Date:
June 9th 2007
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2007/159/23:38:03 976 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 81 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : -0 14745
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
160/16:40:51
976 -14
6 41
0 41
1
000/17:02:48
000 29
6 4
0 130
1
000/00:00:29
524 -24
6 -0
0 99
5
161/01:10:26
787 117
5 143
6 143
6
001/01:32:22
811 -15
6 -0
0 180
2
000/00:01:35
645 -81
1 0
0 129
0
161/15:27:52
502 -64
5 80
7 80
7
001/15:49:48
526 9
4 -0
0 179
8
000/00:00:54
324 47
6 0
1 174
2
161/17:00:44
144 -6
8 9
2 9
2
001/17:22:40
167 0
2 -0
2 181
9
000/00:00:14
335 6
1 0
1 178
3
161/18:17:37
250 -2
6 2
4 2
8
001/18:39:33
274 0
7 0
4 182
9
000/00:00:12
548 0
9 1
6 179
6
Coasting Arc #1 (Orbit 4)
---------------------------------------
Vector Time (GMT): 2007/160/04:26:37
000
Vector Time (MET): 000/04:48:33
024
Weight (LBS) : 255388
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -16418
20 A = 6568023
65 meter
Y = -4567837
24 meter E =
0059915
Z = 4749199
32 I = 51
79742
XDOT = 6918
093006 Wp = 350
28128
YDOT = -2580
159405 meter/sec RA = 144
70277 deg
ZDOT = -2403
524334 TA = 123
20411
MA = 122
62822
Ha = 124
705 n
mi
Hp = 85
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -53865
48 X = 11541
27
Y = -14986342
66 feet Y = -4567864
87 meter
Z = 15581362
58 Z = 4749187
10
XDOT = 22697
155531 XDOT = 6958
079588
YDOT = -8465
089913 feet/sec YDOT = -2502
648243 meter/sec
ZDOT = -7885
578525 ZDOT = -2369
819157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8888205
67 X = 2709125
09
Y = -12066983
20 feet Y = -3678016
48 meter
Z = 15580755
57 Z = 4749014
30
XDOT = 22386
594546 XDOT = 6823
434017
YDOT = 6241
956786 feet/sec YDOT = 1902
548428 meter/sec
ZDOT = -7758
608458 ZDOT = -2364
823858
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 31600U 07024A 07160
22728080
00014500 00000-0 95600-4 0 9002
2 31600 51
6274 145
4301 0057504 343
6441 16
2893 16
29670823 59
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07160
22728080 = yrday
fracday
Element set: 900
Inclination: 51
6274 deg
RA of node: 145
4301 deg
Eccentricity:
0057504
Arg of perigee: 343
6441 deg
Mean anomaly: 16
2893 deg
Mean motion: 16
29670823 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 5
Checksum: 251
Coasting Arc #2 (Orbit 12)
---------------------------------------
Vector Time (GMT): 2007/160/16:41:06
738
Vector Time (MET): 000/17:03:02
762
Weight (LBS) : 254354
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5352664
03 A = 6590782
39 meter
Y = -370408
00 meter E =
0046001
Z = -3827931
57 I = 51
82820
XDOT = -2554
093640 Wp = 318
29946
YDOT = 6094
630445 meter/sec RA = 141
92661 deg
ZDOT = -4099
585602 TA = 269
32614
MA = 269
85325
Ha = 130
057 n
mi
Hp = 99
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17561233
69 X = 5375000
36
Y = -1215249
35 feet Y = -310483
98 meter
Z = -12558830
62 Z = -3801873
91
XDOT = -8379
572309 XDOT = -2602
074448
YDOT = 19995
506708 feet/sec YDOT = 6065
828922 meter/sec
ZDOT = -13450
083996 ZDOT = -4112
109525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15480443
33 X = -4718439
13
Y = -8525879
82 feet Y = -2598688
17 meter
Z = -12460466
84 Z = -3797950
29
XDOT = 17187
446006 XDOT = 5238
733543
YDOT = -11184
426519 feet/sec YDOT = -3409
013203 meter/sec
ZDOT = -13496
635590 ZDOT = -4113
774528
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 31600U 07024A 07160
71777949
00014500 00000-0 95600-4 0 9015
2 31600 51
6326 142
7101 0049199 311
0653 48
6289 16
22578218 135
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07160
71777949 = yrday
fracday
Element set: 901
Inclination: 51
6326 deg
RA of node: 142
7101 deg
Eccentricity:
0049199
Arg of perigee: 311
0653 deg
Mean anomaly: 48
6289 deg
Mean motion: 16
22578218 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 13
Checksum: 280
Coasting Arc #3 (Orbit 18)
---------------------------------------
Vector Time (GMT): 2007/161/01:11:14
609
Vector Time (MET): 001/01:33:10
633
Weight (LBS) : 250780
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2105205
37 A = 6666158
69 meter
Y = -5269055
36 meter E =
0073770
Z = 3405245
33 I = 51
83828
XDOT = 6246
130679 Wp = 131
23238
YDOT = -504
366562 meter/sec RA = 139
91811 deg
ZDOT = -4626
719144 TA = 7
88850
MA = 7
77311
Ha = 180
230 n
mi
Hp = 128
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6906841
76 X = 2147369
63
Y = -17286927
05 feet Y = -5245301
18 meter
Z = 11172064
74 Z = 3415574
48
XDOT = 20492
554720 XDOT = 6273
777650
YDOT = -1654
745938 feet/sec YDOT = -434
431155 meter/sec
ZDOT = -15179
524752 ZDOT = -4596
308050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17826521
87 X = 5433523
87
Y = 5281920
93 feet Y = 1609929
50 meter
Z = 11210431
28 Z = 3416939
46
XDOT = 3860
825928 XDOT = 1176
779743
YDOT = 19048
890795 feet/sec YDOT = 5806
101914 meter/sec
ZDOT = -15064
733621 ZDOT = -4591
730808
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 31600U 07024A 07161
08807867
00014500 00000-0 95600-4 0 9020
2 31600 51
6295 140
6689 0065110 138
5173 222
0970 15
95588654 193
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
08807867 = yrday
fracday
Element set: 902
Inclination: 51
6295 deg
RA of node: 140
6689 deg
Eccentricity:
0065110
Arg of perigee: 138
5173 deg
Mean anomaly: 222
0970 deg
Mean motion: 15
95588654 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 19
Checksum: 293
Coasting Arc #4 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2007/161/15:28:19
664
Vector Time (MET): 001/15:50:15
688
Weight (LBS) : 248794
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1947240
72 A = 6708647
92 meter
Y = 5465602
59 meter E =
0004193
Z = -3373042
63 I = 51
85388
XDOT = -6094
748970 Wp = 122
86657
YDOT = 704
038188 meter/sec RA = 136
77686 deg
ZDOT = 4661
200120 TA = 197
41091
MA = 197
42529
Ha = 179
805 n
mi
Hp = 174
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6388585
05 X = -1991768
81
Y = 17931767
02 feet Y = 5443599
99 meter
Z = -11066412
81 Z = -3382610
06
XDOT = -19995
895570 XDOT = -6124
805349
YDOT = 2309
836574 feet/sec YDOT = 635
780477 meter/sec
ZDOT = 15292
651312 ZDOT = 4631
518536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17808706
78 X = 5428093
83
Y = -6665277
07 feet Y = -2031576
45 meter
Z = -11101883
83 Z = -3383854
19
XDOT = 14179
819455 XDOT = 4322
008970
YDOT = 12611
697913 feet/sec YDOT = 3844
045524 meter/sec
ZDOT = 15180
635130 ZDOT = 4627
057588
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 31600U 07024A 07161
65171211
00014500 00000-0 95600-4 0 9031
2 31600 51
6312 137
6861 0002610 211
5476 148
5535 15
80526528 280
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
65171211 = yrday
fracday
Element set: 903
Inclination: 51
6312 deg
RA of node: 137
6861 deg
Eccentricity:
0002610
Arg of perigee: 211
5476 deg
Mean anomaly: 148
5535 deg
Mean motion: 15
80526528 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 28
Checksum: 251
Coasting Arc #5 (Orbit 28)
---------------------------------------
Vector Time (GMT): 2007/161/17:00:51
311
Vector Time (MET): 001/17:22:47
335
Weight (LBS) : 248569
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2446214
66 A = 6714660
00 meter
Y = 5513548
00 meter E =
0005549
Z = -2942264
69 I = 51
86093
XDOT = -5836
930287 Wp = 347
58474
YDOT = 94
983063 meter/sec RA = 136
44599 deg
ZDOT = 5034
413213 TA = 338
53832
MA = 338
56157
Ha = 181
938 n
mi
Hp = 178
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8025638
65 X = -2493334
00
Y = 18089068
24 feet Y = 5485956
44 meter
Z = -9653099
38 Z = -2954262
46
XDOT = -19150
033749 XDOT = -5862
014831
YDOT = 311
624223 feet/sec YDOT = 29
633383 meter/sec
ZDOT = 16517
103716 ZDOT = 5005
996137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15282599
56 X = 4658136
34
Y = -12538082
11 feet Y = -3821607
43 meter
Z = -9697744
11 Z = -2955872
40
XDOT = 16393
788935 XDOT = 4996
826867
YDOT = 7298
945507 feet/sec YDOT = 2224
718590 meter/sec
ZDOT = 16409
788965 ZDOT = 5001
703677
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 31600U 07024A 07161
71493726
00014500 00000-0 95600-4 0 9047
2 31600 51
6329 137
3581 0006609 304
5096 55
5445 15
78822423 295
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
71493726 = yrday
fracday
Element set: 904
Inclination: 51
6329 deg
RA of node: 137
3581 deg
Eccentricity:
0006609
Arg of perigee: 304
5096 deg
Mean anomaly: 55
5445 deg
Mean motion: 15
78822423 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 29
Checksum: 282
Coasting Arc #6 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2007/161/18:17:43
524
Vector Time (MET): 001/18:39:39
548
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2893220
14 A = 6707596
67 meter
Y = 2972624
62 meter E =
0008922
Z = -5277705
97 I = 51
83420
XDOT = -5545
730399 Wp = 59
75180
YDOT = 5345
817326 meter/sec RA = 136
19647 deg
ZDOT = -24
789888 TA = 209
98810
MA = 210
03923
Ha = 182
917 n
mi
Hp = 179
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9492192
06 X = 2885435
55
Y = 9752705
44 feet Y = 3004904
16 meter
Z = -17315308
30 Z = -5263669
15
XDOT = -18194
653540 XDOT = -5604
918700
YDOT = 17538
770756 feet/sec YDOT = 5283
530872 meter/sec
ZDOT = -81
331654 ZDOT = -51
874619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8218254
83 X = -2504924
07
Y = -10932649
45 feet Y = -3332271
55 meter
Z = -17261933
23 Z = -5261437
25
XDOT = 19551
675361 XDOT = 5959
350650
YDOT = -14385
688936 feet/sec YDOT = -4384
757988 meter/sec
ZDOT = -182
978234 ZDOT = -55
771766
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 31600U 07024A 07161
77823170
00014500 00000-0 95600-4 0 9054
2 31600 51
6331 137
0320 0008623 300
8600 59
1716 15
78396168 309
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07161
77823170 = yrday
fracday
Element set: 905
Inclination: 51
6331 deg
RA of node: 137
0320 deg
Eccentricity:
0008623
Arg of perigee: 300
8600 deg
Mean anomaly: 59
1716 deg
Mean motion: 15
78396168 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 30
Checksum: 253
Coasting Arc #7 (Orbit 45)
---------------------------------------
Vector Time (GMT): 2007/162/18:20:59
136
Vector Time (MET): 002/18:42:55
160
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5370454
43 A = 6716978
70 meter
Y = -3137031
37 meter E =
0003513
Z = -2536117
95 I = 51
88548
XDOT = 715
619495 Wp = 292
97486
YDOT = 5528
955648 meter/sec RA = 131
05297 deg
ZDOT = -5316
478996 TA = 275
70455
MA = 275
74461
Ha = 183
011 n
mi
Hp = 179
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17619601
14 X = 5417421
13
Y = -10292097
67 feet Y = -3076771
01 meter
Z = -8320596
96 Z = -2509914
21
XDOT = 2347
832988 XDOT = 679
627131
YDOT = 18139
618269 feet/sec YDOT = 5536
750041 meter/sec
ZDOT = -17442
516390 ZDOT = -5313
089184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18612344
04 X = -5673042
46
Y = 8461049
21 feet Y = 2578927
80 meter
Z = -8221997
82 Z = -2506064
93
XDOT = 10
528059 XDOT = 3
208952
YDOT = -16936
476574 feet/sec YDOT = -5162
238060 meter/sec
ZDOT = -17429
051117 ZDOT = -5312
374780
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 31600U 07024A 07162
79123531
00014500 00000-0 95600-4 0 9062
2 31600 51
6329 131
7950 0008691 303
4564 56
5770 15
78385670 463
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07162
79123531 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 131
7950 deg
Eccentricity:
0008691
Arg of perigee: 303
4564 deg
Mean anomaly: 56
5770 deg
Mean motion: 15
78385670 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 46
Checksum: 285
Coasting Arc #8 (Orbit 61)
---------------------------------------
Vector Time (GMT): 2007/163/18:24:20
156
Vector Time (MET): 003/18:46:16
179
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1569270
42 A = 6716067
92 meter
Y = -5904703
28 meter E =
0007286
Z = 2787431
92 I = 51
90145
XDOT = 5654
853384 Wp = 64
81904
YDOT = -934
081814 meter/sec RA = 125
84306 deg
ZDOT = -5148
835344 TA = 83
34786
MA = 83
26493
Ha = 183
125 n
mi
Hp = 178
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5148525
01 X = 1621576
71
Y = -19372386
08 feet Y = -5886879
96 meter
Z = 9145117
85 Z = 2795181
66
XDOT = 18552
668584 XDOT = 5689
881255
YDOT = -3064
572881 feet/sec YDOT = -870
710391 meter/sec
ZDOT = -16892
504410 ZDOT = -5121
278722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6420760
94 X = -1957047
93
Y = 18974903
40 feet Y = 5783550
56 meter
Z = 9173696
23 Z = 2796142
61
XDOT = -17430
062300 XDOT = -5312
682989
YDOT = 2239
881991 feet/sec YDOT = 682
716031 meter/sec
ZDOT = -16788
520144 ZDOT = -5117
140940
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 31600U 07024A 07163
80421281
00014500 00000-0 95600-4 0 9079
2 31600 51
6330 126
5573 0008698 308
8264 51
2124 15
78470664 622
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07163
80421281 = yrday
fracday
Element set: 907
Inclination: 51
6330 deg
RA of node: 126
5573 deg
Eccentricity:
0008698
Arg of perigee: 308
8264 deg
Mean anomaly: 51
2124 deg
Mean motion: 15
78470664 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 62
Checksum: 271
Coasting Arc #9 (Orbit 77)
---------------------------------------
Vector Time (GMT): 2007/164/18:27:27
754
Vector Time (MET): 004/18:49:23
778
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3744824
77 A = 6707391
90 meter
Y = -1792333
13 meter E =
0006450
Z = 5271275
06 I = 51
88780
XDOT = 3700
441464 Wp = 321
66508
YDOT = -6750
929501 meter/sec RA = 120
70602 deg
ZDOT = 338
602174 TA = 125
16374
MA = 125
10330
Ha = 183
309 n
mi
Hp = 178
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12286170
49 X = -3750131
22
Y = -5880358
05 feet Y = -1834200
23 meter
Z = 17294209
53 Z = 5253069
27
XDOT = 12140
555983 XDOT = 3773
939291
YDOT = -22148
718836 feet/sec YDOT = -6709
178392 meter/sec
ZDOT = 1110
899520 ZDOT = 356
756381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12149611
57 X = 3703201
61
Y = 6347989
11 feet Y = 1934867
08 meter
Z = 17225221
40 Z = 5250247
48
XDOT = -12506
429082 XDOT = -3811
959584
YDOT = 20784
293437 feet/sec YDOT = 6335
052640 meter/sec
ZDOT = 1178
700237 ZDOT = 359
267832
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 31600U 07024A 07164
81716599
00014500 00000-0 95600-4 0 9081
2 31600 51
6327 121
3191 0008673 311
9123 48
1302 15
78482628 782
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07164
81716599 = yrday
fracday
Element set: 908
Inclination: 51
6327 deg
RA of node: 121
3191 deg
Eccentricity:
0008673
Arg of perigee: 311
9123 deg
Mean anomaly: 48
1302 deg
Mean motion: 15
78482628 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 78
Checksum: 283
Coasting Arc #10 (Orbit 93)
---------------------------------------
Vector Time (GMT): 2007/165/18:30:46
966
Vector Time (MET): 005/18:52:42
990
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4249142
43 A = 6716917
49 meter
Y = 4632911
81 meter E =
0012511
Z = 2342294
27 I = 51
93361
XDOT = -2368
513813 Wp = 34
92226
YDOT = -4925
802172 meter/sec RA = 115
56021 deg
ZDOT = 5442
096067 TA = 351
40365
MA = 351
42505
Ha = 183
385 n
mi
Hp = 178
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13940756
01 X = -4311961
72
Y = 15199841
88 feet Y = 4585089
82 meter
Z = 7684692
48 Z = 2321500
18
XDOT = -7770
714608 XDOT = -2339
746839
YDOT = -16160
768281 feet/sec YDOT = -4952
103179 meter/sec
ZDOT = 17854
645890 ZDOT = 5430
658631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14080290
70 X = 4291672
61
Y = -15110214
21 feet Y = -4605593
29 meter
Z = 7606655
63 Z = 2318508
64
XDOT = 6665
225825 XDOT = 2031
560832
YDOT = 15183
997644 feet/sec YDOT = 4628
082482 meter/sec
ZDOT = 17810
865011 ZDOT = 5428
751655
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 31600U 07024A 07165
83009223
00014500 00000-0 95600-4 0 9094
2 31600 51
6321 116
0806 0008799 314
8186 45
2264 15
78547623 940
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07165
83009223 = yrday
fracday
Element set: 909
Inclination: 51
6321 deg
RA of node: 116
0806 deg
Eccentricity:
0008799
Arg of perigee: 314
8186 deg
Mean anomaly: 45
2264 deg
Mean motion: 15
78547623 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 94
Checksum: 284
Coasting Arc #11 (Orbit 108)
---------------------------------------
Vector Time (GMT): 2007/166/18:34:03
875
Vector Time (MET): 006/18:55:59
899
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 247809
05 A = 6715348
35 meter
Y = 6013157
38 meter E =
0008313
Z = -2967755
07 I = 51
93943
XDOT = -5193
436433 Wp = 349
09645
YDOT = 2690
565193 meter/sec RA = 110
35288 deg
ZDOT = 5023
592179 TA = 336
72887
MA = 336
76648
Ha = 183
454 n
mi
Hp = 178
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 813021
81 X = 195032
10
Y = 19728206
62 feet Y = 6015631
66 meter
Z = -9736729
22 Z = -2966678
16
XDOT = -17038
833441 XDOT = -5247
512095
YDOT = 8827
313624 feet/sec YDOT = 2632
242017 meter/sec
ZDOT = 16481
601637 ZDOT = 4998
231707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1363799
32 X = -415686
03
Y = -19700145
98 feet Y = -6004604
49 meter
Z = -9731974
96 Z = -2966305
97
XDOT = 15466
556270 XDOT = 4714
206351
YDOT = -9156
244739 feet/sec YDOT = -2790
823396 meter/sec
ZDOT = 16386
072510 ZDOT = 4994
474901
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 31600U 07024A 07166
77968893
00014500 00000-0 95600-4 0 9107
2 31600 51
6316 111
1695 0008755 318
2679 41
7818 15
78569637 1095
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07166
77968893 = yrday
fracday
Element set: 910
Inclination: 51
6316 deg
RA of node: 111
1695 deg
Eccentricity:
0008755
Arg of perigee: 318
2679 deg
Mean anomaly: 41
7818 deg
Mean motion: 15
78569637 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 109
Checksum: 322
Coasting Arc #12 (Orbit 124)
---------------------------------------
Vector Time (GMT): 2007/167/18:37:21
000
Vector Time (MET): 007/18:59:17
024
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4121162
86 A = 6707057
61 meter
Y = 577558
96 meter E =
0012417
Z = -5268690
39 I = 51
91979
XDOT = -1660
733351 Wp = 50
98552
YDOT = 7505
350781 meter/sec RA = 105
21926 deg
ZDOT = -469
364564 TA = 214
53340
MA = 214
61413
Ha = 183
559 n
mi
Hp = 178
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13520875
51 X = 4139999
07
Y = 1894878
47 feet Y = 623706
05 meter
Z = -17285729
64 Z = -5248624
06
XDOT = -5448
600232 XDOT = -1742
175284
YDOT = 24623
854268 feet/sec YDOT = 7486
342552 meter/sec
ZDOT = -1539
909986 ZDOT = -477
628698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13702910
82 X = -4176647
22
Y = -1119480
82 feet Y = -341217
75 meter
Z = -17209825
27 Z = -5245554
74
XDOT = 3952
808874 XDOT = 1204
816145
YDOT = -23893
542418 feet/sec YDOT = -7282
751729 meter/sec
ZDOT = -1570
292441 ZDOT = -478
625136
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 31600U 07024A 07167
79256651
00014500 00000-0 95600-4 0 9113
2 31600 51
6308 105
9311 0008670 322
3422 37
7135 15
78614120 1253
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07167
79256651 = yrday
fracday
Element set: 911
Inclination: 51
6308 deg
RA of node: 105
9311 deg
Eccentricity:
0008670
Arg of perigee: 322
3422 deg
Mean anomaly: 37
7135 deg
Mean motion: 15
78614120 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 125
Checksum: 256
Coasting Arc #13 (Orbit 140)
---------------------------------------
Vector Time (GMT): 2007/168/18:40:48
616
Vector Time (MET): 008/19:02:44
640
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2850582
32 A = 6716626
79 meter
Y = -5619310
27 meter E =
0003183
Z = -2330757
23 I = 51
95892
XDOT = 3600
900881 Wp = 345
58211
YDOT = 4086
989824 meter/sec RA = 100
07424 deg
ZDOT = -5444
877649 TA = 220
55408
MA = 220
57780
Ha = 183
603 n
mi
Hp = 177
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9352304
21 X = 2924468
61
Y = -18436057
33 feet Y = -5587050
98 meter
Z = -7646841
31 Z = -2316730
77
XDOT = 11813
979270 XDOT = 3581
426243
YDOT = 13408
759266 feet/sec YDOT = 4127
110569 meter/sec
ZDOT = -17863
771814 ZDOT = -5427
431254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7717310
09 X = -2352236
12
Y = 19198835
47 feet Y = 5851805
05 meter
Z = -7594460
32 Z = -2314791
51
XDOT = -11659
531102 XDOT = -3553
825080
YDOT = -11732
841607 feet/sec YDOT = -3576
170122 meter/sec
ZDOT = -17797
364740 ZDOT = -5424
636773
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 31600U 07024A 07168
80541803
00014500 00000-0 95600-4 0 9123
2 31600 51
6309 100
6934 0008697 326
0734 33
9874 15
78651626 1411
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07168
80541803 = yrday
fracday
Element set: 912
Inclination: 51
6309 deg
RA of node: 100
6934 deg
Eccentricity:
0008697
Arg of perigee: 326
0734 deg
Mean anomaly: 33
9874 deg
Mean motion: 15
78651626 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 141
Checksum: 284
Coasting Arc #14 (Orbit 156)
---------------------------------------
Vector Time (GMT): 2007/169/18:43:53
273
Vector Time (MET): 009/19:05:49
297
Weight (LBS) : 248488
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1873729
42 A = 6714946
02 meter
Y = -5705371
10 meter E =
0010514
Z = 3004711
82 I = 51
95751
XDOT = 4262
216335 Wp = 55
36860
YDOT = -4037
057832 meter/sec RA = 94
86798 deg
ZDOT = -4989
589536 TA = 90
00850
MA = 89
88802
Ha = 183
685 n
mi
Hp = 177
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6147406
24 X = -1824449
60
Y = -18718409
13 feet Y = -5726029
23 meter
Z = 9857978
41 Z = 2995728
20
XDOT = 13983
649394 XDOT = 4331
237851
YDOT = -13244
940395 feet/sec YDOT = -3989
054869 meter/sec
ZDOT = -16370
044408 ZDOT = -4968
716906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8394422
12 X = 2558619
86
Y = 17843323
76 feet Y = 5438645
08 meter
Z = 9823372
98 Z = 2994164
08
XDOT = -11090
603212 XDOT = -3380
415859
YDOT = 14219
501406 feet/sec YDOT = 4334
104028 meter/sec
ZDOT = -16291
600395 ZDOT = -4965
679800
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 31600U 07024A 07169
81825089
00014500 00000-0 95600-4 0 9137
2 31600 51
6311 95
4540 0008781 328
8712 31
1933 15
78690063 1579
Satellite: SHUTTLE
Catalog Number: 31600
Epoch time: 07169
81825089 = yrday
fracday
Element set: 913
Inclination: 51
6311 deg
RA of node: 95
4540 deg
Eccentricity:
0008781
Arg of perigee: 328
8712 deg
Mean anomaly: 31
1933 deg
Mean motion: 15
78690063 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 157
Checksum: 286
SPACE SHUTTLE ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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