Date: October 19th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 4036 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1229)
---------------------------------------

Vector Time (GMT): 2006/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4337356
60                 A    =         6712713
23  meter
 Y    =         961070
70  meter          E    =           
0025986
 Z    =       -5054787
58                 I    =           51
30375
 XDOT =        232
027837                 Wp   =           89
02728
 YDOT =      -7507
390280  meter/sec      RA   =          281
80175  deg
 ZDOT =      -1633
286329                 TA   =          165
21230
                                          MA   =          165
13615
                                          Ha   =            190
271  n
mi
                                          Hp   =            174
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14230172
57                 X    =        -4323225
65
 Y    =        3153119
11  feet           Y    =          912646
82  meter
 Z    =      -16583948
74                 Z    =        -5075824
30
 XDOT =        761
246184                 XDOT =         323
893535
 YDOT =     -24630
545537  feet/sec       YDOT =       -7504
282022  meter/sec
 ZDOT =      -5358
550949                 ZDOT =       -1631
935744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11612635
21                 X    =         3539531
21
 Y    =       -8659365
61  feet           Y    =        -2639374
64  meter
 Z    =      -16662215
28                 Z    =        -5078643
22
 XDOT =       8719
324055                 XDOT =        2657
649972
 YDOT =      21953
397536  feet/sec       YDOT =        6691
395569  meter/sec
 ZDOT =      -5354
533629                 ZDOT =       -1632
061850


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   06289
51866449  
00020000  00000-0  20000-3 0  9007
2 25544  51
6310 282
3685 0012875 101
3794 258
8818 15
76909084 12305


Satellite: ISS
Catalog Number: 25544
Epoch time:      06289
51866449   =   yrday
fracday
Element set:     900
Inclination:       51
6310  deg
RA of node:       282
3685  deg
Eccentricity:     
0012875     
Arg of perigee:   101
3794  deg
Mean anomaly:     258
8818  deg
Mean motion:   15
76909084  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1230
Checksum:              314


Coasting Arc #2 (Orbit 1245)
---------------------------------------

Vector Time (GMT): 2006/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -423169
85                 A    =         6723711
00  meter
 Y    =        6687102
77  meter          E    =           
0025238
 Z    =         435529
89                 I    =           51
33643
 XDOT =      -4842
945814                 Wp   =          117
51248
 YDOT =        100
693600  meter/sec      RA   =          276
60205  deg
 ZDOT =      -5998
259999                 TA   =           57
72250
                                          MA   =           57
47823
                                          Ha   =            190
172  n
mi
                                          Hp   =            174
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1388352
53                 X    =         -500030
26
 Y    =       21939313
53  feet           Y    =         6681940
92  meter
 Z    =        1428903
84                 Z    =          433287
10
 XDOT =     -15888
929835                 XDOT =       -4814
573108
 YDOT =        330
359579  feet/sec       YDOT =          46
695448  meter/sec
 ZDOT =     -19679
330705                 ZDOT =       -6021
718334

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8050835
55                 X    =        -2453894
67
 Y    =      -20456448
17  feet           Y    =        -6235125
40  meter
 Z    =        1421457
88                 Z    =          433260
36
 XDOT =      12655
053265                 XDOT =        3857
260235
 YDOT =      -6412
098820  feet/sec       YDOT =       -1954
407720  meter/sec
 ZDOT =     -19766
739424                 ZDOT =       -6024
902176


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   06290
53260399  
00020000  00000-0  20000-3 0  9014
2 25544  51
6306 277
1372 0012853 104
5429 255
7162 15
76953820 12463


Satellite: ISS
Catalog Number: 25544
Epoch time:      06290
53260399   =   yrday
fracday
Element set:     901
Inclination:       51
6306  deg
RA of node:       277
1372  deg
Eccentricity:     
0012853     
Arg of perigee:   104
5429  deg
Mean anomaly:     255
7162  deg
Mean motion:   15
76953820  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1246
Checksum:              289


Coasting Arc #3 (Orbit 1261)
---------------------------------------

Vector Time (GMT): 2006/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4150260
94                 A    =         6711779
75  meter
 Y    =         792053
30  meter          E    =           
0014943
 Z    =        5202106
51                 I    =           51
29374
 XDOT =       -686
774963                 Wp   =          100
68347
 YDOT =       7662
203386  meter/sec      RA   =          271
41930  deg
 ZDOT =       -619
943544                 TA   =          355
21756
                                          MA   =          355
23182
                                          Ha   =            189
983  n
mi
                                          Hp   =            174
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13616341
66                 X    =         4115824
40
 Y    =        2598600
05  feet           Y    =          838271
57  meter
 Z    =       17067278
58                 Z    =         5222185
05
 XDOT =      -2253
198697                 XDOT =        -769
392128
 YDOT =      25138
462554  feet/sec       YDOT =        7654
061517  meter/sec
 ZDOT =      -2033
935511                 ZDOT =        -623
481061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13285589
29                 X    =        -4049447
62
 Y    =        3617604
98  feet           Y    =         1102646
00  meter
 Z    =       17142214
91                 Z    =         5224947
10
 XDOT =      -8786
237901                 XDOT =       -2678
045312
 YDOT =     -22591
049375  feet/sec       YDOT =       -6885
751850  meter/sec
 ZDOT =      -2046
066554                 ZDOT =        -623
641086


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   06291
54652873  
00020000  00000-0  20000-3 0  9029
2 25544  51
6300 271
9063 0012715 108
6048 251
6499 15
76964434 12624


Satellite: ISS
Catalog Number: 25544
Epoch time:      06291
54652873   =   yrday
fracday
Element set:     902
Inclination:       51
6300  deg
RA of node:       271
9063  deg
Eccentricity:     
0012715     
Arg of perigee:   108
6048  deg
Mean anomaly:     251
6499  deg
Mean motion:   15
76964434  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1262
Checksum:              295


Coasting Arc #4 (Orbit 1277)
---------------------------------------

Vector Time (GMT): 2006/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         782013
96                 A    =         6722559
37  meter
 Y    =       -6499105
21  meter          E    =           
0024262
 Z    =        1505235
64                 I    =           51
33156
 XDOT =       4745
178533                 Wp   =           86
20107
 YDOT =       1923
143371  meter/sec      RA   =          266
25749  deg
 ZDOT =       5760
134350                 TA   =          290
47868
                                          MA   =          290
73897
                                          Ha   =            189
979  n
mi
                                          Hp   =            174
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2565662
61                 X    =          847317
44
 Y    =      -21322523
66  feet           Y    =        -6489995
08  meter
 Z    =        4938437
13                 Z    =         1509193
75
 XDOT =      15568
171040                 XDOT =        4695
338807
 YDOT =       6309
525495  feet/sec       YDOT =        1975
928270  meter/sec
 ZDOT =      18898
078576                 ZDOT =        5783
065660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7452033
06                 X    =         2271379
68
 Y    =       20138590
22  feet           Y    =         6138242
30  meter
 Z    =        4952291
19                 Z    =         1509458
35
 XDOT =     -15171
668558                 XDOT =       -4624
324576
 YDOT =        882
936404  feet/sec       YDOT =         269
119016  meter/sec
 ZDOT =      18983
803305                 ZDOT =        5786
263247


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   06292
56043649  
00020000  00000-0  20000-3 0  9038
2 25544  51
6301 266
6757 0012789 113
2976 246
9536 15
77039743 12782


Satellite: ISS
Catalog Number: 25544
Epoch time:      06292
56043649   =   yrday
fracday
Element set:     903
Inclination:       51
6301  deg
RA of node:       266
6757  deg
Eccentricity:     
0012789     
Arg of perigee:   113
2976  deg
Mean anomaly:     246
9536  deg
Mean motion:   15
77039743  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1278
Checksum:              322


Coasting Arc #5 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2006/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4162033
20                 A    =         6714249
35  meter
 Y    =       -2539783
95  meter          E    =           
0023524
 Z    =       -4638923
31                 I    =           51
30653
 XDOT =       1170
340576                 Wp   =          112
82967
 YDOT =      -7056
305196  meter/sec      RA   =          261
03860  deg
 ZDOT =       2815
618286                 TA   =          185
14684
                                          MA   =          185
17106
                                          Ha   =            189
993  n
mi
                                          Hp   =            174
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13654964
56                 X    =        -4110788
08
 Y    =       -8332624
51  feet           Y    =        -2586039
85  meter
 Z    =      -15219564
68                 Z    =        -4659018
31
 XDOT =       3839
700053                 XDOT =        1235
480100
 YDOT =     -23150
607597  feet/sec       YDOT =       -7042
853426  meter/sec
 ZDOT =       9237
592803                 ZDOT =        2821
462556

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15895477
09                 X    =         4844941
42
 Y    =         963622
10  feet           Y    =          293712
01  meter
 Z    =      -15294805
59                 Z    =        -4661856
74
 XDOT =       7625
034957                 XDOT =        2324
110655
 YDOT =      21049
769989  feet/sec       YDOT =        6415
969893  meter/sec
 ZDOT =       9258
396913                 ZDOT =        2821
959379


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   06293
51096491  
00020000  00000-0  20000-3 0  9048
2 25544  51
6304 261
7707 0012665 115
6565 244
5909 15
76987207 12930


Satellite: ISS
Catalog Number: 25544
Epoch time:      06293
51096491   =   yrday
fracday
Element set:     904
Inclination:       51
6304  deg
RA of node:       261
7707  deg
Eccentricity:     
0012665     
Arg of perigee:   115
6565  deg
Mean anomaly:     244
5909  deg
Mean motion:   15
76987207  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1293
Checksum:              310


Coasting Arc #6 (Orbit 1308)
---------------------------------------

Vector Time (GMT): 2006/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1320794
10                 A    =         6718664
19  meter
 Y    =        5687191
59  meter          E    =           
0017047
 Z    =       -3331336
07                 I    =           51
32853
 XDOT =      -4797
795434                 Wp   =          111
92392
 YDOT =      -3823
590306  meter/sec      RA   =          255
90336  deg
 ZDOT =      -4650
620840                 TA   =          107
47800
                                          MA   =          107
29159
                                          Ha   =            189
845  n
mi
                                          Hp   =            174
822

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4333313
97                 X    =        -1368107
43
 Y    =       18658765
06  feet           Y    =         5672157
04  meter
 Z    =      -10929580
27                 Z    =        -3337867
84
 XDOT =     -15740
798668                 XDOT =       -4732
090442
 YDOT =     -12544
587617  feet/sec       YDOT =       -3876
874754  meter/sec
 ZDOT =     -15257
942388                 ZDOT =       -4673
769382

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5330160
38                 X    =        -1624632
89
 Y    =      -18384804
80  feet           Y    =        -5603688
50  meter
 Z    =      -10953136
12                 Z    =        -3338515
89
 XDOT =      18438
256098                 XDOT =        5619
980459
 YDOT =       3747
005814  feet/sec       YDOT =        1142
087372  meter/sec
 ZDOT =     -15344
742053                 ZDOT =       -4677
077378


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   06294
52484486  
00020000  00000-0  20000-3 0  9056
2 25544  51
6312 256
5388 0012647 119
3213 240
9217 15
77043421 13099


Satellite: ISS
Catalog Number: 25544
Epoch time:      06294
52484486   =   yrday
fracday
Element set:     905
Inclination:       51
6312  deg
RA of node:       256
5388  deg
Eccentricity:     
0012647     
Arg of perigee:   119
3213  deg
Mean anomaly:     240
9217  deg
Mean motion:   15
77043421  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1309
Checksum:              287


Coasting Arc #7 (Orbit 1324)
---------------------------------------

Vector Time (GMT): 2006/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4224382
18                 A    =         6718563
93  meter
 Y    =        4007657
71  meter          E    =           
0024163
 Z    =        3324311
47                 I    =           51
33687
 XDOT =      -1886
506031                 Wp   =          106
82146
 YDOT =       5863
463729  meter/sec      RA   =          250
67099  deg
 ZDOT =      -4650
611520                 TA   =           33
76207
                                          MA   =           33
60842
                                          Ha   =            189
670  n
mi
                                          Hp   =            174
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13859521
59                 X    =         4163104
63
 Y    =       13148483
29  feet           Y    =         4054554
57  meter
 Z    =       10906533
70                 Z    =         3344685
18
 XDOT =      -6189
324249                 XDOT =       -1929
339371
 YDOT =      19237
085725  feet/sec       YDOT =        5842
128142  meter/sec
 ZDOT =     -15257
911811                 ZDOT =       -4659
880662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18528624
58                 X    =        -5647524
77
 Y    =       -4470436
24  feet           Y    =        -1362588
97  meter
 Z    =       10983018
71                 Z    =         3347624
10
 XDOT =      -4675
441354                 XDOT =       -1425
074525
 YDOT =     -18357
368767  feet/sec       YDOT =       -5595
326000  meter/sec
 ZDOT =     -15291
647132                 ZDOT =       -4660
894046


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   06295
53870945  
00020000  00000-0  20000-3 0  9068
2 25544  51
6314 251
3079 0012546 123
1643 237
0727 15
77067091 13259


Satellite: ISS
Catalog Number: 25544
Epoch time:      06295
53870945   =   yrday
fracday
Element set:     906
Inclination:       51
6314  deg
RA of node:       251
3079  deg
Eccentricity:     
0012546     
Arg of perigee:   123
1643  deg
Mean anomaly:     237
0727  deg
Mean motion:   15
77067091  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1325
Checksum:              289


Coasting Arc #8 (Orbit 1340)
---------------------------------------

Vector Time (GMT): 2006/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2034994
10                 A    =         6713967
91  meter
 Y    =       -4429727
94  meter          E    =           
0020580
 Z    =        4607125
82                 I    =           51
33339
 XDOT =       4890
959554                 Wp   =          123
35917
 YDOT =       5236
270553  meter/sec      RA   =          245
53858  deg
 ZDOT =       2853
945597                 TA   =          298
24800
                                          MA   =          298
45560
                                          Ha   =            189
551  n
mi
                                          Hp   =            174
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6676489
83                 X    =         2061995
39
 Y    =      -14533228
13  feet           Y    =        -4406820
49  meter
 Z    =       15115242
19                 Z    =         4617077
76
 XDOT =      16046
455229                 XDOT =        4818
178945
 YDOT =      17179
365330  feet/sec       YDOT =        5290
557062  meter/sec
 ZDOT =       9363
338573                 ZDOT =        2877
529801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1844417
75                 X    =          562178
53
 Y    =       15851945
39  feet           Y    =         4831672
95  meter
 Z    =       15151723
78                 Z    =         4618245
41
 XDOT =     -21406
274158                 XDOT =       -6524
632364
 YDOT =      -6607
384167  feet/sec       YDOT =       -2013
930694  meter/sec
 ZDOT =       9451
960506                 ZDOT =        2880
957562


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   06296
55255684  
00020000  00000-0  20000-3 0  9079
2 25544  51
6323 246
0775 0012488 128
0163 232
2131 15
77126183 13411


Satellite: ISS
Catalog Number: 25544
Epoch time:      06296
55255684   =   yrday
fracday
Element set:     907
Inclination:       51
6323  deg
RA of node:       246
0775  deg
Eccentricity:     
0012488     
Arg of perigee:   128
0163  deg
Mean anomaly:     232
2131  deg
Mean motion:   15
77126183  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1341
Checksum:              282


Coasting Arc #9 (Orbit 1355)
---------------------------------------

Vector Time (GMT): 2006/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4248714
26                 A    =         6722288
91  meter
 Y    =       -4984574
83  meter          E    =           
0014499
 Z    =       -1531025
69                 I    =           51
37412
 XDOT =       2888
967356                 Wp   =           96
71541
 YDOT =      -4215
969177  meter/sec      RA   =          240
32153  deg
 ZDOT =       5753
790825                 TA   =          246
34520
                                          MA   =          246
49745
                                          Ha   =            189
568  n
mi
                                          Hp   =            175
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13939351
23                 X    =        -4185222
59
 Y    =      -16353591
95  feet           Y    =        -5031731
28  meter
 Z    =       -5023050
17                 Z    =        -1551512
45
 XDOT =       9478
239358                 XDOT =        2907
944432
 YDOT =     -13831
919872  feet/sec       YDOT =       -4183
557122  meter/sec
 ZDOT =      18877
266487                 ZDOT =        5767
871907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20466237
16                 X    =         6238109
09
 Y    =        6488349
22  feet           Y    =         1977648
84  meter
 Z    =       -5100095
72                 Z    =        -1554509
18
 XDOT =       -139
668878                 XDOT =         -42
571074
 YDOT =      15205
515905  feet/sec       YDOT =        4634
641248  meter/sec
 ZDOT =      18929
172467                 ZDOT =        5769
611768


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   06297
50302735  
00020000  00000-0  20000-3 0  9086
2 25544  51
6320 241
1728 0012487 130
8258 229
3991 15
77104824 13562


Satellite: ISS
Catalog Number: 25544
Epoch time:      06297
50302735   =   yrday
fracday
Element set:     908
Inclination:       51
6320  deg
RA of node:       241
1728  deg
Eccentricity:     
0012487     
Arg of perigee:   130
8258  deg
Mean anomaly:     229
3991  deg
Mean motion:   15
77104824  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1356
Checksum:              290


Coasting Arc #10 (Orbit 1371)
---------------------------------------

Vector Time (GMT): 2006/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3089541
20                 A    =         6711316
23  meter
 Y    =        2885191
12  meter          E    =           
0024864
 Z    =       -5232421
38                 I    =           51
35312
 XDOT =      -4731
652183                 Wp   =          108
03216
 YDOT =      -6036
286614  meter/sec      RA   =          235
16128  deg
 ZDOT =       -544
286234                 TA   =          156
82387
                                          MA   =          156
71154
                                          Ha   =            189
439  n
mi
                                          Hp   =            175
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10136290
03                 X    =        -3096155
28
 Y    =        9465850
13  feet           Y    =         2850605
37  meter
 Z    =      -17166736
80                 Z    =        -5247446
77
 XDOT =     -15523
793251                 XDOT =       -4661
157795
 YDOT =     -19804
089942  feet/sec       YDOT =       -6088
804398  meter/sec
 ZDOT =      -1785
715990                 ZDOT =        -567
102269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3263740
13                 X    =          994787
99
 Y    =      -13408287
28  feet           Y    =        -4086845
96  meter
 Z    =      -17222351
15                 Z    =        -5249372
63
 XDOT =      22820
471312                 XDOT =        6955
679656
 YDOT =       7918
034367  feet/sec       YDOT =        2413
416875  meter/sec
 ZDOT =      -1871
592969                 ZDOT =        -570
461537


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   06298
51684575  
00020000  00000-0  20000-3 0  9094
2 25544  51
6327 235
9410 0012417 134
8587 225
3589 15
77127758 13728


Satellite: ISS
Catalog Number: 25544
Epoch time:      06298
51684575   =   yrday
fracday
Element set:     909
Inclination:       51
6327  deg
RA of node:       235
9410  deg
Eccentricity:     
0012417     
Arg of perigee:   134
8587  deg
Mean anomaly:     225
3589  deg
Mean motion:   15
77127758  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1372
Checksum:              324


Coasting Arc #11 (Orbit 1387)
---------------------------------------

Vector Time (GMT): 2006/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3922698
52                 A    =         6723099
61  meter
 Y    =        5414002
40  meter          E    =           
0023439
 Z    =        -597641
49                 I    =           51
41088
 XDOT =      -4217
202856                 Wp   =          139
26341
 YDOT =       2410
767844  meter/sec      RA   =          229
98442  deg
 ZDOT =      -5990
061446                 TA   =           47
27729
                                          MA   =           47
08021
                                          Ha   =            189
370  n
mi
                                          Hp   =            175
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12869745
78                 X    =         3864770
15
 Y    =       17762475
06  feet           Y    =         5457544
32  meter
 Z    =       -1960766
06                 Z    =         -578724
95
 XDOT =     -13835
967376                 XDOT =       -4214
747569
 YDOT =       7909
343320  feet/sec       YDOT =        2363
622789  meter/sec
 ZDOT =     -19652
432564                 ZDOT =       -6010
543061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20610255
73                 X    =        -6282005
95
 Y    =       -7525132
14  feet           Y    =        -2293660
28  meter
 Z    =       -1889503
98                 Z    =         -575920
81
 XDOT =       6410
065356                 XDOT =        1953
787921
 YDOT =     -12729
881200  feet/sec       YDOT =       -3880
067790  meter/sec
 ZDOT =     -19728
458852                 ZDOT =       -6013
234258


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   06299
53064855  
00020000  00000-0  20000-3 0  9102
2 25544  51
6331 230
7098 0012444 138
7830 221
4277 15
77146659 13881


Satellite: ISS
Catalog Number: 25544
Epoch time:      06299
53064855   =   yrday
fracday
Element set:     910
Inclination:       51
6331  deg
RA of node:       230
7098  deg
Eccentricity:     
0012444     
Arg of perigee:   138
7830  deg
Mean anomaly:     221
4277  deg
Mean motion:   15
77146659  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1388
Checksum:              305


Coasting Arc #12 (Orbit 1403)
---------------------------------------

Vector Time (GMT): 2006/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 454754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4271114
51                 A    =         6712120
62  meter
 Y    =       -1365829
90  meter          E    =           
0013745
 Z    =        4982286
15                 I    =           51
39326
 XDOT =       4160
860871                 Wp   =          119
03951
 YDOT =       6225
950368  meter/sec      RA   =          224
78726  deg
 ZDOT =      -1862
908721                 TA   =          348
94046
                                          MA   =          348
97064
                                          Ha   =            189
099  n
mi
                                          Hp   =            175
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14012842
87                 X    =         4261866
40
 Y    =       -4481069
24  feet           Y    =        -1318119
94  meter
 Z    =       16346083
16                 Z    =         5003013
12
 XDOT =      13651
118343                 XDOT =        4099
982051
 YDOT =      20426
346353  feet/sec       YDOT =        6272
139141  meter/sec
 ZDOT =      -6111
905253                 ZDOT =       -1842
842329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8838249
61                 X    =        -2693898
48
 Y    =       11653275
42  feet           Y    =         3551918
35  meter
 Z    =       16423175
61                 Z    =         5005783
93
 XDOT =     -22073
069240                 XDOT =       -6727
871504
 YDOT =      -8246
585896  feet/sec       YDOT =       -2513
559381  meter/sec
 ZDOT =      -6036
236147                 ZDOT =       -1839
844778


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   06300
54443477  
00020000  00000-0  20000-3 0  9118
2 25544  51
6327 225
4791 0012344 142
5309 217
6718 15
77192526 14040


Satellite: ISS
Catalog Number: 25544
Epoch time:      06300
54443477   =   yrday
fracday
Element set:     911
Inclination:       51
6327  deg
RA of node:       225
4791  deg
Eccentricity:     
0012344     
Arg of perigee:   142
5309  deg
Mean anomaly:     217
6718  deg
Mean motion:   15
77192526  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1404
Checksum:              280

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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