Date: March 14th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 3058)
---------------------------------------

Vector Time (GMT): 2009/070/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -486668
35                 A    =         6739632
78  meter
 Y    =       -6712885
19  meter          E    =           
0021646
 Z    =         100576
15                 I    =           51
98911
 XDOT =       4722
315151                 Wp   =          123
86279
 YDOT =       -446
914725  meter/sec      RA   =           86
52265  deg
 ZDOT =      -6065
477345                 TA   =           55
05058
                                          MA   =           54
84747
                                          Ha   =            197
572  n
mi
                                          Hp   =            184
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1596680
94                 X    =         -412056
15
 Y    =      -22023901
53  feet           Y    =        -6717910
21  meter
 Z    =         329974
26                 Z    =           98393
95
 XDOT =      15493
159943                 XDOT =        4756
426281
 YDOT =      -1466
255659  feet/sec       YDOT =        -393
917015  meter/sec
 ZDOT =     -19899
860055                 ZDOT =       -6042
453723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -420541
54                 X    =         -128181
06
 Y    =      -22077831
97  feet           Y    =        -6729323
19  meter
 Z    =         320923
33                 Z    =           97817
43
 XDOT =      14053
977415                 XDOT =        4283
652316
 YDOT =       -600
437803  feet/sec       YDOT =        -183
013442  meter/sec
 ZDOT =     -19809
990169                 ZDOT =       -6038
085004


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   09070
55538322  
00010596  00000-0  82463-4 0  9009
2 25544  51
6383  87
1024 0009632 111
2562 248
9630 15
71383304 30592


Satellite: ISS
Catalog Number: 25544
Epoch time:      09070
55538322   =   yrday
fracday
Element set:     900
Inclination:       51
6383  deg
RA of node:        87
1024  deg
Eccentricity:     
0009632     
Arg of perigee:   111
2562  deg
Mean anomaly:     248
9630  deg
Mean motion:   15
71383304  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3059
Checksum:              291


Coasting Arc #2 (Orbit 3074)
---------------------------------------

Vector Time (GMT): 2009/071/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3843726
54                 A    =         6727903
43  meter
 Y    =        1824667
82  meter          E    =           
0013276
 Z    =        5202499
31                 I    =           51
94620
 XDOT =      -1984
988247                 Wp   =          117
18910
 YDOT =      -7362
313523  meter/sec      RA   =           81
43961  deg
 ZDOT =       1107
539559                 TA   =          322
24656
                                          MA   =          322
33964
                                          Ha   =            197
588  n
mi
                                          Hp   =            184
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12610651
39                 X    =        -3889117
24
 Y    =        5986442
99  feet           Y    =         1781431
82  meter
 Z    =       17068567
31                 Z    =         5183716
17
 XDOT =      -6512
428633                 XDOT =       -1907
894292
 YDOT =     -24154
571927  feet/sec       YDOT =       -7384
079641  meter/sec
 ZDOT =       3633
659970                 ZDOT =        1098
084634

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12917454
46                 X    =        -3937240
12
 Y    =        5522591
17  feet           Y    =         1683285
79  meter
 Z    =       16995363
34                 Z    =         5180186
75
 XDOT =      -5251
925605                 XDOT =       -1600
786924
 YDOT =     -23433
261010  feet/sec       YDOT =       -7142
457956  meter/sec
 ZDOT =       3596
167866                 ZDOT =        1096
111966


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   09071
57289769  
00010596  00000-0  82463-4 0  9011
2 25544  51
6377  81
8964 0009507 114
8518 245
3633 15
71402289 30756


Satellite: ISS
Catalog Number: 25544
Epoch time:      09071
57289769   =   yrday
fracday
Element set:     901
Inclination:       51
6377  deg
RA of node:        81
8964  deg
Eccentricity:     
0009507     
Arg of perigee:   114
8518  deg
Mean anomaly:     245
3633  deg
Mean motion:   15
71402289  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3075
Checksum:              337


Coasting Arc #3 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2009/072/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2863923
77                 A    =         6738061
66  meter
 Y    =        5831454
97  meter          E    =           
0013143
 Z    =       -1795056
25                 I    =           51
97550
 XDOT =      -3720
488704                 Wp   =           84
21506
 YDOT =       3571
331244  meter/sec      RA   =           76
32129  deg
 ZDOT =       5702
874810                 TA   =          256
02502
                                          MA   =          256
17121
                                          Ha   =            197
409  n
mi
                                          Hp   =            184
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9396075
35                 X    =         2807222
65
 Y    =       19132070
12  feet           Y    =         5863163
83  meter
 Z    =       -5889292
17                 Z    =        -1781281
65
 XDOT =     -12206
327770                 XDOT =       -3787
850870
 YDOT =      11716
966023  feet/sec       YDOT =        3529
350487  meter/sec
 ZDOT =      18710
219194                 ZDOT =        5684
636759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9064649
62                 X    =         2762905
21
 Y    =       19307778
13  feet           Y    =         5885010
77  meter
 Z    =       -5835060
61                 Z    =        -1778526
47
 XDOT =     -11126
750114                 XDOT =       -3391
433435
 YDOT =      10819
975106  feet/sec       YDOT =        3297
928412  meter/sec
 ZDOT =      18639
274227                 ZDOT =        5681
250784


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   09072
52680587  
00010596  00000-0  82463-4 0  9021
2 25544  51
6380  77
0169 0009627 118
3451 241
8683 15
71450322 30906


Satellite: ISS
Catalog Number: 25544
Epoch time:      09072
52680587   =   yrday
fracday
Element set:     902
Inclination:       51
6380  deg
RA of node:        77
0169  deg
Eccentricity:     
0009627     
Arg of perigee:   118
3451  deg
Mean anomaly:     241
8683  deg
Mean motion:   15
71450322  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3090
Checksum:              307


Coasting Arc #4 (Orbit 3105)
---------------------------------------

Vector Time (GMT): 2009/073/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2423960
89                 A    =         6730148
23  meter
 Y    =       -4220475
74  meter          E    =           
0018211
 Z    =       -4663228
07                 I    =           51
94015
 XDOT =       4313
301763                 Wp   =           94
20830
 YDOT =       5662
666247  meter/sec      RA   =           71
26399  deg
 ZDOT =      -2893
905990                 TA   =          147
27269
                                          MA   =          147
15974
                                          Ha   =            197
347  n
mi
                                          Hp   =            184
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7952627
60                 X    =         2493627
91
 Y    =      -13846705
18  feet           Y    =        -4192980
43  meter
 Z    =      -15299304
70                 Z    =        -4651282
93
 XDOT =      14151
252502                 XDOT =        4263
718374
 YDOT =      18578
301335  feet/sec       YDOT =        5710
622641  meter/sec
 ZDOT =      -9494
442226                 ZDOT =       -2873
072864

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8065863
72                 X    =         2458475
26
 Y    =      -13832312
29  feet           Y    =        -4216088
79  meter
 Z    =      -15252974
59                 Z    =        -4649106
65
 XDOT =      13163
681915                 XDOT =        4012
290248
 YDOT =      18015
639029  feet/sec       YDOT =        5491
166776  meter/sec
 ZDOT =      -9412
670587                 ZDOT =       -2868
981995


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   09073
54429592  
00010596  00000-0  82463-4 0  9032
2 25544  51
6376  71
8098 0009461 121
8778 238
3306 15
71432888 31069


Satellite: ISS
Catalog Number: 25544
Epoch time:      09073
54429592   =   yrday
fracday
Element set:     903
Inclination:       51
6376  deg
RA of node:        71
8098  deg
Eccentricity:     
0009461     
Arg of perigee:   121
8778  deg
Mean anomaly:     238
3306  deg
Mean motion:   15
71432888  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3106
Checksum:              331


Coasting Arc #5 (Orbit 3121)
---------------------------------------

Vector Time (GMT): 2009/074/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4466171
02                 A    =         6734921
59  meter
 Y    =       -3855666
84  meter          E    =           
0021331
 Z    =        3223357
44                 I    =           51
94599
 XDOT =       1540
120757                 Wp   =          106
35274
 YDOT =      -5821
367368  meter/sec      RA   =           66
12295  deg
 ZDOT =      -4809
190408                 TA   =           36
14055
                                          MA   =           35
99657
                                          Ha   =            197
237  n
mi
                                          Hp   =            184
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14652792
05                 X    =        -4438382
85
 Y    =      -12649825
59  feet           Y    =        -3905454
62  meter
 Z    =       10575319
68                 Z    =         3201728
50
 XDOT =       5052
889623                 XDOT =        1628
463960
 YDOT =     -19098
974303  feet/sec       YDOT =       -5803
651153  meter/sec
 ZDOT =     -15778
183753                 ZDOT =       -4801
493599

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14906695
67                 X    =        -4543560
84
 Y    =      -12421671
97  feet           Y    =        -3786125
62  meter
 Z    =       10490580
48                 Z    =         3197528
93
 XDOT =       3943
483194                 XDOT =        1201
973678
 YDOT =     -18089
043445  feet/sec       YDOT =       -5513
540442  meter/sec
 ZDOT =     -15748
551234                 ZDOT =       -4800
158416


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   09074
56177195  
00010596  00000-0  82463-4 0  9045
2 25544  51
6378  66
6041 0009262 125
3527 234
8502 15
71479240 31221


Satellite: ISS
Catalog Number: 25544
Epoch time:      09074
56177195   =   yrday
fracday
Element set:     904
Inclination:       51
6378  deg
RA of node:        66
6041  deg
Eccentricity:     
0009262     
Arg of perigee:   125
3527  deg
Mean anomaly:     234
8502  deg
Mean motion:   15
71479240  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3122
Checksum:              306


Coasting Arc #6 (Orbit 3137)
---------------------------------------

Vector Time (GMT): 2009/075/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -120472
03                 A    =         6733525
70  meter
 Y    =        5662904
66  meter          E    =           
0020245
 Z    =        3630965
18                 I    =           51
92916
 XDOT =      -5578
309803                 Wp   =          109
78663
 YDOT =      -2960
515262  meter/sec      RA   =           61
07887  deg
 ZDOT =       4405
707173                 TA   =          293
48982
                                          MA   =          293
70246
                                          Ha   =            197
043  n
mi
                                          Hp   =            184
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -395249
44                 X    =         -201425
16
 Y    =       18579083
53  feet           Y    =         5661104
97  meter
 Z    =       11912615
42                 Z    =         3630183
09
 XDOT =     -18301
541350                 XDOT =       -5566
192323
 YDOT =      -9712
976580  feet/sec       YDOT =       -3022
827260  meter/sec
 ZDOT =      14454
419860                 ZDOT =        4378
637340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         141749
26                 X    =           43205
17
 Y    =       18584446
31  feet           Y    =         5664539
24  meter
 Z    =       11909963
71                 Z    =         3630156
94
 XDOT =     -17336
390290                 XDOT =       -5284
131760
 YDOT =      -9118
770313  feet/sec       YDOT =       -2779
401191  meter/sec
 ZDOT =      14348
501614                 ZDOT =        4373
423292


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   09075
57923433  
00010596  00000-0  82463-4 0  9052
2 25544  51
6382  61
3992 0009282 130
3292 229
8682 15
71521740 31383


Satellite: ISS
Catalog Number: 25544
Epoch time:      09075
57923433   =   yrday
fracday
Element set:     905
Inclination:       51
6382  deg
RA of node:        61
3992  deg
Eccentricity:     
0009282     
Arg of perigee:   130
3292  deg
Mean anomaly:     229
8682  deg
Mean motion:   15
71521740  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3138
Checksum:              315


Coasting Arc #7 (Orbit 3152)
---------------------------------------

Vector Time (GMT): 2009/076/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4981847
52                 A    =         6731218
81  meter
 Y    =        1254349
32  meter          E    =           
0017787
 Z    =       -4367860
17                 I    =           51
90562
 XDOT =       1311
475322                 Wp   =          121
54324
 YDOT =       6744
974514  meter/sec      RA   =           55
93163  deg
 ZDOT =       3433
960256                 TA   =          183
06436
                                          MA   =          183
07527
                                          Ha   =            197
046  n
mi
                                          Hp   =            184
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16344644
11                 X    =         4988669
10
 Y    =        4115319
29  feet           Y    =         1310097
28  meter
 Z    =      -14330249
89                 Z    =        -4343641
92
 XDOT =       4302
740558                 XDOT =        1219
272937
 YDOT =      22129
181477  feet/sec       YDOT =        6759
124747  meter/sec
 ZDOT =      11266
273807                 ZDOT =        3440
107253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16611686
07                 X    =         5063241
91
 Y    =        3292301
15  feet           Y    =         1003493
39  meter
 Z    =      -14235587
27                 Z    =        -4339007
00
 XDOT =       5574
029573                 XDOT =        1698
964214
 YDOT =      20679
548280  feet/sec       YDOT =        6303
126316  meter/sec
 ZDOT =      11290
748704                 ZDOT =        3441
420205


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   09076
53309519  
00010596  00000-0  82463-4 0  9063
2 25544  51
6383  56
5182 0009241 132
4788 227
7156 15
71482232 31531


Satellite: ISS
Catalog Number: 25544
Epoch time:      09076
53309519   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:        56
5182  deg
Eccentricity:     
0009241     
Arg of perigee:   132
4788  deg
Mean anomaly:     227
7156  deg
Mean motion:   15
71482232  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3153
Checksum:              314


Coasting Arc #8 (Orbit 3168)
---------------------------------------

Vector Time (GMT): 2009/077/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2400320
34                 A    =         6736824
13  meter
 Y    =       -5844268
29  meter          E    =           
0014902
 Z    =       -2328736
99                 I    =           51
90833
 XDOT =       5438
583577                 Wp   =          135
32143
 YDOT =        -76
754878  meter/sec      RA   =           50
87785  deg
 ZDOT =      -5444
425766                 TA   =           70
74619
                                          MA   =           70
58503
                                          Ha   =            196
883  n
mi
                                          Hp   =            184
919

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7875066
72                 X    =        -2323477
86
 Y    =      -19174108
57  feet           Y    =        -5870680
47  meter
 Z    =       -7640213
21                 Z    =        -2340210
88
 XDOT =      17843
121971                 XDOT =        5465
485493
 YDOT =       -251
820466  feet/sec       YDOT =         -15
787165  meter/sec
 ZDOT =     -17862
289258                 ZDOT =       -5417
939982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9097012
26                 X    =        -2772769
34
 Y    =      -18606843
22  feet           Y    =        -5671365
81  meter
 Z    =       -7685422
98                 Z    =        -2342516
92
 XDOT =      16532
087127                 XDOT =        5038
980156
 YDOT =       -789
633998  feet/sec       YDOT =        -240
680443  meter/sec
 ZDOT =     -17758
861022                 ZDOT =       -5412
900840


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   09077
55053175  
00010596  00000-0  82463-4 0  9071
2 25544  51
6391  51
3118 0009182 136
2788 223
9103 15
71531979 31698


Satellite: ISS
Catalog Number: 25544
Epoch time:      09077
55053175   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:        51
3118  deg
Eccentricity:     
0009182     
Arg of perigee:   136
2788  deg
Mean anomaly:     223
9103  deg
Mean motion:   15
71531979  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3169
Checksum:              319


Coasting Arc #9 (Orbit 3184)
---------------------------------------

Vector Time (GMT): 2009/078/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4226545
41                 A    =         6728180
52  meter
 Y    =        1344053
55  meter          E    =           
0011030
 Z    =        5049613
32                 I    =           51
85970
 XDOT =      -4129
060463                 Wp   =          110
40800
 YDOT =      -6254
085952  meter/sec      RA   =           45
74396  deg
 ZDOT =      -1792
024807                 TA   =          356
78778
                                          MA   =          356
79486
                                          Ha   =            196
926  n
mi
                                          Hp   =            185
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13866618
79                 X    =        -4265790
57
 Y    =        4409624
52  feet           Y    =         1296570
56  meter
 Z    =       16566972
85                 Z    =         5028985
62
 XDOT =     -13546
786297                 XDOT =       -4050
114108
 YDOT =     -20518
654699  feet/sec       YDOT =       -6299
818144  meter/sec
 ZDOT =      -5879
346481                 ZDOT =       -1811
891658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13541775
20                 X    =        -4127533
08
 Y    =        5568477
78  feet           Y    =         1697272
03  meter
 Z    =       16486505
82                 Z    =         5025086
97
 XDOT =     -14784
421976                 XDOT =       -4506
291818
 YDOT =     -18322
009720  feet/sec       YDOT =       -5584
548563  meter/sec
 ZDOT =      -5957
358760                 ZDOT =       -1815
802950


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   09078
56795461  
00010596  00000-0  82463-4 0  9085
2 25544  51
6392  46
1064 0009145 140
3872 219
7960 15
71545657 31850


Satellite: ISS
Catalog Number: 25544
Epoch time:      09078
56795461   =   yrday
fracday
Element set:     908
Inclination:       51
6392  deg
RA of node:        46
1064  deg
Eccentricity:     
0009145     
Arg of perigee:   140
3872  deg
Mean anomaly:     219
7960  deg
Mean motion:   15
71545657  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3185
Checksum:              335


Coasting Arc #10 (Orbit 3200)
---------------------------------------

Vector Time (GMT): 2009/079/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4656303
29                 A    =         6738773
62  meter
 Y    =        4805812
48  meter          E    =           
0016225
 Z    =         778686
42                 I    =           51
87432
 XDOT =      -3927
439418                 Wp   =           87
69496
 YDOT =       2818
343023  meter/sec      RA   =           40
66519  deg
 ZDOT =       5984
865387                 TA   =          280
75444
                                          MA   =          280
93706
                                          Ha   =            196
680  n
mi
                                          Hp   =            185
096

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15276585
58                 X    =         4598435
15
 Y    =       15767101
30  feet           Y    =         4857558
44  meter
 Z    =        2554745
47                 Z    =          801165
72
 XDOT =     -12885
299927                 XDOT =       -3987
735732
 YDOT =       9246
532228  feet/sec       YDOT =        2774
087185  meter/sec
 ZDOT =      19635
385129                 ZDOT =        5965
639572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16779353
30                 X    =         5114346
89
 Y    =       14141105
31  feet           Y    =         4310208
90  meter
 Z    =        2642861
77                 Z    =          805544
27
 XDOT =     -10964
519522                 XDOT =       -3341
985550
 YDOT =       9291
558575  feet/sec       YDOT =        2832
067054  meter/sec
 ZDOT =      19560
490645                 ZDOT =        5962
037549


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   09079
58536205  
00010596  00000-0  82463-4 0  9098
2 25544  51
6392  40
9002 0009180 144
5944 215
5828 15
71586033 32018


Satellite: ISS
Catalog Number: 25544
Epoch time:      09079
58536205   =   yrday
fracday
Element set:     909
Inclination:       51
6392  deg
RA of node:        40
9002  deg
Eccentricity:     
0009180     
Arg of perigee:   144
5944  deg
Mean anomaly:     215
5828  deg
Mean motion:   15
71586033  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3201
Checksum:              306


Coasting Arc #11 (Orbit 3215)
---------------------------------------

Vector Time (GMT): 2009/080/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2442356
73                 A    =         6727002
96  meter
 Y    =       -3376483
81  meter          E    =           
0021277
 Z    =       -5297813
36                 I    =           51
81211
 XDOT =       6242
502104                 Wp   =          111
11583
 YDOT =       4477
690536  meter/sec      RA   =           35
55391  deg
 ZDOT =         16
640675                 TA   =          159
08567
                                          MA   =          158
99851
                                          Ha   =            196
570  n
mi
                                          Hp   =            185
334

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8012981
40                 X    =         2505667
08
 Y    =      -11077702
79  feet           Y    =        -3348818
23  meter
 Z    =      -17381277
44                 Z    =        -5285794
61
 XDOT =      20480
649947                 XDOT =        6191
887029
 YDOT =      14690
585749  feet/sec       YDOT =        4547
214830  meter/sec
 ZDOT =         54
595390                 ZDOT =          46
843157

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6745432
11                 X    =         2056007
71
 Y    =      -11960105
21  feet           Y    =        -3645440
07  meter
 Z    =      -17334566
75                 Z    =        -5283575
95
 XDOT =      21202
344897                 XDOT =        6462
474725
 YDOT =      11672
010513  feet/sec       YDOT =        3557
628804  meter/sec
 ZDOT =        172
852170                 ZDOT =          52
685341


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   09080
53916962  
00010596  00000-0  82463-4 0  9109
2 25544  51
6400  36
0189 0009035 148
1743 211
9966 15
71584544 32160


Satellite: ISS
Catalog Number: 25544
Epoch time:      09080
53916962   =   yrday
fracday
Element set:     910
Inclination:       51
6400  deg
RA of node:        36
0189  deg
Eccentricity:     
0009035     
Arg of perigee:   148
1743  deg
Mean anomaly:     211
9966  deg
Mean motion:   15
71584544  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3216
Checksum:              309


Coasting Arc #12 (Orbit 3231)
---------------------------------------

Vector Time (GMT): 2009/081/12:33:35
153
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6039877
91                 A    =         6738792
83  meter
 Y    =       -2863896
74  meter          E    =           
0022002
 Z    =         752037
46                 I    =           51
82792
 XDOT =       1434
800554                 Wp   =          136
85029
 YDOT =      -4622
857487  meter/sec      RA   =           30
44277  deg
 ZDOT =      -5994
543019                 TA   =           34
97393
                                          MA   =           34
82961
                                          Ha   =            196
488  n
mi
                                          Hp   =            185
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19815872
42                 X    =        -6011057
66
 Y    =       -9395986
68  feet           Y    =        -2931276
98  meter
 Z    =        2467314
51                 Z    =          722766
35
 XDOT =       4707
350899                 XDOT =        1515
507485
 YDOT =     -15166
855271  feet/sec       YDOT =       -4606
361862  meter/sec
 ZDOT =     -19667
135889                 ZDOT =       -5987
376507

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20919383
89                 X    =        -6376228
21
 Y    =       -6624552
32  feet           Y    =        -2019163
55  meter
 Z    =        2352804
83                 Z    =          717134
91
 XDOT =       2239
934424                 XDOT =         682
732012
 YDOT =     -14154
641044  feet/sec       YDOT =       -4314
334590  meter/sec
 ZDOT =     -19639
460003                 ZDOT =       -5986
107409


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   09081
55655029  
00010596  00000-0  82463-4 0  9117
2 25544  51
6407  30
8128 0009086 151
8636 208
3018 15
71602736 32320


Satellite: ISS
Catalog Number: 25544
Epoch time:      09081
55655029   =   yrday
fracday
Element set:     911
Inclination:       51
6407  deg
RA of node:        30
8128  deg
Eccentricity:     
0009086     
Arg of perigee:   151
8636  deg
Mean anomaly:     208
3018  deg
Mean motion:   15
71602736  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3232
Checksum:              297

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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