Date: December 7th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12665 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


There are no maneuvers



Coasting Arc #1 (Orbit 3786)
---------------------------------------

Vector Time (GMT): 2007/339/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4863447
35                 A    =         6716458
39  meter
 Y    =       -2460329
80  meter          E    =           
0010003
 Z    =        3918029
37                 I    =           51
34848
 XDOT =        106
632467                 Wp   =          102
03157
 YDOT =       6590
892456  meter/sec      RA   =          298
07224  deg
 ZDOT =       3995
758072                 TA   =          306
33463
                                          MA   =          306
42693
                                          Ha   =            184
793  n
mi
                                          Hp   =            179
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15956192
09                 X    =         4871564
18
 Y    =       -8071948
15  feet           Y    =        -2405898
97  meter
 Z    =       12854427
06                 Z    =         3941675
99
 XDOT =        349
844053                 XDOT =          13
513092
 YDOT =      21623
662914  feet/sec       YDOT =        6591
563834  meter/sec
 ZDOT =      13109
442492                 ZDOT =        3996
050555

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9498614
85                 X    =         2895177
81
 Y    =      -15073669
88  feet           Y    =        -4594454
58  meter
 Z    =       12944245
84                 Z    =         3945406
13
 XDOT =      10223
970871                 XDOT =        3116
266321
 YDOT =      17731
375687  feet/sec       YDOT =        5404
523309  meter/sec
 ZDOT =      13111
216321                 ZDOT =        3996
298735


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07339
93621092  
00020000  00000-0  20000-3 0  9003
2 25544  51
6366 298
3847 0001079 268
8901  91
2140 15
77140841 37871


Satellite: ISS
Catalog Number: 25544
Epoch time:      07339
93621092   =   yrday
fracday
Element set:     900
Inclination:       51
6366  deg
RA of node:       298
3847  deg
Eccentricity:     
0001079     
Arg of perigee:   268
8901  deg
Mean anomaly:      91
2140  deg
Mean motion:   15
77140841  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3787
Checksum:              306


Coasting Arc #2 (Orbit 3801)
---------------------------------------

Vector Time (GMT): 2007/340/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         323512
52                 A    =         6720163
11  meter
 Y    =       -6176948
66  meter          E    =           
0004274
 Z    =       -2625402
96                 I    =           51
34868
 XDOT =       5334
415175                 Wp   =           47
28815
 YDOT =      -1931
341153  meter/sec      RA   =          292
84190  deg
 ZDOT =       5209
532491                 TA   =          282
69223
                                          MA   =          282
74001
                                          Ha   =            184
910  n
mi
                                          Hp   =            179
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1061392
77                 X    =          405314
07
 Y    =      -20265579
58  feet           Y    =        -6172873
27  meter
 Z    =       -8613526
76                 Z    =        -2623633
32
 XDOT =      17501
362124                 XDOT =        5330
307729
 YDOT =      -6336
421107  feet/sec       YDOT =       -1871
712277  meter/sec
 ZDOT =      17091
642030                 ZDOT =        5235
437456

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9744716
41                 X    =        -2970189
56
 Y    =      -17803545
15  feet           Y    =        -5426520
56  meter
 Z    =       -8607403
54                 Z    =        -2623536
60
 XDOT =      10147
440658                 XDOT =        3092
939913
 YDOT =     -13851
958674  feet/sec       YDOT =       -4222
077004  meter/sec
 ZDOT =      17190
118953                 ZDOT =        5239
548257


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07340
88665119  
00020000  00000-0  20000-3 0  9018
2 25544  51
6366 293
4797 0000887 264
2844  95
8219 15
77169456 38021


Satellite: ISS
Catalog Number: 25544
Epoch time:      07340
88665119   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       293
4797  deg
Eccentricity:     
0000887     
Arg of perigee:   264
2844  deg
Mean anomaly:      95
8219  deg
Mean motion:   15
77169456  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3802
Checksum:              331


Coasting Arc #3 (Orbit 3817)
---------------------------------------

Vector Time (GMT): 2007/341/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4439403
82                 A    =         6712077
17  meter
 Y    =         781801
61  meter          E    =           
0012542
 Z    =       -4984508
45                 I    =           51
31213
 XDOT =        794
545127                 Wp   =           75
33862
 YDOT =      -7422
856553  meter/sec      RA   =          287
69844  deg
 ZDOT =      -1872
696156                 TA   =          176
50294
                                          MA   =          176
49416
                                          Ha   =            184
881  n
mi
                                          Hp   =            178
933

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14564973
18                 X    =        -4423601
75
 Y    =        2564965
92  feet           Y    =          732246
72  meter
 Z    =      -16353374
17                 Z    =        -5006037
04
 XDOT =       2606
775350                 XDOT =         886
586993
 YDOT =     -24353
203913  feet/sec       YDOT =       -7413
456611  meter/sec
 ZDOT =      -6144
016261                 ZDOT =       -1868
613615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10773056
61                 X    =        -3283627
66
 Y    =        9998623
39  feet           Y    =         3047580
41  meter
 Z    =      -16435301
10                 Z    =        -5009479
77
 XDOT =     -10248
531232                 XDOT =       -3123
752320
 YDOT =     -21112
976948  feet/sec       YDOT =       -6435
235374  meter/sec
 ZDOT =      -6129
205851                 ZDOT =       -1868
181943


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07341
90042549  
00020000  00000-0  20000-3 0  9029
2 25544  51
6369 288
2489 0000718 265
6832  94
4250 15
77226535 38188


Satellite: ISS
Catalog Number: 25544
Epoch time:      07341
90042549   =   yrday
fracday
Element set:     902
Inclination:       51
6369  deg
RA of node:       288
2489  deg
Eccentricity:     
0000718     
Arg of perigee:   265
6832  deg
Mean anomaly:      94
4250  deg
Mean motion:   15
77226535  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3818
Checksum:              309


Coasting Arc #4 (Orbit 3833)
---------------------------------------

Vector Time (GMT): 2007/342/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1005644
87                 A    =         6722663
99  meter
 Y    =        6616971
09  meter          E    =           
0012428
 Z    =         562060
06                 I    =           51
34088
 XDOT =      -4853
134518                 Wp   =          131
21395
 YDOT =       -222
776041  meter/sec      RA   =          282
49373  deg
 ZDOT =      -5983
154005                 TA   =           42
63408
                                          MA   =           42
53769
                                          Ha   =            184
688  n
mi
                                          Hp   =            179
028

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3299359
80                 X    =        -1082292
54
 Y    =       21709222
73  feet           Y    =         6605296
75  meter
 Z    =        1844029
08                 Z    =          556989
38
 XDOT =     -15922
357344                 XDOT =       -4821
217093
 YDOT =       -730
892522  feet/sec       YDOT =        -276
867162  meter/sec
 ZDOT =     -19629
770359                 ZDOT =       -6006
653477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9326504
55                 X    =         2842718
59
 Y    =       19881169
39  feet           Y    =         6059780
43  meter
 Z    =        1825372
98                 Z    =          556373
68
 XDOT =     -12095
774311                 XDOT =       -3686
792010
 YDOT =       7508
361235  feet/sec       YDOT =        2288
548504  meter/sec
 ZDOT =     -19719
310942                 ZDOT =       -6010
445975


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07342
91416892  
00020000  00000-0  20000-3 0  9038
2 25544  51
6368 283
0166 0000929 280
1578  79
9482 15
77302754 38346


Satellite: ISS
Catalog Number: 25544
Epoch time:      07342
91416892   =   yrday
fracday
Element set:     903
Inclination:       51
6368  deg
RA of node:       283
0166  deg
Eccentricity:     
0000929     
Arg of perigee:   280
1578  deg
Mean anomaly:      79
9482  deg
Mean motion:   15
77302754  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3834
Checksum:              316


Coasting Arc #5 (Orbit 3849)
---------------------------------------

Vector Time (GMT): 2007/343/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4052568
58                 A    =         6710954
50  meter
 Y    =        1210512
03  meter          E    =           
0002304
 Z    =        5208800
54                 I    =           51
29586
 XDOT =      -1463
123519                 Wp   =           59
24941
 YDOT =       7543
248422  meter/sec      RA   =          277
31006  deg
 ZDOT =       -613
323659                 TA   =           36
61043
                                          MA   =           36
59469
                                          Ha   =            184
736  n
mi
                                          Hp   =            179
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13295828
69                 X    =         4013427
48
 Y    =        3971496
16  feet           Y    =         1255610
43  meter
 Z    =       17089240
63                 Z    =         5228393
34
 XDOT =      -4800
274011                 XDOT =       -1544
385067
 YDOT =      24748
190360  feet/sec       YDOT =        7526
432691  meter/sec
 ZDOT =      -2012
216730                 ZDOT =        -620
627752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13106135
12                 X    =         3994749
98
 Y    =       -4268508
49  feet           Y    =        -1301041
39  meter
 Z    =       17164004
34                 Z    =         5231588
52
 XDOT =       9874
811968                 XDOT =        3009
842688
 YDOT =      22101
816163  feet/sec       YDOT =        6736
633567  meter/sec
 ZDOT =      -2039
288917                 ZDOT =        -621
575262


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07343
92788827  
00020000  00000-0  20000-3 0  9041
2 25544  51
6367 277
7848 0000645 263
6937  96
4154 15
77257839 38503


Satellite: ISS
Catalog Number: 25544
Epoch time:      07343
92788827   =   yrday
fracday
Element set:     904
Inclination:       51
6367  deg
RA of node:       277
7848  deg
Eccentricity:     
0000645     
Arg of perigee:   263
6937  deg
Mean anomaly:      96
4154  deg
Mean motion:   15
77257839  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3850
Checksum:              346


Coasting Arc #6 (Orbit 3865)
---------------------------------------

Vector Time (GMT): 2007/344/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1535335
31                 A    =         6721462
03  meter
 Y    =       -6333090
43  meter          E    =           
0013366
 Z    =        1620746
24                 I    =           51
33089
 XDOT =       4486
192849                 Wp   =           62
66441
 YDOT =       2559
554787  meter/sec      RA   =          272
14673  deg
 ZDOT =       5721
747819                 TA   =          315
34248
                                          MA   =          315
45006
                                          Ha   =            184
640  n
mi
                                          Hp   =            178
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5037189
35                 X    =         1598165
41
 Y    =      -20777855
73  feet           Y    =        -6315570
42  meter
 Z    =        5317408
91                 Z    =         1628356
50
 XDOT =      14718
480475                 XDOT =        4429
442605
 YDOT =       8397
489458  feet/sec       YDOT =        2609
403649  meter/sec
 ZDOT =      18772
138514                 ZDOT =        5743
404556

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8083232
96                 X    =        -2463769
41
 Y    =      -19785133
67  feet           Y    =        -6030508
74  meter
 Z    =        5345767
81                 Z    =         1629390
03
 XDOT =      15321
791852                 XDOT =        4670
082157
 YDOT =      -1138
871825  feet/sec       YDOT =        -347
128132  meter/sec
 ZDOT =      18854
909225                 ZDOT =        5746
976332


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07344
94157356  
00020000  00000-0  20000-3 0  9052
2 25544  51
6376 272
5532 0000788 257
4008 102
7069 15
77367681 38664


Satellite: ISS
Catalog Number: 25544
Epoch time:      07344
94157356   =   yrday
fracday
Element set:     905
Inclination:       51
6376  deg
RA of node:       272
5532  deg
Eccentricity:     
0000788     
Arg of perigee:   257
4008  deg
Mean anomaly:     102
7069  deg
Mean motion:   15
77367681  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3866
Checksum:              318


Coasting Arc #7 (Orbit 3880)
---------------------------------------

Vector Time (GMT): 2007/345/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3798268
02                 A    =         6713567
65  meter
 Y    =       -3209209
11  meter          E    =           
0009539
 Z    =       -4520096
28                 I    =           51
30511
 XDOT =       2082
120779                 Wp   =          112
27078
 YDOT =      -6755
305661  meter/sec      RA   =          266
92450  deg
 ZDOT =       3048
117863                 TA   =          188
20706
                                          MA   =          188
22268
                                          Ha   =            184
628  n
mi
                                          Hp   =            178
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12461509
26                 X    =        -3740141
94
 Y    =      -10528901
28  feet           Y    =        -3251357
74  meter
 Z    =      -14829712
22                 Z    =        -4538407
72
 XDOT =       6831
104918                 XDOT =        2142
697602
 YDOT =     -22163
076314  feet/sec       YDOT =       -6731
684017  meter/sec
 ZDOT =      10000
386688                 ZDOT =        3058
378866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16217432
29                 X    =        -4943073
36
 Y    =       -1028506
76  feet           Y    =         -313488
86  meter
 Z    =      -14899812
19                 Z    =        -4541462
76
 XDOT =      -7910
268874                 XDOT =       -2411
049953
 YDOT =     -20628
062366  feet/sec       YDOT =       -6287
433409  meter/sec
 ZDOT =      10038
800530                 ZDOT =        3059
826402


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07345
89188036  
00020000  00000-0  20000-3 0  9067
2 25544  51
6381 267
6490 0000736 263
8246  96
2835 15
77384935 38812


Satellite: ISS
Catalog Number: 25544
Epoch time:      07345
89188036   =   yrday
fracday
Element set:     906
Inclination:       51
6381  deg
RA of node:       267
6490  deg
Eccentricity:     
0000736     
Arg of perigee:   263
8246  deg
Mean anomaly:      96
2835  deg
Mean motion:   15
77384935  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3881
Checksum:              331


Coasting Arc #8 (Orbit 3896)
---------------------------------------

Vector Time (GMT): 2007/346/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2141601
55                 A    =         6716764
56  meter
 Y    =        5263068
00  meter          E    =           
0004732
 Z    =       -3586476
86                 I    =           51
31905
 XDOT =      -4228
668489                 Wp   =           79
83063
 YDOT =      -4707
943219  meter/sec      RA   =          261
78855  deg
 ZDOT =      -4387
798272                 TA   =          143
30626
                                          MA   =          143
27385
                                          Ha   =            184
536  n
mi
                                          Hp   =            178
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7026251
81                 X    =        -2182872
33
 Y    =       17267283
46  feet           Y    =         5238889
20  meter
 Z    =      -11766656
38                 Z    =        -3596980
21
 XDOT =     -13873
584282                 XDOT =       -4154
394107
 YDOT =     -15446
007935  feet/sec       YDOT =       -4754
814611  meter/sec
 ZDOT =     -14395
663623                 ZDOT =       -4408
161503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5066063
16                 X    =         1544136
05
 Y    =       17914560
96  feet           Y    =         5460358
18  meter
 Z    =      -11806142
66                 Z    =        -3598512
28
 XDOT =     -19054
751374                 XDOT =       -5807
888219
 YDOT =      -4141
269138  feet/sec       YDOT =       -1262
258833  meter/sec
 ZDOT =     -14473
746752                 ZDOT =       -4411
598010


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07346
90551242  
00020000  00000-0  20000-3 0  9074
2 25544  51
6379 262
4169 0000760 269
6166  90
4911 15
77436342 38975


Satellite: ISS
Catalog Number: 25544
Epoch time:      07346
90551242   =   yrday
fracday
Element set:     907
Inclination:       51
6379  deg
RA of node:       262
4169  deg
Eccentricity:     
0000760     
Arg of perigee:   269
6166  deg
Mean anomaly:      90
4911  deg
Mean motion:   15
77436342  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3897
Checksum:              311


Coasting Arc #9 (Orbit 3912)
---------------------------------------

Vector Time (GMT): 2007/347/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3580057
92                 A    =         6718520
43  meter
 Y    =        4858778
89  meter          E    =           
0012591
 Z    =        2939016
34                 I    =           51
33041
 XDOT =      -2869
778123                 Wp   =           97
92479
 YDOT =       5137
035281  meter/sec      RA   =          256
55313  deg
 ZDOT =      -4980
371038                 TA   =           47
96691
                                          MA   =           47
85981
                                          Ha   =            184
459  n
mi
                                          Hp   =            178
709

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11745596
86                 X    =         3511183
05
 Y    =       15940875
61  feet           Y    =         4898427
62  meter
 Z    =        9642442
07                 Z    =         2956241
62
 XDOT =      -9415
282557                 XDOT =       -2902
814227
 YDOT =      16853
790291  feet/sec       YDOT =        5104
759765  meter/sec
 ZDOT =     -16339
799993                 ZDOT =       -4994
391948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19093438
06                 X    =         5819679
92
 Y    =        5121626
00  feet           Y    =         1561071
61  meter
 Z    =        9708595
16                 Z    =         2959179
80
 XDOT =       3644
691009                 XDOT =        1110
901819
 YDOT =      17588
341470  feet/sec       YDOT =        5360
926480  meter/sec
 ZDOT =     -16392
701515                 ZDOT =       -4996
495422


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07347
91911708  
00020000  00000-0  20000-3 0  9084
2 25544  51
6376 257
1844 0000757 265
9042  94
2036 15
77462585 39138


Satellite: ISS
Catalog Number: 25544
Epoch time:      07347
91911708   =   yrday
fracday
Element set:     908
Inclination:       51
6376  deg
RA of node:       257
1844  deg
Eccentricity:     
0000757     
Arg of perigee:   265
9042  deg
Mean anomaly:      94
2036  deg
Mean motion:   15
77462585  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3913
Checksum:              314


Coasting Arc #10 (Orbit 3928)
---------------------------------------

Vector Time (GMT): 2007/348/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2922798
33                 A    =         6711606
78  meter
 Y    =       -3561258
40  meter          E    =           
0005697
 Z    =        4877881
36                 I    =           51
31674
 XDOT =       3950
251342                 Wp   =          127
41056
 YDOT =       6247
317463  meter/sec      RA   =          251
41061  deg
 ZDOT =       2188
928922                 TA   =          301
23041
                                          MA   =          301
28622
                                          Ha   =            184
231  n
mi
                                          Hp   =            178
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9589233
36                 X    =         2938707
81
 Y    =      -11683918
64  feet           Y    =        -3528485
62  meter
 Z    =       16003547
76                 Z    =         4892118
53
 XDOT =      12960
142197                 XDOT =        3869
465892
 YDOT =      20496
448369  feet/sec       YDOT =        6291
039466  meter/sec
 ZDOT =       7181
525334                 ZDOT =        2207
923711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -158649
48                 X    =          -48356
36
 Y    =      -15057040
24  feet           Y    =        -4589385
87  meter
 Z    =       16057436
34                 Z    =         4894306
60
 XDOT =      21936
490548                 XDOT =        6686
242319
 YDOT =       7523
449891  feet/sec       YDOT =        2293
147527  meter/sec
 ZDOT =       7254
581291                 ZDOT =        2211
196378


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07348
93269181  
00020000  00000-0  20000-3 0  9099
2 25544  51
6384 251
9520 0000899 273
0037  87
1025 15
77554594 39299


Satellite: ISS
Catalog Number: 25544
Epoch time:      07348
93269181   =   yrday
fracday
Element set:     909
Inclination:       51
6384  deg
RA of node:       251
9520  deg
Eccentricity:     
0000899     
Arg of perigee:   273
0037  deg
Mean anomaly:      87
1025  deg
Mean motion:   15
77554594  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3929
Checksum:              320


Coasting Arc #11 (Orbit 3943)
---------------------------------------

Vector Time (GMT): 2007/349/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3240554
99                 A    =         6721809
31  meter
 Y    =       -5833625
89  meter          E    =           
0010140
 Z    =        -764318
86                 I    =           51
36213
 XDOT =       3905
230371                 Wp   =           35
42880
 YDOT =      -2943
444875  meter/sec      RA   =          246
20112  deg
 ZDOT =       5955
822876                 TA   =          316
19463
                                          MA   =          316
27502
                                          Ha   =            184
342  n
mi
                                          Hp   =            178
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10631742
09                 X    =        -3171368
73
 Y    =      -19139192
54  feet           Y    =        -5869476
70  meter
 Z    =       -2507607
80                 Z    =         -779893
98
 XDOT =      12812
435600                 XDOT =        3908
921863
 YDOT =      -9656
971376  feet/sec       YDOT =       -2899
754301  meter/sec
 ZDOT =      19540
101299                 ZDOT =        5974
803175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20529998
59                 X    =        -6257543
57
 Y    =       -7586654
45  feet           Y    =        -2312412
28  meter
 Z    =       -2567598
08                 Z    =         -782603
90
 XDOT =       2779
356440                 XDOT =         847
147843
 YDOT =     -14107
071130  feet/sec       YDOT =       -4299
835281  meter/sec
 ZDOT =      19612
133713                 ZDOT =        5977
778356


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07349
88289575  
00020000  00000-0  20000-3 0  9105
2 25544  51
6387 247
0467 0000794 283
5147  76
5929 15
77554371 39445


Satellite: ISS
Catalog Number: 25544
Epoch time:      07349
88289575   =   yrday
fracday
Element set:     910
Inclination:       51
6387  deg
RA of node:       247
0467  deg
Eccentricity:     
0000794     
Arg of perigee:   283
5147  deg
Mean anomaly:      76
5929  deg
Mean motion:   15
77554371  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3944
Checksum:              342


Coasting Arc #12 (Orbit 3959)
---------------------------------------

Vector Time (GMT): 2007/350/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3935949
62                 A    =         6709872
79  meter
 Y    =        1526628
31  meter          E    =           
0014184
 Z    =       -5227604
59                 I    =           51
33543
 XDOT =      -3357
445396                 Wp   =           93
19150
 YDOT =      -6906
737686  meter/sec      RA   =          241
02133  deg
 ZDOT =        511
300501                 TA   =          181
68677
                                          MA   =          181
69156
                                          Ha   =            184
262  n
mi
                                          Hp   =            178
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12913220
53                 X    =        -3927333
23
 Y    =        5008623
06  feet           Y    =         1482662
89  meter
 Z    =      -17150933
71                 Z    =        -5246704
45
 XDOT =     -11015
240799                 XDOT =       -3282
447485
 YDOT =     -22659
900543  feet/sec       YDOT =       -6943
863251  meter/sec
 ZDOT =       1677
495081                 ZDOT =         495
171585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6240337
15                 X    =        -1902054
76
 Y    =       12263716
26  feet           Y    =         3737980
72  meter
 Z    =      -17223575
47                 Z    =        -5249745
80
 XDOT =     -22408
621045                 XDOT =       -6830
147695
 YDOT =      -9135
887008  feet/sec       YDOT =       -2784
618360  meter/sec
 ZDOT =       1615
268453                 ZDOT =         492
333824


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07350
89641908  
00020000  00000-0  20000-3 0  9111
2 25544  51
6387 241
8146 0000803 288
6282  71
4796 15
77623903 39600


Satellite: ISS
Catalog Number: 25544
Epoch time:      07350
89641908   =   yrday
fracday
Element set:     911
Inclination:       51
6387  deg
RA of node:       241
8146  deg
Eccentricity:     
0000803     
Arg of perigee:   288
6282  deg
Mean anomaly:      71
4796  deg
Mean motion:   15
77623903  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3960
Checksum:              313


Coasting Arc #13 (Orbit 3975)
---------------------------------------

Vector Time (GMT): 2007/351/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2491144
31                 A    =         6720641
25  meter
 Y    =        6017289
23  meter          E    =           
0007251
 Z    =       -1647084
70                 I    =           51
38750
 XDOT =      -5133
739470                 Wp   =          146
52355
 YDOT =        565
262384  meter/sec      RA   =          235
85752  deg
 ZDOT =      -5717
377638                 TA   =           51
76408
                                          MA   =           51
69884
                                          Ha   =            184
220  n
mi
                                          Hp   =            178
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8173045
65                 X    =         2431674
22
 Y    =       19741762
56  feet           Y    =         6044814
23  meter
 Z    =       -5403821
19                 Z    =        -1635126
61
 XDOT =     -16842
977264                 XDOT =       -5111
904561
 YDOT =       1854
535382  feet/sec       YDOT =         507
976522  meter/sec
 ZDOT =     -18757
800648                 ZDOT =       -5742
264464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19412316
50                 X    =         5916874
07
 Y    =        8955189
66  feet           Y    =         2729541
81  meter
 Z    =       -5357582
86                 Z    =        -1632991
26
 XDOT =     -10395
906442                 XDOT =       -3168
672284
 YDOT =      11291
930953  feet/sec       YDOT =        3441
780555  meter/sec
 ZDOT =     -18852
609687                 ZDOT =       -5746
275433


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   07351
90991587  
00020000  00000-0  20000-3 0  9126
2 25544  51
6390 236
5810 0000832 288
8790  71
2285 15
77651087 39763


Satellite: ISS
Catalog Number: 25544
Epoch time:      07351
90991587   =   yrday
fracday
Element set:     912
Inclination:       51
6390  deg
RA of node:       236
5810  deg
Eccentricity:     
0000832     
Arg of perigee:   288
8790  deg
Mean anomaly:      71
2285  deg
Mean motion:   15
77651087  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3976
Checksum:              321


Coasting Arc #14 (Orbit 3991)
---------------------------------------

Vector Time (GMT): 2007/352/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4992459
76                 A    =         6712934
62  meter
 Y    =         470036
02  meter          E    =           
0008451
 Z    =        4458507
72                 I    =           51
37966
 XDOT =       2205
345375                 Wp   =           63
04258
 YDOT =       6674
653441  meter/sec      RA   =          230
63695  deg
 ZDOT =      -3164
756452                 TA   =           58
69634
                                          MA   =           58
61362
                                          Ha   =            184
106  n
mi
                                          Hp   =            178
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16379461
16                 X    =         4965173
80
 Y    =        1542112
94  feet           Y    =          525711
59  meter
 Z    =       14627649
99                 Z    =         4482695
15
 XDOT =       7235
385088                 XDOT =        2145
918482
 YDOT =      21898
469293  feet/sec       YDOT =        6698
982864  meter/sec
 ZDOT =     -10383
059226                 ZDOT =       -3154
186524

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12855049
03                 X    =         3918218
94
 Y    =      -10134345
16  feet           Y    =        -3088948
41  meter
 Z    =       14719910
57                 Z    =         4486628
74
 XDOT =      19655
282391                 XDOT =        5990
930073
 YDOT =       9870
779153  feet/sec       YDOT =        3008
613486  meter/sec
 ZDOT =     -10342
037714                 ZDOT =       -3152
253095


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   07352
92338683  
00020000  00000-0  20000-3 0  9132
2 25544  51
6394 231
3483 0000781 300
9558  59
1530 15
77676182 39926


Satellite: ISS
Catalog Number: 25544
Epoch time:      07352
92338683   =   yrday
fracday
Element set:     913
Inclination:       51
6394  deg
RA of node:       231
3483  deg
Eccentricity:     
0000781     
Arg of perigee:   300
9558  deg
Mean anomaly:      59
1530  deg
Mean motion:   15
77676182  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3992
Checksum:              310


Coasting Arc #15 (Orbit 4007)
---------------------------------------

Vector Time (GMT): 2007/353/21:09:12
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1193899
02                 A    =         6715489
96  meter
 Y    =       -5454273
90  meter          E    =           
0010945
 Z    =        3722814
21                 I    =           51
40845
 XDOT =       6252
688919                 Wp   =           94
86170
 YDOT =       1534
226453  meter/sec      RA   =          225
50506  deg
 ZDOT =       4241
427759                 TA   =          310
35354
                                          MA   =          310
44907
                                          Ha   =            184
083  n
mi
                                          Hp   =            178
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3916991
54                 X    =        -1150904
80
 Y    =      -17894599
40  feet           Y    =        -5467384
77  meter
 Z    =       12213957
39                 Z    =         3717118
00
 XDOT =      20514
071257                 XDOT =        6214
463843
 YDOT =       5033
551354  feet/sec       YDOT =        1603
933378  meter/sec
 ZDOT =      13915
445403                 ZDOT =        4271
711112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15410090
06                 X    =        -4696995
45
 Y    =       -9931419
77  feet           Y    =        -3027096
75  meter
 Z    =       12191648
42                 Z    =         3716014
44
 XDOT =      17352
593967                 XDOT =        5289
070641
 YDOT =      -9654
108565  feet/sec       YDOT =       -2942
572291  meter/sec
 ZDOT =      14031
068964                 ZDOT =        4276
669820


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   07353
93682920  
00020000  00000-0  20000-3 0  9141
2 25544  51
6395 226
1147 0000876 299
3047  60
8030 15
77751893 40081


Satellite: ISS
Catalog Number: 25544
Epoch time:      07353
93682920   =   yrday
fracday
Element set:     914
Inclination:       51
6395  deg
RA of node:       226
1147  deg
Eccentricity:     
0000876     
Arg of perigee:   299
3047  deg
Mean anomaly:      60
8030  deg
Mean motion:   15
77751893  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4008
Checksum:              304

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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