Date: June 11th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4843 76 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 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 937)
---------------------------------------

Vector Time (GMT): 2007/159/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6130183
23                 A    =         6718727
87  meter
 Y    =       -1997272
27  meter          E    =           
0003782
 Z    =       -1882542
48                 I    =           51
81392
 XDOT =        -34
978413                 Wp   =          232
44316
 YDOT =       5230
312435  meter/sec      RA   =          148
67705  deg
 ZDOT =      -5657
531902                 TA   =          328
44787
                                          MA   =          328
47054
                                          Ha   =            182
719  n
mi
                                          Hp   =            180
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20112149
70                 X    =         6161206
46
 Y    =       -6552730
54  feet           Y    =        -1928547
44  meter
 Z    =       -6176320
49                 Z    =        -1852686
92
 XDOT =       -114
758572                 XDOT =         -65
978653
 YDOT =      17159
817701  feet/sec       YDOT =        5229
748627  meter/sec
 ZDOT =     -18561
456373                 ZDOT =       -5657
776507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16810918
52                 X    =         5123967
97
 Y    =      -12892123
62  feet           Y    =        -3929519
28  meter
 Z    =       -6063822
61                 Z    =        -1848253
13
 XDOT =       4768
256410                 XDOT =        1453
364554
 YDOT =      14956
732761  feet/sec       YDOT =        4558
812145  meter/sec
 ZDOT =     -18561
736557                 ZDOT =       -5657
617302


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   07159
37211558  
00020000  00000-0  20000-3 0  9003
2 25544  51
6323 149
4668 0008192 294
2706  65
7603 15
78210966  9382


Satellite: ISS
Catalog Number: 25544
Epoch time:      07159
37211558   =   yrday
fracday
Element set:     900
Inclination:       51
6323  deg
RA of node:       149
4668  deg
Eccentricity:     
0008192     
Arg of perigee:   294
2706  deg
Mean anomaly:      65
7603  deg
Mean motion:   15
78210966  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             938
Checksum:              307


Coasting Arc #2 (Orbit 953)
---------------------------------------

Vector Time (GMT): 2007/160/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1208566
62                 A    =         6712183
02  meter
 Y    =       -5054536
55  meter          E    =           
0007228
 Z    =        4250329
23                 I    =           51
81554
 XDOT =       6667
709186                 Wp   =           17
62162
 YDOT =      -1428
145162  meter/sec      RA   =          143
47944  deg
 ZDOT =      -3585
973464                 TA   =          108
72760
                                          MA   =          108
64915
                                          Ha   =            182
860  n
mi
                                          Hp   =            179
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3965113
59                 X    =         1244349
92
 Y    =      -16583125
17  feet           Y    =        -5040822
09  meter
 Z    =       13944649
71                 Z    =         4256286
82
 XDOT =      21875
686306                 XDOT =        6700
603459
 YDOT =      -4685
515624  feet/sec       YDOT =       -1353
398766  meter/sec
 ZDOT =     -11765
004803                 ZDOT =       -3553
501815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2152601
42                 X    =         -656112
91
 Y    =      -16896088
34  feet           Y    =        -5149927
73  meter
 Z    =       13966528
83                 Z    =         4256997
99
 XDOT =      17688
672091                 XDOT =        5391
507253
 YDOT =     -11900
024973  feet/sec       YDOT =       -3627
127612  meter/sec
 ZDOT =     -11642
549998                 ZDOT =       -3548
649239


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   07160
38523366  
00020000  00000-0  20000-3 0  9010
2 25544  51
6315 144
2305 0008290 298
2625  61
7703 15
78254412  9546


Satellite: ISS
Catalog Number: 25544
Epoch time:      07160
38523366   =   yrday
fracday
Element set:     901
Inclination:       51
6315  deg
RA of node:       144
2305  deg
Eccentricity:     
0008290     
Arg of perigee:   298
2625  deg
Mean anomaly:      61
7703  deg
Mean motion:   15
78254412  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             954
Checksum:              278


Coasting Arc #3 (Orbit 969)
---------------------------------------

Vector Time (GMT): 2007/161/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5266533
21                 A    =         6712708
98  meter
 Y    =         321775
12  meter          E    =           
0003758
 Z    =        4145756
43                 I    =           51
83901
 XDOT =       2571
236230                 Wp   =           62
69408
 YDOT =      -6225
751419  meter/sec      RA   =          138
37442  deg
 ZDOT =       3748
680680                 TA   =          349
09700
                                          MA   =          349
10515
                                          Ha   =            183
171  n
mi
                                          Hp   =            179
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17278652
27                 X    =        -5289879
47
 Y    =        1055692
65  feet           Y    =          262750
74  meter
 Z    =       13601563
08                 Z    =         4120114
67
 XDOT =       8435
814404                 XDOT =        2622
451790
 YDOT =     -20425
693631  feet/sec       YDOT =       -6196
712520  meter/sec
 ZDOT =      12298
821130                 ZDOT =        3761
295505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15767890
79                 X    =        -4806053
11
 Y    =        7325565
14  feet           Y    =         2232832
26  meter
 Z    =       13504760
07                 Z    =         4116250
87
 XDOT =        856
715858                 XDOT =         261
126994
 YDOT =     -20920
811177  feet/sec       YDOT =       -6376
663247  meter/sec
 ZDOT =      12345
706204                 ZDOT =        3762
971251


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   07161
39833691  
00020000  00000-0  20000-3 0  9028
2 25544  51
6311 138
9933 0008081 302
9453  57
0935 15
78247439  9703


Satellite: ISS
Catalog Number: 25544
Epoch time:      07161
39833691   =   yrday
fracday
Element set:     902
Inclination:       51
6311  deg
RA of node:       138
9933  deg
Eccentricity:     
0008081     
Arg of perigee:   302
9453  deg
Mean anomaly:      57
0935  deg
Mean motion:   15
78247439  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             970
Checksum:              303


Coasting Arc #4 (Orbit 984)
---------------------------------------

Vector Time (GMT): 2007/162/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3072117
82                 A    =         6718095
33  meter
 Y    =        5608911
71  meter          E    =           
0010050
 Z    =       -2036091
36                 I    =           51
87963
 XDOT =      -5236
430412                 Wp   =          347
16098
 YDOT =       -837
874096  meter/sec      RA   =          133
17763  deg
 ZDOT =       5597
121781                 TA   =          350
15656
                                          MA   =          350
17623
                                          Ha   =            183
107  n
mi
                                          Hp   =            179
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10079126
71                 X    =        -3124718
06
 Y    =       18401941
30  feet           Y    =         5574263
76  meter
 Z    =       -6680089
76                 Z    =        -2051142
85
 XDOT =     -17179
889804                 XDOT =       -5253
862184
 YDOT =      -2748
930760  feet/sec       YDOT =        -896
529097  meter/sec
 ZDOT =      18363
260437                 ZDOT =        5571
640371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2262880
02                 X    =         -689725
83
 Y    =       20840968
22  feet           Y    =         6352327
11  meter
 Z    =       -6736264
24                 Z    =        -2053213
34
 XDOT =     -15504
407849                 XDOT =       -4725
743513
 YDOT =       4216
241650  feet/sec       YDOT =        1285
110455  meter/sec
 ZDOT =      18266
916619                 ZDOT =        5567
756185


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   07162
34810412  
00020000  00000-0  20000-3 0  9031
2 25544  51
6320 134
0842 0008095 306
0745  53
9670 15
78309250  9850


Satellite: ISS
Catalog Number: 25544
Epoch time:      07162
34810412   =   yrday
fracday
Element set:     903
Inclination:       51
6320  deg
RA of node:       134
0842  deg
Eccentricity:     
0008095     
Arg of perigee:   306
0745  deg
Mean anomaly:      53
9670  deg
Mean motion:   15
78309250  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             985
Checksum:              273


Coasting Arc #5 (Orbit 1000)
---------------------------------------

Vector Time (GMT): 2007/163/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3747123
53                 A    =         6708088
49  meter
 Y    =        1888996
39  meter          E    =           
0010798
 Z    =       -5241365
36                 I    =           51
86430
 XDOT =      -4255
032711                 Wp   =           51
28510
 YDOT =       6376
641240  meter/sec      RA   =          128
05058  deg
 ZDOT =       -738
229350                 TA   =          211
68238
                                          MA   =          211
74741
                                          Ha   =            183
403  n
mi
                                          Hp   =            179
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12293712
37                 X    =         3751183
99
 Y    =        6197494
73  feet           Y    =         1930922
48  meter
 Z    =      -17196080
59                 Z    =        -5223151
35
 XDOT =     -13960
081072                 XDOT =       -4322
434761
 YDOT =      20920
738976  feet/sec       YDOT =        6328
682347  meter/sec
 ZDOT =      -2422
012303                 ZDOT =        -759
063189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13832140
44                 X    =         4216036
41
 Y    =         765058
93  feet           Y    =          233189
96  meter
 Z    =      -17127056
62                 Z    =        -5220326
86
 XDOT =      -4430
862793                 XDOT =       -1350
526979
 YDOT =      23730
938629  feet/sec       YDOT =        7233
190094  meter/sec
 ZDOT =      -2499
951856                 ZDOT =        -761
985326


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   07163
36117234  
00020000  00000-0  20000-3 0  9047
2 25544  51
6319 128
8473 0008216 309
9174  50
1269 15
78292254 10010


Satellite: ISS
Catalog Number: 25544
Epoch time:      07163
36117234   =   yrday
fracday
Element set:     904
Inclination:       51
6319  deg
RA of node:       128
8473  deg
Eccentricity:     
0008216     
Arg of perigee:   309
9174  deg
Mean anomaly:      50
1269  deg
Mean motion:   15
78292254  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1001
Checksum:              279


Coasting Arc #6 (Orbit 1016)
---------------------------------------

Vector Time (GMT): 2007/164/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4139201
35                 A    =         6719620
34  meter
 Y    =       -5229063
03  meter          E    =           
0002530
 Z    =        -810394
84                 I    =           51
91945
 XDOT =       3301
446039                 Wp   =          162
45610
 YDOT =       3540
921256  meter/sec      RA   =          122
90065  deg
 ZDOT =      -5992
341295                 TA   =           26
35913
                                          MA   =           26
34626
                                          Ha   =            183
466  n
mi
                                          Hp   =            178
887

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13580056
91                 X    =         4201302
66
 Y    =      -17155718
61  feet           Y    =        -5182428
76  meter
 Z    =       -2658775
71                 Z    =         -790136
59
 XDOT =      10831
515876                 XDOT =        3290
715653
 YDOT =      11617
195723  feet/sec       YDOT =        3577
781147  meter/sec
 ZDOT =     -19659
912386                 ZDOT =       -5976
327974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5295264
62                 X    =         1613996
66
 Y    =      -21238991
00  feet           Y    =        -6473644
46  meter
 Z    =       -2582856
77                 Z    =         -787254
74
 XDOT =      13213
870286                 XDOT =        4027
587663
 YDOT =       5674
930760  feet/sec       YDOT =        1729
718896  meter/sec
 ZDOT =     -19599
004821                 ZDOT =       -5973
776669


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   07164
37422313  
00020000  00000-0  20000-3 0  9057
2 25544  51
6310 123
6099 0008145 314
3601  45
6897 15
78326543 10176


Satellite: ISS
Catalog Number: 25544
Epoch time:      07164
37422313   =   yrday
fracday
Element set:     905
Inclination:       51
6310  deg
RA of node:       123
6099  deg
Eccentricity:     
0008145     
Arg of perigee:   314
3601  deg
Mean anomaly:      45
6897  deg
Mean motion:   15
78326543  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1017
Checksum:              275


Coasting Arc #7 (Orbit 1032)
---------------------------------------

Vector Time (GMT): 2007/165/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2022116
05                 A    =         6709755
55  meter
 Y    =       -4237062
37  meter          E    =           
0009811
 Z    =        4796824
70                 I    =           51
90097
 XDOT =       5014
787674                 Wp   =            4
60133
 YDOT =      -5272
576898  meter/sec      RA   =          117
72295  deg
 ZDOT =      -2533
364007                 TA   =          110
14815
                                          MA   =          110
04258
                                          Ha   =            183
613  n
mi
                                          Hp   =            178
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6634239
02                 X    =        -1997888
60
 Y    =      -13901123
28  feet           Y    =        -4259540
47  meter
 Z    =       15737613
84                 Z    =         4787059
04
 XDOT =      16452
715467                 XDOT =        5085
680408
 YDOT =     -17298
480635  feet/sec       YDOT =       -5216
101758  meter/sec
 ZDOT =      -8311
561702                 ZDOT =       -2508
831000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12031757
91                 X    =        -3667279
81
 Y    =       -9678143
67  feet           Y    =        -2949898
19  meter
 Z    =       15700228
71                 Z    =         4785429
71
 XDOT =       6786
128179                 XDOT =        2068
411869
 YDOT =     -21823
365815  feet/sec       YDOT =       -6651
761901  meter/sec
 ZDOT =      -8219
479100                 ZDOT =       -2505
297230


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   07165
38725551  
00020000  00000-0  20000-3 0  9060
2 25544  51
6308 118
3726 0008249 318
4384  41
6154 15
78373077 10333


Satellite: ISS
Catalog Number: 25544
Epoch time:      07165
38725551   =   yrday
fracday
Element set:     906
Inclination:       51
6308  deg
RA of node:       118
3726  deg
Eccentricity:     
0008249     
Arg of perigee:   318
4384  deg
Mean anomaly:      41
6154  deg
Mean motion:   15
78373077  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1033
Checksum:              295


Coasting Arc #8 (Orbit 1048)
---------------------------------------

Vector Time (GMT): 2007/166/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4444347
72                 A    =         6714609
75  meter
 Y    =        3663579
29  meter          E    =           
0009747
 Z    =        3438759
60                 I    =           51
92974
 XDOT =      -1399
405179                 Wp   =           49
18283
 YDOT =      -6024
279653  meter/sec      RA   =          112
61936  deg
 ZDOT =       4607
326844                 TA   =          351
44590
                                          MA   =          351
46250
                                          Ha   =            183
846  n
mi
                                          Hp   =            178
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14581193
32                 X    =        -4501688
98
 Y    =       12019617
11  feet           Y    =         3613558
66  meter
 Z    =       11282019
70                 Z    =         3417030
53
 XDOT =      -4591
224342                 XDOT =       -1354
318381
 YDOT =     -19764
697024  feet/sec       YDOT =       -6039
677608  meter/sec
 ZDOT =      15115
901720                 ZDOT =        4600
636582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7782734
91                 X    =        -2372177
60
 Y    =       17272753
26  feet           Y    =         5264735
19  meter
 Z    =       11200330
12                 Z    =         3413860
62
 XDOT =     -11707
384619                 XDOT =       -3568
410832
 YDOT =     -15064
672157  feet/sec       YDOT =       -4591
712074  meter/sec
 ZDOT =      15089
933278                 ZDOT =        4599
411663


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   07166
40027086  
00020000  00000-0  20000-3 0  9073
2 25544  51
6308 113
1358 0008323 322
1006  37
9573 15
78392590 10494


Satellite: ISS
Catalog Number: 25544
Epoch time:      07166
40027086   =   yrday
fracday
Element set:     907
Inclination:       51
6308  deg
RA of node:       113
1358  deg
Eccentricity:     
0008323     
Arg of perigee:   322
1006  deg
Mean anomaly:      37
9573  deg
Mean motion:   15
78392590  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1049
Checksum:              279


Coasting Arc #9 (Orbit 1063)
---------------------------------------

Vector Time (GMT): 2007/167/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         494342
21                 A    =         6715964
84  meter
 Y    =        6027884
27  meter          E    =           
0008815
 Z    =       -2907929
91                 I    =           51
94489
 XDOT =      -5056
666306                 Wp   =          357
31421
 YDOT =       2856
889830  meter/sec      RA   =          107
42175  deg
 ZDOT =       5070
461259                 TA   =          329
29819
                                          MA   =          329
34974
                                          Ha   =            183
932  n
mi
                                          Hp   =            178
056

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1621857
65                 X    =          441026
91
 Y    =       19776523
19  feet           Y    =         6033114
87  meter
 Z    =       -9540452
48                 Z    =        -2905656
49
 XDOT =     -16590
112554                 XDOT =       -5112
867895
 YDOT =       9372
998129  feet/sec       YDOT =        2800
027916  meter/sec
 ZDOT =      16635
371585                 ZDOT =        5045
760257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10574288
37                 X    =         3223043
10
 Y    =       16795911
00  feet           Y    =         5119393
67  meter
 Z    =       -9531176
43                 Z    =        -2905102
58
 XDOT =      -9286
593823                 XDOT =       -2830
553797
 YDOT =      15218
982604  feet/sec       YDOT =        4638
745898  meter/sec
 ZDOT =      16542
345574                 ZDOT =        5042
106931


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   07167
34995638  
00020000  00000-0  20000-3 0  9085
2 25544  51
6312 108
2266 0008325 326
3877  33
6759 15
78407912 10647


Satellite: ISS
Catalog Number: 25544
Epoch time:      07167
34995638   =   yrday
fracday
Element set:     908
Inclination:       51
6312  deg
RA of node:       108
2266  deg
Eccentricity:     
0008325     
Arg of perigee:   326
3877  deg
Mean anomaly:      33
6759  deg
Mean motion:   15
78407912  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1064
Checksum:              314


Coasting Arc #10 (Orbit 1079)
---------------------------------------

Vector Time (GMT): 2007/168/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4289058
40                 A    =         6708568
26  meter
 Y    =       -1099825
63  meter          E    =           
0013599
 Z    =       -5050028
48                 I    =           51
92686
 XDOT =       -197
841256                 Wp   =           40
52776
 YDOT =       7485
580772  meter/sec      RA   =          102
31161  deg
 ZDOT =      -1790
846013                 TA   =          212
24524
                                          MA   =          212
32845
                                          Ha   =            184
036  n
mi
                                          Hp   =            177
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14071713
91                 X    =         4325569
91
 Y    =       -3608351
81  feet           Y    =        -1051657
72  meter
 Z    =      -16568334
90                 Z    =        -5029103
99
 XDOT =       -649
085484                 XDOT =        -272
831893
 YDOT =      24558
992034  feet/sec       YDOT =        7482
949499  meter/sec
 ZDOT =      -5875
479045                 ZDOT =       -1791
987626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10754125
75                 X    =         3277857
53
 Y    =       -9899113
06  feet           Y    =        -3017249
66  meter
 Z    =      -16489372
22                 Z    =        -5025960
65
 XDOT =      10393
014806                 XDOT =        3167
790913
 YDOT =      21124
341302  feet/sec       YDOT =        6438
699229  meter/sec
 ZDOT =      -5878
946115                 ZDOT =       -1791
902776


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   07168
36293697  
00020000  00000-0  20000-3 0  9095
2 25544  51
6307 102
9888 0008357 329
8821  30
1863 15
78432791 10803


Satellite: ISS
Catalog Number: 25544
Epoch time:      07168
36293697   =   yrday
fracday
Element set:     909
Inclination:       51
6307  deg
RA of node:       102
9888  deg
Eccentricity:     
0008357     
Arg of perigee:   329
8821  deg
Mean anomaly:      30
1863  deg
Mean motion:   15
78432791  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1080
Checksum:              320


Coasting Arc #11 (Orbit 1095)
---------------------------------------

Vector Time (GMT): 2007/169/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         775817
70                 A    =         6719446
65  meter
 Y    =       -6673322
98  meter          E    =           
0005313
 Z    =          77465
78                 I    =           51
96905
 XDOT =       4722
710395                 Wp   =          100
95458
 YDOT =        474
589905  meter/sec      RA   =           97
14799  deg
 ZDOT =      -6066
641876                 TA   =           78
20671
                                          MA   =           78
14712
                                          Ha   =            184
127  n
mi
                                          Hp   =            177
547

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2545333
66                 X    =          850005
80
 Y    =      -21894104
26  feet           Y    =        -6664232
56  meter
 Z    =         254152
82                 Z    =           81413
55
 XDOT =      15494
456678                 XDOT =        4746
522738
 YDOT =       1557
053495  feet/sec       YDOT =         527
536230  meter/sec
 ZDOT =     -19903
680696                 ZDOT =       -6043
641297

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8504314
83                 X    =        -2592115
16
 Y    =      -20334693
31  feet           Y    =        -6198014
52  meter
 Z    =         268319
82                 Z    =           81783
88
 XDOT =      12885
805555                 XDOT =        3927
593533
 YDOT =      -5664
794098  feet/sec       YDOT =       -1726
629241  meter/sec
 ZDOT =     -19816
684639                 ZDOT =       -6040
125478


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   07169
37589895  
00020000  00000-0  20000-3 0  9107
2 25544  51
6307  97
7512 0008510 334
0450  26
0287 15
78482159 10969


Satellite: ISS
Catalog Number: 25544
Epoch time:      07169
37589895   =   yrday
fracday
Element set:     910
Inclination:       51
6307  deg
RA of node:        97
7512  deg
Eccentricity:     
0008510     
Arg of perigee:   334
0450  deg
Mean anomaly:      26
0287  deg
Mean motion:   15
78482159  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1096
Checksum:              308


Coasting Arc #12 (Orbit 1111)
---------------------------------------

Vector Time (GMT): 2007/170/08:15:27
185
Vector Time (MET): N/A
Weight (LBS)     : 480788
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3920338
24                 A    =         6708187
61  meter
 Y    =       -1938420
42  meter          E    =           
0010779
 Z    =        5088539
25                 I    =           51
93295
 XDOT =       1527
620446                 Wp   =            3
63079
 YDOT =      -7377
452707  meter/sec      RA   =           91
98729  deg
 ZDOT =      -1622
719320                 TA   =          101
94209
                                          MA   =          101
82123
                                          Ha   =            184
290  n
mi
                                          Hp   =            177
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12862002
11                 X    =        -3923090
06
 Y    =       -6359647
05  feet           Y    =        -1982276
10  meter
 Z    =       16694682
58                 Z    =         5069487
47
 XDOT =       5011
878105                 XDOT =        1617
885443
 YDOT =     -24204
241166  feet/sec       YDOT =       -7359
865024  meter/sec
 ZDOT =      -5323
882284                 ZDOT =       -1615
080243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14393951
42                 X    =        -4387276
39
 Y    =        1047476
85  feet           Y    =          319270
94  meter
 Z    =       16622442
36                 Z    =         5066520
43
 XDOT =      -7785
949888                 XDOT =       -2373
157526
 YDOT =     -22390
635303  feet/sec       YDOT =       -6824
665640  meter/sec
 ZDOT =      -5295
839873                 ZDOT =       -1614
171993


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   07170
38884287  
00020000  00000-0  20000-3 0  9114
2 25544  51
6303  92
5136 0008548 336
8976  23
1803 15
78496069 11120


Satellite: ISS
Catalog Number: 25544
Epoch time:      07170
38884287   =   yrday
fracday
Element set:     911
Inclination:       51
6303  deg
RA of node:        92
5136  deg
Eccentricity:     
0008548     
Arg of perigee:   336
8976  deg
Mean anomaly:      23
1803  deg
Mean motion:   15
78496069  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1112
Checksum:              306

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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