Date: January 26th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 200 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

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


357/10:54:56 325 -43 9 50 7 50 7
N/A -0 3 0 0 133 9
000/00:00:36 650 -25 3 -0 0 118 9

357/11:31:07 795 12 8 24 4 24 4
N/A -9 8 -0 0 136 8
000/00:00:17 591 18 3 0 0 127 7

357/12:07:43 653 -1 2 -0 0 3 4
N/A 2 4 -3 4 136 8
000/00:00:02 447 2 1 -0 0 127 6

359/07:54:40 538 -6 3 9 8 9 8
N/A -5 9 0 0 136 9
000/00:00:07 077 4 7 0 0 131 8

360/06:15:57 021 -25 4 36 3 36 3
N/A -19 5 -0 0 154 1
000/00:00:26 042 17 1 0 0 135 3

360/07:00:50 655 58 2 83 2 83 2
N/A 44 6 -0 0 182 6
000/00:00:59 309 -39 2 0 1 153 3

360/07:46:31 677 -33 3 44 1 44 3
N/A -22 4 0 0 183 1
000/00:00:31 354 18 8 -4 2 177 5

Coasting Arc #1 (Orbit 1)
---------------------------------------

Vector Time (GMT): 2007/357/07:13:19
000
Vector Time (MET): N/A
Weight (LBS)     : 15432
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2284552
13                 A    =         6585732
04  meter
 Y    =       -4768454
40  meter          E    =           
0040804
 Z    =        3889324
59                 I    =           51
48651
 XDOT =       6715
785278                 Wp   =           84
85803
 YDOT =         52
479072  meter/sec      RA   =          208
57089  deg
 ZDOT =       3977
916883                 TA   =          324
36632
                                          MA   =          324
63805
                                          Ha   =            125
479  n
mi
                                          Hp   =             97
726

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7495249
78                 X    =        -2249954
46
 Y    =      -15644535
42  feet           Y    =        -4793808
88  meter
 Z    =       12760251
29                 Z    =         3878309
28
 XDOT =      22033
416266                 XDOT =        6695
375243
 YDOT =        172
175433  feet/sec       YDOT =         127
463878  meter/sec
 ZDOT =      13050
908408                 ZDOT =        4010
492736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12257214
44                 X    =         3735998
96
 Y    =       12319675
67  feet           Y    =         3755037
14  meter
 Z    =       12717726
06                 Z    =         3876362
90
 XDOT =     -19915
599143                 XDOT =       -6070
274619
 YDOT =       6107
703910  feet/sec       YDOT =        1861
628152  meter/sec
 ZDOT =      13175
165527                 ZDOT =        4015
790453


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

ISS
1 25544U 98067A   07357
35412034  
00020000  00000-0  20000-3 0  9003
2 25544  51
6448 209
2179 0030128  78
4753 281
9817 16
24369710    25


Satellite: ISS
Catalog Number: 25544
Epoch time:      07357
35412034   =   yrday
fracday
Element set:     900
Inclination:       51
6448  deg
RA of node:       209
2179  deg
Eccentricity:     
0030128     
Arg of perigee:    78
4753  deg
Mean anomaly:     281
9817  deg
Mean motion:   16
24369710  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               2
Checksum:              280


Coasting Arc #2 (Orbit 3)
---------------------------------------

Vector Time (GMT): 2007/357/10:55:14
650
Vector Time (MET): N/A
Weight (LBS)     : 15351
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2136530
07                 A    =         6610957
49  meter
 Y    =        4762847
11  meter          E    =           
0017968
 Z    =       -4050044
80                 I    =           51
49029
 XDOT =      -6782
353240                 Wp   =          160
97858
 YDOT =       -159
453966  meter/sec      RA   =          207
71638  deg
 ZDOT =      -3786
895822                 TA   =           70
59215
                                          MA   =           70
39804
                                          Ha   =            133
921  n
mi
                                          Hp   =            118
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7009613
10                 X    =         2102786
83
 Y    =       15626138
81  feet           Y    =         4786551
14  meter
 Z    =      -13287548
55                 Z    =        -4039746
51
 XDOT =     -22251
815092                 XDOT =       -6761
670020
 YDOT =       -523
142934  feet/sec       YDOT =        -235
181679  meter/sec
 ZDOT =     -12424
198891                 ZDOT =       -3819
794382

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16942888
08                 X    =        -5164192
29
 Y    =        2702831
09  feet           Y    =          823822
92  meter
 Z    =      -13247757
70                 Z    =        -4037916
55
 XDOT =       6563
939195                 XDOT =        2000
688666
 YDOT =     -20018
820848  feet/sec       YDOT =       -6101
736594  meter/sec
 ZDOT =     -12549
701585                 ZDOT =       -3825
149043


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

ISS
1 25544U 98067A   07357
47722491  
00020000  00000-0  20000-3 0  9018
2 25544  51
6460 208
5389 0019673 184
0736 176
0292 16
14840982    48


Satellite: ISS
Catalog Number: 25544
Epoch time:      07357
47722491   =   yrday
fracday
Element set:     901
Inclination:       51
6460  deg
RA of node:       208
5389  deg
Eccentricity:     
0019673     
Arg of perigee:   184
0736  deg
Mean anomaly:     176
0292  deg
Mean motion:   16
14840982  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               4
Checksum:              298


Coasting Arc #3 (Orbit 4)
---------------------------------------

Vector Time (GMT): 2007/357/11:31:16
591
Vector Time (MET): N/A
Weight (LBS)     : 15312
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5071139
22                 A    =         6630014
94  meter
 Y    =       -3989223
26  meter          E    =           
0017461
 Z    =        1495926
11                 I    =           51
51279
 XDOT =       4134
157227                 Wp   =           71
42114
 YDOT =      -3056
670235  meter/sec      RA   =          207
56799  deg
 ZDOT =       5814
462654                 TA   =          305
34974
                                          MA   =          305
51282
                                          Ha   =            136
833  n
mi
                                          Hp   =            127
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16637595
87                 X    =        -5033421
18
 Y    =      -13088002
81  feet           Y    =        -4045721
02  meter
 Z    =        4907894
05                 Z    =         1471381
26
 XDOT =      13563
507964                 XDOT =        4139
784446
 YDOT =     -10028
445652  feet/sec       YDOT =       -3010
409449  meter/sec
 ZDOT =      19076
321043                 ZDOT =        5834
559499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14835579
04                 X    =         4521884
49
 Y    =      -15130278
65  feet           Y    =        -4611708
93  meter
 Z    =        4813844
66                 Z    =         1467259
85
 XDOT =       7390
026112                 XDOT =        2252
479959
 YDOT =      13391
721289  feet/sec       YDOT =        4081
796649  meter/sec
 ZDOT =      19152
649876                 ZDOT =        5837
727682


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

ISS
1 25544U 98067A   07357
53928631  
00020000  00000-0  20000-3 0  9020
2 25544  51
6456 208
2025 0004067 107
3821 252
7806 16
10260058    51


Satellite: ISS
Catalog Number: 25544
Epoch time:      07357
53928631   =   yrday
fracday
Element set:     902
Inclination:       51
6456  deg
RA of node:       208
2025  deg
Eccentricity:     
0004067     
Arg of perigee:   107
3821  deg
Mean anomaly:     252
7806  deg
Mean motion:   16
10260058  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               5
Checksum:              263


Coasting Arc #4 (Orbit 4)
---------------------------------------

Vector Time (GMT): 2007/357/12:07:44
877
Vector Time (MET): N/A
Weight (LBS)     : 15307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6173959
21                 A    =         6630026
68  meter
 Y    =        1919891
23  meter          E    =           
0018407
 Z    =        1429962
82                 I    =           51
50598
 XDOT =       -226
257291                 Wp   =          116
13939
 YDOT =       5112
325514  meter/sec      RA   =          207
40409  deg
 ZDOT =      -5838
013952                 TA   =           47
84438
                                          MA   =           47
68816
                                          Ha   =            136
818  n
mi
                                          Hp   =            127
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20255771
70                 X    =         6145085
32
 Y    =        6298855
73  feet           Y    =         1988770
21  meter
 Z    =        4691479
07                 Z    =         1459886
24
 XDOT =       -742
313948                 XDOT =        -255
047201
 YDOT =      16772
721501  feet/sec       YDOT =        5109
635576  meter/sec
 ZDOT =     -19153
589082                 ZDOT =       -5839
182017

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5284972
44                 X    =        -1610859
60
 Y    =       20517187
36  feet           Y    =         6253638
71  meter
 Z    =        4805823
11                 Z    =         1464814
88
 XDOT =     -15287
341371                 XDOT =       -4659
581650
 YDOT =        586
265213  feet/sec       YDOT =         178
693637  meter/sec
 ZDOT =     -19157
497100                 ZDOT =       -5839
205116


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

ISS
1 25544U 98067A   07357
53928738  
00020000  00000-0  20000-3 0  9039
2 25544  51
6380 208
2051 0004139 105
8457 254
3182 16
10247232    58


Satellite: ISS
Catalog Number: 25544
Epoch time:      07357
53928738   =   yrday
fracday
Element set:     903
Inclination:       51
6380  deg
RA of node:       208
2051  deg
Eccentricity:     
0004139     
Arg of perigee:   105
8457  deg
Mean anomaly:     254
3182  deg
Mean motion:   16
10247232  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:               5
Checksum:              269


Coasting Arc #5 (Orbit 20)
---------------------------------------

Vector Time (GMT): 2007/358/12:07:44
877
Vector Time (MET): N/A
Weight (LBS)     : 15307
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4890398
86                 A    =         6628056
22  meter
 Y    =        3880950
26  meter          E    =           
0009702
 Z    =       -2221330
64                 I    =           51
52759
 XDOT =      -4708
046182                 Wp   =          128
20672
 YDOT =       2802
653299  meter/sec      RA   =          202
01147  deg
 ZDOT =      -5490
346501                 TA   =           77
14441
                                          MA   =           77
03603
                                          Ha   =            136
338  n
mi
                                          Hp   =            127
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16044615
69                 X    =         4857428
78
 Y    =       12732776
46  feet           Y    =         3935453
57  meter
 Z    =       -7287830
17                 Z    =        -2197652
52
 XDOT =     -15446
345741                 XDOT =       -4712
365005
 YDOT =       9195
056754  feet/sec       YDOT =        2749
982188  meter/sec
 ZDOT =     -18012
947839                 ZDOT =       -5513
228010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11627984
00                 X    =        -3544209
52
 Y    =       16901413
22  feet           Y    =         5151550
75  meter
 Z    =       -7197081
15                 Z    =        -2193670
33
 XDOT =      -8968
618881                 XDOT =       -2733
635035
 YDOT =     -13846
798494  feet/sec       YDOT =       -4220
504181  meter/sec
 ZDOT =     -18099
939311                 ZDOT =       -5516
861502


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

ISS
1 25544U 98067A   07358
53215062  
00020000  00000-0  20000-3 0  9040
2 25544  51
6361 202
8262 0003831 111
3793 248
7798 16
10517156   217


Satellite: ISS
Catalog Number: 25544
Epoch time:      07358
53215062   =   yrday
fracday
Element set:     904
Inclination:       51
6361  deg
RA of node:       202
8262  deg
Eccentricity:     
0003831     
Arg of perigee:   111
3793  deg
Mean anomaly:     248
7798  deg
Mean motion:   16
10517156  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              21
Checksum:              269


Coasting Arc #6 (Orbit 33)
---------------------------------------

Vector Time (GMT): 2007/359/07:54:44
077
Vector Time (MET): N/A
Weight (LBS)     : 15291
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4871384
99                 A    =         6626941
34  meter
 Y    =        1870744
58  meter          E    =           
0005109
 Z    =       -4088955
64                 I    =           51
53483
 XDOT =      -4929
753635                 Wp   =           85
90851
 YDOT =      -4669
660021  meter/sec      RA   =          197
49201  deg
 ZDOT =       3740
956202                 TA   =          222
11708
                                          MA   =          222
15636
                                          Ha   =            136
910  n
mi
                                          Hp   =            131
798

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15982234
21                 X    =        -4872078
69
 Y    =        6137613
44  feet           Y    =         1816266
85  meter
 Z    =      -13415208
81                 Z    =        -4112621
93
 XDOT =     -16173
732399                 XDOT =       -4895
343090
 YDOT =     -15320
406892  feet/sec       YDOT =       -4724
595601  meter/sec
 ZDOT =      12273
478354                 ZDOT =        3717
090443

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10380042
54                 X    =         3163836
97
 Y    =      -13525213
04  feet           Y    =        -4122484
93  meter
 Z    =      -13505305
10                 Z    =        -4116416
99
 XDOT =      20859
511555                 XDOT =        6357
979122
 YDOT =       3858
851598  feet/sec       YDOT =        1176
177967  meter/sec
 ZDOT =      12181
913491                 ZDOT =        3713
047232


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

ISS
1 25544U 98067A   07359
33871659  
00020000  00000-0  20000-3 0  9050
2 25544  51
6382 198
4562 0004117 321
7112  38
3776 16
08909618   341


Satellite: ISS
Catalog Number: 25544
Epoch time:      07359
33871659   =   yrday
fracday
Element set:     905
Inclination:       51
6382  deg
RA of node:       198
4562  deg
Eccentricity:     
0004117     
Arg of perigee:   321
7112  deg
Mean anomaly:      38
3776  deg
Mean motion:   16
08909618  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              34
Checksum:              303


Coasting Arc #7 (Orbit 48)
---------------------------------------

Vector Time (GMT): 2007/360/06:16:10
042
Vector Time (MET): N/A
Weight (LBS)     : 15234
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4667597
63                 A    =         6645185
54  meter
 Y    =        2305073
91  meter          E    =           
0024944
 Z    =       -4103718
33                 I    =           51
56109
 XDOT =      -5353
002018                 Wp   =          315
28587
 YDOT =      -4211
238530  meter/sec      RA   =          192
44946  deg
 ZDOT =       3727
149911                 TA   =          352
49350
                                          MA   =          352
53078
                                          Ha   =            154
108  n
mi
                                          Hp   =            135
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15313640
52                 X    =        -4673091
58
 Y    =        7562578
44  feet           Y    =         2252848
11  meter
 Z    =      -13463642
82                 Z    =        -4126406
19
 XDOT =     -17562
342579                 XDOT =       -5323
619023
 YDOT =     -13816
399377  feet/sec       YDOT =       -4270
935130  meter/sec
 ZDOT =      12228
182123                 ZDOT =        3701
216102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14091328
03                 X    =         4295036
78
 Y    =       -9529044
54  feet           Y    =        -2904452
77  meter
 Z    =      -13549968
31                 Z    =        -4130030
34
 XDOT =      18622
952169                 XDOT =        5676
275821
 YDOT =      10311
412485  feet/sec       YDOT =        3142
918525  meter/sec
 ZDOT =      12128
758903                 ZDOT =        3696
845714


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

ISS
1 25544U 98067A   07360
27030398  
00020000  00000-0  20000-3 0  9063
2 25544  51
6371 193
4195 0032599 308
9061  50
9211 16
02268344   499


Satellite: ISS
Catalog Number: 25544
Epoch time:      07360
27030398   =   yrday
fracday
Element set:     906
Inclination:       51
6371  deg
RA of node:       193
4195  deg
Eccentricity:     
0032599     
Arg of perigee:   308
9061  deg
Mean anomaly:      50
9211  deg
Mean motion:   16
02268344  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              49
Checksum:              284


Coasting Arc #8 (Orbit 49)
---------------------------------------

Vector Time (GMT): 2007/360/07:01:20
309
Vector Time (MET): N/A
Weight (LBS)     : 15103
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4780958
14                 A    =         6689219
73  meter
 Y    =       -2254055
74  meter          E    =           
0040841
 Z    =        4056594
55                 I    =           51
56301
 XDOT =       5247
154817                 Wp   =          113
34836
 YDOT =       4240
229936  meter/sec      RA   =          192
28194  deg
 ZDOT =      -3814
056922                 TA   =           15
63998
                                          MA   =           15
51418
                                          Ha   =            182
558  n
mi
                                          Hp   =            153
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15685558
21                 X    =         4786102
09
 Y    =       -7395195
99  feet           Y    =        -2200564
22  meter
 Z    =       13309037
25                 Z    =         4079832
26
 XDOT =      17215
074860                 XDOT =        5217
877674
 YDOT =      13911
515538  feet/sec       YDOT =        4298
743495  meter/sec
 ZDOT =     -12513
310113                 ZDOT =       -3788
637056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12352942
43                 X    =        -3765176
85
 Y    =       12073476
21  feet           Y    =         3679995
55  meter
 Z    =       13397466
85                 Z    =         4083547
89
 XDOT =     -19991
916979                 XDOT =       -6093
536295
 YDOT =      -6626
804906  feet/sec       YDOT =       -2019
850135  meter/sec
 ZDOT =     -12415
844390                 ZDOT =       -3784
349370


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

ISS
1 25544U 98067A   07360
33317854  
00020000  00000-0  20000-3 0  9076
2 25544  51
6372 193
0883 0033116 124
2210 236
2105 15
86570115   507


Satellite: ISS
Catalog Number: 25544
Epoch time:      07360
33317854   =   yrday
fracday
Element set:     907
Inclination:       51
6372  deg
RA of node:       193
0883  deg
Eccentricity:     
0033116     
Arg of perigee:   124
2210  deg
Mean anomaly:     236
2105  deg
Mean motion:   15
86570115  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              50
Checksum:              255


Coasting Arc #9 (Orbit 49)
---------------------------------------

Vector Time (GMT): 2007/360/07:46:47
354
Vector Time (MET): N/A
Weight (LBS)     : 15034
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4829947
03                 A    =         6712535
82  meter
 Y    =        2271792
63  meter          E    =           
0006148
 Z    =       -4076465
71                 I    =           51
56517
 XDOT =      -5198
008964                 Wp   =          101
07638
 YDOT =      -4212
380272  meter/sec      RA   =          192
11668  deg
 ZDOT =       3814
936055                 TA   =          208
13100
                                          MA   =          208
16423
                                          Ha   =            183
076  n
mi
                                          Hp   =            177
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15846282
91                 X    =        -4835189
15
 Y    =        7453387
91  feet           Y    =         2217752
75  meter
 Z    =      -13374231
33                 Z    =        -4099941
64
 XDOT =     -17053
835184                 XDOT =       -5169
051161
 YDOT =     -13820
145249  feet/sec       YDOT =       -4270
346036  meter/sec
 ZDOT =      12516
194405                 ZDOT =        3789
754170

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9833252
39                 X    =         2997175
33
 Y    =      -14407193
07  feet           Y    =        -4391312
45  meter
 Z    =      -13463568
34                 Z    =        -4103695
63
 XDOT =      20712
193370                 XDOT =        6313
076539
 YDOT =       2541
580981  feet/sec       YDOT =         774
673883  meter/sec
 ZDOT =      12419
639323                 ZDOT =        3785
506066


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

ISS
1 25544U 98067A   07360
33317170  
00020000  00000-0  20000-3 0  9088
2 25544  51
6383 193
0888 0001888 319
7968  40
3058 15
78325878   502


Satellite: ISS
Catalog Number: 25544
Epoch time:      07360
33317170   =   yrday
fracday
Element set:     908
Inclination:       51
6383  deg
RA of node:       193
0888  deg
Eccentricity:     
0001888     
Arg of perigee:   319
7968  deg
Mean anomaly:      40
3058  deg
Mean motion:   15
78325878  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              50
Checksum:              312

INTERNATIONAL SPACE STATION 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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