Date:
June 10th 2008
SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2008/152/21:02:11 970 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 69 ET - UTC (sec) : 65 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
163/12:57:17
637 -2
5 -0
0 3
0
010/15:55:05
666 -1
1 0
0 186
3
000/00:00:11
333 1
3 -3
0 180
3
163/13:25:14
751 1
2 1
5 1
5
010/16:23:02
781 0
9 0
0 186
5
000/00:00:05
561 -0
3 -0
0 181
3
Coasting Arc #1 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2008/161/10:33:31
000
Vector Time (MET): 008/13:31:19
030
Weight (LBS) : 213147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4038480
58 A = 6712596
04 meter
Y = 1316317
20 meter E =
0006468
Z = 5199629
81 I = 51
88995
XDOT = -3578
806968 Wp = 350
89336
YDOT = -6738
544048 meter/sec RA = 55
72618 deg
ZDOT = -1067
632304 TA = 109
28553
MA = 109
21556
Ha = 185
550 n
mi
Hp = 180
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13249608
19 X = -4078158
42
Y = 4318625
99 feet Y = 1270934
05 meter
Z = 17059152
93 Z = 5179914
77
XDOT = -11741
492677 XDOT = -3498
003184
YDOT = -22108
084148 feet/sec YDOT = -6778
112376 meter/sec
ZDOT = -3502
730656 ZDOT = -1084
822699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3930699
77 X = -1198077
29
Y = 13465970
36 feet Y = 4104427
77 meter
Z = 16983362
09 Z = 5176528
77
XDOT = -23891
453445 XDOT = -7282
115010
YDOT = -2446
787911 feet/sec YDOT = -745
780955 meter/sec
ZDOT = -3569
478411 ZDOT = -1087
977020
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 32960U 08027A 08161
48566522
00020000 00000-0 70000-3 0 9005
2 32960 51
6393 56
1031 0005960 316
2323 43
8368 15
76782446 1378
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08161
48566522 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 56
1031 deg
Eccentricity:
0005960
Arg of perigee: 316
2323 deg
Mean anomaly: 43
8368 deg
Mean motion: 15
76782446 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 137
Checksum: 283
Coasting Arc #2 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2008/162/10:37:47
356
Vector Time (MET): 009/13:35:35
385
Weight (LBS) : 213147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1468607
77 A = 6719882
74 meter
Y = 5724131
08 meter E =
0010572
Z = 3185320
53 I = 51
89736
XDOT = -5883
648594 Wp = 59
75893
YDOT = -1186
433692 meter/sec RA = 50
60632 deg
ZDOT = 4838
131724 TA = 337
32363
MA = 337
37030
Ha = 185
649 n
mi
Hp = 180
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4818266
97 X = 1389016
80
Y = 18779957
61 feet Y = 5740108
48 meter
Z = 10450526
68 Z = 3192262
40
XDOT = -19303
309034 XDOT = -5893
447146
YDOT = -3892
498988 feet/sec YDOT = -1252
283403 meter/sec
ZDOT = 15873
135576 ZDOT = 4809
525056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18432868
71 X = 5618338
38
Y = 5963432
66 feet Y = 1817654
27 meter
Z = 10477730
41 Z = 3193612
23
XDOT = -13179
763778 XDOT = -4017
191999
YDOT = 13005
022047 feet/sec YDOT = 3963
930720 meter/sec
ZDOT = 15762
902850 ZDOT = 4804
532789
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 32960U 08027A 08162
49972106
00020000 00000-0 70000-3 0 9017
2 32960 51
6398 50
8734 0005911 320
7123 39
3612 15
76770600 1537
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08162
49972106 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 50
8734 deg
Eccentricity:
0005911
Arg of perigee: 320
7123 deg
Mean anomaly: 39
3612 deg
Mean motion: 15
76770600 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 153
Checksum: 274
Coasting Arc #3 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2008/163/10:42:06
087
Vector Time (MET): 010/13:39:54
117
Weight (LBS) : 213147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5533791
56 A = 6722237
94 meter
Y = 3014193
26 meter E =
0009073
Z = -2325625
39 I = 51
88552
XDOT = -663
473572 Wp = 2
84481
YDOT = 5412
302030 meter/sec RA = 45
40659 deg
ZDOT = 5445
811400 TA = 331
04708
MA = 331
09738
Ha = 185
975 n
mi
Hp = 180
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18155484
11 X = 5510972
58
Y = 9889085
51 feet Y = 3075947
98 meter
Z = -7630004
55 Z = -2298797
22
XDOT = -2176
750564 XDOT = -750
400306
YDOT = 17756
896425 feet/sec YDOT = 5404
395998 meter/sec
ZDOT = 17866
835301 ZDOT = 5442
377746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17678540
38 X = 5388419
11
Y = -10791387
81 feet Y = -3289215
00 meter
Z = -7526469
57 Z = -2294067
93
XDOT = 13436
691418 XDOT = 4095
503544
YDOT = 9582
414531 feet/sec YDOT = 2920
719949 meter/sec
ZDOT = 17854
063851 ZDOT = 5441
918662
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 32960U 08027A 08163
45045022
00020000 00000-0 70000-3 0 9023
2 32960 51
6405 45
9714 0006046 323
5696 36
5057 15
76688529 1681
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08163
45045022 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 45
9714 deg
Eccentricity:
0006046
Arg of perigee: 323
5696 deg
Mean anomaly: 36
5057 deg
Mean motion: 15
76688529 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 168
Checksum: 294
Coasting Arc #4 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2008/163/12:57:23
303
Vector Time (MET): 010/15:55:11
333
Weight (LBS) : 213073
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5586551
86 A = 6721087
52 meter
Y = -2438721
14 meter E =
0011227
Z = 2826754
84 I = 51
88010
XDOT = -86
324772 Wp = 72
20311
YDOT = -5757
043222 meter/sec RA = 44
92119 deg
ZDOT = -5117
473551 TA = 75
46993
MA = 75
34541
Ha = 186
332 n
mi
Hp = 180
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18328582
23 X = -5572598
40
Y = -8001053
62 feet Y = -2501115
49 meter
Z = 9274130
06 Z = 2799648
89
XDOT = -283
217757 XDOT = 2
917639
YDOT = -18887
937081 feet/sec YDOT = -5757
508955 meter/sec
ZDOT = -16789
611387 ZDOT = -5117
676845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6753840
68 X = -2058570
64
Y = 18875058
43 feet Y = 5753117
81 meter
Z = 9169573
57 Z = 2794886
02
XDOT = -17456
792658 XDOT = -5320
830402
YDOT = 1942
778483 feet/sec YDOT = 592
158882 meter/sec
ZDOT = -16790
869827 ZDOT = -5117
857123
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 32960U 08027A 08163
57721636
00020000 00000-0 70000-3 0 9039
2 32960 51
6408 45
3182 0006276 335
2832 24
8031 15
76711459 1708
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08163
57721636 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 45
3182 deg
Eccentricity:
0006276
Arg of perigee: 335
2832 deg
Mean anomaly: 24
8031 deg
Mean motion: 15
76711459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 170
Checksum: 277
Coasting Arc #5 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2008/163/13:25:17
532
Vector Time (MET): 010/16:23:05
561
Weight (LBS) : 213029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1835179
12 A = 6713743
73 meter
Y = -3893928
05 meter E =
0012777
Z = -5162142
75 I = 51
85103
XDOT = 6048
218668 Wp = 51
99243
YDOT = 4579
032000 meter/sec RA = 44
85484 deg
ZDOT = -1298
351326 TA = 205
58882
MA = 205
65211
Ha = 186
461 n
mi
Hp = 181
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6020928
88 X = 1903662
07
Y = -12775354
50 feet Y = -3873022
49 meter
Z = -16936163
87 Z = -5153061
55
XDOT = 19843
237100 XDOT = 6002
872866
YDOT = 15023
070865 feet/sec YDOT = 4646
413261 meter/sec
ZDOT = -4259
682829 ZDOT = -1269
078580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13697283
73 X = -4174932
08
Y = -3608021
27 feet Y = -1099724
88 meter
Z = -16901524
03 Z = -5151584
53
XDOT = 10759
559400 XDOT = 3279
513705
YDOT = -21337
207853 feet/sec YDOT = -6503
580954 meter/sec
ZDOT = -4146
607605 ZDOT = -1263
885998
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 32960U 08027A 08163
57721664
00020000 00000-0 70000-3 0 9041
2 32960 51
6395 45
3173 0006676 324
1763 35
8953 15
76423299 1704
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08163
57721664 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 45
3173 deg
Eccentricity:
0006676
Arg of perigee: 324
1763 deg
Mean anomaly: 35
8953 deg
Mean motion: 15
76423299 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 170
Checksum: 305
Coasting Arc #6 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2008/164/13:30:13
155
Vector Time (MET): 011/16:28:01
185
Weight (LBS) : 213029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4241485
76 A = 6724390
64 meter
Y = -5009489
77 meter E =
0001844
Z = -1458052
14 I = 51
86502
XDOT = 4551
920864 Wp = 128
28502
YDOT = -2161
337751 meter/sec RA = 39
70246 deg
ZDOT = -5821
835518 TA = 67
71806
MA = 67
69851
Ha = 186
568 n
mi
Hp = 181
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13915635
69 X = -4178070
62
Y = -16435333
90 feet Y = -5056565
73 meter
Z = -4783635
65 Z = -1478504
04
XDOT = 14934
123571 XDOT = 4604
032586
YDOT = -7091
003121 feet/sec YDOT = -2110
143441 meter/sec
ZDOT = -19100
510230 ZDOT = -5799
595834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12874806
95 X = -3924241
16
Y = 17240678
47 feet Y = 5254958
80 meter
Z = -4862781
00 Z = -1482175
65
XDOT = -9047
495105 XDOT = -2757
676508
YDOT = -12114
128639 feet/sec YDOT = -3692
386409 meter/sec
ZDOT = -19015
066997 ZDOT = -5795
792421
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 32960U 08027A 08164
59149304
00020000 00000-0 70000-3 0 9050
2 32960 51
6395 40
0902 0006621 326
9592 33
1158 15
76406482 1866
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08164
59149304 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 40
0902 deg
Eccentricity:
0006621
Arg of perigee: 326
9592 deg
Mean anomaly: 33
1158 deg
Mean motion: 15
76406482 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 186
Checksum: 286
Coasting Arc #7 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2008/165/13:34:36
312
Vector Time (MET): 012/16:32:24
342
Weight (LBS) : 213029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5468281
63 A = 6718585
02 meter
Y = -35202
56 meter E =
0011014
Z = 3902825
56 I = 51
82264
XDOT = -2880
703547 Wp = 44
59316
YDOT = -5867
981034 meter/sec RA = 34
50592 deg
ZDOT = -4074
513383 TA = 87
76087
MA = 87
63476
Ha = 186
678 n
mi
Hp = 180
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17940556
52 X = -5486440
97
Y = -115493
96 feet Y = -96454
12 meter
Z = 12804545
80 Z = 3876216
28
XDOT = -9451
127124 XDOT = -2795
079321
YDOT = -19251
906280 feet/sec YDOT = -5899
715371 meter/sec
ZDOT = -13367
826060 ZDOT = -4088
300843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4591870
42 X = 1399602
11
Y = 17418514
29 feet Y = 5309163
16 meter
Z = 12702101
65 Z = 3871600
58
XDOT = -14866
179107 XDOT = -4531
211392
YDOT = 13741
486483 feet/sec YDOT = 4188
405080 meter/sec
ZDOT = -13421
376793 ZDOT = -4090
835647
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 32960U 08027A 08165
60575393
00020000 00000-0 70000-3 0 9065
2 32960 51
6396 34
8615 0006848 330
8130 29
2651 15
76490891 2022
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08165
60575393 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 34
8615 deg
Eccentricity:
0006848
Arg of perigee: 330
8130 deg
Mean anomaly: 29
2651 deg
Mean motion: 15
76490891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 202
Checksum: 297
Coasting Arc #8 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2008/166/13:39:13
227
Vector Time (MET): 013/16:37:01
257
Weight (LBS) : 213029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 135690
77 A = 6714623
30 meter
Y = 4541646
60 meter E =
0003591
Z = 4940955
91 I = 51
78266
XDOT = -7109
516635 Wp = 39
94535
YDOT = -2090
009895 meter/sec RA = 29
38935 deg
ZDOT = 2118
203884 TA = 29
58903
MA = 29
56871
Ha = 186
907 n
mi
Hp = 180
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 445179
68 X = 60892
75
Y = 14900415
36 feet Y = 4542744
94 meter
Z = 16210485
26 Z = 4941434
16
XDOT = -23325
185812 XDOT = -7095
907378
YDOT = -6856
987846 feet/sec YDOT = -2169
436836 meter/sec
ZDOT = 6949
487809 ZDOT = 2083
698189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14123321
65 X = 4304788
44
Y = -4762459
05 feet Y = -1451597
52 meter
Z = 16212685
31 Z = 4941626
48
XDOT = 44
637095 XDOT = 13
605387
YDOT = 23316
773009 feet/sec YDOT = 7106
952413 meter/sec
ZDOT = 6816
480703 ZDOT = 2077
663318
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 32960U 08027A 08166
62000791
00020000 00000-0 70000-3 0 9074
2 32960 51
6383 29
6329 0006728 336
0149 24
0701 15
76431988 2185
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08166
62000791 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 29
6329 deg
Eccentricity:
0006728
Arg of perigee: 336
0149 deg
Mean anomaly: 24
0701 deg
Mean motion: 15
76431988 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 218
Checksum: 289
Coasting Arc #9 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2008/167/13:44:18
250
Vector Time (MET): 014/16:42:06
279
Weight (LBS) : 213029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5799090
45 A = 6724838
48 meter
Y = 3290844
37 meter E =
0016573
Z = 790720
56 I = 51
79036
XDOT = -2992
339196 Wp = 30
41804
YDOT = 3824
189385 meter/sec RA = 24
21738 deg
ZDOT = 5989
751278 TA = 338
20154
MA = 338
27198
Ha = 186
859 n
mi
Hp = 180
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19025887
31 X = 5758019
49
Y = 10796733
49 feet Y = 3355463
33 meter
Z = 2594227
57 Z = 818793
69
XDOT = -9817
385815 XDOT = -3063
976913
YDOT = 12546
553101 feet/sec YDOT = 3790
325686 meter/sec
ZDOT = 19651
414954 ZDOT = 5975
041035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3817217
56 X = 1163487
91
Y = -21526933
44 feet Y = -6561409
31 meter
Z = 2702562
80 Z = 823741
14
XDOT = 13575
106932 XDOT = 4137
692593
YDOT = 4883
115924 feet/sec YDOT = 1488
373734 meter/sec
ZDOT = 19595
078901 ZDOT = 5972
580049
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 32960U 08027A 08167
63424263
00020000 00000-0 70000-3 0 9081
2 32960 51
6374 24
4041 0006674 338
6527 21
4358 15
76493078 2342
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08167
63424263 = yrday
fracday
Element set: 908
Inclination: 51
6374 deg
RA of node: 24
4041 deg
Eccentricity:
0006674
Arg of perigee: 338
6527 deg
Mean anomaly: 21
4358 deg
Mean motion: 15
76493078 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 234
Checksum: 293
Coasting Arc #10 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2008/168/13:48:48
021
Vector Time (MET): 015/16:46:36
050
Weight (LBS) : 213029
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4796908
54 A = 6717093
19 meter
Y = -1927068
77 meter E =
0006859
Z = -4292135
13 I = 51
73653
XDOT = 5016
040551 Wp = 61
45783
YDOT = 4665
017153 meter/sec RA = 19
02174 deg
ZDOT = 3518
904145 TA = 244
09547
MA = 244
16619
Ha = 186
978 n
mi
Hp = 180
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15737888
90 X = 4838951
39
Y = -6322404
10 feet Y = -1873191
06 meter
Z = -14081808
17 Z = -4268729
81
XDOT = 16456
825954 XDOT = 4946
408447
YDOT = 15305
174388 feet/sec YDOT = 4720
719352 meter/sec
ZDOT = 11544
961107 ZDOT = 3543
104078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11712426
26 X = -3569947
52
Y = -12369261
05 feet Y = -3770150
77 meter
Z = -13991844
56 Z = -4264714
22
XDOT = 7276
107846 XDOT = 2217
757672
YDOT = -20027
153027 feet/sec YDOT = -6104
276243 meter/sec
ZDOT = 11638
489326 ZDOT = 3547
411547
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 32960U 08027A 08168
58507368
00020000 00000-0 70000-3 0 9095
2 32960 51
6369 19
5019 0006538 342
5260 17
5678 15
76516797 2494
Satellite: SHUTTLE
Catalog Number: 32960
Epoch time: 08168
58507368 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 19
5019 deg
Eccentricity:
0006538
Arg of perigee: 342
5260 deg
Mean anomaly: 17
5678 deg
Mean motion: 15
76516797 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 249
Checksum: 329
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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