Date: September 22nd 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 3875 01 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


262/00:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 190 2
000/00:00:00 000 0 0 0 0 179 5

263/05:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 190 3
000/00:00:00 000 0 0 0 0 179 2

Coasting Arc #1 (Orbit 779)
---------------------------------------

Vector Time (GMT): 2006/260/22:47:48
000
Vector Time (MET): N/A
Weight (LBS)     : 465373
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4553035
20                 A    =         6717688
61  meter
 Y    =       -1748061
56  meter          E    =           
0016684
 Z    =        4621363
41                 I    =           51
91701
 XDOT =       -270
316394                 Wp   =           23
08510
 YDOT =      -7113
868020  meter/sec      RA   =           68
95125  deg
 ZDOT =      -2938
606036                 TA   =           96
00601
                                          MA   =           95
81586
                                          Ha   =            190
006  n
mi
                                          Hp   =            179
788

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14937779
52                 X    =        -4555599
28
 Y    =       -5735110
11  feet           Y    =        -1798990
35  meter
 Z    =       15161953
44                 Z    =         4599238
78
 XDOT =       -886
864810                 XDOT =        -176
472967
 YDOT =     -23339
462007  feet/sec       YDOT =       -7116
366210  meter/sec
 ZDOT =      -9641
095918                 ZDOT =       -2939
691114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11769154
62                 X    =        -3587238
33
 Y    =      -10955161
30  feet           Y    =        -3339133
16  meter
 Z    =       15079291
02                 Z    =         4596167
90
 XDOT =       7190
754876                 XDOT =        2191
742086
 YDOT =     -21086
855537  feet/sec       YDOT =       -6427
273568  meter/sec
 ZDOT =      -9646
107984                 ZDOT =       -2940
133714


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   06260
99232069  
00020000  00000-0  20000-3 0  9003
2 25544  51
6331  69
3911 0011792 355
4686   4
6369 15
75860262  7802


Satellite: ISS
Catalog Number: 25544
Epoch time:      06260
99232069   =   yrday
fracday
Element set:     900
Inclination:       51
6331  deg
RA of node:        69
3911  deg
Eccentricity:     
0011792     
Arg of perigee:   355
4686  deg
Mean anomaly:       4
6369  deg
Mean motion:   15
75860262  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             780
Checksum:              297


Coasting Arc #2 (Orbit 795)
---------------------------------------

Vector Time (GMT): 2006/261/22:47:48
000
Vector Time (MET): N/A
Weight (LBS)     : 465373
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         225384
74                 A    =         6722698
51  meter
 Y    =        5953349
29  meter          E    =           
0018238
 Z    =        3088477
84                 I    =           51
92233
 XDOT =      -5451
583132                 Wp   =           44
48306
 YDOT =      -2351
139666  meter/sec      RA   =           63
86819  deg
 ZDOT =       4925
273909                 TA   =          351
29683
                                          MA   =          351
32841
                                          Ha   =            190
095  n
mi
                                          Hp   =            179
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         739451
25                 X    =          143793
68
 Y    =       19531985
86  feet           Y    =         5955413
60  meter
 Z    =       10132801
32                 Z    =         3089374
31
 XDOT =     -17885
771431                 XDOT =       -5448
813074
 YDOT =      -7713
712815  feet/sec       YDOT =       -2412
086583  meter/sec
 ZDOT =      16159
035135                 ZDOT =        4898
797184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6382508
75                 X    =        -1945388
67
 Y    =       18472267
71  feet           Y    =         5630347
20  meter
 Z    =       10136953
69                 Z    =         3089743
48
 XDOT =     -12653
730000                 XDOT =       -3856
856904
 YDOT =     -13193
629952  feet/sec       YDOT =       -4021
418409  meter/sec
 ZDOT =      16060
074272                 ZDOT =        4895
110638


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   06262
00695956  
00020000  00000-0  20000-3 0  9016
2 25544  51
6328  64
1655 0011841 359
0362   1
0777 15
75869658  7961


Satellite: ISS
Catalog Number: 25544
Epoch time:      06262
00695956   =   yrday
fracday
Element set:     901
Inclination:       51
6328  deg
RA of node:        64
1655  deg
Eccentricity:     
0011841     
Arg of perigee:   359
0362  deg
Mean anomaly:       1
0777  deg
Mean motion:   15
75869658  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             796
Checksum:              309


Coasting Arc #3 (Orbit 796)
---------------------------------------

Vector Time (GMT): 2006/262/00:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450157
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2522060
11                 A    =         6716051
68  meter
 Y    =        3711792
35  meter          E    =           
0009781
 Z    =        4990328
84                 I    =           51
89801
 XDOT =      -4645
627236                 Wp   =           27
16574
 YDOT =      -5821
907208  meter/sec      RA   =           63
50194  deg
 ZDOT =       1989
471465                 TA   =           43
72931
                                          MA   =           43
65187
                                          Ha   =            190
201  n
mi
                                          Hp   =            179
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8274475
43                 X    =        -2587620
35
 Y    =       12177796
43  feet           Y    =         3683222
94  meter
 Z    =       16372469
96                 Z    =         4977917
37
 XDOT =     -15241
559172                 XDOT =       -4589
845005
 YDOT =     -19100
745432  feet/sec       YDOT =       -5873
545200  meter/sec
 ZDOT =       6527
137351                 ZDOT =        1967
038962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7482958
90                 X    =        -2280805
87
 Y    =       12738383
72  feet           Y    =         3882659
36  meter
 Z    =       16326737
22                 Z    =         4976389
51
 XDOT =     -15660
313817                 XDOT =       -4773
263651
 YDOT =     -17427
533761  feet/sec       YDOT =       -5311
912290  meter/sec
 ZDOT =       6442
769543                 ZDOT =        1963
756157


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   06262
07037477  
00020000  00000-0  20000-3 0  9022
2 25544  51
6318  63
8383 0011983 358
7280   1
3852 15
75865698  7974


Satellite: ISS
Catalog Number: 25544
Epoch time:      06262
07037477   =   yrday
fracday
Element set:     902
Inclination:       51
6318  deg
RA of node:        63
8383  deg
Eccentricity:     
0011983     
Arg of perigee:   358
7280  deg
Mean anomaly:       1
3852  deg
Mean motion:   15
75865698  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             797
Checksum:              318


Coasting Arc #4 (Orbit 811)
---------------------------------------

Vector Time (GMT): 2006/263/00:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450157
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4197911
09                 A    =         6726289
93  meter
 Y    =        5116193
87  meter          E    =           
0020548
 Z    =       -1133604
41                 I    =           51
91871
 XDOT =      -3091
444668                 Wp   =           18
19851
 YDOT =       3839
986655  meter/sec      RA   =           58
34409  deg
 ZDOT =       5930
238716                 TA   =          329
41593
                                          MA   =          329
53558
                                          Ha   =            190
274  n
mi
                                          Hp   =            179
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13772674
17                 X    =         4145895
92
 Y    =       16785412
95  feet           Y    =         5162846
33  meter
 Z    =       -3719174
59                 Z    =        -1113337
76
 XDOT =     -10142
535001                 XDOT =       -3162
962016
 YDOT =      12598
381415  feet/sec       YDOT =        3805
016912  meter/sec
 ZDOT =      19456
163766                 ZDOT =        5915
046615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15213950
12                 X    =         4637212
00
 Y    =       15509138
72  feet           Y    =         4727185
48  meter
 Z    =       -3642971
16                 Z    =        -1110377
61
 XDOT =      -7972
606233                 XDOT =       -2430
050380
 YDOT =      12340
281344  feet/sec       YDOT =        3761
317754  meter/sec
 ZDOT =      19400
089552                 ZDOT =        5913
147295


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   06263
02158786  
00020000  00000-0  20000-3 0  9036
2 25544  51
6317  58
9391 0011981   3
1144 357
0093 15
75882311  8122


Satellite: ISS
Catalog Number: 25544
Epoch time:      06263
02158786   =   yrday
fracday
Element set:     903
Inclination:       51
6317  deg
RA of node:        58
9391  deg
Eccentricity:     
0011981     
Arg of perigee:     3
1144  deg
Mean anomaly:     357
0093  deg
Mean motion:   15
75882311  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             812
Checksum:              280


Coasting Arc #5 (Orbit 815)
---------------------------------------

Vector Time (GMT): 2006/263/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5009898
12                 A    =         6719739
07  meter
 Y    =       -1917873
55  meter          E    =           
0018320
 Z    =        4047750
43                 I    =           51
89726
 XDOT =       -630
234408                 Wp   =           37
62592
 YDOT =      -6615
857473  meter/sec      RA   =           57
22555  deg
 ZDOT =      -3891
310511                 TA   =           92
42866
                                          MA   =           92
21891
                                          Ha   =            190
323  n
mi
                                          Hp   =            179
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16436673
63                 X    =        -5007742
98
 Y    =       -6292236
04  feet           Y    =        -1973884
68  meter
 Z    =       13280021
10                 Z    =         4023417
85
 XDOT =      -2067
698190                 XDOT =        -537
304958
 YDOT =     -21705
569136  feet/sec       YDOT =       -6622
385768  meter/sec
 ZDOT =     -12766
766769                 ZDOT =       -3894
146006

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8325312
41                 X    =        -2537555
22
 Y    =       15583711
51  feet           Y    =         4749915
27  meter
 Z    =       13189107
01                 Z    =         4020039
82
 XDOT =     -20647
564385                 XDOT =       -6293
377624
 YDOT =       -150
426821  feet/sec       YDOT =         -45
850095  meter/sec
 ZDOT =     -12778
234581                 ZDOT =       -3894
805900


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   06263
27524283  
00020000  00000-0  20000-3 0  9043
2 25544  51
6355  57
6335 0012175   3
3354 356
7889 15
75901127  8169


Satellite: ISS
Catalog Number: 25544
Epoch time:      06263
27524283   =   yrday
fracday
Element set:     904
Inclination:       51
6355  deg
RA of node:        57
6335  deg
Eccentricity:     
0012175     
Arg of perigee:     3
3354  deg
Mean anomaly:     356
7889  deg
Mean motion:   15
75901127  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             816
Checksum:              294


Coasting Arc #6 (Orbit 831)
---------------------------------------

Vector Time (GMT): 2006/264/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         425763
92                 A    =         6720305
57  meter
 Y    =        5475297
65  meter          E    =           
0016349
 Z    =        3854230
83                 I    =           51
88334
 XDOT =      -6025
416860                 Wp   =           50
55098
 YDOT =      -2451
218421  meter/sec      RA   =           52
14398  deg
 ZDOT =       4146
398215                 TA   =          356
34883
                                          MA   =          356
36074
                                          Ha   =            190
450  n
mi
                                          Hp   =            178
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1396863
24                 X    =          345783
61
 Y    =       17963574
96  feet           Y    =         5479611
89  meter
 Z    =       12645114
27                 Z    =         3856104
48
 XDOT =     -19768
428020                 XDOT =       -6017
701603
 YDOT =      -8042
055186  feet/sec       YDOT =       -2518
554504  meter/sec
 ZDOT =      13603
668683                 ZDOT =        4117
145720

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18000982
62                 X    =         5486699
50
 Y    =         640599
86  feet           Y    =          195254
84  meter
 Z    =       12652842
52                 Z    =         3856586
40
 XDOT =     -10112
366789                 XDOT =       -3082
249397
 YDOT =      17534
647007  feet/sec       YDOT =        5344
560408  meter/sec
 ZDOT =      13494
354286                 ZDOT =        4113
079186


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   06264
28985606  
00020000  00000-0  20000-3 0  9056
2 25544  51
6361  52
4070 0012223   7
2242 352
9096 15
75889842  8323


Satellite: ISS
Catalog Number: 25544
Epoch time:      06264
28985606   =   yrday
fracday
Element set:     905
Inclination:       51
6361  deg
RA of node:        52
4070  deg
Eccentricity:     
0012223     
Arg of perigee:     7
2242  deg
Mean anomaly:     352
9096  deg
Mean motion:   15
75889842  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             832
Checksum:              291


Coasting Arc #7 (Orbit 846)
---------------------------------------

Vector Time (GMT): 2006/265/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5490348
99                 A    =         6722558
12  meter
 Y    =        2290613
76  meter          E    =           
0014741
 Z    =       -3120755
26                 I    =           51
87279
 XDOT =        291
491502                 Wp   =           25
73118
 YDOT =       5942
767286  meter/sec      RA   =           46
95969  deg
 ZDOT =       4896
332320                 TA   =          298
07340
                                          MA   =          298
22236
                                          Ha   =            190
568  n
mi
                                          Hp   =            178
754

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18012956
01                 X    =         5479487
10
 Y    =        7515136
99  feet           Y    =         2351948
88  meter
 Z    =      -10238698
35                 Z    =        -3094109
63
 XDOT =        956
336950                 XDOT =         201
231413
 YDOT =      19497
267999  feet/sec       YDOT =        5945
522653  meter/sec
 ZDOT =      16064
082414                 ZDOT =        4897
528642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9145474
24                 X    =         2787540
55
 Y    =      -17301252
45  feet           Y    =        -5273421
75  meter
 Z    =      -10139121
10                 Z    =        -3090404
11
 XDOT =      18232
604793                 XDOT =        5557
297941
 YDOT =        262
462921  feet/sec       YDOT =          79
998698  meter/sec
 ZDOT =      16069
349332                 ZDOT =        4897
937676


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   06265
24104401  
00020000  00000-0  20000-3 0  9060
2 25544  51
6363  47
5078 0012282   9
7755 350
3646 15
75915295  8470


Satellite: ISS
Catalog Number: 25544
Epoch time:      06265
24104401   =   yrday
fracday
Element set:     906
Inclination:       51
6363  deg
RA of node:        47
5078  deg
Eccentricity:     
0012282     
Arg of perigee:     9
7755  deg
Mean anomaly:     350
3646  deg
Mean motion:   15
75915295  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             847
Checksum:              292


Coasting Arc #8 (Orbit 862)
---------------------------------------

Vector Time (GMT): 2006/266/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =           4162
48                 A    =         6717345
63  meter
 Y    =       -4883588
38  meter          E    =           
0020212
 Z    =       -4630630
30                 I    =           51
83514
 XDOT =       6544
962635                 Wp   =           39
24938
 YDOT =       2783
380720  meter/sec      RA   =           41
87082  deg
 ZDOT =      -2921
137681                 TA   =          201
81168
                                          MA   =          201
89786
                                          Ha   =            190
545  n
mi
                                          Hp   =            178
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          13656
43                 X    =           81266
09
 Y    =      -16022271
59  feet           Y    =        -4883111
12  meter
 Z    =      -15192356
62                 Z    =        -4630422
37
 XDOT =      21472
974524                 XDOT =        6527
542532
 YDOT =       9131
826508  feet/sec       YDOT =        2856
472468  meter/sec
 ZDOT =      -9583
785042                 ZDOT =       -2889
384539

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15969859
10                 X    =        -4867613
05
 Y    =       -1296286
54  feet           Y    =         -395108
14  meter
 Z    =      -15192245
21                 Z    =        -4630596
34
 XDOT =      10622
817785                 XDOT =        3237
834861
 YDOT =     -19617
131380  feet/sec       YDOT =       -5979
301645  meter/sec
 ZDOT =      -9465
118399                 ZDOT =       -2884
968088


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   06266
25563377  
00020000  00000-0  20000-3 0  9074
2 25544  51
6362  42
2815 0012301  13
2725 346
8760 15
75943146  8630


Satellite: ISS
Catalog Number: 25544
Epoch time:      06266
25563377   =   yrday
fracday
Element set:     907
Inclination:       51
6362  deg
RA of node:        42
2815  deg
Eccentricity:     
0012301     
Arg of perigee:    13
2725  deg
Mean anomaly:     346
8760  deg
Mean motion:   15
75943146  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             863
Checksum:              286


Coasting Arc #9 (Orbit 878)
---------------------------------------

Vector Time (GMT): 2006/267/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5926785
94                 A    =         6725052
46  meter
 Y    =       -2520633
88  meter          E    =           
0017896
 Z    =        1934869
94                 I    =           51
83949
 XDOT =        374
295228                 Wp   =           69
21972
 YDOT =      -5238
301048  meter/sec      RA   =           36
69470  deg
 ZDOT =      -5629
744734                 TA   =           89
31598
                                          MA   =           89
11092
                                          Ha   =            190
683  n
mi
                                          Hp   =            178
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19444835
77                 X    =        -5907558
75
 Y    =       -8269796
19  feet           Y    =        -2586802
82  meter
 Z    =        6347998
51                 Z    =         1906124
15
 XDOT =       1228
002718                 XDOT =         460
191456
 YDOT =     -17186
027059  feet/sec       YDOT =       -5233
635647  meter/sec
 ZDOT =     -18470
291121                 ZDOT =       -5627
717324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9379645
01                 X    =        -2858915
80
 Y    =       18970127
15  feet           Y    =         5782094
76  meter
 Z    =        6240575
89                 Z    =         1902127
53
 XDOT =     -15697
168358                 XDOT =       -4784
496916
 YDOT =      -1634
890591  feet/sec       YDOT =        -498
314652  meter/sec
 ZDOT =     -18463
445854                 ZDOT =       -5627
658296


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   06267
27021295  
00020000  00000-0  20000-3 0  9086
2 25544  51
6366  37
0555 0012345  17
8052 342
3542 15
75953300  8797


Satellite: ISS
Catalog Number: 25544
Epoch time:      06267
27021295   =   yrday
fracday
Element set:     908
Inclination:       51
6366  deg
RA of node:        37
0555  deg
Eccentricity:     
0012345     
Arg of perigee:    17
8052  deg
Mean anomaly:     342
3542  deg
Mean motion:   15
75953300  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             879
Checksum:              285


Coasting Arc #10 (Orbit 894)
---------------------------------------

Vector Time (GMT): 2006/268/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -697237
71                 A    =         6715207
93  meter
 Y    =        4292680
58  meter          E    =           
0012080
 Z    =        5107815
07                 I    =           51
78271
 XDOT =      -6983
598514                 Wp   =           42
37134
 YDOT =      -2909
041159  meter/sec      RA   =           31
58562  deg
 ZDOT =       1498
229573                 TA   =           33
35102
                                          MA   =           33
27498
                                          Ha   =            190
810  n
mi
                                          Hp   =            178
039

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2287525
28                 X    =         -770000
49
 Y    =       14083597
71  feet           Y    =         4284477
19  meter
 Z    =       16757923
44                 Z    =         5104250
80
 XDOT =     -22912
068614                 XDOT =       -6957
828425
 YDOT =      -9544
098290  feet/sec       YDOT =       -2986
991438  meter/sec
 ZDOT =       4915
451355                 ZDOT =        1464
365484

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13975467
36                 X    =         4259722
45
 Y    =        2948281
02  feet           Y    =          898636
05  meter
 Z    =       16745221
57                 Z    =         5103943
54
 XDOT =     -10250
281852                 XDOT =       -3124
285908
 YDOT =      21514
394388  feet/sec       YDOT =        6557
587409  meter/sec
 ZDOT =       4788
915537                 ZDOT =        1459
661456


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   06268
28477926  
00020000  00000-0  20000-3 0  9095
2 25544  51
6363  31
8290 0012390  21
2898 338
8779 15
75960599  8957


Satellite: ISS
Catalog Number: 25544
Epoch time:      06268
28477926   =   yrday
fracday
Element set:     909
Inclination:       51
6363  deg
RA of node:        31
8290  deg
Eccentricity:     
0012390     
Arg of perigee:    21
2898  deg
Mean anomaly:     338
8779  deg
Mean motion:   15
75960599  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             895
Checksum:              344


Coasting Arc #11 (Orbit 909)
---------------------------------------

Vector Time (GMT): 2006/269/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6196401
74                 A    =         6726369
50  meter
 Y    =        2500152
00  meter          E    =           
0023063
 Z    =        -659149
31                 I    =           51
79491
 XDOT =      -1253
497896                 Wp   =           31
30121
 YDOT =       4662
477637  meter/sec      RA   =           26
42642  deg
 ZDOT =       6013
656567                 TA   =          321
52193
                                          MA   =          321
68615
                                          Ha   =            190
839  n
mi
                                          Hp   =            177
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20329402
03                 X    =         6171186
25
 Y    =        8202598
42  feet           Y    =         2569302
58  meter
 Z    =       -2162563
35                 Z    =         -629108
00
 XDOT =      -4112
525907                 XDOT =       -1334
755003
 YDOT =      15296
842642  feet/sec       YDOT =        4648
006287  meter/sec
 ZDOT =      19729
844380                 ZDOT =        6007
369361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8674412
62                 X    =         2643960
97
 Y    =      -20144344
51  feet           Y    =        -6139996
21  meter
 Z    =       -2050326
28                 Z    =         -624939
45
 XDOT =      13725
139409                 XDOT =        4183
422492
 YDOT =       3944
036297  feet/sec       YDOT =        1202
142263  meter/sec
 ZDOT =      19707
043963                 ZDOT =        6006
707000


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   06269
23592359  
00020000  00000-0  20000-3 0  9101
2 25544  51
6356  26
9292 0012429  24
1096 336
0647 15
75984161  9104


Satellite: ISS
Catalog Number: 25544
Epoch time:      06269
23592359   =   yrday
fracday
Element set:     910
Inclination:       51
6356  deg
RA of node:        26
9292  deg
Eccentricity:     
0012429     
Arg of perigee:    24
1096  deg
Mean anomaly:     336
0647  deg
Mean motion:   15
75984161  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             910
Checksum:              297


Coasting Arc #12 (Orbit 925)
---------------------------------------

Vector Time (GMT): 2006/270/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1545000
32                 A    =         6714356
63  meter
 Y    =       -3870635
82  meter          E    =           
0023530
 Z    =       -5282153
30                 I    =           51
72766
 XDOT =       7153
370426                 Wp   =           62
28971
 YDOT =       2819
096720  meter/sec      RA   =           21
28921  deg
 ZDOT =         37
396366                 TA   =          208
00183
                                          MA   =          208
12862
                                          Ha   =            190
836  n
mi
                                          Hp   =            177
652

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5068898
68                 X    =         1613827
70
 Y    =      -12698936
42  feet           Y    =        -3852974
08  meter
 Z    =      -17329899
27                 Z    =        -5274480
26
 XDOT =      23469
063078                 XDOT =        7121
133573
 YDOT =       9249
004988  feet/sec       YDOT =        2898
909425  meter/sec
 ZDOT =        122
691488                 ZDOT =          72
069709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12666981
34                 X    =        -3860895
91
 Y    =       -5241802
58  feet           Y    =        -1597701
43  meter
 Z    =      -17301827
02                 Z    =        -5273596
88
 XDOT =       9009
827165                 XDOT =        2746
195320
 YDOT =     -22487
450893  feet/sec       YDOT =       -6854
175032  meter/sec
 ZDOT =        252
223075                 ZDOT =          76
877593


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   06270
25046655  
00020000  00000-0  20000-3 0  9119
2 25544  51
6346  21
7021 0012410  28
1296 332
0536 15
76021086  9261


Satellite: ISS
Catalog Number: 25544
Epoch time:      06270
25046655   =   yrday
fracday
Element set:     911
Inclination:       51
6346  deg
RA of node:        21
7021  deg
Eccentricity:     
0012410     
Arg of perigee:    28
1296  deg
Mean anomaly:     332
0536  deg
Mean motion:   15
76021086  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             926
Checksum:              252


Coasting Arc #13 (Orbit 941)
---------------------------------------

Vector Time (GMT): 2006/271/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6236813
19                 A    =         6726151
94  meter
 Y    =       -2415157
78  meter          E    =           
0013401
 Z    =        -741419
02                 I    =           51
74080
 XDOT =       2340
540158                 Wp   =           79
03266
 YDOT =      -4234
485579  meter/sec      RA   =           16
15326  deg
 ZDOT =      -5983
371659                 TA   =          109
03367
                                          MA   =          108
88846
                                          Ha   =            190
903  n
mi
                                          Hp   =            177
466

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20461985
52                 X    =        -6205741
28
 Y    =       -7923745
98  feet           Y    =        -2484727
55  meter
 Z    =       -2432477
11                 Z    =         -771642
48
 XDOT =       7678
937526                 XDOT =        2416
783441
 YDOT =     -13892
669222  feet/sec       YDOT =       -4207
886111  meter/sec
 ZDOT =     -19630
484446                 ZDOT =       -5971
815891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7696284
79                 X    =        -2345827
60
 Y    =       20534940
71  feet           Y    =         6259049
93  meter
 Z    =       -2545379
53                 Z    =         -775831
68
 XDOT =     -12480
586567                 XDOT =       -3804
082786
 YDOT =      -7071
198623  feet/sec       YDOT =       -2155
301340  meter/sec
 ZDOT =     -19587
991876                 ZDOT =       -5970
419924


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   06271
26499770  
00020000  00000-0  20000-3 0  9122
2 25544  51
6347  16
4762 0012412  31
8731 328
3182 15
76024350  9422


Satellite: ISS
Catalog Number: 25544
Epoch time:      06271
26499770   =   yrday
fracday
Element set:     912
Inclination:       51
6347  deg
RA of node:        16
4762  deg
Eccentricity:     
0012412     
Arg of perigee:    31
8731  deg
Mean anomaly:     328
3182  deg
Mean motion:   15
76024350  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             942
Checksum:              276


Coasting Arc #14 (Orbit 957)
---------------------------------------

Vector Time (GMT): 2006/272/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2540460
77                 A    =         6715207
31  meter
 Y    =        3588540
42  meter          E    =           
0017273
 Z    =        5069172
58                 I    =           51
67577
 XDOT =      -7047
007092                 Wp   =           40
60944
 YDOT =      -2674
306822  meter/sec      RA   =           10
98486  deg
 ZDOT =      -1622
518525                 TA   =           65
04009
                                          MA   =           64
86074
                                          Ha   =            191
017  n
mi
                                          Hp   =            177
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8334845
04                 X    =        -2605024
97
 Y    =       11773426
58  feet           Y    =         3559770
56  meter
 Z    =       16631143
62                 Z    =         5056674
04
 XDOT =     -23120
102007                 XDOT =       -7008
696863
 YDOT =      -8773
972513  feet/sec       YDOT =       -2752
896144  meter/sec
 ZDOT =      -5323
223507                 ZDOT =       -1656
660316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12006971
87                 X    =         3659725
03
 Y    =        8089924
17  feet           Y    =         2465808
89  meter
 Z    =       16585050
70                 Z    =         5055123
45
 XDOT =      -7527
080660                 XDOT =       -2294
254185
 YDOT =      22453
857871  feet/sec       YDOT =        6843
935879  meter/sec
 ZDOT =      -5450
758736                 ZDOT =       -1661
391263


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   06272
27951611  
00020000  00000-0  20000-3 0  9132
2 25544  51
6342  11
2487 0012371  35
6426 324
5562 15
76041283  9582


Satellite: ISS
Catalog Number: 25544
Epoch time:      06272
27951611   =   yrday
fracday
Element set:     913
Inclination:       51
6342  deg
RA of node:        11
2487  deg
Eccentricity:     
0012371     
Arg of perigee:    35
6426  deg
Mean anomaly:     324
5562  deg
Mean motion:   15
76041283  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             958
Checksum:              276

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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