Date:
February 20th 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
051/00:10:07
260 -0
1 -0
1 0
1
011/14:56:00
279 -0
1 0
1 190
9
000/00:00:00
558 0
1 0
0 180
2
051/02:09:12
562 0
2 -0
0 3
0
011/16:55:05
581 2
6 -0
0 190
5
000/00:00:11
162 -1
4 -3
0 180
4
051/02:37:12
560 -0
5 -3
0 3
0
011/17:23:05
579 2
9 0
0 189
4
000/00:00:11
158 -0
7 0
0 180
3
052/08:05:17
144 -14
4 -33
0 33
0
012/22:51:10
163 -18
0 -0
0 189
2
000/00:00:20
326 23
6 0
4 161
2
Coasting Arc #1 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2010/050/13:07:36
000
Vector Time (MET): 011/03:53:29
019
Weight (LBS) : 209941
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1700304
55 A = 6719403
53 meter
Y = -4762697
64 meter E =
0017461
Z = 4427708
37 I = 51
94345
XDOT = 4960
131949 Wp = 22
69234
YDOT = -4869
021236 meter/sec RA = 113
62350 deg
ZDOT = -3312
563638 TA = 100
52560
MA = 100
32883
Ha = 190
745 n
mi
Hp = 180
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5578427
00 X = -1668402
44
Y = -15625648
42 feet Y = -4781542
53 meter
Z = 14526602
28 Z = 4419526
01
XDOT = 16273
398783 XDOT = 5030
328617
YDOT = -15974
479122 feet/sec YDOT = -4813
133290 meter/sec
ZDOT = -10867
990939 ZDOT = -3288
296906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1571848
02 X = -479099
28
Y = -16545602
23 feet Y = -5043099
56 meter
Z = 14493938
41 Z = 4417752
43
XDOT = 18609
261775 XDOT = 5672
102989
YDOT = -11261
818709 feet/sec YDOT = -3432
602342 meter/sec
ZDOT = -10771
813130 ZDOT = -3283
248642
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
58874169
00020000 00000-0 20000-3 0 9003
2 36394 51
6439 114
3097 0012948 351
5651 8
5294 15
75506382 1786
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10050
58874169 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 114
3097 deg
Eccentricity:
0012948
Arg of perigee: 351
5651 deg
Mean anomaly: 8
5294 deg
Mean motion: 15
75506382 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 178
Checksum: 306
Coasting Arc #2 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2010/051/00:10:07
539
Vector Time (MET): 011/14:56:00
558
Weight (LBS) : 209937
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197290
61 A = 6724096
16 meter
Y = -4334359
40 meter E =
0011710
Z = -2984654
91 I = 51
96616
XDOT = 2072
811107 Wp = 12
83918
YDOT = 5459
027602 meter/sec RA = 111
31451 deg
ZDOT = -5005
279783 TA = 201
41959
MA = 201
46863
Ha = 190
874 n
mi
Hp = 180
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13770638
48 X = 4259969
40
Y = -14220339
22 feet Y = -4287048
36 meter
Z = -9792174
89 Z = -2964112
32
XDOT = 6800
561374 XDOT = 2035
896570
YDOT = 17910
195546 feet/sec YDOT = 5482
012179 meter/sec
ZDOT = -16421
521598 ZDOT = -4995
299949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18928638
50 X = -5769449
02
Y = 5928153
80 feet Y = 1806901
28 meter
Z = -9710759
90 Z = -2959839
62
XDOT = 2887
818364 XDOT = 880
207037
YDOT = -17653
867174 feet/sec YDOT = -5380
898715 meter/sec
ZDOT = -16381
698096 ZDOT = -4993
141580
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
03275014
00020000 00000-0 20000-3 0 9019
2 36394 51
6455 112
0257 0013208 352
9436 7
1540 15
75502486 1851
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
03275014 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 112
0257 deg
Eccentricity:
0013208
Arg of perigee: 352
9436 deg
Mean anomaly: 7
1540 deg
Mean motion: 15
75502486 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 185
Checksum: 257
Coasting Arc #3 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2010/051/02:09:18
143
Vector Time (MET): 011/16:55:11
162
Weight (LBS) : 209864
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 350183
52 A = 6723580
65 meter
Y = 5938692
44 meter E =
0013600
Z = -3118927
23 I = 51
96331
XDOT = -5201
707429 Wp = 8
11520
YDOT = 2875
332564 meter/sec RA = 110
83970 deg
ZDOT = 4906
570381 TA = 315
76038
MA = 315
86903
Ha = 190
525 n
mi
Hp = 180
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1148896
07 X = 298867
22
Y = 19483899
08 feet Y = 5942323
25 meter
Z = -10232700
87 Z = -3117350
82
XDOT = -17065
969256 XDOT = -5257
324345
YDOT = 9433
505788 feet/sec YDOT = 2816
823369 meter/sec
ZDOT = 16097
671855 ZDOT = 4881
165566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1706224
99 X = -520057
38
Y = -19446425
98 feet Y = -5927270
64 meter
Z = -10226229
29 Z = -3116954
69
XDOT = 15495
664329 XDOT = 4723
078488
YDOT = -9744
660203 feet/sec YDOT = -2970
172430 meter/sec
ZDOT = 15996
896812 ZDOT = 4875
854148
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
09617768
00020000 00000-0 20000-3 0 9022
2 36394 51
6431 111
6973 0012690 348
4895 11
5977 15
75530611 1863
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
09617768 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 111
6973 deg
Eccentricity:
0012690
Arg of perigee: 348
4895 deg
Mean anomaly: 11
5977 deg
Mean motion: 15
75530611 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 186
Checksum: 302
Coasting Arc #4 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2010/051/02:37:18
138
Vector Time (MET): 011/17:23:11
158
Weight (LBS) : 209791
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4366070
81 A = 6715133
75 meter
Y = 264988
80 meter E =
0008900
Z = 5093471
54 I = 51
93958
XDOT = 1441
005517 Wp = 356
49332
YDOT = -7392
672784 meter/sec RA = 110
77775 deg
ZDOT = 1628
660996 TA = 77
98557
MA = 77
88582
Ha = 189
399 n
mi
Hp = 180
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14324379
29 X = -4393453
63
Y = 869385
82 feet Y = 215986
89 meter
Z = 16710864
64 Z = 5072194
85
XDOT = 4727
708389 XDOT = 1515
694890
YDOT = -24254
175801 feet/sec YDOT = -7376
132551 meter/sec
ZDOT = 5343
375970 ZDOT = 1635
842910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14136249
47 X = 4308728
84
Y = -2987696
71 feet Y = -910649
96 meter
Z = 16626388
36 Z = 5067723
17
XDOT = -1285
007249 XDOT = -391
670210
YDOT = 23650
633826 feet/sec YDOT = 7208
713190 meter/sec
ZDOT = 5371
630320 ZDOT = 1637
272921
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
15958458
00020000 00000-0 20000-3 0 9034
2 36394 51
6428 111
3703 0012691 338
7198 21
3436 15
76051647 1874
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10051
15958458 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 111
3703 deg
Eccentricity:
0012691
Arg of perigee: 338
7198 deg
Mean anomaly: 21
3436 deg
Mean motion: 15
76051647 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 187
Checksum: 295
Coasting Arc #5 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2010/052/02:42:21
347
Vector Time (MET): 012/17:28:14
366
Weight (LBS) : 209791
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2597538
10 A = 6725692
33 meter
Y = 6089902
78 meter E =
0021040
Z = 1101450
86 I = 51
98440
XDOT = -4041
231501 Wp = 21
40334
YDOT = -2801
683659 meter/sec RA = 105
62728 deg
ZDOT = 5943
986141 TA = 350
61946
MA = 350
65870
Ha = 189
376 n
mi
Hp = 179
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8522106
63 X = -2670828
50
Y = 19979996
01 feet Y = 6060430
80 meter
Z = 3613683
93 Z = 1088654
10
XDOT = -13258
633533 XDOT = -4038
460573
YDOT = -9191
875523 feet/sec YDOT = -2846
882577 meter/sec
ZDOT = 19501
266868 ZDOT = 5924
360760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4672020
04 X = 1424031
71
Y = -21221733
77 feet Y = -6468384
45 meter
Z = 3563074
26 Z = 1086025
03
XDOT = 13303
510909 XDOT = 4054
910125
YDOT = 6198
901735 feet/sec YDOT = 1889
425249 meter/sec
ZDOT = 19423
238176 ZDOT = 5920
202996
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
17406232
00020000 00000-0 20000-3 0 9046
2 36394 51
6419 106
1436 0012649 342
1608 17
9111 15
76106252 2030
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10052
17406232 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 106
1436 deg
Eccentricity:
0012649
Arg of perigee: 342
1608 deg
Mean anomaly: 17
9111 deg
Mean motion: 15
76106252 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 203
Checksum: 253
Coasting Arc #6 (Orbit 205)
---------------------------------------
Vector Time (GMT): 2010/052/08:05:27
307
Vector Time (MET): 012/22:51:20
326
Weight (LBS) : 209106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3270738
54 A = 6706340
78 meter
Y = -5401950
99 meter E =
0033158
Z = -2322382
96 I = 51
98326
XDOT = 3275
652403 Wp = 20
28180
YDOT = 4325
649300 meter/sec RA = 104
48560 deg
ZDOT = -5440
986696 TA = 185
70165
MA = 185
73950
Ha = 189
177 n
mi
Hp = 161
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10730769
48 X = 3342213
15
Y = -17722936
31 feet Y = -5364957
20 meter
Z = -7619366
68 Z = -2306320
26
XDOT = 10746
891085 XDOT = 3253
445034
YDOT = 14191
762795 feet/sec YDOT = 4362
173995 meter/sec
ZDOT = -17851
006221 ZDOT = -5425
127667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18040532
24 X = 5498754
23
Y = 10235052
50 feet Y = 3119644
00 meter
Z = -7555761
41 Z = -2302996
08
XDOT = -13110
705346 XDOT = -3996
142990
YDOT = 9959
809082 feet/sec YDOT = 3035
749808 meter/sec
ZDOT = -17787
882781 ZDOT = -5421
746672
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
36419237
00020000 00000-0 20000-3 0 9057
2 36394 51
6450 105
1620 0036068 11
8813 348
3197 15
82296703 2064
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10052
36419237 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 105
1620 deg
Eccentricity:
0036068
Arg of perigee: 11
8813 deg
Mean anomaly: 348
3197 deg
Mean motion: 15
82296703 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 206
Checksum: 278
Coasting Arc #7 (Orbit 221)
---------------------------------------
Vector Time (GMT): 2010/053/08:06:33
906
Vector Time (MET): 013/22:52:26
925
Weight (LBS) : 209106
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1040780
13 A = 6705747
61 meter
Y = -6115858
53 meter E =
0039144
Z = 2573849
79 I = 51
98794
XDOT = 4686
238215 Wp = 36
46126
YDOT = -3053
294972 meter/sec RA = 99
26425 deg
ZDOT = -5288
432196 TA = 114
43563
MA = 114
02676
Ha = 189
295 n
mi
Hp = 160
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3414632
96 X = -984782
45
Y = -20065152
67 feet Y = -6127189
86 meter
Z = 8444389
07 Z = 2568929
66
XDOT = 15374
797292 XDOT = 4745
739418
YDOT = -10017
371955 feet/sec YDOT = -3000
531071 meter/sec
ZDOT = -17350
499330 ZDOT = -5265
522248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19856550
37 X = 6052276
55
Y = -4507815
34 feet Y = -1373982
12 meter
Z = 8424653
41 Z = 2567834
36
XDOT = 10483
996289 XDOT = 3195
522069
YDOT = 13483
983821 feet/sec YDOT = 4109
918269 meter/sec
ZDOT = -17259
612132 ZDOT = -5260
729778
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
37469690
00020000 00000-0 20000-3 0 9068
2 36394 51
6451 99
9091 0036049 15
8178 344
4107 15
82312405 2228
Satellite: SHUTTLE
Catalog Number: 36394
Epoch time: 10053
37469690 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 99
9091 deg
Eccentricity:
0036049
Arg of perigee: 15
8178 deg
Mean anomaly: 344
4107 deg
Mean motion: 15
82312405 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 222
Checksum: 293
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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