Date: September 22nd 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 3875 01 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


263/05:38:00 000 0 0 0 0 0 0
N/A 0 0 0 0 190 3
000/00:00:00 000 0 0 0 0 179 1

Coasting Arc #1 (Orbit 806)
---------------------------------------

Vector Time (GMT): 2006/262/15:45:24
000
Vector Time (MET): N/A
Weight (LBS)     : 465373
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3460279
09                 A    =         6714537
64  meter
 Y    =        2287919
64  meter          E    =           
0011531
 Z    =        5277282
12                 I    =           51
88826
 XDOT =      -3993
758216                 Wp   =           12
82529
 YDOT =      -6586
962469  meter/sec      RA   =           60
21787  deg
 ZDOT =        247
949113                 TA   =           74
89508
                                          MA   =           74
76754
                                          Ha   =            190
051  n
mi
                                          Hp   =            179
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11352621
67                 X    =        -3511241
64
 Y    =        7506298
04  feet           Y    =         2248940
24  meter
 Z    =       17313917
72                 Z    =         5260348
29
 XDOT =     -13102
881285                 XDOT =       -3921
009553
 YDOT =     -21610
769256  feet/sec       YDOT =       -6631
216113  meter/sec
 ZDOT =        813
481342                 ZDOT =         228
724662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         648932
46                 X    =          197794
61
 Y    =      -13673889
27  feet           Y    =        -4167801
45  meter
 Z    =       17251142
42                 Z    =         5258148
21
 XDOT =      24191
707564                 XDOT =        7373
632466
 YDOT =       2037
566661  feet/sec       YDOT =         621
050318  meter/sec
 ZDOT =        740
959902                 ZDOT =         225
844578


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06262
70449562  
00020000  00000-0  20000-3 0  9002
2 25544  51
6349  60
5710 0011689   1
1508 358
9681 15
75957702  8072


Satellite: ISS
Catalog Number: 25544
Epoch time:      06262
70449562   =   yrday
fracday
Element set:     900
Inclination:       51
6349  deg
RA of node:        60
5710  deg
Eccentricity:     
0011689     
Arg of perigee:     1
1508  deg
Mean anomaly:     358
9681  deg
Mean motion:   15
75957702  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             807
Checksum:              296


Coasting Arc #2 (Orbit 815)
---------------------------------------

Vector Time (GMT): 2006/263/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5011766
05                 A    =         6719653
92  meter
 Y    =       -1939083
52  meter          E    =           
0018493
 Z    =        4035143
09                 I    =           51
89663
 XDOT =       -609
096563                 Wp   =           37
93713
 YDOT =      -6607
928929  meter/sec      RA   =           57
22682  deg
 ZDOT =      -3908
247438                 TA   =           92
32764
                                          MA   =           92
11588
                                          Ha   =            190
313  n
mi
                                          Hp   =            179
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16442801
99                 X    =        -5009312
35
 Y    =       -6361822
57  feet           Y    =        -1995113
87  meter
 Z    =       13238658
44                 Z    =         4010802
16
 XDOT =      -1998
348303                 XDOT =        -516
175065
 YDOT =     -21679
556853  feet/sec       YDOT =       -6614
220895  meter/sec
 ZDOT =     -12822
334115                 ZDOT =       -3910
980266

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8395086
75                 X    =        -2558822
44
 Y    =       15580784
06  feet           Y    =         4749022
98  meter
 Z    =       13147710
35                 Z    =         4007422
11
 XDOT =     -20613
183629                 XDOT =       -6282
898370
 YDOT =       -211
154950  feet/sec       YDOT =         -64
360029  meter/sec
 ZDOT =     -12833
418355                 ZDOT =       -3911
625914


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06263
27520526  
00020000  00000-0  20000-3 0  9016
2 25544  51
6347  57
6351 0012298   3
9252 356
2006 15
75946547  8168


Satellite: ISS
Catalog Number: 25544
Epoch time:      06263
27520526   =   yrday
fracday
Element set:     901
Inclination:       51
6347  deg
RA of node:        57
6351  deg
Eccentricity:     
0012298     
Arg of perigee:     3
9252  deg
Mean anomaly:     356
2006  deg
Mean motion:   15
75946547  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             816
Checksum:              286


Coasting Arc #3 (Orbit 831)
---------------------------------------

Vector Time (GMT): 2006/264/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         391432
53                 A    =         6720097
82  meter
 Y    =        5461128
59  meter          E    =           
0016407
 Z    =        3877467
34                 I    =           51
88231
 XDOT =      -6028
626254                 Wp   =           50
60135
 YDOT =      -2492
255167  meter/sec      RA   =           52
14483  deg
 ZDOT =       4117
482792                 TA   =          356
67206
                                          MA   =          356
68296
                                          Ha   =            190
440  n
mi
                                          Hp   =            178
783

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1284227
45                 X    =          311500
33
 Y    =       17917088
56  feet           Y    =         5465059
19  meter
 Z    =       12721349
53                 Z    =         3879174
33
 XDOT =     -19778
957527                 XDOT =       -6020
311414
 YDOT =      -8176
690182  feet/sec       YDOT =       -2559
623790  meter/sec
 ZDOT =      13508
801811                 ZDOT =        4088
216165

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17942438
67                 X    =         5468855
31
 Y    =         747907
78  feet           Y    =          227962
29  meter
 Z    =       12728454
94                 Z    =         3879633
07
 XDOT =     -10239
463642                 XDOT =       -3120
988518
 YDOT =      17534
174176  feet/sec       YDOT =        5344
416289  meter/sec
 ZDOT =      13399
429162                 ZDOT =        4084
146008


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06264
28978912  
00020000  00000-0  20000-3 0  9025
2 25544  51
6353  52
4083 0012345   7
8079 352
3275 15
75935271  8328


Satellite: ISS
Catalog Number: 25544
Epoch time:      06264
28978912   =   yrday
fracday
Element set:     902
Inclination:       51
6353  deg
RA of node:        52
4083  deg
Eccentricity:     
0012345     
Arg of perigee:     7
8079  deg
Mean anomaly:     352
3275  deg
Mean motion:   15
75935271  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             832
Checksum:              295


Coasting Arc #4 (Orbit 846)
---------------------------------------

Vector Time (GMT): 2006/265/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5492368
88                 A    =         6722537
79  meter
 Y    =        2338754
70  meter          E    =           
0015012
 Z    =       -3080799
34                 I    =           51
87238
 XDOT =        232
655789                 Wp   =           25
63520
 YDOT =       5918
127407  meter/sec      RA   =           46
96028  deg
 ZDOT =       4929
562504                 TA   =          298
70288
                                          MA   =          298
85369
                                          Ha   =            190
558  n
mi
                                          Hp   =            178
619

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18019582
95                 X    =         5480774
42
 Y    =        7673079
74  feet           Y    =         2400108
33  meter
 Z    =      -10107609
40                 Z    =        -3054145
69
 XDOT =        763
306393                 XDOT =         142
514172
 YDOT =      19416
428501  feet/sec       YDOT =        5920
225505  meter/sec
 ZDOT =      16173
105327                 ZDOT =        4930
473291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9303288
86                 X    =         2835642
45
 Y    =      -17292603
31  feet           Y    =        -5270785
49  meter
 Z    =      -10007995
67                 Z    =        -3050437
08
 XDOT =      18134
926628                 XDOT =        5527
525636
 YDOT =        436
326742  feet/sec       YDOT =         132
992391  meter/sec
 ZDOT =      16177
305161                 ZDOT =        4930
842613


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06265
24094985  
00020000  00000-0  20000-3 0  9032
2 25544  51
6355  47
5087 0012402  10
3727 349
7691 15
75960051  8474


Satellite: ISS
Catalog Number: 25544
Epoch time:      06265
24094985   =   yrday
fracday
Element set:     903
Inclination:       51
6355  deg
RA of node:        47
5087  deg
Eccentricity:     
0012402     
Arg of perigee:    10
3727  deg
Mean anomaly:     349
7691  deg
Mean motion:   15
75960051  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             847
Checksum:              298


Coasting Arc #5 (Orbit 862)
---------------------------------------

Vector Time (GMT): 2006/266/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          73574
02                 A    =         6717095
93  meter
 Y    =       -4853792
93  meter          E    =           
0020519
 Z    =       -4661172
09                 I    =           51
83395
 XDOT =       6544
366755                 Wp   =           39
81826
 YDOT =       2850
698213  meter/sec      RA   =           41
87049  deg
 ZDOT =      -2856
677002                 TA   =          201
93668
                                          MA   =          202
02464
                                          Ha   =            190
534  n
mi
                                          Hp   =            178
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         241384
57                 X    =          150487
66
 Y    =      -15924517
49  feet           Y    =        -4852540
54  meter
 Z    =      -15292559
36                 Z    =        -4660627
43
 XDOT =      21471
019538                 XDOT =        6525
880802
 YDOT =       9352
684426  feet/sec       YDOT =        2923
777344  meter/sec
 ZDOT =      -9372
299875                 ZDOT =       -2824
929349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15855293
20                 X    =        -4832693
37
 Y    =       -1516607
33  feet           Y    =         -462261
91  meter
 Z    =      -15291189
47                 Z    =        -4660754
55
 XDOT =      10826
754078                 XDOT =        3299
994643
 YDOT =     -19605
843960  feet/sec       YDOT =       -5975
861239  meter/sec
 ZDOT =      -9253
644542                 ZDOT =       -2820
510856


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06266
25551090  
00020000  00000-0  20000-3 0  9040
2 25544  51
6354  42
2822 0012422  13
8806 346
2697 15
75988233  8638


Satellite: ISS
Catalog Number: 25544
Epoch time:      06266
25551090   =   yrday
fracday
Element set:     904
Inclination:       51
6354  deg
RA of node:        42
2822  deg
Eccentricity:     
0012422     
Arg of perigee:    13
8806  deg
Mean anomaly:     346
2697  deg
Mean motion:   15
75988233  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             863
Checksum:              290


Coasting Arc #6 (Orbit 878)
---------------------------------------

Vector Time (GMT): 2006/267/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5921141
61                 A    =         6725053
04  meter
 Y    =       -2588631
07  meter          E    =           
0017902
 Z    =        1861192
32                 I    =           51
83912
 XDOT =        475
595951                 Wp   =           69
77431
 YDOT =      -5194
754439  meter/sec      RA   =           36
69486  deg
 ZDOT =      -5662
255472                 TA   =           89
61685
                                          MA   =           89
41171
                                          Ha   =            190
672  n
mi
                                          Hp   =            178
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19426317
63                 X    =        -5900796
57
 Y    =       -8492884
08  feet           Y    =        -2654730
65  meter
 Z    =        6106274
01                 Z    =         1832476
67
 XDOT =       1560
354171                 XDOT =         561
155639
 YDOT =     -17043
157607  feet/sec       YDOT =       -5188
958122  meter/sec
 ZDOT =     -18576
953647                 ZDOT =       -5659
736758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9601213
65                 X    =        -2926449
92
 Y    =       18937442
29  feet           Y    =         5772132
41  meter
 Z    =        5998954
50                 Z    =         1828481
33
 XDOT =     -15537
715910                 XDOT =       -4735
895809
 YDOT =      -1942
873377  feet/sec       YDOT =        -592
187805  meter/sec
 ZDOT =     -18568
272321                 ZDOT =       -5659
609403


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06267
27006176  
00020000  00000-0  20000-3 0  9054
2 25544  51
6358  37
0560 0012456  18
4126 341
7487 15
75995089  8797


Satellite: ISS
Catalog Number: 25544
Epoch time:      06267
27006176   =   yrday
fracday
Element set:     905
Inclination:       51
6358  deg
RA of node:        37
0560  deg
Eccentricity:     
0012456     
Arg of perigee:    18
4126  deg
Mean anomaly:     341
7487  deg
Mean motion:   15
75995089  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             879
Checksum:              313


Coasting Arc #7 (Orbit 894)
---------------------------------------

Vector Time (GMT): 2006/268/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -804707
43                 A    =         6714985
46  meter
 Y    =        4247109
76  meter          E    =           
0012221
 Z    =        5129853
85                 I    =           51
78161
 XDOT =      -6968
560419                 Wp   =           41
60536
 YDOT =      -2995
700716  meter/sec      RA   =           31
58398  deg
 ZDOT =       1394
146229                 TA   =           35
13265
                                          MA   =           35
05212
                                          Ha   =            190
799  n
mi
                                          Hp   =            177
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2640116
24                 X    =         -877059
71
 Y    =       13934087
16  feet           Y    =         4237706
88  meter
 Z    =       16830229
17                 Z    =         5125768
49
 XDOT =     -22862
731033                 XDOT =       -6941
316782
 YDOT =      -9828
414421  feet/sec       YDOT =       -3073
474599  meter/sec
 ZDOT =       4573
970568                 ZDOT =        1360
358782

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13811783
90                 X    =         4209831
73
 Y    =        3294921
05  feet           Y    =         1004291
94  meter
 Z    =       16815580
08                 Z    =         5125388
81
 XDOT =     -10507
009067                 XDOT =       -3202
536364
 YDOT =      21463
638763  feet/sec       YDOT =        6542
117095  meter/sec
 ZDOT =       4447
708633                 ZDOT =        1355
661591


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06268
28459994  
00020000  00000-0  20000-3 0  9067
2 25544  51
6356  31
8291 0012504  21
8734 338
2961 15
76004880  8952


Satellite: ISS
Catalog Number: 25544
Epoch time:      06268
28459994   =   yrday
fracday
Element set:     906
Inclination:       51
6356  deg
RA of node:        31
8291  deg
Eccentricity:     
0012504     
Arg of perigee:    21
8734  deg
Mean anomaly:     338
2961  deg
Mean motion:   15
76004880  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             895
Checksum:              311


Coasting Arc #8 (Orbit 909)
---------------------------------------

Vector Time (GMT): 2006/269/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6172773
18                 A    =         6726297
93  meter
 Y    =        2582209
40  meter          E    =           
0023436
 Z    =        -552382
61                 I    =           51
79432
 XDOT =      -1398
273814                 Wp   =           32
04088
 YDOT =       4603
138606  meter/sec      RA   =           26
42621  deg
 ZDOT =       6027
881515                 TA   =          321
94909
                                          MA   =          322
11438
                                          Ha   =            190
823  n
mi
                                          Hp   =            177
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20251880
53                 X    =         6146123
21
 Y    =        8471815
61  feet           Y    =         2651087
73  meter
 Z    =       -1812278
90                 Z    =         -522459
58
 XDOT =      -4587
512513                 XDOT =       -1478
925727
 YDOT =      15102
160782  feet/sec       YDOT =        4587
051676  meter/sec
 ZDOT =      19776
514156                 ZDOT =        6020
892447

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8941701
11                 X    =         2725430
50
 Y    =      -20058640
47  feet           Y    =        -6113873
61  meter
 Z    =       -1700471
52                 Z    =         -518303
72
 XDOT =      13525
684841                 XDOT =        4122
628739
 YDOT =       4395
116214  feet/sec       YDOT =        1339
631422  meter/sec
 ZDOT =      19751
091397                 ZDOT =        6020
132658


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   06269
23571835  
00020000  00000-0  20000-3 0  9073
2 25544  51
6349  26
9291 0012541  24
7353 335
4410 15
76028311  9100


Satellite: ISS
Catalog Number: 25544
Epoch time:      06269
23571835   =   yrday
fracday
Element set:     907
Inclination:       51
6349  deg
RA of node:        26
9291  deg
Eccentricity:     
0012541     
Arg of perigee:    24
7353  deg
Mean anomaly:     335
4410  deg
Mean motion:   15
76028311  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             910
Checksum:              275


Coasting Arc #9 (Orbit 925)
---------------------------------------

Vector Time (GMT): 2006/270/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1688235
08                 A    =         6714248
76  meter
 Y    =       -3813082
53  meter          E    =           
0023548
 Z    =       -5279947
21                 I    =           51
72692
 XDOT =       7110
968497                 Wp   =           62
98216
 YDOT =       2919
707793  meter/sec      RA   =           21
28635  deg
 ZDOT =        176
210861                 TA   =          208
62584
                                          MA   =          208
75532
                                          Ha   =            190
825  n
mi
                                          Hp   =            177
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5538828
99                 X    =         1756397
53
 Y    =      -12510113
28  feet           Y    =        -3793822
78  meter
 Z    =      -17322661
44                 Z    =        -5271579
94
 XDOT =      23329
949137                 XDOT =        7076
935400
 YDOT =       9579
093808  feet/sec       YDOT =        2999
036296  meter/sec
 ZDOT =        578
119623                 ZDOT =         210
673846

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12475293
93                 X    =        -3802469
59
 Y    =       -5710524
61  feet           Y    =        -1740567
90  meter
 Z    =      -17291995
56                 Z    =        -5270600
25
 XDOT =       9304
860493                 XDOT =        2836
121478
 YDOT =     -22357
793525  feet/sec       YDOT =       -6814
655467  meter/sec
 ZDOT =        706
880874                 ZDOT =         215
457290


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
25023394  
00020000  00000-0  20000-3 0  9080
2 25544  51
6338  21
7017 0012524  28
7386 331
4466 15
76063478  9265


Satellite: ISS
Catalog Number: 25544
Epoch time:      06270
25023394   =   yrday
fracday
Element set:     908
Inclination:       51
6338  deg
RA of node:        21
7017  deg
Eccentricity:     
0012524     
Arg of perigee:    28
7386  deg
Mean anomaly:     331
4466  deg
Mean motion:   15
76063478  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             926
Checksum:              287


Coasting Arc #10 (Orbit 941)
---------------------------------------

Vector Time (GMT): 2006/271/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6182240
84                 A    =         6725938
56  meter
 Y    =       -2509200
12  meter          E    =           
0013286
 Z    =        -875297
62                 I    =           51
73965
 XDOT =       2522
790485                 Wp   =           77
95654
 YDOT =      -4162
339639  meter/sec      RA   =           16
15246  deg
 ZDOT =      -5959
525851                 TA   =          111
57883
                                          MA   =          111
43720
                                          Ha   =            190
891  n
mi
                                          Hp   =            177
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20282942
39                 X    =        -6149471
03
 Y    =       -8232283
85  feet           Y    =        -2578150
14  meter
 Z    =       -2871711
35                 Z    =         -905251
84
 XDOT =       8276
871669                 XDOT =        2598
097636
 YDOT =     -13655
969943  feet/sec       YDOT =       -4133
707381  meter/sec
 ZDOT =     -19552
250167                 ZDOT =       -5947
086970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8006812
68                 X    =        -2440476
51
 Y    =       20356913
30  feet           Y    =         6204787
17  meter
 Z    =       -2983623
12                 Z    =         -909408
33
 XDOT =     -12263
516016                 XDOT =       -3737
919682
 YDOT =      -7648
638342  feet/sec       YDOT =       -2331
304967  meter/sec
 ZDOT =     -19506
458447                 ZDOT =       -5945
568535


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
26473808  
00020000  00000-0  20000-3 0  9092
2 25544  51
6339  16
4755 0012521  32
4734 327
7198 15
76064860  9426


Satellite: ISS
Catalog Number: 25544
Epoch time:      06271
26473808   =   yrday
fracday
Element set:     909
Inclination:       51
6339  deg
RA of node:        16
4755  deg
Eccentricity:     
0012521     
Arg of perigee:    32
4734  deg
Mean anomaly:     327
7198  deg
Mean motion:   15
76064860  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             942
Checksum:              300


Coasting Arc #11 (Orbit 957)
---------------------------------------

Vector Time (GMT): 2006/272/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2713183
26                 A    =         6715276
54  meter
 Y    =        3521111
99  meter          E    =           
0017775
 Z    =        5026879
62                 I    =           51
67563
 XDOT =      -6961
954428                 Wp   =           41
43629
 YDOT =      -2789
668847  meter/sec      RA   =           10
98115  deg
 ZDOT =      -1786
889284                 TA   =           65
83944
                                          MA   =           65
65370
                                          Ha   =            191
004  n
mi
                                          Hp   =            177
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8901519
87                 X    =        -2776775
18
 Y    =       11552204
70  feet           Y    =         3490416
08  meter
 Z    =       16492387
22                 Z    =         5013544
35
 XDOT =     -22841
057835                 XDOT =       -6921
562032
 YDOT =      -9152
456846  feet/sec       YDOT =       -2867
295420  meter/sec
 ZDOT =      -5862
497652                 ZDOT =       -1820
612827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11801853
52                 X    =         3597204
95
 Y    =        8661858
35  feet           Y    =         2640134
42  meter
 Z    =       16443168
46                 Z    =         5011877
75
 XDOT =      -7871
681549                 XDOT =       -2399
288536
 YDOT =      22197
623822  feet/sec       YDOT =        6765
835741  meter/sec
 ZDOT =      -5988
489818                 ZDOT =       -1825
291697


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
27922975  
00020000  00000-0  20000-3 0  9100
2 25544  51
6334  11
2478 0012483  36
2206 323
9801 15
76084120  9586


Satellite: ISS
Catalog Number: 25544
Epoch time:      06272
27922975   =   yrday
fracday
Element set:     910
Inclination:       51
6334  deg
RA of node:        11
2478  deg
Eccentricity:     
0012483     
Arg of perigee:    36
2206  deg
Mean anomaly:     323
9801  deg
Mean motion:   15
76084120  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             958
Checksum:              278


Coasting Arc #12 (Orbit 973)
---------------------------------------

Vector Time (GMT): 2006/273/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5883141
22                 A    =         6723978
44  meter
 Y    =        2355482
50  meter          E    =           
0025495
 Z    =        2203709
32                 I    =           51
67643
 XDOT =      -3666
712018                 Wp   =           56
53873
 YDOT =       3988
683554  meter/sec      RA   =            5
86619  deg
 ZDOT =       5493
978692                 TA   =          328
21158
                                          MA   =          328
36523
                                          Ha   =            190
883  n
mi
                                          Hp   =            176
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19301644
44                 X    =         5845659
32
 Y    =        7727960
96  feet           Y    =         2421061
45  meter
 Z    =        7230017
44                 Z    =         2232198
87
 XDOT =     -12029
895072                 XDOT =       -3737
730521
 YDOT =      13086
232131  feet/sec       YDOT =        3947
283208  meter/sec
 ZDOT =      18024
864474                 ZDOT =        5475
993171

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6843727
23                 X    =         2085968
06
 Y    =      -19593054
32  feet           Y    =        -5971962
96  meter
 Z    =        7336459
01                 Z    =         2236152
71
 XDOT =      12195
462561                 XDOT =        3717
176989
 YDOT =      11022
279186  feet/sec       YDOT =        3359
590696  meter/sec
 ZDOT =      17958
379308                 ZDOT =        5473
714013


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
29370935  
00020000  00000-0  20000-3 0  9117
2 25544  51
6325   6
0201 0012454  40
3742 319
8345 15
76121398  9745


Satellite: ISS
Catalog Number: 25544
Epoch time:      06273
29370935   =   yrday
fracday
Element set:     911
Inclination:       51
6325  deg
RA of node:         6
0201  deg
Eccentricity:     
0012454     
Arg of perigee:    40
3742  deg
Mean anomaly:     319
8345  deg
Mean motion:   15
76121398  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             974
Checksum:              274


Coasting Arc #13 (Orbit 988)
---------------------------------------

Vector Time (GMT): 2006/274/05:38:00
000
Vector Time (MET): N/A
Weight (LBS)     : 480828
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3659905
40                 A    =         6717618
23  meter
 Y    =       -3476543
31  meter          E    =           
0018496
 Z    =       -4444200
14                 I    =           51
62609
 XDOT =       6448
621923                 Wp   =           71
93027
 YDOT =       2651
561904  meter/sec      RA   =             
67053  deg
 ZDOT =       3253
036973                 TA   =          230
62398
                                          MA   =          230
78796
                                          Ha   =            191
056  n
mi
                                          Hp   =            176
827

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12007563
64                 X    =         3720097
81
 Y    =      -11405981
98  feet           Y    =        -3435279
65  meter
 Z    =      -14580709
13                 Z    =        -4426274
04
 XDOT =      21156
896072                 XDOT =        6402
689765
 YDOT =       8699
350080  feet/sec       YDOT =        2723
417131  meter/sec
 ZDOT =      10672
693482                 ZDOT =        3284
252988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12140876
93                 X    =        -3700539
29
 Y    =      -11349320
19  feet           Y    =        -3459272
79  meter
 Z    =      -14514376
56                 Z    =        -4423981
98
 XDOT =       6532
458019                 XDOT =        1991
093204
 YDOT =     -20716
039395  feet/sec       YDOT =       -6314
248808  meter/sec
 ZDOT =      10789
336224                 ZDOT =        3288
589681


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
24477441  
00020000  00000-0  20000-3 0  9124
2 25544  51
6321   1
1189 0012541  44
4813 315
7356 15
76124132  9895


Satellite: ISS
Catalog Number: 25544
Epoch time:      06274
24477441   =   yrday
fracday
Element set:     912
Inclination:       51
6321  deg
RA of node:         1
1189  deg
Eccentricity:     
0012541     
Arg of perigee:    44
4813  deg
Mean anomaly:     315
7356  deg
Mean motion:   15
76124132  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             989
Checksum:              271

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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