Date: September 25th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 3552 09 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


267/19:33:56 053 0 7 10 2 10 2
N/A -8 3 0 0 189 0
000/00:01:52 106 -5 9 0 0 181 4

Coasting Arc #1 (Orbit 2565)
---------------------------------------

Vector Time (GMT): 2007/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2011073
40                 A    =         6711945
86  meter
 Y    =       -3685761
97  meter          E    =           
0020942
 Z    =       -5252910
15                 I    =           51
48685
 XDOT =       6946
353208                 Wp   =           62
38041
 YDOT =      -3284
636175  meter/sec      RA   =          336
74743  deg
 ZDOT =       -346
213082                 TA   =          204
27237
                                          MA   =          204
37116
                                          Ha   =            188
400  n
mi
                                          Hp   =            177
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6598009
85                 X    =        -1944191
31
 Y    =      -12092394
91  feet           Y    =        -3707876
94  meter
 Z    =      -17233957
19                 Z    =        -5262517
58
 XDOT =      22789
872730                 XDOT =        6984
248084
 YDOT =     -10776
365402  feet/sec       YDOT =       -3206
746246  meter/sec
 ZDOT =      -1135
869691                 ZDOT =        -312
375417

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5918858
96                 X    =         1804068
21
 Y    =       12387651
93  feet           Y    =         3775756
31  meter
 Z    =      -17270848
77                 Z    =        -5264154
71
 XDOT =     -22379
073415                 XDOT =       -6821
141577
 YDOT =       9248
934049  feet/sec       YDOT =        2819
075098  meter/sec
 ZDOT =      -1007
813497                 ZDOT =        -307
181554


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   07262
51637699  
00020000  00000-0  20000-3 0  9002
2 25544  51
6353 337
1650 0009650  22
0216 338
1362 15
76879361 25661


Satellite: ISS
Catalog Number: 25544
Epoch time:      07262
51637699   =   yrday
fracday
Element set:     900
Inclination:       51
6353  deg
RA of node:       337
1650  deg
Eccentricity:     
0009650     
Arg of perigee:    22
0216  deg
Mean anomaly:     338
1362  deg
Mean motion:   15
76879361  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2566
Checksum:              295


Coasting Arc #2 (Orbit 2581)
---------------------------------------

Vector Time (GMT): 2007/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6126647
68                 A    =         6723631
87  meter
 Y    =        2684006
40  meter          E    =           
0011166
 Z    =        -697681
23                 I    =           51
50037
 XDOT =      -1370
518847                 Wp   =           86
57160
 YDOT =      -4659
690598  meter/sec      RA   =          331
58321  deg
 ZDOT =      -5972
208609                 TA   =          101
04598
                                          MA   =          100
92038
                                          Ha   =            188
500  n
mi
                                          Hp   =            177
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20100550
14                 X    =        -6152816
07
 Y    =        8805795
28  feet           Y    =         2615348
46  meter
 Z    =       -2288980
41                 Z    =         -727508
15
 XDOT =      -4496
452910                 XDOT =       -1289
299605
 YDOT =     -15287
698811  feet/sec       YDOT =       -4674
562356  meter/sec
 ZDOT =     -19593
860266                 ZDOT =       -5978
669363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20345346
18                 X    =         6201261
52
 Y    =       -8192155
61  feet           Y    =        -2496969
03  meter
 Z    =       -2401885
30                 Z    =         -732094
64
 XDOT =       3322
894712                 XDOT =        1012
818308
 YDOT =      13930
039685  feet/sec       YDOT =        4245
876096  meter/sec
 ZDOT =     -19618
923095                 ZDOT =       -5979
847759


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   07263
53033400  
00020000  00000-0  20000-3 0  9016
2 25544  51
6350 331
9346 0009798  26
7887 333
3782 15
76922929 25820


Satellite: ISS
Catalog Number: 25544
Epoch time:      07263
53033400   =   yrday
fracday
Element set:     901
Inclination:       51
6350  deg
RA of node:       331
9346  deg
Eccentricity:     
0009798     
Arg of perigee:    26
7887  deg
Mean anomaly:     333
3782  deg
Mean motion:   15
76922929  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2582
Checksum:              308


Coasting Arc #3 (Orbit 2597)
---------------------------------------

Vector Time (GMT): 2007/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         427648
94                 A    =         6712877
00  meter
 Y    =        4479315
94  meter          E    =           
0015181
 Z    =        4976774
79                 I    =           51
44014
 XDOT =      -6932
036965                 Wp   =           38
58773
 YDOT =       2789
014836  meter/sec      RA   =          326
38994  deg
 ZDOT =      -1899
766812                 TA   =           69
86189
                                          MA   =           69
69863
                                          Ha   =            188
469  n
mi
                                          Hp   =            176
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1403047
71                 X    =          353352
49
 Y    =       14695918
42  feet           Y    =         4483682
75  meter
 Z    =       16328001
27                 Z    =         4978671
83
 XDOT =     -22742
903430                 XDOT =       -6953
480214
 YDOT =       9150
311142  feet/sec       YDOT =        2711
376981  meter/sec
 ZDOT =      -6232
830749                 ZDOT =       -1933
494756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1117875
26                 X    =         -340728
38
 Y    =      -14711786
29  feet           Y    =        -4484152
46  meter
 Z    =       16335724
22                 Z    =         4979128
74
 XDOT =      21753
062281                 XDOT =        6630
333383
 YDOT =      -8769
451776  feet/sec       YDOT =       -2672
928901  meter/sec
 ZDOT =      -6360
532897                 ZDOT =       -1938
690427


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   07264
54427587  
00020000  00000-0  20000-3 0  9022
2 25544  51
6355 326
7040 0009782  29
3699 330
8014 15
76977827 25985


Satellite: ISS
Catalog Number: 25544
Epoch time:      07264
54427587   =   yrday
fracday
Element set:     902
Inclination:       51
6355  deg
RA of node:       326
7040  deg
Eccentricity:     
0009782     
Arg of perigee:    29
3699  deg
Mean anomaly:     330
8014  deg
Mean motion:   15
76977827  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2598
Checksum:              329


Coasting Arc #4 (Orbit 2613)
---------------------------------------

Vector Time (GMT): 2007/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5844094
50                 A    =         6720882
65  meter
 Y    =       -2083878
38  meter          E    =           
0022197
 Z    =        2549555
29                 I    =           51
44304
 XDOT =       -302
025829                 Wp   =           58
83099
 YDOT =       5627
905945  meter/sec      RA   =          321
25608  deg
 ZDOT =       5269
953794                 TA   =          330
24992
                                          MA   =          330
37595
                                          Ha   =            188
594  n
mi
                                          Hp   =            176
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19173538
39                 X    =         5854577
14
 Y    =       -6836871
32  feet           Y    =        -2018467
75  meter
 Z    =        8364682
71                 Z    =         2577971
35
 XDOT =       -990
898389                 XDOT =        -390
535897
 YDOT =      18464
258349  feet/sec       YDOT =        5624
033749  meter/sec
 ZDOT =      17289
874651                 ZDOT =        5268
271445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19098344
65                 X    =        -5821175
45
 Y    =        6914375
73  feet           Y    =         2107501
72  meter
 Z    =        8472304
33                 Z    =         2582358
36
 XDOT =       1517
463505                 XDOT =         462
522876
 YDOT =     -17075
730149  feet/sec       YDOT =       -5204
682549  meter/sec
 ZDOT =      17284
150595                 ZDOT =        5268
209101


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   07265
55820826  
00020000  00000-0  20000-3 0  9038
2 25544  51
6349 321
4738 0009994  34
4606 325
7205 15
76953359 26142


Satellite: ISS
Catalog Number: 25544
Epoch time:      07265
55820826   =   yrday
fracday
Element set:     903
Inclination:       51
6349  deg
RA of node:       321
4738  deg
Eccentricity:     
0009994     
Arg of perigee:    34
4606  deg
Mean anomaly:     325
7205  deg
Mean motion:   15
76953359  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2614
Checksum:              312


Coasting Arc #5 (Orbit 2628)
---------------------------------------

Vector Time (GMT): 2007/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         877865
06                 A    =         6716598
90  meter
 Y    =       -5310081
52  meter          E    =           
0014277
 Z    =       -4025243
26                 I    =           51
40686
 XDOT =       6386
865435                 Wp   =           66
55317
 YDOT =      -1866
843255  meter/sec      RA   =          316
03427  deg
 ZDOT =       3872
065432                 TA   =          243
42633
                                          MA   =          243
57272
                                          Ha   =            188
705  n
mi
                                          Hp   =            176
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2880134
72                 X    =          956731
79
 Y    =      -17421527
28  feet           Y    =        -5299823
95  meter
 Z    =      -13206178
69                 Z    =        -4020786
79
 XDOT =      20954
282923                 XDOT =        6388
456331
 YDOT =      -6124
813828  feet/sec       YDOT =       -1795
412639  meter/sec
 ZDOT =      12703
626744                 ZDOT =        3903
096680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2583417
58                 X    =         -787425
68
 Y    =       17480291
77  feet           Y    =         5327992
93  meter
 Z    =      -13189893
77                 Z    =        -4020279
62
 XDOT =     -19472
953906                 XDOT =       -5935
356351
 YDOT =       6755
716853  feet/sec       YDOT =        2059
142497  meter/sec
 ZDOT =      12821
200216                 ZDOT =        3907
901826


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   07266
50875621  
00020000  00000-0  20000-3 0  9048
2 25544  51
6345 316
5704 0010092  38
2420 321
9459 15
77000341 26293


Satellite: ISS
Catalog Number: 25544
Epoch time:      07266
50875621   =   yrday
fracday
Element set:     904
Inclination:       51
6345  deg
RA of node:       316
5704  deg
Eccentricity:     
0010092     
Arg of perigee:    38
2420  deg
Mean anomaly:     321
9459  deg
Mean motion:   15
77000341  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2629
Checksum:              273


Coasting Arc #6 (Orbit 2644)
---------------------------------------

Vector Time (GMT): 2007/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509113
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5233278
17                 A    =         6716250
19  meter
 Y    =        1041629
47  meter          E    =           
0017377
 Z    =       -4097871
06                 I    =           51
38621
 XDOT =       1653
286236                 Wp   =           53
99131
 YDOT =      -6499
132360  meter/sec      RA   =          310
90941  deg
 ZDOT =      -3764
431793                 TA   =          177
22437
                                          MA   =          177
21471
                                          Ha   =            188
789  n
mi
                                          Hp   =            176
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17169547
81                 X    =        -5224630
19
 Y    =        3417419
52  feet           Y    =          983156
04  meter
 Z    =      -13444458
86                 Z    =        -4123273
36
 XDOT =       5424
167442                 XDOT =        1744
124537
 YDOT =     -21322
612729  feet/sec       YDOT =       -6480
136754  meter/sec
 ZDOT =     -12350
498010                 ZDOT =       -3756
179014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16949650
35                 X    =         5166253
43
 Y    =       -4072191
27  feet           Y    =        -1241203
90  meter
 Z    =      -13540761
18                 Z    =        -4127224
01
 XDOT =      -4966
620035                 XDOT =       -1513
825787
 YDOT =      20281
984434  feet/sec       YDOT =        6181
948856  meter/sec
 ZDOT =     -12319
952915                 ZDOT =       -3755
121648


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   07267
52266163  
00020000  00000-0  20000-3 0  9057
2 25544  51
6349 311
3393 0010126  42
1165 318
0776 15
76998319 26459


Satellite: ISS
Catalog Number: 25544
Epoch time:      07267
52266163   =   yrday
fracday
Element set:     905
Inclination:       51
6349  deg
RA of node:       311
3393  deg
Eccentricity:     
0010126     
Arg of perigee:    42
1165  deg
Mean anomaly:     318
0776  deg
Mean motion:   15
76998319  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2645
Checksum:              298


Coasting Arc #7 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2007/267/19:34:52
106
Vector Time (MET): N/A
Weight (LBS)     : 508517
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5299841
43                 A    =         6722738
85  meter
 Y    =        1727525
85  meter          E    =           
0008167
 Z    =       -3767221
21                 I    =           51
38378
 XDOT =        896
301013                 Wp   =           65
74235
 YDOT =      -6388
001015  meter/sec      RA   =          309
27520  deg
 ZDOT =      -4194
108886                 TA   =          160
03520
                                          MA   =          160
00323
                                          Ha   =            188
989  n
mi
                                          Hp   =            181
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17387931
20                 X    =        -5300464
51
 Y    =        5667735
74  feet           Y    =         1668256
24  meter
 Z    =      -12359649
63                 Z    =        -3792969
48
 XDOT =       2940
620122                 XDOT =         988
040202
 YDOT =     -20958
008581  feet/sec       YDOT =       -6377
465474  meter/sec
 ZDOT =     -13760
199756                 ZDOT =       -4189
531300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12738816
42                 X    =        -3882791
24
 Y    =      -13029409
17  feet           Y    =        -3971363
91  meter
 Z    =      -12457181
53                 Z    =        -3796948
93
 XDOT =      19183
340569                 XDOT =        5847
082206
 YDOT =      -5627
429944  feet/sec       YDOT =       -1715
240647  meter/sec
 ZDOT =     -13743
595157                 ZDOT =       -4189
047804


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   07267
83952281  
00020000  00000-0  20000-3 0  9065
2 25544  51
6345 309
7053 0002283  39
4045 320
7285 15
75114410 26502


Satellite: ISS
Catalog Number: 25544
Epoch time:      07267
83952281   =   yrday
fracday
Element set:     906
Inclination:       51
6345  deg
RA of node:       309
7053  deg
Eccentricity:     
0002283     
Arg of perigee:    39
4045  deg
Mean anomaly:     320
7285  deg
Mean motion:   15
75114410  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2650
Checksum:              279


Coasting Arc #8 (Orbit 2665)
---------------------------------------

Vector Time (GMT): 2007/268/19:34:52
106
Vector Time (MET): N/A
Weight (LBS)     : 508517
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -657995
54                 A    =         6724068
72  meter
 Y    =        5777092
12  meter          E    =           
0014217
 Z    =        3366724
46                 I    =           51
37047
 XDOT =      -5826
284021                 Wp   =           83
31206
 YDOT =       2035
584801  meter/sec      RA   =          304
06064  deg
 ZDOT =      -4613
355679                 TA   =           56
78902
                                          MA   =           56
65280
                                          Ha   =            189
014  n
mi
                                          Hp   =            181
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2158778
00                 X    =         -738901
96
 Y    =       18953714
29  feet           Y    =         5769282
00  meter
 Z    =       11045683
92                 Z    =         3363330
80
 XDOT =     -19115
105056                 XDOT =       -5826
202250
 YDOT =       6678
427826  feet/sec       YDOT =        1970
431995  meter/sec
 ZDOT =     -15135
681363                 ZDOT =       -4641
659908

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17870780
77                 X    =        -5447013
98
 Y    =        6693853
15  feet           Y    =         2040286
44  meter
 Z    =       11033506
50                 Z    =         3363012
78
 XDOT =     -14154
539662                 XDOT =       -4314
303689
 YDOT =     -12564
960465  feet/sec       YDOT =       -3829
799950  meter/sec
 ZDOT =     -15242
873701                 ZDOT =       -4646
027904


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   07268
85463786  
00020000  00000-0  20000-3 0  9076
2 25544  51
6341 304
4832 0002263  42
7212 317
4127 15
75120023 26668


Satellite: ISS
Catalog Number: 25544
Epoch time:      07268
85463786   =   yrday
fracday
Element set:     907
Inclination:       51
6341  deg
RA of node:       304
4832  deg
Eccentricity:     
0002263     
Arg of perigee:    42
7212  deg
Mean anomaly:     317
4127  deg
Mean motion:   15
75120023  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2666
Checksum:              276


Coasting Arc #9 (Orbit 2681)
---------------------------------------

Vector Time (GMT): 2007/269/19:34:52
106
Vector Time (MET): N/A
Weight (LBS)     : 508517
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4877939
76                 A    =         6720929
85  meter
 Y    =       -1785371
36  meter          E    =           
0011079
 Z    =        4256303
40                 I    =           51
34494
 XDOT =       -570
631623                 Wp   =           97
49827
 YDOT =       6836
666240  meter/sec      RA   =          298
94617  deg
 ZDOT =       3512
493721                 TA   =          316
75523
                                          MA   =          316
84216
                                          Ha   =            188
902  n
mi
                                          Hp   =            181
385

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16003739
38                 X    =         4876864
91
 Y    =       -5857517
59  feet           Y    =        -1730829
05  meter
 Z    =       13964250
01                 Z    =         4279998
28
 XDOT =      -1872
150994                 XDOT =        -664
101100
 YDOT =      22430
007348  feet/sec       YDOT =        6829
762859  meter/sec
 ZDOT =      11523
929531                 ZDOT =        3509
493822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12688299
71                 X    =         3867393
75
 Y    =       11266027
44  feet           Y    =         3433885
16  meter
 Z    =       14053972
42                 Z    =         4283650
79
 XDOT =     -19860
853445                 XDOT =       -6053
588130
 YDOT =       7968
130592  feet/sec       YDOT =        2428
686204  meter/sec
 ZDOT =      11513
380859                 ZDOT =        3509
278486


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   07269
86974051  
00020000  00000-0  20000-3 0  9081
2 25544  51
6338 299
2602 0002285  46
8091 313
3264 15
75141797 26820


Satellite: ISS
Catalog Number: 25544
Epoch time:      07269
86974051   =   yrday
fracday
Element set:     908
Inclination:       51
6338  deg
RA of node:       299
2602  deg
Eccentricity:     
0002285     
Arg of perigee:    46
8091  deg
Mean anomaly:     313
3264  deg
Mean motion:   15
75141797  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2682
Checksum:              313


Coasting Arc #10 (Orbit 2696)
---------------------------------------

Vector Time (GMT): 2007/270/19:34:52
106
Vector Time (MET): N/A
Weight (LBS)     : 508517
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         308363
07                 A    =         6725603
16  meter
 Y    =       -6136309
13  meter          E    =           
0007086
 Z    =       -2734966
12                 I    =           51
34830
 XDOT =       5371
246316                 Wp   =           54
79473
 YDOT =      -2012
869735  meter/sec      RA   =          293
73212  deg
 ZDOT =       5135
161628                 TA   =          273
82391
                                          MA   =          273
90493
                                          Ha   =            188
993  n
mi
                                          Hp   =            181
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1011689
87                 X    =          390243
50
 Y    =      -20132247
80  feet           Y    =        -6132403
26  meter
 Z    =       -8972985
95                 Z    =        -2733268
64
 XDOT =      17622
199199                 XDOT =        5368
409179
 YDOT =      -6603
903329  feet/sec       YDOT =       -1952
820835  meter/sec
 ZDOT =      16847
643137                 ZDOT =        5161
248897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18093753
66                 X    =         5514976
12
 Y    =       -8890954
47  feet           Y    =        -2709962
92  meter
 Z    =       -8967296
23                 Z    =        -2733231
89
 XDOT =      13664
881627                 XDOT =        4165
055920
 YDOT =      10761
444563  feet/sec       YDOT =        3280
088303  meter/sec
 ZDOT =      16946
416262                 ZDOT =        5165
267677


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   07270
82138833  
00020000  00000-0  20000-3 0  9090
2 25544  51
6341 294
3636 0002299  49
0883 311
0480 15
75165762 26975


Satellite: ISS
Catalog Number: 25544
Epoch time:      07270
82138833   =   yrday
fracday
Element set:     909
Inclination:       51
6341  deg
RA of node:       294
3636  deg
Eccentricity:     
0002299     
Arg of perigee:    49
0883  deg
Mean anomaly:     311
0480  deg
Mean motion:   15
75165762  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2697
Checksum:              307


Coasting Arc #11 (Orbit 2712)
---------------------------------------

Vector Time (GMT): 2007/271/19:34:52
106
Vector Time (MET): N/A
Weight (LBS)     : 508517
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4525251
97                 A    =         6719122
44  meter
 Y    =        1675033
79  meter          E    =           
0013498
 Z    =       -4688770
96                 I    =           51
31694
 XDOT =        137
880308                 Wp   =           67
56320
 YDOT =      -7198
804096  meter/sec      RA   =          288
60916  deg
 ZDOT =      -2705
928919                 TA   =          175
65648
                                          MA   =          175
64475
                                          Ha   =            188
995  n
mi
                                          Hp   =            181
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14846627
19                 X    =        -4520868
41
 Y    =        5495517
68  feet           Y    =         1624454
09  meter
 Z    =      -15383106
83                 Z    =        -4710744
57
 XDOT =        452
363214                 XDOT =         231
513370
 YDOT =     -23618
123676  feet/sec       YDOT =       -7196
738872  meter/sec
 ZDOT =      -8877
719550                 ZDOT =       -2705
031217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12169765
51                 X    =        -3709344
53
 Y    =       -9997658
19  feet           Y    =        -3047286
22  meter
 Z    =      -15466307
49                 Z    =        -4714130
52
 XDOT =      19941
243259                 XDOT =        6078
090945
 YDOT =     -10549
550109  feet/sec       YDOT =       -3215
502873  meter/sec
 ZDOT =      -8875
194203                 ZDOT =       -2705
159193


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   07271
83646707  
00020000  00000-0  20000-3 0  9108
2 25544  51
6346 289
1404 0002383  51
7220 308
4157 15
75196030 27136


Satellite: ISS
Catalog Number: 25544
Epoch time:      07271
83646707   =   yrday
fracday
Element set:     910
Inclination:       51
6346  deg
RA of node:       289
1404  deg
Eccentricity:     
0002383     
Arg of perigee:    51
7220  deg
Mean anomaly:     308
4157  deg
Mean motion:   15
75196030  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2713
Checksum:              276


Coasting Arc #12 (Orbit 2728)
---------------------------------------

Vector Time (GMT): 2007/272/19:34:52
106
Vector Time (MET): N/A
Weight (LBS)     : 508517
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          96695
20                 A    =         6727136
62  meter
 Y    =        6422430
91  meter          E    =           
0015596
 Z    =        1978012
98                 I    =           51
33545
 XDOT =      -5010
179868                 Wp   =          104
76078
 YDOT =       1800
796256  meter/sec      RA   =          283
40213  deg
 ZDOT =      -5569
483421                 TA   =           53
09576
                                          MA   =           52
95295
                                          Ha   =            189
044  n
mi
                                          Hp   =            181
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         317241
47                 X    =           15262
38
 Y    =       21070967
55  feet           Y    =         6423056
95  meter
 Z    =        6489543
89                 Z    =         1978284
76
 XDOT =     -16437
597992                 XDOT =       -5002
888118
 YDOT =       5908
124198  feet/sec       YDOT =        1744
810212  meter/sec
 ZDOT =     -18272
583403                 ZDOT =       -5593
805757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17885684
39                 X    =        -5451556
60
 Y    =       11142936
64  feet           Y    =         3396367
09  meter
 Z    =        6491359
84                 Z    =         1978566
48
 XDOT =     -12695
263693                 XDOT =       -3869
516374
 YDOT =      -9616
604478  feet/sec       YDOT =       -2931
141045  meter/sec
 ZDOT =     -18364
687040                 ZDOT =       -5597
556610


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   07272
85153446  
00020000  00000-0  20000-3 0  9115
2 25544  51
6343 283
9172 0002343  57
5205 302
6185 15
75175113 27293


Satellite: ISS
Catalog Number: 25544
Epoch time:      07272
85153446   =   yrday
fracday
Element set:     911
Inclination:       51
6343  deg
RA of node:       283
9172  deg
Eccentricity:     
0002343     
Arg of perigee:    57
5205  deg
Mean anomaly:     302
6185  deg
Mean motion:   15
75175113  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2729
Checksum:              280


Coasting Arc #13 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2007/273/19:34:52
106
Vector Time (MET): N/A
Weight (LBS)     : 508517
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4251193
65                 A    =         6717717
98  meter
 Y    =       -1443890
55  meter          E    =           
0006774
 Z    =        4991958
24                 I    =           51
29935
 XDOT =        391
462902                 Wp   =          106
42463
 YDOT =       7477
725324  meter/sec      RA   =          278
26703  deg
 ZDOT =       1825
572658                 TA   =          325
88531
                                          MA   =          325
92883
                                          Ha   =            188
858  n
mi
                                          Hp   =            181
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13947485
74                 X    =         4242772
98
 Y    =       -4737173
73  feet           Y    =        -1396398
38  meter
 Z    =       16377815
75                 Z    =         5012590
49
 XDOT =       1284
327107                 XDOT =         298
948286
 YDOT =      24533
219567  feet/sec       YDOT =        7481
585609  meter/sec
 ZDOT =       5989
411608                 ZDOT =        1827
249696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11382985
63                 X    =         3469534
02
 Y    =        9210592
38  feet           Y    =         2807388
56  meter
 Z    =       16455960
87                 Z    =         5015776
87
 XDOT =     -19435
163025                 XDOT =       -5923
837690
 YDOT =      13282
250679  feet/sec       YDOT =        4048
430007  meter/sec
 ZDOT =       5996
688742                 ZDOT =        1827
790729


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   07273
86658725  
00020000  00000-0  20000-3 0  9128
2 25544  51
6349 278
6939 0002345  58
4800 301
6592 15
75223898 27457


Satellite: ISS
Catalog Number: 25544
Epoch time:      07273
86658725   =   yrday
fracday
Element set:     912
Inclination:       51
6349  deg
RA of node:       278
6939  deg
Eccentricity:     
0002345     
Arg of perigee:    58
4800  deg
Mean anomaly:     301
6592  deg
Mean motion:   15
75223898  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2745
Checksum:              327

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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