Date: December 6th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3778)
---------------------------------------

Vector Time (GMT): 2007/339/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2444971
82                 A    =         6712604
78  meter
 Y    =       -3751987
84  meter          E    =           
0012532
 Z    =       -5011642
92                 I    =           51
34132
 XDOT =       4955
116290                 Wp   =          103
82699
 YDOT =      -5611
942327  meter/sec      RA   =          300
44873  deg
 ZDOT =       1784
787892                 TA   =          183
44477
                                          MA   =          183
45340
                                          Ha   =            185
166  n
mi
                                          Hp   =            179
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8021561
08                 X    =        -2378488
64
 Y    =      -12309671
41  feet           Y    =        -3778956
73  meter
 Z    =      -16442398
05                 Z    =        -5023359
69
 XDOT =      16256
943210                 XDOT =        5008
831245
 YDOT =     -18411
884276  feet/sec       YDOT =       -5556
231231  meter/sec
 ZDOT =       5855
603320                 ZDOT =        1808
990331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14199169
20                 X    =         4327906
77
 Y    =        3574231
60  feet           Y    =         1089425
79  meter
 Z    =      -16487400
30                 Z    =        -5025359
61
 XDOT =        988
832329                 XDOT =         301
396094
 YDOT =      23493
625354  feet/sec       YDOT =        7160
857008  meter/sec
 ZDOT =       5947
222248                 ZDOT =        1812
713341


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   07339
42944669  
00020000  00000-0  20000-3 0  9005
2 25544  51
6370 301
0096 0000830 277
1851  82
9220 15
77016612 37790


Satellite: ISS
Catalog Number: 25544
Epoch time:      07339
42944669   =   yrday
fracday
Element set:     900
Inclination:       51
6370  deg
RA of node:       301
0096  deg
Eccentricity:     
0000830     
Arg of perigee:   277
1851  deg
Mean anomaly:      82
9220  deg
Mean motion:   15
77016612  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3779
Checksum:              287


Coasting Arc #2 (Orbit 3794)
---------------------------------------

Vector Time (GMT): 2007/340/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4339513
47                 A    =         6720639
82  meter
 Y    =        4471557
85  meter          E    =           
0004529
 Z    =       -2516050
01                 I    =           51
35504
 XDOT =      -2240
072652                 Wp   =          133
18032
 YDOT =      -5140
124346  meter/sec      RA   =          295
30536  deg
 ZDOT =      -5280
589811                 TA   =           75
46533
                                          MA   =           75
41509
                                          Ha   =            185
100  n
mi
                                          Hp   =            179
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14237248
90                 X    =        -4376969
79
 Y    =       14670465
39  feet           Y    =         4422821
79  meter
 Z    =       -8254757
24                 Z    =        -2537222
34
 XDOT =      -7349
319725                 XDOT =       -2156
775795
 YDOT =     -16863
925021  feet/sec       YDOT =       -5164
707802  meter/sec
 ZDOT =     -17324
769721                 ZDOT =       -5291
270550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          -8491
00                 X    =           -2588
06
 Y    =      -20410568
97  feet           Y    =        -6221141
42  meter
 Z    =       -8334952
33                 Z    =        -2540493
47
 XDOT =      15451
332641                 XDOT =        4709
566189
 YDOT =       7073
250138  feet/sec       YDOT =        2155
926642  meter/sec
 ZDOT =     -17365
965094                 ZDOT =       -5293
146161


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   07340
44330772  
00020000  00000-0  20000-3 0  9014
2 25544  51
6366 295
7782 0000748 284
2581  75
8501 15
77068864 37950


Satellite: ISS
Catalog Number: 25544
Epoch time:      07340
44330772   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       295
7782  deg
Eccentricity:     
0000748     
Arg of perigee:   284
2581  deg
Mean anomaly:      75
8501  deg
Mean motion:   15
77068864  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3795
Checksum:              316


Coasting Arc #3 (Orbit 3810)
---------------------------------------

Vector Time (GMT): 2007/341/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1533011
56                 A    =         6716274
55  meter
 Y    =        5158708
11  meter          E    =           
0010026
 Z    =        4011824
92                 I    =           51
32913
 XDOT =      -4934
813964                 Wp   =           74
49466
 YDOT =       4483
165687  meter/sec      RA   =          290
07675  deg
 ZDOT =      -3868
429221                 TA   =           55
55321
                                          MA   =           55
45851
                                          Ha   =            184
968  n
mi
                                          Hp   =            179
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5029565
50                 X    =         1455723
02
 Y    =       16924895
37  feet           Y    =         5175418
46  meter
 Z    =       13162155
25                 Z    =         4019085
38
 XDOT =     -16190
334529                 XDOT =       -4965
786096
 YDOT =      14708
548841  feet/sec       YDOT =        4427
809121  meter/sec
 ZDOT =     -12691
696920                 ZDOT =       -3892
477734

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15479926
30                 X    =        -4718281
54
 Y    =       -8448558
55  feet           Y    =        -2575120
65  meter
 Z    =       13190325
38                 Z    =         4020411
17
 XDOT =        359
354768                 XDOT =         109
531333
 YDOT =     -20670
148604  feet/sec       YDOT =       -6300
261294  meter/sec
 ZDOT =     -12782
850574                 ZDOT =       -3896
212855


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   07341
45714747  
00020000  00000-0  20000-3 0  9025
2 25544  51
6364 290
5474 0000937 290
3680  69
7384 15
77112686 38119


Satellite: ISS
Catalog Number: 25544
Epoch time:      07341
45714747   =   yrday
fracday
Element set:     902
Inclination:       51
6364  deg
RA of node:       290
5474  deg
Eccentricity:     
0000937     
Arg of perigee:   290
3680  deg
Mean anomaly:      69
7384  deg
Mean motion:   15
77112686  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3811
Checksum:              306


Coasting Arc #4 (Orbit 3826)
---------------------------------------

Vector Time (GMT): 2007/342/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4247872
83                 A    =         6715767
71  meter
 Y    =       -3198006
20  meter          E    =           
0009455
 Z    =        4096131
33                 I    =           51
31961
 XDOT =       1344
573495                 Wp   =          104
24223
 YDOT =       6599
903646  meter/sec      RA   =          284
94671  deg
 ZDOT =       3748
903686                 TA   =          307
17978
                                          MA   =          307
26607
                                          Ha   =            184
804  n
mi
                                          Hp   =            179
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13936590
65                 X    =         4263419
05
 Y    =      -10492146
31  feet           Y    =        -3150417
75  meter
 Z    =       13438751
09                 Z    =         4116805
21
 XDOT =       4411
330364                 XDOT =        1252
460582
 YDOT =      21653
227185  feet/sec       YDOT =        6614
423851  meter/sec
 ZDOT =      12299
552775                 ZDOT =        3755
212973

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2068209
83                 X    =         -630390
35
 Y    =       17260416
15  feet           Y    =         5260974
84  meter
 Z    =       13517184
12                 Z    =         4120037
72
 XDOT =     -17342
257569                 XDOT =       -5285
920107
 YDOT =     -11753
818840  feet/sec       YDOT =       -3582
563983  meter/sec
 ZDOT =      12324
244574                 ZDOT =        3756
429746


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   07342
47096665  
00020000  00000-0  20000-3 0  9031
2 25544  51
6367 285
3169 0000994 287
0686  73
0370 15
77166717 38271


Satellite: ISS
Catalog Number: 25544
Epoch time:      07342
47096665   =   yrday
fracday
Element set:     903
Inclination:       51
6367  deg
RA of node:       285
3169  deg
Eccentricity:     
0000994     
Arg of perigee:   287
0686  deg
Mean anomaly:      73
0370  deg
Mean motion:   15
77166717  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3827
Checksum:              324


Coasting Arc #5 (Orbit 3841)
---------------------------------------

Vector Time (GMT): 2007/343/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -865296
41                 A    =         6720725
62  meter
 Y    =       -6224231
33  meter          E    =           
0005469
 Z    =       -2378451
56                 I    =           51
32991
 XDOT =       4818
452455                 Wp   =           37
48835
 YDOT =      -2714
698114  meter/sec      RA   =          279
71740  deg
 ZDOT =       5361
913077                 TA   =          295
55073
                                          MA   =          295
60726
                                          Ha   =            184
989  n
mi
                                          Hp   =            179
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2838899
00                 X    =         -784077
53
 Y    =      -20420706
47  feet           Y    =        -6233453
07  meter
 Z    =       -7803318
77                 Z    =        -2382458
96
 XDOT =      15808
571045                 XDOT =        4822
402872
 YDOT =      -8906
489874  feet/sec       YDOT =       -2660
794224  meter/sec
 ZDOT =      17591
578337                 ZDOT =        5385
330667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16846586
34                 X    =         5134839
52
 Y    =       11874717
74  feet           Y    =         3619413
97  meter
 Z    =       -7819206
55                 Z    =        -2383294
16
 XDOT =      -3325
310329                 XDOT =       -1013
554588
 YDOT =      16336
635251  feet/sec       YDOT =        4979
406424  meter/sec
 ZDOT =      17680
517630                 ZDOT =        5389
021774


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   07343
42140561  
00020000  00000-0  20000-3 0  9043
2 25544  51
6367 280
4127 0000851 302
7124  57
3958 15
77156040 38427


Satellite: ISS
Catalog Number: 25544
Epoch time:      07343
42140561   =   yrday
fracday
Element set:     904
Inclination:       51
6367  deg
RA of node:       280
4127  deg
Eccentricity:     
0000851     
Arg of perigee:   302
7124  deg
Mean anomaly:      57
3958  deg
Mean motion:   15
77156040  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3842
Checksum:              272


Coasting Arc #6 (Orbit 3857)
---------------------------------------

Vector Time (GMT): 2007/344/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4183385
25                 A    =         6711850
45  meter
 Y    =        1426335
92  meter          E    =           
0013138
 Z    =       -5062829
11                 I    =           51
29724
 XDOT =       -660
973061                 Wp   =           75
06554
 YDOT =      -7505
656120  meter/sec      RA   =          274
56829  deg
 ZDOT =      -1568
435909                 TA   =          179
79705
                                          MA   =          179
79652
                                          Ha   =            184
929  n
mi
                                          Hp   =            179
019

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13725017
23                 X    =        -4174429
23
 Y    =        4679579
79  feet           Y    =         1379605
87  meter
 Z    =      -16610331
73                 Z    =        -5083130
25
 XDOT =      -2168
546789                 XDOT =        -569
375280
 YDOT =     -24624
856038  feet/sec       YDOT =       -7512
535080  meter/sec
 ZDOT =      -5145
787104                 ZDOT =       -1571
425738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5640248
71                 X    =         1719147
81
 Y    =      -13262409
03  feet           Y    =        -4042382
27  meter
 Z    =      -16687533
86                 Z    =        -5086360
32
 XDOT =      18767
796568                 XDOT =        5720
424394
 YDOT =      14471
396754  feet/sec       YDOT =        4410
881731  meter/sec
 ZDOT =      -5157
930320                 ZDOT =       -1572
137161


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   07344
43518638  
00020000  00000-0  20000-3 0  9050
2 25544  51
6373 275
1812 0000949 303
8329  56
2745 15
77187876 38583


Satellite: ISS
Catalog Number: 25544
Epoch time:      07344
43518638   =   yrday
fracday
Element set:     905
Inclination:       51
6373  deg
RA of node:       275
1812  deg
Eccentricity:     
0000949     
Arg of perigee:   303
8329  deg
Mean anomaly:      56
2745  deg
Mean motion:   15
77187876  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3858
Checksum:              325


Coasting Arc #7 (Orbit 3873)
---------------------------------------

Vector Time (GMT): 2007/345/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         308621
24                 A    =         6722969
94  meter
 Y    =        6703808
39  meter          E    =           
0011803
 Z    =         293432
06                 I    =           51
33447
 XDOT =      -4801
896538                 Wp   =          132
14021
 YDOT =        490
418566  meter/sec      RA   =          269
36916  deg
 ZDOT =      -6007
526368                 TA   =           44
65265
                                          MA   =           44
55766
                                          Ha   =            184
865  n
mi
                                          Hp   =            179
090

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1012536
86                 X    =          232209
84
 Y    =       21994122
00  feet           Y    =         6706832
28  meter
 Z    =         962703
60                 Z    =          294746
89
 XDOT =     -15754
253734                 XDOT =       -4777
839894
 YDOT =       1608
984798  feet/sec       YDOT =         436
856573  meter/sec
 ZDOT =     -19709
732177                 ZDOT =       -6030
795642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17259651
83                 X    =        -5260741
88
 Y    =      -13669677
06  feet           Y    =        -4166517
57  meter
 Z    =         968390
24                 Z    =          295165
34
 XDOT =       8051
669766                 XDOT =        2454
148945
 YDOT =     -11602
567855  feet/sec       YDOT =       -3536
462682  meter/sec
 ZDOT =     -19798
344591                 ZDOT =       -6034
535431


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   07345
44894684  
00020000  00000-0  20000-3 0  9061
2 25544  51
6376 269
9503 0001025 309
4079  50
6995 15
77228764 38749


Satellite: ISS
Catalog Number: 25544
Epoch time:      07345
44894684   =   yrday
fracday
Element set:     906
Inclination:       51
6376  deg
RA of node:       269
9503  deg
Eccentricity:     
0001025     
Arg of perigee:   309
4079  deg
Mean anomaly:      50
6995  deg
Mean motion:   15
77228764  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3874
Checksum:              332


Coasting Arc #8 (Orbit 3889)
---------------------------------------

Vector Time (GMT): 2007/346/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4228904
77                 A    =         6711099
30  meter
 Y    =         587634
99  meter          E    =           
0003281
 Z    =        5176323
65                 I    =           51
29644
 XDOT =         49
686479                 Wp   =           40
48186
 YDOT =       7654
416846  meter/sec      RA   =          264
18156  deg
 ZDOT =       -906
763820                 TA   =           58
20405
                                          MA   =           58
17210
                                          Ha   =            184
705  n
mi
                                          Hp   =            179
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13874359
48                 X    =         4196873
72
 Y    =        1927936
32  feet           Y    =          634745
06  meter
 Z    =       16982689
14                 Z    =         5196790
03
 XDOT =        163
013382                 XDOT =         -31
505158
 YDOT =      25112
916161  feet/sec       YDOT =        7654
518651  meter/sec
 ZDOT =      -2974
946915                 ZDOT =        -906
718410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10335890
17                 X    =        -3150379
33
 Y    =        9312737
53  feet           Y    =         2838522
40  meter
 Z    =       17060738
97                 Z    =         5200113
24
 XDOT =     -18669
798464                 XDOT =       -5690
554572
 YDOT =     -15256
014101  feet/sec       YDOT =       -4650
033098  meter/sec
 ZDOT =      -2973
993138                 ZDOT =        -906
473108


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   07346
46268749  
00020000  00000-0  20000-3 0  9072
2 25544  51
6377 264
7199 0001057 312
7048  47
4028 15
77257794 38906


Satellite: ISS
Catalog Number: 25544
Epoch time:      07346
46268749   =   yrday
fracday
Element set:     907
Inclination:       51
6377  deg
RA of node:       264
7199  deg
Eccentricity:     
0001057     
Arg of perigee:   312
7048  deg
Mean anomaly:      47
4028  deg
Mean motion:   15
77257794  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3890
Checksum:              330


Coasting Arc #9 (Orbit 3905)
---------------------------------------

Vector Time (GMT): 2007/347/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         255271
67                 A    =         6721326
59  meter
 Y    =       -6449997
95  meter          E    =           
0013772
 Z    =        1848168
38                 I    =           51
33526
 XDOT =       4941
732335                 Wp   =           62
38936
 YDOT =       1816
370996  meter/sec      RA   =          259
02283  deg
 ZDOT =       5630
811651                 TA   =          318
25224
                                          MA   =          318
35724
                                          Ha   =            184
765  n
mi
                                          Hp   =            178
980

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         837505
47                 X    =          318399
49
 Y    =      -21161410
61  feet           Y    =        -6446790
67  meter
 Z    =        6063544
56                 Z    =         1849560
88
 XDOT =      16213
032595                 XDOT =        4893
700655
 YDOT =       5959
222429  feet/sec       YDOT =        1871
362863  meter/sec
 ZDOT =      18473
791505                 ZDOT =        5654
702189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15932754
63                 X    =         4856303
61
 Y    =       13949829
62  feet           Y    =         4251908
07  meter
 Z    =        6068185
08                 Z    =         1849582
81
 XDOT =     -13755
899310                 XDOT =       -4192
798110
 YDOT =       7598
871720  feet/sec       YDOT =        2316
136100  meter/sec
 ZDOT =      18565
025618                 ZDOT =        5658
619808


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   07347
47640760  
00020000  00000-0  20000-3 0  9082
2 25544  51
6374 259
4883 0001065 313
6648  46
4428 15
77297509 39068


Satellite: ISS
Catalog Number: 25544
Epoch time:      07347
47640760   =   yrday
fracday
Element set:     908
Inclination:       51
6374  deg
RA of node:       259
4883  deg
Eccentricity:     
0001065     
Arg of perigee:   313
6648  deg
Mean anomaly:      46
4428  deg
Mean motion:   15
77297509  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3906
Checksum:              322


Coasting Arc #10 (Orbit 3920)
---------------------------------------

Vector Time (GMT): 2007/348/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4404979
16                 A    =         6714195
82  meter
 Y    =       -2517253
54  meter          E    =           
0008524
 Z    =       -4406136
70                 I    =           51
31828
 XDOT =        704
110744                 Wp   =          107
19623
 YDOT =      -6937
656443  meter/sec      RA   =          253
79829  deg
 ZDOT =       3262
305698                 TA   =          195
66707
                                          MA   =          195
69346
                                          Ha   =            184
741  n
mi
                                          Hp   =            178
836

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14452031
36                 X    =        -4355099
28
 Y    =       -8258705
83  feet           Y    =        -2566233
06  meter
 Z    =      -14455829
08                 Z    =        -4427415
22
 XDOT =       2310
074618                 XDOT =         765
788675
 YDOT =     -22761
340035  feet/sec       YDOT =       -6929
438229  meter/sec
 ZDOT =      10703
102685                 ZDOT =        3265
875207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15359922
36                 X    =         4681704
34
 Y    =       -6227461
06  feet           Y    =        -1898130
13  meter
 Z    =      -14537191
63                 Z    =        -4430936
01
 XDOT =      16084
902884                 XDOT =        4902
678399
 YDOT =      14678
675578  feet/sec       YDOT =        4474
060316  meter/sec
 ZDOT =      10715
980448                 ZDOT =        3266
230841


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   07348
42675305  
00020000  00000-0  20000-3 0  9092
2 25544  51
6374 254
5837 0001146 318
4537  41
6541 15
77315290 39211


Satellite: ISS
Catalog Number: 25544
Epoch time:      07348
42675305   =   yrday
fracday
Element set:     909
Inclination:       51
6374  deg
RA of node:       254
5837  deg
Eccentricity:     
0001146     
Arg of perigee:   318
4537  deg
Mean anomaly:      41
6541  deg
Mean motion:   15
77315290  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3921
Checksum:              295


Coasting Arc #11 (Orbit 3936)
---------------------------------------

Vector Time (GMT): 2007/349/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1055238
40                 A    =         6716554
14  meter
 Y    =        5492183
14  meter          E    =           
0005641
 Z    =       -3725860
08                 I    =           51
33640
 XDOT =      -5144
306970                 Wp   =           66
20808
 YDOT =      -3858
933523  meter/sec      RA   =          248
66496  deg
 ZDOT =      -4234
176808                 TA   =          159
03188
                                          MA   =          159
00874
                                          Ha   =            184
732  n
mi
                                          Hp   =            178
810

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3462068
25                 X    =        -1098474
87
 Y    =       18018973
54  feet           Y    =         5480141
50  meter
 Z    =      -12223950
40                 Z    =        -3731090
87
 XDOT =     -16877
647540                 XDOT =       -5080
204608
 YDOT =     -12660
543053  feet/sec       YDOT =       -3916
101225  meter/sec
 ZDOT =     -13891
656194                 ZDOT =       -4259
012528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12334786
49                 X    =        -3759642
92
 Y    =      -13566459
26  feet           Y    =        -4135056
78  meter
 Z    =      -12243304
82                 Z    =        -3731759
31
 XDOT =      19237
644962                 XDOT =        5863
634184
 YDOT =      -4876
803134  feet/sec       YDOT =       -1486
449595  meter/sec
 ZDOT =     -13986
728941                 ZDOT =       -4263
154981


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   07349
44043586  
00020000  00000-0  20000-3 0  9107
2 25544  51
6378 249
3517 0001156 325
2578  34
8511 15
77361111 39375


Satellite: ISS
Catalog Number: 25544
Epoch time:      07349
44043586   =   yrday
fracday
Element set:     910
Inclination:       51
6378  deg
RA of node:       249
3517  deg
Eccentricity:     
0001156     
Arg of perigee:   325
2578  deg
Mean anomaly:      34
8511  deg
Mean motion:   15
77361111  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3937
Checksum:              294


Coasting Arc #12 (Orbit 3952)
---------------------------------------

Vector Time (GMT): 2007/350/10:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4542437
44                 A    =         6719078
66  meter
 Y    =        4071934
03  meter          E    =           
0012752
 Z    =        2803729
86                 I    =           51
35704
 XDOT =      -1789
680037                 Wp   =           95
54020
 YDOT =       5510
170149  meter/sec      RA   =          243
43269  deg
 ZDOT =      -5084
469468                 TA   =           52
13819
                                          MA   =           52
02289
                                          Ha   =            184
665  n
mi
                                          Hp   =            178
778

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14903009
96                 X    =         4482946
81
 Y    =       13359363
61  feet           Y    =         4122397
27  meter
 Z    =        9198588
77                 Z    =         2825652
91
 XDOT =      -5871
653666                 XDOT =       -1826
463111
 YDOT =      18077
986054  feet/sec       YDOT =        5489
951707  meter/sec
 ZDOT =     -16681
330277                 ZDOT =       -5093
252619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19542332
88                 X    =        -5956503
06
 Y    =        4137274
98  feet           Y    =         1261041
41  meter
 Z    =        9282592
24                 Z    =         2829334
11
 XDOT =     -10908
372831                 XDOT =       -3324
872039
 YDOT =     -13889
191598  feet/sec       YDOT =       -4233
425599  meter/sec
 ZDOT =     -16714
217929                 ZDOT =       -5094
493625


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   07350
45409971  
00020000  00000-0  20000-3 0  9115
2 25544  51
6379 244
1199 0001175 327
0225  33
0866 15
77381989 39532


Satellite: ISS
Catalog Number: 25544
Epoch time:      07350
45409971   =   yrday
fracday
Element set:     911
Inclination:       51
6379  deg
RA of node:       244
1199  deg
Eccentricity:     
0001175     
Arg of perigee:   327
0225  deg
Mean anomaly:      33
0866  deg
Mean motion:   15
77381989  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3953
Checksum:              309

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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