Date: September 29th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6081 61 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 930)
---------------------------------------

Vector Time (GMT): 2006/270/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4235070
34                 A    =         6721499
84  meter
 Y    =       -4167935
10  meter          E    =           
0014517
 Z    =       -3162237
23                 I    =           51
74811
 XDOT =       5617
014305                 Wp   =           48
10187
 YDOT =      -2038
889007  meter/sec      RA   =           19
73495  deg
 ZDOT =      -4840
026758                 TA   =          168
64222
                                          MA   =          168
60943
                                          Ha   =            190
551  n
mi
                                          Hp   =            177
215

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13894587
74                 X    =        -4172787
30
 Y    =      -13674327
77  feet           Y    =        -4214945
83  meter
 Z    =      -10374794
06                 Z    =        -3182660
21
 XDOT =      18428
524623                 XDOT =        5662
908383
 YDOT =      -6689
268395  feet/sec       YDOT =       -1975
819936  meter/sec
 ZDOT =     -15879
352879                 ZDOT =       -4812
627279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17743130
33                 X    =         5408106
13
 Y    =        7976987
11  feet           Y    =         2431385
67  meter
 Z    =      -10451419
18                 Z    =        -3185592
57
 XDOT =     -14429
484544                 XDOT =       -4398
106889
 YDOT =      11443
654656  feet/sec       YDOT =        3488
025939  meter/sec
 ZDOT =     -15777
556007                 ZDOT =       -4808
999071


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
56687201  
00020000  00000-0  20000-3 0  9009
2 25544  51
6371  20
0715 0012201  31
5505 328
6389 15
76203053  9319


Satellite: ISS
Catalog Number: 25544
Epoch time:      06270
56687201   =   yrday
fracday
Element set:     900
Inclination:       51
6371  deg
RA of node:        20
0715  deg
Eccentricity:     
0012201     
Arg of perigee:    31
5505  deg
Mean anomaly:     328
6389  deg
Mean motion:   15
76203053  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             931
Checksum:              250


Coasting Arc #2 (Orbit 946)
---------------------------------------

Vector Time (GMT): 2006/271/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5344574
31                 A    =         6719888
07  meter
 Y    =        1646824
77  meter          E    =           
0022041
 Z    =        3719304
76                 I    =           51
71545
 XDOT =      -4425
991519                 Wp   =           58
71710
 YDOT =      -4635
847561  meter/sec      RA   =           14
53800  deg
 ZDOT =      -4277
624806                 TA   =           76
41410
                                          MA   =           76
16870
                                          Ha   =            190
714  n
mi
                                          Hp   =            177
031

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17534692
63                 X    =        -5380660
12
 Y    =        5402968
40  feet           Y    =         1586857
02  meter
 Z    =       12202443
45                 Z    =         3693252
74
 XDOT =     -14520
969549                 XDOT =       -4353
043615
 YDOT =     -15209
473626  feet/sec       YDOT =       -4684
933588  meter/sec
 ZDOT =     -14034
202119                 ZDOT =       -4298
949415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14409133
92                 X    =         4391904
02
 Y    =      -11462468
86  feet           Y    =        -3493760
51  meter
 Z    =       12105610
54                 Z    =         3689790
09
 XDOT =      18167
191939                 XDOT =        5537
360103
 YDOT =       7827
202847  feet/sec       YDOT =        2385
731428  meter/sec
 ZDOT =     -14114
245412                 ZDOT =       -4302
022002


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
58127367  
00020000  00000-0  20000-3 0  9015
2 25544  51
6370  14
8446 0012403  35
3920 324
8065 15
76236964  9470


Satellite: ISS
Catalog Number: 25544
Epoch time:      06271
58127367   =   yrday
fracday
Element set:     901
Inclination:       51
6370  deg
RA of node:        14
8446  deg
Eccentricity:     
0012403     
Arg of perigee:    35
3920  deg
Mean anomaly:     324
8065  deg
Mean motion:   15
76236964  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             947
Checksum:              287


Coasting Arc #3 (Orbit 962)
---------------------------------------

Vector Time (GMT): 2006/272/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3415920
99                 A    =         6717837
61  meter
 Y    =        3943234
51  meter          E    =           
0018506
 Z    =        4213151
52                 I    =           51
68153
 XDOT =      -6567
680101                 Wp   =           68
39135
 YDOT =       1811
145642  meter/sec      RA   =            9
44031  deg
 ZDOT =       3623
858151                 TA   =          344
81427
                                          MA   =          344
86975
                                          Ha   =            190
558  n
mi
                                          Hp   =            176
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11207089
87                 X    =         3351106
33
 Y    =       12937121
10  feet           Y    =         3981070
80  meter
 Z    =       13822675
60                 Z    =         4229588
87
 XDOT =     -21547
506894                 XDOT =       -6605
048725
 YDOT =       5942
078878  feet/sec       YDOT =        1737
493239  meter/sec
 ZDOT =      11889
298397                 ZDOT =        3591
861207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15223958
68                 X    =        -4640262
60
 Y    =       -7712860
26  feet           Y    =        -2350879
81  meter
 Z    =       13884422
76                 Z    =         4231972
06
 XDOT =      17149
492161                 XDOT =        5227
165211
 YDOT =     -12626
872905  feet/sec       YDOT =       -3848
670862  meter/sec
 ZDOT =      11770
335664                 ZDOT =        3587
598310


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
59565438  
00020000  00000-0  20000-3 0  9023
2 25544  51
6371   9
6172 0012338  38
8220 321
3828 15
76287691  9637


Satellite: ISS
Catalog Number: 25544
Epoch time:      06272
59565438   =   yrday
fracday
Element set:     902
Inclination:       51
6371  deg
RA of node:         9
6172  deg
Eccentricity:     
0012338     
Arg of perigee:    38
8220  deg
Mean anomaly:     321
3828  deg
Mean motion:   15
76287691  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             963
Checksum:              302


Coasting Arc #4 (Orbit 977)
---------------------------------------

Vector Time (GMT): 2006/273/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6034250
77                 A    =         6723019
34  meter
 Y    =       -1548301
97  meter          E    =           
0017784
 Z    =       -2517842
32                 I    =           51
67001
 XDOT =       3347
718983                 Wp   =           43
42268
 YDOT =       4461
514115  meter/sec      RA   =            4
24397  deg
 ZDOT =       5314
347802                 TA   =          288
04323
                                          MA   =          288
23692
                                          Ha   =            190
790  n
mi
                                          Hp   =            176
696

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19797410
67                 X    =         6063346
94
 Y    =       -5079730
87  feet           Y    =        -1480660
93  meter
 Z    =       -8260637
53                 Z    =        -2488457
03
 XDOT =      10983
329998                 XDOT =        3271
764553
 YDOT =      14637
513501  feet/sec       YDOT =        4498
525427  meter/sec
 ZDOT =      17435
524285                 ZDOT =        5330
426704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16191223
41                 X    =        -4935084
89
 Y    =       12545070
86  feet           Y    =         3823737
60  meter
 Z    =       -8151364
87                 Z    =        -2484536
01
 XDOT =     -14891
499125                 XDOT =       -4538
928933
 YDOT =      -7926
375709  feet/sec       YDOT =       -2415
959316  meter/sec
 ZDOT =      17496
005555                 ZDOT =        5332
782493


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
54662066  
00020000  00000-0  20000-3 0  9035
2 25544  51
6366   4
7176 0012475  41
6205 318
5906 15
76271480  9788


Satellite: ISS
Catalog Number: 25544
Epoch time:      06273
54662066   =   yrday
fracday
Element set:     903
Inclination:       51
6366  deg
RA of node:         4
7176  deg
Eccentricity:     
0012475     
Arg of perigee:    41
6205  deg
Mean anomaly:     318
5906  deg
Mean motion:   15
76271480  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             978
Checksum:              295


Coasting Arc #5 (Orbit 993)
---------------------------------------

Vector Time (GMT): 2006/274/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2340367
56                 A    =         6714888
74  meter
 Y    =       -3897371
57  meter          E    =           
0024615
 Z    =       -4964051
04                 I    =           51
61392
 XDOT =       7206
956860                 Wp   =           60
26265
 YDOT =      -1725
044411  meter/sec      RA   =          359
12905  deg
 ZDOT =      -2039
014984                 TA   =          189
93053
                                          MA   =          189
97926
                                          Ha   =            190
755  n
mi
                                          Hp   =            176
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7678371
27                 X    =        -2272498
11
 Y    =      -12786652
15  feet           Y    =        -3923163
38  meter
 Z    =      -16286256
70                 Z    =        -4975255
74
 XDOT =      23644
871587                 XDOT =        7235
616116
 YDOT =      -5659
594524  feet/sec       YDOT =       -1644
291985  meter/sec
 ZDOT =      -6689
681705                 ZDOT =       -2003
933829

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12192088
31                 X    =         3716148
52
 Y    =        8510628
15  feet           Y    =         2594039
46  meter
 Z    =      -16328509
01                 Z    =        -4976929
55
 XDOT =     -18608
931671                 XDOT =       -5672
002373
 YDOT =      14046
283848  feet/sec       YDOT =        4281
307317  meter/sec
 ZDOT =      -6559
207385                 ZDOT =       -1999
246411


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
56096531  
00020000  00000-0  20000-3 0  9047
2 25544  51
6360 359
4898 0012488  45
7533 314
4654 15
76302069  9947


Satellite: ISS
Catalog Number: 25544
Epoch time:      06274
56096531   =   yrday
fracday
Element set:     904
Inclination:       51
6360  deg
RA of node:       359
4898  deg
Eccentricity:     
0012488     
Arg of perigee:    45
7533  deg
Mean anomaly:     314
4654  deg
Mean motion:   15
76302069  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             994
Checksum:              316


Coasting Arc #6 (Orbit 1009)
---------------------------------------

Vector Time (GMT): 2006/275/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6481972
44                 A    =         6725042
96  meter
 Y    =        1479777
29  meter          E    =           
0020931
 Z    =         995077
40                 I    =           51
62064
 XDOT =      -1956
433676                 Wp   =           88
21395
 YDOT =      -4512
497871  meter/sec      RA   =          353
94779  deg
 ZDOT =      -5926
261310                 TA   =           80
90239
                                          MA   =           80
66562
                                          Ha   =            190
806  n
mi
                                          Hp   =            176
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21266313
78                 X    =        -6502871
67
 Y    =        4854912
36  feet           Y    =         1407175
45  meter
 Z    =        3264689
64                 Z    =          963537
14
 XDOT =      -6418
745655                 XDOT =       -1877
040146
 YDOT =     -14804
783040  feet/sec       YDOT =       -4533
931998  meter/sec
 ZDOT =     -19443
114533                 ZDOT =       -5935
572744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17148669
57                 X    =         5226914
49
 Y    =      -13509317
15  feet           Y    =        -4117639
87  meter
 Z    =        3147372
90                 Z    =          959319
26
 XDOT =      11062
818826                 XDOT =        3371
947178
 YDOT =       9419
827949  feet/sec       YDOT =        2871
163559  meter/sec
 ZDOT =     -19478
397693                 ZDOT =       -5937
015617


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
57528997  
00020000  00000-0  20000-3 0  9056
2 25544  51
6363 354
2619 0012745  49
3870 310
8400 15
76369842 10105


Satellite: ISS
Catalog Number: 25544
Epoch time:      06275
57528997   =   yrday
fracday
Element set:     905
Inclination:       51
6363  deg
RA of node:       354
2619  deg
Eccentricity:     
0012745     
Arg of perigee:    49
3870  deg
Mean anomaly:     310
8400  deg
Mean motion:   15
76369842  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1010
Checksum:              303


Coasting Arc #7 (Orbit 1025)
---------------------------------------

Vector Time (GMT): 2006/276/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1068341
97                 A    =         6713246
91  meter
 Y    =        4035018
07  meter          E    =           
0014393
 Z    =        5246974
40                 I    =           51
55328
 XDOT =      -7524
958560                 Wp   =           59
46024
 YDOT =       1685
896977  meter/sec      RA   =          348
80191  deg
 ZDOT =        242
393882                 TA   =           28
27976
                                          MA   =           28
20169
                                          Ha   =            190
738  n
mi
                                          Hp   =            176
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3505058
95                 X    =          997653
56
 Y    =       13238248
25  feet           Y    =         4046569
87  meter
 Z    =       17214482
95                 Z    =         5251992
52
 XDOT =     -24688
184251                 XDOT =       -7544
428729
 YDOT =       5531
158061  feet/sec       YDOT =        1601
639869  meter/sec
 ZDOT =        795
255518                 ZDOT =         205
790234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8934459
76                 X    =        -2723223
34
 Y    =      -10346481
45  feet           Y    =        -3153607
54  meter
 Z    =       17233711
98                 Z    =         5252835
41
 XDOT =      18912
581959                 XDOT =        5764
554981
 YDOT =     -15270
327584  feet/sec       YDOT =       -4654
395848  meter/sec
 ZDOT =        659
100973                 ZDOT =         200
893977


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
58959424  
00020000  00000-0  20000-3 0  9062
2 25544  51
6363 349
0343 0012626  52
9791 307
2527 15
76407584 10264


Satellite: ISS
Catalog Number: 25544
Epoch time:      06276
58959424   =   yrday
fracday
Element set:     906
Inclination:       51
6363  deg
RA of node:       349
0343  deg
Eccentricity:     
0012626     
Arg of perigee:    52
9791  deg
Mean anomaly:     307
2527  deg
Mean motion:   15
76407584  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1026
Checksum:              308


Coasting Arc #8 (Orbit 1041)
---------------------------------------

Vector Time (GMT): 2006/277/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6531868
61                 A    =         6725301
13  meter
 Y    =       -1437410
18  meter          E    =           
0026307
 Z    =         579490
61                 I    =           51
56542
 XDOT =        511
711320                 Wp   =           53
35132
 YDOT =       4814
719017  meter/sec      RA   =          343
64655  deg
 ZDOT =       6003
236278                 TA   =          312
97546
                                          MA   =          313
19573
                                          Ha   =            190
982  n
mi
                                          Hp   =            175
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21430015
13                 X    =         6544641
40
 Y    =       -4715912
66  feet           Y    =        -1364295
74  meter
 Z    =        1901215
92                 Z    =          611253
66
 XDOT =       1678
842915                 XDOT =         428
671704
 YDOT =      15796
322234  feet/sec       YDOT =        4819
977409  meter/sec
 ZDOT =      19695
657080                 ZDOT =        6005
520114

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16857754
33                 X    =        -5138243
52
 Y    =       14029906
79  feet           Y    =         4276315
59  meter
 Z    =        2019365
59                 Z    =          615502
63
 XDOT =      -7629
164550                 XDOT =       -2325
369355
 YDOT =     -12079
377430  feet/sec       YDOT =       -3681
794241  meter/sec
 ZDOT =      19704
806248                 ZDOT =        6006
024944


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
60388314  
00020000  00000-0  20000-3 0  9071
2 25544  51
6359 343
8066 0013013  56
3161 303
9242 15
76367275 10420


Satellite: ISS
Catalog Number: 25544
Epoch time:      06277
60388314   =   yrday
fracday
Element set:     907
Inclination:       51
6359  deg
RA of node:       343
8066  deg
Eccentricity:     
0013013     
Arg of perigee:    56
3161  deg
Mean anomaly:     303
9242  deg
Mean motion:   15
76367275  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1042
Checksum:              283


Coasting Arc #9 (Orbit 1056)
---------------------------------------

Vector Time (GMT): 2006/278/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         180454
96                 A    =         6714108
92  meter
 Y    =       -4412714
54  meter          E    =           
0024761
 Z    =       -5077281
80                 I    =           51
50143
 XDOT =       7360
485736                 Wp   =           81
44780
 YDOT =      -1532
884585  meter/sec      RA   =          338
46519  deg
 ZDOT =       1604
116152                 TA   =          203
95761
                                          MA   =          204
07302
                                          Ha   =            190
904  n
mi
                                          Hp   =            175
717

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         592043
82                 X    =          254449
86
 Y    =      -14477409
92  feet           Y    =        -4410283
35  meter
 Z    =      -16657748
68                 Z    =        -5076224
99
 XDOT =      24148
575248                 XDOT =        7369
287043
 YDOT =      -5029
148900  feet/sec       YDOT =       -1450
526191  meter/sec
 ZDOT =       5262
848268                 ZDOT =        1639
895209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6269885
79                 X    =         1911061
19
 Y    =       13066979
56  feet           Y    =         3982815
37  meter
 Z    =      -16654401
29                 Z    =        -5076261
51
 XDOT =     -17888
786021                 XDOT =       -5452
501979
 YDOT =      15417
924345  feet/sec       YDOT =        4699
383340  meter/sec
 ZDOT =       5395
942747                 ZDOT =        1644
683349


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
55475658  
00020000  00000-0  20000-3 0  9085
2 25544  51
6361 338
9052 0012903  60
0085 300
2358 15
76420203 10572


Satellite: ISS
Catalog Number: 25544
Epoch time:      06278
55475658   =   yrday
fracday
Element set:     908
Inclination:       51
6361  deg
RA of node:       338
9052  deg
Eccentricity:     
0012903     
Arg of perigee:    60
0085  deg
Mean anomaly:     300
2358  deg
Mean motion:   15
76420203  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1057
Checksum:              279


Coasting Arc #10 (Orbit 1072)
---------------------------------------

Vector Time (GMT): 2006/279/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6246316
70                 A    =         6722909
41  meter
 Y    =        1170352
02  meter          E    =           
0015922
 Z    =       -2209817
29                 I    =           51
50634
 XDOT =        924
580625                 Wp   =           84
73996
 YDOT =      -5331
601959  meter/sec      RA   =          333
33435  deg
 ZDOT =      -5469
439264                 TA   =          120
07154
                                          MA   =          119
91355
                                          Ha   =            190
891  n
mi
                                          Hp   =            175
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20493165
02                 X    =        -6248204
44
 Y    =        3839737
59  feet           Y    =         1100491
47  meter
 Z    =       -7250056
72                 Z    =        -2240167
05
 XDOT =       3033
401002                 XDOT =        1010
700575
 YDOT =     -17492
132411  feet/sec       YDOT =       -5320
781791  meter/sec
 ZDOT =     -17944
354540                 ZDOT =       -5464
737882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15951719
30                 X    =         4862084
04
 Y    =      -13364358
60  feet           Y    =        -4073456
50  meter
 Z    =       -7362967
51                 Z    =        -2244232
50
 XDOT =       4860
896180                 XDOT =        1481
601156
 YDOT =      15621
493641  feet/sec       YDOT =        4761
431262  meter/sec
 ZDOT =     -17927
553506                 ZDOT =       -5464
318309


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
56900423  
00020000  00000-0  20000-3 0  9091
2 25544  51
6363 333
6766 0013075  64
0762 296
1748 15
76486243 10735


Satellite: ISS
Catalog Number: 25544
Epoch time:      06279
56900423   =   yrday
fracday
Element set:     909
Inclination:       51
6363  deg
RA of node:       333
6766  deg
Eccentricity:     
0013075     
Arg of perigee:    64
0762  deg
Mean anomaly:     296
1748  deg
Mean motion:   15
76486243  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1073
Checksum:              308


Coasting Arc #11 (Orbit 1088)
---------------------------------------

Vector Time (GMT): 2006/280/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1360324
95                 A    =         6716739
35  meter
 Y    =        4924177
57  meter          E    =           
0022611
 Z    =        4347579
96                 I    =           51
45962
 XDOT =      -6851
188246                 Wp   =           68
31685
 YDOT =       1100
832662  meter/sec      RA   =          328
12422  deg
 ZDOT =      -3368
305768                 TA   =           55
72830
                                          MA   =           55
51438
                                          Ha   =            190
890  n
mi
                                          Hp   =            175
352

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4463008
38                 X    =        -1436406
90
 Y    =       16155438
23  feet           Y    =         4908540
61  meter
 Z    =       14263713
78                 Z    =         4340786
16
 XDOT =     -22477
651727                 XDOT =       -6846
625736
 YDOT =       3611
655716  feet/sec       YDOT =        1024
244121  meter/sec
 ZDOT =     -11050
871941                 ZDOT =       -3401
578560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4232086
52                 X    =        -1289939
97
 Y    =      -16239110
37  feet           Y    =        -4949680
84  meter
 Z    =       14239062
36                 Z    =         4340066
21
 XDOT =      16345
492463                 XDOT =        4982
106103
 YDOT =     -14122
191703  feet/sec       YDOT =       -4304
444031  meter/sec
 ZDOT =     -11174
678005                 ZDOT =       -3406
041856


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
58323131  
00020000  00000-0  20000-3 0  9102
2 25544  51
6350 328
4483 0013071  67
4790 292
7757 15
76534722 10898


Satellite: ISS
Catalog Number: 25544
Epoch time:      06280
58323131   =   yrday
fracday
Element set:     910
Inclination:       51
6350  deg
RA of node:       328
4483  deg
Eccentricity:     
0013071     
Arg of perigee:    67
4790  deg
Mean anomaly:     292
7757  deg
Mean motion:   15
76534722  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1089
Checksum:              292


Coasting Arc #12 (Orbit 1104)
---------------------------------------

Vector Time (GMT): 2006/281/13:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465611
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5631978
83                 A    =         6719322
42  meter
 Y    =        -672378
06  meter          E    =           
0024810
 Z    =        3578217
13                 I    =           51
44452
 XDOT =      -2099
548647                 Wp   =           81
93197
 YDOT =       5977
918609  meter/sec      RA   =          323
00609  deg
 ZDOT =       4405
419188                 TA   =          321
09125
                                          MA   =          321
26955
                                          Ha   =            190
899  n
mi
                                          Hp   =            175
202

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18477620
84                 X    =         5621696
10
 Y    =       -2205964
75  feet           Y    =         -609455
46  meter
 Z    =       11739557
52                 Z    =         3605553
03
 XDOT =      -6888
282962                 XDOT =       -2187
639790
 YDOT =      19612
593862  feet/sec       YDOT =        5953
947968  meter/sec
 ZDOT =      14453
475027                 ZDOT =        4395
005049

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14587756
46                 X    =        -4446348
17
 Y    =       11449317
42  feet           Y    =         3489751
95  meter
 Z    =       11841302
95                 Z    =         3609229
14
 XDOT =      -3398
394820                 XDOT =       -1035
830741
 YDOT =     -19314
628971  feet/sec       YDOT =       -5887
098910  meter/sec
 ZDOT =      14415
473751                 ZDOT =        4393
836399


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
59744112  
00020000  00000-0  20000-3 0  9111
2 25544  51
6345 323
2194 0013299  71
5600 288
7009 15
76520869 11053


Satellite: ISS
Catalog Number: 25544
Epoch time:      06281
59744112   =   yrday
fracday
Element set:     911
Inclination:       51
6345  deg
RA of node:       323
2194  deg
Eccentricity:     
0013299     
Arg of perigee:    71
5600  deg
Mean anomaly:     288
7009  deg
Mean motion:   15
76520869  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1105
Checksum:              286

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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