Date: November 13th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 1671)
---------------------------------------

Vector Time (GMT): 2006/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4395936
16                 A    =         6710265
44  meter
 Y    =        1200373
41  meter          E    =           
0009036
 Z    =       -4928670
29                 I    =           51
82888
 XDOT =      -4101
845319                 Wp   =          137
92884
 YDOT =       6150
768567  meter/sec      RA   =          137
03486  deg
 ZDOT =      -2169
314129                 TA   =          111
13366
                                          MA   =          111
03706
                                          Ha   =            185
682  n
mi
                                          Hp   =            178
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14422362
73                 X    =         4406129
57
 Y    =        3938232
97  feet           Y    =         1249588
38  meter
 Z    =      -16170178
11                 Z    =        -4907289
78
 XDOT =     -13457
497767                 XDOT =       -4159
780956
 YDOT =      20179
686900  feet/sec       YDOT =        6104
575601  meter/sec
 ZDOT =      -7117
172339                 ZDOT =       -2189
381628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12079126
50                 X    =        -3681717
76
 Y    =        8954880
30  feet           Y    =         2729447
51  meter
 Z    =      -16090174
27                 Z    =        -4904285
12
 XDOT =      -6881
710600                 XDOT =       -2097
545391
 YDOT =     -22151
581411  feet/sec       YDOT =       -6751
802014  meter/sec
 ZDOT =      -7191
286024                 ZDOT =       -2191
903980


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   06317
51959513  
00020000  00000-0  20000-3 0  9004
2 25544  51
6281 137
8275 0011798 210
6304 149
4173 15
78013028 16720


Satellite: ISS
Catalog Number: 25544
Epoch time:      06317
51959513   =   yrday
fracday
Element set:     900
Inclination:       51
6281  deg
RA of node:       137
8275  deg
Eccentricity:     
0011798     
Arg of perigee:   210
6304  deg
Mean anomaly:     149
4173  deg
Mean motion:   15
78013028  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1672
Checksum:              286


Coasting Arc #2 (Orbit 1687)
---------------------------------------

Vector Time (GMT): 2006/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4110188
54                 A    =         6720398
63  meter
 Y    =       -5269741
00  meter          E    =           
0018124
 Z    =         580443
28                 I    =           51
88421
 XDOT =       4092
278006                 Wp   =          169
04583
 YDOT =       2525
835384  meter/sec      RA   =          131
85996  deg
 ZDOT =      -6033
253167                 TA   =            4
64014
                                          MA   =            4
62336
                                          Ha   =            185
197  n
mi
                                          Hp   =            178
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13484870
52                 X    =         4165990
31
 Y    =      -17289176
52  feet           Y    =        -5223466
61  meter
 Z    =        1904341
48                 Z    =          600546
28
 XDOT =      13426
108943                 XDOT =        4093
038493
 YDOT =       8286
861497  feet/sec       YDOT =        2571
601910  meter/sec
 ZDOT =     -19794
137687                 ZDOT =       -6013
370682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5595746
40                 X    =         1705583
50
 Y    =       21193305
48  feet           Y    =         6459719
51  meter
 Z    =        1978711
51                 Z    =          603111
27
 XDOT =     -13246
798431                 XDOT =       -4037
624162
 YDOT =       5342
562089  feet/sec       YDOT =        1628
412925  meter/sec
 ZDOT =     -19719
546577                 ZDOT =       -6010
517797


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   06318
53282902  
00020000  00000-0  20000-3 0  9019
2 25544  51
6284 132
5913 0011671 216
0547 143
9832 15
78095763 16887


Satellite: ISS
Catalog Number: 25544
Epoch time:      06318
53282902   =   yrday
fracday
Element set:     901
Inclination:       51
6284  deg
RA of node:       132
5913  deg
Eccentricity:     
0011671     
Arg of perigee:   216
0547  deg
Mean anomaly:     143
9832  deg
Mean motion:   15
78095763  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1688
Checksum:              298


Coasting Arc #3 (Orbit 1703)
---------------------------------------

Vector Time (GMT): 2006/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2696825
27                 A    =         6708834
26  meter
 Y    =       -3241229
91  meter          E    =           
0008700
 Z    =        5221049
30                 I    =           51
86203
 XDOT =       5119
089929                 Wp   =          210
49479
 YDOT =      -5689
300094  meter/sec      RA   =          126
70734  deg
 ZDOT =       -895
749825                 TA   =          247
95835
                                          MA   =          248
05078
                                          Ha   =            185
242  n
mi
                                          Hp   =            178
422

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8847851
93                 X    =        -2685744
33
 Y    =      -10633956
40  feet           Y    =        -3271325
46  meter
 Z    =       17129426
83                 Z    =         5207974
73
 XDOT =      16794
914466                 XDOT =        5186
679485
 YDOT =     -18665
682722  feet/sec       YDOT =       -5631
677659  meter/sec
 ZDOT =      -2938
811762                 ZDOT =        -870
716763

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13864238
38                 X    =         4225819
86
 Y    =        -913049
87  feet           Y    =         -278297
60  meter
 Z    =       17080164
23                 Z    =         5206034
06
 XDOT =       5027
227252                 XDOT =        1532
298866
 YDOT =      23587
101932  feet/sec       YDOT =        7189
348669  meter/sec
 ZDOT =      -2846
079061                 ZDOT =        -867
484898


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   06319
54603884  
00020000  00000-0  20000-3 0  9028
2 25544  51
6276 127
3546 0011724 218
3351 141
6982 15
78048275 17045


Satellite: ISS
Catalog Number: 25544
Epoch time:      06319
54603884   =   yrday
fracday
Element set:     902
Inclination:       51
6276  deg
RA of node:       127
3546  deg
Eccentricity:     
0011724     
Arg of perigee:   218
3351  deg
Mean anomaly:     141
6982  deg
Mean motion:   15
78048275  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1704
Checksum:              295


Coasting Arc #4 (Orbit 1719)
---------------------------------------

Vector Time (GMT): 2006/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4636326
85                 A    =         6718508
77  meter
 Y    =        4381476
34  meter          E    =           
0006530
 Z    =        2111380
99                 I    =           51
91177
 XDOT =      -2096
892753                 Wp   =          125
73904
 YDOT =      -4903
749238  meter/sec      RA   =          121
58344  deg
 ZDOT =       5555
959441                 TA   =          257
79112
                                          MA   =          257
86426
                                          Ha   =            184
830  n
mi
                                          Hp   =            178
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15211046
10                 X    =        -4695233
49
 Y    =       14374922
38  feet           Y    =         4329300
95  meter
 Z    =        6927102
99                 Z    =         2088714
22
 XDOT =      -6879
569399                 XDOT =       -2068
892959
 YDOT =     -16088
416134  feet/sec       YDOT =       -4927
041432  meter/sec
 ZDOT =      18228
213388                 ZDOT =        5545
840402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2917292
06                 X    =         -889190
62
 Y    =      -20752384
74  feet           Y    =        -6325326
87  meter
 Z    =        6843026
18                 Z    =         2085754
38
 XDOT =      15650
298167                 XDOT =        4770
210881
 YDOT =       3815
087103  feet/sec       YDOT =        1162
838549  meter/sec
 ZDOT =      18189
769900                 ZDOT =        5544
241866


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   06320
55921538  
00020000  00000-0  20000-3 0  9031
2 25544  51
6278 122
1175 0011773 222
4966 137
5288 15
78146677 17206


Satellite: ISS
Catalog Number: 25544
Epoch time:      06320
55921538   =   yrday
fracday
Element set:     903
Inclination:       51
6278  deg
RA of node:       122
1175  deg
Eccentricity:     
0011773     
Arg of perigee:   222
4966  deg
Mean anomaly:     137
5288  deg
Mean motion:   15
78146677  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1720
Checksum:              299


Coasting Arc #5 (Orbit 1734)
---------------------------------------

Vector Time (GMT): 2006/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1016946
70                 A    =         6712921
46  meter
 Y    =        5209560
17  meter          E    =           
0010769
 Z    =       -4116107
86                 I    =           51
90801
 XDOT =      -5334
752139                 Wp   =          185
91891
 YDOT =       4051
876771  meter/sec      RA   =          116
39003  deg
 ZDOT =       3798
870407                 TA   =          122
94518
                                          MA   =          122
84157
                                          Ha   =            184
549  n
mi
                                          Hp   =            178
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3336439
29                 X    =          978612
93
 Y    =       17091732
84  feet           Y    =         5220718
04  meter
 Z    =      -13504290
88                 Z    =        -4111260
34
 XDOT =     -17502
467649                 XDOT =       -5398
119016
 YDOT =      13293
558959  feet/sec       YDOT =        3991
866180  meter/sec
 ZDOT =      12463
485586                 ZDOT =        3772
799705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16039134
82                 X    =        -4888728
29
 Y    =       -6820003
53  feet           Y    =        -2078737
07  meter
 Z    =      -13485501
00                 Z    =        -4110380
70
 XDOT =      -1568
796012                 XDOT =        -478
169024
 YDOT =     -20837
489357  feet/sec       YDOT =       -6351
266756  meter/sec
 ZDOT =      12366
643173                 ZDOT =        3769
352839


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   06321
50904388  
00020000  00000-0  20000-3 0  9042
2 25544  51
6287 117
2081 0011658 225
8778 134
1429 15
78183643 17357


Satellite: ISS
Catalog Number: 25544
Epoch time:      06321
50904388   =   yrday
fracday
Element set:     904
Inclination:       51
6287  deg
RA of node:       117
2081  deg
Eccentricity:     
0011658     
Arg of perigee:   225
8778  deg
Mean anomaly:     134
1429  deg
Mean motion:   15
78183643  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1735
Checksum:              301


Coasting Arc #6 (Orbit 1750)
---------------------------------------

Vector Time (GMT): 2006/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4552880
88                 A    =         6712204
00  meter
 Y    =       -2438603
72  meter          E    =           
0004436
 Z    =       -4283563
70                 I    =           51
91788
 XDOT =        322
968864                 Wp   =          191
22598
 YDOT =       6834
344674  meter/sec      RA   =          111
29225  deg
 ZDOT =      -3551
121512                 TA   =           42
97054
                                          MA   =           42
93590
                                          Ha   =            184
294  n
mi
                                          Hp   =            178
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14937273
23                 X    =         4600620
70
 Y    =       -8000668
38  feet           Y    =        -2387423
74  meter
 Z    =      -14053686
68                 Z    =        -4261329
31
 XDOT =       1059
609133                 XDOT =         263
773480
 YDOT =      22422
390663  feet/sec       YDOT =        6837
625496  meter/sec
 ZDOT =     -11650
661128                 ZDOT =       -3549
695922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1567273
56                 X    =         -477704
98
 Y    =       16940927
92  feet           Y    =         5163594
83  meter
 Z    =      -13970953
80                 Z    =        -4258346
72
 XDOT =     -18115
398896                 XDOT =       -5521
573583
 YDOT =     -11269
013243  feet/sec       YDOT =       -3434
795236  meter/sec
 ZDOT =     -11644
448756                 ZDOT =       -3549
227981


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   06322
52216522  
00020000  00000-0  20000-3 0  9052
2 25544  51
6290 111
9719 0011527 230
3830 129
6319 15
78238999 17515


Satellite: ISS
Catalog Number: 25544
Epoch time:      06322
52216522   =   yrday
fracday
Element set:     905
Inclination:       51
6290  deg
RA of node:       111
9719  deg
Eccentricity:     
0011527     
Arg of perigee:   230
3830  deg
Mean anomaly:     129
6319  deg
Mean motion:   15
78238999  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1751
Checksum:              289


Coasting Arc #7 (Orbit 1766)
---------------------------------------

Vector Time (GMT): 2006/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         361734
68                 A    =         6718589
05  meter
 Y    =       -6442867
60  meter          E    =           
0012955
 Z    =        1838899
93                 I    =           51
94843
 XDOT =       5026
091110                 Wp   =          164
30050
 YDOT =      -1342
052769  meter/sec      RA   =          106
10199  deg
 ZDOT =      -5693
745252                 TA   =          355
33274
                                          MA   =          355
34480
                                          Ha   =            183
960  n
mi
                                          Hp   =            179
001

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1186793
59                 X    =          424819
52
 Y    =      -21138017
06  feet           Y    =        -6438469
89  meter
 Z    =        6033136
24                 Z    =         1840810
05
 XDOT =      16489
800231                 XDOT =        5068
384622
 YDOT =      -4403
060267  feet/sec       YDOT =       -1285
611337  meter/sec
 ZDOT =     -18680
266574                 ZDOT =       -5669
225105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17239981
30                 X    =         5254746
30
 Y    =       12285402
72  feet           Y    =         3744590
75  meter
 Z    =        6039445
54                 Z    =         1840823
00
 XDOT =      -4263
447055                 XDOT =       -1299
498662
 YDOT =      15116
267270  feet/sec       YDOT =        4607
438264  meter/sec
 ZDOT =     -18588
846258                 ZDOT =       -5665
880339


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   06323
53525744  
00020000  00000-0  20000-3 0  9064
2 25544  51
6286 106
7343 0011602 234
4645 125
5439 15
78265444 17678


Satellite: ISS
Catalog Number: 25544
Epoch time:      06323
53525744   =   yrday
fracday
Element set:     906
Inclination:       51
6286  deg
RA of node:       106
7343  deg
Eccentricity:     
0011602     
Arg of perigee:   234
4645  deg
Mean anomaly:     125
5439  deg
Mean motion:   15
78265444  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1767
Checksum:              294


Coasting Arc #8 (Orbit 1782)
---------------------------------------

Vector Time (GMT): 2006/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4156129
92                 A    =         6707910
95  meter
 Y    =        -242370
11  meter          E    =           
0010073
 Z    =        5266345
17                 I    =           51
92083
 XDOT =       1080
118849                 Wp   =          226
31595
 YDOT =      -7610
314096  meter/sec      RA   =          100
97566  deg
 ZDOT =        495
947193                 TA   =          218
95587
                                          MA   =          219
02848
                                          Ha   =            183
622  n
mi
                                          Hp   =            179
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13635596
85                 X    =        -4178694
54
 Y    =        -795177
52  feet           Y    =         -288972
94  meter
 Z    =       17278035
33                 Z    =         5246099
24
 XDOT =       3543
697012                 XDOT =        1162
728872
 YDOT =     -24968
222100  feet/sec       YDOT =       -7597
773761  meter/sec
 ZDOT =       1627
123338                 ZDOT =         501
394497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7825900
27                 X    =         2385334
40
 Y    =      -11310435
84  feet           Y    =        -3447420
84  meter
 Z    =       17202373
09                 Z    =         5243283
32
 XDOT =      18655
037234                 XDOT =        5686
055349
 YDOT =      15443
181176  feet/sec       YDOT =        4707
081623  meter/sec
 ZDOT =       1646
510540                 ZDOT =         501
856413


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   06324
54832038  
00020000  00000-0  20000-3 0  9074
2 25544  51
6299 101
4973 0011474 238
9927 121
0112 15
78318285 17831


Satellite: ISS
Catalog Number: 25544
Epoch time:      06324
54832038   =   yrday
fracday
Element set:     907
Inclination:       51
6299  deg
RA of node:       101
4973  deg
Eccentricity:     
0011474     
Arg of perigee:   238
9927  deg
Mean anomaly:     121
0112  deg
Mean motion:   15
78318285  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1783
Checksum:              297


Coasting Arc #9 (Orbit 1798)
---------------------------------------

Vector Time (GMT): 2006/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1468797
08                 A    =         6719283
75  meter
 Y    =        6474090
93  meter          E    =           
0002720
 Z    =        1026673
58                 I    =           51
96538
 XDOT =      -4480
346276                 Wp   =           28
12511
 YDOT =      -1961
077997  meter/sec      RA   =           95
83396  deg
 ZDOT =       5952
600281                 TA   =          343
06365
                                          MA   =          343
07273
                                          Ha   =            183
223  n
mi
                                          Hp   =            179
284

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4818888
06                 X    =        -1546069
64
 Y    =       21240455
82  feet           Y    =         6457233
85  meter
 Z    =        3368351
65                 Z    =         1019351
04
 XDOT =     -14699
298807                 XDOT =       -4487
001709
 YDOT =      -6433
982931  feet/sec       YDOT =       -2011
217641  meter/sec
 ZDOT =      19529
528480                 ZDOT =        5930
817738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15877575
76                 X    =        -4839485
09
 Y    =      -14915072
35  feet           Y    =        -4546114
05  meter
 Z    =        3341802
36                 Z    =         1018581
36
 XDOT =      11951
370308                 XDOT =        3642
777670
 YDOT =      -8362
252195  feet/sec       YDOT =       -2548
814469  meter/sec
 ZDOT =      19447
905288                 ZDOT =        5927
721532


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   06325
56135244  
00020000  00000-0  20000-3 0  9083
2 25544  51
6313  96
2604 0011446 242
5492 117
4510 15
78383384 17997


Satellite: ISS
Catalog Number: 25544
Epoch time:      06325
56135244   =   yrday
fracday
Element set:     908
Inclination:       51
6313  deg
RA of node:        96
2604  deg
Eccentricity:     
0011446     
Arg of perigee:   242
5492  deg
Mean anomaly:     117
4510  deg
Mean motion:   15
78383384  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1799
Checksum:              292


Coasting Arc #10 (Orbit 1813)
---------------------------------------

Vector Time (GMT): 2006/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3643279
88                 A    =         6710077
29  meter
 Y    =        3116885
44  meter          E    =           
0008112
 Z    =       -4697853
85                 I    =           51
93654
 XDOT =      -2251
264117                 Wp   =          180
23203
 YDOT =       6825
800063  meter/sec      RA   =           90
65648  deg
 ZDOT =       2774
856500                 TA   =          117
03177
                                          MA   =          116
94895
                                          Ha   =            182
866  n
mi
                                          Hp   =            179
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11953017
97                 X    =         3630977
53
 Y    =       10226002
11  feet           Y    =         3157558
48  meter
 Z    =      -15412906
34                 Z    =        -4680183
82
 XDOT =      -7386
037129                 XDOT =       -2340
903925
 YDOT =      22394
357161  feet/sec       YDOT =        6800
123597  meter/sec
 ZDOT =       9103
859909                 ZDOT =        2763
702787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14818080
52                 X    =        -4516550
94
 Y    =        5469261
28  feet           Y    =         1667030
84  meter
 Z    =      -15346501
58                 Z    =        -4677613
68
 XDOT =     -15462
746549                 XDOT =       -4713
045148
 YDOT =     -16389
798551  feet/sec       YDOT =       -4995
610598  meter/sec
 ZDOT =       9063
027369                 ZDOT =        2762
410742


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   06326
51104455  
00020000  00000-0  20000-3 0  9090
2 25544  51
6316  91
3516 0011413 246
9816 113
0146 15
78414952 18141


Satellite: ISS
Catalog Number: 25544
Epoch time:      06326
51104455   =   yrday
fracday
Element set:     909
Inclination:       51
6316  deg
RA of node:        91
3516  deg
Eccentricity:     
0011413     
Arg of perigee:   246
9816  deg
Mean anomaly:     113
0146  deg
Mean motion:   15
78414952  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1814
Checksum:              273


Coasting Arc #11 (Orbit 1829)
---------------------------------------

Vector Time (GMT): 2006/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2453914
91                 A    =         6713831
51  meter
 Y    =       -5082705
43  meter          E    =           
0005979
 Z    =       -3628918
10                 I    =           51
94924
 XDOT =       3853
298253                 Wp   =          242
56681
 YDOT =       5012
377812  meter/sec      RA   =           85
55560  deg
 ZDOT =      -4411
952057                 TA   =          340
80934
                                          MA   =          340
83185
                                          Ha   =            182
548  n
mi
                                          Hp   =            179
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8050901
93                 X    =         2528197
02
 Y    =      -16675542
75  feet           Y    =        -5054848
53  meter
 Z    =      -11905899
27                 Z    =        -3616817
05
 XDOT =      12642
054636                 XDOT =        3818
395635
 YDOT =      16444
809094  feet/sec       YDOT =        5055
273024  meter/sec
 ZDOT =     -14474
908325                 ZDOT =       -4393
316417

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10805890
72                 X    =         3293635
49
 Y    =       15072605
10  feet           Y    =         4594130
03  meter
 Z    =      -11861302
07                 Z    =        -3615324
87
 XDOT =     -19417
966207                 XDOT =       -5918
596100
 YDOT =       2578
254552  feet/sec       YDOT =         785
851987  meter/sec
 ZDOT =     -14404
660856                 ZDOT =       -4390
540629


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   06327
52402016  
00020000  00000-0  20000-3 0  9108
2 25544  51
6323  86
1142 0011398 251
2520 108
7409 15
78447112 18304


Satellite: ISS
Catalog Number: 25544
Epoch time:      06327
52402016   =   yrday
fracday
Element set:     910
Inclination:       51
6323  deg
RA of node:        86
1142  deg
Eccentricity:     
0011398     
Arg of perigee:   251
2520  deg
Mean anomaly:     108
7409  deg
Mean motion:   15
78447112  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1830
Checksum:              254


Coasting Arc #12 (Orbit 1845)
---------------------------------------

Vector Time (GMT): 2006/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3028587
29                 A    =         6716366
56  meter
 Y    =       -5363200
09  meter          E    =           
0006283
 Z    =        2667775
79                 I    =           51
95500
 XDOT =       3392
060641                 Wp   =          156
21776
 YDOT =      -4521
825836  meter/sec      RA   =           80
35955  deg
 ZDOT =      -5241
069544                 TA   =          353
47178
                                          MA   =          353
47996
                                          Ha   =            182
138  n
mi
                                          Hp   =            179
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9936310
02                 X    =        -2981349
90
 Y    =      -17595800
84  feet           Y    =        -5396803
70  meter
 Z    =        8752545
24                 Z    =         2653176
67
 XDOT =      11128
807876                 XDOT =        3467
832748
 YDOT =     -14835
386601  feet/sec       YDOT =       -4483
469515  meter/sec
 ZDOT =     -17195
110054                 ZDOT =       -5224
407276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20217072
77                 X    =         6162163
78
 Y    =        -758823
47  feet           Y    =         -231289
39  meter
 Z    =        8697336
81                 Z    =         2650948
26
 XDOT =       7943
822709                 XDOT =        2421
277162
 YDOT =      15320
725369  feet/sec       YDOT =        4669
757093  meter/sec
 ZDOT =     -17133
390941                 ZDOT =       -5222
257559


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   06328
53696645  
00020000  00000-0  20000-3 0  9114
2 25544  51
6327  80
8774 0011273 255
3251 104
6665 15
78487173 18465


Satellite: ISS
Catalog Number: 25544
Epoch time:      06328
53696645   =   yrday
fracday
Element set:     911
Inclination:       51
6327  deg
RA of node:        80
8774  deg
Eccentricity:     
0011273     
Arg of perigee:   255
3251  deg
Mean anomaly:     104
6665  deg
Mean motion:   15
78487173  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1846
Checksum:              311

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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