Date: August 27th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3866)
---------------------------------------

Vector Time (GMT): 2008/233/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1666202
79                 A    =         6729260
65  meter
 Y    =        4031735
26  meter          E    =           
0009573
 Z    =        5115318
34                 I    =           51
85441
 XDOT =      -6091
011011                 Wp   =           65
35706
 YDOT =      -4460
347614  meter/sec      RA   =           45
39248  deg
 ZDOT =       1533
174785                 TA   =            9
99359
                                          MA   =            9
97457
                                          Ha   =            197
287  n
mi
                                          Hp   =            186
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5466544
57                 X    =        -1736011
68
 Y    =       13227477
89  feet           Y    =         4012712
62  meter
 Z    =       16782540
50                 Z    =         5107054
30
 XDOT =     -19983
631927                 XDOT =       -6048
129857
 YDOT =     -14633
686398  feet/sec       YDOT =       -4528
221010  meter/sec
 ZDOT =       5030
101002                 ZDOT =        1503
689003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8426428
13                 X    =         2568375
29
 Y    =      -11614808
24  feet           Y    =        -3540193
55  meter
 Z    =       16750954
74                 Z    =         5105691
00
 XDOT =      15310
292121                 XDOT =        4666
577039
 YDOT =      18189
012796  feet/sec       YDOT =        5544
011100  meter/sec
 ZDOT =       4915
740384                 ZDOT =        1498
317669


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   08233
60126787  
00020000  00000-0  20000-3 0  9002
2 25544  51
6390  45
6923 0008287  36
4855 323
6870 15
71047972 38677


Satellite: ISS
Catalog Number: 25544
Epoch time:      08233
60126787   =   yrday
fracday
Element set:     900
Inclination:       51
6390  deg
RA of node:        45
6923  deg
Eccentricity:     
0008287     
Arg of perigee:    36
4855  deg
Mean anomaly:     323
6870  deg
Mean motion:   15
71047972  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3867
Checksum:              311


Coasting Arc #2 (Orbit 3881)
---------------------------------------

Vector Time (GMT): 2008/234/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5794533
19                 A    =         6738385
99  meter
 Y    =        2582970
86  meter          E    =           
0014326
 Z    =       -2259609
89                 I    =           51
86533
 XDOT =       -281
543330                 Wp   =           41
42456
 YDOT =       5397
478281  meter/sec      RA   =           40
26307  deg
 ZDOT =       5478
050842                 TA   =          293
32525
                                          MA   =          293
47593
                                          Ha   =            197
309  n
mi
                                          Hp   =            186
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19010935
65                 X    =         5776196
12
 Y    =        8474313
83  feet           Y    =         2647666
12  meter
 Z    =       -7413418
28                 Z    =        -2231504
57
 XDOT =       -923
698590                 XDOT =        -368
489288
 YDOT =      17708
262076  feet/sec       YDOT =        5393
843805  meter/sec
 ZDOT =      17972
607748                 ZDOT =        5476
471868

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16838980
39                 X    =        -5132521
22
 Y    =      -12299614
61  feet           Y    =        -3748922
53  meter
 Z    =       -7304564
31                 Z    =        -2226431
20
 XDOT =       3838
804163                 XDOT =        1170
067509
 YDOT =     -15866
270498  feet/sec       YDOT =       -4836
039248  meter/sec
 ZDOT =      17966
975420                 ZDOT =        5476
334108


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   08234
55539571  
00020000  00000-0  20000-3 0  9017
2 25544  51
6406  40
8142 0008269  40
8167 319
3613 15
71065571 38829


Satellite: ISS
Catalog Number: 25544
Epoch time:      08234
55539571   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:        40
8142  deg
Eccentricity:     
0008269     
Arg of perigee:    40
8167  deg
Mean anomaly:     319
3613  deg
Mean motion:   15
71065571  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3882
Checksum:              288


Coasting Arc #3 (Orbit 3897)
---------------------------------------

Vector Time (GMT): 2008/235/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1232033
57                 A    =         6732383
65  meter
 Y    =       -5028171
91  meter          E    =           
0016721
 Z    =       -4321593
56                 I    =           51
82278
 XDOT =       6701
991449                 Wp   =           56
68065
 YDOT =       1363
353593  meter/sec      RA   =           35
20856  deg
 ZDOT =      -3497
643145                 TA   =          177
92770
                                          MA   =          177
92076
                                          Ha   =            197
279  n
mi
                                          Hp   =            185
865

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4042104
88                 X    =        -1154722
59
 Y    =      -16496627
01  feet           Y    =        -5041516
89  meter
 Z    =      -14178456
55                 Z    =        -4327391
09
 XDOT =      21988
160923                 XDOT =        6703
239077
 YDOT =       4472
944860  feet/sec       YDOT =        1438
306152  meter/sec
 ZDOT =     -11475
207169                 ZDOT =       -3465
081712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         686749
11                 X    =          209321
13
 Y    =       16951622
61  feet           Y    =         5166854
57  meter
 Z    =      -14201296
12                 Z    =        -4328555
06
 XDOT =     -19531
325197                 XDOT =       -5953
147920
 YDOT =      -8714
623623  feet/sec       YDOT =       -2656
217280  meter/sec
 ZDOT =     -11349
238861                 ZDOT =       -3459
248005


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   08235
57312074  
00020000  00000-0  20000-3 0  9028
2 25544  51
6410  35
6107 0008330  44
0774 316
1050 15
71089505 38986


Satellite: ISS
Catalog Number: 25544
Epoch time:      08235
57312074   =   yrday
fracday
Element set:     902
Inclination:       51
6410  deg
RA of node:        35
6107  deg
Eccentricity:     
0008330     
Arg of perigee:    44
0774  deg
Mean anomaly:     316
1050  deg
Mean motion:   15
71089505  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3898
Checksum:              266


Coasting Arc #4 (Orbit 3913)
---------------------------------------

Vector Time (GMT): 2008/236/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5568082
91                 A    =         6734420
59  meter
 Y    =         207636
55  meter          E    =           
0019044
 Z    =        3772985
62                 I    =           51
80465
 XDOT =      -3094
476313                 Wp   =           68
42557
 YDOT =      -5638
253104  meter/sec      RA   =           30
05699  deg
 ZDOT =      -4232
585735                 TA   =           66
05983
                                          MA   =           65
86050
                                          Ha   =            197
414  n
mi
                                          Hp   =            185
830

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18267988
54                 X    =        -5588319
42
 Y    =         681222
27  feet           Y    =          145257
73  meter
 Z    =       12378561
76                 Z    =         3745886
67
 XDOT =     -10152
481341                 XDOT =       -3010
637289
 YDOT =     -18498
205721  feet/sec       YDOT =       -5672
388370  meter/sec
 ZDOT =     -13886
436140                 ZDOT =       -4247
415334

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18169510
15                 X    =         5538066
69
 Y    =        2575660
29  feet           Y    =          785061
26  meter
 Z    =       12273839
47                 Z    =         3741066
27
 XDOT =       6827
176527                 XDOT =        2080
923406
 YDOT =      18664
229702  feet/sec       YDOT =        5688
857213  meter/sec
 ZDOT =     -13944
230992                 ZDOT =       -4250
201606


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   08236
59083479  
00020000  00000-0  20000-3 0  9036
2 25544  51
6409  30
4061 0008296  48
1779 312
0090 15
71085603 39140


Satellite: ISS
Catalog Number: 25544
Epoch time:      08236
59083479   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:        30
4061  deg
Eccentricity:     
0008296     
Arg of perigee:    48
1779  deg
Mean anomaly:     312
0090  deg
Mean motion:   15
71085603  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3914
Checksum:              288


Coasting Arc #5 (Orbit 3929)
---------------------------------------

Vector Time (GMT): 2008/237/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4070978
41                 A    =         6736450
18  meter
 Y    =        4464515
54  meter          E    =           
0020745
 Z    =        2953634
26                 I    =           51
78773
 XDOT =      -5579
432661                 Wp   =           70
64853
 YDOT =       1754
899930  meter/sec      RA   =           25
00463  deg
 ZDOT =       5015
816824                 TA   =          323
33524
                                          MA   =          323
47702
                                          Ha   =            197
212  n
mi
                                          Hp   =            185
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13356228
38                 X    =         4006404
72
 Y    =       14647360
69  feet           Y    =         4509678
32  meter
 Z    =        9690401
12                 Z    =         2973254
49
 XDOT =     -18305
225266                 XDOT =       -5623
007458
 YDOT =       5757
545702  feet/sec       YDOT =        1692
263544  meter/sec
 ZDOT =      16456
091943                 ZDOT =        4988
606240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10784659
06                 X    =        -3287164
08
 Y    =      -16587414
75  feet           Y    =        -5055844
02  meter
 Z    =        9766610
79                 Z    =         2976862
97
 XDOT =      17873
851643                 XDOT =        5447
949981
 YDOT =      -1952
029848  feet/sec       YDOT =        -594
978698  meter/sec
 ZDOT =      16351
064028                 ZDOT =        4983
804316


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   08237
60853460  
00020000  00000-0  20000-3 0  9045
2 25544  51
6422  25
2026 0008245  51
6205 308
5696 15
71154411 39309


Satellite: ISS
Catalog Number: 25544
Epoch time:      08237
60853460   =   yrday
fracday
Element set:     904
Inclination:       51
6422  deg
RA of node:        25
2026  deg
Eccentricity:     
0008245     
Arg of perigee:    51
6205  deg
Mean anomaly:     308
5696  deg
Mean motion:   15
71154411  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3930
Checksum:              266


Coasting Arc #6 (Orbit 3944)
---------------------------------------

Vector Time (GMT): 2008/238/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3860784
02                 A    =         6730275
20  meter
 Y    =       -2664712
32  meter          E    =           
0018105
 Z    =       -4840955
49                 I    =           51
73968
 XDOT =       5952
008569                 Wp   =           85
64440
 YDOT =       4199
322677  meter/sec      RA   =           19
85767  deg
 ZDOT =       2444
523784                 TA   =          208
20907
                                          MA   =          208
30726
                                          Ha   =            197
353  n
mi
                                          Hp   =            185
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12666614
23                 X    =         3913810
65
 Y    =       -8742494
47  feet           Y    =        -2621241
97  meter
 Z    =      -15882399
91                 Z    =        -4822071
32
 XDOT =      19527
587168                 XDOT =        5892
733728
 YDOT =      13777
305370  feet/sec       YDOT =        4265
549863  meter/sec
 ZDOT =       8020
091155                 ZDOT =        2473
294777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13876739
81                 X    =        -4229630
29
 Y    =        6827645
69  feet           Y    =         2081066
41  meter
 Z    =      -15809626
79                 Z    =        -4818774
25
 XDOT =     -16812
215536                 XDOT =       -5124
363295
 YDOT =     -15410
623064  feet/sec       YDOT =       -4697
157910  meter/sec
 ZDOT =       8131
650785                 ZDOT =        2478
527159


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   08238
56262010  
00020000  00000-0  20000-3 0  9057
2 25544  51
6422  20
3249 0008356  54
5137 305
6803 15
71147166 39454


Satellite: ISS
Catalog Number: 25544
Epoch time:      08238
56262010   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:        20
3249  deg
Eccentricity:     
0008356     
Arg of perigee:    54
5137  deg
Mean anomaly:     305
6803  deg
Mean motion:   15
71147166  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3945
Checksum:              273


Coasting Arc #7 (Orbit 3960)
---------------------------------------

Vector Time (GMT): 2008/239/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6062946
43                 A    =         6739482
17  meter
 Y    =       -2648346
58  meter          E    =           
0012780
 Z    =       -1285742
76                 I    =           51
74339
 XDOT =       2975
986406                 Wp   =          101
23509
 YDOT =      -3993
263799  meter/sec      RA   =           14
78152  deg
 ZDOT =      -5859
538979                 TA   =           92
82492
                                          MA   =           92
67865
                                          Ha   =            197
343  n
mi
                                          Hp   =            185
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19891556
53                 X    =        -6026635
76
 Y    =       -8688801
12  feet           Y    =        -2715942
83  meter
 Z    =       -4218316
13                 Z    =        -1315108
16
 XDOT =       9763
734928                 XDOT =        3048
882766
 YDOT =     -13101
259182  feet/sec       YDOT =       -3959
576646  meter/sec
 ZDOT =     -19224
209250                 ZDOT =       -5844
905009

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18613863
71                 X    =         5673505
66
 Y    =       11122989
71  feet           Y    =         3390287
26  meter
 Z    =       -4332049
71                 Z    =        -1320408
75
 XDOT =     -10634
671457                 XDOT =       -3241
447860
 YDOT =      10395
393761  feet/sec       YDOT =        3168
516018  meter/sec
 ZDOT =     -19167
972438                 ZDOT =       -5842
397999


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   08239
58029807  
00020000  00000-0  20000-3 0  9066
2 25544  51
6425  15
1198 0008417  57
9120 302
2858 15
71169786 39612


Satellite: ISS
Catalog Number: 25544
Epoch time:      08239
58029807   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:        15
1198  deg
Eccentricity:     
0008417     
Arg of perigee:    57
9120  deg
Mean anomaly:     302
2858  deg
Mean motion:   15
71169786  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3961
Checksum:              310


Coasting Arc #8 (Orbit 3976)
---------------------------------------

Vector Time (GMT): 2008/240/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1156143
66                 A    =         6728138
95  meter
 Y    =        4021122
54  meter          E    =           
0011076
 Z    =        5260836
19                 I    =           51
67771
 XDOT =      -7522
186683                 Wp   =           62
33138
 YDOT =      -1612
546003  meter/sec      RA   =            9
65675  deg
 ZDOT =       -414
843890                 TA   =           31
63742
                                          MA   =           31
57090
                                          Ha   =            197
386  n
mi
                                          Hp   =            185
290

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3793122
24                 X    =        -1226578
32
 Y    =       13192659
25  feet           Y    =         4007799
83  meter
 Z    =       17259961
24                 Z    =         5255048
82
 XDOT =     -24679
090168                 XDOT =       -7501
580670
 YDOT =      -5290
505258  feet/sec       YDOT =       -1696
548193  meter/sec
 ZDOT =      -1361
036386                 ZDOT =        -451
336068

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5305715
58                 X    =         1617182
11
 Y    =      -12690296
21  feet           Y    =        -3868002
28  meter
 Z    =       17237925
07                 Z    =         5254119
56
 XDOT =      23022
435667                 XDOT =        7017
238391
 YDOT =       7559
435694  feet/sec       YDOT =        2304
116000  meter/sec
 ZDOT =      -1502
238820                 ZDOT =        -457
882392


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   08240
59796333  
00020000  00000-0  20000-3 0  9075
2 25544  51
6433   9
9158 0008425  60
6944 299
5058 15
71205013 39773


Satellite: ISS
Catalog Number: 25544
Epoch time:      08240
59796333   =   yrday
fracday
Element set:     907
Inclination:       51
6433  deg
RA of node:         9
9158  deg
Eccentricity:     
0008425     
Arg of perigee:    60
6944  deg
Mean anomaly:     299
5058  deg
Mean motion:   15
71205013  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3977
Checksum:              310


Coasting Arc #9 (Orbit 3991)
---------------------------------------

Vector Time (GMT): 2008/241/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6708206
87                 A    =         6740088
89  meter
 Y    =          80433
28  meter          E    =           
0019218
 Z    =        -571288
06                 I    =           51
68910
 XDOT =        441
597139                 Wp   =           50
54380
 YDOT =       4795
300535  meter/sec      RA   =            4
54467  deg
 ZDOT =       6006
157723                 TA   =          303
24836
                                          MA   =          303
43239
                                          Ha   =            197
468  n
mi
                                          Hp   =            185
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22008552
71                 X    =         6709584
04
 Y    =         263888
71  feet           Y    =          155456
02  meter
 Z    =       -1874304
64                 Z    =         -538696
87
 XDOT =       1448
809511                 XDOT =         358
766232
 YDOT =      15732
613305  feet/sec       YDOT =        4799
775522  meter/sec
 ZDOT =      19705
241873                 ZDOT =        6008
101828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21901694
59                 X    =        -6675636
51
 Y    =       -2284346
93  feet           Y    =         -696268
94  meter
 Z    =       -1748307
97                 Z    =         -532884
27
 XDOT =        -52
504582                 XDOT =         -16
003397
 YDOT =     -14191
790219  feet/sec       YDOT =       -4325
657659  meter/sec
 ZDOT =      19713
162156                 ZDOT =        6008
571825


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   08241
55201468  
00020000  00000-0  20000-3 0  9083
2 25544  51
6438   5
0374 0008533  63
8711 296
3327 15
71180086 39925


Satellite: ISS
Catalog Number: 25544
Epoch time:      08241
55201468   =   yrday
fracday
Element set:     908
Inclination:       51
6438  deg
RA of node:         5
0374  deg
Eccentricity:     
0008533     
Arg of perigee:    63
8711  deg
Mean anomaly:     296
3327  deg
Mean motion:   15
71180086  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3992
Checksum:              290


Coasting Arc #10 (Orbit 4007)
---------------------------------------

Vector Time (GMT): 2008/242/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1882357
79                 A    =         6728958
28  meter
 Y    =       -4009372
17  meter          E    =           
0021992
 Z    =       -5085263
90                 I    =           51
62284
 XDOT =       7374
221080                 Wp   =           73
49512
 YDOT =      -1374
215195  meter/sec      RA   =          359
45080  deg
 ZDOT =      -1645
915103                 TA   =          180
63733
                                          MA   =          180
64014
                                          Ha   =            197
389  n
mi
                                          Hp   =            185
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6175714
55                 X    =        -1812681
61
 Y    =      -13154108
17  feet           Y    =        -4030032
29  meter
 Z    =      -16683936
68                 Z    =        -5094238
92
 XDOT =      24193
638715                 XDOT =        7397
035120
 YDOT =      -4508
580035  feet/sec       YDOT =       -1291
624875  meter/sec
 ZDOT =      -5399
983935                 ZDOT =       -1610
036364

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5080941
08                 X    =         1548670
84
 Y    =       13571429
05  feet           Y    =         4136571
57  meter
 Z    =      -16718974
44                 Z    =        -5095943
41
 XDOT =     -23503
533227                 XDOT =       -7163
876928
 YDOT =       2316
714927  feet/sec       YDOT =         706
134710  meter/sec
 ZDOT =      -5261
403345                 ZDOT =       -1603
675740


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   08242
56965681  
00020000  00000-0  20000-3 0  9090
2 25544  51
6440 359
8336 0008397  67
5941 292
6109 15
71199298 40081


Satellite: ISS
Catalog Number: 25544
Epoch time:      08242
56965681   =   yrday
fracday
Element set:     909
Inclination:       51
6440  deg
RA of node:       359
8336  deg
Eccentricity:     
0008397     
Arg of perigee:    67
5941  deg
Mean anomaly:     292
6109  deg
Mean motion:   15
71199298  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4008
Checksum:              333


Coasting Arc #11 (Orbit 4023)
---------------------------------------

Vector Time (GMT): 2008/243/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5868397
73                 A    =         6737943
76  meter
 Y    =        2391137
66  meter          E    =           
0021511
 Z    =        2268836
28                 I    =           51
62358
 XDOT =      -3735
313209                 Wp   =           94
09829
 YDOT =      -3960
544490  meter/sec      RA   =          354
30255  deg
 ZDOT =      -5444
745516                 TA   =           60
43527
                                          MA   =           60
22104
                                          Ha   =            197
490  n
mi
                                          Hp   =            185
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19253273
38                 X    =        -5905721
09
 Y    =        7844939
84  feet           Y    =         2325305
27  meter
 Z    =        7443688
59                 Z    =         2240237
28
 XDOT =     -12254
964595                 XDOT =       -3664
298957
 YDOT =     -12993
912368  feet/sec       YDOT =       -4001
918076  meter/sec
 ZDOT =     -17863
338308                 ZDOT =       -5462
718739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19714755
10                 X    =         6009057
35
 Y    =       -6722398
79  feet           Y    =        -2048987
15  meter
 Z    =        7333341
86                 Z    =         2235202
60
 XDOT =      10894
991953                 XDOT =        3320
793547
 YDOT =      12233
657004  feet/sec       YDOT =        3728
818655  meter/sec
 ZDOT =     -17933
158482                 ZDOT =       -5466
026705


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   08243
58728741  
00020000  00000-0  20000-3 0  9109
2 25544  51
6437 354
6297 0008587  71
7867 288
4229 15
71219642 40241


Satellite: ISS
Catalog Number: 25544
Epoch time:      08243
58728741   =   yrday
fracday
Element set:     910
Inclination:       51
6437  deg
RA of node:       354
6297  deg
Eccentricity:     
0008587     
Arg of perigee:    71
7867  deg
Mean anomaly:     288
4229  deg
Mean motion:   15
71219642  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4024
Checksum:              322


Coasting Arc #12 (Orbit 4039)
---------------------------------------

Vector Time (GMT): 2008/244/13:13:25
434
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4468949
17                 A    =         6731852
01  meter
 Y    =        2613114
52  meter          E    =           
0017397
 Z    =        4288758
96                 I    =           51
57544
 XDOT =      -5650
219187                 Wp   =           92
38349
 YDOT =       3899
937058  meter/sec      RA   =          349
22943  deg
 ZDOT =       3498
523242                 TA   =          322
13684
                                          MA   =          322
25907
                                          Ha   =            197
267  n
mi
                                          Hp   =            184
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14661906
74                 X    =         4418562
96
 Y    =        8573210
36  feet           Y    =         2662807
40  meter
 Z    =       14070731
50                 Z    =         4310346
36
 XDOT =     -18537
464523                 XDOT =       -5710
403996
 YDOT =      12795
069088  feet/sec       YDOT =        3836
416736  meter/sec
 ZDOT =      11478
094626                 ZDOT =        3470
928352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14223568
32                 X    =        -4335343
62
 Y    =       -9154226
44  feet           Y    =        -2790208
22  meter
 Z    =       14154404
70                 Z    =         4314262
55
 XDOT =      18436
131094                 XDOT =        5619
332758
 YDOT =     -10997
369080  feet/sec       YDOT =       -3351
998096  meter/sec
 ZDOT =      11371
767114                 ZDOT =        3466
114616


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   08244
60490338  
00020000  00000-0  20000-3 0  9112
2 25544  51
6441 349
4253 0008513  74
8354 285
3749 15
71276829 40405


Satellite: ISS
Catalog Number: 25544
Epoch time:      08244
60490338   =   yrday
fracday
Element set:     911
Inclination:       51
6441  deg
RA of node:       349
4253  deg
Eccentricity:     
0008513     
Arg of perigee:    74
8354  deg
Mean anomaly:     285
3749  deg
Mean motion:   15
71276829  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4040
Checksum:              299

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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