Date:
February 15th 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
050/05:59:38
107 -0
1 0
6 0
6
010/20:45:31
126 0
6 -0
0 188
9
000/00:00:02
253 -0
2 0
0 180
3
050/07:10:37
682 0
3 0
4 0
4
010/21:56:30
702 0
0 -0
0 190
6
000/00:00:01
403 -0
3 0
0 180
7
051/00:10:07
266 -0
1 -0
1 0
2
011/14:56:00
285 -0
1 0
0 190
9
000/00:00:00
570 0
1 0
0 180
4
051/02:09:12
585 0
1 -0
0 3
0
011/16:55:05
604 2
7 -0
0 190
5
000/00:00:11
208 -1
3 -3
0 180
7
051/02:37:06
980 -0
6 -3
0 3
0
011/17:22:59
999 2
9 0
0 189
4
000/00:00:11
203 -0
6 -0
0 180
5
Coasting Arc #1 (Orbit 89)
---------------------------------------
Vector Time (GMT): 2010/045/00:03:45
999
Vector Time (MET): 005/14:49:39
018
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3007035
49 A = 6722795
37 meter
Y = 5248225
54 meter E =
0011423
Z = -2917818
44 I = 51
85904
XDOT = -5796
600571 Wp = 347
74482
YDOT = -515
011594 meter/sec RA = 142
07050 deg
ZDOT = 5054
846033 TA = 338
72143
MA = 338
76890
Ha = 188
399 n
mi
Hp = 181
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9865602
01 X = -3051354
45
Y = 17218587
74 feet Y = 5214334
01 meter
Z = -9572895
13 Z = -2932533
90
XDOT = -19017
718410 XDOT = -5814
962300
YDOT = -1689
670584 feet/sec YDOT = -579
968236 meter/sec
ZDOT = 16584
140529 ZDOT = 5026
642402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18045085
08 X = 5500141
93
Y = -8189447
63 feet Y = -2496143
64 meter
Z = -9631097
54 Z = -2935558
53
XDOT = 13891
676505 XDOT = 4234
182999
YDOT = 11265
990997 feet/sec YDOT = 3433
874056 meter/sec
ZDOT = 16472
159984 ZDOT = 5020
714363
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 10045
00857703
00020000 00000-0 20000-3 0 9009
2 36394 51
6459 143
0443 0011537 324
5250 35
5143 15
75975778 905
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10045
00857703 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 143
0443 deg
Eccentricity:
0011537
Arg of perigee: 324
5250 deg
Mean anomaly: 35
5143 deg
Mean motion: 15
75975778 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 90
Checksum: 281
Coasting Arc #2 (Orbit 105)
---------------------------------------
Vector Time (GMT): 2010/046/00:08:46
485
Vector Time (MET): 006/14:54:39
504
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3366858
19 A = 6714464
23 meter
Y = 2499882
70 meter E =
0014314
Z = -5252551
91 I = 51
85512
XDOT = -5229
072072 Wp = 38
06305
YDOT = 5608
021239 meter/sec RA = 136
94809 deg
ZDOT = -672
678577 TA = 225
49828
MA = 225
61536
Ha = 188
597 n
mi
Hp = 181
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11046122
68 X = 3364154
65
Y = 8201714
88 feet Y = 2537536
76 meter
Z = -17232781
87 Z = -5236202
81
XDOT = -17155
748269 XDOT = -5288
157232
YDOT = 18399
019812 feet/sec YDOT = 5549
186353 meter/sec
ZDOT = -2206
950712 ZDOT = -698
224414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4728267
05 X = -1441175
80
Y = -13006333
15 feet Y = -3964330
34 meter
Z = -17167775
42 Z = -5232737
95
XDOT = 23519
758038 XDOT = 7168
822250
YDOT = -5459
879959 feet/sec YDOT = -1664
171412 meter/sec
ZDOT = -2308
137953 ZDOT = -703
520448
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 10046
02312372
00020000 00000-0 20000-3 0 9011
2 36394 51
6465 137
8195 0011569 328
9204 31
1275 15
76037389 1063
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10046
02312372 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 137
8195 deg
Eccentricity:
0011569
Arg of perigee: 328
9204 deg
Mean anomaly: 31
1275 deg
Mean motion: 15
76037389 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 106
Checksum: 281
Coasting Arc #3 (Orbit 121)
---------------------------------------
Vector Time (GMT): 2010/047/00:13:41
578
Vector Time (MET): 007/14:59:34
597
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5286853
00 A = 6724882
82 meter
Y = -3719166
28 meter E =
0004614
Z = -1864550
98 I = 51
91181
XDOT = 1503
893897 Wp = 348
92798
YDOT = 4983
068835 meter/sec RA = 131
80822 deg
ZDOT = -5668
625316 TA = 211
69002
MA = 211
71780
Ha = 188
675 n
mi
Hp = 180
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17345318
24 X = 5337126
71
Y = -12201989
11 feet Y = -3659734
32 meter
Z = -6117293
25 Z = -1838745
77
XDOT = 4934
035094 XDOT = 1475
568641
YDOT = 16348
651034 feet/sec YDOT = 4999
736115 meter/sec
ZDOT = -18597
852086 ZDOT = -5661
388593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21194381
24 X = -6460047
40
Y = 1337138
35 feet Y = 407559
77 meter
Z = -6014993
35 Z = -1833369
97
XDOT = 4327
925221 XDOT = 1319
151607
YDOT = -15031
632698 feet/sec YDOT = -4581
641646 meter/sec
ZDOT = -18568
920206 ZDOT = -5659
806879
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 10047
03763894
00020000 00000-0 20000-3 0 9023
2 36394 51
6467 132
5943 0011589 332
1959 27
8584 15
76049932 1224
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10047
03763894 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 132
5943 deg
Eccentricity:
0011589
Arg of perigee: 332
1959 deg
Mean anomaly: 27
8584 deg
Mean motion: 15
76049932 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 122
Checksum: 314
Coasting Arc #4 (Orbit 137)
---------------------------------------
Vector Time (GMT): 2010/048/00:18:11
137
Vector Time (MET): 008/15:04:04
156
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 591860
17 A = 6720301
01 meter
Y = -5606918
12 meter E =
0013870
Z = 3661404
61 I = 51
91593
XDOT = 5930
113839 Wp = 31
68833
YDOT = -2239
577574 meter/sec RA = 126
61695 deg
ZDOT = -4369
200608 TA = 104
52695
MA = 104
37305
Ha = 188
795 n
mi
Hp = 180
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1941798
47 X = 636759
49
Y = -18395400
65 feet Y = -5600044
86 meter
Z = 12012482
33 Z = 3664389
16
XDOT = 19455
754066 XDOT = 5975
953204
YDOT = -7347
695454 feet/sec YDOT = -2172
973576 meter/sec
ZDOT = -14334
647665 ZDOT = -4340
281207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10646873
25 X = -3245166
97
Y = 15117075
33 feet Y = 4607684
56 meter
Z = 12024109
19 Z = 3664948
48
XDOT = -19530
878860 XDOT = -5953
011876
YDOT = -2395
482546 feet/sec YDOT = -730
143080 meter/sec
ZDOT = -14219
918129 ZDOT = -4334
231046
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
05212214
00020000 00000-0 20000-3 0 9032
2 36394 51
6461 127
3689 0011697 336
9366 23
1272 15
76122317 1380
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10048
05212214 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 127
3689 deg
Eccentricity:
0011697
Arg of perigee: 336
9366 deg
Mean anomaly: 23
1272 deg
Mean motion: 15
76122317 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 138
Checksum: 279
Coasting Arc #5 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2010/049/00:23:01
671
Vector Time (MET): 009/15:08:54
690
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4393966
27 A = 6714951
83 meter
Y = -416609
85 meter E =
0007976
Z = 5058172
48 I = 51
91566
XDOT = 2679
890492 Wp = 3
46146
YDOT = -7008
516395 meter/sec RA = 121
50792 deg
ZDOT = 1758
388182 TA = 69
73075
MA = 69
64503
Ha = 189
002 n
mi
Hp = 180
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14415899
83 X = -4413549
77
Y = -1366830
21 feet Y = -465880
09 meter
Z = 16595054
08 Z = 5036779
36
XDOT = 8792
291639 XDOT = 2749
559681
YDOT = -22993
820193 feet/sec YDOT = -6978
143200 meter/sec
ZDOT = 5768
990097 ZDOT = 1771
576457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12290608
00 X = 3746177
32
Y = 7838356
77 feet Y = 2389131
14 meter
Z = 16510097
84 Z = 5032277
82
XDOT = -17713
887048 XDOT = -5399
192772
YDOT = 15567
594823 feet/sec YDOT = 4745
002902 meter/sec
ZDOT = 5821
082076 ZDOT = 1774
265817
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
06657311
00020000 00000-0 20000-3 0 9046
2 36394 51
6465 122
1427 0011732 340
7007 19
3711 15
76169511 1542
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10049
06657311 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 122
1427 deg
Eccentricity:
0011732
Arg of perigee: 340
7007 deg
Mean anomaly: 19
3711 deg
Mean motion: 15
76169511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 154
Checksum: 265
Coasting Arc #6 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2010/050/00:28:02
351
Vector Time (MET): 010/15:13:55
370
Weight (LBS) : 210828
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3626539
80 A = 6725457
85 meter
Y = 5558440
85 meter E =
0020807
Z = 999893
19 I = 51
96607
XDOT = -3532
588261 Wp = 22
90949
YDOT = -3382
010451 meter/sec RA = 116
35393 deg
ZDOT = 5965
904628 TA = 347
99317
MA = 348
04269
Ha = 189
036 n
mi
Hp = 179
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11898096
44 X = -3693314
37
Y = 18236354
48 feet Y = 5517492
59 meter
Z = 3280489
46 Z = 982113
25
XDOT = -11589
856500 XDOT = -3523
468969
YDOT = -11095
834813 feet/sec YDOT = -3421
482806 meter/sec
ZDOT = 19573
177912 ZDOT = 5948
765786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18489034
58 X = 5635457
74
Y = -11521362
43 feet Y = -3511711
27 meter
Z = 3210100
16 Z = 978438
53
XDOT = 5103
051529 XDOT = 1555
410106
YDOT = 13644
587896 feet/sec YDOT = 4158
870391 meter/sec
ZDOT = 19504
999922 ZDOT = 5945
123976
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
08099214
00020000 00000-0 20000-3 0 9053
2 36394 51
6462 116
9163 0011877 344
2091 15
8701 15
76223032 1706
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10050
08099214 = yrday
fracday
Element set: 905
Inclination: 51
6462 deg
RA of node: 116
9163 deg
Eccentricity:
0011877
Arg of perigee: 344
2091 deg
Mean anomaly: 15
8701 deg
Mean motion: 15
76223032 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 170
Checksum: 266
Coasting Arc #7 (Orbit 172)
---------------------------------------
Vector Time (GMT): 2010/050/05:59:39
234
Vector Time (MET): 010/20:45:32
253
Weight (LBS) : 210813
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4694940
61 A = 6717379
28 meter
Y = -1677961
97 meter E =
0015386
Z = -4514211
60 I = 51
93769
XDOT = -551
341874 Wp = 22
91549
YDOT = 6991
965648 meter/sec RA = 115
18153 deg
ZDOT = -3162
104003 TA = 215
56530
MA = 215
66794
Ha = 188
924 n
mi
Hp = 180
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15403348
44 X = 4735293
17
Y = -5505124
56 feet Y = -1625208
06 meter
Z = -14810405
52 Z = -4491305
75
XDOT = -1808
864415 XDOT = -614
165269
YDOT = 22939
519844 feet/sec YDOT = 6985
445528 meter/sec
ZDOT = -10374
356964 ZDOT = -3164
935231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3476971
08 X = -1059780
78
Y = 16067487
39 feet Y = 4897370
16 meter
Z = -14719516
73 Z = -4486508
70
XDOT = -17408
762629 XDOT = -5306
190849
YDOT = -13312
348802 feet/sec YDOT = -4057
603915 meter/sec
ZDOT = -10385
339807 ZDOT = -3165
451573
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
27119372
00020000 00000-0 20000-3 0 9063
2 36394 51
6429 115
9320 0011225 343
2375 16
8417 15
76127194 1734
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10050
27119372 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 115
9320 deg
Eccentricity:
0011225
Arg of perigee: 343
2375 deg
Mean anomaly: 16
8417 deg
Mean motion: 15
76127194 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 173
Checksum: 274
Coasting Arc #8 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2010/050/07:10:38
384
Vector Time (MET): 010/21:56:31
403
Weight (LBS) : 210804
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1258295
25 A = 6726610
08 meter
Y = -6318351
86 meter E =
0012719
Z = 1939709
33 I = 51
96263
XDOT = 5190
604605 Wp = 58
41764
YDOT = -707
433750 meter/sec RA = 114
88703 deg
ZDOT = -5638
100222 TA = 100
11050
MA = 99
96699
Ha = 190
627 n
mi
Hp = 180
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4128265
26 X = 1319467
87
Y = -20729500
84 feet Y = -6303931
42 meter
Z = 6363875
75 Z = 1945970
86
XDOT = 17029
542667 XDOT = 5225
521756
YDOT = -2320
976871 feet/sec YDOT = -649
164660 meter/sec
ZDOT = -18497
704141 ZDOT = -5612
799695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19126844
87 X = 5829862
32
Y = 8978001
31 feet Y = 2736494
80 meter
Z = 6388504
63 Z = 1947216
21
XDOT = -1233
360007 XDOT = -375
928130
YDOT = 15796
322582 feet/sec YDOT = 4814
719123 meter/sec
ZDOT = -18397
270646 ZDOT = -5607
488093
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
33462653
00020000 00000-0 20000-3 0 9074
2 36394 51
6431 115
6046 0012269 349
5551 10
5356 15
75378102 1743
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10050
33462653 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 115
6046 deg
Eccentricity:
0012269
Arg of perigee: 349
5551 deg
Mean anomaly: 10
5356 deg
Mean motion: 15
75378102 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 174
Checksum: 274
Coasting Arc #9 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2010/051/00:10:07
551
Vector Time (MET): 011/14:56:00
570
Weight (LBS) : 210800
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4258913
47 A = 6723908
63 meter
Y = -4161536
32 meter E =
0012051
Z = -3139098
56 I = 51
96518
XDOT = 1900
750711 Wp = 12
48384
YDOT = 5632
338237 meter/sec RA = 111
30743 deg
ZDOT = -4880
006597 TA = 203
82076
MA = 203
87659
Ha = 190
880 n
mi
Hp = 180
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13972813
22 X = 4320404
41
Y = -13653334
39 feet Y = -4113542
48 meter
Z = -10298879
80 Z = -3118259
50
XDOT = 6236
058762 XDOT = 1861
301448
YDOT = 18478
799990 feet/sec YDOT = 5653
383577 meter/sec
ZDOT = -16010
520331 ZDOT = -4870
868785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18839289
63 X = -5742215
48
Y = 5331860
42 feet Y = 1625151
06 meter
Z = -10216281
38 Z = -3113922
56
XDOT = 3613
495343 XDOT = 1101
393380
YDOT = -17890
766301 feet/sec YDOT = -5453
105569 meter/sec
ZDOT = -15974
034121 ZDOT = -4868
885600
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
03238958
00020000 00000-0 20000-3 0 9082
2 36394 51
6459 112
0198 0012972 352
0106 8
0849 15
75425805 1852
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
03238958 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 112
0198 deg
Eccentricity:
0012972
Arg of perigee: 352
0106 deg
Mean anomaly: 8
0849 deg
Mean motion: 15
75425805 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 185
Checksum: 291
Coasting Arc #10 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2010/051/02:09:18
189
Vector Time (MET): 011/16:55:11
208
Weight (LBS) : 210727
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 189498
51 A = 6724222
71 meter
Y = 6024197
57 meter E =
0013937
Z = -2965169
74 I = 51
96508
XDOT = -5212
256840 Wp = 6
26149
YDOT = 2632
353745 meter/sec RA = 110
83268 deg
ZDOT = 5030
663026 TA = 319
65094
MA = 319
75426
Ha = 190
550 n
mi
Hp = 180
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 621714
26 X = 136490
62
Y = 19764427
73 feet Y = 6026021
14 meter
Z = -9728247
19 Z = -2964378
05
XDOT = -17100
580183 XDOT = -5265
757370
YDOT = 8636
331185 feet/sec YDOT = 2573
738362 meter/sec
ZDOT = 16504
799953 ZDOT = 5005
212107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1183492
29 X = -360728
45
Y = -19740410
71 feet Y = -6016877
18 meter
Z = -9724888
50 Z = -2964146
02
XDOT = 15531
546521 XDOT = 4734
015380
YDOT = -8986
875294 feet/sec YDOT = -2739
199590 meter/sec
ZDOT = 16403
833162 ZDOT = 4999
888348
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
09582024
00020000 00000-0 20000-3 0 9095
2 36394 51
6435 111
6914 0012521 347
3169 12
7678 15
75447607 1860
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
09582024 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 111
6914 deg
Eccentricity:
0012521
Arg of perigee: 347
3169 deg
Mean anomaly: 12
7678 deg
Mean motion: 15
75447607 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 186
Checksum: 292
Coasting Arc #11 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2010/051/02:37:12
581
Vector Time (MET): 011/17:23:05
600
Weight (LBS) : 210654
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4328158
05 A = 6715191
09 meter
Y = 79050
07 meter E =
0009023
Z = 5132720
67 I = 51
93942
XDOT = 1584
146357 Wp = 352
98149
YDOT = -7398
195385 meter/sec RA = 110
76916 deg
ZDOT = 1458
799216 TA = 83
15638
MA = 83
05372
Ha = 189
447 n
mi
Hp = 180
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14199993
61 X = -4353654
10
Y = 259350
63 feet Y = 30482
90 meter
Z = 16839634
74 Z = 5111632
74
XDOT = 5197
330567 XDOT = 1659
712019
YDOT = -24272
294569 feet/sec YDOT = -7380
048753 meter/sec
ZDOT = 4786
086666 ZDOT = 1466
678630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14104918
50 X = 4299179
16
Y = -2360386
14 feet Y = -719445
70 meter
Z = 16755901
38 Z = 5107198
74
XDOT = -1714
341088 XDOT = -522
531163
YDOT = 23739
984779 feet/sec YDOT = 7235
947361 meter/sec
ZDOT = 4817
110475 ZDOT = 1468
255273
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
15923048
00020000 00000-0 20000-3 0 9109
2 36394 51
6432 111
3645 0012630 337
4792 22
5816 15
75970742 1873
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
15923048 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 111
3645 deg
Eccentricity:
0012630
Arg of perigee: 337
4792 deg
Mean anomaly: 22
5816 deg
Mean motion: 15
75970742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 187
Checksum: 279
Coasting Arc #12 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2010/052/02:42:09
376
Vector Time (MET): 012/17:28:02
395
Weight (LBS) : 210654
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2654774
36 A = 6725835
41 meter
Y = 6049417
34 meter E =
0020733
Z = 1186718
39 I = 51
98452
XDOT = -3991
601641 Wp = 21
57645
YDOT = -2916
096323 meter/sec RA = 105
62180 deg
ZDOT = 5922
085239 TA = 351
39204
MA = 351
42755
Ha = 189
432 n
mi
Hp = 180
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8709889
63 X = -2728021
76
Y = 19847169
75 feet Y = 6019305
22 meter
Z = 3893433
04 Z = 1173643
68
XDOT = -13095
805910 XDOT = -3987
447982
YDOT = -9567
245155 feet/sec YDOT = -2960
732233 meter/sec
ZDOT = 19429
413514 ZDOT = 5902
704316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4901309
12 X = 1493919
02
Y = -21122251
66 feet Y = -6438062
30 meter
Z = 3841718
24 Z = 1170955
72
XDOT = 13214
232225 XDOT = 4027
697982
YDOT = 6594
273926 feet/sec YDOT = 2009
934693 meter/sec
ZDOT = 19352
351695 ZDOT = 5898
596797
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 10052
17376058
00020000 00000-0 20000-3 0 9116
2 36394 51
6423 106
1381 0012594 340
9169 19
1522 15
76026239 2037
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10052
17376058 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 106
1381 deg
Eccentricity:
0012594
Arg of perigee: 340
9169 deg
Mean anomaly: 19
1522 deg
Mean motion: 15
76026239 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 203
Checksum: 270
Coasting Arc #13 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2010/053/02:47:02
127
Vector Time (MET): 013/17:32:55
146
Weight (LBS) : 210654
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2358229
92 A = 6719154
36 meter
Y = 4790800
72 meter E =
0010317
Z = -4074954
35 I = 51
96900
XDOT = -4055
259161 Wp = 21
69743
YDOT = 5281
825256 meter/sec RA = 100
43927 deg
ZDOT = 3875
312062 TA = 287
93159
MA = 288
04404
Ha = 189
555 n
mi
Hp = 179
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7736974
81 X = 2324250
84
Y = 15717850
12 feet Y = 4816995
23 meter
Z = -13369272
80 Z = -4063580
67
XDOT = -13304
656040 XDOT = -4132
875212
YDOT = 17328
823018 feet/sec YDOT = 5236
019626 meter/sec
ZDOT = 12714
278420 ZDOT = 3855
423380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11125631
23 X = -3391092
40
Y = -13577251
54 feet Y = -4138346
27 meter
Z = -13323949
02 Z = -4061139
66
XDOT = 8184
811812 XDOT = 2494
730640
YDOT = -19066
368442 feet/sec YDOT = -5811
429101 meter/sec
ZDOT = 12635
464493 ZDOT = 3851
289577
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 10053
12487293
00020000 00000-0 20000-3 0 9127
2 36394 51
6421 101
2384 0012475 344
8442 15
2346 15
76047357 2180
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10053
12487293 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 101
2384 deg
Eccentricity:
0012475
Arg of perigee: 344
8442 deg
Mean anomaly: 15
2346 deg
Mean motion: 15
76047357 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 218
Checksum: 274
Coasting Arc #14 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2010/054/02:51:29
832
Vector Time (MET): 014/17:37:22
852
Weight (LBS) : 210654
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4001555
17 A = 6716357
05 meter
Y = -2495626
87 meter E =
0018137
Z = -4795966
08 I = 51
96426
XDOT = 1351
511345 Wp = 28
90006
YDOT = 7124
110787 meter/sec RA = 95
34185 deg
ZDOT = -2567
946979 TA = 215
96165
MA = 216
08383
Ha = 189
628 n
mi
Hp = 179
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13128461
86 X = 4052475
84
Y = -8187752
21 feet Y = -2450571
37 meter
Z = -15734796
84 Z = -4776403
20
XDOT = 4434
092338 XDOT = 1284
181648
YDOT = 23373
066885 feet/sec YDOT = 7138
855290 meter/sec
ZDOT = -8425
022898 ZDOT = -2561
544798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10651387
41 X = -3246542
88
Y = 11330507
10 feet Y = 3453538
57 meter
Z = -15657176
75 Z = -4772307
47
XDOT = -9553
092304 XDOT = -2911
782534
YDOT = -20639
696645 feet/sec YDOT = -6290
979537 meter/sec
ZDOT = -8399
374950 ZDOT = -2560
129485
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 10054
13937900
00020000 00000-0 20000-3 0 9135
2 36394 51
6422 96
0133 0012456 349
5283 10
5620 15
76083398 2344
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10054
13937900 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 96
0133 deg
Eccentricity:
0012456
Arg of perigee: 349
5283 deg
Mean anomaly: 10
5620 deg
Mean motion: 15
76083398 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 234
Checksum: 276
Coasting Arc #15 (Orbit 249)
---------------------------------------
Vector Time (GMT): 2010/055/02:56:14
326
Vector Time (MET): 015/17:42:07
345
Weight (LBS) : 210654
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 124893
67 A = 6726058
60 meter
Y = -6726367
30 meter E =
0007866
Z = -133078
60 I = 51
99944
XDOT = 4735
555536 Wp = 59
64689
YDOT = 202
712242 meter/sec RA = 90
17819 deg
ZDOT = -6061
890929 TA = 121
79127
MA = 121
71464
Ha = 189
714 n
mi
Hp = 179
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 409756
13 X = 200784
53
Y = -22068134
19 feet Y = -6724545
41 meter
Z = -436609
57 Z = -132287
73
XDOT = 15536
599526 XDOT = 4762
382339
YDOT = 665
066410 feet/sec YDOT = 255
845215 meter/sec
ZDOT = -19888
093598 ZDOT = -6038
820895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6121556
56 X = 1865850
44
Y = 21206120
59 feet Y = 6463625
56 meter
Z = -433669
51 Z = -132182
47
XDOT = -13605
270659 XDOT = -4146
886497
YDOT = 3540
161415 feet/sec YDOT = 1079
041199 meter/sec
ZDOT = -19796
452897 ZDOT = -6033
958843
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 10055
15386788
00020000 00000-0 20000-3 0 9141
2 36394 51
6424 90
7867 0012692 353
0100 7
0885 15
76147207 2503
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10055
15386788 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 90
7867 deg
Eccentricity:
0012692
Arg of perigee: 353
0100 deg
Mean anomaly: 7
0885 deg
Mean motion: 15
76147207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 250
Checksum: 291
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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