Date: July 28th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7750 02 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


205/16:28:18 127 -10 4 11 2 11 2
N/A -3 4 0 0 193 9
000/00:20:36 255 2 5 0 3 185 5

Coasting Arc #1 (Orbit 3424)
---------------------------------------

Vector Time (GMT): 2008/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4584305
09                 A    =         6721298
24  meter
 Y    =        2639750
23  meter          E    =           
0015165
 Z    =       -4155839
60                 I    =           51
58210
 XDOT =      -5551
814824                 Wp   =           73
36651
 YDOT =      -3819
103805  meter/sec      RA   =          188
60564  deg
 ZDOT =       3713
753634                 TA   =          234
59056
                                          MA   =          234
73229
                                          Ha   =            191
568  n
mi
                                          Hp   =            179
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15040371
05                 X    =        -4593294
35
 Y    =        8660597
88  feet           Y    =         2588435
93  meter
 Z    =      -13634644
36                 Z    =        -4178131
61
 XDOT =     -18214
615565                 XDOT =       -5526
736957
 YDOT =     -12529
868126  feet/sec       YDOT =       -3881
047427  meter/sec
 ZDOT =      12184
231083                 ZDOT =        3686
843805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15106809
15                 X    =         4604555
43
 Y    =        8405812
29  feet           Y    =         2562091
59  meter
 Z    =      -13720381
95                 Z    =        -4181972
42
 XDOT =       -770
534111                 XDOT =        -234
858797
 YDOT =      21020
421535  feet/sec       YDOT =        6407
024484  meter/sec
 ZDOT =      12080
030785                 ZDOT =        3681
993383


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   08205
50925000  
00020000  00000-0  20000-3 0  9005
2 25544  51
6374 189
5898 0010000  43
7935 316
4020 15
75149493 34256


Satellite: ISS
Catalog Number: 25544
Epoch time:      08205
50925000   =   yrday
fracday
Element set:     900
Inclination:       51
6374  deg
RA of node:       189
5898  deg
Eccentricity:     
0010000     
Arg of perigee:    43
7935  deg
Mean anomaly:     316
4020  deg
Mean motion:   15
75149493  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3425
Checksum:              273


Coasting Arc #2 (Orbit 3427)
---------------------------------------

Vector Time (GMT): 2008/205/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5825892
65                 A    =         6732094
12  meter
 Y    =        1590097
06  meter          E    =           
0011467
 Z    =       -2962421
30                 I    =           51
60298
 XDOT =      -3760
231692                 Wp   =            9
06988
 YDOT =      -4496
349106  meter/sec      RA   =          187
61127  deg
 ZDOT =       4995
153457                 TA   =          316
73954
                                          MA   =          316
82954
                                          Ha   =            193
897  n
mi
                                          Hp   =            185
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19113821
03                 X    =        -5828849
59
 Y    =        5216853
88  feet           Y    =         1524932
26  meter
 Z    =       -9719229
98                 Z    =        -2990730
33
 XDOT =     -12336
718148                 XDOT =       -3733
938690
 YDOT =     -14751
801528  feet/sec       YDOT =       -4538
251513  meter/sec
 ZDOT =      16388
298744                 ZDOT =        4976
949947

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17760196
97                 X    =         5413308
04
 Y    =       -8660099
09  feet           Y    =        -2639598
20  meter
 Z    =       -9828287
62                 Z    =        -2995662
07
 XDOT =      14318
368110                 XDOT =        4364
238600
 YDOT =      10896
019167  feet/sec       YDOT =        3321
106642  meter/sec
 ZDOT =      16317
618396                 ZDOT =        4973
610087


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   08205
69957900  
00020000  00000-0  20000-3 0  9010
2 25544  51
6402 188
6113 0010128 345
5083  14
5787 15
72658063 34280


Satellite: ISS
Catalog Number: 25544
Epoch time:      08205
69957900   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:       188
6113  deg
Eccentricity:     
0010128     
Arg of perigee:   345
5083  deg
Mean anomaly:      14
5787  deg
Mean motion:   15
72658063  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3428
Checksum:              292


Coasting Arc #3 (Orbit 3443)
---------------------------------------

Vector Time (GMT): 2008/206/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4066679
75                 A    =         6728658
55  meter
 Y    =        3445882
78  meter          E    =           
0013613
 Z    =       -4119682
93                 I    =           51
62120
 XDOT =      -6125
951734                 Wp   =           23
33852
 YDOT =       2715
714551  meter/sec      RA   =          182
53369  deg
 ZDOT =      -3767
569068                 TA   =          207
92950
                                          MA   =          208
00263
                                          Ha   =            194
120  n
mi
                                          Hp   =            185
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13342125
17                 X    =         4047857
70
 Y    =       11305389
68  feet           Y    =         3491253
81  meter
 Z    =      -13516020
12                 Z    =        -4099972
51
 XDOT =     -20098
266845                 XDOT =       -6137
561886
 YDOT =       8909
824644  feet/sec       YDOT =        2647
146022  meter/sec
 ZDOT =     -12360
790907                 ZDOT =       -3797
356831

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15428704
46                 X    =        -4702669
12
 Y    =       -8356940
16  feet           Y    =        -2547195
36  meter
 Z    =      -13439626
84                 Z    =        -4096398
26
 XDOT =      17201
428674                 XDOT =        5242
995460
 YDOT =     -11651
935418  feet/sec       YDOT =       -3551
509916  meter/sec
 ZDOT =     -12475
448943                 ZDOT =       -3802
516838


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   08206
71627875  
00020000  00000-0  20000-3 0  9020
2 25544  51
6408 183
4006 0010195 349
6142  10
4808 15
72684831 34444


Satellite: ISS
Catalog Number: 25544
Epoch time:      08206
71627875   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:       183
4006  deg
Eccentricity:     
0010195     
Arg of perigee:   349
6142  deg
Mean anomaly:      10
4808  deg
Mean motion:   15
72684831  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3444
Checksum:              286


Coasting Arc #4 (Orbit 3459)
---------------------------------------

Vector Time (GMT): 2008/207/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4779618
30                 A    =         6730222
11  meter
 Y    =       -3075490
60  meter          E    =           
0015418
 Z    =        3605249
52                 I    =           51
65527
 XDOT =       5419
329966                 Wp   =           44
64944
 YDOT =       3235
767584  meter/sec      RA   =          177
35711  deg
 ZDOT =      -4402
179665                 TA   =           92
27429
                                          MA   =           92
09774
                                          Ha   =            194
213  n
mi
                                          Hp   =            185
042

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15681162
39                 X    =         4796140
05
 Y    =      -10090192
26  feet           Y    =        -3021950
14  meter
 Z    =       11828246
45                 Z    =         3628508
72
 XDOT =      17779
953956                 XDOT =        5404
129302
 YDOT =      10616
035381  feet/sec       YDOT =        3296
285089  meter/sec
 ZDOT =     -14442
846669                 ZDOT =       -4375
889171

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13023045
46                 X    =        -3969424
26
 Y    =       13266018
01  feet           Y    =         4043482
29  meter
 Z    =       11917688
57                 Z    =         3632511
47
 XDOT =     -18786
837754                 XDOT =       -5726
228147
 YDOT =      -5494
516734  feet/sec       YDOT =       -1674
728701  meter/sec
 ZDOT =     -14341
080143                 ZDOT =       -4371
161228


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   08207
73296902  
00020000  00000-0  20000-3 0  9037
2 25544  51
6401 178
1896 0010171 353
5211   6
5818 15
72678585 34604


Satellite: ISS
Catalog Number: 25544
Epoch time:      08207
73296902   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:       178
1896  deg
Eccentricity:     
0010171     
Arg of perigee:   353
5211  deg
Mean anomaly:       6
5818  deg
Mean motion:   15
72678585  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3460
Checksum:              293


Coasting Arc #5 (Orbit 3475)
---------------------------------------

Vector Time (GMT): 2008/208/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5303974
93                 A    =         6730528
32  meter
 Y    =       -2109704
05  meter          E    =           
0015203
 Z    =        3546952
96                 I    =           51
68573
 XDOT =       4664
157476                 Wp   =           50
74244
 YDOT =      -4199
110144  meter/sec      RA   =          172
28492  deg
 ZDOT =       4473
731421                 TA   =          351
53071
                                          MA   =          351
55634
                                          Ha   =            194
465  n
mi
                                          Hp   =            184
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17401492
55                 X    =        -5297220
13
 Y    =       -6921601
22  feet           Y    =        -2168978
82  meter
 Z    =       11636984
79                 Z    =         3521202
39
 XDOT =      15302
353923                 XDOT =        4689
033368
 YDOT =     -13776
608084  feet/sec       YDOT =       -4146
814332  meter/sec
 ZDOT =      14677
596524                 ZDOT =        4496
449794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18607405
41                 X    =         5671537
17
 Y    =        2606273
83  feet           Y    =          794392
26  meter
 Z    =       11537405
34                 Z    =         3516601
15
 XDOT =     -11349
447685                 XDOT =       -3459
311655
 YDOT =      15620
401838  feet/sec       YDOT =        4761
098480  meter/sec
 ZDOT =      14764
852382                 ZDOT =        4500
327006


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   08208
74964816  
00020000  00000-0  20000-3 0  9046
2 25544  51
6406 172
9780 0010248 357
2768   2
8337 15
72691049 34768


Satellite: ISS
Catalog Number: 25544
Epoch time:      08208
74964816   =   yrday
fracday
Element set:     904
Inclination:       51
6406  deg
RA of node:       172
9780  deg
Eccentricity:     
0010248     
Arg of perigee:   357
2768  deg
Mean anomaly:       2
8337  deg
Mean motion:   15
72691049  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3476
Checksum:              316


Coasting Arc #6 (Orbit 3490)
---------------------------------------

Vector Time (GMT): 2008/209/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3275006
56                 A    =         6728173
61  meter
 Y    =        4134181
68  meter          E    =           
0010684
 Z    =       -4179125
46                 I    =           51
70732
 XDOT =      -6582
557522                 Wp   =           46
01374
 YDOT =      -1489
329785  meter/sec      RA   =          167
11272  deg
 ZDOT =       3698
265130                 TA   =          261
68069
                                          MA   =          261
80184
                                          Ha   =            194
394  n
mi
                                          Hp   =            184
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10744772
18                 X    =        -3300690
85
 Y    =       13563588
17  feet           Y    =         4097415
70  meter
 Z    =      -13711041
52                 Z    =        -4195097
16
 XDOT =     -21596
317331                 XDOT =       -6583
379824
 YDOT =      -4886
252574  feet/sec       YDOT =       -1562
944879  meter/sec
 ZDOT =      12133
415781                 ZDOT =        3666
284920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6895118
23                 X    =         2101632
04
 Y    =      -15817565
20  feet           Y    =        -4821193
87  meter
 Z    =      -13772279
71                 Z    =        -4197790
86
 XDOT =      21043
565323                 XDOT =        6414
078710
 YDOT =      -1246
441792  feet/sec       YDOT =        -379
915458  meter/sec
 ZDOT =      12009
843274                 ZDOT =        3660
600230


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   08209
70277446  
00020000  00000-0  20000-3 0  9050
2 25544  51
6407 168
0928 0010285 359
9616    
1544 15
72717573 34910


Satellite: ISS
Catalog Number: 25544
Epoch time:      08209
70277446   =   yrday
fracday
Element set:     905
Inclination:       51
6407  deg
RA of node:       168
0928  deg
Eccentricity:     
0010285     
Arg of perigee:   359
9616  deg
Mean anomaly:        
1544  deg
Mean motion:   15
72717573  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3491
Checksum:              302


Coasting Arc #7 (Orbit 3506)
---------------------------------------

Vector Time (GMT): 2008/210/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6056766
70                 A    =         6732238
53  meter
 Y    =         455439
27  meter          E    =           
0009432
 Z    =       -2918319
26                 I    =           51
74898
 XDOT =      -2809
133560                 Wp   =           30
22883
 YDOT =       5083
865700  meter/sec      RA   =          162
04170  deg
 ZDOT =      -5035
813304                 TA   =          183
23942
                                          MA   =          183
24553
                                          Ha   =            194
507  n
mi
                                          Hp   =            184
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19871281
84                 X    =         6065400
32
 Y    =        1494223
34  feet           Y    =          523218
28  meter
 Z    =       -9574538
25                 Z    =        -2888874
66
 XDOT =      -9216
317455                 XDOT =       -2841
310494
 YDOT =      16679
349410  feet/sec       YDOT =        5052
273290  meter/sec
 ZDOT =     -16521
697192                 ZDOT =       -5049
537278

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19592532
22                 X    =        -5971803
82
 Y    =        3923974
12  feet           Y    =         1196027
31  meter
 Z    =       -9460836
98                 Z    =        -2883663
11
 XDOT =       4582
046908                 XDOT =        1396
607898
 YDOT =     -17090
185286  feet/sec       YDOT =       -5209
088475  meter/sec
 ZDOT =     -16574
178388                 ZDOT =       -5051
809573


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   08210
71943300  
00020000  00000-0  20000-3 0  9063
2 25544  51
6407 162
8814 0010186   3
1630 356
9595 15
72712526 35079


Satellite: ISS
Catalog Number: 25544
Epoch time:      08210
71943300   =   yrday
fracday
Element set:     906
Inclination:       51
6407  deg
RA of node:       162
8814  deg
Eccentricity:     
0010186     
Arg of perigee:     3
1630  deg
Mean anomaly:     356
9595  deg
Mean motion:   15
72712526  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3507
Checksum:              274


Coasting Arc #8 (Orbit 3522)
---------------------------------------

Vector Time (GMT): 2008/211/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1600637
31                 A    =         6726353
67  meter
 Y    =       -4631396
19  meter          E    =           
0016369
 Z    =        4606940
97                 I    =           51
75787
 XDOT =       7093
483640                 Wp   =           32
31823
 YDOT =       -500
995033  meter/sec      RA   =          156
87780  deg
 ZDOT =      -2949
846070                 TA   =           86
97502
                                          MA   =           86
78772
                                          Ha   =            194
521  n
mi
                                          Hp   =            184
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5251434
74                 X    =         1629927
99
 Y    =      -15194869
40  feet           Y    =        -4613333
96  meter
 Z    =       15114635
74                 Z    =         4614787
12
 XDOT =      23272
584121                 XDOT =        7112
888259
 YDOT =      -1643
684492  feet/sec       YDOT =        -421
562632  meter/sec
 ZDOT =      -9677
972669                 ZDOT =       -2915
339357

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -608911
26                 X    =         -185596
15
 Y    =       16037077
03  feet           Y    =         4888101
08  meter
 Z    =       15144478
33                 Z    =         4616037
00
 XDOT =     -20716
337831                 XDOT =       -6314
339771
 YDOT =       8283
782514  feet/sec       YDOT =        2524
896910  meter/sec
 ZDOT =      -9544
803734                 ZDOT =       -2909
256178


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   08211
73607928  
00020000  00000-0  20000-3 0  9070
2 25544  51
6410 157
6697 0010379   6
8912 353
2391 15
72796565 35238


Satellite: ISS
Catalog Number: 25544
Epoch time:      08211
73607928   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       157
6697  deg
Eccentricity:     
0010379     
Arg of perigee:     6
8912  deg
Mean anomaly:     353
2391  deg
Mean motion:   15
72796565  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3523
Checksum:              310


Coasting Arc #9 (Orbit 3538)
---------------------------------------

Vector Time (GMT): 2008/212/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6200349
48                 A    =         6733647
63  meter
 Y    =        1347892
55  meter          E    =           
0021194
 Z    =        2214029
95                 I    =           51
80821
 XDOT =        808
693113                 Wp   =           46
09297
 YDOT =      -5342
026779  meter/sec      RA   =          151
80302  deg
 ZDOT =       5498
946645                 TA   =          338
68978
                                          MA   =          338
77791
                                          Ha   =            194
783  n
mi
                                          Hp   =            184
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20342353
93                 X    =        -6225716
14
 Y    =        4422219
66  feet           Y    =         1278414
51  meter
 Z    =        7263877
78                 Z    =         2183847
85
 XDOT =       2653
192628                 XDOT =         841
656063
 YDOT =     -17526
334576  feet/sec       YDOT =       -5332
800051  meter/sec
 ZDOT =      18041
163534                 ZDOT =        5502
954438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18094964
32                 X    =         5515345
13
 Y    =      -10373873
90  feet           Y    =        -3161956
76  meter
 Z    =        7147469
28                 Z    =         2178548
64
 XDOT =       2107
680216                 XDOT =         642
420930
 YDOT =      16158
152983  feet/sec       YDOT =        4925
005029  meter/sec
 ZDOT =      18056
120336                 ZDOT =        5503
505478


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   08212
75271748  
00020000  00000-0  20000-3 0  9081
2 25544  51
6409 152
4579 0010386  10
8017 349
3367 15
72763282 35393


Satellite: ISS
Catalog Number: 25544
Epoch time:      08212
75271748   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       152
4579  deg
Eccentricity:     
0010386     
Arg of perigee:    10
8017  deg
Mean anomaly:     349
3367  deg
Mean motion:   15
72763282  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3539
Checksum:              306


Coasting Arc #10 (Orbit 3553)
---------------------------------------

Vector Time (GMT): 2008/213/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         174597
95                 A    =         6724962
89  meter
 Y    =        4553432
85  meter          E    =           
0016237
 Z    =       -4956418
20                 I    =           51
80458
 XDOT =      -6932
533928                 Wp   =           66
27100
 YDOT =       2563
138307  meter/sec      RA   =          146
65194  deg
 ZDOT =       2122
373887                 TA   =          224
22365
                                          MA   =          224
35353
                                          Ha   =            194
741  n
mi
                                          Hp   =            183
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         572827
91                 X    =          147744
54
 Y    =       14939084
14  feet           Y    =         4555235
79  meter
 Z    =      -16261214
55                 Z    =        -4955634
66
 XDOT =     -22744
533884                 XDOT =       -6970
989964
 YDOT =       8409
246415  feet/sec       YDOT =        2485
399442  meter/sec
 ZDOT =       6963
168921                 ZDOT =        2088
603386

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5388768
34                 X    =        -1642496
59
 Y    =      -13949135
08  feet           Y    =        -4251696
37  meter
 Z    =      -16257744
98                 Z    =        -4955360
67
 XDOT =      17902
338045                 XDOT =        5456
632636
 YDOT =     -14834
538477  feet/sec       YDOT =       -4521
567328  meter/sec
 ZDOT =       6833
006452                 ZDOT =        2082
700367


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   08213
70580422  
00020000  00000-0  20000-3 0  9090
2 25544  51
6408 147
5720 0010319  14
0339 346
1108 15
72795371 35543


Satellite: ISS
Catalog Number: 25544
Epoch time:      08213
70580422   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:       147
5720  deg
Eccentricity:     
0010319     
Arg of perigee:    14
0339  deg
Mean anomaly:     346
1108  deg
Mean motion:   15
72795371  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3554
Checksum:              275


Coasting Arc #11 (Orbit 3569)
---------------------------------------

Vector Time (GMT): 2008/214/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5796993
21                 A    =         6734715
69  meter
 Y    =       -3084387
57  meter          E    =           
0008712
 Z    =       -1511553
09                 I    =           51
86088
 XDOT =       1115
553133                 Wp   =           70
07209
 YDOT =       4926
132478  meter/sec      RA   =          141
57071  deg
 ZDOT =      -5797
712854                 TA   =          126
49964
                                          MA   =          126
41936
                                          Ha   =            194
817  n
mi
                                          Hp   =            183
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19019006
60                 X    =         5838395
14
 Y    =      -10119381
81  feet           Y    =        -3019330
63  meter
 Z    =       -4959163
67                 Z    =        -1483291
76
 XDOT =       3659
951223                 XDOT =        1088
548930
 YDOT =      16161
851961  feet/sec       YDOT =        4938
456804  meter/sec
 ZDOT =     -19021
367632                 ZDOT =       -5792
358755

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14561010
30                 X    =        -4438195
94
 Y    =       15911291
87  feet           Y    =         4849761
76  meter
 Z    =       -4850316
98                 Z    =        -1478376
61
 XDOT =      -7800
806119                 XDOT =       -2377
685705
 YDOT =     -12906
172611  feet/sec       YDOT =       -3933
801412  meter/sec
 ZDOT =     -19000
206098                 ZDOT =       -5791
262819


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   08214
72242073  
00020000  00000-0  20000-3 0  9102
2 25544  51
6409 142
3611 0010187  17
7396 342
4120 15
72773057 35700


Satellite: ISS
Catalog Number: 25544
Epoch time:      08214
72242073   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       142
3611  deg
Eccentricity:     
0010187     
Arg of perigee:    17
7396  deg
Mean anomaly:     342
4120  deg
Mean motion:   15
72773057  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3570
Checksum:              264


Coasting Arc #12 (Orbit 3585)
---------------------------------------

Vector Time (GMT): 2008/215/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1737730
05                 A    =         6723987
54  meter
 Y    =       -3941020
02  meter          E    =           
0013942
 Z    =        5159488
23                 I    =           51
84737
 XDOT =       6156
886984                 Wp   =           31
11361
 YDOT =      -4440
979917  meter/sec      RA   =          136
43401  deg
 ZDOT =      -1305
285397                 TA   =           71
40644
                                          MA   =           71
25507
                                          Ha   =            194
885  n
mi
                                          Hp   =            183
464

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5701214
08                 X    =        -1718595
04
 Y    =      -12929855
70  feet           Y    =        -3960345
67  meter
 Z    =       16927454
84                 Z    =         5151092
76
 XDOT =      20199
760446                 XDOT =        6212
429825
 YDOT =     -14570
144086  feet/sec       YDOT =       -4371
819425  meter/sec
 ZDOT =      -4282
432405                 ZDOT =       -1275
241352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9966181
66                 X    =         3037692
17
 Y    =       10073238
27  feet           Y    =         3070323
02  meter
 Z    =       16894639
13                 Z    =         5149486
01
 XDOT =     -13090
916417                 XDOT =       -3990
111324
 YDOT =      20013
375687  feet/sec       YDOT =        6100
076909  meter/sec
 ZDOT =      -4166
826485                 ZDOT =       -1270
048713


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   08215
73902490  
00020000  00000-0  20000-3 0  9111
2 25544  51
6408 137
1490 0010268  21
3572 338
8017 15
72825063 35869


Satellite: ISS
Catalog Number: 25544
Epoch time:      08215
73902490   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:       137
1490  deg
Eccentricity:     
0010268     
Arg of perigee:    21
3572  deg
Mean anomaly:     338
8017  deg
Mean motion:   15
72825063  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3586
Checksum:              282


Coasting Arc #13 (Orbit 3601)
---------------------------------------

Vector Time (GMT): 2008/216/16:38:36
255
Vector Time (MET): N/A
Weight (LBS)     : 661018
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4838923
27                 A    =         6735263
88  meter
 Y    =        4604814
76  meter          E    =           
0022994
 Z    =         754246
55                 I    =           51
90456
 XDOT =      -2801
128333                 Wp   =           40
96333
 YDOT =      -3940
758628  meter/sec      RA   =          131
34148  deg
 ZDOT =       6002
893598                 TA   =          327
23337
                                          MA   =          327
37577
                                          Ha   =            194
919  n
mi
                                          Hp   =            183
284

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15875732
51                 X    =        -4893719
32
 Y    =       15107659
98  feet           Y    =         4550396
73  meter
 Z    =        2474562
18                 Z    =          730606
65
 XDOT =      -9190
053587                 XDOT =       -2786
014335
 YDOT =     -12928
998122  feet/sec       YDOT =       -3971
998220  meter/sec
 ZDOT =      19694
532801                 ZDOT =        5989
322526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9237487
91                 X    =         2815586
32
 Y    =      -19884428
69  feet           Y    =        -6060773
87  meter
 Z    =        2383703
70                 Z    =          726552
89
 XDOT =      11947
797969                 XDOT =        3641
688821
 YDOT =       7939
902018  feet/sec       YDOT =        2420
082135  meter/sec
 ZDOT =      19641
722742                 ZDOT =        5986
797092


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   08216
75561895  
00020000  00000-0  20000-3 0  9125
2 25544  51
6397 131
9367 0010248  25
1321 335
0338 15
72841324 36025


Satellite: ISS
Catalog Number: 25544
Epoch time:      08216
75561895   =   yrday
fracday
Element set:     912
Inclination:       51
6397  deg
RA of node:       131
9367  deg
Eccentricity:     
0010248     
Arg of perigee:    25
1321  deg
Mean anomaly:     335
0338  deg
Mean motion:   15
72841324  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3602
Checksum:              282

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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