Date: December 21st 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 2256)
---------------------------------------

Vector Time (GMT): 2006/354/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5006459
25                 A    =         6717589
39  meter
 Y    =        -927253
85  meter          E    =           
0021845
 Z    =        4363984
41                 I    =           51
37013
 XDOT =      -1647
388843                 Wp   =           19
28500
 YDOT =       6757
619195  meter/sec      RA   =          306
27608  deg
 ZDOT =       3341
378978                 TA   =           37
12773
                                          MA   =           36
97683
                                          Ha   =            193
560  n
mi
                                          Hp   =            175
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16425391
25                 X    =         4995256
34
 Y    =       -3042171
44  feet           Y    =         -871332
32  meter
 Z    =       14317534
16                 Z    =         4388278
48
 XDOT =      -5404
819040                 XDOT =       -1739
062915
 YDOT =      22170
666650  feet/sec       YDOT =        6738
683965  meter/sec
 ZDOT =      10962
529457                 ZDOT =        3333
154551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5625593
68                 X    =         1714680
95
 Y    =       15645879
36  feet           Y    =         4768864
03  meter
 Z    =       14408303
99                 Z    =         4391651
06
 XDOT =     -21619
397116                 XDOT =       -6589
592241
 YDOT =      -2247
498620  feet/sec       YDOT =        -685
037579  meter/sec
 ZDOT =      10932
528221                 ZDOT =        3332
234602


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   06354
58402864  
00020000  00000-0  20000-3 0  9004
2 25544  51
6347 306
5574 0023937 356
8370   3
2639 15
76160267 22574


Satellite: ISS
Catalog Number: 25544
Epoch time:      06354
58402864   =   yrday
fracday
Element set:     900
Inclination:       51
6347  deg
RA of node:       306
5574  deg
Eccentricity:     
0023937     
Arg of perigee:   356
8370  deg
Mean anomaly:       3
2639  deg
Mean motion:   15
76160267  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2257
Checksum:              300


Coasting Arc #2 (Orbit 2271)
---------------------------------------

Vector Time (GMT): 2006/355/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1543547
52                 A    =         6723760
37  meter
 Y    =       -6112256
55  meter          E    =           
0028628
 Z    =       -2291967
21                 I    =           51
37467
 XDOT =       5449
894436                 Wp   =            8
44146
 YDOT =       -644
865006  meter/sec      RA   =          301
06027  deg
 ZDOT =       5426
445900                 TA   =          325
62307
                                          MA   =          325
80797
                                          Ha   =            193
864  n
mi
                                          Hp   =            175
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5064132
28                 X    =         1622914
84
 Y    =      -20053335
13  feet           Y    =        -6094551
55  meter
 Z    =       -7519577
46                 Z    =        -2284277
04
 XDOT =      17880
231089                 XDOT =        5430
339746
 YDOT =      -2115
698839  feet/sec       YDOT =        -584
031615  meter/sec
 ZDOT =      17803
300196                 ZDOT =        5452
873798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20640997
63                 X    =         6291376
08
 Y    =        1467080
38  feet           Y    =          447166
10  meter
 Z    =       -7491503
36                 Z    =        -2283410
22
 XDOT =       5343
784883                 XDOT =        1628
785632
 YDOT =      15618
716264  feet/sec       YDOT =        4760
584717  meter/sec
 ZDOT =      17902
092336                 ZDOT =        5456
557744


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   06355
53507177  
00020000  00000-0  20000-3 0  9014
2 25544  51
6344 301
6574 0024082    
5129 359
6055 15
76158445 22726


Satellite: ISS
Catalog Number: 25544
Epoch time:      06355
53507177   =   yrday
fracday
Element set:     901
Inclination:       51
6344  deg
RA of node:       301
6574  deg
Eccentricity:     
0024082     
Arg of perigee:      
5129  deg
Mean anomaly:     359
6055  deg
Mean motion:   15
76158445  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2272
Checksum:              282


Coasting Arc #3 (Orbit 2287)
---------------------------------------

Vector Time (GMT): 2006/356/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4498633
66                 A    =         6714835
89  meter
 Y    =          94741
89  meter          E    =           
0030847
 Z    =       -5004335
35                 I    =           51
33246
 XDOT =       1894
552814                 Wp   =           28
58107
 YDOT =      -7225
205666  meter/sec      RA   =          295
92297  deg
 ZDOT =      -1817
822244                 TA   =          223
66741
                                          MA   =          223
91189
                                          Ha   =            193
854  n
mi
                                          Hp   =            174
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14759296
79                 X    =        -4475048
77
 Y    =         310832
97  feet           Y    =           44568
41  meter
 Z    =      -16418423
05                 Z    =        -5026132
23
 XDOT =       6215
724456                 XDOT =        1984
035853
 YDOT =     -23704
742998  feet/sec       YDOT =       -7203
519084  meter/sec
 ZDOT =      -5963
983741                 ZDOT =       -1808
402481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3155176
73                 X    =         -961697
87
 Y    =      -14328092
56  feet           Y    =        -4367202
61  meter
 Z    =      -16499960
54                 Z    =        -5029187
97
 XDOT =      23422
267142                 XDOT =        7139
107025
 YDOT =       1753
549511  feet/sec       YDOT =         534
481891  meter/sec
 ZDOT =      -5929
570693                 ZDOT =       -1807
333147


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   06356
54948402  
00020000  00000-0  20000-3 0  9027
2 25544  51
6351 296
4302 0023972   4
5997 355
5383 15
76240365 22887


Satellite: ISS
Catalog Number: 25544
Epoch time:      06356
54948402   =   yrday
fracday
Element set:     902
Inclination:       51
6351  deg
RA of node:       296
4302  deg
Eccentricity:     
0023972     
Arg of perigee:     4
5997  deg
Mean anomaly:     355
5383  deg
Mean motion:   15
76240365  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2288
Checksum:              306


Coasting Arc #4 (Orbit 2303)
---------------------------------------

Vector Time (GMT): 2006/357/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1743334
68                 A    =         6725396
73  meter
 Y    =        6453189
19  meter          E    =           
0021201
 Z    =         817034
37                 I    =           51
35741
 XDOT =      -4861
848569                 Wp   =           42
47721
 YDOT =       -549
243351  meter/sec      RA   =          290
72564  deg
 ZDOT =      -5930
642703                 TA   =          128
58661
                                          MA   =          128
39651
                                          Ha   =            193
946  n
mi
                                          Hp   =            174
643

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5719601
98                 X    =        -1819334
55
 Y    =       21171880
54  feet           Y    =         6433269
19  meter
 Z    =        2680558
95                 Z    =          808381
72
 XDOT =     -15950
946749                 XDOT =       -4826
535853
 YDOT =      -1801
979499  feet/sec       YDOT =        -603
412906  meter/sec
 ZDOT =     -19457
489184                 ZDOT =       -5954
175608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21905338
21                 X    =        -6676747
09
 Y    =       -1134493
03  feet           Y    =         -345793
48  meter
 Z    =        2648934
17                 Z    =          807395
13
 XDOT =      -1666
809856                 XDOT =        -508
043644
 YDOT =     -14268
758774  feet/sec       YDOT =       -4349
117674  meter/sec
 ZDOT =     -19545
603091                 ZDOT =       -5957
499822


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   06357
56386272  
00020000  00000-0  20000-3 0  9032
2 25544  51
6352 291
2027 0023903   8
4598 351
6964 15
76281935 23048


Satellite: ISS
Catalog Number: 25544
Epoch time:      06357
56386272   =   yrday
fracday
Element set:     903
Inclination:       51
6352  deg
RA of node:       291
2027  deg
Eccentricity:     
0023903     
Arg of perigee:     8
4598  deg
Mean anomaly:     351
6964  deg
Mean motion:   15
76281935  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2304
Checksum:              302


Coasting Arc #5 (Orbit 2319)
---------------------------------------

Vector Time (GMT): 2006/358/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4048310
14                 A    =         6713334
98  meter
 Y    =        1094663
17  meter          E    =           
0024362
 Z    =        5235990
41                 I    =           51
30825
 XDOT =      -2035
812105                 Wp   =           17
14335
 YDOT =       7437
434166  meter/sec      RA   =          285
55867  deg
 ZDOT =         42
069219                 TA   =           72
58925
                                          MA   =           72
32302
                                          Ha   =            193
800  n
mi
                                          Hp   =            174
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13281857
43                 X    =         4010333
41
 Y    =        3591414
59  feet           Y    =         1139720
64  meter
 Z    =       17178446
23                 Z    =         5255564
75
 XDOT =      -6679
173572                 XDOT =       -2119
031597
 YDOT =      24401
030727  feet/sec       YDOT =        7414
203275  meter/sec
 ZDOT =        138
022372                 ZDOT =          31
978141

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -491074
01                 X    =         -149679
36
 Y    =       13657914
02  feet           Y    =         4162932
19  meter
 Z    =       17251818
49                 Z    =         5258354
28
 XDOT =     -24285
327334                 XDOT =       -7402
167771
 YDOT =       -906
239248  feet/sec       YDOT =        -276
221723  meter/sec
 ZDOT =        101
139555                 ZDOT =          30
827336


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   06358
57820632  
00020000  00000-0  20000-3 0  9048
2 25544  51
6348 285
9752 0023812  11
9522 348
2202 15
76373911 23204


Satellite: ISS
Catalog Number: 25544
Epoch time:      06358
57820632   =   yrday
fracday
Element set:     904
Inclination:       51
6348  deg
RA of node:       285
9752  deg
Eccentricity:     
0023812     
Arg of perigee:    11
9522  deg
Mean anomaly:     348
2202  deg
Mean motion:   15
76373911  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2320
Checksum:              284


Coasting Arc #6 (Orbit 2335)
---------------------------------------

Vector Time (GMT): 2006/359/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1776788
39                 A    =         6725236
76  meter
 Y    =       -6420890
92  meter          E    =           
0035601
 Z    =         737202
57                 I    =           51
34181
 XDOT =       4499
968774                 Wp   =           28
98020
 YDOT =       1940
934942  meter/sec      RA   =          280
38944  deg
 ZDOT =       5970
613701                 TA   =          339
11650
                                          MA   =          339
26156
                                          Ha   =            194
003  n
mi
                                          Hp   =            174
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5829358
22                 X    =         1844874
48
 Y    =      -21065915
08  feet           Y    =        -6400641
26  meter
 Z    =        2418643
60                 Z    =          745998
87
 XDOT =      14763
677079                 XDOT =        4448
926665
 YDOT =       6367
896790  feet/sec       YDOT =        1990
970124  meter/sec
 ZDOT =      19588
627627                 ZDOT =        5992
350529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21848619
27                 X    =         6659459
15
 Y    =         485264
65  feet           Y    =          147908
66  meter
 Z    =        2450793
05                 Z    =          747001
72
 XDOT =      -2553
512404                 XDOT =        -778
310581
 YDOT =      14174
193621  feet/sec       YDOT =        4320
294216  meter/sec
 ZDOT =      19670
197533                 ZDOT =        5995
476208


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   06359
59252061  
00020000  00000-0  20000-3 0  9057
2 25544  51
6347 280
7473 0023893  16
1128 344
0791 15
76366188 23366


Satellite: ISS
Catalog Number: 25544
Epoch time:      06359
59252061   =   yrday
fracday
Element set:     905
Inclination:       51
6347  deg
RA of node:       280
7473  deg
Eccentricity:     
0023893     
Arg of perigee:    16
1128  deg
Mean anomaly:     344
0791  deg
Mean motion:   15
76366188  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2336
Checksum:              305


Coasting Arc #7 (Orbit 2350)
---------------------------------------

Vector Time (GMT): 2006/360/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3829280
13                 A    =         6714191
08  meter
 Y    =       -2309682
66  meter          E    =           
0028585
 Z    =       -5021261
06                 I    =           51
30182
 XDOT =       2068
811223                 Wp   =           47
48785
 YDOT =      -7198
697566  meter/sec      RA   =          275
19043  deg
 ZDOT =       1758
945182                 TA   =          239
40444
                                          MA   =          239
68670
                                          Ha   =            193
965  n
mi
                                          Hp   =            173
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12563255
03                 X    =        -3778776
12
 Y    =       -7577699
02  feet           Y    =        -2352221
02  meter
 Z    =      -16473953
62                 Z    =        -5039741
10
 XDOT =       6787
438397                 XDOT =        2140
609735
 YDOT =     -23617
774166  feet/sec       YDOT =       -7175
161663  meter/sec
 ZDOT =       5770
817527                 ZDOT =        1769
169226

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4055525
24                 X    =         1236124
09
 Y    =      -14018457
64  feet           Y    =        -4272825
89  meter
 Z    =      -16543385
62                 Z    =        -5042423
94
 XDOT =      23540
199322                 XDOT =        7175
052753
 YDOT =         53
682500  feet/sec       YDOT =          16
362426  meter/sec
 ZDOT =       5808
209071                 ZDOT =        1770
342125


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   06360
54340720  
00020000  00000-0  20000-3 0  9065
2 25544  51
6351 275
8459 0023768  19
6802 340
5274 15
76434177 23516


Satellite: ISS
Catalog Number: 25544
Epoch time:      06360
54340720   =   yrday
fracday
Element set:     906
Inclination:       51
6351  deg
RA of node:       275
8459  deg
Eccentricity:     
0023768     
Arg of perigee:    19
6802  deg
Mean anomaly:     340
5274  deg
Mean motion:   15
76434177  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2351
Checksum:              293


Coasting Arc #8 (Orbit 2366)
---------------------------------------

Vector Time (GMT): 2006/361/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1875747
33                 A    =         6722738
40  meter
 Y    =        6034049
62  meter          E    =           
0022203
 Z    =       -2337591
10                 I    =           51
32999
 XDOT =      -4298
796738                 Wp   =           37
23007
 YDOT =      -3415
033630  meter/sec      RA   =          270
04739  deg
 ZDOT =      -5375
063256                 TA   =          169
15399
                                          MA   =          169
10603
                                          Ha   =            194
027  n
mi
                                          Hp   =            173
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6154026
66                 X    =        -1931725
94
 Y    =       19796750
73  feet           Y    =         6012761
16  meter
 Z    =       -7669262
14                 Z    =        -2346838
98
 XDOT =     -14103
663838                 XDOT =       -4234
178817
 YDOT =     -11204
178576  feet/sec       YDOT =       -3462
743459  meter/sec
 ZDOT =     -17634
721969                 ZDOT =       -5395
790079

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20715350
39                 X    =        -6314038
80
 Y    =        -369998
75  feet           Y    =         -112775
62  meter
 Z    =       -7703137
30                 Z    =        -2347916
25
 XDOT =       6844
250062                 XDOT =        2086
127419
 YDOT =     -15056
755225  feet/sec       YDOT =       -4589
298992  meter/sec
 ZDOT =     -17712
699465                 ZDOT =       -5398
830797


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   06361
55765575  
00020000  00000-0  20000-3 0  9077
2 25544  51
6353 270
6168 0023635  23
4708 336
7530 15
76474640 23677


Satellite: ISS
Catalog Number: 25544
Epoch time:      06361
55765575   =   yrday
fracday
Element set:     907
Inclination:       51
6353  deg
RA of node:       270
6168  deg
Eccentricity:     
0023635     
Arg of perigee:    23
4708  deg
Mean anomaly:     336
7530  deg
Mean motion:   15
76474640  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2367
Checksum:              306


Coasting Arc #9 (Orbit 2382)
---------------------------------------

Vector Time (GMT): 2006/362/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3739539
54                 A    =         6716995
28  meter
 Y    =        3621084
11  meter          E    =           
0031478
 Z    =        4242710
04                 I    =           51
31224
 XDOT =      -2240
721890                 Wp   =           40
02985
 YDOT =       6479
318085  meter/sec      RA   =          264
82328  deg
 ZDOT =      -3516
728405                 TA   =           85
93319
                                          MA   =           85
57345
                                          Ha   =            193
986  n
mi
                                          Hp   =            173
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12268830
52                 X    =         3678159
77
 Y    =       11880197
23  feet           Y    =         3662558
16  meter
 Z    =       13919652
35                 Z    =         4260728
00
 XDOT =      -7351
449771                 XDOT =       -2295
924328
 YDOT =      21257
605267  feet/sec       YDOT =        6453
952745  meter/sec
 ZDOT =     -11537
822851                 ZDOT =       -3527
747378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7765330
62                 X    =        -2366872
77
 Y    =       15148230
89  feet           Y    =         4617180
77  meter
 Z    =       13987521
27                 Z    =         4263396
48
 XDOT =     -21356
319083                 XDOT =       -6509
406056
 YDOT =       -141
217724  feet/sec       YDOT =         -43
043162  meter/sec
 ZDOT =     -11578
270923                 ZDOT =       -3529
056977


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   06362
57187180  
00020000  00000-0  20000-3 0  9081
2 25544  51
6349 265
3878 0023718  27
2491 332
9912 15
76555105 23830


Satellite: ISS
Catalog Number: 25544
Epoch time:      06362
57187180   =   yrday
fracday
Element set:     908
Inclination:       51
6349  deg
RA of node:       265
3878  deg
Eccentricity:     
0023718     
Arg of perigee:    27
2491  deg
Mean anomaly:     332
9912  deg
Mean motion:   15
76555105  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2383
Checksum:              313


Coasting Arc #10 (Orbit 2398)
---------------------------------------

Vector Time (GMT): 2006/363/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2070962
67                 A    =         6718823
34  meter
 Y    =       -5183078
07  meter          E    =           
0030471
 Z    =        3703572
59                 I    =           51
32294
 XDOT =       4331
448219                 Wp   =           51
55696
 YDOT =       4775
624894  meter/sec      RA   =          259
69573  deg
 ZDOT =       4256
556011                 TA   =          353
53371
                                          MA   =          353
57294
                                          Ha   =            194
016  n
mi
                                          Hp   =            172
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6794496
94                 X    =         2110775
28
 Y    =      -17004849
31  feet           Y    =        -5159697
22  meter
 Z    =       12150828
69                 Z    =         3713729
50
 XDOT =      14210
788120                 XDOT =        4257
046899
 YDOT =      15668
060675  feet/sec       YDOT =        4823
645082  meter/sec
 ZDOT =      13965
078777                 ZDOT =        4277
418111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18253447
92                 X    =         5563650
93
 Y    =        1109905
84  feet           Y    =          338299
30  meter
 Z    =       12188210
49                 Z    =         3714966
56
 XDOT =     -10419
669366                 XDOT =       -3175
915223
 YDOT =      16971
091488  feet/sec       YDOT =        5172
788686  meter/sec
 ZDOT =      14043
735480                 ZDOT =        4280
530574


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   06363
58605743  
00020000  00000-0  20000-3 0  9094
2 25544  51
6354 260
1587 0023676  31
2214 329
0351 15
76570307 23999


Satellite: ISS
Catalog Number: 25544
Epoch time:      06363
58605743   =   yrday
fracday
Element set:     909
Inclination:       51
6354  deg
RA of node:       260
1587  deg
Eccentricity:     
0023676     
Arg of perigee:    31
2214  deg
Mean anomaly:     329
0351  deg
Mean motion:   15
76570307  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2399
Checksum:              295


Coasting Arc #11 (Orbit 2413)
---------------------------------------

Vector Time (GMT): 2006/364/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3814319
05                 A    =         6720588
70  meter
 Y    =       -4610347
17  meter          E    =           
0027191
 Z    =       -3050007
69                 I    =           51
33607
 XDOT =       2584
736106                 Wp   =           40
58026
 YDOT =      -5353
213174  meter/sec      RA   =          254
46679  deg
 ZDOT =       4904
156162                 TA   =          283
85638
                                          MA   =          284
15876
                                          Ha   =            193
968  n
mi
                                          Hp   =            172
679

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12514170
11                 X    =        -3747665
55
 Y    =      -15125810
93  feet           Y    =        -4652627
90  meter
 Z    =      -10006586
91                 Z    =        -3068376
49
 XDOT =       8480
105334                 XDOT =        2620
580763
 YDOT =     -17563
035349  feet/sec       YDOT =       -5324
109488  meter/sec
 ZDOT =      16089
751187                 ZDOT =        4916
799194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10219506
68                 X    =         3114905
64
 Y    =      -16720178
89  feet           Y    =        -5096310
53  meter
 Z    =      -10075896
61                 Z    =        -3071133
29
 XDOT =      18122
208753                 XDOT =        5523
649228
 YDOT =       1440
232472  feet/sec       YDOT =         438
982858  meter/sec
 ZDOT =      16136
421145                 ZDOT =        4918
381165


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   06364
53682648  
00020000  00000-0  20000-3 0  9101
2 25544  51
6355 255
2567 0023570  34
3380 325
9302 15
76624256 24146


Satellite: ISS
Catalog Number: 25544
Epoch time:      06364
53682648   =   yrday
fracday
Element set:     910
Inclination:       51
6355  deg
RA of node:       255
2567  deg
Eccentricity:     
0023570     
Arg of perigee:    34
3380  deg
Mean anomaly:     325
9302  deg
Mean motion:   15
76624256  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2414
Checksum:              289


Coasting Arc #12 (Orbit 2429)
---------------------------------------

Vector Time (GMT): 2006/365/12:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 473517
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2531290
33                 A    =         6714733
31  meter
 Y    =        4054792
21  meter          E    =           
0033667
 Z    =       -4746768
79                 I    =           51
32519
 XDOT =      -4377
025983                 Wp   =           48
99041
 YDOT =      -5760
296195  meter/sec      RA   =          249
33347  deg
 ZDOT =      -2576
608563                 TA   =          195
50620
                                          MA   =          195
60959
                                          Ha   =            193
992  n
mi
                                          Hp   =            172
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8304758
32                 X    =        -2553384
47
 Y    =       13303124
05  feet           Y    =         4026363
16  meter
 Z    =      -15573388
40                 Z    =        -4759118
82
 XDOT =     -14360
321467                 XDOT =       -4299
771505
 YDOT =     -18898
609563  feet/sec       YDOT =       -5808
810155  meter/sec
 ZDOT =      -8453
440166                 ZDOT =       -2597
685506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15315885
93                 X    =        -4668282
03
 Y    =       -3152638
40  feet           Y    =         -960924
18  meter
 Z    =      -15619124
68                 Z    =        -4760709
20
 XDOT =      12607
442093                 XDOT =        3842
748350
 YDOT =     -18813
704574  feet/sec       YDOT =       -5734
417154  meter/sec
 ZDOT =      -8533
032362                 ZDOT =       -2600
868264


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   06365
55095079  
00020000  00000-0  20000-3 0  9111
2 25544  51
6351 250
0271 0023482  38
0555 322
2263 15
76685051 24308


Satellite: ISS
Catalog Number: 25544
Epoch time:      06365
55095079   =   yrday
fracday
Element set:     911
Inclination:       51
6351  deg
RA of node:       250
0271  deg
Eccentricity:     
0023482     
Arg of perigee:    38
0555  deg
Mean anomaly:     322
2263  deg
Mean motion:   15
76685051  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2430
Checksum:              271

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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