Date: September 26th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2144)
---------------------------------------

Vector Time (GMT): 2009/266/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1671985
12                 A    =         6721516
39  meter
 Y    =       -4497806
04  meter          E    =           
0014204
 Z    =        4694184
75                 I    =           51
73623
 XDOT =       7200
992341                 Wp   =           93
51142
 YDOT =       -199
770955  meter/sec      RA   =          160
88747  deg
 ZDOT =      -2750
032802                 TA   =           23
53632
                                          MA   =           23
47139
                                          Ha   =            192
510  n
mi
                                          Hp   =            180
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5485515
49                 X    =         1699352
28
 Y    =      -14756581
49  feet           Y    =        -4478955
76  meter
 Z    =       15400868
59                 Z    =         4702373
97
 XDOT =      23625
302956                 XDOT =        7216
050367
 YDOT =       -655
416519  feet/sec       YDOT =        -119
161108  meter/sec
 ZDOT =      -9022
417330                 ZDOT =       -2715
013310

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1212403
13                 X    =         -369540
47
 Y    =       15664988
88  feet           Y    =         4774688
61  meter
 Z    =       15432839
42                 Z    =         4703929
46
 XDOT =     -21479
461256                 XDOT =       -6546
939791
 YDOT =       7110
534187  feet/sec       YDOT =        2167
290820  meter/sec
 ZDOT =      -8884
469813                 ZDOT =       -2707
986399


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   09266
58162077  
00020000  00000-0  20000-3 0  9008
2 25544  51
6405 161
7028 0008594 121
0139 239
1870 15
74352076 21453


Satellite: ISS
Catalog Number: 25544
Epoch time:      09266
58162077   =   yrday
fracday
Element set:     900
Inclination:       51
6405  deg
RA of node:       161
7028  deg
Eccentricity:     
0008594     
Arg of perigee:   121
0139  deg
Mean anomaly:     239
1870  deg
Mean motion:   15
74352076  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2145
Checksum:              283


Coasting Arc #2 (Orbit 2160)
---------------------------------------

Vector Time (GMT): 2009/267/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6210886
39                 A    =         6728651
21  meter
 Y    =         639689
60  meter          E    =           
0020541
 Z    =        2492736
30                 I    =           51
78723
 XDOT =       1606
874735                 Wp   =           93
89994
 YDOT =      -5323
447032  meter/sec      RA   =          155
80021  deg
 ZDOT =       5330
915349                 TA   =          294
25771
                                          MA   =          294
47217
                                          Ha   =            192
591  n
mi
                                          Hp   =            180
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20376923
87                 X    =        -6229687
30
 Y    =        2098719
17  feet           Y    =          570130
74  meter
 Z    =        8178268
68                 Z    =         2462517
79
 XDOT =       5271
898737                 XDOT =        1640
386096
 YDOT =     -17465
377402  feet/sec       YDOT =       -5305
290547  meter/sec
 ZDOT =      17489
879754                 ZDOT =        5338
803129

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18967291
21                 X    =         5781230
36
 Y    =       -7861175
84  feet           Y    =        -2396086
39  meter
 Z    =        8059249
69                 Z    =         2456459
31
 XDOT =       -523
781801                 XDOT =        -159
648693
 YDOT =      16830
990902  feet/sec       YDOT =        5130
086027  meter/sec
 ZDOT =      17520
617994                 ZDOT =        5340
284365


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   09267
59724921  
00020000  00000-0  20000-3 0  9013
2 25544  51
6402 156
4841 0008596 124
6616 235
5358 15
74320689 21619


Satellite: ISS
Catalog Number: 25544
Epoch time:      09267
59724921   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:       156
4841  deg
Eccentricity:     
0008596     
Arg of perigee:   124
6616  deg
Mean anomaly:     235
5358  deg
Mean motion:   15
74320689  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2161
Checksum:              304


Coasting Arc #3 (Orbit 2175)
---------------------------------------

Vector Time (GMT): 2009/268/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1139870
96                 A    =         6721976
60  meter
 Y    =        4790870
82  meter          E    =           
0018711
 Z    =       -4593740
23                 I    =           51
79192
 XDOT =      -6972
013469                 Wp   =          118
85400
 YDOT =       1215
758155  meter/sec      RA   =          150
62844  deg
 ZDOT =       2998
270439                 TA   =          180
90910
                                          MA   =          180
91251
                                          Ha   =            192
386  n
mi
                                          Hp   =            180
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3739734
13                 X    =        -1171042
85
 Y    =       15718080
12  feet           Y    =         4777949
76  meter
 Z    =      -15071326
21                 Z    =        -4599353
55
 XDOT =     -22874
059938                 XDOT =       -6999
655282
 YDOT =       3988
707856  feet/sec       YDOT =        1137
638485  meter/sec
 ZDOT =       9836
845273                 ZDOT =        2964
332968

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1280298
61                 X    =         -390235
02
 Y    =      -16085595
74  feet           Y    =        -4902889
58  meter
 Z    =      -15093143
24                 Z    =        -4600390
06
 XDOT =      19472
870924                 XDOT =        5935
331058
 YDOT =     -10653
396029  feet/sec       YDOT =       -3247
155110  meter/sec
 ZDOT =       9703
194465                 ZDOT =        2957
533673


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   09268
54938491  
00020000  00000-0  20000-3 0  9029
2 25544  51
6399 151
5914 0008495 129
0630 231
1291 15
74361360 21769


Satellite: ISS
Catalog Number: 25544
Epoch time:      09268
54938491   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       151
5914  deg
Eccentricity:     
0008495     
Arg of perigee:   129
0630  deg
Mean anomaly:     231
1291  deg
Mean motion:   15
74361360  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2176
Checksum:              300


Coasting Arc #4 (Orbit 2191)
---------------------------------------

Vector Time (GMT): 2009/269/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5958471
80                 A    =         6727937
46  meter
 Y    =       -1456646
52  meter          E    =           
0013208
 Z    =       -2760795
46                 I    =           51
83692
 XDOT =      -1009
574271                 Wp   =          130
02419
 YDOT =       5617
053758  meter/sec      RA   =          145
54796  deg
 ZDOT =      -5167
064385                 TA   =           81
44266
                                          MA   =           81
29301
                                          Ha   =            192
389  n
mi
                                          Hp   =            180
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19548792
00                 X    =         5987728
94
 Y    =       -4779024
02  feet           Y    =        -1389851
85  meter
 Z    =       -9057727
90                 Z    =        -2731777
97
 XDOT =      -3312
251546                 XDOT =       -1047
209311
 YDOT =      18428
654063  feet/sec       YDOT =        5605
553584  meter/sec
 ZDOT =     -16952
310975                 ZDOT =       -5172
060438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17050116
32                 X    =        -5196875
46
 Y    =       10786321
32  feet           Y    =         3287670
74  meter
 Z    =       -8943465
76                 Z    =        -2725968
36
 XDOT =      -2051
033668                 XDOT =        -625
155062
 YDOT =     -17246
639879  feet/sec       YDOT =       -5256
775835  meter/sec
 ZDOT =     -16971
648800                 ZDOT =       -5172
958554


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   09269
56498277  
00020000  00000-0  20000-3 0  9036
2 25544  51
6396 146
3730 0008452 133
8493 226
3370 15
74352459 21928


Satellite: ISS
Catalog Number: 25544
Epoch time:      09269
56498277   =   yrday
fracday
Element set:     903
Inclination:       51
6396  deg
RA of node:       146
3730  deg
Eccentricity:     
0008452     
Arg of perigee:   133
8493  deg
Mean anomaly:     226
3370  deg
Mean motion:   15
74352459  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2192
Checksum:              316


Coasting Arc #5 (Orbit 2207)
---------------------------------------

Vector Time (GMT): 2009/270/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         590872
62                 A    =         6722344
67  meter
 Y    =       -5008826
50  meter          E    =           
0014392
 Z    =        4430773
83                 I    =           51
84337
 XDOT =       6636
789136                 Wp   =          101
09083
 YDOT =      -2135
749901  meter/sec      RA   =          140
37670  deg
 ZDOT =      -3293
199171                 TA   =           21
83876
                                          MA   =           21
77747
                                          Ha   =            192
101  n
mi
                                          Hp   =            180
766

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1938558
47                 X    =          625314
31
 Y    =      -16433157
80  feet           Y    =        -5002026
31  meter
 Z    =       14536659
55                 Z    =         4433728
10
 XDOT =      21774
242571                 XDOT =        6676
176010
 YDOT =      -7007
053482  feet/sec       YDOT =       -2061
313288  meter/sec
 ZDOT =     -10804
459221                 ZDOT =       -3260
861827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3766578
84                 X    =         1148053
23
 Y    =       16102483
18  feet           Y    =         4908036
87  meter
 Z    =       14547992
11                 Z    =         4434227
99
 XDOT =     -17046
426253                 XDOT =       -5195
750722
 YDOT =      13652
280143  feet/sec       YDOT =        4161
214988  meter/sec
 ZDOT =     -10677
142879                 ZDOT =       -3254
393149


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   09270
58056371  
00020000  00000-0  20000-3 0  9046
2 25544  51
6399 141
1540 0008279 137
1268 223
0542 15
74439937 22087


Satellite: ISS
Catalog Number: 25544
Epoch time:      09270
58056371   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       141
1540  deg
Eccentricity:     
0008279     
Arg of perigee:   137
1268  deg
Mean anomaly:     223
0542  deg
Mean motion:   15
74439937  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2208
Checksum:              295


Coasting Arc #6 (Orbit 2223)
---------------------------------------

Vector Time (GMT): 2009/271/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5592249
31                 A    =         6727164
84  meter
 Y    =        2237199
14  meter          E    =           
0019011
 Z    =        2986387
28                 I    =           51
88047
 XDOT =        342
571873                 Wp   =          104
80058
 YDOT =      -5853
107729  meter/sec      RA   =          135
30091  deg
 ZDOT =       4995
206337                 TA   =          289
57652
                                          MA   =          289
78167
                                          Ha   =            192
085  n
mi
                                          Hp   =            180
958

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18347274
63                 X    =        -5631357
78
 Y    =        7339892
19  feet           Y    =         2174444
78  meter
 Z    =        9797858
52                 Z    =         2959124
99
 XDOT =       1123
923467                 XDOT =         383
731019
 YDOT =     -19203
109347  feet/sec       YDOT =       -5849
046540  meter/sec
 ZDOT =      16388
472235                 ZDOT =        4996
970782

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14647794
27                 X    =         4464647
69
 Y    =      -13342791
45  feet           Y    =        -4066882
83  meter
 Z    =        9690540
48                 Z    =         2953676
74
 XDOT =       4816
743753                 XDOT =        1468
143496
 YDOT =      17269
959372  feet/sec       YDOT =        5263
883617  meter/sec
 ZDOT =      16395
065115                 ZDOT =        4997
215847


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   09271
59613165  
00020000  00000-0  20000-3 0  9059
2 25544  51
6388 135
9347 0008274 141
4482 218
7274 15
74431293 22240


Satellite: ISS
Catalog Number: 25544
Epoch time:      09271
59613165   =   yrday
fracday
Element set:     905
Inclination:       51
6388  deg
RA of node:       135
9347  deg
Eccentricity:     
0008274     
Arg of perigee:   141
4482  deg
Mean anomaly:     218
7274  deg
Mean motion:   15
74431293  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2224
Checksum:              301


Coasting Arc #7 (Orbit 2238)
---------------------------------------

Vector Time (GMT): 2009/272/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          -8324
27                 A    =         6722986
41  meter
 Y    =        5206984
77  meter          E    =           
0016106
 Z    =       -4269830
30                 I    =           51
88632
 XDOT =      -6140
968979                 Wp   =          127
81496
 YDOT =       2926
798895  meter/sec      RA   =          130
12941  deg
 ZDOT =       3580
636347                 TA   =          178
48580
                                          MA   =          178
48092
                                          Ha   =            191
953  n
mi
                                          Hp   =            180
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -27310
59                 X    =          -45806
94
 Y    =       17083283
37  feet           Y    =         5206681
85  meter
 Z    =      -14008629
58                 Z    =        -4269962
10
 XDOT =     -20147
536019                 XDOT =       -6190
634663
 YDOT =       9602
358580  feet/sec       YDOT =        2857
849485  meter/sec
 ZDOT =      11747
494578                 ZDOT =        3550
682640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6331759
46                 X    =        -1929920
28
 Y    =      -15866397
27  feet           Y    =        -4836077
89  meter
 Z    =      -14008828
60                 Z    =        -4269890
96
 XDOT =      14111
939920                 XDOT =        4301
319288
 YDOT =     -15901
168496  feet/sec       YDOT =       -4846
676158  meter/sec
 ZDOT =      11629
601476                 ZDOT =        3544
702530


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   09272
54821205  
00020000  00000-0  20000-3 0  9062
2 25544  51
6379 131
0409 0008335 144
9968 215
1745 15
74451056 22390


Satellite: ISS
Catalog Number: 25544
Epoch time:      09272
54821205   =   yrday
fracday
Element set:     906
Inclination:       51
6379  deg
RA of node:       131
0409  deg
Eccentricity:     
0008335     
Arg of perigee:   144
9968  deg
Mean anomaly:     215
1745  deg
Mean motion:   15
74451056  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2239
Checksum:              294


Coasting Arc #8 (Orbit 2254)
---------------------------------------

Vector Time (GMT): 2009/273/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5136812
00                 A    =         6726242
13  meter
 Y    =       -2842573
70  meter          E    =           
0011705
 Z    =       -3281898
07                 I    =           51
91488
 XDOT =        315
420875                 Wp   =          130
63380
 YDOT =       6043
126909  meter/sec      RA   =          125
05903  deg
 ZDOT =      -4758
932212                 TA   =           87
67763
                                          MA   =           87
54361
                                          Ha   =            191
909  n
mi
                                          Hp   =            181
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16853057
76                 X    =         5184159
31
 Y    =       -9326029
20  feet           Y    =        -2784866
37  meter
 Z    =      -10767382
11                 Z    =        -3256828
10
 XDOT =       1034
845389                 XDOT =         270
940271
 YDOT =      19826
531855  feet/sec       YDOT =        6046
405053  meter/sec
 ZDOT =     -15613
294660                 ZDOT =       -4757
508411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12043585
97                 X    =        -3670885
00
 Y    =       15101892
69  feet           Y    =         4603056
89  meter
 Z    =      -10668728
52                 Z    =        -3251828
45
 XDOT =      -7544
388595                 XDOT =       -2299
529644
 YDOT =     -16999
184686  feet/sec       YDOT =       -5181
351492  meter/sec
 ZDOT =     -15607
311931                 ZDOT =       -4757
108677


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   09273
56374926  
00020000  00000-0  20000-3 0  9079
2 25544  51
6372 125
8222 0008273 148
8344 211
3312 15
74467698 22554


Satellite: ISS
Catalog Number: 25544
Epoch time:      09273
56374926   =   yrday
fracday
Element set:     907
Inclination:       51
6372  deg
RA of node:       125
8222  deg
Eccentricity:     
0008273     
Arg of perigee:   148
8344  deg
Mean anomaly:     211
3312  deg
Mean motion:   15
74467698  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2255
Checksum:              305


Coasting Arc #9 (Orbit 2270)
---------------------------------------

Vector Time (GMT): 2009/274/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -589563
17                 A    =         6723618
99  meter
 Y    =       -5328856
88  meter          E    =           
0014969
 Z    =        4041794
48                 I    =           51
92289
 XDOT =       5594
337574                 Wp   =          109
55026
 YDOT =      -3588
503194  meter/sec      RA   =          119
88815  deg
 ZDOT =      -3908
466706                 TA   =           20
56718
                                          MA   =           20
50698
                                          Ha   =            191
710  n
mi
                                          Hp   =            181
217

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1934262
37                 X    =         -549565
61
 Y    =      -17483126
25  feet           Y    =        -5335225
70  meter
 Z    =       13260480
58                 Z    =         4039028
02
 XDOT =      18354
125898                 XDOT =        5653
035821
 YDOT =     -11773
304441  feet/sec       YDOT =       -3525
616185  meter/sec
 ZDOT =     -12823
053496                 ZDOT =       -3881
146296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8827751
95                 X    =         2690698
79
 Y    =       15223979
68  feet           Y    =         4640269
01  meter
 Z    =       13249251
22                 Z    =         4038371
77
 XDOT =     -11081
375514                 XDOT =       -3377
603257
 YDOT =      17511
059275  feet/sec       YDOT =        5337
370867  meter/sec
 ZDOT =     -12715
568046                 ZDOT =       -3875
705141


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   09274
57926975  
00020000  00000-0  20000-3 0  9089
2 25544  51
6373 120
6023 0008198 153
6020 206
5563 15
74507670 22715


Satellite: ISS
Catalog Number: 25544
Epoch time:      09274
57926975   =   yrday
fracday
Element set:     908
Inclination:       51
6373  deg
RA of node:       120
6023  deg
Eccentricity:     
0008198     
Arg of perigee:   153
6020  deg
Mean anomaly:     206
5563  deg
Mean motion:   15
74507670  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2271
Checksum:              296


Coasting Arc #10 (Orbit 2286)
---------------------------------------

Vector Time (GMT): 2009/275/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4612573
57                 A    =         6725298
89  meter
 Y    =        3378253
59  meter          E    =           
0017458
 Z    =        3535966
62                 I    =           51
94118
 XDOT =      -1038
101559                 Wp   =          118
02885
 YDOT =      -6159
482202  meter/sec      RA   =          114
81976  deg
 ZDOT =       4505
772725                 TA   =          283
88639
                                          MA   =          284
08054
                                          Ha   =            191
617  n
mi
                                          Hp   =            181
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15133115
38                 X    =        -4667184
26
 Y    =       11083509
15  feet           Y    =         3326368
10  meter
 Z    =       11600940
36                 Z    =         3513425
47
 XDOT =      -3405
845011                 XDOT =        -991
036504
 YDOT =     -20208
274941  feet/sec       YDOT =       -6170
827242  meter/sec
 ZDOT =      14782
718914                 ZDOT =        4500
844531

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9227082
58                 X    =         2812414
77
 Y    =      -16394071
29  feet           Y    =        -4996912
93  meter
 Z    =       11512278
10                 Z    =         3508942
36
 XDOT =      10371
042192                 XDOT =        3161
093660
 YDOT =      16261
576046  feet/sec       YDOT =        4956
528379  meter/sec
 ZDOT =      14762
921697                 ZDOT =        4499
738533


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   09275
59477508  
00020000  00000-0  20000-3 0  9096
2 25544  51
6360 115
3821 0008289 157
7302 202
4223 15
74537717 22877


Satellite: ISS
Catalog Number: 25544
Epoch time:      09275
59477508   =   yrday
fracday
Element set:     909
Inclination:       51
6360  deg
RA of node:       115
3821  deg
Eccentricity:     
0008289     
Arg of perigee:   157
7302  deg
Mean anomaly:     202
4223  deg
Mean motion:   15
74537717  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2287
Checksum:              305


Coasting Arc #11 (Orbit 2301)
---------------------------------------

Vector Time (GMT): 2009/276/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1225953
37                 A    =         6724381
06  meter
 Y    =        5419159
44  meter          E    =           
0012926
 Z    =       -3803141
77                 I    =           51
94919
 XDOT =      -4964
424312                 Wp   =          136
95023
 YDOT =       4084
307813  meter/sec      RA   =          109
64872  deg
 ZDOT =       4218
646360                 TA   =          177
21803
                                          MA   =          177
21083
                                          Ha   =            191
526  n
mi
                                          Hp   =            181
419

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4022156
74                 X    =         1183739
57
 Y    =       17779394
50  feet           Y    =         5432632
35  meter
 Z    =      -12477499
25                 Z    =        -3797289
09
 XDOT =     -16287
481339                 XDOT =       -5030
220555
 YDOT =      13399
960017  feet/sec       YDOT =        4028
425250  meter/sec
 ZDOT =      13840
703282                 ZDOT =        4194
368528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11353928
03                 X    =        -3460677
26
 Y    =      -14281320
53  feet           Y    =        -4352946
50  meter
 Z    =      -12454107
89                 Z    =        -3796012
08
 XDOT =       7958
032274                 XDOT =        2425
608237
 YDOT =     -18315
849221  feet/sec       YDOT =       -5582
670842  meter/sec
 ZDOT =      13745
230208                 ZDOT =        4189
546167


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   09276
54679764  
00020000  00000-0  20000-3 0  9102
2 25544  51
6355 110
4875 0008384 160
1913 199
9578 15
74541432 23028


Satellite: ISS
Catalog Number: 25544
Epoch time:      09276
54679764   =   yrday
fracday
Element set:     910
Inclination:       51
6355  deg
RA of node:       110
4875  deg
Eccentricity:     
0008384     
Arg of perigee:   160
1913  deg
Mean anomaly:     199
9578  deg
Mean motion:   15
74541432  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2302
Checksum:              312


Coasting Arc #12 (Orbit 2317)
---------------------------------------

Vector Time (GMT): 2009/277/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4075376
03                 A    =         6724174
80  meter
 Y    =       -3722220
11  meter          E    =           
0010572
 Z    =       -3842822
60                 I    =           51
95773
 XDOT =       1758
151057                 Wp   =          126
59353
 YDOT =       6222
591213  meter/sec      RA   =          104
58280  deg
 ZDOT =      -4176
787089                 TA   =           99
91883
                                          MA   =           99
79948
                                          Ha   =            191
430  n
mi
                                          Hp   =            181
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13370656
28                 X    =         4135363
80
 Y    =      -12212008
22  feet           Y    =        -3676311
80  meter
 Z    =      -12607685
69                 Z    =        -3822877
92
 XDOT =       5768
212128                 XDOT =        1708
728818
 YDOT =      20415
325501  feet/sec       YDOT =        6241
975163  meter/sec
 ZDOT =     -13703
369713                 ZDOT =       -4168
366443

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6582158
30                 X    =        -2006241
85
 Y    =       16927905
47  feet           Y    =         5159625
59  meter
 Z    =      -12529267
38                 Z    =        -3818920
70
 XDOT =     -13108
643776                 XDOT =       -3995
514623
 YDOT =     -15180
585620  feet/sec       YDOT =       -4627
042497  meter/sec
 ZDOT =     -13669
816570                 ZDOT =       -4166
560091


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   09277
56227115  
00020000  00000-0  20000-3 0  9115
2 25544  51
6355 105
2678 0008280 163
2194 196
9245 15
74581509 23185


Satellite: ISS
Catalog Number: 25544
Epoch time:      09277
56227115   =   yrday
fracday
Element set:     911
Inclination:       51
6355  deg
RA of node:       105
2678  deg
Eccentricity:     
0008280     
Arg of perigee:   163
2194  deg
Mean anomaly:     196
9245  deg
Mean motion:   15
74581509  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2318
Checksum:              302


Coasting Arc #13 (Orbit 2333)
---------------------------------------

Vector Time (GMT): 2009/278/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1869427
43                 A    =         6725245
29  meter
 Y    =       -5422762
53  meter          E    =           
0016028
 Z    =        3491618
14                 I    =           51
96734
 XDOT =       4351
469564                 Wp   =          118
97684
 YDOT =      -4441
100743  meter/sec      RA   =           99
41312  deg
 ZDOT =      -4559
584710                 TA   =           19
71262
                                          MA   =           19
65074
                                          Ha   =            191
329  n
mi
                                          Hp   =            181
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6133292
09                 X    =        -1825612
30
 Y    =      -17791215
64  feet           Y    =        -5443422
32  meter
 Z    =       11455440
09                 Z    =         3482643
07
 XDOT =      14276
474949                 XDOT =        4422
957517
 YDOT =     -14570
540494  feet/sec       YDOT =       -4392
040683  meter/sec
 ZDOT =     -14959
267420                 ZDOT =       -4538
270745

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13711422
34                 X    =         4179241
53
 Y    =       12921214
83  feet           Y    =         3938386
28  meter
 Z    =       11419756
50                 Z    =         3480741
78
 XDOT =      -5074
924253                 XDOT =       -1546
836912
 YDOT =      18555
503934  feet/sec       YDOT =        5655
717599  meter/sec
 ZDOT =     -14875
481574                 ZDOT =       -4534
046784


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   09278
57772785  
00020000  00000-0  20000-3 0  9126
2 25544  51
6352 100
0471 0008324 168
2758 191
8601 15
74580371 23340


Satellite: ISS
Catalog Number: 25544
Epoch time:      09278
57772785   =   yrday
fracday
Element set:     912
Inclination:       51
6352  deg
RA of node:       100
0471  deg
Eccentricity:     
0008324     
Arg of perigee:   168
2758  deg
Mean anomaly:     191
8601  deg
Mean motion:   15
74580371  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2334
Checksum:              298


Coasting Arc #14 (Orbit 2349)
---------------------------------------

Vector Time (GMT): 2009/279/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3524596
29                 A    =         6723096
25  meter
 Y    =        3987045
70  meter          E    =           
0015739
 Z    =        4106318
67                 I    =           51
96457
 XDOT =      -2527
562690                 Wp   =          133
33410
 YDOT =      -6190
402112  meter/sec      RA   =           94
34637  deg
 ZDOT =       3821
432461                 TA   =          277
52762
                                          MA   =          277
70640
                                          Ha   =            191
131  n
mi
                                          Hp   =            181
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11563636
11                 X    =        -3588866
46
 Y    =       13080858
60  feet           Y    =         3947272
45  meter
 Z    =       13472174
10                 Z    =         4089039
39
 XDOT =      -8292
528510                 XDOT =       -2476
717023
 YDOT =     -20309
718214  feet/sec       YDOT =       -6218
382316  meter/sec
 ZDOT =      12537
508075                 ZDOT =        3809
277053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3997769
64                 X    =         1218520
19
 Y    =      -17049037
55  feet           Y    =        -5196546
64  meter
 Z    =       13404259
52                 Z    =         4085618
30
 XDOT =      15792
652168                 XDOT =        4813
600381
 YDOT =      13573
427803  feet/sec       YDOT =        4137
180794  meter/sec
 ZDOT =      12489
255092                 ZDOT =        3806
724952


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   09279
59316702  
00020000  00000-0  20000-3 0  9133
2 25544  51
6355  94
8266 0008368 172
1573 187
9722 15
74641034 23504


Satellite: ISS
Catalog Number: 25544
Epoch time:      09279
59316702   =   yrday
fracday
Element set:     913
Inclination:       51
6355  deg
RA of node:        94
8266  deg
Eccentricity:     
0008368     
Arg of perigee:   172
1573  deg
Mean anomaly:     187
9722  deg
Mean motion:   15
74641034  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2350
Checksum:              309


Coasting Arc #15 (Orbit 2364)
---------------------------------------

Vector Time (GMT): 2009/280/12:55:40
959
Vector Time (MET): N/A
Weight (LBS)     : 730797
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2546003
50                 A    =         6726042
22  meter
 Y    =        5373192
96  meter          E    =           
0009046
 Z    =       -3157241
05                 I    =           51
97703
 XDOT =      -3740
531078                 Wp   =          144
62198
 YDOT =       4633
034411  meter/sec      RA   =           89
17894  deg
 ZDOT =       4868
122114                 TA   =          178
84169
                                          MA   =          178
83959
                                          Ha   =            191
000  n
mi
                                          Hp   =            181
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8353029
86                 X    =         2501068
02
 Y    =       17628585
81  feet           Y    =         5401412
54  meter
 Z    =      -10358402
41                 Z    =        -3144981
53
 XDOT =     -12272
083589                 XDOT =       -3815
709558
 YDOT =      15200
244129  feet/sec       YDOT =        4590
785371  meter/sec
 ZDOT =      15971
529244                 ZDOT =        4849
767392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15994959
85                 X    =        -4875263
76
 Y    =      -11211873
25  feet           Y    =        -3417378
97  meter
 Z    =      -10309791
64                 Z    =        -3142424
49
 XDOT =       2473
580742                 XDOT =         753
947410
 YDOT =     -18149
909036  feet/sec       YDOT =       -5532
092274  meter/sec
 ZDOT =      15899
395478                 ZDOT =        4846
135742


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   09280
54512722  
00020000  00000-0  20000-3 0  9141
2 25544  51
6369  89
9328 0008375 174
5743 185
5513 15
74647268 23659


Satellite: ISS
Catalog Number: 25544
Epoch time:      09280
54512722   =   yrday
fracday
Element set:     914
Inclination:       51
6369  deg
RA of node:        89
9328  deg
Eccentricity:     
0008375     
Arg of perigee:   174
5743  deg
Mean anomaly:     185
5513  deg
Mean motion:   15
74647268  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2365
Checksum:              322

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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