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
049/07:10:38
104 -0
1 0
6 0
6
009/21:56:31
123 0
6 -0
0 188
8
000/00:00:02
246 -0
2 0
0 180
6
049/08:10:37
680 0
3 0
4 0
4
009/22:56:30
700 -0
2 -0
0 190
4
000/00:00:01
399 -0
1 0
0 180
8
051/00:10:07
260 -0
1 -0
1 0
1
011/14:56:00
279 -0
1 0
1 190
7
000/00:00:00
559 0
1 0
0 180
2
051/02:09:12
568 0
2 -0
0 3
0
011/16:55:05
588 2
6 -0
0 190
3
000/00:00:11
175 -1
4 -3
0 180
4
051/02:37:12
566 -0
6 -3
0 3
0
011/17:23:05
585 2
9 0
0 189
2
000/00:00:11
171 -0
6 0
0 180
2
Coasting Arc #1 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2010/048/12:32:00
000
Vector Time (MET): 009/03:17:53
019
Weight (LBS) : 210299
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1525237
31 A = 6722788
77 meter
Y = -5984708
98 meter E =
0012022
Z = 2659332
54 I = 51
93377
XDOT = 5567
249242 Wp = 49
57475
YDOT = -918
540055 meter/sec RA = 124
00518 deg
ZDOT = -5237
149911 TA = 100
27082
MA = 100
13524
Ha = 188
642 n
mi
Hp = 180
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5004059
41 X = 1579161
63
Y = -19634871
98 feet Y = -5967342
40 meter
Z = 8724844
29 Z = 2666873
30
XDOT = 18265
253418 XDOT = 5602
552325
YDOT = -3013
582858 feet/sec YDOT = -856
054872 meter/sec
ZDOT = -17182
250364 ZDOT = -5210
018872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12893972
57 X = 3930082
84
Y = -15613937
98 feet Y = -4759128
29 meter
Z = 8754549
01 Z = 2668386
54
XDOT = 16745
428936 XDOT = 5104
006740
YDOT = 4212
627671 feet/sec YDOT = 1284
008914 meter/sec
ZDOT = -17074
566169 ZDOT = -5204
327768
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 10048
55930782
00020000 00000-0 20000-3 0 9001
2 36394 51
6457 124
7563 0011478 338
1816 21
8859 15
76213317 1464
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10048
55930782 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 124
7563 deg
Eccentricity:
0011478
Arg of perigee: 338
1816 deg
Mean anomaly: 21
8859 deg
Mean motion: 15
76213317 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 146
Checksum: 302
Coasting Arc #2 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2010/049/07:10:39
227
Vector Time (MET): 009/21:56:32
246
Weight (LBS) : 210200
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4779737
71 A = 6717015
57 meter
Y = -1041169
48 meter E =
0015149
Z = -4614821
04 I = 51
92403
XDOT = -1352
313990 Wp = 22
99768
YDOT = 6970
794664 meter/sec RA = 120
05970 deg
ZDOT = -2962
960984 TA = 217
66139
MA = 217
76755
Ha = 188
757 n
mi
Hp = 180
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15681554
16 X = 4813448
29
Y = -3415910
38 feet Y = -987504
06 meter
Z = -15140488
97 Z = -4591519
46
XDOT = -4436
725689 XDOT = -1415
808379
YDOT = 22870
061232 feet/sec YDOT = 6955
309261 meter/sec
ZDOT = -9721
000603 ZDOT = -2969
684980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -771548
48 X = -235167
98
Y = 16117570
77 feet Y = 4912635
57 meter
Z = -15048010
37 Z = -4586633
56
XDOT = -19788
189387 XDOT = -6031
440125
YDOT = -10079
876131 feet/sec YDOT = -3072
346245 meter/sec
ZDOT = -9747
430694 ZDOT = -2971
016876
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 10049
32011923
00020000 00000-0 20000-3 0 9015
2 36394 51
6440 120
8331 0011114 339
3022 20
7690 15
76115591 1584
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10049
32011923 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 120
8331 deg
Eccentricity:
0011114
Arg of perigee: 339
3022 deg
Mean anomaly: 20
7690 deg
Mean motion: 15
76115591 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 158
Checksum: 246
Coasting Arc #3 (Orbit 158)
---------------------------------------
Vector Time (GMT): 2010/049/08:10:38
380
Vector Time (MET): 009/22:56:31
399
Weight (LBS) : 210191
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1656367
27 A = 6718493
19 meter
Y = -4512192
30 meter E =
0016008
Z = 4697250
68 I = 51
92416
XDOT = 5290
774145 Wp = 15
54916
YDOT = -4854
602237 meter/sec RA = 119
80255 deg
ZDOT = -2780
420363 TA = 101
84443
MA = 101
66485
Ha = 190
394 n
mi
Hp = 180
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5434275
81 X = -1628580
34
Y = -14803780
52 feet Y = -4530568
55 meter
Z = 15410927
43 Z = 4689271
85
XDOT = 17358
182891 XDOT = 5358
199824
YDOT = -15927
172692 feet/sec YDOT = -4795
030499 meter/sec
ZDOT = -9122
114051 ZDOT = -2754
554135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14796284
01 X = 4509907
37
Y = -5543824
97 feet Y = -1689757
85 meter
Z = 15379074
74 Z = 4687541
98
XDOT = 15545
570598 XDOT = 4738
289918
YDOT = 16311
954825 feet/sec YDOT = 4971
883831 meter/sec
ZDOT = -9019
598358 ZDOT = -2749
173580
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 10049
38355003
00020000 00000-0 20000-3 0 9022
2 36394 51
6448 120
5063 0012114 347
1522 12
9332 15
75449431 1593
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10049
38355003 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 120
5063 deg
Eccentricity:
0012114
Arg of perigee: 347
1522 deg
Mean anomaly: 12
9332 deg
Mean motion: 15
75449431 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 159
Checksum: 262
Coasting Arc #4 (Orbit 174)
---------------------------------------
Vector Time (GMT): 2010/050/08:15:18
369
Vector Time (MET): 010/23:01:11
388
Weight (LBS) : 210191
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4687452
55 A = 6720407
55 meter
Y = 2463987
84 meter E =
0012463
Z = 4124288
98 I = 51
94638
XDOT = -186
597812 Wp = 40
90394
YDOT = -6707
902543 meter/sec RA = 114
70685 deg
ZDOT = 3798
263557 TA = 10
38581
MA = 10
36008
Ha = 190
476 n
mi
Hp = 180
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15378781
33 X = -4734705
48
Y = 8083949
61 feet Y = 2411279
10 meter
Z = 13531131
82 Z = 4101402
72
XDOT = -612
197545 XDOT = -129
987903
YDOT = -22007
554275 feet/sec YDOT = -6709
673442 meter/sec
ZDOT = 12461
494610 ZDOT = 3797
494801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8679455
70 X = -2645498
10
Y = -15131845
49 feet Y = -4612186
51 meter
Z = 13440349
16 Z = 4096618
43
XDOT = 20860
513768 XDOT = 6358
284597
YDOT = -908
047715 feet/sec YDOT = -276
772943 meter/sec
ZDOT = 12458
194654 ZDOT = 3797
257731
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 10050
39840945
00020000 00000-0 20000-3 0 9030
2 36394 51
6456 115
2833 0012188 350
3932 9
6997 15
75561887 1758
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10050
39840945 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 115
2833 deg
Eccentricity:
0012188
Arg of perigee: 350
3932 deg
Mean anomaly: 9
6997 deg
Mean motion: 15
75561887 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 175
Checksum: 315
Coasting Arc #5 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2010/051/00:10:07
540
Vector Time (MET): 011/14:56:00
559
Weight (LBS) : 210187
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4208798
07 A = 6723839
27 meter
Y = -4302628
76 meter E =
0011527
Z = -3013406
97 I = 51
96667
XDOT = 2041
341094 Wp = 13
42001
YDOT = 5491
669296 meter/sec RA = 111
31251 deg
ZDOT = -4982
865229 TA = 201
21739
MA = 201
26523
Ha = 190
670 n
mi
Hp = 180
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13808392
61 X = 4271260
68
Y = -14116236
08 feet Y = -4255190
18 meter
Z = -9886505
79 Z = -2992809
00
XDOT = 6697
313301 XDOT = 2003
954822
YDOT = 18017
287716 feet/sec YDOT = 5514
299139 meter/sec
ZDOT = -16347
983034 ZDOT = -4973
039421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18912799
19 X = -5764621
19
Y = 5818365
73 feet Y = 1773437
87 meter
Z = -9804869
77 Z = -2988524
31
XDOT = 3021
958172 XDOT = 921
092851
YDOT = -17699
884962 feet/sec YDOT = -5394
924936 meter/sec
ZDOT = -16308
769970 ZDOT = -4970
913087
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 10051
03268271
00020000 00000-0 20000-3 0 9049
2 36394 51
6463 112
0238 0012886 352
9621 7
1360 15
75566693 1856
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
03268271 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 112
0238 deg
Eccentricity:
0012886
Arg of perigee: 352
9621 deg
Mean anomaly: 7
1360 deg
Mean motion: 15
75566693 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 185
Checksum: 282
Coasting Arc #6 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2010/051/02:09:18
156
Vector Time (MET): 011/16:55:11
175
Weight (LBS) : 210114
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 318731
59 A = 6723479
45 meter
Y = 5955990
36 meter E =
0013407
Z = -3089086
48 I = 51
96434
XDOT = -5204
148653 Wp = 8
21878
YDOT = 2828
080087 meter/sec RA = 110
83765 deg
ZDOT = 4931
363344 TA = 316
05624
MA = 316
16277
Ha = 190
320 n
mi
Hp = 180
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1045707
33 X = 267079
15
Y = 19540650
78 feet Y = 5959267
40 meter
Z = -10134798
17 Z = -3087663
69
XDOT = -17073
978519 XDOT = -5259
357171
YDOT = 9278
477976 feet/sec YDOT = 2769
545864 meter/sec
ZDOT = 16179
013596 ZDOT = 4905
947662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1603965
07 X = -488888
55
Y = -19505810
00 feet Y = -5945370
89 meter
Z = -10128935
92 Z = -3087299
67
XDOT = 15503
768251 XDOT = 4725
548563
YDOT = -9597
374973 feet/sec YDOT = -2925
279892 meter/sec
ZDOT = 16078
193714 ZDOT = 4900
633444
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 10051
09610765
00020000 00000-0 20000-3 0 9055
2 36394 51
6439 111
6954 0012375 348
3703 11
7173 15
75594457 1865
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
09610765 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 111
6954 deg
Eccentricity:
0012375
Arg of perigee: 348
3703 deg
Mean anomaly: 11
7173 deg
Mean motion: 15
75594457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 186
Checksum: 297
Coasting Arc #7 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2010/051/02:37:18
152
Vector Time (MET): 011/17:23:11
171
Weight (LBS) : 210041
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4357062
68 A = 6714907
96 meter
Y = 220329
78 meter E =
0008657
Z = 5103158
73 I = 51
94020
XDOT = 1475
680743 Wp = 356
07226
YDOT = -7394
716012 meter/sec RA = 110
77528 deg
ZDOT = 1587
808022 TA = 78
80563
MA = 78
70833
Ha = 189
194 n
mi
Hp = 180
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14294825
08 X = -4383993
60
Y = 722866
73 feet Y = 171431
18 meter
Z = 16742646
75 Z = 5081926
89
XDOT = 4841
472253 XDOT = 1550
588850
YDOT = -24260
879306 feet/sec YDOT = -7377
786600 meter/sec
ZDOT = 5209
343903 ZDOT = 1595
158918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14128813
95 X = 4306462
49
Y = -2838462
95 feet Y = -865163
51 meter
Z = 16658347
00 Z = 5077464
17
XDOT = -1386
408081 XDOT = -422
577183
YDOT = 23674
707623 feet/sec YDOT = 7216
050883 meter/sec
ZDOT = 5238
269179 ZDOT = 1596
624446
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 10051
15951201
00020000 00000-0 20000-3 0 9066
2 36394 51
6436 111
3684 0012400 338
3574 21
7064 15
76115805 1871
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
15951201 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 111
3684 deg
Eccentricity:
0012400
Arg of perigee: 338
3574 deg
Mean anomaly: 21
7064 deg
Mean motion: 15
76115805 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 187
Checksum: 264
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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