = -4054609
82 meter E =
0010034
Z = 5268063
73 I = 51
72653
XDOT = 7381
087163 Wp = 322
51708
YDOT = -2172
080247 meter/sec RA = 161
84804 deg
ZDOT = -298
488644 TA = 130
35712
MA = 130
26946
Ha = 187
653 n
mi
Hp = 182
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3198080
15 X = -954930
48
Y = -13302525
64 feet Y = -4065405
14 meter
Z = 17283673
65 Z = 5263376
38
XDOT = 24216
165234 XDOT = 7406
289023
YDOT = -7126
247529 feet/sec YDOT = -2089
357568 meter/sec
ZDOT = -979
293452 ZDOT = -262
571217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6782711
06 X = 2067370
33
Y = 11909151
62 feet Y = 3629909
41 meter
Z = 17264912
92 Z = 5262345
46
XDOT = -20513
484699 XDOT = -6252
510136
YDOT = 12932
180565 feet/sec YDOT = 3941
728636 meter/sec
ZDOT = -836
853039 ZDOT = -255
072806
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 10041
20376499
00020000 00000-0 20000-3 0 9049
2 36394 51
6440 162
6306 0011323 310
9490 49
0694 15
75988662 309
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10041
20376499 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 162
6306 deg
Eccentricity:
0011323
Arg of perigee: 310
9490 deg
Mean anomaly: 49
0694 deg
Mean motion: 15
75988662 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 285
Coasting Arc #6 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2010/042/03:50:13
702
Vector Time (MET): 002/18:36:06
721
Weight (LBS) : 246615
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6200965
81 A = 6723872
01 meter
Y = 501996
32 meter E =
0012799
Z = 2528047
54 I = 51
78641
XDOT = 1737
533832 Wp = 25
24929
YDOT = -5305
125849 meter/sec RA = 156
71321 deg
ZDOT = 5316
926405 TA = 3
37969
MA = 3
37105
Ha = 188
045 n
mi
Hp = 182
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20344376
02 X = -6218401
24
Y = 1646969
55 feet Y = 432520
53 meter
Z = 8294119
22 Z = 2497881
83
XDOT = 5700
570314 XDOT = 1770
929736
YDOT = -17405
268532 feet/sec YDOT = -5285
499213 meter/sec
ZDOT = 17443
984270 ZDOT = 5325
448002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18900237
25 X = 5760792
31
Y = -7833161
01 feet Y = -2387547
48 meter
Z = 8174422
21 Z = 2491563
89
XDOT = -550
781489 XDOT = -167
878198
YDOT = 16904
711004 feet/sec YDOT = 5152
555914 meter/sec
ZDOT = 17477
591950 ZDOT = 5327
170026
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 10042
21832701
00020000 00000-0 20000-3 0 9055
2 36394 51
6440 157
4050 0011448 315
5826 44
4419 15
75971278 465
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10042
21832701 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 157
4050 deg
Eccentricity:
0011448
Arg of perigee: 315
5826 deg
Mean anomaly: 44
4419 deg
Mean motion: 15
75971278 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 46
Checksum: 277
Coasting Arc #7 (Orbit 60)
---------------------------------------
Vector Time (GMT): 2010/043/03:54:33
157
Vector Time (MET): 003/18:40:26
177
Weight (LBS) : 246615
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3519993
91 A = 6722031
15 meter
Y = 4755021
72 meter E =
0009896
Z = -3178153
77 I = 51
80805
XDOT = -5892
622263 Wp = 342
12468
YDOT = -1132
213194 meter/sec RA = 151
51110 deg
ZDOT = 4837
740008 TA = 340
85283
MA = 340
89000
Ha = 188
076 n
mi
Hp = 181
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11548536
45 X = -3557492
21
Y = 15600464
96 feet Y = 4715429
33 meter
Z = -10427013
68 Z = -3195344
35
XDOT = -19332
750208 XDOT = -5903
017013
YDOT = -3714
610215 feet/sec YDOT = -1198
199757 meter/sec
ZDOT = 15871
850421 ZDOT = 4809
089283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5470671
33 X = 1667460
62
Y = -18584709
54 feet Y = -5664619
47 meter
Z = -10495053
20 Z = -3198892
22
XDOT = 18171
295954 XDOT = 5538
611007
YDOT = -3540
120304 feet/sec YDOT = -1079
028669 meter/sec
ZDOT = 15758
088101 ZDOT = 4803
065253
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 10043
16946607
00020000 00000-0 20000-3 0 9062
2 36394 51
6440 152
5064 0011574 318
6853 41
3435 15
75996520 618
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10043
16946607 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 152
5064 deg
Eccentricity:
0011574
Arg of perigee: 318
6853 deg
Mean anomaly: 41
3435 deg
Mean motion: 15
75996520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 61
Checksum: 287
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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