Date: July 18th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6619 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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


202/01:19:29 707 -1 0 3 4 3 4
N/A 3 2 0 1 186 9
000/00:04:59 415 0 0 0 2 172 6

204/22:30:58 096 2 2 11 1 11 1
N/A -10 7 -0 0 187 3
000/00:19:56 192 2 0 0 5 179 5

Coasting Arc #1 (Orbit 1540)
---------------------------------------

Vector Time (GMT): 2007/197/12:47:21
841
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2446116
69                 A    =         6705850
47  meter
 Y    =       -3494596
63  meter          E    =           
0022446
 Z    =       -5193358
51                 I    =           51
37564
 XDOT =       5581
832317                 Wp   =           87
26919
 YDOT =      -5218
809849  meter/sec      RA   =          311
60373  deg
 ZDOT =        886
978557                 TA   =          191
19264
                                          MA   =          191
24265
                                          Ha   =            185
219  n
mi
                                          Hp   =            172
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8025317
22                 X    =        -2381629
99
 Y    =      -11465212
04  feet           Y    =        -3521589
17  meter
 Z    =      -17038577
79                 Z    =        -5205085
34
 XDOT =      18313
098152                 XDOT =        5635
466286
 YDOT =     -17122
079556  feet/sec       YDOT =       -5156
090908  meter/sec
 ZDOT =       2910
034635                 ZDOT =         914
223985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4824250
48                 X    =        -1470431
55
 Y    =       13078853
71  feet           Y    =         3986434
61  meter
 Z    =      -17083329
01                 Z    =        -5206998
68
 XDOT =     -23573
858086                 XDOT =       -7185
311945
 YDOT =      -4779
058911  feet/sec       YDOT =       -1456
657156  meter/sec
 ZDOT =       3012
561816                 ZDOT =         918
228842


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   07197
54720373  
00020000  00000-0  20000-3 0  9004
2 25544  51
6358 312
1054 0008355  70
7109 289
4960 15
79113360 15416


Satellite: ISS
Catalog Number: 25544
Epoch time:      07197
54720373   =   yrday
fracday
Element set:     900
Inclination:       51
6358  deg
RA of node:       312
1054  deg
Eccentricity:     
0008355     
Arg of perigee:    70
7109  deg
Mean anomaly:     289
4960  deg
Mean motion:   15
79113360  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1541
Checksum:              282


Coasting Arc #2 (Orbit 1556)
---------------------------------------

Vector Time (GMT): 2007/198/12:47:21
841
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5093881
79                 A    =         6715001
96  meter
 Y    =        3655435
20  meter          E    =           
0012138
 Z    =       -2412496
23                 I    =           51
38824
 XDOT =      -1338
058670                 Wp   =           96
58261
 YDOT =      -5377
836407  meter/sec      RA   =          306
43984  deg
 ZDOT =      -5347
639577                 TA   =          110
77765
                                          MA   =          110
64756
                                          Ha   =            185
184  n
mi
                                          Hp   =            172
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16712210
61                 X    =        -5122659
61
 Y    =       11992897
65  feet           Y    =         3598311
94  meter
 Z    =       -7915013
87                 Z    =        -2437311
23
 XDOT =      -4389
956266                 XDOT =       -1251
846162
 YDOT =     -17643
820232  feet/sec       YDOT =       -5392
316648  meter/sec
 ZDOT =     -17544
749269                 ZDOT =       -5353
930969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19507245
22                 X    =         5945808
34
 Y    =        6411409
45  feet           Y    =         1954197
60  meter
 Z    =       -8008510
16                 Z    =        -2440993
90
 XDOT =     -11267
236543                 XDOT =       -3434
253698
 YDOT =      12434
447934  feet/sec       YDOT =        3790
019730  meter/sec
 ZDOT =     -17569
146276                 ZDOT =       -5355
075785


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   07198
55974371  
00020000  00000-0  20000-3 0  9016
2 25544  51
6354 306
8653 0008325  74
6128 285
5957 15
79131959 15572


Satellite: ISS
Catalog Number: 25544
Epoch time:      07198
55974371   =   yrday
fracday
Element set:     901
Inclination:       51
6354  deg
RA of node:       306
8653  deg
Eccentricity:     
0008325     
Arg of perigee:    74
6128  deg
Mean anomaly:     285
5957  deg
Mean motion:   15
79131959  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1557
Checksum:              330


Coasting Arc #3 (Orbit 1572)
---------------------------------------

Vector Time (GMT): 2007/199/12:47:21
841
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -28278
53                 A    =         6711767
40  meter
 Y    =        5639628
09  meter          E    =           
0020400
 Z    =        3624121
67                 I    =           51
36107
 XDOT =      -5740
650405                 Wp   =           81
87337
 YDOT =       2777
287658  meter/sec      RA   =          301
19812  deg
 ZDOT =      -4343
008485                 TA   =           54
32873
                                          MA   =           54
13899
                                          Ha   =            185
210  n
mi
                                          Hp   =            172
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -92777
31                 X    =         -108944
58
 Y    =       18502716
85  feet           Y    =         5638860
47  meter
 Z    =       11890162
97                 Z    =         3623788
94
 XDOT =     -18834
154873                 XDOT =       -5750
182628
 YDOT =       9111
836147  feet/sec       YDOT =        2713
039624  meter/sec
 ZDOT =     -14248
715502                 ZDOT =       -4370
918926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14862218
14                 X    =         4530004
09
 Y    =      -11022188
17  feet           Y    =        -3359562
95  meter
 Z    =       11889531
26                 Z    =         3623929
13
 XDOT =      17768
905502                 XDOT =        5415
962397
 YDOT =       8392
276158  feet/sec       YDOT =        2557
965773  meter/sec
 ZDOT =     -14354
017996                 ZDOT =       -4375
104685


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   07199
57226073  
00020000  00000-0  20000-3 0  9029
2 25544  51
6351 301
6255 0008458  77
5864 282
6248 15
79165421 15736


Satellite: ISS
Catalog Number: 25544
Epoch time:      07199
57226073   =   yrday
fracday
Element set:     902
Inclination:       51
6351  deg
RA of node:       301
6255  deg
Eccentricity:     
0008458     
Arg of perigee:    77
5864  deg
Mean anomaly:     282
6248  deg
Mean motion:   15
79165421  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1573
Checksum:              307


Coasting Arc #4 (Orbit 1588)
---------------------------------------

Vector Time (GMT): 2007/200/12:47:21
841
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4653027
24                 A    =         6707375
35  meter
 Y    =        -887381
39  meter          E    =           
0014722
 Z    =        4737187
24                 I    =           51
33301
 XDOT =      -1236
942780                 Wp   =           98
89841
 YDOT =       7178
869355  meter/sec      RA   =          296
04817  deg
 ZDOT =       2550
758856                 TA   =          326
01364
                                          MA   =          326
10786
                                          Ha   =            184
956  n
mi
                                          Hp   =            172
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15265837
40                 X    =         4639592
18
 Y    =       -2911356
28  feet           Y    =         -835424
18  meter
 Z    =       15541952
87                 Z    =         4759758
61
 XDOT =      -4058
211219                 XDOT =       -1329
516970
 YDOT =      23552
720982  feet/sec       YDOT =        7164
519321  meter/sec
 ZDOT =       8368
631418                 ZDOT =        2544
525679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11646278
33                 X    =        -3549785
64
 Y    =      -10160067
40  feet           Y    =        -3096788
54  meter
 Z    =       15627262
00                 Z    =         4763189
46
 XDOT =      20338
181179                 XDOT =        6199
077623
 YDOT =     -10431
409881  feet/sec       YDOT =       -3179
493732  meter/sec
 ZDOT =       8345
851737                 ZDOT =        2543
815609


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   07200
58475281  
00020000  00000-0  20000-3 0  9031
2 25544  51
6350 296
3850 0008305  81
0610 279
1496 15
79229554 15897


Satellite: ISS
Catalog Number: 25544
Epoch time:      07200
58475281   =   yrday
fracday
Element set:     903
Inclination:       51
6350  deg
RA of node:       296
3850  deg
Eccentricity:     
0008305     
Arg of perigee:    81
0610  deg
Mean anomaly:     279
1496  deg
Mean motion:   15
79229554  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1589
Checksum:              300


Coasting Arc #5 (Orbit 1603)
---------------------------------------

Vector Time (GMT): 2007/201/12:47:21
841
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1954800
25                 A    =         6717283
55  meter
 Y    =       -6396673
85  meter          E    =           
0018205
 Z    =        -559209
42                 I    =           51
35417
 XDOT =       4762
903734                 Wp   =           58
54772
 YDOT =        945
364411  meter/sec      RA   =          290
82608  deg
 ZDOT =       5987
772472                 TA   =          295
32867
                                          MA   =          295
51713
                                          Ha   =            185
149  n
mi
                                          Hp   =            172
760

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6413386
64                 X    =         2028900
02
 Y    =      -20986462
78  feet           Y    =        -6374399
81  meter
 Z    =       -1834676
57                 Z    =         -549533
70
 XDOT =      15626
324586                 XDOT =        4722
891323
 YDOT =       3101
589276  feet/sec       YDOT =         998
401608  meter/sec
 ZDOT =      19644
922807                 ZDOT =        6010
813322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20348232
33                 X    =        -6202141
21
 Y    =        8224535
87  feet           Y    =         2506838
53  meter
 Z    =       -1798787
68                 Z    =         -548270
49
 XDOT =      -6760
906811                 XDOT =       -2060
724396
 YDOT =     -12522
803056  feet/sec       YDOT =       -3816
950372  meter/sec
 ZDOT =      19732
215177                 ZDOT =        6014
379186


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   07201
53394581  
00020000  00000-0  20000-3 0  9041
2 25544  51
6345 291
4727 0008384  82
6558 277
5560 15
79199936 16047


Satellite: ISS
Catalog Number: 25544
Epoch time:      07201
53394581   =   yrday
fracday
Element set:     904
Inclination:       51
6345  deg
RA of node:       291
4727  deg
Eccentricity:     
0008384     
Arg of perigee:    82
6558  deg
Mean anomaly:     277
5560  deg
Mean motion:   15
79199936  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1604
Checksum:              320


Coasting Arc #6 (Orbit 1612)
---------------------------------------

Vector Time (GMT): 2007/202/01:21:59
415
Vector Time (MET): N/A
Weight (LBS)     : 508908
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3762322
26                 A    =         6706971
90  meter
 Y    =        1904311
37  meter          E    =           
0013829
 Z    =        5204063
19                 I    =           51
30958
 XDOT =      -2824
980566                 Wp   =           79
82440
 YDOT =       7160
929616  meter/sec      RA   =          288
10362  deg
 ZDOT =       -574
333731                 TA   =           15
66676
                                          MA   =           15
62401
                                          Ha   =            186
865  n
mi
                                          Hp   =            172
626

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12343576
97                 X    =         3715468
16
 Y    =        6247740
71  feet           Y    =         1946121
30  meter
 Z    =       17073698
14                 Z    =         5222226
78
 XDOT =      -9268
308944                 XDOT =       -2902
055192
 YDOT =      23493
863568  feet/sec       YDOT =        7128
908202  meter/sec
 ZDOT =      -1884
297018                 ZDOT =        -588
243907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4965961
93                 X    =         1513625
19
 Y    =       12821009
45  feet           Y    =         3907843
68  meter
 Z    =       17142644
59                 Z    =         5225078
07
 XDOT =     -21625
927814                 XDOT =       -6591
582798
 YDOT =      10981
297775  feet/sec       YDOT =        3347
099562  meter/sec
 ZDOT =      -1936
120401                 ZDOT =        -590
129498


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   07202
10347595  
00020000  00000-0  20000-3 0  9059
2 25544  51
6351 288
5259 0011093  83
8325 276
4104 15
78653530 16133


Satellite: ISS
Catalog Number: 25544
Epoch time:      07202
10347595   =   yrday
fracday
Element set:     905
Inclination:       51
6351  deg
RA of node:       288
5259  deg
Eccentricity:     
0011093     
Arg of perigee:    83
8325  deg
Mean anomaly:     276
4104  deg
Mean motion:   15
78653530  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1613
Checksum:              284


Coasting Arc #7 (Orbit 1628)
---------------------------------------

Vector Time (GMT): 2007/203/01:21:59
415
Vector Time (MET): N/A
Weight (LBS)     : 508908
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2932819
20                 A    =         6717275
56  meter
 Y    =       -5698560
46  meter          E    =           
0024981
 Z    =        1978512
35                 I    =           51
33634
 XDOT =       3690
210278                 Wp   =           76
35975
 YDOT =       3852
391493  meter/sec      RA   =          282
93290  deg
 ZDOT =       5572
734991                 TA   =          305
83591
                                          MA   =          306
06773
                                          Ha   =            186
991  n
mi
                                          Hp   =            172
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9622110
25                 X    =         2986712
17
 Y    =      -18696064
51  feet           Y    =        -5665462
91  meter
 Z    =        6491182
26                 Z    =         1992890
22
 XDOT =      12106
989101                 XDOT =        3619
786808
 YDOT =      12639
079703  feet/sec       YDOT =        3893
263153  meter/sec
 ZDOT =      18283
251282                 ZDOT =        5590
491291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19474694
73                 X    =         5935886
96
 Y    =       -7884371
26  feet           Y    =        -2403156
36  meter
 Z    =        6544939
72                 Z    =         1994897
63
 XDOT =        249
152928                 XDOT =          75
941813
 YDOT =      15991
627920  feet/sec       YDOT =        4874
248190  meter/sec
 ZDOT =      18350
880264                 ZDOT =        5593
348305


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   07203
11632642  
00020000  00000-0  20000-3 0  9062
2 25544  51
6349 283
2876 0011148  86
9236 273
3205 15
78641477 16295


Satellite: ISS
Catalog Number: 25544
Epoch time:      07203
11632642   =   yrday
fracday
Element set:     906
Inclination:       51
6349  deg
RA of node:       283
2876  deg
Eccentricity:     
0011148     
Arg of perigee:    86
9236  deg
Mean anomaly:     273
3205  deg
Mean motion:   15
78641477  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1629
Checksum:              299


Coasting Arc #8 (Orbit 1643)
---------------------------------------

Vector Time (GMT): 2007/204/01:21:59
415
Vector Time (MET): N/A
Weight (LBS)     : 508908
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2648788
21                 A    =         6711646
72  meter
 Y    =       -4659605
43  meter          E    =           
0018279
 Z    =       -4056946
40                 I    =           51
31245
 XDOT =       3822
071153                 Wp   =           97
97355
 YDOT =      -5482
222825  meter/sec      RA   =          277
69399  deg
 ZDOT =       3813
324791                 TA   =          211
38565
                                          MA   =          211
49486
                                          Ha   =            186
887  n
mi
                                          Hp   =            172
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8690250
02                 X    =        -2576779
11
 Y    =      -15287419
40  feet           Y    =        -4688822
56  meter
 Z    =      -13310191
59                 Z    =        -4069639
82
 XDOT =      12539
603520                 XDOT =        3864
565735
 YDOT =     -17986
295358  feet/sec       YDOT =       -5439
245140  meter/sec
 ZDOT =      12510
908107                 ZDOT =        3831
994905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3175267
95                 X    =          967821
67
 Y    =      -17258276
68  feet           Y    =        -5260322
73  meter
 Z    =      -13358757
32                 Z    =        -4071749
23
 XDOT =      19837
660482                 XDOT =        6046
518915
 YDOT =      -6057
667911  feet/sec       YDOT =       -1846
377179  meter/sec
 ZDOT =      12580
932887                 ZDOT =        3834
668344


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   07204
06585212  
00020000  00000-0  20000-3 0  9078
2 25544  51
6347 278
3766 0010998  90
4329 269
8096 15
78683753 16449


Satellite: ISS
Catalog Number: 25544
Epoch time:      07204
06585212   =   yrday
fracday
Element set:     907
Inclination:       51
6347  deg
RA of node:       278
3766  deg
Eccentricity:     
0010998     
Arg of perigee:    90
4329  deg
Mean anomaly:     269
8096  deg
Mean motion:   15
78683753  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1644
Checksum:              329


Coasting Arc #9 (Orbit 1657)
---------------------------------------

Vector Time (GMT): 2007/204/22:40:56
192
Vector Time (MET): N/A
Weight (LBS)     : 508148
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2393036
64                 A    =         6720783
66  meter
 Y    =       -5320298
65  meter          E    =           
0006815
 Z    =       -3341527
71                 I    =           51
31735
 XDOT =       3969
973012                 Wp   =           78
66606
 YDOT =      -4691
834890  meter/sec      RA   =          273
07963  deg
 ZDOT =       4636
431222                 TA   =          241
78656
                                          MA   =          241
85539
                                          Ha   =            187
289  n
mi
                                          Hp   =            179
533

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7851170
07                 X    =        -2317133
93
 Y    =      -17455048
07  feet           Y    =        -5346634
08  meter
 Z    =      -10963017
43                 Z    =        -3352969
41
 XDOT =      13024
845839                 XDOT =        3999
619872
 YDOT =     -15393
159087  feet/sec       YDOT =       -4647
275291  meter/sec
 ZDOT =      15211
388524                 ZDOT =        4655
788662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15689511
99                 X    =         4782163
26
 Y    =      -10917607
07  feet           Y    =        -3327686
63  meter
 Z    =      -11006924
87                 Z    =        -3354910
70
 XDOT =      16746
057396                 XDOT =        5104
198294
 YDOT =       8686
987874  feet/sec       YDOT =        2647
793904  meter/sec
 ZDOT =      15284
106660                 ZDOT =        4658
595710


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   07204
95206369  
00020000  00000-0  20000-3 0  9080
2 25544  51
6342 273
7929 0002230  56
4762 303
6615 15
76281048 16585


Satellite: ISS
Catalog Number: 25544
Epoch time:      07204
95206369   =   yrday
fracday
Element set:     908
Inclination:       51
6342  deg
RA of node:       273
7929  deg
Eccentricity:     
0002230     
Arg of perigee:    56
4762  deg
Mean anomaly:     303
6615  deg
Mean motion:   15
76281048  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1658
Checksum:              297


Coasting Arc #10 (Orbit 1673)
---------------------------------------

Vector Time (GMT): 2007/205/22:40:56
192
Vector Time (MET): N/A
Weight (LBS)     : 508148
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3481136
73                 A    =         6716693
68  meter
 Y    =        3581859
21  meter          E    =           
0012285
 Z    =       -4502852
58                 I    =           51
30411
 XDOT =      -2706
539833                 Wp   =           67
42084
 YDOT =      -6507
702692  meter/sec      RA   =          267
95171  deg
 ZDOT =      -3086
280853                 TA   =          171
66271
                                          MA   =          171
64227
                                          Ha   =            187
275  n
mi
                                          Hp   =            179
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11421052
27                 X    =        -3499056
94
 Y    =       11751506
60  feet           Y    =         3542831
68  meter
 Z    =      -14773138
39                 Z    =        -4519806
85
 XDOT =      -8879
723863                 XDOT =       -2618
576060
 YDOT =     -21350
730617  feet/sec       YDOT =       -6537
476436  meter/sec
 ZDOT =     -10125
593351                 ZDOT =       -3099
216508

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13816989
04                 X    =        -4211418
26
 Y    =       -8702953
49  feet           Y    =        -2652660
22  meter
 Z    =      -14836892
35                 Z    =        -4522284
79
 XDOT =      18467
834573                 XDOT =        5628
995978
 YDOT =     -11984
372486  feet/sec       YDOT =       -3652
836734  meter/sec
 ZDOT =     -10175
295360                 ZDOT =       -3101
430026


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   07205
96642238  
00020000  00000-0  20000-3 0  9092
2 25544  51
6347 268
5653 0002280  57
7720 302
3665 15
76316858 16746


Satellite: ISS
Catalog Number: 25544
Epoch time:      07205
96642238   =   yrday
fracday
Element set:     909
Inclination:       51
6347  deg
RA of node:       268
5653  deg
Eccentricity:     
0002280     
Arg of perigee:    57
7720  deg
Mean anomaly:     302
3665  deg
Mean motion:   15
76316858  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1674
Checksum:              310


Coasting Arc #11 (Orbit 1689)
---------------------------------------

Vector Time (GMT): 2007/206/22:40:56
192
Vector Time (MET): N/A
Weight (LBS)     : 508148
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2361860
23                 A    =         6723898
59  meter
 Y    =        5967172
55  meter          E    =           
0015728
 Z    =        1984463
23                 I    =           51
33012
 XDOT =      -4049
464672                 Wp   =          105
52771
 YDOT =       3464
971615  meter/sec      RA   =          262
73357  deg
 ZDOT =      -5566
998519                 TA   =           52
23914
                                          MA   =           52
09675
                                          Ha   =            187
304  n
mi
                                          Hp   =            179
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7748885
28                 X    =         2285318
80
 Y    =       19577337
76  feet           Y    =         5993155
90  meter
 Z    =        6510706
12                 Z    =         1995752
14
 XDOT =     -13285
645249                 XDOT =       -4060
866262
 YDOT =      11368
017111  feet/sec       YDOT =        3419
625405  meter/sec
 ZDOT =     -18264
430835                 ZDOT =       -5586
697792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17391704
86                 X    =        -5300991
64
 Y    =       11843934
26  feet           Y    =         3610031
16  meter
 Z    =        6554120
41                 Z    =         1997695
90
 XDOT =     -13134
261993                 XDOT =       -4003
323055
 YDOT =      -9079
891956  feet/sec       YDOT =       -2767
551068  meter/sec
 ZDOT =     -18338
591472                 ZDOT =       -5589
602681


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   07206
98076457  
00020000  00000-0  20000-3 0  9101
2 25544  51
6342 263
3375 0002262  63
7649 296
3748 15
76302609 16903


Satellite: ISS
Catalog Number: 25544
Epoch time:      07206
98076457   =   yrday
fracday
Element set:     910
Inclination:       51
6342  deg
RA of node:       263
3375  deg
Eccentricity:     
0002262     
Arg of perigee:    63
7649  deg
Mean anomaly:     296
3748  deg
Mean motion:   15
76302609  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1690
Checksum:              306


Coasting Arc #12 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2007/207/22:40:56
192
Vector Time (MET): N/A
Weight (LBS)     : 508148
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3639746
86                 A    =         6714051
19  meter
 Y    =       -2427002
54  meter          E    =           
0005948
 Z    =        5088609
11                 I    =           51
30265
 XDOT =       2722
595017                 Wp   =          106
30933
 YDOT =       7070
707457  meter/sec      RA   =          257
58721  deg
 ZDOT =       1421
938916                 TA   =          330
00324
                                          MA   =          330
03731
                                          Ha   =            187
110  n
mi
                                          Hp   =            179
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11941426
70                 X    =         3641896
20
 Y    =       -7962606
76  feet           Y    =        -2386289
70  meter
 Z    =       16694911
78                 Z    =         5106295
60
 XDOT =       8932
398349                 XDOT =        2636
419534
 YDOT =      23197
859111  feet/sec       YDOT =        7100
670969  meter/sec
 ZDOT =       4665
153923                 ZDOT =        1434
957031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10548724
08                 X    =         3215251
10
 Y    =        9617419
70  feet           Y    =         2931389
52  meter
 Z    =       16761578
57                 Z    =         5108929
15
 XDOT =     -19717
469695                 XDOT =       -6009
884763
 YDOT =      13391
699455  feet/sec       YDOT =        4081
789994  meter/sec
 ZDOT =       4715
250211                 ZDOT =        1437
208264


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   07207
99508678  
00020000  00000-0  20000-3 0  9119
2 25544  51
6344 258
1096 0002239  63
7634 296
3760 15
76363993 17060


Satellite: ISS
Catalog Number: 25544
Epoch time:      07207
99508678   =   yrday
fracday
Element set:     911
Inclination:       51
6344  deg
RA of node:       258
1096  deg
Eccentricity:     
0002239     
Arg of perigee:    63
7634  deg
Mean anomaly:     296
3760  deg
Mean motion:   15
76363993  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1706
Checksum:              321


Coasting Arc #13 (Orbit 1720)
---------------------------------------

Vector Time (GMT): 2007/208/22:40:56
192
Vector Time (MET): N/A
Weight (LBS)     : 508148
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2372883
50                 A    =         6725275
64  meter
 Y    =       -6270024
02  meter          E    =           
0013306
 Z    =        -456676
85                 I    =           51
34822
 XDOT =       4369
687372                 Wp   =           45
27356
 YDOT =      -2081
915439  meter/sec      RA   =          252
39395  deg
 ZDOT =       5995
125866                 TA   =          309
73398
                                          MA   =          309
85116
                                          Ha   =            187
149  n
mi
                                          Hp   =            179
354

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7785050
85                 X    =        -2300376
39
 Y    =      -20570944
96  feet           Y    =        -6296153
46  meter
 Z    =       -1498283
63                 Z    =         -468029
06
 XDOT =      14336
244659                 XDOT =        4363
520143
 YDOT =      -6830
431230  feet/sec       YDOT =       -2033
086625  meter/sec
 ZDOT =      19669
048118                 ZDOT =        6016
338132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17918665
98                 X    =         5461609
39
 Y    =      -12749875
11  feet           Y    =        -3886161
93  meter
 Z    =       -1541992
64                 Z    =         -469999
36
 XDOT =       9292
349518                 XDOT =        2832
308133
 YDOT =      10715
658755  feet/sec       YDOT =        3266
132789  meter/sec
 ZDOT =      19749
107069                 ZDOT =        6019
527834


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   07208
94599898  
00020000  00000-0  20000-3 0  9120
2 25544  51
6343 253
2083 0002205  64
6697 295
4696 15
76393138 17212


Satellite: ISS
Catalog Number: 25544
Epoch time:      07208
94599898   =   yrday
fracday
Element set:     912
Inclination:       51
6343  deg
RA of node:       253
2083  deg
Eccentricity:     
0002205     
Arg of perigee:    64
6697  deg
Mean anomaly:     295
4696  deg
Mean motion:   15
76393138  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1721
Checksum:              324

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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