Date: December 9th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 3335)
---------------------------------------

Vector Time (GMT): 2009/342/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5115937
44                 A    =         6724738
73  meter
 Y    =       -4178798
01  meter          E    =           
0012120
 Z    =       -1259794
31                 I    =           51
90861
 XDOT =       2196
632121                 Wp   =          103
62804
 YDOT =       4448
962849  meter/sec      RA   =          132
15988  deg
 ZDOT =      -5886
860591                 TA   =           90
14232
                                          MA   =           90
00344
                                          Ha   =            189
040  n
mi
                                          Hp   =            177
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16784571
66                 X    =         5168405
14
 Y    =      -13709967
21  feet           Y    =        -4121295
12  meter
 Z    =       -4133183
42                 Z    =        -1234813
84
 XDOT =       7206
798296                 XDOT =        2175
317201
 YDOT =      14596
334805  feet/sec       YDOT =        4473
408144  meter/sec
 ZDOT =     -19313
847084                 ZDOT =       -5876
240752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18679927
41                 X    =        -5693641
87
 Y    =      -11025014
93  feet           Y    =        -3360424
55  meter
 Z    =       -4034551
99                 Z    =        -1229731
45
 XDOT =      10356
760774                 XDOT =        3156
740684
 YDOT =     -10556
570771  feet/sec       YDOT =       -3217
642771  meter/sec
 ZDOT =     -19271
684351                 ZDOT =       -5874
009390


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   09342
12393879  
00016717  00000-0  10270-3 0  9007
2 25544  51
6431 132
9429 0007665  54
2272 305
9604 15
76382488 33362


Satellite: ISS
Catalog Number: 25544
Epoch time:      09342
12393879   =   yrday
fracday
Element set:     900
Inclination:       51
6431  deg
RA of node:       132
9429  deg
Eccentricity:     
0007665     
Arg of perigee:    54
2272  deg
Mean anomaly:     305
9604  deg
Mean motion:   15
76382488  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3336
Checksum:              323


Coasting Arc #2 (Orbit 3351)
---------------------------------------

Vector Time (GMT): 2009/343/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1504683
62                 A    =         6714990
36  meter
 Y    =       -4356832
21  meter          E    =           
0014346
 Z    =        4875444
49                 I    =           51
89527
 XDOT =       5741
092221                 Wp   =           57
98305
 YDOT =      -4594
477282  meter/sec      RA   =          126
99523  deg
 ZDOT =      -2321
512373                 TA   =           54
57910
                                          MA   =           54
44522
                                          Ha   =            189
087  n
mi
                                          Hp   =            177
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4936626
05                 X    =        -1479537
14
 Y    =      -14294068
93  feet           Y    =        -4373518
18  meter
 Z    =       15995552
78                 Z    =         4868195
48
 XDOT =      18835
604399                 XDOT =        5803
319353
 YDOT =     -15073
744362  feet/sec       YDOT =       -4529
928920  meter/sec
 ZDOT =      -7616
510410                 ZDOT =       -2293
471068

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11501576
23                 X    =        -3505680
43
 Y    =        9865385
41  feet           Y    =         3006969
47  meter
 Z    =       15966725
00                 Z    =         4866657
78
 XDOT =     -20168
872765                 XDOT =       -6147
472419
 YDOT =     -11300
176640  feet/sec       YDOT =       -3444
293840  meter/sec
 ZDOT =      -7505
779575                 ZDOT =       -2287
761614


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   09343
13822837  
00016717  00000-0  10270-3 0  9011
2 25544  51
6430 127
7165 0007693  57
7443 302
4466 15
76402611 33526


Satellite: ISS
Catalog Number: 25544
Epoch time:      09343
13822837   =   yrday
fracday
Element set:     901
Inclination:       51
6430  deg
RA of node:       127
7165  deg
Eccentricity:     
0007693     
Arg of perigee:    57
7443  deg
Mean anomaly:     302
4466  deg
Mean motion:   15
76402611  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3352
Checksum:              301


Coasting Arc #3 (Orbit 3367)
---------------------------------------

Vector Time (GMT): 2009/344/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4853591
30                 A    =         6722109
39  meter
 Y    =        3740620
70  meter          E    =           
0021141
 Z    =        2737488
73                 I    =           51
93634
 XDOT =      -1333
560865                 Wp   =           72
63002
 YDOT =      -5547
550253  meter/sec      RA   =          121
90211  deg
 ZDOT =       5189
583796                 TA   =          318
57233
                                          MA   =          318
73244
                                          Ha   =            189
134  n
mi
                                          Hp   =            177
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15923855
99                 X    =        -4908357
24
 Y    =       12272377
64  feet           Y    =         3686038
59  meter
 Z    =        8981262
22                 Z    =         2713776
91
 XDOT =      -4375
199689                 XDOT =       -1296
638438
 YDOT =     -18200
624189  feet/sec       YDOT =       -5562
256817  meter/sec
 ZDOT =      17026
193558                 ZDOT =        5183
194597

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17402631
39                 X    =         5304322
05
 Y    =       10149003
40  feet           Y    =         3093416
24  meter
 Z    =        8887612
97                 Z    =         2708944
43
 XDOT =     -14416
567559                 XDOT =       -4394
169792
 YDOT =       9755
849377  feet/sec       YDOT =        2973
582890  meter/sec
 ZDOT =      17000
727707                 ZDOT =        5181
821805


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   09344
15250409  
00016717  00000-0  10270-3 0  9025
2 25544  51
6429 122
4891 0007725  61
1461 299
0478 15
76417079 33682


Satellite: ISS
Catalog Number: 25544
Epoch time:      09344
15250409   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:       122
4891  deg
Eccentricity:     
0007725     
Arg of perigee:    61
1461  deg
Mean anomaly:     299
0478  deg
Mean motion:   15
76417079  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3368
Checksum:              321


Coasting Arc #4 (Orbit 3382)
---------------------------------------

Vector Time (GMT): 2009/345/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         878314
62                 A    =         6718099
15  meter
 Y    =        5299802
17  meter          E    =           
0013962
 Z    =       -4045267
41                 I    =           51
93857
 XDOT =      -5378
419539                 Wp   =           86
21684
 YDOT =       3869
067337  meter/sec      RA   =          116
72029  deg
 ZDOT =       3913
598891                 TA   =          223
96448
                                          MA   =          224
07563
                                          Ha   =            189
048  n
mi
                                          Hp   =            177
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2881609
66                 X    =          838637
52
 Y    =       17387802
41  feet           Y    =         5309402
48  meter
 Z    =      -13271874
71                 Z    =        -4041096
45
 XDOT =     -17645
733395                 XDOT =       -5440
296243
 YDOT =      12693
790475  feet/sec       YDOT =        3808
576395  meter/sec
 ZDOT =      12839
891374                 ZDOT =        3887
320118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14814916
35                 X    =         4515586
50
 Y    =       -9570787
45  feet           Y    =        -2917176
01  meter
 Z    =      -13255198
46                 Z    =        -4040184
49
 XDOT =      17951
462908                 XDOT =        5471
605894
 YDOT =      10205
069318  feet/sec       YDOT =        3110
505128  meter/sec
 ZDOT =      12736
082175                 ZDOT =        3881
957847


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   09345
10337437  
00016717  00000-0  10270-3 0  9039
2 25544  51
6433 117
5883 0007730  64
4255 295
7708 15
76450912 33835


Satellite: ISS
Catalog Number: 25544
Epoch time:      09345
10337437   =   yrday
fracday
Element set:     903
Inclination:       51
6433  deg
RA of node:       117
5883  deg
Eccentricity:     
0007730     
Arg of perigee:    64
4255  deg
Mean anomaly:     295
7708  deg
Mean motion:   15
76450912  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3383
Checksum:              318


Coasting Arc #5 (Orbit 3398)
---------------------------------------

Vector Time (GMT): 2009/346/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4541255
68                 A    =         6718166
20  meter
 Y    =       -2904229
93  meter          E    =           
0014910
 Z    =       -4025229
11                 I    =           51
95217
 XDOT =        712
751505                 Wp   =           69
77446
 YDOT =       6567
194991  meter/sec      RA   =          111
63885  deg
 ZDOT =      -3940
819386                 TA   =          159
66984
                                          MA   =          159
61042
                                          Ha   =            189
043  n
mi
                                          Hp   =            177
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14899132
81                 X    =         4592947
95
 Y    =       -9528313
41  feet           Y    =        -2853157
50  meter
 Z    =      -13206132
27                 Z    =        -4003042
02
 XDOT =       2338
423572                 XDOT =         658
407133
 YDOT =      21545
915324  feet/sec       YDOT =        6574
861930  meter/sec
 ZDOT =     -12929
197461                 ZDOT =       -3937
488139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14828667
31                 X    =        -4519777
80
 Y    =       -9756607
60  feet           Y    =        -2973814
00  meter
 Z    =      -13118463
26                 Z    =        -3998507
60
 XDOT =      17953
022222                 XDOT =        5472
081173
 YDOT =      -9949
435664  feet/sec       YDOT =       -3032
587990  meter/sec
 ZDOT =     -12915
811258                 ZDOT =       -3936
739272


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   09346
11762281  
00016717  00000-0  10270-3 0  9041
2 25544  51
6440 112
3607 0007784  67
7782 292
4207 15
76481802 33997


Satellite: ISS
Catalog Number: 25544
Epoch time:      09346
11762281   =   yrday
fracday
Element set:     904
Inclination:       51
6440  deg
RA of node:       112
3607  deg
Eccentricity:     
0007784     
Arg of perigee:    67
7782  deg
Mean anomaly:     292
4207  deg
Mean motion:   15
76481802  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3399
Checksum:              322


Coasting Arc #6 (Orbit 3414)
---------------------------------------

Vector Time (GMT): 2009/347/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -437870
92                 A    =         6721850
95  meter
 Y    =       -6109648
37  meter          E    =           
0020754
 Z    =        2750513
06                 I    =           51
97432
 XDOT =       5024
941286                 Wp   =           90
23958
 YDOT =      -2707
716564  meter/sec      RA   =          106
45853  deg
 ZDOT =      -5181
395440                 TA   =           58
42696
                                          MA   =           58
22451
                                          Ha   =            189
079  n
mi
                                          Hp   =            177
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1436584
40                 X    =         -382880
95
 Y    =      -20044778
13  feet           Y    =        -6114237
77  meter
 Z    =        9023992
98                 Z    =         2748518
69
 XDOT =      16486
027841                 XDOT =        5080
016703
 YDOT =      -8883
584529  feet/sec       YDOT =       -2651
216144  meter/sec
 ZDOT =     -16999
328870                 ZDOT =       -5156
850383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17506880
21                 X    =        -5336097
09
 Y    =        9874799
39  feet           Y    =         3009838
85  meter
 Z    =        9015921
30                 Z    =         2748052
81
 XDOT =     -14375
318220                 XDOT =       -4381
596994
 YDOT =      -9953
919272  feet/sec       YDOT =       -3033
954594  meter/sec
 ZDOT =     -16902
313921                 ZDOT =       -5151
825283


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   09347
13185813  
00016717  00000-0  10270-3 0  9055
2 25544  51
6438 107
1333 0007767  71
7618 288
4391 15
76475396 34155


Satellite: ISS
Catalog Number: 25544
Epoch time:      09347
13185813   =   yrday
fracday
Element set:     905
Inclination:       51
6438  deg
RA of node:       107
1333  deg
Eccentricity:     
0007767     
Arg of perigee:    71
7618  deg
Mean anomaly:     288
4391  deg
Mean motion:   15
76475396  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3415
Checksum:              334


Coasting Arc #7 (Orbit 3430)
---------------------------------------

Vector Time (GMT): 2009/348/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4250117
42                 A    =         6714684
94  meter
 Y    =        1749741
39  meter          E    =           
0013229
 Z    =        4884430
92                 I    =           51
95864
 XDOT =       -364
844155                 Wp   =           96
70167
 YDOT =      -7350
870495  meter/sec      RA   =          101
36863  deg
 ZDOT =       2309
024010                 TA   =          330
92247
                                          MA   =          330
99608
                                          Ha   =            189
145  n
mi
                                          Hp   =            177
171

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13943954
79                 X    =        -4293095
50
 Y    =        5740621
36  feet           Y    =         1701973
09  meter
 Z    =       16025035
82                 Z    =         4863679
37
 XDOT =      -1196
995260                 XDOT =        -293
835312
 YDOT =     -24117
029184  feet/sec       YDOT =       -7354
553687  meter/sec
 ZDOT =       7575
538092                 ZDOT =        2307
423033

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11342049
22                 X    =         3457056
60
 Y    =       10068238
38  feet           Y    =         3068799
06  meter
 Z    =       15942988
35                 Z    =         4859422
85
 XDOT =     -20364
714605                 XDOT =       -6207
165012
 YDOT =      10920
232628  feet/sec       YDOT =        3328
486905  meter/sec
 ZDOT =       7568
999725                 ZDOT =        2307
031116


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   09348
14607837  
00016717  00000-0  10270-3 0  9063
2 25544  51
6445 101
9058 0007734  75
0176 285
1844 15
76517293 34317


Satellite: ISS
Catalog Number: 25544
Epoch time:      09348
14607837   =   yrday
fracday
Element set:     906
Inclination:       51
6445  deg
RA of node:       101
9058  deg
Eccentricity:     
0007734     
Arg of perigee:    75
0176  deg
Mean anomaly:     285
1844  deg
Mean motion:   15
76517293  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3431
Checksum:              324


Coasting Arc #8 (Orbit 3445)
---------------------------------------

Vector Time (GMT): 2009/349/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         233824
09                 A    =         6724312
65  meter
 Y    =        6606182
76  meter          E    =           
0015912
 Z    =       -1211759
26                 I    =           51
99695
 XDOT =      -4781
221857                 Wp   =           55
79634
 YDOT =       1241
884101  meter/sec      RA   =           96
20800  deg
 ZDOT =       5911
260507                 TA   =          290
97578
                                          MA   =          291
14596
                                          Ha   =            188
979  n
mi
                                          Hp   =            177
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         767139
41                 X    =          165821
80
 Y    =       21673827
95  feet           Y    =         6608417
48  meter
 Z    =       -3975588
11                 Z    =        -1210787
49
 XDOT =     -15686
423415                 XDOT =       -4823
469647
 YDOT =       4074
422903  feet/sec       YDOT =        1188
180533  meter/sec
 ZDOT =      19393
899300                 ZDOT =        5887
930615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18925479
41                 X    =         5768486
12
 Y    =      -10592519
54  feet           Y    =        -3228599
96  meter
 Z    =       -3971571
53                 Z    =        -1210535
00
 XDOT =      10062
604414                 XDOT =        3067
081825
 YDOT =      10819
834689  feet/sec       YDOT =        3297
885613  meter/sec
 ZDOT =      19301
626505                 ZDOT =        5883
135759


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   09349
09689829  
00016717  00000-0  10270-3 0  9070
2 25544  51
6454  97
0052 0007699  77
8242 282
3785 15
76539855 34467


Satellite: ISS
Catalog Number: 25544
Epoch time:      09349
09689829   =   yrday
fracday
Element set:     907
Inclination:       51
6454  deg
RA of node:        97
0052  deg
Eccentricity:     
0007699     
Arg of perigee:    77
8242  deg
Mean anomaly:     282
3785  deg
Mean motion:   15
76539855  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3446
Checksum:              371


Coasting Arc #9 (Orbit 3461)
---------------------------------------

Vector Time (GMT): 2009/350/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4144674
66                 A    =         6712842
90  meter
 Y    =        -355805
66  meter          E    =           
0022658
 Z    =       -5287883
15                 I    =           51
96104
 XDOT =        159
566580                 Wp   =           84
89887
 YDOT =       7676
726515  meter/sec      RA   =           91
09214  deg
 ZDOT =       -390
933128                 TA   =          181
39632
                                          MA   =          181
40266
                                          Ha   =            188
929  n
mi
                                          Hp   =            177
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13598013
96                 X    =         4174033
07
 Y    =       -1167341
41  feet           Y    =         -309292
47  meter
 Z    =      -17348698
00                 Z    =        -5267676
90
 XDOT =        523
512400                 XDOT =          75
611316
 YDOT =      25186
110614  feet/sec       YDOT =        7678
041527  meter/sec
 ZDOT =      -1282
589003                 ZDOT =        -390
360647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7489257
78                 X    =        -2282725
77
 Y    =      -11530272
59  feet           Y    =        -3514427
09  meter
 Z    =      -17268752
81                 Z    =        -5263515
86
 XDOT =      21119
373913                 XDOT =        6437
185169
 YDOT =     -11797
749605  feet/sec       YDOT =       -3595
954080  meter/sec
 ZDOT =      -1280
136145                 ZDOT =        -390
185497


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
11109258  
00016717  00000-0  10270-3 0  9089
2 25544  51
6459  91
7776 0007687  80
9118 279
2917 15
76569347 34629


Satellite: ISS
Catalog Number: 25544
Epoch time:      09350
11109258   =   yrday
fracday
Element set:     908
Inclination:       51
6459  deg
RA of node:        91
7776  deg
Eccentricity:     
0007687     
Arg of perigee:    80
9118  deg
Mean anomaly:     279
2917  deg
Mean motion:   15
76569347  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3462
Checksum:              352


Coasting Arc #10 (Orbit 3477)
---------------------------------------

Vector Time (GMT): 2009/351/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -46299
34                 A    =         6724839
94  meter
 Y    =       -6698395
85  meter          E    =           
0016760
 Z    =        -544414
92                 I    =           52
00083
 XDOT =       4761
608707                 Wp   =          117
67506
 YDOT =        445
925515  meter/sec      RA   =           85
96348  deg
 ZDOT =      -6039
466020                 TA   =           68
22522
                                          MA   =           68
04696
                                          Ha   =            188
975  n
mi
                                          Hp   =            177
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -151900
71                 X    =           31251
42
 Y    =      -21976364
34  feet           Y    =        -6698479
90  meter
 Z    =       -1786138
18                 Z    =         -544452
54
 XDOT =      15622
075812                 XDOT =        4785
607123
 YDOT =       1463
010221  feet/sec       YDOT =         499
307784  meter/sec
 ZDOT =     -19814
521063                 ZDOT =       -6016
275680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19130144
40                 X    =        -5830868
01
 Y    =       10817585
31  feet           Y    =         3297200
00  meter
 Z    =       -1786442
36                 Z    =         -544507
63
 XDOT =      -5591
739225                 XDOT =       -1704
362116
 YDOT =     -13065
530925  feet/sec       YDOT =       -3982
373826  meter/sec
 ZDOT =     -19722
740560                 ZDOT =       -6011
491323


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
12527466  
00016717  00000-0  10270-3 0  9097
2 25544  51
6461  86
5502 0007617  85
7575 274
4459 15
76535181 34788


Satellite: ISS
Catalog Number: 25544
Epoch time:      09351
12527466   =   yrday
fracday
Element set:     909
Inclination:       51
6461  deg
RA of node:        86
5502  deg
Eccentricity:     
0007617     
Arg of perigee:    85
7575  deg
Mean anomaly:     274
4459  deg
Mean motion:   15
76535181  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3478
Checksum:              339


Coasting Arc #11 (Orbit 3493)
---------------------------------------

Vector Time (GMT): 2009/352/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4217581
96                 A    =         6713431
52  meter
 Y    =       -1107159
19  meter          E    =           
0011966
 Z    =        5095478
22                 I    =           51
96007
 XDOT =         44
848423                 Wp   =           74
29261
 YDOT =      -7546
219870  meter/sec      RA   =           80
81398  deg
 ZDOT =      -1596
295229                 TA   =           30
97711
                                          MA   =           30
90659
                                          Ha   =            188
927  n
mi
                                          Hp   =            176
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13837211
15                 X    =        -4229640
94
 Y    =       -3632412
05  feet           Y    =        -1154390
89  meter
 Z    =       16717448
24                 Z    =         5074959
76
 XDOT =        147
140496                 XDOT =         136
982751
 YDOT =     -24757
939206  feet/sec       YDOT =       -7545
202953  meter/sec
 ZDOT =      -5237
189070                 ZDOT =       -1595
854719

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3847201
15                 X    =         1172626
91
 Y    =       13877000
05  feet           Y    =         4229709
62  meter
 Z    =       16636220
08                 Z    =         5070719
88
 XDOT =     -20495
899274                 XDOT =       -6247
150099
 YDOT =      11983
515808  feet/sec       YDOT =        3652
575618  meter/sec
 ZDOT =      -5235
613414                 ZDOT =       -1595
814969


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
13944027  
00016717  00000-0  10270-3 0  9107
2 25544  51
6463  81
3226 0007528  87
5088 272
6938 15
76634256 34949


Satellite: ISS
Catalog Number: 25544
Epoch time:      09352
13944027   =   yrday
fracday
Element set:     910
Inclination:       51
6463  deg
RA of node:        81
3226  deg
Eccentricity:     
0007528     
Arg of perigee:    87
5088  deg
Mean anomaly:     272
6938  deg
Mean motion:   15
76634256  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3494
Checksum:              330


Coasting Arc #12 (Orbit 3509)
---------------------------------------

Vector Time (GMT): 2009/353/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -161777
58                 A    =         6722651
63  meter
 Y    =        6340640
12  meter          E    =           
0021350
 Z    =        2201927
15                 I    =           51
98443
 XDOT =      -4975
541236                 Wp   =           77
84199
 YDOT =      -2057
366235  meter/sec      RA   =           75
71501  deg
 ZDOT =       5518
646332                 TA   =          306
75756
                                          MA   =          306
95338
                                          Ha   =            188
850  n
mi
                                          Hp   =            177
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -530766
34                 X    =         -243364
23
 Y    =       20802625
07  feet           Y    =         6338374
54  meter
 Z    =        7224170
43                 Z    =         2200943
96
 XDOT =     -16323
954187                 XDOT =       -4978
974097
 YDOT =      -6749
889221  feet/sec       YDOT =       -2113
025647  meter/sec
 ZDOT =      18105
795051                 ZDOT =        5494
466608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18110649
66                 X    =         5520126
02
 Y    =      -10251318
43  feet           Y    =        -3124601
86  meter
 Z    =        7220415
52                 Z    =         2200782
65
 XDOT =       1956
411348                 XDOT =         596
314179
 YDOT =      16234
379183  feet/sec       YDOT =        4948
238775  meter/sec
 ZDOT =      18010
050748                 ZDOT =        5489
463468


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
15359601  
00016717  00000-0  10270-3 0  9119
2 25544  51
6458  76
0946 0007560  90
6590 269
5441 15
76610831 35108


Satellite: ISS
Catalog Number: 25544
Epoch time:      09353
15359601   =   yrday
fracday
Element set:     911
Inclination:       51
6458  deg
RA of node:        76
0946  deg
Eccentricity:     
0007560     
Arg of perigee:    90
6590  deg
Mean anomaly:     269
5441  deg
Mean motion:   15
76610831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3510
Checksum:              311


Coasting Arc #13 (Orbit 3524)
---------------------------------------

Vector Time (GMT): 2009/354/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4491722
55                 A    =         6716441
85  meter
 Y    =        2436252
87  meter          E    =           
0016320
 Z    =       -4374593
63                 I    =           51
95461
 XDOT =       -407
388522                 Wp   =          103
16071
 YDOT =       6878
200342  meter/sec      RA   =           70
53844  deg
 ZDOT =       3419
220465                 TA   =          201
16957
                                          MA   =          201
23719
                                          Ha   =            188
764  n
mi
                                          Hp   =            177
108

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14736622
52                 X    =         4485396
97
 Y    =        7992955
60  feet           Y    =         2486447
14  meter
 Z    =      -14352341
31                 Z    =        -4352788
02
 XDOT =      -1336
576517                 XDOT =        -500
881354
 YDOT =      22566
274089  feet/sec       YDOT =        6873
121510  meter/sec
 ZDOT =      11217
914913                 ZDOT =        3417
015149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1097544
90                 X    =         -334531
69
 Y    =      -16802447
25  feet           Y    =        -5121385
92  meter
 Z    =      -14265982
10                 Z    =        -4348271
34
 XDOT =      18641
222021                 XDOT =        5681
844472
 YDOT =     -10715
280967  feet/sec       YDOT =       -3266
017639  meter/sec
 ZDOT =      11209
330313                 ZDOT =        3416
603879


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
10435337  
00016717  00000-0  10270-3 0  9127
2 25544  51
6453  71
1930 0007478  94
3650 265
8369 15
76641642 35256


Satellite: ISS
Catalog Number: 25544
Epoch time:      09354
10435337   =   yrday
fracday
Element set:     912
Inclination:       51
6453  deg
RA of node:        71
1930  deg
Eccentricity:     
0007478     
Arg of perigee:    94
3650  deg
Mean anomaly:     265
8369  deg
Mean motion:   15
76641642  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3525
Checksum:              317


Coasting Arc #14 (Orbit 3540)
---------------------------------------

Vector Time (GMT): 2009/355/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         630726
77                 A    =         6718736
12  meter
 Y    =       -5582658
66  meter          E    =           
0013012
 Z    =       -3696015
72                 I    =           51
95045
 XDOT =       5321
515280                 Wp   =           89
27461
 YDOT =       3468
514522  meter/sec      RA   =           65
45519  deg
 ZDOT =      -4343
807675                 TA   =          134
98616
                                          MA   =          134
88062
                                          Ha   =            188
728  n
mi
                                          Hp   =            177
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2069313
56                 X    =          711060
64
 Y    =      -18315809
26  feet           Y    =        -5575155
93  meter
 Z    =      -12126035
83                 Z    =        -3692757
14
 XDOT =      17459
039631                 XDOT =        5303
435553
 YDOT =      11379
640819  feet/sec       YDOT =        3527
922226  meter/sec
 ZDOT =     -14251
337515                 ZDOT =       -4317
999429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16518199
88                 X    =        -5034747
32
 Y    =        8198162
52  feet           Y    =         2498799
94  meter
 Z    =      -12113252
09                 Z    =        -3692119
24
 XDOT =        564
967106                 XDOT =         172
201974
 YDOT =     -19705
195510  feet/sec       YDOT =       -6006
143592  meter/sec
 ZDOT =     -14149
112041                 ZDOT =       -4312
649350


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
11848249  
00016717  00000-0  10270-3 0  9130
2 25544  51
6444  65
9648 0007403  98
3374 261
8630 15
76638921 35419


Satellite: ISS
Catalog Number: 25544
Epoch time:      09355
11848249   =   yrday
fracday
Element set:     913
Inclination:       51
6444  deg
RA of node:        65
9648  deg
Eccentricity:     
0007403     
Arg of perigee:    98
3374  deg
Mean anomaly:     261
8630  deg
Mean motion:   15
76638921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3541
Checksum:              333


Coasting Arc #15 (Orbit 3556)
---------------------------------------

Vector Time (GMT): 2009/356/02:16:09
706
Vector Time (MET): N/A
Weight (LBS)     : 743802
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4802874
03                 A    =         6720340
90  meter
 Y    =       -3514763
20  meter          E    =           
0020512
 Z    =        3100926
62                 I    =           51
94318
 XDOT =       1090
107229                 Wp   =           96
89920
 YDOT =      -5845
117354  meter/sec      RA   =           60
27003  deg
 ZDOT =      -4911
695828                 TA   =           47
16846
                                          MA   =           46
99626
                                          Ha   =            188
669  n
mi
                                          Hp   =            176
980

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15757460
73                 X    =        -4778278
05
 Y    =      -11531375
32  feet           Y    =        -3568334
53  meter
 Z    =       10173643
75                 Z    =         3077653
76
 XDOT =       3576
467288                 XDOT =        1179
247373
 YDOT =     -19176
894205  feet/sec       YDOT =       -5832
428272  meter/sec
 ZDOT =     -16114
487626                 ZDOT =       -4906
184123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -699292
19                 X    =         -213144
26
 Y    =       19561403
43  feet           Y    =         5962315
77  meter
 Z    =       10081453
20                 Z    =         3072826
94
 XDOT =     -16518
725852                 XDOT =       -5034
907640
 YDOT =       7746
076803  feet/sec       YDOT =        2361
004210  meter/sec
 ZDOT =     -16092
787502                 ZDOT =       -4905
081630


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
13259763  
00016717  00000-0  10270-3 0  9141
2 25544  51
6449  60
7362 0007381 100
5742 259
6255 15
76714765 35576


Satellite: ISS
Catalog Number: 25544
Epoch time:      09356
13259763   =   yrday
fracday
Element set:     914
Inclination:       51
6449  deg
RA of node:        60
7362  deg
Eccentricity:     
0007381     
Arg of perigee:   100
5742  deg
Mean anomaly:     259
6255  deg
Mean motion:   15
76714765  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3557
Checksum:              331

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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