Date: February 22nd 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 2759)
---------------------------------------

Vector Time (GMT): 2009/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5631918
65                 A    =         6736670
35  meter
 Y    =       -2074396
59  meter          E    =           
0020197
 Z    =        3048374
97                 I    =           51
62417
 XDOT =       4212
520104                 Wp   =           76
56076
 YDOT =       4160
538190  meter/sec      RA   =          183
49657  deg
 ZDOT =      -4919
634967                 TA   =           68
15428
                                          MA   =           67
93958
                                          Ha   =            197
650  n
mi
                                          Hp   =            185
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18477423
40                 X    =         5639888
23
 Y    =       -6805763
08  feet           Y    =        -2011372
67  meter
 Z    =       10001230
23                 Z    =         3075753
50
 XDOT =      13820
604017                 XDOT =        4189
581303
 YDOT =      13650
059680  feet/sec       YDOT =        4207
516829  meter/sec
 ZDOT =     -16140
534668                 ZDOT =       -4899
226726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19342409
56                 X    =         5895566
43
 Y    =        3385457
37  feet           Y    =         1031887
41  meter
 Z    =       10107821
90                 Z    =         3080864
11
 XDOT =       5403
791077                 XDOT =        1647
075520
 YDOT =      17386
169019  feet/sec       YDOT =        5299
304317  meter/sec
 ZDOT =     -16060
591408                 ZDOT =       -4895
268261


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   09051
53818306  
00010596  00000-0  82463-4 0  9009
2 25544  51
6391 184
3449 0008912  47
4699 312
7214 15
70982036 27605


Satellite: ISS
Catalog Number: 25544
Epoch time:      09051
53818306   =   yrday
fracday
Element set:     900
Inclination:       51
6391  deg
RA of node:       184
3449  deg
Eccentricity:     
0008912     
Arg of perigee:    47
4699  deg
Mean anomaly:     312
7214  deg
Mean motion:   15
70982036  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2760
Checksum:              314


Coasting Arc #2 (Orbit 2775)
---------------------------------------

Vector Time (GMT): 2009/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4925692
96                 A    =         6734889
01  meter
 Y    =       -2756948
33  meter          E    =           
0019385
 Z    =        3653385
26                 I    =           51
64938
 XDOT =       5248
515735                 Wp   =           76
35543
 YDOT =      -3588
984827  meter/sec      RA   =          178
43419  deg
 ZDOT =       4353
237666                 TA   =          327
49997
                                          MA   =          327
61918
                                          Ha   =            197
721  n
mi
                                          Hp   =            185
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16160409
98                 X    =        -4912245
23
 Y    =       -9045106
08  feet           Y    =        -2811955
09  meter
 Z    =       11986172
11                 Z    =         3629489
57
 XDOT =      17219
539814                 XDOT =        5267
111610
 YDOT =     -11774
884602  feet/sec       YDOT =       -3530
188876  meter/sec
 ZDOT =      14282
275807                 ZDOT =        4378
779450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9748573
90                 X    =        -2971365
33
 Y    =      -15816739
34  feet           Y    =        -4820942
15  meter
 Z    =       11892736
45                 Z    =         3624906
07
 XDOT =      19550
812846                 XDOT =        5959
087756
 YDOT =      -1199
756204  feet/sec       YDOT =        -365
685691  meter/sec
 ZDOT =      14381
583812                 ZDOT =        4383
506746


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   09052
55595205  
00010596  00000-0  82463-4 0  9013
2 25544  51
6405 179
1416 0008892  50
8416 309
3534 15
71046754 27762


Satellite: ISS
Catalog Number: 25544
Epoch time:      09052
55595205   =   yrday
fracday
Element set:     901
Inclination:       51
6405  deg
RA of node:       179
1416  deg
Eccentricity:     
0008892     
Arg of perigee:    50
8416  deg
Mean anomaly:     309
3534  deg
Mean motion:   15
71046754  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2776
Checksum:              315


Coasting Arc #3 (Orbit 2790)
---------------------------------------

Vector Time (GMT): 2009/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3266179
52                 A    =         6732123
82  meter
 Y    =        3903305
90  meter          E    =           
0016214
 Z    =       -4419322
14                 I    =           51
66995
 XDOT =      -6681
596809                 Wp   =           83
35554
 YDOT =      -1851
288396  meter/sec      RA   =          173
27451  deg
 ZDOT =       3315
246817                 TA   =          219
94599
                                          MA   =          220
06539
                                          Ha   =            197
712  n
mi
                                          Hp   =            185
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10715812
08                 X    =        -3288116
53
 Y    =       12806121
72  feet           Y    =         3866658
82  meter
 Z    =      -14499088
39                 Z    =        -4435242
17
 XDOT =     -21921
249372                 XDOT =       -6676
503221
 YDOT =      -6073
780827  feet/sec       YDOT =       -1925
977341  meter/sec
 ZDOT =      10876
794019                 ZDOT =        3282
800956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15425239
19                 X    =        -4701612
91
 Y    =        6252415
87  feet           Y    =         1905736
36  meter
 Z    =      -14560846
05                 Z    =        -4438145
88
 XDOT =     -16038
620176                 XDOT =       -4888
571430
 YDOT =     -14626
435086  feet/sec       YDOT =       -4458
137414  meter/sec
 ZDOT =      10750
074743                 ZDOT =        3276
622782


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   09053
51010280  
00010596  00000-0  82463-4 0  9026
2 25544  51
6408 174
2642 0008992  53
6863 306
5128 15
71030204 27918


Satellite: ISS
Catalog Number: 25544
Epoch time:      09053
51010280   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:       174
2642  deg
Eccentricity:     
0008992     
Arg of perigee:    53
6863  deg
Mean anomaly:     306
5128  deg
Mean motion:   15
71030204  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2791
Checksum:              284


Coasting Arc #4 (Orbit 2806)
---------------------------------------

Vector Time (GMT): 2009/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6404125
93                 A    =         6738754
00  meter
 Y    =         339102
76  meter          E    =           
0011939
 Z    =       -2079244
56                 I    =           51
72204
 XDOT =      -2053
375002                 Wp   =           91
27363
 YDOT =       4904
574546  meter/sec      RA   =          168
20707  deg
 ZDOT =      -5552
195366                 TA   =          111
85995
                                          MA   =          111
73293
                                          Ha   =            197
786  n
mi
                                          Hp   =            185
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21010911
83                 X    =         6409958
37
 Y    =        1112541
86  feet           Y    =          410749
94  meter
 Z    =       -6821668
51                 Z    =        -2048120
04
 XDOT =      -6736
794625                 XDOT =       -2081
095350
 YDOT =      16091
123838  feet/sec       YDOT =        4881
457269  meter/sec
 ZDOT =     -18215
864062                 ZDOT =       -5562
237934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18204502
04                 X    =         5548732
22
 Y    =       10627061
28  feet           Y    =         3239128
28  meter
 Z    =       -6700223
91                 Z    =        -2042228
25
 XDOT =     -12488
084488                 XDOT =       -3806
368152
 YDOT =       9941
396591  feet/sec       YDOT =        3030
137681  meter/sec
 ZDOT =     -18254
608733                 ZDOT =       -5564
004742


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   09054
52785114  
00010596  00000-0  82463-4 0  9034
2 25544  51
6414 169
0599 0009073  57
6129 302
5910 15
71055984 28073


Satellite: ISS
Catalog Number: 25544
Epoch time:      09054
52785114   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:       169
0599  deg
Eccentricity:     
0009073     
Arg of perigee:    57
6129  deg
Mean anomaly:     302
5910  deg
Mean motion:   15
71055984  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2807
Checksum:              317


Coasting Arc #5 (Orbit 2822)
---------------------------------------

Vector Time (GMT): 2009/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         230226
92                 A    =         6728943
99  meter
 Y    =       -4317003
11  meter          E    =           
0013340
 Z    =        5147987
30                 I    =           51
71885
 XDOT =       7495
612969                 Wp   =           59
00887
 YDOT =      -1189
628744  meter/sec      RA   =          163
07076  deg
 ZDOT =      -1323
555896                 TA   =           43
68603
                                          MA   =           43
58052
                                          Ha   =            197
768  n
mi
                                          Hp   =            185
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         755337
66                 X    =          253475
91
 Y    =      -14163396
02  feet           Y    =        -4314298
24  meter
 Z    =       16889722
11                 Z    =         5149162
47
 XDOT =      24591
906065                 XDOT =        7514
787938
 YDOT =      -3902
981443  feet/sec       YDOT =       -1105
701312  meter/sec
 ZDOT =      -4342
374987                 ZDOT =       -1287
096498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6857185
44                 X    =         2090070
12
 Y    =      -12410049
96  feet           Y    =        -3782583
23  meter
 Z    =       16893925
02                 Z    =         5149268
35
 XDOT =      22897
457788                 XDOT =        6979
145134
 YDOT =       6892
828822  feet/sec       YDOT =        2100
934225  meter/sec
 ZDOT =      -4200
243936                 ZDOT =       -1280
234352


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   09055
54558748  
00010596  00000-0  82463-4 0  9049
2 25544  51
6421 163
8565 0009149  60
4365 299
7708 15
71089164 28231


Satellite: ISS
Catalog Number: 25544
Epoch time:      09055
54558748   =   yrday
fracday
Element set:     904
Inclination:       51
6421  deg
RA of node:       163
8565  deg
Eccentricity:     
0009149     
Arg of perigee:    60
4365  deg
Mean anomaly:     299
7708  deg
Mean motion:   15
71089164  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2823
Checksum:              340


Coasting Arc #6 (Orbit 2838)
---------------------------------------

Vector Time (GMT): 2009/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6292930
47                 A    =         6740517
59  meter
 Y    =        2382657
63  meter          E    =           
0021549
 Z    =         191407
03                 I    =           51
78570
 XDOT =      -1514
239367                 Wp   =           54
38203
 YDOT =      -4522
030999  meter/sec      RA   =          157
97881  deg
 ZDOT =       6045
635710                 TA   =          307
69191
                                          MA   =          307
88712
                                          Ha   =            197
852  n
mi
                                          Hp   =            185
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20646097
35                 X    =        -6320035
84
 Y    =        7817118
22  feet           Y    =         2312134
88  meter
 Z    =         627975
82                 Z    =          160770
61
 XDOT =      -4967
976925                 XDOT =       -1492
928687
 YDOT =     -14836
059708  feet/sec       YDOT =       -4538
844447  meter/sec
 ZDOT =      19834
762827                 ZDOT =        6038
331837

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22010119
61                 X    =        -6708684
46
 Y    =       -1748978
48  feet           Y    =         -533088
64  meter
 Z    =         508660
79                 Z    =          155039
81
 XDOT =       1611
817768                 XDOT =         491
282056
 YDOT =     -13980
554253  feet/sec       YDOT =       -4261
272936  meter/sec
 ZDOT =      19805
865767                 ZDOT =        6036
827886


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   09056
56331380  
00010596  00000-0  82463-4 0  9054
2 25544  51
6425 158
6535 0009242  63
9825 296
2287 15
71072045 28398


Satellite: ISS
Catalog Number: 25544
Epoch time:      09056
56331380   =   yrday
fracday
Element set:     905
Inclination:       51
6425  deg
RA of node:       158
6535  deg
Eccentricity:     
0009242     
Arg of perigee:    63
9825  deg
Mean anomaly:     296
2287  deg
Mean motion:   15
71072045  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2839
Checksum:              322


Coasting Arc #7 (Orbit 2853)
---------------------------------------

Vector Time (GMT): 2009/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2721233
88                 A    =         6728681
88  meter
 Y    =        3249341
87  meter          E    =           
0023518
 Z    =       -5246366
29                 I    =           51
77255
 XDOT =      -6466
095136                 Wp   =           77
45883
 YDOT =       4055
271722  meter/sec      RA   =          152
88148  deg
 ZDOT =       -840
423332                 TA   =          184
52166
                                          MA   =          184
54295
                                          Ha   =            197
820  n
mi
                                          Hp   =            185
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8927932
67                 X    =         2710182
42
 Y    =       10660570
43  feet           Y    =         3279710
01  meter
 Z    =      -17212487
82                 Z    =        -5233173
90
 XDOT =     -21214
222888                 XDOT =       -6506
878730
 YDOT =      13304
697252  feet/sec       YDOT =        3982
735971  meter/sec
 ZDOT =      -2757
294395                 ZDOT =        -871
934520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3842230
36                 X    =         1171111
81
 Y    =       13430270
62  feet           Y    =         4093546
48  meter
 Z    =      -17160727
77                 Z    =        -5230589
82
 XDOT =     -23815
149363                 XDOT =       -7258
857526
 YDOT =       3125
689616  feet/sec       YDOT =         952
710195  meter/sec
 ZDOT =      -2879
880027                 ZDOT =        -877
787432


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   09057
51742015  
00010596  00000-0  82463-4 0  9062
2 25544  51
6422 153
7756 0009113  67
2984 292
9140 15
71087360 28540


Satellite: ISS
Catalog Number: 25544
Epoch time:      09057
51742015   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       153
7756  deg
Eccentricity:     
0009113     
Arg of perigee:    67
2984  deg
Mean anomaly:     292
9140  deg
Mean motion:   15
71087360  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2854
Checksum:              312


Coasting Arc #8 (Orbit 2869)
---------------------------------------

Vector Time (GMT): 2009/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4729044
01                 A    =         6739223
58  meter
 Y    =       -4503890
39  meter          E    =           
0021703
 Z    =        1636673
69                 I    =           51
83325
 XDOT =       4437
297841                 Wp   =           98
90818
 YDOT =       2546
550750  meter/sec      RA   =          147
75733  deg
 ZDOT =      -5752
271849                 TA   =           63
08081
                                          MA   =           62
85922
                                          Ha   =            197
871  n
mi
                                          Hp   =            184
938

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15515236
26                 X    =         4771105
22
 Y    =      -14776543
28  feet           Y    =        -4450772
14  meter
 Z    =        5369664
35                 Z    =         1659749
69
 XDOT =      14558
063782                 XDOT =        4436
435269
 YDOT =       8354
825294  feet/sec       YDOT =        2596
165845  meter/sec
 ZDOT =     -18872
282968                 ZDOT =       -5730
718042

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20066876
37                 X    =         6116383
92
 Y    =       -7444362
94  feet           Y    =        -2269041
83  meter
 Z    =        5459305
44                 Z    =         1663996
30
 XDOT =       9621
539587                 XDOT =        2932
645266
 YDOT =      12012
646336  feet/sec       YDOT =        3661
454603  meter/sec
 ZDOT =     -18787
959502                 ZDOT =       -5726
570056


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   09058
53512381  
00010596  00000-0  82463-4 0  9077
2 25544  51
6414 148
5720 0009296  71
5314 288
6858 15
71108399 28703


Satellite: ISS
Catalog Number: 25544
Epoch time:      09058
53512381   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       148
5720  deg
Eccentricity:     
0009296     
Arg of perigee:    71
5314  deg
Mean anomaly:     288
6858  deg
Mean motion:   15
71108399  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2870
Checksum:              330


Coasting Arc #9 (Orbit 2885)
---------------------------------------

Vector Time (GMT): 2009/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4760801
36                 A    =         6730997
16  meter
 Y    =        -964073
49  meter          E    =           
0016319
 Z    =        4646215
62                 I    =           51
83033
 XDOT =       4018
697277                 Wp   =           94
30652
 YDOT =      -5909
948374  meter/sec      RA   =          142
69382  deg
 ZDOT =       2881
682636                 TA   =          327
24065
                                          MA   =          327
34173
                                          Ha   =            197
920  n
mi
                                          Hp   =            184
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15619427
05                 X    =        -4772237
42
 Y    =       -3162970
78  feet           Y    =        -1017375
11  meter
 Z    =       15243489
57                 Z    =         4623060
12
 XDOT =      13184
702352                 XDOT =        4070
486029
 YDOT =     -19389
594402  feet/sec       YDOT =       -5864
719161  meter/sec
 ZDOT =       9454
339356                 ZDOT =        2901
331598

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13328983
44                 X    =        -4062674
15
 Y    =       -8891459
51  feet           Y    =        -2710116
86  meter
 Z    =       15153052
76                 Z    =         4618650
48
 XDOT =      18861
817751                 XDOT =        5749
082050
 YDOT =     -11977
912510  feet/sec       YDOT =       -3650
867733  meter/sec
 ZDOT =       9530
494091                 ZDOT =        2904
894599


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   09059
55281369  
00010596  00000-0  82463-4 0  9080
2 25544  51
6415 143
3676 0009211  74
7264 285
4910 15
71159024 28865


Satellite: ISS
Catalog Number: 25544
Epoch time:      09059
55281369   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:       143
3676  deg
Eccentricity:     
0009211     
Arg of perigee:    74
7264  deg
Mean anomaly:     285
4910  deg
Mean motion:   15
71159024  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2886
Checksum:              325


Coasting Arc #10 (Orbit 2900)
---------------------------------------

Vector Time (GMT): 2009/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2131655
31                 A    =         6735489
90  meter
 Y    =        5471058
71  meter          E    =           
0013992
 Z    =       -3309560
48                 I    =           51
86752
 XDOT =      -6040
924911                 Wp   =           81
08077
 YDOT =        495
202995  meter/sec      RA   =          137
54891  deg
 ZDOT =       4728
564326                 TA   =          240
29244
                                          MA   =          240
43178
                                          Ha   =            197
818  n
mi
                                          Hp   =            184
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6993619
79                 X    =        -2176597
99
 Y    =       17949667
68  feet           Y    =         5446969
81  meter
 Z    =      -10858138
05                 Z    =        -3320025
52
 XDOT =     -19819
307451                 XDOT =       -6068
983794
 YDOT =       1624
681741  feet/sec       YDOT =         427
493261  meter/sec
 ZDOT =      15513
662487                 ZDOT =        4699
149455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12986424
48                 X    =        -3958262
18
 Y    =       14197739
89  feet           Y    =         4327471
12  meter
 Z    =      -10898504
98                 Z    =        -3321864
32
 XDOT =     -18099
975500                 XDOT =       -5516
872532
 YDOT =      -4782
946752  feet/sec       YDOT =       -1457
842170  meter/sec
 ZDOT =      15398
921422                 ZDOT =        4693
591249


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   09060
50689001  
00010596  00000-0  82463-4 0  9093
2 25544  51
6407 138
4896 0009284  77
7078 282
5123 15
71159611 29015


Satellite: ISS
Catalog Number: 25544
Epoch time:      09060
50689001   =   yrday
fracday
Element set:     909
Inclination:       51
6407  deg
RA of node:       138
4896  deg
Eccentricity:     
0009284     
Arg of perigee:    77
7078  deg
Mean anomaly:     282
5123  deg
Mean motion:   15
71159611  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2901
Checksum:              318


Coasting Arc #11 (Orbit 2916)
---------------------------------------

Vector Time (GMT): 2009/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5442975
43                 A    =         6734999
23  meter
 Y    =       -1847494
68  meter          E    =           
0014476
 Z    =       -3524119
42                 I    =           51
88574
 XDOT =       -829
448630                 Wp   =           83
06854
 YDOT =       6157
096069  meter/sec      RA   =          132
50175  deg
 ZDOT =      -4522
991195                 TA   =          138
56292
                                          MA   =          138
45305
                                          Ha   =            197
893  n
mi
                                          Hp   =            184
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17857530
93                 X    =         5480349
36
 Y    =       -6061334
25  feet           Y    =        -1786419
32  meter
 Z    =      -11562071
59                 Z    =        -3497586
70
 XDOT =      -2721
288157                 XDOT =        -876
264862
 YDOT =      20200
446422  feet/sec       YDOT =        6147
558761  meter/sec
 ZDOT =     -14839
209956                 ZDOT =       -4527
134585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18913188
01                 X    =         5764739
71
 Y    =         550077
94  feet           Y    =          167663
76  meter
 Z    =      -11458683
03                 Z    =        -3492606
59
 XDOT =      -9455
712186                 XDOT =       -2882
101074
 YDOT =      16643
815419  feet/sec       YDOT =        5073
034940  meter/sec
 ZDOT =     -14854
859757                 ZDOT =       -4527
761254


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   09061
52455992  
00010596  00000-0  82463-4 0  9108
2 25544  51
6399 133
2848 0009363  81
3539 278
8683 15
71157285 29177


Satellite: ISS
Catalog Number: 25544
Epoch time:      09061
52455992   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       133
2848  deg
Eccentricity:     
0009363     
Arg of perigee:    81
3539  deg
Mean anomaly:     278
8683  deg
Mean motion:   15
71157285  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2917
Checksum:              345


Coasting Arc #12 (Orbit 2932)
---------------------------------------

Vector Time (GMT): 2009/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -666598
93                 A    =         6731291
30  meter
 Y    =       -4947178
78  meter          E    =           
0017916
 Z    =        4503123
77                 I    =           51
89376
 XDOT =       5962
015138                 Wp   =           75
83077
 YDOT =      -3706
637290  meter/sec      RA   =          127
35677  deg
 ZDOT =      -3174
829629                 TA   =           45
82136
                                          MA   =           45
67426
                                          Ha   =            197
775  n
mi
                                          Hp   =            184
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2187004
36                 X    =         -633104
44
 Y    =      -16230901
52  feet           Y    =        -4954445
74  meter
 Z    =       14774028
11                 Z    =         4499966
87
 XDOT =      19560
417118                 XDOT =        6018
442921
 YDOT =     -12160
883498  feet/sec       YDOT =       -3639
651107  meter/sec
 ZDOT =     -10416
107706                 ZDOT =       -3145
729217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3237995
81                 X    =          986941
12
 Y    =      -16066006
36  feet           Y    =        -4896918
74  meter
 Z    =       14761296
75                 Z    =         4499243
25
 XDOT =      21371
051327                 XDOT =        6513
896444
 YDOT =      -5203
496976  feet/sec       YDOT =       -1586
025878  meter/sec
 ZDOT =     -10302
839632                 ZDOT =       -3140
305520


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   09062
54221635  
00010596  00000-0  82463-4 0  9117
2 25544  51
6406 128
0803 0009267  83
8774 276
3444 15
71223461 29336


Satellite: ISS
Catalog Number: 25544
Epoch time:      09062
54221635   =   yrday
fracday
Element set:     911
Inclination:       51
6406  deg
RA of node:       128
0803  deg
Eccentricity:     
0009267     
Arg of perigee:    83
8774  deg
Mean anomaly:     276
3444  deg
Mean motion:   15
71223461  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2933
Checksum:              303

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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

<[program_url]/list/[list]>

If you're still having trouble, please contact the list owner at:

<mailto:[list_owner_email]>

The following physical address is associated with this mailing list:

[physical_address]

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list