Date: October 10th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7427 1 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 1118)
---------------------------------------

Vector Time (GMT): 2006/282/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2266242
75                 A    =         6712380
66  meter
 Y    =        3552524
16  meter          E    =           
0015530
 Z    =        5212552
95                 I    =           51
40411
 XDOT =      -6054
311672                 Wp   =           73
04363
 YDOT =       4747
790796  meter/sec      RA   =          318
34192  deg
 ZDOT =       -597
629674                 TA   =           22
67719
                                          MA   =           22
60865
                                          Ha   =            190
369  n
mi
                                          Hp   =            175
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7435179
62                 X    =         2201027
21
 Y    =       11655263
00  feet           Y    =         3577502
01  meter
 Z    =       17101551
66                 Z    =         5223404
15
 XDOT =     -19863
227271                 XDOT =       -6104
048902
 YDOT =      15576
741458  feet/sec       YDOT =        4679
810022  meter/sec
 ZDOT =      -1960
727276                 ZDOT =        -627
163183

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6227913
17                 X    =        -1898267
93
 Y    =      -12285754
48  feet           Y    =        -3744697
97  meter
 Z    =       17142446
01                 Z    =         5225017
54
 XDOT =      20315
544088                 XDOT =        6192
177838
 YDOT =     -13213
944822  feet/sec       YDOT =       -4027
610382  meter/sec
 ZDOT =      -2070
122333                 ZDOT =        -630
973287


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
48403028  
00020000  00000-0  20000-3 0  9006
2 25544  51
6351 318
6473 0012657  75
6042 284
6526 15
76754467 11197


Satellite: ISS
Catalog Number: 25544
Epoch time:      06282
48403028   =   yrday
fracday
Element set:     900
Inclination:       51
6351  deg
RA of node:       318
6473  deg
Eccentricity:     
0012657     
Arg of perigee:    75
6042  deg
Mean anomaly:     284
6526  deg
Mean motion:   15
76754467  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1119
Checksum:              295


Coasting Arc #2 (Orbit 1134)
---------------------------------------

Vector Time (GMT): 2006/283/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5244685
86                 A    =         6723534
29  meter
 Y    =       -3946265
04  meter          E    =           
0026754
 Z    =        1408018
38                 I    =           51
42059
 XDOT =       1948
730501                 Wp   =           69
21835
 YDOT =       4689
053496  meter/sec      RA   =          313
18785  deg
 ZDOT =       5804
176840                 TA   =          306
34538
                                          MA   =          306
59202
                                          Ha   =            190
579  n
mi
                                          Hp   =            174
887

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17206974
59                 X    =         5281583
68
 Y    =      -12947063
77  feet           Y    =        -3887409
76  meter
 Z    =        4619482
88                 Z    =         1433587
25
 XDOT =       6393
472772                 XDOT =        1867
955727
 YDOT =      15384
033778  feet/sec       YDOT =        4710
393608  meter/sec
 ZDOT =      19042
574933                 ZDOT =        5813
447814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18111095
69                 X    =        -5520261
97
 Y    =       11610787
92  feet           Y    =         3538968
16  meter
 Z    =        4714220
36                 Z    =         1436894
37
 XDOT =      -4260
286239                 XDOT =       -1298
535246
 YDOT =     -14494
621206  feet/sec       YDOT =       -4417
960543  meter/sec
 ZDOT =      19077
730808                 ZDOT =        5814
892350


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
49809593  
00020000  00000-0  20000-3 0  9016
2 25544  51
6346 313
4176 0013007  78
8718 281
3909 15
76730261 11352


Satellite: ISS
Catalog Number: 25544
Epoch time:      06283
49809593   =   yrday
fracday
Element set:     901
Inclination:       51
6346  deg
RA of node:       313
4176  deg
Eccentricity:     
0013007     
Arg of perigee:    78
8718  deg
Mean anomaly:     281
3909  deg
Mean motion:   15
76730261  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1135
Checksum:              300


Coasting Arc #3 (Orbit 1149)
---------------------------------------

Vector Time (GMT): 2006/284/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1164209
17                 A    =         6714513
00  meter
 Y    =       -4646294
61  meter          E    =           
0023671
 Z    =       -4726515
84                 I    =           51
37243
 XDOT =       5910
678518                 Wp   =           94
43478
 YDOT =      -4150
806377  meter/sec      RA   =          307
97858  deg
 ZDOT =       2633
999408                 TA   =          201
52786
                                          MA   =          201
62756
                                          Ha   =            190
497  n
mi
                                          Hp   =            174
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3819583
91                 X    =        -1089206
15
 Y    =      -15243748
72  feet           Y    =        -4658893
98  meter
 Z    =      -15506941
74                 Z    =        -4731989
59
 XDOT =      19391
989890                 XDOT =        5943
858380
 YDOT =     -13618
131157  feet/sec       YDOT =       -4084
524433  meter/sec
 ZDOT =       8641
730342                 ZDOT =        2662
794533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2836466
78                 X    =          864555
07
 Y    =       15435793
18  feet           Y    =         4704829
76  meter
 Z    =      -15527945
25                 Z    =        -4732917
71
 XDOT =     -18981
415592                 XDOT =       -5785
535472
 YDOT =      12257
297345  feet/sec       YDOT =        3736
024231  meter/sec
 ZDOT =       8748
467485                 ZDOT =        2666
532889


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   06284
44875572  
00020000  00000-0  20000-3 0  9023
2 25544  51
6348 308
5143 0012957  82
4321 277
8315 15
76790966 11503


Satellite: ISS
Catalog Number: 25544
Epoch time:      06284
44875572   =   yrday
fracday
Element set:     902
Inclination:       51
6348  deg
RA of node:       308
5143  deg
Eccentricity:     
0012957     
Arg of perigee:    82
4321  deg
Mean anomaly:     277
8315  deg
Mean motion:   15
76790966  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1150
Checksum:              308


Coasting Arc #4 (Orbit 1165)
---------------------------------------

Vector Time (GMT): 2006/285/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5033451
64                 A    =         6719699
73  meter
 Y    =        3171040
56  meter          E    =           
0017537
 Z    =       -3139761
14                 I    =           51
37489
 XDOT =       -750
324420                 Wp   =           89
83029
 YDOT =      -5945
548747  meter/sec      RA   =          302
84760  deg
 ZDOT =      -4825
065173                 TA   =          126
85730
                                          MA   =          126
69638
                                          Ha   =            190
439  n
mi
                                          Hp   =            174
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16513948
97                 X    =        -5053283
95
 Y    =       10403676
37  feet           Y    =         3114642
90  meter
 Z    =      -10301053
60                 Z    =        -3164262
09
 XDOT =      -2461
694291                 XDOT =        -660
345079
 YDOT =     -19506
393526  feet/sec       YDOT =       -5953
436076  meter/sec
 ZDOT =     -15830
266314                 ZDOT =       -4828
491879

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16872257
00                 X    =         5142663
93
 Y    =       -9715632
59  feet           Y    =        -2961324
81  meter
 Z    =      -10391925
95                 Z    =        -3167459
03
 XDOT =        858
638385                 XDOT =         261
712980
 YDOT =      18357
262066  feet/sec       YDOT =        5595
293478  meter/sec
 ZDOT =     -15843
815406                 ZDOT =       -4829
194936


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   06285
46276941  
00020000  00000-0  20000-3 0  9032
2 25544  51
6354 303
2838 0013083  86
4400 273
8261 15
76851320 11661


Satellite: ISS
Catalog Number: 25544
Epoch time:      06285
46276941   =   yrday
fracday
Element set:     903
Inclination:       51
6354  deg
RA of node:       303
2838  deg
Eccentricity:     
0013083     
Arg of perigee:    86
4400  deg
Mean anomaly:     273
8261  deg
Mean motion:   15
76851320  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1166
Checksum:              285


Coasting Arc #5 (Orbit 1181)
---------------------------------------

Vector Time (GMT): 2006/286/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         233992
82                 A    =         6718395
70  meter
 Y    =        5683217
09  meter          E    =           
0025188
 Z    =        3554483
93                 I    =           51
35557
 XDOT =      -5562
352594                 Wp   =           88
07082
 YDOT =       3010
022114  meter/sec      RA   =          297
61913  deg
 ZDOT =      -4418
798205                 TA   =           49
20182
                                          MA   =           48
98359
                                          Ha   =            190
355  n
mi
                                          Hp   =            174
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         767692
97                 X    =          153157
69
 Y    =       18645725
37  feet           Y    =         5685381
70  meter
 Z    =       11661692
69                 Z    =         3555424
43
 XDOT =     -18249
188301                 XDOT =       -5574
131734
 YDOT =       9875
400635  feet/sec       YDOT =        2947
755020  meter/sec
 ZDOT =     -14497
369438                 ZDOT =       -4445
848944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -254051
79                 X    =          -77434
99
 Y    =      -18657133
55  feet           Y    =        -5686694
31  meter
 Z    =       11665947
41                 Z    =         3555780
77
 XDOT =      17040
968406                 XDOT =        5194
087170
 YDOT =      -9416
583075  feet/sec       YDOT =       -2870
174521  meter/sec
 ZDOT =     -14597
767857                 ZDOT =       -4449
399643


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   06286
47675623  
00020000  00000-0  20000-3 0  9045
2 25544  51
6345 298
0538 0013044  89
8684 270
3975 15
76906267 11820


Satellite: ISS
Catalog Number: 25544
Epoch time:      06286
47675623   =   yrday
fracday
Element set:     904
Inclination:       51
6345  deg
RA of node:       298
0538  deg
Eccentricity:     
0013044     
Arg of perigee:    89
8684  deg
Mean anomaly:     270
3975  deg
Mean motion:   15
76906267  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1182
Checksum:              327


Coasting Arc #6 (Orbit 1197)
---------------------------------------

Vector Time (GMT): 2006/287/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4641960
14                 A    =         6715216
24  meter
 Y    =       -1961969
30  meter          E    =           
0021991
 Z    =        4421851
12                 I    =           51
33270
 XDOT =       -117
205905                 Wp   =          101
01888
 YDOT =       7013
165955  meter/sec      RA   =          292
48994  deg
 ZDOT =       3217
129064                 TA   =          316
62190
                                          MA   =          316
79477
                                          Ha   =            190
303  n
mi
                                          Hp   =            174
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15229528
03                 X    =         4642073
45
 Y    =       -6436907
15  feet           Y    =        -1910059
71  meter
 Z    =       14507385
57                 Z    =         4444402
19
 XDOT =       -384
533809                 XDOT =        -211
247730
 YDOT =      23009
074654  feet/sec       YDOT =        7011
329468  meter/sec
 ZDOT =      10554
885380                 ZDOT =        3216
331270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15193174
60                 X    =        -4630879
62
 Y    =        6332619
45  feet           Y    =         1930182
41  meter
 Z    =       14591158
63                 Z    =         4447385
15
 XDOT =       1062
955294                 XDOT =         323
988773
 YDOT =     -21897
466158  feet/sec       YDOT =       -6674
347685  meter/sec
 ZDOT =      10552
844752                 ZDOT =        3216
507080


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   06287
49071838  
00020000  00000-0  20000-3 0  9057
2 25544  51
6341 292
8235 0013212  93
9200 266
3475 15
76921918 11986


Satellite: ISS
Catalog Number: 25544
Epoch time:      06287
49071838   =   yrday
fracday
Element set:     905
Inclination:       51
6341  deg
RA of node:       292
8235  deg
Eccentricity:     
0013212     
Arg of perigee:    93
9200  deg
Mean anomaly:     266
3475  deg
Mean motion:   15
76921918  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1198
Checksum:              305


Coasting Arc #7 (Orbit 1212)
---------------------------------------

Vector Time (GMT): 2006/288/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         382651
64                 A    =         6722024
73  meter
 Y    =       -6429794
78  meter          E    =           
0017853
 Z    =       -1929699
86                 I    =           51
34773
 XDOT =       5109
256005                 Wp   =           78
10355
 YDOT =      -1360
973691  meter/sec      RA   =          287
26907  deg
 ZDOT =       5595
158037                 TA   =          260
33599
                                          MA   =          260
53771
                                          Ha   =            190
267  n
mi
                                          Hp   =            174
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1255418
75                 X    =          463896
24
 Y    =      -21095127
24  feet           Y    =        -6425061
53  meter
 Z    =       -6331036
30                 Z    =        -1927643
50
 XDOT =      16762
650936                 XDOT =        5096
914443
 YDOT =      -4465
136783  feet/sec       YDOT =       -1303
908089  meter/sec
 ZDOT =      18356
817707                 ZDOT =        5619
948988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1072622
98                 X    =         -326935
48
 Y    =       21107250
42  feet           Y    =         6433489
93  meter
 Z    =       -6324235
13                 Z    =        -1927626
87
 XDOT =     -15074
942122                 XDOT =       -4594
842359
 YDOT =       4715
218827  feet/sec       YDOT =        1437
198698  meter/sec
 ZDOT =      18449
019670                 ZDOT =        5623
261195


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   06288
44128287  
00020000  00000-0  20000-3 0  9065
2 25544  51
6350 287
9205 0013192  97
8037 262
4626 15
76998549 12133


Satellite: ISS
Catalog Number: 25544
Epoch time:      06288
44128287   =   yrday
fracday
Element set:     906
Inclination:       51
6350  deg
RA of node:       287
9205  deg
Eccentricity:     
0013192     
Arg of perigee:    97
8037  deg
Mean anomaly:     262
4626  deg
Mean motion:   15
76998549  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1213
Checksum:              320


Coasting Arc #8 (Orbit 1228)
---------------------------------------

Vector Time (GMT): 2006/289/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4299338
16                 A    =         6711990
58  meter
 Y    =         303245
55  meter          E    =           
0027123
 Z    =       -5168610
80                 I    =           51
30600
 XDOT =        747
774778                 Wp   =           90
98026
 YDOT =      -7573
875606  meter/sec      RA   =          282
11463  deg
 ZDOT =      -1071
680928                 TA   =          168
75889
                                          MA   =          168
69818
                                          Ha   =            190
218  n
mi
                                          Hp   =            174
349

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14105440
16                 X    =        -4277301
21
 Y    =         994900
09  feet           Y    =          255291
02  meter
 Z    =      -16957384
52                 Z    =        -5189443
61
 XDOT =       2453
329325                 XDOT =         837
617396
 YDOT =     -24848
673247  feet/sec       YDOT =       -7565
011272  meter/sec
 ZDOT =      -3516
013542                 ZDOT =       -1067
829747

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13978930
31                 X    =         4260777
96
 Y    =       -1380261
13  feet           Y    =         -420703
59  meter
 Z    =      -17034980
04                 Z    =        -5192261
92
 XDOT =      -1888
662199                 XDOT =        -575
664238
 YDOT =      23887
907181  feet/sec       YDOT =        7281
034109  meter/sec
 ZDOT =      -3502
685844                 ZDOT =       -1067
618645


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   06289
45519208  
00020000  00000-0  20000-3 0  9075
2 25544  51
6345 282
6893 0013047 101
4523 258
8108 15
76986391 12296


Satellite: ISS
Catalog Number: 25544
Epoch time:      06289
45519208   =   yrday
fracday
Element set:     907
Inclination:       51
6345  deg
RA of node:       282
6893  deg
Eccentricity:     
0013047     
Arg of perigee:   101
4523  deg
Mean anomaly:     258
8108  deg
Mean motion:   15
76986391  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1229
Checksum:              313


Coasting Arc #9 (Orbit 1244)
---------------------------------------

Vector Time (GMT): 2006/290/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -888102
68                 A    =         6723545
90  meter
 Y    =        6655983
40  meter          E    =           
0024358
 Z    =         -99004
75                 I    =           51
33948
 XDOT =      -4764
259538                 Wp   =          119
57870
 YDOT =       -708
583487  meter/sec      RA   =          276
92420  deg
 ZDOT =      -6018
515627                 TA   =           61
50308
                                          MA   =           61
25799
                                          Ha   =            190
157  n
mi
                                          Hp   =            174
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2913722
69                 X    =         -961983
85
 Y    =       21837215
88  feet           Y    =         6645639
05  meter
 Z    =        -324818
74                 Z    =         -103498
97
 XDOT =     -15630
772761                 XDOT =       -4726
744838
 YDOT =      -2324
748974  feet/sec       YDOT =        -761
650606  meter/sec
 ZDOT =     -19745
786177                 ZDOT =       -6041
569452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1932687
09                 X    =          589083
02
 Y    =      -21945568
03  feet           Y    =        -6689009
13  meter
 Z    =        -340659
77                 Z    =         -103833
10
 XDOT =      14009
639592                 XDOT =        4270
138148
 YDOT =       1487
345943  feet/sec       YDOT =         453
343043  meter/sec
 ZDOT =     -19831
797696                 ZDOT =       -6044
731938


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   06290
46907422  
00020000  00000-0  20000-3 0  9088
2 25544  51
6331 277
4577 0013176 105
0954 255
1670 15
77038078 12456


Satellite: ISS
Catalog Number: 25544
Epoch time:      06290
46907422   =   yrday
fracday
Element set:     908
Inclination:       51
6331  deg
RA of node:       277
4577  deg
Eccentricity:     
0013176     
Arg of perigee:   105
0954  deg
Mean anomaly:     255
1670  deg
Mean motion:   15
77038078  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1245
Checksum:              296


Coasting Arc #10 (Orbit 1260)
---------------------------------------

Vector Time (GMT): 2006/291/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4051531
03                 A    =         6711812
27  meter
 Y    =        1534968
70  meter          E    =           
0015890
 Z    =        5112248
58                 I    =           51
29770
 XDOT =      -1243
449982                 Wp   =           96
31340
 YDOT =       7511
416863  meter/sec      RA   =          271
72986  deg
 ZDOT =      -1268
238347                 TA   =            5
85016
                                          MA   =            5
83162
                                          Ha   =            189
905  n
mi
                                          Hp   =            174
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13292424
65                 X    =         4009230
98
 Y    =        5035986
56  feet           Y    =         1580038
95  meter
 Z    =       16772469
08                 Z    =         5131828
33
 XDOT =      -4079
560310                 XDOT =       -1321
190319
 YDOT =      24643
756113  feet/sec       YDOT =        7497
077176  meter/sec
 ZDOT =      -4160
886966                 ZDOT =       -1274
468368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13485971
79                 X    =        -4110524
20
 Y    =       -4209290
24  feet           Y    =        -1282991
67  meter
 Z    =       16845648
50                 Z    =         5134553
66
 XDOT =       2216
725792                 XDOT =         675
658021
 YDOT =     -23864
192619  feet/sec       YDOT =       -7273
805910  meter/sec
 ZDOT =      -4183
073341                 ZDOT =       -1275
000754


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   06291
48292773  
00020000  00000-0  20000-3 0  9098
2 25544  51
6324 272
2263 0013053 108
7363 251
5219 15
77096832 12610


Satellite: ISS
Catalog Number: 25544
Epoch time:      06291
48292773   =   yrday
fracday
Element set:     909
Inclination:       51
6324  deg
RA of node:       272
2263  deg
Eccentricity:     
0013053     
Arg of perigee:   108
7363  deg
Mean anomaly:     251
5219  deg
Mean motion:   15
77096832  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1261
Checksum:              290


Coasting Arc #11 (Orbit 1276)
---------------------------------------

Vector Time (GMT): 2006/292/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1293770
61                 A    =         6721311
49  meter
 Y    =       -6251849
35  meter          E    =           
0025210
 Z    =        2080137
96                 I    =           51
33066
 XDOT =       4592
377412                 Wp   =           90
33625
 YDOT =       2805
838631  meter/sec      RA   =          266
57760  deg
 ZDOT =       5518
978319                 TA   =          293
04073
                                          MA   =          293
30638
                                          Ha   =            189
865  n
mi
                                          Hp   =            174
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4244654
23                 X    =         1353478
39
 Y    =      -20511316
75  feet           Y    =        -6237047
72  meter
 Z    =        6824599
61                 Z    =         2086568
62
 XDOT =      15066
855025                 XDOT =        4533
850143
 YDOT =       9205
507318  feet/sec       YDOT =        2856
866234  meter/sec
 ZDOT =      18106
884250                 ZDOT =        5541
146146

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2572445
56                 X    =         -784081
41
 Y    =       20779746
33  feet           Y    =         6333666
68  meter
 Z    =        6847702
56                 Z    =         2087179
74
 XDOT =     -14132
181213                 XDOT =       -4307
488834
 YDOT =      -7805
891383  feet/sec       YDOT =       -2379
235693  meter/sec
 ZDOT =      18189
885365                 ZDOT =        5544
277059


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   06292
49675291  
00020000  00000-0  20000-3 0  9102
2 25544  51
6323 266
9955 0012993 113
0659 247
1877 15
77160195 12778


Satellite: ISS
Catalog Number: 25544
Epoch time:      06292
49675291   =   yrday
fracday
Element set:     910
Inclination:       51
6323  deg
RA of node:       266
9955  deg
Eccentricity:     
0012993     
Arg of perigee:   113
0659  deg
Mean anomaly:     247
1877  deg
Mean motion:   15
77160195  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1277
Checksum:              322


Coasting Arc #12 (Orbit 1291)
---------------------------------------

Vector Time (GMT): 2006/293/10:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3981890
77                 A    =         6715140
09  meter
 Y    =       -3316657
78  meter          E    =           
0021742
 Z    =       -4293002
85                 I    =           51
31262
 XDOT =       1794
649283                 Wp   =          113
83590
 YDOT =      -6626
656314  meter/sec      RA   =          261
35018  deg
 ZDOT =       3460
151500                 TA   =          191
35072
                                          MA   =          191
39984
                                          Ha   =            189
849  n
mi
                                          Hp   =            174
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13063946
09                 X    =        -3923652
39
 Y    =      -10881423
17  feet           Y    =        -3360860
11  meter
 Z    =      -14084655
01                 Z    =        -4312205
65
 XDOT =       5887
956965                 XDOT =        1851
806921
 YDOT =     -21740
998407  feet/sec       YDOT =       -6606
267770  meter/sec
 ZDOT =      11352
203085                 ZDOT =        3469
009318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13972349
66                 X    =         4258772
18
 Y    =        9581830
11  feet           Y    =         2920541
82  meter
 Z    =      -14156678
32                 Z    =        -4314955
55
 XDOT =      -3008
412567                 XDOT =        -916
964150
 YDOT =      21181
717386  feet/sec       YDOT =        6456
187459  meter/sec
 ZDOT =      11384
297502                 ZDOT =        3469
933878


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   06293
44719003  
00020000  00000-0  20000-3 0  9119
2 25544  51
6321 262
0902 0012959 115
9110 244
3392 15
77147500 12923


Satellite: ISS
Catalog Number: 25544
Epoch time:      06293
44719003   =   yrday
fracday
Element set:     911
Inclination:       51
6321  deg
RA of node:       262
0902  deg
Eccentricity:     
0012959     
Arg of perigee:   115
9110  deg
Mean anomaly:     244
3392  deg
Mean motion:   15
77147500  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1292
Checksum:              264

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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