Date:
February 17th 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
049/07:10:38
106 -0
1 0
6 0
6
009/21:56:31
125 0
6 -0
0 188
8
000/00:00:02
250 -0
2 0
0 180
6
049/08:10:37
682 0
3 0
4 0
4
009/22:56:30
701 -0
2 -0
0 190
4
000/00:00:01
401 -0
1 0
0 180
9
051/00:10:07
265 -0
1 -0
1 0
2
011/14:56:00
285 -0
1 0
0 190
7
000/00:00:00
569 0
1 0
0 180
2
051/02:09:12
578 0
2 -0
0 3
0
011/16:55:05
597 2
6 -0
0 190
4
000/00:00:11
195 -1
4 -3
0 180
4
051/02:37:12
576 -0
5 -3
0 3
0
011/17:23:05
595 2
9 0
0 189
2
000/00:00:11
190 -0
6 0
0 180
3
Coasting Arc #1 (Orbit 114)
---------------------------------------
Vector Time (GMT): 2010/046/13:11:12
000
Vector Time (MET): 007/03:57:05
019
Weight (LBS) : 210582
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1317167
53 A = 6715340
58 meter
Y = -4284344
26 meter E =
0013082
Z = 5005224
16 I = 51
87029
XDOT = 6172
188412 Wp = 355
19012
YDOT = -4176
396854 meter/sec RA = 134
13628 deg
ZDOT = -1938
221953 TA = 113
54078
MA = 113
40330
Ha = 188
430 n
mi
Hp = 181
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4321415
79 X = -1293450
75
Y = -14056247
58 feet Y = -4298948
23 meter
Z = 16421339
12 Z = 4998883
30
XDOT = 20249
961980 XDOT = 6227
869553
YDOT = -13702
089415 feet/sec YDOT = -4107
029257 meter/sec
ZDOT = -6358
995908 ZDOT = -1908
102804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22870
54 X = 6970
94
Y = -14733771
85 feet Y = -4490853
66 meter
Z = 16395991
98 Z = 4997498
36
XDOT = 22398
476943 XDOT = 6827
055772
YDOT = -6954
108199 feet/sec YDOT = -2119
612179 meter/sec
ZDOT = -6239
590841 ZDOT = -1901
827288
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
59378279
00020000 00000-0 20000-3 0 9000
2 36394 51
6463 134
8796 0011406 329
3315 30
7182 15
76095962 1156
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10046
59378279 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 134
8796 deg
Eccentricity:
0011406
Arg of perigee: 329
3315 deg
Mean anomaly: 30
7182 deg
Mean motion: 15
76095962 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 115
Checksum: 303
Coasting Arc #2 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2010/047/13:15:55
357
Vector Time (MET): 008/04:01:48
376
Weight (LBS) : 210582
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5264147
35 A = 6720162
36 meter
Y = 1845521
71 meter E =
0011181
Z = 3734082
17 I = 51
90610
XDOT = 816
792636 Wp = 37
22734
YDOT = -6352
068262 meter/sec RA = 129
02817 deg
ZDOT = 4292
993750 TA = 7
74963
MA = 7
73237
Ha = 188
694 n
mi
Hp = 180
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17270824
65 X = -5302542
34
Y = 6054861
26 feet Y = 1786410
34 meter
Z = 12250925
77 Z = 3708416
13
XDOT = 2679
765866 XDOT = 866
943813
YDOT = -20840
118970 feet/sec YDOT = -6342
648993 meter/sec
ZDOT = 14084
625164 ZDOT = 4297
083770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18327111
42 X = -5586103
56
Y = 1242686
56 feet Y = 378770
86 meter
Z = 12149099
90 Z = 3703045
65
XDOT = 8117
506192 XDOT = 2474
215887
YDOT = -18070
014975 feet/sec YDOT = -5507
740564 meter/sec
ZDOT = 14100
608975 ZDOT = 4297
865616
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
60827209
00020000 00000-0 20000-3 0 9016
2 36394 51
6455 129
6543 0011338 334
1265 25
9331 15
76120894 1314
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10047
60827209 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 129
6543 deg
Eccentricity:
0011338
Arg of perigee: 334
1265 deg
Mean anomaly: 25
9331 deg
Mean motion: 15
76120894 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 131
Checksum: 277
Coasting Arc #3 (Orbit 145)
---------------------------------------
Vector Time (GMT): 2010/048/13:20:33
570
Vector Time (MET): 009/04:06:26
589
Weight (LBS) : 210582
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2417282
85 A = 6724800
32 meter
Y = 6023434
08 meter E =
0016736
Z = -1719399
09 I = 51
93947
XDOT = -5128
774776 Wp = 1
63713
YDOT = -424
127266 meter/sec RA = 123
83775 deg
ZDOT = 5742
389358 TA = 339
38271
MA = 339
45016
Ha = 188
794 n
mi
Hp = 180
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7930718
03 X = -2476140
02
Y = 19761922
83 feet Y = 5996059
49 meter
Z = -5641073
12 Z = -1731285
32
XDOT = -16826
688896 XDOT = -5151
543218
YDOT = -1391
493656 feet/sec YDOT = -481
636528 meter/sec
ZDOT = 18839
860099 ZDOT = 5717
418903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12207365
60 X = -3720805
04
Y = 17432100
61 feet Y = 5313304
27 meter
Z = -5688029
70 Z = -1733711
45
XDOT = -14898
989545 XDOT = -4541
212013
YDOT = -4337
265016 feet/sec YDOT = -1321
998377 meter/sec
ZDOT = 18740
701404 ZDOT = 5712
165788
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
55932682
00020000 00000-0 20000-3 0 9024
2 36394 51
6449 124
7554 0011535 338
3773 21
6903 15
76133557 1468
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10048
55932682 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 124
7554 deg
Eccentricity:
0011535
Arg of perigee: 338
3773 deg
Mean anomaly: 21
6903 deg
Mean motion: 15
76133557 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 146
Checksum: 299
Coasting Arc #4 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2010/049/07:10:39
231
Vector Time (MET): 009/21:56:32
250
Weight (LBS) : 210567
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4783433
38 A = 6717128
12 meter
Y = -1060232
53 meter E =
0015121
Z = -4606773
42 I = 51
92399
XDOT = -1335
157412 Wp = 22
72966
YDOT = 6967
057590 meter/sec RA = 120
05882 deg
ZDOT = -2979
390497 TA = 217
75088
MA = 217
85706
Ha = 188
802 n
mi
Hp = 180
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15693679
07 X = 4817317
87
Y = -3478453
18 feet Y = -1006524
78 meter
Z = -15114086
01 Z = -4583453
46
XDOT = -4380
437705 XDOT = -1398
531458
YDOT = 22857
800493 feet/sec YDOT = 6951
764813 meter/sec
ZDOT = -9774
903207 ZDOT = -2986
030855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -714213
06 X = -217692
14
Y = 16145283
39 feet Y = 4921082
38 meter
Z = -15021535
18 Z = -4578563
92
XDOT = -19788
940660 XDOT = -6031
669113
YDOT = -10026
200666 feet/sec YDOT = -3055
985963 meter/sec
ZDOT = -9801
001359 ZDOT = -2987
345214
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
32015107
00020000 00000-0 20000-3 0 9035
2 36394 51
6438 120
8320 0011133 339
2014 20
8695 15
76087392 1583
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10049
32015107 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 120
8320 deg
Eccentricity:
0011133
Arg of perigee: 339
2014 deg
Mean anomaly: 20
8695 deg
Mean motion: 15
76087392 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 158
Checksum: 265
Coasting Arc #5 (Orbit 158)
---------------------------------------
Vector Time (GMT): 2010/049/08:10:38
382
Vector Time (MET): 009/22:56:31
401
Weight (LBS) : 210558
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1671213
77 A = 6718541
90 meter
Y = -4498693
64 meter E =
0016003
Z = 4705030
57 I = 51
92390
XDOT = 5284
567014 Wp = 15
25688
YDOT = -4871
095325 meter/sec RA = 119
80170 deg
ZDOT = -2763
186469 TA = 101
95376
MA = 101
77431
Ha = 190
439 n
mi
Hp = 180
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5482984
82 X = -1643614
56
Y = -14759493
57 feet Y = -4517237
04 meter
Z = 15436452
01 Z = 4696979
17
XDOT = 17337
818287 XDOT = 5352
093959
YDOT = -15981
283875 feet/sec YDOT = -4811
592468 meter/sec
ZDOT = -9065
572404 ZDOT = -2737
350148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14751932
47 X = 4496389
02
Y = -5592628
57 feet Y = -1704633
19 meter
Z = 15404311
66 Z = 4695234
19
XDOT = 15596
098021 XDOT = 4753
690677
YDOT = 16294
419863 feet/sec YDOT = 4966
539174 meter/sec
ZDOT = -8963
176088 ZDOT = -2731
976072
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
38358299
00020000 00000-0 20000-3 0 9044
2 36394 51
6446 120
5053 0012135 347
0365 13
0485 15
75421336 1592
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10049
38358299 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 120
5053 deg
Eccentricity:
0012135
Arg of perigee: 347
0365 deg
Mean anomaly: 13
0485 deg
Mean motion: 15
75421336 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 159
Checksum: 283
Coasting Arc #6 (Orbit 174)
---------------------------------------
Vector Time (GMT): 2010/050/08:10:46
344
Vector Time (MET): 010/22:56:39
363
Weight (LBS) : 210558
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4402953
08 A = 6724262
74 meter
Y = 4164057
77 meter E =
0017996
Z = 2885925
79 I = 51
95879
XDOT = -1855
469125 Wp = 38
88143
YDOT = -5491
033164 meter/sec RA = 114
72058 deg
ZDOT = 5088
851406 TA = 354
20628
MA = 354
22707
Ha = 190
492 n
mi
Hp = 180
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14445384
13 X = -4463231
64
Y = 13661606
87 feet Y = 4114459
18 meter
Z = 9468260
45 Z = 2864389
91
XDOT = -6087
497128 XDOT = -1818
618625
YDOT = -18015
200668 feet/sec YDOT = -5511
586360 meter/sec
ZDOT = 16695
706714 ZDOT = 5079
927323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13935898
45 X = -4247661
85
Y = -14237572
00 feet Y = -4339611
95 meter
Z = 9382902
47 Z = 2859908
67
XDOT = 16855
346665 XDOT = 5137
509663
YDOT = -5511
721820 feet/sec YDOT = -1679
972811 meter/sec
ZDOT = 16660
069583 ZDOT = 5077
989209
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
39846072
00020000 00000-0 20000-3 0 9059
2 36394 51
6453 115
2823 0012172 350
5175 9
5758 15
75530428 1759
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10050
39846072 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 115
2823 deg
Eccentricity:
0012172
Arg of perigee: 350
5175 deg
Mean anomaly: 9
5758 deg
Mean motion: 15
75530428 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 175
Checksum: 285
Coasting Arc #7 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2010/051/00:10:07
550
Vector Time (MET): 011/14:56:00
569
Weight (LBS) : 210554
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197748
73 A = 6723987
47 meter
Y = -4332140
27 meter E =
0011431
Z = -2986635
06 I = 51
96675
XDOT = 2070
903142 Wp = 13
25954
YDOT = 5461
335627 meter/sec RA = 111
31177 deg
ZDOT = -5003
920885 TA = 201
02635
MA = 201
07338
Ha = 190
716 n
mi
Hp = 180
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13772141
51 X = 4260412
28
Y = -14213058
62 feet Y = -4284824
19 meter
Z = -9798671
47 Z = -2966090
28
XDOT = 6794
301647 XDOT = 2033
956324
YDOT = 17917
767805 feet/sec YDOT = 5484
298677 meter/sec
ZDOT = -16417
063270 ZDOT = -4993
950397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18926525
24 X = -5768804
89
Y = 5921031
92 feet Y = 1804730
53 meter
Z = -9717247
70 Z = -2961817
10
XDOT = 2896
415695 XDOT = 882
827504
YDOT = -17657
692601 feet/sec YDOT = -5382
064705 meter/sec
ZDOT = -16377
276803 ZDOT = -4991
793969
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
03274528
00020000 00000-0 20000-3 0 9063
2 36394 51
6462 112
0229 0012908 352
8578 7
2400 15
75538832 1850
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
03274528 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 112
0229 deg
Eccentricity:
0012908
Arg of perigee: 352
8578 deg
Mean anomaly: 7
2400 deg
Mean motion: 15
75538832 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 185
Checksum: 280
Coasting Arc #8 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2010/051/02:09:18
176
Vector Time (MET): 011/16:55:11
195
Weight (LBS) : 210481
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 347330
89 A = 6723495
18 meter
Y = 5940438
76 meter E =
0013328
Z = -3116050
37 I = 51
96394
XDOT = -5201
702946 Wp = 8
29255
YDOT = 2870
994815 meter/sec RA = 110
83694 deg
ZDOT = 4908
928226 TA = 315
62234
MA = 315
72908
Ha = 190
374 n
mi
Hp = 180
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1139537
05 X = 295981
30
Y = 19489628
47 feet Y = 5944037
47 meter
Z = -10223262
38 Z = -3114487
91
XDOT = -17065
954548 XDOT = -5257
282786
YDOT = 9419
274329 feet/sec YDOT = 2812
485878 meter/sec
ZDOT = 16105
407566 ZDOT = 4883
523523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1697006
65 X = -517247
63
Y = -19452390
10 feet Y = -5929088
50 meter
Z = -10216846
09 Z = -3114094
69
XDOT = 15495
600032 XDOT = 4723
058890
YDOT = -9731
147057 feet/sec YDOT = -2966
053623 meter/sec
ZDOT = 16004
632809 ZDOT = 4878
212080
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
09617135
00020000 00000-0 20000-3 0 9075
2 36394 51
6437 111
6946 0012408 348
2575 11
8297 15
75563443 1866
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
09617135 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 111
6946 deg
Eccentricity:
0012408
Arg of perigee: 348
2575 deg
Mean anomaly: 11
8297 deg
Mean motion: 15
75563443 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 186
Checksum: 298
Coasting Arc #9 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2010/051/02:37:18
171
Vector Time (MET): 011/17:23:11
190
Weight (LBS) : 210408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4365176
84 A = 6715036
00 meter
Y = 261106
68 meter E =
0008620
Z = 5094383
05 I = 51
94017
XDOT = 1443
993492 Wp = 356
36377
YDOT = -7392
934493 meter/sec RA = 110
77495 deg
ZDOT = 1624
783750 TA = 78
15169
MA = 78
05503
Ha = 189
246 n
mi
Hp = 180
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14321446
33 X = -4392520
73
Y = 856649
22 feet Y = 212114
99 meter
Z = 16713855
17 Z = 5073110
80
XDOT = 4737
511458 XDOT = 1518
704406
YDOT = -24255
034427 feet/sec YDOT = -7376
360709 meter/sec
ZDOT = 5330
655348 ZDOT = 1631
980232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14135237
68 X = 4308420
44
Y = -2974703
27 feet Y = -906689
56 meter
Z = 16629396
37 Z = 5068640
01
XDOT = -1293
643620 XDOT = -394
302575
YDOT = 23653
016759 feet/sec YDOT = 7209
439508 meter/sec
ZDOT = 5358
967538 ZDOT = 1633
413306
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
15957694
00020000 00000-0 20000-3 0 9080
2 36394 51
6434 111
3675 0012423 338
2641 21
7994 15
76084581 1876
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
15957694 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 111
3675 deg
Eccentricity:
0012423
Arg of perigee: 338
2641 deg
Mean anomaly: 21
7994 deg
Mean motion: 15
76084581 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 187
Checksum: 303
Coasting Arc #10 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2010/052/02:42:20
142
Vector Time (MET): 012/17:28:13
161
Weight (LBS) : 210408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2601983
23 A = 6725591
49 meter
Y = 6086843
39 meter E =
0020762
Z = 1108416
83 I = 51
98498
XDOT = -4037
200521 Wp = 21
71244
YDOT = -2810
828119 meter/sec RA = 105
62446 deg
ZDOT = 5942
194169 TA = 350
38727
MA = 350
42693
Ha = 189
222 n
mi
Hp = 179
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8536690
39 X = -2675272
91
Y = 19969958
61 feet Y = 6057321
67 meter
Z = 3636538
15 Z = 1095598
47
XDOT = -13245
408532 XDOT = -4034
318881
YDOT = -9221
877032 feet/sec YDOT = -2855
981318 meter/sec
ZDOT = 19495
387693 ZDOT = 5922
588638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4690214
14 X = 1429577
27
Y = -21214201
93 feet Y = -6466088
75 meter
Z = 3585842
62 Z = 1092964
83
XDOT = 13296
043666 XDOT = 4052
634109
YDOT = 6230
825812 feet/sec YDOT = 1899
155707 meter/sec
ZDOT = 19417
437521 ZDOT = 5918
434956
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
17403344
00020000 00000-0 20000-3 0 9092
2 36394 51
6425 106
1407 0012381 341
6928 18
3789 15
76139368 2037
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10052
17403344 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 106
1407 deg
Eccentricity:
0012381
Arg of perigee: 341
6928 deg
Mean anomaly: 18
3789 deg
Mean motion: 15
76139368 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 203
Checksum: 286
Coasting Arc #11 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2010/053/02:47:15
427
Vector Time (MET): 013/17:33:08
446
Weight (LBS) : 210408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2375453
48 A = 6718770
10 meter
Y = 4767944
32 meter E =
0010227
Z = -4091546
78 I = 51
96900
XDOT = -4042
018657 Wp = 23
66233
YDOT = 5308
738055 meter/sec RA = 100
44169 deg
ZDOT = 3852
108807 TA = 285
68301
MA = 285
79582
Ha = 189
340 n
mi
Hp = 179
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7793482
55 X = 2341809
43
Y = 15642861
96 feet Y = 4794333
41 meter
Z = -13423709
92 Z = -4080088
62
XDOT = -13261
216065 XDOT = -4119
824074
YDOT = 17417
119604 feet/sec YDOT = 5263
079505 meter/sec
ZDOT = 12638
152255 ZDOT = 3832
283986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11177371
03 X = -3406862
69
Y = -13480638
24 feet Y = -4108898
54 meter
Z = -13378051
36 Z = -4077630
05
XDOT = 8110
017700 XDOT = 2471
933395
YDOT = -19147
699231 feet/sec YDOT = -5836
218726 meter/sec
ZDOT = 12559
592818 ZDOT = 3828
163891
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
12507656
00020000 00000-0 20000-3 0 9101
2 36394 51
6422 101
2406 0012257 345
6251 14
4563 15
76161887 2188
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10053
12507656 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 101
2406 deg
Eccentricity:
0012257
Arg of perigee: 345
6251 deg
Mean anomaly: 14
4563 deg
Mean motion: 15
76161887 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 218
Checksum: 266
Coasting Arc #12 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2010/054/02:52:09
745
Vector Time (MET): 014/17:38:02
764
Weight (LBS) : 210408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4038056
00 A = 6715733
77 meter
Y = -2289810
93 meter E =
0018285
Z = -4866847
44 I = 51
96347
XDOT = 1200
747317 Wp = 31
23031
YDOT = 7213
865357 meter/sec RA = 95
34065 deg
ZDOT = -2386
486716 TA = 215
51242
MA = 215
63427
Ha = 189
409 n
mi
Hp = 179
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13248215
21 X = 4087015
63
Y = -7512503
04 feet Y = -2244358
01 meter
Z = -15967347
26 Z = -4847112
00
XDOT = 3939
459703 XDOT = 1131
543185
YDOT = 23667
537260 feet/sec YDOT = 7226
912579 meter/sec
ZDOT = -7829
680826 ZDOT = -2380
821486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10911905
83 X = -3325948
90
Y = 10741412
88 feet Y = 3273982
65 meter
Z = -15889035
43 Z = -4842978
00
XDOT = -9254
595344 XDOT = -2820
800661
YDOT = -21004
936239 feet/sec YDOT = -6402
304566 meter/sec
ZDOT = -7806
957030 ZDOT = -2379
560503
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
13950856
00020000 00000-0 20000-3 0 9118
2 36394 51
6424 96
0150 0012233 350
3161 9
7769 15
76198302 2349
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10054
13950856 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 96
0150 deg
Eccentricity:
0012233
Arg of perigee: 350
3161 deg
Mean anomaly: 9
7769 deg
Mean motion: 15
76198302 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 234
Checksum: 274
Coasting Arc #13 (Orbit 249)
---------------------------------------
Vector Time (GMT): 2010/055/02:57:01
968
Vector Time (MET): 015/17:42:54
987
Weight (LBS) : 210408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 327476
89 A = 6725672
31 meter
Y = -6709163
10 meter E =
0007404
Z = -392263
51 I = 51
99948
XDOT = 4723
047801 Wp = 58
27721
YDOT = 579
479910 meter/sec RA = 90
17934 deg
ZDOT = -6047
403931 TA = 125
96551
MA = 125
89682
Ha = 189
493 n
mi
Hp = 179
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1074399
26 X = 404419
26
Y = -22011689
98 feet Y = -6705068
76 meter
Z = -1286953
76 Z = -390485
95
XDOT = 15495
563650 XDOT = 4745
589934
YDOT = 1901
180808 feet/sec YDOT = 632
448974 meter/sec
ZDOT = -19840
564079 ZDOT = -6024
405055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5539257
08 X = 1688365
56
Y = 21330800
96 feet Y = 6501628
13 meter
Z = -1280094
07 Z = -390172
67
XDOT = -13911
864327 XDOT = -4240
336247
YDOT = 2443
165368 feet/sec YDOT = 744
676804 meter/sec
ZDOT = -19749
194740 ZDOT = -6019
554557
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
15392251
00020000 00000-0 20000-3 0 9121
2 36394 51
6426 90
7879 0012464 353
8842 6
2168 15
76262492 2505
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10055
15392251 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 90
7879 deg
Eccentricity:
0012464
Arg of perigee: 353
8842 deg
Mean anomaly: 6
2168 deg
Mean motion: 15
76262492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 250
Checksum: 293
Coasting Arc #14 (Orbit 265)
---------------------------------------
Vector Time (GMT): 2010/056/03:01:36
374
Vector Time (MET): 016/17:47:29
394
Weight (LBS) : 210408
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3846931
84 A = 6716930
68 meter
Y = -3095568
48 meter E =
0017318
Z = 4555111
15 I = 51
96793
XDOT = 1821
047759 Wp = 25
60507
YDOT = -6821
532814 meter/sec RA = 85
00761 deg
ZDOT = -3078
254362 TA = 94
98401
MA = 94
78629
Ha = 189
645 n
mi
Hp = 179
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12621167
45 X = -3834140
23
Y = -10156064
58 feet Y = -3138537
56 meter
Z = 14944590
39 Z = 4536454
24
XDOT = 5974
566139 XDOT = 1912
183922
YDOT = -22380
357001 feet/sec YDOT = -6800
648536 meter/sec
ZDOT = -10099
259719 ZDOT = -3069
186689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15370189
60 X = 4684833
79
Y = 5330021
20 feet Y = 1624590
46 meter
Z = 14870388
13 Z = 4532494
30
XDOT = 2173
079605 XDOT = 662
354664
YDOT = 21990
093127 feet/sec YDOT = 6702
580385 meter/sec
ZDOT = -10063
439849 ZDOT = -3067
336466
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 10056
16832330
00020000 00000-0 20000-3 0 9131
2 36394 51
6422 85
5611 0012108 358
0564 2
0551 15
76215134 2668
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10056
16832330 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 85
5611 deg
Eccentricity:
0012108
Arg of perigee: 358
0564 deg
Mean anomaly: 2
0551 deg
Mean motion: 15
76215134 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 266
Checksum: 256
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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