Date: September 6th 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


There are no maneuvers



Coasting Arc #1 (Orbit 86)
---------------------------------------

Vector Time (GMT): 2008/247/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5131530
25                 A    =         6730463
09  meter
 Y    =        1188135
42  meter          E    =           
0015862
 Z    =        4177059
49                 I    =           51
49247
 XDOT =      -4218
736600                 Wp   =           94
44100
 YDOT =       5307
632090  meter/sec      RA   =          333
91486  deg
 ZDOT =       3659
897916                 TA   =          318
12335
                                          MA   =          318
24457
                                          Ha   =            195
481  n
mi
                                          Hp   =            184
757

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16835729
16                 X    =         5097571
47
 Y    =        3898082
07  feet           Y    =         1245329
46  meter
 Z    =       13704263
43                 Z    =         4201906
01
 XDOT =     -13840
999345                 XDOT =       -4295
553032
 YDOT =      17413
491110  feet/sec       YDOT =        5260
026412  meter/sec
 ZDOT =      12007
539094                 ZDOT =        3639
216394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16418016
22                 X    =        -5004211
34
 Y    =       -5142120
21  feet           Y    =        -1567318
24  meter
 Z    =       13800398
53                 Z    =         4206361
47
 XDOT =      14799
590659                 XDOT =        4510
915233
 YDOT =     -15125
701935  feet/sec       YDOT =       -4610
313950  meter/sec
 ZDOT =      11928
070179                 ZDOT =        3635
675791


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   08247
59154239  
00020000  00000-0  20000-3 0  9008
2 25544  51
6427 334
1302 0006278  76
2956 283
8905 15
71903324   876


Satellite: ISS
Catalog Number: 25544
Epoch time:      08247
59154239   =   yrday
fracday
Element set:     900
Inclination:       51
6427  deg
RA of node:       334
1302  deg
Eccentricity:     
0006278     
Arg of perigee:    76
2956  deg
Mean anomaly:     283
8905  deg
Mean motion:   15
71903324  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              87
Checksum:              296


Coasting Arc #2 (Orbit 101)
---------------------------------------

Vector Time (GMT): 2008/248/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2550014
21                 A    =         6732163
79  meter
 Y    =       -5009243
99  meter          E    =           
0012004
 Z    =       -3715245
64                 I    =           51
47150
 XDOT =       6392
680511                 Wp   =           89
59807
 YDOT =         96
128493  meter/sec      RA   =          328
73412  deg
 ZDOT =       4270
067714                 TA   =          225
58460
                                          MA   =          225
68292
                                          Ha   =            195
632  n
mi
                                          Hp   =            184
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8366188
34                 X    =         2623886
94
 Y    =      -16434527
54  feet           Y    =        -4980315
33  meter
 Z    =      -12189126
12                 Z    =        -3702678
02
 XDOT =      20973
361258                 XDOT =        6370
387143
 YDOT =        315
382195  feet/sec       YDOT =         167
490609  meter/sec
 ZDOT =      14009
408512                 ZDOT =        4301
069361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9370474
06                 X    =        -2856120
49
 Y    =       15920180
49  feet           Y    =         4852471
01  meter
 Z    =      -12140991
20                 Z    =        -3700574
12
 XDOT =     -19678
857461                 XDOT =       -5998
115754
 YDOT =       -837
667722  feet/sec       YDOT =        -255
321122  meter/sec
 ZDOT =      14129
234874                 ZDOT =        4306
590790


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   08248
54516499  
00020000  00000-0  20000-3 0  9015
2 25544  51
6418 329
2490 0006430  79
3380 280
8506 15
71921548  1024


Satellite: ISS
Catalog Number: 25544
Epoch time:      08248
54516499   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:       329
2490  deg
Eccentricity:     
0006430     
Arg of perigee:    79
3380  deg
Mean anomaly:     280
8506  deg
Mean motion:   15
71921548  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             102
Checksum:              291


Coasting Arc #3 (Orbit 117)
---------------------------------------

Vector Time (GMT): 2008/249/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5806033
59                 A    =         6733451
30  meter
 Y    =        1053695
88  meter          E    =           
0011113
 Z    =       -3253463
22                 I    =           51
45124
 XDOT =       1583
554566                 Wp   =           87
21174
 YDOT =      -5847
990521  meter/sec      RA   =          323
65245  deg
 ZDOT =      -4733
330369                 TA   =          130
91226
                                          MA   =          130
81597
                                          Ha   =            195
645  n
mi
                                          Hp   =            184
565

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19048666
62                 X    =        -5801579
84
 Y    =        3457007
47  feet           Y    =          988794
33  meter
 Z    =      -10674091
93                 Z    =        -3281658
28
 XDOT =       5195
388996                 XDOT =        1671
823829
 YDOT =     -19186
320608  feet/sec       YDOT =       -5829
788821  meter/sec
 ZDOT =     -15529
299111                 ZDOT =       -4725
422941

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19111803
25                 X    =         5825277
63
 Y    =       -2684281
11  feet           Y    =         -818168
88  meter
 Z    =      -10782970
40                 Z    =        -3286649
38
 XDOT =      -6253
521641                 XDOT =       -1906
073396
 YDOT =      17562
682092  feet/sec       YDOT =        5353
105502  meter/sec
 ZDOT =     -15499
247844                 ZDOT =       -4724
170743


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   08249
56235117  
00020000  00000-0  20000-3 0  9024
2 25544  51
6414 324
0410 0006490  82
3688 277
8211 15
71909552  1183


Satellite: ISS
Catalog Number: 25544
Epoch time:      08249
56235117   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:       324
0410  deg
Eccentricity:     
0006490     
Arg of perigee:    82
3688  deg
Mean anomaly:     277
8211  deg
Mean motion:   15
71909552  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             118
Checksum:              279


Coasting Arc #4 (Orbit 133)
---------------------------------------

Vector Time (GMT): 2008/250/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -197319
12                 A    =         6729126
14  meter
 Y    =        4981209
17  meter          E    =           
0014982
 Z    =        4509686
62                 I    =           51
41459
 XDOT =      -6585
250289                 Wp   =           73
81840
 YDOT =       2543
852913  meter/sec      RA   =          318
47007  deg
 ZDOT =      -3085
383227                 TA   =           47
06332
                                          MA   =           46
93773
                                          Ha   =            195
534  n
mi
                                          Hp   =            184
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -647372
44                 X    =         -274912
47
 Y    =       16342549
76  feet           Y    =         4978568
77  meter
 Z    =       14795559
78                 Z    =         4508539
58
 XDOT =     -21605
151867                 XDOT =       -6598
218331
 YDOT =       8345
974123  feet/sec       YDOT =        2470
140350  meter/sec
 ZDOT =     -10122
648383                 ZDOT =       -3117
406000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1113504
12                 X    =          339396
06
 Y    =      -16321042
92  feet           Y    =        -4974653
88  meter
 Z    =       14791561
09                 Z    =         4508467
82
 XDOT =      20545
722238                 XDOT =        6262
336138
 YDOT =      -7921
690697  feet/sec       YDOT =       -2414
531325  meter/sec
 ZDOT =     -10246
191819                 ZDOT =       -3123
039267


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   08250
57952383  
00020000  00000-0  20000-3 0  9039
2 25544  51
6418 318
8335 0006358  84
4613 275
7275 15
71969503  1345


Satellite: ISS
Catalog Number: 25544
Epoch time:      08250
57952383   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:       318
8335  deg
Eccentricity:     
0006358     
Arg of perigee:    84
4613  deg
Mean anomaly:     275
7275  deg
Mean motion:   15
71969503  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             134
Checksum:              306


Coasting Arc #5 (Orbit 149)
---------------------------------------

Vector Time (GMT): 2008/251/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5452249
43                 A    =         6736135
73  meter
 Y    =       -3340255
86  meter          E    =           
0020538
 Z    =        2091919
87                 I    =           51
41628
 XDOT =       1089
115934                 Wp   =           75
38244
 YDOT =       5259
889279  meter/sec      RA   =          313
37618  deg
 ZDOT =       5520
073894                 TA   =          308
05724
                                          MA   =          308
24238
                                          Ha   =            195
681  n
mi
                                          Hp   =            184
503

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17887957
43                 X    =         5479033
29
 Y    =      -10958844
70  feet           Y    =        -3279135
94  meter
 Z    =        6863254
16                 Z    =         2118471
97
 XDOT =       3573
215006                 XDOT =        1003
402483
 YDOT =      17256
854591  feet/sec       YDOT =        5271
589082  meter/sec
 ZDOT =      18110
478656                 ZDOT =        5525
156700

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17915457
66                 X    =        -5460631
49
 Y    =       10848803
83  feet           Y    =         3306715
41  meter
 Z    =        6965585
99                 Z    =         2123110
61
 XDOT =      -2572
127568                 XDOT =        -783
984483
 YDOT =     -15971
515432  feet/sec       YDOT =       -4868
117904  meter/sec
 ZDOT =      18130
584015                 ZDOT =        5526
202008


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   08251
59668935  
00020000  00000-0  20000-3 0  9040
2 25544  51
6412 313
6258 0006686  87
6020 272
5908 15
71928105  1506


Satellite: ISS
Catalog Number: 25544
Epoch time:      08251
59668935   =   yrday
fracday
Element set:     904
Inclination:       51
6412  deg
RA of node:       313
6258  deg
Eccentricity:     
0006686     
Arg of perigee:    87
6020  deg
Mean anomaly:     272
5908  deg
Mean motion:   15
71928105  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             150
Checksum:              298


Coasting Arc #6 (Orbit 164)
---------------------------------------

Vector Time (GMT): 2008/252/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1990178
07                 A    =         6726962
44  meter
 Y    =       -3996629
80  meter          E    =           
0019915
 Z    =       -5049450
56                 I    =           51
36682
 XDOT =       5625
229158                 Wp   =           98
77183
 YDOT =      -4947
857545  meter/sec      RA   =          308
20507  deg
 ZDOT =       1701
842206                 TA   =          187
68694
                                          MA   =          187
71751
                                          Ha   =            195
644  n
mi
                                          Hp   =            184
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6529455
59                 X    =        -1920809
89
 Y    =      -13112302
48  feet           Y    =        -4018497
17  meter
 Z    =      -16566438
84                 Z    =        -5058950
41
 XDOT =      18455
476239                 XDOT =        5671
871579
 YDOT =     -16233
128430  feet/sec       YDOT =       -4884
692229  meter/sec
 ZDOT =       5583
471804                 ZDOT =        1729
282766

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6578990
47                 X    =         2005276
30
 Y    =       13040457
33  feet           Y    =         3974731
39  meter
 Z    =      -16603509
25                 Z    =        -5060749
62
 XDOT =     -17291
789162                 XDOT =       -5270
537336
 YDOT =      15955
938137  feet/sec       YDOT =        4863
369944  meter/sec
 ZDOT =       5689
097371                 ZDOT =        1734
036879


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   08252
55026890  
00020000  00000-0  20000-3 0  9056
2 25544  51
6418 308
7434 0006556  90
7881 269
4032 15
71946442  1652


Satellite: ISS
Catalog Number: 25544
Epoch time:      08252
55026890   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:       308
7434  deg
Eccentricity:     
0006556     
Arg of perigee:    90
7881  deg
Mean anomaly:     269
4032  deg
Mean motion:   15
71946442  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             165
Checksum:              300


Coasting Arc #7 (Orbit 180)
---------------------------------------

Vector Time (GMT): 2008/253/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4213279
49                 A    =         6737534
41  meter
 Y    =        5178126
71  meter          E    =           
0015459
 Z    =        -880261
71                 I    =           51
38616
 XDOT =      -3271
229159                 Wp   =          122
53535
 YDOT =      -3655
582232  meter/sec      RA   =          303
08883  deg
 ZDOT =      -5930
299380                 TA   =           67
09598
                                          MA   =           66
93288
                                          Ha   =            195
595  n
mi
                                          Hp   =            184
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13823095
44                 X    =        -4266592
86
 Y    =       16988604
70  feet           Y    =         5130713
31  meter
 Z    =       -2887997
72                 Z    =         -900859
18
 XDOT =     -10732
379131                 XDOT =       -3201
300506
 YDOT =     -11993
380025  feet/sec       YDOT =       -3691
771937  meter/sec
 ZDOT =     -19456
362796                 ZDOT =       -5946
021144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13320927
71                 X    =         4060218
77
 Y    =      -17371818
68  feet           Y    =        -5294930
33  meter
 Z    =       -2967151
66                 Z    =         -904387
83
 XDOT =       9688
581091                 XDOT =        2953
079516
 YDOT =      10717
260382  feet/sec       YDOT =        3266
620965  meter/sec
 ZDOT =     -19517
457387                 ZDOT =       -5948
921012


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   08253
56741016  
00020000  00000-0  20000-3 0  9063
2 25544  51
6420 303
5354 0006697  94
3173 265
8754 15
71994381  1813


Satellite: ISS
Catalog Number: 25544
Epoch time:      08253
56741016   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:       303
5354  deg
Eccentricity:     
0006697     
Arg of perigee:    94
3173  deg
Mean anomaly:     265
8754  deg
Mean motion:   15
71994381  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             181
Checksum:              298


Coasting Arc #8 (Orbit 196)
---------------------------------------

Vector Time (GMT): 2008/254/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3569428
15                 A    =         6725779
86  meter
 Y    =        2222403
20  meter          E    =           
0009106
 Z    =        5241553
45                 I    =           51
33074
 XDOT =      -3790
891114                 Wp   =           91
84563
 YDOT =       6703
274698  meter/sec      RA   =          297
93802  deg
 ZDOT =       -260
522404                 TA   =             
63688
                                          MA   =             
63572
                                          Ha   =            195
487  n
mi
                                          Hp   =            184
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11710722
29                 X    =         3518849
24
 Y    =        7291349
09  feet           Y    =         2262035
80  meter
 Z    =       17196697
66                 Z    =         5258770
77
 XDOT =     -12437
306803                 XDOT =       -3864
300899
 YDOT =      21992
371056  feet/sec       YDOT =        6660
472314  meter/sec
 ZDOT =       -854
732298                 ZDOT =        -279
116746

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11931375
99                 X    =        -3636683
40
 Y    =       -6756236
77  feet           Y    =        -2059300
97  meter
 Z    =       17263450
71                 Z    =         5261899
78
 XDOT =      10927
397522                 XDOT =        3330
670765
 YDOT =     -21664
503174  feet/sec       YDOT =       -6603
340567  meter/sec
 ZDOT =       -926
001935                 ZDOT =        -282
245390


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   08254
58453996  
00020000  00000-0  20000-3 0  9074
2 25544  51
6409 298
3279 0006736  97
8167 262
3760 15
72015326  1972


Satellite: ISS
Catalog Number: 25544
Epoch time:      08254
58453996   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       298
3279  deg
Eccentricity:     
0006736     
Arg of perigee:    97
8167  deg
Mean anomaly:     262
3760  deg
Mean motion:   15
72015326  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             197
Checksum:              328


Coasting Arc #9 (Orbit 211)
---------------------------------------

Vector Time (GMT): 2008/255/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2289303
63                 A    =         6737731
25  meter
 Y    =       -6318419
25  meter          E    =           
0015918
 Z    =        -422161
55                 I    =           51
35900
 XDOT =       4651
658239                 Wp   =           62
90302
 YDOT =       1297
060359  meter/sec      RA   =          292
79523  deg
 ZDOT =       5992
623458                 TA   =          292
49305
                                          MA   =          292
66150
                                          Ha   =            195
568  n
mi
                                          Hp   =            184
393

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7510838
68                 X    =         2361837
83
 Y    =      -20729721
94  feet           Y    =        -6292413
38  meter
 Z    =       -1385044
44                 Z    =         -410863
89
 XDOT =      15261
345930                 XDOT =        4607
697731
 YDOT =       4255
447372  feet/sec       YDOT =        1348
832200  meter/sec
 ZDOT =      19660
838118                 ZDOT =        6015
114228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6205896
72                 X    =        -1891557
32
 Y    =       21159830
46  feet           Y    =         6449516
32  meter
 Z    =       -1341953
10                 Z    =         -409027
30
 XDOT =     -13842
244620                 XDOT =       -4219
116160
 YDOT =      -2846
084135  feet/sec       YDOT =        -867
486444  meter/sec
 ZDOT =      19747
896377                 ZDOT =        6019
158816


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   08255
53808956  
00020000  00000-0  20000-3 0  9081
2 25544  51
6414 293
4459 0006710 100
7107 259
4810 15
72023039  2125


Satellite: ISS
Catalog Number: 25544
Epoch time:      08255
53808956   =   yrday
fracday
Element set:     908
Inclination:       51
6414  deg
RA of node:       293
4459  deg
Eccentricity:     
0006710     
Arg of perigee:   100
7107  deg
Mean anomaly:     259
4810  deg
Mean motion:   15
72023039  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             212
Checksum:              278


Coasting Arc #10 (Orbit 227)
---------------------------------------

Vector Time (GMT): 2008/256/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4335999
09                 A    =         6726196
51  meter
 Y    =          -3031
77  meter          E    =           
0020609
 Z    =       -5159926
29                 I    =           51
30982
 XDOT =       1393
650285                 Wp   =           88
41146
 YDOT =      -7463
845408  meter/sec      RA   =          287
66654  deg
 ZDOT =      -1170
201382                 TA   =          170
35497
                                          MA   =          170
31534
                                          Ha   =            195
531  n
mi
                                          Hp   =            184
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14225718
79                 X    =        -4310577
14
 Y    =          -9946
74  feet           Y    =          -51377
49  meter
 Z    =      -16928892
03                 Z    =        -5180928
65
 XDOT =       4572
343456                 XDOT =        1482
693207
 YDOT =     -24487
681786  feet/sec       YDOT =       -7447
762993  meter/sec
 ZDOT =      -3839
243378                 ZDOT =       -1163
214480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14084309
66                 X    =         4292897
58
 Y    =       -1117124
50  feet           Y    =         -340499
55  meter
 Z    =      -17010079
77                 Z    =        -5184672
31
 XDOT =      -2707
604550                 XDOT =        -825
277867
 YDOT =      23749
105641  feet/sec       YDOT =        7238
727399  meter/sec
 ZDOT =      -3812
932481                 ZDOT =       -1162
181820


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   08256
55519736  
00020000  00000-0  20000-3 0  9090
2 25544  51
6413 288
2375 0006667 104
8333 255
3568 15
72022911  2280


Satellite: ISS
Catalog Number: 25544
Epoch time:      08256
55519736   =   yrday
fracday
Element set:     909
Inclination:       51
6413  deg
RA of node:       288
2375  deg
Eccentricity:     
0006667     
Arg of perigee:   104
8333  deg
Mean anomaly:     255
3568  deg
Mean motion:   15
72022911  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             228
Checksum:              302


Coasting Arc #11 (Orbit 243)
---------------------------------------

Vector Time (GMT): 2008/257/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -123990
55                 A    =         6736580
86  meter
 Y    =        6529455
98  meter          E    =           
0020808
 Z    =        1614676
05                 I    =           51
33585
 XDOT =      -4983
454148                 Wp   =          113
55624
 YDOT =       1332
334360  meter/sec      RA   =          282
49785  deg
 ZDOT =      -5720
418702                 TA   =           48
54157
                                          MA   =           48
36306
                                          Ha   =            195
495  n
mi
                                          Hp   =            184
367

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -406793
13                 X    =         -204838
52
 Y    =       21422099
68  feet           Y    =         6527617
51  meter
 Z    =        5297493
59                 Z    =         1613876
89
 XDOT =     -16349
915183                 XDOT =       -4970
193555
 YDOT =       4371
175721  feet/sec       YDOT =        1276
680259  meter/sec
 ZDOT =     -18767
777895                 ZDOT =       -5744
596049

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1640912
95                 X    =         -500150
27
 Y    =      -21363646
25  feet           Y    =        -6511639
38  meter
 Z    =        5295025
71                 Z    =         1613923
84
 XDOT =      14184
261410                 XDOT =        4323
362878
 YDOT =      -5804
899866  feet/sec       YDOT =       -1769
333479  meter/sec
 ZDOT =     -18861
112749                 ZDOT =       -5748
867166


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   08257
57229371  
00020000  00000-0  20000-3 0  9108
2 25544  51
6396 283
0289 0006791 107
3796 252
8110 15
72060473  2444


Satellite: ISS
Catalog Number: 25544
Epoch time:      08257
57229371   =   yrday
fracday
Element set:     910
Inclination:       51
6396  deg
RA of node:       283
0289  deg
Eccentricity:     
0006791     
Arg of perigee:   107
3796  deg
Mean anomaly:     252
8110  deg
Mean motion:   15
72060473  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             244
Checksum:              294


Coasting Arc #12 (Orbit 259)
---------------------------------------

Vector Time (GMT): 2008/258/12:53:42
871
Vector Time (MET): N/A
Weight (LBS)     : 661688
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4144427
36                 A    =         6727745
65  meter
 Y    =       -2315725
84  meter          E    =           
0013941
 Z    =        4758461
72                 I    =           51
30026
 XDOT =       1107
021825                 Wp   =          115
37117
 YDOT =       7193
853132  meter/sec      RA   =          277
38871  deg
 ZDOT =       2525
091700                 TA   =          309
73468
                                          MA   =          309
85745
                                          Ha   =            195
355  n
mi
                                          Hp   =            184
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13597202
64                 X    =         4146898
46
 Y    =       -7597525
71  feet           Y    =        -2269366
23  meter
 Z    =       15611751
04                 Z    =         4778601
50
 XDOT =       3631
961369                 XDOT =        1014
230312
 YDOT =      23601
880355  feet/sec       YDOT =        7205
713883  meter/sec
 ZDOT =       8284
421589                 ZDOT =        2530
243587

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12553269
96                 X    =        -3826236
68
 Y    =        9088004
49  feet           Y    =         2770023
77  meter
 Z    =       15689380
95                 Z    =         4782123
31
 XDOT =      -5589
330393                 XDOT =       -1703
627904
 YDOT =     -22123
915254  feet/sec       YDOT =       -6743
369369  meter/sec
 ZDOT =       8305
032394                 ZDOT =        2531
373874


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   08258
58937836  
00020000  00000-0  20000-3 0  9113
2 25544  51
6388 277
8202 0006714 110
8421 249
3460 15
72065476  2605


Satellite: ISS
Catalog Number: 25544
Epoch time:      08258
58937836   =   yrday
fracday
Element set:     911
Inclination:       51
6388  deg
RA of node:       277
8202  deg
Eccentricity:     
0006714     
Arg of perigee:   110
8421  deg
Mean anomaly:     249
3460  deg
Mean motion:   15
72065476  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             260
Checksum:              300

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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