Date: January 19th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 2209)
---------------------------------------

Vector Time (GMT): 2009/016/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5128696
28                 A    =         6737721
70  meter
 Y    =       -2863364
79  meter          E    =           
0003320
 Z    =       -3298061
42                 I    =           51
66039
 XDOT =       4980
607130                 Wp   =          273
61080
 YDOT =      -3487
405150  meter/sec      RA   =            2
81148  deg
 ZDOT =      -4713
137898                 TA   =          305
01228
                                          MA   =          305
04344
                                          Ha   =            193
230  n
mi
                                          Hp   =            192
584

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16826431
37                 X    =        -5080275
32
 Y    =       -9394241
44  feet           Y    =        -2920445
98  meter
 Z    =      -10820411
48                 Z    =        -3322858
80
 XDOT =      16340
574575                 XDOT =        5042
128965
 YDOT =     -11441
617947  feet/sec       YDOT =       -3431
364932  meter/sec
 ZDOT =     -15463
050848                 ZDOT =       -4688
793142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1190467
95                 X    =         -362854
63
 Y    =      -19179707
81  feet           Y    =        -5845974
94  meter
 Z    =      -10917117
93                 Z    =        -3327537
55
 XDOT =      17121
298143                 XDOT =        5218
571674
 YDOT =       7692
969203  feet/sec       YDOT =        2344
817013  meter/sec
 ZDOT =     -15368
487999                 ZDOT =       -4684
315142


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   09016
54575237  
00010596  00000-0  82463-4 0  9004
2 25544  51
6401   3
1542 0008078 273
4222  86
6015 15
70373981 22104


Satellite: ISS
Catalog Number: 25544
Epoch time:      09016
54575237   =   yrday
fracday
Element set:     900
Inclination:       51
6401  deg
RA of node:         3
1542  deg
Eccentricity:     
0008078     
Arg of perigee:   273
4222  deg
Mean anomaly:      86
6015  deg
Mean motion:   15
70373981  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2210
Checksum:              278


Coasting Arc #2 (Orbit 2225)
---------------------------------------

Vector Time (GMT): 2009/017/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2780331
06                 A    =         6732747
47  meter
 Y    =        3880524
65  meter          E    =           
0004905
 Z    =        4750979
18                 I    =           51
61404
 XDOT =      -7002
566046                 Wp   =          342
30696
 YDOT =      -1796
366683  meter/sec      RA   =          357
65834  deg
 ZDOT =      -2626
865306                 TA   =          133
54285
                                          MA   =          133
50210
                                          Ha   =            193
771  n
mi
                                          Hp   =            192
884

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9121821
06                 X    =        -2846596
24
 Y    =       12731380
07  feet           Y    =         3849062
62  meter
 Z    =       15587202
03                 Z    =         4737311
71
 XDOT =     -22974
298052                 XDOT =       -6969
197628
 YDOT =      -5893
591479  feet/sec       YDOT =       -1874
486732  meter/sec
 ZDOT =      -8618
324495                 ZDOT =       -2660
802462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15704076
46                 X    =        -4786602
51
 Y    =        -571177
46  feet           Y    =         -174094
89  meter
 Z    =       15534228
78                 Z    =         4734832
93
 XDOT =      -7898
088749                 XDOT =       -2407
337451
 YDOT =     -21182
686088  feet/sec       YDOT =       -6456
482719  meter/sec
 ZDOT =      -8750
543518                 ZDOT =       -2667
165664


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   09017
56392417  
00010596  00000-0  82463-4 0  9015
2 25544  51
6400 357
9537 0008225 277
5404  82
4822 15
70397006 22269


Satellite: ISS
Catalog Number: 25544
Epoch time:      09017
56392417   =   yrday
fracday
Element set:     901
Inclination:       51
6400  deg
RA of node:       357
9537  deg
Eccentricity:     
0008225     
Arg of perigee:   277
5404  deg
Mean anomaly:      82
4822  deg
Mean motion:   15
70397006  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2226
Checksum:              304


Coasting Arc #3 (Orbit 2241)
---------------------------------------

Vector Time (GMT): 2009/018/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6627567
02                 A    =         6741641
74  meter
 Y    =          92736
75  meter          E    =           
0009494
 Z    =        1196501
39                 I    =           51
61550
 XDOT =      -1129
838128                 Wp   =           23
38647
 YDOT =       4840
922699  meter/sec      RA   =          352
58041  deg
 ZDOT =       5875
768692                 TA   =          349
71217
                                          MA   =          349
73159
                                          Ha   =            193
804  n
mi
                                          Hp   =            192
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21743986
29                 X    =         6620225
11
 Y    =         304254
42  feet           Y    =          166808
92  meter
 Z    =        3925529
50                 Z    =         1228680
00
 XDOT =      -3706
818004                 XDOT =       -1212
429321
 YDOT =      15882
292318  feet/sec       YDOT =        4827
826012  meter/sec
 ZDOT =      19277
456337                 ZDOT =        5870
079695

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12143155
07                 X    =         3701233
67
 Y    =       18012165
38  feet           Y    =         5490108
01  meter
 Z    =        4050799
41                 Z    =         1234683
66
 XDOT =     -13908
480593                 XDOT =       -4239
304885
 YDOT =       5040
912809  feet/sec       YDOT =        1536
470224  meter/sec
 ZDOT =      19255
597463                 ZDOT =        5869
106107


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   09018
58208012  
00010596  00000-0  82463-4 0  9026
2 25544  51
6402 352
7528 0008140 280
4070  79
6174 15
70449627 22425


Satellite: ISS
Catalog Number: 25544
Epoch time:      09018
58208012   =   yrday
fracday
Element set:     902
Inclination:       51
6402  deg
RA of node:       352
7528  deg
Eccentricity:     
0008140     
Arg of perigee:   280
4070  deg
Mean anomaly:      79
6174  deg
Mean motion:   15
70449627  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2242
Checksum:              291


Coasting Arc #4 (Orbit 2256)
---------------------------------------

Vector Time (GMT): 2009/019/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -858073
70                 A    =         6730283
22  meter
 Y    =       -4099562
39  meter          E    =           
0007378
 Z    =       -5274289
98                 I    =           51
54855
 XDOT =       7514
868812                 Wp   =           73
99953
 YDOT =      -1632
662093  meter/sec      RA   =          347
45571  deg
 ZDOT =         48
483893                 TA   =          196
44975
                                          MA   =          196
47371
                                          Ha   =            194
185  n
mi
                                          Hp   =            192
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2815202
43                 X    =         -786546
63
 Y    =      -13450007
84  feet           Y    =        -4108757
50  meter
 Z    =      -17304100
98                 Z    =        -5278285
07
 XDOT =      24655
081403                 XDOT =        7532
331463
 YDOT =      -5356
502929  feet/sec       YDOT =       -1548
528836  meter/sec
 ZDOT =        159
067889                 ZDOT =          85
033082

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9325022
02                 X    =         2842266
71
 Y    =      -10066041
95  feet           Y    =        -3068129
59  meter
 Z    =      -17319894
63                 Z    =        -5279103
88
 XDOT =      18024
383283                 XDOT =        5493
832025
 YDOT =      16190
744961  feet/sec       YDOT =        4934
939064  meter/sec
 ZDOT =        301
250013                 ZDOT =          91
821004


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   09019
53658978  
00010596  00000-0  82463-4 0  9033
2 25544  51
6407 347
8767 0008206 285
3740  74
6514 15
70434464 22573


Satellite: ISS
Catalog Number: 25544
Epoch time:      09019
53658978   =   yrday
fracday
Element set:     903
Inclination:       51
6407  deg
RA of node:       347
8767  deg
Eccentricity:     
0008206     
Arg of perigee:   285
3740  deg
Mean anomaly:      74
6514  deg
Mean motion:   15
70434464  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2257
Checksum:              336


Coasting Arc #5 (Orbit 2272)
---------------------------------------

Vector Time (GMT): 2009/020/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6013259
04                 A    =         6741769
52  meter
 Y    =        2833348
16  meter          E    =           
0006120
 Z    =        1101915
07                 I    =           51
55944
 XDOT =      -2952
062691                 Wp   =          142
18981
 YDOT =      -3968
588605  meter/sec      RA   =          342
33170  deg
 ZDOT =      -5892
782444                 TA   =           25
75869
                                          MA   =           25
72823
                                          Ha   =            194
411  n
mi
                                          Hp   =            192
345

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19728540
16                 X    =        -6049847
93
 Y    =        9295761
67  feet           Y    =         2765899
72  meter
 Z    =        3615206
93                 Z    =         1072614
37
 XDOT =      -9685
245048                 XDOT =       -2878
840112
 YDOT =     -13020
303823  feet/sec       YDOT =       -4001
190298  meter/sec
 ZDOT =     -19333
275736                 ZDOT =       -5906
945944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19266482
29                 X    =        -5872423
80
 Y    =      -10258639
87  feet           Y    =        -3126833
43  meter
 Z    =        3501309
95                 Z    =         1067199
27
 XDOT =       3953
754970                 XDOT =        1205
104515
 YDOT =     -14057
313606  feet/sec       YDOT =       -4284
669187  meter/sec
 ZDOT =     -19388
645012                 ZDOT =       -5909
659000


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   09020
55471757  
00010596  00000-0  82463-4 0  9046
2 25544  51
6411 342
6758 0008221 289
4748  70
5525 15
70461968 22735


Satellite: ISS
Catalog Number: 25544
Epoch time:      09020
55471757   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:       342
6758  deg
Eccentricity:     
0008221     
Arg of perigee:   289
4748  deg
Mean anomaly:      70
5525  deg
Mean motion:   15
70461968  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2273
Checksum:              321


Coasting Arc #6 (Orbit 2288)
---------------------------------------

Vector Time (GMT): 2009/021/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4051145
45                 A    =         6732033
17  meter
 Y    =        2436388
49  meter          E    =           
0001655
 Z    =        4794511
41                 I    =           51
50033
 XDOT =      -5686
645206                 Wp   =          254
07379
 YDOT =       4539
966694  meter/sec      RA   =          337
24550  deg
 ZDOT =       2498
186707                 TA   =          171
41399
                                          MA   =          171
41116
                                          Ha   =            194
419  n
mi
                                          Hp   =            192
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13291159
60                 X    =         4000309
71
 Y    =        7993400
54  feet           Y    =         2481405
99  meter
 Z    =       15730024
30                 Z    =         4814068
39
 XDOT =     -18656
972462                 XDOT =       -5749
124792
 YDOT =      14894
903853  feet/sec       YDOT =        4476
025721  meter/sec
 ZDOT =       8196
150612                 ZDOT =        2470
410085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1759885
21                 X    =          536413
01
 Y    =       15331231
65  feet           Y    =         4672959
41  meter
 Z    =       15806301
91                 Z    =         4817760
82
 XDOT =     -22109
800263                 XDOT =       -6739
067120
 YDOT =      -5800
014346  feet/sec       YDOT =       -1767
844373  meter/sec
 ZDOT =       8088
283828                 ZDOT =        2465
308911


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   09021
57282820  
00010596  00000-0  82463-4 0  9051
2 25544  51
6417 337
4752 0008330 292
4593  67
5686 15
70524395 22895


Satellite: ISS
Catalog Number: 25544
Epoch time:      09021
57282820   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:       337
4752  deg
Eccentricity:     
0008330     
Arg of perigee:   292
4593  deg
Mean anomaly:      67
5686  deg
Mean motion:   15
70524395  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2289
Checksum:              326


Coasting Arc #7 (Orbit 2303)
---------------------------------------

Vector Time (GMT): 2009/022/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3577146
65                 A    =         6737872
46  meter
 Y    =       -4746349
46  meter          E    =           
0005605
 Z    =       -3166133
01                 I    =           51
49259
 XDOT =       5878
833905                 Wp   =          327
60583
 YDOT =       1219
799173  meter/sec      RA   =          332
08209  deg
 ZDOT =       4814
122802                 TA   =          355
46503
                                          MA   =          355
47010
                                          Ha   =            194
805  n
mi
                                          Hp   =            191
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11736045
44                 X    =         3645335
48
 Y    =      -15572012
66  feet           Y    =        -4705966
12  meter
 Z    =      -10387575
51                 Z    =        -3148590
43
 XDOT =      19287
512812                 XDOT =        5841
371253
 YDOT =       4001
965792  feet/sec       YDOT =        1285
329709  meter/sec
 ZDOT =      15794
366148                 ZDOT =        4842
590823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19527869
34                 X    =         5952094
57
 Y    =        -541341
77  feet           Y    =         -165000
97  meter
 Z    =      -10319560
74                 Z    =        -3145402
11
 XDOT =       8848
980106                 XDOT =        2697
169136
 YDOT =      16054
670053  feet/sec       YDOT =        4893
463432  meter/sec
 ZDOT =      15905
267103                 ZDOT =        4847
925413


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   09022
52729564  
00010596  00000-0  82463-4 0  9069
2 25544  51
6414 332
5987 0008337 297
1595  62
8716 15
70498093 23044


Satellite: ISS
Catalog Number: 25544
Epoch time:      09022
52729564   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       332
5987  deg
Eccentricity:     
0008337     
Arg of perigee:   297
1595  deg
Mean anomaly:      62
8716  deg
Mean motion:   15
70498093  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2304
Checksum:              333


Coasting Arc #8 (Orbit 2319)
---------------------------------------

Vector Time (GMT): 2009/023/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5772504
40                 A    =         6736788
66  meter
 Y    =         477921
44  meter          E    =           
0005050
 Z    =       -3442930
35                 I    =           51
46520
 XDOT =       2241
380255                 Wp   =          336
21185
 YDOT =      -5778
148269  meter/sec      RA   =          327
01198  deg
 ZDOT =      -4553
168286                 TA   =          244
57153
                                          MA   =          244
62379
                                          Ha   =            194
864  n
mi
                                          Hp   =            191
419

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18938662
73                 X    =        -5760694
80
 Y    =        1567983
73  feet           Y    =          413436
34  meter
 Z    =      -11295703
25                 Z    =        -3470943
85
 XDOT =       7353
609762                 XDOT =        2327
943875
 YDOT =     -18957
179361  feet/sec       YDOT =       -5752
599370  meter/sec
 ZDOT =     -14938
216163                 ZDOT =       -4542
070246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13265949
59                 X    =        -4043461
44
 Y    =      -13515581
74  feet           Y    =        -4119549
31  meter
 Z    =      -11404738
61                 Z    =        -3476164
33
 XDOT =      18350
485300                 XDOT =        5593
227919
 YDOT =      -5423
707944  feet/sec       YDOT =       -1653
146181  meter/sec
 ZDOT =     -14895
353929                 ZDOT =       -4540
103878


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   09023
54537793  
00010596  00000-0  82463-4 0  9074
2 25544  51
6423 327
3973 0008280 301
3322  58
7028 15
70548456 23201


Satellite: ISS
Catalog Number: 25544
Epoch time:      09023
54537793   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:       327
3973  deg
Eccentricity:     
0008280     
Arg of perigee:   301
3322  deg
Mean anomaly:      58
7028  deg
Mean motion:   15
70548456  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2320
Checksum:              305


Coasting Arc #9 (Orbit 2335)
---------------------------------------

Vector Time (GMT): 2009/024/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -265970
90                 A    =         6732770
81  meter
 Y    =        4894068
93  meter          E    =           
0008313
 Z    =        4619369
60                 I    =           51
42762
 XDOT =      -6728
273038                 Wp   =            4
33768
 YDOT =       2363
073128  meter/sec      RA   =          321
84236  deg
 ZDOT =      -2882
497257                 TA   =          114
34763
                                          MA   =          114
26082
                                          Ha   =            195
036  n
mi
                                          Hp   =            191
316

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -872607
95                 X    =         -343116
93
 Y    =       16056656
60  feet           Y    =         4890662
90  meter
 Z    =       15155412
07                 Z    =         4617890
63
 XDOT =     -22074
386607                 XDOT =       -6740
194953
 YDOT =       7752
864593  feet/sec       YDOT =        2287
767294  meter/sec
 ZDOT =      -9457
011997                 ZDOT =       -2915
211128

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12798772
11                 X    =        -3901065
74
 Y    =        9743437
73  feet           Y    =         2969799
82  meter
 Z    =       15149951
63                 Z    =         4617705
26
 XDOT =     -19526
555942                 XDOT =       -5951
694251
 YDOT =     -10703
897237  feet/sec       YDOT =       -3262
547878  meter/sec
 ZDOT =      -9584
237032                 ZDOT =       -2921
275447


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   09024
56344515  
00010596  00000-0  82463-4 0  9086
2 25544  51
6424 322
1965 0008264 304
8880  55
1504 15
70555025 23362


Satellite: ISS
Catalog Number: 25544
Epoch time:      09024
56344515   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       322
1965  deg
Eccentricity:     
0008264     
Arg of perigee:   304
8880  deg
Mean anomaly:      55
1504  deg
Mean motion:   15
70555025  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2336
Checksum:              298


Coasting Arc #10 (Orbit 2351)
---------------------------------------

Vector Time (GMT): 2009/025/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5518481
88                 A    =         6740935
49  meter
 Y    =       -3554552
54  meter          E    =           
0013173
 Z    =        1494609
22                 I    =           51
43314
 XDOT =       1559
481147                 Wp   =           26
38368
 YDOT =       4851
428136  meter/sec      RA   =          316
75374  deg
 ZDOT =       5772
061910                 TA   =          350
11198
                                          MA   =          350
13788
                                          Ha   =            195
119  n
mi
                                          Hp   =            191
068

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18105255
50                 X    =         5550558
99
 Y    =      -11661917
77  feet           Y    =        -3492662
44  meter
 Z    =        4903573
55                 Z    =         1521494
89
 XDOT =       5116
407964                 XDOT =        1477
076916
 YDOT =      15916
758977  feet/sec       YDOT =        4868
405951  meter/sec
 ZDOT =      18937
210991                 ZDOT =        5779
437896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20731178
00                 X    =         6318863
05
 Y    =        5743126
13  feet           Y    =         1750504
85  meter
 Z    =        5008033
29                 Z    =         1526448
55
 XDOT =      -8137
449723                 XDOT =       -2480
294676
 YDOT =      12813
464913  feet/sec       YDOT =        3905
544106  meter/sec
 ZDOT =      18966
231616                 ZDOT =        5780
907397


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   09025
58149668  
00010596  00000-0  82463-4 0  9092
2 25544  51
6425 316
9946 0008328 308
9704  51
0715 15
70575315 23525


Satellite: ISS
Catalog Number: 25544
Epoch time:      09025
58149668   =   yrday
fracday
Element set:     909
Inclination:       51
6425  deg
RA of node:       316
9946  deg
Eccentricity:     
0008328     
Arg of perigee:   308
9704  deg
Mean anomaly:      51
0715  deg
Mean motion:   15
70575315  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2352
Checksum:              327


Coasting Arc #11 (Orbit 2366)
---------------------------------------

Vector Time (GMT): 2009/026/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2789235
47                 A    =         6729850
05  meter
 Y    =       -3171905
47  meter          E    =           
0009883
 Z    =       -5246477
94                 I    =           51
37617
 XDOT =       5369
525195                 Wp   =           61
87582
 YDOT =      -5484
595978  meter/sec      RA   =          311
60942  deg
 ZDOT =        466
467376                 TA   =          212
54698
                                          MA   =          212
60794
                                          Ha   =            195
232  n
mi
                                          Hp   =            190
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9151035
02                 X    =        -2728073
70
 Y    =      -10406514
01  feet           Y    =        -3202754
03  meter
 Z    =      -17212854
14                 Z    =        -5259879
29
 XDOT =      17616
552476                 XDOT =        5428
189831
 YDOT =     -17994
081294  feet/sec       YDOT =       -5424
222848  meter/sec
 ZDOT =       1530
404776                 ZDOT =         492
693942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1515827
91                 X    =          462024
35
 Y    =      -13708872
54  feet           Y    =        -4178464
35  meter
 Z    =      -17265236
84                 Z    =        -5262444
19
 XDOT =      24164
746832                 XDOT =        7365
414834
 YDOT =        638
011907  feet/sec       YDOT =         194
466029  meter/sec
 ZDOT =       1632
172090                 ZDOT =         497
486053


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   09026
53590543  
00010596  00000-0  82463-4 0  9102
2 25544  51
6431 312
1185 0008312 312
5395  47
5064 15
70613122 23677


Satellite: ISS
Catalog Number: 25544
Epoch time:      09026
53590543   =   yrday
fracday
Element set:     910
Inclination:       51
6431  deg
RA of node:       312
1185  deg
Eccentricity:     
0008312     
Arg of perigee:   312
5395  deg
Mean anomaly:      47
5064  deg
Mean motion:   15
70613122  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2367
Checksum:              279


Coasting Arc #12 (Orbit 2382)
---------------------------------------

Vector Time (GMT): 2009/027/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3537973
32                 A    =         6741634
47  meter
 Y    =        5696142
75  meter          E    =           
0005236
 Z    =         678613
26                 I    =           51
39724
 XDOT =      -4417
394355                 Wp   =          115
43390
 YDOT =      -2029
625093  meter/sec      RA   =          306
47953  deg
 ZDOT =      -5960
375638                 TA   =           57
16343
                                          MA   =           57
11303
                                          Ha   =            195
438  n
mi
                                          Hp   =            190
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11607524
02                 X    =        -3604702
07
 Y    =       18688132
40  feet           Y    =         5656205
96  meter
 Z    =        2226421
45                 Z    =          661264
40
 XDOT =     -14492
763632                 XDOT =       -4365
416841
 YDOT =      -6658
874978  feet/sec       YDOT =       -2078
732121  meter/sec
 ZDOT =     -19555
038182                 ZDOT =       -5981
708554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21542271
63                 X    =        -6566084
39
 Y    =        4495115
27  feet           Y    =         1370111
13  meter
 Z    =        2159243
02                 Z    =          658137
27
 XDOT =      -4782
039479                 XDOT =       -1457
565633
 YDOT =     -13429
435898  feet/sec       YDOT =       -4093
292062  meter/sec
 ZDOT =     -19638
235421                 ZDOT =       -5985
734156


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   09027
55392739  
00010596  00000-0  82463-4 0  9113
2 25544  51
6431 306
9170 0008274 315
9930  44
0572 15
70615406 23832


Satellite: ISS
Catalog Number: 25544
Epoch time:      09027
55392739   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:       306
9170  deg
Eccentricity:     
0008274     
Arg of perigee:   315
9930  deg
Mean anomaly:      44
0572  deg
Mean motion:   15
70615406  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2383
Checksum:              305

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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