Date: February 5th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13347 25 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 744)
---------------------------------------

Vector Time (GMT): 2008/035/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5580633
87                 A    =         6719310
89  meter
 Y    =       -3165359
33  meter          E    =           
0012141
 Z    =       -1977160
81                 I    =           51
56890
 XDOT =       3968
035197                 Wp   =           23
32798
 YDOT =       3513
522925  meter/sec      RA   =          344
59162  deg
 ZDOT =       5597
571625                 TA   =          314
58906
                                          MA   =          314
68808
                                          Ha   =            185
169  n
mi
                                          Hp   =            177
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18309166
23                 X    =         5625219
07
 Y    =      -10385037
18  feet           Y    =        -3102704
08  meter
 Z    =       -6486748
06                 Z    =        -1949942
75
 XDOT =      13018
488179                 XDOT =        3901
260273
 YDOT =      11527
306186  feet/sec       YDOT =        3557
521987  meter/sec
 ZDOT =      18364
736302                 ZDOT =        5616
685887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19366076
92                 X    =         5902780
25
 Y    =       -8328602
49  feet           Y    =        -2538558
04  meter
 Z    =       -6382939
04                 Z    =        -1945519
82
 XDOT =      10976
900251                 XDOT =        3345
759196
 YDOT =      11451
009222  feet/sec       YDOT =        3490
267611  meter/sec
 ZDOT =      18438
190715                 ZDOT =        5619
960530


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   08035
61591913  
00020000  00000-0  20000-3 0  9000
2 25544  51
6411 345
0863 0005766   5
0302 355
0920 15
77946243  7451


Satellite: ISS
Catalog Number: 25544
Epoch time:      08035
61591913   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:       345
0863  deg
Eccentricity:     
0005766     
Arg of perigee:     5
0302  deg
Mean anomaly:     355
0920  deg
Mean motion:   15
77946243  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             745
Checksum:              273


Coasting Arc #2 (Orbit 760)
---------------------------------------

Vector Time (GMT): 2008/036/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2273844
90                 A    =         6708858
55  meter
 Y    =       -3576384
95  meter          E    =           
0017201
 Z    =       -5214939
47                 I    =           51
50718
 XDOT =       6927
111625                 Wp   =           64
95911
 YDOT =      -3259
891692  meter/sec      RA   =          339
44331  deg
 ZDOT =       -779
615595                 TA   =          197
57399
                                          MA   =          197
63358
                                          Ha   =            185
095  n
mi
                                          Hp   =            176
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7460121
05                 X    =        -2208351
75
 Y    =      -11733546
42  feet           Y    =        -3601445
90  meter
 Z    =      -17109381
47                 Z    =        -5225826
59
 XDOT =      22726
744176                 XDOT =        6966
836518
 YDOT =     -10695
182718  feet/sec       YDOT =       -3182
206633  meter/sec
 ZDOT =      -2557
793946                 ZDOT =        -745
868391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6257060
74                 X    =        -1907152
11
 Y    =      -12358798
93  feet           Y    =        -3766961
91  meter
 Z    =      -17151376
97                 Z    =        -5227739
70
 XDOT =      22723
912813                 XDOT =        6926
248625
 YDOT =      -8110
361844  feet/sec       YDOT =       -2472
038290  meter/sec
 ZDOT =      -2429
018041                 ZDOT =        -740
364699


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   08036
62919323  
00020000  00000-0  20000-3 0  9012
2 25544  51
6417 339
8519 0005761   9
1290 350
9979 15
78017968  7612


Satellite: ISS
Catalog Number: 25544
Epoch time:      08036
62919323   =   yrday
fracday
Element set:     901
Inclination:       51
6417  deg
RA of node:       339
8519  deg
Eccentricity:     
0005761     
Arg of perigee:     9
1290  deg
Mean anomaly:     350
9979  deg
Mean motion:   15
78017968  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             761
Checksum:              316


Coasting Arc #3 (Orbit 776)
---------------------------------------

Vector Time (GMT): 2008/037/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6237407
00                 A    =         6720504
71  meter
 Y    =        2404069
32  meter          E    =           
0008429
 Z    =        -682298
05                 I    =           51
51989
 XDOT =      -1169
159069                 Wp   =          108
65931
 YDOT =      -4712
653362  meter/sec      RA   =          334
26834  deg
 ZDOT =      -5979
514869                 TA   =           78
79362
                                          MA   =           78
69889
                                          Ha   =            185
093  n
mi
                                          Hp   =            176
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20463933
72                 X    =        -6260511
72
 Y    =        7887366
54  feet           Y    =         2334189
92  meter
 Z    =       -2238510
65                 Z    =         -712654
45
 XDOT =      -3835
823718                 XDOT =       -1087
328088
 YDOT =     -15461
461162  feet/sec       YDOT =       -4725
269851  meter/sec
 ZDOT =     -19617
830934                 ZDOT =       -5984
995837

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20981568
60                 X    =        -6395182
11
 Y    =        6342290
75  feet           Y    =         1933130
22  meter
 Z    =       -2354398
30                 Z    =         -717620
60
 XDOT =      -2100
233068                 XDOT =        -640
151039
 YDOT =     -14165
903619  feet/sec       YDOT =       -4317
767423  meter/sec
 ZDOT =     -19639
263878                 ZDOT =       -5986
047630


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   08037
64243083  
00020000  00000-0  20000-3 0  9029
2 25544  51
6418 334
6172 0005561  12
3610 347
7691 15
78030114  7771


Satellite: ISS
Catalog Number: 25544
Epoch time:      08037
64243083   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:       334
6172  deg
Eccentricity:     
0005561     
Arg of perigee:    12
3610  deg
Mean anomaly:     347
7691  deg
Mean motion:   15
78030114  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             777
Checksum:              272


Coasting Arc #4 (Orbit 792)
---------------------------------------

Vector Time (GMT): 2008/038/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -210350
76                 A    =         6710079
84  meter
 Y    =        4629742
06  meter          E    =           
0011600
 Z    =        4849571
86                 I    =           51
46000
 XDOT =      -7055
202152                 Wp   =           37
96232
 YDOT =       2096
438554  meter/sec      RA   =          329
06550  deg
 ZDOT =      -2295
512197                 TA   =           74
47621
                                          MA   =           74
34816
                                          Ha   =            185
007  n
mi
                                          Hp   =            176
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -690127
18                 X    =         -285663
22
 Y    =       15189442
44  feet           Y    =         4626968
69  meter
 Z    =       15910668
83                 Z    =         4848367
09
 XDOT =     -23146
988688                 XDOT =       -7066
969664
 YDOT =       6878
079247  feet/sec       YDOT =        2017
477475  meter/sec
 ZDOT =      -7531
207995                 ZDOT =       -2329
813870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1649553
08                 X    =         -502783
78
 Y    =       15119730
80  feet           Y    =         4608493
95  meter
 Z    =       15906524
92                 Z    =         4848308
79
 XDOT =     -22357
638218                 XDOT =       -6814
608129
 YDOT =       5662
872970  feet/sec       YDOT =        1726
043681  meter/sec
 ZDOT =      -7662
215849                 ZDOT =       -2335
443391


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   08038
65562856  
00020000  00000-0  20000-3 0  9034
2 25544  51
6418 329
3825 0005717  14
6070 345
5260 15
78159979  7932


Satellite: ISS
Catalog Number: 25544
Epoch time:      08038
65562856   =   yrday
fracday
Element set:     903
Inclination:       51
6418  deg
RA of node:       329
3825  deg
Eccentricity:     
0005717     
Arg of perigee:    14
6070  deg
Mean anomaly:     345
5260  deg
Mean motion:   15
78159979  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             793
Checksum:              318


Coasting Arc #5 (Orbit 808)
---------------------------------------

Vector Time (GMT): 2008/039/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5799862
34                 A    =         6715831
89  meter
 Y    =       -1081394
25  meter          E    =           
0015941
 Z    =        3189073
05                 I    =           51
45517
 XDOT =      -1549
312388                 Wp   =           67
53005
 YDOT =       5847
621434  meter/sec      RA   =          323
92930  deg
 ZDOT =       4787
627343                 TA   =          329
91366
                                          MA   =          330
00514
                                          Ha   =            184
998  n
mi
                                          Hp   =            176
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19028419
74                 X    =         5796032
10
 Y    =       -3547881
41  feet           Y    =        -1016558
23  meter
 Z    =       10462838
08                 Z    =         3217238
69
 XDOT =      -5083
045891                 XDOT =       -1637
843010
 YDOT =      19185
109690  feet/sec       YDOT =        5829
801247  meter/sec
 ZDOT =      15707
438790                 ZDOT =        4779
885832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19095941
95                 X    =         5820443
11
 Y    =       -2783759
64  feet           Y    =         -848489
94  meter
 Z    =       10570472
28                 Z    =         3221879
95
 XDOT =      -6140
744712                 XDOT =       -1871
698988
 YDOT =      17569
561314  feet/sec       YDOT =        5355
202288  meter/sec
 ZDOT =      15678
420018                 ZDOT =        4778
782421


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   08039
66879243  
00020000  00000-0  20000-3 0  9048
2 25544  51
6418 324
1473 0005728  19
4641 340
6742 15
78158799  8091


Satellite: ISS
Catalog Number: 25544
Epoch time:      08039
66879243   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:       324
1473  deg
Eccentricity:     
0005728     
Arg of perigee:    19
4641  deg
Mean anomaly:     340
6742  deg
Mean motion:   15
78158799  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             809
Checksum:              321


Coasting Arc #6 (Orbit 823)
---------------------------------------

Vector Time (GMT): 2008/040/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2346264
21                 A    =         6715798
36  meter
 Y    =       -5431852
47  meter          E    =           
0008918
 Z    =       -3175382
10                 I    =           51
43241
 XDOT =       6023
130251                 Wp   =           46
47064
 YDOT =       -196
377022  meter/sec      RA   =          318
69697  deg
 ZDOT =       4800
808111                 TA   =          276
31560
                                          MA   =          276
41716
                                          Ha   =            185
005  n
mi
                                          Hp   =            176
340

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7697717
22                 X    =         2422254
71
 Y    =      -17821038
28  feet           Y    =        -5405190
44  meter
 Z    =      -10417920
26                 Z    =        -3163799
43
 XDOT =      19760
926019                 XDOT =        6001
557613
 YDOT =       -644
281569  feet/sec       YDOT =        -129
143382  meter/sec
 ZDOT =      15750
682778                 ZDOT =        4830
015391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8163388
95                 X    =         2488200
95
 Y    =      -17638393
90  feet           Y    =        -5376182
46  meter
 Z    =      -10374172
73                 Z    =        -3162047
85
 XDOT =      18394
761477                 XDOT =        5606
723298
 YDOT =       -788
167005  feet/sec       YDOT =        -240
233303  meter/sec
 ZDOT =      15862
388948                 ZDOT =        4834
856151


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   08040
61859677  
00020000  00000-0  20000-3 0  9055
2 25544  51
6415 319
2393 0005624  20
9817 339
1578 15
78226802  8249


Satellite: ISS
Catalog Number: 25544
Epoch time:      08040
61859677   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       319
2393  deg
Eccentricity:     
0005624     
Arg of perigee:    20
9817  deg
Mean anomaly:     339
1578  deg
Mean motion:   15
78226802  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             824
Checksum:              306


Coasting Arc #7 (Orbit 839)
---------------------------------------

Vector Time (GMT): 2008/041/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4525025
53                 A    =         6709456
02  meter
 Y    =        -903486
21  meter          E    =           
0016734
 Z    =       -4886035
68                 I    =           51
38992
 XDOT =       3659
263171                 Wp   =           58
93452
 YDOT =      -6400
983445  meter/sec      RA   =          313
55536  deg
 ZDOT =      -2202
328623                 TA   =          189
56414
                                          MA   =          189
59604
                                          Ha   =            184
922  n
mi
                                          Hp   =            175
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14845884
28                 X    =        -4490851
25
 Y    =       -2964193
60  feet           Y    =         -953896
75  meter
 Z    =      -16030300
78                 Z    =        -4907934
80
 XDOT =      12005
456599                 XDOT =        3741
266312
 YDOT =     -21000
601853  feet/sec       YDOT =       -6359
605071  meter/sec
 ZDOT =      -7225
487608                 ZDOT =       -2184
352789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14737565
13                 X    =        -4492009
85
 Y    =       -3048801
38  feet           Y    =         -929274
66  meter
 Z    =      -16114163
05                 Z    =        -4911596
90
 XDOT =      11944
217382                 XDOT =        3640
597458
 YDOT =     -19856
421213  feet/sec       YDOT =       -6052
237186  meter/sec
 ZDOT =      -7157
391090                 ZDOT =       -2181
572804


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   08041
63168591  
00020000  00000-0  20000-3 0  9067
2 25544  51
6407 314
0033 0005569  24
2578 335
8848 15
78299970  8400


Satellite: ISS
Catalog Number: 25544
Epoch time:      08041
63168591   =   yrday
fracday
Element set:     906
Inclination:       51
6407  deg
RA of node:       314
0033  deg
Eccentricity:     
0005569     
Arg of perigee:    24
2578  deg
Mean anomaly:     335
8848  deg
Mean motion:   15
78299970  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             840
Checksum:              309


Coasting Arc #8 (Orbit 855)
---------------------------------------

Vector Time (GMT): 2008/042/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3830690
83                 A    =         6719826
27  meter
 Y    =        5493736
03  meter          E    =           
0013264
 Z    =         506349
46                 I    =           51
40569
 XDOT =      -4218
735353                 Wp   =          106
12842
 YDOT =      -2377
614990  meter/sec      RA   =          308
34683  deg
 ZDOT =      -5993
715198                 TA   =           68
33643
                                          MA   =           68
19523
                                          Ha   =            184
938  n
mi
                                          Hp   =            176
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12567883
29                 X    =        -3894297
65
 Y    =       18024068
34  feet           Y    =         5450543
44  meter
 Z    =        1661251
50                 Z    =          487585
52
 XDOT =     -13840
995252                 XDOT =       -4162
718945
 YDOT =      -7800
574113  feet/sec       YDOT =       -2424
478292  meter/sec
 ZDOT =     -19664
419940                 ZDOT =       -6014
073402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12369671
32                 X    =        -3770275
82
 Y    =       18167043
23  feet           Y    =         5537314
78  meter
 Z    =        1590049
76                 Z    =          484647
17
 XDOT =     -12493
104543                 XDOT =       -3807
898265
 YDOT =      -6740
645071  feet/sec       YDOT =       -2054
548618  meter/sec
 ZDOT =     -19742
540438                 ZDOT =       -6017
526325


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   08042
64473945  
00020000  00000-0  20000-3 0  9072
2 25544  51
6405 308
7675 0005398  29
6236 330
5235 15
78314385  8567


Satellite: ISS
Catalog Number: 25544
Epoch time:      08042
64473945   =   yrday
fracday
Element set:     907
Inclination:       51
6405  deg
RA of node:       308
7675  deg
Eccentricity:     
0005398     
Arg of perigee:    29
6236  deg
Mean anomaly:     330
5235  deg
Mean motion:   15
78314385  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             856
Checksum:              311


Coasting Arc #9 (Orbit 871)
---------------------------------------

Vector Time (GMT): 2008/043/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2784086
55                 A    =         6707949
91  meter
 Y    =        3268707
72  meter          E    =           
0009041
 Z    =        5149687
92                 I    =           51
34889
 XDOT =      -4875
643893                 Wp   =           41
24362
 YDOT =       5875
891285  meter/sec      RA   =          303
15367  deg
 ZDOT =      -1085
934916                 TA   =           59
18812
                                          MA   =           59
09918
                                          Ha   =            184
747  n
mi
                                          Hp   =            175
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9134142
22                 X    =         2722312
43
 Y    =       10724106
71  feet           Y    =         3299495
64  meter
 Z    =       16895301
58                 Z    =         5163062
79
 XDOT =     -15996
206998                 XDOT =       -4935
711423
 YDOT =      19277
858547  feet/sec       YDOT =        5821
033189  meter/sec
 ZDOT =      -3562
778595                 ZDOT =       -1109
766539

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9341912
99                 X    =         2847415
08
 Y    =       10460628
88  feet           Y    =         3188399
68  meter
 Z    =       16946803
22                 Z    =         5165385
62
 XDOT =     -14653
880947                 XDOT =       -4466
502913
 YDOT =      19046
599839  feet/sec       YDOT =        5805
403631  meter/sec
 ZDOT =      -3653
324293                 ZDOT =       -1113
533244


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   08043
65775302  
00020000  00000-0  20000-3 0  9087
2 25544  51
6400 303
5304 0005411  31
4445 328
7043 15
78415853  8729


Satellite: ISS
Catalog Number: 25544
Epoch time:      08043
65775302   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       303
5304  deg
Eccentricity:     
0005411     
Arg of perigee:    31
4445  deg
Mean anomaly:     328
7043  deg
Mean motion:   15
78415853  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             872
Checksum:              268


Coasting Arc #10 (Orbit 887)
---------------------------------------

Vector Time (GMT): 2008/044/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4466344
76                 A    =         6717033
78  meter
 Y    =       -4425224
97  meter          E    =           
0018387
 Z    =        2335385
44                 I    =           51
36423
 XDOT =       2187
603254                 Wp   =           62
80733
 YDOT =       5065
978854  meter/sec      RA   =          297
99360  deg
 ZDOT =       5391
494225                 TA   =          323
66467
                                          MA   =          323
78937
                                          Ha   =            184
666  n
mi
                                          Hp   =            175
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14653362
07                 X    =         4504151
58
 Y    =      -14518454
63  feet           Y    =        -4375068
40  meter
 Z    =        7662025
72                 Z    =         2357174
51
 XDOT =       7177
176029                 XDOT =        2104
601453
 YDOT =      16620
665530  feet/sec       YDOT =        5089
977719  meter/sec
 ZDOT =      17688
629346                 ZDOT =        5401
919961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13928663
07                 X    =         4245456
50
 Y    =      -15173063
95  feet           Y    =        -4624749
89  meter
 Z    =        7744911
77                 Z    =         2360649
11
 XDOT =       6725
020505                 XDOT =        2049
786250
 YDOT =      15262
986551  feet/sec       YDOT =        4652
158301  meter/sec
 ZDOT =      17729
038607                 ZDOT =        5403
810967


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   08044
67073072  
00020000  00000-0  20000-3 0  9096
2 25544  51
6389 298
2929 0005307  34
2119 325
9387 15
78479303  8888


Satellite: ISS
Catalog Number: 25544
Epoch time:      08044
67073072   =   yrday
fracday
Element set:     909
Inclination:       51
6389  deg
RA of node:       298
2929  deg
Eccentricity:     
0005307     
Arg of perigee:    34
2119  deg
Mean anomaly:     325
9387  deg
Mean motion:   15
78479303  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             888
Checksum:              326


Coasting Arc #11 (Orbit 902)
---------------------------------------

Vector Time (GMT): 2008/045/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1066420
80                 A    =         6712869
26  meter
 Y    =       -5404841
71  meter          E    =           
0009789
 Z    =       -3841973
24                 I    =           51
33706
 XDOT =       5203
477644                 Wp   =           75
67205
 YDOT =      -3931
142080  meter/sec      RA   =          292
75448  deg
 ZDOT =       4097
035778                 TA   =          237
22451
                                          MA   =          237
31887
                                          Ha   =            184
696  n
mi
                                          Hp   =            175
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3498755
89                 X    =         -987240
38
 Y    =      -17732420
29  feet           Y    =        -5416324
16  meter
 Z    =      -12604899
07                 Z    =        -3846961
73
 XDOT =      17071
777046                 XDOT =        5227
147125
 YDOT =     -12897
447770  feet/sec       YDOT =       -3872
821646  meter/sec
 ZDOT =      13441
718431                 ZDOT =        4122
371313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4538081
86                 X    =        -1383207
35
 Y    =      -17481136
64  feet           Y    =        -5328250
45  meter
 Z    =      -12624546
64                 Z    =        -3847961
81
 XDOT =      14873
906272                 XDOT =        4533
566632
 YDOT =     -13612
069894  feet/sec       YDOT =       -4148
958904  meter/sec
 ZDOT =      13538
226330                 ZDOT =        4126
451386


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   08045
62036488  
00020000  00000-0  20000-3 0  9104
2 25544  51
6380 293
3824 0005284  38
1934 321
9605 15
78520467  9036


Satellite: ISS
Catalog Number: 25544
Epoch time:      08045
62036488   =   yrday
fracday
Element set:     910
Inclination:       51
6380  deg
RA of node:       293
3824  deg
Eccentricity:     
0005284     
Arg of perigee:    38
1934  deg
Mean anomaly:     321
9605  deg
Mean motion:   15
78520467  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             903
Checksum:              292


Coasting Arc #12 (Orbit 918)
---------------------------------------

Vector Time (GMT): 2008/046/14:41:25
713
Vector Time (MET): N/A
Weight (LBS)     : 525189
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4482210
08                 A    =         6710162
12  meter
 Y    =        2137369
68  meter          E    =           
0015128
 Z    =       -4528139
24                 I    =           51
31734
 XDOT =       -305
169305                 Wp   =           60
27872
 YDOT =      -7066
005945  meter/sec      RA   =          287
61098  deg
 ZDOT =      -3033
400986                 TA   =          179
39443
                                          MA   =          179
39260
                                          Ha   =            184
687  n
mi
                                          Hp   =            175
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14705413
64                 X    =        -4483780
83
 Y    =        7012367
71  feet           Y    =         2087238
51  meter
 Z    =      -14856099
88                 Z    =        -4549917
16
 XDOT =      -1001
211630                 XDOT =        -211
397990
 YDOT =     -23182
434202  feet/sec       YDOT =       -7068
894056  meter/sec
 ZDOT =      -9952
102974                 ZDOT =       -3034
656088

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14011617
21                 X    =        -4270740
93
 Y    =        8162190
56  feet           Y    =         2487835
68  meter
 Z    =      -14939190
84                 Z    =        -4553465
37
 XDOT =      -2205
440368                 XDOT =        -672
218224
 YDOT =     -22010
272751  feet/sec       YDOT =       -6708
731134  meter/sec
 ZDOT =      -9957
645624                 ZDOT =       -3035
090386


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   08046
63327185  
00020000  00000-0  20000-3 0  9114
2 25544  51
6369 288
1451 0005270  42
0201 318
1368 15
78570420  9192


Satellite: ISS
Catalog Number: 25544
Epoch time:      08046
63327185   =   yrday
fracday
Element set:     911
Inclination:       51
6369  deg
RA of node:       288
1451  deg
Eccentricity:     
0005270     
Arg of perigee:    42
0201  deg
Mean anomaly:     318
1368  deg
Mean motion:   15
78570420  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             919
Checksum:              278

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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