Date: October 12th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 2690 98 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2897)
---------------------------------------

Vector Time (GMT): 2007/283/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3743116
13                 A    =         6727356
84  meter
 Y    =        5475413
47  meter          E    =           
0011106
 Z    =       -1104696
14                 I    =           51
41370
 XDOT =      -4568
863741                 Wp   =          129
25573
 YDOT =       1945
048215  meter/sec      RA   =          228
00570  deg
 ZDOT =      -5886
690251                 TA   =           62
87728
                                          MA   =           62
76406
                                          Ha   =            188
784  n
mi
                                          Hp   =            180
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12280564
74                 X    =         3686977
56
 Y    =       17963954
97  feet           Y    =         5516957
14  meter
 Z    =       -3624331
17                 Z    =        -1086648
51
 XDOT =     -14989
710437                 XDOT =       -4561
676941
 YDOT =       6381
391781  feet/sec       YDOT =        1893
996318  meter/sec
 ZDOT =     -19313
288226                 ZDOT =       -5908
868927

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20102251
76                 X    =        -6127166
33
 Y    =       -8361379
02  feet           Y    =        -2548548
33  meter
 Z    =       -3555072
44                 Z    =        -1083586
08
 XDOT =       8391
411841                 XDOT =        2557
702329
 YDOT =     -11993
027497  feet/sec       YDOT =       -3655
474781  meter/sec
 ZDOT =     -19397
270669                 ZDOT =       -5912
288100


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   07283
57133927  
00020000  00000-0  20000-3 0  9006
2 25544  51
6348 228
7539 0002799  77
8215 282
3262 15
75514814 28985


Satellite: ISS
Catalog Number: 25544
Epoch time:      07283
57133927   =   yrday
fracday
Element set:     900
Inclination:       51
6348  deg
RA of node:       228
7539  deg
Eccentricity:     
0002799     
Arg of perigee:    77
8215  deg
Mean anomaly:     282
3262  deg
Mean motion:   15
75514814  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2898
Checksum:              323


Coasting Arc #2 (Orbit 2913)
---------------------------------------

Vector Time (GMT): 2007/284/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4216883
94                 A    =         6716788
61  meter
 Y    =       -1528465
86  meter          E    =           
0008066
 Z    =        4994463
82                 I    =           51
39880
 XDOT =       4385
219957                 Wp   =           63
70516
 YDOT =       6065
960326  meter/sec      RA   =          222
81655  deg
 ZDOT =      -1840
300850                 TA   =           44
11544
                                          MA   =           44
05113
                                          Ha   =            188
608  n
mi
                                          Hp   =            180
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13834921
06                 X    =         4209399
27
 Y    =       -5014651
78  feet           Y    =        -1481351
79  meter
 Z    =       16386036
14                 Z    =         5014931
85
 XDOT =      14387
204582                 XDOT =        4326
003621
 YDOT =      19901
444640  feet/sec       YDOT =        6114
667120  meter/sec
 ZDOT =      -6037
732447                 ZDOT =       -1819
141183

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8588873
48                 X    =        -2617888
64
 Y    =       11842119
24  feet           Y    =         3609477
95  meter
 Z    =       16463578
52                 Z    =         5018098
73
 XDOT =     -22220
713117                 XDOT =       -6772
873358
 YDOT =      -7808
723374  feet/sec       YDOT =       -2380
098884  meter/sec
 ZDOT =      -5956
574819                 ZDOT =       -1815
564005


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   07284
58618565  
00020000  00000-0  20000-3 0  9015
2 25544  51
6348 223
5303 0002779  80
3590 279
7887 15
75545380 29144


Satellite: ISS
Catalog Number: 25544
Epoch time:      07284
58618565   =   yrday
fracday
Element set:     901
Inclination:       51
6348  deg
RA of node:       223
5303  deg
Eccentricity:     
0002779     
Arg of perigee:    80
3590  deg
Mean anomaly:     279
7887  deg
Mean motion:   15
75545380  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2914
Checksum:              321


Coasting Arc #3 (Orbit 2929)
---------------------------------------

Vector Time (GMT): 2007/285/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3858413
88                 A    =         6725925
91  meter
 Y    =       -5086773
80  meter          E    =           
0016830
 Z    =        2091569
93                 I    =           51
45177
 XDOT =       5126
816936                 Wp   =           72
05471
 YDOT =      -1603
675379  meter/sec      RA   =          217
68758  deg
 ZDOT =       5526
259374                 TA   =          311
40240
                                          MA   =          311
54694
                                          Ha   =            188
754  n
mi
                                          Hp   =            180
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12658838
18                 X    =        -3811406
78
 Y    =      -16688890
42  feet           Y    =        -5129657
83  meter
 Z    =        6862106
06                 Z    =         2072939
69
 XDOT =      16820
265539                 XDOT =        5117
522139
 YDOT =      -5261
402163  feet/sec       YDOT =       -1546
396100  meter/sec
 ZDOT =      18130
772223                 ZDOT =        5551
143624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19971732
25                 X    =         6087383
99
 Y    =        6392988
64  feet           Y    =         1948582
94  meter
 Z    =        6790681
42                 Z    =         2069799
70
 XDOT =     -10214
038172                 XDOT =       -3113
238835
 YDOT =      12439
960700  feet/sec       YDOT =        3791
700021  meter/sec
 ZDOT =      18225
083339                 ZDOT =        5555
005402


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   07285
60102197  
00020000  00000-0  20000-3 0  9029
2 25544  51
6350 218
3057 0002797  83
7584 276
3899 15
75545880 29304


Satellite: ISS
Catalog Number: 25544
Epoch time:      07285
60102197   =   yrday
fracday
Element set:     902
Inclination:       51
6350  deg
RA of node:       218
3057  deg
Eccentricity:     
0002797     
Arg of perigee:    83
7584  deg
Mean anomaly:     276
3899  deg
Mean motion:   15
75545880  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2930
Checksum:              315


Coasting Arc #4 (Orbit 2944)
---------------------------------------

Vector Time (GMT): 2007/286/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4747485
00                 A    =         6718473
58  meter
 Y    =        1306802
21  meter          E    =           
0013180
 Z    =       -4583349
82                 I    =           51
45136
 XDOT =      -4387
238324                 Wp   =          105
48088
 YDOT =      -5585
224657  meter/sec      RA   =          212
48525  deg
 ZDOT =       2955
479720                 TA   =          193
92343
                                          MA   =          193
95981
                                          Ha   =            188
683  n
mi
                                          Hp   =            180
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15575738
18                 X    =        -4739479
29
 Y    =        4287408
81  feet           Y    =         1253757
76  meter
 Z    =      -15037236
94                 Z    =        -4606394
35
 XDOT =     -14393
826523                 XDOT =       -4338
815026
 YDOT =     -18324
227878  feet/sec       YDOT =       -5634
014395  meter/sec
 ZDOT =       9696
455773                 ZDOT =        2934
283716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10018608
09                 X    =         3053671
74
 Y    =      -12568922
27  feet           Y    =        -3831007
51  meter
 Z    =      -15124604
92                 Z    =        -4609979
58
 XDOT =      21539
806547                 XDOT =        6565
333035
 YDOT =       5613
002140  feet/sec       YDOT =        1710
843052  meter/sec
 ZDOT =       9615
218311                 ZDOT =        2930
718541


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   07286
55242014  
00020000  00000-0  20000-3 0  9038
2 25544  51
6356 213
4080 0002780  86
9533 273
1949 15
75570037 29452


Satellite: ISS
Catalog Number: 25544
Epoch time:      07286
55242014   =   yrday
fracday
Element set:     903
Inclination:       51
6356  deg
RA of node:       213
4080  deg
Eccentricity:     
0002780     
Arg of perigee:    86
9533  deg
Mean anomaly:     273
1949  deg
Mean motion:   15
75570037  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2945
Checksum:              292


Coasting Arc #5 (Orbit 2960)
---------------------------------------

Vector Time (GMT): 2007/287/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3745416
03                 A    =         6723652
87  meter
 Y    =        4676534
21  meter          E    =           
0007165
 Z    =       -3055396
47                 I    =           51
49428
 XDOT =      -5759
514593                 Wp   =          101
74159
 YDOT =       1414
147193  meter/sec      RA   =          207
37268  deg
 ZDOT =      -4906
870204                 TA   =          113
74648
                                          MA   =          113
67131
                                          Ha   =            188
666  n
mi
                                          Hp   =            180
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12288110
35                 X    =         3707686
94
 Y    =       15342960
01  feet           Y    =         4718206
58  meter
 Z    =      -10024266
62                 Z    =        -3037292
43
 XDOT =     -18896
045252                 XDOT =       -5751
062374
 YDOT =       4639
590529  feet/sec       YDOT =        1349
788238  meter/sec
 ZDOT =     -16098
655524                 ZDOT =       -4934
830201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19088614
80                 X    =        -5818209
79
 Y    =       -4838901
95  feet           Y    =        -1474897
31  meter
 Z    =       -9954888
85                 Z    =        -3034250
12
 XDOT =      11884
735416                 XDOT =        3622
467355
 YDOT =     -13621
441377  feet/sec       YDOT =       -4151
815332  meter/sec
 ZDOT =     -16204
690740                 ZDOT =       -4939
189738


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   07287
56723442  
00020000  00000-0  20000-3 0  9040
2 25544  51
6360 208
1838 0002724  90
8594 269
2882 15
75587302 29611


Satellite: ISS
Catalog Number: 25544
Epoch time:      07287
56723442   =   yrday
fracday
Element set:     904
Inclination:       51
6360  deg
RA of node:       208
1838  deg
Eccentricity:     
0002724     
Arg of perigee:    90
8594  deg
Mean anomaly:     269
2882  deg
Mean motion:   15
75587302  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2961
Checksum:              313


Coasting Arc #6 (Orbit 2976)
---------------------------------------

Vector Time (GMT): 2007/288/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5299967
71                 A    =         6720751
64  meter
 Y    =       -1221794
96  meter          E    =           
0013676
 Z    =        3937721
40                 I    =           51
51038
 XDOT =       4155
837911                 Wp   =           82
04888
 YDOT =       5119
879116  meter/sec      RA   =          202
16485  deg
 ZDOT =      -3991
304780                 TA   =           49
42860
                                          MA   =           49
30964
                                          Ha   =            188
546  n
mi
                                          Hp   =            180
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17388345
52                 X    =         5294106
85
 Y    =       -4008513
64  feet           Y    =        -1162560
51  meter
 Z    =       12919033
46                 Z    =         3963455
08
 XDOT =      13634
638815                 XDOT =        4117
667333
 YDOT =      16797
503663  feet/sec       YDOT =        5166
138644  meter/sec
 ZDOT =     -13094
831956                 ZDOT =       -3971
207876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11190680
55                 X    =        -3410919
43
 Y    =       13807960
23  feet           Y    =         4208666
28  meter
 Z    =       13016645
88                 Z    =         3967473
66
 XDOT =     -20132
017855                 XDOT =       -6136
239042
 YDOT =      -4002
357433  feet/sec       YDOT =       -1219
918545  meter/sec
 ZDOT =     -13017
821474                 ZDOT =       -3967
831985


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   07288
58203809  
00020000  00000-0  20000-3 0  9054
2 25544  51
6352 202
9596 0002775  93
6990 266
4491 15
75603895 29770


Satellite: ISS
Catalog Number: 25544
Epoch time:      07288
58203809   =   yrday
fracday
Element set:     905
Inclination:       51
6352  deg
RA of node:       202
9596  deg
Eccentricity:     
0002775     
Arg of perigee:    93
6990  deg
Mean anomaly:     266
4491  deg
Mean motion:   15
75603895  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2977
Checksum:              336


Coasting Arc #7 (Orbit 2992)
---------------------------------------

Vector Time (GMT): 2007/289/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3450475
38                 A    =         6721139
60  meter
 Y    =       -4271109
38  meter          E    =           
0014101
 Z    =        3866028
06                 I    =           51
53915
 XDOT =       6375
329584                 Wp   =           98
82201
 YDOT =      -1438
533281  meter/sec      RA   =          197
06037  deg
 ZDOT =       4086
033615                 TA   =          308
50472
                                          MA   =          308
63109
                                          Ha   =            188
669  n
mi
                                          Hp   =            180
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11320457
28                 X    =        -3421239
66
 Y    =      -14012826
05  feet           Y    =        -4309531
15  meter
 Z    =       12683819
11                 Z    =         3849336
19
 XDOT =      20916
435642                 XDOT =        6371
091960
 YDOT =      -4719
597377  feet/sec       YDOT =       -1367
264505  meter/sec
 ZDOT =      13405
622096                 ZDOT =        4116
995386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17666877
42                 X    =         5384864
24
 Y    =        3743283
88  feet           Y    =         1140952
93  meter
 Z    =       12619848
74                 Z    =         3846529
90
 XDOT =     -12974
194663                 XDOT =       -3954
534533
 YDOT =      15478
391872  feet/sec       YDOT =        4717
813843  meter/sec
 ZDOT =      13523
082727                 ZDOT =        4121
835615


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   07289
59683016  
00020000  00000-0  20000-3 0  9069
2 25544  51
6355 197
7348 0002740  96
8266 263
3210 15
75613961 29930


Satellite: ISS
Catalog Number: 25544
Epoch time:      07289
59683016   =   yrday
fracday
Element set:     906
Inclination:       51
6355  deg
RA of node:       197
7348  deg
Eccentricity:     
0002740     
Arg of perigee:    96
8266  deg
Mean anomaly:     263
3210  deg
Mean motion:   15
75613961  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2993
Checksum:              321


Coasting Arc #8 (Orbit 3007)
---------------------------------------

Vector Time (GMT): 2007/290/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5799153
19                 A    =         6723127
42  meter
 Y    =        1326276
57  meter          E    =           
0007060
 Z    =       -3137936
84                 I    =           51
57464
 XDOT =      -3692
640355                 Wp   =           87
15580
 YDOT =      -4703
369643  meter/sec      RA   =          191
85521  deg
 ZDOT =       4846
060728                 TA   =          236
29324
                                          MA   =          236
36056
                                          Ha   =            188
484  n
mi
                                          Hp   =            180
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19026093
15                 X    =        -5798308
97
 Y    =        4351301
08  feet           Y    =         1261431
95  meter
 Z    =      -10295068
37                 Z    =        -3166107
62
 XDOT =     -12114
961793                 XDOT =       -3663
313888
 YDOT =     -15431
002766  feet/sec       YDOT =       -4744
498976  meter/sec
 ZDOT =      15899
149369                 ZDOT =        4828
192642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11756637
86                 X    =         3583423
22
 Y    =      -15507912
68  feet           Y    =        -4726811
78  meter
 Z    =      -10401951
01                 Z    =        -3170514
67
 XDOT =      18131
021706                 XDOT =        5526
335416
 YDOT =       3147
916777  feet/sec       YDOT =         959
485034  meter/sec
 ZDOT =      15830
647042                 ZDOT =        4825
181219


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   07290
54818697  
00020000  00000-0  20000-3 0  9072
2 25544  51
6357 192
8367 0002596  99
7609 260
3849 15
75641760 30082


Satellite: ISS
Catalog Number: 25544
Epoch time:      07290
54818697   =   yrday
fracday
Element set:     907
Inclination:       51
6357  deg
RA of node:       192
8367  deg
Eccentricity:     
0002596     
Arg of perigee:    99
7609  deg
Mean anomaly:     260
3849  deg
Mean motion:   15
75641760  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3008
Checksum:              336


Coasting Arc #9 (Orbit 3023)
---------------------------------------

Vector Time (GMT): 2007/291/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2939323
20                 A    =         6718495
61  meter
 Y    =        3983788
98  meter          E    =           
0012267
 Z    =       -4553473
67                 I    =           51
58742
 XDOT =      -6882
487492                 Wp   =           76
43625
 YDOT =       1610
746107  meter/sec      RA   =          186
75047  deg
 ZDOT =      -3037
508865                 TA   =          163
32713
                                          MA   =          163
28676
                                          Ha   =            188
432  n
mi
                                          Hp   =            180
392

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9643448
81                 X    =         2916677
74
 Y    =       13070173
82  feet           Y    =         4016531
63  meter
 Z    =      -14939218
06                 Z    =        -4539249
12
 XDOT =     -22580
339540                 XDOT =       -6885
231656
 YDOT =       5284
600087  feet/sec       YDOT =        1533
766954  meter/sec
 ZDOT =      -9965
580265                 ZDOT =       -3070
951184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15910039
40                 X    =        -4849380
01
 Y    =       -3510515
65  feet           Y    =        -1070005
17  meter
 Z    =      -14884646
82                 Z    =        -4536840
35
 XDOT =      13308
972389                 XDOT =        4056
574784
 YDOT =     -17581
360279  feet/sec       YDOT =       -5358
798613  meter/sec
 ZDOT =     -10092
473559                 ZDOT =       -3076
185941


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   07291
56295709  
00020000  00000-0  20000-3 0  9089
2 25544  51
6356 187
6118 0002473 103
0706 257
0734 15
75664180 30243


Satellite: ISS
Catalog Number: 25544
Epoch time:      07291
56295709   =   yrday
fracday
Element set:     908
Inclination:       51
6356  deg
RA of node:       187
6118  deg
Eccentricity:     
0002473     
Arg of perigee:   103
0706  deg
Mean anomaly:     257
0734  deg
Mean motion:   15
75664180  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3024
Checksum:              294


Coasting Arc #10 (Orbit 3039)
---------------------------------------

Vector Time (GMT): 2007/292/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6182834
64                 A    =         6725416
28  meter
 Y    =       -1525163
68  meter          E    =           
0016695
 Z    =        2138719
29                 I    =           51
63977
 XDOT =       3017
953289                 Wp   =          109
28431
 YDOT =       4452
563364  meter/sec      RA   =          181
55807  deg
 ZDOT =      -5519
994412                 TA   =           46
76064
                                          MA   =           46
62139
                                          Ha   =            188
443  n
mi
                                          Hp   =            180
280

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20284890
55                 X    =         6189040
07
 Y    =       -5003817
86  feet           Y    =        -1455989
05  meter
 Z    =        7016795
58                 Z    =         2168770
98
 XDOT =       9901
421551                 XDOT =        2994
755263
 YDOT =      14608
147520  feet/sec       YDOT =        4486
182164  meter/sec
 ZDOT =     -18110
217888                 ZDOT =       -5505
389303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11731489
72                 X    =        -3575758
07
 Y    =       17241631
93  feet           Y    =         5255249
41  meter
 Z    =        7130825
72                 Z    =         2173475
68
 XDOT =     -15942
952863                 XDOT =       -4859
412033
 YDOT =      -3341
717861  feet/sec       YDOT =       -1018
555604  meter/sec
 ZDOT =     -18054
132455                 ZDOT =       -5502
899572


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   07292
57771787  
00020000  00000-0  20000-3 0  9097
2 25544  51
6355 182
3871 0002634 107
5371 252
6081 15
75656136 30402


Satellite: ISS
Catalog Number: 25544
Epoch time:      07292
57771787   =   yrday
fracday
Element set:     909
Inclination:       51
6355  deg
RA of node:       182
3871  deg
Eccentricity:     
0002634     
Arg of perigee:   107
5371  deg
Mean anomaly:     252
6081  deg
Mean motion:   15
75656136  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3040
Checksum:              301


Coasting Arc #11 (Orbit 3055)
---------------------------------------

Vector Time (GMT): 2007/293/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2299921
96                 A    =         6716499
11  meter
 Y    =       -3830258
94  meter          E    =           
0008095
 Z    =        5010221
10                 I    =           51
63879
 XDOT =       7233
196821                 Wp   =          120
53486
 YDOT =      -1916
037408  meter/sec      RA   =          176
44408  deg
 ZDOT =       1849
333907                 TA   =          311
61284
                                          MA   =          311
68216
                                          Ha   =            188
460  n
mi
                                          Hp   =            180
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7545675
73                 X    =        -2281259
55
 Y    =      -12566466
35  feet           Y    =        -3855873
58  meter
 Z    =       16437733
26                 Z    =         4999093
31
 XDOT =      23730
960700                 XDOT =        7245
100808
 YDOT =      -6286
211967  feet/sec       YDOT =       -1835
085130  meter/sec
 ZDOT =       6067
368460                 ZDOT =        1884
502150

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14147457
88                 X    =         4312145
16
 Y    =        4013450
82  feet           Y    =         1223299
81  meter
 Z    =       16394938
91                 Z    =         4997177
38
 XDOT =     -12797
526166                 XDOT =       -3900
685975
 YDOT =      19697
190214  feet/sec       YDOT =        6003
703577  meter/sec
 ZDOT =       6200
808674                 ZDOT =        1890
006484


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   07293
59246585  
00020000  00000-0  20000-3 0  9105
2 25544  51
6356 177
1619 0002502 109
8265 250
3169 15
75679841 30563


Satellite: ISS
Catalog Number: 25544
Epoch time:      07293
59246585   =   yrday
fracday
Element set:     910
Inclination:       51
6356  deg
RA of node:       177
1619  deg
Eccentricity:     
0002502     
Arg of perigee:   109
8265  deg
Mean anomaly:     250
3169  deg
Mean motion:   15
75679841  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3056
Checksum:              310


Coasting Arc #12 (Orbit 3070)
---------------------------------------

Vector Time (GMT): 2007/294/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6383609
63                 A    =         6726798
90  meter
 Y    =        1826020
63  meter          E    =           
0010408
 Z    =       -1058811
60                 I    =           51
70234
 XDOT =      -2230
344543                 Wp   =           50
67862
 YDOT =      -4389
154441  meter/sec      RA   =          171
27137  deg
 ZDOT =       5922
335721                 TA   =          297
74582
                                          MA   =          297
85134
                                          Ha   =            188
248  n
mi
                                          Hp   =            180
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20943601
14                 X    =        -6398410
44
 Y    =        5990881
32  feet           Y    =         1754552
70  meter
 Z    =       -3473791
32                 Z    =        -1089859
59
 XDOT =      -7317
403356                 XDOT =       -2209
868608
 YDOT =     -14400
112994  feet/sec       YDOT =       -4413
980742  meter/sec
 ZDOT =      19430
235304                 ZDOT =        5911
550441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10936958
33                 X    =         3333584
90
 Y    =      -18816900
42  feet           Y    =        -5735391
25  meter
 Z    =       -3591589
45                 Z    =        -1094716
46
 XDOT =      13960
250428                 XDOT =        4255
084330
 YDOT =       4440
674227  feet/sec       YDOT =        1353
517504  meter/sec
 ZDOT =      19388
665340                 ZDOT =        5909
665196


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   07294
54378209  
00020000  00000-0  20000-3 0  9111
2 25544  51
6352 172
2631 0002313 113
1814 246
9593 15
75705721 30713


Satellite: ISS
Catalog Number: 25544
Epoch time:      07294
54378209   =   yrday
fracday
Element set:     911
Inclination:       51
6352  deg
RA of node:       172
2631  deg
Eccentricity:     
0002313     
Arg of perigee:   113
1814  deg
Mean anomaly:     246
9593  deg
Mean motion:   15
75705721  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3071
Checksum:              276

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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