Date: September 30th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 960)
---------------------------------------

Vector Time (GMT): 2006/272/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6594876
84                 A    =         6725442
88  meter
 Y    =       -1309498
73  meter          E    =           
0015731
 Z    =        -189925
66                 I    =           51
71082
 XDOT =       1084
763094                 Wp   =           87
26535
 YDOT =      -4649
296893  meter/sec      RA   =            9
95295  deg
 ZDOT =      -6038
178288                 TA   =           94
79629
                                          MA   =           94
61664
                                          Ha   =            190
378  n
mi
                                          Hp   =            176
794

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21636735
04                 X    =        -6578821
06
 Y    =       -4296255
67  feet           Y    =        -1383156
52  meter
 Z    =        -623115
68                 Z    =         -221924
99
 XDOT =       3558
934035                 XDOT =        1166
004311
 YDOT =     -15253
598731  feet/sec       YDOT =       -4636
712184  meter/sec
 ZDOT =     -19810
296220                 ZDOT =       -6032
711138

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19753404
86                 X    =         6020837
80
 Y    =        9810509
17  feet           Y    =         2990243
20  meter
 Z    =        -742492
84                 Z    =         -226311
82
 XDOT =      -6818
563071                 XDOT =       -2078
298024
 YDOT =      12320
386024  feet/sec       YDOT =        3755
253660  meter/sec
 ZDOT =     -19790
534540                 ZDOT =       -6032
154928


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
46883213  
00020000  00000-0  20000-3 0  9001
2 25544  51
6372  10
2699 0011969  39
6340 320
5697 15
76359565  9614


Satellite: ISS
Catalog Number: 25544
Epoch time:      06272
46883213   =   yrday
fracday
Element set:     900
Inclination:       51
6372  deg
RA of node:        10
2699  deg
Eccentricity:     
0011969     
Arg of perigee:    39
6340  deg
Mean anomaly:     320
5697  deg
Mean motion:   15
76359565  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             961
Checksum:              307


Coasting Arc #2 (Orbit 976)
---------------------------------------

Vector Time (GMT): 2006/273/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1590215
22                 A    =         6713736
30  meter
 Y    =        3970133
15  meter          E    =           
0015970
 Z    =        5167304
76                 I    =           51
64421
 XDOT =      -7477
780617                 Wp   =           45
66188
 YDOT =      -1517
717201  meter/sec      RA   =            4
79049  deg
 ZDOT =      -1122
063348                 TA   =           55
10532
                                          MA   =           54
95532
                                          Ha   =            190
496  n
mi
                                          Hp   =            176
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5217241
55                 X    =        -1659593
66
 Y    =       13025371
22  feet           Y    =         3951962
51  meter
 Z    =       16953099
60                 Z    =         5159410
94
 XDOT =     -24533
400976                 XDOT =       -7454
802700
 YDOT =      -4979
387144  feet/sec       YDOT =       -1601
209397  meter/sec
 ZDOT =      -3681
310196                 ZDOT =       -1158
334922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8342200
93                 X    =         2542702
84
 Y    =      -11325474
44  feet           Y    =        -3452004
61  meter
 Z    =       16924207
61                 Z    =         5158498
48
 XDOT =      21717
730384                 XDOT =        6619
564221
 YDOT =      10229
279814  feet/sec       YDOT =        3117
884487  meter/sec
 ZDOT =      -3816
635348                 ZDOT =       -1163
310454


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   06273
48314018  
00020000  00000-0  20000-3 0  9017
2 25544  51
6380   5
0425 0012093  43
1430 317
0680 15
76391976  9773


Satellite: ISS
Catalog Number: 25544
Epoch time:      06273
48314018   =   yrday
fracday
Element set:     901
Inclination:       51
6380  deg
RA of node:         5
0425  deg
Eccentricity:     
0012093     
Arg of perigee:    43
1430  deg
Mean anomaly:     317
0680  deg
Mean motion:   15
76391976  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             977
Checksum:              272


Coasting Arc #3 (Orbit 992)
---------------------------------------

Vector Time (GMT): 2006/274/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6339674
14                 A    =         6723938
03  meter
 Y    =        1340987
95  meter          E    =           
0025960
 Z    =        1742004
17                 I    =           51
65096
 XDOT =      -2538
907132                 Wp   =           56
51307
 YDOT =       4529
596678  meter/sec      RA   =          359
66371  deg
 ZDOT =       5706
448565                 TA   =          322
81852
                                          MA   =          322
99802
                                          Ha   =            190
437  n
mi
                                          Hp   =            176
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20799455
83                 X    =         6315745
46
 Y    =        4399566
76  feet           Y    =         1411747
90  meter
 Z    =        5715236
79                 Z    =         1772744
33
 XDOT =      -8329
747809                 XDOT =       -2617
090034
 YDOT =      14860
881488  feet/sec       YDOT =        4500
768058  meter/sec
 ZDOT =      18721
944110                 ZDOT =        5693
924600

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19213113
75                 X    =        -5856157
07
 Y    =       -9028043
78  feet           Y    =        -2751747
74  meter
 Z    =        5829937
17                 Z    =         1776964
85
 XDOT =      10946
823278                 XDOT =        3336
591735
 YDOT =     -11139
838227  feet/sec       YDOT =       -3395
422691  meter/sec
 ZDOT =      18675
874687                 ZDOT =        5692
406605


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   06274
49742641  
00020000  00000-0  20000-3 0  9027
2 25544  51
6384 359
8151 0012151  47
2069 313
0115 15
76419936  9935


Satellite: ISS
Catalog Number: 25544
Epoch time:      06274
49742641   =   yrday
fracday
Element set:     902
Inclination:       51
6384  deg
RA of node:       359
8151  deg
Eccentricity:     
0012151     
Arg of perigee:    47
2069  deg
Mean anomaly:     313
0115  deg
Mean motion:   15
76419936  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             993
Checksum:              294


Coasting Arc #4 (Orbit 1007)
---------------------------------------

Vector Time (GMT): 2006/275/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2821370
71                 A    =         6715856
49  meter
 Y    =       -3968475
41  meter          E    =           
0019850
 Z    =       -4639991
63                 I    =           51
59574
 XDOT =       6954
576376                 Wp   =           77
62842
 YDOT =       1609
705183  meter/sec      RA   =          354
47099  deg
 ZDOT =       2866
475727                 TA   =          220
69007
                                          MA   =          220
83854
                                          Ha   =            190
463  n
mi
                                          Hp   =            176
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9256465
57                 X    =         2888077
33
 Y    =      -13019932
45  feet           Y    =        -3936552
38  meter
 Z    =      -15223069
64                 Z    =        -4626123
29
 XDOT =      22816
851628                 XDOT =        6922
134707
 YDOT =       5281
184982  feet/sec       YDOT =        1687
293765  meter/sec
 ZDOT =       9404
447923                 ZDOT =        2900
182285

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11884849
30                 X    =        -3622502
07
 Y    =       10747365
09  feet           Y    =         3275796
88  meter
 Z    =      -15171919
65                 Z    =        -4624401
11
 XDOT =     -20346
978107                 XDOT =       -6201
758927
 YDOT =      -9113
914640  feet/sec       YDOT =       -2777
921182  meter/sec
 ZDOT =       9530
240063                 ZDOT =        2904
817171


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   06275
44830036  
00020000  00000-0  20000-3 0  9030
2 25544  51
6385 354
9150 0012145  50
5358 309
6879 15
76468139 10087


Satellite: ISS
Catalog Number: 25544
Epoch time:      06275
44830036   =   yrday
fracday
Element set:     903
Inclination:       51
6385  deg
RA of node:       354
9150  deg
Eccentricity:     
0012145     
Arg of perigee:    50
5358  deg
Mean anomaly:     309
6879  deg
Mean motion:   15
76468139  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1008
Checksum:              299


Coasting Arc #5 (Orbit 1023)
---------------------------------------

Vector Time (GMT): 2006/276/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5705314
00                 A    =         6720520
82  meter
 Y    =       -1530457
19  meter          E    =           
0015915
 Z    =       -3224935
38                 I    =           51
58370
 XDOT =       3919
681869                 Wp   =           65
06724
 YDOT =      -4585
451534  meter/sec      RA   =          349
36013  deg
 ZDOT =      -4770
046426                 TA   =          152
63694
                                          MA   =          152
55303
                                          Ha   =            190
478  n
mi
                                          Hp   =            175
982

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18718221
80                 X    =        -5672110
02
 Y    =       -5021185
01  feet           Y    =        -1594071
66  meter
 Z    =      -10580496
64                 Z    =        -3252571
09
 XDOT =      12859
848653                 XDOT =        3993
837746
 YDOT =     -15044
132330  feet/sec       YDOT =       -4541
205063  meter/sec
 ZDOT =     -15649
758614                 ZDOT =       -4750
824273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17323531
98                 X    =         5280212
55
 Y    =        8560702
03  feet           Y    =         2609301
98  meter
 Z    =      -10683663
03                 Z    =        -3256380
49
 XDOT =     -15004
960564                 XDOT =       -4573
511980
 YDOT =      10969
770107  feet/sec       YDOT =        3343
585929  meter/sec
 ZDOT =     -15578
745907                 ZDOT =       -4748
401753


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   06276
46254511  
00020000  00000-0  20000-3 0  9042
2 25544  51
6385 349
6867 0012152  54
2802 305
9491 15
76477021 10243


Satellite: ISS
Catalog Number: 25544
Epoch time:      06276
46254511   =   yrday
fracday
Element set:     904
Inclination:       51
6385  deg
RA of node:       349
6867  deg
Eccentricity:     
0012152     
Arg of perigee:    54
2802  deg
Mean anomaly:     305
9491  deg
Mean motion:   15
76477021  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1024
Checksum:              287


Coasting Arc #6 (Orbit 1039)
---------------------------------------

Vector Time (GMT): 2006/277/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3950411
30                 A    =         6719516
03  meter
 Y    =        4077704
24  meter          E    =           
0023712
 Z    =        3581729
66                 I    =           51
55251
 XDOT =      -6020
899510                 Wp   =           71
70723
 YDOT =      -1931
066916  meter/sec      RA   =          344
14937  deg
 ZDOT =      -4411
076784                 TA   =           65
34899
                                          MA   =           65
10222
                                          Ha   =            190
596  n
mi
                                          Hp   =            175
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12960667
00                 X    =        -4013114
60
 Y    =       13378294
76  feet           Y    =         4033178
22  meter
 Z    =       11751081
55                 Z    =         3562385
91
 XDOT =     -19753
607317                 XDOT =       -5977
430292
 YDOT =      -6335
521378  feet/sec       YDOT =       -1998
153222  meter/sec
 ZDOT =     -14472
036693                 ZDOT =       -4440
220665

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15198090
41                 X    =         4632377
96
 Y    =      -10846734
78  feet           Y    =        -3306084
76  meter
 Z    =       11679553
50                 Z    =         3559927
91
 XDOT =      17441
101002                 XDOT =        5316
047585
 YDOT =       8626
922313  feet/sec       YDOT =        2629
485921  meter/sec
 ZDOT =     -14580
875966                 ZDOT =       -4444
250994


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   06277
47676854  
00020000  00000-0  20000-3 0  9053
2 25544  51
6384 344
4590 0012338  57
9053 302
3307 15
76510603 10401


Satellite: ISS
Catalog Number: 25544
Epoch time:      06277
47676854   =   yrday
fracday
Element set:     905
Inclination:       51
6384  deg
RA of node:       344
4590  deg
Eccentricity:     
0012338     
Arg of perigee:    57
9053  deg
Mean anomaly:     302
3307  deg
Mean motion:   15
76510603  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1040
Checksum:              286


Coasting Arc #7 (Orbit 1055)
---------------------------------------

Vector Time (GMT): 2006/278/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4729974
94                 A    =         6716460
54  meter
 Y    =        1896820
88  meter          E    =           
0019653
 Z    =        4356700
63                 I    =           51
51611
 XDOT =      -5029
023443                 Wp   =           82
02565
 YDOT =       4790
565365  meter/sec      RA   =          339
03724  deg
 ZDOT =       3364
001982                 TA   =          334
08613
                                          MA   =          334
18442
                                          Ha   =            190
353  n
mi
                                          Hp   =            175
704

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15518290
49                 X    =         4687248
66
 Y    =        6223165
60  feet           Y    =         1949475
59  meter
 Z    =       14293637
24                 Z    =         4379575
07
 XDOT =     -16499
420744                 XDOT =       -5098
560281
 YDOT =      15717
077968  feet/sec       YDOT =        4733
939549  meter/sec
 ZDOT =      11036
751911                 ZDOT =        3339
401451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14235876
75                 X    =        -4339095
23
 Y    =       -8627521
60  feet           Y    =        -2629668
58  meter
 Z    =       14379112
62                 Z    =         4382753
53
 XDOT =      18245
326415                 XDOT =        5561
175491
 YDOT =     -11807
643980  feet/sec       YDOT =       -3598
969885  meter/sec
 ZDOT =      10945
739278                 ZDOT =        3336
261332


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   06278
49096853  
00020000  00000-0  20000-3 0  9062
2 25544  51
6384 339
2307 0012234  61
4419 298
7975 15
76571166 10567


Satellite: ISS
Catalog Number: 25544
Epoch time:      06278
49096853   =   yrday
fracday
Element set:     906
Inclination:       51
6384  deg
RA of node:       339
2307  deg
Eccentricity:     
0012234     
Arg of perigee:    61
4419  deg
Mean anomaly:     298
7975  deg
Mean motion:   15
76571166  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1056
Checksum:              321


Coasting Arc #8 (Orbit 1070)
---------------------------------------

Vector Time (GMT): 2006/279/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4719681
61                 A    =         6722888
94  meter
 Y    =       -4256198
55  meter          E    =           
0018266
 Z    =       -2186273
83                 I    =           51
51077
 XDOT =       4786
061707                 Wp   =           56
19654
 YDOT =       2510
162541  meter/sec      RA   =          333
83024  deg
 ZDOT =       5487
985117                 TA   =          279
24680
                                          MA   =          279
45335
                                          Ha   =            190
565  n
mi
                                          Hp   =            175
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15484519
72                 X    =         4777544
91
 Y    =      -13963906
00  feet           Y    =        -4203097
13  meter
 Z    =       -7172814
39                 Z    =        -2163204
32
 XDOT =      15702
302188                 XDOT =        4730
976980
 YDOT =       8235
441406  feet/sec       YDOT =        2563
375473  meter/sec
 ZDOT =      18005
200515                 ZDOT =        5511
102093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17372845
63                 X    =        -5295243
35
 Y    =       11582863
73  feet           Y    =         3530456
86  meter
 Z    =       -7087438
94                 Z    =        -2160251
39
 XDOT =     -13409
606306                 XDOT =       -4087
248002
 YDOT =      -9129
329217  feet/sec       YDOT =       -2782
619545  meter/sec
 ZDOT =      18091
658825                 ZDOT =        5514
337610


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   06279
44176364  
00020000  00000-0  20000-3 0  9075
2 25544  51
6378 334
3301 0012312  63
9857 296
2574 15
76548589 10718


Satellite: ISS
Catalog Number: 25544
Epoch time:      06279
44176364   =   yrday
fracday
Element set:     907
Inclination:       51
6378  deg
RA of node:       334
3301  deg
Eccentricity:     
0012312     
Arg of perigee:    63
9857  deg
Mean anomaly:     296
2574  deg
Mean motion:   15
76548589  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1071
Checksum:              315


Coasting Arc #9 (Orbit 1086)
---------------------------------------

Vector Time (GMT): 2006/280/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3570255
81                 A    =         6713492
41  meter
 Y    =       -2576569
45  meter          E    =           
0026090
 Z    =       -5091256
81                 I    =           51
45354
 XDOT =       5718
163452                 Wp   =           73
34686
 YDOT =      -4902
226146  meter/sec      RA   =          328
69583  deg
 ZDOT =      -1528
079593                 TA   =          181
92040
                                          MA   =          181
93044
                                          Ha   =            190
509  n
mi
                                          Hp   =            175
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11713437
70                 X    =        -3516445
98
 Y    =       -8453311
83  feet           Y    =        -2616193
58  meter
 Z    =      -16703598
45                 Z    =        -5108470
56
 XDOT =      18760
378781                 XDOT =        5779
979127
 YDOT =     -16083
419115  feet/sec       YDOT =       -4837
936969  meter/sec
 ZDOT =      -5013
384493                 ZDOT =       -1500
149620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10453893
81                 X    =         3186346
83
 Y    =        9860082
27  feet           Y    =         3005353
08  meter
 Z    =      -16768070
45                 Z    =        -5110907
87
 XDOT =     -19958
598971                 XDOT =       -6083
380966
 YDOT =      12805
694658  feet/sec       YDOT =        3903
175732  meter/sec
 ZDOT =      -4909
990215                 ZDOT =       -1496
565018


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   06280
45592343  
00020000  00000-0  20000-3 0  9088
2 25544  51
6368 329
1012 0012306  68
2353 292
0120 15
76587287 10876


Satellite: ISS
Catalog Number: 25544
Epoch time:      06280
45592343   =   yrday
fracday
Element set:     908
Inclination:       51
6368  deg
RA of node:       329
1012  deg
Eccentricity:     
0012306     
Arg of perigee:    68
2353  deg
Mean anomaly:     292
0120  deg
Mean motion:   15
76587287  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1087
Checksum:              286


Coasting Arc #10 (Orbit 1102)
---------------------------------------

Vector Time (GMT): 2006/281/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5177148
47                 A    =         6724564
79  meter
 Y    =        4262535
79  meter          E    =           
0022226
 Z    =         437192
50                 I    =           51
46772
 XDOT =      -3371
816389                 Wp   =          101
45427
 YDOT =      -3453
549526  meter/sec      RA   =          323
51008  deg
 ZDOT =      -6004
445208                 TA   =           73
77533
                                          MA   =           73
53089
                                          Ha   =            190
509  n
mi
                                          Hp   =            175
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16985395
23                 X    =        -5226551
81
 Y    =       13984697
48  feet           Y    =         4204365
84  meter
 Z    =        1434358
58                 Z    =          411921
05
 XDOT =     -11062
389728                 XDOT =       -3303
778474
 YDOT =     -11330
543063  feet/sec       YDOT =       -3490
874944  meter/sec
 ZDOT =     -19699
623387                 ZDOT =       -6020
660452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18426731
28                 X    =         5616467
69
 Y    =      -12032899
84  feet           Y    =        -3667627
87  meter
 Z    =        1340781
50                 Z    =          408670
20
 XDOT =       8764
839929                 XDOT =        2671
523210
 YDOT =      11121
536131  feet/sec       YDOT =        3389
844213  meter/sec
 ZDOT =     -19760
489606                 ZDOT =       -6022
997232


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   06281
47006119  
00020000  00000-0  20000-3 0  9093
2 25544  51
6365 323
8720 0012539  71
7449 288
5079 15
76654042 11039


Satellite: ISS
Catalog Number: 25544
Epoch time:      06281
47006119   =   yrday
fracday
Element set:     909
Inclination:       51
6365  deg
RA of node:       323
8720  deg
Eccentricity:     
0012539     
Arg of perigee:    71
7449  deg
Mean anomaly:     288
5079  deg
Mean motion:   15
76654042  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1103
Checksum:              294


Coasting Arc #11 (Orbit 1118)
---------------------------------------

Vector Time (GMT): 2006/282/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2341893
81                 A    =         6712476
56  meter
 Y    =        3492768
71  meter          E    =           
0015137
 Z    =        5219827
84                 I    =           51
40543
 XDOT =      -6015
756837                 Wp   =           73
37987
 YDOT =       4806
106528  meter/sec      RA   =          318
33902  deg
 ZDOT =       -511
449463                 TA   =           21
51636
                                          MA   =           21
45281
                                          Ha   =            190
334  n
mi
                                          Hp   =            175
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7683378
64                 X    =         2277305
50
 Y    =       11459214
91  feet           Y    =         3518596
03  meter
 Z    =       17125419
43                 Z    =         5231048
09
 XDOT =     -19736
735031                 XDOT =       -6066
567686
 YDOT =      15768
066036  feet/sec       YDOT =        4738
550894  meter/sec
 ZDOT =      -1677
983802                 ZDOT =        -540
798277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6493092
90                 X    =        -1979094
72
 Y    =      -12113562
16  feet           Y    =        -3692213
75  meter
 Z    =       17167680
70                 Z    =         5232709
08
 XDOT =      20221
456239                 XDOT =        6163
499862
 YDOT =     -13396
692839  feet/sec       YDOT =       -4083
311977  meter/sec
 ZDOT =      -1786
683090                 ZDOT =        -544
581006


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   06282
48417551  
00020000  00000-0  20000-3 0  9103
2 25544  51
6365 318
6427 0012375  75
4072 284
8464 15
76708682 11190


Satellite: ISS
Catalog Number: 25544
Epoch time:      06282
48417551   =   yrday
fracday
Element set:     910
Inclination:       51
6365  deg
RA of node:       318
6427  deg
Eccentricity:     
0012375     
Arg of perigee:    75
4072  deg
Mean anomaly:     284
8464  deg
Mean motion:   15
76708682  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1119
Checksum:              305


Coasting Arc #12 (Orbit 1134)
---------------------------------------

Vector Time (GMT): 2006/283/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 450477
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5214441
31                 A    =         6723786
46  meter
 Y    =       -4016704
50  meter          E    =           
0026399
 Z    =        1320580
35                 I    =           51
42239
 XDOT =       2052
839434                 Wp   =           68
43806
 YDOT =       4609
604063  meter/sec      RA   =          313
18395  deg
 ZDOT =       5831
378109                 TA   =          306
13563
                                          MA   =          306
37965
                                          Ha   =            190
556  n
mi
                                          Hp   =            175
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17107747
07                 X    =         5252553
81
 Y    =      -13178164
36  feet           Y    =        -3958180
64  meter
 Z    =        4332612
70                 Z    =         1346005
25
 XDOT =       6735
037512                 XDOT =        1972
813194
 YDOT =      15123
372909  feet/sec       YDOT =        4632
112564  meter/sec
 ZDOT =      19131
817942                 ZDOT =        5841
156674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18031207
95                 X    =        -5495912
18
 Y    =       11848607
52  feet           Y    =         3611455
57  meter
 Z    =        4426804
52                 Z    =         1349290
02
 XDOT =      -4602
746081                 XDOT =       -1402
917005
 YDOT =     -14266
322929  feet/sec       YDOT =       -4348
375229  meter/sec
 ZDOT =      19168
854388                 ZDOT =        5842
666818


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   06283
49827201  
00020000  00000-0  20000-3 0  9113
2 25544  51
6360 313
4134 0012723  78
6121 281
6472 15
76678904 11355


Satellite: ISS
Catalog Number: 25544
Epoch time:      06283
49827201   =   yrday
fracday
Element set:     911
Inclination:       51
6360  deg
RA of node:       313
4134  deg
Eccentricity:     
0012723     
Arg of perigee:    78
6121  deg
Mean anomaly:     281
6472  deg
Mean motion:   15
76678904  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1135
Checksum:              280

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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