Date: August 23rd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4467 02 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 2078)
---------------------------------------

Vector Time (GMT): 2007/231/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2000175
83                 A    =         6714490
41  meter
 Y    =        3760718
47  meter          E    =           
0006347
 Z    =       -5195709
82                 I    =           51
83941
 XDOT =      -5998
328696                 Wp   =          117
45977
 YDOT =       4702
933916  meter/sec      RA   =          135
43193  deg
 ZDOT =       1093
029938                 TA   =          162
95166
                                          MA   =          162
93032
                                          Ha   =            185
116  n
mi
                                          Hp   =            184
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6562256
66                 X    =         1983214
04
 Y    =       12338315
20  feet           Y    =         3782990
88  meter
 Z    =      -17046292
05                 Z    =        -5186034
07
 XDOT =     -19679
556088                 XDOT =       -6055
781525
 YDOT =      15429
573216  feet/sec       YDOT =        4635
535956  meter/sec
 ZDOT =       3586
056227                 ZDOT =        1063
750689

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9512936
68                 X    =        -2899543
10
 Y    =      -10298902
40  feet           Y    =        -3139105
45  meter
 Z    =      -17009113
80                 Z    =        -5184377
89
 XDOT =      14500
359207                 XDOT =        4419
709486
 YDOT =     -19143
956493  feet/sec       YDOT =       -5835
077939  meter/sec
 ZDOT =       3475
610971                 ZDOT =        1059
366224


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
64608892  
00020000  00000-0  20000-3 0  9005
2 25544  51
6328 136
2877 0008731 264
4902  95
5266 15
76100517 20791


Satellite: ISS
Catalog Number: 25544
Epoch time:      07231
64608892   =   yrday
fracday
Element set:     900
Inclination:       51
6328  deg
RA of node:       136
2877  deg
Eccentricity:     
0008731     
Arg of perigee:   264
4902  deg
Mean anomaly:      95
5266  deg
Mean motion:   15
76100517  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2079
Checksum:              298


Coasting Arc #2 (Orbit 2094)
---------------------------------------

Vector Time (GMT): 2007/232/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5116518
69                 A    =         6725127
82  meter
 Y    =       -4033715
95  meter          E    =           
0007788
 Z    =       -1645932
10                 I    =           51
89443
 XDOT =       1892
089178                 Wp   =          211
11789
 YDOT =       4752
992480  meter/sec      RA   =          130
32159  deg
 ZDOT =      -5761
027605                 TA   =          347
01781
                                          MA   =          347
03785
                                          Ha   =            184
970  n
mi
                                          Hp   =            184
639

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16786478
63                 X    =         5169239
66
 Y    =      -13233976
20  feet           Y    =        -3976205
30  meter
 Z    =       -5400039
69                 Z    =        -1620948
21
 XDOT =       6207
641661                 XDOT =        1866
785881
 YDOT =      15593
807348  feet/sec       YDOT =        4774
009674  meter/sec
 ZDOT =     -18901
009203                 ZDOT =       -5751
897091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12709699
99                 X    =        -3873916
56
 Y    =       17216171
33  feet           Y    =         5247489
02  meter
 Z    =       -5305788
40                 Z    =        -1617204
30
 XDOT =      -8963
821754                 XDOT =       -2732
172871
 YDOT =     -12437
302084  feet/sec       YDOT =       -3790
889675  meter/sec
 ZDOT =     -18865
774398                 ZDOT =       -5750
288036


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
66057145  
00020000  00000-0  20000-3 0  9018
2 25544  51
6326 131
0616 0008835 267
8601  92
1551 15
76079443 20952


Satellite: ISS
Catalog Number: 25544
Epoch time:      07232
66057145   =   yrday
fracday
Element set:     901
Inclination:       51
6326  deg
RA of node:       131
0616  deg
Eccentricity:     
0008835     
Arg of perigee:   267
8601  deg
Mean anomaly:      92
1551  deg
Mean motion:   15
76079443  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2095
Checksum:              282


Coasting Arc #3 (Orbit 2110)
---------------------------------------

Vector Time (GMT): 2007/233/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1354590
94                 A    =         6716290
55  meter
 Y    =       -4552393
51  meter          E    =           
0004594
 Z    =        4752236
80                 I    =           51
88297
 XDOT =       5687
519934                 Wp   =          329
87799
 YDOT =      -4463
516462  meter/sec      RA   =          125
15064  deg
 ZDOT =      -2651
836584                 TA   =          146
09353
                                          MA   =          146
06415
                                          Ha   =            184
713  n
mi
                                          Hp   =            184
511

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4444196
00                 X    =        -1326670
17
 Y    =      -14935674
25  feet           Y    =        -4567385
49  meter
 Z    =       15591328
09                 Z    =         4745723
76
 XDOT =      18659
842304                 XDOT =        5749
891039
 YDOT =     -14644
082881  feet/sec       YDOT =       -4399
566512  meter/sec
 ZDOT =      -8700
251261                 ZDOT =       -2624
055455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8552415
28                 X    =         2606776
18
 Y    =       13056379
86  feet           Y    =         3979584
58  meter
 Z    =       15566049
37                 Z    =         4744531
85
 XDOT =     -12878
070725                 XDOT =       -3925
235957
 YDOT =      18694
178495  feet/sec       YDOT =        5697
985605  meter/sec
 ZDOT =      -8595
431015                 ZDOT =       -2619
887373


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
67503923  
00020000  00000-0  20000-3 0  9021
2 25544  51
6326 125
8336 0008890 272
2550  87
7596 15
76138287 21116


Satellite: ISS
Catalog Number: 25544
Epoch time:      07233
67503923   =   yrday
fracday
Element set:     902
Inclination:       51
6326  deg
RA of node:       125
8336  deg
Eccentricity:     
0008890     
Arg of perigee:   272
2550  deg
Mean anomaly:      87
7596  deg
Mean motion:   15
76138287  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2111
Checksum:              299


Coasting Arc #4 (Orbit 2126)
---------------------------------------

Vector Time (GMT): 2007/234/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4793073
56                 A    =         6722313
02  meter
 Y    =        3674005
77  meter          E    =           
0005114
 Z    =        2945443
00                 I    =           51
91797
 XDOT =      -1265
477268                 Wp   =           58
54472
 YDOT =      -5691
155839  meter/sec      RA   =          120
06048  deg
 ZDOT =       5035
831986                 TA   =          335
29792
                                          MA   =          335
32241
                                          Ha   =            185
093  n
mi
                                          Hp   =            184
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15725306
95                 X    =        -4848108
96
 Y    =       12053824
71  feet           Y    =         3620098
99  meter
 Z    =        9663526
90                 Z    =         2922024
95
 XDOT =      -4151
828306                 XDOT =       -1226
206895
 YDOT =     -18671
771124  feet/sec       YDOT =       -5705
087907  meter/sec
 ZDOT =      16521
758484                 ZDOT =        5029
779311

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11471489
26                 X    =         3496509
93
 Y    =      -16207567
11  feet           Y    =        -4940066
45  meter
 Z    =        9575146
14                 Z    =         2918504
54
 XDOT =       8432
881951                 XDOT =        2570
342419
 YDOT =      15722
798935  feet/sec       YDOT =        4792
309115  meter/sec
 ZDOT =      16498
085530                 ZDOT =        5028
616469


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
68949462  
00020000  00000-0  20000-3 0  9036
2 25544  51
6316 120
6055 0008951 275
7131  84
3012 15
76165750 21275


Satellite: ISS
Catalog Number: 25544
Epoch time:      07234
68949462   =   yrday
fracday
Element set:     903
Inclination:       51
6316  deg
RA of node:       120
6055  deg
Eccentricity:     
0008951     
Arg of perigee:   275
7131  deg
Mean anomaly:      84
3012  deg
Mean motion:   15
76165750  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2127
Checksum:              283


Coasting Arc #5 (Orbit 2141)
---------------------------------------

Vector Time (GMT): 2007/235/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         918201
20                 A    =         6719256
59  meter
 Y    =        5362275
29  meter          E    =           
0002237
 Z    =       -3942168
26                 I    =           51
92050
 XDOT =      -5288
336060                 Wp   =          253
53810
 YDOT =       3878
164920  meter/sec      RA   =          114
87721  deg
 ZDOT =       4040
970256                 TA   =           58
26621
                                          MA   =           58
24441
                                          Ha   =            185
256  n
mi
                                          Hp   =            184
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3012471
13                 X    =          877321
36
 Y    =       17592766
70  feet           Y    =         5372314
85  meter
 Z    =      -12933622
90                 Z    =        -3937806
58
 XDOT =     -17350
183923                 XDOT =       -5350
939358
 YDOT =      12723
638188  feet/sec       YDOT =        3818
677434  meter/sec
 ZDOT =      13257
776429                 ZDOT =        4015
127978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8458309
74                 X    =        -2578092
81
 Y    =      -15731574
28  feet           Y    =        -4794983
84  meter
 Z    =      -12916407
81                 Z    =        -3936921
10
 XDOT =      11394
980355                 XDOT =        3473
190012
 YDOT =     -16938
605537  feet/sec       YDOT =       -5162
886968  meter/sec
 ZDOT =      13160
212289                 ZDOT =        4011
232706


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
64053589  
00020000  00000-0  20000-3 0  9040
2 25544  51
6309 115
7040 0008808 279
2320  80
7848 15
76166569 21429


Satellite: ISS
Catalog Number: 25544
Epoch time:      07235
64053589   =   yrday
fracday
Element set:     904
Inclination:       51
6309  deg
RA of node:       115
7040  deg
Eccentricity:     
0008808     
Arg of perigee:   279
2320  deg
Mean anomaly:      80
7848  deg
Mean motion:   15
76166569  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2142
Checksum:              301


Coasting Arc #6 (Orbit 2157)
---------------------------------------

Vector Time (GMT): 2007/236/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4447022
09                 A    =         6718906
83  meter
 Y    =       -3008492
06  meter          E    =           
0004662
 Z    =       -4041156
16                 I    =           51
93018
 XDOT =        888
857612                 Wp   =          339
63899
 YDOT =       6574
424578  meter/sec      RA   =          109
79725  deg
 ZDOT =      -3910
671966                 TA   =          250
16771
                                          MA   =          250
21797
                                          Ha   =            185
418  n
mi
                                          Hp   =            184
005

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14589967
48                 X    =         4499963
92
 Y    =       -9870380
77  feet           Y    =        -2958466
67  meter
 Z    =      -13258386
34                 Z    =        -4019424
42
 XDOT =       2916
199513                 XDOT =         834
272440
 YDOT =      21569
634442  feet/sec       YDOT =        6584
059343  meter/sec
 ZDOT =     -12830
288602                 ZDOT =       -3906
486104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10576612
93                 X    =        -3223751
62
 Y    =       14163217
76  feet           Y    =         4316948
77  meter
 Z    =      -13176300
60                 Z    =        -4016136
42
 XDOT =      -8918
191315                 XDOT =       -2718
264713
 YDOT =     -18597
772385  feet/sec       YDOT =       -5668
601023  meter/sec
 ZDOT =     -12813
590249                 ZDOT =       -3905
582308


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
65496630  
00020000  00000-0  20000-3 0  9051
2 25544  51
6307 110
4773 0008742 283
7322  76
2869 15
76195505 21583


Satellite: ISS
Catalog Number: 25544
Epoch time:      07236
65496630   =   yrday
fracday
Element set:     905
Inclination:       51
6307  deg
RA of node:       110
4773  deg
Eccentricity:     
0008742     
Arg of perigee:   283
7322  deg
Mean anomaly:      76
2869  deg
Mean motion:   15
76195505  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2158
Checksum:              306


Coasting Arc #7 (Orbit 2173)
---------------------------------------

Vector Time (GMT): 2007/237/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -688233
78                 A    =         6722414
94  meter
 Y    =       -6067660
94  meter          E    =           
0004761
 Z    =        2807253
28                 I    =           51
95135
 XDOT =       4924
519007                 Wp   =           85
66915
 YDOT =      -2940
411000  meter/sec      RA   =          104
61635  deg
 ZDOT =      -5140
392098                 TA   =           62
29793
                                          MA   =           62
24964
                                          Ha   =            185
559  n
mi
                                          Hp   =            183
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2257984
85                 X    =         -633970
04
 Y    =      -19907024
09  feet           Y    =        -6075053
89  meter
 Z    =        9210148
57                 Z    =         2804041
42
 XDOT =      16156
558423                 XDOT =        4982
003788
 YDOT =      -9647
017716  feet/sec       YDOT =       -2885
020592  meter/sec
 ZDOT =     -16864
803472                 ZDOT =       -5116
329706

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9069701
16                 X    =         2764444
91
 Y    =       17870837
48  feet           Y    =         5447031
26  meter
 Z    =        9197207
68                 Z    =         2803308
90
 XDOT =     -10594
083493                 XDOT =       -3229
076649
 YDOT =      14022
433423  feet/sec       YDOT =        4274
037707  meter/sec
 ZDOT =     -16773
857726                 ZDOT =       -5112
671835


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   07237
66938201  
00020000  00000-0  20000-3 0  9069
2 25544  51
6311 105
2493 0009000 287
2931  72
7248 15
76230319 21745


Satellite: ISS
Catalog Number: 25544
Epoch time:      07237
66938201   =   yrday
fracday
Element set:     906
Inclination:       51
6311  deg
RA of node:       105
2493  deg
Eccentricity:     
0009000     
Arg of perigee:   287
2931  deg
Mean anomaly:      72
7248  deg
Mean motion:   15
76230319  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2174
Checksum:              276


Coasting Arc #8 (Orbit 2189)
---------------------------------------

Vector Time (GMT): 2007/238/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4185094
18                 A    =         6715799
77  meter
 Y    =        2053437
81  meter          E    =           
0002188
 Z    =        4836284
76                 I    =           51
93396
 XDOT =       -729
363711                 Wp   =          258
14794
 YDOT =      -7264
583431  meter/sec      RA   =           99
52695  deg
 ZDOT =       2453
799072                 TA   =          167
98596
                                          MA   =          167
98074
                                          Ha   =            185
858  n
mi
                                          Hp   =            183
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13730623
96                 X    =        -4231238
33
 Y    =        6737000
69  feet           Y    =         2006379
62  meter
 Z    =       15867075
99                 Z    =         4815841
93
 XDOT =      -2392
925562                 XDOT =        -659
995735
 YDOT =     -23833
935141  feet/sec       YDOT =       -7272
351783  meter/sec
 ZDOT =       8050
521890                 ZDOT =        2450
424231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10433065
23                 X    =         3179998
28
 Y    =      -11292308
98  feet           Y    =        -3441895
78  meter
 Z    =       15789750
50                 Z    =         4812715
95
 XDOT =      10096
911253                 XDOT =        3077
538550
 YDOT =      20564
050574  feet/sec       YDOT =        6267
922615  meter/sec
 ZDOT =       8036
811311                 ZDOT =        2449
620088


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   07238
68378781  
00020000  00000-0  20000-3 0  9074
2 25544  51
6303 100
0209 0008800 291
2220  68
8004 15
76209256 21907


Satellite: ISS
Catalog Number: 25544
Epoch time:      07238
68378781   =   yrday
fracday
Element set:     907
Inclination:       51
6303  deg
RA of node:       100
0209  deg
Eccentricity:     
0008800     
Arg of perigee:   291
2220  deg
Mean anomaly:      68
8004  deg
Mean motion:   15
76209256  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2190
Checksum:              273


Coasting Arc #9 (Orbit 2204)
---------------------------------------

Vector Time (GMT): 2007/239/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         621392
15                 A    =         6724914
36  meter
 Y    =        6534758
31  meter          E    =           
0010727
 Z    =       -1427697
61                 I    =           51
96884
 XDOT =      -4717
119886                 Wp   =          345
31346
 YDOT =       1725
536836  meter/sec      RA   =           94
36270  deg
 ZDOT =       5845
580252                 TA   =          359
03321
                                          MA   =          359
03529
                                          Ha   =            185
875  n
mi
                                          Hp   =            183
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2038688
17                 X    =          555208
70
 Y    =       21439495
77  feet           Y    =         6541337
00  meter
 Z    =       -4684047
28                 Z    =        -1424839
77
 XDOT =     -15476
115110                 XDOT =       -4764
460750
 YDOT =       5661
210093  feet/sec       YDOT =        1672
522700  meter/sec
 ZDOT =      19178
412901                 ZDOT =        5822
549910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10033125
44                 X    =        -3058096
63
 Y    =      -19059216
23  feet           Y    =        -5809249
11  meter
 Z    =       -4672386
77                 Z    =        -1424143
49
 XDOT =      10887
596181                 XDOT =        3318
539316
 YDOT =     -10411
137551  feet/sec       YDOT =       -3173
314725  meter/sec
 ZDOT =      19091
223349                 ZDOT =        5819
004877


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   07239
63477882  
00020000  00000-0  20000-3 0  9083
2 25544  51
6305  95
1194 0008662 294
0797  65
9460 15
76243481 22051


Satellite: ISS
Catalog Number: 25544
Epoch time:      07239
63477882   =   yrday
fracday
Element set:     908
Inclination:       51
6305  deg
RA of node:        95
1194  deg
Eccentricity:     
0008662     
Arg of perigee:   294
0797  deg
Mean anomaly:      65
9460  deg
Mean motion:   15
76243481  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2205
Checksum:              316


Coasting Arc #10 (Orbit 2220)
---------------------------------------

Vector Time (GMT): 2007/240/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4097133
06                 A    =         6713809
59  meter
 Y    =        -914708
44  meter          E    =           
0009095
 Z    =       -5246198
66                 I    =           51
93265
 XDOT =        705
845217                 Wp   =           51
99937
 YDOT =       7627
581422  meter/sec      RA   =           89
25237  deg
 ZDOT =       -774
099054                 TA   =          210
63688
                                          MA   =          210
69001
                                          Ha   =            186
036  n
mi
                                          Hp   =            183
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13442037
59                 X    =         4132541
65
 Y    =       -3001011
95  feet           Y    =         -868694
20  meter
 Z    =      -17211937
86                 Z    =        -5226209
06
 XDOT =       2315
765146                 XDOT =         624
260382
 YDOT =      25024
873432  feet/sec       YDOT =        7635
018390  meter/sec
 ZDOT =      -2539
695059                 ZDOT =        -770
868557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11254858
07                 X    =        -3430480
74
 Y    =        8100898
36  feet           Y    =         2469153
82  meter
 Z    =      -17136185
92                 Z    =        -5223109
47
 XDOT =     -11427
411832                 XDOT =       -3483
075126
 YDOT =     -21252
758714  feet/sec       YDOT =       -6477
840856  meter/sec
 ZDOT =      -2526
482354                 ZDOT =        -770
071821


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   07240
64915679  
00020000  00000-0  20000-3 0  9098
2 25544  51
6306  89
8921 0008538 298
4691  61
5613 15
76279509 22213


Satellite: ISS
Catalog Number: 25544
Epoch time:      07240
64915679   =   yrday
fracday
Element set:     909
Inclination:       51
6306  deg
RA of node:        89
8921  deg
Eccentricity:     
0008538     
Arg of perigee:   298
4691  deg
Mean anomaly:      61
5613  deg
Mean motion:   15
76279509  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2221
Checksum:              323


Coasting Arc #11 (Orbit 2236)
---------------------------------------

Vector Time (GMT): 2007/241/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -610238
12                 A    =         6725561
92  meter
 Y    =       -6694471
65  meter          E    =           
0003976
 Z    =        -101602
98                 I    =           51
97048
 XDOT =       4733
782841                 Wp   =          164
80664
 YDOT =       -340
319665  meter/sec      RA   =           84
11424  deg
 ZDOT =      -6065
249775                 TA   =           16
29271
                                          MA   =           16
27993
                                          Ha   =            186
177  n
mi
                                          Hp   =            182
611

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2002093
58                 X    =         -534840
63
 Y    =      -21963489
68  feet           Y    =        -6700874
12  meter
 Z    =        -333343
11                 Z    =         -104383
99
 XDOT =      15530
783599                 XDOT =        4766
700123
 YDOT =      -1116
534335  feet/sec       YDOT =        -287
200107  meter/sec
 ZDOT =     -19899
113436                 ZDOT =       -6042
173312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10838769
91                 X    =         3303657
07
 Y    =       19207201
81  feet           Y    =         5854355
11  meter
 Z    =        -344732
28                 Z    =         -105074
40
 XDOT =     -12405
150585                 XDOT =       -3781
089898
 YDOT =       6647
976403  feet/sec       YDOT =        2026
303208  meter/sec
 ZDOT =     -19811
573964                 ZDOT =       -6038
567744


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   07241
66351945  
00020000  00000-0  20000-3 0  9103
2 25544  51
6301  84
6628 0008808 303
0837  56
9481 15
76325427 22379


Satellite: ISS
Catalog Number: 25544
Epoch time:      07241
66351945   =   yrday
fracday
Element set:     910
Inclination:       51
6301  deg
RA of node:        84
6628  deg
Eccentricity:     
0008808     
Arg of perigee:   303
0837  deg
Mean anomaly:      56
9481  deg
Mean motion:   15
76325427  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2237
Checksum:              294


Coasting Arc #12 (Orbit 2252)
---------------------------------------

Vector Time (GMT): 2007/242/15:10:06
062
Vector Time (MET): N/A
Weight (LBS)     : 511203
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4223454
60                 A    =         6714004
92  meter
 Y    =        -321180
62  meter          E    =           
0008013
 Z    =        5213602
82                 I    =           51
92690
 XDOT =       -676
048346                 Wp   =          331
55872
 YDOT =      -7604
804081  meter/sec      RA   =           78
97250  deg
 ZDOT =      -1009
881816                 TA   =          128
06615
                                          MA   =          127
99383
                                          Ha   =            186
443  n
mi
                                          Hp   =            182
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13856478
33                 X    =        -4244875
87
 Y    =       -1053742
20  feet           Y    =         -368529
16  meter
 Z    =       17104996
14                 Z    =         5193033
34
 XDOT =      -2218
006383                 XDOT =        -586
054242
 YDOT =     -24950
144624  feet/sec       YDOT =       -7611
860909  meter/sec
 ZDOT =      -3313
260551                 ZDOT =       -1012
947031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13071553
11                 X    =         3984209
39
 Y    =       -4991270
43  feet           Y    =        -1521339
23  meter
 Z    =       17026889
79                 Z    =         5189796
01
 XDOT =      12256
293484                 XDOT =        3735
718254
 YDOT =      20681
842431  feet/sec       YDOT =        6303
825573  meter/sec
 ZDOT =      -3325
836643                 ZDOT =       -1013
715009


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   07242
67787257  
00020000  00000-0  20000-3 0  9115
2 25544  51
6304  79
4342 0008532 306
6830  53
3549 15
76263004 22539


Satellite: ISS
Catalog Number: 25544
Epoch time:      07242
67787257   =   yrday
fracday
Element set:     911
Inclination:       51
6304  deg
RA of node:        79
4342  deg
Eccentricity:     
0008532     
Arg of perigee:   306
6830  deg
Mean anomaly:      53
3549  deg
Mean motion:   15
76263004  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2253
Checksum:              286

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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