Date: August 13th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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


226/08:06:18 565 -0 9 9 6 9 6
N/A 9 2 0 0 196 8
000/00:16:33 129 2 8 -0 2 187 4

Coasting Arc #1 (Orbit 3723)
---------------------------------------

Vector Time (GMT): 2008/224/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1712891
87                 A    =         6733591
34  meter
 Y    =       -6212085
09  meter          E    =           
0012385
 Z    =       -1965802
20                 I    =           51
98474
 XDOT =       4319
167638                 Wp   =           86
87187
 YDOT =       2963
218379  meter/sec      RA   =           91
61901  deg
 ZDOT =      -5630
141805                 TA   =          114
86604
                                          MA   =          114
73722
                                          Ha   =            195
182  n
mi
                                          Hp   =            182
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5619723
99                 X    =         1791778
52
 Y    =      -20380856
59  feet           Y    =        -6192489
27  meter
 Z    =       -6449482
29                 Z    =        -1957290
06
 XDOT =      14170
497501                 XDOT =        4313
061398
 YDOT =       9721
845075  feet/sec       YDOT =        3011
484219  meter/sec
 ZDOT =     -18471
593847                 ZDOT =       -5609
174018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18922650
62                 X    =        -5767623
91
 Y    =        9450390
49  feet           Y    =         2880479
02  meter
 Z    =       -6417152
66                 Z    =        -1955948
13
 XDOT =      -1653
568255                 XDOT =        -504
007604
 YDOT =     -15732
289377  feet/sec       YDOT =       -4795
201802  meter/sec
 ZDOT =     -18390
298878                 ZDOT =       -5605
363098


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   08224
50716127  
00020000  00000-0  20000-3 0  9004
2 25544  51
6423  92
2159 0010002  53
1634 307
0444 15
72917973 37245


Satellite: ISS
Catalog Number: 25544
Epoch time:      08224
50716127   =   yrday
fracday
Element set:     900
Inclination:       51
6423  deg
RA of node:        92
2159  deg
Eccentricity:     
0010002     
Arg of perigee:    53
1634  deg
Mean anomaly:     307
0444  deg
Mean motion:   15
72917973  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3724
Checksum:              261


Coasting Arc #2 (Orbit 3739)
---------------------------------------

Vector Time (GMT): 2008/225/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4055346
28                 A    =         6724109
25  meter
 Y    =       -1845870
42  meter          E    =           
0015690
 Z    =        5027355
05                 I    =           51
95323
 XDOT =       1020
547298                 Wp   =           55
54024
 YDOT =      -7403
276776  meter/sec      RA   =           86
48133  deg
 ZDOT =      -1882
173177                 TA   =           52
59794
                                          MA   =           52
45522
                                          Ha   =            195
222  n
mi
                                          Hp   =            182
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13304941
87                 X    =        -4058825
73
 Y    =       -6056005
30  feet           Y    =        -1891239
59  meter
 Z    =       16493947
00                 Z    =         5007645
79
 XDOT =       3348
252291                 XDOT =        1112
399212
 YDOT =     -24288
965799  feet/sec       YDOT =       -7391
350669  meter/sec
 ZDOT =      -6175
108848                 ZDOT =       -1876
993061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4717765
03                 X    =         1437974
78
 Y    =       13926652
86  feet           Y    =         4244843
79  meter
 Z    =       16417612
47                 Z    =         5004088
28
 XDOT =     -19047
077991                 XDOT =       -5805
549372
 YDOT =      13758
965820  feet/sec       YDOT =        4193
732782  meter/sec
 ZDOT =      -6155
756015                 ZDOT =       -1876
274433


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   08225
52366894  
00020000  00000-0  20000-3 0  9010
2 25544  51
6425  87
0036 0010073  55
8961 304
3156 15
73002901 37408


Satellite: ISS
Catalog Number: 25544
Epoch time:      08225
52366894   =   yrday
fracday
Element set:     901
Inclination:       51
6425  deg
RA of node:        87
0036  deg
Eccentricity:     
0010073     
Arg of perigee:    55
8961  deg
Mean anomaly:     304
3156  deg
Mean motion:   15
73002901  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3740
Checksum:              270


Coasting Arc #3 (Orbit 3752)
---------------------------------------

Vector Time (GMT): 2008/226/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3102191
61                 A    =         6736941
42  meter
 Y    =        5158756
30  meter          E    =           
0011237
 Z    =       -3017618
65                 I    =           51
97328
 XDOT =      -3260
316081                 Wp   =           29
82501
 YDOT =       4868
698838  meter/sec      RA   =           82
06049  deg
 ZDOT =       4988
979772                 TA   =          295
50122
                                          MA   =          295
61740
                                          Ha   =            196
834  n
mi
                                          Hp   =            187
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10177794
00                 X    =         3058933
82
 Y    =       16925053
48  feet           Y    =         5193205
21  meter
 Z    =       -9900323
67                 Z    =        -3002653
03
 XDOT =     -10696
575068                 XDOT =       -3338
751511
 YDOT =      15973
421384  feet/sec       YDOT =        4831
801084  meter/sec
 ZDOT =      16368
043870                 ZDOT =        4972
951348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17747423
32                 X    =         5409414
63
 Y    =       -8730687
62  feet           Y    =        -2661113
59  meter
 Z    =       -9842021
83                 Z    =        -2999848
25
 XDOT =      14342
816509                 XDOT =        4371
690472
 YDOT =      10838
120546  feet/sec       YDOT =        3303
459142  meter/sec
 ZDOT =      16306
532599                 ZDOT =        4970
231136


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   08226
34957788  
00020000  00000-0  20000-3 0  9020
2 25544  51
6414  82
7688 0008326   9
2353 350
8961 15
70958162 37537


Satellite: ISS
Catalog Number: 25544
Epoch time:      08226
34957788   =   yrday
fracday
Element set:     902
Inclination:       51
6414  deg
RA of node:        82
7688  deg
Eccentricity:     
0008326     
Arg of perigee:     9
2353  deg
Mean anomaly:     350
8961  deg
Mean motion:   15
70958162  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3753
Checksum:              319


Coasting Arc #4 (Orbit 3768)
---------------------------------------

Vector Time (GMT): 2008/227/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1771054
82                 A    =         6734796
39  meter
 Y    =       -5327174
81  meter          E    =           
0012144
 Z    =       -3735194
53                 I    =           51
96160
 XDOT =       4493
313996                 Wp   =           38
69863
 YDOT =       4511
085512  meter/sec      RA   =           77
02067  deg
 ZDOT =      -4301
477458                 TA   =          185
99627
                                          MA   =          186
01082
                                          Ha   =            196
862  n
mi
                                          Hp   =            187
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5810547
30                 X    =         1848637
06
 Y    =      -17477607
63  feet           Y    =        -5306935
77  meter
 Z    =      -12254575
22                 Z    =        -3726402
88
 XDOT =      14741
843819                 XDOT =        4463
431768
 YDOT =      14800
149317  feet/sec       YDOT =        4561
165594  meter/sec
 ZDOT =     -14112
458851                 ZDOT =       -4279
721575

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17027283
77                 X    =        -5189916
09
 Y    =       -7079610
08  feet           Y    =        -2157865
15  meter
 Z    =      -12221070
78                 Z    =        -3724982
37
 XDOT =      15277
062998                 XDOT =        4656
448802
 YDOT =     -12517
535561  feet/sec       YDOT =       -3815
344839  meter/sec
 ZDOT =     -14027
967419                 ZDOT =       -4275
724469


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   08227
36737965  
00020000  00000-0  20000-3 0  9037
2 25544  51
6421  77
5654 0008410  12
8777 347
2598 15
70977752 37693


Satellite: ISS
Catalog Number: 25544
Epoch time:      08227
36737965   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:        77
5654  deg
Eccentricity:     
0008410     
Arg of perigee:    12
8777  deg
Mean anomaly:     347
2598  deg
Mean motion:   15
70977752  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3769
Checksum:              332


Coasting Arc #5 (Orbit 3784)
---------------------------------------

Vector Time (GMT): 2008/228/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4438416
06                 A    =         6732508
06  meter
 Y    =       -2519756
38  meter          E    =           
0016006
 Z    =        4387564
40                 I    =           51
94544
 XDOT =        539
500746                 Wp   =           44
84814
 YDOT =      -6888
201757  meter/sec      RA   =           71
88056  deg
 ZDOT =      -3391
544761                 TA   =           79
27009
                                          MA   =           79
08992
                                          Ha   =            197
019  n
mi
                                          Hp   =            186
998

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14561732
48                 X    =        -4431223
42
 Y    =       -8266917
27  feet           Y    =        -2569349
34  meter
 Z    =       14394896
32                 Z    =         4366020
35
 XDOT =       1770
015572                 XDOT =         632
960791
 YDOT =     -22599
087129  feet/sec       YDOT =       -6881
645992  meter/sec
 ZDOT =     -11127
115358                 ZDOT =       -3388
697308

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9020671
36                 X    =        -2749500
63
 Y    =       14191913
20  feet           Y    =         4325695
14  meter
 Z    =       14311397
62                 Z    =         4362113
99
 XDOT =     -21437
569478                 XDOT =       -6534
171177
 YDOT =      -2354
071840  feet/sec       YDOT =        -717
521097  meter/sec
 ZDOT =     -11116
724683                 ZDOT =       -3388
377683


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   08228
38517256  
00020000  00000-0  20000-3 0  9040
2 25544  51
6414  72
3619 0008468  16
4213 343
7221 15
70991940 37854


Satellite: ISS
Catalog Number: 25544
Epoch time:      08228
38517256   =   yrday
fracday
Element set:     904
Inclination:       51
6414  deg
RA of node:        72
3619  deg
Eccentricity:     
0008468     
Arg of perigee:    16
4213  deg
Mean anomaly:     343
7221  deg
Mean motion:   15
70991940  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3785
Checksum:              296


Coasting Arc #6 (Orbit 3800)
---------------------------------------

Vector Time (GMT): 2008/229/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         931855
51                 A    =         6738900
30  meter
 Y    =        6326673
53  meter          E    =           
0020619
 Z    =        2086182
53                 I    =           51
95701
 XDOT =      -5207
284421                 Wp   =           51
07190
 YDOT =      -1079
341757  meter/sec      RA   =           66
83164  deg
 ZDOT =       5575
350230                 TA   =          332
11942
                                          MA   =          332
22976
                                          Ha   =            197
089  n
mi
                                          Hp   =            186
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3057268
73                 X    =          850906
29
 Y    =       20756802
90  feet           Y    =         6336641
39  meter
 Z    =        6844430
89                 Z    =         2090512
97
 XDOT =     -17084
266473                 XDOT =       -5221
911514
 YDOT =      -3541
147498  feet/sec       YDOT =       -1137
654570  meter/sec
 ZDOT =      18291
831463                 ZDOT =        5550
018205

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20849882
45                 X    =         6355044
17
 Y    =       -2288443
94  feet           Y    =         -697517
71  meter
 Z    =        6861735
87                 Z    =         2091457
09
 XDOT =      -4308
443464                 XDOT =       -1313
213568
 YDOT =      15533
500306  feet/sec       YDOT =        4734
610893  meter/sec
 ZDOT =      18193
816951                 ZDOT =        5545
475407


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   08229
40295684  
00020000  00000-0  20000-3 0  9053
2 25544  51
6418  67
1579 0008536  20
0388 340
1107 15
70979954 38019


Satellite: ISS
Catalog Number: 25544
Epoch time:      08229
40295684   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:        67
1579  deg
Eccentricity:     
0008536     
Arg of perigee:    20
0388  deg
Mean anomaly:     340
1107  deg
Mean motion:   15
70979954  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3801
Checksum:              304


Coasting Arc #7 (Orbit 3815)
---------------------------------------

Vector Time (GMT): 2008/230/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4267464
90                 A    =         6729198
15  meter
 Y    =        -633846
69  meter          E    =           
0017971
 Z    =       -5177842
08                 I    =           51
91229
 XDOT =       2643
629510                 Wp   =           72
52993
 YDOT =       7093
715868  meter/sec      RA   =           61
70968  deg
 ZDOT =       1319
450167                 TA   =          210
01929
                                          MA   =          210
12243
                                          Ha   =            197
088  n
mi
                                          Hp   =            186
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14000869
08                 X    =         4299388
06
 Y    =       -2079549
50  feet           Y    =         -585946
91  meter
 Z    =      -16987670
87                 Z    =        -5157033
59
 XDOT =       8673
325164                 XDOT =        2557
700434
 YDOT =      23273
346025  feet/sec       YDOT =        7122
797992  meter/sec
 ZDOT =       4328
904747                 ZDOT =        1332
084007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1827405
30                 X    =         -556993
13
 Y    =      -14132721
28  feet           Y    =        -4307653
45  meter
 Z    =      -16907294
34                 Z    =        -5153343
32
 XDOT =      22393
580590                 XDOT =        6825
563364
 YDOT =      -8097
989917  feet/sec       YDOT =       -2468
267327  meter/sec
 ZDOT =       4378
375341                 ZDOT =        1334
528804


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   08230
35711955  
00020000  00000-0  20000-3 0  9064
2 25544  51
6421  62
2793 0008485  22
7838 337
3699 15
71019537 38162


Satellite: ISS
Catalog Number: 25544
Epoch time:      08230
35711955   =   yrday
fracday
Element set:     906
Inclination:       51
6421  deg
RA of node:        62
2793  deg
Eccentricity:     
0008485     
Arg of perigee:    22
7838  deg
Mean anomaly:     337
3699  deg
Mean motion:   15
71019537  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3816
Checksum:              308


Coasting Arc #8 (Orbit 3831)
---------------------------------------

Vector Time (GMT): 2008/231/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3569769
99                 A    =         6740733
09  meter
 Y    =       -5713690
68  meter          E    =           
0011894
 Z    =        -206368
80                 I    =           51
93599
 XDOT =       4116
317278                 Wp   =           95
01134
 YDOT =      -2364
017805  meter/sec      RA   =           56
62941  deg
 ZDOT =      -6050
411342                 TA   =           87
21731
                                          MA   =           87
08118
                                          Ha   =            197
143  n
mi
                                          Hp   =            186
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11711843
80                 X    =        -3504610
79
 Y    =      -18745704
33  feet           Y    =        -5753245
58  meter
 Z    =        -677062
99                 Z    =         -223552
14
 XDOT =      13504
977947                 XDOT =        4171
837543
 YDOT =      -7755
963927  feet/sec       YDOT =       -2317
676429  meter/sec
 ZDOT =     -19850
430911                 ZDOT =       -6030
279679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18753480
98                 X    =        -5716061
00
 Y    =       11695321
87  feet           Y    =         3564734
11  meter
 Z    =        -743994
58                 Z    =         -226769
55
 XDOT =      -6894
137183                 XDOT =       -2101
333013
 YDOT =     -12255
937997  feet/sec       YDOT =       -3735
609902  meter/sec
 ZDOT =     -19772
826271                 ZDOT =       -6026
757447


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   08231
37488602  
00020000  00000-0  20000-3 0  9078
2 25544  51
6422  57
0753 0008359  26
8428 333
3165 15
70988831 38324


Satellite: ISS
Catalog Number: 25544
Epoch time:      08231
37488602   =   yrday
fracday
Element set:     907
Inclination:       51
6422  deg
RA of node:        57
0753  deg
Eccentricity:     
0008359     
Arg of perigee:    26
8428  deg
Mean anomaly:     333
3165  deg
Mean motion:   15
70988831  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3832
Checksum:              304


Coasting Arc #9 (Orbit 3847)
---------------------------------------

Vector Time (GMT): 2008/232/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2606953
07                 A    =         6728768
47  meter
 Y    =        3320128
05  meter          E    =           
0009111
 Z    =        5233167
55                 I    =           51
87938
 XDOT =      -5283
016191                 Wp   =           50
78676
 YDOT =      -5535
189059  meter/sec      RA   =           51
53997  deg
 ZDOT =        884
576476                 TA   =           30
84625
                                          MA   =           30
79275
                                          Ha   =            197
283  n
mi
                                          Hp   =            186
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8552995
64                 X    =        -2669307
06
 Y    =       10892808
58  feet           Y    =         3290627
10  meter
 Z    =       17169184
89                 Z    =         5220351
56
 XDOT =     -17332
730287                 XDOT =       -5225
025248
 YDOT =     -18160
069091  feet/sec       YDOT =       -5593
942522  meter/sec
 ZDOT =       2902
153794                 ZDOT =         859
052827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11034431
60                 X    =         3363294
75
 Y    =        8469756
21  feet           Y    =         2581581
69  meter
 Z    =       17119943
69                 Z    =         5218158
84
 XDOT =     -17253
051496                 XDOT =       -5258
730096
 YDOT =      16842
346572  feet/sec       YDOT =        5133
547235  meter/sec
 ZDOT =       2803
004108                 ZDOT =         854
355652


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   08232
39264118  
00020000  00000-0  20000-3 0  9086
2 25544  51
6424  51
8712 0008534  29
9592 330
2056 15
71044508 38481


Satellite: ISS
Catalog Number: 25544
Epoch time:      08232
39264118   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:        51
8712  deg
Eccentricity:     
0008534     
Arg of perigee:    29
9592  deg
Mean anomaly:     330
2056  deg
Mean motion:   15
71044508  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3848
Checksum:              289


Coasting Arc #10 (Orbit 3862)
---------------------------------------

Vector Time (GMT): 2008/233/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5369623
07                 A    =         6739330
80  meter
 Y    =        3675081
65  meter          E    =           
0016284
 Z    =       -1729653
59                 I    =           51
89567
 XDOT =      -1528
292788                 Wp   =           34
58764
 YDOT =       4910
424760  meter/sec      RA   =           46
42081  deg
 ZDOT =       5728
174780                 TA   =          306
35742
                                          MA   =          306
50759
                                          Ha   =            197
297  n
mi
                                          Hp   =            186
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17616873
59                 X    =         5336530
95
 Y    =       12057354
49  feet           Y    =         3734942
79  meter
 Z    =       -5674716
50                 Z    =        -1703648
54
 XDOT =      -5014
083950                 XDOT =       -1610
914685
 YDOT =      16110
317453  feet/sec       YDOT =        4892
872688  meter/sec
 ZDOT =      18793
224343                 ZDOT =        5720
549555

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11455110
70                 X    =         3491517
74
 Y    =      -18045741
00  feet           Y    =        -5500341
86  meter
 Z    =       -5573877
48                 Z    =        -1698917
86
 XDOT =      14958
053439                 XDOT =        4559
214688
 YDOT =       3739
817553  feet/sec       YDOT =        1139
896390  meter/sec
 ZDOT =      18764
186018                 ZDOT =        5719
323898


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
34677897  
00020000  00000-0  20000-3 0  9095
2 25544  51
6423  46
9924 0008593  32
2989 327
8698 15
71049642 38637


Satellite: ISS
Catalog Number: 25544
Epoch time:      08233
34677897   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:        46
9924  deg
Eccentricity:     
0008593     
Arg of perigee:    32
2989  deg
Mean anomaly:     327
8698  deg
Mean motion:   15
71049642  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3863
Checksum:              344


Coasting Arc #11 (Orbit 3878)
---------------------------------------

Vector Time (GMT): 2008/234/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -76854
84                 A    =         6731314
66  meter
 Y    =       -4907696
24  meter          E    =           
0018239
 Z    =       -4624244
43                 I    =           51
84740
 XDOT =       6562
204450                 Wp   =           54
38277
 YDOT =       2684
101132  meter/sec      RA   =           41
36114  deg
 ZDOT =      -2955
441629                 TA   =          186
31192
                                          MA   =          186
33493
                                          Ha   =            197
250  n
mi
                                          Hp   =            186
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -252148
41                 X    =             493
28
 Y    =      -16101365
61  feet           Y    =        -4908123
25  meter
 Z    =      -15171405
62                 Z    =        -4624429
86
 XDOT =      21529
542158                 XDOT =        6546
059693
 YDOT =       8806
106076  feet/sec       YDOT =        2757
393175  meter/sec
 ZDOT =      -9696
330805                 ZDOT =       -2923
601671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16072103
66                 X    =        -4898777
20
 Y    =         985022
82  feet           Y    =          300234
96  meter
 Z    =      -15172551
39                 Z    =        -4624593
66
 XDOT =       7767
388974                 XDOT =        2367
500159
 YDOT =     -20833
069716  feet/sec       YDOT =       -6349
919649  meter/sec
 ZDOT =      -9573
032272                 ZDOT =       -2917
860237


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
36451659  
00020000  00000-0  20000-3 0  9106
2 25544  51
6419  41
7882 0008533  35
4676 324
7052 15
71064452 38793


Satellite: ISS
Catalog Number: 25544
Epoch time:      08234
36451659   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:        41
7882  deg
Eccentricity:     
0008533     
Arg of perigee:    35
4676  deg
Mean anomaly:     324
7052  deg
Mean motion:   15
71064452  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3879
Checksum:              301


Coasting Arc #12 (Orbit 3894)
---------------------------------------

Vector Time (GMT): 2008/235/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5754277
90                 A    =         6735571
30  meter
 Y    =        -936746
82  meter          E    =           
0019200
 Z    =        3364711
22                 I    =           51
83999
 XDOT =      -1790
988448                 Wp   =           69
67687
 YDOT =      -5855
138857  meter/sec      RA   =           36
21515  deg
 ZDOT =      -4665
097974                 TA   =           70
84965
                                          MA   =           70
64190
                                          Ha   =            197
324  n
mi
                                          Hp   =            185
937

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18878864
49                 X    =        -5759720
58
 Y    =       -3073316
34  feet           Y    =        -1001124
93  meter
 Z    =       11039078
81                 Z    =         3336743
62
 XDOT =      -5875
946352                 XDOT =       -1702
719964
 YDOT =     -19209
773152  feet/sec       YDOT =       -5874
673136  meter/sec
 ZDOT =     -15305
439547                 ZDOT =       -4673
584280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1776377
25                 X    =         -541439
78
 Y    =       19107012
26  feet           Y    =         5823817
34  meter
 Z    =       10930902
31                 Z    =         3331739
02
 XDOT =     -17377
798457                 XDOT =       -5296
752970
 YDOT =       7212
416808  feet/sec       YDOT =        2198
344643  meter/sec
 ZDOT =     -15338
743894                 ZDOT =       -4675
249139


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
38224417  
00020000  00000-0  20000-3 0  9110
2 25544  51
6426  36
5843 0008662  38
6859 321
4921 15
71123540 38952


Satellite: ISS
Catalog Number: 25544
Epoch time:      08235
38224417   =   yrday
fracday
Element set:     911
Inclination:       51
6426  deg
RA of node:        36
5843  deg
Eccentricity:     
0008662     
Arg of perigee:    38
6859  deg
Mean anomaly:     321
4921  deg
Mean motion:   15
71123540  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3895
Checksum:              294


Coasting Arc #13 (Orbit 3910)
---------------------------------------

Vector Time (GMT): 2008/236/08:14:35
129
Vector Time (MET): N/A
Weight (LBS)     : 661191
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3029556
47                 A    =         6735432
13  meter
 Y    =        4951732
01  meter          E    =           
0019297
 Z    =        3393782
98                 I    =           51
81409
 XDOT =      -6127
102979                 Wp   =           70
70674
 YDOT =        558
731243  meter/sec      RA   =           31
16499  deg
 ZDOT =       4639
268140                 TA   =          329
24292
                                          MA   =          329
35586
                                          Ha   =            197
326  n
mi
                                          Hp   =            185
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9939489
74                 X    =         2957473
82
 Y    =       16245839
93  feet           Y    =         4985207
09  meter
 Z    =       11134458
61                 Z    =         3408325
71
 XDOT =     -20102
043893                 XDOT =       -6155
432209
 YDOT =       1833
107752  feet/sec       YDOT =         490
055881  meter/sec
 ZDOT =      15220
695997                 ZDOT =        4609
433798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15344919
06                 X    =         4677131
33
 Y    =      -11224524
82  feet           Y    =        -3421235
17  meter
 Z    =       11191087
59                 Z    =         3411043
50
 XDOT =       2728
933730                 XDOT =         831
779001
 YDOT =      18840
080277  feet/sec       YDOT =        5742
456469  meter/sec
 ZDOT =      15105
431510                 ZDOT =        4604
135524


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
39996400  
00020000  00000-0  20000-3 0  9121
2 25544  51
6415  31
3799 0008605  42
4093 317
7732 15
71087648 39118


Satellite: ISS
Catalog Number: 25544
Epoch time:      08236
39996400   =   yrday
fracday
Element set:     912
Inclination:       51
6415  deg
RA of node:        31
3799  deg
Eccentricity:     
0008605     
Arg of perigee:    42
4093  deg
Mean anomaly:     317
7732  deg
Mean motion:   15
71087648  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3911
Checksum:              301

INTERNATIONAL SPACE STATION ORBITAL DATA:

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

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

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

   David Cottle
   Director Of Engineering
   IDB Communications

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