Date: November 4th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6673 62 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 1514)
---------------------------------------

Vector Time (GMT): 2006/307/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6586752
88                 A    =         6721288
69  meter
 Y    =         -40187
03  meter          E    =           
0023765
 Z    =        1261032
44                 I    =           51
60655
 XDOT =       1160
797210                 Wp   =          143
87298
 YDOT =       4873
312410  meter/sec      RA   =          188
37605  deg
 ZDOT =      -5871
042133                 TA   =           22
24591
                                          MA   =           22
14298
                                          Ha   =            187
843  n
mi
                                          Hp   =            176
177

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21610081
64                 X    =         6580586
67
 Y    =        -131847
20  feet           Y    =           33435
25  meter
 Z    =        4137245
55                 Z    =         1293016
81
 XDOT =       3808
389796                 XDOT =        1134
738145
 YDOT =      15988
557774  feet/sec       YDOT =        4886
147250  meter/sec
 ZDOT =     -19261
949256                 ZDOT =       -5865
466233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11671671
57                 X    =        -3557525
50
 Y    =       18159945
36  feet           Y    =         5535151
35  meter
 Z    =        4256557
29                 Z    =         1297398
66
 XDOT =     -14209
618104                 XDOT =       -4331
091598
 YDOT =      -4595
372091  feet/sec       YDOT =       -1400
669413  meter/sec
 ZDOT =     -19240
463609                 ZDOT =       -5864
493308


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
57589314  
00020000  00000-0  20000-3 0  9007
2 25544  51
6350 189
1879 0012137 170
0893 190
0513 15
77579121 15153


Satellite: ISS
Catalog Number: 25544
Epoch time:      06307
57589314   =   yrday
fracday
Element set:     900
Inclination:       51
6350  deg
RA of node:       189
1879  deg
Eccentricity:     
0012137     
Arg of perigee:   170
0893  deg
Mean anomaly:     190
0513  deg
Mean motion:   15
77579121  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1515
Checksum:              292


Coasting Arc #2 (Orbit 1530)
---------------------------------------

Vector Time (GMT): 2006/308/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         139984
00                 A    =         6709724
51  meter
 Y    =       -4165039
50  meter          E    =           
0012675
 Z    =        5255811
78                 I    =           51
59587
 XDOT =       7700
727671                 Wp   =          164
17862
 YDOT =        371
992243  meter/sec      RA   =          183
22302  deg
 ZDOT =         77
646395                 TA   =          285
01493
                                          MA   =          285
15518
                                          Ha   =            187
616  n
mi
                                          Hp   =            176
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         459265
08                 X    =          161015
02
 Y    =      -13664827
75  feet           Y    =        -4163356
54  meter
 Z    =       17243476
96                 Z    =         5256542
92
 XDOT =      25264
854565                 XDOT =        7695
618458
 YDOT =       1220
446992  feet/sec       YDOT =         458
077485  meter/sec
 ZDOT =        254
745389                 ZDOT =         115
045349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11383286
58                 X    =         3469625
75
 Y    =        7568698
59  feet           Y    =         2306939
33  meter
 Z    =       17245623
43                 Z    =         5256466
02
 XDOT =     -13904
494710                 XDOT =       -4238
089988
 YDOT =      19923
806375  feet/sec       YDOT =        6072
776183  meter/sec
 ZDOT =        394
321875                 ZDOT =         120
189308


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
58938482  
00020000  00000-0  20000-3 0  9014
2 25544  51
6343 183
9541 0011967 174
6056 185
5240 15
77647664 15316


Satellite: ISS
Catalog Number: 25544
Epoch time:      06308
58938482   =   yrday
fracday
Element set:     901
Inclination:       51
6343  deg
RA of node:       183
9541  deg
Eccentricity:     
0011967     
Arg of perigee:   174
6056  deg
Mean anomaly:     185
5240  deg
Mean motion:   15
77647664  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1531
Checksum:              312


Coasting Arc #3 (Orbit 1546)
---------------------------------------

Vector Time (GMT): 2006/309/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6586545
64                 A    =         6721089
30  meter
 Y    =        -690413
61  meter          E    =           
0012654
 Z    =        1153340
90                 I    =           51
66201
 XDOT =       1535
546211                 Wp   =          110
95745
 YDOT =      -4713
563126  meter/sec      RA   =          178
06782  deg
 ZDOT =       5891
421095                 TA   =          261
67737
                                          MA   =          261
82087
                                          Ha   =            187
361  n
mi
                                          Hp   =            176
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21609401
72                 X    =        -6583938
73
 Y    =       -2265136
50  feet           Y    =         -764053
48  meter
 Z    =        3783926
83                 Z    =         1121348
66
 XDOT =       5037
881271                 XDOT =        1559
519358
 YDOT =     -15464
445950  feet/sec       YDOT =       -4696
257972  meter/sec
 ZDOT =      19328
809367                 ZDOT =        5898
939096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13114705
70                 X    =         3997362
30
 Y    =      -17349102
49  feet           Y    =        -5288006
44  meter
 Z    =        3664467
99                 Z    =         1116929
84
 XDOT =       9427
922397                 XDOT =        2873
630747
 YDOT =      11255
472694  feet/sec       YDOT =        3430
668077  meter/sec
 ZDOT =      19356
207549                 ZDOT =        5899
772061


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
60285190  
00020000  00000-0  20000-3 0  9020
2 25544  51
6330 178
7194 0011973 179
2499 180
8686 15
77713628 15470


Satellite: ISS
Catalog Number: 25544
Epoch time:      06309
60285190   =   yrday
fracday
Element set:     902
Inclination:       51
6330  deg
RA of node:       178
7194  deg
Eccentricity:     
0011973     
Arg of perigee:   179
2499  deg
Mean anomaly:     180
8686  deg
Mean motion:   15
77713628  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1547
Checksum:              322


Coasting Arc #4 (Orbit 1561)
---------------------------------------

Vector Time (GMT): 2006/310/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2505596
71                 A    =         6711822
41  meter
 Y    =        4076904
19  meter          E    =           
0018577
 Z    =       -4721592
53                 I    =           51
65811
 XDOT =      -7103
002235                 Wp   =          147
06840
 YDOT =      -1248
640904  meter/sec      RA   =          172
87223  deg
 ZDOT =       2680
795189                 TA   =          149
36039
                                          MA   =          149
25177
                                          Ha   =            187
157  n
mi
                                          Hp   =            176
685

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8220461
64                 X    =        -2528061
60
 Y    =       13375669
90  feet           Y    =         4048759
94  meter
 Z    =      -15490789
16                 Z    =        -4733819
41
 XDOT =     -23303
813107                 XDOT =       -7101
535086
 YDOT =      -4096
590892  feet/sec       YDOT =       -1328
062597  meter/sec
 ZDOT =       8795
259807                 ZDOT =        2646
291153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7486987
18                 X    =        -2282033
69
 Y    =      -13748866
21  feet           Y    =        -4190654
42  meter
 Z    =      -15535854
80                 Z    =        -4735328
54
 XDOT =      14260
140332                 XDOT =        4346
490773
 YDOT =     -17596
536721  feet/sec       YDOT =       -5363
424393  meter/sec
 ZDOT =       8666
340158                 ZDOT =        2641
500480


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
55295732  
00020000  00000-0  20000-3 0  9030
2 25544  51
6316 173
8113 0011892 182
9236 177
1861 15
77728977 15625


Satellite: ISS
Catalog Number: 25544
Epoch time:      06310
55295732   =   yrday
fracday
Element set:     903
Inclination:       51
6316  deg
RA of node:       173
8113  deg
Eccentricity:     
0011892     
Arg of perigee:   182
9236  deg
Mean anomaly:     177
1861  deg
Mean motion:   15
77728977  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1562
Checksum:              307


Coasting Arc #5 (Orbit 1577)
---------------------------------------

Vector Time (GMT): 2006/311/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5580796
12                 A    =         6716554
56  meter
 Y    =        1535170
96  meter          E    =           
0012279
 Z    =       -3398216
89                 I    =           51
70122
 XDOT =      -4079
645138                 Wp   =          164
28148
 YDOT =       4623
837747  meter/sec      RA   =          167
75787  deg
 ZDOT =      -4626
501766                 TA   =           55
89435
                                          MA   =           55
77790
                                          Ha   =            187
057  n
mi
                                          Hp   =            176
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18309698
55                 X    =         5579723
23
 Y    =        5036650
13  feet           Y    =         1597572
83  meter
 Z    =      -11149005
53                 Z    =        -3371107
08
 XDOT =     -13384
662525                 XDOT =       -4108
570989
 YDOT =      15170
071348  feet/sec       YDOT =        4578
055592  meter/sec
 ZDOT =     -15178
811569                 ZDOT =       -4646
391069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13344240
64                 X    =        -4067324
55
 Y    =       13593911
16  feet           Y    =         4143424
12  meter
 Z    =      -11047626
51                 Z    =        -3367316
56
 XDOT =      -5783
171546                 XDOT =       -1762
710687
 YDOT =     -18030
799865  feet/sec       YDOT =       -5495
787799  meter/sec
 ZDOT =     -15252
409061                 ZDOT =       -4648
934282


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
56637866  
00020000  00000-0  20000-3 0  9041
2 25544  51
6306 168
5775 0011854 187
1314 172
9684 15
77753478 15788


Satellite: ISS
Catalog Number: 25544
Epoch time:      06311
56637866   =   yrday
fracday
Element set:     904
Inclination:       51
6306  deg
RA of node:       168
5775  deg
Eccentricity:     
0011854     
Arg of perigee:   187
1314  deg
Mean anomaly:     172
9684  deg
Mean motion:   15
77753478  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1578
Checksum:              331


Coasting Arc #6 (Orbit 1593)
---------------------------------------

Vector Time (GMT): 2006/312/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4431665
36                 A    =         6717004
69  meter
 Y    =       -3960961
28  meter          E    =           
0016393
 Z    =        3105127
29                 I    =           51
73180
 XDOT =       5499
159654                 Wp   =          139
95899
 YDOT =       2316
300940  meter/sec      RA   =          162
54735  deg
 ZDOT =      -4891
875460                 TA   =            3
90073
                                          MA   =            3
88796
                                          Ha   =            186
597  n
mi
                                          Hp   =            177
122

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14539584
51                 X    =         4460543
53
 Y    =      -12995279
78  feet           Y    =        -3911242
79  meter
 Z    =       10187425
50                 Z    =         3126726
54
 XDOT =      18041
862382                 XDOT =        5496
614112
 YDOT =       7599
412532  feet/sec       YDOT =        2377
781864  meter/sec
 ZDOT =     -16049
460172                 ZDOT =       -4865
165894

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4624887
62                 X    =         1409665
75
 Y    =       18901035
20  feet           Y    =         5761035
53  meter
 Z    =       10267508
73                 Z    =         3129536
66
 XDOT =     -13876
191784                 XDOT =       -4229
463256
 YDOT =      12062
779883  feet/sec       YDOT =        3676
735308  meter/sec
 ZDOT =     -15949
456960                 ZDOT =       -4861
394481


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
57977430  
00020000  00000-0  20000-3 0  9058
2 25544  51
6311 163
3423 0011752 191
8515 168
2375 15
77833614 15943


Satellite: ISS
Catalog Number: 25544
Epoch time:      06312
57977430   =   yrday
fracday
Element set:     905
Inclination:       51
6311  deg
RA of node:       163
3423  deg
Eccentricity:     
0011752     
Arg of perigee:   191
8515  deg
Mean anomaly:     168
2375  deg
Mean motion:   15
77833614  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1594
Checksum:              293


Coasting Arc #7 (Orbit 1609)
---------------------------------------

Vector Time (GMT): 2006/313/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3830669
70                 A    =         6711110
47  meter
 Y    =       -2572595
19  meter          E    =           
0015178
 Z    =        4875993
27                 I    =           51
73687
 XDOT =       5892
113061                 Wp   =          169
82645
 YDOT =      -4404
282602  meter/sec      RA   =          157
43191  deg
 ZDOT =       2289
489923                 TA   =          257
84920
                                          MA   =          258
01927
                                          Ha   =            186
660  n
mi
                                          Hp   =            177
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12567813
96                 X    =        -3825304
96
 Y    =       -8440272
93  feet           Y    =        -2615402
36  meter
 Z    =       15997353
23                 Z    =         4857396
33
 XDOT =      19331
079598                 XDOT =        5929
802335
 YDOT =     -14449
746071  feet/sec       YDOT =       -4338
183226  meter/sec
 ZDOT =       7511
449879                 ZDOT =        2318
205394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13287662
70                 X    =         4050079
59
 Y    =       -7406312
34  feet           Y    =        -2257444
00  meter
 Z    =       15927586
85                 Z    =         4854728
47
 XDOT =       3508
894291                 XDOT =        1069
510980
 YDOT =      22789
811294  feet/sec       YDOT =        6946
334482  meter/sec
 ZDOT =       7618
050593                 ZDOT =        2321
981821


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
59314979  
00020000  00000-0  20000-3 0  9065
2 25544  51
6299 158
1067 0011742 194
8551 165
2270 15
77795088 16108


Satellite: ISS
Catalog Number: 25544
Epoch time:      06313
59314979   =   yrday
fracday
Element set:     906
Inclination:       51
6299  deg
RA of node:       158
1067  deg
Eccentricity:     
0011742     
Arg of perigee:   194
8551  deg
Mean anomaly:     165
2270  deg
Mean motion:   15
77795088  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1610
Checksum:              315


Coasting Arc #8 (Orbit 1624)
---------------------------------------

Vector Time (GMT): 2006/314/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5617291
63                 A    =         6720925
54  meter
 Y    =        3618458
51  meter          E    =           
0004251
 Z    =        -745409
66                 I    =           51
79629
 XDOT =      -3154
483181                 Wp   =          138
33300
 YDOT =      -3666
587190  meter/sec      RA   =          152
24879  deg
 ZDOT =       5989
222102                 TA   =          213
55618
                                          MA   =          213
58311
                                          Ha   =            186
372  n
mi
                                          Hp   =            177
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18429434
50                 X    =        -5653715
14
 Y    =       11871583
02  feet           Y    =         3555439
25  meter
 Z    =       -2445569
75                 Z    =         -772786
96
 XDOT =     -10349
354267                 XDOT =       -3142
343363
 YDOT =     -12029
485533  feet/sec       YDOT =       -3701
795019  meter/sec
 ZDOT =      19649
678813                 ZDOT =        5973
926596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2528792
36                 X    =         -770775
91
 Y    =      -21764095
49  feet           Y    =        -6633696
31  meter
 Z    =       -2547294
10                 Z    =         -776415
24
 XDOT =      13822
407721                 XDOT =        4213
069873
 YDOT =      -3893
102102  feet/sec       YDOT =       -1186
617521  meter/sec
 ZDOT =      19592
082714                 ZDOT =        5971
666811


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
54316335  
00020000  00000-0  20000-3 0  9070
2 25544  51
6295 153
1980 0011886 198
6265 161
4467 15
77865037 16250


Satellite: ISS
Catalog Number: 25544
Epoch time:      06314
54316335   =   yrday
fracday
Element set:     907
Inclination:       51
6295  deg
RA of node:       153
1980  deg
Eccentricity:     
0011886     
Arg of perigee:   198
6265  deg
Mean anomaly:     161
4467  deg
Mean motion:   15
77865037  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1625
Checksum:              312


Coasting Arc #9 (Orbit 1640)
---------------------------------------

Vector Time (GMT): 2006/315/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1627968
22                 A    =         6709116
43  meter
 Y    =        3866563
60  meter          E    =           
0016083
 Z    =       -5245602
66                 I    =           51
78129
 XDOT =      -6705
734574                 Wp   =          139
92908
 YDOT =       3725
486557  meter/sec      RA   =          147
09549  deg
 ZDOT =        653
999926                 TA   =          136
34168
                                          MA   =          136
21434
                                          Ha   =            186
173  n
mi
                                          Hp   =            177
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5341103
07                 X    =         1610093
22
 Y    =       12685576
10  feet           Y    =         3884668
86  meter
 Z    =      -17209982
49                 Z    =        -5237737
06
 XDOT =     -22000
441516                 XDOT =       -6750
072144
 YDOT =      12222
724924  feet/sec       YDOT =        3650
251364  meter/sec
 ZDOT =       2145
669047                 ZDOT =         621
315696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13793022
03                 X    =        -4204113
11
 Y    =        -481248
75  feet           Y    =         -146684
62  meter
 Z    =      -17180094
98                 Z    =        -5236492
95
 XDOT =      -1724
649467                 XDOT =        -525
673158
 YDOT =     -24115
236173  feet/sec       YDOT =       -7350
323986  meter/sec
 ZDOT =       2024
133203                 ZDOT =         616
955800


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
55648934  
00020000  00000-0  20000-3 0  9086
2 25544  51
6294 147
9625 0011847 201
8627 158
2034 15
77908097 16418


Satellite: ISS
Catalog Number: 25544
Epoch time:      06315
55648934   =   yrday
fracday
Element set:     908
Inclination:       51
6294  deg
RA of node:       147
9625  deg
Eccentricity:     
0011847     
Arg of perigee:   201
8627  deg
Mean anomaly:     158
2034  deg
Mean motion:   15
77908097  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1641
Checksum:              316


Coasting Arc #10 (Orbit 1656)
---------------------------------------

Vector Time (GMT): 2006/316/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5844872
66                 A    =         6719457
16  meter
 Y    =       -2722254
62  meter          E    =           
0016218
 Z    =       -1854388
07                 I    =           51
84042
 XDOT =        616
788420                 Wp   =          182
50666
 YDOT =       5183
472156  meter/sec      RA   =          141
96492  deg
 ZDOT =      -5679
329516                 TA   =           18
07376
                                          MA   =           18
01617
                                          Ha   =            185
894  n
mi
                                          Hp   =            177
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19176091
40                 X    =         5883887
26
 Y    =       -8931281
56  feet           Y    =        -2656675
77  meter
 Z    =       -6083950
36                 Z    =        -1825898
77
 XDOT =       2023
584054                 XDOT =         586
369700
 YDOT =      17006
142244  feet/sec       YDOT =        5190
199640  meter/sec
 ZDOT =     -18632
970854                 ZDOT =       -5676
406749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         268638
71                 X    =           81881
08
 Y    =       21182466
04  feet           Y    =         6456415
65  meter
 Z    =       -5977933
54                 Z    =        -1822074
14
 XDOT =     -14838
064102                 XDOT =       -4522
641938
 YDOT =      -5053
770436  feet/sec       YDOT =       -1540
389229  meter/sec
 ZDOT =     -18621
360739                 ZDOT =       -5675
790753


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
56978978  
00020000  00000-0  20000-3 0  9093
2 25544  51
6299 142
7275 0011652 206
3141 153
7434 15
77969279 16572


Satellite: ISS
Catalog Number: 25544
Epoch time:      06316
56978978   =   yrday
fracday
Element set:     909
Inclination:       51
6299  deg
RA of node:       142
7275  deg
Eccentricity:     
0011652     
Arg of perigee:   206
3141  deg
Mean anomaly:     153
7434  deg
Mean motion:   15
77969279  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1657
Checksum:              337


Coasting Arc #11 (Orbit 1672)
---------------------------------------

Vector Time (GMT): 2006/317/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         471736
80                 A    =         6712733
16  meter
 Y    =       -5106939
26  meter          E    =           
0007778
 Z    =        4324042
96                 I    =           51
83891
 XDOT =       6474
412742                 Wp   =          155
94157
 YDOT =      -2339
316989  meter/sec      RA   =          136
77108  deg
 ZDOT =      -3473
989482                 TA   =          328
99422
                                          MA   =          329
04010
                                          Ha   =            185
748  n
mi
                                          Hp   =            178
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1547692
92                 X    =          507802
59
 Y    =      -16755050
06  feet           Y    =        -5101462
53  meter
 Z    =       14186492
66                 Z    =         4326422
11
 XDOT =      21241
511622                 XDOT =        6516
966326
 YDOT =      -7674
924506  feet/sec       YDOT =       -2266
678461  meter/sec
 ZDOT =     -11397
603287                 ZDOT =       -3442
433139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14818220
37                 X    =         4516593
57
 Y    =        7957053
58  feet           Y    =         2425309
93  meter
 Z    =       14194691
72                 Z    =         4326542
04
 XDOT =       -767
399095                 XDOT =        -233
903244
 YDOT =      21523
762006  feet/sec       YDOT =        6560
442659  meter/sec
 ZDOT =     -11280
073962                 ZDOT =       -3438
166544


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06317
58306694  
00020000  00000-0  20000-3 0  9108
2 25544  51
6293 137
4917 0011813 209
9536 150
0954 15
77961520 16732


Satellite: ISS
Catalog Number: 25544
Epoch time:      06317
58306694   =   yrday
fracday
Element set:     910
Inclination:       51
6293  deg
RA of node:       137
4917  deg
Eccentricity:     
0011813     
Arg of perigee:   209
9536  deg
Mean anomaly:     150
0954  deg
Mean motion:   15
77961520  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1673
Checksum:              302


Coasting Arc #12 (Orbit 1688)
---------------------------------------

Vector Time (GMT): 2006/318/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 470356
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5255909
39                 A    =         6713757
51  meter
 Y    =        1159834
56  meter          E    =           
0012757
 Z    =        4018402
28                 I    =           51
86299
 XDOT =       1595
203236                 Wp   =          161
43901
 YDOT =      -6430
169065  meter/sec      RA   =          131
66955  deg
 ZDOT =       3927
164255                 TA   =          248
07912
                                          MA   =          248
21478
                                          Ha   =            185
458  n
mi
                                          Hp   =            178
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17243797
22                 X    =        -5288009
15
 Y    =        3805231
50  feet           Y    =         1100880
49  meter
 Z    =       13183734
52                 Z    =         3992790
76
 XDOT =       5233
606417                 XDOT =        1647
909990
 YDOT =     -21096
355201  feet/sec       YDOT =       -6412
036015  meter/sec
 ZDOT =      12884
397163                 ZDOT =        3935
041736

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3031317
61                 X    =          923945
61
 Y    =      -17468492
53  feet           Y    =        -5324396
52  meter
 Z    =       13088241
58                 Z    =         3989296
03
 XDOT =      16299
831552                 XDOT =        4968
188657
 YDOT =      12541
272732  feet/sec       YDOT =        3822
579929  meter/sec
 ZDOT =      12912
954733                 ZDOT =        3935
868603


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06318
59631720  
00020000  00000-0  20000-3 0  9112
2 25544  51
6295 132
2555 0011842 213
9655 146
0753 15
78043300 16891


Satellite: ISS
Catalog Number: 25544
Epoch time:      06318
59631720   =   yrday
fracday
Element set:     911
Inclination:       51
6295  deg
RA of node:       132
2555  deg
Eccentricity:     
0011842     
Arg of perigee:   213
9655  deg
Mean anomaly:     146
0753  deg
Mean motion:   15
78043300  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1689
Checksum:              285

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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