Date: January 29th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9526 06 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


035/08:30:34 844 -2 4 4 6 4 6
N/A -2 8 -0 0 196 4
000/00:01:05 688 -2 8 0 0 191 3

Coasting Arc #1 (Orbit 2398)
---------------------------------------

Vector Time (GMT): 2009/028/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4553471
82                 A    =         6730966
57  meter
 Y    =         144966
60  meter          E    =           
0003121
 Z    =        4954372
75                 I    =           51
34488
 XDOT =      -2405
630986                 Wp   =          350
62136
 YDOT =       7028
815073  meter/sec      RA   =          301
38255  deg
 ZDOT =       2008
516687                 TA   =           79
87195
                                          MA   =           79
83675
                                          Ha   =            195
463  n
mi
                                          Hp   =            190
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14939211
99                 X    =         4527445
54
 Y    =         475612
22  feet           Y    =          195740
58  meter
 Z    =       16254503
78                 Z    =         4976429
72
 XDOT =      -7892
490111                 XDOT =       -2493
806320
 YDOT =      23060
416905  feet/sec       YDOT =        7001
420866  meter/sec
 ZDOT =       6589
621675                 ZDOT =        1996
616372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10093439
21                 X    =         3076480
27
 Y    =       10896286
02  feet           Y    =         3321187
98  meter
 Z    =       16340397
51                 Z    =         4980553
16
 XDOT =     -21185
103215                 XDOT =       -6457
219460
 YDOT =       9826
671575  feet/sec       YDOT =        2995
169496  meter/sec
 ZDOT =       6543
757021                 ZDOT =        1994
537140


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
57197910  
00010596  00000-0  82463-4 0  9008
2 25544  51
6428 301
7247 0008353 320
1051  39
9496 15
70652307 23992


Satellite: ISS
Catalog Number: 25544
Epoch time:      09028
57197910   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:       301
7247  deg
Eccentricity:     
0008353     
Arg of perigee:   320
1051  deg
Mean anomaly:      39
9496  deg
Mean motion:   15
70652307  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2399
Checksum:              310


Coasting Arc #2 (Orbit 2413)
---------------------------------------

Vector Time (GMT): 2009/029/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         570485
17                 A    =         6738401
69  meter
 Y    =       -6122442
44  meter          E    =           
0009386
 Z    =       -2742175
74                 I    =           51
35603
 XDOT =       5452
647780                 Wp   =          354
28198
 YDOT =      -1786
724387  meter/sec      RA   =          296
21272  deg
 ZDOT =       5131
275026                 TA   =          334
28692
                                          MA   =          334
33355
                                          Ha   =            195
687  n
mi
                                          Hp   =            190
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1871670
51                 X    =          652225
62
 Y    =      -20086753
41  feet           Y    =        -6115605
91  meter
 Z    =       -8996639
57                 Z    =        -2739205
84
 XDOT =      17889
264370                 XDOT =        5447
295739
 YDOT =      -5861
956649  feet/sec       YDOT =       -1725
779628  meter/sec
 ZDOT =      16834
891816                 ZDOT =        5157
750385

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15421345
91                 X    =         4700426
23
 Y    =      -13013965
22  feet           Y    =        -3966656
60  meter
 Z    =       -8985495
86                 Z    =        -2738779
14
 XDOT =      15868
522274                 XDOT =        4836
725589
 YDOT =       7126
643986  feet/sec       YDOT =        2172
201087  meter/sec
 ZDOT =      16937
856762                 ZDOT =        5162
658741


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
52635394  
00010596  00000-0  82463-4 0  9018
2 25544  51
6431 296
8480 0008425 323
8345  36
2246 15
70674931 24143


Satellite: ISS
Catalog Number: 25544
Epoch time:      09029
52635394   =   yrday
fracday
Element set:     901
Inclination:       51
6431  deg
RA of node:       296
8480  deg
Eccentricity:     
0008425     
Arg of perigee:   323
8345  deg
Mean anomaly:      36
2246  deg
Mean motion:   15
70674931  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2414
Checksum:              311


Coasting Arc #3 (Orbit 2429)
---------------------------------------

Vector Time (GMT): 2009/030/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4527657
24                 A    =         6735158
34  meter
 Y    =        3190623
85  meter          E    =           
0009072
 Z    =       -3840358
75                 I    =           51
33338
 XDOT =      -1037
962089                 Wp   =            9
90170
 YDOT =      -6418
481492  meter/sec      RA   =          291
13039  deg
 ZDOT =      -4101
476071                 TA   =          216
96354
                                          MA   =          217
02608
                                          Ha   =            195
852  n
mi
                                          Hp   =            189
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14854518
51                 X    =        -4544343
40
 Y    =       10467926
00  feet           Y    =         3139899
62  meter
 Z    =      -12599602
19                 Z    =        -3862394
26
 XDOT =      -3405
387430                 XDOT =        -946
188562
 YDOT =     -21058
010145  feet/sec       YDOT =       -6429
575494  meter/sec
 ZDOT =     -13456
286321                 ZDOT =       -4106
295422

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17932957
74                 X    =        -5465965
52
 Y    =       -2545473
20  feet           Y    =         -775860
23  meter
 Z    =      -12685178
88                 Z    =        -3866442
52
 XDOT =      11860
298954                 XDOT =        3615
019121
 YDOT =     -16282
500446  feet/sec       YDOT =       -4962
906136  meter/sec
 ZDOT =     -13475
499738                 ZDOT =       -4107
332320


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
54433960  
00010596  00000-0  82463-4 0  9028
2 25544  51
6430 291
6462 0008541 327
1357  32
9272 15
70686983 24304


Satellite: ISS
Catalog Number: 25544
Epoch time:      09030
54433960   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:       291
6462  deg
Eccentricity:     
0008541     
Arg of perigee:   327
1357  deg
Mean anomaly:      32
9272  deg
Mean motion:   15
70686983  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2430
Checksum:              302


Coasting Arc #4 (Orbit 2445)
---------------------------------------

Vector Time (GMT): 2009/031/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2229549
57                 A    =         6733469
99  meter
 Y    =        4690949
00  meter          E    =           
0011791
 Z    =        4287368
64                 I    =           51
31830
 XDOT =      -4396
034207                 Wp   =           25
71211
 YDOT =       5273
458502  meter/sec      RA   =          285
94707  deg
 ZDOT =      -3469
753787                 TA   =           99
65154
                                          MA   =           99
51831
                                          Ha   =            195
953  n
mi
                                          Hp   =            189
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7314795
18                 X    =         2156101
93
 Y    =       15390252
64  feet           Y    =         4715470
49  meter
 Z    =       14066170
09                 Z    =         4298021
21
 XDOT =     -14422
684407                 XDOT =       -4437
820967
 YDOT =      17301
373039  feet/sec       YDOT =        5224
065826  meter/sec
 ZDOT =     -11383
706651                 ZDOT =       -3491
210962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5035561
33                 X    =        -1534839
09
 Y    =       16242883
88  feet           Y    =         4950831
01  meter
 Z    =       14107979
70                 Z    =         4300112
21
 XDOT =     -21083
563122                 XDOT =       -6426
270039
 YDOT =       3463
382248  feet/sec       YDOT =        1055
638909  meter/sec
 ZDOT =     -11466
881059                 ZDOT =       -3495
105347


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
56231115  
00010596  00000-0  82463-4 0  9030
2 25544  51
6426 286
4438 0008625 331
4286  28
6401 15
70739152 24466


Satellite: ISS
Catalog Number: 25544
Epoch time:      09031
56231115   =   yrday
fracday
Element set:     903
Inclination:       51
6426  deg
RA of node:       286
4438  deg
Eccentricity:     
0008625     
Arg of perigee:   331
4286  deg
Mean anomaly:      28
6401  deg
Mean motion:   15
70739152  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2446
Checksum:              296


Coasting Arc #5 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2009/032/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2817576
08                 A    =         6739583
95  meter
 Y    =       -5735901
69  meter          E    =           
0015828
 Z    =        2107817
27                 I    =           51
33168
 XDOT =       3746
132043                 Wp   =           37
01952
 YDOT =       3867
436710  meter/sec      RA   =          280
85671  deg
 ZDOT =       5507
729632                 TA   =          346
63265
                                          MA   =          346
67453
                                          Ha   =            196
084  n
mi
                                          Hp   =            189
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9244016
02                 X    =         2871267
18
 Y    =      -18818575
09  feet           Y    =        -5704093
72  meter
 Z    =        6915410
98                 Z    =         2121635
30
 XDOT =      12290
459460                 XDOT =        3675
852026
 YDOT =      12688
440650  feet/sec       YDOT =        3908
935155  meter/sec
 ZDOT =      18069
979106                 ZDOT =        5525
757462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19350634
51                 X    =         5898073
40
 Y    =       -8025098
33  feet           Y    =        -2446049
97  meter
 Z    =        6968805
55                 Z    =         2124091
93
 XDOT =        160
739751                 XDOT =          48
993476
 YDOT =      16165
723905  feet/sec       YDOT =        4927
312646  meter/sec
 ZDOT =      18140
450276                 ZDOT =        5529
209244


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
58027025  
00010596  00000-0  82463-4 0  9047
2 25544  51
6425 281
2408 0008663 335
2365  24
8380 15
70717223 24624


Satellite: ISS
Catalog Number: 25544
Epoch time:      09032
58027025   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:       281
2408  deg
Eccentricity:     
0008663     
Arg of perigee:   335
2365  deg
Mean anomaly:      24
8380  deg
Mean motion:   15
70717223  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2462
Checksum:              291


Coasting Arc #6 (Orbit 2476)
---------------------------------------

Vector Time (GMT): 2009/033/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3958759
12                 A    =         6729864
30  meter
 Y    =       -1811367
67  meter          E    =           
0012139
 Z    =       -5140290
65                 I    =           51
29484
 XDOT =       1750
564262                 Wp   =           62
18395
 YDOT =      -7380
083904  meter/sec      RA   =          275
69267  deg
 ZDOT =       1260
307153                 TA   =          219
89637
                                          MA   =          219
98565
                                          Ha   =            196
126  n
mi
                                          Hp   =            189
010

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12988054
86                 X    =        -3913239
49
 Y    =       -5942807
32  feet           Y    =        -1855382
18  meter
 Z    =      -16864470
65                 Z    =        -5159411
62
 XDOT =       5743
321068                 XDOT =        1826
837182
 YDOT =     -24212
873700  feet/sec       YDOT =       -7360
081644  meter/sec
 ZDOT =       4134
865989                 ZDOT =        1268
996411

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5958872
73                 X    =        -1816264
41
 Y    =      -12883212
63  feet           Y    =        -3926803
21  meter
 Z    =      -16939054
46                 Z    =        -5163023
80
 XDOT =      19115
757914                 XDOT =        5826
483012
 YDOT =     -14288
268674  feet/sec       YDOT =       -4355
064292  meter/sec
 ZDOT =       4168
171689                 ZDOT =        1270
458731


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   09033
53459259  
00010596  00000-0  82463-4 0  9052
2 25544  51
6422 276
3633 0008678 338
0647  22
0142 15
70765435 24776


Satellite: ISS
Catalog Number: 25544
Epoch time:      09033
53459259   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       276
3633  deg
Eccentricity:     
0008678     
Arg of perigee:   338
0647  deg
Mean anomaly:      22
0142  deg
Mean motion:   15
70765435  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2477
Checksum:              318


Coasting Arc #7 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2009/034/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 640390
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -127357
86                 A    =         6741478
85  meter
 Y    =        6739569
40  meter          E    =           
0005808
 Z    =         -75327
01                 I    =           51
33196
 XDOT =      -4802
842638                 Wp   =           94
96604
 YDOT =       -153
403062  meter/sec      RA   =          270
57022  deg
 ZDOT =      -6003
395970                 TA   =           85
85397
                                          MA   =           85
78760
                                          Ha   =            196
333  n
mi
                                          Hp   =            188
988

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -417840
75                 X    =         -202345
45
 Y    =       22111448
17  feet           Y    =         6737725
94  meter
 Z    =        -247135
85                 Z    =          -76127
53
 XDOT =     -15757
357736                 XDOT =       -4771
607157
 YDOT =       -503
290885  feet/sec       YDOT =        -206
936306  meter/sec
 ZDOT =     -19696
181003                 ZDOT =       -6026
652103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14368657
22                 X    =        -4379566
72
 Y    =       16811636
22  feet           Y    =         5124186
72  meter
 Z    =        -249768
30                 Z    =          -76129
38
 XDOT =     -10535
314169                 XDOT =       -3211
163759
 YDOT =      -9279
121389  feet/sec       YDOT =       -2828
276199  meter/sec
 ZDOT =     -19786
752592                 ZDOT =       -6031
002190


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   09034
55252531  
00010596  00000-0  82463-4 0  9060
2 25544  51
6422 271
1612 0008531 341
5857  18
4994 15
70733685 24930


Satellite: ISS
Catalog Number: 25544
Epoch time:      09034
55252531   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       271
1612  deg
Eccentricity:     
0008531     
Arg of perigee:   341
5857  deg
Mean anomaly:      18
4994  deg
Mean motion:   15
70733685  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2493
Checksum:              310


Coasting Arc #8 (Orbit 2505)
---------------------------------------

Vector Time (GMT): 2009/035/08:31:07
688
Vector Time (MET): N/A
Weight (LBS)     : 640039
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2413360
01                 A    =         6738717
51  meter
 Y    =        5277485
75  meter          E    =           
0005696
 Z    =       -3431674
25                 I    =           51
31463
 XDOT =      -3956
866855                 Wp   =            5
43426
 YDOT =      -4770
082958  meter/sec      RA   =          266
31173  deg
 ZDOT =      -4548
115054                 TA   =          215
26470
                                          MA   =          215
30239
                                          Ha   =            196
438  n
mi
                                          Hp   =            191
335

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7917847
79                 X    =        -2455524
10
 Y    =       17314585
79  feet           Y    =         5250262
63  meter
 Z    =      -11258773
80                 Z    =        -3443500
29
 XDOT =     -12981
846637                 XDOT =       -3881
139254
 YDOT =     -15649
878472  feet/sec       YDOT =       -4813
907227  meter/sec
 ZDOT =     -14921
637315                 ZDOT =       -4567
153662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15992884
69                 X    =        -4874631
25
 Y    =      -10280287
30  feet           Y    =        -3133431
57  meter
 Z    =      -11304446
68                 Z    =        -3445595
35
 XDOT =      16604
789531                 XDOT =        5061
139849
 YDOT =      -9323
869775  feet/sec       YDOT =       -2841
915507  meter/sec
 ZDOT =     -14996
124139                 ZDOT =       -4570
818638


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   09035
37959474  
00010596  00000-0  82463-4 0  9072
2 25544  51
6415 266
9336 0007046 320
8407  39
2244 15
69907506 25065


Satellite: ISS
Catalog Number: 25544
Epoch time:      09035
37959474   =   yrday
fracday
Element set:     907
Inclination:       51
6415  deg
RA of node:       266
9336  deg
Eccentricity:     
0007046     
Arg of perigee:   320
8407  deg
Mean anomaly:      39
2244  deg
Mean motion:   15
69907506  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2506
Checksum:              327


Coasting Arc #9 (Orbit 2521)
---------------------------------------

Vector Time (GMT): 2009/036/08:31:07
688
Vector Time (MET): N/A
Weight (LBS)     : 640039
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4189802
08                 A    =         6734109
70  meter
 Y    =        2367223
27  meter          E    =           
0009730
 Z    =        4712421
85                 I    =           51
30185
 XDOT =      -1038
645589                 Wp   =           15
22488
 YDOT =       7144
361017  meter/sec      RA   =          261
13818  deg
 ZDOT =      -2654
918561                 TA   =          101
07670
                                          MA   =          100
96727
                                          Ha   =            196
516  n
mi
                                          Hp   =            191
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13746069
82                 X    =         4140128
30
 Y    =        7766480
54  feet           Y    =         2413797
95  meter
 Z    =       15460701
59                 Z    =         4732655
10
 XDOT =      -3407
629885                 XDOT =       -1105
560924
 YDOT =      23439
504649  feet/sec       YDOT =        7132
372349  meter/sec
 ZDOT =      -8710
362732                 ZDOT =       -2660
126178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9450223
19                 X    =        -2880428
03
 Y    =       12550604
95  feet           Y    =         3825424
39  meter
 Z    =       15539676
51                 Z    =         4736493
40
 XDOT =     -21901
957269                 XDOT =       -6675
716575
 YDOT =      -5639
765290  feet/sec       YDOT =       -1719
000460  meter/sec
 ZDOT =      -8730
123754                 ZDOT =       -2660
941720


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   09036
39808027  
00010596  00000-0  82463-4 0  9083
2 25544  51
6409 261
7353 0007102 324
4570  35
6117 15
69919331 25220


Satellite: ISS
Catalog Number: 25544
Epoch time:      09036
39808027   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       261
7353  deg
Eccentricity:     
0007102     
Arg of perigee:   324
4570  deg
Mean anomaly:      35
6117  deg
Mean motion:   15
69919331  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2522
Checksum:              303


Coasting Arc #10 (Orbit 2537)
---------------------------------------

Vector Time (GMT): 2009/037/08:31:07
688
Vector Time (MET): N/A
Weight (LBS)     : 640039
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -760427
36                 A    =         6743330
33  meter
 Y    =       -6604222
46  meter          E    =           
0015717
 Z    =        1068846
34                 I    =           51
33866
 XDOT =       4948
696392                 Wp   =           29
45789
 YDOT =        386
601882  meter/sec      RA   =          256
04122  deg
 ZDOT =       5886
303623                 TA   =          342
27171
                                          MA   =          342
32649
                                          Ha   =            196
701  n
mi
                                          Hp   =            191
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2494840
42                 X    =         -691713
48
 Y    =      -21667396
53  feet           Y    =        -6612341
89  meter
 Z    =        3506713
71                 Z    =         1065318
63
 XDOT =      16235
880550                 XDOT =        4915
411614
 YDOT =       1268
378878  feet/sec       YDOT =         441
754497  meter/sec
 ZDOT =      19312
019762                 ZDOT =        5910
263020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21812621
56                 X    =         6648487
05
 Y    =         -97154
84  feet           Y    =          -29612
80  meter
 Z    =        3492483
86                 Z    =         1064509
08
 XDOT =      -3055
613683                 XDOT =        -931
351051
 YDOT =      14293
499662  feet/sec       YDOT =        4356
658697  meter/sec
 ZDOT =      19405
373253                 ZDOT =        5914
757767


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   09037
41655351  
00010596  00000-0  82463-4 0  9098
2 25544  51
6410 256
5361 0007178 328
6110  31
4622 15
69919518 25381


Satellite: ISS
Catalog Number: 25544
Epoch time:      09037
41655351   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:       256
5361  deg
Eccentricity:     
0007178     
Arg of perigee:   328
6110  deg
Mean anomaly:      31
4622  deg
Mean motion:   15
69919518  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2538
Checksum:              309


Coasting Arc #11 (Orbit 2552)
---------------------------------------

Vector Time (GMT): 2009/038/08:31:07
688
Vector Time (MET): N/A
Weight (LBS)     : 640039
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3874779
24                 A    =         6731644
51  meter
 Y    =        1672216
37  meter          E    =           
0013511
 Z    =       -5254793
33                 I    =           51
30844
 XDOT =      -2719
288264                 Wp   =           59
23235
 YDOT =      -7183
463381  meter/sec      RA   =          250
90635  deg
 ZDOT =       -274
539884                 TA   =          208
10810
                                          MA   =          208
18111
                                          Ha   =            196
757  n
mi
                                          Hp   =            190
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12712530
32                 X    =        -3867664
17
 Y    =        5486274
17  feet           Y    =         1628926
46  meter
 Z    =      -17240135
61                 Z    =        -5273599
07
 XDOT =      -8921
549421                 XDOT =       -2637
425859
 YDOT =     -23567
793246  feet/sec       YDOT =       -7213
414307  meter/sec
 ZDOT =       -900
721403                 ZDOT =        -287
551434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4279305
83                 X    =        -1304332
42
 Y    =      -13071656
11  feet           Y    =        -3984240
78  meter
 Z    =      -17313268
18                 Z    =        -5277084
14
 XDOT =      23346
789154                 XDOT =        7116
101334
 YDOT =      -6355
070820  feet/sec       YDOT =       -1937
025586  meter/sec
 ZDOT =       -951
952094                 ZDOT =        -290
154998


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   09038
37135896  
00010596  00000-0  82463-4 0  9103
2 25544  51
6413 251
6624 0007185 332
0763  28
0012 15
69969356 25530


Satellite: ISS
Catalog Number: 25544
Epoch time:      09038
37135896   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:       251
6624  deg
Eccentricity:     
0007185     
Arg of perigee:   332
0763  deg
Mean anomaly:      28
0012  deg
Mean motion:   15
69969356  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2553
Checksum:              313


Coasting Arc #12 (Orbit 2568)
---------------------------------------

Vector Time (GMT): 2009/039/08:31:07
688
Vector Time (MET): N/A
Weight (LBS)     : 640039
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3758162
76                 A    =         6742695
19  meter
 Y    =        5385279
23  meter          E    =           
0009470
 Z    =        1521026
91                 I    =           51
35571
 XDOT =      -3276
689779                 Wp   =           90
31182
 YDOT =       3919
167307  meter/sec      RA   =          245
76271  deg
 ZDOT =      -5749
120702                 TA   =           72
89587
                                          MA   =           72
79218
                                          Ha   =            196
940  n
mi
                                          Hp   =            190
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12329930
32                 X    =         3690275
74
 Y    =       17668238
95  feet           Y    =         5426925
56  meter
 Z    =        4990245
75                 Z    =         1539118
76
 XDOT =     -10750
294550                 XDOT =       -3292
343772
 YDOT =      12858
160455  feet/sec       YDOT =        3882
438149  meter/sec
 ZDOT =     -18861
944561                 ZDOT =       -5765
076205

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18558892
31                 X    =        -5656750
37
 Y    =       10910943
67  feet           Y    =         3325655
63  meter
 Z    =        5061148
74                 Z    =         1542638
14
 XDOT =     -11209
156068                 XDOT =       -3416
550770
 YDOT =     -10241
864900  feet/sec       YDOT =       -3121
720422  meter/sec
 ZDOT =     -18923
802529                 ZDOT =       -5767
975011


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   09039
38980712  
00010596  00000-0  82463-4 0  9111
2 25544  51
6407 246
4633 0007139 335
5883  24
4939 15
69950510 25692


Satellite: ISS
Catalog Number: 25544
Epoch time:      09039
38980712   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:       246
4633  deg
Eccentricity:     
0007139     
Arg of perigee:   335
5883  deg
Mean anomaly:      24
4939  deg
Mean motion:   15
69950510  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2569
Checksum:              333


Coasting Arc #13 (Orbit 2584)
---------------------------------------

Vector Time (GMT): 2009/040/08:31:07
688
Vector Time (MET): N/A
Weight (LBS)     : 640039
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1436998
95                 A    =         6734807
21  meter
 Y    =       -4793182
87  meter          E    =           
0006517
 Z    =        4500995
30                 I    =           51
34282
 XDOT =       5393
673946                 Wp   =           58
80798
 YDOT =       4531
709864  meter/sec      RA   =          240
67370  deg
 ZDOT =       3103
907404                 TA   =             
10585
                                          MA   =             
10572
                                          Ha   =            197
006  n
mi
                                          Hp   =            190
371

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4714563
48                 X    =         1468626
04
 Y    =      -15725665
57  feet           Y    =        -4776936
69  meter
 Z    =       14767044
94                 Z    =         4508052
80
 XDOT =      17695
780662                 XDOT =        5327
521044
 YDOT =      14867
814516  feet/sec       YDOT =        4591
655168  meter/sec
 ZDOT =      10183
423241                 ZDOT =        3129
948314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15422433
81                 X    =         4700757
83
 Y    =        5556132
72  feet           Y    =         1693509
25  meter
 Z    =       14794161
25                 Z    =         4509260
35
 XDOT =     -15485
159630                 XDOT =       -4719
876655
 YDOT =      15596
805471  feet/sec       YDOT =        4753
906308  meter/sec
 ZDOT =      10285
246772                 ZDOT =        3134
943216


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   09040
40824084  
00010596  00000-0  82463-4 0  9126
2 25544  51
6408 241
2636 0007311 339
8208  20
2663 15
69986611 25856


Satellite: ISS
Catalog Number: 25544
Epoch time:      09040
40824084   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:       241
2636  deg
Eccentricity:     
0007311     
Arg of perigee:   339
8208  deg
Mean anomaly:      20
2663  deg
Mean motion:   15
69986611  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2585
Checksum:              302

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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