Date: May 27th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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 238)
---------------------------------------

Vector Time (GMT): 2009/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1183241
88                 A    =         6732589
38  meter
 Y    =        6204093
42  meter          E    =           
0022796
 Z    =        2294668
80                 I    =           51
94968
 XDOT =      -5339
901201                 Wp   =           59
64723
 YDOT =      -1014
164337  meter/sec      RA   =           62
68123  deg
 ZDOT =       5466
819605                 TA   =          326
05139
                                          MA   =          326
19706
                                          Ha   =            194
701  n
mi
                                          Hp   =            182
520

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3882027
17                 X    =         1102631
47
 Y    =       20354637
19  feet           Y    =         6216873
97  meter
 Z    =        7528440
95                 Z    =         2300222
44
 XDOT =     -17519
360895                 XDOT =       -5354
720974
 YDOT =      -3327
310817  feet/sec       YDOT =       -1073
962117  meter/sec
 ZDOT =      17935
759858                 ZDOT =        5440
841790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19821079
04                 X    =         6041464
89
 Y    =        6014461
24  feet           Y    =         1833207
79  meter
 Z    =        7550489
73                 Z    =         2301389
27
 XDOT =     -10664
373592                 XDOT =       -3250
501071
 YDOT =      12638
824960  feet/sec       YDOT =        3852
313848  meter/sec
 ZDOT =      17833
960879                 ZDOT =        5435
791276


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   09145
55896977  
00010596  00000-0  82463-4 0  9005
2 25544  51
6417  62
9997 0009680  41
3196 318
8698 15
73048772  2396


Satellite: ISS
Catalog Number: 25544
Epoch time:      09145
55896977   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:        62
9997  deg
Eccentricity:     
0009680     
Arg of perigee:    41
3196  deg
Mean anomaly:     318
8698  deg
Mean motion:   15
73048772  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             239
Checksum:              361


Coasting Arc #2 (Orbit 253)
---------------------------------------

Vector Time (GMT): 2009/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4624045
82                 A    =         6724503
18  meter
 Y    =         119409
62  meter          E    =           
0018710
 Z    =       -4895396
92                 I    =           51
90867
 XDOT =       2271
012545                 Wp   =           79
61298
 YDOT =       6965
858025  meter/sec      RA   =           57
53467  deg
 ZDOT =       2325
818984                 TA   =          212
93760
                                          MA   =          213
05431
                                          Ha   =            194
694  n
mi
                                          Hp   =            182
483

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15170754
00                 X    =         4646148
02
 Y    =         391763
85  feet           Y    =          171242
92  meter
 Z    =      -16061013
53                 Z    =        -4872879
42
 XDOT =       7450
828561                 XDOT =        2181
651865
 YDOT =      22853
864910  feet/sec       YDOT =        6990
753722  meter/sec
 ZDOT =       7630
639710                 ZDOT =        2336
635932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7178158
56                 X    =         2187902
73
 Y    =      -13476090
05  feet           Y    =        -4107512
25  meter
 Z    =      -15972803
39                 Z    =        -4868510
47
 XDOT =      22770
304890                 XDOT =        6940
388930
 YDOT =       3075
965549  feet/sec       YDOT =         937
554299  meter/sec
 ZDOT =       7673
335075                 ZDOT =        2338
832531


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   09146
51187304  
00010596  00000-0  82463-4 0  9010
2 25544  51
6423  58
1130 0009624  44
5962 315
5974 15
73088705  2541


Satellite: ISS
Catalog Number: 25544
Epoch time:      09146
51187304   =   yrday
fracday
Element set:     901
Inclination:       51
6423  deg
RA of node:        58
1130  deg
Eccentricity:     
0009624     
Arg of perigee:    44
5962  deg
Mean anomaly:     315
5974  deg
Mean motion:   15
73088705  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             254
Checksum:              301


Coasting Arc #3 (Orbit 269)
---------------------------------------

Vector Time (GMT): 2009/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2746808
63                 A    =         6733295
09  meter
 Y    =       -5883010
39  meter          E    =           
0011663
 Z    =       -1795298
05                 I    =           51
92190
 XDOT =       5121
950507                 Wp   =           87
15597
 YDOT =       -661
957554  meter/sec      RA   =           52
46000  deg
 ZDOT =      -5698
500463                 TA   =          112
63367
                                          MA   =          112
51028
                                          Ha   =            194
641  n
mi
                                          Hp   =            182
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9011839
32                 X    =        -2672098
42
 Y    =      -19301215
18  feet           Y    =        -5913308
75  meter
 Z    =       -5890085
47                 Z    =        -1808461
67
 XDOT =      16804
299565                 XDOT =        5156
654277
 YDOT =      -2171
776751  feet/sec       YDOT =        -604
485841  meter/sec
 ZDOT =     -18695
867662                 ZDOT =       -5673
533808

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21285669
57                 X    =        -6487872
08
 Y    =        -238936
31  feet           Y    =          -72827
79  meter
 Z    =       -5941922
48                 Z    =        -1811097
97
 XDOT =       5327
801912                 XDOT =        1623
914023
 YDOT =     -14639
677383  feet/sec       YDOT =       -4462
173666  meter/sec
 ZDOT =     -18598
092107                 ZDOT =       -5668
698474


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   09147
52828463  
00010596  00000-0  82463-4 0  9021
2 25544  51
6426  52
9000 0009491  48
4804 311
7172 15
73103996  2708


Satellite: ISS
Catalog Number: 25544
Epoch time:      09147
52828463   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:        52
9000  deg
Eccentricity:     
0009491     
Arg of perigee:    48
4804  deg
Mean anomaly:     311
7172  deg
Mean motion:   15
73103996  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             270
Checksum:              299


Coasting Arc #4 (Orbit 285)
---------------------------------------

Vector Time (GMT): 2009/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4238671
48                 A    =         6723444
60  meter
 Y    =        1259209
33  meter          E    =           
0014855
 Z    =        5057181
95                 I    =           51
86994
 XDOT =      -3991
520430                 Wp   =           52
13846
 YDOT =      -6355
327299  meter/sec      RA   =           47
31813  deg
 ZDOT =      -1750
646054                 TA   =           54
71688
                                          MA   =           54
57801
                                          Ha   =            194
675  n
mi
                                          Hp   =            182
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13906402
48                 X    =        -4277003
96
 Y    =        4131264
20  feet           Y    =         1211594
90  meter
 Z    =       16591804
29                 Z    =         5036497
61
 XDOT =     -13095
539467                 XDOT =       -3911
653124
 YDOT =     -20850
811350  feet/sec       YDOT =       -6399
515970  meter/sec
 ZDOT =      -5743
589417                 ZDOT =       -1769
843840

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2072855
60                 X    =         -631806
39
 Y    =       14451269
95  feet           Y    =         4404747
08  meter
 Z    =       16510827
05                 Z    =         5032500
09
 XDOT =     -23342
163567                 XDOT =       -7114
691455
 YDOT =       3346
982978  feet/sec       YDOT =        1020
160412  meter/sec
 ZDOT =      -5819
088783                 ZDOT =       -1773
658261


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   09148
54467477  
00010596  00000-0  82463-4 0  9039
2 25544  51
6422  47
6871 0009495  51
2221 308
9789 15
73190921  2863


Satellite: ISS
Catalog Number: 25544
Epoch time:      09148
54467477   =   yrday
fracday
Element set:     903
Inclination:       51
6422  deg
RA of node:        47
6871  deg
Eccentricity:     
0009495     
Arg of perigee:    51
2221  deg
Mean anomaly:     308
9789  deg
Mean motion:   15
73190921  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             286
Checksum:              332


Coasting Arc #5 (Orbit 301)
---------------------------------------

Vector Time (GMT): 2009/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4172198
99                 A    =         6733840
85  meter
 Y    =        5118895
25  meter          E    =           
0023486
 Z    =        1256672
67                 I    =           51
88414
 XDOT =      -4469
424697                 Wp   =           57
06899
 YDOT =       2181
185865  meter/sec      RA   =           42
23185  deg
 ZDOT =       5887
550786                 TA   =          316
67633
                                          MA   =          316
86075
                                          Ha   =            194
650  n
mi
                                          Hp   =            181
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13688316
88                 X    =         4108543
88
 Y    =       16794275
77  feet           Y    =         5165195
14  meter
 Z    =        4122941
84                 Z    =         1276787
23
 XDOT =     -14663
466854                 XDOT =       -4522
083482
 YDOT =       7156
121605  feet/sec       YDOT =        2130
910933  meter/sec
 ZDOT =      19316
111504                 ZDOT =        5865
710762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20861795
44                 X    =         6358675
25
 Y    =       -5791824
98  feet           Y    =        -1765348
25  meter
 Z    =        4201978
28                 Z    =         1280762
98
 XDOT =        215
632981                 XDOT =          65
724933
 YDOT =      14883
451068  feet/sec       YDOT =        4536
475886  meter/sec
 ZDOT =      19230
645738                 ZDOT =        5861
500821


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   09149
56104824  
00010596  00000-0  82463-4 0  9047
2 25544  51
6426  42
4738 0009555  55
0923 305
1136 15
73168613  3027


Satellite: ISS
Catalog Number: 25544
Epoch time:      09149
56104824   =   yrday
fracday
Element set:     904
Inclination:       51
6426  deg
RA of node:        42
4738  deg
Eccentricity:     
0009555     
Arg of perigee:    55
0923  deg
Mean anomaly:     305
1136  deg
Mean motion:   15
73168613  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             302
Checksum:              294


Coasting Arc #6 (Orbit 316)
---------------------------------------

Vector Time (GMT): 2009/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3501438
89                 A    =         6722799
67  meter
 Y    =       -2474525
44  meter          E    =           
0022291
 Z    =       -5196549
68                 I    =           51
82487
 XDOT =       5457
904268                 Wp   =           82
81042
 YDOT =       5280
409212  meter/sec      RA   =           37
09530  deg
 ZDOT =       1170
075702                 TA   =          198
31860
                                          MA   =          198
39901
                                          Ha   =            194
566  n
mi
                                          Hp   =            181
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11487660
42                 X    =         3554093
09
 Y    =       -8118521
78  feet           Y    =        -2435075
32  meter
 Z    =      -17049047
51                 Z    =        -5179412
08
 XDOT =      17906
510066                 XDOT =        5392
768185
 YDOT =      17324
177206  feet/sec       YDOT =        5341
078360  meter/sec
 ZDOT =       3838
831044                 ZDOT =        1196
432550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3035384
84                 X    =         -925185
30
 Y    =      -13818258
83  feet           Y    =        -4211805
29  meter
 Z    =      -16982017
57                 Z    =        -5176118
95
 XDOT =      21864
256733                 XDOT =        6664
225452
 YDOT =      -9619
441884  feet/sec       YDOT =       -2932
005886  meter/sec
 ZDOT =       3942
330175                 ZDOT =        1201
622237


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   09150
51387804  
00010596  00000-0  82463-4 0  9056
2 25544  51
6430  37
5862 0009423  58
3901 301
8180 15
73222070  3177


Satellite: ISS
Catalog Number: 25544
Epoch time:      09150
51387804   =   yrday
fracday
Element set:     905
Inclination:       51
6430  deg
RA of node:        37
5862  deg
Eccentricity:     
0009423     
Arg of perigee:    58
3901  deg
Mean anomaly:     301
8180  deg
Mean motion:   15
73222070  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             317
Checksum:              283


Coasting Arc #7 (Orbit 332)
---------------------------------------

Vector Time (GMT): 2009/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5305488
15                 A    =         6734126
20  meter
 Y    =       -4065830
69  meter          E    =           
0015186
 Z    =        -810471
25                 I    =           51
83874
 XDOT =       3479
328030                 Wp   =          103
88824
 YDOT =      -3367
364829  meter/sec      RA   =           31
99697  deg
 ZDOT =      -5980
173477                 TA   =           84
91768
                                          MA   =           84
74436
                                          Ha   =            194
560  n
mi
                                          Hp   =            181
887

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17406457
18                 X    =        -5255691
89
 Y    =      -13339339
54  feet           Y    =        -4124881
25  meter
 Z    =       -2659026
41                 Z    =         -836124
83
 XDOT =      11415
118208                 XDOT =        3545
774559
 YDOT =     -11047
784871  feet/sec       YDOT =       -3328
084844  meter/sec
 ZDOT =     -19619
991721                 ZDOT =       -5963
109783

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18813449
18                 X    =        -5734339
31
 Y    =       11244166
07  feet           Y    =         3427221
82  meter
 Z    =       -2759712
26                 Z    =         -841160
30
 XDOT =      -5196
695843                 XDOT =       -1583
952893
 YDOT =     -13419
026940  feet/sec       YDOT =       -4090
119411  meter/sec
 ZDOT =     -19553
291294                 ZDOT =       -5959
843186


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   09151
53021280  
00010596  00000-0  82463-4 0  9063
2 25544  51
6432  32
3727 0009268  62
8699 297
3408 15
73204769  3338


Satellite: ISS
Catalog Number: 25544
Epoch time:      09151
53021280   =   yrday
fracday
Element set:     906
Inclination:       51
6432  deg
RA of node:        32
3727  deg
Eccentricity:     
0009268     
Arg of perigee:    62
8699  deg
Mean anomaly:     297
3408  deg
Mean motion:   15
73204769  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             333
Checksum:              311


Coasting Arc #8 (Orbit 348)
---------------------------------------

Vector Time (GMT): 2009/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2514765
60                 A    =         6722251
03  meter
 Y    =        3356649
19  meter          E    =           
0012289
 Z    =        5244355
55                 I    =           51
77386
 XDOT =      -6604
787155                 Wp   =           64
28390
 YDOT =      -3920
747336  meter/sec      RA   =           26
86505  deg
 ZDOT =       -651
235726                 TA   =           31
92705
                                          MA   =           31
85264
                                          Ha   =            194
549  n
mi
                                          Hp   =            181
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8250543
30                 X    =        -2577589
63
 Y    =       11012628
58  feet           Y    =         3328175
84  meter
 Z    =       17205890
92                 Z    =         5231986
45
 XDOT =     -21669
249195                 XDOT =       -6557
290202
 YDOT =     -12863
344277  feet/sec       YDOT =       -3994
340292  meter/sec
 ZDOT =      -2136
600150                 ZDOT =        -683
207022

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7358657
50                 X    =         2242918
81
 Y    =       11698705
14  feet           Y    =         3565765
33  meter
 Z    =       17157581
21                 Z    =         5229630
75
 XDOT =     -18823
783811                 XDOT =       -5737
489305
 YDOT =      15188
893504  feet/sec       YDOT =        4629
574740  meter/sec
 ZDOT =      -2262
024656                 ZDOT =        -689
465115


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   09152
54652585  
00010596  00000-0  82463-4 0  9074
2 25544  51
6433  27
1592 0009274  65
4375 294
7754 15
73295891  3496


Satellite: ISS
Catalog Number: 25544
Epoch time:      09152
54652585   =   yrday
fracday
Element set:     907
Inclination:       51
6433  deg
RA of node:        27
1592  deg
Eccentricity:     
0009274     
Arg of perigee:    65
4375  deg
Mean anomaly:     294
7754  deg
Mean motion:   15
73295891  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             349
Checksum:              340


Coasting Arc #9 (Orbit 364)
---------------------------------------

Vector Time (GMT): 2009/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6138197
98                 A    =         6734066
81  meter
 Y    =        2728216
46  meter          E    =           
0021814
 Z    =         328950
78                 I    =           51
78651
 XDOT =      -2220
432248                 Wp   =           56
73361
 YDOT =       4234
303761  meter/sec      RA   =           21
75388  deg
 ZDOT =       6040
480330                 TA   =          306
83553
                                          MA   =          307
03540
                                          Ha   =            194
441  n
mi
                                          Hp   =            181
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20138444
83                 X    =         6105636
40
 Y    =        8950841
39  feet           Y    =         2796675
28  meter
 Z    =        1079234
86                 Z    =          358691
69
 XDOT =      -7284
882705                 XDOT =       -2296
959818
 YDOT =      13892
072708  feet/sec       YDOT =        4209
045070  meter/sec
 ZDOT =      19817
848851                 ZDOT =        6029
507901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15206036
66                 X    =         4634799
98
 Y    =      -15943200
12  feet           Y    =        -4859487
40  meter
 Z    =        1195863
16                 Z    =          364499
09
 XDOT =       9427
600731                 XDOT =        2873
532703
 YDOT =      10535
968094  feet/sec       YDOT =        3211
363075  meter/sec
 ZDOT =      19775
046407                 ZDOT =        6027
434145


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   09153
56282128  
00010596  00000-0  82463-4 0  9080
2 25544  51
6430  21
9454 0009221  68
9879 291
2270 15
73318092  3653


Satellite: ISS
Catalog Number: 25544
Epoch time:      09153
56282128   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:        21
9454  deg
Eccentricity:     
0009221     
Arg of perigee:    68
9879  deg
Mean anomaly:     291
2270  deg
Mean motion:   15
73318092  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             365
Checksum:              313


Coasting Arc #10 (Orbit 379)
---------------------------------------

Vector Time (GMT): 2009/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1358437
19                 A    =         6721996
79  meter
 Y    =       -3949502
20  meter          E    =           
0023871
 Z    =       -5287279
89                 I    =           51
71720
 XDOT =       7323
578664                 Wp   =           83
72588
 YDOT =       2314
974202  meter/sec      RA   =           16
62598  deg
 ZDOT =        155
522840                 TA   =          187
73350
                                          MA   =          187
77037
                                          Ha   =            194
392  n
mi
                                          Hp   =            181
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4456814
92                 X    =         1428185
25
 Y    =      -12957684
40  feet           Y    =        -3933920
74  meter
 Z    =      -17346718
80                 Z    =        -5280511
57
 XDOT =      24027
489054                 XDOT =        7296
392409
 YDOT =       7595
059719  feet/sec       YDOT =        2396
718711  meter/sec
 ZDOT =        510
245537                 ZDOT =         191
035553

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10814518
67                 X    =        -3296265
29
 Y    =       -8469026
79  feet           Y    =        -2581359
37  meter
 Z    =      -17320369
76                 Z    =        -5279248
70
 XDOT =      14274
819274                 XDOT =        4350
964915
 YDOT =     -19535
280731  feet/sec       YDOT =       -5954
353567  meter/sec
 ZDOT =        649
461728                 ZDOT =         197
955935


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   09154
51558135  
00010596  00000-0  82463-4 0  9091
2 25544  51
6423  17
0570 0009175  72
0184 288
1978 15
73342486  3804


Satellite: ISS
Catalog Number: 25544
Epoch time:      09154
51558135   =   yrday
fracday
Element set:     909
Inclination:       51
6423  deg
RA of node:        17
0570  deg
Eccentricity:     
0009175     
Arg of perigee:    72
0184  deg
Mean anomaly:     288
1978  deg
Mean motion:   15
73342486  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             380
Checksum:              315


Coasting Arc #11 (Orbit 395)
---------------------------------------

Vector Time (GMT): 2009/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6601020
22                 A    =         6734084
50  meter
 Y    =       -1309006
50  meter          E    =           
0018751
 Z    =          42710
29                 I    =           51
72909
 XDOT =        876
639664                 Wp   =          109
77989
 YDOT =      -4687
476793  meter/sec      RA   =           11
50333  deg
 ZDOT =      -6043
823138                 TA   =           69
75693
                                          MA   =           69
55543
                                          Ha   =            194
405  n
mi
                                          Hp   =            181
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21656890
48                 X    =        -6586099
56
 Y    =       -4294640
74  feet           Y    =        -1382739
54  meter
 Z    =         140125
62                 Z    =           10678
08
 XDOT =       2876
114382                 XDOT =         958
350924
 YDOT =     -15378
860871  feet/sec       YDOT =       -4677
215953  meter/sec
 ZDOT =     -19828
816068                 ZDOT =       -6039
366551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10676758
87                 X    =        -3254276
10
 Y    =       19325917
49  feet           Y    =         5890539
65  meter
 Z    =          14588
90                 Z    =            4446
70
 XDOT =     -12332
167477                 XDOT =       -3758
844647
 YDOT =      -6747
316746  feet/sec       YDOT =       -2056
582144  meter/sec
 ZDOT =     -19811
548271                 ZDOT =       -6038
559913


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   09155
53184086  
00010596  00000-0  82463-4 0  9106
2 25544  51
6423  11
8438 0009119  76
5228 283
6950 15
73329247  3962


Satellite: ISS
Catalog Number: 25544
Epoch time:      09155
53184086   =   yrday
fracday
Element set:     910
Inclination:       51
6423  deg
RA of node:        11
8438  deg
Eccentricity:     
0009119     
Arg of perigee:    76
5228  deg
Mean anomaly:     283
6950  deg
Mean motion:   15
73329247  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             396
Checksum:              318


Coasting Arc #12 (Orbit 411)
---------------------------------------

Vector Time (GMT): 2009/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672334
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -147037
40                 A    =         6721894
89  meter
 Y    =        4170001
96  meter          E    =           
0011401
 Z    =        5260282
31                 I    =           51
65841
 XDOT =      -7678
175912                 Wp   =           83
66434
 YDOT =       -630
669854  meter/sec      RA   =            6
37841  deg
 ZDOT =        286
039021                 TA   =            3
62838
                                          MA   =            3
62012
                                          Ha   =            194
371  n
mi
                                          Hp   =            181
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -482406
17                 X    =         -219210
02
 Y    =       13681108
80  feet           Y    =         4167953
29  meter
 Z    =       17258144
07                 Z    =         5259393
38
 XDOT =     -25190
865853                 XDOT =       -7671
942538
 YDOT =      -2069
126817  feet/sec       YDOT =        -716
496895  meter/sec
 ZDOT =        938
448232                 ZDOT =         248
752914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12935633
36                 X    =         3942781
05
 Y    =        4493255
65  feet           Y    =         1369544
32  meter
 Z    =       17254826
39                 Z    =         5259271
08
 XDOT =      -8901
466810                 XDOT =       -2713
167084
 YDOT =      22592
589300  feet/sec       YDOT =        6886
221219  meter/sec
 ZDOT =        792
357218                 ZDOT =         241
510480


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   09156
54807995  
00010596  00000-0  82463-4 0  9110
2 25544  51
6416   6
6292 0009087  79
6179 280
6007 15
73371468  4128


Satellite: ISS
Catalog Number: 25544
Epoch time:      09156
54807995   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:         6
6292  deg
Eccentricity:     
0009087     
Arg of perigee:    79
6179  deg
Mean anomaly:     280
6007  deg
Mean motion:   15
73371468  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             412
Checksum:              328

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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