Date: January 3rd 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) : 65 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 1965)
---------------------------------------

Vector Time (GMT): 2009/001/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4096735
47                 A    =         6729446
27  meter
 Y    =       -2908049
91  meter          E    =           
0011976
 Z    =        4465779
46                 I    =           51
95809
 XDOT =       1313
352829                 Wp   =          103
07988
 YDOT =      -6858
283467  meter/sec      RA   =           79
43851  deg
 ZDOT =      -3256
585391                 TA   =           19
40025
                                          MA   =           19
35470
                                          Ha   =            195
310  n
mi
                                          Hp   =            185
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13440733
17                 X    =        -4085606
41
 Y    =       -9540846
17  feet           Y    =        -2953800
13  meter
 Z    =       14651507
43                 Z    =         4445904
53
 XDOT =       4308
900356                 XDOT =        1405
765399
 YDOT =     -22500
930011  feet/sec       YDOT =       -6843
079820  meter/sec
 ZDOT =     -10684
335273                 ZDOT =       -3249
981292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6911673
28                 X    =         2106678
02
 Y    =      -15039145
82  feet           Y    =        -4583931
65  meter
 Z    =       14573969
58                 Z    =         4442145
93
 XDOT =      21824
084991                 XDOT =        6651
981105
 YDOT =       -314
243457  feet/sec       YDOT =         -95
781406  meter/sec
 ZDOT =     -10659
098946                 ZDOT =       -3248
893359


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   09001
54197331  
00010596  00000-0  82463-4 0  9003
2 25544  51
6421  79
9558 0006875 152
5003 207
6524 15
71945191 19667


Satellite: ISS
Catalog Number: 25544
Epoch time:      09001
54197331   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:        79
9558  deg
Eccentricity:     
0006875     
Arg of perigee:   152
5003  deg
Mean anomaly:     207
6524  deg
Mean motion:   15
71945191  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1966
Checksum:              310


Coasting Arc #2 (Orbit 1989)
---------------------------------------

Vector Time (GMT): 2009/002/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -46083
83                 A    =         6735877
39  meter
 Y    =        6348066
00  meter          E    =           
0016325
 Z    =        2241674
04                 I    =           51
97252
 XDOT =      -5014
000593                 Wp   =           96
64150
 YDOT =      -1987
868296  meter/sec      RA   =           74
38485  deg
 ZDOT =       5490
457075                 TA   =          288
36374
                                          MA   =          288
54121
                                          Ha   =            195
165  n
mi
                                          Hp   =            185
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -151193
67                 X    =         -127955
09
 Y    =       20826988
19  feet           Y    =         6347092
74  meter
 Z    =        7354573
61                 Z    =         2241251
75
 XDOT =     -16450
133180                 XDOT =       -5018
070713
 YDOT =      -6521
877612  feet/sec       YDOT =       -2043
960900  meter/sec
 ZDOT =      18013
310615                 ZDOT =        5466
089221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20447343
63                 X    =        -6232350
34
 Y    =        3963628
87  feet           Y    =         1208114
08  meter
 Z    =        7353355
32                 Z    =         2241302
70
 XDOT =       3378
645470                 XDOT =        1029
811139
 YDOT =     -16030
603964  feet/sec       YDOT =       -4886
128088  meter/sec
 ZDOT =      17918
350305                 ZDOT =        5461
513173


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   09002
55914702  
00010596  00000-0  82463-4 0  9015
2 25544  51
6415  74
7484 0006936 155
4610 204
6883 15
71937958 19909


Satellite: ISS
Catalog Number: 25544
Epoch time:      09002
55914702   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:        74
7484  deg
Eccentricity:     
0006936     
Arg of perigee:   155
4610  deg
Mean anomaly:     204
6883  deg
Mean motion:   15
71937958  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1990
Checksum:              324


Coasting Arc #3 (Orbit 2004)
---------------------------------------

Vector Time (GMT): 2009/003/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4432966
42                 A    =         6727118
87  meter
 Y    =         546427
46  meter          E    =           
0018006
 Z    =       -5046070
86                 I    =           51
93327
 XDOT =       1222
775510                 Wp   =          121
66235
 YDOT =       7353
121440  meter/sec      RA   =           69
25185  deg
 ZDOT =       1866
084313                 TA   =          166
32857
                                          MA   =          166
27974
                                          Ha   =            195
027  n
mi
                                          Hp   =            185
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14543853
08                 X    =         4451039
52
 Y    =        1792741
01  feet           Y    =          596100
84  meter
 Z    =      -16555350
59                 Z    =        -5024491
65
 XDOT =       4011
730676                 XDOT =        1131
395752
 YDOT =      24124
414174  feet/sec       YDOT =        7366
284170  meter/sec
 ZDOT =       6122
323860                 ZDOT =        1871
803060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1415436
44                 X    =          431425
03
 Y    =       14680216
72  feet           Y    =         4474530
06  meter
 Z    =      -16471338
52                 Z    =        -5020463
98
 XDOT =     -21623
307352                 XDOT =       -6590
784081
 YDOT =       8995
881268  feet/sec       YDOT =        2741
944611  meter/sec
 ZDOT =       6145
064595                 ZDOT =        1873
015689


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   09003
51273332  
00010596  00000-0  82463-4 0  9020
2 25544  51
6409  69
8661 0006773 158
3540 201
7909 15
71951113 20051


Satellite: ISS
Catalog Number: 25544
Epoch time:      09003
51273332   =   yrday
fracday
Element set:     902
Inclination:       51
6409  deg
RA of node:        69
8661  deg
Eccentricity:     
0006773     
Arg of perigee:   158
3540  deg
Mean anomaly:     201
7909  deg
Mean motion:   15
71951113  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2005
Checksum:              291


Coasting Arc #4 (Orbit 2020)
---------------------------------------

Vector Time (GMT): 2009/004/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2168009
74                 A    =         6737461
73  meter
 Y    =       -6290240
05  meter          E    =           
0016322
 Z    =       -1007508
82                 I    =           51
95744
 XDOT =       4829
020590                 Wp   =          149
40529
 YDOT =       -719
374020  meter/sec      RA   =           64
17789  deg
 ZDOT =      -5955
648150                 TA   =           41
55389
                                          MA   =           41
42993
                                          Ha   =            194
915  n
mi
                                          Hp   =            185
713

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7112892
86                 X    =        -2092615
82
 Y    =      -20637270
51  feet           Y    =        -6314062
37  meter
 Z    =       -3305475
14                 Z    =        -1017858
34
 XDOT =      15843
243404                 XDOT =        4865
637310
 YDOT =      -2360
150985  feet/sec       YDOT =        -665
167952  meter/sec
 ZDOT =     -19539
528050                 ZDOT =       -5932
099871

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18416383
27                 X    =         5613313
62
 Y    =      -11707108
55  feet           Y    =        -3568326
69  meter
 Z    =       -3346159
26                 Z    =        -1019909
34
 XDOT =       5159
434197                 XDOT =        1572
595543
 YDOT =      13623
415250  feet/sec       YDOT =        4152
416968  meter/sec
 ZDOT =     -19447
935429                 ZDOT =       -5927
730719


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   09004
52987797  
00010596  00000-0  82463-4 0  9030
2 25544  51
6414  64
6581 0006770 161
0096 199
1320 15
71986648 20211


Satellite: ISS
Catalog Number: 25544
Epoch time:      09004
52987797   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:        64
6581  deg
Eccentricity:     
0006770     
Arg of perigee:   161
0096  deg
Mean anomaly:     199
1320  deg
Mean motion:   15
71986648  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2021
Checksum:              321


Coasting Arc #5 (Orbit 2036)
---------------------------------------

Vector Time (GMT): 2009/005/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3774397
60                 A    =         6725786
91  meter
 Y    =        1753681
87  meter          E    =           
0007032
 Z    =        5279531
12                 I    =           51
90456
 XDOT =      -3684
201634                 Wp   =          143
28003
 YDOT =      -6751
904002  meter/sec      RA   =           59
06536  deg
 ZDOT =       -396
370305                 TA   =          310
43881
                                          MA   =          310
50012
                                          Ha   =            194
849  n
mi
                                          Hp   =            185
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12383194
23                 X    =        -3819374
12
 Y    =        5753549
45  feet           Y    =         1711222
44  meter
 Z    =       17321296
34                 Z    =         5261085
95
 XDOT =     -12087
275701                 XDOT =       -3606
501413
 YDOT =     -22151
916016  feet/sec       YDOT =       -6792
668401  meter/sec
 ZDOT =      -1300
427509                 ZDOT =        -414
080064

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8688420
14                 X    =        -2648230
46
 Y    =      -10650628
26  feet           Y    =        -3246311
49  meter
 Z    =       17249626
39                 Z    =         5257686
12
 XDOT =      17657
305615                 XDOT =        5381
946751
 YDOT =     -16594
706593  feet/sec       YDOT =       -5058
066570  meter/sec
 ZDOT =      -1369
775348                 ZDOT =        -417
507526


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   09005
54700649  
00010596  00000-0  82463-4 0  9043
2 25544  51
6415  59
4506 0006709 165
5375 194
5981 15
72023129 20378


Satellite: ISS
Catalog Number: 25544
Epoch time:      09005
54700649   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:        59
4506  deg
Eccentricity:     
0006709     
Arg of perigee:   165
5375  deg
Mean anomaly:     194
5981  deg
Mean motion:   15
72023129  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2037
Checksum:              311


Coasting Arc #6 (Orbit 2051)
---------------------------------------

Vector Time (GMT): 2009/006/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4149506
01                 A    =         6737867
24  meter
 Y    =        5298303
89  meter          E    =           
0009641
 Z    =        -304641
32                 I    =           51
92871
 XDOT =      -3574
205265                 Wp   =           76
47882
 YDOT =       3137
610188  meter/sec      RA   =           53
96479  deg
 ZDOT =       6046
412538                 TA   =          280
22816
                                          MA   =          280
33687
                                          Ha   =            194
686  n
mi
                                          Hp   =            186
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13613864
86                 X    =         4091431
00
 Y    =       17382886
77  feet           Y    =         5344381
39  meter
 Z    =        -999479
39                 Z    =         -284623
42
 XDOT =     -11726
395225                 XDOT =       -3638
397384
 YDOT =      10293
996681  feet/sec       YDOT =        3097
281767  meter/sec
 ZDOT =      19837
311477                 ZDOT =        6028
893404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13127984
14                 X    =        -4001409
56
 Y    =       17756924
36  feet           Y    =         5412310
54  meter
 Z    =        -921248
03                 Z    =         -280796
40
 XDOT =     -11780
929486                 XDOT =       -3590
827307
 YDOT =      -7713
980494  feet/sec       YDOT =       -2351
221255  meter/sec
 ZDOT =      19769
325997                 ZDOT =        6025
690564


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   09006
50055330  
00010596  00000-0  82463-4 0  9051
2 25544  51
6415  54
5680 0006484 167
1704 192
9625 15
71987722 20522


Satellite: ISS
Catalog Number: 25544
Epoch time:      09006
50055330   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:        54
5680  deg
Eccentricity:     
0006484     
Arg of perigee:   167
1704  deg
Mean anomaly:     192
9625  deg
Mean motion:   15
71987722  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2052
Checksum:              303


Coasting Arc #7 (Orbit 2067)
---------------------------------------

Vector Time (GMT): 2009/007/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2317742
26                 A    =         6726060
78  meter
 Y    =       -3572986
88  meter          E    =           
0016043
 Z    =       -5218424
53                 I    =           51
87196
 XDOT =       5600
789527                 Wp   =          106
28211
 YDOT =       5159
129806  meter/sec      RA   =           48
87381  deg
 ZDOT =      -1051
873298                 TA   =          153
74099
                                          MA   =          153
65957
                                          Ha   =            194
588  n
mi
                                          Hp   =            186
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7604141
27                 X    =         2382873
94
 Y    =      -11722397
90  feet           Y    =        -3546703
65  meter
 Z    =      -17120815
40                 Z    =        -5207007
21
 XDOT =      18375
293724                 XDOT =        5547
792845
 YDOT =      16926
278892  feet/sec       YDOT =        5221
464906  meter/sec
 ZDOT =      -3451
027881                 ZDOT =       -1024
792616

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13422624
91                 X    =         4091216
07
 Y    =        4072213
96  feet           Y    =         1241210
81  meter
 Z    =      -17076595
41                 Z    =        -5204946
28
 XDOT =     -10734
871239                 XDOT =       -3271
988754
 YDOT =      21452
605658  feet/sec       YDOT =        6538
754205  meter/sec
 ZDOT =      -3345
322233                 ZDOT =       -1019
654217


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   09007
51765507  
00010596  00000-0  82463-4 0  9068
2 25544  51
6424  49
3597 0006628 171
2723 188
8556 15
72031320 20687


Satellite: ISS
Catalog Number: 25544
Epoch time:      09007
51765507   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:        49
3597  deg
Eccentricity:     
0006628     
Arg of perigee:   171
2723  deg
Mean anomaly:     188
8556  deg
Mean motion:   15
72031320  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2068
Checksum:              315


Coasting Arc #8 (Orbit 2083)
---------------------------------------

Vector Time (GMT): 2009/008/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5480363
43                 A    =         6736674
11  meter
 Y    =       -3587111
36  meter          E    =           
0018527
 Z    =        1527482
01                 I    =           51
88723
 XDOT =       1536
180461                 Wp   =          134
78674
 YDOT =      -4830
512292  meter/sec      RA   =           43
74738  deg
 ZDOT =      -5802
435806                 TA   =           28
43593
                                          MA   =           28
33496
                                          Ha   =            194
436  n
mi
                                          Hp   =            186
098

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17980194
99                 X    =        -5447264
66
 Y    =      -11768738
06  feet           Y    =        -3648211
14  meter
 Z    =        5011423
91                 Z    =         1500938
28
 XDOT =       5039
962144                 XDOT =        1618
268972
 YDOT =     -15848
137441  feet/sec       YDOT =       -4812
873907  meter/sec
 ZDOT =     -19036
862879                 ZDOT =       -5794
774455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5838801
45                 X    =         1779666
68
 Y    =      -20705696
96  feet           Y    =        -6311096
43  meter
 Z    =        4907900
60                 Z    =         1495928
10
 XDOT =      15153
234518                 XDOT =        4618
705881
 YDOT =       -255
998830  feet/sec       YDOT =         -78
028443  meter/sec
 ZDOT =     -19007
327793                 ZDOT =       -5793
433511


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   09008
53474162  
00010596  00000-0  82463-4 0  9076
2 25544  51
6419  44
1517 0006518 173
8931 186
2311 15
72082412 20840


Satellite: ISS
Catalog Number: 25544
Epoch time:      09008
53474162   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:        44
1517  deg
Eccentricity:     
0006518     
Arg of perigee:   173
8931  deg
Mean anomaly:     186
2311  deg
Mean motion:   15
72082412  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2084
Checksum:              296


Coasting Arc #9 (Orbit 2099)
---------------------------------------

Vector Time (GMT): 2009/009/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -267284
97                 A    =         6727435
52  meter
 Y    =        4660905
99  meter          E    =           
0011884
 Z    =        4842158
49                 I    =           51
83357
 XDOT =      -6698
189560                 Wp   =          147
59139
 YDOT =      -2918
308476  meter/sec      RA   =           38
67500  deg
 ZDOT =       2426
772748                 TA   =          278
70533
                                          MA   =          278
83992
                                          Ha   =            194
303  n
mi
                                          Hp   =            186
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -876919
19                 X    =         -342906
21
 Y    =       15291686
33  feet           Y    =         4657493
40  meter
 Z    =       15886346
74                 Z    =         4840677
15
 XDOT =     -21975
687532                 XDOT =       -6676
847433
 YDOT =      -9574
502873  feet/sec       YDOT =       -2993
092602  meter/sec
 ZDOT =       7961
852849                 ZDOT =        2394
284600

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14815626
21                 X    =        -4515802
87
 Y    =        3908511
96  feet           Y    =         1191314
45  meter
 Z    =       15880850
90                 Z    =         4840483
35
 XDOT =       2418
056858                 XDOT =         737
023730
 YDOT =     -22837
245005  feet/sec       YDOT =       -6960
792278  meter/sec
 ZDOT =       7835
224634                 ZDOT =        2388
176468


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   09009
55181443  
00010596  00000-0  82463-4 0  9087
2 25544  51
6412  38
9434 0006506 176
7159 183
4047 15
72093005 21007


Satellite: ISS
Catalog Number: 25544
Epoch time:      09009
55181443   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:        38
9434  deg
Eccentricity:     
0006506     
Arg of perigee:   176
7159  deg
Mean anomaly:     183
4047  deg
Mean motion:   15
72093005  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2100
Checksum:              294


Coasting Arc #10 (Orbit 2114)
---------------------------------------

Vector Time (GMT): 2009/010/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6010385
39                 A    =         6734435
61  meter
 Y    =        1465244
84  meter          E    =           
0005378
 Z    =       -2669679
89                 I    =           51
83475
 XDOT =        962
430416                 Wp   =          131
13401
 YDOT =       5561
319131  meter/sec      RA   =           33
52661  deg
 ZDOT =       5222
411197                 TA   =          198
60442
                                          MA   =          198
62409
                                          Ha   =            194
124  n
mi
                                          Hp   =            186
304

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19719112
18                 X    =         6006522
67
 Y    =        4807233
72  feet           Y    =         1532435
29  meter
 Z    =       -8758792
28                 Z    =        -2640491
09
 XDOT =       3157
580106                 XDOT =         874
802231
 YDOT =      18245
797673  feet/sec       YDOT =        5571
590767  meter/sec
 ZDOT =      17133
895002                 ZDOT =        5226
874675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2028072
99                 X    =          618156
65
 Y    =       20243981
70  feet           Y    =         6170365
62  meter
 Z    =       -8645082
32                 Z    =        -2635021
09
 XDOT =     -14719
712135                 XDOT =       -4486
568259
 YDOT =       8794
407873  feet/sec       YDOT =        2680
535520  meter/sec
 ZDOT =      17151
591292                 ZDOT =        5227
805026


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   09010
50530654  
00010596  00000-0  82463-4 0  9097
2 25544  51
6422  34
0609 0006511 180
0571 180
0592 15
72148754 21157


Satellite: ISS
Catalog Number: 25544
Epoch time:      09010
50530654   =   yrday
fracday
Element set:     909
Inclination:       51
6422  deg
RA of node:        34
0609  deg
Eccentricity:     
0006511     
Arg of perigee:   180
0571  deg
Mean anomaly:     180
0592  deg
Mean motion:   15
72148754  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2115
Checksum:              274


Coasting Arc #11 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2009/011/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1943066
43                 A    =         6729629
95  meter
 Y    =       -4852381
32  meter          E    =           
0008143
 Z    =       -4242914
70                 I    =           51
79263
 XDOT =       6777
292889                 Wp   =          114
50424
 YDOT =        438
502637  meter/sec      RA   =           28
46405  deg
 ZDOT =      -3613
901469                 TA   =          118
82241
                                          MA   =          118
74064
                                          Ha   =            193
967  n
mi
                                          Hp   =            186
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6374889
85                 X    =        -1868051
07
 Y    =      -15919886
21  feet           Y    =        -4873689
78  meter
 Z    =      -13920323
80                 Z    =        -4252172
36
 XDOT =      22235
212892                 XDOT =        6789
441036
 YDOT =       1438
656945  feet/sec       YDOT =         514
358684  meter/sec
 ZDOT =     -11856
632116                 ZDOT =       -3580
948598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12732772
29                 X    =         3880948
99
 Y    =      -11443162
24  feet           Y    =        -3487875
85  meter
 Z    =      -13956645
74                 Z    =        -4253985
62
 XDOT =       5581
580112                 XDOT =        1701
265618
 YDOT =      20480
276823  feet/sec       YDOT =        6242
388376  meter/sec
 ZDOT =     -11728
320349                 ZDOT =       -3574
792042


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   09011
52235056  
00010596  00000-0  82463-4 0  9100
2 25544  51
6414  28
8517 0006398 184
7567 175
3535 15
72138248 21315


Satellite: ISS
Catalog Number: 25544
Epoch time:      09011
52235056   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:        28
8517  deg
Eccentricity:     
0006398     
Arg of perigee:   184
7567  deg
Mean anomaly:     175
3535  deg
Mean motion:   15
72138248  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2131
Checksum:              305


Coasting Arc #12 (Orbit 2146)
---------------------------------------

Vector Time (GMT): 2009/012/12:00:01
000
Vector Time (MET): N/A
Weight (LBS)     : 640263
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5627418
11                 A    =         6731765
67  meter
 Y    =         678517
09  meter          E    =           
0012365
 Z    =        3617184
46                 I    =           51
77257
 XDOT =      -3473
944601                 Wp   =          115
55504
 YDOT =      -5277
048883  meter/sec      RA   =           23
30196  deg
 ZDOT =      -4408
292873                 TA   =           21
22519
                                          MA   =           21
17394
                                          Ha   =            193
875  n
mi
                                          Hp   =            186
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18462657
83                 X    =        -5652158
31
 Y    =        2226105
94  feet           Y    =          615449
32  meter
 Z    =       11867403
08                 Z    =         3589787
17
 XDOT =     -11397
456040                 XDOT =       -3393
263465
 YDOT =     -17313
152502  feet/sec       YDOT =       -5315
444965  meter/sec
 ZDOT =     -14462
903126                 ZDOT =       -4424
973439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8822431
42                 X    =        -2689077
10
 Y    =      -16447166
37  feet           Y    =        -5013096
31  meter
 Z    =       11760780
58                 Z    =         3584685
92
 XDOT =      10804
176495                 XDOT =        3293
112996
 YDOT =     -16199
194413  feet/sec       YDOT =       -4937
514457  meter/sec
 ZDOT =     -14528
153111                 ZDOT =       -4428
181068


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   09012
53937965  
00010596  00000-0  82463-4 0  9111
2 25544  51
6405  23
6427 0006257 188
6886 171
4169 15
72183546 21477


Satellite: ISS
Catalog Number: 25544
Epoch time:      09012
53937965   =   yrday
fracday
Element set:     911
Inclination:       51
6405  deg
RA of node:        23
6427  deg
Eccentricity:     
0006257     
Arg of perigee:   188
6886  deg
Mean anomaly:     171
4169  deg
Mean motion:   15
72183546  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2147
Checksum:              328

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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