Date: June 1st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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 2541)
---------------------------------------

Vector Time (GMT): 2008/149/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1775283
29                 A    =         6723784
50  meter
 Y    =       -6269352
48  meter          E    =           
0009153
 Z    =        1637705
08                 I    =           51
94089
 XDOT =       5108
728670                 Wp   =          130
77642
 YDOT =        -64
066750  meter/sec      RA   =          117
15961  deg
 ZDOT =      -5768
180444                 TA   =           31
18933
                                          MA   =           31
13505
                                          Ha   =            184
150  n
mi
                                          Hp   =            181
946

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5824420
23                 X    =         1837300
51
 Y    =      -20568741
73  feet           Y    =        -6249153
65  meter
 Z    =        5373048
17                 Z    =         1646479
48
 XDOT =      16760
920833                 XDOT =        5137
086321
 YDOT =       -210
192748  feet/sec       YDOT =          -6
778898  meter/sec
 ZDOT =     -18924
476521                 ZDOT =       -5743
293217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13632766
58                 X    =        -4155267
25
 Y    =      -16455620
64  feet           Y    =        -5015673
17  meter
 Z    =        5406188
95                 Z    =         1647806
39
 XDOT =       8212
524259                 XDOT =        2503
177394
 YDOT =     -13005
593078  feet/sec       YDOT =       -3964
104770  meter/sec
 ZDOT =     -18828
745676                 ZDOT =       -5739
001682


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   08149
50644650  
00020000  00000-0  20000-3 0  9001
2 25544  51
6344 117
8609 0005717 273
1706  86
8804 15
76537762 25429


Satellite: ISS
Catalog Number: 25544
Epoch time:      08149
50644650   =   yrday
fracday
Element set:     900
Inclination:       51
6344  deg
RA of node:       117
8609  deg
Eccentricity:     
0005717     
Arg of perigee:   273
1706  deg
Mean anomaly:      86
8804  deg
Mean motion:   15
76537762  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2542
Checksum:              302


Coasting Arc #2 (Orbit 2557)
---------------------------------------

Vector Time (GMT): 2008/150/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4178354
92                 A    =         6713185
43  meter
 Y    =        -588044
55  meter          E    =           
0003021
 Z    =        5223871
23                 I    =           51
91710
 XDOT =       2187
113355                 Wp   =          247
21180
 YDOT =      -7328
320205  meter/sec      RA   =          112
04861  deg
 ZDOT =        923
715381                 TA   =          194
02131
                                          MA   =          194
02970
                                          Ha   =            184
339  n
mi
                                          Hp   =            181
984

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13708513
51                 X    =        -4196845
65
 Y    =       -1929280
03  feet           Y    =         -634873
18  meter
 Z    =       17138685
15                 Z    =         5203527
61
 XDOT =       7175
568749                 XDOT =        2264
409945
 YDOT =     -24043
045291  feet/sec       YDOT =       -7303
430550  meter/sec
 ZDOT =       3030
562273                 ZDOT =         934
527559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9254733
26                 X    =        -2820842
70
 Y    =       10424672
97  feet           Y    =         3177440
32  meter
 Z    =       17060366
31                 Z    =         5199999
65
 XDOT =     -15290
088331                 XDOT =       -4660
418923
 YDOT =     -18604
559805  feet/sec       YDOT =       -5670
669828  meter/sec
 ZDOT =       3071
446427                 ZDOT =         936
176871


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   08150
52064834  
00020000  00000-0  20000-3 0  9016
2 25544  51
6343 112
6325 0005766 276
7756  83
2753 15
76531728 25581


Satellite: ISS
Catalog Number: 25544
Epoch time:      08150
52064834   =   yrday
fracday
Element set:     901
Inclination:       51
6343  deg
RA of node:       112
6325  deg
Eccentricity:     
0005766     
Arg of perigee:   276
7756  deg
Mean anomaly:      83
2753  deg
Mean motion:   15
76531728  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2558
Checksum:              299


Coasting Arc #3 (Orbit 2573)
---------------------------------------

Vector Time (GMT): 2008/151/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1993156
32                 A    =         6724858
42  meter
 Y    =        6415735
86  meter          E    =           
0010092
 Z    =          52611
37                 I    =           51
96662
 XDOT =      -4519
526378                 Wp   =           18
90022
 YDOT =      -1456
398088  meter/sec      RA   =          106
90731  deg
 ZDOT =       6069
529552                 TA   =          341
66943
                                          MA   =          341
70578
                                          Ha   =            184
267  n
mi
                                          Hp   =            181
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6539226
76                 X    =        -2065005
53
 Y    =       21049002
17  feet           Y    =         6393045
51  meter
 Z    =         172609
47                 Z    =           42754
57
 XDOT =     -14827
842449                 XDOT =       -4532
389925
 YDOT =      -4778
208951  feet/sec       YDOT =       -1507
010543  meter/sec
 ZDOT =      19913
154698                 ZDOT =        6047
541967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14192337
48                 X    =         4325824
46
 Y    =       16864490
00  feet           Y    =         5140296
55  meter
 Z    =         135302
57                 Z    =           41240
22
 XDOT =     -10855
329472                 XDOT =       -3308
704423
 YDOT =       8965
759123  feet/sec       YDOT =        2732
763381  meter/sec
 ZDOT =      19828
426171                 ZDOT =        6043
704297


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   08151
53483742  
00020000  00000-0  20000-3 0  9022
2 25544  51
6342 107
4036 0005668 279
5141  80
5383 15
76578459 25740


Satellite: ISS
Catalog Number: 25544
Epoch time:      08151
53483742   =   yrday
fracday
Element set:     902
Inclination:       51
6342  deg
RA of node:       107
4036  deg
Eccentricity:     
0005668     
Arg of perigee:   279
5141  deg
Mean anomaly:      80
5383  deg
Mean motion:   15
76578459  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2574
Checksum:              304


Coasting Arc #4 (Orbit 2588)
---------------------------------------

Vector Time (GMT): 2008/152/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3755552
97                 A    =         6713171
04  meter
 Y    =        1975795
09  meter          E    =           
0008775
 Z    =       -5209353
14                 I    =           51
93509
 XDOT =      -2354
418611                 Wp   =           93
63550
 YDOT =       7253
727600  meter/sec      RA   =          101
76437  deg
 ZDOT =       1054
792100                 TA   =          186
38040
                                          MA   =          186
39158
                                          Ha   =            184
496  n
mi
                                          Hp   =            182
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12321368
02                 X    =         3758486
78
 Y    =        6482267
34  feet           Y    =         2017808
84  meter
 Z    =      -17091053
60                 Z    =        -5191100
95
 XDOT =      -7724
470508                 XDOT =       -2440
480036
 YDOT =      23798
318898  feet/sec       YDOT =        7226
917826  meter/sec
 ZDOT =       3460
604003                 ZDOT =        1043
145914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12037137
97                 X    =         3668919
65
 Y    =       -7165536
27  feet           Y    =        -2184055
46  meter
 Z    =      -17020646
66                 Z    =        -5187893
10
 XDOT =      15665
554915                 XDOT =        4774
861138
 YDOT =      18208
283693  feet/sec       YDOT =        5549
884870  meter/sec
 ZDOT =       3416
478635                 ZDOT =        1041
342688


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   08152
48563171  
00020000  00000-0  20000-3 0  9033
2 25544  51
6349 102
5014 0005799 284
8013  75
2508 15
76560020 25892


Satellite: ISS
Catalog Number: 25544
Epoch time:      08152
48563171   =   yrday
fracday
Element set:     903
Inclination:       51
6349  deg
RA of node:       102
5014  deg
Eccentricity:     
0005799     
Arg of perigee:   284
8013  deg
Mean anomaly:      75
2508  deg
Mean motion:   15
76560020  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2589
Checksum:              287


Coasting Arc #5 (Orbit 2604)
---------------------------------------

Vector Time (GMT): 2008/153/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2109783
09                 A    =         6723463
10  meter
 Y    =       -6130256
51  meter          E    =           
0004112
 Z    =       -1771099
93                 I    =           51
97575
 XDOT =       4142
779526                 Wp   =          193
01256
 YDOT =       3077
486053  meter/sec      RA   =           96
65667  deg
 ZDOT =      -5718
386227                 TA   =            6
53158
                                          MA   =            6
52622
                                          Ha   =            184
587  n
mi
                                          Hp   =            181
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6921860
53                 X    =         2186779
65
 Y    =      -20112390
14  feet           Y    =        -6106232
94  meter
 Z    =       -5810695
30                 Z    =        -1760664
25
 XDOT =      13591
796345                 XDOT =        4135
838175
 YDOT =      10096
739020  feet/sec       YDOT =        3123
775017  meter/sec
 ZDOT =     -18761
109669                 ZDOT =       -5698
276572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13746940
57                 X    =        -4190067
49
 Y    =      -16245015
37  feet           Y    =        -4951480
68  meter
 Z    =       -5771106
54                 Z    =        -1759033
27
 XDOT =      14489
033193                 XDOT =        4416
257317
 YDOT =      -5625
216207  feet/sec       YDOT =       -1714
565900  meter/sec
 ZDOT =     -18683
455205                 ZDOT =       -5694
717146


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   08153
49980053  
00020000  00000-0  20000-3 0  9048
2 25544  51
6358  97
2728 0005866 289
3318  70
7212 15
76591359 26057


Satellite: ISS
Catalog Number: 25544
Epoch time:      08153
49980053   =   yrday
fracday
Element set:     904
Inclination:       51
6358  deg
RA of node:        97
2728  deg
Eccentricity:     
0005866     
Arg of perigee:   289
3318  deg
Mean anomaly:      70
7212  deg
Mean motion:   15
76591359  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2605
Checksum:              317


Coasting Arc #6 (Orbit 2620)
---------------------------------------

Vector Time (GMT): 2008/154/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3529954
11                 A    =         6715545
78  meter
 Y    =       -3361693
01  meter          E    =           
0006241
 Z    =        4620212
71                 I    =           51
95191
 XDOT =       2482
161679                 Wp   =           19
51281
 YDOT =      -6669
500757  meter/sec      RA   =           91
48618  deg
 ZDOT =      -2949
444292                 TA   =           99
61320
                                          MA   =           99
54269
                                          Ha   =            184
783  n
mi
                                          Hp   =            181
836

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11581214
26                 X    =        -3514545
38
 Y    =      -11029176
54  feet           Y    =        -3401081
67  meter
 Z    =       15158178
18                 Z    =         4603100
65
 XDOT =       8143
575062                 XDOT =        2570
884763
 YDOT =     -21881
564163  feet/sec       YDOT =       -6641
247189  meter/sec
 ZDOT =      -9676
654501                 ZDOT =       -2937
171408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15360947
98                 X    =        -4682016
95
 Y    =        4670057
12  feet           Y    =         1423433
41  meter
 Z    =       15092033
26                 Z    =         4600051
74
 XDOT =     -14604
353652                 XDOT =       -4451
406993
 YDOT =     -16842
902998  feet/sec       YDOT =       -5133
716834  meter/sec
 ZDOT =      -9630
028091                 ZDOT =       -2935
232562


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   08154
51395864  
00020000  00000-0  20000-3 0  9053
2 25544  51
6365  92
0446 0005892 293
0681  66
9862 15
76604706 26216


Satellite: ISS
Catalog Number: 25544
Epoch time:      08154
51395864   =   yrday
fracday
Element set:     905
Inclination:       51
6365  deg
RA of node:        92
0446  deg
Eccentricity:     
0005892     
Arg of perigee:   293
0681  deg
Mean anomaly:      66
9862  deg
Mean motion:   15
76604706  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2621
Checksum:              311


Coasting Arc #7 (Orbit 2636)
---------------------------------------

Vector Time (GMT): 2008/155/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2250565
51                 A    =         6719970
70  meter
 Y    =        5395377
95  meter          E    =           
0008020
 Z    =        3304530
72                 I    =           51
96732
 XDOT =      -4001
584453                 Wp   =           68
31896
 YDOT =      -4575
195148  meter/sec      RA   =           86
40091  deg
 ZDOT =       4738
511741                 TA   =          330
34494
                                          MA   =          330
39038
                                          Ha   =            184
941  n
mi
                                          Hp   =            181
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7383745
11                 X    =        -2326783
27
 Y    =       17701371
23  feet           Y    =         5369783
98  meter
 Z    =       10841636
21                 Z    =         3293413
31
 XDOT =     -13128
557917                 XDOT =       -3973
145679
 YDOT =     -15010
482768  feet/sec       YDOT =       -4619
785153  meter/sec
 ZDOT =      15546
298363                 ZDOT =        4719
139842

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11947424
56                 X    =         3641575
00
 Y    =       15034390
64  feet           Y    =         4582482
27  meter
 Z    =       10799326
62                 Z    =         3291634
75
 XDOT =     -18418
182510                 XDOT =       -5613
862029
 YDOT =       3508
541370  feet/sec       YDOT =        1069
403410  meter/sec
 ZDOT =      15471
351041                 ZDOT =        4715
667797


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   08155
52810507  
00020000  00000-0  20000-3 0  9062
2 25544  51
6372  86
8160 0005908 296
5616  63
4943 15
76633160 26377


Satellite: ISS
Catalog Number: 25544
Epoch time:      08155
52810507   =   yrday
fracday
Element set:     906
Inclination:       51
6372  deg
RA of node:        86
8160  deg
Eccentricity:     
0005908     
Arg of perigee:   296
5616  deg
Mean anomaly:      63
4943  deg
Mean motion:   15
76633160  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2637
Checksum:              301


Coasting Arc #8 (Orbit 2651)
---------------------------------------

Vector Time (GMT): 2008/156/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3486632
56                 A    =         6719359
85  meter
 Y    =        4538091
09  meter          E    =           
0002621
 Z    =       -3518691
01                 I    =           51
96230
 XDOT =      -2721
945210                 Wp   =          359
78749
 YDOT =       5603
264996  meter/sec      RA   =           81
21721  deg
 ZDOT =       4531
993367                 TA   =          318
52923
                                          MA   =          318
54911
                                          Ha   =            185
159  n
mi
                                          Hp   =            181
719

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11439083
20                 X    =         3452721
08
 Y    =       14888750
31  feet           Y    =         4576891
81  meter
 Z    =      -11544261
83                 Z    =        -3501834
14
 XDOT =      -8930
266438                 XDOT =       -2806
415279
 YDOT =      18383
415340  feet/sec       YDOT =        5572
353318  meter/sec
 ZDOT =      14868
744642                 ZDOT =        4518
566144

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18531857
09                 X    =         5648510
04
 Y    =       -3255828
37  feet           Y    =         -992376
49  meter
 Z    =      -11478995
86                 Z    =        -3498797
94
 XDOT =      11840
337110                 XDOT =        3608
934751
 YDOT =      15181
851032  feet/sec       YDOT =        4627
428195  meter/sec
 ZDOT =      14817
549987                 ZDOT =        4516
389236


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   08156
47885828  
00020000  00000-0  20000-3 0  9076
2 25544  51
6374  81
9144 0006017 300
8876  59
1696 15
76629282 26520


Satellite: ISS
Catalog Number: 25544
Epoch time:      08156
47885828   =   yrday
fracday
Element set:     907
Inclination:       51
6374  deg
RA of node:        81
9144  deg
Eccentricity:     
0006017     
Arg of perigee:   300
8876  deg
Mean anomaly:      59
1696  deg
Mean motion:   15
76629282  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2652
Checksum:              328


Coasting Arc #9 (Orbit 2667)
---------------------------------------

Vector Time (GMT): 2008/157/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2561655
31                 A    =         6715856
95  meter
 Y    =       -4293327
91  meter          E    =           
0008123
 Z    =       -4491516
13                 I    =           51
94606
 XDOT =       4001
302792                 Wp   =           31
81356
 YDOT =       5743
663001  meter/sec      RA   =           76
13302  deg
 ZDOT =      -3204
009916                 TA   =          206
25884
                                          MA   =          206
30005
                                          Ha   =            185
197  n
mi
                                          Hp   =            181
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8404380
95                 X    =         2631292
57
 Y    =      -14085721
48  feet           Y    =        -4264291
64  meter
 Z    =      -14735945
31                 Z    =        -4478903
41
 XDOT =      13127
633832                 XDOT =        3952
343369
 YDOT =      18844
038716  feet/sec       YDOT =        5788
134830  meter/sec
 ZDOT =     -10511
843555                 ZDOT =       -3184
689203

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8759372
88                 X    =        -2669856
85
 Y    =      -13918773
44  feet           Y    =        -4242442
14  meter
 Z    =      -14687763
12                 Z    =        -4476830
20
 XDOT =      21747
520514                 XDOT =        6628
644253
 YDOT =      -2658
160099  feet/sec       YDOT =        -810
207198  meter/sec
 ZDOT =     -10436
988837                 ZDOT =       -3181
194198


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   08157
49298395  
00020000  00000-0  20000-3 0  9087
2 25544  51
6383  76
6858 0005972 305
4452  54
6155 15
76670128 26685


Satellite: ISS
Catalog Number: 25544
Epoch time:      08157
49298395   =   yrday
fracday
Element set:     908
Inclination:       51
6383  deg
RA of node:        76
6858  deg
Eccentricity:     
0005972     
Arg of perigee:   305
4452  deg
Mean anomaly:      54
6155  deg
Mean motion:   15
76670128  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2668
Checksum:              334


Coasting Arc #10 (Orbit 2683)
---------------------------------------

Vector Time (GMT): 2008/158/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3501125
76                 A    =         6722898
32  meter
 Y    =       -5380771
68  meter          E    =           
0008559
 Z    =        1986323
75                 I    =           51
96169
 XDOT =       3212
894335                 Wp   =          100
18366
 YDOT =      -4172
924887  meter/sec      RA   =           70
95819  deg
 ZDOT =      -5622
118358                 TA   =           57
77304
                                          MA   =           57
69011
                                          Ha   =            185
341  n
mi
                                          Hp   =            181
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11486633
06                 X    =        -3450346
06
 Y    =      -17653450
39  feet           Y    =        -5419639
76  meter
 Z    =        6516810
22                 Z    =         1969437
60
 XDOT =      10540
991913                 XDOT =        3286
628943
 YDOT =     -13690
698448  feet/sec       YDOT =       -4136
583035  meter/sec
 ZDOT =     -18445
270205                 ZDOT =       -5606
331951

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20907138
37                 X    =        -6372495
78
 Y    =        2706929
64  feet           Y    =          825072
16  meter
 Z    =        6451353
51                 Z    =         1966372
55
 XDOT =      -7506
670170                 XDOT =       -2288
033068
 YDOT =     -14013
132648  feet/sec       YDOT =       -4271
202831  meter/sec
 ZDOT =     -18384
854159                 ZDOT =       -5603
703548


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   08158
50709877  
00020000  00000-0  20000-3 0  9093
2 25544  51
6385  71
4573 0006008 309
0127  51
0502 15
76672906 26845


Satellite: ISS
Catalog Number: 25544
Epoch time:      08158
50709877   =   yrday
fracday
Element set:     909
Inclination:       51
6385  deg
RA of node:        71
4573  deg
Eccentricity:     
0006008     
Arg of perigee:   309
0127  deg
Mean anomaly:      51
0502  deg
Mean motion:   15
76672906  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2684
Checksum:              300


Coasting Arc #11 (Orbit 2699)
---------------------------------------

Vector Time (GMT): 2008/159/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3111464
56                 A    =         6712878
14  meter
 Y    =        2952323
66  meter          E    =           
0002014
 Z    =        5164527
49                 I    =           51
91748
 XDOT =      -3999
330219                 Wp   =          324
94992
 YDOT =      -6459
378293  meter/sec      RA   =           65
85213  deg
 ZDOT =       1284
919407                 TA   =          112
82924
                                          MA   =          112
80798
                                          Ha   =            185
490  n
mi
                                          Hp   =            181
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10208217
05                 X    =        -3169334
80
 Y    =        9686101
24  feet           Y    =         2917204
98  meter
 Z    =       16943987
83                 Z    =         5149272
07
 XDOT =     -13121
162135                 XDOT =       -3933
045052
 YDOT =     -21192
186001  feet/sec       YDOT =       -6503
730704  meter/sec
 ZDOT =       4215
614853                 ZDOT =        1265
650647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4477102
89                 X    =         1364620
96
 Y    =       13414996
94  feet           Y    =         4088891
07  meter
 Z    =       16885508
08                 Z    =         5146702
86
 XDOT =     -23771
743743                 XDOT =       -7245
627493
 YDOT =       2729
097070  feet/sec       YDOT =         831
828787  meter/sec
 ZDOT =       4140
891231                 ZDOT =        1262
143647


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   08159
52120104  
00020000  00000-0  20000-3 0  9108
2 25544  51
6384  66
2283 0006090 311
7831  48
2813 15
76721660 27001


Satellite: ISS
Catalog Number: 25544
Epoch time:      08159
52120104   =   yrday
fracday
Element set:     910
Inclination:       51
6384  deg
RA of node:        66
2283  deg
Eccentricity:     
0006090     
Arg of perigee:   311
7831  deg
Mean anomaly:      48
2813  deg
Mean motion:   15
76721660  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2700
Checksum:              261


Coasting Arc #12 (Orbit 2714)
---------------------------------------

Vector Time (GMT): 2008/160/11:19:00
000
Vector Time (MET): N/A
Weight (LBS)     : 629858
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3433581
81                 A    =         6724508
52  meter
 Y    =        5767521
64  meter          E    =           
0013674
 Z    =        -219940
37                 I    =           51
94341
 XDOT =      -3985
615744                 Wp   =           16
64177
 YDOT =       2600
046105  meter/sec      RA   =           60
70332  deg
 ZDOT =       6064
973463                 TA   =          340
97450
                                          MA   =          341
02553
                                          Ha   =            185
680  n
mi
                                          Hp   =            181
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11265032
17                 X    =         3369901
70
 Y    =       18922315
10  feet           Y    =         5805561
90  meter
 Z    =        -721589
13                 Z    =         -203413
93
 XDOT =     -13076
167140                 XDOT =       -4043
855973
 YDOT =       8530
334991  feet/sec       YDOT =        2555
150094  meter/sec
 ZDOT =      19898
206901                 ZDOT =        6045
470419

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21860066
43                 X    =         6662948
25
 Y    =       -2679713
83  feet           Y    =         -816776
77  meter
 Z    =        -657478
93                 Z    =         -200399
58
 XDOT =       2290
699353                 XDOT =         698
205163
 YDOT =      13915
477395  feet/sec       YDOT =        4241
437510  meter/sec
 ZDOT =      19823
341878                 ZDOT =        6042
154605


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   08160
47191437  
00020000  00000-0  20000-3 0  9112
2 25544  51
6386  61
3259 0006149 316
7697  43
2984 15
76692609 27152


Satellite: ISS
Catalog Number: 25544
Epoch time:      08160
47191437   =   yrday
fracday
Element set:     911
Inclination:       51
6386  deg
RA of node:        61
3259  deg
Eccentricity:     
0006149     
Arg of perigee:   316
7697  deg
Mean anomaly:      43
2984  deg
Mean motion:   15
76692609  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2715
Checksum:              316

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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