Date: March 5th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 1186)
---------------------------------------

Vector Time (GMT): 2008/063/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -708117
47                 A    =         6716015
05  meter
 Y    =       -4457981
74  meter          E    =           
0007149
 Z    =        4971130
22                 I    =           51
51075
 XDOT =       7384
315717                 Wp   =          145
17386
 YDOT =       1013
903352  meter/sec      RA   =          199
84920  deg
 ZDOT =       1953
953198                 TA   =          285
88348
                                          MA   =          285
96226
                                          Ha   =            187
167  n
mi
                                          Hp   =            181
097

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2323220
05                 X    =         -682363
32
 Y    =      -14625924
34  feet           Y    =        -4465756
24  meter
 Z    =       16309482
34                 Z    =         4967752
88
 XDOT =      24226
757601                 XDOT =        7362
937536
 YDOT =       3326
454567  feet/sec       YDOT =        1096
359478  meter/sec
 ZDOT =       6410
607606                 ZDOT =        1989
773467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3576300
53                 X    =        -1090056
40
 Y    =      -14386254
74  feet           Y    =        -4384930
45  meter
 Z    =       16296011
09                 Z    =         4967024
18
 XDOT =      23329
364963                 XDOT =        7110
790441
 YDOT =       1644
276511  feet/sec       YDOT =         501
175480  meter/sec
 ZDOT =       6547
917166                 ZDOT =        1995
805152


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   08063
61661172  
00020000  00000-0  20000-3 0  9006
2 25544  51
6375 200
5580 0002631 197
3086 162
7989 15
75899067 11871


Satellite: ISS
Catalog Number: 25544
Epoch time:      08063
61661172   =   yrday
fracday
Element set:     900
Inclination:       51
6375  deg
RA of node:       200
5580  deg
Eccentricity:     
0002631     
Arg of perigee:   197
3086  deg
Mean anomaly:     162
7989  deg
Mean motion:   15
75899067  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1187
Checksum:              309


Coasting Arc #2 (Orbit 1201)
---------------------------------------

Vector Time (GMT): 2008/064/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6582723
69                 A    =         6726228
27  meter
 Y    =        -831508
70  meter          E    =           
0007255
 Z    =       -1086784
28                 I    =           51
57361
 XDOT =       -346
998996                 Wp   =           43
39965
 YDOT =      -4932
564598  meter/sec      RA   =          194
66571  deg
 ZDOT =       5904
155284                 TA   =          304
69295
                                          MA   =          304
76128
                                          Ha   =            187
045  n
mi
                                          Hp   =            181
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21596862
48                 X    =        -6567657
11
 Y    =       -2728046
93  feet           Y    =         -905036
27  meter
 Z    =       -3565565
23                 Z    =        -1118725
75
 XDOT =      -1138
448151                 XDOT =        -320
497130
 YDOT =     -16182
954719  feet/sec       YDOT =       -4936
296555  meter/sec
 ZDOT =      19370
588202                 ZDOT =        5902
534146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21739175
22                 X    =        -6626100
61
 Y    =        -621934
30  feet           Y    =         -189565
57  meter
 Z    =       -3688010
74                 Z    =        -1124105
67
 XDOT =      -2857
764843                 XDOT =        -871
046724
 YDOT =     -14400
314677  feet/sec       YDOT =       -4389
215914  meter/sec
 ZDOT =      19363
779839                 ZDOT =        5902
080095


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   08064
56781217  
00020000  00000-0  20000-3 0  9015
2 25544  51
6379 195
6595 0002363 201
4424 158
6642 15
75896593 12029


Satellite: ISS
Catalog Number: 25544
Epoch time:      08064
56781217   =   yrday
fracday
Element set:     901
Inclination:       51
6379  deg
RA of node:       195
6595  deg
Eccentricity:     
0002363     
Arg of perigee:   201
4424  deg
Mean anomaly:     158
6642  deg
Mean motion:   15
75896593  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1202
Checksum:              306


Coasting Arc #3 (Orbit 1217)
---------------------------------------

Vector Time (GMT): 2008/065/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -161026
66                 A    =         6714605
74  meter
 Y    =        4197730
15  meter          E    =           
0013847
 Z    =       -5249989
57                 I    =           51
56379
 XDOT =      -7627
123439                 Wp   =           94
65429
 YDOT =       -892
268237  meter/sec      RA   =          189
52589  deg
 ZDOT =       -481
683241                 TA   =          170
77434
                                          MA   =          170
74888
                                          Ha   =            186
864  n
mi
                                          Hp   =            181
104

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -528302
70                 X    =         -182451
49
 Y    =       13772080
53  feet           Y    =         4195809
35  meter
 Z    =      -17224375
24                 Z    =        -5250824
11
 XDOT =     -25023
370862                 XDOT =       -7614
239224
 YDOT =      -2927
389230  feet/sec       YDOT =        -977
487073  meter/sec
 ZDOT =      -1580
325593                 ZDOT =        -518
703547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1143912
45                 X    =          348664
51
 Y    =       13731291
25  feet           Y    =         4185297
57  meter
 Z    =      -17227057
60                 Z    =        -5250807
16
 XDOT =     -24183
358883                 XDOT =       -7371
087788
 YDOT =       -137
042767  feet/sec       YDOT =         -41
770636  meter/sec
 ZDOT =      -1722
245048                 ZDOT =        -524
940291


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   08065
58239234  
00020000  00000-0  20000-3 0  9026
2 25544  51
6382 190
4344 0002349 207
4395 152
6646 15
75962524 12188


Satellite: ISS
Catalog Number: 25544
Epoch time:      08065
58239234   =   yrday
fracday
Element set:     902
Inclination:       51
6382  deg
RA of node:       190
4344  deg
Eccentricity:     
0002349     
Arg of perigee:   207
4395  deg
Mean anomaly:     152
6646  deg
Mean motion:   15
75962524  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1218
Checksum:              296


Coasting Arc #4 (Orbit 1233)
---------------------------------------

Vector Time (GMT): 2008/066/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6675378
38                 A    =         6726450
98  meter
 Y    =         721491
87  meter          E    =           
0012684
 Z    =        -266108
78                 I    =           51
63301
 XDOT =       -746
464997                 Wp   =          147
10170
 YDOT =       4733
971370  meter/sec      RA   =          184
37073  deg
 ZDOT =      -6034
328164                 TA   =           35
79353
                                          MA   =           35
70859
                                          Ha   =            186
794  n
mi
                                          Hp   =            181
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21900847
71                 X    =         6668107
10
 Y    =        2367099
32  feet           Y    =          796099
08  meter
 Z    =        -873060
31                 Z    =         -233698
24
 XDOT =      -2449
032142                 XDOT =        -770
032492
 YDOT =      15531
402134  feet/sec       YDOT =        4725
491694  meter/sec
 ZDOT =     -19797
664581                 ZDOT =       -6038
012052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22026662
42                 X    =         6713726
71
 Y    =        -527208
48  feet           Y    =         -160693
14  meter
 Z    =        -748810
71                 Z    =         -228237
51
 XDOT =       -317
316754                 XDOT =         -96
718146
 YDOT =      14097
568009  feet/sec       YDOT =        4296
938729  meter/sec
 ZDOT =     -19811
192118                 ZDOT =       -6038
451357


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   08066
59693969  
00020000  00000-0  20000-3 0  9038
2 25544  51
6380 185
2088 0002303 209
3895 150
7140 15
76007724 12348


Satellite: ISS
Catalog Number: 25544
Epoch time:      08066
59693969   =   yrday
fracday
Element set:     903
Inclination:       51
6380  deg
RA of node:       185
2088  deg
Eccentricity:     
0002303     
Arg of perigee:   209
3895  deg
Mean anomaly:     150
7140  deg
Mean motion:   15
76007724  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1234
Checksum:              298


Coasting Arc #5 (Orbit 1249)
---------------------------------------

Vector Time (GMT): 2008/067/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1155098
62                 A    =         6714460
18  meter
 Y    =       -4115706
20  meter          E    =           
0001786
 Z    =        5176451
39                 I    =           51
62365
 XDOT =       7590
820377                 Wp   =           79
45518
 YDOT =        758
396587  meter/sec      RA   =          179
20708  deg
 ZDOT =      -1090
226953                 TA   =           20
94531
                                          MA   =           20
93800
                                          Ha   =            186
484  n
mi
                                          Hp   =            181
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3789693
64                 X    =         1175889
41
 Y    =      -13502973
09  feet           Y    =        -4102672
45  meter
 Z    =       16983108
23                 Z    =         5182113
68
 XDOT =      24904
266328                 XDOT =        7587
071738
 YDOT =       2488
177779  feet/sec       YDOT =         843
260403  meter/sec
 ZDOT =      -3576
860081                 ZDOT =       -1053
360583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1650991
15                 X    =          503222
10
 Y    =      -13901308
87  feet           Y    =        -4237118
95  meter
 Z    =       17004289
61                 Z    =         5182907
47
 XDOT =      24003
944587                 XDOT =        7316
402310
 YDOT =      -1354
114153  feet/sec       YDOT =        -412
733994  meter/sec
 ZDOT =      -3435
528339                 ZDOT =       -1047
149038


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   08067
61145149  
00020000  00000-0  20000-3 0  9045
2 25544  51
6389 179
9825 0002151 218
4357 141
6654 15
76106977 12508


Satellite: ISS
Catalog Number: 25544
Epoch time:      08067
61145149   =   yrday
fracday
Element set:     904
Inclination:       51
6389  deg
RA of node:       179
9825  deg
Eccentricity:     
0002151     
Arg of perigee:   218
4357  deg
Mean anomaly:     141
6654  deg
Mean motion:   15
76106977  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1250
Checksum:              305


Coasting Arc #6 (Orbit 1265)
---------------------------------------

Vector Time (GMT): 2008/068/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6486982
86                 A    =         6725041
98  meter
 Y    =        -627490
15  meter          E    =           
0012295
 Z    =        1636552
67                 I    =           51
68829
 XDOT =       1917
519643                 Wp   =           66
95485
 YDOT =      -4762
437226  meter/sec      RA   =          174
08175  deg
 ZDOT =       5745
385291                 TA   =          311
12803
                                          MA   =          311
23408
                                          Ha   =            186
488  n
mi
                                          Hp   =            181
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21282752
18                 X    =        -6487434
03
 Y    =       -2058694
73  feet           Y    =         -700033
64  meter
 Z    =        5369267
30                 Z    =         1605038
25
 XDOT =       6291
074943                 XDOT =        1942
721710
 YDOT =     -15624
794048  feet/sec       YDOT =       -4740
852889  meter/sec
 ZDOT =      18849
689274                 ZDOT =        5754
762227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21360104
30                 X    =        -6510559
79
 Y    =        1490808
37  feet           Y    =          454398
39  meter
 Z    =        5248450
26                 Z    =         1599727
64
 XDOT =       3626
300722                 XDOT =        1105
296460
 YDOT =     -14874
228737  feet/sec       YDOT =       -4533
664919  meter/sec
 ZDOT =      18885
022030                 ZDOT =        5756
154715


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   08068
62593239  
00020000  00000-0  20000-3 0  9055
2 25544  51
6387 174
7568 0001983 221
4503 138
6511 15
76121012 12664


Satellite: ISS
Catalog Number: 25544
Epoch time:      08068
62593239   =   yrday
fracday
Element set:     905
Inclination:       51
6387  deg
RA of node:       174
7568  deg
Eccentricity:     
0001983     
Arg of perigee:   221
4503  deg
Mean anomaly:     138
6511  deg
Mean motion:   15
76121012  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1266
Checksum:              291


Coasting Arc #7 (Orbit 1280)
---------------------------------------

Vector Time (GMT): 2008/069/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2183682
85                 A    =         6716130
00  meter
 Y    =        4242435
67  meter          E    =           
0010739
 Z    =       -4736726
06                 I    =           51
68711
 XDOT =      -7185
000758                 Wp   =          117
53803
 YDOT =       -730
296809  meter/sec      RA   =          168
89821  deg
 ZDOT =       2657
985005                 TA   =          178
57953
                                          MA   =          178
57648
                                          Ha   =            186
315  n
mi
                                          Hp   =            180
825

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7164313
82                 X    =        -2207950
09
 Y    =       13918752
21  feet           Y    =         4217880
32  meter
 Z    =      -15540439
82                 Z    =        -4747393
71
 XDOT =     -23572
837131                 XDOT =       -7189
212406
 YDOT =      -2395
986905  feet/sec       YDOT =        -810
666868  meter/sec
 ZDOT =       8720
423244                 ZDOT =        2623
070304

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4422260
66                 X    =        -1347905
05
 Y    =       14974880
66  feet           Y    =         4564343
63  meter
 Z    =      -15580785
77                 Z    =        -4749023
50
 XDOT =     -22571
182100                 XDOT =       -6879
696304
 YDOT =       2269
437423  feet/sec       YDOT =         691
724527  meter/sec
 ZDOT =       8586
560717                 ZDOT =        2617
183707


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   08069
57697652  
00020000  00000-0  20000-3 0  9065
2 25544  51
6378 169
8577 0001831 226
7563 133
3449 15
76191760 12811


Satellite: ISS
Catalog Number: 25544
Epoch time:      08069
57697652   =   yrday
fracday
Element set:     906
Inclination:       51
6378  deg
RA of node:       169
8577  deg
Eccentricity:     
0001831     
Arg of perigee:   226
7563  deg
Mean anomaly:     133
3449  deg
Mean motion:   15
76191760  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1281
Checksum:              328


Coasting Arc #8 (Orbit 1296)
---------------------------------------

Vector Time (GMT): 2008/070/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5985116
60                 A    =         6722109
13  meter
 Y    =         705635
48  meter          E    =           
0003978
 Z    =       -2976581
67                 I    =           51
73483
 XDOT =      -3069
270982                 Wp   =          135
81690
 YDOT =       4994
272988  meter/sec      RA   =          163
79572  deg
 ZDOT =      -4994
315205                 TA   =           78
51718
                                          MA   =           78
47251
                                          Ha   =            186
287  n
mi
                                          Hp   =            180
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19636209
32                 X    =         5991240
93
 Y    =        2315077
05  feet           Y    =          772598
48  meter
 Z    =       -9765687
88                 Z    =        -2947491
18
 XDOT =     -10069
786687                 XDOT =       -3100
628137
 YDOT =      16385
410066  feet/sec       YDOT =        4959
774914  meter/sec
 ZDOT =     -16385
548572                 ZDOT =       -5009
302284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19758086
58                 X    =         6022264
79
 Y    =       -1650634
66  feet           Y    =         -503113
44  meter
 Z    =       -9654137
86                 Z    =        -2942581
22
 XDOT =      -6636
004954                 XDOT =       -2022
654310
 YDOT =      16602
603454  feet/sec       YDOT =        5060
473533  meter/sec
 ZDOT =     -16442
358298                 ZDOT =       -5011
630809


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   08070
59139181  
00020000  00000-0  20000-3 0  9078
2 25544  51
6370 164
6308 0001789 232
2373 127
8630 15
76213565 12976


Satellite: ISS
Catalog Number: 25544
Epoch time:      08070
59139181   =   yrday
fracday
Element set:     907
Inclination:       51
6370  deg
RA of node:       164
6308  deg
Eccentricity:     
0001789     
Arg of perigee:   232
2373  deg
Mean anomaly:     127
8630  deg
Mean motion:   15
76213565  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1297
Checksum:              296


Coasting Arc #9 (Orbit 1312)
---------------------------------------

Vector Time (GMT): 2008/071/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3120286
78                 A    =         6718992
81  meter
 Y    =       -4506500
05  meter          E    =           
0009547
 Z    =        3878657
06                 I    =           51
75352
 XDOT =       6459
741316                 Wp   =           83
27333
 YDOT =        937
595828  meter/sec      RA   =          158
60022  deg
 ZDOT =      -4097
679370                 TA   =           49
37736
                                          MA   =           49
29436
                                          Ha   =            185
966  n
mi
                                          Hp   =            180
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10237161
35                 X    =         3151605
42
 Y    =      -14785105
14  feet           Y    =        -4471431
90  meter
 Z    =       12725252
84                 Z    =         3893891
74
 XDOT =      21193
377022                 XDOT =        6468
682678
 YDOT =       3076
101797  feet/sec       YDOT =        1009
882117  meter/sec
 ZDOT =     -13443
829955                 ZDOT =       -4066
276252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6733463
51                 X    =         2052359
68
 Y    =      -16630819
91  feet           Y    =        -5069073
91  meter
 Z    =       12783081
17                 Z    =         3896283
14
 XDOT =      20219
119108                 XDOT =        6162
787504
 YDOT =      -2078
825675  feet/sec       YDOT =        -633
626066  meter/sec
 ZDOT =     -13323
382492                 ZDOT =       -4060
966984


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   08071
60577153  
00020000  00000-0  20000-3 0  9087
2 25544  51
6374 159
4036 0001734 244
9689 115
1295 15
76308346 13138


Satellite: ISS
Catalog Number: 25544
Epoch time:      08071
60577153   =   yrday
fracday
Element set:     908
Inclination:       51
6374  deg
RA of node:       159
4036  deg
Eccentricity:     
0001734     
Arg of perigee:   244
9689  deg
Mean anomaly:     115
1295  deg
Mean motion:   15
76308346  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1313
Checksum:              297


Coasting Arc #10 (Orbit 1328)
---------------------------------------

Vector Time (GMT): 2008/072/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5221056
38                 A    =         6718300
58  meter
 Y    =       -1006583
15  meter          E    =           
0009401
 Z    =        4101090
70                 I    =           51
77712
 XDOT =       4028
804160                 Wp   =          109
84914
 YDOT =      -5355
749688  meter/sec      RA   =          153
50756  deg
 ZDOT =       3804
354023                 TA   =          301
17402
                                          MA   =          301
26616
                                          Ha   =            186
098  n
mi
                                          Hp   =            180
732

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17129450
06                 X    =        -5229334
92
 Y    =       -3302438
15  feet           Y    =        -1065014
17  meter
 Z    =       13455021
99                 Z    =         4075706
74
 XDOT =      13217
861418                 XDOT =        4069
912696
 YDOT =     -17571
357245  feet/sec       YDOT =       -5310
467357  meter/sec
 ZDOT =      12481
476455                 ZDOT =        3824
025931

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17501726
45                 X    =        -5334526
22
 Y    =         790732
59  feet           Y    =          241015
29  meter
 Z    =       13357622
82                 Z    =         4071403
44
 XDOT =       8756
095079                 XDOT =        2668
857780
 YDOT =     -18871
466941  feet/sec       YDOT =       -5752
023124  meter/sec
 ZDOT =      12556
218326                 ZDOT =        3827
135346


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   08072
62011977  
00020000  00000-0  20000-3 0  9098
2 25544  51
6366 154
1763 0001608 246
3160 113
7836 15
76338769 13292


Satellite: ISS
Catalog Number: 25544
Epoch time:      08072
62011977   =   yrday
fracday
Element set:     909
Inclination:       51
6366  deg
RA of node:       154
1763  deg
Eccentricity:     
0001608     
Arg of perigee:   246
3160  deg
Mean anomaly:     113
7836  deg
Mean motion:   15
76338769  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1329
Checksum:              302


Coasting Arc #11 (Orbit 1343)
---------------------------------------

Vector Time (GMT): 2008/073/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3838708
43                 A    =         6722234
97  meter
 Y    =        4831881
52  meter          E    =           
0003519
 Z    =       -2664582
62                 I    =           51
81634
 XDOT =      -5462
436354                 Wp   =           49
44474
 YDOT =      -1460
306962  meter/sec      RA   =          148
31681  deg
 ZDOT =       5228
058763                 TA   =          280
26937
                                          MA   =          280
30905
                                          Ha   =            185
919  n
mi
                                          Hp   =            180
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12594187
78                 X    =        -3879509
98
 Y    =       15852629
65  feet           Y    =         4788726
75  meter
 Z    =       -8742068
96                 Z    =        -2683330
11
 XDOT =     -17921
379115                 XDOT =       -5471
097852
 YDOT =      -4791
033339  feet/sec       YDOT =       -1521
439450  meter/sec
 ZDOT =      17152
423762                 ZDOT =        5201
501328

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8195684
60                 X    =        -2498044
67
 Y    =       18479689
01  feet           Y    =         5632609
21  meter
 Z    =       -8813345
01                 Z    =        -2686307
56
 XDOT =     -17296
353275                 XDOT =       -5271
928478
 YDOT =        450
398283  feet/sec       YDOT =         137
281397  meter/sec
 ZDOT =      17050
462788                 ZDOT =        5196
981058


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   08073
57104145  
00020000  00000-0  20000-3 0  9105
2 25544  51
6362 149
2754 0001454 252
5551 107
5455 15
76389257 13448


Satellite: ISS
Catalog Number: 25544
Epoch time:      08073
57104145   =   yrday
fracday
Element set:     910
Inclination:       51
6362  deg
RA of node:       149
2754  deg
Eccentricity:     
0001454     
Arg of perigee:   252
5551  deg
Mean anomaly:     107
5455  deg
Mean motion:   15
76389257  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1344
Checksum:              285


Coasting Arc #12 (Orbit 1359)
---------------------------------------

Vector Time (GMT): 2008/074/13:34:31
211
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4276932
32                 A    =         6714880
07  meter
 Y    =        1635268
66  meter          E    =           
0011097
 Z    =       -4921703
06                 I    =           51
81635
 XDOT =      -4704
072663                 Wp   =           73
29777
 YDOT =       5679
207237  meter/sec      RA   =          143
21568  deg
 ZDOT =      -2201
802313                 TA   =          175
36305
                                          MA   =          175
35277
                                          Ha   =            185
912  n
mi
                                          Hp   =            180
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14031930
19                 X    =         4282237
14
 Y    =        5365054
67  feet           Y    =         1683125
44  meter
 Z    =      -16147319
76                 Z    =        -4900913
03
 XDOT =     -15433
309261                 XDOT =       -4756
532967
 YDOT =      18632
569676  feet/sec       YDOT =        5626
310301  meter/sec
 ZDOT =      -7223
760870                 ZDOT =       -2224
781882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15041541
99                 X    =         4584662
00
 Y    =        1415764
20  feet           Y    =          431524
93  meter
 Z    =      -16067434
08                 Z    =        -4897353
91
 XDOT =      -9779
162812                 XDOT =       -2980
688825
 YDOT =      20958
250727  feet/sec       YDOT =        6388
074822  meter/sec
 ZDOT =      -7311
171146                 ZDOT =       -2228
444965


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   08074
58532546  
00020000  00000-0  20000-3 0  9118
2 25544  51
6369 144
0472 0001381 259
3979 100
7030 15
76411998 13603


Satellite: ISS
Catalog Number: 25544
Epoch time:      08074
58532546   =   yrday
fracday
Element set:     911
Inclination:       51
6369  deg
RA of node:       144
0472  deg
Eccentricity:     
0001381     
Arg of perigee:   259
3979  deg
Mean anomaly:     100
7030  deg
Mean motion:   15
76411998  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1360
Checksum:              293

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 may contain past, current and future orbital data 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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