Date: September 24th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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


276/12:05:13 167 -4 0 5 1 5 1
N/A -2 2 0 0 193 7
000/00:10:26 334 2 2 0 2 188 8

Coasting Arc #1 (Orbit 386)
---------------------------------------

Vector Time (GMT): 2008/266/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4578694
63                 A    =         6726817
83  meter
 Y    =         296176
60  meter          E    =           
0018362
 Z    =       -4935925
50                 I    =           51
35337
 XDOT =      -2692
630149                 Wp   =          116
21022
 YDOT =      -6888
586682  meter/sec      RA   =          235
63929  deg
 ZDOT =       2082
428082                 TA   =          174
10511
                                          MA   =          174
08347
                                          Ha   =            194
895  n
mi
                                          Hp   =            184
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15021964
03                 X    =        -4557688
30
 Y    =         971708
00  feet           Y    =          245092
50  meter
 Z    =      -16193981
30                 Z    =        -4958117
86
 XDOT =      -8834
088415                 XDOT =       -2625
516838
 YDOT =     -22600
350006  feet/sec       YDOT =       -6918
321999  meter/sec
 ZDOT =       6832
113130                 ZDOT =        2069
510174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7755644
13                 X    =         2363920
33
 Y    =      -12793264
99  feet           Y    =        -3899387
17  meter
 Z    =      -16279772
88                 Z    =        -4962074
77
 XDOT =      22674
625060                 XDOT =        6911
225718
 YDOT =       5108
173806  feet/sec       YDOT =        1556
971376  meter/sec
 ZDOT =       6781
470315                 ZDOT =        2066
992152


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   08266
66220033  
00020000  00000-0  20000-3 0  9003
2 25544  51
6402 236
4920 0006256 138
2664 221
8977 15
72145162  3873


Satellite: ISS
Catalog Number: 25544
Epoch time:      08266
66220033   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:       236
4920  deg
Eccentricity:     
0006256     
Arg of perigee:   138
2664  deg
Mean anomaly:     221
8977  deg
Mean motion:   15
72145162  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             387
Checksum:              278


Coasting Arc #2 (Orbit 402)
---------------------------------------

Vector Time (GMT): 2008/267/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3362055
33                 A    =         6736754
70  meter
 Y    =        5688331
67  meter          E    =           
0015380
 Z    =       -1278927
93                 I    =           51
40469
 XDOT =      -4781
846776                 Wp   =          142
92946
 YDOT =       1524
403979  meter/sec      RA   =          230
52805  deg
 ZDOT =      -5838
891392                 TA   =           51
14215
                                          MA   =           51
00501
                                          Ha   =            194
843  n
mi
                                          Hp   =            185
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11030365
24                 X    =         3304410
40
 Y    =       18662505
50  feet           Y    =         5725605
80  meter
 Z    =       -4195957
79                 Z    =        -1262735
13
 XDOT =     -15688
473674                 XDOT =       -4770
173251
 YDOT =       5001
325390  feet/sec       YDOT =        1470
995850  meter/sec
 ZDOT =     -19156
467822                 ZDOT =       -5862
093238

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21654151
55                 X    =        -6600185
39
 Y    =       -1257843
35  feet           Y    =         -383390
65  meter
 Z    =       -4132757
10                 Z    =        -1259664
36
 XDOT =       4463
452673                 XDOT =        1360
460375
 YDOT =     -14135
651580  feet/sec       YDOT =       -4308
546602  meter/sec
 ZDOT =     -19246
048500                 ZDOT =       -5866
195583


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   08267
67922311  
00020000  00000-0  20000-3 0  9014
2 25544  51
6405 231
2832 0006308 142
9356 217
2243 15
72151495  4039


Satellite: ISS
Catalog Number: 25544
Epoch time:      08267
67922311   =   yrday
fracday
Element set:     901
Inclination:       51
6405  deg
RA of node:       231
2832  deg
Eccentricity:     
0006308     
Arg of perigee:   142
9356  deg
Mean anomaly:     217
2243  deg
Mean motion:   15
72151495  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             403
Checksum:              265


Coasting Arc #3 (Orbit 418)
---------------------------------------

Vector Time (GMT): 2008/268/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3581730
16                 A    =         6725327
53  meter
 Y    =       -2289853
16  meter          E    =           
0007112
 Z    =        5205650
83                 I    =           51
38630
 XDOT =       4912
151172                 Wp   =          121
01916
 YDOT =       5880
773743  meter/sec      RA   =          225
37039  deg
 ZDOT =       -795
775257                 TA   =          336
56149
                                          MA   =          336
59389
                                          Ha   =            194
496  n
mi
                                          Hp   =            185
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11751083
19                 X    =         3581781
43
 Y    =       -7512641
59  feet           Y    =        -2249799
73  meter
 Z    =       17078906
94                 Z    =         5223051
02
 XDOT =      16115
981537                 XDOT =        4849
892050
 YDOT =      19293
877108  feet/sec       YDOT =        5935
356117  meter/sec
 ZDOT =      -2610
811212                 ZDOT =        -772
063516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -40807
75                 X    =          -12438
20
 Y    =       13864727
41  feet           Y    =         4225968
91  meter
 Z    =       17145975
35                 Z    =         5226093
29
 XDOT =     -23954
406300                 XDOT =       -7301
303040
 YDOT =       3032
657619  feet/sec       YDOT =         924
354042  meter/sec
 ZDOT =      -2518
494355                 ZDOT =        -767
637079


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   08268
69622915  
00020000  00000-0  20000-3 0  9025
2 25544  51
6401 226
0745 0006147 147
0888 213
0658 15
72233110  4193


Satellite: ISS
Catalog Number: 25544
Epoch time:      08268
69622915   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       226
0745  deg
Eccentricity:     
0006147     
Arg of perigee:   147
0888  deg
Mean anomaly:     213
0658  deg
Mean motion:   15
72233110  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             419
Checksum:              280


Coasting Arc #4 (Orbit 434)
---------------------------------------

Vector Time (GMT): 2008/269/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5080362
40                 A    =         6737263
14  meter
 Y    =       -4419915
73  meter          E    =           
0012479
 Z    =         115539
02                 I    =           51
44831
 XDOT =       3232
792326                 Wp   =           75
11101
 YDOT =      -3544
546941  meter/sec      RA   =          220
23983  deg
 ZDOT =       6015
818510                 TA   =          286
14595
                                          MA   =          286
28327
                                          Ha   =            194
574  n
mi
                                          Hp   =            185
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16667855
64                 X    =        -5031121
87
 Y    =      -14501035
85  feet           Y    =        -4476451
95  meter
 Z    =         379065
02                 Z    =           90978
56
 XDOT =      10606
274035                 XDOT =        3242
964076
 YDOT =     -11629
091015  feet/sec       YDOT =       -3508
338764  meter/sec
 ZDOT =      19736
937370                 ZDOT =        6031
548285

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21130349
85                 X    =         6440530
64
 Y    =       -6455155
17  feet           Y    =        -1967531
29  meter
 Z    =         283601
25                 Z    =           86441
66
 XDOT =       3832
792765                 XDOT =        1168
235235
 YDOT =      13519
616199  feet/sec       YDOT =        4120
779017  meter/sec
 ZDOT =      19797
415965                 ZDOT =        6034
252386


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   08269
71322318  
00020000  00000-0  20000-3 0  9034
2 25544  51
6406 220
8651 0006157 150
1682 209
9833 15
72214526  4351


Satellite: ISS
Catalog Number: 25544
Epoch time:      08269
71322318   =   yrday
fracday
Element set:     903
Inclination:       51
6406  deg
RA of node:       220
8651  deg
Eccentricity:     
0006157     
Arg of perigee:   150
1682  deg
Mean anomaly:     209
9833  deg
Mean motion:   15
72214526  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             435
Checksum:              277


Coasting Arc #5 (Orbit 449)
---------------------------------------

Vector Time (GMT): 2008/270/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1957893
63                 A    =         6725168
45  meter
 Y    =        3740410
56  meter          E    =           
0018112
 Z    =       -5249636
47                 I    =           51
43186
 XDOT =      -6492
534055                 Wp   =          104
53544
 YDOT =      -4083
009341  meter/sec      RA   =          215
10657  deg
 ZDOT =       -493
625305                 TA   =          160
78681
                                          MA   =          160
71842
                                          Ha   =            194
415  n
mi
                                          Hp   =            185
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6423535
52                 X    =        -1974072
20
 Y    =       12271688
17  feet           Y    =         3718425
37  meter
 Z    =      -17223216
75                 Z    =        -5259187
52
 XDOT =     -21300
964746                 XDOT =       -6443
996702
 YDOT =     -13395
699937  feet/sec       YDOT =       -4155
341259  meter/sec
 ZDOT =      -1619
505593                 ZDOT =        -525
047805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7259960
75                 X    =        -2212836
04
 Y    =      -11742596
71  feet           Y    =        -3579143
48  meter
 Z    =      -17259771
92                 Z    =        -5260778
48
 XDOT =      21593
281851                 XDOT =        6581
632308
 YDOT =     -10818
850358  feet/sec       YDOT =       -3297
585589  meter/sec
 ZDOT =      -1741
490522                 ZDOT =        -530
806311


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   08270
66663942  
00020000  00000-0  20000-3 0  9042
2 25544  51
6413 215
9813 0006137 153
9154 206
2319 15
72257947  4507


Satellite: ISS
Catalog Number: 25544
Epoch time:      08270
66663942   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       215
9813  deg
Eccentricity:     
0006137     
Arg of perigee:   153
9154  deg
Mean anomaly:     206
2319  deg
Mean motion:   15
72257947  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             450
Checksum:              291


Coasting Arc #6 (Orbit 465)
---------------------------------------

Vector Time (GMT): 2008/271/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6114314
72                 A    =         6736792
83  meter
 Y    =        2626821
25  meter          E    =           
0019267
 Z    =         977185
97                 I    =           51
49570
 XDOT =      -1106
751807                 Wp   =          134
99586
 YDOT =       4800
917128  meter/sec      RA   =          209
95791  deg
 ZDOT =      -5923
072017                 TA   =           34
30503
                                          MA   =           34
18075
                                          Ha   =            194
416  n
mi
                                          Hp   =            185
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20060087
65                 X    =         6079739
73
 Y    =        8618179
94  feet           Y    =         2695001
82  meter
 Z    =        3205990
71                 Z    =         1006805
22
 XDOT =      -3631
075482                 XDOT =       -1131
580822
 YDOT =      15751
040447  feet/sec       YDOT =        4788
401401  meter/sec
 ZDOT =     -19432
650976                 ZDOT =       -5928
509410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17489099
69                 X    =        -5330677
59
 Y    =       13040775
88  feet           Y    =         3974828
49  meter
 Z    =        3320854
55                 Z    =         1012196
47
 XDOT =     -10925
923146                 XDOT =       -3330
221375
 YDOT =      -9652
698277  feet/sec       YDOT =       -2942
142435  meter/sec
 ZDOT =     -19453
177933                 ZDOT =       -5929
328634


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   08271
68360369  
00020000  00000-0  20000-3 0  9053
2 25544  51
6415 210
7723 0006295 158
2391 201
9039 15
72226757  4661


Satellite: ISS
Catalog Number: 25544
Epoch time:      08271
68360369   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       210
7723  deg
Eccentricity:     
0006295     
Arg of perigee:   158
2391  deg
Mean anomaly:     201
9039  deg
Mean motion:   15
72226757  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             466
Checksum:              296


Coasting Arc #7 (Orbit 481)
---------------------------------------

Vector Time (GMT): 2008/272/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -90341
70                 A    =         6726048
82  meter
 Y    =       -4456592
59  meter          E    =           
0010918
 Z    =        5033838
02                 I    =           51
48654
 XDOT =       7271
982061                 Wp   =          144
97050
 YDOT =       1836
582518  meter/sec      RA   =          204
84909  deg
 ZDOT =       1745
816219                 TA   =          288
12808
                                          MA   =          288
24695
                                          Ha   =            194
232  n
mi
                                          Hp   =            185
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -296396
66                 X    =          -64954
38
 Y    =      -14621366
78  feet           Y    =        -4457460
40  meter
 Z    =       16515216
62                 Z    =         5033461
25
 XDOT =      23858
208861                 XDOT =        7242
423677
 YDOT =       6025
533195  feet/sec       YDOT =        1917
736923  meter/sec
 ZDOT =       5727
743501                 ZDOT =        1781
071892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12973470
71                 X    =         3954313
87
 Y    =        6754633
05  feet           Y    =         2058812
15  meter
 Z    =       16513285
18                 Z    =         5033249
32
 XDOT =     -16339
233326                 XDOT =       -4980
198318
 YDOT =      16960
066961  feet/sec       YDOT =        5169
428410  meter/sec
 ZDOT =       5864
335019                 ZDOT =        1787
449314


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   08272
70055011  
00020000  00000-0  20000-3 0  9063
2 25544  51
6420 205
5630 0006097 161
9910 198
1470 15
72287203  4821


Satellite: ISS
Catalog Number: 25544
Epoch time:      08272
70055011   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       205
5630  deg
Eccentricity:     
0006097     
Arg of perigee:   161
9910  deg
Mean anomaly:     198
1470  deg
Mean motion:   15
72287203  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             482
Checksum:              266


Coasting Arc #8 (Orbit 496)
---------------------------------------

Vector Time (GMT): 2008/273/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6395377
31                 A    =         6735101
82  meter
 Y    =        -565978
98  meter          E    =           
0005681
 Z    =       -2041491
19                 I    =           51
54458
 XDOT =      -1312
986000                 Wp   =           99
20874
 YDOT =      -5154
673319  meter/sec      RA   =          199
68418  deg
 ZDOT =       5554
495028                 TA   =          238
02613
                                          MA   =          238
08136
                                          Ha   =            194
025  n
mi
                                          Hp   =            185
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20982209
02                 X    =        -6378655
77
 Y    =       -1856886
43  feet           Y    =         -637402
48  meter
 Z    =       -6697805
75                 Z    =        -2072519
75
 XDOT =      -4307
696850                 XDOT =       -1282
231182
 YDOT =     -16911
657870  feet/sec       YDOT =       -5169
183411  meter/sec
 ZDOT =      18223
408883                 ZDOT =        5548
191627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11487297
90                 X    =         3501328
40
 Y    =      -17610217
73  feet           Y    =        -5367594
37  meter
 Z    =       -6817913
37                 Z    =        -2078099
99
 XDOT =      15715
698504                 XDOT =        4790
144904
 YDOT =       3221
091598  feet/sec       YDOT =         981
788719  meter/sec
 ZDOT =      18198
473422                 ZDOT =        5546
894699


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   08273
65392371  
00020000  00000-0  20000-3 0  9072
2 25544  51
6419 200
6791 0005966 166
7975 193
3345 15
72313090  4979


Satellite: ISS
Catalog Number: 25544
Epoch time:      08273
65392371   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:       200
6791  deg
Eccentricity:     
0005966     
Arg of perigee:   166
7975  deg
Mean anomaly:     193
3345  deg
Mean motion:   15
72313090  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             497
Checksum:              313


Coasting Arc #9 (Orbit 512)
---------------------------------------

Vector Time (GMT): 2008/274/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2171780
31                 A    =         6727642
33  meter
 Y    =        4371396
89  meter          E    =           
0011084
 Z    =       -4638047
60                 I    =           51
54684
 XDOT =      -7118
033819                 Wp   =          102
28896
 YDOT =        500
853694  meter/sec      RA   =          194
59497  deg
 ZDOT =      -2869
058908                 TA   =          139
30420
                                          MA   =          139
22133
                                          Ha   =            193
884  n
mi
                                          Hp   =            185
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7125263
47                 X    =         2145268
47
 Y    =       14341853
30  feet           Y    =         4395534
38  meter
 Z    =      -15216691
59                 Z    =        -4627561
63
 XDOT =     -23353
129328                 XDOT =       -7109
167770
 YDOT =       1643
220781  feet/sec       YDOT =         421
305073  meter/sec
 ZDOT =      -9412
922926                 ZDOT =       -2903
617492

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16052871
79                 X    =        -4892915
32
 Y    =        -102851
47  feet           Y    =          -31349
13  meter
 Z    =      -15175657
06                 Z    =        -4625540
27
 XDOT =       9130
009868                 XDOT =        2782
827008
 YDOT =     -20324
536637  feet/sec       YDOT =       -6194
918767  meter/sec
 ZDOT =      -9546
581478                 ZDOT =       -2909
798034


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   08274
67084038  
00020000  00000-0  20000-3 0  9084
2 25544  51
6413 195
4695 0005939 171
9223 188
2036 15
72336344  5137


Satellite: ISS
Catalog Number: 25544
Epoch time:      08274
67084038   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       195
4695  deg
Eccentricity:     
0005939     
Arg of perigee:   171
9223  deg
Mean anomaly:     188
2036  deg
Mean motion:   15
72336344  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             513
Checksum:              303


Coasting Arc #10 (Orbit 528)
---------------------------------------

Vector Time (GMT): 2008/275/15:35:44
821
Vector Time (MET): N/A
Weight (LBS)     : 614388
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5871173
66                 A    =         6732875
05  meter
 Y    =       -1404556
17  meter          E    =           
0015539
 Z    =        2960197
00                 I    =           51
59411
 XDOT =       3627
092174                 Wp   =          118
72676
 YDOT =       4613
738882  meter/sec      RA   =          189
42171  deg
 ZDOT =      -4992
378880                 TA   =           27
09027
                                          MA   =           27
00927
                                          Ha   =            193
610  n
mi
                                          Hp   =            185
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19262380
78                 X    =         5872062
86
 Y    =       -4608123
91  feet           Y    =        -1338896
16  meter
 Z    =        9711932
42                 Z    =         2988722
03
 XDOT =      11899
908707                 XDOT =        3599
483632
 YDOT =      15136
938590  feet/sec       YDOT =        4654
144442  meter/sec
 ZDOT =     -16379
195801                 ZDOT =       -4974
825433

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4304324
03                 X    =        -1311957
96
 Y    =       19276766
95  feet           Y    =         5875558
57  meter
 Z    =        9822158
70                 Z    =         2993793
97
 XDOT =     -17462
573704                 XDOT =       -5322
592465
 YDOT =       4432
103506  feet/sec       YDOT =        1350
905149  meter/sec
 ZDOT =     -16310
789258                 ZDOT =       -4971
528566


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   08275
68774142  
00020000  00000-0  20000-3 0  9099
2 25544  51
6415 190
2604 0005858 175
0569 185
0652 15
72389026  5291


Satellite: ISS
Catalog Number: 25544
Epoch time:      08275
68774142   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       190
2604  deg
Eccentricity:     
0005858     
Arg of perigee:   175
0569  deg
Mean anomaly:     185
0652  deg
Mean motion:   15
72389026  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             529
Checksum:              312


Coasting Arc #11 (Orbit 541)
---------------------------------------

Vector Time (GMT): 2008/276/12:10:26
334
Vector Time (MET): N/A
Weight (LBS)     : 614022
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5546188
63                 A    =         6735025
22  meter
 Y    =        2070090
97  meter          E    =           
0003569
 Z    =       -3216601
34                 I    =           51
61612
 XDOT =      -4334
733560                 Wp   =          156
29754
 YDOT =      -4182
836502  meter/sec      RA   =          185
02549  deg
 ZDOT =       4780
816096                 TA   =          166
18045
                                          MA   =          166
17068
                                          Ha   =            193
745  n
mi
                                          Hp   =            188
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18196156
91                 X    =        -5553298
49
 Y    =        6791637
06  feet           Y    =         2008030
39  meter
 Z    =      -10553154
01                 Z    =        -3243562
70
 XDOT =     -14221
566799                 XDOT =       -4310
863102
 YDOT =     -13723
216869  feet/sec       YDOT =       -4231
176309  meter/sec
 ZDOT =      15685
092179                 ZDOT =        4759
815662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16060316
19                 X    =         4895184
37
 Y    =      -10820554
43  feet           Y    =        -3298104
99  meter
 Z    =      -10657268
21                 Z    =        -3248335
35
 XDOT =      16319
739286                 XDOT =        4974
256534
 YDOT =       8850
109731  feet/sec       YDOT =        2697
513446  meter/sec
 ZDOT =      15603
390691                 ZDOT =        4755
913483


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   08276
51396328  
00020000  00000-0  20000-3 0  9100
2 25544  51
6408 186
0275 0004940 219
6138 140
4664 15
71396245  5421


Satellite: ISS
Catalog Number: 25544
Epoch time:      08276
51396328   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:       186
0275  deg
Eccentricity:     
0004940     
Arg of perigee:   219
6138  deg
Mean anomaly:     140
4664  deg
Mean motion:   15
71396245  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             542
Checksum:              293


Coasting Arc #12 (Orbit 557)
---------------------------------------

Vector Time (GMT): 2008/277/12:10:26
334
Vector Time (MET): N/A
Weight (LBS)     : 614022
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4895412
87                 A    =         6733934
63  meter
 Y    =        2866988
19  meter          E    =           
0003312
 Z    =       -3626987
39                 I    =           51
64188
 XDOT =      -5281
105701                 Wp   =          145
18125
 YDOT =       3474
754889  meter/sec      RA   =          179
96005  deg
 ZDOT =      -4385
984295                 TA   =           78
20589
                                          MA   =           78
16873
                                          Ha   =            193
617  n
mi
                                          Hp   =            189
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16061065
83                 X    =         4880609
53
 Y    =        9406129
23  feet           Y    =         2921648
65  meter
 Z    =      -11899564
94                 Z    =        -3603241
00
 XDOT =     -17326
462275                 XDOT =       -5298
261680
 YDOT =      11400
114465  feet/sec       YDOT =        3415
602473  meter/sec
 ZDOT =     -14389
712254                 ZDOT =       -4411
682232

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17963679
66                 X    =        -5475329
56
 Y    =       -5091659
48  feet           Y    =        -1551937
81  meter
 Z    =      -11807369
11                 Z    =        -3598886
11
 XDOT =      13488
948604                 XDOT =        4111
431535
 YDOT =     -14026
335913  feet/sec       YDOT =       -4275
227186  meter/sec
 ZDOT =     -14488
802527                 ZDOT =       -4416
187010


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   08277
53147991  
00020000  00000-0  20000-3 0  9114
2 25544  51
6411 180
8224 0004953 224
7689 135
3074 15
71412942  5581


Satellite: ISS
Catalog Number: 25544
Epoch time:      08277
53147991   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:       180
8224  deg
Eccentricity:     
0004953     
Arg of perigee:   224
7689  deg
Mean anomaly:     135
3074  deg
Mean motion:   15
71412942  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             558
Checksum:              297


Coasting Arc #13 (Orbit 573)
---------------------------------------

Vector Time (GMT): 2008/278/12:10:26
334
Vector Time (MET): N/A
Weight (LBS)     : 614022
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3458610
25                 A    =         6731116
52  meter
 Y    =       -3778955
31  meter          E    =           
0005121
 Z    =        4362001
46                 I    =           51
66160
 XDOT =       6581
937116                 Wp   =           90
06851
 YDOT =       2098
434301  meter/sec      RA   =          174
79562  deg
 ZDOT =      -3397
423929                 TA   =           34
18598
                                          MA   =           34
15302
                                          Ha   =            193
283  n
mi
                                          Hp   =            189
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11347146
48                 X    =         3479419
85
 Y    =      -12398147
35  feet           Y    =        -3740162
73  meter
 Z    =       14311028
40                 Z    =         4378854
31
 XDOT =      21594
281876                 XDOT =        6574
487297
 YDOT =       6884
626973  feet/sec       YDOT =        2171
995624  meter/sec
 ZDOT =     -11146
403968                 ZDOT =       -3365
466365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7565359
26                 X    =        -2305921
50
 Y    =       14945806
51  feet           Y    =         4555481
83  meter
 Z    =       14375866
29                 Z    =         4381764
05
 XDOT =     -21618
728170                 XDOT =       -6589
388346
 YDOT =       -330
200397  feet/sec       YDOT =        -100
645081  meter/sec
 ZDOT =     -11022
499406                 ZDOT =       -3359
657819


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   08278
54898170  
00020000  00000-0  20000-3 0  9129
2 25544  51
6404 175
6171 0004902 229
2852 130
7884 15
71449124  5740


Satellite: ISS
Catalog Number: 25544
Epoch time:      08278
54898170   =   yrday
fracday
Element set:     912
Inclination:       51
6404  deg
RA of node:       175
6171  deg
Eccentricity:     
0004902     
Arg of perigee:   229
2852  deg
Mean anomaly:     130
7884  deg
Mean motion:   15
71449124  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             574
Checksum:              301

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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