Date: October 14th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4520 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1150)
---------------------------------------

Vector Time (GMT): 2006/284/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4171177
72                 A    =         6724132
22  meter
 Y    =        5267576
18  meter          E    =           
0022360
 Z    =         -87499
84                 I    =           51
40487
 XDOT =      -3729
711857                 Wp   =          108
16404
 YDOT =      -3032
441611  meter/sec      RA   =          307
77872  deg
 ZDOT =      -6020
937936                 TA   =           72
79058
                                          MA   =           72
54595
                                          Ha   =            190
405  n
mi
                                          Hp   =            174
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13684966
26                 X    =        -4229345
40
 Y    =       17282074
07  feet           Y    =         5220606
53  meter
 Z    =        -287072
95                 Z    =         -107904
97
 XDOT =     -12236
587457                 XDOT =       -3666
276300
 YDOT =      -9948
955417  feet/sec       YDOT =       -3073
794500  meter/sec
 ZDOT =     -19753
733385                 ZDOT =       -6038
903191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9725070
27                 X    =         2964201
42
 Y    =      -19781872
19  feet           Y    =        -6029514
64  meter
 Z    =        -362405
13                 Z    =         -110461
09
 XDOT =      12512
300459                 XDOT =        3813
749180
 YDOT =       6454
231989  feet/sec       YDOT =        1967
249910  meter/sec
 ZDOT =     -19821
064787                 ZDOT =       -6041
460547


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   06284
51212143  
00020000  00000-0  20000-3 0  9008
2 25544  51
6351 308
1888 0012886  83
1185 277
1445 15
76829739 11515


Satellite: ISS
Catalog Number: 25544
Epoch time:      06284
51212143   =   yrday
fracday
Element set:     900
Inclination:       51
6351  deg
RA of node:       308
1888  deg
Eccentricity:     
0012886     
Arg of perigee:    83
1185  deg
Mean anomaly:     277
1445  deg
Mean motion:   15
76829739  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1151
Checksum:              295


Coasting Arc #2 (Orbit 1166)
---------------------------------------

Vector Time (GMT): 2006/285/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2755555
65                 A    =         6712420
19  meter
 Y    =        3312229
41  meter          E    =           
0016479
 Z    =        5133722
11                 I    =           51
34844
 XDOT =      -4867
098544                 Wp   =           79
15904
 YDOT =       5874
004198  meter/sec      RA   =          302
59162  deg
 ZDOT =      -1171
176643                 TA   =           22
08098
                                          MA   =           22
01008
                                          Ha   =            190
314  n
mi
                                          Hp   =            174
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9040536
92                 X    =         2693374
00
 Y    =       10866894
38  feet           Y    =         3342695
76  meter
 Z    =       16842920
29                 Z    =         5146957
82
 XDOT =     -15968
171077                 XDOT =       -4926
731295
 YDOT =      19271
667316  feet/sec       YDOT =        5819
244210  meter/sec
 ZDOT =      -3842
443054                 ZDOT =       -1194
966048

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11189007
35                 X    =        -3410409
44
 Y    =       -8540985
64  feet           Y    =        -2603292
42  meter
 Z    =       16892671
31                 Z    =         5148886
22
 XDOT =      10510
941741                 XDOT =        3203
735043
 YDOT =     -21583
550551  feet/sec       YDOT =       -6578
666208  meter/sec
 ZDOT =      -3930
309104                 ZDOT =       -1197
958215


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   06285
52612689  
00020000  00000-0  20000-3 0  9010
2 25544  51
6343 302
9590 0012917  86
8256 273
4386 15
76861659 11679


Satellite: ISS
Catalog Number: 25544
Epoch time:      06285
52612689   =   yrday
fracday
Element set:     901
Inclination:       51
6343  deg
RA of node:       302
9590  deg
Eccentricity:     
0012917     
Arg of perigee:    86
8256  deg
Mean anomaly:     273
4386  deg
Mean motion:   15
76861659  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1167
Checksum:              321


Coasting Arc #3 (Orbit 1182)
---------------------------------------

Vector Time (GMT): 2006/286/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4241131
42                 A    =         6722425
77  meter
 Y    =       -4835253
69  meter          E    =           
0026602
 Z    =        1921338
02                 I    =           51
36807
 XDOT =       2662
538134                 Wp   =           78
12573
 YDOT =       4584
435600  meter/sec      RA   =          297
44240  deg
 ZDOT =       5600
211305                 TA   =          303
36873
                                          MA   =          303
62303
                                          Ha   =            190
387  n
mi
                                          Hp   =            174
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13914473
16                 X    =         4285551
08
 Y    =      -15863693
21  feet           Y    =        -4787578
68  meter
 Z    =        6303602
43                 Z    =         1942049
46
 XDOT =       8735
361331                 XDOT =        2583
871372
 YDOT =      15040
799211  feet/sec       YDOT =        4613
769636  meter/sec
 ZDOT =      18373
396671                 ZDOT =        5612
955035

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9576217
88                 X    =        -2918831
21
 Y    =       18777502
81  feet           Y    =         5723382
86  meter
 Z    =        6380138
61                 Z    =         1944666
25
 XDOT =     -10682
127465                 XDOT =       -3255
912451
 YDOT =     -11772
710752  feet/sec       YDOT =       -3588
322237  meter/sec
 ZDOT =      18421
487496                 ZDOT =        5614
869389


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   06286
54011817  
00020000  00000-0  20000-3 0  9020
2 25544  51
6344 297
7293 0012963  90
1337 270
1313 15
76856351 11835


Satellite: ISS
Catalog Number: 25544
Epoch time:      06286
54011817   =   yrday
fracday
Element set:     902
Inclination:       51
6344  deg
RA of node:       297
7293  deg
Eccentricity:     
0012963     
Arg of perigee:    90
1337  deg
Mean anomaly:     270
1313  deg
Mean motion:   15
76856351  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1183
Checksum:              287


Coasting Arc #4 (Orbit 1197)
---------------------------------------

Vector Time (GMT): 2006/287/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1932516
84                 A    =         6715394
71  meter
 Y    =       -4670063
21  meter          E    =           
0022205
 Z    =       -4442846
66                 I    =           51
33300
 XDOT =       4834
450135                 Wp   =          100
76554
 YDOT =      -5044
153953  meter/sec      RA   =          292
22218  deg
 ZDOT =       3208
765322                 TA   =          201
49937
                                          MA   =          201
59277
                                          Ha   =            190
335  n
mi
                                          Hp   =            174
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6340278
35                 X    =        -1858569
22
 Y    =      -15321729
70  feet           Y    =        -4691260
21  meter
 Z    =      -14576268
56                 Z    =        -4452055
28
 XDOT =      15861
056873                 XDOT =        4874
907545
 YDOT =     -16549
061524  feet/sec       YDOT =       -4989
866253  meter/sec
 ZDOT =      10527
445281                 ZDOT =        3232
349501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10045956
45                 X    =         3062007
53
 Y    =       13153463
34  feet           Y    =         4009175
63  meter
 Z    =      -14611204
49                 Z    =        -4453495
13
 XDOT =      -9969
942346                 XDOT =       -3038
838427
 YDOT =      19371
051220  feet/sec       YDOT =        5904
296412  meter/sec
 ZDOT =      10614
658305                 ZDOT =        3235
347852


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   06287
49071871  
00020000  00000-0  20000-3 0  9032
2 25544  51
6348 292
8261 0012833  93
6826 266
5807 15
76871798 11982


Satellite: ISS
Catalog Number: 25544
Epoch time:      06287
49071871   =   yrday
fracday
Element set:     903
Inclination:       51
6348  deg
RA of node:       292
8261  deg
Eccentricity:     
0012833     
Arg of perigee:    93
6826  deg
Mean anomaly:     266
5807  deg
Mean motion:   15
76871798  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1198
Checksum:              336


Coasting Arc #5 (Orbit 1213)
---------------------------------------

Vector Time (GMT): 2006/288/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4193387
91                 A    =         6718188
05  meter
 Y    =        3832574
40  meter          E    =           
0018254
 Z    =       -3601213
31                 I    =           51
33198
 XDOT =      -1800
409675                 Wp   =           92
37493
 YDOT =      -6064
872511  meter/sec      RA   =          287
09137  deg
 ZDOT =      -4377
892089                 TA   =          130
91777
                                          MA   =          130
75956
                                          Ha   =            190
266  n
mi
                                          Hp   =            174
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13757834
35                 X    =        -4218438
48
 Y    =       12574062
98  feet           Y    =         3785541
49  meter
 Z    =      -11815004
30                 Z    =        -3621645
81
 XDOT =      -5906
855890                 XDOT =       -1711
190486
 YDOT =     -19897
875692  feet/sec       YDOT =       -6084
506903  meter/sec
 ZDOT =     -14363
163023                 ZDOT =       -4386
421729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9659054
25                 X    =         2944079
73
 Y    =      -15883793
98  feet           Y    =        -4841380
41  meter
 Z    =      -11890632
96                 Z    =        -3624264
93
 XDOT =       9968
853848                 XDOT =        3038
506653
 YDOT =      16790
396037  feet/sec       YDOT =        5117
712712  meter/sec
 ZDOT =     -14395
762411                 ZDOT =       -4387
828383


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   06288
50467804  
00020000  00000-0  20000-3 0  9041
2 25544  51
6334 287
5949 0012875  97
7983 262
4644 15
76908747 12144


Satellite: ISS
Catalog Number: 25544
Epoch time:      06288
50467804   =   yrday
fracday
Element set:     904
Inclination:       51
6334  deg
RA of node:       287
5949  deg
Eccentricity:     
0012875     
Arg of perigee:    97
7983  deg
Mean anomaly:     262
4644  deg
Mean motion:   15
76908747  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1214
Checksum:              337


Coasting Arc #6 (Orbit 1229)
---------------------------------------

Vector Time (GMT): 2006/289/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1286457
98                 A    =         6719614
41  meter
 Y    =        5824017
46  meter          E    =           
0025936
 Z    =        3068715
78                 I    =           51
32939
 XDOT =      -4749
695110                 Wp   =           97
84851
 YDOT =       3634
372499  meter/sec      RA   =          281
85967  deg
 ZDOT =      -4874
850681                 TA   =           46
27945
                                          MA   =           46
06495
                                          Ha   =            190
141  n
mi
                                          Hp   =            174
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4220662
66                 X    =         1206330
03
 Y    =       19107668
84  feet           Y    =         5837955
43  meter
 Z    =       10067965
16                 Z    =         3074770
61
 XDOT =     -15582
989206                 XDOT =       -4766
300856
 YDOT =      11923
794288  feet/sec       YDOT =        3581
165771  meter/sec
 ZDOT =     -15993
604596                 ZDOT =       -4897
965305

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9605008
19                 X    =        -2927606
50
 Y    =      -17034965
68  feet           Y    =        -5192257
54  meter
 Z    =       10091317
36                 Z    =         3075833
53
 XDOT =      10055
809747                 XDOT =        3065
010811
 YDOT =     -15256
226691  feet/sec       YDOT =       -4650
097895  meter/sec
 ZDOT =     -16079
253006                 ZDOT =       -4900
956316


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   06289
51862047  
00020000  00000-0  20000-3 0  9052
2 25544  51
6326 282
3642 0012824 100
8898 259
3711 15
76968445 12302


Satellite: ISS
Catalog Number: 25544
Epoch time:      06289
51862047   =   yrday
fracday
Element set:     905
Inclination:       51
6326  deg
RA of node:       282
3642  deg
Eccentricity:     
0012824     
Arg of perigee:   100
8898  deg
Mean anomaly:     259
3711  deg
Mean motion:   15
76968445  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1230
Checksum:              306


Coasting Arc #7 (Orbit 1245)
---------------------------------------

Vector Time (GMT): 2006/290/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4098878
36                 A    =         6713860
89  meter
 Y    =       -2401505
95  meter          E    =           
0019999
 Z    =        4730876
86                 I    =           51
30459
 XDOT =       1223
678201                 Wp   =          110
09973
 YDOT =       7173
370813  meter/sec      RA   =          276
72353  deg
 ZDOT =       2565
618620                 TA   =          314
60316
                                          MA   =          314
76616
                                          Ha   =            190
048  n
mi
                                          Hp   =            174
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13447763
66                 X    =         4102445
74
 Y    =       -7878956
52  feet           Y    =        -2355649
85  meter
 Z    =       15521249
53                 Z    =         4750798
17
 XDOT =       4014
692262                 XDOT =        1130
910199
 YDOT =      23534
681145  feet/sec       YDOT =        7186
536091  meter/sec
 ZDOT =       8417
383924                 ZDOT =        2571
337627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10251831
44                 X    =        -3124758
22
 Y    =       11641320
11  feet           Y    =         3548274
37  meter
 Z    =       15595162
98                 Z    =         4753405
67
 XDOT =     -10236
331291                 XDOT =       -3120
033777
 YDOT =     -20388
670331  feet/sec       YDOT =       -6214
466717  meter/sec
 ZDOT =       8439
675484                 ZDOT =        2572
413087


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   06290
53254775  
00020000  00000-0  20000-3 0  9060
2 25544  51
6318 277
1336 0012767 104
9488 255
3092 15
76963974 12468


Satellite: ISS
Catalog Number: 25544
Epoch time:      06290
53254775   =   yrday
fracday
Element set:     906
Inclination:       51
6318  deg
RA of node:       277
1336  deg
Eccentricity:     
0012767     
Arg of perigee:   104
9488  deg
Mean anomaly:     255
3092  deg
Mean motion:   15
76963974  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1246
Checksum:              320


Coasting Arc #8 (Orbit 1260)
---------------------------------------

Vector Time (GMT): 2006/291/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -869911
41                 A    =         6722840
39  meter
 Y    =       -6538968
45  meter          E    =           
0017925
 Z    =       -1302009
74                 I    =           51
33338
 XDOT =       4710
345427                 Wp   =           80
52217
 YDOT =      -1772
566644  meter/sec      RA   =          271
50948  deg
 ZDOT =       5826
101383                 TA   =          265
11836
                                          MA   =          265
32304
                                          Ha   =            190
092  n
mi
                                          Hp   =            174
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2854040
05                 X    =         -790402
09
 Y    =      -21453308
58  feet           Y    =        -6548251
80  meter
 Z    =       -4271685
51                 Z    =        -1306042
32
 XDOT =      15453
889196                 XDOT =        4701
513906
 YDOT =      -5815
507362  feet/sec       YDOT =       -1719
941994  meter/sec
 ZDOT =      19114
505849                 ZDOT =        5848
963190

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9691264
47                 X    =         2953897
41
 Y    =       19347688
95  feet           Y    =         5897175
59  meter
 Z    =       -4287611
89                 Z    =        -1306864
10
 XDOT =     -11191
092071                 XDOT =       -3411
044863
 YDOT =       9808
942788  feet/sec       YDOT =        2989
765762  meter/sec
 ZDOT =      19199
462423                 ZDOT =        5851
996147


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   06291
48308869  
00020000  00000-0  20000-3 0  9070
2 25544  51
6317 272
2302 0012948 108
8267 251
4303 15
77019679 12619


Satellite: ISS
Catalog Number: 25544
Epoch time:      06291
48308869   =   yrday
fracday
Element set:     907
Inclination:       51
6317  deg
RA of node:       272
2302  deg
Eccentricity:     
0012948     
Arg of perigee:   108
8267  deg
Mean anomaly:     251
4303  deg
Mean motion:   15
77019679  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1261
Checksum:              301


Coasting Arc #9 (Orbit 1276)
---------------------------------------

Vector Time (GMT): 2006/292/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4171357
58                 A    =         6711616
53  meter
 Y    =         617363
33  meter          E    =           
0027138
 Z    =       -5244427
99                 I    =           51
29553
 XDOT =       -741
851400                 Wp   =           98
84647
 YDOT =      -7643
645620  meter/sec      RA   =          266
34141  deg
 ZDOT =       -315
234547                 TA   =          168
17284
                                          MA   =          168
10898
                                          Ha   =            190
032  n
mi
                                          Hp   =            174
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13685556
35                 X    =        -4152474
05
 Y    =        2025470
24  feet           Y    =          570822
16  meter
 Z    =      -17206128
57                 Z    =        -5264646
97
 XDOT =      -2433
895670                 XDOT =        -654
792578
 YDOT =     -25077
577495  feet/sec       YDOT =       -7651
454663  meter/sec
 ZDOT =      -1034
234077                 ZDOT =        -318
626593

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12069238
12                 X    =         3678703
78
 Y    =       -6567703
92  feet           Y    =        -2001836
16  meter
 Z    =      -17281394
59                 Z    =        -5267369
07
 XDOT =      10409
994098                 XDOT =        3172
966201
 YDOT =      21840
189396  feet/sec       YDOT =        6656
889728  meter/sec
 ZDOT =      -1047
930123                 ZDOT =        -319
409101


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   06292
49698307  
00020000  00000-0  20000-3 0  9082
2 25544  51
6314 266
9978 0012755 112
2225 248
0294 15
76997878 12777


Satellite: ISS
Catalog Number: 25544
Epoch time:      06292
49698307   =   yrday
fracday
Element set:     908
Inclination:       51
6314  deg
RA of node:       266
9978  deg
Eccentricity:     
0012755     
Arg of perigee:   112
2225  deg
Mean anomaly:     248
0294  deg
Mean motion:   15
76997878  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1277
Checksum:              341


Coasting Arc #10 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2006/293/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         416580
87                 A    =         6723268
61  meter
 Y    =        6659342
52  meter          E    =           
0022658
 Z    =        -764134
61                 I    =           51
33890
 XDOT =      -4879
012928                 Wp   =          126
88131
 YDOT =       -362
805840  meter/sec      RA   =          261
16354  deg
 ZDOT =      -5956
438405                 TA   =           61
49711
                                          MA   =           61
26912
                                          Ha   =            189
898  n
mi
                                          Hp   =            174
738

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1366735
12                 X    =          345796
32
 Y    =       21848236
61  feet           Y    =         6663605
14  meter
 Z    =       -2507003
33                 Z    =         -762283
14
 XDOT =     -16007
260264                 XDOT =       -4845
657402
 YDOT =      -1190
307875  feet/sec       YDOT =        -417
179506  meter/sec
 ZDOT =     -19542
120751                 ZDOT =       -5980
060142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9139994
38                 X    =        -2785870
29
 Y    =      -19892537
93  feet           Y    =        -6063245
56  meter
 Z    =       -2499182
06                 Z    =         -761750
69
 XDOT =      13814
079210                 XDOT =        4210
531343
 YDOT =      -3936
627002  feet/sec       YDOT =       -1199
883910  meter/sec
 ZDOT =     -19630
203812                 ZDOT =       -5983
286122


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   06293
51086011  
00020000  00000-0  20000-3 0  9090
2 25544  51
6318 261
7661 0012695 115
5816 244
6662 15
77047119 12932


Satellite: ISS
Catalog Number: 25544
Epoch time:      06293
51086011   =   yrday
fracday
Element set:     909
Inclination:       51
6318  deg
RA of node:       261
7661  deg
Eccentricity:     
0012695     
Arg of perigee:   115
5816  deg
Mean anomaly:     244
6662  deg
Mean motion:   15
77047119  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1293
Checksum:              294


Coasting Arc #11 (Orbit 1308)
---------------------------------------

Vector Time (GMT): 2006/294/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4373883
03                 A    =         6712676
48  meter
 Y    =        1205813
64  meter          E    =           
0016091
 Z    =        4932757
90                 I    =           51
30900
 XDOT =        209
025409                 Wp   =          100
36393
 YDOT =       7450
487034  meter/sec      RA   =          255
95799  deg
 ZDOT =      -2003
957386                 TA   =            9
08033
                                          MA   =            9
05127
                                          Ha   =            189
675  n
mi
                                          Hp   =            174
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14350009
93                 X    =         4336111
28
 Y    =        3956081
49  feet           Y    =         1254513
86  meter
 Z    =       16183588
91                 Z    =         4953914
99
 XDOT =        685
778901                 XDOT =         135
432620
 YDOT =      24443
855099  feet/sec       YDOT =        7452
412902  meter/sec
 ZDOT =      -6574
663341                 ZDOT =       -2003
121019

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14702580
25                 X    =        -4481346
46
 Y    =        1686340
01  feet           Y    =          513996
43  meter
 Z    =       16262604
56                 Z    =         4956841
87
 XDOT =      -9721
850791                 XDOT =       -2963
220121
 YDOT =     -21313
276372  feet/sec       YDOT =       -6496
286638  meter/sec
 ZDOT =      -6570
515351                 ZDOT =       -2002
693079


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   06294
52471999  
00020000  00000-0  20000-3 0  9107
2 25544  51
6317 256
5352 0012569 119
6872 240
5545 15
77070857 13095


Satellite: ISS
Catalog Number: 25544
Epoch time:      06294
52471999   =   yrday
fracday
Element set:     910
Inclination:       51
6317  deg
RA of node:       256
5352  deg
Eccentricity:     
0012569     
Arg of perigee:   119
6872  deg
Mean anomaly:     240
5545  deg
Mean motion:   15
77070857  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1309
Checksum:              314


Coasting Arc #12 (Orbit 1324)
---------------------------------------

Vector Time (GMT): 2006/295/11:32:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         114797
52                 A    =         6720178
03  meter
 Y    =       -6161205
08  meter          E    =           
0024256
 Z    =        2666586
01                 I    =           51
34371
 XDOT =       5203
294268                 Wp   =          100
25660
 YDOT =       2356
142432  meter/sec      RA   =          250
81612  deg
 ZDOT =       5175
799923                 TA   =          290
31146
                                          MA   =          290
57197
                                          Ha   =            189
668  n
mi
                                          Hp   =            174
833

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         376632
27                 X    =          170730
25
 Y    =      -20213927
44  feet           Y    =        -6159608
54  meter
 Z    =        8748641
77                 Z    =         2667279
76
 XDOT =      17071
175421                 XDOT =        5151
416971
 YDOT =       7730
126089  feet/sec       YDOT =        2414
038648  meter/sec
 ZDOT =      16980
970877                 ZDOT =        5200
952205

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7606775
62                 X    =         2318545
21
 Y    =       18731025
87  feet           Y    =         5709216
68  meter
 Z    =        8750376
09                 Z    =         2667114
63
 XDOT =     -17282
283428                 XDOT =       -5267
639989
 YDOT =      -1025
932324  feet/sec       YDOT =        -312
704172  meter/sec
 ZDOT =      17075
037046                 ZDOT =        5204
471291


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   06295
53856120  
00020000  00000-0  20000-3 0  9113
2 25544  51
6324 251
3043 0012620 124
2854 235
9507 15
77135071 13257


Satellite: ISS
Catalog Number: 25544
Epoch time:      06295
53856120   =   yrday
fracday
Element set:     911
Inclination:       51
6324  deg
RA of node:       251
3043  deg
Eccentricity:     
0012620     
Arg of perigee:   124
2854  deg
Mean anomaly:     235
9507  deg
Mean motion:   15
77135071  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1325
Checksum:              262

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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