Date: November 2nd 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5704 87 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 1482)
---------------------------------------

Vector Time (GMT): 2006/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         562671
22                 A    =         6710199
48  meter
 Y    =       -4186331
73  meter          E    =           
0014665
 Z    =        5209818
99                 I    =           51
51245
 XDOT =       7428
759410                 Wp   =          154
17778
 YDOT =       1931
431243  meter/sec      RA   =          198
94559  deg
 ZDOT =        735
893878                 TA   =          288
73953
                                          MA   =          288
89862
                                          Ha   =            188
165  n
mi
                                          Hp   =            175
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1846034
19                 X    =          584132
77
 Y    =      -13734684
14  feet           Y    =        -4179919
50  meter
 Z    =       17092581
99                 Z    =         5212604
73
 XDOT =      24372
570243                 XDOT =        7403
034855
 YDOT =       6336
716677  feet/sec       YDOT =        2014
359938  meter/sec
 ZDOT =       2414
349992                 ZDOT =         771
920845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7468124
66                 X    =         2276284
40
 Y    =       11659387
85  feet           Y    =         3553781
42  meter
 Z    =       17102384
01                 Z    =         5212806
65
 XDOT =     -21900
183996                 XDOT =       -6675
176082
 YDOT =      10222
360788  feet/sec       YDOT =        3115
775568  meter/sec
 ZDOT =       2549
007555                 ZDOT =         776
937503


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06305
54882443  
00020000  00000-0  20000-3 0  9001
2 25544  51
6351 199
6524 0012177 162
4826 197
6761 15
77550379 14838


Satellite: ISS
Catalog Number: 25544
Epoch time:      06305
54882443   =   yrday
fracday
Element set:     900
Inclination:       51
6351  deg
RA of node:       199
6524  deg
Eccentricity:     
0012177     
Arg of perigee:   162
4826  deg
Mean anomaly:     197
6761  deg
Mean motion:   15
77550379  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1483
Checksum:              311


Coasting Arc #2 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2006/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6392339
89                 A    =         6721941
75  meter
 Y    =       -2011208
65  meter          E    =           
0013431
 Z    =         543826
11                 I    =           51
57998
 XDOT =       1914
777486                 Wp   =          104
63251
 YDOT =      -4429
578877  meter/sec      RA   =          193
77452  deg
 ZDOT =       5998
916340                 TA   =          261
29332
                                          MA   =          261
44547
                                          Ha   =            188
002  n
mi
                                          Hp   =            176
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20972243
73                 X    =        -6372017
05
 Y    =       -6598453
57  feet           Y    =        -2082577
69  meter
 Z    =        1784206
41                 Z    =          512820
88
 XDOT =       6282
078367                 XDOT =        1935
025052
 YDOT =     -14532
739098  feet/sec       YDOT =       -4408
053365  meter/sec
 ZDOT =      19681
484055                 ZDOT =        6008
267860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20180385
27                 X    =         6150981
43
 Y    =       -8747967
52  feet           Y    =        -2666380
50  meter
 Z    =        1668263
69                 Z    =          508486
77
 XDOT =       4209
684513                 XDOT =        1283
111840
 YDOT =      13555
601237  feet/sec       YDOT =        4131
747257  meter/sec
 ZDOT =      19715
743825                 ZDOT =        6009
358718


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06306
56237257  
00020000  00000-0  20000-3 0  9012
2 25544  51
6355 194
4190 0012065 166
4030 193
7462 15
77564467 14996


Satellite: ISS
Catalog Number: 25544
Epoch time:      06306
56237257   =   yrday
fracday
Element set:     901
Inclination:       51
6355  deg
RA of node:       194
4190  deg
Eccentricity:     
0012065     
Arg of perigee:   166
4030  deg
Mean anomaly:     193
7462  deg
Mean motion:   15
77564467  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1499
Checksum:              300


Coasting Arc #3 (Orbit 1513)
---------------------------------------

Vector Time (GMT): 2006/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2784810
21                 A    =         6711126
30  meter
 Y    =        3568719
50  meter          E    =           
0021063
 Z    =       -4971664
12                 I    =           51
57197
 XDOT =      -6946
522683                 Wp   =          136
26823
 YDOT =      -2641
447314  meter/sec      RA   =          188
58534  deg
 ZDOT =       1984
978211                 TA   =          153
01889
                                          MA   =          152
90923
                                          Ha   =            187
782  n
mi
                                          Hp   =            176
139

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9136516
43                 X    =        -2800357
03
 Y    =       11708397
32  feet           Y    =         3537491
16  meter
 Z    =      -16311234
00                 Z    =        -4985230
96
 XDOT =     -22790
428749                 XDOT =       -6926
112302
 YDOT =      -8666
165727  feet/sec       YDOT =       -2719
013018  meter/sec
 ZDOT =       6512
395705                 ZDOT =        1951
280703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1080806
92                 X    =         -329429
95
 Y    =      -14756597
06  feet           Y    =        -4497810
78  meter
 Z    =      -16361343
30                 Z    =        -4986937
44
 XDOT =      21704
375993                 XDOT =        6615
493803
 YDOT =      -8706
611732  feet/sec       YDOT =       -2653
775256  meter/sec
 ZDOT =       6386
316485                 ZDOT =        1946
549265


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06307
51255411  
00020000  00000-0  20000-3 0  9021
2 25544  51
6356 189
5127 0012004 170
4249 189
7147 15
77601408 15142


Satellite: ISS
Catalog Number: 25544
Epoch time:      06307
51255411   =   yrday
fracday
Element set:     902
Inclination:       51
6356  deg
RA of node:       189
5127  deg
Eccentricity:     
0012004     
Arg of perigee:   170
4249  deg
Mean anomaly:     189
7147  deg
Mean motion:   15
77601408  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1514
Checksum:              275


Coasting Arc #4 (Orbit 1529)
---------------------------------------

Vector Time (GMT): 2006/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5510439
07                 A    =         6718531
01  meter
 Y    =        2580914
97  meter          E    =           
0015187
 Z    =       -2833371
37                 I    =           51
62475
 XDOT =      -4379
503542                 Wp   =          160
63461
 YDOT =       3778
900869  meter/sec      RA   =          183
45935  deg
 ZDOT =      -5097
033985                 TA   =           51
94326
                                          MA   =           51
80633
                                          Ha   =            187
750  n
mi
                                          Hp   =            176
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18078868
35                 X    =         5494933
83
 Y    =        8467568
80  feet           Y    =         2642449
07  meter
 Z    =       -9295837
84                 Z    =        -2806638
44
 XDOT =     -14368
449940                 XDOT =       -4396
672960
 YDOT =      12397
968731  feet/sec       YDOT =        3729
830838  meter/sec
 ZDOT =     -16722
552445                 ZDOT =       -5118
352010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19048815
22                 X    =        -5806078
88
 Y    =        6126884
52  feet           Y    =         1867474
40  meter
 Z    =       -9195745
10                 Z    =        -2802863
10
 XDOT =       2476
266025                 XDOT =         754
765884
 YDOT =     -17409
732114  feet/sec       YDOT =       -5306
486348  meter/sec
 ZDOT =     -16801
556002                 ZDOT =       -5121
114269


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06308
52606122  
00020000  00000-0  20000-3 0  9033
2 25544  51
6352 184
2795 0012063 175
1820 184
9463 15
77594056 15309


Satellite: ISS
Catalog Number: 25544
Epoch time:      06308
52606122   =   yrday
fracday
Element set:     903
Inclination:       51
6352  deg
RA of node:       184
2795  deg
Eccentricity:     
0012063     
Arg of perigee:   175
1820  deg
Mean anomaly:     184
9463  deg
Mean motion:   15
77594056  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1530
Checksum:              284


Coasting Arc #5 (Orbit 1545)
---------------------------------------

Vector Time (GMT): 2006/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4711795
20                 A    =         6715719
19  meter
 Y    =       -3048890
15  meter          E    =           
0016018
 Z    =        3668805
76                 I    =           51
64458
 XDOT =       5487
403565                 Wp   =          131
65277
 YDOT =       3263
145188  meter/sec      RA   =          178
24568  deg
 ZDOT =      -4334
008774                 TA   =            4
09880
                                          MA   =            4
08570
                                          Ha   =            187
271  n
mi
                                          Hp   =            176
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15458645
68                 X    =         4727715
11
 Y    =      -10002920
44  feet           Y    =        -2996111
36  meter
 Z    =       12036764
30                 Z    =         3691735
01
 XDOT =      18003
292535                 XDOT =        5471
561339
 YDOT =      10705
856917  feet/sec       YDOT =        3324
419953  meter/sec
 ZDOT =     -14219
188891                 ZDOT =       -4307
388413

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4169944
62                 X    =        -1270999
12
 Y    =       17876888
49  feet           Y    =         5448875
61  meter
 Z    =       12121891
68                 Z    =         3694752
58
 XDOT =     -19152
789808                 XDOT =       -5837
770333
 YDOT =       5110
040968  feet/sec       YDOT =        1557
540487  meter/sec
 ZDOT =     -14119
417138                 ZDOT =       -4303
598344


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06309
53954633  
00020000  00000-0  20000-3 0  9049
2 25544  51
6349 179
0460 0011795 178
6062 181
5138 15
77689713 15467


Satellite: ISS
Catalog Number: 25544
Epoch time:      06309
53954633   =   yrday
fracday
Element set:     904
Inclination:       51
6349  deg
RA of node:       179
0460  deg
Eccentricity:     
0011795     
Arg of perigee:   178
6062  deg
Mean anomaly:     181
5138  deg
Mean motion:   15
77689713  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1546
Checksum:              318


Coasting Arc #6 (Orbit 1561)
---------------------------------------

Vector Time (GMT): 2006/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3855930
53                 A    =         6712953
88  meter
 Y    =       -3132693
24  meter          E    =           
0017090
 Z    =        4515950
04                 I    =           51
66214
 XDOT =       6273
246854                 Wp   =          153
61630
 YDOT =      -3224
785969  meter/sec      RA   =          173
13176  deg
 ZDOT =       3099
858470                 TA   =          265
42607
                                          MA   =          265
62130
                                          Ha   =            187
320  n
mi
                                          Hp   =            176
859

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12650690
73                 X    =        -3842552
12
 Y    =      -10277864
95  feet           Y    =        -3175737
90  meter
 Z    =       14816109
04                 Z    =         4497249
59
 XDOT =      20581
518549                 XDOT =        6293
781569
 YDOT =     -10580
006461  feet/sec       YDOT =       -3154
520442  meter/sec
 ZDOT =      10170
139338                 ZDOT =        3130
384563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16275665
28                 X    =         4960822
78
 Y    =       -1688987
66  feet           Y    =         -514803
44  meter
 Z    =       14745901
50                 Z    =         4494550
78
 XDOT =      -7218
115760                 XDOT =       -2200
081684
 YDOT =      20787
607079  feet/sec       YDOT =        6336
062638  meter/sec
 ZDOT =      10283
602743                 ZDOT =        3134
442116


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   06310
55301271  
00020000  00000-0  20000-3 0  9058
2 25544  51
6339 173
8116 0011793 182
4182 177
6928 15
77664763 15629


Satellite: ISS
Catalog Number: 25544
Epoch time:      06310
55301271   =   yrday
fracday
Element set:     905
Inclination:       51
6339  deg
RA of node:       173
8116  deg
Eccentricity:     
0011793     
Arg of perigee:   182
4182  deg
Mean anomaly:     177
6928  deg
Mean motion:   15
77664763  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1562
Checksum:              299


Coasting Arc #7 (Orbit 1576)
---------------------------------------

Vector Time (GMT): 2006/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6022014
23                 A    =         6720506
32  meter
 Y    =        2550682
42  meter          E    =           
0006286
 Z    =       -1565046
37                 I    =           51
71553
 XDOT =      -3182
623947                 Wp   =          147
51796
 YDOT =      -3976
923603  meter/sec      RA   =          167
93231  deg
 ZDOT =       5770
111476                 TA   =          195
23460
                                          MA   =          195
25354
                                          Ha   =            187
007  n
mi
                                          Hp   =            177
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19757264
54                 X    =        -6042485
82
 Y    =        8368380
65  feet           Y    =         2483226
60  meter
 Z    =       -5134666
57                 Z    =        -1594351
63
 XDOT =     -10441
679615                 XDOT =       -3165
947838
 YDOT =     -13047
649616  feet/sec       YDOT =       -4012
420762  meter/sec
 ZDOT =      18930
811929                 ZDOT =        5754
689991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7747050
89                 X    =         2361301
11
 Y    =      -19980767
73  feet           Y    =        -6090138
00  meter
 Z    =       -5243683
90                 Z    =        -1598274
85
 XDOT =      15250
060746                 XDOT =        4648
218515
 YDOT =        964
552082  feet/sec       YDOT =         293
995475  meter/sec
 ZDOT =      18872
721333                 ZDOT =        5752
405462


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   06311
50311596  
00020000  00000-0  20000-3 0  9066
2 25544  51
6329 168
9041 0011772 187
1470 172
9529 15
77712918 15776


Satellite: ISS
Catalog Number: 25544
Epoch time:      06311
50311596   =   yrday
fracday
Element set:     906
Inclination:       51
6329  deg
RA of node:       168
9041  deg
Eccentricity:     
0011772     
Arg of perigee:   187
1470  deg
Mean anomaly:     172
9529  deg
Mean motion:   15
77712918  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1577
Checksum:              304


Coasting Arc #8 (Orbit 1592)
---------------------------------------

Vector Time (GMT): 2006/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1610166
36                 A    =         6709448
91  meter
 Y    =        3851613
86  meter          E    =           
0016655
 Z    =       -5262802
54                 I    =           51
70497
 XDOT =      -7254
982452                 Wp   =          130
52103
 YDOT =       2549
185875  meter/sec      RA   =          162
79034  deg
 ZDOT =       -365
407450                 TA   =          136
07800
                                          MA   =          135
94549
                                          Ha   =            186
796  n
mi
                                          Hp   =            177
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5282698
03                 X    =         1592543
72
 Y    =       12636528
41  feet           Y    =         3869521
64  meter
 Z    =      -17266412
52                 Z    =        -5255022
58
 XDOT =     -23802
435865                 XDOT =       -7281
173471
 YDOT =       8363
470718  feet/sec       YDOT =        2467
910236  meter/sec
 ZDOT =      -1198
843340                 ZDOT =        -400
716303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12893865
23                 X    =        -3930050
12
 Y    =       -4728298
19  feet           Y    =        -1441185
29  meter
 Z    =      -17236855
46                 Z    =        -5253793
54
 XDOT =       9844
586836                 XDOT =        3000
630068
 YDOT =     -22132
425814  feet/sec       YDOT =       -6745
963388  meter/sec
 ZDOT =      -1330
285846                 ZDOT =        -405
471126


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   06312
51654050  
00020000  00000-0  20000-3 0  9074
2 25544  51
6317 163
6688 0011770 191
0605 169
0303 15
77763552 15939


Satellite: ISS
Catalog Number: 25544
Epoch time:      06312
51654050   =   yrday
fracday
Element set:     907
Inclination:       51
6317  deg
RA of node:       163
6688  deg
Eccentricity:     
0011770     
Arg of perigee:   191
0605  deg
Mean anomaly:     169
0303  deg
Mean motion:   15
77763552  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1593
Checksum:              285


Coasting Arc #9 (Orbit 1608)
---------------------------------------

Vector Time (GMT): 2006/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6386941
73                 A    =         6721152
89  meter
 Y    =       -1822105
90  meter          E    =           
0019619
 Z    =        -945373
79                 I    =           51
77139
 XDOT =        511
625910                 Wp   =          170
93461
 YDOT =       4868
773998  meter/sec      RA   =          157
63953  deg
 ZDOT =      -5963
104849                 TA   =           19
39946
                                          MA   =           19
32489
                                          Ha   =            186
711  n
mi
                                          Hp   =            177
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20954533
24                 X    =         6411434
61
 Y    =       -5978037
73  feet           Y    =        -1750546
54  meter
 Z    =       -3101620
04                 Z    =         -914286
19
 XDOT =       1678
562696                 XDOT =         486
112746
 YDOT =      15973
667974  feet/sec       YDOT =        4874
353232  meter/sec
 ZDOT =     -19563
992287                 ZDOT =       -5960
680811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9660709
28                 X    =        -2944584
19
 Y    =       19550064
75  feet           Y    =         5958859
74  meter
 Z    =       -2985818
11                 Z    =         -910077
36
 XDOT =     -11606
866958                 XDOT =       -3537
773049
 YDOT =      -8703
487306  feet/sec       YDOT =       -2652
822931  meter/sec
 ZDOT =     -19554
289403                 ZDOT =       -5960
147410


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   06313
52994530  
00020000  00000-0  20000-3 0  9087
2 25544  51
6319 158
4352 0011858 195
1976 164
8834 15
77757317 16096


Satellite: ISS
Catalog Number: 25544
Epoch time:      06313
52994530   =   yrday
fracday
Element set:     908
Inclination:       51
6319  deg
RA of node:       158
4352  deg
Eccentricity:     
0011858     
Arg of perigee:   195
1976  deg
Mean anomaly:     164
8834  deg
Mean motion:   15
77757317  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1609
Checksum:              325


Coasting Arc #10 (Orbit 1624)
---------------------------------------

Vector Time (GMT): 2006/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         672590
79                 A    =         6711186
89  meter
 Y    =       -4625981
64  meter          E    =           
0007803
 Z    =        4810759
64                 I    =           51
76420
 XDOT =       7141
671006                 Wp   =          164
77321
 YDOT =      -1526
970293  meter/sec      RA   =          152
45467  deg
 ZDOT =      -2473
284204                 TA   =          309
29507
                                          MA   =          309
36424
                                          Ha   =            186
402  n
mi
                                          Hp   =            177
595

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2206662
69                 X    =          700899
08
 Y    =      -15177105
11  feet           Y    =        -4618302
50  meter
 Z    =       15783332
15                 Z    =         4814095
48
 XDOT =      23430
679154                 XDOT =        7170
229933
 YDOT =      -5009
745055  feet/sec       YDOT =       -1446
948268  meter/sec
 ZDOT =      -8114
449488                 ZDOT =       -2438
520289

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10019240
73                 X    =         3053864
57
 Y    =       11595474
29  feet           Y    =         3534300
56  meter
 Z    =       15795165
23                 Z    =         4814366
36
 XDOT =     -10855
724962                 XDOT =       -3308
824968
 YDOT =      20227
927450  feet/sec       YDOT =        6165
472287  meter/sec
 ZDOT =      -7984
868023                 ZDOT =       -2433
787774


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   06314
54332787  
00020000  00000-0  20000-3 0  9091
2 25544  51
6317 153
1999 0011788 199
5660 160
5055 15
77818241 16253


Satellite: ISS
Catalog Number: 25544
Epoch time:      06314
54332787   =   yrday
fracday
Element set:     909
Inclination:       51
6317  deg
RA of node:       153
1999  deg
Eccentricity:     
0011788     
Arg of perigee:   199
5660  deg
Mean anomaly:     160
5055  deg
Mean motion:   15
77818241  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1625
Checksum:              316


Coasting Arc #11 (Orbit 1640)
---------------------------------------

Vector Time (GMT): 2006/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5836356
62                 A    =         6716672
45  meter
 Y    =         699855
23  meter          E    =           
0013088
 Z    =        3254029
64                 I    =           51
80671
 XDOT =       1980
510423                 Wp   =          141
76707
 YDOT =      -5719
181458  meter/sec      RA   =          147
34383  deg
 ZDOT =       4762
021272                 TA   =          256
27499
                                          MA   =          256
42071
                                          Ha   =            186
178  n
mi
                                          Hp   =            177
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19148151
64                 X    =        -5859556
38
 Y    =        2296112
95  feet           Y    =          634459
90  meter
 Z    =       10675950
27                 Z    =         3225620
02
 XDOT =       6497
737608                 XDOT =        2021
182636
 YDOT =     -18763
718693  feet/sec       YDOT =       -5696
807220  meter/sec
 ZDOT =      15623
429370                 ZDOT =        4771
741079

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10653583
02                 X    =         3247212
10
 Y    =      -16145484
81  feet           Y    =        -4921143
77  meter
 Z    =       10569969
21                 Z    =         3221726
61
 XDOT =       9005
594760                 XDOT =        2744
905283
 YDOT =      16237
656209  feet/sec       YDOT =        4949
237612  meter/sec
 ZDOT =      15658
953160                 ZDOT =        4772
848923


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   06315
55669004  
00020000  00000-0  20000-3 0  9100
2 25544  51
6308 147
9642 0011839 203
7602 156
3018 15
77867752 16411


Satellite: ISS
Catalog Number: 25544
Epoch time:      06315
55669004   =   yrday
fracday
Element set:     910
Inclination:       51
6308  deg
RA of node:       147
9642  deg
Eccentricity:     
0011839     
Arg of perigee:   203
7602  deg
Mean anomaly:     156
3018  deg
Mean motion:   15
77867752  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1641
Checksum:              293


Coasting Arc #12 (Orbit 1655)
---------------------------------------

Vector Time (GMT): 2006/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2644039
52                 A    =         6716568
70  meter
 Y    =        5269536
77  meter          E    =           
0010009
 Z    =       -3228105
72                 I    =           51
82951
 XDOT =      -6026
312731                 Wp   =          184
11747
 YDOT =        -83
512340  meter/sec      RA   =          142
13944  deg
 ZDOT =       4788
942951                 TA   =          138
22926
                                          MA   =          138
15282
                                          Ha   =            185
976  n
mi
                                          Hp   =            177
934

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8674670
33                 X    =        -2687085
99
 Y    =       17288506
47  feet           Y    =         5239729
14  meter
 Z    =      -10590898
02                 Z    =        -3241054
87
 XDOT =     -19771
367229                 XDOT =       -6048
195045
 YDOT =       -273
990616  feet/sec       YDOT =        -151
024513  meter/sec
 ZDOT =      15711
755089                 ZDOT =        4759
613675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7936749
79                 X    =        -2419121
34
 Y    =      -17610760
04  feet           Y    =        -5367759
66  meter
 Z    =      -10638543
87                 Z    =        -3242628
17
 XDOT =      11492
306575                 XDOT =        3502
855044
 YDOT =     -14625
611108  feet/sec       YDOT =       -4457
886266  meter/sec
 ZDOT =      15602
225237                 ZDOT =        4755
558252


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   06316
50669966  
00020000  00000-0  20000-3 0  9114
2 25544  51
6303 143
0554 0011779 206
6068 153
4494 15
77880338 16563


Satellite: ISS
Catalog Number: 25544
Epoch time:      06316
50669966   =   yrday
fracday
Element set:     911
Inclination:       51
6303  deg
RA of node:       143
0554  deg
Eccentricity:     
0011779     
Arg of perigee:   206
6068  deg
Mean anomaly:     153
4494  deg
Mean motion:   15
77880338  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1656
Checksum:              309

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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