Date: August 14th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6200 0 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


235/17:58:05 000 0 0 0 0 0 0
014/19:21:23 047 0 0 0 0 184 7
000/00:00:00 000 0 0 0 0 183 8

Coasting Arc #1 (Orbit 1985)
---------------------------------------

Vector Time (GMT): 2007/225/17:58:05
000
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6410785
16                 A    =         6725676
40  meter
 Y    =        1979537
79  meter          E    =           
0004474
 Z    =        -421530
96                 I    =           51
73235
 XDOT =      -1771
649398                 Wp   =             
58837
 YDOT =      -4455
040286  meter/sec      RA   =          165
68096  deg
 ZDOT =       6027
621223                 TA   =          354
83092
                                          MA   =          354
83554
                                          Ha   =            185
979  n
mi
                                          Hp   =            182
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21032759
71                 X    =        -6430396
51
 Y    =        6494546
56  feet           Y    =         1907739
14  meter
 Z    =       -1382975
60                 Z    =         -452721
42
 XDOT =      -5812
498025                 XDOT =       -1750
981233
 YDOT =     -14616
273903  feet/sec       YDOT =       -4474
736495  meter/sec
 ZDOT =      19775
660182                 ZDOT =        6019
064809

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8335815
50                 X    =         2540756
57
 Y    =      -20364920
37  feet           Y    =        -6207227
73  meter
 Z    =       -1500978
17                 Z    =         -457498
15
 XDOT =      13567
140084                 XDOT =        4135
264298
 YDOT =       4099
321506  feet/sec       YDOT =        1249
473195  meter/sec
 ZDOT =      19742
640955                 ZDOT =        6017
556963


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   07225
74954961  
00020000  00000-0  20000-3 0  9000
2 25544  51
6331 166
6653 0008449 241
9279 118
1032 15
76252900 19860


Satellite: ISS
Catalog Number: 25544
Epoch time:      07225
74954961   =   yrday
fracday
Element set:     900
Inclination:       51
6331  deg
RA of node:       166
6653  deg
Eccentricity:     
0008449     
Arg of perigee:   241
9279  deg
Mean anomaly:     118
1032  deg
Mean motion:   15
76252900  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1986
Checksum:              302


Coasting Arc #2 (Orbit 2001)
---------------------------------------

Vector Time (GMT): 2007/226/18:02:51
596
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1160160
55                 A    =         6715346
77  meter
 Y    =        4485121
93  meter          E    =           
0008182
 Z    =       -4867455
87                 I    =           51
72466
 XDOT =      -7311
110149                 Wp   =          150
18250
 YDOT =        640
478991  meter/sec      RA   =          160
50203  deg
 ZDOT =       2327
478483                 TA   =          142
49412
                                          MA   =          142
43701
                                          Ha   =            185
752  n
mi
                                          Hp   =            183
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3806301
02                 X    =        -1186582
85
 Y    =       14714966
97  feet           Y    =         4472000
69  meter
 Z    =      -15969343
40                 Z    =        -4873155
94
 XDOT =     -23986
581854                 XDOT =       -7329
034960
 YDOT =       2101
309024  feet/sec       YDOT =         558
621782  meter/sec
 ZDOT =       7636
084261                 ZDOT =        2291
918257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9464956
66                 X    =        -2884918
79
 Y    =      -11864260
84  feet           Y    =        -3616226
70  meter
 Z    =      -15990372
71                 Z    =        -4873865
60
 XDOT =      12004
517203                 XDOT =        3658
976844
 YDOT =     -19710
366381  feet/sec       YDOT =       -6007
719673  meter/sec
 ZDOT =       7501
332402                 ZDOT =        2286
406116


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   07226
76392237  
00020000  00000-0  20000-3 0  9016
2 25544  51
6322 161
4367 0008466 245
3482 114
6801 15
76279298 20022


Satellite: ISS
Catalog Number: 25544
Epoch time:      07226
76392237   =   yrday
fracday
Element set:     901
Inclination:       51
6322  deg
RA of node:       161
4367  deg
Eccentricity:     
0008466     
Arg of perigee:   245
3482  deg
Mean anomaly:     114
6801  deg
Mean motion:   15
76279298  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2002
Checksum:              290


Coasting Arc #3 (Orbit 2017)
---------------------------------------

Vector Time (GMT): 2007/227/18:07:53
868
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5193034
51                 A    =         6718452
86  meter
 Y    =        1172122
62  meter          E    =           
0000956
 Z    =       -4097262
91                 I    =           51
76114
 XDOT =      -4186
802278                 Wp   =          237
66009
 YDOT =       5222
817454  meter/sec      RA   =          155
38330  deg
 ZDOT =      -3812
264018                 TA   =          353
28322
                                          MA   =          353
28450
                                          Ha   =            185
666  n
mi
                                          Hp   =            183
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17037514
81                 X    =         5199445
18
 Y    =        3845546
65  feet           Y    =         1230229
91  meter
 Z    =      -13442463
60                 Z    =        -4072019
94
 XDOT =     -13736
227947                 XDOT =       -4226
374406
 YDOT =      17135
227868  feet/sec       YDOT =        5175
777020  meter/sec
 ZDOT =     -12507
427881                 ZDOT =       -3832
699315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12964529
13                 X    =        -3951588
48
 Y    =       11813316
81  feet           Y    =         3600698
96  meter
 Z    =      -13346591
25                 Z    =        -4068041
01
 XDOT =      -5338
493015                 XDOT =       -1627
172671
 YDOT =     -20076
827759  feet/sec       YDOT =       -6119
417101  meter/sec
 ZDOT =     -12584
235972                 ZDOT =       -3835
675124


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   07227
77828581  
00020000  00000-0  20000-3 0  9025
2 25544  51
6314 156
2094 0008440 249
3760 110
6500 15
76288570 20189


Satellite: ISS
Catalog Number: 25544
Epoch time:      07227
77828581   =   yrday
fracday
Element set:     902
Inclination:       51
6314  deg
RA of node:       156
2094  deg
Eccentricity:     
0008440     
Arg of perigee:   249
3760  deg
Mean anomaly:     110
6500  deg
Mean motion:   15
76288570  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2018
Checksum:              286


Coasting Arc #4 (Orbit 2033)
---------------------------------------

Vector Time (GMT): 2007/228/18:12:25
858
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5230929
89                 A    =         6724897
75  meter
 Y    =       -4051762
00  meter          E    =           
0010309
 Z    =        1162935
31                 I    =           51
80982
 XDOT =       3784
339645                 Wp   =          159
91241
 YDOT =       3188
199557  meter/sec      RA   =          150
18666  deg
 ZDOT =      -5908
286945                 TA   =            7
36399
                                          MA   =            7
34886
                                          Ha   =            185
203  n
mi
                                          Hp   =            183
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17161843
46                 X    =         5270199
24
 Y    =      -13293182
40  feet           Y    =        -3993047
22  meter
 Z    =        3815404
55                 Z    =         1188442
30
 XDOT =      12415
812482                 XDOT =        3777
108568
 YDOT =      10459
972300  feet/sec       YDOT =        3230
477744  meter/sec
 ZDOT =     -19384
143520                 ZDOT =       -5889
920373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1861397
57                 X    =          567353
98
 Y    =       21610864
17  feet           Y    =         6586991
40  meter
 Z    =        3911601
95                 Z    =         1192256
27
 XDOT =     -14007
262497                 XDOT =       -4269
413609
 YDOT =       4705
764633  feet/sec       YDOT =        1434
317060  meter/sec
 ZDOT =     -19314
080492                 ZDOT =       -5886
931734


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   07228
79263825  
00020000  00000-0  20000-3 0  9033
2 25544  51
6318 150
9812 0008503 254
5131 105
5095 15
76344632 20344


Satellite: ISS
Catalog Number: 25544
Epoch time:      07228
79263825   =   yrday
fracday
Element set:     903
Inclination:       51
6318  deg
RA of node:       150
9812  deg
Eccentricity:     
0008503     
Arg of perigee:   254
5131  deg
Mean anomaly:     105
5095  deg
Mean motion:   15
76344632  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2034
Checksum:              279


Coasting Arc #5 (Orbit 2049)
---------------------------------------

Vector Time (GMT): 2007/229/18:17:18
367
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -875135
81                 A    =         6714362
21  meter
 Y    =       -4284858
91  meter          E    =           
0004399
 Z    =        5098657
21                 I    =           51
79706
 XDOT =       6802
371622                 Wp   =          280
01789
 YDOT =      -3253
527111  meter/sec      RA   =          145
02514  deg
 ZDOT =      -1567
056645                 TA   =          184
98650
                                          MA   =          184
99088
                                          Ha   =            185
250  n
mi
                                          Hp   =            183
679

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2871180
49                 X    =         -851925
05
 Y    =      -14057936
04  feet           Y    =        -4294515
42  meter
 Z    =       16727878
00                 Z    =         5094462
19
 XDOT =      22317
492197                 XDOT =        6845
859910
 YDOT =     -10674
301544  feet/sec       YDOT =       -3177
215993  meter/sec
 ZDOT =      -5141
261960                 ZDOT =       -1533
905307

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13604429
97                 X    =         4146630
25
 Y    =        4619446
08  feet           Y    =         1408007
17  meter
 Z    =       16711413
72                 Z    =         5093638
90
 XDOT =      -1878
409009                 XDOT =        -572
539066
 YDOT =      23673
237598  feet/sec       YDOT =        7215
602820  meter/sec
 ZDOT =      -5015
964824                 ZDOT =       -1528
866078


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   07229
80698417  
00020000  00000-0  20000-3 0  9046
2 25544  51
6307 145
7524 0008467 256
2134 103
8088 15
76288387 20500


Satellite: ISS
Catalog Number: 25544
Epoch time:      07229
80698417   =   yrday
fracday
Element set:     904
Inclination:       51
6307  deg
RA of node:       145
7524  deg
Eccentricity:     
0008467     
Arg of perigee:   256
2134  deg
Mean anomaly:     103
8088  deg
Mean motion:   15
76288387  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2050
Checksum:              308


Coasting Arc #6 (Orbit 2065)
---------------------------------------

Vector Time (GMT): 2007/230/18:21:44
463
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5632379
61                 A    =         6720352
39  meter
 Y    =        1177360
84  meter          E    =           
0004451
 Z    =        3470108
17                 I    =           51
84004
 XDOT =       1561
528587                 Wp   =          114
29991
 YDOT =      -6003
982875  meter/sec      RA   =          139
90655  deg
 ZDOT =       4565
251975                 TA   =          286
75539
                                          MA   =          286
80423
                                          Ha   =            184
944  n
mi
                                          Hp   =            183
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18478935
71                 X    =        -5661983
52
 Y    =        3862732
40  feet           Y    =         1114210
81  meter
 Z    =       11384869
32                 Z    =         3442674
26
 XDOT =       5123
125285                 XDOT =        1606
372858
 YDOT =     -19698
106544  feet/sec       YDOT =       -5986
270319  meter/sec
 ZDOT =      14977
860812                 ZDOT =        4572
946687

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5474594
91                 X    =         1668656
53
 Y    =      -18132163
43  feet           Y    =        -5526683
41  meter
 Z    =       11280978
50                 Z    =         3438442
25
 XDOT =      13568
155943                 XDOT =        4135
573932
 YDOT =      13445
885226  feet/sec       YDOT =        4098
305817  meter/sec
 ZDOT =      15006
269335                 ZDOT =        4573
910893


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   07230
82131728  
00020000  00000-0  20000-3 0  9058
2 25544  51
6300 140
5232 0008522 259
5406 100
4798 15
76348913 20662


Satellite: ISS
Catalog Number: 25544
Epoch time:      07230
82131728   =   yrday
fracday
Element set:     905
Inclination:       51
6300  deg
RA of node:       140
5232  deg
Eccentricity:     
0008522     
Arg of perigee:   259
5406  deg
Mean anomaly:     100
4798  deg
Mean motion:   15
76348913  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2066
Checksum:              272


Coasting Arc #7 (Orbit 2080)
---------------------------------------

Vector Time (GMT): 2007/231/18:26:19
917
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3264427
62                 A    =         6723749
08  meter
 Y    =        5524610
98  meter          E    =           
0005713
 Z    =       -1995754
93                 I    =           51
87337
 XDOT =      -5176
892766                 Wp   =          316
01489
 YDOT =      -1029
981916  meter/sec      RA   =          134
70683  deg
 ZDOT =       5611
091089                 TA   =           21
80466
                                          MA   =           21
78035
                                          Ha   =            184
688  n
mi
                                          Hp   =            183
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10710064
38                 X    =        -3316267
02
 Y    =       18125364
10  feet           Y    =         5487816
52  meter
 Z    =       -6547752
39                 Z    =        -2011739
24
 XDOT =     -16984
556319                 XDOT =       -5192
248224
 YDOT =      -3379
205761  feet/sec       YDOT =       -1087
958883  meter/sec
 ZDOT =      18409
091500                 ZDOT =        5585
904450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11479879
93                 X    =        -3499067
40
 Y    =      -17625504
62  feet           Y    =        -5372253
81  meter
 Z    =       -6607670
36                 Z    =        -2014017
93
 XDOT =       9346
899095                 XDOT =        2848
934844
 YDOT =     -12960
116752  feet/sec       YDOT =       -3950
243586  meter/sec
 ZDOT =      18313
433903                 ZDOT =        5581
934654


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   07231
77224801  
00020000  00000-0  20000-3 0  9069
2 25544  51
6304 135
6213 0008358 262
7251  97
2964 15
76341772 20812


Satellite: ISS
Catalog Number: 25544
Epoch time:      07231
77224801   =   yrday
fracday
Element set:     906
Inclination:       51
6304  deg
RA of node:       135
6213  deg
Eccentricity:     
0008358     
Arg of perigee:   262
7251  deg
Mean anomaly:      97
2964  deg
Mean motion:   15
76341772  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2081
Checksum:              283


Coasting Arc #8 (Orbit 2096)
---------------------------------------

Vector Time (GMT): 2007/232/18:31:05
354
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2792967
19                 A    =         6713454
97  meter
 Y    =        3106194
81  meter          E    =           
0006857
 Z    =       -5261417
70                 I    =           51
85859
 XDOT =      -5219
738984                 Wp   =          103
76462
 YDOT =       5633
834482  meter/sec      RA   =          129
56657  deg
 ZDOT =        554
218707                 TA   =          171
49191
                                          MA   =          171
48028
                                          Ha   =            184
263  n
mi
                                          Hp   =            183
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9163278
18                 X    =         2783584
66
 Y    =       10190927
86  feet           Y    =         3137375
14  meter
 Z    =      -17261869
09                 Z    =        -5247872
12
 XDOT =     -17125
127900                 XDOT =       -5285
041706
 YDOT =      18483
708930  feet/sec       YDOT =        5575
099265  meter/sec
 ZDOT =       1818
302846                 ZDOT =         528
702900

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13095288
31                 X    =        -3991443
88
 Y    =        4256616
97  feet           Y    =         1297416
85  meter
 Z    =      -17210096
99                 Z    =        -5245637
56
 XDOT =      -9503
413815                 XDOT =       -2896
640531
 YDOT =     -22260
303016  feet/sec       YDOT =       -6784
940359  meter/sec
 ZDOT =       1722
235061                 ZDOT =         524
937247


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   07232
78656388  
00020000  00000-0  20000-3 0  9071
2 25544  51
6308 130
3937 0008240 266
2770  93
7452 15
76366221 20972


Satellite: ISS
Catalog Number: 25544
Epoch time:      07232
78656388   =   yrday
fracday
Element set:     907
Inclination:       51
6308  deg
RA of node:       130
3937  deg
Eccentricity:     
0008240     
Arg of perigee:   266
2770  deg
Mean anomaly:      93
7452  deg
Mean motion:   15
76366221  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2097
Checksum:              305


Coasting Arc #9 (Orbit 2112)
---------------------------------------

Vector Time (GMT): 2007/233/18:35:59
550
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5053304
22                 A    =         6721780
83  meter
 Y    =       -3343590
49  meter          E    =           
0004531
 Z    =       -2903861
33                 I    =           51
90459
 XDOT =        881
900925                 Wp   =          246
03691
 YDOT =       5736
254291  meter/sec      RA   =          124
44070  deg
 ZDOT =      -5065
839411                 TA   =          327
27181
                                          MA   =          327
29988
                                          Ha   =            183
456  n
mi
                                          Hp   =            183
171

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16579082
08                 X    =         5104423
56
 Y    =      -10969785
08  feet           Y    =        -3286795
59  meter
 Z    =       -9527104
11                 Z    =        -2879188
49
 XDOT =       2893
375739                 XDOT =         842
300594
 YDOT =      18819
731925  feet/sec       YDOT =        5745
895106  meter/sec
 ZDOT =     -16620
208040                 ZDOT =       -5061
650976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3927348
32                 X    =         1197055
77
 Y    =       19533169
83  feet           Y    =         5953710
17  meter
 Z    =       -9433931
91                 Z    =        -2875462
45
 XDOT =     -17141
008604                 XDOT =       -5224
579423
 YDOT =      -4579
643661  feet/sec       YDOT =       -1395
875388  meter/sec
 ZDOT =     -16603
598810                 ZDOT =       -5060
776917


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   07233
80086928  
00020000  00000-0  20000-3 0  9083
2 25544  51
6311 125
1649 0008280 271
0717  88
9499 15
76389311 21138


Satellite: ISS
Catalog Number: 25544
Epoch time:      07233
80086928   =   yrday
fracday
Element set:     908
Inclination:       51
6311  deg
RA of node:       125
1649  deg
Eccentricity:     
0008280     
Arg of perigee:   271
0717  deg
Mean anomaly:      88
9499  deg
Mean motion:   15
76389311  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2113
Checksum:              303


Coasting Arc #10 (Orbit 2128)
---------------------------------------

Vector Time (GMT): 2007/234/18:40:47
990
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1123882
62                 A    =         6722562
58  meter
 Y    =       -6110713
58  meter          E    =           
0005755
 Z    =        2558424
11                 I    =           51
92238
 XDOT =       5449
228159                 Wp   =          117
59191
 YDOT =      -1222
296531  meter/sec      RA   =          119
24226  deg
 ZDOT =      -5306
771296                 TA   =           33
48088
                                          MA   =           33
44452
                                          Ha   =            184
202  n
mi
                                          Hp   =            183
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3687278
93                 X    =         1179701
71
 Y    =      -20048272
89  feet           Y    =        -6097833
77  meter
 Z    =        8393779
87                 Z    =         2564019
04
 XDOT =      17878
045141                 XDOT =        5488
270246
 YDOT =      -4010
159222  feet/sec       YDOT =       -1161
141511  meter/sec
 ZDOT =     -17410
666982                 ZDOT =       -5280
204354

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17621562
47                 X    =         5371052
24
 Y    =       10230634
00  feet           Y    =         3118297
24  meter
 Z    =        8414242
47                 Z    =         2564661
11
 XDOT =      -1585
118164                 XDOT =        -483
144016
 YDOT =      16984
271740  feet/sec       YDOT =        5176
806026  meter/sec
 ZDOT =     -17310
032400                 ZDOT =       -5276
097876


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   07234
81516603  
00020000  00000-0  20000-3 0  9094
2 25544  51
6310 119
9363 0008334 273
9621  86
0591 15
76374557 21291


Satellite: ISS
Catalog Number: 25544
Epoch time:      07234
81516603   =   yrday
fracday
Element set:     909
Inclination:       51
6310  deg
RA of node:       119
9363  deg
Eccentricity:     
0008334     
Arg of perigee:   273
9621  deg
Mean anomaly:      86
0591  deg
Mean motion:   15
76374557  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2129
Checksum:              297


Coasting Arc #11 (Orbit 2143)
---------------------------------------

Vector Time (GMT): 2007/235/17:58:05
000
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4148083
50                 A    =         6713484
17  meter
 Y    =         771711
74  meter          E    =           
0007093
 Z    =       -5227817
54                 I    =           51
90565
 XDOT =      -2486
609936                 Wp   =           64
98140
 YDOT =       7231
371348  meter/sec      RA   =          114
29130  deg
 ZDOT =       -903
578824                 TA   =          196
43200
                                          MA   =          196
45500
                                          Ha   =            184
698  n
mi
                                          Hp   =            183
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13609197
83                 X    =         4164541
35
 Y    =        2531862
67  feet           Y    =          818190
36  meter
 Z    =      -17151632
34                 Z    =        -5207626
31
 XDOT =      -8158
169083                 XDOT =       -2562
898015
 YDOT =      23724
971613  feet/sec       YDOT =        7203
138192  meter/sec
 ZDOT =      -2964
497453                 ZDOT =        -915
843429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8965603
90                 X    =        -2732716
07
 Y    =       10670699
00  feet           Y    =         3252429
06  meter
 Z    =      -17074929
44                 Z    =        -5204438
49
 XDOT =     -15839
015608                 XDOT =       -4827
731957
 YDOT =     -18135
261723  feet/sec       YDOT =       -5527
627773  meter/sec
 ZDOT =      -3010
131477                 ZDOT =        -917
488074


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   07235
76605992  
00020000  00000-0  20000-3 0  9101
2 25544  51
6319 115
0362 0008190 278
5750  81
4487 15
76422171 21446


Satellite: ISS
Catalog Number: 25544
Epoch time:      07235
76605992   =   yrday
fracday
Element set:     910
Inclination:       51
6319  deg
RA of node:       115
0362  deg
Eccentricity:     
0008190     
Arg of perigee:   278
5750  deg
Mean anomaly:      81
4487  deg
Mean motion:   15
76422171  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2144
Checksum:              289


Coasting Arc #12 (Orbit 2159)
---------------------------------------

Vector Time (GMT): 2007/236/18:03:04
586
Vector Time (MET): N/A
Weight (LBS)     : 515214
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3409564
35                 A    =         6723860
84  meter
 Y    =       -5501345
35  meter          E    =           
0005344
 Z    =       -1809817
55                 I    =           51
95141
 XDOT =       3349
858894                 Wp   =          221
55106
 YDOT =       3953
191110  meter/sec      RA   =          109
14779  deg
 ZDOT =      -5700
105501                 TA   =          338
44588
                                          MA   =          338
46837
                                          Ha   =            184
869  n
mi
                                          Hp   =            183
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11186234
74                 X    =         3479619
45
 Y    =      -18049033
31  feet           Y    =        -5462825
87  meter
 Z    =       -5937721
61                 Z    =        -1793084
31
 XDOT =      10990
350702                 XDOT =        3333
094452
 YDOT =      12969
787106  feet/sec       YDOT =        3990
557754  meter/sec
 ZDOT =     -18701
133533                 ZDOT =       -5683
872577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10882380
17                 X    =         3316949
48
 Y    =       18254183
54  feet           Y    =         5563875
14  meter
 Z    =       -5874910
56                 Z    =        -1790672
74
 XDOT =     -15285
206433                 XDOT =       -4658
930921
 YDOT =       3107
634686  feet/sec       YDOT =         947
207052  meter/sec
 ZDOT =     -18639
048291                 ZDOT =       -5681
181919


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   07236
78033727  
00020000  00000-0  20000-3 0  9116
2 25544  51
6318 109
8068 0008311 282
8834  77
1402 15
76434376 21602


Satellite: ISS
Catalog Number: 25544
Epoch time:      07236
78033727   =   yrday
fracday
Element set:     911
Inclination:       51
6318  deg
RA of node:       109
8068  deg
Eccentricity:     
0008311     
Arg of perigee:   282
8834  deg
Mean anomaly:      77
1402  deg
Mean motion:   15
76434376  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2160
Checksum:              290

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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