Date: July 7th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6189 25 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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


There are no maneuvers



Coasting Arc #1 (Orbit 1381)
---------------------------------------

Vector Time (GMT): 2007/187/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5303806
22                 A    =         6714604
44  meter
 Y    =       -2777254
06  meter          E    =           
0010788
 Z    =       -3054977
92                 I    =           51
65949
 XDOT =       4708
318800                 Wp   =           57
01541
 YDOT =      -3585
418360  meter/sec      RA   =            3
83618  deg
 ZDOT =      -4921
462559                 TA   =          158
39956
                                          MA   =          158
35402
                                          Ha   =            185
405  n
mi
                                          Hp   =            174
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17400939
04                 X    =        -5257515
95
 Y    =       -9111725
91  feet           Y    =        -2836305
03  meter
 Z    =      -10022893
44                 Z    =        -3080631
49
 XDOT =      15447
240156                 XDOT =        4771
968934
 YDOT =     -11763
183596  feet/sec       YDOT =       -3532
410853  meter/sec
 ZDOT =     -16146
530707                 ZDOT =       -4898
435517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9618246
42                 X    =        -2931641
51
 Y    =       17068834
26  feet           Y    =         5202580
68  meter
 Z    =      -10120220
05                 Z    =        -3084643
07
 XDOT =     -10056
031277                 XDOT =       -3065
078333
 YDOT =     -15175
544344  feet/sec       YDOT =       -4625
505916  meter/sec
 ZDOT =     -16059
812989                 ZDOT =       -4895
030999


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   07187
48372591  
00020000  00000-0  20000-3 0  9001
2 25544  51
6325   4
1634 0008430  34
2057 325
9650 15
78726316 13828


Satellite: ISS
Catalog Number: 25544
Epoch time:      07187
48372591   =   yrday
fracday
Element set:     900
Inclination:       51
6325  deg
RA of node:         4
1634  deg
Eccentricity:     
0008430     
Arg of perigee:    34
2057  deg
Mean anomaly:     325
9650  deg
Mean motion:   15
78726316  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1382
Checksum:              281


Coasting Arc #2 (Orbit 1397)
---------------------------------------

Vector Time (GMT): 2007/188/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5284434
92                 A    =         6714285
18  meter
 Y    =        2645254
18  meter          E    =           
0018858
 Z    =        3178614
99                 I    =           51
62997
 XDOT =      -4759
879017                 Wp   =           71
75168
 YDOT =      -3694
163605  meter/sec      RA   =          358
61370  deg
 ZDOT =      -4809
968708                 TA   =           71
07720
                                          MA   =           70
87287
                                          Ha   =            185
383  n
mi
                                          Hp   =            174
342

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17337384
92                 X    =        -5329062
89
 Y    =        8678655
46  feet           Y    =         2585910
76  meter
 Z    =       10428526
87                 Z    =         3152835
17
 XDOT =     -15616
400973                 XDOT =       -4694
850672
 YDOT =     -12119
959333  feet/sec       YDOT =       -3747
027091  meter/sec
 ZDOT =     -15780
737230                 ZDOT =       -4832
934627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8465133
18                 X    =         2580172
59
 Y    =       17500398
03  feet           Y    =         5334121
32  meter
 Z    =       10331298
95                 Z    =         3148979
92
 XDOT =     -11032
826783                 XDOT =       -3362
805604
 YDOT =      14761
040731  feet/sec       YDOT =        4499
165215  meter/sec
 ZDOT =     -15867
992948                 ZDOT =       -4836
564250


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   07188
49650828  
00020000  00000-0  20000-3 0  9016
2 25544  51
6328 358
9239 0008313  36
6955 323
4779 15
78777521 13981


Satellite: ISS
Catalog Number: 25544
Epoch time:      07188
49650828   =   yrday
fracday
Element set:     901
Inclination:       51
6328  deg
RA of node:       358
9239  deg
Eccentricity:     
0008313     
Arg of perigee:    36
6955  deg
Mean anomaly:     323
4779  deg
Mean motion:   15
78777521  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1398
Checksum:              339


Coasting Arc #3 (Orbit 1413)
---------------------------------------

Vector Time (GMT): 2007/189/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2714044
14                 A    =         6707927
35  meter
 Y    =        3629881
84  meter          E    =           
0010950
 Z    =        4935174
13                 I    =           51
57868
 XDOT =      -7022
397064                 Wp   =           73
91471
 YDOT =       2447
749490  meter/sec      RA   =          353
48056  deg
 ZDOT =       2060
770022                 TA   =          356
15247
                                          MA   =          356
16088
                                          Ha   =            185
442  n
mi
                                          Hp   =            174
147

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8904344
28                 X    =         2649278
33
 Y    =       11909061
14  feet           Y    =         3659869
00  meter
 Z    =       16191516
18                 Z    =         4948202
16
 XDOT =     -23039
360446                 XDOT =       -7059
257100
 YDOT =       8030
674180  feet/sec       YDOT =        2369
014724  meter/sec
 ZDOT =       6761
056503                 ZDOT =        2026
565963

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11865081
11                 X    =         3616476
72
 Y    =       -8872563
53  feet           Y    =        -2704357
36  meter
 Z    =       16241174
44                 Z    =         4950309
97
 XDOT =       7498
173049                 XDOT =        2285
443145
 YDOT =      22171
478226  feet/sec       YDOT =        6757
866563  meter/sec
 ZDOT =       6631
944389                 ZDOT =        2021
416650


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   07189
50927307  
00020000  00000-0  20000-3 0  9029
2 25544  51
6319 353
6846 0008437  41
7763 318
4045 15
78753930 14145


Satellite: ISS
Catalog Number: 25544
Epoch time:      07189
50927307   =   yrday
fracday
Element set:     902
Inclination:       51
6319  deg
RA of node:       353
6846  deg
Eccentricity:     
0008437     
Arg of perigee:    41
7763  deg
Mean anomaly:     318
4045  deg
Mean motion:   15
78753930  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1414
Checksum:              306


Coasting Arc #4 (Orbit 1428)
---------------------------------------

Vector Time (GMT): 2007/190/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6524854
09                 A    =         6718501
21  meter
 Y    =       -1543905
05  meter          E    =           
0020224
 Z    =        -235678
47                 I    =           51
58627
 XDOT =       1299
698491                 Wp   =           44
11799
 YDOT =       4620
341385  meter/sec      RA   =          348
28477  deg
 ZDOT =       6037
974422                 TA   =          313
31247
                                          MA   =          313
48092
                                          Ha   =            185
446  n
mi
                                          Hp   =            173
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21407001
61                 X    =         6542778
21
 Y    =       -5065305
28  feet           Y    =        -1470840
21  meter
 Z    =        -773223
33                 Z    =         -203937
35
 XDOT =       4264
102662                 XDOT =        1218
605089
 YDOT =      15158
600346  feet/sec       YDOT =        4634
420930  meter/sec
 ZDOT =      19809
627368                 ZDOT =        6044
092164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5538680
77                 X    =        -1688189
90
 Y    =      -21293451
72  feet           Y    =        -6490244
08  meter
 Z    =        -653329
34                 Z    =         -199134
78
 XDOT =      13510
003981                 XDOT =        4117
849214
 YDOT =      -4084
198884  feet/sec       YDOT =       -1244
863820  meter/sec
 ZDOT =      19833
250126                 ZDOT =        6045
174638


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   07190
45871729  
00020000  00000-0  20000-3 0  9032
2 25544  51
6319 348
7727 0008337  45
9541 314
2310 15
78812133 14293


Satellite: ISS
Catalog Number: 25544
Epoch time:      07190
45871729   =   yrday
fracday
Element set:     903
Inclination:       51
6319  deg
RA of node:       348
7727  deg
Eccentricity:     
0008337     
Arg of perigee:    45
9541  deg
Mean anomaly:     314
2310  deg
Mean motion:   15
78812133  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1429
Checksum:              297


Coasting Arc #5 (Orbit 1444)
---------------------------------------

Vector Time (GMT): 2007/191/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         508060
67                 A    =         6707191
94  meter
 Y    =       -4372296
18  meter          E    =           
0020017
 Z    =       -5077175
17                 I    =           51
52045
 XDOT =       7469
680773                 Wp   =           82
57411
 YDOT =       -957
645675  meter/sec      RA   =          343
09450  deg
 ZDOT =       1580
010460                 TA   =          202
58826
                                          MA   =          202
67649
                                          Ha   =            185
455  n
mi
                                          Hp   =            173
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1666865
71                 X    =          581578
59
 Y    =      -14344803
74  feet           Y    =        -4366202
72  meter
 Z    =      -16657398
86                 Z    =        -5074529
28
 XDOT =      24506
826684                 XDOT =        7472
158731
 YDOT =      -3141
882135  feet/sec       YDOT =        -874
101961  meter/sec
 ZDOT =       5183
761353                 ZDOT =        1616
304059

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14402916
71                 X    =        -4390009
01
 Y    =       -1194154
55  feet           Y    =         -363978
31  meter
 Z    =      -16647845
43                 Z    =        -5074263
29
 XDOT =      -4189
999333                 XDOT =       -1277
111797
 YDOT =     -23284
491939  feet/sec       YDOT =       -7097
113143  meter/sec
 ZDOT =       5320
940939                 ZDOT =        1621
822798


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   07191
47143820  
00020000  00000-0  20000-3 0  9040
2 25544  51
6321 343
5334 0008399  50
3623 309
8282 15
78847044 14457


Satellite: ISS
Catalog Number: 25544
Epoch time:      07191
47143820   =   yrday
fracday
Element set:     904
Inclination:       51
6321  deg
RA of node:       343
5334  deg
Eccentricity:     
0008399     
Arg of perigee:    50
3623  deg
Mean anomaly:     309
8282  deg
Mean motion:   15
78847044  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1445
Checksum:              289


Coasting Arc #6 (Orbit 1460)
---------------------------------------

Vector Time (GMT): 2007/192/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6073408
73                 A    =         6714550
25  meter
 Y    =          -7567
05  meter          E    =           
0011476
 Z    =       -2877161
91                 I    =           51
51905
 XDOT =       2391
464585                 Wp   =           73
17969
 YDOT =      -5297
469695  meter/sec      RA   =          337
95029  deg
 ZDOT =      -5047
498941                 TA   =          139
97482
                                          MA   =          139
89019
                                          Ha   =            185
441  n
mi
                                          Hp   =            173
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19925881
66                 X    =        -6058896
04
 Y    =         -24826
29  feet           Y    =          -75401
56  meter
 Z    =       -9439507
57                 Z    =        -2906631
20
 XDOT =       7846
012419                 XDOT =        2475
043691
 YDOT =     -17380
149918  feet/sec       YDOT =       -5270
258598  meter/sec
 ZDOT =     -16560
035897                 ZDOT =       -5035
679361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1098907
30                 X    =          334946
94
 Y    =       19842299
32  feet           Y    =         6047932
83  meter
 Z    =       -9550981
11                 Z    =        -2911139
04
 XDOT =     -16354
250046                 XDOT =       -4984
775414
 YDOT =      -7023
361906  feet/sec       YDOT =       -2140
720709  meter/sec
 ZDOT =     -16515
874741                 ZDOT =       -5034
038621


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   07192
48413658  
00020000  00000-0  20000-3 0  9052
2 25544  51
6324 338
2938 0008531  53
3113 306
8835 15
78904712 14611


Satellite: ISS
Catalog Number: 25544
Epoch time:      07192
48413658   =   yrday
fracday
Element set:     905
Inclination:       51
6324  deg
RA of node:       338
2938  deg
Eccentricity:     
0008531     
Arg of perigee:    53
3113  deg
Mean anomaly:     306
8835  deg
Mean motion:   15
78904712  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1461
Checksum:              295


Coasting Arc #7 (Orbit 1476)
---------------------------------------

Vector Time (GMT): 2007/193/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3441088
87                 A    =         6713586
47  meter
 Y    =        4722990
19  meter          E    =           
0020274
 Z    =        3292704
55                 I    =           51
48860
 XDOT =      -6021
589388                 Wp   =           77
92639
 YDOT =      -1095
886842  meter/sec      RA   =          332
71677  deg
 ZDOT =      -4692
621870                 TA   =           63
21756
                                          MA   =           63
01029
                                          Ha   =            185
493  n
mi
                                          Hp   =            173
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11289661
63                 X    =        -3509641
50
 Y    =       15495374
65  feet           Y    =         4684125
98  meter
 Z    =       10802836
44                 Z    =         3275822
42
 XDOT =     -19755
870695                 XDOT =       -5986
091785
 YDOT =      -3595
429271  feet/sec       YDOT =       -1163
024118  meter/sec
 ZDOT =     -15395
741042                 ZDOT =       -4721
788515

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16289787
84                 X    =         4965127
33
 Y    =       10176991
19  feet           Y    =         3101946
92  meter
 Z    =       10739461
47                 Z    =         3273387
86
 XDOT =      -1393
688690                 XDOT =        -424
796313
 YDOT =      18692
944040  feet/sec       YDOT =        5697
609343  meter/sec
 ZDOT =     -15506
190396                 ZDOT =       -4726
286833


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   07193
49681426  
00020000  00000-0  20000-3 0  9065
2 25544  51
6319 333
0537 0008383  57
5577 302
6398 15
78899635 14770


Satellite: ISS
Catalog Number: 25544
Epoch time:      07193
49681426   =   yrday
fracday
Element set:     906
Inclination:       51
6319  deg
RA of node:       333
0537  deg
Eccentricity:     
0008383     
Arg of perigee:    57
5577  deg
Mean anomaly:     302
6398  deg
Mean motion:   15
78899635  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1477
Checksum:              337


Coasting Arc #8 (Orbit 1492)
---------------------------------------

Vector Time (GMT): 2007/194/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4119987
26                 A    =         6707469
03  meter
 Y    =        1999819
89  meter          E    =           
0012506
 Z    =        4889723
70                 I    =           51
44461
 XDOT =      -5156
062127                 Wp   =           86
62897
 YDOT =       5319
476007  meter/sec      RA   =          327
57423  deg
 ZDOT =       2164
807892                 TA   =          342
33042
                                          MA   =          342
37388
                                          Ha   =            185
256  n
mi
                                          Hp   =            173
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13517018
56                 X    =         4073565
75
 Y    =        6561088
89  feet           Y    =         2045631
30  meter
 Z    =       16042400
59                 Z    =         4909625
97
 XDOT =     -16916
214327                 XDOT =       -5225
678165
 YDOT =      17452
349103  feet/sec       YDOT =        5261
428315  meter/sec
 ZDOT =       7102
388096                 ZDOT =        2139
592167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5314041
63                 X    =         1619719
89
 Y    =      -13967477
60  feet           Y    =        -4257287
17  meter
 Z    =       16117903
90                 Z    =         4912737
11
 XDOT =      17902
096462                 XDOT =        5456
559002
 YDOT =      14912
530726  feet/sec       YDOT =        4545
339365  meter/sec
 ZDOT =       7007
545127                 ZDOT =        2135
899755


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   07194
50946886  
00020000  00000-0  20000-3 0  9073
2 25544  51
6327 327
8141 0008339  60
6996 299
5002 15
78971853 14939


Satellite: ISS
Catalog Number: 25544
Epoch time:      07194
50946886   =   yrday
fracday
Element set:     907
Inclination:       51
6327  deg
RA of node:       327
8141  deg
Eccentricity:     
0008339     
Arg of perigee:    60
6996  deg
Mean anomaly:     299
5002  deg
Mean motion:   15
78971853  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1493
Checksum:              334


Coasting Arc #9 (Orbit 1507)
---------------------------------------

Vector Time (GMT): 2007/195/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5171061
68                 A    =         6718003
25  meter
 Y    =       -4267364
29  meter          E    =           
0019897
 Z    =        -278768
09                 I    =           51
45783
 XDOT =       3244
525216                 Wp   =           51
80447
 YDOT =       3557
822222  meter/sec      RA   =          322
36740  deg
 ZDOT =       6023
667153                 TA   =          305
15087
                                          MA   =          305
33714
                                          Ha   =            185
426  n
mi
                                          Hp   =            173
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16965425
47                 X    =         5219749
83
 Y    =      -14000539
01  feet           Y    =        -4209266
29  meter
 Z    =        -914593
47                 Z    =         -253530
16
 XDOT =      10644
767768                 XDOT =        3175
238697
 YDOT =      11672
645086  feet/sec       YDOT =        3593
715735  meter/sec
 ZDOT =      19762
687510                 ZDOT =        6039
261151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15750958
50                 X    =        -4800892
15
 Y    =      -15359455
43  feet           Y    =        -4681562
01  meter
 Z    =        -819554
83                 Z    =         -249800
31
 XDOT =       9346
989516                 XDOT =        2848
962404
 YDOT =     -10583
980507  feet/sec       YDOT =       -3225
997259  meter/sec
 ZDOT =      19822
061740                 ZDOT =        6041
764418


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   07195
45881441  
00020000  00000-0  20000-3 0  9084
2 25544  51
6341 322
9027 0008466  64
7550 295
4492 15
78983762 15083


Satellite: ISS
Catalog Number: 25544
Epoch time:      07195
45881441   =   yrday
fracday
Element set:     908
Inclination:       51
6341  deg
RA of node:       322
9027  deg
Eccentricity:     
0008466     
Arg of perigee:    64
7550  deg
Mean anomaly:     295
4492  deg
Mean motion:   15
78983762  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1508
Checksum:              319


Coasting Arc #10 (Orbit 1523)
---------------------------------------

Vector Time (GMT): 2007/196/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1445128
54                 A    =         6706696
98  meter
 Y    =       -4174018
83  meter          E    =           
0021253
 Z    =       -5064842
27                 I    =           51
39797
 XDOT =       6305
417807                 Wp   =           89
05361
 YDOT =      -4109
969376  meter/sec      RA   =          317
16844  deg
 ZDOT =       1594
093104                 TA   =          196
28677
                                          MA   =          196
35517
                                          Ha   =            185
380  n
mi
                                          Hp   =            173
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4741235
36                 X    =        -1373743
13
 Y    =      -13694287
49  feet           Y    =        -4189779
05  meter
 Z    =      -16616936
57                 Z    =        -5071689
87
 XDOT =      20687
066297                 XDOT =        6343
163825
 YDOT =     -13484
151495  feet/sec       YDOT =       -4039
247878  meter/sec
 ZDOT =       5229
964251                 ZDOT =        1624
815093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13005476
88                 X    =        -3964069
35
 Y    =        6324068
04  feet           Y    =         1927575
94  meter
 Z    =      -16643291
08                 Z    =        -5072875
12
 XDOT =     -15500
451169                 XDOT =       -4724
537516
 YDOT =     -17860
648939  feet/sec       YDOT =       -5443
925797  meter/sec
 ZDOT =       5345
768880                 ZDOT =        1629
390355


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   07196
47142783  
00020000  00000-0  20000-3 0  9097
2 25544  51
6342 317
6642 0008476  68
1375 292
0692 15
79025282 15240


Satellite: ISS
Catalog Number: 25544
Epoch time:      07196
47142783   =   yrday
fracday
Element set:     909
Inclination:       51
6342  deg
RA of node:       317
6642  deg
Eccentricity:     
0008476     
Arg of perigee:    68
1375  deg
Mean anomaly:     292
0692  deg
Mean motion:   15
79025282  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1524
Checksum:              309


Coasting Arc #11 (Orbit 1539)
---------------------------------------

Vector Time (GMT): 2007/197/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5469872
10                 A    =         6714007
34  meter
 Y    =        2574267
17  meter          E    =           
0012276
 Z    =       -2932811
19                 I    =           51
40279
 XDOT =        -88
206188                 Wp   =           84
78846
 YDOT =      -5858
551598  meter/sec      RA   =          312
01426  deg
 ZDOT =      -4994
620520                 TA   =          129
16240
                                          MA   =          129
05326
                                          Ha   =            185
343  n
mi
                                          Hp   =            173
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17945774
61                 X    =        -5484004
68
 Y    =        8445758
43  feet           Y    =         2513021
39  meter
 Z    =       -9622083
96                 Z    =        -2959417
16
 XDOT =       -289
390382                 XDOT =           1
573944
 YDOT =     -19220
969809  feet/sec       YDOT =       -5859
035251  meter/sec
 ZDOT =     -16386
550264                 ZDOT =       -4994
831804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10902507
25                 X    =         3323084
21
 Y    =       16509842
99  feet           Y    =         5032200
14  meter
 Z    =       -9722478
16                 Z    =        -2963411
34
 XDOT =     -17793
869753                 XDOT =       -5423
571501
 YDOT =       2131
843957  feet/sec       YDOT =         649
786038  meter/sec
 ZDOT =     -16387
983764                 ZDOT =       -4995
057451


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
48401949  
00020000  00000-0  20000-3 0  9103
2 25544  51
6342 312
4234 0008451  71
4109 288
7974 15
79048497 15401


Satellite: ISS
Catalog Number: 25544
Epoch time:      07197
48401949   =   yrday
fracday
Element set:     910
Inclination:       51
6342  deg
RA of node:       312
4234  deg
Eccentricity:     
0008451     
Arg of perigee:    71
4109  deg
Mean anomaly:     288
7974  deg
Mean motion:   15
79048497  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1540
Checksum:              306


Coasting Arc #12 (Orbit 1555)
---------------------------------------

Vector Time (GMT): 2007/198/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1145987
18                 A    =         6713369
58  meter
 Y    =        5786966
20  meter          E    =           
0021181
 Z    =        3187757
50                 I    =           51
38243
 XDOT =      -5872
893493                 Wp   =           85
90516
 YDOT =       1484
185274  meter/sec      RA   =          306
77257  deg
 ZDOT =      -4776
964972                 TA   =           56
61798
                                          MA   =           56
41548
                                          Ha   =            185
368  n
mi
                                          Hp   =            173
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3759800
47                 X    =        -1226097
93
 Y    =       18986109
57  feet           Y    =         5773702
81  meter
 Z    =       10458521
97                 Z    =         3181996
53
 XDOT =     -19268
023270                 XDOT =       -5865
848264
 YDOT =       4869
374257  feet/sec       YDOT =        1418
551252  meter/sec
 ZDOT =     -15672
457257                 ZDOT =       -4805
477576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19351740
24                 X    =         5898410
43
 Y    =         748892
89  feet           Y    =          228262
55  meter
 Z    =       10437358
25                 Z    =         3181306
79
 XDOT =       7913
675899                 XDOT =        2412
088414
 YDOT =      16749
639956  feet/sec       YDOT =        5105
290259  meter/sec
 ZDOT =     -15780
183566                 ZDOT =       -4809
799951


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
49659008  
00020000  00000-0  20000-3 0  9117
2 25544  51
6344 307
1840 0008472  75
1932 285
0172 15
79067387 15561


Satellite: ISS
Catalog Number: 25544
Epoch time:      07198
49659008   =   yrday
fracday
Element set:     911
Inclination:       51
6344  deg
RA of node:       307
1840  deg
Eccentricity:     
0008472     
Arg of perigee:    75
1932  deg
Mean anomaly:     285
0172  deg
Mean motion:   15
79067387  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1556
Checksum:              310

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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