Date:
September 4th 2009
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2009/241/03:59:36 958 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 70 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
251/20:41:43
171 0
2 -0
0 3
0
010/16:42:06
213 -2
4 0
0 193
2
000/00:00:12
426 1
8 -3
0 180
9
251/21:09:49
377 1
9 -6
0 6
0
010/17:10:12
419 -3
6 0
0 191
7
000/00:00:24
838 4
4 0
1 179
1
Coasting Arc #1 (Orbit 67)
---------------------------------------
Vector Time (GMT): 2009/245/08:40:52
000
Vector Time (MET): 004/04:41:15
042
Weight (LBS) : 217347
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4209425
02 A = 6720445
69 meter
Y = -242398
96 meter E =
0021879
Z = -5251168
33 I = 51
28628
XDOT = 168
977226 Wp = 74
38663
YDOT = -7680
203747 meter/sec RA = 269
91128 deg
ZDOT = 225
651833 TA = 197
73161
MA = 197
80808
Ha = 193
101 n
mi
Hp = 181
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13810449
55 X = -4180892
75
Y = -795272
19 feet Y = -289311
83 meter
Z = -17228242
54 Z = -5271548
12
XDOT = 554
387223 XDOT = 253
749867
YDOT = -25197
518856 feet/sec YDOT = -7677
840150 meter/sec
ZDOT = 740
327536 ZDOT = 226
678820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4189372
46 X = 1276920
73
Y = 13078254
91 feet Y = 3986252
10 meter
Z = -17308429
23 Z = -5275609
23
XDOT = -22754
997941 XDOT = -6935
723372
YDOT = 8245
263886 feet/sec YDOT = 2513
156432 meter/sec
ZDOT = 743
943557 ZDOT = 226
753996
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 00128U 09245
37723178
00020000 00000-0 20000-3 0 9008
2 00128 51
6405 270
5976 0008768 43
7161 316
4695 15
73887543 680
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09245
37723178 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 270
5976 deg
Eccentricity:
0008768
Arg of perigee: 43
7161 deg
Mean anomaly: 316
4695 deg
Mean motion: 15
73887543 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 68
Checksum: 300
Coasting Arc #2 (Orbit 83)
---------------------------------------
Vector Time (GMT): 2009/246/08:41:27
355
Vector Time (MET): 005/04:41:50
397
Weight (LBS) : 217347
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 274701
52 A = 6732314
45 meter
Y = 6712359
95 meter E =
0014424
Z = -424676
54 I = 51
32742
XDOT = -4829
379807 Wp = 100
02611
YDOT = -170
206888 meter/sec RA = 264
75637 deg
ZDOT = -5989
281102 TA = 84
60888
MA = 84
44434
Ha = 193
181 n
mi
Hp = 181
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 901251
71 X = 201685
32
Y = 22022178
32 feet Y = 6715023
55 meter
Z = -1393295
72 Z = -423519
72
XDOT = -15844
421939 XDOT = -4798
023096
YDOT = -558
421550 feet/sec YDOT = -224
036805 meter/sec
ZDOT = -19649
872382 ZDOT = -6012
665774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20043481
00 X = 6109253
01
Y = -9168488
76 feet Y = -2794555
37 meter
Z = -1388362
01 Z = -423172
74
XDOT = 4761
587164 XDOT = 1451
331767
YDOT = 13311
577017 feet/sec YDOT = 4057
368675 meter/sec
ZDOT = -19741
878639 ZDOT = -6017
324609
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 00128U 09246
39312133
00020000 00000-0 20000-3 0 9017
2 00128 51
6400 265
3810 0008925 48
2449 311
9475 15
73922981 848
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09246
39312133 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 265
3810 deg
Eccentricity:
0008925
Arg of perigee: 48
2449 deg
Mean anomaly: 311
9475 deg
Mean motion: 15
73922981 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 84
Checksum: 267
Coasting Arc #3 (Orbit 99)
---------------------------------------
Vector Time (GMT): 2009/247/08:42:16
817
Vector Time (MET): 006/04:42:39
859
Weight (LBS) : 217347
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4256448
61 A = 6720404
41 meter
Y = 145025
14 meter E =
0011996
Z = 5191129
28 I = 51
29195
XDOT = 740
756072 Wp = 53
54440
YDOT = 7629
267361 meter/sec RA = 259
58332 deg
ZDOT = -812
179722 TA = 44
26374
MA = 44
16786
Ha = 192
981 n
mi
Hp = 181
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13964726
42 X = 4229293
21
Y = 475804
25 feet Y = 192471
75 meter
Z = 17031264
03 Z = 5211740
96
XDOT = 2430
302074 XDOT = 659
334625
YDOT = 25030
404727 feet/sec YDOT = 7637
095627 meter/sec
ZDOT = -2664
631633 ZDOT = -808
779422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5071541
50 X = -1545805
85
Y = -12913190
21 feet Y = -3935940
38 meter
Z = 17112361
42 Z = 5215847
76
XDOT = 21056
942588 XDOT = 6418
156101
YDOT = -11818
826608 feet/sec YDOT = -3602
378350 meter/sec
ZDOT = -2650
806937 ZDOT = -807
965954
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 00128U 09247
40899939
00020000 00000-0 20000-3 0 9025
2 00128 51
6402 260
1641 0008799 51
1634 309
0313 15
73966880 1007
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09247
40899939 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 260
1641 deg
Eccentricity:
0008799
Arg of perigee: 51
1634 deg
Mean anomaly: 309
0313 deg
Mean motion: 15
73966880 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 100
Checksum: 274
Coasting Arc #4 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2009/248/08:43:28
194
Vector Time (MET): 007/04:43:51
236
Weight (LBS) : 217347
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -901149
61 A = 6731900
66 meter
Y = -6565806
27 meter E =
0022989
Z = 1116498
78 I = 51
33613
XDOT = 4974
180725 Wp = 56
26688
YDOT = 329
489386 meter/sec RA = 254
43833 deg
ZDOT = 5878
451422 TA = 316
01718
MA = 316
19989
Ha = 193
341 n
mi
Hp = 180
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2956527
58 X = -833086
38
Y = -21541359
16 feet Y = -6575502
81 meter
Z = 3663053
73 Z = 1112286
84
XDOT = 16319
490568 XDOT = 4941
570278
YDOT = 1081
001923 feet/sec YDOT = 384
931718 meter/sec
ZDOT = 19286
257947 ZDOT = 5902
536660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18327684
24 X = -5586278
16
Y = 11704323
86 feet Y = 3567477
91 meter
Z = 3646089
15 Z = 1111327
97
XDOT = -4934
391604 XDOT = -1504
002561
YDOT = -13840
152009 feet/sec YDOT = -4218
478332 meter/sec
ZDOT = 19381
033119 ZDOT = 5907
338895
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 00128U 09248
42487237
00020000 00000-0 20000-3 0 9033
2 00128 51
6396 254
9474 0009163 55
0040 305
1982 15
73913792 1164
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09248
42487237 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 254
9474 deg
Eccentricity:
0009163
Arg of perigee: 55
0040 deg
Mean anomaly: 305
1982 deg
Mean motion: 15
73913792 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 116
Checksum: 279
Coasting Arc #5 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2009/249/08:45:03
672
Vector Time (MET): 008/04:45:26
714
Weight (LBS) : 217347
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494050
57 A = 6721480
89 meter
Y = -609006
02 meter E =
0020496
Z = -4978130
23 I = 51
31084
XDOT = -1132
883446 Wp = 85
94490
YDOT = -7353
125306 meter/sec RA = 249
24757 deg
ZDOT = 1930
541816 TA = 202
78034
MA = 202
87140
Ha = 193
298 n
mi
Hp = 180
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14744260
41 X = -4462723
67
Y = -1998051
25 feet Y = -659086
38 meter
Z = -16332448
27 Z = -4999886
21
XDOT = -3716
809206 XDOT = -1059
953568
YDOT = -24124
426856 feet/sec YDOT = -7365
385947 meter/sec
ZDOT = 6333
798609 ZDOT = 1925
216002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4644382
89 X = 1415607
90
Y = 14036050
00 feet Y = 4278188
04 meter
Z = -16418078
40 Z = -5004230
30
XDOT = -18995
056781 XDOT = -5789
693307
YDOT = 13637
365751 feet/sec YDOT = 4156
669081 meter/sec
ZDOT = 6312
396766 ZDOT = 1924
018534
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 00128U 09249
37724039
00020000 00000-0 20000-3 0 9043
2 00128 51
6398 250
0563 0009076 58
4651 301
7397 15
73945877 1318
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09249
37724039 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 250
0563 deg
Eccentricity:
0009076
Arg of perigee: 58
4651 deg
Mean anomaly: 301
7397 deg
Mean motion: 15
73945877 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 131
Checksum: 293
Coasting Arc #6 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2009/250/08:45:41
351
Vector Time (MET): 009/04:46:04
393
Weight (LBS) : 217347
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1338250
97 A = 6730570
51 meter
Y = 6307763
04 meter E =
0012641
Z = -1937373
08 I = 51
35448
XDOT = -5253
612295 Wp = 95
52140
YDOT = -591
851927 meter/sec RA = 244
12107 deg
ZDOT = -5588
413142 TA = 106
09691
MA = 105
95771
Ha = 193
341 n
mi
Hp = 180
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4390587
16 X = 1277028
47
Y = 20694760
61 feet Y = 6322385
69 meter
Z = -6356210
90 Z = -1931021
00
XDOT = -17236
260811 XDOT = -5219
455983
YDOT = -1941
771415 feet/sec YDOT = -650
410348 meter/sec
ZDOT = -18334
688785 ZDOT = -5613
852324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16377694
28 X = 4991921
22
Y = -13403115
41 feet Y = -4085269
58 meter
Z = -6330830
67 Z = -1929637
19
XDOT = 5130
604010 XDOT = 1563
808102
YDOT = 14926
214960 feet/sec YDOT = 4549
510320 meter/sec
ZDOT = -18434
810920 ZDOT = -5618
930368
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 00128U 09250
39309115
00020000 00000-0 20000-3 0 9052
2 00128 51
6406 244
8389 0009218 62
7087 297
5014 15
73993773 1477
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09250
39309115 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 244
8389 deg
Eccentricity:
0009218
Arg of perigee: 62
7087 deg
Mean anomaly: 297
5014 deg
Mean motion: 15
73993773 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 147
Checksum: 291
Coasting Arc #7 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2009/251/08:46:25
705
Vector Time (MET): 010/04:46:48
747
Weight (LBS) : 233712
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4713267
01 A = 6722098
69 meter
Y = 438524
17 meter E =
0016332
Z = 4763071
79 I = 51
33980
XDOT = 1896
122701 Wp = 63
51297
YDOT = 7037
150250 meter/sec RA = 238
92464 deg
ZDOT = -2510
368436 TA = 51
20911
MA = 51
06334
Ha = 193
182 n
mi
Hp = 180
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15463474
44 X = 4684874
69
Y = 1438727
61 feet Y = 491072
23 meter
Z = 15626875
95 Z = 4785900
06
XDOT = 6220
875002 XDOT = 1829
486179
YDOT = 23087
763287 feet/sec YDOT = 7057
981077 meter/sec
ZDOT = -8236
116917 ZDOT = -2501
319265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6043285
35 X = -1841993
38
Y = -14207450
39 feet Y = -4330430
88 meter
Z = 15716719
96 Z = 4790456
24
XDOT = 16294
048681 XDOT = 4966
426038
YDOT = -16051
892377 feet/sec YDOT = -4892
616797 meter/sec
ZDOT = -8200
076901 ZDOT = -2499
383440
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 00128U 09251
40893058
00020000 00000-0 20000-3 0 9060
2 00128 51
6399 239
6223 0009166 66
1679 294
0444 15
74025506 1632
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09251
40893058 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 239
6223 deg
Eccentricity:
0009166
Arg of perigee: 66
1679 deg
Mean anomaly: 294
0444 deg
Mean motion: 15
74025506 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 163
Checksum: 284
Coasting Arc #8 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2009/251/20:41:49
384
Vector Time (MET): 010/16:42:12
426
Weight (LBS) : 233630
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 419970
52 A = 6724869
41 meter
Y = -5298035
98 meter E =
0017835
Z = 4103829
20 I = 51
35704
XDOT = 5835
075951 Wp = 83
40992
YDOT = 3372
896532 meter/sec RA = 236
40831 deg
ZDOT = 3745
384839 TA = 328
07998
MA = 328
18792
Ha = 193
163 n
mi
Hp = 180
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1377856
04 X = 459246
99
Y = -17382007
82 feet Y = -5293119
82 meter
Z = 13464006
56 Z = 4105965
10
XDOT = 19143
949970 XDOT = 5778
731369
YDOT = 11065
933503 feet/sec YDOT = 3437
832928 meter/sec
ZDOT = 12288
008002 ZDOT = 3773
594903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15990202
55 X = 4873813
74
Y = -6937477
91 feet Y = -2114543
27 meter
Z = 13472081
45 Z = 4106290
42
XDOT = -1427
103140 XDOT = -434
981037
YDOT = 20864
676562 feet/sec YDOT = 6359
553416 meter/sec
ZDOT = 12399
211395 ZDOT = 3779
279633
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 00128U 09251
91684850
00020000 00000-0 20000-3 0 9075
2 00128 51
6404 237
0137 0008888 58
2778 301
9250 15
73985434 1713
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09251
91684850 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 237
0137 deg
Eccentricity:
0008888
Arg of perigee: 58
2778 deg
Mean anomaly: 301
9250 deg
Mean motion: 15
73985434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 171
Checksum: 290
Coasting Arc #9 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2009/251/21:10:01
796
Vector Time (MET): 010/17:10:24
838
Weight (LBS) : 233468
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4598554
25 A = 6727796
91 meter
Y = 4657033
93 meter E =
0018709
Z = 1549822
86 I = 51
37856
XDOT = -2548
095375 Wp = 81
78972
YDOT = 4448
404428 meter/sec RA = 236
26701 deg
ZDOT = -5744
616257 TA = 81
05664
MA = 80
84491
Ha = 191
741 n
mi
Hp = 179
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15087120
23 X = 4538607
87
Y = 15278982
71 feet Y = 4708122
57 meter
Z = 5084720
68 Z = 1572017
03
XDOT = -8359
892964 XDOT = -2569
742218
YDOT = 14594
502718 feet/sec YDOT = 4419
788814 meter/sec
ZDOT = -18847
166198 ZDOT = -5757
047830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3952975
13 X = -1204866
82
Y = 21084208
35 feet Y = 6426466
70 meter
Z = 5172334
10 Z = 1576527
43
XDOT = -15154
859626 XDOT = -4619
201214
YDOT = 1843
013940 feet/sec YDOT = 561
750649 meter/sec
ZDOT = -18895
802684 ZDOT = -5759
440658
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 00128U 09251
91681875
00020000 00000-0 20000-3 0 9080
2 00128 51
6403 237
0135 0010963 33
1248 327
0600 15
75161271 1716
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09251
91681875 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 237
0135 deg
Eccentricity:
0010963
Arg of perigee: 33
1248 deg
Mean anomaly: 327
0600 deg
Mean motion: 15
75161271 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 171
Checksum: 248
Coasting Arc #10 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2009/252/21:10:40
921
Vector Time (MET): 011/17:11:03
963
Weight (LBS) : 233468
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2452919
59 A = 6717304
01 meter
Y = -3524800
55 meter E =
0011755
Z = 5155928
48 I = 51
35946
XDOT = 5435
647320 Wp = 56
56124
YDOT = 5361
576702 meter/sec RA = 231
12442 deg
ZDOT = 1084
017638 TA = 23
09713
MA = 23
04434
Ha = 191
780 n
mi
Hp = 179
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8047636
46 X = 2467105
37
Y = -11564306
27 feet Y = -3497291
11 meter
Z = 16915775
87 Z = 5167879
45
XDOT = 17833
488582 XDOT = 5370
023233
YDOT = 17590
474745 feet/sec YDOT = 5421
994412 meter/sec
ZDOT = 3556
488315 ZDOT = 1110
264760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14028066
38 X = 4275754
63
Y = -353944
46 feet Y = -107882
27 meter
Z = 16962581
82 Z = 5170194
94
XDOT = -3808
884848 XDOT = -1160
948102
YDOT = 23723
748824 feet/sec YDOT = 7230
998641 meter/sec
ZDOT = 3660
099295 ZDOT = 1115
598265
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 00128U 09252
93191549
00020000 00000-0 20000-3 0 9098
2 00128 51
6393 231
7907 0010897 37
4998 322
6924 15
75121308 1871
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09252
93191549 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 231
7907 deg
Eccentricity:
0010897
Arg of perigee: 37
4998 deg
Mean anomaly: 322
6924 deg
Mean motion: 15
75121308 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 187
Checksum: 301
Coasting Arc #11 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2009/253/21:10:45
662
Vector Time (MET): 012/17:11:08
704
Weight (LBS) : 233468
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4954317
43 A = 6728769
70 meter
Y = -4506559
52 meter E =
0021846
Z = -535308
49 I = 51
41721
XDOT = 2899
622523 Wp = 40
98857
YDOT = -3881
562245 meter/sec RA = 225
94642 deg
ZDOT = 5995
126469 TA = 313
16148
MA = 313
34388
Ha = 191
806 n
mi
Hp = 178
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16254322
29 X = -4900955
63
Y = -14785300
26 feet Y = -4561663
25 meter
Z = -1756261
44 Z = -559247
14
XDOT = 9513
197255 XDOT = 2913
687805
YDOT = -12734
784270 feet/sec YDOT = -3849
058291 meter/sec
ZDOT = 19669
050096 ZDOT = 6009
247147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2049633
91 X = 624728
41
Y = -21869300
30 feet Y = -6665762
73 meter
Z = -1850744
74 Z = -564107
00
XDOT = 14231
668607 XDOT = 4337
812591
YDOT = -294
847821 feet/sec YDOT = -89
869616 meter/sec
ZDOT = 19724
376030 ZDOT = 6011
989814
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 00128U 09253
88355765
00020000 00000-0 20000-3 0 9107
2 00128 51
6383 226
8945 0010831 40
6402 319
5568 15
75149722 2028
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09253
88355765 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 226
8945 deg
Eccentricity:
0010831
Arg of perigee: 40
6402 deg
Mean anomaly: 319
5568 deg
Mean motion: 15
75149722 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 202
Checksum: 277
Coasting Arc #12 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2009/254/21:15:59
992
Vector Time (MET): 013/17:16:23
034
Weight (LBS) : 233468
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4274124
26 A = 6718001
48 meter
Y = 1546452
90 meter E =
0020769
Z = -4963138
51 I = 51
40222
XDOT = -4454
098301 Wp = 78
40961
YDOT = -5941
450019 meter/sec RA = 220
75493 deg
ZDOT = 1995
617514 TA = 210
92444
MA = 211
04690
Ha = 191
839 n
mi
Hp = 178
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14022717
40 X = -4266989
14
Y = 5073664
36 feet Y = 1498697
07 meter
Z = -16283262
83 Z = -4983884
97
XDOT = -14613
183401 XDOT = -4397
023343
YDOT = -19492
946256 feet/sec YDOT = -5990
939262 meter/sec
ZDOT = 6547
301554 ZDOT = 1974
117966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12741308
95 X = -3883550
97
Y = -7574638
74 feet Y = -2308749
89 meter
Z = -16364816
40 Z = -4987996
04
XDOT = 5271
463262 XDOT = 1606
742002
YDOT = -22750
181513 feet/sec YDOT = -6934
255325 meter/sec
ZDOT = 6462
316411 ZDOT = 1969
714042
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 00128U 09254
89863304
00020000 00000-0 20000-3 0 9113
2 00128 51
6374 221
6713 0010812 45
5108 314
6938 15
75186716 2188
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09254
89863304 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 221
6713 deg
Eccentricity:
0010812
Arg of perigee: 45
5108 deg
Mean anomaly: 314
6938 deg
Mean motion: 15
75186716 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 218
Checksum: 273
Coasting Arc #13 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2009/255/21:21:07
428
Vector Time (MET): 014/17:21:30
470
Weight (LBS) : 233468
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2211418
86 A = 6722883
45 meter
Y = 5189389
67 meter E =
0016091
Z = -3676581
85 I = 51
44218
XDOT = -6360
643900 Wp = 59
82396
YDOT = -335
432232 meter/sec RA = 215
61939 deg
ZDOT = -4305
379898 TA = 164
46404
MA = 164
41460
Ha = 191
916 n
mi
Hp = 178
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7255311
22 X = 2171086
03
Y = 17025556
66 feet Y = 5213893
59 meter
Z = -12062276
41 Z = -3665936
68
XDOT = -20868
254264 XDOT = -6335
505536
YDOT = -1100
499450 feet/sec YDOT = -406
420083 meter/sec
ZDOT = -14125
262133 ZDOT = -4336
218859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7890287
12 X = -2404959
52
Y = 16771089
06 feet Y = 5111827
94 meter
Z = -12020048
81 Z = -3663710
88
XDOT = -11732
281648 XDOT = -3575
999446
YDOT = -15716
105289 feet/sec YDOT = -4790
268892 meter/sec
ZDOT = -14246
668589 ZDOT = -4342
384586
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 00128U 09255
91369575
00020000 00000-0 20000-3 0 9129
2 00128 51
6372 216
4491 0010915 49
4507 310
7605 15
75218271 2349
Satellite: SHUTTLE
Catalog Number: 00128
Epoch time: 09255
91369575 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 216
4491 deg
Eccentricity:
0010915
Arg of perigee: 49
4507 deg
Mean anomaly: 310
7605 deg
Mean motion: 15
75218271 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 234
Checksum: 270
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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