Date: January 22nd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 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 2288)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4052005
36                 A    =         6732028
62  meter
 Y    =        2435882
38  meter          E    =           
0001652
 Z    =        4794020
11                 I    =           51
49956
 XDOT =      -5685
946502                 Wp   =          256
68714
 YDOT =       4540
265998  meter/sec      RA   =          337
24860  deg
 ZDOT =       2499
279423                 TA   =          168
78940
                                          MA   =          168
78572
                                          Ha   =            194
445  n
mi
                                          Hp   =            192
048

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13293980
83                 X    =         4001177
60
 Y    =        7991740
10  feet           Y    =         2480909
55  meter
 Z    =       15728412
43                 Z    =         4813581
29
 XDOT =     -18654
680126                 XDOT =       -5748
434795
 YDOT =      14895
885820  feet/sec       YDOT =        4476
332789  meter/sec
 ZDOT =       8199
735640                 ZDOT =        2471
506175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1762930
89                 X    =          537341
34
 Y    =       15332453
34  feet           Y    =         4673331
78  meter
 Z    =       15804706
36                 Z    =         4817274
50
 XDOT =     -22109
097080                 XDOT =       -6738
852790
 YDOT =      -5797
839042  feet/sec       YDOT =       -1767
181340  meter/sec
 ZDOT =       8091
882002                 ZDOT =        2466
405634


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
57283020  
00010596  00000-0  82463-4 0  9009
2 25544  51
6410 337
4783 0008375 292
8803  67
1474 15
70526653 22899


Satellite: ISS
Catalog Number: 25544
Epoch time:      09021
57283020   =   yrday
fracday
Element set:     900
Inclination:       51
6410  deg
RA of node:       337
4783  deg
Eccentricity:     
0008375     
Arg of perigee:   292
8803  deg
Mean anomaly:      67
1474  deg
Mean motion:   15
70526653  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2289
Checksum:              308


Coasting Arc #2 (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    =        3576792
40                 A    =         6737868
32  meter
 Y    =       -4746281
37  meter          E    =           
0005676
 Z    =       -3166528
41                 I    =           51
49179
 XDOT =       5879
269902                 Wp   =          327
89325
 YDOT =       1219
607281  meter/sec      RA   =          332
08508  deg
 ZDOT =       4813
726931                 TA   =          355
17143
                                          MA   =          355
17690
                                          Ha   =            194
834  n
mi
                                          Hp   =            191
847

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11734883
20                 X    =         3644982
42
 Y    =      -15571789
27  feet           Y    =        -4705901
98  meter
 Z    =      -10388872
72                 Z    =        -3148987
54
 XDOT =      19288
943249                 XDOT =        5841
811287
 YDOT =       4001
336224  feet/sec       YDOT =        1285
142715  meter/sec
 ZDOT =      15793
067358                 ZDOT =        4842
197080

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19526972
60                 X    =         5951821
25
 Y    =        -542102
81  feet           Y    =         -165232
93  meter
 Z    =      -10320864
64                 Z    =        -3145799
54
 XDOT =       8850
315394                 XDOT =        2697
576132
 YDOT =      16055
463221  feet/sec       YDOT =        4893
705190  meter/sec
 ZDOT =      15903
976589                 ZDOT =        4847
532064


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
52729661  
00010596  00000-0  82463-4 0  9012
2 25544  51
6407 332
6017 0008384 297
5831  62
4478 15
70499144 23049


Satellite: ISS
Catalog Number: 25544
Epoch time:      09022
52729661   =   yrday
fracday
Element set:     901
Inclination:       51
6407  deg
RA of node:       332
6017  deg
Eccentricity:     
0008384     
Arg of perigee:   297
5831  deg
Mean anomaly:      62
4478  deg
Mean motion:   15
70499144  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2304
Checksum:              311


Coasting Arc #3 (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    =       -5772741
03                 A    =         6736790
11  meter
 Y    =         477992
63  meter          E    =           
0005125
 Z    =       -3442595
84                 I    =           51
46441
 XDOT =       2241
143581                 Wp   =          336
45860
 YDOT =      -5778
017255  meter/sec      RA   =          327
01487  deg
 ZDOT =      -4553
381379                 TA   =          244
32025
                                          MA   =          244
37319
                                          Ha   =            194
896  n
mi
                                          Hp   =            191
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18939439
08                 X    =        -5760933
83
 Y    =        1568217
30  feet           Y    =          413504
88  meter
 Z    =      -11294605
76                 Z    =        -3470610
49
 XDOT =       7352
833272                 XDOT =        2327
706788
 YDOT =     -18956
749524  feet/sec       YDOT =       -5752
471005  meter/sec
 ZDOT =     -14938
915284                 ZDOT =       -4542
284489

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13266629
39                 X    =        -4043668
64
 Y    =      -13516034
50  feet           Y    =        -4119687
32  meter
 Z    =      -11403645
61                 Z    =        -3475831
18
 XDOT =      18349
628064                 XDOT =        5592
966634
 YDOT =      -5423
977885  feet/sec       YDOT =       -1653
228459  meter/sec
 ZDOT =     -14896
057521                 ZDOT =       -4540
318332


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
54537858  
00010596  00000-0  82463-4 0  9021
2 25544  51
6416 327
4003 0008329 301
7671  58
2678 15
70548313 23201


Satellite: ISS
Catalog Number: 25544
Epoch time:      09023
54537858   =   yrday
fracday
Element set:     902
Inclination:       51
6416  deg
RA of node:       327
4003  deg
Eccentricity:     
0008329     
Arg of perigee:   301
7671  deg
Mean anomaly:      58
2678  deg
Mean motion:   15
70548313  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2320
Checksum:              302


Coasting Arc #4 (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    =        -265602
19                 A    =         6732774
03  meter
 Y    =        4893930
64  meter          E    =           
0008394
 Z    =        4619584
01                 I    =           51
42681
 XDOT =      -6728
414517                 Wp   =            4
26003
 YDOT =       2363
279598  meter/sec      RA   =          321
84517  deg
 ZDOT =      -2881
904969                 TA   =          114
41974
                                          MA   =          114
33213
                                          Ha   =            195
070  n
mi
                                          Hp   =            191
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -871398
27                 X    =         -342747
74
 Y    =       16056202
90  feet           Y    =         4890528
74  meter
 Z    =       15156115
51                 Z    =         4618106
83
 XDOT =     -22074
850778                 XDOT =       -6740
341608
 YDOT =       7753
541988  feet/sec       YDOT =        2287
972152  meter/sec
 ZDOT =      -9455
068795                 ZDOT =       -2914
619540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12797641
95                 X    =        -3900721
27
 Y    =        9744055
84  feet           Y    =         2969988
22  meter
 Z    =       15150662
04                 Z    =         4617921
79
 XDOT =     -19527
334425                 XDOT =       -5951
931533
 YDOT =     -10703
898262  feet/sec       YDOT =       -3262
548190  meter/sec
 ZDOT =      -9582
296547                 ZDOT =       -2920
683988


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
56344629  
00010596  00000-0  82463-4 0  9037
2 25544  51
6417 322
1994 0008314 305
3354  54
7030 15
70553638 23361


Satellite: ISS
Catalog Number: 25544
Epoch time:      09024
56344629   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:       322
1994  deg
Eccentricity:     
0008314     
Arg of perigee:   305
3354  deg
Mean anomaly:      54
7030  deg
Mean motion:   15
70553638  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2336
Checksum:              298


Coasting Arc #5 (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    =        5518317
96                 A    =         6740944
58  meter
 Y    =       -3555211
22  meter          E    =           
0013250
 Z    =        1493438
95                 I    =           51
43234
 XDOT =       1560
761760                 Wp   =           26
21594
 YDOT =       4850
668385  meter/sec      RA   =          316
75646  deg
 ZDOT =       5772
431665                 TA   =          350
26674
                                          MA   =          350
29239
                                          Ha   =            195
156  n
mi
                                          Hp   =            191
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18104717
73                 X    =         5550408
14
 Y    =      -11664078
81  feet           Y    =        -3493322
88  meter
 Z    =        4899734
10                 Z    =         1520323
86
 XDOT =       5120
609450                 XDOT =        1478
364133
 YDOT =      15914
266356  feet/sec       YDOT =        4867
660557  meter/sec
 ZDOT =      18938
424099                 ZDOT =        5779
813888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20732448
91                 X    =         6319250
43
 Y    =        5741303
79  feet           Y    =         1749949
40  meter
 Z    =        5004190
83                 Z    =         1525277
37
 XDOT =      -8132
931578                 XDOT =       -2478
917545
 YDOT =      12814
846739  feet/sec       YDOT =        3905
965286  meter/sec
 ZDOT =      18967
468961                 ZDOT =        5781
284539


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
58149910  
00010596  00000-0  82463-4 0  9047
2 25544  51
6418 316
9975 0008378 309
4231  50
6188 15
70572686 23522


Satellite: ISS
Catalog Number: 25544
Epoch time:      09025
58149910   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:       316
9975  deg
Eccentricity:     
0008378     
Arg of perigee:   309
4231  deg
Mean anomaly:      50
6188  deg
Mean motion:   15
70572686  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2352
Checksum:              329


Coasting Arc #6 (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    =       -2791238
58                 A    =         6729860
31  meter
 Y    =       -3169955
64  meter          E    =           
0009933
 Z    =       -5246607
73                 I    =           51
37535
 XDOT =       5368
393713                 Wp   =           61
44380
 YDOT =      -5485
912863  meter/sec      RA   =          311
61210  deg
 ZDOT =        463
850332                 TA   =          212
95352
                                          MA   =          213
01548
                                          Ha   =            195
271  n
mi
                                          Hp   =            190
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9157606
89                 X    =        -2730097
83
 Y    =      -10400116
92  feet           Y    =        -3200826
72  meter
 Z    =      -17213279
97                 Z    =        -5260018
86
 XDOT =      17612
840265                 XDOT =        5427
085872
 YDOT =     -17998
401783  feet/sec       YDOT =       -5425
552232  meter/sec
 ZDOT =       1521
818676                 ZDOT =         490
071469

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1506671
79                 X    =          459233
56
 Y    =      -13709366
33  feet           Y    =        -4178614
86  meter
 Z    =      -17265700
63                 Z    =        -5262585
55
 XDOT =      24165
404789                 XDOT =        7365
615380
 YDOT =        633
058135  feet/sec       YDOT =         192
956119  meter/sec
 ZDOT =       1623
564768                 ZDOT =         494
862541


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
53590980  
00010596  00000-0  82463-4 0  9051
2 25544  51
6424 312
1212 0008363 313
0015  47
0445 15
70609316 23679


Satellite: ISS
Catalog Number: 25544
Epoch time:      09026
53590980   =   yrday
fracday
Element set:     905
Inclination:       51
6424  deg
RA of node:       312
1212  deg
Eccentricity:     
0008363     
Arg of perigee:   313
0015  deg
Mean anomaly:      47
0445  deg
Mean motion:   15
70609316  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2367
Checksum:              280


Coasting Arc #7 (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    =       -3535565
95                 A    =         6741646
56  meter
 Y    =        5697284
21  meter          E    =           
0005219
 Z    =         682242
76                 I    =           51
39640
 XDOT =      -4420
150040                 Wp   =          114
43805
 YDOT =      -2025
315577  meter/sec      RA   =          306
48210  deg
 ZDOT =      -5959
707459                 TA   =           58
11945
                                          MA   =           58
06868
                                          Ha   =            195
479  n
mi
                                          Hp   =            190
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11599625
81                 X    =        -3602325
27
 Y    =       18691877
32  feet           Y    =         5657374
16  meter
 Z    =        2238329
27                 Z    =          664905
53
 XDOT =     -14501
804592                 XDOT =       -4368
223756
 YDOT =      -6644
736145  feet/sec       YDOT =       -2074
453707  meter/sec
 ZDOT =     -19552
845993                 ZDOT =       -5981
053886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21539575
80                 X    =        -6565262
70
 Y    =        4503364
96  feet           Y    =         1372625
64  meter
 Z    =        2171196
16                 Z    =          661780
59
 XDOT =      -4797
916972                 XDOT =       -1462
405093
 YDOT =     -13426
421171  feet/sec       YDOT =       -4092
373173  meter/sec
 ZDOT =     -19636
095560                 ZDOT =       -5985
081927


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
55393461  
00010596  00000-0  82463-4 0  9060
2 25544  51
6424 306
9197 0008326 316
4703  43
5800 15
70610427 23831


Satellite: ISS
Catalog Number: 25544
Epoch time:      09027
55393461   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:       306
9197  deg
Eccentricity:     
0008326     
Arg of perigee:   316
4703  deg
Mean anomaly:      43
5800  deg
Mean motion:   15
70610427  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2383
Checksum:              301


Coasting Arc #8 (Orbit 2398)
---------------------------------------

Vector Time (GMT): 2009/028/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4546140
58                 A    =         6730923
87  meter
 Y    =         165937
41  meter          E    =           
0003195
 Z    =        4960411
28                 I    =           51
34415
 XDOT =      -2422
901168                 Wp   =          350
07355
 YDOT =       7028
514606  meter/sec      RA   =          301
37553  deg
 ZDOT =       1988
722497                 TA   =           80
62013
                                          MA   =           80
58401
                                          Ha   =            195
473  n
mi
                                          Hp   =            190
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14915159
37                 X    =         4519851
01
 Y    =         544414
06  feet           Y    =          216627
92  meter
 Z    =       16274315
23                 Z    =         4982432
00
 XDOT =      -7949
150813                 XDOT =       -2510
975705
 YDOT =      23059
431122  feet/sec       YDOT =        7000
927838  meter/sec
 ZDOT =       6524
680108                 ZDOT =        1976
738530

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10027506
34                 X    =         3056383
93
 Y    =       10927440
42  feet           Y    =         3330683
84  meter
 Z    =       16360069
21                 Z    =         4986549
09
 XDOT =     -21221
681980                 XDOT =       -6468
368668
 YDOT =       9790
740958  feet/sec       YDOT =        2984
217844  meter/sec
 ZDOT =       6478
489727                 ZDOT =        1974
643669


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   09028
57194366  
00010596  00000-0  82463-4 0  9077
2 25544  51
6421 301
7178 0008388 320
3518  39
7030 15
70658163 23994


Satellite: ISS
Catalog Number: 25544
Epoch time:      09028
57194366   =   yrday
fracday
Element set:     907
Inclination:       51
6421  deg
RA of node:       301
7178  deg
Eccentricity:     
0008388     
Arg of perigee:   320
3518  deg
Mean anomaly:      39
7030  deg
Mean motion:   15
70658163  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2399
Checksum:              321


Coasting Arc #9 (Orbit 2413)
---------------------------------------

Vector Time (GMT): 2009/029/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         588068
38                 A    =         6738425
67  meter
 Y    =       -6128453
97  meter          E    =           
0009501
 Z    =       -2724848
25                 I    =           51
35553
 XDOT =       5449
967548                 Wp   =          354
36116
 YDOT =      -1760
405950  meter/sec      RA   =          296
20581  deg
 ZDOT =       5143
316094                 TA   =          334
42822
                                          MA   =          334
47518
                                          Ha   =            195
697  n
mi
                                          Hp   =            190
045

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1929358
20                 X    =          669790
57
 Y    =      -20106476
28  feet           Y    =        -6121420
92  meter
 Z    =       -8939790
84                 Z    =        -2721792
97
 XDOT =      17880
470958                 XDOT =        5444
262917
 YDOT =      -5775
610073  feet/sec       YDOT =       -1699
493135  meter/sec
 ZDOT =      16874
396634                 ZDOT =        5169
777577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15476140
19                 X    =         4717127
53
 Y    =      -12987953
86  feet           Y    =        -3958728
34  meter
 Z    =       -8928315
13                 Z    =        -2721350
45
 XDOT =      15803
589670                 XDOT =        4816
934132
 YDOT =       7178
065044  feet/sec       YDOT =        2187
874226  meter/sec
 ZDOT =      16977
309350                 ZDOT =        5174
683890


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   09029
52631494  
00010596  00000-0  82463-4 0  9082
2 25544  51
6424 296
8410 0008459 324
0807  35
9784 15
70680968 24141


Satellite: ISS
Catalog Number: 25544
Epoch time:      09029
52631494   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       296
8410  deg
Eccentricity:     
0008459     
Arg of perigee:   324
0807  deg
Mean anomaly:      35
9784  deg
Mean motion:   15
70680968  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2414
Checksum:              333


Coasting Arc #10 (Orbit 2429)
---------------------------------------

Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4531133
18                 A    =         6735088
39  meter
 Y    =        3167311
46  meter          E    =           
0009183
 Z    =       -3855516
47                 I    =           51
33257
 XDOT =      -1016
901133                 Wp   =           10
21105
 YDOT =      -6433
709047  meter/sec      RA   =          291
12324  deg
 ZDOT =      -4082
788738                 TA   =          216
89685
                                          MA   =          216
96006
                                          Ha   =            195
861  n
mi
                                          Hp   =            189
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14865922
51                 X    =        -4547484
76
 Y    =       10391441
81  feet           Y    =         3116550
24  meter
 Z    =      -12649332
26                 Z    =        -3877568
06
 XDOT =      -3336
289808                 XDOT =        -925
049673
 YDOT =     -21107
969314  feet/sec       YDOT =       -6444
567097  meter/sec
 ZDOT =     -13394
976175                 ZDOT =       -4087
505588

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17888501
48                 X    =        -5452415
25
 Y    =       -2608696
08  feet           Y    =         -795130
57  meter
 Z    =      -12734973
16                 Z    =        -3881619
82
 XDOT =      11939
964497                 XDOT =        3639
301179
 YDOT =     -16274
832678  feet/sec       YDOT =       -4960
569000  meter/sec
 ZDOT =     -13413
791554                 ZDOT =       -4088
523666


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   09030
54429653  
00010596  00000-0  82463-4 0  9099
2 25544  51
6423 291
6391 0008575 327
3894  32
6737 15
70693710 24301


Satellite: ISS
Catalog Number: 25544
Epoch time:      09030
54429653   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:       291
6391  deg
Eccentricity:     
0008575     
Arg of perigee:   327
3894  deg
Mean anomaly:      32
6737  deg
Mean motion:   15
70693710  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2430
Checksum:              320


Coasting Arc #11 (Orbit 2445)
---------------------------------------

Vector Time (GMT): 2009/031/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2212161
01                 A    =         6733505
18  meter
 Y    =        4712207
12  meter          E    =           
0011842
 Z    =        4273082
61                 I    =           51
31784
 XDOT =      -4407
253036                 Wp   =           26
08101
 YDOT =       5248
952887  meter/sec      RA   =          285
93973  deg
 ZDOT =      -3492
580983                 TA   =           99
55057
                                          MA   =           99
41673
                                          Ha   =            195
962  n
mi
                                          Hp   =            189
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7257746
09                 X    =         2138546
34
 Y    =       15459997
11  feet           Y    =         4736533
22  meter
 Z    =       14019299
90                 Z    =         4283650
29
 XDOT =     -14459
491589                 XDOT =       -4448
654048
 YDOT =      17220
974039  feet/sec       YDOT =        5199
436912  meter/sec
 ZDOT =     -11458
599024                 ZDOT =       -3514
091720

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5124517
26                 X    =        -1561952
86
 Y    =       16256104
47  feet           Y    =         4954860
64  meter
 Z    =       14060780
52                 Z    =         4285725
90
 XDOT =     -21055
249281                 XDOT =       -6417
639981
 YDOT =       3385
968983  feet/sec       YDOT =        1032
043346  meter/sec
 ZDOT =     -11541
983716                 ZDOT =       -3517
996637


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   09031
56226377  
00010596  00000-0  82463-4 0  9102
2 25544  51
6419 286
4365 0008657 331
6770  28
3920 15
70745573 24469


Satellite: ISS
Catalog Number: 25544
Epoch time:      09031
56226377   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       286
4365  deg
Eccentricity:     
0008657     
Arg of perigee:   331
6770  deg
Mean anomaly:      28
3920  deg
Mean motion:   15
70745573  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2446
Checksum:              321


Coasting Arc #12 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2009/032/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 639525
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2833580
03                 A    =         6739518
50  meter
 Y    =       -5718835
06  meter          E    =           
0015822
 Z    =        2132383
33                 I    =           51
33089
 XDOT =       3730
158913                 Wp   =           37
21505
 YDOT =       3900
535407  meter/sec      RA   =          280
84949  deg
 ZDOT =       5495
269135                 TA   =          346
73044
                                          MA   =          346
77201
                                          Ha   =            196
092  n
mi
                                          Hp   =            189
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9296522
39                 X    =         2886959
76
 Y    =      -18762582
21  feet           Y    =        -5686849
87  meter
 Z    =        6996008
32                 Z    =         2146278
36
 XDOT =      12238
054177                 XDOT =        3659
570498
 YDOT =      12797
032175  feet/sec       YDOT =        3941
853506  meter/sec
 ZDOT =      18029
098211                 ZDOT =        5513
218620

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19352624
94                 X    =         5898680
08
 Y    =       -7948681
36  feet           Y    =        -2422758
08  meter
 Z    =        7049703
87                 Z    =         2148749
74
 XDOT =         55
357199                 XDOT =          16
872874
 YDOT =      16212
510505  feet/sec       YDOT =        4941
573202  meter/sec
 ZDOT =      18099
266691                 ZDOT =        5516
656487


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   09032
58021828  
00010596  00000-0  82463-4 0  9110
2 25544  51
6418 281
2334 0008697 335
4820  24
5927 15
70724106 24621


Satellite: ISS
Catalog Number: 25544
Epoch time:      09032
58021828   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:       281
2334  deg
Eccentricity:     
0008697     
Arg of perigee:   335
4820  deg
Mean anomaly:      24
5927  deg
Mean motion:   15
70724106  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2462
Checksum:              301

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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