Date: July 11th 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


There are no maneuvers



Coasting Arc #1 (Orbit 3204)
---------------------------------------

Vector Time (GMT): 2008/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3523784
24                 A    =         6718648
49  meter
 Y    =       -2911201
73  meter          E    =           
0006519
 Z    =        4919625
50                 I    =           51
30101
 XDOT =       2789
875670                 Wp   =           30
26263
 YDOT =       6877
170536  meter/sec      RA   =          260
86643  deg
 ZDOT =       2075
644204                 TA   =           39
57223
                                          MA   =           39
52465
                                          Ha   =            190
080  n
mi
                                          Hp   =            181
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11560971
93                 X    =         3532177
37
 Y    =       -9551186
78  feet           Y    =        -2871750
39  meter
 Z    =       16140503
62                 Z    =         4936763
99
 XDOT =       9153
135401                 XDOT =        2702
683670
 YDOT =      22562
895458  feet/sec       YDOT =        6907
880774  meter/sec
 ZDOT =       6809
856313                 ZDOT =        2088
986331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12493345
25                 X    =        -3807971
63
 Y    =       -8165163
30  feet           Y    =        -2488741
77  meter
 Z    =       16206280
59                 Z    =         4939674
33
 XDOT =      18304
786720                 XDOT =        5579
298992
 YDOT =     -14416
570036  feet/sec       YDOT =       -4394
170547  meter/sec
 ZDOT =       6861
882585                 ZDOT =        2091
501812


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   08191
55117999  
00020000  00000-0  20000-3 0  9004
2 25544  51
6396 261
3770 0009221 348
7281  11
3674 15
75014161 32058


Satellite: ISS
Catalog Number: 25544
Epoch time:      08191
55117999   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:       261
3770  deg
Eccentricity:     
0009221     
Arg of perigee:   348
7281  deg
Mean anomaly:      11
3674  deg
Mean motion:   15
75014161  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3205
Checksum:              284


Coasting Arc #2 (Orbit 3219)
---------------------------------------

Vector Time (GMT): 2008/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2746730
41                 A    =         6728425
57  meter
 Y    =       -5948939
42  meter          E    =           
0016505
 Z    =       -1485938
80                 I    =           51
33890
 XDOT =       3936
573230                 Wp   =           13
62600
 YDOT =      -3252
551303  meter/sec      RA   =          255
66944  deg
 ZDOT =       5773
659323                 TA   =          329
92097
                                          MA   =          330
01566
                                          Ha   =            190
411  n
mi
                                          Hp   =            181
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9011582
72                 X    =        -2672785
89
 Y    =      -19517517
78  feet           Y    =        -5979241
30  meter
 Z    =       -4875127
29                 Z    =        -1499103
50
 XDOT =      12915
266502                 XDOT =        3944
603901
 YDOT =     -10671
100075  feet/sec       YDOT =       -3208
486096  meter/sec
 ZDOT =      18942
451848                 ZDOT =        5792
802239

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15778318
66                 X    =        -4809231
53
 Y    =       14583700
33  feet           Y    =         4445111
86  meter
 Z    =       -4926391
59                 Z    =        -1501564
16
 XDOT =     -13047
624347                 XDOT =       -3976
915901
 YDOT =      -7724
388245  feet/sec       YDOT =       -2354
393537  meter/sec
 ZDOT =      19015
922800                 ZDOT =        5796
053269


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   08192
50291724  
00020000  00000-0  20000-3 0  9010
2 25544  51
6390 256
4824 0009481 352
8317   7
2710 15
74973309 32200


Satellite: ISS
Catalog Number: 25544
Epoch time:      08192
50291724   =   yrday
fracday
Element set:     901
Inclination:       51
6390  deg
RA of node:       256
4824  deg
Eccentricity:     
0009481     
Arg of perigee:   352
8317  deg
Mean anomaly:       7
2710  deg
Mean motion:   15
74973309  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3220
Checksum:              282


Coasting Arc #3 (Orbit 3235)
---------------------------------------

Vector Time (GMT): 2008/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3386219
50                 A    =         6717807
07  meter
 Y    =        2740957
14  meter          E    =           
0017915
 Z    =       -5127516
43                 I    =           51
31159
 XDOT =      -3480
029544                 Wp   =           48
76854
 YDOT =      -6735
362218  meter/sec      RA   =          250
52873  deg
 ZDOT =      -1293
521415                 TA   =          208
73867
                                          MA   =          208
83749
                                          Ha   =            190
502  n
mi
                                          Hp   =            181
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11109644
03                 X    =        -3391709
14
 Y    =        8992641
55  feet           Y    =         2703060
51  meter
 Z    =      -16822560
47                 Z    =        -5143979
62
 XDOT =     -11417
419764                 XDOT =       -3398
171328
 YDOT =     -22097
645072  feet/sec       YDOT =       -6773
820031  meter/sec
 ZDOT =      -4243
836664                 ZDOT =       -1310
229481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12090414
25                 X    =         3685158
26
 Y    =        7482213
61  feet           Y    =         2280578
71  meter
 Z    =      -16885754
23                 Z    =        -5146777
89
 XDOT =     -16633
742970                 XDOT =       -5069
964857
 YDOT =      17089
922051  feet/sec       YDOT =        5209
008241  meter/sec
 ZDOT =      -4308
831085                 ZDOT =       -1313
331715


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   08193
51809229  
00020000  00000-0  20000-3 0  9028
2 25544  51
6387 251
2607 0009375 357
0949   3
0159 15
75009458 32362


Satellite: ISS
Catalog Number: 25544
Epoch time:      08193
51809229   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:       251
2607  deg
Eccentricity:     
0009375     
Arg of perigee:   357
0949  deg
Mean anomaly:       3
0159  deg
Mean motion:   15
75009458  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3236
Checksum:              302


Coasting Arc #4 (Orbit 3251)
---------------------------------------

Vector Time (GMT): 2008/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3327390
50                 A    =         6728859
01  meter
 Y    =        5799324
13  meter          E    =           
0011172
 Z    =         756586
65                 I    =           51
36103
 XDOT =      -3855
836539                 Wp   =           82
47067
 YDOT =       2998
300447  meter/sec      RA   =          245
34477  deg
 ZDOT =      -5948
283067                 TA   =           89
25270
                                          MA   =           89
12469
                                          Ha   =            190
635  n
mi
                                          Hp   =            181
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10916635
49                 X    =         3258618
88
 Y    =       19026653
96  feet           Y    =         5836148
28  meter
 Z    =        2482239
66                 Z    =          772584
96
 XDOT =     -12650
382347                 XDOT =       -3860
181791
 YDOT =       9836
943724  feet/sec       YDOT =        2955
158908  meter/sec
 ZDOT =     -19515
364392                 ZDOT =       -5967
024786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14149776
22                 X    =         4312851
79
 Y    =      -16752843
49  feet           Y    =        -5106266
69  meter
 Z    =        2544419
97                 Z    =          775539
21
 XDOT =      12310
800146                 XDOT =        3752
331885
 YDOT =       7385
850643  feet/sec       YDOT =        2251
207276  meter/sec
 ZDOT =     -19587
319685                 ZDOT =       -5970
215040


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   08194
53325490  
00020000  00000-0  20000-3 0  9035
2 25544  51
6392 246
0390 0009588   1
7130 358
4065 15
75073976 32527


Satellite: ISS
Catalog Number: 25544
Epoch time:      08194
53325490   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:       246
0390  deg
Eccentricity:     
0009588     
Arg of perigee:     1
7130  deg
Mean anomaly:     358
4065  deg
Mean motion:   15
75073976  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3252
Checksum:              294


Coasting Arc #5 (Orbit 3267)
---------------------------------------

Vector Time (GMT): 2008/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3383735
80                 A    =         6717094
04  meter
 Y    =       -2509547
29  meter          E    =           
0009189
 Z    =        5228298
63                 I    =           51
33418
 XDOT =       4131
902846                 Wp   =           22
03613
 YDOT =       6489
637280  meter/sec      RA   =          240
19194  deg
 ZDOT =        448
980124                 TA   =           63
73192
                                          MA   =           63
63753
                                          Ha   =            190
613  n
mi
                                          Hp   =            180
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11101495
39                 X    =         3386148
40
 Y    =       -8233422
87  feet           Y    =        -2471695
83  meter
 Z    =       17153210
72                 Z    =         5244742
21
 XDOT =      13556
111698                 XDOT =        4056
846541
 YDOT =      21291
460892  feet/sec       YDOT =        6535
422848  meter/sec
 ZDOT =       1473
031902                 ZDOT =         468
871670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11628174
31                 X    =        -3544267
53
 Y    =       -7324455
26  feet           Y    =        -2232493
96  meter
 Z    =       17216358
72                 Z    =         5247546
14
 XDOT =      14492
523960                 XDOT =        4417
321303
 YDOT =     -19426
705517  feet/sec       YDOT =       -5921
259842  meter/sec
 ZDOT =       1550
286979                 ZDOT =         472
527471


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   08195
54840655  
00020000  00000-0  20000-3 0  9043
2 25544  51
6385 240
8176 0009523   5
6254 354
5015 15
75078550 32684


Satellite: ISS
Catalog Number: 25544
Epoch time:      08195
54840655   =   yrday
fracday
Element set:     904
Inclination:       51
6385  deg
RA of node:       240
8176  deg
Eccentricity:     
0009523     
Arg of perigee:     5
6254  deg
Mean anomaly:     354
5015  deg
Mean motion:   15
75078550  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3268
Checksum:              299


Coasting Arc #6 (Orbit 3282)
---------------------------------------

Vector Time (GMT): 2008/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3869673
85                 A    =         6729220
21  meter
 Y    =       -5490207
95  meter          E    =           
0020963
 Z    =         -29576
58                 I    =           51
39027
 XDOT =       3922
061347                 Wp   =           29
42888
 YDOT =      -2787
056246  meter/sec      RA   =          235
02407  deg
 ZDOT =       6024
962987                 TA   =          330
24826
                                          MA   =          330
36730
                                          Ha   =            190
937  n
mi
                                          Hp   =            180
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12695780
36                 X    =        -3807850
20
 Y    =      -18012493
29  feet           Y    =        -5533135
19  meter
 Z    =         -97036
02                 Z    =          -48226
20
 XDOT =      12867
655339                 XDOT =        3923
667130
 YDOT =      -9143
885323  feet/sec       YDOT =       -2743
189638  meter/sec
 ZDOT =      19766
938935                 ZDOT =        6044
019656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11953846
04                 X    =        -3643532
27
 Y    =       18512672
15  feet           Y    =         5642662
47  meter
 Z    =        -169423
21                 Z    =          -51640
19
 XDOT =     -11902
045433                 XDOT =       -3627
743448
 YDOT =      -7534
984438  feet/sec       YDOT =       -2296
663257  meter/sec
 ZDOT =      19840
139418                 ZDOT =        6047
274495


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   08196
50010173  
00020000  00000-0  20000-3 0  9055
2 25544  51
6384 235
9223 0009808   9
6268 350
5082 15
75040987 32836


Satellite: ISS
Catalog Number: 25544
Epoch time:      08196
50010173   =   yrday
fracday
Element set:     905
Inclination:       51
6384  deg
RA of node:       235
9223  deg
Eccentricity:     
0009808     
Arg of perigee:     9
6268  deg
Mean anomaly:     350
5082  deg
Mean motion:   15
75040987  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3283
Checksum:              293


Coasting Arc #7 (Orbit 3298)
---------------------------------------

Vector Time (GMT): 2008/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3496668
72                 A    =         6717070
97  meter
 Y    =        2354510
68  meter          E    =           
0019224
 Z    =       -5243907
49                 I    =           51
36806
 XDOT =      -4694
904506                 Wp   =           63
65021
 YDOT =      -6077
277295  meter/sec      RA   =          229
85851  deg
 ZDOT =        411
461021                 TA   =          210
22148
                                          MA   =          210
33250
                                          Ha   =            190
937  n
mi
                                          Hp   =            180
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11472010
23                 X    =        -3497263
62
 Y    =        7724772
57  feet           Y    =         2315406
59  meter
 Z    =      -17204420
89                 Z    =        -5260895
16
 XDOT =     -15403
230005                 XDOT =       -4628
597276
 YDOT =     -19938
573804  feet/sec       YDOT =       -6129
407745  meter/sec
 ZDOT =       1349
937733                 ZDOT =         388
813276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11549282
23                 X    =         3520221
22
 Y    =        7459426
65  feet           Y    =         2273633
24  meter
 Z    =      -17269692
01                 Z    =        -5263802
13
 XDOT =     -11803
873281                 XDOT =       -3597
820576
 YDOT =      21125
220396  feet/sec       YDOT =        6438
967177  meter/sec
 ZDOT =       1262
072353                 ZDOT =         384
679653


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   08197
51523144  
00020000  00000-0  20000-3 0  9065
2 25544  51
6389 230
7004 0009643  13
3597 346
7820 15
75081720 32999


Satellite: ISS
Catalog Number: 25544
Epoch time:      08197
51523144   =   yrday
fracday
Element set:     906
Inclination:       51
6389  deg
RA of node:       230
7004  deg
Eccentricity:     
0009643     
Arg of perigee:    13
3597  deg
Mean anomaly:     346
7820  deg
Mean motion:   15
75081720  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3299
Checksum:              296


Coasting Arc #8 (Orbit 3314)
---------------------------------------

Vector Time (GMT): 2008/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4303793
68                 A    =         6728740
18  meter
 Y    =        5117754
73  meter          E    =           
0009768
 Z    =        -764294
86                 I    =           51
42691
 XDOT =      -4129
076141                 Wp   =           83
72554
 YDOT =       2592
910967  meter/sec      RA   =          224
70766  deg
 ZDOT =      -5952
895011                 TA   =          104
62624
                                          MA   =          104
51792
                                          Ha   =            191
047  n
mi
                                          Hp   =            180
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14120058
00                 X    =         4249959
02
 Y    =       16790533
90  feet           Y    =         5165581
36  meter
 Z    =       -2507529
06                 Z    =         -743517
09
 XDOT =     -13546
837734                 XDOT =       -4128
845889
 YDOT =       8506
925745  feet/sec       YDOT =        2546
739677  meter/sec
 ZDOT =     -19530
495442                 ZDOT =       -5972
952764

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9609097
00                 X    =         2928852
76
 Y    =      -19732231
34  feet           Y    =        -6014384
11  meter
 Z    =       -2426946
59                 Z    =         -739733
32
 XDOT =      11788
485052                 XDOT =        3593
130244
 YDOT =       8125
603460  feet/sec       YDOT =        2476
683935  meter/sec
 ZDOT =     -19607
586992                 ZDOT =       -5976
392515


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   08198
53034922  
00020000  00000-0  20000-3 0  9070
2 25544  51
6381 225
4782 0009719  17
9297 342
2208 15
75122395 33150


Satellite: ISS
Catalog Number: 25544
Epoch time:      08198
53034922   =   yrday
fracday
Element set:     907
Inclination:       51
6381  deg
RA of node:       225
4782  deg
Eccentricity:     
0009719     
Arg of perigee:    17
9297  deg
Mean anomaly:     342
2208  deg
Mean motion:   15
75122395  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3315
Checksum:              302


Coasting Arc #9 (Orbit 3330)
---------------------------------------

Vector Time (GMT): 2008/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3737926
88                 A    =         6717378
30  meter
 Y    =       -2212826
91  meter          E    =           
0013521
 Z    =        5119982
54                 I    =           51
40951
 XDOT =       5132
491240                 Wp   =           31
87815
 YDOT =       5596
318354  meter/sec      RA   =          219
52917  deg
 ZDOT =      -1315
462448                 TA   =           70
80902
                                          MA   =           70
66274
                                          Ha   =            191
019  n
mi
                                          Hp   =            179
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12263539
62                 X    =         3737521
72
 Y    =       -7259930
82  feet           Y    =        -2171030
45  meter
 Z    =       16797842
97                 Z    =         5138139
71
 XDOT =      16838
882021                 XDOT =        5075
921034
 YDOT =      18360
624522  feet/sec       YDOT =        5653
396750  meter/sec
 ZDOT =      -4315
821681                 ZDOT =       -1290
665619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11712117
65                 X    =        -3569853
46
 Y    =       -7973535
39  feet           Y    =        -2430333
59  meter
 Z    =       16867648
37                 Z    =         5141259
22
 XDOT =       8960
239332                 XDOT =        2731
080948
 YDOT =     -22177
166625  feet/sec       YDOT =       -6759
600387  meter/sec
 ZDOT =      -4219
681733                 ZDOT =       -1286
158992


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   08199
54545525  
00020000  00000-0  20000-3 0  9089
2 25544  51
6370 220
2560 0009788  21
8858 338
2722 15
75148689 33316


Satellite: ISS
Catalog Number: 25544
Epoch time:      08199
54545525   =   yrday
fracday
Element set:     908
Inclination:       51
6370  deg
RA of node:       220
2560  deg
Eccentricity:     
0009788     
Arg of perigee:    21
8858  deg
Mean anomaly:     338
2722  deg
Mean motion:   15
75148689  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3331
Checksum:              317


Coasting Arc #10 (Orbit 3346)
---------------------------------------

Vector Time (GMT): 2008/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4620876
27                 A    =         6727950
30  meter
 Y    =       -4629121
78  meter          E    =           
0022767
 Z    =        1518603
46                 I    =           51
46857
 XDOT =       4444
031913                 Wp   =           47
11006
 YDOT =      -2529
297618  meter/sec      RA   =          214
39640  deg
 ZDOT =       5773
407714                 TA   =          329
69457
                                          MA   =          329
82603
                                          Ha   =            191
218  n
mi
                                          Hp   =            179
829

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15160355
20                 X    =        -4576146
21
 Y    =      -15187407
41  feet           Y    =        -4680545
22  meter
 Z    =        4982294
82                 Z    =         1496263
57
 XDOT =      14580
157194                 XDOT =        4443
939012
 YDOT =      -8298
220532  feet/sec       YDOT =       -2479
603363  meter/sec
 ZDOT =      18941
626358                 ZDOT =        5794
995766

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7021913
73                 X    =        -2140279
31
 Y    =       20298812
55  feet           Y    =         6187078
07  meter
 Z    =        4895703
42                 Z    =         1492210
40
 XDOT =     -12308
304707                 XDOT =       -3751
571275
 YDOT =      -8877
661034  feet/sec       YDOT =       -2705
911083  meter/sec
 ZDOT =      19024
637800                 ZDOT =        5798
709602


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   08200
56055035  
00020000  00000-0  20000-3 0  9097
2 25544  51
6371 215
0342 0009867  25
3862 334
7785 15
75150721 33476


Satellite: ISS
Catalog Number: 25544
Epoch time:      08200
56055035   =   yrday
fracday
Element set:     909
Inclination:       51
6371  deg
RA of node:       215
0342  deg
Eccentricity:     
0009867     
Arg of perigee:    25
3862  deg
Mean anomaly:     334
7785  deg
Mean motion:   15
75150721  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3347
Checksum:              285


Coasting Arc #11 (Orbit 3361)
---------------------------------------

Vector Time (GMT): 2008/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4032377
42                 A    =         6718355
16  meter
 Y    =        2222194
67  meter          E    =           
0017621
 Z    =       -4905441
09                 I    =           51
46145
 XDOT =      -5407
106132                 Wp   =           73
18821
 YDOT =      -5015
886846  meter/sec      RA   =          209
20750  deg
 ZDOT =       2183
998810                 TA   =          218
03399
                                          MA   =          218
15853
                                          Ha   =            191
237  n
mi
                                          Hp   =            179
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13229584
72                 X    =        -4033097
42
 Y    =        7290664
94  feet           Y    =         2177098
98  meter
 Z    =      -16093966
84                 Z    =        -4925031
41
 XDOT =     -17739
849515                 XDOT =       -5361
225071
 YDOT =     -16456
321673  feet/sec       YDOT =       -5076
095982  meter/sec
 ZDOT =       7165
350426                 ZDOT =        2157
842371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12445775
47                 X    =         3793472
36
 Y    =        8417102
30  feet           Y    =         2565532
78  meter
 Z    =      -16169308
51                 Z    =        -4928405
23
 XDOT =      -6016
778608                 XDOT =       -1833
914120
 YDOT =      22394
601754  feet/sec       YDOT =        6825
874615  meter/sec
 ZDOT =       7063
986423                 ZDOT =        2153
103062


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   08201
51219030  
00020000  00000-0  20000-3 0  9102
2 25544  51
6372 210
1382 0009831  28
4017 331
7681 15
75148941 33624


Satellite: ISS
Catalog Number: 25544
Epoch time:      08201
51219030   =   yrday
fracday
Element set:     910
Inclination:       51
6372  deg
RA of node:       210
1382  deg
Eccentricity:     
0009831     
Arg of perigee:    28
4017  deg
Mean anomaly:     331
7681  deg
Mean motion:   15
75148941  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3362
Checksum:              258


Coasting Arc #12 (Orbit 3377)
---------------------------------------

Vector Time (GMT): 2008/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4777237
24                 A    =         6726558
53  meter
 Y    =        4144331
36  meter          E    =           
0010251
 Z    =       -2306263
95                 I    =           51
51441
 XDOT =      -4826
413727                 Wp   =           67
19565
 YDOT =       2558
297318  meter/sec      RA   =          204
08919  deg
 ZDOT =      -5415
473215                 TA   =          138
75989
                                          MA   =          138
68241
                                          Ha   =            191
330  n
mi
                                          Hp   =            179
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15673350
53                 X    =         4741742
80
 Y    =       13596887
67  feet           Y    =         4197554
98  meter
 Z    =       -7566482
78                 Z    =        -2283142
34
 XDOT =     -15834
690704                 XDOT =       -4828
355454
 YDOT =       8393
363903  feet/sec       YDOT =        2504
315356  meter/sec
 ZDOT =     -17767
300574                 ZDOT =       -5438
923880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4666859
65                 X    =         1422458
82
 Y    =      -20250862
09  feet           Y    =        -6172462
76  meter
 Z    =       -7476893
65                 Z    =        -2278957
19
 XDOT =      13300
638500                 XDOT =        4054
034615
 YDOT =       9639
783417  feet/sec       YDOT =        2938
205985  meter/sec
 ZDOT =     -17857
503340                 ZDOT =       -5442
967018


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   08202
52726204  
00020000  00000-0  20000-3 0  9111
2 25544  51
6361 204
9149 0009856  32
8368 327
3406 15
75179460 33782


Satellite: ISS
Catalog Number: 25544
Epoch time:      08202
52726204   =   yrday
fracday
Element set:     911
Inclination:       51
6361  deg
RA of node:       204
9149  deg
Eccentricity:     
0009856     
Arg of perigee:    32
8368  deg
Mean anomaly:     327
3406  deg
Mean motion:   15
75179460  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3378
Checksum:              295

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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