Date: December 18th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 95 ET - UTC (sec) : 66 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 3468)
---------------------------------------

Vector Time (GMT): 2009/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3050655
13                 A    =         6717727
68  meter
 Y    =        4442500
07  meter          E    =           
0018217
 Z    =        3996553
59                 I    =           51
97772
 XDOT =      -3201
894927                 Wp   =           95
69598
 YDOT =      -5785
527960  meter/sec      RA   =           89
03615  deg
 ZDOT =       3969
910065                 TA   =          313
43000
                                          MA   =          313
58146
                                          Ha   =            188
803  n
mi
                                          Hp   =            177
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10008711
04                 X    =        -3119519
86
 Y    =       14575131
46  feet           Y    =         4408000
16  meter
 Z    =       13112052
48                 Z    =         3981566
86
 XDOT =     -10504
904615                 XDOT =       -3156
247383
 YDOT =     -18981
390946  feet/sec       YDOT =       -5821
078849  meter/sec
 ZDOT =      13024
639322                 ZDOT =        3954
465111

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13540088
09                 X    =        -4127018
85
 Y    =      -11437816
72  feet           Y    =        -3486246
54  meter
 Z    =       13052855
52                 Z    =         3978510
36
 XDOT =      19075
008714                 XDOT =        5814
062656
 YDOT =      -7722
815755  feet/sec       YDOT =       -2353
914242  meter/sec
 ZDOT =      12963
384734                 ZDOT =        3951
239667


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   09350
55474530  
00016717  00000-0  10270-3 0  9007
2 25544  51
6450  89
4929 0007424  87
1594 273
0420 15
76649911 34694


Satellite: ISS
Catalog Number: 25544
Epoch time:      09350
55474530   =   yrday
fracday
Element set:     900
Inclination:       51
6450  deg
RA of node:        89
4929  deg
Eccentricity:     
0007424     
Arg of perigee:    87
1594  deg
Mean anomaly:     273
0420  deg
Mean motion:   15
76649911  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3469
Checksum:              325


Coasting Arc #2 (Orbit 3483)
---------------------------------------

Vector Time (GMT): 2009/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2748456
58                 A    =         6721462
58  meter
 Y    =        5488352
55  meter          E    =           
0011734
 Z    =       -2744839
81                 I    =           51
98857
 XDOT =      -3608
112855                 Wp   =           76
48484
 YDOT =       4392
516765  meter/sec      RA   =           83
85721  deg
 ZDOT =       5191
131984                 TA   =          252
30861
                                          MA   =          252
43675
                                          Ha   =            188
753  n
mi
                                          Hp   =            177
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9017246
00                 X    =         2700214
54
 Y    =       18006406
00  feet           Y    =         5518818
11  meter
 Z    =       -9005379
94                 Z    =        -2731604
09
 XDOT =     -11837
640602                 XDOT =       -3682
180202
 YDOT =      14411
144243  feet/sec       YDOT =        4351
753764  meter/sec
 ZDOT =      17031
272913                 ZDOT =        5173
424526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18665288
58                 X    =        -5689179
96
 Y    =        7621762
42  feet           Y    =         2323113
19  meter
 Z    =       -8952876
09                 Z    =        -2728836
63
 XDOT =     -12869
642247                 XDOT =       -3922
666957
 YDOT =     -11675
289014  feet/sec       YDOT =       -3558
628091  meter/sec
 ZDOT =      16961
297432                 ZDOT =        5169
803457


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   09351
50549591  
00016717  00000-0  10270-3 0  9014
2 25544  51
6452  84
5929 0007347  88
8057 271
3949 15
76624935 34841


Satellite: ISS
Catalog Number: 25544
Epoch time:      09351
50549591   =   yrday
fracday
Element set:     901
Inclination:       51
6452  deg
RA of node:        84
5929  deg
Eccentricity:     
0007347     
Arg of perigee:    88
8057  deg
Mean anomaly:     271
3949  deg
Mean motion:   15
76624935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3484
Checksum:              349


Coasting Arc #3 (Orbit 3499)
---------------------------------------

Vector Time (GMT): 2009/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3316825
81                 A    =         6714094
35  meter
 Y    =       -3138954
57  meter          E    =           
0019694
 Z    =       -4939474
10                 I    =           51
95929
 XDOT =       3079
222252                 Wp   =           80
98049
 YDOT =       6697
067399  meter/sec      RA   =           78
76599  deg
 ZDOT =      -2192
558057                 TA   =          167
81965
                                          MA   =          167
77197
                                          Ha   =            188
684  n
mi
                                          Hp   =            177
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10881974
45                 X    =         3375674
66
 Y    =      -10298407
38  feet           Y    =        -3101534
09  meter
 Z    =      -16205623
68                 Z    =        -4923218
51
 XDOT =      10102
435210                 XDOT =        3014
756642
 YDOT =      21972
005901  feet/sec       YDOT =        6731
140960  meter/sec
 ZDOT =      -7193
431947                 ZDOT =       -2177
754812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9602016
49                 X    =         2926694
62
 Y    =       11591145
47  feet           Y    =         3532981
14  meter
 Z    =      -16141357
67                 Z    =        -4919885
82
 XDOT =     -21710
567844                 XDOT =       -6617
381079
 YDOT =       8069
378359  feet/sec       YDOT =        2459
546524  meter/sec
 ZDOT =      -7134
698307                 ZDOT =       -2174
656044


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   09352
51961009  
00016717  00000-0  10270-3 0  9029
2 25544  51
6449  79
3651 0007353  93
3030 266
8976 15
76660537 35006


Satellite: ISS
Catalog Number: 25544
Epoch time:      09352
51961009   =   yrday
fracday
Element set:     902
Inclination:       51
6449  deg
RA of node:        79
3651  deg
Eccentricity:     
0007353     
Arg of perigee:    93
3030  deg
Mean anomaly:     266
8976  deg
Mean motion:   15
76660537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3500
Checksum:              319


Coasting Arc #4 (Orbit 3515)
---------------------------------------

Vector Time (GMT): 2009/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2628634
65                 A    =         6724063
64  meter
 Y    =       -6094472
90  meter          E    =           
0020728
 Z    =        1025633
00                 I    =           51
98558
 XDOT =       4041
233709                 Wp   =          114
23120
 YDOT =      -2759
720825  meter/sec      RA   =           73
60665  deg
 ZDOT =      -5956
088362                 TA   =           54
59201
                                          MA   =           54
39860
                                          Ha   =            188
695  n
mi
                                          Hp   =            176
919

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8624129
42                 X    =        -2565272
13
 Y    =      -19994989
84  feet           Y    =        -6123513
71  meter
 Z    =        3364937
68                 Z    =         1013016
24
 XDOT =      13258
640778                 XDOT =        4100
726505
 YDOT =      -9054
202182  feet/sec       YDOT =       -2714
195919  meter/sec
 ZDOT =     -19540
972315                 ZDOT =       -5936
311998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20359858
78                 X    =         6205684
96
 Y    =       -7745050
71  feet           Y    =        -2360691
46  meter
 Z    =        3314871
41                 Z    =         1010372
81
 XDOT =       7885
645450                 XDOT =        2403
544733
 YDOT =      12278
008465  feet/sec       YDOT =        3742
336980  meter/sec
 ZDOT =     -19462
757045                 ZDOT =       -5932
248347


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   09353
53370537  
00016717  00000-0  10270-3 0  9033
2 25544  51
6443  74
1372 0007535  96
3994 263
8029 15
76700226 35160


Satellite: ISS
Catalog Number: 25544
Epoch time:      09353
53370537   =   yrday
fracday
Element set:     903
Inclination:       51
6443  deg
RA of node:        74
1372  deg
Eccentricity:     
0007535     
Arg of perigee:    96
3994  deg
Mean anomaly:     263
8029  deg
Mean motion:   15
76700226  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3516
Checksum:              317


Coasting Arc #5 (Orbit 3531)
---------------------------------------

Vector Time (GMT): 2009/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3786291
02                 A    =         6712200
63  meter
 Y    =        1664997
03  meter          E    =           
0009736
 Z    =        5278167
85                 I    =           51
93707
 XDOT =      -2933
244809                 Wp   =           98
57737
 YDOT =      -7132
586357  meter/sec      RA   =           68
48401  deg
 ZDOT =        144
164842                 TA   =          350
05278
                                          MA   =          350
07204
                                          Ha   =            188
633  n
mi
                                          Hp   =            176
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12422214
63                 X    =        -3830268
15
 Y    =        5462588
69  feet           Y    =         1622409
98  meter
 Z    =       17316823
64                 Z    =         5259667
52
 XDOT =      -9623
506592                 XDOT =       -2853
969294
 YDOT =     -23400
873876  feet/sec       YDOT =       -7164
944397  meter/sec
 ZDOT =        472
981766                 ZDOT =         130
106933

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5118788
84                 X    =        -1560206
84
 Y    =      -12668024
58  feet           Y    =        -3861213
89  meter
 Z    =       17243631
48                 Z    =         5255858
88
 XDOT =      22731
383088                 XDOT =        6928
525565
 YDOT =      -8609
844977  feet/sec       YDOT =       -2624
280749  meter/sec
 ZDOT =        417
190515                 ZDOT =         127
159669


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   09354
54777922  
00016717  00000-0  10270-3 0  9045
2 25544  51
6448  68
9086 0007351  99
7036 260
4963 15
76771457 35320


Satellite: ISS
Catalog Number: 25544
Epoch time:      09354
54777922   =   yrday
fracday
Element set:     904
Inclination:       51
6448  deg
RA of node:        68
9086  deg
Eccentricity:     
0007351     
Arg of perigee:    99
7036  deg
Mean anomaly:     260
4963  deg
Mean motion:   15
76771457  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3532
Checksum:              349


Coasting Arc #6 (Orbit 3547)
---------------------------------------

Vector Time (GMT): 2009/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2427192
54                 A    =         6724105
38  meter
 Y    =        6214160
29  meter          E    =           
0019394
 Z    =         788948
61                 I    =           51
96416
 XDOT =      -4716
751336                 Wp   =           70
00183
 YDOT =       1066
330942  meter/sec      RA   =           63
35664  deg
 ZDOT =       6000
414223                 TA   =          298
57337
                                          MA   =          298
76840
                                          Ha   =            188
598  n
mi
                                          Hp   =            176
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7963230
11                 X    =         2353691
76
 Y    =       20387665
01  feet           Y    =         6240891
55  meter
 Z    =        2588414
06                 Z    =          800561
95
 XDOT =     -15474
905959                 XDOT =       -4757
473459
 YDOT =       3498
461095  feet/sec       YDOT =        1013
357149  meter/sec
 ZDOT =      19686
398368                 ZDOT =        5977
401548

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20467158
32                 X    =        -6238389
86
 Y    =        7741098
14  feet           Y    =         2359486
71  meter
 Z    =        2634508
57                 Z    =          802998
21
 XDOT =      -2776
428961                 XDOT =        -846
255547
 YDOT =     -14132
091911  feet/sec       YDOT =       -4307
461615  meter/sec
 ZDOT =      19595
330213                 ZDOT =        5972
656649


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   09355
56183805  
00016717  00000-0  10270-3 0  9050
2 25544  51
6442  63
6804 0007501 101
6684 258
5323 15
76743498 35482


Satellite: ISS
Catalog Number: 25544
Epoch time:      09355
56183805   =   yrday
fracday
Element set:     905
Inclination:       51
6442  deg
RA of node:        63
6804  deg
Eccentricity:     
0007501     
Arg of perigee:   101
6684  deg
Mean anomaly:     258
5323  deg
Mean motion:   15
76743498  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3548
Checksum:              326


Coasting Arc #7 (Orbit 3562)
---------------------------------------

Vector Time (GMT): 2009/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4486805
48                 A    =         6713465
65  meter
 Y    =        -211774
46  meter          E    =           
0020490
 Z    =       -5007862
05                 I    =           51
91327
 XDOT =       2522
910083                 Wp   =          104
52636
 YDOT =       6992
832049  meter/sec      RA   =           58
19723  deg
 ZDOT =       1966
327080                 TA   =          184
42317
                                          MA   =          184
44131
                                          Ha   =            188
494  n
mi
                                          Hp   =            176
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14720490
43                 X    =         4513167
32
 Y    =        -694798
09  feet           Y    =         -161452
52  meter
 Z    =      -16429993
60                 Z    =        -4986001
20
 XDOT =       8277
264052                 XDOT =        2434
975467
 YDOT =      22942
362365  feet/sec       YDOT =        7020
552882  meter/sec
 ZDOT =       6451
204331                 ZDOT =        1978
370351

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         800039
11                 X    =          243851
92
 Y    =       14811188
98  feet           Y    =         4514450
40  meter
 Z    =      -16343466
31                 Z    =        -4981488
53
 XDOT =     -21803
590266                 XDOT =       -6645
734313
 YDOT =       8343
149009  feet/sec       YDOT =        2542
991818  meter/sec
 ZDOT =       6499
013051                 ZDOT =        1980
899178


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   09356
51249824  
00016717  00000-0  10270-3 0  9061
2 25544  51
6435  58
7784 0007470 104
8013 255
3980 15
76789104 35637


Satellite: ISS
Catalog Number: 25544
Epoch time:      09356
51249824   =   yrday
fracday
Element set:     906
Inclination:       51
6435  deg
RA of node:        58
7784  deg
Eccentricity:     
0007470     
Arg of perigee:   104
8013  deg
Mean anomaly:     255
3980  deg
Mean motion:   15
76789104  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3563
Checksum:              332


Coasting Arc #8 (Orbit 3578)
---------------------------------------

Vector Time (GMT): 2009/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1883389
78                 A    =         6721165
24  meter
 Y    =       -5904284
79  meter          E    =           
0012462
 Z    =       -2602742
62                 I    =           51
92302
 XDOT =       5578
014253                 Wp   =          115
34879
 YDOT =        537
871569  meter/sec      RA   =           53
09815  deg
 ZDOT =      -5281
222672                 TA   =           94
11646
                                          MA   =           93
97401
                                          Ha   =            188
457  n
mi
                                          Hp   =            176
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6179100
33                 X    =        -1804583
40
 Y    =      -19371013
09  feet           Y    =        -5924905
14  meter
 Z    =       -8539181
81                 Z    =        -2611701
15
 XDOT =      18300
571697                 XDOT =        5597
240325
 YDOT =       1764
670501  feet/sec       YDOT =         600
356123  meter/sec
 ZDOT =     -17326
846037                 ZDOT =       -5254
077941

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19216723
54                 X    =         5857257
33
 Y    =       -6597437
05  feet           Y    =        -2010898
81  meter
 Z    =       -8574754
57                 Z    =        -2613585
19
 XDOT =      -1798
083794                 XDOT =        -548
055940
 YDOT =      17037
857731  feet/sec       YDOT =        5193
139037  meter/sec
 ZDOT =     -17219
389357                 ZDOT =       -5248
469876


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   09357
52651927  
00016717  00000-0  10270-3 0  9075
2 25544  51
6437  53
5491 0007587 108
2924 251
9067 15
76824333 35794


Satellite: ISS
Catalog Number: 25544
Epoch time:      09357
52651927   =   yrday
fracday
Element set:     907
Inclination:       51
6437  deg
RA of node:        53
5491  deg
Eccentricity:     
0007587     
Arg of perigee:   108
2924  deg
Mean anomaly:     251
9067  deg
Mean motion:   15
76824333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3579
Checksum:              343


Coasting Arc #9 (Orbit 3594)
---------------------------------------

Vector Time (GMT): 2009/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5239243
21                 A    =         6716902
38  meter
 Y    =       -1058073
51  meter          E    =           
0017428
 Z    =        4052827
21                 I    =           51
89023
 XDOT =      -1713
646250                 Wp   =           90
80074
 YDOT =      -6441
290085  meter/sec      RA   =           47
91210  deg
 ZDOT =      -3882
931564                 TA   =           39
03478
                                          MA   =           38
90913
                                          Ha   =            188
409  n
mi
                                          Hp   =            176
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17189118
13                 X    =        -5246710
21
 Y    =       -3471369
80  feet           Y    =        -1116703
88  meter
 Z    =       13296677
19                 Z    =         4027356
67
 XDOT =      -5622
198982                 XDOT =       -1622
628611
 YDOT =     -21132
841486  feet/sec       YDOT =       -6459
943898  meter/sec
 ZDOT =     -12739
276785                 ZDOT =       -3891
035876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2752017
42                 X    =          838814
91
 Y    =      -17395805
03  feet           Y    =        -5302241
37  meter
 Z    =       13195839
57                 Z    =         4022091
90
 XDOT =      19616
404364                 XDOT =        5979
080050
 YDOT =      -6619
763254  feet/sec       YDOT =       -2017
703840  meter/sec
 ZDOT =     -12771
472218                 ZDOT =       -3892
744732


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   09358
54051985  
00016717  00000-0  10270-3 0  9087
2 25544  51
6440  48
3202 0007398 111
3494 248
8461 15
76884740 35956


Satellite: ISS
Catalog Number: 25544
Epoch time:      09358
54051985   =   yrday
fracday
Element set:     908
Inclination:       51
6440  deg
RA of node:        48
3202  deg
Eccentricity:     
0007398     
Arg of perigee:   111
3494  deg
Mean anomaly:     248
8461  deg
Mean motion:   15
76884740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3595
Checksum:              337


Coasting Arc #10 (Orbit 3610)
---------------------------------------

Vector Time (GMT): 2009/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         995444
81                 A    =         6716790
04  meter
 Y    =        5256885
75  meter          E    =           
0018218
 Z    =        4049822
98                 I    =           51
86868
 XDOT =      -6416
818403                 Wp   =          107
62829
 YDOT =      -1791
276501  meter/sec      RA   =           42
82322  deg
 ZDOT =       3882
807971                 TA   =          302
48101
                                          MA   =          302
65698
                                          Ha   =            188
338  n
mi
                                          Hp   =            176
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3265895
04                 X    =          916913
97
 Y    =       17247000
50  feet           Y    =         5267578
00  meter
 Z    =       13286820
80                 Z    =         4054468
54
 XDOT =     -21052
553814                 XDOT =       -6415
173221
 YDOT =      -5876
891407  feet/sec       YDOT =       -1863
024260  meter/sec
 ZDOT =      12738
871297                 ZDOT =        3851
638717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17030665
05                 X    =        -5190946
71
 Y    =        4194066
74  feet           Y    =         1278351
54  meter
 Z    =       13305298
03                 Z    =         4055454
84
 XDOT =       4933
214687                 XDOT =        1503
643836
 YDOT =     -20193
217458  feet/sec       YDOT =       -6154
892681  meter/sec
 ZDOT =      12615
467030                 ZDOT =        3845
194351


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   09359
55450457  
00016717  00000-0  10270-3 0  9097
2 25544  51
6437  43
0911 0007627 114
7527 245
4432 15
76885817 36116


Satellite: ISS
Catalog Number: 25544
Epoch time:      09359
55450457   =   yrday
fracday
Element set:     909
Inclination:       51
6437  deg
RA of node:        43
0911  deg
Eccentricity:     
0007627     
Arg of perigee:   114
7527  deg
Mean anomaly:     245
4432  deg
Mean motion:   15
76885817  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3611
Checksum:              327


Coasting Arc #11 (Orbit 3625)
---------------------------------------

Vector Time (GMT): 2009/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5885654
60                 A    =         6721001
23  meter
 Y    =        1977172
20  meter          E    =           
0010807
 Z    =       -2582888
57                 I    =           51
86089
 XDOT =        437
517212                 Wp   =           91
34155
 YDOT =       5577
967402  meter/sec      RA   =           37
63398  deg
 ZDOT =       5285
502067                 TA   =          239
42656
                                          MA   =          239
53323
                                          Ha   =            188
276  n
mi
                                          Hp   =            176
780

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19309890
41                 X    =         5875655
39
 Y    =        6486785
45  feet           Y    =         2042933
40  meter
 Z    =       -8474043
85                 Z    =        -2554319
90
 XDOT =       1435
423925                 XDOT =         349
434638
 YDOT =      18300
417986  feet/sec       YDOT =        5582
367000  meter/sec
 ZDOT =      17340
886048                 ZDOT =        5287
414100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5000231
83                 X    =        -1524070
66
 Y    =       19795255
58  feet           Y    =         6033593
90  meter
 Z    =       -8360933
59                 Z    =        -2548412
56
 XDOT =     -16703
569497                 XDOT =       -5091
247983
 YDOT =       3082
032260  feet/sec       YDOT =         939
403433  meter/sec
 ZDOT =      17348
541242                 ZDOT =        5287
835370


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   09360
50509831  
00016717  00000-0  10270-3 0  9107
2 25544  51
6444  38
1888 0007667 117
9066 242
2876 15
76933569 36260


Satellite: ISS
Catalog Number: 25544
Epoch time:      09360
50509831   =   yrday
fracday
Element set:     910
Inclination:       51
6444  deg
RA of node:        38
1888  deg
Eccentricity:     
0007667     
Arg of perigee:   117
9066  deg
Mean anomaly:     242
2876  deg
Mean motion:   15
76933569  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3626
Checksum:              341


Coasting Arc #12 (Orbit 3641)
---------------------------------------

Vector Time (GMT): 2009/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         344328
09                 A    =         6712926
99  meter
 Y    =       -4463096
47  meter          E    =           
0019385
 Z    =       -5018932
08                 I    =           51
80972
 XDOT =       6960
198893                 Wp   =           91
90820
 YDOT =       2665
997957  meter/sec      RA   =           32
52754  deg
 ZDOT =      -1900
141931                 TA   =          159
81089
                                          MA   =          159
73413
                                          Ha   =            188
220  n
mi
                                          Hp   =            176
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1129685
32                 X    =          418590
93
 Y    =      -14642704
95  feet           Y    =        -4458830
20  meter
 Z    =      -16466312
61                 Z    =        -5017079
44
 XDOT =      22835
298204                 XDOT =        6939
100573
 YDOT =       8746
712457  feet/sec       YDOT =        2743
713259  meter/sec
 ZDOT =      -6234
061454                 ZDOT =       -1866
379887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14693695
26                 X    =         4478638
31
 Y    =        -140299
10  feet           Y    =          -42763
16  meter
 Z    =      -16459042
62                 Z    =        -5016716
19
 XDOT =      -6592
941644                 XDOT =       -2009
528613
 YDOT =      22513
949382  feet/sec       YDOT =        6862
251772  meter/sec
 ZDOT =      -6100
387526                 ZDOT =       -1859
398118


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   09361
51904706  
00016717  00000-0  10270-3 0  9110
2 25544  51
6451  32
9592 0007600 121
5026 238
6882 15
76921848 36427


Satellite: ISS
Catalog Number: 25544
Epoch time:      09361
51904706   =   yrday
fracday
Element set:     911
Inclination:       51
6451  deg
RA of node:        32
9592  deg
Eccentricity:     
0007600     
Arg of perigee:   121
5026  deg
Mean anomaly:     238
6882  deg
Mean motion:   15
76921848  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3642
Checksum:              311


Coasting Arc #13 (Orbit 3657)
---------------------------------------

Vector Time (GMT): 2009/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6158044
12                 A    =         6723572
12  meter
 Y    =       -2587679
75  meter          E    =           
0020980
 Z    =         676418
98                 I    =           51
81909
 XDOT =       1284
043212                 Wp   =          126
38618
 YDOT =      -4656
999261  meter/sec      RA   =           27
36021  deg
 ZDOT =      -6010
007802                 TA   =           46
24990
                                          MA   =           46
07642
                                          Ha   =            188
141  n
mi
                                          Hp   =            176
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20203556
83                 X    =        -6131936
50
 Y    =       -8489762
95  feet           Y    =        -2656396
75  meter
 Z    =        2219222
37                 Z    =          646565
98
 XDOT =       4212
740196                 XDOT =        1365
218953
 YDOT =     -15278
868966  feet/sec       YDOT =       -4642
185623  meter/sec
 ZDOT =     -19717
873366                 ZDOT =       -6003
573329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6212998
14                 X    =         1893721
83
 Y    =      -21027816
95  feet           Y    =        -6409278
61  meter
 Z    =        2101023
56                 Z    =          640391
98
 XDOT =      14129
553149                 XDOT =        4306
687800
 YDOT =       2167
094409  feet/sec       YDOT =         660
530376  meter/sec
 ZDOT =     -19692
463008                 ZDOT =       -6002
262725


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   09362
53297736  
00016717  00000-0  10270-3 0  9122
2 25544  51
6444  27
7297 0007644 124
2246 235
9644 15
76967737 36585


Satellite: ISS
Catalog Number: 25544
Epoch time:      09362
53297736   =   yrday
fracday
Element set:     912
Inclination:       51
6444  deg
RA of node:        27
7297  deg
Eccentricity:     
0007644     
Arg of perigee:   124
2246  deg
Mean anomaly:     235
9644  deg
Mean motion:   15
76967737  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3658
Checksum:              351


Coasting Arc #14 (Orbit 3673)
---------------------------------------

Vector Time (GMT): 2009/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1931614
21                 A    =         6711598
33  meter
 Y    =        3687615
01  meter          E    =           
0009354
 Z    =        5257086
69                 I    =           51
75098
 XDOT =      -7021
526639                 Wp   =          113
78470
 YDOT =      -3172
409298  meter/sec      RA   =           22
21596  deg
 ZDOT =       -357
825518                 TA   =          339
58319
                                          MA   =          339
62056
                                          Ha   =            188
109  n
mi
                                          Hp   =            176
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6337316
97                 X    =        -1998244
31
 Y    =       12098474
43  feet           Y    =         3665641
16  meter
 Z    =       17247659
75                 Z    =         5247541
61
 XDOT =     -23036
504721                 XDOT =       -6983
792082
 YDOT =     -10408
166989  feet/sec       YDOT =       -3250
717112  meter/sec
 ZDOT =      -1173
968235                 ZDOT =        -391
845135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12819327
52                 X    =        -3907331
03
 Y    =       -4847678
20  feet           Y    =        -1477572
31  meter
 Z    =       17209918
50                 Z    =         5245583
16
 XDOT =       7042
127427                 XDOT =        2146
440440
 YDOT =     -23230
894540  feet/sec       YDOT =       -7080
776656  meter/sec
 ZDOT =      -1308
668471                 ZDOT =        -398
882150


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   09363
54688969  
00016717  00000-0  10270-3 0  9137
2 25544  51
6437  22
5003 0007636 127
5710 232
6149 15
77000064 36742


Satellite: ISS
Catalog Number: 25544
Epoch time:      09363
54688969   =   yrday
fracday
Element set:     913
Inclination:       51
6437  deg
RA of node:        22
5003  deg
Eccentricity:     
0007636     
Arg of perigee:   127
5710  deg
Mean anomaly:     232
6149  deg
Mean motion:   15
77000064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3674
Checksum:              313


Coasting Arc #15 (Orbit 3689)
---------------------------------------

Vector Time (GMT): 2009/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 736597
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5922744
55                 A    =         6722819
10  meter
 Y    =        2892403
22  meter          E    =           
0017933
 Z    =        1300744
95                 I    =           51
76088
 XDOT =      -3184
501247                 Wp   =           82
84016
 YDOT =       3854
529436  meter/sec      RA   =           17
08230  deg
 ZDOT =       5862
621644                 TA   =          291
43033
                                          MA   =          291
62152
                                          Ha   =            187
938  n
mi
                                          Hp   =            176
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19431576
60                 X    =         5883642
22
 Y    =        9489511
87  feet           Y    =         2958415
98  meter
 Z    =        4267535
92                 Z    =         1329423
15
 XDOT =     -10447
838736                 XDOT =       -3255
846115
 YDOT =      12646
093951  feet/sec       YDOT =        3818
518518  meter/sec
 ZDOT =      19234
322978                 ZDOT =        5846
978733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6592272
66                 X    =        -2009324
71
 Y    =       20571748
36  feet           Y    =         6270268
90  meter
 Z    =        4381093
27                 Z    =         1335357
23
 XDOT =     -12537
017095                 XDOT =       -3821
282811
 YDOT =      -8145
794539  feet/sec       YDOT =       -2482
838175  meter/sec
 ZDOT =      19172
439260                 ZDOT =        5843
759487


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   09364
56078431  
00016717  00000-0  10270-3 0  9148
2 25544  51
6439  17
2710 0007549 131
1784 229
0033 15
77021489 36909


Satellite: ISS
Catalog Number: 25544
Epoch time:      09364
56078431   =   yrday
fracday
Element set:     914
Inclination:       51
6439  deg
RA of node:        17
2710  deg
Eccentricity:     
0007549     
Arg of perigee:   131
1784  deg
Mean anomaly:     229
0033  deg
Mean motion:   15
77021489  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3690
Checksum:              311

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics 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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