Date: July 13th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 962)
---------------------------------------

Vector Time (GMT): 2009/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6683162
92                 A    =         6731163
93  meter
 Y    =         172287
38  meter          E    =           
0016209
 Z    =         689030
89                 I    =           51
61727
 XDOT =        497
007903                 Wp   =          154
28824
 YDOT =       4825
206958  meter/sec      RA   =          186
15944  deg
 ZDOT =      -5989
176967                 TA   =           18
19662
                                          MA   =           18
13869
                                          Ha   =            190
131  n
mi
                                          Hp   =            184
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21926387
52                 X    =         6677392
53
 Y    =         565247
30  feet           Y    =          246990
06  meter
 Z    =        2260600
05                 Z    =          721483
18
 XDOT =       1630
603356                 XDOT =         472
108537
 YDOT =      15830
731488  feet/sec       YDOT =        4830
626375  meter/sec
 ZDOT =     -19649
530731                 ZDOT =       -5986
822373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6152890
35                 X    =        -1875400
98
 Y    =      -21038907
43  feet           Y    =        -6412658
98  meter
 Z    =        2388012
01                 Z    =          727866
06
 XDOT =      13007
346266                 XDOT =        3964
639142
 YDOT =      -6046
659938  feet/sec       YDOT =       -1843
021949  meter/sec
 ZDOT =     -19639
999291                 ZDOT =       -5986
271784


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   09191
53316125  
00010596  00000-0  82463-4 0  9006
2 25544  51
6352 187
0208 0007318 209
0752 151
0004 15
74276931  9638


Satellite: ISS
Catalog Number: 25544
Epoch time:      09191
53316125   =   yrday
fracday
Element set:     900
Inclination:       51
6352  deg
RA of node:       187
0208  deg
Eccentricity:     
0007318     
Arg of perigee:   209
0752  deg
Mean anomaly:     151
0004  deg
Mean motion:   15
74276931  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             963
Checksum:              284


Coasting Arc #2 (Orbit 978)
---------------------------------------

Vector Time (GMT): 2009/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -674741
34                 A    =         6719479
06  meter
 Y    =       -4160849
98  meter          E    =           
0007661
 Z    =        5234858
44                 I    =           51
60728
 XDOT =       7661
117848                 Wp   =          190
69347
 YDOT =       -391
899483  meter/sec      RA   =          181
03257  deg
 ZDOT =        668
735124                 TA   =          252
90282
                                          MA   =          252
98675
                                          Ha   =            190
018  n
mi
                                          Hp   =            184
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2213718
31                 X    =         -653593
49
 Y    =      -13651082
61  feet           Y    =        -4168277
69  meter
 Z    =       17174732
43                 Z    =         5231631
49
 XDOT =      25134
901076                 XDOT =        7661
682197
 YDOT =      -1285
759458  feet/sec       YDOT =        -306
225301  meter/sec
 ZDOT =       2194
012875                 ZDOT =         705
953634

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12180949
57                 X    =        -3712753
43
 Y    =        6581848
13  feet           Y    =         2006147
31  meter
 Z    =       17161811
73                 Z    =         5230920
22
 XDOT =      -8818
788670                 XDOT =       -2687
966786
 YDOT =     -22484
541522  feet/sec       YDOT =       -6853
288256  meter/sec
 ZDOT =       2340
115366                 ZDOT =         713
267164


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   09192
54881126  
00010596  00000-0  82463-4 0  9017
2 25544  51
6349 181
8021 0007347 213
9240 146
1454 15
74276727  9791


Satellite: ISS
Catalog Number: 25544
Epoch time:      09192
54881126   =   yrday
fracday
Element set:     901
Inclination:       51
6349  deg
RA of node:       181
8021  deg
Eccentricity:     
0007347     
Arg of perigee:   213
9240  deg
Mean anomaly:     146
1454  deg
Mean motion:   15
74276727  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             979
Checksum:              318


Coasting Arc #3 (Orbit 993)
---------------------------------------

Vector Time (GMT): 2009/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6659642
48                 A    =         6731081
81  meter
 Y    =         848564
77  meter          E    =           
0003832
 Z    =        -466176
31                 I    =           51
67706
 XDOT =      -1016
611557                 Wp   =           51
29236
 YDOT =      -4693
465952  meter/sec      RA   =          175
88480  deg
 ZDOT =       6015
060449                 TA   =          303
64196
                                          MA   =          303
67851
                                          Ha   =            189
804  n
mi
                                          Hp   =            184
448

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21849220
75                 X    =        -6666371
74
 Y    =        2784005
15  feet           Y    =          774055
17  meter
 Z    =       -1529449
83                 Z    =         -498544
76
 XDOT =      -3335
339754                 XDOT =        -993
272620
 YDOT =     -15398
510340  feet/sec       YDOT =       -4704
704414  meter/sec
 ZDOT =      19734
450292                 ZDOT =        6010
178016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10000531
57                 X    =         3048162
02
 Y    =       19614376
11  feet           Y    =         5978461
84  meter
 Z    =       -1656492
40                 Z    =         -504898
88
 XDOT =     -11896
167853                 XDOT =       -3625
951961
 YDOT =       7721
271885  feet/sec       YDOT =        2353
443670  meter/sec
 ZDOT =      19714
994116                 ZDOT =        6009
130207


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   09193
50097240  
00010596  00000-0  82463-4 0  9021
2 25544  51
6350 176
9102 0007403 216
1688 143
8976 15
74343260  9949


Satellite: ISS
Catalog Number: 25544
Epoch time:      09193
50097240   =   yrday
fracday
Element set:     902
Inclination:       51
6350  deg
RA of node:       176
9102  deg
Eccentricity:     
0007403     
Arg of perigee:   216
1688  deg
Mean anomaly:     143
8976  deg
Mean motion:   15
74343260  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             994
Checksum:              310


Coasting Arc #4 (Orbit 1009)
---------------------------------------

Vector Time (GMT): 2009/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1085989
99                 A    =         6719273
74  meter
 Y    =        4041382
45  meter          E    =           
0011089
 Z    =       -5265419
40                 I    =           51
66672
 XDOT =      -7530
799671                 Wp   =          114
73246
 YDOT =       1532
010581  meter/sec      RA   =          170
75670  deg
 ZDOT =       -382
533060                 TA   =          151
66400
                                          MA   =          151
60364
                                          Ha   =            189
600  n
mi
                                          Hp   =            184
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3562959
29                 X    =         1066296
13
 Y    =       13259128
77  feet           Y    =         4053417
02  meter
 Z    =      -17274998
03                 Z    =        -5260191
14
 XDOT =     -24707
348003                 XDOT =       -7545
512905
 YDOT =       5026
281434  feet/sec       YDOT =        1447
714541  meter/sec
 ZDOT =      -1255
029725                 ZDOT =        -419
153030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11102857
43                 X    =         3384150
95
 Y    =       -8120536
55  feet           Y    =        -2475139
54  meter
 Z    =      -17254221
94                 Z    =        -5259086
85
 XDOT =      12853
829224                 XDOT =        3917
847147
 YDOT =      20510
324522  feet/sec       YDOT =        6251
546914  meter/sec
 ZDOT =      -1398
734771                 ZDOT =        -426
334358


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   09194
51660059  
00010596  00000-0  82463-4 0  9038
2 25544  51
6351 171
6908 0007267 221
7573 138
3036 15
74310701 10109


Satellite: ISS
Catalog Number: 25544
Epoch time:      09194
51660059   =   yrday
fracday
Element set:     903
Inclination:       51
6351  deg
RA of node:       171
6908  deg
Eccentricity:     
0007267     
Arg of perigee:   221
7573  deg
Mean anomaly:     138
3036  deg
Mean motion:   15
74310701  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1010
Checksum:              287


Coasting Arc #5 (Orbit 1025)
---------------------------------------

Vector Time (GMT): 2009/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6466553
25                 A    =         6731168
72  meter
 Y    =       -1823963
09  meter          E    =           
0014140
 Z    =         203571
42                 I    =           51
73679
 XDOT =       1474
954142                 Wp   =          163
39540
 YDOT =       4544
461388  meter/sec      RA   =          165
61762  deg
 ZDOT =      -6045
823490                 TA   =           14
39412
                                          MA   =           14
35389
                                          Ha   =            189
329  n
mi
                                          Hp   =            184
927

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21215725
88                 X    =         6485479
59
 Y    =       -5984130
86  feet           Y    =        -1751544
50  meter
 Z    =         667885
25                 Z    =          235031
65
 XDOT =       4839
088394                 XDOT =        1453
397013
 YDOT =      14909
650224  feet/sec       YDOT =        4560
835261  meter/sec
 ZDOT =     -19835
378903                 ZDOT =       -6038
710089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13409602
85                 X    =        -4087246
95
 Y    =      -17490548
30  feet           Y    =        -5331119
12  meter
 Z    =         791321
14                 Z    =          241194
68
 XDOT =      10741
577833                 XDOT =        3274
032923
 YDOT =      -9142
643178  feet/sec       YDOT =       -2786
677641  meter/sec
 ZDOT =     -19807
169128                 ZDOT =       -6037
225150


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   09195
53221678  
00010596  00000-0  82463-4 0  9042
2 25544  51
6355 166
4723 0007211 226
8124 133
2437 15
74346876 10265


Satellite: ISS
Catalog Number: 25544
Epoch time:      09195
53221678   =   yrday
fracday
Element set:     904
Inclination:       51
6355  deg
RA of node:       166
4723  deg
Eccentricity:     
0007211     
Arg of perigee:   226
8124  deg
Mean anomaly:     133
2437  deg
Mean motion:   15
74346876  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1026
Checksum:              307


Coasting Arc #6 (Orbit 1041)
---------------------------------------

Vector Time (GMT): 2009/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1481228
40                 A    =         6719098
79  meter
 Y    =       -3891814
05  meter          E    =           
0005820
 Z    =        5276000
63                 I    =           51
72467
 XDOT =       7234
717147                 Wp   =          214
20462
 YDOT =      -2633
586065  meter/sec      RA   =          160
48957  deg
 ZDOT =         83
807157                 TA   =          234
97363
                                          MA   =          235
02826
                                          Ha   =            189
196  n
mi
                                          Hp   =            185
137

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4859673
22                 X    =        -1463229
25
 Y    =      -12768418
79  feet           Y    =        -3908277
96  meter
 Z    =       17309713
35                 Z    =         5268848
10
 XDOT =      23735
948644                 XDOT =        7263
221533
 YDOT =      -8640
374230  feet/sec       YDOT =       -2552
523856  meter/sec
 ZDOT =        274
957863                 ZDOT =         119
022373

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9863645
08                 X    =        -3006439
02
 Y    =        9504587
27  feet           Y    =         2896998
20  meter
 Z    =       17281390
14                 Z    =         5267367
71
 XDOT =     -16439
490826                 XDOT =       -5010
756804
 YDOT =     -17839
586727  feet/sec       YDOT =       -5437
506035  meter/sec
 ZDOT =        413
103958                 ZDOT =         125
914086


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   09196
54782178  
00010596  00000-0  82463-4 0  9052
2 25544  51
6354 161
2540 0007250 231
0638 128
9879 15
74352257 10424


Satellite: ISS
Catalog Number: 25544
Epoch time:      09196
54782178   =   yrday
fracday
Element set:     905
Inclination:       51
6354  deg
RA of node:       161
2540  deg
Eccentricity:     
0007250     
Arg of perigee:   231
0638  deg
Mean anomaly:     128
9879  deg
Mean motion:   15
74352257  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1042
Checksum:              316


Coasting Arc #7 (Orbit 1057)
---------------------------------------

Vector Time (GMT): 2009/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6137462
63                 A    =         6731054
67  meter
 Y    =        2755788
59  meter          E    =           
0005237
 Z    =          68673
10                 I    =           51
79284
 XDOT =      -1892
201757                 Wp   =           34
26765
 YDOT =      -4370
325485  meter/sec      RA   =          155
35904  deg
 ZDOT =       6048
944270                 TA   =          326
47662
                                          MA   =          326
50975
                                          Ha   =            188
951  n
mi
                                          Hp   =            185
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20136032
24                 X    =        -6168155
78
 Y    =        9041301
16  feet           Y    =         2686984
27  meter
 Z    =         225305
43                 Z    =           38783
05
 XDOT =      -6208
011013                 XDOT =       -1872
576131
 YDOT =     -14338
338206  feet/sec       YDOT =       -4391
376255  meter/sec
 ZDOT =      19845
617684                 ZDOT =        6039
799031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16371030
16                 X    =         4989889
99
 Y    =       14806531
55  feet           Y    =         4513030
82  meter
 Z    =         108066
65                 Z    =           32938
71
 XDOT =      -9508
802321                 XDOT =       -2898
282947
 YDOT =      10358
060618  feet/sec       YDOT =        3157
136877  meter/sec
 ZDOT =      19809
440978                 ZDOT =        6037
917610


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   09197
56341342  
00010596  00000-0  82463-4 0  9060
2 25544  51
6351 156
0349 0007280 234
2703 125
7784 15
74393790 10585


Satellite: ISS
Catalog Number: 25544
Epoch time:      09197
56341342   =   yrday
fracday
Element set:     906
Inclination:       51
6351  deg
RA of node:       156
0349  deg
Eccentricity:     
0007280     
Arg of perigee:   234
2703  deg
Mean anomaly:     125
7784  deg
Mean motion:   15
74393790  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1058
Checksum:              315


Coasting Arc #8 (Orbit 1072)
---------------------------------------

Vector Time (GMT): 2009/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1816935
72                 A    =         6719007
51  meter
 Y    =        3749685
15  meter          E    =           
0009710
 Z    =       -5278656
20                 I    =           51
77946
 XDOT =      -6772
967863                 Wp   =          115
72810
 YDOT =       3644
335219  meter/sec      RA   =          150
22813  deg
 ZDOT =        253
694773                 TA   =          156
69890
                                          MA   =          156
65486
                                          Ha   =            188
729  n
mi
                                          Hp   =            185
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5961075
19                 X    =         1800513
85
 Y    =       12302116
62  feet           Y    =         3769912
18  meter
 Z    =      -17318425
84                 Z    =        -5269868
82
 XDOT =     -22221
023173                 XDOT =       -6814
448462
 YDOT =      11956
480378  feet/sec       YDOT =        3568
363959  meter/sec
 ZDOT =        832
331934                 ZDOT =         220
691453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8647269
17                 X    =         2635687
64
 Y    =      -10644392
45  feet           Y    =        -3244410
82  meter
 Z    =      -17283692
01                 Z    =        -5268069
32
 XDOT =      19368
029522                 XDOT =        5903
375398
 YDOT =      14572
719205  feet/sec       YDOT =        4441
764814  meter/sec
 ZDOT =        702
898146                 ZDOT =         214
243355


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   09198
51552107  
00010596  00000-0  82463-4 0  9070
2 25544  51
6358 151
1419 0007276 239
3135 120
7312 15
74388554 10737


Satellite: ISS
Catalog Number: 25544
Epoch time:      09198
51552107   =   yrday
fracday
Element set:     907
Inclination:       51
6358  deg
RA of node:       151
1419  deg
Eccentricity:     
0007276     
Arg of perigee:   239
3135  deg
Mean anomaly:     120
7312  deg
Mean motion:   15
74388554  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1073
Checksum:              307


Coasting Arc #9 (Orbit 1088)
---------------------------------------

Vector Time (GMT): 2009/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5669598
94                 A    =         6730964
28  meter
 Y    =       -3593616
81  meter          E    =           
0011863
 Z    =        -376306
22                 I    =           51
84594
 XDOT =       2267
273042                 Wp   =          174
20671
 YDOT =       4206
918416  meter/sec      RA   =          145
10761  deg
 ZDOT =      -6043
082507                 TA   =            9
87502
                                          MA   =            9
85173
                                          Ha   =            188
524  n
mi
                                          Hp   =            185
615

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18601046
39                 X    =         5711190
02
 Y    =      -11790081
38  feet           Y    =        -3529983
42  meter
 Z    =       -1234600
46                 Z    =         -348662
96
 XDOT =       7438
559850                 XDOT =        2249
418200
 YDOT =      13802
225773  feet/sec       YDOT =        4232
173627  meter/sec
 ZDOT =     -19826
386177                 ZDOT =       -6032
110737

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18686024
80                 X    =        -5695500
36
 Y    =      -11665904
75  feet           Y    =        -3555767
77  meter
 Z    =       -1126200
52                 Z    =         -343265
92
 XDOT =       8318
070517                 XDOT =        2535
347894
 YDOT =     -11423
485527  feet/sec       YDOT =       -3481
878389  meter/sec
 ZDOT =     -19783
044718                 ZDOT =       -6029
872030


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   09199
53109041  
00010596  00000-0  82463-4 0  9089
2 25544  51
6365 145
9232 0007281 243
3932 116
6486 15
74408933 10892


Satellite: ISS
Catalog Number: 25544
Epoch time:      09199
53109041   =   yrday
fracday
Element set:     908
Inclination:       51
6365  deg
RA of node:       145
9232  deg
Eccentricity:     
0007281     
Arg of perigee:   243
3932  deg
Mean anomaly:     116
6486  deg
Mean motion:   15
74408933  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1089
Checksum:              321


Coasting Arc #10 (Orbit 1104)
---------------------------------------

Vector Time (GMT): 2009/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2141035
62                 A    =         6718942
45  meter
 Y    =       -3599006
50  meter          E    =           
0004476
 Z    =        5257698
81                 I    =           51
83006
 XDOT =       6173
771640                 Wp   =          249
02166
 YDOT =      -4559
716616  meter/sec      RA   =          139
97501  deg
 ZDOT =       -609
127933                 TA   =          206
74242
                                          MA   =          206
76551
                                          Ha   =            188
278  n
mi
                                          Hp   =            185
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7024395
07                 X    =        -2126172
55
 Y    =      -11807764
12  feet           Y    =        -3622866
71  meter
 Z    =       17249668
03                 Z    =         5247333
15
 XDOT =      20255
156298                 XDOT =        6227
259331
 YDOT =     -14959
700183  feet/sec       YDOT =       -4490
378707  meter/sec
 ZDOT =      -1998
451223                 ZDOT =        -579
006910

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7357412
87                 X    =        -2242539
44
 Y    =       11663799
86  feet           Y    =         3555126
20  meter
 Z    =       17208739
50                 Z    =         5245223
80
 XDOT =     -21610
205716                 XDOT =       -6586
790702
 YDOT =     -10866
869337  feet/sec       YDOT =       -3312
221774  meter/sec
 ZDOT =      -1880
349558                 ZDOT =        -573
130545


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   09200
54664706  
00010596  00000-0  82463-4 0  9098
2 25544  51
6370 140
7049 0007308 247
8532 112
1856 15
74443086 11051


Satellite: ISS
Catalog Number: 25544
Epoch time:      09200
54664706   =   yrday
fracday
Element set:     909
Inclination:       51
6370  deg
RA of node:       140
7049  deg
Eccentricity:     
0007308     
Arg of perigee:   247
8532  deg
Mean anomaly:     112
1856  deg
Mean motion:   15
74443086  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1105
Checksum:              299


Coasting Arc #11 (Orbit 1120)
---------------------------------------

Vector Time (GMT): 2009/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5091034
66                 A    =         6730698
47  meter
 Y    =        4340589
36  meter          E    =           
0006919
 Z    =         696908
11                 I    =           51
89194
 XDOT =      -2622
188131                 Wp   =           31
53736
 YDOT =      -4043
202127  meter/sec      RA   =          134
86288  deg
 ZDOT =       6006
069736                 TA   =          336
02896
                                          MA   =          336
06116
                                          Ha   =            187
976  n
mi
                                          Hp   =            185
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16702869
61                 X    =        -5142578
90
 Y    =       14240778
73  feet           Y    =         4283370
10  meter
 Z    =        2286443
93                 Z    =          672051
83
 XDOT =      -8602
979434                 XDOT =       -2605
957452
 YDOT =     -13265
098843  feet/sec       YDOT =       -4072
435354  meter/sec
 ZDOT =      19704
953201                 ZDOT =        5993
369983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20369765
29                 X    =         6208704
46
 Y    =        8203316
43  feet           Y    =         2500370
85  meter
 Z    =        2188999
67                 Z    =          667207
10
 XDOT =      -7109
696520                 XDOT =       -2167
035499
 YDOT =      12390
333297  feet/sec       YDOT =        3776
573589  meter/sec
 ZDOT =      19654
823341                 ZDOT =        5990
790154


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   09201
56219213  
00010596  00000-0  82463-4 0  9102
2 25544  51
6372 135
4852 0007313 251
8406 108
1961 15
74451757 11211


Satellite: ISS
Catalog Number: 25544
Epoch time:      09201
56219213   =   yrday
fracday
Element set:     910
Inclination:       51
6372  deg
RA of node:       135
4852  deg
Eccentricity:     
0007313     
Arg of perigee:   251
8406  deg
Mean anomaly:     108
1961  deg
Mean motion:   15
74451757  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1121
Checksum:              283


Coasting Arc #12 (Orbit 1135)
---------------------------------------

Vector Time (GMT): 2009/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2441582
42                 A    =         6719067
94  meter
 Y    =        3468867
40  meter          E    =           
0008236
 Z    =       -5217518
74                 I    =           51
87416
 XDOT =      -5452
761513                 Wp   =          116
85776
 YDOT =       5339
168250  meter/sec      RA   =          129
72610  deg
 ZDOT =        995
637905                 TA   =          162
62183
                                          MA   =          162
59362
                                          Ha   =            187
719  n
mi
                                          Hp   =            186
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8010441
00                 X    =         2427956
72
 Y    =       11380798
57  feet           Y    =         3496095
31  meter
 Z    =      -17117843
65                 Z    =        -5205690
28
 XDOT =     -17889
637509                 XDOT =       -5516
896272
 YDOT =      17516
956201  feet/sec       YDOT =        5277
833514  meter/sec
 ZDOT =       3266
528561                 ZDOT =         968
994057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6105098
42                 X    =         1860834
00
 Y    =      -12570341
15  feet           Y    =        -3831439
98  meter
 Z    =      -17071163
08                 Z    =        -5203290
51
 XDOT =      23038
281842                 XDOT =        7022
068306
 YDOT =       6883
913210  feet/sec       YDOT =        2098
216746  meter/sec
 ZDOT =       3162
098628                 ZDOT =         963
807662


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   09202
51425432  
00010596  00000-0  82463-4 0  9111
2 25544  51
6382 130
5924 0007311 255
7923 104
2429 15
74469664 11361


Satellite: ISS
Catalog Number: 25544
Epoch time:      09202
51425432   =   yrday
fracday
Element set:     911
Inclination:       51
6382  deg
RA of node:       130
5924  deg
Eccentricity:     
0007311     
Arg of perigee:   255
7923  deg
Mean anomaly:     104
2429  deg
Mean motion:   15
74469664  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1136
Checksum:              292


Coasting Arc #13 (Orbit 1151)
---------------------------------------

Vector Time (GMT): 2009/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4419867
26                 A    =         6730360
99  meter
 Y    =       -4958250
81  meter          E    =           
0009134
 Z    =       -1046780
57                 I    =           51
93124
 XDOT =       2966
114690                 Wp   =          187
57232
 YDOT =       3898
400855  meter/sec      RA   =          124
62419  deg
 ZDOT =      -5944
488741                 TA   =            3
83236
                                          MA   =            3
82537
                                          Ha   =            187
504  n
mi
                                          Hp   =            185
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14500876
84                 X    =         4480067
72
 Y    =      -16267227
07  feet           Y    =        -4908488
52  meter
 Z    =       -3434319
46                 Z    =        -1025163
84
 XDOT =       9731
347408                 XDOT =        2951
178206
 YDOT =      12790
029052  feet/sec       YDOT =        3931
486999  meter/sec
 ZDOT =     -19502
915817                 ZDOT =       -5930
115441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21317204
79                 X    =        -6497484
02
 Y    =       -4587972
66  feet           Y    =        -1398414
07  meter
 Z    =       -3349618
26                 Z    =        -1020963
64
 XDOT =       5921
562263                 XDOT =        1804
892178
 YDOT =     -13323
490406  feet/sec       YDOT =       -4060
999876  meter/sec
 ZDOT =     -19446
201784                 ZDOT =       -5927
202304


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   09203
52977584  
00010596  00000-0  82463-4 0  9124
2 25544  51
6391 125
3738 0007335 259
3666 100
6671 15
74478815 11521


Satellite: ISS
Catalog Number: 25544
Epoch time:      09203
52977584   =   yrday
fracday
Element set:     912
Inclination:       51
6391  deg
RA of node:       125
3738  deg
Eccentricity:     
0007335     
Arg of perigee:   259
3666  deg
Mean anomaly:     100
6671  deg
Mean motion:   15
74478815  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1152
Checksum:              325


Coasting Arc #14 (Orbit 1167)
---------------------------------------

Vector Time (GMT): 2009/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2745802
04                 A    =         6719202
16  meter
 Y    =       -3340094
01  meter          E    =           
0004166
 Z    =        5146727
54                 I    =           51
90985
 XDOT =       4643
151196                 Wp   =          295
54815
 YDOT =      -5979
063412  meter/sec      RA   =          119
48362  deg
 ZDOT =      -1402
233748                 TA   =          167
83722
                                          MA   =          167
82715
                                          Ha   =            187
047  n
mi
                                          Hp   =            185
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9008536
88                 X    =        -2733249
73
 Y    =      -10958313
67  feet           Y    =        -3370729
53  meter
 Z    =       16885589
03                 Z    =         5133418
89
 XDOT =      15233
435682                 XDOT =        4716
476647
 YDOT =     -19616
349776  feet/sec       YDOT =       -5926
730843  meter/sec
 ZDOT =      -4600
504422                 ZDOT =       -1379
500394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4798159
93                 X    =        -1462479
15
 Y    =       13415900
82  feet           Y    =         4089166
57  meter
 Z    =       16833085
23                 Z    =         5130724
38
 XDOT =     -23673
906406                 XDOT =       -7215
806673
 YDOT =      -2802
676014  feet/sec       YDOT =        -854
255649  meter/sec
 ZDOT =      -4511
463281                 ZDOT =       -1375
094008


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   09204
54528391  
00010596  00000-0  82463-4 0  9136
2 25544  51
6388 120
1551 0007407 264
1443  95
8876 15
74533749 11687


Satellite: ISS
Catalog Number: 25544
Epoch time:      09204
54528391   =   yrday
fracday
Element set:     913
Inclination:       51
6388  deg
RA of node:       120
1551  deg
Eccentricity:     
0007407     
Arg of perigee:   264
1443  deg
Mean anomaly:      95
8876  deg
Mean motion:   15
74533749  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1168
Checksum:              323


Coasting Arc #15 (Orbit 1183)
---------------------------------------

Vector Time (GMT): 2009/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3680732
23                 A    =         6729868
98  meter
 Y    =        5448728
47  meter          E    =           
0008250
 Z    =        1408847
21                 I    =           51
95938
 XDOT =      -3319
570892                 Wp   =           36
20039
 YDOT =      -3757
002387  meter/sec      RA   =          114
38911  deg
 ZDOT =       5846
830514                 TA   =          339
22670
                                          MA   =          339
26021
                                          Ha   =            186
685  n
mi
                                          Hp   =            185
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12075893
13                 X    =        -3748231
06
 Y    =       17876405
74  feet           Y    =         5407190
85  meter
 Z    =        4622202
12                 Z    =         1390803
06
 XDOT =     -10890
980617                 XDOT =       -3305
714973
 YDOT =     -12326
123318  feet/sec       YDOT =       -3794
046761  meter/sec
 ZDOT =      19182
514811                 ZDOT =        5830
737741

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21567101
51                 X    =         6573652
54
 Y    =         949339
61  feet           Y    =          289358
71  meter
 Z    =        4551561
97                 Z    =         1387316
09
 XDOT =      -4669
955009                 XDOT =       -1423
402287
 YDOT =      14255
067388  feet/sec       YDOT =        4344
944540  meter/sec
 ZDOT =      19119
038955                 ZDOT =        5827
483073


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   09205
56078182  
00010596  00000-0  82463-4 0  9148
2 25544  51
6389 114
9352 0007336 268
2816  91
7507 15
74517491 11848


Satellite: ISS
Catalog Number: 25544
Epoch time:      09205
56078182   =   yrday
fracday
Element set:     914
Inclination:       51
6389  deg
RA of node:       114
9352  deg
Eccentricity:     
0007336     
Arg of perigee:   268
2816  deg
Mean anomaly:      91
7507  deg
Mean motion:   15
74517491  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1184
Checksum:              326

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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