Date: October 26th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6113 9 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


299/14:46:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 9
000/00:00:00 000 0 0 0 0 175 2

Coasting Arc #1 (Orbit 1370)
---------------------------------------

Vector Time (GMT): 2006/298/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4955850
78                 A    =         6720386
16  meter
 Y    =        3818609
64  meter          E    =           
0025383
 Z    =        2414455
48                 I    =           51
38158
 XDOT =      -1507
456881                 Wp   =          119
33047
 YDOT =       5356
582218  meter/sec      RA   =          235
57068  deg
 ZDOT =      -5347
840669                 TA   =           33
23027
                                          MA   =           33
07112
                                          Ha   =            189
188  n
mi
                                          Hp   =            175
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16259352
94                 X    =         4901052
88
 Y    =       12528246
85  feet           Y    =         3873722
24  meter
 Z    =        7921441
85                 Z    =         2438398
75
 XDOT =      -4945
724674                 XDOT =       -1541
263269
 YDOT =      17574
088643  feet/sec       YDOT =        5339
536167  meter/sec
 ZDOT =     -17545
409019                 ZDOT =       -5355
246044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16833898
65                 X    =        -5130972
31
 Y    =      -11683879
30  feet           Y    =        -3561246
41  meter
 Z    =        8011216
46                 Z    =         2441818
78
 XDOT =       3093
114052                 XDOT =         942
781163
 YDOT =     -16571
363015  feet/sec       YDOT =       -5050
951447  meter/sec
 ZDOT =     -17572
279712                 ZDOT =       -5356
030856


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   06298
45327867  
00020000  00000-0  20000-3 0  9006
2 25544  51
6309 236
2733 0012339 134
9529 225
2638 15
77236127 13714


Satellite: ISS
Catalog Number: 25544
Epoch time:      06298
45327867   =   yrday
fracday
Element set:     900
Inclination:       51
6309  deg
RA of node:       236
2733  deg
Eccentricity:     
0012339     
Arg of perigee:   134
9529  deg
Mean anomaly:     225
2638  deg
Mean motion:   15
77236127  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1371
Checksum:              302


Coasting Arc #2 (Orbit 1386)
---------------------------------------

Vector Time (GMT): 2006/299/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1944717
51                 A    =         6711662
05  meter
 Y    =       -3971350
94  meter          E    =           
0017268
 Z    =        5041611
06                 I    =           51
37002
 XDOT =       5733
792684                 Wp   =          135
47866
 YDOT =       4894
873614  meter/sec      RA   =          230
42763  deg
 ZDOT =       1628
530496                 TA   =          298
75347
                                          MA   =          298
92684
                                          Ha   =            189
051  n
mi
                                          Hp   =            175
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6380306
80                 X    =         1964489
29
 Y    =      -13029366
59  feet           Y    =        -3949493
74  meter
 Z    =       16540718
71                 Z    =         5051106
57
 XDOT =      18811
655786                 XDOT =        5670
720060
 YDOT =      16059
296633  feet/sec       YDOT =        4958
639321  meter/sec
 ZDOT =       5342
947821                 ZDOT =        1656
233045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5385203
20                 X    =        -1641409
93
 Y    =       13428253
59  feet           Y    =         4092931
69  meter
 Z    =       16575574
69                 Z    =         5052235
17
 XDOT =     -18854
628451                 XDOT =       -5746
890752
 YDOT =     -14347
622187  feet/sec       YDOT =       -4373
155243  meter/sec
 ZDOT =       5446
892477                 ZDOT =        1660
212827


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   06299
46701309  
00020000  00000-0  20000-3 0  9016
2 25544  51
6312 231
0422 0012267 139
4291 220
7790 15
77288295 13871


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
46701309   =   yrday
fracday
Element set:     901
Inclination:       51
6312  deg
RA of node:       231
0422  deg
Eccentricity:     
0012267     
Arg of perigee:   139
4291  deg
Mean anomaly:     220
7790  deg
Mean motion:   15
77288295  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1387
Checksum:              289


Coasting Arc #3 (Orbit 1389)
---------------------------------------

Vector Time (GMT): 2006/299/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5037552
97                 A    =         6714202
58  meter
 Y    =         479073
50  meter          E    =           
0017464
 Z    =        4395535
16                 I    =           51
38566
 XDOT =       2233
633201                 Wp   =          109
99080
 YDOT =       6621
309271  meter/sec      RA   =          229
36241  deg
 ZDOT =      -3276
946627                 TA   =           12
94570
                                          MA   =           12
90092
                                          Ha   =            188
901  n
mi
                                          Hp   =            175
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16527404
75                 X    =         5010468
24
 Y    =        1571763
46  feet           Y    =          535254
53  meter
 Z    =       14421047
11                 Z    =         4419942
46
 XDOT =       7328
192917                 XDOT =        2175
346013
 YDOT =      21723
455615  feet/sec       YDOT =        6645
961273  meter/sec
 ZDOT =     -10751
137229                 ZDOT =       -3266
236584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5610377
70                 X    =        -1710043
12
 Y    =       15540740
64  feet           Y    =         4736817
75  meter
 Z    =       14512104
96                 Z    =         4423289
59
 XDOT =     -21744
756634                 XDOT =       -6627
801822
 YDOT =       2165
291877  feet/sec       YDOT =         659
980964  meter/sec
 ZDOT =     -10710
303559                 ZDOT =       -3264
500525


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   06299
65708562  
00020000  00000-0  20000-3 0  9026
2 25544  51
6343 230
0621 0012184 139
6206 220
5865 15
77308058 13906


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
65708562   =   yrday
fracday
Element set:     902
Inclination:       51
6343  deg
RA of node:       230
0621  deg
Eccentricity:     
0012184     
Arg of perigee:   139
6206  deg
Mean anomaly:     220
5865  deg
Mean motion:   15
77308058  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1390
Checksum:              284


Coasting Arc #4 (Orbit 1405)
---------------------------------------

Vector Time (GMT): 2006/300/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1352723
11                 A    =         6716852
60  meter
 Y    =       -5436289
60  meter          E    =           
0022010
 Z    =        3699008
35                 I    =           51
41390
 XDOT =       6274
850197                 Wp   =          120
25686
 YDOT =       1360
489761  meter/sec      RA   =          224
23432  deg
 ZDOT =       4264
382783                 TA   =          284
56591
                                          MA   =          284
80992
                                          Ha   =            188
997  n
mi
                                          Hp   =            175
354

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4438067
94                 X    =        -1309802
71
 Y    =      -17835595
80  feet           Y    =        -5451176
74  meter
 Z    =       12135854
15                 Z    =         3692540
61
 XDOT =      20586
778861                 XDOT =        6238
454613
 YDOT =       4463
549085  feet/sec       YDOT =        1430
454861  meter/sec
 ZDOT =      13990
757161                 ZDOT =        4294
778321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18394202
70                 X    =         5606552
98
 Y    =        -246977
85  feet           Y    =          -75278
85  meter
 Z    =       12110994
57                 Z    =         3691431
15
 XDOT =      -9114
944812                 XDOT =       -2778
235179
 YDOT =      17574
150632  feet/sec       YDOT =        5356
601113  meter/sec
 ZDOT =      14104
273207                 ZDOT =        4298
982474


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   06300
67079313  
00020000  00000-0  20000-3 0  9037
2 25544  51
6343 224
8298 0012219 143
4657 216
7344 15
77303065 14069


Satellite: ISS
Catalog Number: 25544
Epoch time:      06300
67079313   =   yrday
fracday
Element set:     903
Inclination:       51
6343  deg
RA of node:       224
8298  deg
Eccentricity:     
0012219     
Arg of perigee:   143
4657  deg
Mean anomaly:     216
7344  deg
Mean motion:   15
77303065  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1406
Checksum:              278


Coasting Arc #5 (Orbit 1420)
---------------------------------------

Vector Time (GMT): 2006/301/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5824326
91                 A    =         6719043
47  meter
 Y    =       -1796940
94  meter          E    =           
0013411
 Z    =       -2847494
02                 I    =           51
44313
 XDOT =       -694
879180                 Wp   =          128
09910
 YDOT =      -5752
572315  meter/sec      RA   =          219
00744  deg
 ZDOT =       5059
540612                 TA   =          199
13157
                                          MA   =          199
18199
                                          Ha   =            188
763  n
mi
                                          Hp   =            175
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19108684
09                 X    =        -5789967
55
 Y    =       -5895475
52  feet           Y    =        -1861879
52  meter
 Z    =       -9342171
99                 Z    =        -2875705
71
 XDOT =      -2279
787335                 XDOT =        -655
080209
 YDOT =     -18873
268751  feet/sec       YDOT =       -5760
120588  meter/sec
 ZDOT =      16599
542690                 ZDOT =        5056
261193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9856278
04                 X    =         3004193
55
 Y    =      -17342747
98  feet           Y    =        -5286069
58  meter
 Z    =       -9447618
34                 Z    =        -2879634
07
 XDOT =      17677
098668                 XDOT =        5387
979674
 YDOT =       1024
774917  feet/sec       YDOT =         312
351395  meter/sec
 ZDOT =      16586
523015                 ZDOT =        5055
572215


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   06301
62112097  
00020000  00000-0  20000-3 0  9041
2 25544  51
6341 219
9243 0012080 147
7558 212
4348 15
77348998 14213


Satellite: ISS
Catalog Number: 25544
Epoch time:      06301
62112097   =   yrday
fracday
Element set:     904
Inclination:       51
6341  deg
RA of node:       219
9243  deg
Eccentricity:     
0012080     
Arg of perigee:   147
7558  deg
Mean anomaly:     212
4348  deg
Mean motion:   15
77348998  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1421
Checksum:              286


Coasting Arc #6 (Orbit 1436)
---------------------------------------

Vector Time (GMT): 2006/302/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -269483
55                 A    =         6711915
05  meter
 Y    =        4556174
61  meter          E    =           
0019306
 Z    =       -4934278
30                 I    =           51
44173
 XDOT =      -6919
525832                 Wp   =          112
12264
 YDOT =      -2647
590808  meter/sec      RA   =          213
87233  deg
 ZDOT =      -2080
437222                 TA   =          137
72557
                                          MA   =          137
57659
                                          Ha   =            188
565  n
mi
                                          Hp   =            175
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -884132
39                 X    =         -296441
16
 Y    =       14948079
44  feet           Y    =         4553010
57  meter
 Z    =      -16188577
09                 Z    =        -4935652
77
 XDOT =     -22701
856403                 XDOT =       -6879
299307
 YDOT =      -8686
321548  feet/sec       YDOT =       -2724
743783  meter/sec
 ZDOT =      -6825
581438                 ZDOT =       -2113
955113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14493955
88                 X    =        -4417757
75
 Y    =       -3742516
76  feet           Y    =        -1140719
11  meter
 Z    =      -16193072
86                 Z    =        -4935648
61
 XDOT =      12734
177334                 XDOT =        3881
377251
 YDOT =     -19434
913683  feet/sec       YDOT =       -5923
761691  meter/sec
 ZDOT =      -6950
946774                 ZDOT =       -2118
648577


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   06302
63478205  
00020000  00000-0  20000-3 0  9050
2 25544  51
6336 214
6912 0012013 151
9803 208
2011 15
77396520 14379


Satellite: ISS
Catalog Number: 25544
Epoch time:      06302
63478205   =   yrday
fracday
Element set:     905
Inclination:       51
6336  deg
RA of node:       214
6912  deg
Eccentricity:     
0012013     
Arg of perigee:   151
9803  deg
Mean anomaly:     208
2011  deg
Mean motion:   15
77396520  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1437
Checksum:              261


Coasting Arc #7 (Orbit 1452)
---------------------------------------

Vector Time (GMT): 2006/303/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6100095
94                 A    =         6722347
67  meter
 Y    =        2700941
71  meter          E    =           
0024913
 Z    =         700728
22                 I    =           51
50146
 XDOT =      -1371
637315                 Wp   =          141
19775
 YDOT =       4675
029241  meter/sec      RA   =          208
67472  deg
 ZDOT =      -5984
246213                 TA   =           31
13174
                                          MA   =           30
98438
                                          Ha   =            188
561  n
mi
                                          Hp   =            175
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20013438
12                 X    =         6066036
21
 Y    =        8861357
30  feet           Y    =         2768965
91  meter
 Z    =        2298977
11                 Z    =          730280
15
 XDOT =      -4500
122423                 XDOT =       -1394
741467
 YDOT =      15338
022445  feet/sec       YDOT =        4659
561749  meter/sec
 ZDOT =     -19633
353718                 ZDOT =       -5990
965750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12341799
56                 X    =        -3761780
51
 Y    =       18061577
98  feet           Y    =         5505168
97  meter
 Z    =        2409572
35                 Z    =          734437
65
 XDOT =     -12970
266809                 XDOT =       -3953
337324
 YDOT =      -6200
647758  feet/sec       YDOT =       -1889
957437  meter/sec
 ZDOT =     -19657
764359                 ZDOT =       -5991
686577


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   06303
64842209  
00020000  00000-0  20000-3 0  9062
2 25544  51
6338 209
4589 0012231 155
9353 204
2386 15
77382343 14536


Satellite: ISS
Catalog Number: 25544
Epoch time:      06303
64842209   =   yrday
fracday
Element set:     906
Inclination:       51
6338  deg
RA of node:       209
4589  deg
Eccentricity:     
0012231     
Arg of perigee:   155
9353  deg
Mean anomaly:     204
2386  deg
Mean motion:   15
77382343  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1453
Checksum:              290


Coasting Arc #8 (Orbit 1468)
---------------------------------------

Vector Time (GMT): 2006/304/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2163830
46                 A    =         6710314
27  meter
 Y    =       -3596750
60  meter          E    =           
0012306
 Z    =        5229051
36                 I    =           51
48702
 XDOT =       6889
616856                 Wp   =          147
82983
 YDOT =       3430
963375  meter/sec      RA   =          203
50493  deg
 ZDOT =       -500
763579                 TA   =          306
87341
                                          MA   =          306
98615
                                          Ha   =            188
266  n
mi
                                          Hp   =            175
890

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7099181
30                 X    =         2178486
88
 Y    =      -11800362
87  feet           Y    =        -3572471
46  meter
 Z    =       17155680
32                 Z    =         5239599
02
 XDOT =      22603
729843                 XDOT =        6853
171945
 YDOT =      11256
441518  feet/sec       YDOT =        3507
803115  meter/sec
 ZDOT =      -1642
925128                 ZDOT =        -467
381935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10488240
68                 X    =         3196815
76
 Y    =        8849273
90  feet           Y    =         2697258
69  meter
 Z    =       17194518
45                 Z    =         5240889
22
 XDOT =     -14175
995807                 XDOT =       -4320
843522
 YDOT =      19689
045103  feet/sec       YDOT =        6001
220947  meter/sec
 ZDOT =      -1517
932227                 ZDOT =        -462
665743


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   06304
66203629  
00020000  00000-0  20000-3 0  9073
2 25544  51
6335 204
2257 0012025 160
1671 199
9963 15
77460981 14693


Satellite: ISS
Catalog Number: 25544
Epoch time:      06304
66203629   =   yrday
fracday
Element set:     907
Inclination:       51
6335  deg
RA of node:       204
2257  deg
Eccentricity:     
0012025     
Arg of perigee:   160
1671  deg
Mean anomaly:     199
9963  deg
Mean motion:   15
77460981  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1469
Checksum:              298


Coasting Arc #9 (Orbit 1484)
---------------------------------------

Vector Time (GMT): 2006/305/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5694330
96                 A    =         6721150
63  meter
 Y    =       -3205335
21  meter          E    =           
0016492
 Z    =        1573546
18                 I    =           51
54993
 XDOT =       3634
537218                 Wp   =          108
16540
 YDOT =      -3606
365449  meter/sec      RA   =          198
35210  deg
 ZDOT =       5752
162462                 TA   =          269
22848
                                          MA   =          269
41744
                                          Ha   =            188
107  n
mi
                                          Hp   =            176
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18682188
19                 X    =        -5665709
37
 Y    =      -10516191
63  feet           Y    =        -3268852
30  meter
 Z    =        5162553
07                 Z    =         1545952
26
 XDOT =      11924
334704                 XDOT =        3646
650530
 YDOT =     -11831
907640  feet/sec       YDOT =       -3565
654153  meter/sec
 ZDOT =      18871
924087                 ZDOT =        5769
848862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13159853
28                 X    =         4011123
28
 Y    =      -16955513
47  feet           Y    =        -5168040
51  meter
 Z    =        5059171
94                 Z    =         1542035
61
 XDOT =       8723
733330                 XDOT =        2658
993919
 YDOT =      12475
547126  feet/sec       YDOT =        3802
546764  meter/sec
 ZDOT =      18937
389482                 ZDOT =        5772
116314


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   06305
67562819  
00020000  00000-0  20000-3 0  9085
2 25544  51
6328 198
9918 0012019 164
7669 195
3860 15
77519156 14851


Satellite: ISS
Catalog Number: 25544
Epoch time:      06305
67562819   =   yrday
fracday
Element set:     908
Inclination:       51
6328  deg
RA of node:       198
9918  deg
Eccentricity:     
0012019     
Arg of perigee:   164
7669  deg
Mean anomaly:     195
3860  deg
Mean motion:   15
77519156  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1485
Checksum:              338


Coasting Arc #10 (Orbit 1499)
---------------------------------------

Vector Time (GMT): 2006/306/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4143850
93                 A    =         6713101
63  meter
 Y    =        2732382
84  meter          E    =           
0019480
 Z    =       -4537821
26                 I    =           51
54969
 XDOT =      -5904
591194                 Wp   =          141
96862
 YDOT =      -3869
110453  meter/sec      RA   =          193
14430  deg
 ZDOT =       3054
090557                 TA   =          158
53727
                                          MA   =          158
45548
                                          Ha   =            187
950  n
mi
                                          Hp   =            176
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13595311
45                 X    =        -4152052
42
 Y    =        8964510
63  feet           Y    =         2685997
99  meter
 Z    =      -14887865
04                 Z    =        -4557972
56
 XDOT =     -19372
018354                 XDOT =       -5875
723974
 YDOT =     -12693
931934  feet/sec       YDOT =       -3934
977364  meter/sec
 ZDOT =      10019
982141                 ZDOT =        3025
475654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7126066
74                 X    =        -2172025
14
 Y    =      -14566458
63  feet           Y    =        -4439856
59  meter
 Z    =      -14962651
03                 Z    =        -4560616
03
 XDOT =      14056
688948                 XDOT =        4284
478791
 YDOT =     -17086
285737  feet/sec       YDOT =       -5207
899893  meter/sec
 ZDOT =       9912
693750                 ZDOT =        3021
389055


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   06306
62585225  
00020000  00000-0  20000-3 0  9098
2 25544  51
6319 194
0845 0011971 168
2080 191
9368 15
77529713 15002


Satellite: ISS
Catalog Number: 25544
Epoch time:      06306
62585225   =   yrday
fracday
Element set:     909
Inclination:       51
6319  deg
RA of node:       194
0845  deg
Eccentricity:     
0011971     
Arg of perigee:   168
2080  deg
Mean anomaly:     191
9368  deg
Mean motion:   15
77529713  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1500
Checksum:              302


Coasting Arc #11 (Orbit 1515)
---------------------------------------

Vector Time (GMT): 2006/307/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4412667
63                 A    =         6716397
06  meter
 Y    =        3527718
52  meter          E    =           
0013032
 Z    =       -3628376
76                 I    =           51
58803
 XDOT =      -5740
288182                 Wp   =          147
53092
 YDOT =       2696
170438  meter/sec      RA   =          188
02607  deg
 ZDOT =      -4377
736679                 TA   =           76
07274
                                          MA   =           75
92783
                                          Ha   =            187
843  n
mi
                                          Hp   =            176
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14477255
99                 X    =         4390518
73
 Y    =       11573879
65  feet           Y    =         3576939
50  meter
 Z    =      -11904123
24                 Z    =        -3606993
29
 XDOT =     -18832
966477                 XDOT =       -5748
743639
 YDOT =       8845
703536  feet/sec       YDOT =        2631
931979  meter/sec
 ZDOT =     -14362
653145                 ZDOT =       -4405
644392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13147482
91                 X    =        -4007352
79
 Y    =       13137499
35  feet           Y    =         4004309
80  meter
 Z    =      -11823856
60                 Z    =        -3603911
49
 XDOT =      -5705
652392                 XDOT =       -1739
082849
 YDOT =     -18676
247994  feet/sec       YDOT =       -5692
520389  meter/sec
 ZDOT =     -14466
384263                 ZDOT =       -4409
353923


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   06307
63940193  
00020000  00000-0  20000-3 0  9101
2 25544  51
6311 188
8516 0011936 172
2400 187
8951 15
77555640 15169


Satellite: ISS
Catalog Number: 25544
Epoch time:      06307
63940193   =   yrday
fracday
Element set:     910
Inclination:       51
6311  deg
RA of node:       188
8516  deg
Eccentricity:     
0011936     
Arg of perigee:   172
2400  deg
Mean anomaly:     187
8951  deg
Mean motion:   15
77555640  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1516
Checksum:              292


Coasting Arc #12 (Orbit 1531)
---------------------------------------

Vector Time (GMT): 2006/308/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5702045
61                 A    =         6718120
58  meter
 Y    =       -2015947
29  meter          E    =           
0019439
 Z    =        2895552
48                 I    =           51
62351
 XDOT =       4052
516662                 Wp   =          134
67661
 YDOT =       4201
429000  meter/sec      RA   =          182
80991  deg
 ZDOT =      -5048
112161                 TA   =           11
89893
                                          MA   =           11
85307
                                          Ha   =            187
414  n
mi
                                          Hp   =            176
561

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18707498
73                 X    =         5710097
89
 Y    =       -6614000
28  feet           Y    =        -1952138
84  meter
 Z    =        9499844
11                 Z    =         2923273
49
 XDOT =      13295
658339                 XDOT =        4029
758132
 YDOT =      13784
215879  feet/sec       YDOT =        4246
619265  meter/sec
 ZDOT =     -16562
047773                 ZDOT =       -5028
479645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4788504
81                 X    =         1459536
27
 Y    =       19204569
65  feet           Y    =         5853552
83  meter
 Z    =        9602982
49                 Z    =         2926989
06
 XDOT =     -13608
044924                 XDOT =       -4147
732093
 YDOT =      11649
367611  feet/sec       YDOT =        3550
727248  meter/sec
 ZDOT =     -16488
218265                 ZDOT =       -5025
608927


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   06308
65292776  
00020000  00000-0  20000-3 0  9112
2 25544  51
6314 183
6176 0011811 176
9249 183
1990 15
77630260 15323


Satellite: ISS
Catalog Number: 25544
Epoch time:      06308
65292776   =   yrday
fracday
Element set:     911
Inclination:       51
6314  deg
RA of node:       183
6176  deg
Eccentricity:     
0011811     
Arg of perigee:   176
9249  deg
Mean anomaly:     183
1990  deg
Mean motion:   15
77630260  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1532
Checksum:              297


Coasting Arc #13 (Orbit 1547)
---------------------------------------

Vector Time (GMT): 2006/309/14:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2493923
59                 A    =         6711421
37  meter
 Y    =       -3807907
47  meter          E    =           
0016227
 Z    =        4932276
21                 I    =           51
62707
 XDOT =       7154
965226                 Wp   =          161
26763
 YDOT =      -1949
711666  meter/sec      RA   =          177
68639  deg
 ZDOT =       2095
526451                 TA   =          268
34465
                                          MA   =          268
53053
                                          Ha   =            187
550  n
mi
                                          Hp   =            176
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8182164
02                 X    =        -2475118
62
 Y    =      -12493134
75  feet           Y    =        -3835690
96  meter
 Z    =       16182008
55                 Z    =         4920205
84
 XDOT =      23474
295360                 XDOT =        7166
055356
 YDOT =      -6396
691816  feet/sec       YDOT =       -1869
638950  meter/sec
 ZDOT =       6875
086783                 ZDOT =        2130
313335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13108265
87                 X    =         3995399
44
 Y    =       -7257551
20  feet           Y    =        -2212101
61  meter
 Z    =       16136447
61                 Z    =         4918389
23
 XDOT =       3994
153064                 XDOT =        1217
417854
 YDOT =      22912
550706  feet/sec       YDOT =        6983
745455  meter/sec
 ZDOT =       7004
608663                 ZDOT =        2135
004720


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   06309
66643544  
00020000  00000-0  20000-3 0  9128
2 25544  51
6297 178
3832 0011886 179
9056 180
2113 15
77587604 15489


Satellite: ISS
Catalog Number: 25544
Epoch time:      06309
66643544   =   yrday
fracday
Element set:     912
Inclination:       51
6297  deg
RA of node:       178
3832  deg
Eccentricity:     
0011886     
Arg of perigee:   179
9056  deg
Mean anomaly:     180
2113  deg
Mean motion:   15
77587604  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1548
Checksum:              319

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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