Date: October 17th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 746)
---------------------------------------

Vector Time (GMT): 2008/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2487283
55                 A    =         6726200
40  meter
 Y    =       -3690762
80  meter          E    =           
0001546
 Z    =        5042117
43                 I    =           51
91006
 XDOT =       4783
793554                 Wp   =           66
46474
 YDOT =      -5743
821516  meter/sec      RA   =          118
64376  deg
 ZDOT =      -1843
502356                 TA   =           41
25329
                                          MA   =           41
24162
                                          Ha   =            192
163  n
mi
                                          Hp   =            187
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8160379
11                 X    =        -2470322
49
 Y    =      -12108801
83  feet           Y    =        -3718481
97  meter
 Z    =       16542380
02                 Z    =         5030075
18
 XDOT =      15694
860742                 XDOT =        4856
622046
 YDOT =     -18844
558778  feet/sec       YDOT =       -5689
919252  meter/sec
 ZDOT =      -6048
236076                 ZDOT =       -1820
084755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12417171
09                 X    =         3784753
75
 Y    =        7783418
36  feet           Y    =         2372385
92  meter
 Z    =       16495377
12                 Z    =         5027790
95
 XDOT =      -6287
190253                 XDOT =       -1916
335589
 YDOT =      22664
434577  feet/sec       YDOT =        6908
119659  meter/sec
 ZDOT =      -5958
085348                 ZDOT =       -1816
024414


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   08289
54459184  
00020000  00000-0  20000-3 0  9006
2 25544  51
6386 119
3079 0003956 230
8121 129
2690 15
72243818  7479


Satellite: ISS
Catalog Number: 25544
Epoch time:      08289
54459184   =   yrday
fracday
Element set:     900
Inclination:       51
6386  deg
RA of node:       119
3079  deg
Eccentricity:     
0003956     
Arg of perigee:   230
8121  deg
Mean anomaly:     129
2690  deg
Mean motion:   15
72243818  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             747
Checksum:              307


Coasting Arc #2 (Orbit 762)
---------------------------------------

Vector Time (GMT): 2008/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3400003
32                 A    =         6736641
25  meter
 Y    =        5712025
18  meter          E    =           
0009840
 Z    =        1064286
86                 I    =           51
95749
 XDOT =      -3638
908563                 Wp   =           57
30247
 YDOT =      -3278
766412  meter/sec      RA   =          113
56567  deg
 ZDOT =       5937
885908                 TA   =          314
27776
                                          MA   =          314
35845
                                          Ha   =            191
943  n
mi
                                          Hp   =            187
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11154866
54                 X    =        -3468793
70
 Y    =       18740240
11  feet           Y    =         5673619
77  meter
 Z    =        3491754
81                 Z    =         1047601
92
 XDOT =     -11938
676388                 XDOT =       -3630
820560
 YDOT =     -10757
107652  feet/sec       YDOT =       -3319
413488  meter/sec
 ZDOT =      19481
252980                 ZDOT =        5920
227186

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2351293
33                 X    =          716674
21
 Y    =      -21691992
56  feet           Y    =        -6611719
33  meter
 Z    =        3427663
50                 Z    =         1044751
84
 XDOT =      13854
323755                 XDOT =        4222
797880
 YDOT =       4587
310506  feet/sec       YDOT =        1398
212242  meter/sec
 ZDOT =      19412
537598                 ZDOT =        5916
941460


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   08290
56154606  
00020000  00000-0  20000-3 0  9012
2 25544  51
6378 114
0972 0003917 234
3586 125
7212 15
72268947  7634


Satellite: ISS
Catalog Number: 25544
Epoch time:      08290
56154606   =   yrday
fracday
Element set:     901
Inclination:       51
6378  deg
RA of node:       114
0972  deg
Eccentricity:     
0003917     
Arg of perigee:   234
3586  deg
Mean anomaly:     125
7212  deg
Mean motion:   15
72268947  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             763
Checksum:              298


Coasting Arc #3 (Orbit 777)
---------------------------------------

Vector Time (GMT): 2008/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3708929
71                 A    =         6725092
00  meter
 Y    =        1937857
28  meter          E    =           
0012089
 Z    =       -5274756
11                 I    =           51
92941
 XDOT =      -2864
578494                 Wp   =          105
97472
 YDOT =       7111
161076  meter/sec      RA   =          108
44891  deg
 ZDOT =        596
175310                 TA   =          169
68946
                                          MA   =          169
66464
                                          Ha   =            191
865  n
mi
                                          Hp   =            187
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12168404
55                 X    =         3712609
23
 Y    =        6357799
48  feet           Y    =         1979353
33  meter
 Z    =      -17305630
29                 Z    =        -5256728
60
 XDOT =      -9398
223407                 XDOT =       -2946
779947
 YDOT =      23330
580957  feet/sec       YDOT =        7078
668083  meter/sec
 ZDOT =       1955
955742                 ZDOT =         582
059198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13810288
78                 X    =        -4209376
02
 Y    =        -431429
62  feet           Y    =         -131499
75  meter
 Z    =      -17235611
84                 Z    =        -5253414
49
 XDOT =      -1629
563898                 XDOT =        -496
691076
 YDOT =     -24098
656463  feet/sec       YDOT =       -7345
270490  meter/sec
 ZDOT =       1901
928314                 ZDOT =         579
707750


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   08291
51493082  
00020000  00000-0  20000-3 0  9023
2 25544  51
6378 109
2128 0003836 236
2283 123
8514 15
72290661  7786


Satellite: ISS
Catalog Number: 25544
Epoch time:      08291
51493082   =   yrday
fracday
Element set:     902
Inclination:       51
6378  deg
RA of node:       109
2128  deg
Eccentricity:     
0003836     
Arg of perigee:   236
2283  deg
Mean anomaly:     123
8514  deg
Mean motion:   15
72290661  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             778
Checksum:              291


Coasting Arc #4 (Orbit 793)
---------------------------------------

Vector Time (GMT): 2008/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1537257
61                 A    =         6736870
44  meter
 Y    =       -6551996
73  meter          E    =           
0011553
 Z    =          22389
89                 I    =           51
97843
 XDOT =       4622
999465                 Wp   =          152
38021
 YDOT =       1059
742138  meter/sec      RA   =          103
35319  deg
 ZDOT =      -6065
757465                 TA   =           27
37782
                                          MA   =           27
31699
                                          Ha   =            191
597  n
mi
                                          Hp   =            187
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5043496
08                 X    =         1610300
07
 Y    =      -21496052
26  feet           Y    =        -6534397
83  meter
 Z    =          73457
64                 Z    =           30035
27
 XDOT =      15167
321078                 XDOT =        4640
272787
 YDOT =       3476
844285  feet/sec       YDOT =        1111
535988  meter/sec
 ZDOT =     -19900
779084                 ZDOT =       -6043
256347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5112914
82                 X    =         1558416
44
 Y    =       21479527
71  feet           Y    =         6546960
05  meter
 Z    =         102484
09                 Z    =           31237
15
 XDOT =     -13654
669181                 XDOT =       -4161
943166
 YDOT =       3358
628916  feet/sec       YDOT =        1023
710094  meter/sec
 ZDOT =     -19813
504501                 ZDOT =       -6039
156172


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   08292
53186222  
00020000  00000-0  20000-3 0  9032
2 25544  51
6385 104
0034 0003785 244
8411 115
2359 15
72353418  7944


Satellite: ISS
Catalog Number: 25544
Epoch time:      08292
53186222   =   yrday
fracday
Element set:     903
Inclination:       51
6385  deg
RA of node:       104
0034  deg
Eccentricity:     
0003785     
Arg of perigee:   244
8411  deg
Mean anomaly:     115
2359  deg
Mean motion:   15
72353418  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             794
Checksum:              278


Coasting Arc #5 (Orbit 809)
---------------------------------------

Vector Time (GMT): 2008/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4183553
79                 A    =         6725148
28  meter
 Y    =         128996
22  meter          E    =           
0002985
 Z    =        5264767
75                 I    =           51
94358
 XDOT =        591
852484                 Wp   =          193
09412
 YDOT =      -7647
174907  meter/sec      RA   =           98
25839  deg
 ZDOT =        654
904114                 TA   =          250
68711
                                          MA   =          250
71939
                                          Ha   =            191
833  n
mi
                                          Hp   =            187
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13725570
18                 X    =        -4210261
12
 Y    =         423215
94  feet           Y    =           82063
76  meter
 Z    =       17272860
07                 Z    =         5244378
76
 XDOT =       1941
773240                 XDOT =         674
138973
 YDOT =     -25089
156518  feet/sec       YDOT =       -7640
096410  meter/sec
 ZDOT =       2148
635543                 ZDOT =         657
978950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12057733
55                 X    =         3675197
19
 Y    =       -6775251
56  feet           Y    =        -2065096
67  meter
 Z    =       17193868
43                 Z    =         5240691
10
 XDOT =       9410
824868                 XDOT =        2868
419420
 YDOT =      22252
557180  feet/sec       YDOT =        6782
579428  meter/sec
 ZDOT =       2159
866425                 ZDOT =         658
327286


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   08293
54878688  
00020000  00000-0  20000-3 0  9049
2 25544  51
6383  98
7934 0003694 244
7284 115
3495 15
72281035  8102


Satellite: ISS
Catalog Number: 25544
Epoch time:      08293
54878688   =   yrday
fracday
Element set:     904
Inclination:       51
6383  deg
RA of node:        98
7934  deg
Eccentricity:     
0003694     
Arg of perigee:   244
7284  deg
Mean anomaly:     115
3495  deg
Mean motion:   15
72281035  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             810
Checksum:              323


Coasting Arc #6 (Orbit 824)
---------------------------------------

Vector Time (GMT): 2008/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         504711
33                 A    =         6736363
66  meter
 Y    =        6621542
77  meter          E    =           
0006495
 Z    =       -1109024
06                 I    =           51
98604
 XDOT =      -4716
581704                 Wp   =           21
53031
 YDOT =       1349
929606  meter/sec      RA   =           93
14213  deg
 ZDOT =       5930
186025                 TA   =          326
40157
                                          MA   =          326
44274
                                          Ha   =            191
547  n
mi
                                          Hp   =            187
603

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1655877
05                 X    =          436018
17
 Y    =       21724221
70  feet           Y    =         6626802
70  meter
 Z    =       -3638530
38                 Z    =        -1106738
78
 XDOT =     -15474
349424                 XDOT =       -4760
134491
 YDOT =       4428
902906  feet/sec       YDOT =        1296
942357  meter/sec
 ZDOT =      19455
990896                 ZDOT =        5907
166780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11859660
10                 X    =        -3614824
40
 Y    =      -18278424
87  feet           Y    =        -5571263
90  meter
 Z    =       -3629088
99                 Z    =        -1106146
33
 XDOT =      10238
183057                 XDOT =        3120
598196
 YDOT =     -10477
119088  feet/sec       YDOT =       -3193
425898  meter/sec
 ZDOT =      19366
906850                 ZDOT =        5903
033208


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   08294
50213931  
00020000  00000-0  20000-3 0  9051
2 25544  51
6394  93
9094 0003771 246
9246 113
1519 15
72342061  8252


Satellite: ISS
Catalog Number: 25544
Epoch time:      08294
50213931   =   yrday
fracday
Element set:     905
Inclination:       51
6394  deg
RA of node:        93
9094  deg
Eccentricity:     
0003771     
Arg of perigee:   246
9246  deg
Mean anomaly:     113
1519  deg
Mean motion:   15
72342061  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             825
Checksum:              285


Coasting Arc #7 (Orbit 840)
---------------------------------------

Vector Time (GMT): 2008/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3880200
21                 A    =         6725854
57  meter
 Y    =       -2185119
93  meter          E    =           
0009656
 Z    =       -5049097
83                 I    =           51
95177
 XDOT =       1692
007189                 Wp   =           77
95079
 YDOT =       7271
432552  meter/sec      RA   =           88
06872  deg
 ZDOT =      -1847
577986                 TA   =          174
29323
                                          MA   =          174
28222
                                          Ha   =            191
463  n
mi
                                          Hp   =            187
643

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12730315
64                 X    =         3928874
07
 Y    =       -7169028
66  feet           Y    =        -2141457
08  meter
 Z    =      -16565281
60                 Z    =        -5030129
40
 XDOT =       5551
204687                 XDOT =        1619
546400
 YDOT =      23856
406009  feet/sec       YDOT =        7289
948427  meter/sec
 ZDOT =      -6061
607567                 ZDOT =       -1839
534038

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7621419
35                 X    =        -2323008
62
 Y    =       12561592
84  feet           Y    =         3828773
50  meter
 Z    =      -16491962
14                 Z    =        -5026750
06
 XDOT =     -15708
544934                 XDOT =       -4787
964496
 YDOT =     -17442
930455  feet/sec       YDOT =       -5316
605203  meter/sec
 ZDOT =      -6029
794813                 ZDOT =       -1837
881459


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   08295
51903886  
00020000  00000-0  20000-3 0  9069
2 25544  51
6399  88
7008 0003633 251
6498 108
4269 15
72375310  8413


Satellite: ISS
Catalog Number: 25544
Epoch time:      08295
51903886   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:        88
7008  deg
Eccentricity:     
0003633     
Arg of perigee:   251
6498  deg
Mean anomaly:     108
4269  deg
Mean motion:   15
72375310  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             841
Checksum:              314


Coasting Arc #8 (Orbit 856)
---------------------------------------

Vector Time (GMT): 2008/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2394326
73                 A    =         6734922
71  meter
 Y    =       -5924961
05  meter          E    =           
0011145
 Z    =        2106816
57                 I    =           51
97920
 XDOT =       3940
871219                 Wp   =          121
30537
 YDOT =      -3576
918177  meter/sec      RA   =           82
93363  deg
 ZDOT =      -5564
816673                 TA   =           35
27587
                                          MA   =           35
20216
                                          Ha   =            191
382  n
mi
                                          Hp   =            187
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7855402
66                 X    =        -2338129
54
 Y    =      -19438848
59  feet           Y    =        -5951421
56  meter
 Z    =        6912127
87                 Z    =         2095321
39
 XDOT =      12929
367518                 XDOT =        4007
609157
 YDOT =     -11735
295855  feet/sec       YDOT =       -3532
475992  meter/sec
 ZDOT =     -18257
272549                 ZDOT =       -5545
509573

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16676136
91                 X    =         5082886
53
 Y    =       12731993
68  feet           Y    =         3880711
67  meter
 Z    =        6867058
43                 Z    =         2093079
41
 XDOT =      -4335
654123                 XDOT =       -1321
507377
 YDOT =      15513
883622  feet/sec       YDOT =        4728
631728  meter/sec
 ZDOT =     -18182
757407                 ZDOT =       -5542
104458


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   08296
53592635  
00020000  00000-0  20000-3 0  9079
2 25544  51
6391  83
4899 0003785 256
1110 103
9632 15
72369990  8572


Satellite: ISS
Catalog Number: 25544
Epoch time:      08296
53592635   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:        83
4899  deg
Eccentricity:     
0003785     
Arg of perigee:   256
1110  deg
Mean anomaly:     103
9632  deg
Mean motion:   15
72369990  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             857
Checksum:              323


Coasting Arc #9 (Orbit 872)
---------------------------------------

Vector Time (GMT): 2008/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2851531
12                 A    =         6727446
74  meter
 Y    =        3964357
07  meter          E    =           
0005640
 Z    =        4626059
64                 I    =           51
95070
 XDOT =      -3670
340991                 Wp   =          138
71558
 YDOT =      -6090
010784  meter/sec      RA   =           77
87368  deg
 ZDOT =       2950
315571                 TA   =          282
13100
                                          MA   =          282
19418
                                          Ha   =            191
270  n
mi
                                          Hp   =            187
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9355417
07                 X    =        -2918122
10
 Y    =       13006420
83  feet           Y    =         3932097
43  meter
 Z    =       15177361
04                 Z    =         4612044
86
 XDOT =     -12041
801151                 XDOT =       -3616
300984
 YDOT =     -19980
350342  feet/sec       YDOT =       -6130
752404  meter/sec
 ZDOT =       9679
513027                 ZDOT =        2932
616316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1249356
04                 X    =          380803
72
 Y    =      -16023899
31  feet           Y    =        -4884084
51  meter
 Z    =       15123387
84                 Z    =         4609608
61
 XDOT =      19589
477269                 XDOT =        5970
872672
 YDOT =      10616
836731  feet/sec       YDOT =        3236
011836  meter/sec
 ZDOT =       9610
385157                 ZDOT =        2929
245396


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   08297
55280131  
00020000  00000-0  20000-3 0  9088
2 25544  51
6401  78
2800 0003829 260
2749  99
7981 15
72422614  8731


Satellite: ISS
Catalog Number: 25544
Epoch time:      08297
55280131   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:        78
2800  deg
Eccentricity:     
0003829     
Arg of perigee:   260
2749  deg
Mean anomaly:      99
7981  deg
Mean motion:   15
72422614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             873
Checksum:              301


Coasting Arc #10 (Orbit 887)
---------------------------------------

Vector Time (GMT): 2008/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3898841
08                 A    =         6732807
45  meter
 Y    =        4583490
81  meter          E    =           
0001347
 Z    =       -3019157
76                 I    =           51
96211
 XDOT =      -2421
552672                 Wp   =           25
68246
 YDOT =       5340
518335  meter/sec      RA   =           72
72687  deg
 ZDOT =       4982
525959                 TA   =          299
60974
                                          MA   =          299
62315
                                          Ha   =            191
242  n
mi
                                          Hp   =            187
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12791473
38                 X    =         3861964
73
 Y    =       15037699
51  feet           Y    =         4626883
57  meter
 Z    =       -9905373
24                 Z    =        -3000306
70
 XDOT =      -7944
726614                 XDOT =       -2505
295827
 YDOT =      17521
385614  feet/sec       YDOT =        5312
971148  meter/sec
 ZDOT =      16346
869943                 ZDOT =        4970
558194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18916275
27                 X    =        -5765680
70
 Y    =       -5777421
17  feet           Y    =        -1760957
97  meter
 Z    =       -9831914
94                 Z    =        -2996767
67
 XDOT =      -3058
047384                 XDOT =        -932
092843
 YDOT =     -17716
793562  feet/sec       YDOT =       -5400
078678  meter/sec
 ZDOT =      16300
946514                 ZDOT =        4968
528497


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   08298
50611238  
00020000  00000-0  20000-3 0  9091
2 25544  51
6411  73
3962 0003688 264
9804  95
0938 15
72409421  8881


Satellite: ISS
Catalog Number: 25544
Epoch time:      08298
50611238   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:        73
3962  deg
Eccentricity:     
0003688     
Arg of perigee:   264
9804  deg
Mean anomaly:      95
0938  deg
Mean motion:   15
72409421  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             888
Checksum:              314


Coasting Arc #11 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2008/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1285860
70                 A    =         6729565
96  meter
 Y    =       -5220192
09  meter          E    =           
0003960
 Z    =       -4052038
34                 I    =           51
94173
 XDOT =       5062
367736                 Wp   =           53
64253
 YDOT =       4278
288625  meter/sec      RA   =           67
67471  deg
 ZDOT =      -3905
526786                 TA   =          176
21229
                                          MA   =          176
20929
                                          Ha   =            191
169  n
mi
                                          Hp   =            187
595

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4218703
07                 X    =         1363822
64
 Y    =      -17126614
47  feet           Y    =        -5205377
17  meter
 Z    =      -13294089
05                 Z    =        -4045601
84
 XDOT =      16608
818030                 XDOT =        5033
123702
 YDOT =      14036
380002  feet/sec       YDOT =        4334
735220  meter/sec
 ZDOT =     -12813
408090                 ZDOT =       -3881
004572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5868927
95                 X    =         1788849
24
 Y    =       16653074
39  feet           Y    =         5075857
07  meter
 Z    =      -13269588
56                 Z    =        -4044570
59
 XDOT =     -20443
346821                 XDOT =       -6231
132111
 YDOT =      -2928
439487  feet/sec       YDOT =        -892
588356  meter/sec
 ZDOT =     -12718
001038                 ZDOT =       -3876
446717


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   08299
52296473  
00020000  00000-0  20000-3 0  9106
2 25544  51
6413  68
1864 0003749 269
6948  90
3785 15
72426036  9043


Satellite: ISS
Catalog Number: 25544
Epoch time:      08299
52296473   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:        68
1864  deg
Eccentricity:     
0003749     
Arg of perigee:   269
6948  deg
Mean anomaly:      90
3785  deg
Mean motion:   15
72426036  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             904
Checksum:              321


Coasting Arc #12 (Orbit 919)
---------------------------------------

Vector Time (GMT): 2008/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 642288
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4800893
18                 A    =         6730539
29  meter
 Y    =       -2813701
87  meter          E    =           
0008065
 Z    =        3780720
78                 I    =           51
93310
 XDOT =        409
953312                 Wp   =           78
38485
 YDOT =      -6411
884982  meter/sec      RA   =           62
52088  deg
 ZDOT =      -4242
140415                 TA   =           56
06907
                                          MA   =           55
99242
                                          Ha   =            191
291  n
mi
                                          Hp   =            187
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15750961
89                 X    =        -4787439
62
 Y    =       -9231305
36  feet           Y    =        -2867312
82  meter
 Z    =       12403939
58                 Z    =         3757430
27
 XDOT =       1344
991181                 XDOT =         502
229660
 YDOT =     -21036
368051  feet/sec       YDOT =       -6406
784917  meter/sec
 ZDOT =     -13917
783515                 ZDOT =       -4239
924344

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18268374
61                 X    =         5568200
58
 Y    =       -1346582
46  feet           Y    =         -410438
33  meter
 Z    =       12313436
59                 Z    =         3753135
47
 XDOT =      10635
506835                 XDOT =        3241
702483
 YDOT =      16815
836366  feet/sec       YDOT =        5125
466924  meter/sec
 ZDOT =     -13909
733886                 ZDOT =       -4239
686888


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   08300
53980575  
00020000  00000-0  20000-3 0  9114
2 25544  51
6418  62
9766 0003650 273
3693  86
7051 15
72428752  9201


Satellite: ISS
Catalog Number: 25544
Epoch time:      08300
53980575   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:        62
9766  deg
Eccentricity:     
0003650     
Arg of perigee:   273
3693  deg
Mean anomaly:      86
7051  deg
Mean motion:   15
72428752  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             920
Checksum:              297

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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