Date: February 20th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3218)
---------------------------------------

Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6342873
58                 A    =         6718953
96  meter
 Y    =        1845060
83  meter          E    =           
0022367
 Z    =        1148600
13                 I    =           51
60624
 XDOT =      -2338
800492                 Wp   =          188
07975
 YDOT =      -4386
871511  meter/sec      RA   =          351
70056  deg
 ZDOT =      -5904
152459                 TA   =          339
29511
                                          MA   =          339
38559
                                          Ha   =            186
766  n
mi
                                          Hp   =            175
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20809952
70                 X    =        -6368613
47
 Y    =        6053349
18  feet           Y    =         1773987
44  meter
 Z    =        3768373
15                 Z    =         1117724
52
 XDOT =      -7673
229961                 XDOT =       -2260
891400
 YDOT =     -14392
623066  feet/sec       YDOT =       -4412
590098  meter/sec
 ZDOT =     -19370
578935                 ZDOT =       -5915
324535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20906322
01                 X    =        -6372246
95
 Y    =       -5786337
71  feet           Y    =        -1763675
74  meter
 Z    =        3652642
85                 Z    =         1113325
54
 XDOT =        696
926989                 XDOT =         212
423346
 YDOT =     -14696
630742  feet/sec       YDOT =       -4479
533050  meter/sec
 ZDOT =     -19413
088385                 ZDOT =       -5917
109340


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   07050
53377715  
00020000  00000-0  20000-3 0  9009
2 25544  51
6348 352
0191 0020867 225
8056 134
1396 15
78470295 32191


Satellite: ISS
Catalog Number: 25544
Epoch time:      07050
53377715   =   yrday
fracday
Element set:     900
Inclination:       51
6348  deg
RA of node:       352
0191  deg
Eccentricity:     
0020867     
Arg of perigee:   225
8056  deg
Mean anomaly:     134
1396  deg
Mean motion:   15
78470295  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3219
Checksum:              292


Coasting Arc #2 (Orbit 3234)
---------------------------------------

Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         537541
10                 A    =         6707238
69  meter
 Y    =        4156885
52  meter          E    =           
0018431
 Z    =        5246999
71                 I    =           51
53929
 XDOT =      -7545
964159                 Wp   =          226
61354
 YDOT =       1473
779717  meter/sec      RA   =          346
53384  deg
 ZDOT =       -407
864555                 TA   =          227
18804
                                          MA   =          227
34312
                                          Ha   =            186
325  n
mi
                                          Hp   =            175
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1763586
27                 X    =          465529
71
 Y    =       13638075
86  feet           Y    =         4162494
34  meter
 Z    =       17214565
98                 Z    =         5249435
84
 XDOT =     -24757
100260                 XDOT =       -7559
902046
 YDOT =       4835
235292  feet/sec       YDOT =        1389
318571  meter/sec
 ZDOT =      -1338
138303                 ZDOT =        -444
556184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5526209
34                 X    =        -1684388
61
 Y    =       12579161
32  feet           Y    =         3834128
37  meter
 Z    =       17224237
07                 Z    =         5249947
46
 XDOT =     -22833
685869                 XDOT =       -6959
707453
 YDOT =      -8070
367203  feet/sec       YDOT =       -2459
847924  meter/sec
 ZDOT =      -1475
753243                 ZDOT =        -449
809589


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   07051
54670221  
00020000  00000-0  20000-3 0  9010
2 25544  51
6349 346
7824 0020898 230
0598 129
8732 15
78548380 32352


Satellite: ISS
Catalog Number: 25544
Epoch time:      07051
54670221   =   yrday
fracday
Element set:     901
Inclination:       51
6349  deg
RA of node:       346
7824  deg
Eccentricity:     
0020898     
Arg of perigee:   230
0598  deg
Mean anomaly:     129
8732  deg
Mean motion:   15
78548380  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3235
Checksum:              304


Coasting Arc #3 (Orbit 3250)
---------------------------------------

Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6432397
28                 A    =         6717617
95  meter
 Y    =        -612142
95  meter          E    =           
0007798
 Z    =        1856246
49                 I    =           51
54688
 XDOT =      -1140
531656                 Wp   =          208
68332
 YDOT =       5111
258800  meter/sec      RA   =          341
37683  deg
 ZDOT =       5640
856767                 TA   =          171
96191
                                          MA   =          171
94941
                                          Ha   =            186
033  n
mi
                                          Hp   =            175
282

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21103665
61                 X    =         6429747
08
 Y    =       -2008343
02  feet           Y    =         -540227
01  meter
 Z    =        6090047
53                 Z    =         1887488
29
 XDOT =      -3741
901758                 XDOT =       -1225
003646
 YDOT =      16769
221786  feet/sec       YDOT =        5098
032735  meter/sec
 ZDOT =      18506
747923                 ZDOT =        5635
110678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19296194
49                 X    =         5881480
08
 Y    =        8695580
84  feet           Y    =         2650413
04  meter
 Z    =        6207300
11                 Z    =         1891985
07
 XDOT =     -11014
679461                 XDOT =       -3357
274300
 YDOT =      11253
441996  feet/sec       YDOT =        3430
049120  meter/sec
 ZDOT =      18485
808982                 ZDOT =        5634
474578


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   07052
55959858  
00020000  00000-0  20000-3 0  9029
2 25544  51
6346 341
5440 0020868 233
9056 126
0178 15
78578240 32513


Satellite: ISS
Catalog Number: 25544
Epoch time:      07052
55959858   =   yrday
fracday
Element set:     902
Inclination:       51
6346  deg
RA of node:       341
5440  deg
Eccentricity:     
0020868     
Arg of perigee:   233
9056  deg
Mean anomaly:     126
0178  deg
Mean motion:   15
78578240  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3251
Checksum:              304


Coasting Arc #4 (Orbit 3265)
---------------------------------------

Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2409523
79                 A    =         6711507
73  meter
 Y    =       -4683329
84  meter          E    =           
0017197
 Z    =       -4160547
94                 I    =           51
50003
 XDOT =       6771
297101                 Wp   =          215
59687
 YDOT =        201
571605  meter/sec      RA   =          336
15439  deg
 ZDOT =       3673
236388                 TA   =           92
02423
                                          MA   =           91
82728
                                          Ha   =            185
703  n
mi
                                          Hp   =            175
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7905261
78                 X    =         2481925
36
 Y    =      -15365255
39  feet           Y    =        -4655980
50  meter
 Z    =      -13650091
66                 Z    =        -4148666
59
 XDOT =      22215
541670                 XDOT =        6750
696103
 YDOT =        661
324165  feet/sec       YDOT =         277
176950  meter/sec
 ZDOT =      12051
300485                 ZDOT =        3706
080972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14382214
71                 X    =         4383699
04
 Y    =       -9640351
28  feet           Y    =        -2938379
07  meter
 Z    =      -13606056
24                 Z    =        -4147125
94
 XDOT =      18403
219817                 XDOT =        5609
301400
 YDOT =      10173
163119  feet/sec       YDOT =        3100
780119  meter/sec
 ZDOT =      12174
673391                 ZDOT =        3710
840450


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   07053
50916092  
00020000  00000-0  20000-3 0  9039
2 25544  51
6349 336
6333 0020844 237
4989 122
4162 15
78632389 32664


Satellite: ISS
Catalog Number: 25544
Epoch time:      07053
50916092   =   yrday
fracday
Element set:     903
Inclination:       51
6349  deg
RA of node:       336
6333  deg
Eccentricity:     
0020844     
Arg of perigee:   237
4989  deg
Mean anomaly:     122
4162  deg
Mean motion:   15
78632389  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3266
Checksum:              305


Coasting Arc #5 (Orbit 3281)
---------------------------------------

Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5053834
53                 A    =         6710770
74  meter
 Y    =       -1084812
02  meter          E    =           
0012127
 Z    =       -4266993
97                 I    =           51
47314
 XDOT =       4139
907579                 Wp   =          235
39871
 YDOT =      -5485
762247  meter/sec      RA   =          331
02293  deg
 ZDOT =      -3508
410328                 TA   =          359
06583
                                          MA   =          359
06809
                                          Ha   =            185
186  n
mi
                                          Hp   =            175
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16580821
93                 X    =        -5020600
33
 Y    =       -3559094
54  feet           Y    =        -1141141
01  meter
 Z    =      -13999324
05                 Z    =        -4291464
51
 XDOT =      13582
373946                 XDOT =        4217
985512
 YDOT =     -17997
907635  feet/sec       YDOT =       -5439
030945  meter/sec
 ZDOT =     -11510
532572                 ZDOT =       -3488
109204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12950981
92                 X    =        -3947459
29
 Y    =      -10829475
24  feet           Y    =        -3300824
05  meter
 Z    =      -14091359
66                 Z    =        -4295046
42
 XDOT =      19664
038551                 XDOT =        5993
598950
 YDOT =      -8635
995001  feet/sec       YDOT =       -2632
251276  meter/sec
 ZDOT =     -11434
973205                 ZDOT =       -3485
379833


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   07054
52199812  
00020000  00000-0  20000-3 0  9046
2 25544  51
6354 331
3956 0020786 241
5332 118
3740 15
78689295 32828


Satellite: ISS
Catalog Number: 25544
Epoch time:      07054
52199812   =   yrday
fracday
Element set:     904
Inclination:       51
6354  deg
RA of node:       331
3956  deg
Eccentricity:     
0020786     
Arg of perigee:   241
5332  deg
Mean anomaly:     118
3740  deg
Mean motion:   15
78689295  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3282
Checksum:              306


Coasting Arc #6 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2007/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4515624
16                 A    =         6717652
17  meter
 Y    =        4673892
83  meter          E    =           
0016311
 Z    =        1667070
14                 I    =           51
47160
 XDOT =      -4581
076664                 Wp   =          202
20819
 YDOT =      -2396
407778  meter/sec      RA   =          325
79881  deg
 ZDOT =      -5723
134753                 TA   =          319
27306
                                          MA   =          319
39489
                                          Ha   =            185
082  n
mi
                                          Hp   =            175
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14815039
88                 X    =        -4575650
90
 Y    =       15334294
05  feet           Y    =         4623060
94  meter
 Z    =        5469390
23                 Z    =         1644987
81
 XDOT =     -15029
779083                 XDOT =       -4526
137640
 YDOT =      -7862
230242  feet/sec       YDOT =       -2447
328666  meter/sec
 ZDOT =     -18776
688823                 ZDOT =       -5745
255913

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20157960
01                 X    =        -6144146
21
 Y    =        7012609
92  feet           Y    =         2137443
50  meter
 Z    =        5387036
36                 Z    =         1641968
68
 XDOT =      -9278
598765                 XDOT =       -2828
116903
 YDOT =     -12267
867359  feet/sec       YDOT =       -3739
245971  meter/sec
 ZDOT =     -18860
067049                 ZDOT =       -5748
548437


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   07055
53480591  
00020000  00000-0  20000-3 0  9056
2 25544  51
6352 326
1575 0020855 245
2248 114
6748 15
78702288 32981


Satellite: ISS
Catalog Number: 25544
Epoch time:      07055
53480591   =   yrday
fracday
Element set:     905
Inclination:       51
6352  deg
RA of node:       326
1575  deg
Eccentricity:     
0020855     
Arg of perigee:   245
2248  deg
Mean anomaly:     114
6748  deg
Mean motion:   15
78702288  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3298
Checksum:              309


Coasting Arc #7 (Orbit 3313)
---------------------------------------

Vector Time (GMT): 2007/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2759464
57                 A    =         6706480
48  meter
 Y    =        3154947
02  meter          E    =           
0018827
 Z    =        5250194
15                 I    =           51
41194
 XDOT =      -5890
878998                 Wp   =          245
88401
 YDOT =       4951
177647  meter/sec      RA   =          320
62901  deg
 ZDOT =        113
687557                 TA   =          202
99090
                                          MA   =          203
07528
                                          Ha   =            184
678  n
mi
                                          Hp   =            175
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9053361
46                 X    =         2698476
38
 Y    =       10350876
06  feet           Y    =         3185463
77  meter
 Z    =       17225046
44                 Z    =         5263451
33
 XDOT =     -19327
030833                 XDOT =       -5946
358217
 YDOT =      16244
021152  feet/sec       YDOT =        4884
992347  meter/sec
 ZDOT =        372
990674                 ZDOT =          84
935546

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3568606
94                 X    =         1087711
39
 Y    =       13215053
13  feet           Y    =         4027948
19  meter
 Z    =       17275231
67                 Z    =         5265490
61
 XDOT =     -23504
075315                 XDOT =       -7164
042156
 YDOT =       5968
817477  feet/sec       YDOT =        1819
295567  meter/sec
 ZDOT =        265
617360                 ZDOT =          80
960171


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   07056
54758130  
00020000  00000-0  20000-3 0  9066
2 25544  51
6353 320
9187 0020960 249
4423 110
4494 15
78795435 33148


Satellite: ISS
Catalog Number: 25544
Epoch time:      07056
54758130   =   yrday
fracday
Element set:     906
Inclination:       51
6353  deg
RA of node:       320
9187  deg
Eccentricity:     
0020960     
Arg of perigee:   249
4423  deg
Mean anomaly:     110
4494  deg
Mean motion:   15
78795435  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3314
Checksum:              296


Coasting Arc #8 (Orbit 3329)
---------------------------------------

Vector Time (GMT): 2007/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5427391
28                 A    =         6717521
93  meter
 Y    =       -3665946
96  meter          E    =           
0007539
 Z    =        1497908
57                 I    =           51
42835
 XDOT =       1668
004096                 Wp   =          274
33203
 YDOT =       4817
819737  meter/sec      RA   =          315
45391  deg
 ZDOT =       5772
775204                 TA   =          102
23664
                                          MA   =          102
15221
                                          Ha   =            184
422  n
mi
                                          Hp   =            175
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17806401
84                 X    =         5460704
65
 Y    =      -12027385
03  feet           Y    =        -3605068
60  meter
 Z    =        4914398
19                 Z    =         1524355
07
 XDOT =       5472
454383                 XDOT =        1585
964124
 YDOT =      15806
495201  feet/sec       YDOT =        4836
013463  meter/sec
 ZDOT =      18939
551193                 ZDOT =        5780
679010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21182611
01                 X    =         6456459
84
 Y    =       -3470058
61  feet           Y    =        -1057673
86  meter
 Z    =        5013275
40                 Z    =         1528046
34
 XDOT =      -2003
797573                 XDOT =        -610
757500
 YDOT =      15055
930355  feet/sec       YDOT =        4589
047572  meter/sec
 ZDOT =      18969
841439                 ZDOT =        5782
007671


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   07057
56032950  
00020000  00000-0  20000-3 0  9075
2 25544  51
6356 315
6794 0020862 253
5709 106
3163 15
78804026 33302


Satellite: ISS
Catalog Number: 25544
Epoch time:      07057
56032950   =   yrday
fracday
Element set:     907
Inclination:       51
6356  deg
RA of node:       315
6794  deg
Eccentricity:     
0020862     
Arg of perigee:   253
5709  deg
Mean anomaly:     106
3163  deg
Mean motion:   15
78804026  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3330
Checksum:              289


Coasting Arc #9 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2007/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -200588
58                 A    =         6710157
19  meter
 Y    =       -5117722
33  meter          E    =           
0014346
 Z    =       -4329584
62                 I    =           51
38465
 XDOT =       6184
380434                 Wp   =          236
78842
 YDOT =      -3121
737914  meter/sec      RA   =          310
22547  deg
 ZDOT =       3387
660833                 TA   =           67
49733
                                          MA   =           67
34552
                                          Ha   =            184
182  n
mi
                                          Hp   =            175
053

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -658099
03                 X    =         -122314
80
 Y    =      -16790427
58  feet           Y    =        -5119527
74  meter
 Z    =      -14204673
94                 Z    =        -4330368
96
 XDOT =      20289
962055                 XDOT =        6202
372323
 YDOT =     -10241
922290  feet/sec       YDOT =       -3052
480144  meter/sec
 ZDOT =      11114
372813                 ZDOT =        3417
747419

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6242988
45                 X    =         1902862
88
 Y    =      -15597262
20  feet           Y    =        -4754045
52  meter
 Z    =      -14208265
96                 Z    =        -4330679
46
 XDOT =      21503
162159                 XDOT =        6554
163826
 YDOT =      -1667
569593  feet/sec       YDOT =        -508
275212  meter/sec
 ZDOT =      11226
993177                 ZDOT =        3421
987520


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   07058
50975167  
00020000  00000-0  20000-3 0  9087
2 25544  51
6359 310
7682 0020966 257
2948 102
5874 15
78862951 33452


Satellite: ISS
Catalog Number: 25544
Epoch time:      07058
50975167   =   yrday
fracday
Element set:     908
Inclination:       51
6359  deg
RA of node:       310
7682  deg
Eccentricity:     
0020966     
Arg of perigee:   257
2948  deg
Mean anomaly:     102
5874  deg
Mean motion:   15
78862951  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3345
Checksum:              331


Coasting Arc #10 (Orbit 3360)
---------------------------------------

Vector Time (GMT): 2007/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5071705
76                 A    =         6710687
05  meter
 Y    =        1487731
57  meter          E    =           
0013322
 Z    =       -4123179
91                 I    =           51
36942
 XDOT =       1066
388101                 Wp   =          267
86668
 YDOT =      -6679
141791  meter/sec      RA   =          305
08427  deg
 ZDOT =      -3711
890880                 TA   =          324
07376
                                          MA   =          324
16326
                                          Ha   =            183
892  n
mi
                                          Hp   =            174
931

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16639454
58                 X    =        -5067935
78
 Y    =        4881009
09  feet           Y    =         1431037
94  meter
 Z    =      -13527493
16                 Z    =        -4147808
39
 XDOT =       3498
648624                 XDOT =        1159
027125
 YDOT =     -21913
194851  feet/sec       YDOT =       -6666
698926  meter/sec
 ZDOT =     -12178
119685                 ZDOT =       -3706
485411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17161061
21                 X    =        -5230691
46
 Y    =       -1920226
95  feet           Y    =         -585285
17  meter
 Z    =      -13619819
24                 Z    =        -4151320
90
 XDOT =      11640
622305                 XDOT =        3548
061679
 YDOT =     -17566
630310  feet/sec       YDOT =       -5354
308918  meter/sec
 ZDOT =     -12158
666330                 ZDOT =       -3705
961497


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   07059
52243993  
00020000  00000-0  20000-3 0  9096
2 25544  51
6358 305
5297 0021072 261
4000  98
4778 15
78908721 33610


Satellite: ISS
Catalog Number: 25544
Epoch time:      07059
52243993   =   yrday
fracday
Element set:     909
Inclination:       51
6358  deg
RA of node:       305
5297  deg
Eccentricity:     
0021072     
Arg of perigee:   261
4000  deg
Mean anomaly:      98
4778  deg
Mean motion:   15
78908721  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3361
Checksum:              308


Coasting Arc #11 (Orbit 3376)
---------------------------------------

Vector Time (GMT): 2007/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1888744
42                 A    =         6716787
83  meter
 Y    =        6185229
54  meter          E    =           
0011091
 Z    =        1802625
05                 I    =           51
37433
 XDOT =      -5234
705529                 Wp   =          225
53684
 YDOT =         41
556981  meter/sec      RA   =          299
84933  deg
 ZDOT =      -5656
369251                 TA   =          294
36174
                                          MA   =          294
47748
                                          Ha   =            183
846  n
mi
                                          Hp   =            174
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6196668
04                 X    =        -1966524
73
 Y    =       20292747
82  feet           Y    =         6163673
72  meter
 Z    =        5914124
19                 Z    =         1793260
65
 XDOT =     -17174
230737                 XDOT =       -5207
304380
 YDOT =        136
341802  feet/sec       YDOT =         -16
827431  meter/sec
 ZDOT =     -18557
641899                 ZDOT =       -5681
732129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13325325
67                 X    =        -4061559
26
 Y    =       16523784
92  feet           Y    =         5036449
64  meter
 Z    =        5879745
02                 Z    =         1792146
28
 XDOT =     -14693
685201                 XDOT =       -4478
635249
 YDOT =      -5246
147104  feet/sec       YDOT =       -1599
025637  meter/sec
 ZDOT =     -18652
913722                 ZDOT =       -5685
408103


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   07060
53509984  
00020000  00000-0  20000-3 0  9106
2 25544  51
6355 300
2908 0020917 264
9480  94
9298 15
78926669 33771


Satellite: ISS
Catalog Number: 25544
Epoch time:      07060
53509984   =   yrday
fracday
Element set:     910
Inclination:       51
6355  deg
RA of node:       300
2908  deg
Eccentricity:     
0020917     
Arg of perigee:   264
9480  deg
Mean anomaly:      94
9298  deg
Mean motion:   15
78926669  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3377
Checksum:              329


Coasting Arc #12 (Orbit 3392)
---------------------------------------

Vector Time (GMT): 2007/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 479216
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3900221
57                 A    =         6705899
06  meter
 Y    =        1562350
57  meter          E    =           
0018659
 Z    =        5242554
29                 I    =           51
32490
 XDOT =      -3075
309555                 Wp   =          267
69279
 YDOT =       7051
716251  meter/sec      RA   =          294
67257  deg
 ZDOT =        186
214903                 TA   =          180
53003
                                          MA   =          180
53201
                                          Ha   =            183
723  n
mi
                                          Hp   =            174
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12796002
52                 X    =         3856994
62
 Y    =        5125822
07  feet           Y    =         1605723
65  meter
 Z    =       17199981
26                 Z    =         5261395
93
 XDOT =     -10089
598278                 XDOT =       -3154
838866
 YDOT =      23135
552005  feet/sec       YDOT =        7016
881762  meter/sec
 ZDOT =        610
941282                 ZDOT =         171
081875

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10046907
45                 X    =         3062297
39
 Y    =        9307226
45  feet           Y    =         2836842
62  meter
 Z    =       17270966
23                 Z    =         5264190
51
 XDOT =     -16982
250548                 XDOT =       -5176
189967
 YDOT =      17300
948220  feet/sec       YDOT =        5273
329018  meter/sec
 ZDOT =        555
014299                 ZDOT =         169
168358


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   07061
54772688  
00020000  00000-0  20000-3 0  9112
2 25544  51
6353 295
0507 0021038 269
2399  90
6356 15
79003334 33939


Satellite: ISS
Catalog Number: 25544
Epoch time:      07061
54772688   =   yrday
fracday
Element set:     911
Inclination:       51
6353  deg
RA of node:       295
0507  deg
Eccentricity:     
0021038     
Arg of perigee:   269
2399  deg
Mean anomaly:      90
6356  deg
Mean motion:   15
79003334  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3393
Checksum:              303

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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