Date: December 5th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 2010)
---------------------------------------

Vector Time (GMT): 2006/338/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2114615
55                 A    =         6720491
52  meter
 Y    =        4785877
21  meter          E    =           
0014562
 Z    =        4222760
32                 I    =           51
77131
 XDOT =      -6780
388493                 Wp   =          303
96538
 YDOT =       -199
932744  meter/sec      RA   =           26
68608  deg
 ZDOT =       3638
855829                 TA   =          109
11673
                                          MA   =          108
95900
                                          Ha   =            191
470  n
mi
                                          Hp   =            179
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6937715
04                 X    =         2040428
24
 Y    =       15701696
87  feet           Y    =         4809108
49  meter
 Z    =       13854200
52                 Z    =         4232853
93
 XDOT =     -22245
369073                 XDOT =       -6795
326115
 YDOT =       -655
947324  feet/sec       YDOT =        -275
838950  meter/sec
 ZDOT =      11938
503377                 ZDOT =        3605
879758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16192857
55                 X    =         4935582
98
 Y    =        5603973
02  feet           Y    =         1708090
98  meter
 Z    =       13892476
29                 Z    =         4234426
77
 XDOT =     -15201
956825                 XDOT =       -4633
556440
 YDOT =      14773
026742  feet/sec       YDOT =        4502
818551  meter/sec
 ZDOT =      11815
199578                 ZDOT =        3601
272832


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   06338
98305627  
00020000  00000-0  20000-3 0  9009
2 25544  51
6356  26
8881 0024320 297
4594  62
4097 15
75365135 20115


Satellite: ISS
Catalog Number: 25544
Epoch time:      06338
98305627   =   yrday
fracday
Element set:     900
Inclination:       51
6356  deg
RA of node:        26
8881  deg
Eccentricity:     
0024320     
Arg of perigee:   297
4594  deg
Mean anomaly:      62
4097  deg
Mean motion:   15
75365135  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2011
Checksum:              296


Coasting Arc #2 (Orbit 2025)
---------------------------------------

Vector Time (GMT): 2006/339/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6107722
80                 A    =         6724867
16  meter
 Y    =          52475
57  meter          E    =           
0022624
 Z    =       -2778662
93                 I    =           51
76047
 XDOT =       2301
992353                 Wp   =          311
50123
 YDOT =       5266
479057  meter/sec      RA   =           21
50035  deg
 ZDOT =       5147
347308                 TA   =           16
68136
                                          MA   =           16
60706
                                          Ha   =            191
766  n
mi
                                          Hp   =            178
961

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20038460
64                 X    =         6120180
48
 Y    =         172163
95  feet           Y    =          120845
67  meter
 Z    =       -9116348
19                 Z    =        -2748960
96
 XDOT =       7552
468350                 XDOT =        2217
925566
 YDOT =      17278
474597  feet/sec       YDOT =        5291
750241  meter/sec
 ZDOT =      16887
622403                 ZDOT =        5158
327281

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13494008
91                 X    =         4112973
91
 Y    =      -14882667
07  feet           Y    =        -4536236
92  meter
 Z    =       -9005292
55                 Z    =        -2744813
17
 XDOT =      16776
563246                 XDOT =        5113
496477
 YDOT =       4943
266294  feet/sec       YDOT =        1506
707566  meter/sec
 ZDOT =      16929
264894                 ZDOT =        5160
039940


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   06339
93455816  
00020000  00000-0  20000-3 0  9012
2 25544  51
6358  21
9909 0024422 301
0940  58
7828 15
75414231 20262


Satellite: ISS
Catalog Number: 25544
Epoch time:      06339
93455816   =   yrday
fracday
Element set:     901
Inclination:       51
6358  deg
RA of node:        21
9909  deg
Eccentricity:     
0024422     
Arg of perigee:   301
0940  deg
Mean anomaly:      58
7828  deg
Mean motion:   15
75414231  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2026
Checksum:              286


Coasting Arc #3 (Orbit 2041)
---------------------------------------

Vector Time (GMT): 2006/340/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1848474
68                 A    =         6718309
78  meter
 Y    =       -4419755
94  meter          E    =           
0020011
 Z    =       -4709524
94                 I    =           51
71190
 XDOT =       7210
385674                 Wp   =          331
81283
 YDOT =       -106
078189  meter/sec      RA   =           16
40496  deg
 ZDOT =      -2708
523668                 TA   =          271
45880
                                          MA   =          271
68803
                                          Ha   =            191
863  n
mi
                                          Hp   =            178
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6064549
48                 X    =        -1776036
81
 Y    =      -14500511
62  feet           Y    =        -4440020
75  meter
 Z    =      -15451197
30                 Z    =        -4718329
72
 XDOT =      23656
120979                 XDOT =        7224
193561
 YDOT =       -348
025555  feet/sec       YDOT =         -25
369968  meter/sec
 ZDOT =      -8886
232505                 ZDOT =       -2673
461870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14890260
07                 X    =        -4538551
27
 Y    =       -4928488
46  feet           Y    =        -1502203
28  meter
 Z    =      -15484613
40                 Z    =        -4719710
16
 XDOT =      14841
612938                 XDOT =        4523
723624
 YDOT =     -17106
909601  feet/sec       YDOT =       -5214
186046  meter/sec
 ZDOT =      -8755
144899                 ZDOT =       -2668
568165


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   06340
94947187  
00020000  00000-0  20000-3 0  9023
2 25544  51
6356  16
7675 0024484 305
1294  54
7575 15
75463201 20421


Satellite: ISS
Catalog Number: 25544
Epoch time:      06340
94947187   =   yrday
fracday
Element set:     902
Inclination:       51
6356  deg
RA of node:        16
7675  deg
Eccentricity:     
0024484     
Arg of perigee:   305
1294  deg
Mean anomaly:      54
7575  deg
Mean motion:   15
75463201  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2042
Checksum:              296


Coasting Arc #4 (Orbit 2057)
---------------------------------------

Vector Time (GMT): 2006/341/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6455387
57                 A    =         6726501
39  meter
 Y    =         248589
42  meter          E    =           
0011317
 Z    =        1900672
94                 I    =           51
71159
 XDOT =      -1845
200735                 Wp   =          327
86194
 YDOT =      -4899
060905  meter/sec      RA   =           11
22484  deg
 ZDOT =      -5632
156855                 TA   =          191
06238
                                          MA   =          191
08728
                                          Ha   =            192
098  n
mi
                                          Hp   =            178
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21179093
09                 X    =        -6466920
69
 Y    =         815582
08  feet           Y    =          176336
89  meter
 Z    =        6235803
60                 Z    =         1869284
65
 XDOT =      -6053
808185                 XDOT =       -1762
921581
 YDOT =     -16073
034465  feet/sec       YDOT =       -4919
233988  meter/sec
 ZDOT =     -18478
204904                 ZDOT =       -5640
921804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12933459
87                 X    =        -3942118
57
 Y    =       16834324
25  feet           Y    =         5131102
03  meter
 Z    =        6118459
60                 Z    =         1864906
48
 XDOT =     -14936
924031                 XDOT =       -4552
774445
 YDOT =      -4754
882697  feet/sec       YDOT =       -1449
288246  meter/sec
 ZDOT =     -18511
528423                 ZDOT =       -5642
313863


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   06341
96436461  
00020000  00000-0  20000-3 0  9035
2 25544  51
6355  11
5433 0024296 309
0154  50
8846 15
75461912 20586


Satellite: ISS
Catalog Number: 25544
Epoch time:      06341
96436461   =   yrday
fracday
Element set:     903
Inclination:       51
6355  deg
RA of node:        11
5433  deg
Eccentricity:     
0024296     
Arg of perigee:   309
0154  deg
Mean anomaly:      50
8846  deg
Mean motion:   15
75461912  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2058
Checksum:              283


Coasting Arc #5 (Orbit 2073)
---------------------------------------

Vector Time (GMT): 2006/342/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1326225
05                 A    =         6716609
25  meter
 Y    =        4190193
80  meter          E    =           
0019605
 Z    =        5087818
31                 I    =           51
65067
 XDOT =      -7514
768403                 Wp   =          314
24926
 YDOT =        463
887210  meter/sec      RA   =            6
10988  deg
 ZDOT =       1593
994669                 TA   =          120
53390
                                          MA   =          120
34026
                                          Ha   =            192
322  n
mi
                                          Hp   =            178
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4351132
05                 X    =         1254555
49
 Y    =       13747354
98  feet           Y    =         4204622
92  meter
 Z    =       16692317
29                 Z    =         5094087
62
 XDOT =     -24654
751977                 XDOT =       -7527
140465
 YDOT =       1521
939665  feet/sec       YDOT =         379
783492  meter/sec
 ZDOT =       5229
641304                 ZDOT =        1557
458000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13386824
63                 X    =         4080304
15
 Y    =        5283566
34  feet           Y    =         1610431
02  meter
 Z    =       16716232
49                 Z    =         5095107
66
 XDOT =     -13877
806656                 XDOT =       -4229
955469
 YDOT =      19226
470747  feet/sec       YDOT =        5860
228284  meter/sec
 ZDOT =       5093
063022                 ZDOT =        1552
365609


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   06342
97923292  
00020000  00000-0  20000-3 0  9041
2 25544  51
6357   6
3180 0024374 313
0864  46
8260 15
75503786 20748


Satellite: ISS
Catalog Number: 25544
Epoch time:      06342
97923292   =   yrday
fracday
Element set:     904
Inclination:       51
6357  deg
RA of node:         6
3180  deg
Eccentricity:     
0024374     
Arg of perigee:   313
0864  deg
Mean anomaly:      46
8260  deg
Mean motion:   15
75503786  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2074
Checksum:              291


Coasting Arc #6 (Orbit 2088)
---------------------------------------

Vector Time (GMT): 2006/343/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6625457
64                 A    =         6727480
83  meter
 Y    =        -586538
58  meter          E    =           
0027825
 Z    =        -879118
67                 I    =           51
65871
 XDOT =       1216
336879                 Wp   =          337
71516
 YDOT =       4740
855283  meter/sec      RA   =             
94141  deg
 ZDOT =       5968
001605                 TA   =           12
66780
                                          MA   =           12
59802
                                          Ha   =            192
562  n
mi
                                          Hp   =            178
352

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21737065
75                 X    =         6635794
57
 Y    =       -1924339
17  feet           Y    =         -512391
13  meter
 Z    =       -2884247
61                 Z    =         -846907
24
 XDOT =       3990
606558                 XDOT =        1134
242174
 YDOT =      15553
987149  feet/sec       YDOT =        4753
997294  meter/sec
 ZDOT =      19580
057760                 ZDOT =        5973
711727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11800570
90                 X    =         3596814
01
 Y    =      -18374700
82  feet           Y    =        -5600608
81  meter
 Z    =       -2763854
04                 Z    =         -842422
71
 XDOT =      13333
422148                 XDOT =        4064
027071
 YDOT =       5596
057201  feet/sec       YDOT =        1705
678235  meter/sec
 ZDOT =      19601
947168                 ZDOT =        5974
673497


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   06343
93065108  
00020000  00000-0  20000-3 0  9052
2 25544  51
6352   1
4196 0024518 316
6409  43
2826 15
75546889 20896


Satellite: ISS
Catalog Number: 25544
Epoch time:      06343
93065108   =   yrday
fracday
Element set:     905
Inclination:       51
6352  deg
RA of node:         1
4196  deg
Eccentricity:     
0024518     
Arg of perigee:   316
6409  deg
Mean anomaly:      43
2826  deg
Mean motion:   15
75546889  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2089
Checksum:              300


Coasting Arc #7 (Orbit 2104)
---------------------------------------

Vector Time (GMT): 2006/344/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -775393
12                 A    =         6715572
56  meter
 Y    =       -4116537
68  meter          E    =           
0019657
 Z    =       -5249506
40                 I    =           51
58975
 XDOT =       7641
186995                 Wp   =          357
86530
 YDOT =       -888
533474  meter/sec      RA   =          355
80424  deg
 ZDOT =       -412
532272                 TA   =          268
10350
                                          MA   =          268
32864
                                          Ha   =            192
683  n
mi
                                          Hp   =            178
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2543940
67                 X    =         -703802
67
 Y    =      -13505701
05  feet           Y    =        -4124807
74  meter
 Z    =      -17222790
02                 Z    =        -5253099
78
 XDOT =      25069
511140                 XDOT =        7652
558797
 YDOT =      -2915
136070  feet/sec       YDOT =        -803
021852  meter/sec
 ZDOT =      -1353
452337                 ZDOT =        -375
383903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12283312
71                 X    =        -3743953
71
 Y    =       -6125082
87  feet           Y    =        -1866925
26  meter
 Z    =      -17236695
73                 Z    =        -5253744
86
 XDOT =      12232
658654                 XDOT =        3728
514358
 YDOT =     -20934
772194  feet/sec       YDOT =       -6380
918565  meter/sec
 ZDOT =      -1214
628950                 ZDOT =        -370
218904


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   06344
94547566  
00020000  00000-0  20000-3 0  9068
2 25544  51
6342 356
1948 0024469 320
5532  39
3850 15
75604963 21056


Satellite: ISS
Catalog Number: 25544
Epoch time:      06344
94547566   =   yrday
fracday
Element set:     906
Inclination:       51
6342  deg
RA of node:       356
1948  deg
Eccentricity:     
0024469     
Arg of perigee:   320
5532  deg
Mean anomaly:      39
3850  deg
Mean motion:   15
75604963  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2105
Checksum:              306


Coasting Arc #8 (Orbit 2120)
---------------------------------------

Vector Time (GMT): 2006/345/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6666038
92                 A    =         6727586
82  meter
 Y    =         940698
07  meter          E    =           
0012769
 Z    =        -194954
22                 I    =           51
60215
 XDOT =       -489
853975                 Wp   =          330
62341
 YDOT =      -4755
956640  meter/sec      RA   =          350
65247  deg
 ZDOT =      -6021
692061                 TA   =          211
49331
                                          MA   =          211
56981
                                          Ha   =            192
927  n
mi
                                          Hp   =            178
039

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21870206
44                 X    =        -6675115
45
 Y    =        3086279
77  feet           Y    =          866103
99  meter
 Z    =        -639613
57                 Z    =         -227359
84
 XDOT =      -1607
132464                 XDOT =        -407
383467
 YDOT =     -15603
532285  feet/sec       YDOT =       -4760
972810  meter/sec
 ZDOT =     -19756
207549                 ZDOT =       -6023
871876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10285496
66                 X    =        -3135019
38
 Y    =       19541495
87  feet           Y    =         5956247
94  meter
 Z    =        -760694
15                 Z    =         -231859
58
 XDOT =     -12107
359366                 XDOT =       -3690
323135
 YDOT =      -7161
041267  feet/sec       YDOT =       -2182
685378  meter/sec
 ZDOT =     -19764
901796                 ZDOT =       -6024
342067


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   06345
96027831  
00020000  00000-0  20000-3 0  9070
2 25544  51
6344 350
9708 0024362 324
2911  35
6622 15
75601793 21210


Satellite: ISS
Catalog Number: 25544
Epoch time:      06345
96027831   =   yrday
fracday
Element set:     907
Inclination:       51
6344  deg
RA of node:       350
9708  deg
Eccentricity:     
0024362     
Arg of perigee:   324
2911  deg
Mean anomaly:      35
6622  deg
Mean motion:   15
75601793  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2121
Checksum:              282


Coasting Arc #9 (Orbit 2136)
---------------------------------------

Vector Time (GMT): 2006/346/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          68039
87                 A    =         6715712
80  meter
 Y    =        4255219
61  meter          E    =           
0024596
 Z    =        5206646
51                 I    =           51
53404
 XDOT =      -7543
770641                 Wp   =          335
75109
 YDOT =       1227
296553  meter/sec      RA   =          345
48791  deg
 ZDOT =       -883
876736                 TA   =          122
80454
                                          MA   =          122
56740
                                          Ha   =            193
105  n
mi
                                          Hp   =            177
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         223227
93                 X    =           -4840
71
 Y    =       13960694
25  feet           Y    =         4255572
54  meter
 Z    =       17082173
58                 Z    =         5206800
37
 XDOT =     -24749
903679                 XDOT =       -7552
640040
 YDOT =       4026
563493  feet/sec       YDOT =        1142
888400  meter/sec
 ZDOT =      -2899
858059                 ZDOT =        -920
545996

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11536047
09                 X    =         3516187
15
 Y    =        7863469
35  feet           Y    =         2396785
46  meter
 Z    =       17083235
53                 Z    =         5206970
19
 XDOT =     -10239
009838                 XDOT =       -3120
850199
 YDOT =      21765
174946  feet/sec       YDOT =        6634
025324  meter/sec
 ZDOT =      -3036
849376                 ZDOT =        -925
631690


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   06346
97505660  
00020000  00000-0  20000-3 0  9084
2 25544  51
6339 345
7447 0024362 328
1970  31
7721 15
75647191 21370


Satellite: ISS
Catalog Number: 25544
Epoch time:      06346
97505660   =   yrday
fracday
Element set:     908
Inclination:       51
6339  deg
RA of node:       345
7447  deg
Eccentricity:     
0024362     
Arg of perigee:   328
1970  deg
Mean anomaly:      31
7721  deg
Mean motion:   15
75647191  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2137
Checksum:              306


Coasting Arc #10 (Orbit 2152)
---------------------------------------

Vector Time (GMT): 2006/347/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6466684
81                 A    =         6726547
38  meter
 Y    =       -1186282
44  meter          E    =           
0028412
 Z    =        1331057
09                 I    =           51
54279
 XDOT =       -275
593474                 Wp   =             
93966
 YDOT =       5030
485172  meter/sec      RA   =          340
35201  deg
 ZDOT =       5848
431798                 TA   =           13
73901
                                          MA   =           13
66184
                                          Ha   =            193
155  n
mi
                                          Hp   =            177
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21216157
51                 X    =         6473003
28
 Y    =       -3892002
77  feet           Y    =        -1113933
17  meter
 Z    =        4366985
20                 Z    =         1362487
77
 XDOT =       -904
178064                 XDOT =        -360
235450
 YDOT =      16504
216443  feet/sec       YDOT =        5026
929582  meter/sec
 ZDOT =      19187
768366                 ZDOT =        5846
887781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8562301
38                 X    =         2609789
46
 Y    =      -19771717
98  feet           Y    =        -6026419
64  meter
 Z    =        4484389
39                 Z    =         1366841
89
 XDOT =      11706
873807                 XDOT =        3568
255136
 YDOT =       9401
551950  feet/sec       YDOT =        2865
593034  meter/sec
 ZDOT =      19182
569725                 ZDOT =        5846
847252


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   06347
98981147  
00020000  00000-0  20000-3 0  9095
2 25544  51
6328 340
5186 0024318 332
0166  27
9689 15
75699683 21534


Satellite: ISS
Catalog Number: 25544
Epoch time:      06347
98981147   =   yrday
fracday
Element set:     909
Inclination:       51
6328  deg
RA of node:       340
5186  deg
Eccentricity:     
0024318     
Arg of perigee:   332
0166  deg
Mean anomaly:      27
9689  deg
Mean motion:   15
75699683  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2153
Checksum:              331


Coasting Arc #11 (Orbit 2167)
---------------------------------------

Vector Time (GMT): 2006/348/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         517994
25                 A    =         6716719
40  meter
 Y    =       -4547505
99  meter          E    =           
0018714
 Z    =       -4911597
02                 I    =           51
48247
 XDOT =       7253
637857                 Wp   =            6
32073
 YDOT =      -1473
283279  meter/sec      RA   =          335
16303  deg
 ZDOT =       2148
147417                 TA   =          284
44435
                                          MA   =          284
65194
                                          Ha   =            193
354  n
mi
                                          Hp   =            177
348

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1699456
21                 X    =          592666
54
 Y    =      -14919639
07  feet           Y    =        -4541295
51  meter
 Z    =      -16114163
46                 Z    =        -4908899
62
 XDOT =      23798
024464                 XDOT =        7259
137774
 YDOT =      -4833
606558  feet/sec       YDOT =       -1392
138521  meter/sec
 ZDOT =       7047
727746                 ZDOT =        2183
399235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11565787
22                 X    =        -3525251
94
 Y    =       -9592945
86  feet           Y    =        -2923929
90  meter
 Z    =      -16104595
65                 Z    =        -4908680
76
 XDOT =       8122
174436                 XDOT =        2475
638768
 YDOT =     -21740
101736  feet/sec       YDOT =       -6626
383009  meter/sec
 ZDOT =       7179
388493                 ZDOT =        2188
277613


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   06348
94112379  
00020000  00000-0  20000-3 0  9107
2 25544  51
6317 335
6192 0024186 335
8191  24
1836 15
75733230 21682


Satellite: ISS
Catalog Number: 25544
Epoch time:      06348
94112379   =   yrday
fracday
Element set:     910
Inclination:       51
6317  deg
RA of node:       335
6192  deg
Eccentricity:     
0024186     
Arg of perigee:   335
8191  deg
Mean anomaly:      24
1836  deg
Mean motion:   15
75733230  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2168
Checksum:              291


Coasting Arc #12 (Orbit 2183)
---------------------------------------

Vector Time (GMT): 2006/349/22:17:48
224
Vector Time (MET): N/A
Weight (LBS)     : 469411
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6144033
92                 A    =         6724498
60  meter
 Y    =        1314141
97  meter          E    =           
0019621
 Z    =       -2424350
67                 I    =           51
48383
 XDOT =        950
829897                 Wp   =          346
80834
 YDOT =      -5450
820034  meter/sec      RA   =          330
04220  deg
 ZDOT =      -5337
056459                 TA   =          220
58457
                                          MA   =          220
73101
                                          Ha   =            193
543  n
mi
                                          Hp   =            176
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20157591
60                 X    =        -6146494
98
 Y    =        4311489
39  feet           Y    =         1245422
47  meter
 Z    =       -7953906
40                 Z    =        -2454204
65
 XDOT =       3119
520660                 XDOT =        1037
637889
 YDOT =     -17883
267829  feet/sec       YDOT =       -5439
701371  meter/sec
 ZDOT =     -17510
027754                 ZDOT =       -5332
227002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6951701
82                 X    =        -2118878
72
 Y    =       19359886
97  feet           Y    =         5900893
55  meter
 Z    =       -8065400
52                 Z    =        -2458334
08
 XDOT =     -12081
253813                 XDOT =       -3682
366162
 YDOT =     -11662
383343  feet/sec       YDOT =       -3554
694443  meter/sec
 ZDOT =     -17492
587952                 ZDOT =       -5331
740808


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   06349
95583320  
00020000  00000-0  20000-3 0  9118
2 25544  51
6315 330
3942 0024238 339
8757  20
1449 15
75776452 21842


Satellite: ISS
Catalog Number: 25544
Epoch time:      06349
95583320   =   yrday
fracday
Element set:     911
Inclination:       51
6315  deg
RA of node:       330
3942  deg
Eccentricity:     
0024238     
Arg of perigee:   339
8757  deg
Mean anomaly:      20
1449  deg
Mean motion:   15
75776452  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2184
Checksum:              302

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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