Date: April 24th 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


116/04:28:00 598 -5 5 8 2 8 2
N/A 0 4 -0 2 189 7
000/00:12:01 195 -6 1 -0 0 179 4

Coasting Arc #1 (Orbit 1954)
---------------------------------------

Vector Time (GMT): 2008/112/06:06:59
969
Vector Time (MET): N/A
Weight (LBS)     : 614728
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1938686
34                 A    =         6720074
05  meter
 Y    =        5821766
59  meter          E    =           
0016162
 Z    =        2725385
23                 I    =           51
39666
 XDOT =      -5718
370936                 Wp   =           91
97154
 YDOT =        515
576430  meter/sec      RA   =          309
18755  deg
 ZDOT =      -5143
424142                 TA   =           56
73502
                                          MA   =           56
58027
                                          Ha   =            186
397  n
mi
                                          Hp   =            177
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6360519
48                 X    =        -2016881
83
 Y    =       19100284
08  feet           Y    =         5799649
86  meter
 Z    =        8941552
59                 Z    =         2715777
00
 XDOT =     -18761
059502                 XDOT =       -5698
724889
 YDOT =       1691
523722  feet/sec       YDOT =         451
740211  meter/sec
 ZDOT =     -16874
751123                 ZDOT =       -5171
156790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19697344
41                 X    =        -6003750
58
 Y    =        4235457
57  feet           Y    =         1290967
47  meter
 Z    =        8905276
26                 Z    =         2714328
20
 XDOT =     -10672
247417                 XDOT =       -3252
901013
 YDOT =     -13750
957899  feet/sec       YDOT =       -4191
291968  meter/sec
 ZDOT =     -16981
072408                 ZDOT =       -5175
830870


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   08112
29205406  
00020000  00000-0  20000-3 0  9009
2 25544  51
6398 309
6023 0003397  54
2033 305
9447 15
77129976 19552


Satellite: ISS
Catalog Number: 25544
Epoch time:      08112
29205406   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:       309
6023  deg
Eccentricity:     
0003397     
Arg of perigee:    54
2033  deg
Mean anomaly:     305
9447  deg
Mean motion:   15
77129976  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1955
Checksum:              293


Coasting Arc #2 (Orbit 1970)
---------------------------------------

Vector Time (GMT): 2008/113/06:06:59
969
Vector Time (MET): N/A
Weight (LBS)     : 614728
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4541093
11                 A    =         6712402
51  meter
 Y    =         316111
15  meter          E    =           
0007892
 Z    =        4926873
01                 I    =           51
35396
 XDOT =      -2705
828944                 Wp   =          101
33920
 YDOT =       6925
171348  meter/sec      RA   =          304
04895  deg
 ZDOT =       2045
344869                 TA   =          328
78420
                                          MA   =          328
83105
                                          Ha   =            186
162  n
mi
                                          Hp   =            177
857

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14898599
44                 X    =         4513286
48
 Y    =        1037110
07  feet           Y    =          366736
64  meter
 Z    =       16164281
52                 Z    =         4948866
52
 XDOT =      -8877
391549                 XDOT =       -2793
002292
 YDOT =      22720
378437  feet/sec       YDOT =        6894
425755  meter/sec
 ZDOT =       6710
449046                 ZDOT =        2031
988140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6892480
91                 X    =         2100828
18
 Y    =       13145424
51  feet           Y    =         4006725
39  meter
 Z    =       16248673
21                 Z    =         4952595
59
 XDOT =     -23058
780675                 XDOT =       -7028
316350
 YDOT =       3840
885599  feet/sec       YDOT =        1170
701931  meter/sec
 ZDOT =       6659
900937                 ZDOT =        2029
937805


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   08113
30585955  
00020000  00000-0  20000-3 0  9013
2 25544  51
6398 304
3713 0003284  57
4670 302
6812 15
77183020 19715


Satellite: ISS
Catalog Number: 25544
Epoch time:      08113
30585955   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       304
3713  deg
Eccentricity:     
0003284     
Arg of perigee:    57
4670  deg
Mean anomaly:     302
6812  deg
Mean motion:   15
77183020  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1971
Checksum:              280


Coasting Arc #3 (Orbit 1985)
---------------------------------------

Vector Time (GMT): 2008/114/06:06:59
969
Vector Time (MET): N/A
Weight (LBS)     : 614728
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2677889
59                 A    =         6722909
33  meter
 Y    =       -6113798
14  meter          E    =           
0013815
 Z    =        -755803
90                 I    =           51
37429
 XDOT =       4701
973523                 Wp   =           43
89810
 YDOT =       1332
086360  meter/sec      RA   =          298
84494  deg
 ZDOT =       5958
822936                 TA   =          307
82112
                                          MA   =          307
94609
                                          Ha   =            186
340  n
mi
                                          Hp   =            177
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8785726
99                 X    =         2749727
63
 Y    =      -20058392
84  feet           Y    =        -6083450
74  meter
 Z    =       -2479671
60                 Z    =         -742620
27
 XDOT =      15426
422321                 XDOT =        4657
781070
 YDOT =       4370
362073  feet/sec       YDOT =        1384
419149  meter/sec
 ZDOT =      19549
944017                 ZDOT =        5981
558242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21635596
34                 X    =         6594529
77
 Y    =       -3416782
28  feet           Y    =        -1041435
24  meter
 Z    =       -2429704
34                 Z    =         -740573
88
 XDOT =       4336
704797                 XDOT =        1321
827622
 YDOT =      13674
253194  feet/sec       YDOT =        4167
912374  meter/sec
 ZDOT =      19637
283784                 ZDOT =        5985
444097


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   08114
25628615  
00020000  00000-0  20000-3 0  9020
2 25544  51
6401 299
4671 0003381  58
4024 301
7470 15
77176503 19863


Satellite: ISS
Catalog Number: 25544
Epoch time:      08114
25628615   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       299
4671  deg
Eccentricity:     
0003381     
Arg of perigee:    58
4024  deg
Mean anomaly:     301
7470  deg
Mean motion:   15
77176503  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1986
Checksum:              285


Coasting Arc #4 (Orbit 2001)
---------------------------------------

Vector Time (GMT): 2008/115/06:06:59
969
Vector Time (MET): N/A
Weight (LBS)     : 614728
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3669367
69                 A    =         6710975
28  meter
 Y    =       -2073259
12  meter          E    =           
0017980
 Z    =       -5237903
20                 I    =           51
32230
 XDOT =       3361
811839                 Wp   =           87
30376
 YDOT =      -6909
125815  meter/sec      RA   =          293
66773  deg
 ZDOT =        381
632172                 TA   =          186
32813
                                          MA   =          186
35087
                                          Ha   =            186
284  n
mi
                                          Hp   =            177
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12038607
90                 X    =        -3620466
30
 Y    =       -6802031
23  feet           Y    =        -2114018
35  meter
 Z    =      -17184721
78                 Z    =        -5255610
60
 XDOT =      11029
566400                 XDOT =        3436
966977
 YDOT =     -22667
735615  feet/sec       YDOT =       -6871
111923  meter/sec
 ZDOT =       1252
074055                 ZDOT =         398
146238

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -953618
16                 X    =         -290662
81
 Y    =      -13709124
39  feet           Y    =        -4178541
11  meter
 Z    =      -17252851
72                 Z    =        -5258669
21
 XDOT =      23977
613480                 XDOT =        7308
376589
 YDOT =      -3314
434063  feet/sec       YDOT =       -1010
239502  meter/sec
 ZDOT =       1314
740634                 ZDOT =         400
732945


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   08115
27005408  
00020000  00000-0  20000-3 0  9033
2 25544  51
6409 294
2358 0003389  61
8010 298
3497 15
77226915 20020


Satellite: ISS
Catalog Number: 25544
Epoch time:      08115
27005408   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       294
2358  deg
Eccentricity:     
0003389     
Arg of perigee:    61
8010  deg
Mean anomaly:     298
3497  deg
Mean motion:   15
77226915  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2002
Checksum:              285


Coasting Arc #5 (Orbit 2016)
---------------------------------------

Vector Time (GMT): 2008/116/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2752976
20                 A    =         6727280
15  meter
 Y    =        6076849
55  meter          E    =           
0017205
 Z    =        -805435
15                 I    =           51
35106
 XDOT =      -4123
603711                 Wp   =          139
01890
 YDOT =      -2645
305400  meter/sec      RA   =          288
83145  deg
 ZDOT =      -5948
239623                 TA   =           49
80931
                                          MA   =           49
65883
                                          Ha   =            189
746  n
mi
                                          Hp   =            179
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9032074
16                 X    =        -2816811
17
 Y    =       19937170
43  feet           Y    =         6045707
33  meter
 Z    =       -2642503
77                 Z    =         -818963
92
 XDOT =     -13528
883565                 XDOT =       -4064
821199
 YDOT =      -8678
823490  feet/sec       YDOT =       -2691
088823  meter/sec
 ZDOT =     -19515
221861                 ZDOT =       -5968
129724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21319588
38                 X    =        -6498210
54
 Y    =       -4926513
74  feet           Y    =        -1501601
39  meter
 Z    =       -2693801
82                 Z    =         -821070
79
 XDOT =       5515
921069                 XDOT =        1681
252742
 YDOT =     -13306
067114  feet/sec       YDOT =       -4055
689256  meter/sec
 ZDOT =     -19591
785780                 ZDOT =       -5971
576306


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   08116
22048255  
00020000  00000-0  20000-3 0  9047
2 25544  51
6400 289
3315 0006872 136
6595 223
5111 15
75619929 20176


Satellite: ISS
Catalog Number: 25544
Epoch time:      08116
22048255   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       289
3315  deg
Eccentricity:     
0006872     
Arg of perigee:   136
6595  deg
Mean anomaly:     223
5111  deg
Mean motion:   15
75619929  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2017
Checksum:              285


Coasting Arc #6 (Orbit 2032)
---------------------------------------

Vector Time (GMT): 2008/117/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3534893
65                 A    =         6716100
89  meter
 Y    =        2627930
09  meter          E    =           
0008537
 Z    =        5062365
87                 I    =           51
30539
 XDOT =      -2958
475232                 Wp   =          105
57575
 YDOT =       6951
174552  meter/sec      RA   =          283
64065  deg
 ZDOT =      -1542
729643                 TA   =          359
27752
                                          MA   =          359
27875
                                          Ha   =            189
458  n
mi
                                          Hp   =            179
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11597420
12                 X    =         3480652
74
 Y    =        8621817
87  feet           Y    =         2667155
67  meter
 Z    =       16608811
93                 Z    =         5079406
96
 XDOT =      -9706
283570                 XDOT =       -3028
490106
 YDOT =      22805
690787  feet/sec       YDOT =        6917
699822  meter/sec
 ZDOT =      -5061
448959                 ZDOT =       -1557
271638

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5971234
92                 X    =        -1820032
40
 Y    =       13076528
03  feet           Y    =         3985725
74  meter
 Z    =       16674450
48                 Z    =         5082372
50
 XDOT =     -23390
996200                 XDOT =       -7129
575642
 YDOT =      -4157
335909  feet/sec       YDOT =       -1267
155985  meter/sec
 ZDOT =      -5116
546637                 ZDOT =       -1559
523415


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   08117
23525087  
00020000  00000-0  20000-3 0  9053
2 25544  51
6396 284
1080 0006686 140
2546 219
9109 15
75683307 20337


Satellite: ISS
Catalog Number: 25544
Epoch time:      08117
23525087   =   yrday
fracday
Element set:     905
Inclination:       51
6396  deg
RA of node:       284
1080  deg
Eccentricity:     
0006686     
Arg of perigee:   140
2546  deg
Mean anomaly:     219
9109  deg
Mean motion:   15
75683307  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2033
Checksum:              292


Coasting Arc #7 (Orbit 2048)
---------------------------------------

Vector Time (GMT): 2008/118/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2415940
07                 A    =         6725838
67  meter
 Y    =       -5983801
23  meter          E    =           
0017001
 Z    =        1880742
22                 I    =           51
33280
 XDOT =       4031
511991                 Wp   =           89
30289
 YDOT =       3405
147637  meter/sec      RA   =          278
49954  deg
 ZDOT =       5611
666328                 TA   =          291
69684
                                          MA   =          291
87776
                                          Ha   =            189
510  n
mi
                                          Hp   =            179
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7926312
55                 X    =         2473535
95
 Y    =      -19631893
80  feet           Y    =        -5956462
89  meter
 Z    =        6170414
09                 Z    =         1892618
46
 XDOT =      13226
745376                 XDOT =        3965
874855
 YDOT =      11171
744217  feet/sec       YDOT =        3449
862975  meter/sec
 ZDOT =      18410
978766                 ZDOT =        5631
092294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20920434
13                 X    =         6376548
32
 Y    =        3164838
35  feet           Y    =          964642
73  meter
 Z    =        6215378
42                 Z    =         1894447
34
 XDOT =      -7623
881770                 XDOT =       -2323
759163
 YDOT =      13813
829260  feet/sec       YDOT =        4210
455159  meter/sec
 ZDOT =      18485
851809                 ZDOT =        5634
487631


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   08118
25000229  
00020000  00000-0  20000-3 0  9063
2 25544  51
6398 278
8833 0006661 143
4827 216
6793 15
75683062 20493


Satellite: ISS
Catalog Number: 25544
Epoch time:      08118
25000229   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       278
8833  deg
Eccentricity:     
0006661     
Arg of perigee:   143
4827  deg
Mean anomaly:     216
6793  deg
Mean motion:   15
75683062  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2049
Checksum:              308


Coasting Arc #8 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2008/119/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3544359
50                 A    =         6717795
88  meter
 Y    =       -3323219
97  meter          E    =           
0016651
 Z    =       -4655338
32                 I    =           51
30349
 XDOT =       2611
996459                 Wp   =          123
27281
 YDOT =      -6678
634828  meter/sec      RA   =          273
28866  deg
 ZDOT =       2777
057612                 TA   =          174
29775
                                          MA   =          174
27876
                                          Ha   =            189
361  n
mi
                                          Hp   =            179
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11628476
04                 X    =        -3484320
43
 Y    =      -10902952
67  feet           Y    =        -3362519
11  meter
 Z    =      -15273419
70                 Z    =        -4672411
21
 XDOT =       8569
542188                 XDOT =        2672
993376
 YDOT =     -21911
531589  feet/sec       YDOT =       -6649
085072  meter/sec
 ZDOT =       9111
081405                 ZDOT =        2789
894581

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7719010
62                 X    =         2352754
44
 Y    =      -13874329
93  feet           Y    =        -4228895
76  meter
 Z    =      -15339264
17                 Z    =        -4675407
72
 XDOT =      22323
780504                 XDOT =        6804
288298
 YDOT =       2286
437902  feet/sec       YDOT =         696
906273  meter/sec
 ZDOT =       9159
657061                 ZDOT =        2791
863472


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   08119
20131320  
00020000  00000-0  20000-3 0  9077
2 25544  51
6402 273
9853 0006557 147
2004 212
9568 15
75718636 20642


Satellite: ISS
Catalog Number: 25544
Epoch time:      08119
20131320   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:       273
9853  deg
Eccentricity:     
0006557     
Arg of perigee:   147
2004  deg
Mean anomaly:     212
9568  deg
Mean motion:   15
75718636  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2064
Checksum:              281


Coasting Arc #9 (Orbit 2079)
---------------------------------------

Vector Time (GMT): 2008/120/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2182694
24                 A    =         6723406
36  meter
 Y    =        5631551
62  meter          E    =           
0010362
 Z    =       -2950854
35                 I    =           51
32248
 XDOT =      -4119
205253                 Wp   =          135
31358
 YDOT =      -4194
056804  meter/sec      RA   =          268
16216  deg
 ZDOT =      -4975
071057                 TA   =           78
90203
                                          MA   =           78
78553
                                          Ha   =            189
183  n
mi
                                          Hp   =            179
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7161070
33                 X    =        -2231170
14
 Y    =       18476219
23  feet           Y    =         5606872
54  meter
 Z    =       -9681280
67                 Z    =        -2961575
48
 XDOT =     -13514
452930                 XDOT =       -4047
832428
 YDOT =     -13760
028883  feet/sec       YDOT =       -4239
720886  meter/sec
 ZDOT =     -16322
411605                 ZDOT =       -4994
908994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19695274
91                 X    =        -6003119
79
 Y    =       -1990172
93  feet           Y    =         -606604
71  meter
 Z    =       -9721839
28                 Z    =        -2963216
61
 XDOT =       9595
318729                 XDOT =        2924
653149
 YDOT =     -15134
788055  feet/sec       YDOT =       -4613
083399  meter/sec
 ZDOT =     -16398
962779                 ZDOT =       -4998
403855


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   08120
21602698  
00020000  00000-0  20000-3 0  9082
2 25544  51
6405 268
7607 0006481 151
9196 208
2318 15
75737810 20808


Satellite: ISS
Catalog Number: 25544
Epoch time:      08120
21602698   =   yrday
fracday
Element set:     908
Inclination:       51
6405  deg
RA of node:       268
7607  deg
Eccentricity:     
0006481     
Arg of perigee:   151
9196  deg
Mean anomaly:     208
2318  deg
Mean motion:   15
75737810  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2080
Checksum:              292


Coasting Arc #10 (Orbit 2095)
---------------------------------------

Vector Time (GMT): 2008/121/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3693060
03                 A    =         6720142
01  meter
 Y    =        3956041
51  meter          E    =           
0013865
 Z    =        3969748
56                 I    =           51
31363
 XDOT =      -2400
795104                 Wp   =          104
66357
 YDOT =       6187
982041  meter/sec      RA   =          262
93988  deg
 ZDOT =      -3925
219336                 TA   =           26
07279
                                          MA   =           26
00302
                                          Ha   =            188
963  n
mi
                                          Hp   =            179
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12116338
67                 X    =         3629264
06
 Y    =       12979138
82  feet           Y    =         3996982
66  meter
 Z    =       13024109
46                 Z    =         3987534
64
 XDOT =      -7876
624358                 XDOT =       -2450
743555
 YDOT =      20301
778349  feet/sec       YDOT =        6160
855765  meter/sec
 ZDOT =     -12878
016193                 ZDOT =       -3937
003680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9090304
81                 X    =        -2770724
91
 Y    =       15193315
99  feet           Y    =         4630922
71  meter
 Z    =       13092770
62                 Z    =         3990676
48
 XDOT =     -20566
458055                 XDOT =       -6268
656415
 YDOT =      -1146
806499  feet/sec       YDOT =        -349
546621  meter/sec
 ZDOT =     -12922
591048                 ZDOT =       -3938
805751


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   08121
23072207  
00020000  00000-0  20000-3 0  9093
2 25544  51
6399 263
5360 0006361 154
4775 205
6704 15
75787001 20961


Satellite: ISS
Catalog Number: 25544
Epoch time:      08121
23072207   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       263
5360  deg
Eccentricity:     
0006361     
Arg of perigee:   154
4775  deg
Mean anomaly:     205
6704  deg
Mean motion:   15
75787001  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2096
Checksum:              286


Coasting Arc #11 (Orbit 2111)
---------------------------------------

Vector Time (GMT): 2008/122/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2051881
44                 A    =         6720571
52  meter
 Y    =       -5106884
01  meter          E    =           
0015516
 Z    =        3851332
05                 I    =           51
32038
 XDOT =       4385
040596                 Wp   =          119
54223
 YDOT =       4850
476627  meter/sec      RA   =          257
81889  deg
 ZDOT =       4075
674219                 TA   =          287
71720
                                          MA   =          287
88651
                                          Ha   =            188
927  n
mi
                                          Hp   =            179
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6731894
48                 X    =         2090125
68
 Y    =      -16754868
81  feet           Y    =        -5083724
88  meter
 Z    =       12635603
84                 Z    =         3861393
05
 XDOT =      14386
616130                 XDOT =        4310
676845
 YDOT =      15913
637227  feet/sec       YDOT =        4899
096857  meter/sec
 ZDOT =      13371
634578                 ZDOT =        4096
796310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17975887
84                 X    =         5479050
61
 Y    =        1395693
22  feet           Y    =          425407
29  meter
 Z    =       12673674
03                 Z    =         3862935
85
 XDOT =     -10856
353259                 XDOT =       -3309
016473
 YDOT =      17072
596207  feet/sec       YDOT =        5203
727324  meter/sec
 ZDOT =      13453
197258                 ZDOT =        4100
534524


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   08122
24539837  
00020000  00000-0  20000-3 0  9104
2 25544  51
6403 258
3106 0006276 158
3630 201
7800 15
75796422 21125


Satellite: ISS
Catalog Number: 25544
Epoch time:      08122
24539837   =   yrday
fracday
Element set:     910
Inclination:       51
6403  deg
RA of node:       258
3106  deg
Eccentricity:     
0006276     
Arg of perigee:   158
3630  deg
Mean anomaly:     201
7800  deg
Mean motion:   15
75796422  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2112
Checksum:              271


Coasting Arc #12 (Orbit 2126)
---------------------------------------

Vector Time (GMT): 2008/123/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3979041
87                 A    =         6722782
45  meter
 Y    =       -4469677
60  meter          E    =           
0007741
 Z    =       -3074430
22                 I    =           51
33594
 XDOT =       2373
423596                 Wp   =          127
66421
 YDOT =      -5461
726173  meter/sec      RA   =          252
59551  deg
 ZDOT =       4872
318593                 TA   =          196
51517
                                          MA   =          196
54040
                                          Ha   =            188
730  n
mi
                                          Hp   =            179
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13054599
30                 X    =        -3913830
27
 Y    =      -14664296
59  feet           Y    =        -4513808
91  meter
 Z    =      -10086713
33                 Z    =        -3093602
26
 XDOT =       7786
822821                 XDOT =        2410
651911
 YDOT =     -17919
049123  feet/sec       YDOT =       -5434
977028  meter/sec
 ZDOT =      15985
297220                 ZDOT =        4883
939280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9864315
76                 X    =         3006643
44
 Y    =      -16931043
12  feet           Y    =        -5160581
94  meter
 Z    =      -10160757
68                 Z    =        -3096998
94
 XDOT =      18192
333331                 XDOT =        5545
023199
 YDOT =        986
807199  feet/sec       YDOT =         300
778834  meter/sec
 ZDOT =      16029
312159                 ZDOT =        4885
734346


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   08123
19663927  
00020000  00000-0  20000-3 0  9118
2 25544  51
6404 253
4118 0006109 163
3141 196
8225 15
75834628 21275


Satellite: ISS
Catalog Number: 25544
Epoch time:      08123
19663927   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:       253
4118  deg
Eccentricity:     
0006109     
Arg of perigee:   163
3141  deg
Mean anomaly:     196
8225  deg
Mean motion:   15
75834628  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2127
Checksum:              285


Coasting Arc #13 (Orbit 2142)
---------------------------------------

Vector Time (GMT): 2008/124/04:34:01
195
Vector Time (MET): N/A
Weight (LBS)     : 614216
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2163156
28                 A    =         6717594
50  meter
 Y    =        4398306
31  meter          E    =           
0011470
 Z    =       -4602246
37                 I    =           51
32853
 XDOT =      -4723
773149                 Wp   =          101
54911
 YDOT =      -5342
658192  meter/sec      RA   =          247
47026  deg
 ZDOT =      -2893
979985                 TA   =          139
70208
                                          MA   =          139
61702
                                          Ha   =            188
506  n
mi
                                          Hp   =            180
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7096969
43                 X    =        -2189820
75
 Y    =       14430138
82  feet           Y    =         4373967
60  meter
 Z    =      -15099233
49                 Z    =        -4612819
93
 XDOT =     -15497
943402                 XDOT =       -4649
620921
 YDOT =     -17528
406143  feet/sec       YDOT =       -5395
067504  meter/sec
 ZDOT =      -9494
684989                 ZDOT =       -2916
748428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15933460
39                 X    =        -4856518
73
 Y    =       -1872931
08  feet           Y    =         -570869
39  meter
 Z    =      -15139342
88                 Z    =        -4614471
71
 XDOT =      11334
700020                 XDOT =        3454
816566
 YDOT =     -19189
119007  feet/sec       YDOT =       -5848
843473  meter/sec
 ZDOT =      -9582
625858                 ZDOT =       -2920
784362


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   08124
21127868  
00020000  00000-0  20000-3 0  9122
2 25544  51
6403 248
1862 0006001 168
0370 192
0938 15
75868822 21438


Satellite: ISS
Catalog Number: 25544
Epoch time:      08124
21127868   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:       248
1862  deg
Eccentricity:     
0006001     
Arg of perigee:   168
0370  deg
Mean anomaly:     192
0938  deg
Mean motion:   15
75868822  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2143
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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