Date: November 8th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4843 76 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


There are no maneuvers



Coasting Arc #1 (Orbit 3339)
---------------------------------------

Vector Time (GMT): 2007/311/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4126208
86                 A    =         6715934
35  meter
 Y    =        1831153
64  meter          E    =           
0014289
 Z    =       -4985354
73                 I    =           51
94485
 XDOT =       -802
617878                 Wp   =          113
45918
 YDOT =       7373
232673  meter/sec      RA   =           83
75979  deg
 ZDOT =       2042
967649                 TA   =          176
25596
                                          MA   =          176
24526
                                          Ha   =            187
513  n
mi
                                          Hp   =            180
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13537430
63                 X    =         4129644
62
 Y    =        6007721
91  feet           Y    =         1877314
46  meter
 Z    =      -16356150
69                 Z    =        -4965300
66
 XDOT =      -2633
260755                 XDOT =        -894
931490
 YDOT =      24190
395909  feet/sec       YDOT =        7363
741190  meter/sec
 ZDOT =       6702
649767                 ZDOT =        2038
844192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8765657
32                 X    =        -2671772
35
 Y    =       12042248
11  feet           Y    =         3670477
22  meter
 Z    =      -16279616
95                 Z    =        -4962027
25
 XDOT =     -22192
911402                 XDOT =       -6764
399395
 YDOT =      -7109
027982  feet/sec       YDOT =       -2166
831729  meter/sec
 ZDOT =       6687
794975                 ZDOT =        2038
439908


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   07311
60150001  
00020000  00000-0  20000-3 0  9004
2 25544  51
6396  84
4258 0002429 164
2874 195
8366 15
75947747 33406


Satellite: ISS
Catalog Number: 25544
Epoch time:      07311
60150001   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:        84
4258  deg
Eccentricity:     
0002429     
Arg of perigee:   164
2874  deg
Mean anomaly:     195
8366  deg
Mean motion:   15
75947747  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3340
Checksum:              292


Coasting Arc #2 (Orbit 3355)
---------------------------------------

Vector Time (GMT): 2007/312/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         665334
13                 A    =         6724126
59  meter
 Y    =       -6242599
82  meter          E    =           
0007619
 Z    =       -2402086
47                 I    =           51
96824
 XDOT =       4833
320145                 Wp   =          143
81508
 YDOT =       2590
504622  meter/sec      RA   =           78
66929  deg
 ZDOT =      -5408
171224                 TA   =           63
16554
                                          MA   =           63
08766
                                          Ha   =            187
457  n
mi
                                          Hp   =            180
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2182854
75                 X    =          746759
65
 Y    =      -20480970
53  feet           Y    =        -6234704
35  meter
 Z    =       -7880861
14                 Z    =        -2398656
51
 XDOT =      15857
349557                 XDOT =        4830
266277
 YDOT =       8499
030912  feet/sec       YDOT =        2644
536577  meter/sec
 ZDOT =     -17743
343910                 ZDOT =       -5384
697558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19649897
57                 X    =         5989288
78
 Y    =        6189597
88  feet           Y    =         1886589
43  meter
 Z    =       -7868505
86                 Z    =        -2398320
59
 XDOT =     -11004
288338                 XDOT =       -3354
107086
 YDOT =      12553
888696  feet/sec       YDOT =        3826
425275  meter/sec
 ZDOT =     -17653
711749                 ZDOT =       -5380
851341


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   07312
61608378  
00020000  00000-0  20000-3 0  9012
2 25544  51
6398  79
2003 0002379 169
2901 190
8314 15
75949229 33560


Satellite: ISS
Catalog Number: 25544
Epoch time:      07312
61608378   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:        79
2003  deg
Eccentricity:     
0002379     
Arg of perigee:   169
2901  deg
Mean anomaly:     190
8314  deg
Mean motion:   15
75949229  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3356
Checksum:              304


Coasting Arc #3 (Orbit 3371)
---------------------------------------

Vector Time (GMT): 2007/313/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4353744
96                 A    =         6718263
41  meter
 Y    =       -2646857
44  meter          E    =           
0009413
 Z    =        4371465
60                 I    =           51
94239
 XDOT =        747
646383                 Wp   =           83
47855
 YDOT =      -6872
611601  meter/sec      RA   =           73
49604  deg
 ZDOT =      -3409
382235                 TA   =           40
73278
                                          MA   =           40
66243
                                          Ha   =            187
444  n
mi
                                          Hp   =            180
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14283940
15                 X    =        -4345060
32
 Y    =       -8683915
49  feet           Y    =        -2695495
10  meter
 Z    =       14342078
72                 Z    =         4350335
38
 XDOT =       2452
908081                 XDOT =         841
004117
 YDOT =     -22547
938323  feet/sec       YDOT =       -6863
728871  meter/sec
 ZDOT =     -11185
637254                 ZDOT =       -3405
523545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11110712
42                 X    =         3386545
15
 Y    =      -12581819
08  feet           Y    =        -3834938
46  meter
 Z    =       14261362
30                 Z    =         4346863
23
 XDOT =      20818
104902                 XDOT =        6345
358374
 YDOT =       5693
795076  feet/sec       YDOT =        1735
468739  meter/sec
 ZDOT =     -11171
707533                 ZDOT =       -3405
136456


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   07313
63064702  
00020000  00000-0  20000-3 0  9023
2 25544  51
6403  73
9749 0002180 170
3008 189
8199 15
75992923 33722


Satellite: ISS
Catalog Number: 25544
Epoch time:      07313
63064702   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:        73
9749  deg
Eccentricity:     
0002180     
Arg of perigee:   170
3008  deg
Mean anomaly:     189
8199  deg
Mean motion:   15
75992923  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3372
Checksum:              297


Coasting Arc #4 (Orbit 3387)
---------------------------------------

Vector Time (GMT): 2007/314/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -696903
13                 A    =         6721070
48  meter
 Y    =        5689657
33  meter          E    =           
0012728
 Z    =        3501130
78                 I    =           51
94303
 XDOT =      -5186
363744                 Wp   =          101
79105
 YDOT =      -3441
049370  meter/sec      RA   =           68
41676  deg
 ZDOT =       4543
328660                 TA   =          299
66056
                                          MA   =          299
78724
                                          Ha   =            187
210  n
mi
                                          Hp   =            180
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2286427
60                 X    =         -777482
37
 Y    =       18666854
77  feet           Y    =         5681413
42  meter
 Z    =       11486649
53                 Z    =         3497549
72
 XDOT =     -17015
629083                 XDOT =       -5169
571346
 YDOT =     -11289
532053  feet/sec       YDOT =       -3498
952607  meter/sec
 ZDOT =      14905
933924                 ZDOT =        4518
173051

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18040900
37                 X    =        -5498866
43
 Y    =       -5338908
61  feet           Y    =        -1627299
35  meter
 Z    =       11473635
17                 Z    =         3497164
00
 XDOT =      13516
910944                 XDOT =        4119
954456
 YDOT =     -13732
967599  feet/sec       YDOT =       -4185
808524  meter/sec
 ZDOT =      14809
811336                 ZDOT =        4514
030495


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   07314
64518904  
00020000  00000-0  20000-3 0  9034
2 25544  51
6405  68
7493 0002175 176
1131 184
0050 15
76033305 33888


Satellite: ISS
Catalog Number: 25544
Epoch time:      07314
64518904   =   yrday
fracday
Element set:     903
Inclination:       51
6405  deg
RA of node:        68
7493  deg
Eccentricity:     
0002175     
Arg of perigee:   176
1131  deg
Mean anomaly:     184
0050  deg
Mean motion:   15
76033305  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3388
Checksum:              274


Coasting Arc #5 (Orbit 3402)
---------------------------------------

Vector Time (GMT): 2007/315/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4714073
42                 A    =         6721163
60  meter
 Y    =        3307457
97  meter          E    =           
0005548
 Z    =       -3472433
91                 I    =           51
93134
 XDOT =       -926
519114                 Wp   =          114
25494
 YDOT =       6120
150324  meter/sec      RA   =           63
23626  deg
 ZDOT =       4575
030680                 TA   =          204
75620
                                          MA   =          204
78284
                                          Ha   =            187
104  n
mi
                                          Hp   =            180
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15466120
16                 X    =         4693607
55
 Y    =       10851240
06  feet           Y    =         3360059
25  meter
 Z    =      -11392499
69                 Z    =        -3449581
67
 XDOT =      -3039
760874                 XDOT =       -1017
112062
 YDOT =      20079
233348  feet/sec       YDOT =        6109
282571  meter/sec
 ZDOT =      15009
943176                 ZDOT =        4570
309936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12984524
67                 X    =        -3957683
12
 Y    =       13796187
95  feet           Y    =         4205078
09  meter
 Z    =      -11305160
34                 Z    =        -3445812
87
 XDOT =     -18409
645846                 XDOT =       -5611
260054
 YDOT =      -5050
377552  feet/sec       YDOT =       -1539
355078  meter/sec
 ZDOT =      14992
626038                 ZDOT =        4569
752416


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   07315
59630525  
00020000  00000-0  20000-3 0  9044
2 25544  51
6403  63
8513 0002047 179
2077 180
9091 15
76053996 34032


Satellite: ISS
Catalog Number: 25544
Epoch time:      07315
59630525   =   yrday
fracday
Element set:     904
Inclination:       51
6403  deg
RA of node:        63
8513  deg
Eccentricity:     
0002047     
Arg of perigee:   179
2077  deg
Mean anomaly:     180
9091  deg
Mean motion:   15
76053996  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3403
Checksum:              288


Coasting Arc #6 (Orbit 3418)
---------------------------------------

Vector Time (GMT): 2007/316/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1000913
45                 A    =         6717822
56  meter
 Y    =       -4962306
10  meter          E    =           
0008839
 Z    =       -4424442
51                 I    =           51
90552
 XDOT =       5608
462966                 Wp   =           80
81418
 YDOT =       4091
029006  meter/sec      RA   =           58
15445  deg
 ZDOT =      -3323
814337                 TA   =          155
92639
                                          MA   =          155
88505
                                          Ha   =            187
048  n
mi
                                          Hp   =            180
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3283836
77                 X    =         1077822
05
 Y    =      -16280531
82  feet           Y    =        -4950682
88  meter
 Z    =      -14515887
51                 Z    =        -4419393
59
 XDOT =      18400
469050                 XDOT =        5578
446565
 YDOT =      13422
011173  feet/sec       YDOT =        4153
578496  meter/sec
 ZDOT =     -10904
902680                 ZDOT =       -3296
640185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15717551
65                 X    =         4790709
74
 Y    =        5416674
29  feet           Y    =         1651002
33  meter
 Z    =      -14497189
39                 Z    =        -4418743
33
 XDOT =     -15274
321745                 XDOT =       -4655
613268
 YDOT =      15450
694954  feet/sec       YDOT =        4709
371822  meter/sec
 ZDOT =     -10801
028535                 ZDOT =       -3292
153497


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   07316
61080917  
00020000  00000-0  20000-3 0  9053
2 25544  51
6398  58
6254 0001960 182
6697 177
4457 15
76059073 34194


Satellite: ISS
Catalog Number: 25544
Epoch time:      07316
61080917   =   yrday
fracday
Element set:     905
Inclination:       51
6398  deg
RA of node:        58
6254  deg
Eccentricity:     
0001960     
Arg of perigee:   182
6697  deg
Mean anomaly:     177
4457  deg
Mean motion:   15
76059073  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3419
Checksum:              319


Coasting Arc #7 (Orbit 3434)
---------------------------------------

Vector Time (GMT): 2007/317/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5074278
65                 A    =         6723926
93  meter
 Y    =       -3766121
03  meter          E    =           
0014520
 Z    =        2275707
57                 I    =           51
91073
 XDOT =       1423
145053                 Wp   =          114
35027
 YDOT =      -5237
535986  meter/sec      RA   =           52
97829  deg
 ZDOT =      -5473
174453                 TA   =           40
15041
                                          MA   =           40
04322
                                          Ha   =            186
937  n
mi
                                          Hp   =            180
557

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16647895
83                 X    =        -5042843
42
 Y    =      -12356040
12  feet           Y    =        -3822688
96  meter
 Z    =        7466232
18                 Z    =         2251132
10
 XDOT =       4669
111067                 XDOT =        1508
194529
 YDOT =     -17183
517015  feet/sec       YDOT =       -5221
145476  meter/sec
 ZDOT =     -17956
609097                 ZDOT =       -5466
054593

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14126096
20                 X    =         4305634
12
 Y    =      -15220763
16  feet           Y    =        -4639288
61  meter
 Z    =        7372283
30                 Z    =         2247071
95
 XDOT =      15440
574806                 XDOT =        4706
287201
 YDOT =       5611
315729  feet/sec       YDOT =        1710
329034  meter/sec
 ZDOT =     -17930
048732                 ZDOT =       -5465
078854


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   07317
62529185  
00020000  00000-0  20000-3 0  9061
2 25544  51
6403  53
3996 0001692 184
7176 175
3973 15
76129786 34350


Satellite: ISS
Catalog Number: 25544
Epoch time:      07317
62529185   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:        53
3996  deg
Eccentricity:     
0001692     
Arg of perigee:   184
7176  deg
Mean anomaly:     175
3973  deg
Mean motion:   15
76129786  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3435
Checksum:              323


Coasting Arc #8 (Orbit 3450)
---------------------------------------

Vector Time (GMT): 2007/318/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1551941
36                 A    =         6715062
86  meter
 Y    =        4169351
83  meter          E    =           
0006406
 Z    =        5027632
74                 I    =           51
86248
 XDOT =      -5999
144255                 Wp   =          138
81761
 YDOT =      -4469
988136  meter/sec      RA   =           47
87936  deg
 ZDOT =       1849
025339                 TA   =          293
38747
                                          MA   =          293
45484
                                          Ha   =            186
844  n
mi
                                          Hp   =            180
549

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5091671
14                 X    =        -1622872
16
 Y    =       13678975
82  feet           Y    =         4151600
04  meter
 Z    =       16494858
06                 Z    =         5019921
39
 XDOT =     -19682
231807                 XDOT =       -5957
696709
 YDOT =     -14665
315406  feet/sec       YDOT =       -4536
842407  meter/sec
 ZDOT =       6066
356100                 ZDOT =        1819
981134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13134359
52                 X    =        -4003352
78
 Y    =       -6440620
26  feet           Y    =        -1963101
05  meter
 Z    =       16465929
90                 Z    =         5018815
43
 XDOT =      15974
615308                 XDOT =        4869
062746
 YDOT =     -17300
991631  feet/sec       YDOT =       -5273
342249  meter/sec
 ZDOT =       5955
318871                 ZDOT =        1815
181192


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   07318
63975445  
00020000  00000-0  20000-3 0  9078
2 25544  51
6401  48
1734 0001719 189
5790 170
5341 15
76152642 34516


Satellite: ISS
Catalog Number: 25544
Epoch time:      07318
63975445   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:        48
1734  deg
Eccentricity:     
0001719     
Arg of perigee:   189
5790  deg
Mean anomaly:     170
5341  deg
Mean motion:   15
76152642  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3451
Checksum:              296


Coasting Arc #9 (Orbit 3465)
---------------------------------------

Vector Time (GMT): 2007/319/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5348078
61                 A    =         6725787
55  meter
 Y    =        3970283
61  meter          E    =           
0008971
 Z    =        -906470
84                 I    =           51
87742
 XDOT =      -2212
567875                 Wp   =           42
64046
 YDOT =       4334
278021  meter/sec      RA   =           42
71998  deg
 ZDOT =       5970
588110                 TA   =          307
48956
                                          MA   =          307
57110
                                          Ha   =            186
817  n
mi
                                          Hp   =            180
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17546189
65                 X    =         5307688
36
 Y    =       13025864
88  feet           Y    =         4029863
11  meter
 Z    =       -2973985
69                 Z    =         -880587
19
 XDOT =      -7259
080956                 XDOT =       -2289
874496
 YDOT =      14220
072246  feet/sec       YDOT =        4309
103038  meter/sec
 ZDOT =      19588
543669                 ZDOT =        5959
651898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14328687
89                 X    =        -4367384
07
 Y    =       16516943
62  feet           Y    =         5034364
41  meter
 Z    =       -2875029
54                 Z    =         -876309
00
 XDOT =     -12411
478212                 XDOT =       -3783
018559
 YDOT =      -7388
625247  feet/sec       YDOT =       -2252
052975  meter/sec
 ZDOT =      19547
350865                 ZDOT =        5958
032544


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   07319
59079593  
00020000  00000-0  20000-3 0  9084
2 25544  51
6396  43
2737 0001407 191
5247 168
5885 15
76128040 34663


Satellite: ISS
Catalog Number: 25544
Epoch time:      07319
59079593   =   yrday
fracday
Element set:     908
Inclination:       51
6396  deg
RA of node:        43
2737  deg
Eccentricity:     
0001407     
Arg of perigee:   191
5247  deg
Mean anomaly:     168
5885  deg
Mean motion:   15
76128040  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3466
Checksum:              319


Coasting Arc #10 (Orbit 3481)
---------------------------------------

Vector Time (GMT): 2007/320/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2377373
92                 A    =         6713909
30  meter
 Y    =       -3413124
77  meter          E    =           
0014766
 Z    =       -5282782
25                 I    =           51
81598
 XDOT =       6179
747348                 Wp   =           94
10879
 YDOT =       4579
712955  meter/sec      RA   =           37
59213  deg
 ZDOT =       -179
316804                 TA   =          174
20065
                                          MA   =          174
18353
                                          Ha   =            186
710  n
mi
                                          Hp   =            180
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7799783
22                 X    =         2441026
47
 Y    =      -11197915
92  feet           Y    =        -3386183
33  meter
 Z    =      -17331962
77                 Z    =        -5271078
45
 XDOT =      20274
761642                 XDOT =        6128
948112
 YDOT =      15025
304971  feet/sec       YDOT =        4648
534371  meter/sec
 ZDOT =       -588
309723                 ZDOT =        -149
418202

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10710861
64                 X    =         3264670
63
 Y    =        8546226
78  feet           Y    =         2604889
92  meter
 Z    =      -17287750
68                 Z    =        -5269306
41
 XDOT =     -15575
872124                 XDOT =       -4747
525823
 YDOT =      18571
915752  feet/sec       YDOT =        5660
719921  meter/sec
 ZDOT =       -474
001145                 ZDOT =        -144
475549


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   07320
60522033  
00020000  00000-0  20000-3 0  9091
2 25544  51
6399  38
0467 0001478 193
2867 166
8259 15
76177886 34829


Satellite: ISS
Catalog Number: 25544
Epoch time:      07320
60522033   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:        38
0467  deg
Eccentricity:     
0001478     
Arg of perigee:   193
2867  deg
Mean anomaly:     166
8259  deg
Mean motion:   15
76177886  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3482
Checksum:              322


Coasting Arc #11 (Orbit 3497)
---------------------------------------

Vector Time (GMT): 2007/321/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5377730
57                 A    =         6725633
10  meter
 Y    =       -3983706
64  meter          E    =           
0011688
 Z    =        -604762
14                 I    =           51
83288
 XDOT =       3277
927533                 Wp   =          144
48792
 YDOT =      -3521
476748  meter/sec      RA   =           32
45737  deg
 ZDOT =      -6018
576827                 TA   =           42
08510
                                          MA   =           41
99539
                                          Ha   =            186
603  n
mi
                                          Hp   =            180
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17643473
01                 X    =        -5329846
61
 Y    =      -13069903
69  feet           Y    =        -4043575
71  meter
 Z    =       -1984127
77                 Z    =         -630771
44
 XDOT =      10754
355423                 XDOT =        3346
299159
 YDOT =     -11553
401404  feet/sec       YDOT =       -3484
438472  meter/sec
 ZDOT =     -19745
986965                 ZDOT =       -6002
486559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13798968
14                 X    =         4205925
49
 Y    =      -17067469
21  feet           Y    =        -5202164
61  meter
 Z    =       -2083568
65                 Z    =         -635071
72
 XDOT =       9842
196762                 XDOT =        2999
901573
 YDOT =      10334
933348  feet/sec       YDOT =        3150
087684  meter/sec
 ZDOT =     -19685
083208                 ZDOT =       -6000
013362


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   07321
61962421  
00020000  00000-0  20000-3 0  9104
2 25544  51
6404  32
8199 0001309 191
8670 168
2464 15
76241138 34982


Satellite: ISS
Catalog Number: 25544
Epoch time:      07321
61962421   =   yrday
fracday
Element set:     910
Inclination:       51
6404  deg
RA of node:        32
8199  deg
Eccentricity:     
0001309     
Arg of perigee:   191
8670  deg
Mean anomaly:     168
2464  deg
Mean motion:   15
76241138  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3498
Checksum:              288


Coasting Arc #12 (Orbit 3513)
---------------------------------------

Vector Time (GMT): 2007/322/14:08:18
812
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3364909
14                 A    =         6714431
28  meter
 Y    =        2782819
89  meter          E    =           
0003987
 Z    =        5097953
11                 I    =           51
76944
 XDOT =      -6064
357637                 Wp   =           65
34826
 YDOT =      -4498
849235  meter/sec      RA   =           27
29739  deg
 ZDOT =      -1544
428716                 TA   =           39
44570
                                          MA   =           39
41668
                                          Ha   =            186
628  n
mi
                                          Hp   =            180
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11039728
14                 X    =        -3420542
29
 Y    =        9129986
53  feet           Y    =         2744880
31  meter
 Z    =       16725567
95                 Z    =         5081471
10
 XDOT =     -19896
186473                 XDOT =       -6006
097432
 YDOT =     -14760
004052  feet/sec       YDOT =       -4566
338508  meter/sec
 ZDOT =      -5067
023347                 ZDOT =       -1573
748491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8850897
18                 X    =        -2697753
46
 Y    =      -11356922
94  feet           Y    =        -3461590
11  meter
 Z    =       16663096
80                 Z    =         5078911
91
 XDOT =      14420
216356                 XDOT =        4395
281945
 YDOT =     -18849
566310  feet/sec       YDOT =       -5745
347811  meter/sec
 ZDOT =      -5179
122013                 ZDOT =       -1578
596390


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   07322
63400809  
00020000  00000-0  20000-3 0  9115
2 25544  51
6396  27
5933 0001257 195
7796 164
3329 15
76279581 35142


Satellite: ISS
Catalog Number: 25544
Epoch time:      07322
63400809   =   yrday
fracday
Element set:     911
Inclination:       51
6396  deg
RA of node:        27
5933  deg
Eccentricity:     
0001257     
Arg of perigee:   195
7796  deg
Mean anomaly:     164
3329  deg
Mean motion:   15
76279581  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3514
Checksum:              309

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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