Date:
April 6th 2010
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
095/13:08:00
410 24
4 97
8 97
8
000/02:46:35
454 -67
9 0
0 180
0
000/00:01:05
107 66
0 -0
0 138
7
096/01:56:35
624 -14
7 61
6 61
6
000/15:35:10
668 42
2 -0
0 181
0
000/00:00:41
664 -42
4 0
0 171
5
096/13:34:45
819 3
9 3
0 4
0
001/03:13:20
863 -0
5 2
6 181
7
000/00:00:17
386 0
3 0
0 172
7
097/03:35:14
771 6
1 20
6 20
6
001/17:13:49
815 18
4 0
0 184
1
000/00:00:15
672 -7
2 0
0 181
6
097/05:06:50
920 2
5 8
9 8
9
001/18:45:25
964 7
9 -0
1 189
2
000/00:00:13
928 -3
2 0
0 181
8
097/06:23:44
350 1
7 2
5 2
9
001/20:02:19
393 2
4 -0
0 190
8
000/00:00:12
787 -0
0 1
5 181
9
Coasting Arc #1 (Orbit 2)
---------------------------------------
Vector Time (GMT): 2010/095/11:58:54
000
Vector Time (MET): 000/01:37:29
044
Weight (LBS) : 251459
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 973839
20 A = 6621365
36 meter
Y = -5180578
05 meter E =
0025765
Z = 4021952
21 I = 51
34158
XDOT = 5443
680414 Wp = 173
26347
YDOT = 3995
064543 meter/sec RA = 243
03058 deg
ZDOT = 3800
003056 TA = 237
70476
MA = 237
95460
Ha = 140
347 n
mi
Hp = 123
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3195010
49 X = 1012159
11
Y = -16996647
14 feet Y = -5169473
70 meter
Z = 13195381
28 Z = 4026776
25
XDOT = 17859
843878 XDOT = 5380
142623
YDOT = 13107
167136 feet/sec YDOT = 4055
583795 meter/sec
ZDOT = 12467
201627 ZDOT = 3826
294006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -675481
28 X = -205886
69
Y = -17266617
84 feet Y = -5262865
12 meter
Z = 13214379
54 Z = 4027742
88
XDOT = 18963
208370 XDOT = 5779
985911
YDOT = 8949
346826 feet/sec YDOT = 2727
760913 meter/sec
ZDOT = 12571
775776 ZDOT = 3831
877257
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 10095
55248149
00020000 00000-0 20000-3 0 9007
2 36507 51
6471 243
6078 0024117 198
0006 162
0325 16
11086581 35
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10095
55248149 = yrday
fracday
Element set: 900
Inclination: 51
6471 deg
RA of node: 243
6078 deg
Eccentricity:
0024117
Arg of perigee: 198
0006 deg
Mean anomaly: 162
0325 deg
Mean motion: 16
11086581 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3
Checksum: 260
Coasting Arc #2 (Orbit 2)
---------------------------------------
Vector Time (GMT): 2010/095/13:08:32
963
Vector Time (MET): 000/02:47:08
007
Weight (LBS) : 249052
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4413423
41 A = 6677361
20 meter
Y = -4319303
98 meter E =
0063315
Z = -2430164
53 I = 51
35993
XDOT = 2132
471779 Wp = 318
21401
YDOT = -5212
083895 meter/sec RA = 242
71917 deg
ZDOT = 5359
094900 TA = 13
82782
MA = 13
65521
Ha = 179
982 n
mi
Hp = 138
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14479735
58 X = -4352990
89
Y = -14170944
82 feet Y = -4368319
64 meter
Z = -7972980
74 Z = -2451458
04
XDOT = 6996
298489 XDOT = 2164
562305
YDOT = -17100
012780 feet/sec YDOT = -5188
057843 meter/sec
ZDOT = 17582
332349 ZDOT = 5369
532421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19592753
79 X = -5971871
36
Y = -5024351
50 feet Y = -1531422
34 meter
Z = -8057712
60 Z = -2455990
80
XDOT = -2976
682927 XDOT = -907
292956
YDOT = -16822
055387 feet/sec YDOT = -5127
362482 meter/sec
ZDOT = 17623
630148 ZDOT = 5371
682469
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 10095
55246607
00020000 00000-0 20000-3 0 9015
2 36507 51
6490 243
6089 0063594 313
1960 46
3910 15
92496979 37
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10095
55246607 = yrday
fracday
Element set: 901
Inclination: 51
6490 deg
RA of node: 243
6089 deg
Eccentricity:
0063594
Arg of perigee: 313
1960 deg
Mean anomaly: 46
3910 deg
Mean motion: 15
92496979 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3
Checksum: 300
Coasting Arc #3 (Orbit 11)
---------------------------------------
Vector Time (GMT): 2010/096/01:56:56
456
Vector Time (MET): 000/15:35:31
500
Weight (LBS) : 247548
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4642090
51 A = 6709772
62 meter
Y = 4227486
14 meter E =
0008050
Z = 2372053
98 I = 51
36807
XDOT = -1967
054426 Wp = 264
36107
YDOT = 5163
884693 meter/sec RA = 239
89780 deg
ZDOT = -5369
950927 TA = 248
73978
MA = 248
82576
Ha = 180
961 n
mi
Hp = 171
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15229955
73 X = 4582950
03
Y = 13869705
17 feet Y = 4279066
12 meter
Z = 7782329
34 Z = 2394461
44
XDOT = -6453
590638 XDOT = -1998
565579
YDOT = 16941
878914 feet/sec YDOT = 5141
711647 meter/sec
ZDOT = -17617
949236 ZDOT = -5379
583456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20564835
11 X = -6268161
74
Y = 110095
10 feet Y = 33556
99 meter
Z = 7871490
27 Z = 2399230
23
XDOT = -6819
466594 XDOT = -2078
573418
YDOT = -15255
013607 feet/sec YDOT = -4649
728147 meter/sec
ZDOT = -17656
049432 ZDOT = -5381
563867
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 10096
11753240
00020000 00000-0 20000-3 0 9025
2 36507 51
6488 240
6355 0021653 278
0979 81
7732 15
81011854 124
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10096
11753240 = yrday
fracday
Element set: 902
Inclination: 51
6488 deg
RA of node: 240
6355 deg
Eccentricity:
0021653
Arg of perigee: 278
0979 deg
Mean anomaly: 81
7732 deg
Mean motion: 15
81011854 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 12
Checksum: 277
Coasting Arc #4 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2010/096/13:34:54
513
Vector Time (MET): 001/03:13:29
556
Weight (LBS) : 247435
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1025246
31 A = 6710043
76 meter
Y = -5948345
94 meter E =
0009645
Z = 2928030
95 I = 51
36747
XDOT = 5681
850443 Wp = 315
45299
YDOT = 1472
452614 meter/sec RA = 237
40962 deg
ZDOT = 4997
496271 TA = 78
51402
MA = 78
40573
Ha = 181
666 n
mi
Hp = 172
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3363669
01 X = -972878
41
Y = -19515570
66 feet Y = -5959517
98 meter
Z = 9606400
74 Z = 2923177
66
XDOT = 18641
241612 XDOT = 5640
686128
YDOT = 4830
881281 feet/sec YDOT = 1535
760393 meter/sec
ZDOT = 16395
985141 ZDOT = 5024
998523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14637199
31 X = -4461418
35
Y = -13352829
46 feet Y = -4069942
42 meter
Z = 9586920
48 Z = 2922093
36
XDOT = 16655
259983 XDOT = 5076
523243
YDOT = -6446
376803 feet/sec YDOT = -1964
855650 meter/sec
ZDOT = 16505
302445 ZDOT = 5030
816185
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 10096
62321501
00020000 00000-0 20000-3 0 9033
2 36507 51
6448 238
0033 0020702 284
3303 75
5565 15
80486067 204
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10096
62321501 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 238
0033 deg
Eccentricity:
0020702
Arg of perigee: 284
3303 deg
Mean anomaly: 75
5565 deg
Mean motion: 15
80486067 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 20
Checksum: 255
Coasting Arc #5 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2010/097/03:35:22
607
Vector Time (MET): 001/17:13:57
651
Weight (LBS) : 246933
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4811024
88 A = 6715062
51 meter
Y = 292364
64 meter E =
0003440
Z = 4675389
49 I = 51
35724
XDOT = 2235
531379 Wp = 29
43821
YDOT = 6851
112823 meter/sec RA = 234
33168 deg
ZDOT = -2725
000638 TA = 87
50684
MA = 87
46746
Ha = 184
116 n
mi
Hp = 181
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15784202
35 X = 4784685
99
Y = 959201
58 feet Y = 346017
26 meter
Z = 15339204
36 Z = 4698697
31
XDOT = 7334
420536 XDOT = 2171
992334
YDOT = 22477
404274 feet/sec YDOT = 6875
756515 meter/sec
ZDOT = -8940
290807 ZDOT = -2714
295044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6674584
28 X = -2034413
29
Y = 14235908
29 feet Y = 4339104
85 meter
Z = 15431822
38 Z = 4703619
46
XDOT = -22579
451262 XDOT = -6882
216745
YDOT = -928
081293 feet/sec YDOT = -282
879178 meter/sec
ZDOT = -8897
521961 ZDOT = -2711
964694
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 10097
19241874
00020000 00000-0 20000-3 0 9041
2 36507 51
6445 235
0586 0005188 263
0566 97
0008 15
76625058 297
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10097
19241874 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 235
0586 deg
Eccentricity:
0005188
Arg of perigee: 263
0566 deg
Mean anomaly: 97
0008 deg
Mean motion: 15
76625058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 29
Checksum: 296
Coasting Arc #6 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2010/097/05:06:57
884
Vector Time (MET): 001/18:45:32
928
Weight (LBS) : 246715
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4854445
65 A = 6719940
61 meter
Y = 394339
07 meter E =
0008140
Z = 4622850
90 I = 51
36001
XDOT = 2155
303020 Wp = 91
56144
YDOT = 6832
288492 meter/sec RA = 234
00210 deg
ZDOT = -2842
006192 TA = 26
62947
MA = 26
58768
Ha = 189
214 n
mi
Hp = 181
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15926658
95 X = 4827218
46
Y = 1293763
37 feet Y = 448472
28 meter
Z = 15166833
67 Z = 4646367
50
XDOT = 7071
204133 XDOT = 2092
548822
YDOT = 22415
644659 feet/sec YDOT = 6856
039405 meter/sec
ZDOT = -9324
167295 ZDOT = -2831
688445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -923746
69 X = -281557
99
Y = 15863023
71 feet Y = 4835049
63 meter
Z = 15260285
18 Z = 4651334
92
XDOT = -21086
043430 XDOT = -6427
026037
YDOT = 7715
126908 feet/sec YDOT = 2351
570681 meter/sec
ZDOT = -9282
939362 ZDOT = -2829
439917
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 10097
25585960
00020000 00000-0 20000-3 0 9056
2 36507 51
6454 234
7323 0003930 165
9080 194
2194 15
74983928 305
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10097
25585960 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 234
7323 deg
Eccentricity:
0003930
Arg of perigee: 165
9080 deg
Mean anomaly: 194
2194 deg
Mean motion: 15
74983928 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 30
Checksum: 299
Coasting Arc #7 (Orbit 30)
---------------------------------------
Vector Time (GMT): 2010/097/06:23:50
743
Vector Time (MET): 001/20:02:25
787
Weight (LBS) : 246632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1032957
28 A = 6721715
02 meter
Y = -4796538
06 meter E =
0012677
Z = 4588522
94 I = 51
36062
XDOT = 5863
601286 Wp = 123
40411
YDOT = 4062
015260 meter/sec RA = 233
76981 deg
ZDOT = 2913
493818 TA = 297
57856
MA = 297
70726
Ha = 190
760 n
mi
Hp = 181
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3388967
46 X = 1064226
19
Y = -15736673
43 feet Y = -4784811
93 meter
Z = 15054209
11 Z = 4593617
12
XDOT = 19237
537029 XDOT = 5803
590174
YDOT = 13326
821719 feet/sec YDOT = 4127
250092 meter/sec
ZDOT = 9558
706752 ZDOT = 2941
833104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15890794
25 X = 4843514
09
Y = -2450664
33 feet Y = -746962
49 meter
Z = 15074286
23 Z = 4594642
44
XDOT = -5900
338322 XDOT = -1798
423121
YDOT = 21485
913890 feet/sec YDOT = 6548
906554 meter/sec
ZDOT = 9671
445725 ZDOT = 2947
856657
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 10097
31933126
00020000 00000-0 20000-3 0 9065
2 36507 51
6444 234
4056 0004541 137
7553 222
3961 15
74445444 317
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10097
31933126 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 234
4056 deg
Eccentricity:
0004541
Arg of perigee: 137
7553 deg
Mean anomaly: 222
3961 deg
Mean motion: 15
74445444 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 31
Checksum: 270
Coasting Arc #8 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2010/098/06:24:46
078
Vector Time (MET): 002/20:03:21
122
Weight (LBS) : 246632
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5336582
62 A = 6728818
90 meter
Y = -3529866
54 meter E =
0006946
Z = -2086094
47 I = 51
40320
XDOT = 1288
430721 Wp = 79
39846
YDOT = -5201
813565 meter/sec RA = 228
56688 deg
ZDOT = 5522
751693 TA = 257
23481
MA = 257
31245
Ha = 190
563 n
mi
Hp = 181
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17508473
17 X = -5286580
59
Y = -11580926
97 feet Y = -3589263
91 meter
Z = -6844141
95 Z = -2111897
79
XDOT = 4227
134912 XDOT = 1319
674218
YDOT = -17066
317469 feet/sec YDOT = -5187
230605 meter/sec
ZDOT = 18119
264084 ZDOT = 5529
086991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4255655
43 X = 1297123
78
Y = -20521651
15 feet Y = -6254999
27 meter
Z = -6946798
71 Z = -2117384
25
XDOT = 15877
888058 XDOT = 4839
580280
YDOT = -2830
958506 feet/sec YDOT = -862
876153 meter/sec
ZDOT = 18144
254071 ZDOT = 5530
368641
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 10098
27137874
00020000 00000-0 20000-3 0 9078
2 36507 51
6435 229
5125 0004362 143
2969 216
8494 15
74492395 465
Satellite: SHUTTLE
Catalog Number: 36507
Epoch time: 10098
27137874 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 229
5125 deg
Eccentricity:
0004362
Arg of perigee: 143
2969 deg
Mean anomaly: 216
8494 deg
Mean motion: 15
74492395 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 46
Checksum: 311
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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