Date: December 13th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9256 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2111)
---------------------------------------

Vector Time (GMT): 2006/345/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         498899
59                 A    =         6715614
02  meter
 Y    =       -4211809
84  meter          E    =           
0017110
 Z    =       -5204402
30                 I    =           51
57789
 XDOT =       7653
594405                 Wp   =          358
94229
 YDOT =       -165
917536  meter/sec      RA   =          353
49830  deg
 ZDOT =        884
731949                 TA   =          279
38736
                                          MA   =          279
58076
                                          Ha   =            192
545  n
mi
                                          Hp   =            178
168

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1636809
69                 X    =          571241
60
 Y    =      -13818273
75  feet           Y    =        -4205825
88  meter
 Z    =      -17074810
69                 Z    =        -5201803
33
 XDOT =      25110
217865                 XDOT =        7650
583021
 YDOT =       -544
348872  feet/sec       YDOT =         -80
347714  meter/sec
 ZDOT =       2902
663874                 ZDOT =         921
905770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6337058
84                 X    =         1931535
53
 Y    =       12400846
01  feet           Y    =         3779777
87  meter
 Z    =      -17065570
57                 Z    =        -5201585
91
 XDOT =     -19541
888881                 XDOT =       -5956
367731
 YDOT =      14096
297654  feet/sec       YDOT =        4296
551525  meter/sec
 ZDOT =       3041
664695                 ZDOT =         927
099399


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
38927283  
00020000  00000-0  20000-3 0  9009
2 25544  51
6343 353
9122 0023964 322
1656  37
7823 15
75669038 21124


Satellite: ISS
Catalog Number: 25544
Epoch time:      06345
38927283   =   yrday
fracday
Element set:     900
Inclination:       51
6343  deg
RA of node:       353
9122  deg
Eccentricity:     
0023964     
Arg of perigee:   322
1656  deg
Mean anomaly:      37
7823  deg
Mean motion:   15
75669038  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2112
Checksum:              295


Coasting Arc #2 (Orbit 2127)
---------------------------------------

Vector Time (GMT): 2006/346/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6591555
21                 A    =         6726358
30  meter
 Y    =         265133
80  meter          E    =           
0015205
 Z    =       -1348810
97                 I    =           51
58747
 XDOT =       1002
431254                 Wp   =          328
10863
 YDOT =      -4921
057810  meter/sec      RA   =          348
36623  deg
 ZDOT =      -5823
617035                 TA   =          226
70355
                                          MA   =          226
83046
                                          Ha   =            192
681  n
mi
                                          Hp   =            177
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21625837
30                 X    =        -6587477
78
 Y    =         869861
54  feet           Y    =          191446
28  meter
 Z    =       -4425232
85                 Z    =        -1380822
91
 XDOT =       3288
816451                 XDOT =        1085
674867
 YDOT =     -16145
202788  feet/sec       YDOT =       -4909
382133  meter/sec
 ZDOT =     -19106
355101                 ZDOT =       -5818
545429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17150842
04                 X    =         5227576
65
 Y    =      -13160870
91  feet           Y    =        -4011433
45  meter
 Z    =       -4544917
86                 Z    =        -1385290
96
 XDOT =       5571
686247                 XDOT =        1698
249968
 YDOT =      13899
513971  feet/sec       YDOT =        4236
571858  meter/sec
 ZDOT =     -19087
950742                 ZDOT =       -5818
007386


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
40400392  
00020000  00000-0  20000-3 0  9011
2 25544  51
6349 348
6871 0023878 326
5588  33
4067 15
75750546 21283


Satellite: ISS
Catalog Number: 25544
Epoch time:      06346
40400392   =   yrday
fracday
Element set:     901
Inclination:       51
6349  deg
RA of node:       348
6871  deg
Eccentricity:     
0023878     
Arg of perigee:   326
5588  deg
Mean anomaly:      33
4067  deg
Mean motion:   15
75750546  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2128
Checksum:              306


Coasting Arc #3 (Orbit 2143)
---------------------------------------

Vector Time (GMT): 2006/347/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1256363
86                 A    =         6716683
86  meter
 Y    =        4441810
62  meter          E    =           
0025019
 Z    =        4892893
29                 I    =           51
52690
 XDOT =      -7355
924218                 Wp   =          344
99168
 YDOT =        383
920334  meter/sec      RA   =          343
17999  deg
 ZDOT =      -2216
089587                 TA   =          126
71517
                                          MA   =          126
48509
                                          Ha   =            192
837  n
mi
                                          Hp   =            177
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4121928
69                 X    =        -1329708
38
 Y    =       14572869
49  feet           Y    =         4427350
77  meter
 Z    =       16052799
50                 Z    =         4886612
04
 XDOT =     -24133
609639                 XDOT =       -7348
905128
 YDOT =       1259
581149  feet/sec       YDOT =         301
701731  meter/sec
 ZDOT =      -7270
635129                 ZDOT =       -2251
807822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5204041
36                 X    =        -1586191
81
 Y    =      -14248301
20  feet           Y    =        -4342882
20  meter
 Z    =       16029817
83                 Z    =         4885888
47
 XDOT =      17664
263094                 XDOT =        5384
067391
 YDOT =     -14860
134031  feet/sec       YDOT =       -4529
368853  meter/sec
 ZDOT =      -7404
165742                 ZDOT =       -2256
789718


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
41870493  
00020000  00000-0  20000-3 0  9027
2 25544  51
6343 343
4617 0023871 330
2512  29
7293 15
75804023 21447


Satellite: ISS
Catalog Number: 25544
Epoch time:      06347
41870493   =   yrday
fracday
Element set:     902
Inclination:       51
6343  deg
RA of node:       343
4617  deg
Eccentricity:     
0023871     
Arg of perigee:   330
2512  deg
Mean anomaly:      29
7293  deg
Mean motion:   15
75804023  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2144
Checksum:              276


Coasting Arc #4 (Orbit 2159)
---------------------------------------

Vector Time (GMT): 2006/348/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6217101
35                 A    =         6724294
28  meter
 Y    =        -367798
61  meter          E    =           
0025074
 Z    =        2493451
13                 I    =           51
52548
 XDOT =      -1813
267399                 Wp   =            7
12757
 YDOT =       5288
224541  meter/sec      RA   =          338
06192  deg
 ZDOT =       5319
990674                 TA   =           21
21607
                                          MA   =           21
11227
                                          Ha   =            192
991  n
mi
                                          Hp   =            177
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20397314
15                 X    =         6208639
20
 Y    =       -1206688
35  feet           Y    =         -298323
06  meter
 Z    =        8180613
95                 Z    =         2523633
53
 XDOT =      -5949
040024                 XDOT =       -1898
110117
 YDOT =      17349
818048  feet/sec       YDOT =        5267
472731  meter/sec
 ZDOT =      17454
037645                 ZDOT =        5310
976110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15488937
81                 X    =        -4721028
25
 Y    =       13256717
88  feet           Y    =         4040647
61  meter
 Z    =        8293443
35                 Z    =         2527841
53
 XDOT =      -4697
139516                 XDOT =       -1431
688124
 YDOT =     -16348
595976  feet/sec       YDOT =       -4983
052053  meter/sec
 ZDOT =      17420
931065                 ZDOT =        5309
899789


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
43338002  
00020000  00000-0  20000-3 0  9036
2 25544  51
6340 338
2356 0023804 334
9959  25
0050 15
75793321 21604


Satellite: ISS
Catalog Number: 25544
Epoch time:      06348
43338002   =   yrday
fracday
Element set:     903
Inclination:       51
6340  deg
RA of node:       338
2356  deg
Eccentricity:     
0023804     
Arg of perigee:   334
9959  deg
Mean anomaly:      25
0050  deg
Mean motion:   15
75793321  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2160
Checksum:              272


Coasting Arc #5 (Orbit 2174)
---------------------------------------

Vector Time (GMT): 2006/349/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1855069
11                 A    =         6718806
08  meter
 Y    =       -4802097
64  meter          E    =           
0019020
 Z    =       -4305491
90                 I    =           51
48253
 XDOT =       6877
351163                 Wp   =          357
84364
 YDOT =       -430
142200  meter/sec      RA   =          332
85621  deg
 ZDOT =       3461
157427                 TA   =          307
07590
                                          MA   =          307
24964
                                          Ha   =            193
184  n
mi
                                          Hp   =            177
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6086184
75                 X    =         1929544
54
 Y    =      -15754913
50  feet           Y    =        -4780936
38  meter
 Z    =      -14125629
59                 Z    =        -4296299
43
 XDOT =      22563
488067                 XDOT =        6864
836035
 YDOT =      -1411
227691  feet/sec       YDOT =        -353
306162  meter/sec
 ZDOT =      11355
503370                 ZDOT =        3494
537600

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4885053
76                 X    =         1488964
39
 Y    =       16197214
29  feet           Y    =         4936910
92  meter
 Z    =      -14091800
96                 Z    =        -4295180
93
 XDOT =     -15640
699753                 XDOT =       -4767
285285
 YDOT =      14653
089553  feet/sec       YDOT =        4466
261696  meter/sec
 ZDOT =      11480
284182                 ZDOT =        3499
190619


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
38460750  
00020000  00000-0  20000-3 0  9048
2 25544  51
6350 333
3369 0023787 338
3286  21
6869 15
75863404 21752


Satellite: ISS
Catalog Number: 25544
Epoch time:      06349
38460750   =   yrday
fracday
Element set:     904
Inclination:       51
6350  deg
RA of node:       333
3369  deg
Eccentricity:     
0023787     
Arg of perigee:   338
3286  deg
Mean anomaly:      21
6869  deg
Mean motion:   15
75863404  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2175
Checksum:              312


Coasting Arc #6 (Orbit 2190)
---------------------------------------

Vector Time (GMT): 2006/350/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5728197
31                 A    =         6721214
55  meter
 Y    =         296455
27  meter          E    =           
0023312
 Z    =       -3523875
24                 I    =           51
46642
 XDOT =       2462
766147                 Wp   =          354
85814
 YDOT =      -5756
611083  meter/sec      RA   =          327
74471  deg
 ZDOT =      -4462
470990                 TA   =          227
14582
                                          MA   =          227
34188
                                          Ha   =            193
253  n
mi
                                          Hp   =            176
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18793298
27                 X    =        -5713967
98
 Y    =         972622
28  feet           Y    =          232479
37  meter
 Z    =      -11561270
47                 Z    =        -3551668
64
 XDOT =       8079
941426                 XDOT =        2548
632540
 YDOT =     -18886
519300  feet/sec       YDOT =       -5728
590429  meter/sec
 ZDOT =     -14640
652854                 ZDOT =       -4450
298805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13912866
66                 X    =         4240641
76
 Y    =      -12575883
74  feet           Y    =        -3833129
36  meter
 Z    =      -11665175
45                 Z    =        -3555545
48
 XDOT =       4673
901398                 XDOT =        1424
605146
 YDOT =      18785
434134  feet/sec       YDOT =        5725
800324  meter/sec
 ZDOT =     -14595
787109                 ZDOT =       -4448
795911


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   06350
39922235  
00020000  00000-0  20000-3 0  9053
2 25544  51
6347 328
1108 0023700 342
3451  17
6887 15
75926302 21915


Satellite: ISS
Catalog Number: 25544
Epoch time:      06350
39922235   =   yrday
fracday
Element set:     905
Inclination:       51
6347  deg
RA of node:       328
1108  deg
Eccentricity:     
0023700     
Arg of perigee:   342
3451  deg
Mean anomaly:      17
6887  deg
Mean motion:   15
75926302  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2191
Checksum:              280


Coasting Arc #7 (Orbit 2206)
---------------------------------------

Vector Time (GMT): 2006/351/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2415551
81                 A    =         6721516
62  meter
 Y    =        5276036
48  meter          E    =           
0024097
 Z    =        3409805
23                 I    =           51
44314
 XDOT =      -6181
382893                 Wp   =           16
26141
 YDOT =        145
363025  meter/sec      RA   =          322
52843  deg
 ZDOT =      -4573
302735                 TA   =          123
35739
                                          MA   =          123
12652
                                          Ha   =            193
397  n
mi
                                          Hp   =            176
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7925038
76                 X    =        -2490934
13
 Y    =       17309830
98  feet           Y    =         5248602
47  meter
 Z    =       11187025
03                 Z    =         3397887
94
 XDOT =     -20280
127602                 XDOT =       -6160
332340
 YDOT =        476
912811  feet/sec       YDOT =          76
357714  meter/sec
 ZDOT =     -15004
274065                 ZDOT =       -4603
281194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5047723
18                 X    =        -1538546
03
 Y    =      -18383113
21  feet           Y    =        -5603172
91  meter
 Z    =       11143054
17                 Z    =         3396402
91
 XDOT =      13795
726759                 XDOT =        4204
937516
 YDOT =     -13012
074521  feet/sec       YDOT =       -3966
080314  meter/sec
 ZDOT =     -15116
371023                 ZDOT =       -4607
469888


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   06351
41380671  
00020000  00000-0  20000-3 0  9060
2 25544  51
6334 322
8839 0023739 346
3270  13
7248 15
75989343 22078


Satellite: ISS
Catalog Number: 25544
Epoch time:      06351
41380671   =   yrday
fracday
Element set:     906
Inclination:       51
6334  deg
RA of node:       322
8839  deg
Eccentricity:     
0023739     
Arg of perigee:   346
3270  deg
Mean anomaly:      13
7248  deg
Mean motion:   15
75989343  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2207
Checksum:              300


Coasting Arc #8 (Orbit 2222)
---------------------------------------

Vector Time (GMT): 2006/352/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5064727
86                 A    =         6717929
00  meter
 Y    =         110870
31  meter          E    =           
0020444
 Z    =        4397202
04                 I    =           51
40916
 XDOT =      -2980
999976                 Wp   =           12
37267
 YDOT =       6307
736731  meter/sec      RA   =          317
41121  deg
 ZDOT =       3291
370046                 TA   =           44
62470
                                          MA   =           44
46031
                                          Ha   =            193
428  n
mi
                                          Hp   =            176
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16616561
22                 X    =         5041750
58
 Y    =         363747
72  feet           Y    =          167377
71  meter
 Z    =       14426515
88                 Z    =         4421751
02
 XDOT =      -9780
183648                 XDOT =       -3067
301506
 YDOT =      20694
674314  feet/sec       YDOT =        6273
918460  meter/sec
 ZDOT =      10798
458157                 ZDOT =        3276
679559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12698666
98                 X    =        -3870553
70
 Y    =       10598509
56  feet           Y    =         3230425
72  meter
 Z    =       14518341
21                 Z    =         4425190
40
 XDOT =      -5419
697173                 XDOT =       -1651
923698
 YDOT =     -21136
230941  feet/sec       YDOT =       -6442
323191  meter/sec
 ZDOT =      10744
227760                 ZDOT =        3274
840621


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   06352
42836236  
00020000  00000-0  20000-3 0  9076
2 25544  51
6330 317
6568 0023659 350
3675   9
7032 15
75997440 22231


Satellite: ISS
Catalog Number: 25544
Epoch time:      06352
42836236   =   yrday
fracday
Element set:     907
Inclination:       51
6330  deg
RA of node:       317
6568  deg
Eccentricity:     
0023659     
Arg of perigee:   350
3675  deg
Mean anomaly:       9
7032  deg
Mean motion:   15
75997440  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2223
Checksum:              299


Coasting Arc #9 (Orbit 2237)
---------------------------------------

Vector Time (GMT): 2006/353/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2708829
15                 A    =         6724040
13  meter
 Y    =       -5696789
50  meter          E    =           
0027778
 Z    =       -2280726
14                 I    =           51
41106
 XDOT =       5462
208292                 Wp   =            3
09505
 YDOT =        433
289531  meter/sec      RA   =          312
20020  deg
 ZDOT =       5435
601624                 TA   =          331
11935
                                          MA   =          331
27281
                                          Ha   =            193
556  n
mi
                                          Hp   =            175
962

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8887234
75                 X    =         2783409
58
 Y    =      -18690254
26  feet           Y    =        -5666080
45  meter
 Z    =       -7482697
30                 Z    =        -2267386
40
 XDOT =      17920
630878                 XDOT =        5430
551816
 YDOT =       1421
553578  feet/sec       YDOT =         494
192993  meter/sec
 ZDOT =      17833
338663                 ZDOT =        5462
060465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5903699
95                 X    =         1799447
75
 Y    =       19854206
64  feet           Y    =         6051562
18  meter
 Z    =       -7433445
39                 Z    =        -2265714
16
 XDOT =     -12729
431084                 XDOT =       -3879
930594
 YDOT =      10461
463894  feet/sec       YDOT =        3188
654195  meter/sec
 ZDOT =      17932
349890                 ZDOT =        5465
780247


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   06353
37947912  
00020000  00000-0  20000-3 0  9086
2 25544  51
6339 312
7579 0023577 353
9921   6
0957 15
76072769 22381


Satellite: ISS
Catalog Number: 25544
Epoch time:      06353
37947912   =   yrday
fracday
Element set:     908
Inclination:       51
6339  deg
RA of node:       312
7579  deg
Eccentricity:     
0023577     
Arg of perigee:   353
9921  deg
Mean anomaly:       6
0957  deg
Mean motion:   15
76072769  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2238
Checksum:              329


Coasting Arc #10 (Orbit 2253)
---------------------------------------

Vector Time (GMT): 2006/354/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4446799
85                 A    =         6715291
88  meter
 Y    =        -737820
92  meter          E    =           
0029273
 Z    =       -4995260
63                 I    =           51
36262
 XDOT =       3225
257688                 Wp   =           23
74192
 YDOT =      -6729
388340  meter/sec      RA   =          307
06586  deg
 ZDOT =      -1854
550470                 TA   =          228
14782
                                          MA   =          228
39805
                                          Ha   =            193
663  n
mi
                                          Hp   =            175
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14589238
36                 X    =        -4413952
78
 Y    =       -2420672
30  feet           Y    =         -787362
89  meter
 Z    =      -16388650
35                 Z    =        -5016783
62
 XDOT =      10581
554096                 XDOT =        3309
276051
 YDOT =     -22078
045735  feet/sec       YDOT =       -6692
851595  meter/sec
 ZDOT =      -6084
483170                 ZDOT =       -1838
679303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12242815
94                 X    =         3731610
30
 Y    =       -8134551
66  feet           Y    =        -2479411
35  meter
 Z    =      -16469241
56                 Z    =        -5019824
83
 XDOT =       6733
236480                 XDOT =        2052
290479
 YDOT =      22483
354854  feet/sec       YDOT =        6852
926559  meter/sec
 ZDOT =      -6025
875712                 ZDOT =       -1836
686917


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   06354
39397486  
00020000  00000-0  20000-3 0  9095
2 25544  51
6329 307
5307 0023589 357
6874   2
4177 15
76092190 22544


Satellite: ISS
Catalog Number: 25544
Epoch time:      06354
39397486   =   yrday
fracday
Element set:     909
Inclination:       51
6329  deg
RA of node:       307
5307  deg
Eccentricity:     
0023589     
Arg of perigee:   357
6874  deg
Mean anomaly:       2
4177  deg
Mean motion:   15
76092190  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2254
Checksum:              321


Coasting Arc #11 (Orbit 2269)
---------------------------------------

Vector Time (GMT): 2006/355/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2896050
88                 A    =         6725670
58  meter
 Y    =        6013929
08  meter          E    =           
0019625
 Z    =         896150
22                 I    =           51
38178
 XDOT =      -4711
380479                 Wp   =           36
34868
 YDOT =      -1374
804669  meter/sec      RA   =          301
87003  deg
 ZDOT =      -5917
573904                 TA   =          133
84580
                                          MA   =          133
68344
                                          Ha   =            193
796  n
mi
                                          Hp   =            175
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9501479
28                 X    =        -2967437
57
 Y    =       19730738
45  feet           Y    =         5981144
52  meter
 Z    =        2940125
38                 Z    =          881908
96
 XDOT =     -15457
285037                 XDOT =       -4666
910617
 YDOT =      -4510
514006  feet/sec       YDOT =       -1427
240180  meter/sec
 ZDOT =     -19414
612545                 ZDOT =       -5940
353993

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6883521
81                 X    =        -2098097
45
 Y    =      -20796724
92  feet           Y    =        -6338841
75  meter
 Z    =        2887532
79                 Z    =          880119
99
 XDOT =      12649
659135                 XDOT =        3855
616104
 YDOT =      -6932
387754  feet/sec       YDOT =       -2112
991787  meter/sec
 ZDOT =     -19499
986463                 ZDOT =       -5943
595874


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   06355
40843959  
00020000  00000-0  20000-3 0  9101
2 25544  51
6324 302
3030 0023711   1
6289 358
4949 15
76166630 22708


Satellite: ISS
Catalog Number: 25544
Epoch time:      06355
40843959   =   yrday
fracday
Element set:     910
Inclination:       51
6324  deg
RA of node:       302
3030  deg
Eccentricity:     
0023711     
Arg of perigee:     1
6289  deg
Mean anomaly:     358
4949  deg
Mean motion:   15
76166630  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2270
Checksum:              281


Coasting Arc #12 (Orbit 2285)
---------------------------------------

Vector Time (GMT): 2006/356/09:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 469410
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3829106
01                 A    =         6713877
99  meter
 Y    =        1715232
38  meter          E    =           
0023615
 Z    =        5236996
44                 I    =           51
32765
 XDOT =      -3332
188835                 Wp   =           10
72470
 YDOT =       6949
332350  meter/sec      RA   =          296
70711  deg
 ZDOT =        183
095004                 TA   =           77
66416
                                          MA   =           77
39990
                                          Ha   =            193
783  n
mi
                                          Hp   =            175
052

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12562683
75                 X    =         3784201
26
 Y    =        5627402
82  feet           Y    =         1757799
57  meter
 Z    =       17181746
85                 Z    =         5255489
33
 XDOT =     -10932
378067                 XDOT =       -3410
539028
 YDOT =      22799
646816  feet/sec       YDOT =        6911
631853  meter/sec
 ZDOT =        600
705395                 ZDOT =         166
718262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12790478
84                 X    =        -3898537
95
 Y    =        4848019
17  feet           Y    =         1477676
24  meter
 Z    =       17251129
56                 Z    =         5258144
29
 XDOT =      -8056
984398                 XDOT =       -2455
768844
 YDOT =     -22914
172204  feet/sec       YDOT =       -6984
239688  meter/sec
 ZDOT =        540
232107                 ZDOT =         164
662746


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   06356
42287441  
00020000  00000-0  20000-3 0  9113
2 25544  51
6318 297
0754 0023600   5
2471 354
8936 15
76186423 22869


Satellite: ISS
Catalog Number: 25544
Epoch time:      06356
42287441   =   yrday
fracday
Element set:     911
Inclination:       51
6318  deg
RA of node:       297
0754  deg
Eccentricity:     
0023600     
Arg of perigee:     5
2471  deg
Mean anomaly:     354
8936  deg
Mean motion:   15
76186423  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2286
Checksum:              294

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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