Date: September 10th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6189 25 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2375)
---------------------------------------

Vector Time (GMT): 2007/250/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2369407
41                 A    =         6712640
28  meter
 Y    =       -3421008
91  meter          E    =           
0014721
 Z    =       -5277448
94                 I    =           51
81442
 XDOT =       6121
766512                 Wp   =           52
95384
 YDOT =       4657
456080  meter/sec      RA   =           38
80170  deg
 ZDOT =       -262
445689                 TA   =          214
51190
                                          MA   =          214
60756
                                          Ha   =            187
293  n
mi
                                          Hp   =            180
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7773646
36                 X    =         2433122
09
 Y    =      -11223782
51  feet           Y    =        -3394156
56  meter
 Z    =      -17314465
04                 Z    =        -5265783
79
 XDOT =      20084
535800                 XDOT =        6070
506059
 YDOT =      15280
367715  feet/sec       YDOT =        4725
626519  meter/sec
 ZDOT =       -861
042287                 ZDOT =        -232
831023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12386769
09                 X    =        -3775487
22
 Y    =        5872699
31  feet           Y    =         1789998
75  meter
 Z    =      -17270579
76                 Z    =        -5264072
71
 XDOT =      -9494
280567                 XDOT =       -2893
856717
 YDOT =     -22304
575341  feet/sec       YDOT =       -6798
434564  meter/sec
 ZDOT =       -748
072421                 ZDOT =        -228
012474


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   07250
47456636  
00020000  00000-0  20000-3 0  9004
2 25544  51
6337  39
2564 0008936 338
8077  21
2711 15
76628196 23761


Satellite: ISS
Catalog Number: 25544
Epoch time:      07250
47456636   =   yrday
fracday
Element set:     900
Inclination:       51
6337  deg
RA of node:        39
2564  deg
Eccentricity:     
0008936     
Arg of perigee:   338
8077  deg
Mean anomaly:      21
2711  deg
Mean motion:   15
76628196  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2376
Checksum:              307


Coasting Arc #2 (Orbit 2391)
---------------------------------------

Vector Time (GMT): 2007/251/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5258077
91                 A    =         6724299
51  meter
 Y    =       -4138238
14  meter          E    =           
0004094
 Z    =        -673992
08                 I    =           51
83091
 XDOT =       3429
954284                 Wp   =           80
89176
 YDOT =      -3385
292980  meter/sec      RA   =           33
66236  deg
 ZDOT =      -6003
260792                 TA   =          106
43202
                                          MA   =          106
38702
                                          Ha   =            187
404  n
mi
                                          Hp   =            179
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17250911
78                 X    =        -5208138
64
 Y    =      -13576896
80  feet           Y    =        -4196757
73  meter
 Z    =       -2211260
12                 Z    =         -699414
08
 XDOT =      11253
130853                 XDOT =        3496
716545
 YDOT =     -11106
604266  feet/sec       YDOT =       -3346
564107  meter/sec
 ZDOT =     -19695
737508                 ZDOT =       -5986
436100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8633088
98                 X    =         2631365
52
 Y    =       20173187
22  feet           Y    =         6148787
46  meter
 Z    =       -2308256
27                 Z    =         -703556
51
 XDOT =     -13823
166702                 XDOT =       -4213
301211
 YDOT =       3680
092222  feet/sec       YDOT =        1121
692109  meter/sec
 ZDOT =     -19632
261112                 ZDOT =       -5983
913187


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   07251
48869810  
00020000  00000-0  20000-3 0  9019
2 25544  51
6336  34
0260 0009243 342
6505  17
4343 15
76694443 23921


Satellite: ISS
Catalog Number: 25544
Epoch time:      07251
48869810   =   yrday
fracday
Element set:     901
Inclination:       51
6336  deg
RA of node:        34
0260  deg
Eccentricity:     
0009243     
Arg of perigee:   342
6505  deg
Mean anomaly:      17
4343  deg
Mean motion:   15
76694443  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2392
Checksum:              282


Coasting Arc #3 (Orbit 2407)
---------------------------------------

Vector Time (GMT): 2007/252/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3641256
40                 A    =         6713678
69  meter
 Y    =        2539026
79  meter          E    =           
0012137
 Z    =        5037788
70                 I    =           51
76982
 XDOT =      -5798
475264                 Wp   =           11
26459
 YDOT =      -4748
269575  meter/sec      RA   =           28
49567  deg
 ZDOT =      -1785
564381                 TA   =           95
96438
                                          MA   =           95
82604
                                          Ha   =            187
628  n
mi
                                          Hp   =            179
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11946379
28                 X    =        -3693849
90
 Y    =        8330140
40  feet           Y    =         2498014
35  meter
 Z    =       16528178
14                 Z    =         5019971
86
 XDOT =     -19023
868975                 XDOT =       -5736
274616
 YDOT =     -15578
312254  feet/sec       YDOT =       -4812
763693  meter/sec
 ZDOT =      -5858
150856                 ZDOT =       -1813
581722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14529027
83                 X    =         4428447
68
 Y    =       -1798906
30  feet           Y    =         -548306
64  meter
 Z    =       16460837
64                 Z    =         5017263
31
 XDOT =       9472
430410                 XDOT =        2887
196789
 YDOT =      21548
001745  feet/sec       YDOT =        6567
830932  meter/sec
 ZDOT =      -5965
073353                 ZDOT =       -1818
154358


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   07252
50281208  
00020000  00000-0  20000-3 0  9023
2 25544  51
6338  28
7963 0008978 346
9885  13
1046 15
76644247 24083


Satellite: ISS
Catalog Number: 25544
Epoch time:      07252
50281208   =   yrday
fracday
Element set:     902
Inclination:       51
6338  deg
RA of node:        28
7963  deg
Eccentricity:     
0008978     
Arg of perigee:   346
9885  deg
Mean anomaly:      13
1046  deg
Mean motion:   15
76644247  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2408
Checksum:              308


Coasting Arc #4 (Orbit 2423)
---------------------------------------

Vector Time (GMT): 2007/253/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4738232
39                 A    =         6721833
60  meter
 Y    =        4104332
80  meter          E    =           
0017266
 Z    =        2395128
69                 I    =           51
77374
 XDOT =      -4906
733576                 Wp   =           42
84757
 YDOT =       2509
356500  meter/sec      RA   =           23
38498  deg
 ZDOT =       5396
652425                 TA   =          344
17460
                                          MA   =          344
22849
                                          Ha   =            187
470  n
mi
                                          Hp   =            179
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15545381
86                 X    =         4680349
99
 Y    =       13465658
79  feet           Y    =         4156994
90  meter
 Z    =        7858033
76                 Z    =         2418005
95
 XDOT =     -16098
207270                 XDOT =       -4960
644602
 YDOT =       8232
796917  feet/sec       YDOT =        2454
185528  meter/sec
 ZDOT =      17705
552574                 ZDOT =        5372
684650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7818911
32                 X    =        -2383204
17
 Y    =      -18985977
28  feet           Y    =        -5786925
87  meter
 Z    =        7945366
66                 Z    =         2421747
76
 XDOT =      16784
864323                 XDOT =        5116
026646
 YDOT =        472
931942  feet/sec       YDOT =         144
149656  meter/sec
 ZDOT =      17614
860535                 ZDOT =        5369
009491


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   07253
51689982  
00020000  00000-0  20000-3 0  9037
2 25544  51
6352  23
5669 0009000 350
0226  10
0758 15
76741964 24245


Satellite: ISS
Catalog Number: 25544
Epoch time:      07253
51689982   =   yrday
fracday
Element set:     903
Inclination:       51
6352  deg
RA of node:        23
5669  deg
Eccentricity:     
0009000     
Arg of perigee:   350
0226  deg
Mean anomaly:      10
0758  deg
Mean motion:   15
76741964  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2424
Checksum:              284


Coasting Arc #5 (Orbit 2438)
---------------------------------------

Vector Time (GMT): 2007/254/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4878960
89                 A    =         6716738
60  meter
 Y    =       -1893958
07  meter          E    =           
0009164
 Z    =       -4211463
02                 I    =           51
73008
 XDOT =       4941
553098                 Wp   =           46
23424
 YDOT =       4650
282585  meter/sec      RA   =           18
19076  deg
 ZDOT =       3644
580150                 TA   =          260
77686
                                          MA   =          260
88052
                                          Ha   =            187
760  n
mi
                                          Hp   =            179
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16007089
54                 X    =         4920235
22
 Y    =       -6213773
20  feet           Y    =        -1839168
30  meter
 Z    =      -13817135
90                 Z    =        -4187660
77
 XDOT =      16212
444547                 XDOT =        4871
481059
 YDOT =      15256
832627  feet/sec       YDOT =        4705
150296  meter/sec
 ZDOT =      11957
283958                 ZDOT =        3668
415543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17189158
91                 X    =        -5239255
63
 Y    =       -1361370
60  feet           Y    =         -414945
76  meter
 Z    =      -13727003
43                 Z    =        -4183990
65
 XDOT =      -8048
803877                 XDOT =       -2453
275422
 YDOT =     -19488
628820  feet/sec       YDOT =       -5940
134064  meter/sec
 ZDOT =      12048
316266                 ZDOT =        3672
326798


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   07254
46758993  
00020000  00000-0  20000-3 0  9042
2 25544  51
6359  18
6651 0009145 353
9775   6
1278 15
76743003 24394


Satellite: ISS
Catalog Number: 25544
Epoch time:      07254
46758993   =   yrday
fracday
Element set:     904
Inclination:       51
6359  deg
RA of node:        18
6651  deg
Eccentricity:     
0009145     
Arg of perigee:   353
9775  deg
Mean anomaly:       6
1278  deg
Mean motion:   15
76743003  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2439
Checksum:              318


Coasting Arc #6 (Orbit 2454)
---------------------------------------

Vector Time (GMT): 2007/255/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3747267
79                 A    =         6717640
78  meter
 Y    =       -4016923
66  meter          E    =           
0012647
 Z    =       -3880308
22                 I    =           51
70619
 XDOT =       6242
680877                 Wp   =           28
03090
 YDOT =      -1865
451779  meter/sec      RA   =           13
09072  deg
 ZDOT =      -4091
937871                 TA   =          199
28506
                                          MA   =          199
33296
                                          Ha   =            187
760  n
mi
                                          Hp   =            178
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12294185
65                 X    =        -3683221
61
 Y    =      -13178883
40  feet           Y    =        -4058469
92  meter
 Z    =      -12730670
03                 Z    =        -3898356
57
 XDOT =      20481
236473                 XDOT =        6282
954558
 YDOT =      -6120
248620  feet/sec       YDOT =       -1795
417727  meter/sec
 ZDOT =     -13424
993014                 ZDOT =       -4061
512971

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5607639
21                 X    =         1709208
43
 Y    =       17076976
31  feet           Y    =         5205062
38  meter
 Z    =      -12799655
86                 Z    =        -3901335
11
 XDOT =     -19989
605592                 XDOT =       -6092
831784
 YDOT =      -3425
564726  feet/sec       YDOT =       -1044
112129  meter/sec
 ZDOT =     -13309
721869                 ZDOT =       -4056
803226


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   07255
48163696  
00020000  00000-0  20000-3 0  9056
2 25544  51
6363  13
4354 0009206 357
7682   2
3440 15
76784703 24558


Satellite: ISS
Catalog Number: 25544
Epoch time:      07255
48163696   =   yrday
fracday
Element set:     905
Inclination:       51
6363  deg
RA of node:        13
4354  deg
Eccentricity:     
0009206     
Arg of perigee:   357
7682  deg
Mean anomaly:       2
3440  deg
Mean motion:   15
76784703  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2455
Checksum:              296


Coasting Arc #7 (Orbit 2470)
---------------------------------------

Vector Time (GMT): 2007/256/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5938584
00                 A    =         6720840
82  meter
 Y    =        1416665
12  meter          E    =           
0015245
 Z    =        2807697
48                 I    =           51
68873
 XDOT =      -3518
202545                 Wp   =           63
07930
 YDOT =      -4563
815922  meter/sec      RA   =            7
88828  deg
 ZDOT =      -5110
657216                 TA   =           84
74698
                                          MA   =           84
57304
                                          Ha   =            187
874  n
mi
                                          Hp   =            178
576

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19483543
30                 X    =        -5967623
34
 Y    =        4647851
45  feet           Y    =         1350094
36  meter
 Z    =        9211605
90                 Z    =         2778777
07
 XDOT =     -11542
659269                 XDOT =       -3442
081030
 YDOT =     -14973
149349  feet/sec       YDOT =       -4602
733213  meter/sec
 ZDOT =     -16767
248085                 ZDOT =       -5127
563481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19756932
04                 X    =         6021912
89
 Y    =        3589142
98  feet           Y    =         1093970
78  meter
 Z    =        9101997
31                 Z    =         2774288
78
 XDOT =       4732
663888                 XDOT =        1442
515953
 YDOT =      16869
535173  feet/sec       YDOT =        5141
834321  meter/sec
 ZDOT =     -16831
959060                 ZDOT =       -5130
381122


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   07256
49566207  
00020000  00000-0  20000-3 0  9064
2 25544  51
6366   8
2057 0009208   1
8228 358
2969 15
76810446 24719


Satellite: ISS
Catalog Number: 25544
Epoch time:      07256
49566207   =   yrday
fracday
Element set:     906
Inclination:       51
6366  deg
RA of node:         8
2057  deg
Eccentricity:     
0009208     
Arg of perigee:     1
8228  deg
Mean anomaly:     358
2969  deg
Mean motion:   15
76810446  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2471
Checksum:              305


Coasting Arc #8 (Orbit 2486)
---------------------------------------

Vector Time (GMT): 2007/257/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2303101
83                 A    =         6713470
66  meter
 Y    =        3981294
06  meter          E    =           
0008483
 Z    =        4883099
79                 I    =           51
63710
 XDOT =      -7236
001407                 Wp   =           46
51997
 YDOT =       1431
573969  meter/sec      RA   =            2
77435  deg
 ZDOT =       2248
964163                 TA   =           21
66250
                                          MA   =           21
62664
                                          Ha   =            187
816  n
mi
                                          Hp   =            178
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7556108
36                 X    =         2234689
81
 Y    =       13061988
37  feet           Y    =         4006666
45  meter
 Z    =       16020668
61                 Z    =         4894121
92
 XDOT =     -23740
162095                 XDOT =       -7262
396838
 YDOT =       4696
764989  feet/sec       YDOT =        1350
509474  meter/sec
 ZDOT =       7378
491348                 ZDOT =        2213
747167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1848589
22                 X    =         -563449
99
 Y    =      -14931033
87  feet           Y    =        -4550979
12  meter
 Z    =       16062972
39                 Z    =         4895993
98
 XDOT =      22663
340357                 XDOT =        6907
786141
 YDOT =       4976
656548  feet/sec       YDOT =        1516
884916  meter/sec
 ZDOT =       7244
988572                 ZDOT =        2208
272517


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   07257
50966273  
00020000  00000-0  20000-3 0  9075
2 25544  51
6376   2
9761 0009318   5
0531 355
0727 15
76892400 24872


Satellite: ISS
Catalog Number: 25544
Epoch time:      07257
50966273   =   yrday
fracday
Element set:     907
Inclination:       51
6376  deg
RA of node:         2
9761  deg
Eccentricity:     
0009318     
Arg of perigee:     5
0531  deg
Mean anomaly:     355
0727  deg
Mean motion:   15
76892400  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2487
Checksum:              299


Coasting Arc #9 (Orbit 2501)
---------------------------------------

Vector Time (GMT): 2007/258/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6540026
86                 A    =         6723562
18  meter
 Y    =       -1100278
48  meter          E    =           
0018752
 Z    =       -1041521
65                 I    =           51
64217
 XDOT =       1713
597617                 Wp   =           23
53975
 YDOT =       4623
950463  meter/sec      RA   =          357
58961  deg
 ZDOT =       5928
698195                 TA   =          325
04894
                                          MA   =          325
17189
                                          Ha   =            188
094  n
mi
                                          Hp   =            177
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21456781
05                 X    =         6556903
85
 Y    =       -3609837
52  feet           Y    =        -1027049
89  meter
 Z    =       -3417065
77                 Z    =        -1009708
79
 XDOT =       5622
039425                 XDOT =        1632
963686
 YDOT =      15170
441152  feet/sec       YDOT =        4642
662337  meter/sec
 ZDOT =      19451
109563                 ZDOT =        5936
826845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21287785
50                 X    =        -6488517
02
 Y    =       -4589590
28  feet           Y    =        -1398907
12  meter
 Z    =       -3296447
78                 Z    =        -1004757
28
 XDOT =        154
827306                 XDOT =          47
191363
 YDOT =     -14581
106159  feet/sec       YDOT =       -4444
321157  meter/sec
 ZDOT =      19482
502478                 ZDOT =        5938
266755


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   07258
46027038  
00020000  00000-0  20000-3 0  9089
2 25544  51
6379 358
0739 0009524   9
2336 350
9002 15
76876942 25024


Satellite: ISS
Catalog Number: 25544
Epoch time:      07258
46027038   =   yrday
fracday
Element set:     908
Inclination:       51
6379  deg
RA of node:       358
0739  deg
Eccentricity:     
0009524     
Arg of perigee:     9
2336  deg
Mean anomaly:     350
9002  deg
Mean motion:   15
76876942  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2502
Checksum:              305


Coasting Arc #10 (Orbit 2517)
---------------------------------------

Vector Time (GMT): 2007/259/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -627524
82                 A    =         6711747
95  meter
 Y    =       -4131631
69  meter          E    =           
0019600
 Z    =       -5266774
18                 I    =           51
57407
 XDOT =       7619
053448                 Wp   =           61
01942
 YDOT =      -1062
932955  meter/sec      RA   =          352
44087  deg
 ZDOT =        -64
809349                 TA   =          208
31109
                                          MA   =          208
41775
                                          Ha   =            188
065  n
mi
                                          Hp   =            177
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2058808
48                 X    =         -555692
31
 Y    =      -13555222
09  feet           Y    =        -4138247
58  meter
 Z    =      -17279442
84                 Z    =        -5269648
11
 XDOT =      24996
894516                 XDOT =        7630
687892
 YDOT =      -3487
312844  feet/sec       YDOT =        -977
667345  meter/sec
 ZDOT =       -212
629098                 ZDOT =         -27
767233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2961630
48                 X    =         -902704
97
 Y    =       13372276
89  feet           Y    =         4075870
00  meter
 Z    =      -17290831
06                 Z    =        -5270245
31
 XDOT =     -23639
303118                 XDOT =       -7205
259590
 YDOT =      -5367
597415  feet/sec       YDOT =       -1636
043692  meter/sec
 ZDOT =        -72
160340                 ZDOT =         -21
994472


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   07259
47422839  
00020000  00000-0  20000-3 0  9090
2 25544  51
6379 352
8447 0009560  12
9628 347
1780 15
76936730 25187


Satellite: ISS
Catalog Number: 25544
Epoch time:      07259
47422839   =   yrday
fracday
Element set:     909
Inclination:       51
6379  deg
RA of node:       352
8447  deg
Eccentricity:     
0009560     
Arg of perigee:    12
9628  deg
Mean anomaly:     347
1780  deg
Mean motion:   15
76936730  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2518
Checksum:              329


Coasting Arc #11 (Orbit 2533)
---------------------------------------

Vector Time (GMT): 2007/260/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6618756
11                 A    =         6723315
66  meter
 Y    =         720587
70  meter          E    =           
0009008
 Z    =        -950301
54                 I    =           51
58476
 XDOT =        312
431991                 Wp   =           80
77416
 YDOT =      -4893
886197  meter/sec      RA   =          347
28735  deg
 ZDOT =      -5933
196634                 TA   =          109
61541
                                          MA   =          109
51815
                                          Ha   =            188
129  n
mi
                                          Hp   =            177
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21715079
09                 X    =        -6621705
45
 Y    =        2364132
87  feet           Y    =          646556
52  meter
 Z    =       -3117787
22                 Z    =         -982463
03
 XDOT =       1025
039340                 XDOT =         395
955686
 YDOT =     -16056
057077  feet/sec       YDOT =       -4889
925504  meter/sec
 ZDOT =     -19465
868222                 ZDOT =       -5931
475855

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21220946
04                 X    =         6468144
35
 Y    =        5101931
86  feet           Y    =         1555068
83  meter
 Z    =       -3239771
87                 Z    =         -987482
47
 XDOT =      -6117
872462                 XDOT =       -1864
727526
 YDOT =      13182
137369  feet/sec       YDOT =        4017
915470  meter/sec
 ZDOT =     -19459
903318                 ZDOT =       -5931
378531


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   07260
48816373  
00020000  00000-0  20000-3 0  9105
2 25544  51
6377 347
6142 0009560  17
0090 343
1393 15
76966798 25349


Satellite: ISS
Catalog Number: 25544
Epoch time:      07260
48816373   =   yrday
fracday
Element set:     910
Inclination:       51
6377  deg
RA of node:       347
6142  deg
Eccentricity:     
0009560     
Arg of perigee:    17
0090  deg
Mean anomaly:     343
1393  deg
Mean motion:   15
76966798  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2534
Checksum:              306


Coasting Arc #12 (Orbit 2549)
---------------------------------------

Vector Time (GMT): 2007/261/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 520639
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1136847
46                 A    =         6713181
42  meter
 Y    =        4452182
77  meter          E    =           
0015478
 Z    =        4890780
88                 I    =           51
52329
 XDOT =      -7368
897609                 Wp   =           34
89564
 YDOT =        547
285187  meter/sec      RA   =          342
09542  deg
 ZDOT =      -2195
169484                 TA   =           76
52217
                                          MA   =           76
34973
                                          Ha   =            188
245  n
mi
                                          Hp   =            177
189

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3729814
50                 X    =        -1210306
72
 Y    =       14606898
84  feet           Y    =         4439059
18  meter
 Z    =       16045869
03                 Z    =         4885079
57
 XDOT =     -24176
173259                 XDOT =       -7363
805910
 YDOT =       1795
555074  feet/sec       YDOT =         464
910474  meter/sec
 ZDOT =      -7201
999621                 ZDOT =       -2230
955599

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8312716
88                 X    =         2533716
10
 Y    =      -12603541
63  feet           Y    =        -3841559
49  meter
 Z    =       16024743
36                 Z    =         4884341
77
 XDOT =      22512
423871                 XDOT =        6861
786796
 YDOT =       5452
105380  feet/sec       YDOT =        1661
801720  meter/sec
 ZDOT =      -7337
763596                 ZDOT =       -2236
550344


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   07261
50207567  
00020000  00000-0  20000-3 0  9119
2 25544  51
6381 342
3838 0009751  20
7675 339
3884 15
77016723 25505


Satellite: ISS
Catalog Number: 25544
Epoch time:      07261
50207567   =   yrday
fracday
Element set:     911
Inclination:       51
6381  deg
RA of node:       342
3838  deg
Eccentricity:     
0009751     
Arg of perigee:    20
7675  deg
Mean anomaly:     339
3884  deg
Mean motion:   15
77016723  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2550
Checksum:              296

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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