Date: December 9th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2066)
---------------------------------------

Vector Time (GMT): 2006/342/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4549124
41                 A    =         6722329
52  meter
 Y    =        3479313
51  meter          E    =           
0016253
 Z    =        3510364
52                 I    =           51
68160
 XDOT =      -5592
558428                 Wp   =          338
78432
 YDOT =       2777
909699  meter/sec      RA   =            8
43762  deg
 ZDOT =       4515
462712                 TA   =           62
97997
                                          MA   =           62
81414
                                          Ha   =            191
951  n
mi
                                          Hp   =            178
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14924948
86                 X    =         4492827
44
 Y    =       11415070
56  feet           Y    =         3529869
03  meter
 Z    =       11516943
97                 Z    =         3532327
95
 XDOT =     -18348
288805                 XDOT =       -5645
141036
 YDOT =       9113
876965  feet/sec       YDOT =        2715
075906  meter/sec
 ZDOT =      14814
510210                 ZDOT =        4488
166784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16007169
29                 X    =        -4878985
20
 Y    =        9742733
79  feet           Y    =         2969585
26  meter
 Z    =       11599465
59                 Z    =         3535517
11
 XDOT =      -1141
570489                 XDOT =        -347
950685
 YDOT =     -19309
486188  feet/sec       YDOT =       -5885
531390  meter/sec
 ZDOT =      14712
749538                 ZDOT =        4484
446059


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   06342
53518261  
00020000  00000-0  20000-3 0  9005
2 25544  51
6341   8
6043 0023926 311
5507  48
3605 15
75545710 20678


Satellite: ISS
Catalog Number: 25544
Epoch time:      06342
53518261   =   yrday
fracday
Element set:     900
Inclination:       51
6341  deg
RA of node:         8
6043  deg
Eccentricity:     
0023926     
Arg of perigee:   311
5507  deg
Mean anomaly:      48
3605  deg
Mean motion:   15
75545710  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2067
Checksum:              265


Coasting Arc #2 (Orbit 2081)
---------------------------------------

Vector Time (GMT): 2006/343/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5093724
48                 A    =         6722107
71  meter
 Y    =       -2530489
16  meter          E    =           
0020057
 Z    =       -3557737
31                 I    =           51
65417
 XDOT =       5008
221809                 Wp   =          324
21159
 YDOT =       3816
648712  meter/sec      RA   =            3
24024  deg
 ZDOT =       4459
212388                 TA   =          353
24248
                                          MA   =          353
26948
                                          Ha   =            192
222  n
mi
                                          Hp   =            178
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16711694
49                 X    =         5138924
99
 Y    =       -8302129
79  feet           Y    =        -2473275
11  meter
 Z    =      -11672366
50                 Z    =        -3532882
60
 XDOT =      16431
173915                 XDOT =        4943
509296
 YDOT =      12521
813359  feet/sec       YDOT =        3872
291014  meter/sec
 ZDOT =      14629
961903                 ZDOT =        4483
385591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2011972
21                 X    =          613249
13
 Y    =       18609477
19  feet           Y    =         5672168
65  meter
 Z    =      -11579704
57                 Z    =        -3529493
95
 XDOT =     -16032
249656                 XDOT =       -4886
629695
 YDOT =      10886
259982  feet/sec       YDOT =        3318
132042  meter/sec
 ZDOT =      14720
790441                 ZDOT =        4486
896927


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   06343
48656892  
00020000  00000-0  20000-3 0  9014
2 25544  51
6353   3
7067 0023914 315
1747  44
7484 15
75624314 20826


Satellite: ISS
Catalog Number: 25544
Epoch time:      06343
48656892   =   yrday
fracday
Element set:     901
Inclination:       51
6353  deg
RA of node:         3
7067  deg
Eccentricity:     
0023914     
Arg of perigee:   315
1747  deg
Mean anomaly:      44
7484  deg
Mean motion:   15
75624314  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2082
Checksum:              292


Coasting Arc #3 (Orbit 2097)
---------------------------------------

Vector Time (GMT): 2006/344/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4116861
34                 A    =         6719577
73  meter
 Y    =       -3219160
30  meter          E    =           
0022389
 Z    =       -4230441
20                 I    =           51
61768
 XDOT =       6092
630119                 Wp   =          339
41869
 YDOT =      -3041
355373  meter/sec      RA   =          358
14294  deg
 ZDOT =      -3588
389144                 TA   =          253
96497
                                          MA   =          254
21166
                                          Ha   =            192
302  n
mi
                                          Hp   =            178
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13506762
93                 X    =        -4060007
59
 Y    =      -10561549
54  feet           Y    =        -3264878
98  meter
 Z    =      -13879400
28                 Z    =        -4250303
14
 XDOT =      19988
943960                 XDOT =        6143
617871
 YDOT =      -9978
200044  feet/sec       YDOT =       -2972
938716  meter/sec
 ZDOT =     -11772
930261                 ZDOT =       -3558
667695

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14386312
33                 X    =         4384948
00
 Y    =       -9216042
40  feet           Y    =        -2809049
72  meter
 Z    =      -13954042
63                 Z    =        -4253192
19
 XDOT =       2166
319514                 XDOT =         660
294188
 YDOT =      21169
456457  feet/sec       YDOT =        6452
450328  meter/sec
 ZDOT =     -11662
125587                 ZDOT =       -3554
615879


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   06344
50135111  
00020000  00000-0  20000-3 0  9025
2 25544  51
6352 358
4822 0023894 319
1427  40
7945 15
75664939 20982


Satellite: ISS
Catalog Number: 25544
Epoch time:      06344
50135111   =   yrday
fracday
Element set:     902
Inclination:       51
6352  deg
RA of node:       358
4822  deg
Eccentricity:     
0023894     
Arg of perigee:   319
1427  deg
Mean anomaly:      40
7945  deg
Mean motion:   15
75664939  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2098
Checksum:              299


Coasting Arc #4 (Orbit 2113)
---------------------------------------

Vector Time (GMT): 2006/345/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5527865
50                 A    =         6724306
24  meter
 Y    =        2794158
50  meter          E    =           
0016115
 Z    =        2642396
10                 I    =           51
60435
 XDOT =      -4332
288516                 Wp   =          356
35849
 YDOT =      -3627
019196  meter/sec      RA   =          352
94452  deg
 ZDOT =      -5213
710218                 TA   =          153
59715
                                          MA   =          153
51494
                                          Ha   =            192
523  n
mi
                                          Hp   =            178
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18136041
66                 X    =        -5571535
61
 Y    =        9167186
68  feet           Y    =         2732098
42  meter
 Z    =        8669278
54                 Z    =         2615435
92
 XDOT =     -14213
544999                 XDOT =       -4266
081435
 YDOT =     -11899
669278  feet/sec       YDOT =       -3675
094580  meter/sec
 ZDOT =     -17105
348485                 ZDOT =       -5234
596000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3033362
91                 X    =         -924569
01
 Y    =      -20136646
84  feet           Y    =        -6137649
96  meter
 Z    =        8568773
10                 Z    =         2611762
04
 XDOT =      14243
542262                 XDOT =        4341
431682
 YDOT =      -9477
765944  feet/sec       YDOT =       -2888
823060  meter/sec
 ZDOT =     -17183
868371                 ZDOT =       -5237
643079


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   06345
51610149  
00020000  00000-0  20000-3 0  9037
2 25544  51
6340 353
2568 0023902 323
3039  36
6488 15
75725611 21145


Satellite: ISS
Catalog Number: 25544
Epoch time:      06345
51610149   =   yrday
fracday
Element set:     903
Inclination:       51
6340  deg
RA of node:       353
2568  deg
Eccentricity:     
0023902     
Arg of perigee:   323
3039  deg
Mean anomaly:      36
6488  deg
Mean motion:   15
75725611  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2114
Checksum:              274


Coasting Arc #5 (Orbit 2129)
---------------------------------------

Vector Time (GMT): 2006/346/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3417880
24                 A    =         6716975
75  meter
 Y    =        3183678
20  meter          E    =           
0017901
 Z    =        4827102
13                 I    =           51
55148
 XDOT =      -6501
409707                 Wp   =          336
16887
 YDOT =       3357
709456  meter/sec      RA   =          347
83190  deg
 ZDOT =       2408
028295                 TA   =           90
40904
                                          MA   =           90
20391
                                          Ha   =            192
661  n
mi
                                          Hp   =            177
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11213517
86                 X    =         3358576
62
 Y    =       10445138
47  feet           Y    =         3221566
85  meter
 Z    =       15836949
24                 Z    =         4843562
47
 XDOT =     -21330
084342                 XDOT =       -6550
170689
 YDOT =      11016
107138  feet/sec       YDOT =        3284
734241  meter/sec
 ZDOT =       7900
355298                 ZDOT =        2376
326187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13268157
19                 X    =        -4044134
31
 Y    =        7538886
38  feet           Y    =         2297852
57  meter
 Z    =       15898869
73                 Z    =         4845975
49
 XDOT =      -3652
413165                 XDOT =       -1113
255533
 YDOT =     -22707
821577  feet/sec       YDOT =       -6921
344017  meter/sec
 ZDOT =       7782
182342                 ZDOT =        2372
009178


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   06346
53082107  
00020000  00000-0  20000-3 0  9048
2 25544  51
6335 348
0307 0023829 327
2809  32
6878 15
75744135 21307


Satellite: ISS
Catalog Number: 25544
Epoch time:      06346
53082107   =   yrday
fracday
Element set:     904
Inclination:       51
6335  deg
RA of node:       348
0307  deg
Eccentricity:     
0023829     
Arg of perigee:   327
2809  deg
Mean anomaly:      32
6878  deg
Mean motion:   15
75744135  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2130
Checksum:              287


Coasting Arc #6 (Orbit 2144)
---------------------------------------

Vector Time (GMT): 2006/347/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5756718
81                 A    =         6725976
06  meter
 Y    =       -3078741
67  meter          E    =           
0028095
 Z    =       -1538458
45                 I    =           51
55551
 XDOT =       3525
960090                 Wp   =          346
19569
 YDOT =       3706
581072  meter/sec      RA   =          342
64420  deg
 ZDOT =       5781
447670                 TA   =          356
77458
                                          MA   =          356
79266
                                          Ha   =            192
770  n
mi
                                          Hp   =            177
601

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18886872
73                 X    =         5798191
48
 Y    =      -10100858
50  feet           Y    =        -3014134
83  meter
 Z    =       -5047435
84                 Z    =        -1510391
63
 XDOT =      11568
110532                 XDOT =        3456
165103
 YDOT =      12160
699054  feet/sec       YDOT =        3745
619595  meter/sec
 ZDOT =      18968
004168                 ZDOT =        5798
407677

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4416683
74                 X    =         1346205
20
 Y    =       20982832
85  feet           Y    =         6395567
45  meter
 Z    =       -4942827
42                 Z    =        -1506573
80
 XDOT =     -13347
889461                 XDOT =       -4068
436708
 YDOT =       7288
659209  feet/sec       YDOT =        2221
583327  meter/sec
 ZDOT =      19031
853001                 ZDOT =        5800
908795


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   06347
48209037  
00020000  00000-0  20000-3 0  9057
2 25544  51
6341 343
1330 0023702 330
8531  29
1308 15
75835458 21452


Satellite: ISS
Catalog Number: 25544
Epoch time:      06347
48209037   =   yrday
fracday
Element set:     905
Inclination:       51
6341  deg
RA of node:       343
1330  deg
Eccentricity:     
0023702     
Arg of perigee:   330
8531  deg
Mean anomaly:      29
1308  deg
Mean motion:   15
75835458  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2145
Checksum:              271


Coasting Arc #7 (Orbit 2160)
---------------------------------------

Vector Time (GMT): 2006/348/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2697806
14                 A    =         6715228
12  meter
 Y    =       -3337286
81  meter          E    =           
0023910
 Z    =       -5172250
35                 I    =           51
49147
 XDOT =       6670
423784                 Wp   =            9
63127
 YDOT =      -3688
819077  meter/sec      RA   =          337
50970  deg
 ZDOT =      -1076
623139                 TA   =          249
94441
                                          MA   =          250
20195
                                          Ha   =            192
958  n
mi
                                          Hp   =            177
326

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8851070
01                 X    =        -2635161
50
 Y    =      -10949103
70  feet           Y    =        -3367104
45  meter
 Z    =      -16969325
28                 Z    =        -5185204
56
 XDOT =      21884
592466                 XDOT =        6716
407010
 YDOT =     -12102
424794  feet/sec       YDOT =       -3613
969492  meter/sec
 ZDOT =      -3532
228147                 ZDOT =       -1044
106509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12864962
14                 X    =         3921240
46
 Y    =       -5572934
47  feet           Y    =        -1698630
43  meter
 Z    =      -17018150
99                 Z    =        -5187132
42
 XDOT =       5516
528518                 XDOT =        1681
437892
 YDOT =      23375
747801  feet/sec       YDOT =        7124
927930  meter/sec
 ZDOT =      -3411
049329                 ZDOT =       -1039
687835


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   06348
49674690  
00020000  00000-0  20000-3 0  9061
2 25544  51
6329 337
9071 0023802 334
7246  25
2751 15
75841198 21613


Satellite: ISS
Catalog Number: 25544
Epoch time:      06348
49674690   =   yrday
fracday
Element set:     906
Inclination:       51
6329  deg
RA of node:       337
9071  deg
Eccentricity:     
0023802     
Arg of perigee:   334
7246  deg
Mean anomaly:      25
2751  deg
Mean motion:   15
75841198  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2161
Checksum:              306


Coasting Arc #8 (Orbit 2176)
---------------------------------------

Vector Time (GMT): 2006/349/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5849891
41                 A    =         6726685
22  meter
 Y    =        3326631
60  meter          E    =           
0013701
 Z    =         289764
85                 I    =           51
50443
 XDOT =      -2593
383003                 Wp   =            2
91557
 YDOT =      -4034
941730  meter/sec      RA   =          332
33706  deg
 ZDOT =      -6007
411101                 TA   =          173
93361
                                          MA   =          173
91700
                                          Ha   =            193
153  n
mi
                                          Hp   =            177
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19192557
11                 X    =        -5888063
13
 Y    =       10914145
67  feet           Y    =         3261001
41  meter
 Z    =         950672
06                 Z    =          261253
31
 XDOT =      -8508
474419                 XDOT =       -2518
887665
 YDOT =     -13237
997802  feet/sec       YDOT =       -4063
525242  meter/sec
 ZDOT =     -19709
354006                 ZDOT =       -6019
829387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5854495
28                 X    =        -1784450
16
 Y    =      -21292919
64  feet           Y    =        -6490081
91  meter
 Z    =         844428
48                 Z    =          257381
80
 XDOT =      13344
953122                 XDOT =        4067
541712
 YDOT =      -4456
482383  feet/sec       YDOT =       -1358
335830  meter/sec
 ZDOT =     -19756
254170                 ZDOT =       -6021
706271


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   06349
51137041  
00020000  00000-0  20000-3 0  9070
2 25544  51
6323 332
6805 0023873 338
8837  21
1340 15
75916548 21771


Satellite: ISS
Catalog Number: 25544
Epoch time:      06349
51137041   =   yrday
fracday
Element set:     907
Inclination:       51
6323  deg
RA of node:       332
6805  deg
Eccentricity:     
0023873     
Arg of perigee:   338
8837  deg
Mean anomaly:      21
1340  deg
Mean motion:   15
75916548  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2177
Checksum:              293


Coasting Arc #9 (Orbit 2192)
---------------------------------------

Vector Time (GMT): 2006/350/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1841491
11                 A    =         6714646
79  meter
 Y    =        3782275
66  meter          E    =           
0024135
 Z    =        5239166
73                 I    =           51
43881
 XDOT =      -6641
805190                 Wp   =          348
41271
 YDOT =       3870
503650  meter/sec      RA   =          327
17254  deg
 ZDOT =       -436
769815                 TA   =          105
88054
                                          MA   =          105
61439
                                          Ha   =            193
261  n
mi
                                          Hp   =            176
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6041637
51                 X    =         1773609
01
 Y    =       12409040
88  feet           Y    =         3802488
05  meter
 Z    =       17188867
22                 Z    =         5247948
40
 XDOT =     -21790
699441                 XDOT =       -6682
470290
 YDOT =      12698
502790  feet/sec       YDOT =        3796
003979  meter/sec
 ZDOT =      -1432
971833                 ZDOT =        -469
134500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13442012
68                 X    =        -4097125
47
 Y    =        2941614
97  feet           Y    =          896604
24  meter
 Z    =       17222137
85                 Z    =         5249307
62
 XDOT =      -7149
299426                 XDOT =       -2179
106465
 YDOT =     -23134
119949  feet/sec       YDOT =       -7051
279760  meter/sec
 ZDOT =      -1553
566099                 ZDOT =        -473
526947


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   06350
52596121  
00020000  00000-0  20000-3 0  9082
2 25544  51
6317 327
4535 0023824 342
4901  17
5439 15
75945097 21932


Satellite: ISS
Catalog Number: 25544
Epoch time:      06350
52596121   =   yrday
fracday
Element set:     908
Inclination:       51
6317  deg
RA of node:       327
4535  deg
Eccentricity:     
0023824     
Arg of perigee:   342
4901  deg
Mean anomaly:      17
5439  deg
Mean motion:   15
75945097  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2193
Checksum:              296


Coasting Arc #10 (Orbit 2208)
---------------------------------------

Vector Time (GMT): 2006/351/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5689849
70                 A    =         6725881
80  meter
 Y    =       -3391605
75  meter          E    =           
0031072
 Z    =        1038967
75                 I    =           51
45450
 XDOT =       1696
674283                 Wp   =           10
55756
 YDOT =       4659
174614  meter/sec      RA   =          322
02284  deg
 ZDOT =       5920
006679                 TA   =             
86965
                                          MA   =             
86426
                                          Ha   =            193
167  n
mi
                                          Hp   =            176
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18667485
90                 X    =         5722305
04
 Y    =      -11127315
46  feet           Y    =        -3327797
37  meter
 Z    =        3408686
83                 Z    =         1066687
80
 XDOT =       5566
516678                 XDOT =        1615
689892
 YDOT =      15286
005951  feet/sec       YDOT =        4677
694111  meter/sec
 ZDOT =      19422
594090                 ZDOT =        5928
053201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6908532
98                 X    =         2105720
85
 Y    =       20587606
90  feet           Y    =         6275102
58  meter
 Z    =        3511970
84                 Z    =         1070448
71
 XDOT =     -14595
709973                 XDOT =       -4448
772400
 YDOT =       1580
660915  feet/sec       YDOT =         481
785447  meter/sec
 ZDOT =      19453
213926                 ZDOT =        5929
339605


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   06351
54051671  
00020000  00000-0  20000-3 0  9092
2 25544  51
6318 322
2275 0023592 346
3458  13
7065 15
76046863 22094


Satellite: ISS
Catalog Number: 25544
Epoch time:      06351
54051671   =   yrday
fracday
Element set:     909
Inclination:       51
6318  deg
RA of node:       322
2275  deg
Eccentricity:     
0023592     
Arg of perigee:   346
3458  deg
Mean anomaly:      13
7065  deg
Mean motion:   15
76046863  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2209
Checksum:              288


Coasting Arc #11 (Orbit 2223)
---------------------------------------

Vector Time (GMT): 2006/352/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1143358
00                 A    =         6715586
48  meter
 Y    =       -4369277
12  meter          E    =           
0021851
 Z    =       -4971349
44                 I    =           51
39797
 XDOT =       6378
932671                 Wp   =           22
64329
 YDOT =      -3855
671075  meter/sec      RA   =          316
82965  deg
 ZDOT =       1944
320835                 TA   =          266
07503
                                          MA   =          266
32487
                                          Ha   =            193
475  n
mi
                                          Hp   =            176
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3751174
54                 X    =        -1070264
93
 Y    =      -14334898
67  feet           Y    =        -4381653
27  meter
 Z    =      -16310201
56                 Z    =        -4976727
12
 XDOT =      20928
256794                 XDOT =        6412
127951
 YDOT =     -12649
839485  feet/sec       YDOT =       -3784
153025  meter/sec
 ZDOT =       6379
005364                 ZDOT =        1975
390083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14774083
59                 X    =         4503140
68
 Y    =        -783899
95  feet           Y    =         -238932
71  meter
 Z    =      -16330807
10                 Z    =        -4977630
00
 XDOT =       8258
246815                 XDOT =        2517
113629
 YDOT =      21887
282004  feet/sec       YDOT =        6671
243555  meter/sec
 ZDOT =       6494
769602                 ZDOT =        1979
605775


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   06352
49163552  
00020000  00000-0  20000-3 0  9101
2 25544  51
6318 317
3273 0023781 350
1043   9
9650 15
76031449 22248


Satellite: ISS
Catalog Number: 25544
Epoch time:      06352
49163552   =   yrday
fracday
Element set:     910
Inclination:       51
6318  deg
RA of node:       317
3273  deg
Eccentricity:     
0023781     
Arg of perigee:   350
1043  deg
Mean anomaly:       9
9650  deg
Mean motion:   15
76031449  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2224
Checksum:              271


Coasting Arc #12 (Orbit 2239)
---------------------------------------

Vector Time (GMT): 2006/353/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5412288
44                 A    =         6723659
09  meter
 Y    =        3239821
23  meter          E    =           
0019902
 Z    =       -2363186
81                 I    =           51
40688
 XDOT =       -899
255252                 Wp   =            4
19121
 YDOT =      -5428
282151  meter/sec      RA   =          311
69763  deg
 ZDOT =      -5365
707449                 TA   =          202
47948
                                          MA   =          202
56680
                                          Ha   =            193
586  n
mi
                                          Hp   =            175
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17756851
84                 X    =        -5436634
29
 Y    =       10629334
74  feet           Y    =         3179162
32  meter
 Z    =       -7753237
58                 Z    =        -2389538
49
 XDOT =      -2950
312507                 XDOT =        -812
422745
 YDOT =     -17809
324642  feet/sec       YDOT =       -5437
851639  meter/sec
 ZDOT =     -17604
027065                 ZDOT =       -5369
866142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7289850
29                 X    =        -2221946
37
 Y    =      -19329104
73  feet           Y    =        -5891511
12  meter
 Z    =       -7851434
93                 Z    =        -2393117
37
 XDOT =      16622
795137                 XDOT =        5066
627958
 YDOT =        910
074243  feet/sec       YDOT =         277
390629  meter/sec
 ZDOT =     -17620
193352                 ZDOT =       -5370
634934


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   06353
50612743  
00020000  00000-0  20000-3 0  9116
2 25544  51
6323 312
0998 0023826 354
1046   5
9834 15
76119372 22407


Satellite: ISS
Catalog Number: 25544
Epoch time:      06353
50612743   =   yrday
fracday
Element set:     911
Inclination:       51
6323  deg
RA of node:       312
0998  deg
Eccentricity:     
0023826     
Arg of perigee:   354
1046  deg
Mean anomaly:       5
9834  deg
Mean motion:   15
76119372  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2240
Checksum:              275

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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