Date: October 25th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4305 56 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 3115)
---------------------------------------

Vector Time (GMT): 2007/297/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4362066
31                 A    =         6723233
75  meter
 Y    =        4286708
90  meter          E    =           
0006252
 Z    =       -2796530
29                 I    =           51
77453
 XDOT =      -5341
452488                 Wp   =           81
20324
 YDOT =      -2094
040942  meter/sec      RA   =          156
60908  deg
 ZDOT =       5132
426880                 TA   =          246
83519
                                          MA   =          246
90107
                                          Ha   =            187
913  n
mi
                                          Hp   =            180
019

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14311241
17                 X    =        -4396091
33
 Y    =       14064005
59  feet           Y    =         4237739
39  meter
 Z    =       -9174968
14                 Z    =        -2817804
68
 XDOT =     -17524
450419                 XDOT =       -5342
572679
 YDOT =      -6870
213064  feet/sec       YDOT =       -2153
778033  meter/sec
 ZDOT =      16838
670867                 ZDOT =        5106
474830

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15970712
94                 X    =         4867873
31
 Y    =      -12085675
96  feet           Y    =        -3683714
03  meter
 Z    =       -9255305
61                 Z    =        -2821017
15
 XDOT =      15691
971745                 XDOT =        4782
912988
 YDOT =       7943
374865  feet/sec       YDOT =        2421
140659  meter/sec
 ZDOT =      16739
724814                 ZDOT =        5102
268123


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   07297
39694683  
00020000  00000-0  20000-3 0  9002
2 25544  51
6382 157
5777 0002396 120
7477 239
3923 15
75924388 31168


Satellite: ISS
Catalog Number: 25544
Epoch time:      07297
39694683   =   yrday
fracday
Element set:     900
Inclination:       51
6382  deg
RA of node:       157
5777  deg
Eccentricity:     
0002396     
Arg of perigee:   120
7477  deg
Mean anomaly:     239
3923  deg
Mean motion:   15
75924388  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3116
Checksum:              332


Coasting Arc #2 (Orbit 3131)
---------------------------------------

Vector Time (GMT): 2007/298/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4270686
16                 A    =         6716683
34  meter
 Y    =        1984427
77  meter          E    =           
0013199
 Z    =       -4801296
71                 I    =           51
77849
 XDOT =      -5195
648793                 Wp   =           79
89837
 YDOT =       5081
799179  meter/sec      RA   =          151
51178  deg
 ZDOT =      -2524
676835                 TA   =          165
43185
                                          MA   =          165
39377
                                          Ha   =            187
835  n
mi
                                          Hp   =            180
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14011437
52                 X    =         4271503
17
 Y    =        6510589
80  feet           Y    =         2032189
36  meter
 Z    =      -15752285
78                 Z    =        -4780547
14
 XDOT =     -17046
091841                 XDOT =       -5239
823259
 YDOT =      16672
569485  feet/sec       YDOT =        5023
451390  meter/sec
 ZDOT =      -8283
060481                 ZDOT =       -2550
025636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13271791
98                 X    =        -4045242
20
 Y    =       -8065673
26  feet           Y    =        -2458417
21  meter
 Z    =      -15673133
73                 Z    =        -4777171
16
 XDOT =      18189
935452                 XDOT =        5544
292326
 YDOT =     -13672
282697  feet/sec       YDOT =       -4167
311766  meter/sec
 ZDOT =      -8378
797925                 ZDOT =       -2553
857608


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   07298
41153680  
00020000  00000-0  20000-3 0  9014
2 25544  51
6381 152
3520 0002276 123
1484 236
9899 15
75958745 31325


Satellite: ISS
Catalog Number: 25544
Epoch time:      07298
41153680   =   yrday
fracday
Element set:     901
Inclination:       51
6381  deg
RA of node:       152
3520  deg
Eccentricity:     
0002276     
Arg of perigee:   123
1484  deg
Mean anomaly:     236
9899  deg
Mean motion:   15
75958745  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3132
Checksum:              301


Coasting Arc #3 (Orbit 3147)
---------------------------------------

Vector Time (GMT): 2007/299/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4649560
69                 A    =         6725560
97  meter
 Y    =       -4585020
45  meter          E    =           
0016434
 Z    =        1576324
83                 I    =           51
83252
 XDOT =       4440
559693                 Wp   =          118
93675
 YDOT =       2502
572374  meter/sec      RA   =          146
33801  deg
 ZDOT =      -5781
543721                 TA   =           43
69768
                                          MA   =           43
56769
                                          Ha   =            187
845  n
mi
                                          Hp   =            180
094

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15254464
20                 X    =         4692827
73
 Y    =      -15042718
00  feet           Y    =        -4532784
49  meter
 Z    =        5171669
39                 Z    =         1599018
35
 XDOT =      14568
765398                 XDOT =        4440
332219
 YDOT =       8210
539284  feet/sec       YDOT =        2552
227897  meter/sec
 ZDOT =     -18968
319295                 ZDOT =       -5759
971286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16600910
15                 X    =        -5059957
41
 Y    =       13509177
25  feet           Y    =         4117597
22  meter
 Z    =        5257387
15                 Z    =         1602451
60
 XDOT =     -12832
774607                 XDOT =       -3911
429700
 YDOT =      -8373
039145  feet/sec       YDOT =       -2552
102331  meter/sec
 ZDOT =     -18885
971060                 ZDOT =       -5756
443979


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   07299
42611072  
00020000  00000-0  20000-3 0  9021
2 25544  51
6374 147
1260 0002370 129
0030 231
1345 15
75936108 31486


Satellite: ISS
Catalog Number: 25544
Epoch time:      07299
42611072   =   yrday
fracday
Element set:     902
Inclination:       51
6374  deg
RA of node:       147
1260  deg
Eccentricity:     
0002370     
Arg of perigee:   129
0030  deg
Mean anomaly:     231
1345  deg
Mean motion:   15
75936108  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3148
Checksum:              259


Coasting Arc #4 (Orbit 3163)
---------------------------------------

Vector Time (GMT): 2007/300/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3482572
71                 A    =         6714796
67  meter
 Y    =       -2440392
06  meter          E    =           
0005962
 Z    =        5193074
83                 I    =           51
82022
 XDOT =       5388
564794                 Wp   =          126
86367
 YDOT =      -5406
596170  meter/sec      RA   =          141
22431  deg
 ZDOT =       1068
594134                 TA   =          312
95307
                                          MA   =          313
00305
                                          Ha   =            187
784  n
mi
                                          Hp   =            180
093

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11425763
47                 X    =        -3480252
95
 Y    =       -8006535
63  feet           Y    =        -2479323
33  meter
 Z    =       17037647
09                 Z    =         5176161
46
 XDOT =      17679
018352                 XDOT =        5443
430450
 YDOT =     -17738
176412  feet/sec       YDOT =       -5346
031449  meter/sec
 ZDOT =       3505
886266                 ZDOT =        1094
905833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10852850
67                 X    =         3307948
88
 Y    =        8891919
96  feet           Y    =         2710257
20  meter
 Z    =       16973022
53                 Z    =         5173377
27
 XDOT =     -18356
926056                 XDOT =       -5595
191062
 YDOT =      15496
047895  feet/sec       YDOT =        4723
195399  meter/sec
 ZDOT =       3605
278427                 ZDOT =        1098
888865


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   07300
44066421  
00020000  00000-0  20000-3 0  9039
2 25544  51
6375 141
8996 0002165 131
3794 228
7556 15
76002054 31648


Satellite: ISS
Catalog Number: 25544
Epoch time:      07300
44066421   =   yrday
fracday
Element set:     903
Inclination:       51
6375  deg
RA of node:       141
8996  deg
Eccentricity:     
0002165     
Arg of perigee:   131
3794  deg
Mean anomaly:     228
7556  deg
Mean motion:   15
76002054  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3164
Checksum:              279


Coasting Arc #5 (Orbit 3178)
---------------------------------------

Vector Time (GMT): 2007/301/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4694038
07                 A    =         6726343
39  meter
 Y    =        4804403
04  meter          E    =           
0011749
 Z    =        -260161
88                 I    =           51
88122
 XDOT =      -3562
352865                 Wp   =           53
04160
 YDOT =      -3163
206278  meter/sec      RA   =          136
07583  deg
 ZDOT =       6053
239724                 TA   =          304
13858
                                          MA   =          304
24996
                                          Ha   =            187
533  n
mi
                                          Hp   =            180
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15400387
37                 X    =        -4746148
90
 Y    =       15762477
17  feet           Y    =         4751620
30  meter
 Z    =        -853549
46                 Z    =         -283092
53
 XDOT =     -11687
509401                 XDOT =       -3556
123118
 YDOT =     -10377
973354  feet/sec       YDOT =       -3203
008043  meter/sec
 ZDOT =      19859
710380                 ZDOT =        6035
948219

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16340823
12                 X    =         4980682
89
 Y    =      -14780045
04  feet           Y    =        -4504957
73  meter
 Z    =        -940176
89                 Z    =         -286565
92
 XDOT =      10056
843324                 XDOT =        3065
325845
 YDOT =       9896
403847  feet/sec       YDOT =        3016
423893  meter/sec
 ZDOT =      19793
556264                 ZDOT =        6033
075949


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   07301
39179313  
00020000  00000-0  20000-3 0  9040
2 25544  51
6374 136
9997 0002026 135
7411 224
3915 15
76037940 31792


Satellite: ISS
Catalog Number: 25544
Epoch time:      07301
39179313   =   yrday
fracday
Element set:     904
Inclination:       51
6374  deg
RA of node:       136
9997  deg
Eccentricity:     
0002026     
Arg of perigee:   135
7411  deg
Mean anomaly:     224
3915  deg
Mean motion:   15
76037940  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3179
Checksum:              294


Coasting Arc #6 (Orbit 3194)
---------------------------------------

Vector Time (GMT): 2007/302/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2754900
63                 A    =         6714298
40  meter
 Y    =        3140029
65  meter          E    =           
0016338
 Z    =       -5270637
86                 I    =           51
86042
 XDOT =      -5324
645363                 Wp   =           98
73438
 YDOT =       5528
246638  meter/sec      RA   =          130
93878  deg
 ZDOT =        509
280381                 TA   =          176
10069
                                          MA   =          176
08794
                                          Ha   =            187
434  n
mi
                                          Hp   =            180
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9038387
89                 X    =         2745188
04
 Y    =       10301934
53  feet           Y    =         3170782
58  meter
 Z    =      -17292118
97                 Z    =        -5257277
58
 XDOT =     -17469
308935                 XDOT =       -5388
541362
 YDOT =      18137
292121  feet/sec       YDOT =        5468
346144  meter/sec
 ZDOT =       1670
867393                 ZDOT =         483
257794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8666233
41                 X    =        -2641467
94
 Y    =      -10699852
10  feet           Y    =        -3261314
92  meter
 Z    =      -17240917
97                 Z    =        -5255031
80
 XDOT =      17491
041795                 XDOT =        5331
269539
 YDOT =     -16706
360503  feet/sec       YDOT =       -5092
098681  meter/sec
 ZDOT =       1572
547796                 ZDOT =         479
312568


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   07302
40631307  
00020000  00000-0  20000-3 0  9050
2 25544  51
6370 131
7727 0001899 139
2060 220
9246 15
76066315 31953


Satellite: ISS
Catalog Number: 25544
Epoch time:      07302
40631307   =   yrday
fracday
Element set:     905
Inclination:       51
6370  deg
RA of node:       131
7727  deg
Eccentricity:     
0001899     
Arg of perigee:   139
2060  deg
Mean anomaly:     220
9246  deg
Mean motion:   15
76066315  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3195
Checksum:              275


Coasting Arc #7 (Orbit 3210)
---------------------------------------

Vector Time (GMT): 2007/303/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4570229
38                 A    =         6725827
77  meter
 Y    =       -4791499
19  meter          E    =           
0011435
 Z    =       -1150495
25                 I    =           51
91723
 XDOT =       2784
779975                 Wp   =          143
37341
 YDOT =       4068
304507  meter/sec      RA   =          125
82078  deg
 ZDOT =      -5920
034921                 TA   =           49
18776
                                          MA   =           49
08864
                                          Ha   =            187
465  n
mi
                                          Hp   =            180
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14994190
86                 X    =         4629057
97
 Y    =      -15720141
70  feet           Y    =        -4740063
29  meter
 Z    =       -3774590
71                 Z    =        -1128150
09
 XDOT =       9136
417240                 XDOT =        2767
839618
 YDOT =      13347
455730  feet/sec       YDOT =        4099
351194  meter/sec
 ZDOT =     -19422
686748                 ZDOT =       -5906
547060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15441604
59                 X    =        -4706601
08
 Y    =       15301495
15  feet           Y    =         4663895
72  meter
 Z    =       -3690154
94                 Z    =        -1124759
22
 XDOT =      -7759
486129                 XDOT =       -2365
091372
 YDOT =     -12470
579011  feet/sec       YDOT =       -3801
032482  meter/sec
 ZDOT =     -19370
885645                 ZDOT =       -5904
245945


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   07303
42081638  
00020000  00000-0  20000-3 0  9060
2 25544  51
6372 126
5470 0001954 147
4267 212
7018 15
76039678 32111


Satellite: ISS
Catalog Number: 25544
Epoch time:      07303
42081638   =   yrday
fracday
Element set:     906
Inclination:       51
6372  deg
RA of node:       126
5470  deg
Eccentricity:     
0001954     
Arg of perigee:   147
4267  deg
Mean anomaly:     212
7018  deg
Mean motion:   15
76039678  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3211
Checksum:              283


Coasting Arc #8 (Orbit 3226)
---------------------------------------

Vector Time (GMT): 2007/304/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2161122
76                 A    =         6715443
96  meter
 Y    =       -3976444
36  meter          E    =           
0006235
 Z    =        4956826
22                 I    =           51
89913
 XDOT =       5101
030129                 Wp   =           72
51682
 YDOT =      -5386
372479  meter/sec      RA   =          120
65990  deg
 ZDOT =      -2093
062367                 TA   =           37
69085
                                          MA   =           37
64718
                                          Ha   =            187
298  n
mi
                                          Hp   =            180
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7090297
76                 X    =        -2140576
65
 Y    =      -13046077
31  feet           Y    =        -4000496
66  meter
 Z    =       16262553
20                 Z    =         4946377
01
 XDOT =      16735
663152                 XDOT =        5171
050101
 YDOT =     -17671
825717  feet/sec       YDOT =       -5328
938252  meter/sec
 ZDOT =      -6867
002517                 ZDOT =       -2068
111431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7047191
12                 X    =         2147983
85
 Y    =       13119317
26  feet           Y    =         3998767
90  meter
 Z    =       16222321
16                 Z    =         4944563
49
 XDOT =     -15998
281566                 XDOT =       -4876
276221
 YDOT =      16984
436001  feet/sec       YDOT =        5176
856093  meter/sec
 ZDOT =      -6772
710258                 ZDOT =       -2064
322087


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   07304
43529917  
00020000  00000-0  20000-3 0  9070
2 25544  51
6373 121
3199 0001728 149
3850 210
7416 15
76129809 32274


Satellite: ISS
Catalog Number: 25544
Epoch time:      07304
43529917   =   yrday
fracday
Element set:     907
Inclination:       51
6373  deg
RA of node:       121
3199  deg
Eccentricity:     
0001728     
Arg of perigee:   149
3850  deg
Mean anomaly:     210
7416  deg
Mean motion:   15
76129809  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3227
Checksum:              296


Coasting Arc #9 (Orbit 3242)
---------------------------------------

Vector Time (GMT): 2007/305/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4309860
39                 A    =         6723454
49  meter
 Y    =        4520227
89  meter          E    =           
0014284
 Z    =        2474102
54                 I    =           51
93895
 XDOT =      -2226
718836                 Wp   =           81
72172
 YDOT =      -5069
766727  meter/sec      RA   =          115
56542  deg
 ZDOT =       5359
522045                 TA   =          306
16718
                                          MA   =          306
29924
                                          Ha   =            187
166  n
mi
                                          Hp   =            180
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14139961
90                 X    =        -4372104
82
 Y    =       14830144
00  feet           Y    =         4471684
47  meter
 Z    =        8117134
32                 Z    =         2453013
97
 XDOT =      -7305
507993                 XDOT =       -2195
898340
 YDOT =     -16633
092935  feet/sec       YDOT =       -5094
495033  meter/sec
 ZDOT =      17583
733745                 ZDOT =        5348
779191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14082551
68                 X    =         4292361
75
 Y    =      -14927863
10  feet           Y    =        -4550012
67  meter
 Z    =        8037425
23                 Z    =         2449807
21
 XDOT =       6430
716882                 XDOT =        1960
082506
 YDOT =      15554
635493  feet/sec       YDOT =        4741
052898  meter/sec
 ZDOT =      17542
251702                 ZDOT =        5346
878319


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   07305
44976528  
00020000  00000-0  20000-3 0  9087
2 25544  51
6364 116
0927 0001681 155
4231 204
7014 15
76151414 32435


Satellite: ISS
Catalog Number: 25544
Epoch time:      07305
44976528   =   yrday
fracday
Element set:     908
Inclination:       51
6364  deg
RA of node:       116
0927  deg
Eccentricity:     
0001681     
Arg of perigee:   155
4231  deg
Mean anomaly:     204
7014  deg
Mean motion:   15
76151414  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3243
Checksum:              274


Coasting Arc #10 (Orbit 3257)
---------------------------------------

Vector Time (GMT): 2007/306/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1775434
55                 A    =         6718048
48  meter
 Y    =        4865496
46  meter          E    =           
0009860
 Z    =       -4288951
54                 I    =           51
93142
 XDOT =      -4779
467270                 Wp   =          117
80704
 YDOT =       4873
915956  meter/sec      RA   =          110
38710  deg
 ZDOT =       3552
283303                 TA   =          188
08359
                                          MA   =          188
09949
                                          Ha   =            187
088  n
mi
                                          Hp   =            180
233

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5824916
50                 X    =         1741731
06
 Y    =       15962914
90  feet           Y    =         4885162
00  meter
 Z    =      -14071363
33                 Z    =        -4280408
17
 XDOT =     -15680
666896                 XDOT =       -4850
869455
 YDOT =      15990
537914  feet/sec       YDOT =        4820
069955  meter/sec
 ZDOT =      11654
472778                 ZDOT =        3528
891036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6287315
70                 X    =        -1916373
82
 Y    =      -15815944
24  feet           Y    =        -4820699
81  meter
 Z    =      -14038274
08                 Z    =        -4278865
94
 XDOT =      14202
540794                 XDOT =        4328
934434
 YDOT =     -15907
092139  feet/sec       YDOT =       -4848
481684  meter/sec
 ZDOT =      11566
031841                 ZDOT =        3525
326505


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   07306
40081109  
00020000  00000-0  20000-3 0  9097
2 25544  51
6355 111
1916 0001685 156
8047 203
3193 15
76166455 32583


Satellite: ISS
Catalog Number: 25544
Epoch time:      07306
40081109   =   yrday
fracday
Element set:     909
Inclination:       51
6355  deg
RA of node:       111
1916  deg
Eccentricity:     
0001685     
Arg of perigee:   156
8047  deg
Mean anomaly:     203
3193  deg
Mean motion:   15
76166455  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3258
Checksum:              282


Coasting Arc #11 (Orbit 3273)
---------------------------------------

Vector Time (GMT): 2007/307/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4054018
32                 A    =         6720124
79  meter
 Y    =       -3901554
31  meter          E    =           
0006158
 Z    =       -3679457
60                 I    =           51
94663
 XDOT =       1880
276265                 Wp   =           94
31920
 YDOT =       6059
648265  meter/sec      RA   =          105
30696  deg
 ZDOT =      -4360
397506                 TA   =          129
71251
                                          MA   =          129
65821
                                          Ha   =            187
044  n
mi
                                          Hp   =            180
261

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13300585
05                 X    =         4115219
16
 Y    =      -12800375
03  feet           Y    =        -3855877
79  meter
 Z    =      -12071711
30                 Z    =        -3659614
27
 XDOT =       6168
885385                 XDOT =        1833
558913
 YDOT =      19880
735777  feet/sec       YDOT =        6080
413368  meter/sec
 ZDOT =     -14305
766095                 ZDOT =       -4351
376486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12828194
59                 X    =        -3910033
71
 Y    =       13341628
96  feet           Y    =         4066528
51  meter
 Z    =      -11996655
26                 Z    =        -3656580
52
 XDOT =      -6092
384695                 XDOT =       -1856
958855
 YDOT =     -18670
223186  feet/sec       YDOT =       -5690
684027  meter/sec
 ZDOT =     -14270
717909                 ZDOT =       -4349
714819


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   07307
41524127  
00020000  00000-0  20000-3 0  9103
2 25544  51
6347 105
9649 0001611 159
6379 200
4850 15
76190202 32749


Satellite: ISS
Catalog Number: 25544
Epoch time:      07307
41524127   =   yrday
fracday
Element set:     910
Inclination:       51
6347  deg
RA of node:       105
9649  deg
Eccentricity:     
0001611     
Arg of perigee:   159
6379  deg
Mean anomaly:     200
4850  deg
Mean motion:   15
76190202  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3274
Checksum:              274


Coasting Arc #12 (Orbit 3289)
---------------------------------------

Vector Time (GMT): 2007/308/09:23:23
224
Vector Time (MET): N/A
Weight (LBS)     : 509051
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1566098
42                 A    =         6721214
78  meter
 Y    =       -5667006
57  meter          E    =           
0013274
 Z    =        3243447
11                 I    =           51
95782
 XDOT =       4522
883955                 Wp   =           98
75349
 YDOT =      -4000
587892  meter/sec      RA   =          100
12455  deg
 ZDOT =      -4791
476284                 TA   =           43
41563
                                          MA   =           43
31116
                                          Ha   =            186
855  n
mi
                                          Hp   =            180
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5138118
18                 X    =        -1518369
04
 Y    =      -18592541
25  feet           Y    =        -5684252
66  meter
 Z    =       10641230
67                 Z    =         3235954
89
 XDOT =      14838
858120                 XDOT =        4590
559483
 YDOT =     -13125
288358  feet/sec       YDOT =       -3949
632108  meter/sec
 ZDOT =     -15720
066550                 ZDOT =       -4769
339323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6276534
65                 X    =         1913087
76
 Y    =       18256729
05  feet           Y    =         5564651
01  meter
 Z    =       10612049
57                 Z    =         3234552
71
 XDOT =     -12802
629221                 XDOT =       -3902
241386
 YDOT =      13518
139883  feet/sec       YDOT =        4120
329036  meter/sec
 ZDOT =     -15636
288344                 ZDOT =       -4765
940687


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   07308
42965104  
00020000  00000-0  20000-3 0  9110
2 25544  51
6352 100
7370 0001463 169
2412 190
8784 15
76251836 32906


Satellite: ISS
Catalog Number: 25544
Epoch time:      07308
42965104   =   yrday
fracday
Element set:     911
Inclination:       51
6352  deg
RA of node:       100
7370  deg
Eccentricity:     
0001463     
Arg of perigee:   169
2412  deg
Mean anomaly:     190
8784  deg
Mean motion:   15
76251836  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3290
Checksum:              278

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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