Date: November 1st 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 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 3210)
---------------------------------------

Vector Time (GMT): 2007/303/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         331542
36                 A    =         6719027
03  meter
 Y    =        5221165
34  meter          E    =           
0010152
 Z    =       -4226796
82                 I    =           51
89313
 XDOT =      -5905
842835                 Wp   =          119
73123
 YDOT =       3323
733320  meter/sec      RA   =          125
68648  deg
 ZDOT =       3643
982837                 TA   =          187
26507
                                          MA   =          187
27979
                                          Ha   =            187
697  n
mi
                                          Hp   =            180
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1087737
39                 X    =          293667
26
 Y    =       17129807
54  feet           Y    =         5224661
36  meter
 Z    =      -13867443
62                 Z    =        -4225277
78
 XDOT =     -19376
124786                 XDOT =       -5960
272530
 YDOT =      10904
636877  feet/sec       YDOT =        3257
386254  meter/sec
 ZDOT =      11955
324268                 ZDOT =        3615
159727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2885850
38                 X    =         -879607
20
 Y    =      -16925216
19  feet           Y    =        -5158805
89  meter
 Z    =      -13861038
78                 Z    =        -4224844
62
 XDOT =      17011
253958                 XDOT =        5185
030207
 YDOT =     -12597
720540  feet/sec       YDOT =       -3839
785221  meter/sec
 ZDOT =      11846
067394                 ZDOT =        3610
681342


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   07303
42101857  
00020000  00000-0  20000-3 0  9000
2 25544  51
6369 126
5523 0002350 153
6818 206
4466 15
75893463 32114


Satellite: ISS
Catalog Number: 25544
Epoch time:      07303
42101857   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       126
5523  deg
Eccentricity:     
0002350     
Arg of perigee:   153
6818  deg
Mean anomaly:     206
4466  deg
Mean motion:   15
75893463  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3211
Checksum:              276


Coasting Arc #2 (Orbit 3226)
---------------------------------------

Vector Time (GMT): 2007/304/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4942457
30                 A    =         6720905
80  meter
 Y    =       -2679804
36  meter          E    =           
0006510
 Z    =       -3687098
30                 I    =           51
91476
 XDOT =        203
906131                 Wp   =           99
59198
 YDOT =       6349
071160  meter/sec      RA   =          120
60628  deg
 ZDOT =      -4348
738392                 TA   =          124
57397
                                          MA   =          124
51253
                                          Ha   =            187
644  n
mi
                                          Hp   =            180
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16215411
07                 X    =         4989967
45
 Y    =       -8792009
05  feet           Y    =        -2624269
15  meter
 Z    =      -12096779
20                 Z    =        -3662972
25
 XDOT =        668
983368                 XDOT =         154
020393
 YDOT =      20830
285957  feet/sec       YDOT =        6351
072675  meter/sec
 ZDOT =     -14267
514409                 ZDOT =       -4347
868615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15133593
29                 X    =        -4612719
23
 Y    =       10649794
06  feet           Y    =         3246057
23  meter
 Z    =      -12005302
46                 Z    =        -3659216
19
 XDOT =      -2422
507973                 XDOT =        -738
380430
 YDOT =     -19493
288216  feet/sec       YDOT =       -5941
554248  meter/sec
 ZDOT =     -14263
447709                 ZDOT =       -4347
498862


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   07304
43562405  
00020000  00000-0  20000-3 0  9013
2 25544  51
6363 121
3270 0002287 158
5910 201
5350 15
75912743 32274


Satellite: ISS
Catalog Number: 25544
Epoch time:      07304
43562405   =   yrday
fracday
Element set:     901
Inclination:       51
6363  deg
RA of node:       121
3270  deg
Eccentricity:     
0002287     
Arg of perigee:   158
5910  deg
Mean anomaly:     201
5350  deg
Mean motion:   15
75912743  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3227
Checksum:              259


Coasting Arc #3 (Orbit 3242)
---------------------------------------

Vector Time (GMT): 2007/305/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -84991
33                 A    =         6721738
12  meter
 Y    =       -5845992
12  meter          E    =           
0013498
 Z    =        3302633
31                 I    =           51
93286
 XDOT =       5419
231716                 Wp   =           99
94509
 YDOT =      -2761
914544  meter/sec      RA   =          115
42416  deg
 ZDOT =      -4735
430537                 TA   =           41
39330
                                          MA   =           41
29111
                                          Ha   =            187
389  n
mi
                                          Hp   =            180
464

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -278842
96                 X    =          -35658
03
 Y    =      -19179764
18  feet           Y    =        -5846666
83  meter
 Z    =       10835411
11                 Z    =         3302340
03
 XDOT =      17779
631614                 XDOT =        5472
717225
 YDOT =      -9061
399424  feet/sec       YDOT =       -2701
014399  meter/sec
 ZDOT =     -15536
189425                 ZDOT =       -4708
973785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2924517
62                 X    =          891392
97
 Y    =       18958574
66  feet           Y    =         5778573
56  meter
 Z    =       10833599
79                 Z    =         3302081
22
 XDOT =     -15098
428952                 XDOT =       -4602
001145
 YDOT =      11175
848368  feet/sec       YDOT =        3406
398582  meter/sec
 ZDOT =     -15435
843829                 ZDOT =       -4704
845199


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   07305
45020468  
00020000  00000-0  20000-3 0  9025
2 25544  51
6371 116
1008 0002074 163
8449 196
2782 15
75999895 32434


Satellite: ISS
Catalog Number: 25544
Epoch time:      07305
45020468   =   yrday
fracday
Element set:     902
Inclination:       51
6371  deg
RA of node:       116
1008  deg
Eccentricity:     
0002074     
Arg of perigee:   163
8449  deg
Mean anomaly:     196
2782  deg
Mean motion:   15
75999895  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3243
Checksum:              301


Coasting Arc #4 (Orbit 3258)
---------------------------------------

Vector Time (GMT): 2007/306/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4529810
12                 A    =         6717833
72  meter
 Y    =        2064832
26  meter          E    =           
0010360
 Z    =        4506106
45                 I    =           51
92920
 XDOT =        -41
184746                 Wp   =          122
11950
 YDOT =      -7025
421683  meter/sec      RA   =          110
34185  deg
 ZDOT =       3167
200990                 TA   =          296
35775
                                          MA   =          296
46408
                                          Ha   =            187
518  n
mi
                                          Hp   =            180
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14861581
76                 X    =        -4574452
82
 Y    =        6774384
05  feet           Y    =         2013927
67  meter
 Z    =       14783813
81                 Z    =         4483991
98
 XDOT =       -135
120559                 XDOT =          21
991776
 YDOT =     -23049
283736  feet/sec       YDOT =       -7025
529050  meter/sec
 ZDOT =      10391
079365                 ZDOT =        3167
154251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13741759
14                 X    =         4188488
19
 Y    =       -8966436
11  feet           Y    =        -2732969
73  meter
 Z    =       14699902
09                 Z    =         4480530
16
 XDOT =       3039
788739                 XDOT =         926
527608
 YDOT =      21750
206340  feet/sec       YDOT =        6629
462893  meter/sec
 ZDOT =      10390
067748                 ZDOT =        3166
892650


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   07306
46476538  
00020000  00000-0  20000-3 0  9031
2 25544  51
6358 110
8740 0002113 165
0694 195
0533 15
75965333 32591


Satellite: ISS
Catalog Number: 25544
Epoch time:      07306
46476538   =   yrday
fracday
Element set:     903
Inclination:       51
6358  deg
RA of node:       110
8740  deg
Eccentricity:     
0002113     
Arg of perigee:   165
0694  deg
Mean anomaly:     195
0533  deg
Mean motion:   15
75965333  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3259
Checksum:              294


Coasting Arc #5 (Orbit 3273)
---------------------------------------

Vector Time (GMT): 2007/307/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          25030
98                 A    =         6724371
02  meter
 Y    =        6367551
96  meter          E    =           
0005176
 Z    =       -2160395
91                 I    =           51
96001
 XDOT =      -5002
717141                 Wp   =           61
65261
 YDOT =       1894
308330  meter/sec      RA   =          105
16880  deg
 ZDOT =       5537
692161                 TA   =          274
27148
                                          MA   =          274
33063
                                          Ha   =            187
275  n
mi
                                          Hp   =            180
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          82122
64                 X    =          -35678
86
 Y    =       20890918
49  feet           Y    =         6367492
42  meter
 Z    =       -7087913
09                 Z    =        -2160421
78
 XDOT =     -16413
113979                 XDOT =       -5050
429223
 YDOT =       6214
922344  feet/sec       YDOT =        1838
098346  meter/sec
 ZDOT =      18168
281367                 ZDOT =        5513
272753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3649281
26                 X    =        -1112300
93
 Y    =      -20570105
70  feet           Y    =        -6269768
22  meter
 Z    =       -7087258
24                 Z    =        -2160196
31
 XDOT =      13728
007291                 XDOT =        4184
296622
 YDOT =      -8649
248652  feet/sec       YDOT =       -2636
290989  meter/sec
 ZDOT =      18075
572575                 ZDOT =        5509
434521


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   07307
41589097  
00020000  00000-0  20000-3 0  9043
2 25544  51
6350 105
9735 0002231 170
3081 189
8127 15
76028299 32741


Satellite: ISS
Catalog Number: 25544
Epoch time:      07307
41589097   =   yrday
fracday
Element set:     904
Inclination:       51
6350  deg
RA of node:       105
9735  deg
Eccentricity:     
0002231     
Arg of perigee:   170
3081  deg
Mean anomaly:     189
8127  deg
Mean motion:   15
76028299  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3274
Checksum:              296


Coasting Arc #6 (Orbit 3289)
---------------------------------------

Vector Time (GMT): 2007/308/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4247830
83                 A    =         6715184
64  meter
 Y    =       -1171736
82  meter          E    =           
0013575
 Z    =       -5078984
42                 I    =           51
93497
 XDOT =         27
887178                 Wp   =           86
52054
 YDOT =       7501
660093  meter/sec      RA   =          100
07254  deg
 ZDOT =      -1710
423946                 TA   =          167
09618
                                          MA   =          167
06141
                                          Ha   =            187
220  n
mi
                                          Hp   =            180
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13936452
85                 X    =         4285290
85
 Y    =       -3844280
92  feet           Y    =        -1124025
79  meter
 Z    =      -16663334
72                 Z    =        -5058257
12
 XDOT =         91
493366                 XDOT =         -47
690524
 YDOT =      24611
745711  feet/sec       YDOT =        7501
549345  meter/sec
 ZDOT =      -5611
627119                 ZDOT =       -1710
472145

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13071186
17                 X    =        -3984097
55
 Y    =        6384783
29  feet           Y    =         1946081
95  meter
 Z    =      -16584588
40                 Z    =        -5054982
54
 XDOT =      -4229
554987                 XDOT =       -1289
168360
 YDOT =     -23206
923095  feet/sec       YDOT =       -7073
470160  meter/sec
 ZDOT =      -5610
927538                 ZDOT =       -1710
210714


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   07308
43040285  
00020000  00000-0  20000-3 0  9058
2 25544  51
6343 100
7469 0002211 170
8689 189
2516 15
76067379 32903


Satellite: ISS
Catalog Number: 25544
Epoch time:      07308
43040285   =   yrday
fracday
Element set:     905
Inclination:       51
6343  deg
RA of node:       100
7469  deg
Eccentricity:     
0002211     
Arg of perigee:   170
8689  deg
Mean anomaly:     189
2516  deg
Mean motion:   15
76067379  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3290
Checksum:              293


Coasting Arc #7 (Orbit 3305)
---------------------------------------

Vector Time (GMT): 2007/309/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -48480
67                 A    =         6725789
93  meter
 Y    =       -6670838
74  meter          E    =           
0014779
 Z    =         793562
86                 I    =           51
97585
 XDOT =       4775
695191                 Wp   =          132
46889
 YDOT =       -755
886503  meter/sec      RA   =           94
92098  deg
 ZDOT =      -6001
871139                 TA   =           38
90703
                                          MA   =           38
80075
                                          Ha   =            186
951  n
mi
                                          Hp   =            180
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -159057
31                 X    =           22262
20
 Y    =      -21885953
86  feet           Y    =        -6670985
32  meter
 Z    =        2603552
68                 Z    =          793499
29
 XDOT =      15668
291310                 XDOT =        4812
949294
 YDOT =      -2479
942595  feet/sec       YDOT =        -702
273779  meter/sec
 ZDOT =     -19691
178276                 ZDOT =       -5978
579828

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4607004
76                 X    =         1404215
05
 Y    =       21396287
04  feet           Y    =         6521588
29  meter
 Z    =        2602531
49                 Z    =          793251
60
 XDOT =     -13388
327190                 XDOT =       -4080
762128
 YDOT =       5291
257418  feet/sec       YDOT =        1612
775261  meter/sec
 ZDOT =     -19602
622539                 ZDOT =       -5974
879350


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   07309
44488818  
00020000  00000-0  20000-3 0  9069
2 25544  51
6348  95
5198 0001902 178
5909 181
5261 15
76152753 33065


Satellite: ISS
Catalog Number: 25544
Epoch time:      07309
44488818   =   yrday
fracday
Element set:     906
Inclination:       51
6348  deg
RA of node:        95
5198  deg
Eccentricity:     
0001902     
Arg of perigee:   178
5909  deg
Mean anomaly:     181
5261  deg
Mean motion:   15
76152753  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3306
Checksum:              316


Coasting Arc #8 (Orbit 3321)
---------------------------------------

Vector Time (GMT): 2007/310/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4137541
35                 A    =         6714137
28  meter
 Y    =         121062
87  meter          E    =           
0003443
 Z    =        5284237
59                 I    =           51
93649
 XDOT =       -101
315916                 Wp   =          132
45159
 YDOT =      -7705
700944  meter/sec      RA   =           89
79920  deg
 ZDOT =         94
895580                 TA   =          316
63879
                                          MA   =          316
66587
                                          Ha   =            187
227  n
mi
                                          Hp   =            180
464

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13574610
71                 X    =        -4164258
09
 Y    =         397187
90  feet           Y    =           74645
23  meter
 Z    =       17336737
49                 Z    =         5264072
01
 XDOT =       -332
401298                 XDOT =         -15
603072
 YDOT =     -25281
171076  feet/sec       YDOT =       -7706
354670  meter/sec
 ZDOT =        311
337205                 ZDOT =          94
611676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13251306
00                 X    =         4038998
07
 Y    =       -3389022
59  feet           Y    =        -1032974
08  meter
 Z    =       17260002
79                 Z    =         5260848
85
 XDOT =       5629
143055                 XDOT =        1715
762803
 YDOT =      23624
728835  feet/sec       YDOT =        7200
817349  meter/sec
 ZDOT =        309
365935                 ZDOT =          94
294737


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   07310
45935357  
00020000  00000-0  20000-3 0  9078
2 25544  51
6341  90
2922 0002133 175
7831 184
3352 15
76094264 33227


Satellite: ISS
Catalog Number: 25544
Epoch time:      07310
45935357   =   yrday
fracday
Element set:     907
Inclination:       51
6341  deg
RA of node:        90
2922  deg
Eccentricity:     
0002133     
Arg of perigee:   175
7831  deg
Mean anomaly:     184
3352  deg
Mean motion:   15
76094264  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3322
Checksum:              277


Coasting Arc #9 (Orbit 3337)
---------------------------------------

Vector Time (GMT): 2007/311/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         117564
93                 A    =         6725793
08  meter
 Y    =        6688886
80  meter          E    =           
0012078
 Z    =         644257
16                 I    =           51
97578
 XDOT =      -4777
149722                 Wp   =           59
74262
 YDOT =       -503
593722  meter/sec      RA   =           84
67429  deg
 ZDOT =       6023
000605                 TA   =          307
24687
                                          MA   =          307
35698
                                          Ha   =            186
899  n
mi
                                          Hp   =            180
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         385711
71                 X    =           39630
27
 Y    =       21945166
66  feet           Y    =         6689765
72  meter
 Z    =        2113704
58                 Z    =          644638
99
 XDOT =     -15673
063391                 XDOT =       -4800
422913
 YDOT =      -1652
210375  feet/sec       YDOT =        -557
144638  meter/sec
 ZDOT =      19760
500673                 ZDOT =        5999
736002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5548660
43                 X    =        -1691231
70
 Y    =      -21235397
49  feet           Y    =        -6472549
15  meter
 Z    =        2115920
92                 Z    =          644932
70
 XDOT =      14179
060389                 XDOT =        4321
777607
 YDOT =      -1719
541806  feet/sec       YDOT =        -524
116343  meter/sec
 ZDOT =      19671
898796                 ZDOT =        5995
994753


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   07311
47378937  
00020000  00000-0  20000-3 0  9087
2 25544  51
6347  85
0646 0002183 181
4612 178
6546 15
76185127 33381


Satellite: ISS
Catalog Number: 25544
Epoch time:      07311
47378937   =   yrday
fracday
Element set:     908
Inclination:       51
6347  deg
RA of node:        85
0646  deg
Eccentricity:     
0002183     
Arg of perigee:   181
4612  deg
Mean anomaly:     178
6546  deg
Mean motion:   15
76185127  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3338
Checksum:              310


Coasting Arc #10 (Orbit 3352)
---------------------------------------

Vector Time (GMT): 2007/312/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4254652
52                 A    =         6714629
28  meter
 Y    =        1007885
30  meter          E    =           
0014279
 Z    =       -5108487
88                 I    =           51
93521
 XDOT =        126
301474                 Wp   =          110
49384
 YDOT =       7526
881155  meter/sec      RA   =           79
52478  deg
 ZDOT =       1588
884006                 TA   =          174
72047
                                          MA   =          174
70540
                                          Ha   =            186
824  n
mi
                                          Hp   =            180
477

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13958833
72                 X    =         4267882
88
 Y    =        3306710
30  feet           Y    =         1055537
29  meter
 Z    =      -16760130
84                 Z    =        -5087785
96
 XDOT =        414
374916                 XDOT =          34
406606
 YDOT =      24694
491977  feet/sec       YDOT =        7527
779693  meter/sec
 ZDOT =       5212
874034                 ZDOT =        1589
274500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14432445
75                 X    =        -4399009
47
 Y    =         355788
99  feet           Y    =          108444
48  meter
 Z    =      -16681225
41                 Z    =        -5084437
51
 XDOT =      -6593
508155                 XDOT =       -2009
701286
 YDOT =     -22741
437762  feet/sec       YDOT =       -6931
590230  meter/sec
 ZDOT =       5215
205883                 ZDOT =        1589
594753


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   07312
42480200  
00020000  00000-0  20000-3 0  9091
2 25544  51
6355  80
1644 0002150 181
9715 178
1441 15
76217358 33535


Satellite: ISS
Catalog Number: 25544
Epoch time:      07312
42480200   =   yrday
fracday
Element set:     909
Inclination:       51
6355  deg
RA of node:        80
1644  deg
Eccentricity:     
0002150     
Arg of perigee:   181
9715  deg
Mean anomaly:     178
1441  deg
Mean motion:   15
76217358  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3353
Checksum:              268


Coasting Arc #11 (Orbit 3368)
---------------------------------------

Vector Time (GMT): 2007/313/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -59554
20                 A    =         6723743
56  meter
 Y    =       -6378733
80  meter          E    =           
0007821
 Z    =       -2115591
85                 I    =           51
96042
 XDOT =       5017
840477                 Wp   =          149
17498
 YDOT =       1792
927742  meter/sec      RA   =           74
42578  deg
 ZDOT =      -5562
670710                 TA   =           54
38370
                                          MA   =           54
31087
                                          Ha   =            186
661  n
mi
                                          Hp   =            180
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -195387
79                 X    =           22055
70
 Y    =      -20927604
35  feet           Y    =        -6378943
39  meter
 Z    =       -6940918
15                 Z    =        -2115683
17
 XDOT =      16462
731224                 XDOT =        5024
442104
 YDOT =       5882
308866  feet/sec       YDOT =        1849
077188  meter/sec
 ZDOT =     -18250
231988                 ZDOT =       -5538
277121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5792048
93                 X    =         1765416
52
 Y    =       20110702
61  feet           Y    =         6129742
16  meter
 Z    =       -6941970
50                 Z    =        -2115912
61
 XDOT =     -16071
261174                 XDOT =       -4898
520406
 YDOT =      -1621
376441  feet/sec       YDOT =        -494
195539  meter/sec
 ZDOT =     -18157
188623                 ZDOT =       -5534
311092


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   07313
43918997  
00020000  00000-0  20000-3 0  9104
2 25544  51
6358  74
9369 0001924 186
4268 173
6871 15
76279709 33696


Satellite: ISS
Catalog Number: 25544
Epoch time:      07313
43918997   =   yrday
fracday
Element set:     910
Inclination:       51
6358  deg
RA of node:        74
9369  deg
Eccentricity:     
0001924     
Arg of perigee:   186
4268  deg
Mean anomaly:     173
6871  deg
Mean motion:   15
76279709  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3369
Checksum:              342


Coasting Arc #12 (Orbit 3384)
---------------------------------------

Vector Time (GMT): 2007/314/09:52:44
280
Vector Time (MET): N/A
Weight (LBS)     : 540904
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4543092
69                 A    =         6717041
09  meter
 Y    =       -2073151
49  meter          E    =           
0008149
 Z    =        4486224
75                 I    =           51
92869
 XDOT =         28
433654                 Wp   =           80
05229
 YDOT =      -7010
291924  meter/sec      RA   =           69
25188  deg
 ZDOT =      -3204
498961                 TA   =           41
85527
                                          MA   =           41
79299
                                          Ha   =            186
777  n
mi
                                          Hp   =            180
382

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14905159
76                 X    =        -4541366
74
 Y    =       -6801678
12  feet           Y    =        -2123945
53  meter
 Z    =       14718585
14                 Z    =         4464157
74
 XDOT =         93
286268                 XDOT =         122
389080
 YDOT =     -22999
645421  feet/sec       YDOT =       -7009
448451  meter/sec
 ZDOT =     -10513
448035                 ZDOT =       -3204
132996

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16307313
56                 X    =         4970469
17
 Y    =        2229392
42  feet           Y    =          679518
81  meter
 Z    =       14634366
91                 Z    =         4460555
03
 XDOT =       6596
611184                 XDOT =        2010
647089
 YDOT =      20892
717371  feet/sec       YDOT =        6368
100255  meter/sec
 ZDOT =     -10512
816548                 ZDOT =       -3204
306484


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   07314
45355465  
00020000  00000-0  20000-3 0  9113
2 25544  51
6360  69
7096 0002050 188
9574 171
1554 15
76268570 33859


Satellite: ISS
Catalog Number: 25544
Epoch time:      07314
45355465   =   yrday
fracday
Element set:     911
Inclination:       51
6360  deg
RA of node:        69
7096  deg
Eccentricity:     
0002050     
Arg of perigee:   188
9574  deg
Mean anomaly:     171
1554  deg
Mean motion:   15
76268570  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3385
Checksum:              304

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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