Date: June 22nd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4574 66 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 1127)
---------------------------------------

Vector Time (GMT): 2007/171/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1188768
62                 A    =         6718578
39  meter
 Y    =       -6312048
24  meter          E    =           
0002698
 Z    =       -1976878
95                 I    =           51
96697
 XDOT =       4557
799695                 Wp   =           33
33906
 YDOT =       2620
135451  meter/sec      RA   =           86
73494  deg
 ZDOT =      -5626
553321                 TA   =          168
59049
                                          MA   =          168
58437
                                          Ha   =            184
645  n
mi
                                          Hp   =            177
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3900159
52                 X    =         1268865
73
 Y    =      -20708819
70  feet           Y    =        -6298306
62  meter
 Z    =       -6485823
32                 Z    =        -1970910
36
 XDOT =      14953
411072                 XDOT =        4555
494696
 YDOT =       8596
244917  feet/sec       YDOT =        2671
091278  meter/sec
 ZDOT =     -18459
820608                 ZDOT =       -5604
416970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11076379
86                 X    =        -3376080
58
 Y    =      -17934971
98  feet           Y    =        -5466579
46  meter
 Z    =       -6463973
33                 Z    =        -1970219
07
 XDOT =      15603
106007                 XDOT =        4755
826711
 YDOT =      -3015
044196  feet/sec       YDOT =        -918
985471  meter/sec
 ZDOT =     -18375
839038                 ZDOT =       -5600
955739


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   07171
40281764  
00020000  00000-0  20000-3 0  9007
2 25544  51
6322  87
2947 0008074 339
3520  20
7318 15
78191165 11289


Satellite: ISS
Catalog Number: 25544
Epoch time:      07171
40281764   =   yrday
fracday
Element set:     900
Inclination:       51
6322  deg
RA of node:        87
2947  deg
Eccentricity:     
0008074     
Arg of perigee:   339
3520  deg
Mean anomaly:      20
7318  deg
Mean motion:   15
78191165  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1128
Checksum:              278


Coasting Arc #2 (Orbit 1143)
---------------------------------------

Vector Time (GMT): 2007/172/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3852327
28                 A    =         6712571
64  meter
 Y    =       -3545324
80  meter          E    =           
0012873
 Z    =        4201608
22                 I    =           51
94396
 XDOT =       1944
636903                 Wp   =           34
98619
 YDOT =      -6487
375743  meter/sec      RA   =           81
54638  deg
 ZDOT =      -3675
245797                 TA   =           92
36942
                                          MA   =           92
22203
                                          Ha   =            184
771  n
mi
                                          Hp   =            177
557

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12638869
02                 X    =        -3832807
12
 Y    =      -11631643
05  feet           Y    =        -3588295
11  meter
 Z    =       13784803
88                 Z    =         4182940
69
 XDOT =       6380
042332                 XDOT =        2034
888705
 YDOT =     -21284
041151  feet/sec       YDOT =       -6465
124599  meter/sec
 ZDOT =     -12057
893034                 ZDOT =       -3665
580480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17230727
36                 X    =        -5251925
70
 Y    =         299718
67  feet           Y    =           91354
25  meter
 Z    =       13713830
66                 Z    =         4179975
58
 XDOT =      -9933
919195                 XDOT =       -3027
858571
 YDOT =     -18629
695851  feet/sec       YDOT =       -5678
331295  meter/sec
 ZDOT =     -12022
084171                 ZDOT =       -3664
331255


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   07172
41594651  
00020000  00000-0  20000-3 0  9012
2 25544  51
6322  82
0587 0008119 342
6263  17
4623 15
78217481 11443


Satellite: ISS
Catalog Number: 25544
Epoch time:      07172
41594651   =   yrday
fracday
Element set:     901
Inclination:       51
6322  deg
RA of node:        82
0587  deg
Eccentricity:     
0008119     
Arg of perigee:   342
6263  deg
Mean anomaly:      17
4623  deg
Mean motion:   15
78217481  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1144
Checksum:              277


Coasting Arc #3 (Orbit 1159)
---------------------------------------

Vector Time (GMT): 2007/173/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2242289
51                 A    =         6712396
71  meter
 Y    =        4724879
05  meter          E    =           
0009210
 Z    =        4197769
87                 I    =           51
93906
 XDOT =      -4240
620794                 Wp   =           57
52566
 YDOT =      -5285
902440  meter/sec      RA   =           76
45048  deg
 ZDOT =       3683
505782                 TA   =          355
12989
                                          MA   =          355
13884
                                          Ha   =            184
817  n
mi
                                          Hp   =            177
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7356592
88                 X    =        -2315349
08
 Y    =       15501571
70  feet           Y    =         4699395
47  meter
 Z    =       13772210
88                 Z    =         4186700
03
 XDOT =     -13912
797882                 XDOT =       -4199
091629
 YDOT =     -17342
199605  feet/sec       YDOT =       -5333
091724  meter/sec
 ZDOT =      12084
992723                 ZDOT =        3663
005095

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5544061
60                 X    =         1689829
98
 Y    =       16273230
39  feet           Y    =         4960080
62  meter
 Z    =       13730889
63                 Z    =         4185175
16
 XDOT =     -20937
022292                 XDOT =       -6381
604395
 YDOT =      -3000
799456  feet/sec       YDOT =        -914
643674  meter/sec
 ZDOT =      12006
894977                 ZDOT =        3659
701589


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   07173
42905849  
00020000  00000-0  20000-3 0  9020
2 25544  51
6329  76
8227 0008017 345
6486  14
4450 15
78265618 11607


Satellite: ISS
Catalog Number: 25544
Epoch time:      07173
42905849   =   yrday
fracday
Element set:     902
Inclination:       51
6329  deg
RA of node:        76
8227  deg
Eccentricity:     
0008017     
Arg of perigee:   345
6486  deg
Mean anomaly:      14
4450  deg
Mean motion:   15
78265618  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1160
Checksum:              299


Coasting Arc #4 (Orbit 1174)
---------------------------------------

Vector Time (GMT): 2007/174/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3464319
87                 A    =         6718451
52  meter
 Y    =        5397007
29  meter          E    =           
0013716
 Z    =       -1976305
26                 I    =           51
95094
 XDOT =      -3250
808987                 Wp   =           12
07065
 YDOT =       4142
291175  meter/sec      RA   =           71
26039  deg
 ZDOT =       5633
649539                 TA   =          325
96864
                                          MA   =          326
05652
                                          Ha   =            185
019  n
mi
                                          Hp   =            177
102

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11365878
84                 X    =         3413312
81
 Y    =       17706716
84  feet           Y    =         5435462
34  meter
 Z    =       -6483941
16                 Z    =        -1959598
75
 XDOT =     -10665
383816                 XDOT =       -3324
254348
 YDOT =      13590
194143  feet/sec       YDOT =        4105
527388  meter/sec
 ZDOT =      18483
102161                 ZDOT =        5617
679260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20614969
90                 X    =         6283442
83
 Y    =        4307763
59  feet           Y    =         1313006
34  meter
 Z    =       -6420179
51                 Z    =        -1956870
71
 XDOT =       2434
905723                 XDOT =         742
159264
 YDOT =      15705
957977  feet/sec       YDOT =        4787
175991  meter/sec
 ZDOT =      18423
184202                 ZDOT =        5615
386545


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   07174
37883877  
00020000  00000-0  20000-3 0  9032
2 25544  51
6326  71
9134 0008203 349
7130  10
3866 15
78242813 11759


Satellite: ISS
Catalog Number: 25544
Epoch time:      07174
37883877   =   yrday
fracday
Element set:     903
Inclination:       51
6326  deg
RA of node:        71
9134  deg
Eccentricity:     
0008203     
Arg of perigee:   349
7130  deg
Mean anomaly:      10
3866  deg
Mean motion:   15
78242813  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1175
Checksum:              293


Coasting Arc #5 (Orbit 1190)
---------------------------------------

Vector Time (GMT): 2007/175/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3466175
21                 A    =         6708072
46  meter
 Y    =       -2346489
28  meter          E    =           
0016762
 Z    =       -5254613
87                 I    =           51
90667
 XDOT =       3572
391095                 Wp   =           55
54693
 YDOT =       6785
311527  meter/sec      RA   =           66
13615  deg
 ZDOT =       -665
747299                 TA   =          208
09815
                                          MA   =          208
18872
                                          Ha   =            185
035  n
mi
                                          Hp   =            176
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11371965
92                 X    =         3517682
44
 Y    =       -7698455
63  feet           Y    =        -2307439
79  meter
 Z    =      -17239546
81                 Z    =        -5237650
35
 XDOT =      11720
443225                 XDOT =        3499
485331
 YDOT =      22261
520759  feet/sec       YDOT =        6824
852471  meter/sec
 ZDOT =      -2184
210297                 ZDOT =        -648
568644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2332849
38                 X    =          711052
49
 Y    =      -13614108
92  feet           Y    =        -4149580
40  meter
 Z    =      -17175670
42                 Z    =        -5235144
34
 XDOT =      23219
827851                 XDOT =        7077
403529
 YDOT =       6683
900695  feet/sec       YDOT =        2037
252932  meter/sec
 ZDOT =      -2118
516307                 ZDOT =        -645
723770


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   07175
39192137  
00020000  00000-0  20000-3 0  9048
2 25544  51
6336  66
6767 0008192 353
3405   6
7650 15
78280328 11917


Satellite: ISS
Catalog Number: 25544
Epoch time:      07175
39192137   =   yrday
fracday
Element set:     904
Inclination:       51
6336  deg
RA of node:        66
6767  deg
Eccentricity:     
0008192     
Arg of perigee:   353
3405  deg
Mean anomaly:       6
7650  deg
Mean motion:   15
78280328  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1191
Checksum:              297


Coasting Arc #6 (Orbit 1206)
---------------------------------------

Vector Time (GMT): 2007/176/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2617661
44                 A    =         6719612
70  meter
 Y    =       -6128021
18  meter          E    =           
0005942
 Z    =        -871549
97                 I    =           51
93381
 XDOT =       4709
172796                 Wp   =           87
40271
 YDOT =      -1165
894573  meter/sec      RA   =           60
99060  deg
 ZDOT =      -5980
690702                 TA   =          102
07844
                                          MA   =          102
01185
                                          Ha   =            185
095  n
mi
                                          Hp   =            176
673

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8588128
08                 X    =        -2544708
60
 Y    =      -20105056
37  feet           Y    =        -6156885
30  meter
 Z    =       -2859415
92                 Z    =         -884090
45
 XDOT =      15450
041981                 XDOT =        4750
913285
 YDOT =      -3825
113427  feet/sec       YDOT =       -1112
999594  meter/sec
 ZDOT =     -19621
688654                 ZDOT =       -5957
712204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20600102
62                 X    =        -6278911
28
 Y    =       -7302584
55  feet           Y    =        -2225827
77  meter
 Z    =       -2907494
78                 Z    =         -886204
41
 XDOT =       7186
375471                 XDOT =        2190
407243
 YDOT =     -12538
861086  feet/sec       YDOT =       -3821
844859  meter/sec
 ZDOT =     -19534
937767                 ZDOT =       -5954
249031


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   07176
40498843  
00020000  00000-0  20000-3 0  9055
2 25544  51
6344  61
4404 0008203 357
1265   2
9852 15
78302626 12072


Satellite: ISS
Catalog Number: 25544
Epoch time:      07176
40498843   =   yrday
fracday
Element set:     905
Inclination:       51
6344  deg
RA of node:        61
4404  deg
Eccentricity:     
0008203     
Arg of perigee:   357
1265  deg
Mean anomaly:       2
9852  deg
Mean motion:   15
78302626  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1207
Checksum:              279


Coasting Arc #7 (Orbit 1222)
---------------------------------------

Vector Time (GMT): 2007/177/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4708508
87                 A    =         6710031
23  meter
 Y    =        -269006
76  meter          E    =           
0013609
 Z    =        4772249
93                 I    =           51
88639
 XDOT =      -2240
389976                 Wp   =           28
84694
 YDOT =      -6907
369830  meter/sec      RA   =           55
81281  deg
 ZDOT =      -2585
108806                 TA   =           86
46146
                                          MA   =           86
30583
                                          Ha   =            185
263  n
mi
                                          Hp   =            176
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15447863
76                 X    =        -4728333
73
 Y    =        -882568
10  feet           Y    =         -321771
67  meter
 Z    =       15656987
95                 Z    =         4749327
64
 XDOT =      -7350
360814                 XDOT =       -2150
426173
 YDOT =     -22661
974508  feet/sec       YDOT =       -6931
919640  meter/sec
 ZDOT =      -8481
328103                 ZDOT =       -2595
775439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10979065
48                 X    =        -3346419
16
 Y    =       11026461
16  feet           Y    =         3360865
36  meter
 Z    =       15570291
21                 Z    =         4745824
76
 XDOT =     -20986
840592                 XDOT =       -6396
789013
 YDOT =      -8793
720100  feet/sec       YDOT =       -2680
325887  meter/sec
 ZDOT =      -8522
398574                 ZDOT =       -2597
627085


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   07177
41803987  
00020000  00000-0  20000-3 0  9067
2 25544  51
6343  56
2044 0008252    
8759 359
2420 15
78331117 12231


Satellite: ISS
Catalog Number: 25544
Epoch time:      07177
41803987   =   yrday
fracday
Element set:     906
Inclination:       51
6343  deg
RA of node:        56
2044  deg
Eccentricity:     
0008252     
Arg of perigee:      
8759  deg
Mean anomaly:     359
2420  deg
Mean motion:   15
78331117  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1223
Checksum:              280


Coasting Arc #8 (Orbit 1238)
---------------------------------------

Vector Time (GMT): 2007/178/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1103939
37                 A    =         6714577
58  meter
 Y    =        5635807
77  meter          E    =           
0015225
 Z    =        3460305
27                 I    =           51
88503
 XDOT =      -5987
939465                 Wp   =           58
52902
 YDOT =      -1643
548266  meter/sec      RA   =           50
70741  deg
 ZDOT =       4580
331604                 TA   =          342
46340
                                          MA   =          342
51592
                                          Ha   =            185
285  n
mi
                                          Hp   =            176
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3621848
32                 X    =         1024027
27
 Y    =       18490182
97  feet           Y    =         5647705
12  meter
 Z    =       11352707
58                 Z    =         3465475
28
 XDOT =     -19645
470685                 XDOT =       -5991
366564
 YDOT =      -5392
218720  feet/sec       YDOT =       -1710
528858  meter/sec
 ZDOT =      15027
334660                 ZDOT =        4551
233379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16348259
00                 X    =         4982949
34
 Y    =        9342444
58  feet           Y    =         2847577
11  meter
 Z    =       11372852
67                 Z    =         3466445
49
 XDOT =     -16260
086067                 XDOT =       -4956
074233
 YDOT =      10266
971299  feet/sec       YDOT =        3129
372852  meter/sec
 ZDOT =      14917
136748                 ZDOT =        4546
743281


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   07178
43107609  
00020000  00000-0  20000-3 0  9079
2 25544  51
6346  50
9674 0008284   4
7277 355
3965 15
78346791 12399


Satellite: ISS
Catalog Number: 25544
Epoch time:      07178
43107609   =   yrday
fracday
Element set:     907
Inclination:       51
6346  deg
RA of node:        50
9674  deg
Eccentricity:     
0008284     
Arg of perigee:     4
7277  deg
Mean anomaly:     355
3965  deg
Mean motion:   15
78346791  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1239
Checksum:              320


Coasting Arc #9 (Orbit 1253)
---------------------------------------

Vector Time (GMT): 2007/179/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5555096
06                 A    =         6716149
54  meter
 Y    =        2418266
10  meter          E    =           
0011535
 Z    =       -2889209
52                 I    =           51
87172
 XDOT =        108
158610                 Wp   =           26
87236
 YDOT =       5797
787794  meter/sec      RA   =           45
50555  deg
 ZDOT =       5078
587835                 TA   =          299
95315
                                          MA   =          300
06762
                                          Ha   =            185
381  n
mi
                                          Hp   =            176
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18225380
77                 X    =         5541677
07
 Y    =        7933943
91  feet           Y    =         2480311
91  meter
 Z    =       -9479033
85                 Z    =        -2862254
86
 XDOT =        354
851083                 XDOT =          18
647949
 YDOT =      19021
613497  feet/sec       YDOT =        5798
495692  meter/sec
 ZDOT =      16662
033580                 ZDOT =        5078
897120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17772607
95                 X    =         5417090
90
 Y    =       -9009607
83  feet           Y    =        -2746128
47  meter
 Z    =       -9376855
89                 Z    =        -2858065
67
 XDOT =      14154
944840                 XDOT =        4314
427187
 YDOT =      10641
129923  feet/sec       YDOT =        3243
416401  meter/sec
 ZDOT =      16663
810246                 ZDOT =        5079
129363


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   07179
38078296  
00020000  00000-0  20000-3 0  9084
2 25544  51
6351  46
0581 0008279   7
8119 352
3174 15
78384185 12546


Satellite: ISS
Catalog Number: 25544
Epoch time:      07179
38078296   =   yrday
fracday
Element set:     908
Inclination:       51
6351  deg
RA of node:        46
0581  deg
Eccentricity:     
0008279     
Arg of perigee:     7
8119  deg
Mean anomaly:     352
3174  deg
Mean motion:   15
78384185  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1254
Checksum:              312


Coasting Arc #10 (Orbit 1269)
---------------------------------------

Vector Time (GMT): 2007/180/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1069886
91                 A    =         6708541
64  meter
 Y    =       -4302655
01  meter          E    =           
0018610
 Z    =       -5050158
71                 I    =           51
82577
 XDOT =       6506
495193                 Wp   =           52
49571
 YDOT =       3705
983269  meter/sec      RA   =           40
38971  deg
 ZDOT =      -1772
360794                 TA   =          200
42977
                                          MA   =          200
50431
                                          Ha   =            185
368  n
mi
                                          Hp   =            175
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3510127
64                 X    =         1142453
01
 Y    =      -14116322
22  feet           Y    =        -4290284
04  meter
 Z    =      -16568762
18                 Z    =        -5044785
93
 XDOT =      21346
769006                 XDOT =        6473
180555
 YDOT =      12158
737760  feet/sec       YDOT =        3778
556683  meter/sec
 ZDOT =      -5814
832002                 ZDOT =       -1740
832377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8770623
46                 X    =        -2673286
03
 Y    =      -11632960
98  feet           Y    =        -3545726
51  meter
 Z    =      -16548891
56                 Z    =        -5044102
15
 XDOT =      22002
757837                 XDOT =        6706
440589
 YDOT =      -8455
811864  feet/sec       YDOT =       -2577
331456  meter/sec
 ZDOT =      -5695
219336                 ZDOT =       -1735
902854


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   07180
39378888  
00020000  00000-0  20000-3 0  9098
2 25544  51
6356  40
8213 0008356  11
6640 348
4718 15
78420022 12702


Satellite: ISS
Catalog Number: 25544
Epoch time:      07180
39378888   =   yrday
fracday
Element set:     909
Inclination:       51
6356  deg
RA of node:        40
8213  deg
Eccentricity:     
0008356     
Arg of perigee:    11
6640  deg
Mean anomaly:     348
4718  deg
Mean motion:   15
78420022  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1270
Checksum:              292


Coasting Arc #11 (Orbit 1285)
---------------------------------------

Vector Time (GMT): 2007/181/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5521054
63                 A    =         6719675
06  meter
 Y    =       -3828820
77  meter          E    =           
0010996
 Z    =          71258
06                 I    =           51
84018
 XDOT =       2652
444976                 Wp   =           93
23125
 YDOT =      -3952
281615  meter/sec      RA   =           35
21860  deg
 ZDOT =      -6055
716153                 TA   =           85
99594
                                          MA   =           85
87025
                                          Ha   =            185
441  n
mi
                                          Hp   =            175
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18113696
30                 X    =        -5478176
02
 Y    =      -12561747
93  feet           Y    =        -3890320
57  meter
 Z    =         233786
28                 Z    =           44540
24
 XDOT =       8702
247297                 XDOT =        2725
860187
 YDOT =     -12966
803199  feet/sec       YDOT =       -3922
208614  meter/sec
 ZDOT =     -19867
835146                 ZDOT =       -6042
653247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21014754
80                 X    =        -6405297
26
 Y    =        6657381
26  feet           Y    =         2029169
81  meter
 Z    =         132347
19                 Z    =           40339
42
 XDOT =      -4389
106978                 XDOT =       -1337
799807
 YDOT =     -13368
923034  feet/sec       YDOT =       -4074
847741  meter/sec
 ZDOT =     -19818
841983                 ZDOT =       -6040
783036


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   07181
40678019  
00020000  00000-0  20000-3 0  9102
2 25544  51
6355  35
5840 0008248  15
0780 345
0630 15
78402195 12865


Satellite: ISS
Catalog Number: 25544
Epoch time:      07181
40678019   =   yrday
fracday
Element set:     910
Inclination:       51
6355  deg
RA of node:        35
5840  deg
Eccentricity:     
0008248     
Arg of perigee:    15
0780  deg
Mean anomaly:     345
0630  deg
Mean motion:   15
78402195  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1286
Checksum:              279


Coasting Arc #12 (Orbit 1301)
---------------------------------------

Vector Time (GMT): 2007/182/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3547336
29                 A    =         6708216
62  meter
 Y    =        2568381
71  meter          E    =           
0012792
 Z    =        5078346
12                 I    =           51
77786
 XDOT =      -5803
346753                 Wp   =           30
67116
 YDOT =      -4817
196956  meter/sec      RA   =           30
04784  deg
 ZDOT =      -1604
896609                 TA   =           74
76205
                                          MA   =           74
62065
                                          Ha   =            185
506  n
mi
                                          Hp   =            175
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11638242
41                 X    =        -3600462
05
 Y    =        8426449
19  feet           Y    =         2528415
25  meter
 Z    =       16661240
54                 Z    =         5060984
88
 XDOT =     -19039
851551                 XDOT =       -5741
252632
 YDOT =     -15804
451956  feet/sec       YDOT =       -4881
745698  meter/sec
 ZDOT =      -5265
408823                 ZDOT =       -1632
939167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -254062
42                 X    =          -77438
23
 Y    =       14441747
62  feet           Y    =         4401844
67  meter
 Z    =       16595844
27                 Z    =         5058413
33
 XDOT =     -22979
082517                 XDOT =       -7004
024351
 YDOT =       5816
537073  feet/sec       YDOT =        1772
880500  meter/sec
 ZDOT =      -5371
967034                 ZDOT =       -1637
375552


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   07182
41975357  
00020000  00000-0  20000-3 0  9110
2 25544  51
6354  30
3467 0008405  17
4197 342
7255 15
78492893 13025


Satellite: ISS
Catalog Number: 25544
Epoch time:      07182
41975357   =   yrday
fracday
Element set:     911
Inclination:       51
6354  deg
RA of node:        30
3467  deg
Eccentricity:     
0008405     
Arg of perigee:    17
4197  deg
Mean anomaly:     342
7255  deg
Mean motion:   15
78492893  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1302
Checksum:              297

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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