Date: March 7th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 2979)
---------------------------------------

Vector Time (GMT): 2009/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2786730
13                 A    =         6739763
92  meter
 Y    =       -6120317
27  meter          E    =           
0019610
 Z    =        -356259
13                 I    =           51
96736
 XDOT =       4194
586993                 Wp   =          118
07151
 YDOT =       2246
890791  meter/sec      RA   =          112
10602  deg
 ZDOT =      -6049
311409                 TA   =           65
77957
                                          MA   =           65
57476
                                          Ha   =            197
725  n
mi
                                          Hp   =            184
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9142815
40                 X    =         2856692
03
 Y    =      -20079781
06  feet           Y    =        -6088763
25  meter
 Z    =       -1168829
17                 Z    =         -342551
50
 XDOT =      13761
768351                 XDOT =        4198
535984
 YDOT =       7371
688947  feet/sec       YDOT =        2293
819141  meter/sec
 ZDOT =     -19846
822207                 ZDOT =       -6028
924957

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14448759
74                 X    =         4403981
97
 Y    =      -16677624
70  feet           Y    =        -5083340
01  meter
 Z    =       -1115804
10                 Z    =         -340097
09
 XDOT =      10012
725525                 XDOT =        3051
878740
 YDOT =       9937
306516  feet/sec       YDOT =        3028
891026  meter/sec
 ZDOT =     -19767
050016                 ZDOT =       -6024
996845


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   09065
53122336  
00010596  00000-0  82463-4 0  9005
2 25544  51
6408 112
7996 0009571  94
1997 266
0259 15
71319588 29809


Satellite: ISS
Catalog Number: 25544
Epoch time:      09065
53122336   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:       112
7996  deg
Eccentricity:     
0009571     
Arg of perigee:    94
1997  deg
Mean anomaly:     266
0259  deg
Mean motion:   15
71319588  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2980
Checksum:              334


Coasting Arc #2 (Orbit 2995)
---------------------------------------

Vector Time (GMT): 2009/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4142391
13                 A    =         6727817
61  meter
 Y    =        -547250
23  meter          E    =           
0012411
 Z    =        5262873
59                 I    =           51
93652
 XDOT =       1779
257557                 Wp   =          102
11026
 YDOT =      -7472
411933  meter/sec      RA   =          107
01525  deg
 ZDOT =        619
674991                 TA   =          342
00582
                                          MA   =          342
04971
                                          Ha   =            197
828  n
mi
                                          Hp   =            184
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13590522
09                 X    =        -4161529
28
 Y    =       -1795440
39  feet           Y    =         -593679
70  meter
 Z    =       17266645
62                 Z    =         5242703
88
 XDOT =       5837
459178                 XDOT =        1859
672878
 YDOT =     -24515
787182  feet/sec       YDOT =       -7452
065595  meter/sec
 ZDOT =       2033
054433                 ZDOT =         628
513966

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12719704
81                 X    =        -3876966
03
 Y    =       -5371209
78  feet           Y    =        -1637144
74  meter
 Z    =       17187849
28                 Z    =         5238856
46
 XDOT =      11743
598496                 XDOT =        3579
448821
 YDOT =     -21156
301323  feet/sec       YDOT =       -6448
440643  meter/sec
 ZDOT =       2066
967198                 ZDOT =         630
011602


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   09066
54879216  
00010596  00000-0  82463-4 0  9014
2 25544  51
6400 107
5952 0009595  98
0632 262
1619 15
71337356 29967


Satellite: ISS
Catalog Number: 25544
Epoch time:      09066
54879216   =   yrday
fracday
Element set:     901
Inclination:       51
6400  deg
RA of node:       107
5952  deg
Eccentricity:     
0009595     
Arg of perigee:    98
0632  deg
Mean anomaly:     262
1619  deg
Mean motion:   15
71337356  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            2996
Checksum:              331


Coasting Arc #3 (Orbit 3010)
---------------------------------------

Vector Time (GMT): 2009/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -257503
32                 A    =         6738831
12  meter
 Y    =        6583052
41  meter          E    =           
0015465
 Z    =       -1414586
39                 I    =           51
98178
 XDOT =      -4890
153392                 Wp   =           71
40805
 YDOT =       1052
102578  meter/sec      RA   =          101
90385  deg
 ZDOT =       5842
909737                 TA   =          273
13726
                                          MA   =          273
31419
                                          Ha   =            197
656  n
mi
                                          Hp   =            184
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -844827
17                 X    =         -324225
34
 Y    =       21597940
99  feet           Y    =         6579799
71  meter
 Z    =       -4641031
46                 Z    =        -1415999
77
 XDOT =     -16043
810340                 XDOT =       -4929
937814
 YDOT =       3451
780112  feet/sec       YDOT =         997
195939  meter/sec
 ZDOT =      19169
651369                 ZDOT =        5819
057280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6176662
07                 X    =        -1882646
60
 Y    =       20712008
10  feet           Y    =         6313020
07  meter
 Z    =       -4646022
67                 Z    =        -1416107
71
 XDOT =     -14994
478410                 XDOT =       -4570
317019
 YDOT =       -234
013256  feet/sec       YDOT =         -71
327241  meter/sec
 ZDOT =      19076
597965                 ZDOT =        5814
547060


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   09067
50275199  
00010596  00000-0  82463-4 0  9022
2 25544  51
6406 102
7155 0009626 101
3187 258
9056 15
71356738 30115


Satellite: ISS
Catalog Number: 25544
Epoch time:      09067
50275199   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       102
7155  deg
Eccentricity:     
0009626     
Arg of perigee:   101
3187  deg
Mean anomaly:     258
9056  deg
Mean motion:   15
71356738  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3011
Checksum:              307


Coasting Arc #4 (Orbit 3026)
---------------------------------------

Vector Time (GMT): 2009/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4087124
47                 A    =         6729722
66  meter
 Y    =       -2326852
41  meter          E    =           
0020510
 Z    =       -4831495
54                 I    =           51
95610
 XDOT =       1120
602311                 Wp   =           86
94605
 YDOT =       7171
403650  meter/sec      RA   =           96
84348  deg
 ZDOT =      -2513
856910                 TA   =          158
54284
                                          MA   =          158
45674
                                          Ha   =            197
649  n
mi
                                          Hp   =            184
515

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13409201
02                 X    =         4136309
95
 Y    =       -7634030
21  feet           Y    =        -2280873
21  meter
 Z    =      -15851363
31                 Z    =        -4811521
08
 XDOT =       3676
516767                 XDOT =        1052
538776
 YDOT =      23528
227199  feet/sec       YDOT =        7183
554096  meter/sec
 ZDOT =      -8247
562042                 ZDOT =       -2508
579098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14906040
25                 X    =         4543361
07
 Y    =       -4284371
17  feet           Y    =        -1305876
33  meter
 Z    =      -15773551
78                 Z    =        -4807778
58
 XDOT =      -2163
377088                 XDOT =        -659
397336
 YDOT =      22662
080449  feet/sec       YDOT =        6907
402121  meter/sec
 ZDOT =      -8226
378533                 ZDOT =       -2507
400177


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   09068
52029571  
00010596  00000-0  82463-4 0  9037
2 25544  51
6407  97
5097 0009635 105
1459 255
0769 15
71358569 30276


Satellite: ISS
Catalog Number: 25544
Epoch time:      09068
52029571   =   yrday
fracday
Element set:     903
Inclination:       51
6407  deg
RA of node:        97
5097  deg
Eccentricity:     
0009635     
Arg of perigee:   105
1459  deg
Mean anomaly:     255
0769  deg
Mean motion:   15
71358569  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3027
Checksum:              333


Coasting Arc #5 (Orbit 3042)
---------------------------------------

Vector Time (GMT): 2009/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2132364
85                 A    =         6735858
24  meter
 Y    =       -5658893
47  meter          E    =           
0022944
 Z    =        2941539
97                 I    =           51
97787
 XDOT =       4069
081191                 Wp   =          101
95454
 YDOT =      -4169
276524  meter/sec      RA   =           91
70726  deg
 ZDOT =      -5042
870736                 TA   =           44
31693
                                          MA   =           44
13347
                                          Ha   =            197
618  n
mi
                                          Hp   =            184
370

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6995947
68                 X    =        -2083216
89
 Y    =      -18565923
45  feet           Y    =        -5682463
70  meter
 Z    =        9650721
69                 Z    =         2931301
12
 XDOT =      13350
003906                 XDOT =        4139
897217
 YDOT =     -13678
728752  feet/sec       YDOT =       -4123
378270  meter/sec
 ZDOT =     -16544
851497                 ZDOT =       -5022
931057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2877981
32                 X    =         -877208
71
 Y    =      -19650262
12  feet           Y    =        -5989399
89  meter
 Z    =        9610288
69                 Z    =         2929215
99
 XDOT =      14648
064348                 XDOT =        4464
730013
 YDOT =     -10244
398077  feet/sec       YDOT =       -3122
492534  meter/sec
 ZDOT =     -16467
320821                 ZDOT =       -5019
239386


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   09069
53782579  
00010596  00000-0  82463-4 0  9044
2 25544  51
6392  92
3039 0009688 107
9139 252
3080 15
71402675 30433


Satellite: ISS
Catalog Number: 25544
Epoch time:      09069
53782579   =   yrday
fracday
Element set:     904
Inclination:       51
6392  deg
RA of node:        92
3039  deg
Eccentricity:     
0009688     
Arg of perigee:   107
9139  deg
Mean anomaly:     252
3080  deg
Mean motion:   15
71402675  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3043
Checksum:              327


Coasting Arc #6 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2009/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2743484
97                 A    =         6733196
48  meter
 Y    =        4778198
72  meter          E    =           
0020933
 Z    =        3857001
57                 I    =           51
96797
 XDOT =      -3568
450849                 Wp   =          104
44982
 YDOT =      -5418
985306  meter/sec      RA   =           86
66390  deg
 ZDOT =       4151
257849                 TA   =          302
27504
                                          MA   =          302
47768
                                          Ha   =            197
620  n
mi
                                          Hp   =            184
436

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9000934
96                 X    =        -2815448
07
 Y    =       15676504
99  feet           Y    =         4747117
55  meter
 Z    =       12654204
62                 Z    =         3843498
55
 XDOT =     -11707
515910                 XDOT =       -3527
755446
 YDOT =     -17778
823181  feet/sec       YDOT =       -5458
661787  meter/sec
 ZDOT =      13619
612366                 ZDOT =        4134
022007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12012339
06                 X    =        -3661360
94
 Y    =       13557120
92  feet           Y    =         4132210
46  meter
 Z    =       12601853
68                 Z    =         3841045
00
 XDOT =      -7023
333817                 XDOT =       -2140
712148
 YDOT =     -18892
753153  feet/sec       YDOT =       -5758
511161  meter/sec
 ZDOT =      13551
880296                 ZDOT =        4130
613114


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
55534353  
00010596  00000-0  82463-4 0  9054
2 25544  51
6387  87
0981 0009690 111
5647 248
6548 15
71395682 30595


Satellite: ISS
Catalog Number: 25544
Epoch time:      09070
55534353   =   yrday
fracday
Element set:     905
Inclination:       51
6387  deg
RA of node:        87
0981  deg
Eccentricity:     
0009690     
Arg of perigee:   111
5647  deg
Mean anomaly:     248
6548  deg
Mean motion:   15
71395682  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3059
Checksum:              339


Coasting Arc #7 (Orbit 3073)
---------------------------------------

Vector Time (GMT): 2009/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3859810
67                 A    =         6732017
41  meter
 Y    =        3593967
98  meter          E    =           
0017527
 Z    =       -4202243
69                 I    =           51
96188
 XDOT =      -1968
761942                 Wp   =          112
66244
 YDOT =       6436
474196  meter/sec      RA   =           81
52037  deg
 ZDOT =       3702
077400                 TA   =          195
03821
                                          MA   =          195
09039
                                          Ha   =            197
469  n
mi
                                          Hp   =            184
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12663420
83                 X    =         3839749
05
 Y    =       11791233
53  feet           Y    =         3637017
99  meter
 Z    =      -13786888
75                 Z    =        -4183542
00
 XDOT =      -6459
192722                 XDOT =       -2058
573244
 YDOT =      21117
041325  feet/sec       YDOT =        6413
956604  meter/sec
 ZDOT =      12145
923228                 ZDOT =        3692
294356

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10382186
14                 X    =         3164490
34
 Y    =       13914797
92  feet           Y    =         4241230
41  meter
 Z    =      -13713581
82                 Z    =        -4179899
74
 XDOT =      -9251
503376                 XDOT =       -2819
858229
 YDOT =      18817
658759  feet/sec       YDOT =        5735
622390  meter/sec
 ZDOT =      12108
221840                 ZDOT =        3690
586017


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
50925284  
00010596  00000-0  82463-4 0  9068
2 25544  51
6395  82
2181 0009548 115
0365 245
1789 15
71406706 30747


Satellite: ISS
Catalog Number: 25544
Epoch time:      09071
50925284   =   yrday
fracday
Element set:     906
Inclination:       51
6395  deg
RA of node:        82
2181  deg
Eccentricity:     
0009548     
Arg of perigee:   115
0365  deg
Mean anomaly:     245
1789  deg
Mean motion:   15
71406706  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3074
Checksum:              315


Coasting Arc #8 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2009/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         570890
63                 A    =         6736647
13  meter
 Y    =       -6202460
96  meter          E    =           
0014721
 Z    =       -2564716
28                 I    =           51
97111
 XDOT =       4904
453369                 Wp   =          122
34266
 YDOT =       2634
426774  meter/sec      RA   =           76
47273  deg
 ZDOT =      -5309
032792                 TA   =           86
56265
                                          MA   =           86
39427
                                          Ha   =            197
428  n
mi
                                          Hp   =            184
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1873000
77                 X    =          652664
05
 Y    =      -20349281
35  feet           Y    =        -6195619
96  meter
 Z    =       -8414423
49                 Z    =        -2561743
67
 XDOT =      16090
726275                 XDOT =        4900
420509
 YDOT =       8643
132461  feet/sec       YDOT =        2689
248159  meter/sec
 ZDOT =     -17418
086587                 ZDOT =       -5285
217085

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5256749
12                 X    =         1602257
13
 Y    =      -19752347
74  feet           Y    =        -6020515
59  meter
 Z    =       -8403288
26                 Z    =        -2561322
26
 XDOT =      13100
544352                 XDOT =        3993
045919
 YDOT =      10815
562326  feet/sec       YDOT =        3296
583397  meter/sec
 ZDOT =     -17324
889268                 ZDOT =       -5280
626249


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
52674393  
00010596  00000-0  82463-4 0  9074
2 25544  51
6384  77
0113 0009610 119
2088 241
0036 15
71431089 30900


Satellite: ISS
Catalog Number: 25544
Epoch time:      09072
52674393   =   yrday
fracday
Element set:     907
Inclination:       51
6384  deg
RA of node:        77
0113  deg
Eccentricity:     
0009610     
Arg of perigee:   119
2088  deg
Mean anomaly:     241
0036  deg
Mean motion:   15
71431089  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3090
Checksum:              294


Coasting Arc #9 (Orbit 3105)
---------------------------------------

Vector Time (GMT): 2009/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4421072
99                 A    =         6728695
36  meter
 Y    =        -904336
92  meter          E    =           
0013125
 Z    =        4979515
93                 I    =           51
93633
 XDOT =       -800
497243                 Wp   =           97
45725
 YDOT =      -7385
873399  meter/sec      RA   =           71
34032  deg
 ZDOT =      -2049
178456                 TA   =           12
29714
                                          MA   =           12
26514
                                          Ha   =            197
411  n
mi
                                          Hp   =            184
577

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14504832
66                 X    =        -4434821
54
 Y    =       -2966984
65  feet           Y    =         -953852
42  meter
 Z    =       16336994
52                 Z    =         4958005
05
 XDOT =      -2626
303291                 XDOT =        -707
893148
 YDOT =     -24231
868106  feet/sec       YDOT =       -7394
307409  meter/sec
 ZDOT =      -6723
026430                 ZDOT =       -2052
841757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13998082
90                 X    =        -4266615
67
 Y    =       -5097694
49  feet           Y    =        -1553777
28  meter
 Z    =       16252930
33                 Z    =         4953893
16
 XDOT =        660
674875                 XDOT =         201
373702
 YDOT =     -23327
038003  feet/sec       YDOT =       -7110
081183  meter/sec
 ZDOT =      -6737
880778                 ZDOT =       -2053
706061


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
54422037  
00010596  00000-0  82463-4 0  9084
2 25544  51
6382  71
8055 0009471 122
7009 237
5067 15
71472865 31061


Satellite: ISS
Catalog Number: 25544
Epoch time:      09073
54422037   =   yrday
fracday
Element set:     908
Inclination:       51
6382  deg
RA of node:        71
8055  deg
Eccentricity:     
0009471     
Arg of perigee:   122
7009  deg
Mean anomaly:     237
5067  deg
Mean motion:   15
71472865  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3106
Checksum:              305


Coasting Arc #10 (Orbit 3121)
---------------------------------------

Vector Time (GMT): 2009/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1962589
50                 A    =         6738766
18  meter
 Y    =        6368014
45  meter          E    =           
0019034
 Z    =         978718
76                 I    =           51
96050
 XDOT =      -4841
821396                 Wp   =           84
01913
 YDOT =        562
226454  meter/sec      RA   =           66
27224  deg
 ZDOT =       5954
482672                 TA   =          286
61337
                                          MA   =          286
82229
                                          Ha   =            197
154  n
mi
                                          Hp   =            184
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6438941
94                 X    =         1886481
00
 Y    =       20892435
87  feet           Y    =         6389535
78  meter
 Z    =        3211019
54                 Z    =          988067
79
 XDOT =     -15885
240799                 XDOT =       -4876
674238
 YDOT =       1844
574981  feet/sec       YDOT =         507
887846  meter/sec
 ZDOT =      19535
704305                 ZDOT =        5930
876429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3624350
96                 X    =         1104702
17
 Y    =       21554098
00  feet           Y    =         6569689
07  meter
 Z    =        3247989
54                 Z    =          989987
21
 XDOT =     -14529
870275                 XDOT =       -4428
704460
 YDOT =       -533
916858  feet/sec       YDOT =        -162
737858  meter/sec
 ZDOT =      19443
564825                 ZDOT =        5926
398559


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
56168157  
00010596  00000-0  82463-4 0  9098
2 25544  51
6385  66
6004 0009581 127
5099 232
6935 15
71539241 31224


Satellite: ISS
Catalog Number: 25544
Epoch time:      09074
56168157   =   yrday
fracday
Element set:     909
Inclination:       51
6385  deg
RA of node:        66
6004  deg
Eccentricity:     
0009581     
Arg of perigee:   127
5099  deg
Mean anomaly:     232
6935  deg
Mean motion:   15
71539241  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3122
Checksum:              322


Coasting Arc #11 (Orbit 3136)
---------------------------------------

Vector Time (GMT): 2009/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3758929
21                 A    =         6727297
85  meter
 Y    =       -1791415
47  meter          E    =           
0023184
 Z    =       -5302979
05                 I    =           51
90818
 XDOT =       3554
173989                 Wp   =          106
11518
 YDOT =       6804
921461  meter/sec      RA   =           61
16418  deg
 ZDOT =        215
020298                 TA   =          165
95574
                                          MA   =          165
89116
                                          Ha   =            197
149  n
mi
                                          Hp   =            184
833

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12332444
93                 X    =         3804442
61
 Y    =       -5877347
35  feet           Y    =        -1749126
65  meter
 Z    =      -17398225
23                 Z    =        -5284607
59
 XDOT =      11660
675816                 XDOT =        3476
771540
 YDOT =      22325
857813  feet/sec       YDOT =        6844
233533  meter/sec
 ZDOT =        705
447171                 ZDOT =         232
098182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13022200
53                 X    =         3969166
72
 Y    =       -4420572
57  feet           Y    =        -1347390
52  meter
 Z    =      -17326611
98                 Z    =        -5281151
33
 XDOT =       8710
604689                 XDOT =        2654
992309
 YDOT =      22560
439586  feet/sec       YDOT =        6876
421986  meter/sec
 ZDOT =        772
620075                 ZDOT =         235
494599


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
51554239  
00010596  00000-0  82463-4 0  9106
2 25544  51
6384  61
7191 0009437 129
7802 230
4192 15
71488576 31373


Satellite: ISS
Catalog Number: 25544
Epoch time:      09075
51554239   =   yrday
fracday
Element set:     910
Inclination:       51
6384  deg
RA of node:        61
7191  deg
Eccentricity:     
0009437     
Arg of perigee:   129
7802  deg
Mean anomaly:     230
4192  deg
Mean motion:   15
71488576  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3137
Checksum:              319


Coasting Arc #12 (Orbit 3152)
---------------------------------------

Vector Time (GMT): 2009/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 638785
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4124944
29                 A    =         6739044
82  meter
 Y    =       -5280467
55  meter          E    =           
0022529
 Z    =         605635
28                 I    =           51
93320
 XDOT =       3415
840567                 Wp   =          130
30286
 YDOT =      -3374
361461  meter/sec      RA   =           56
06325  deg
 ZDOT =      -6024
015034                 TA   =           43
13167
                                          MA   =           42
95538
                                          Ha   =            196
989  n
mi
                                          Hp   =            184
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13533281
79                 X    =        -4068532
70
 Y    =      -17324368
62  feet           Y    =        -5326279
66  meter
 Z    =        1986992
39                 Z    =          585733
55
 XDOT =      11206
826008                 XDOT =        3482
582813
 YDOT =     -11070
739701  feet/sec       YDOT =       -3335
790513  meter/sec
 ZDOT =     -19763
828852                 ZDOT =       -6007
258758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11800362
95                 X    =        -3596750
63
 Y    =      -18556376
72  feet           Y    =        -5655983
62  meter
 Z    =        1908905
52                 Z    =          581834
40
 XDOT =      10988
118962                 XDOT =        3349
178660
 YDOT =      -9060
199585  feet/sec       YDOT =       -2761
548834  meter/sec
 ZDOT =     -19698
628832                 ZDOT =       -6004
142068


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
53297728  
00010596  00000-0  82463-4 0  9117
2 25544  51
6387  56
5128 0009318 133
0110 227
1834 15
71540785 31531


Satellite: ISS
Catalog Number: 25544
Epoch time:      09076
53297728   =   yrday
fracday
Element set:     911
Inclination:       51
6387  deg
RA of node:        56
5128  deg
Eccentricity:     
0009318     
Arg of perigee:   133
0110  deg
Mean anomaly:     227
1834  deg
Mean motion:   15
71540785  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3153
Checksum:              308

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