Date: November 30th 2006

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 1932)
---------------------------------------

Vector Time (GMT): 2006/334/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -61947
19                 A    =         6712338
49  meter
 Y    =       -5309444
76  meter          E    =           
0006554
 Z    =       -4104979
78                 I    =           51
87951
 XDOT =       6047
646096                 Wp   =          310
73579
 YDOT =       2881
703776  meter/sec      RA   =           51
98532  deg
 ZDOT =      -3810
379523                 TA   =          280
29169
                                          MA   =          280
36558
                                          Ha   =            181
807  n
mi
                                          Hp   =            178
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -203238
82                 X    =           17369
94
 Y    =      -17419438
19  feet           Y    =        -5309693
79  meter
 Z    =      -13467781
42                 Z    =        -4105088
33
 XDOT =      19841
358582                 XDOT =        6033
483440
 YDOT =       9454
408714  feet/sec       YDOT =        2949
252920  meter/sec
 ZDOT =     -12501
245154                 ZDOT =       -3781
033834

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16935426
50                 X    =        -5161918
00
 Y    =       -4079384
36  feet           Y    =        -1243396
35  meter
 Z    =      -13468824
07                 Z    =        -4105297
58
 XDOT =      13683
005728                 XDOT =        4170
580146
 YDOT =     -15804
728532  feet/sec       YDOT =       -4817
281257  meter/sec
 ZDOT =     -12391
207219                 ZDOT =       -3776
839960


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   06334
04488403  
00020000  00000-0  20000-3 0  9006
2 25544  51
6346  52
4176 0012343 278
0203  81
9562 15
78391709 19334


Satellite: ISS
Catalog Number: 25544
Epoch time:      06334
04488403   =   yrday
fracday
Element set:     900
Inclination:       51
6346  deg
RA of node:        52
4176  deg
Eccentricity:     
0012343     
Arg of perigee:   278
0203  deg
Mean anomaly:      81
9562  deg
Mean motion:   15
78391709  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1933
Checksum:              282


Coasting Arc #2 (Orbit 1948)
---------------------------------------

Vector Time (GMT): 2006/335/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5410927
69                 A    =         6717886
83  meter
 Y    =       -3407883
20  meter          E    =           
0002956
 Z    =        2052204
85                 I    =           51
87954
 XDOT =       1145
278447                 Wp   =          154
60145
 YDOT =      -5182
351196  meter/sec      RA   =           46
78868  deg
 ZDOT =      -5585
772947                 TA   =            2
54247
                                          MA   =            2
54097
                                          Ha   =            182
024  n
mi
                                          Hp   =            179
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17752387
43                 X    =        -5382387
56
 Y    =      -11180719
17  feet           Y    =        -3468231
75  meter
 Z    =        6732955
55                 Z    =         2025987
12
 XDOT =       3757
475219                 XDOT =        1230
278354
 YDOT =     -17002
464553  feet/sec       YDOT =       -5169
068450  meter/sec
 ZDOT =     -18326
026729                 ZDOT =       -5580
002920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14891051
32                 X    =        -4538792
44
 Y    =       14823217
03  feet           Y    =         4518116
55  meter
 Z    =        6634550
38                 Z    =         2022210
95
 XDOT =     -14620
098481                 XDOT =       -4456
206017
 YDOT =      -6493
556267  feet/sec       YDOT =       -1979
235950  meter/sec
 ZDOT =     -18305
074789                 ZDOT =       -5579
386796


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   06335
05787991  
00020000  00000-0  20000-3 0  9013
2 25544  51
6345  47
1805 0012162 281
7654  78
2147 15
78404224 19495


Satellite: ISS
Catalog Number: 25544
Epoch time:      06335
05787991   =   yrday
fracday
Element set:     901
Inclination:       51
6345  deg
RA of node:        47
1805  deg
Eccentricity:     
0012162     
Arg of perigee:   281
7654  deg
Mean anomaly:      78
2147  deg
Mean motion:   15
78404224  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1949
Checksum:              300


Coasting Arc #3 (Orbit 1964)
---------------------------------------

Vector Time (GMT): 2006/336/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2167616
70                 A    =         6707499
82  meter
 Y    =        3588994
78  meter          E    =           
0009369
 Z    =        5243165
46                 I    =           51
82537
 XDOT =      -6078
593443                 Wp   =          282
58043
 YDOT =      -4678
866923  meter/sec      RA   =           41
65813  deg
 ZDOT =        692
761063                 TA   =          160
86727
                                          MA   =          160
83206
                                          Ha   =            182
365  n
mi
                                          Hp   =            179
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7111603
33                 X    =        -2233059
22
 Y    =       11774917
26  feet           Y    =         3564388
92  meter
 Z    =       17201986
41                 Z    =         5232476
26
 XDOT =     -19942
891874                 XDOT =       -6029
187312
 YDOT =     -15350
613263  feet/sec       YDOT =       -4746
564946  meter/sec
 ZDOT =       2272
838134                 ZDOT =         663
350124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10019890
11                 X    =         3054062
50
 Y    =        9496523
53  feet           Y    =         2894540
37  meter
 Z    =       17162451
98                 Z    =         5231115
36
 XDOT =     -18470
307621                 XDOT =       -5629
749763
 YDOT =      15598
367283  feet/sec       YDOT =        4754
382348  meter/sec
 ZDOT =       2162
351667                 ZDOT =         659
084788


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   06336
07084366  
00020000  00000-0  20000-3 0  9023
2 25544  51
6352  41
9429 0012271 286
3299  73
6516 15
78483207 19659


Satellite: ISS
Catalog Number: 25544
Epoch time:      06336
07084366   =   yrday
fracday
Element set:     902
Inclination:       51
6352  deg
RA of node:        41
9429  deg
Eccentricity:     
0012271     
Arg of perigee:   286
3299  deg
Mean anomaly:      73
6516  deg
Mean motion:   15
78483207  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1965
Checksum:              304


Coasting Arc #4 (Orbit 1980)
---------------------------------------

Vector Time (GMT): 2006/337/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4892404
68                 A    =         6718936
68  meter
 Y    =        4503871
57  meter          E    =           
0012182
 Z    =         903389
23                 I    =           51
84210
 XDOT =      -3852
171014                 Wp   =          357
82820
 YDOT =       2989
060338  meter/sec      RA   =           36
50460  deg
 ZDOT =       5974
344871                 TA   =           12
02926
                                          MA   =           12
00019
                                          Ha   =            182
595  n
mi
                                          Hp   =            178
862

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16051196
45                 X    =         4837289
53
 Y    =       14776481
53  feet           Y    =         4558272
88  meter
 Z    =        2963875
43                 Z    =          927023
80
 XDOT =     -12638
356346                 XDOT =       -3914
331830
 YDOT =       9806
628405  feet/sec       YDOT =        2945
634954  meter/sec
 ZDOT =      19600
868999                 ZDOT =        5955
479905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17566739
58                 X    =         5354342
23
 Y    =      -12917441
01  feet           Y    =        -3937236
02  meter
 Z    =        3052744
60                 Z    =          930476
55
 XDOT =       6249
726341                 XDOT =        1904
916589
 YDOT =      13103
855914  feet/sec       YDOT =        3994
055282  meter/sec
 ZDOT =      19530
696336                 ZDOT =        5952
956243


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   06337
08377899  
00020000  00000-0  20000-3 0  9032
2 25544  51
6350  36
7050 0012373 290
5822  69
4015 15
78534468 19812


Satellite: ISS
Catalog Number: 25544
Epoch time:      06337
08377899   =   yrday
fracday
Element set:     903
Inclination:       51
6350  deg
RA of node:        36
7050  deg
Eccentricity:     
0012373     
Arg of perigee:   290
5822  deg
Mean anomaly:      69
4015  deg
Mean motion:   15
78534468  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1981
Checksum:              306


Coasting Arc #5 (Orbit 1995)
---------------------------------------

Vector Time (GMT): 2006/338/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4478017
20                 A    =         6709516
12  meter
 Y    =       -1627853
15  meter          E    =           
0001612
 Z    =       -4722684
58                 I    =           51
78638
 XDOT =       4799
128445                 Wp   =          335
14974
 YDOT =       5399
316919  meter/sec      RA   =           31
31646  deg
 ZDOT =       2690
525887                 TA   =          321
21785
                                          MA   =          321
22942
                                          Ha   =            182
940  n
mi
                                          Hp   =            178
706

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14691657
47                 X    =         4518829
74
 Y    =       -5340725
55  feet           Y    =        -1577548
57  meter
 Z    =      -15494371
98                 Z    =        -4700830
97
 XDOT =      15745
172063                 XDOT =        4725
325452
 YDOT =      17714
294354  feet/sec       YDOT =        5452
570381  meter/sec
 ZDOT =       8827
184668                 ZDOT =        2713
662135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2686910
77                 X    =         -818970
40
 Y    =      -15481210
22  feet           Y    =        -4718672
88  meter
 Z    =      -15412863
20                 Z    =        -4697840
70
 XDOT =      19047
050710                 XDOT =        5805
541056
 YDOT =     -12177
101906  feet/sec       YDOT =       -3711
580661  meter/sec
 ZDOT =       8914
290581                 ZDOT =        2717
075769


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
03338027  
00020000  00000-0  20000-3 0  9049
2 25544  51
6345  31
7947 0012399 294
4118  65
5753 15
78577890 19963


Satellite: ISS
Catalog Number: 25544
Epoch time:      06338
03338027   =   yrday
fracday
Element set:     904
Inclination:       51
6345  deg
RA of node:        31
7947  deg
Eccentricity:     
0012399     
Arg of perigee:   294
4118  deg
Mean anomaly:      65
5753  deg
Mean motion:   15
78577890  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1996
Checksum:              324


Coasting Arc #6 (Orbit 2011)
---------------------------------------

Vector Time (GMT): 2006/339/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3148979
13                 A    =         6713412
16  meter
 Y    =       -4711165
96  meter          E    =           
0008754
 Z    =       -3601264
55                 I    =           51
77409
 XDOT =       6260
970077                 Wp   =          320
65256
 YDOT =       -797
728115  meter/sec      RA   =           26
20335  deg
 ZDOT =      -4418
599144                 TA   =          262
40774
                                          MA   =          262
50718
                                          Ha   =            183
097  n
mi
                                          Hp   =            178
530

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10331296
37                 X    =        -3078569
57
 Y    =      -15456581
22  feet           Y    =        -4745985
29  meter
 Z    =      -11815172
41                 Z    =        -3616392
35
 XDOT =      20541
240410                 XDOT =        6290
890198
 YDOT =      -2617
218226  feet/sec       YDOT =        -727
546424  meter/sec
 ZDOT =     -14496
716351                 ZDOT =       -4388
110250

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16877338
52                 X    =        -5144212
78
 Y    =        7710043
65  feet           Y    =         2350021
31  meter
 Z    =      -11872260
02                 Z    =        -3618664
86
 XDOT =       1217
186430                 XDOT =         370
998424
 YDOT =     -19545
536162  feet/sec       YDOT =       -5957
479422  meter/sec
 ZDOT =     -14382
822707                 ZDOT =       -4383
884361


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
04626024  
00020000  00000-0  20000-3 0  9059
2 25544  51
6338  26
5573 0012457 298
2085  61
7822 15
78594671 20123


Satellite: ISS
Catalog Number: 25544
Epoch time:      06339
04626024   =   yrday
fracday
Element set:     905
Inclination:       51
6338  deg
RA of node:        26
5573  deg
Eccentricity:     
0012457     
Arg of perigee:   298
2085  deg
Mean anomaly:      61
7822  deg
Mean motion:   15
78594671  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2012
Checksum:              294


Coasting Arc #7 (Orbit 2027)
---------------------------------------

Vector Time (GMT): 2006/340/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6178066
62                 A    =         6715924
21  meter
 Y    =        -148514
55  meter          E    =           
0004758
 Z    =        2632256
80                 I    =           51
75724
 XDOT =      -2111
071002                 Wp   =           38
58914
 YDOT =      -5234
642951  meter/sec      RA   =           20
99207  deg
 ZDOT =      -5241
450676                 TA   =          111
48018
                                          MA   =          111
42943
                                          Ha   =            183
304  n
mi
                                          Hp   =            178
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20269247
46                 X    =        -6188733
92
 Y    =        -487252
47  feet           Y    =         -217661
24  meter
 Z    =        8636013
12                 Z    =         2602217
45
 XDOT =      -6926
085966                 XDOT =       -2026
917274
 YDOT =     -17174
025431  feet/sec       YDOT =       -5257
778642  meter/sec
 ZDOT =     -17196
360486                 ZDOT =       -5251
502920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3328661
09                 X    =        -1014575
90
 Y    =       20048125
80  feet           Y    =         6110668
75  meter
 Z    =        8523684
48                 Z    =         2598019
03
 XDOT =     -16499
564759                 XDOT =       -5029
067338
 YDOT =       4600
274679  feet/sec       YDOT =        1402
163722  meter/sec
 ZDOT =     -17234
530805                 ZDOT =       -5253
084989


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
05911085  
00020000  00000-0  20000-3 0  9067
2 25544  51
6341  21
3188 0012453 303
1119  56
8850 15
78687190 20284


Satellite: ISS
Catalog Number: 25544
Epoch time:      06340
05911085   =   yrday
fracday
Element set:     906
Inclination:       51
6341  deg
RA of node:        21
3188  deg
Eccentricity:     
0012453     
Arg of perigee:   303
1119  deg
Mean anomaly:      56
8850  deg
Mean motion:   15
78687190  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2028
Checksum:              273


Coasting Arc #8 (Orbit 2043)
---------------------------------------

Vector Time (GMT): 2006/341/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         323672
63                 A    =         6707391
74  meter
 Y    =        4308061
81  meter          E    =           
0008050
 Z    =        5135329
80                 I    =           51
70016
 XDOT =      -7516
206289                 Wp   =          307
04835
 YDOT =      -1031
124173  meter/sec      RA   =           15
85968  deg
 ZDOT =       1344
952926                 TA   =          130
13513
                                          MA   =          130
06458
                                          Ha   =            183
544  n
mi
                                          Hp   =            178
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1061918
08                 X    =          250528
58
 Y    =       14134061
05  feet           Y    =         4311271
41  meter
 Z    =       16848194
88                 Z    =         5136725
31
 XDOT =     -24659
469453                 XDOT =       -7510
651067
 YDOT =      -3382
953324  feet/sec       YDOT =       -1115
143741  meter/sec
 ZDOT =       4412
575217                 ZDOT =        1308
452293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14145755
49                 X    =         4311626
27
 Y    =         777730
17  feet           Y    =          237052
15  meter
 Z    =       16853894
50                 Z    =         5137067
04
 XDOT =      -6337
553476                 XDOT =       -1931
686299
 YDOT =      23048
217360  feet/sec       YDOT =        7025
096651  meter/sec
 ZDOT =       4275
979651                 ZDOT =        1303
318598


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
07193516  
00020000  00000-0  20000-3 0  9072
2 25544  51
6330  16
0793 0012298 306
8948  53
1090 15
78667100 20445


Satellite: ISS
Catalog Number: 25544
Epoch time:      06341
07193516   =   yrday
fracday
Element set:     907
Inclination:       51
6330  deg
RA of node:        16
0793  deg
Eccentricity:     
0012298     
Arg of perigee:   306
8948  deg
Mean anomaly:      53
1090  deg
Mean motion:   15
78667100  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2044
Checksum:              279


Coasting Arc #9 (Orbit 2059)
---------------------------------------

Vector Time (GMT): 2006/342/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6514038
29                 A    =         6718652
97  meter
 Y    =        1549279
19  meter          E    =           
0016477
 Z    =         398635
31                 I    =           51
70993
 XDOT =      -1457
193900                 Wp   =            1
35055
 YDOT =       4576
096001  meter/sec      RA   =           10
68450  deg
 ZDOT =       6038
124986                 TA   =            2
99197
                                          MA   =            2
98212
                                          Ha   =            183
631  n
mi
                                          Hp   =            177
843

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21371516
70                 X    =         6494293
40
 Y    =        5082936
96  feet           Y    =         1622012
31  meter
 Z    =        1307858
61                 Z    =          430232
83
 XDOT =      -4780
819882                 XDOT =       -1537
588285
 YDOT =      15013
438323  feet/sec       YDOT =        4559
350356  meter/sec
 ZDOT =      19810
121344                 ZDOT =        6030
851400

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7317797
11                 X    =         2230464
56
 Y    =      -20705175
80  feet           Y    =        -6310937
58  meter
 Z    =        1426186
87                 Z    =          434701
76
 XDOT =      12900
847434                 XDOT =        3932
178298
 YDOT =       5919
912688  feet/sec       YDOT =        1804
389387  meter/sec
 ZDOT =      19783
434998                 ZDOT =        6029
990987


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
08472824  
00020000  00000-0  20000-3 0  9087
2 25544  51
6320  10
8397 0012355 310
4770  49
5318 15
78740760 20608


Satellite: ISS
Catalog Number: 25544
Epoch time:      06342
08472824   =   yrday
fracday
Element set:     908
Inclination:       51
6320  deg
RA of node:        10
8397  deg
Eccentricity:     
0012355     
Arg of perigee:   310
4770  deg
Mean anomaly:      49
5318  deg
Mean motion:   15
78740760  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2060
Checksum:              277


Coasting Arc #10 (Orbit 2074)
---------------------------------------

Vector Time (GMT): 2006/343/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2832278
36                 A    =         6708174
22  meter
 Y    =       -3615309
01  meter          E    =           
0005875
 Z    =       -4890447
76                 I    =           51
64571
 XDOT =       6961
254775                 Wp   =           31
61781
 YDOT =       2443
217198  meter/sec      RA   =            5
49181  deg
 ZDOT =       2231
523166                 TA   =          260
01513
                                          MA   =          260
08144
                                          Ha   =            183
796  n
mi
                                          Hp   =            177
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9292251
84                 X    =         2896251
61
 Y    =      -11861250
04  feet           Y    =        -3583278
51  meter
 Z    =      -16044776
12                 Z    =        -4876533
70
 XDOT =      22838
762385                 XDOT =        6922
576689
 YDOT =       8015
804455  feet/sec       YDOT =        2520
845235  meter/sec
 ZDOT =       7321
270230                 ZDOT =        2265
247280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10980976
19                 X    =        -3347001
54
 Y    =      -10397468
26  feet           Y    =        -3169148
33  meter
 Z    =      -15993150
19                 Z    =        -4874712
18
 XDOT =       9250
974302                 XDOT =        2819
696967
 YDOT =     -21194
983692  feet/sec       YDOT =       -6460
231029  meter/sec
 ZDOT =       7447
657975                 ZDOT =        2270
046151


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
03419711  
00020000  00000-0  20000-3 0  9090
2 25544  51
6311   5
9273 0012225 314
1693  45
8467 15
78789997 20752


Satellite: ISS
Catalog Number: 25544
Epoch time:      06343
03419711   =   yrday
fracday
Element set:     909
Inclination:       51
6311  deg
RA of node:         5
9273  deg
Eccentricity:     
0012225     
Arg of perigee:   314
1693  deg
Mean anomaly:      45
8467  deg
Mean motion:   15
78789997  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2075
Checksum:              304


Coasting Arc #11 (Orbit 2090)
---------------------------------------

Vector Time (GMT): 2006/344/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5189061
54                 A    =         6713528
05  meter
 Y    =       -2667290
91  meter          E    =           
0009643
 Z    =       -3327871
88                 I    =           51
63563
 XDOT =       4894
972092                 Wp   =          339
69603
 YDOT =      -3671
294527  meter/sec      RA   =             
36400  deg
 ZDOT =      -4677
134013                 TA   =          239
49388
                                          MA   =          239
58912
                                          Ha   =            183
911  n
mi
                                          Hp   =            177
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17024480
10                 X    =        -5142683
70
 Y    =       -8750954
44  feet           Y    =        -2725058
17  meter
 Z    =      -10918214
85                 Z    =        -3352967
95
 XDOT =      16059
619723                 XDOT =        4958
381829
 YDOT =     -12044
929550  feet/sec       YDOT =       -3616
201127  meter/sec
 ZDOT =     -15344
927863                 ZDOT =       -4653
200715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9944369
70                 X    =        -3031043
88
 Y    =       16292845
73  feet           Y    =         4966059
38  meter
 Z    =      -11012367
19                 Z    =        -3356569
52
 XDOT =      -9668
505368                 XDOT =       -2946
960436
 YDOT =     -16241
050732  feet/sec       YDOT =       -4950
272263  meter/sec
 ZDOT =     -15255
840252                 ZDOT =       -4649
980109


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
04693625  
00020000  00000-0  20000-3 0  9102
2 25544  51
6308    
6887 0012226 318
5512  41
4725 15
78836714 20917


Satellite: ISS
Catalog Number: 25544
Epoch time:      06344
04693625   =   yrday
fracday
Element set:     910
Inclination:       51
6308  deg
RA of node:          
6887  deg
Eccentricity:     
0012226     
Arg of perigee:   318
5512  deg
Mean anomaly:      41
4725  deg
Mean motion:   15
78836714  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2091
Checksum:              281


Coasting Arc #12 (Orbit 2106)
---------------------------------------

Vector Time (GMT): 2006/345/00:32:03
171
Vector Time (MET): N/A
Weight (LBS)     : 470269
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5424431
51                 A    =         6714754
94  meter
 Y    =        2737771
73  meter          E    =           
0009416
 Z    =        2863121
96                 I    =           51
61199
 XDOT =      -4519
067042                 Wp   =           36
76289
 YDOT =      -3641
742451  meter/sec      RA   =          355
13943  deg
 ZDOT =      -5063
494922                 TA   =          110
29349
                                          MA   =          110
19226
                                          Ha   =            184
026  n
mi
                                          Hp   =            177
038

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17796691
30                 X    =        -5468551
01
 Y    =        8982190
73  feet           Y    =         2676865
76  meter
 Z    =        9393444
76                 Z    =         2836663
21
 XDOT =     -14826
335439                 XDOT =       -4453
411189
 YDOT =     -11947
973920  feet/sec       YDOT =       -3691
909557  meter/sec
 ZDOT =     -16612
516149                 ZDOT =       -5085
289415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7995786
19                 X    =         2437115
63
 Y    =       18311546
32  feet           Y    =         5581359
32  meter
 Z    =        9294807
71                 Z    =         2833057
39
 XDOT =     -11398
022589                 XDOT =       -3474
117285
 YDOT =      13477
818424  feet/sec       YDOT =        4108
039056  meter/sec
 ZDOT =     -16694
434997                 ZDOT =       -5088
463787


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
05964537  
00020000  00000-0  20000-3 0  9118
2 25544  51
6313 355
4485 0012337 321
7617  38
2673 15
78903735 21075


Satellite: ISS
Catalog Number: 25544
Epoch time:      06345
05964537   =   yrday
fracday
Element set:     911
Inclination:       51
6313  deg
RA of node:       355
4485  deg
Eccentricity:     
0012337     
Arg of perigee:   321
7617  deg
Mean anomaly:      38
2673  deg
Mean motion:   15
78903735  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2107
Checksum:              295

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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