Date: March 31st 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 3356)
---------------------------------------

Vector Time (GMT): 2009/089/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5910692
49                 A    =         6734607
00  meter
 Y    =       -1307154
07  meter          E    =           
0011895
 Z    =       -2941441
07                 I    =           51
59226
 XDOT =       3516
932625                 Wp   =          156
31946
 YDOT =      -4667
949203  meter/sec      RA   =          349
81214  deg
 ZDOT =      -5010
390068                 TA   =           57
57964
                                          MA   =           57
46464
                                          Ha   =            195
543  n
mi
                                          Hp   =            186
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19392035
73                 X    =        -5881347
24
 Y    =       -4288563
22  feet           Y    =        -1373086
86  meter
 Z    =       -9650397
21                 Z    =        -2970084
20
 XDOT =      11538
492865                 XDOT =        3593
208849
 YDOT =     -15314
793974  feet/sec       YDOT =       -4628
194438  meter/sec
 ZDOT =     -16438
287626                 ZDOT =       -4993
119256

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19315222
04                 X    =        -5887279
68
 Y    =       -4380919
16  feet           Y    =        -1335304
16  meter
 Z    =       -9762312
00                 Z    =        -2975552
70
 XDOT =      11386
860046                 XDOT =        3470
714942
 YDOT =     -13850
751388  feet/sec       YDOT =       -4221
709023  meter/sec
 ZDOT =     -16371
153603                 ZDOT =       -4989
927618


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   09089
50494112  
00010596  00000-0  82463-4 0  9002
2 25544  51
6437 350
1567 0009325 177
2902 182
8313 15
71796784 33571


Satellite: ISS
Catalog Number: 25544
Epoch time:      09089
50494112   =   yrday
fracday
Element set:     900
Inclination:       51
6437  deg
RA of node:       350
1567  deg
Eccentricity:     
0009325     
Arg of perigee:   177
2902  deg
Mean anomaly:     182
8313  deg
Mean motion:   15
71796784  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3357
Checksum:              323


Coasting Arc #2 (Orbit 3372)
---------------------------------------

Vector Time (GMT): 2009/090/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1853260
04                 A    =         6728629
53  meter
 Y    =        4404179
51  meter          E    =           
0008609
 Z    =        4729423
01                 I    =           51
54290
 XDOT =      -7229
904913                 Wp   =          129
94815
 YDOT =       -197
950036  meter/sec      RA   =          344
64400  deg
 ZDOT =      -2651
016668                 TA   =          346
11084
                                          MA   =          346
13451
                                          Ha   =            195
417  n
mi
                                          Hp   =            186
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6080249
46                 X    =        -1925345
40
 Y    =       14449407
85  feet           Y    =         4383052
23  meter
 Z    =       15516479
70                 Z    =         4720244
72
 XDOT =     -23720
160477                 XDOT =       -7214
275814
 YDOT =       -649
442374  feet/sec       YDOT =        -278
711658  meter/sec
 ZDOT =      -8697
561248                 ZDOT =       -2686
101812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5989811
61                 X    =        -1825694
58
 Y    =       14525122
98  feet           Y    =         4427257
48  meter
 Z    =       15480921
24                 Z    =         4718584
79
 XDOT =     -22616
530122                 XDOT =       -6893
518381
 YDOT =         81
463820  feet/sec       YDOT =          24
830172  meter/sec
 ZDOT =      -8834
559769                 ZDOT =       -2692
773818


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   09090
52218784  
00010596  00000-0  82463-4 0  9016
2 25544  51
6431 344
9500 0009210 181
3630 178
7509 15
71846129 33738


Satellite: ISS
Catalog Number: 25544
Epoch time:      09090
52218784   =   yrday
fracday
Element set:     901
Inclination:       51
6431  deg
RA of node:       344
9500  deg
Eccentricity:     
0009210     
Arg of perigee:   181
3630  deg
Mean anomaly:     178
7509  deg
Mean motion:   15
71846129  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3373
Checksum:              304


Coasting Arc #3 (Orbit 3388)
---------------------------------------

Vector Time (GMT): 2009/091/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6451367
03                 A    =         6737092
89  meter
 Y    =        -994232
25  meter          E    =           
0012298
 Z    =        1664656
35                 I    =           51
54368
 XDOT =       -697
745481                 Wp   =          103
99251
 YDOT =       5103
114425  meter/sec      RA   =          339
55369  deg
 ZDOT =       5713
825679                 TA   =          274
40230
                                          MA   =          274
54281
                                          Ha   =            195
281  n
mi
                                          Hp   =            186
439

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21165902
34                 X    =         6453918
61
 Y    =       -3261916
85  feet           Y    =         -922075
06  meter
 Z    =        5461470
95                 Z    =         1696003
31
 XDOT =      -2289
191209                 XDOT =        -782
514268
 YDOT =      16742
501394  feet/sec       YDOT =        5094
837806  meter/sec
 ZDOT =      18746
147242                 ZDOT =        5710
230174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21028055
32                 X    =         6409351
26
 Y    =       -3886543
27  feet           Y    =        -1184618
39  meter
 Z    =        5583803
31                 Z    =         1701943
25
 XDOT =      -2183
892285                 XDOT =        -665
650369
 YDOT =      15272
979804  feet/sec       YDOT =        4655
204244  meter/sec
 ZDOT =      18732
428865                 ZDOT =        5709
644318


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   09091
53942173  
00010596  00000-0  82463-4 0  9025
2 25544  51
6435 339
7423 0009181 185
2378 174
8689 15
71834034 33892


Satellite: ISS
Catalog Number: 25544
Epoch time:      09091
53942173   =   yrday
fracday
Element set:     902
Inclination:       51
6435  deg
RA of node:       339
7423  deg
Eccentricity:     
0009181     
Arg of perigee:   185
2378  deg
Mean anomaly:     174
8689  deg
Mean motion:   15
71834034  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3389
Checksum:              337


Coasting Arc #4 (Orbit 3403)
---------------------------------------

Vector Time (GMT): 2009/092/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -607870
89                 A    =         6726635
52  meter
 Y    =       -4273420
44  meter          E    =           
0016939
 Z    =       -5171850
88                 I    =           51
48183
 XDOT =       7200
124770                 Wp   =          131
65820
 YDOT =      -2431
249568  meter/sec      RA   =          334
39965  deg
 ZDOT =       1154
009040                 TA   =          149
45392
                                          MA   =          149
35516
                                          Ha   =            195
070  n
mi
                                          Hp   =            186
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1994327
08                 X    =         -534915
80
 Y    =      -14020408
27  feet           Y    =        -4279810
07  meter
 Z    =      -16968014
70                 Z    =        -5174626
72
 XDOT =      23622
456596                 XDOT =        7221
170336
 YDOT =      -7976
540577  feet/sec       YDOT =       -2350
615910  meter/sec
 ZDOT =       3786
118897                 ZDOT =        1189
038209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2550468
70                 X    =         -777382
86
 Y    =      -13916436
04  feet           Y    =        -4241729
70  meter
 Z    =      -16979123
32                 Z    =        -5175236
79
 XDOT =      22186
065330                 XDOT =        6762
312712
 YDOT =      -8886
622694  feet/sec       YDOT =       -2708
642597  meter/sec
 ZDOT =       3922
742082                 ZDOT =        1195
651787


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   09092
49306408  
00010596  00000-0  82463-4 0  9037
2 25544  51
6438 334
8604 0009187 189
5724 170
5264 15
71878411 34047


Satellite: ISS
Catalog Number: 25544
Epoch time:      09092
49306408   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:       334
8604  deg
Eccentricity:     
0009187     
Arg of perigee:   189
5724  deg
Mean anomaly:     170
5264  deg
Mean motion:   15
71878411  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3404
Checksum:              324


Coasting Arc #5 (Orbit 3419)
---------------------------------------

Vector Time (GMT): 2009/093/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5908392
65                 A    =         6738264
03  meter
 Y    =        3197679
95  meter          E    =           
0018433
 Z    =        -338005
52                 I    =           51
49470
 XDOT =      -2024
305909                 Wp   =          162
22717
 YDOT =      -4365
435532  meter/sec      RA   =          329
28330  deg
 ZDOT =      -6016
919770                 TA   =           21
45438
                                          MA   =           21
37722
                                          Ha   =            194
993  n
mi
                                          Hp   =            186
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19384490
31                 X    =        -5942068
56
 Y    =       10491075
95  feet           Y    =         3131420
56  meter
 Z    =       -1108941
98                 Z    =         -366790
10
 XDOT =      -6641
423587                 XDOT =       -1946
111556
 YDOT =     -14322
295051  feet/sec       YDOT =       -4387
635378  meter/sec
 ZDOT =     -19740
550427                 ZDOT =       -6026
563773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18666705
05                 X    =        -5689611
70
 Y    =       11709562
15  feet           Y    =         3569074
54  meter
 Z    =       -1221134
13                 Z    =         -372201
68
 XDOT =      -6576
403867                 XDOT =       -2004
487899
 YDOT =     -12514
261777  feet/sec       YDOT =       -3814
346990  meter/sec
 ZDOT =     -19778
487300                 ZDOT =       -6028
482929


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   09093
51027093  
00010596  00000-0  82463-4 0  9042
2 25544  51
6439 329
6534 0009362 193
5590 166
5322 15
71844488 34208


Satellite: ISS
Catalog Number: 25544
Epoch time:      09093
51027093   =   yrday
fracday
Element set:     904
Inclination:       51
6439  deg
RA of node:       329
6534  deg
Eccentricity:     
0009362     
Arg of perigee:   193
5590  deg
Mean anomaly:     166
5322  deg
Mean motion:   15
71844488  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3420
Checksum:              320


Coasting Arc #6 (Orbit 3435)
---------------------------------------

Vector Time (GMT): 2009/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2816161
67                 A    =         6726080
96  meter
 Y    =        3127701
54  meter          E    =           
0009460
 Z    =        5247377
87                 I    =           51
42961
 XDOT =      -6039
882597                 Wp   =          181
63519
 YDOT =       4755
305221  meter/sec      RA   =          324
15101  deg
 ZDOT =        397
788377                 TA   =          264
52099
                                          MA   =          264
62891
                                          Ha   =            194
632  n
mi
                                          Hp   =            187
044

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9239375
57                 X    =         2755487
32
 Y    =       10261487
99  feet           Y    =         3158854
46  meter
 Z    =       17215806
67                 Z    =         5260911
15
 XDOT =     -19815
887786                 XDOT =       -6094
540684
 YDOT =      15601
395081  feet/sec       YDOT =        4687
458138  meter/sec
 ZDOT =       1305
079976                 ZDOT =         368
313958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9942217
84                 X    =         3030388
00
 Y    =        9486155
11  feet           Y    =         2891380
08  meter
 Z    =       17268855
25                 Z    =         5263547
08
 XDOT =     -17799
973126                 XDOT =       -5425
431809
 YDOT =      16433
552581  feet/sec       YDOT =        5008
946827  meter/sec
 ZDOT =       1190
298059                 ZDOT =         362
802848


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   09094
52746147  
00010596  00000-0  82463-4 0  9053
2 25544  51
6439 324
4461 0009147 197
9535 162
1305 15
71917604 34369


Satellite: ISS
Catalog Number: 25544
Epoch time:      09094
52746147   =   yrday
fracday
Element set:     905
Inclination:       51
6439  deg
RA of node:       324
4461  deg
Eccentricity:     
0009147     
Arg of perigee:   197
9535  deg
Mean anomaly:     162
1305  deg
Mean motion:   15
71917604  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3436
Checksum:              322


Coasting Arc #7 (Orbit 3450)
---------------------------------------

Vector Time (GMT): 2009/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4464397
71                 A    =         6737615
56  meter
 Y    =       -4945474
50  meter          E    =           
0002757
 Z    =       -1008633
26                 I    =           51
44487
 XDOT =       4196
142606                 Wp   =          103
63550
 YDOT =       2586
604516  meter/sec      RA   =          319
00347  deg
 ZDOT =       5903
282803                 TA   =          245
32940
                                          MA   =          245
35811
                                          Ha   =            194
490  n
mi
                                          Hp   =            187
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14646974
13                 X    =         4524266
75
 Y    =      -16225310
05  feet           Y    =        -4895216
33  meter
 Z    =       -3309164
25                 Z    =         -986799
66
 XDOT =      13766
872066                 XDOT =        4138
230049
 YDOT =       8486
235288  feet/sec       YDOT =        2633
204810  meter/sec
 ZDOT =      19367
725733                 ZDOT =        5923
526656

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13000239
84                 X    =         3962473
10
 Y    =      -17588154
06  feet           Y    =        -5360869
36  meter
 Z    =       -3224237
32                 Z    =         -982747
53
 XDOT =      13140
015780                 XDOT =        4005
076810
 YDOT =       6155
367746  feet/sec       YDOT =        1876
156089  meter/sec
 ZDOT =      19446
945027                 ZDOT =        5927
428844


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   09095
48106598  
00010596  00000-0  82463-4 0  9060
2 25544  51
6434 319
5636 0009093 202
3661 157
7105 15
71940759 34516


Satellite: ISS
Catalog Number: 25544
Epoch time:      09095
48106598   =   yrday
fracday
Element set:     906
Inclination:       51
6434  deg
RA of node:       319
5636  deg
Eccentricity:     
0009093     
Arg of perigee:   202
3661  deg
Mean anomaly:     157
7105  deg
Mean motion:   15
71940759  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3451
Checksum:              326


Coasting Arc #8 (Orbit 3466)
---------------------------------------

Vector Time (GMT): 2009/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4326386
92                 A    =         6727034
51  meter
 Y    =       -1263055
63  meter          E    =           
0010047
 Z    =       -5000205
70                 I    =           51
38695
 XDOT =       3992
431566                 Wp   =          118
91170
 YDOT =      -6303
741012  meter/sec      RA   =          313
89206  deg
 ZDOT =      -1869
703074                 TA   =          133
00698
                                          MA   =          132
92275
                                          Ha   =            194
190  n
mi
                                          Hp   =            187
400

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14194182
80                 X    =        -4287651
68
 Y    =       -4143883
28  feet           Y    =        -1311219
64  meter
 Z    =      -16404874
33                 Z    =        -5021129
00
 XDOT =      13098
528760                 XDOT =        4071
706968
 YDOT =     -20681
565000  feet/sec       YDOT =       -6258
652216  meter/sec
 ZDOT =      -6134
196437                 ZDOT =       -1850
114847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14483047
88                 X    =        -4414432
99
 Y    =       -2489561
53  feet           Y    =         -758818
35  meter
 Z    =      -16486658
35                 Z    =        -5025133
46
 XDOT =      10478
206463                 XDOT =        3193
757330
 YDOT =     -21002
793974  feet/sec       YDOT =       -6401
651603  meter/sec
 ZDOT =      -6058
136075                 ZDOT =       -1846
519876


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   09096
49823014  
00010596  00000-0  82463-4 0  9072
2 25544  51
6423 314
3556 0009057 207
0747 152
9944 15
71962092 34674


Satellite: ISS
Catalog Number: 25544
Epoch time:      09096
49823014   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:       314
3556  deg
Eccentricity:     
0009057     
Arg of perigee:   207
0747  deg
Mean anomaly:     152
9944  deg
Mean motion:   15
71962092  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3467
Checksum:              326


Coasting Arc #9 (Orbit 3482)
---------------------------------------

Vector Time (GMT): 2009/097/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2407092
83                 A    =         6735750
45  meter
 Y    =        5865979
92  meter          E    =           
0014925
 Z    =        2243547
91                 I    =           51
39699
 XDOT =      -5449
084006                 Wp   =          144
09075
 YDOT =       -151
500603  meter/sec      RA   =          308
71979  deg
 ZDOT =      -5443
828794                 TA   =           10
64209
                                          MA   =           10
61054
                                          Ha   =            194
044  n
mi
                                          Hp   =            187
700

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7897286
19                 X    =        -2483407
06
 Y    =       19245340
93  feet           Y    =         5838635
91  meter
 Z    =        7360721
49                 Z    =         2231668
35
 XDOT =     -17877
572197                 XDOT =       -5420
539745
 YDOT =       -497
049224  feet/sec       YDOT =        -212
276329  meter/sec
 ZDOT =     -17860
330688                 ZDOT =       -5470
231119

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5320661
10                 X    =        -1621737
50
 Y    =       20127485
57  feet           Y    =         6134857
60  meter
 Z    =        7314737
71                 Z    =         2229532
06
 XDOT =     -16215
507503                 XDOT =       -4942
486687
 YDOT =       2249
365025  feet/sec       YDOT =         685
606460  meter/sec
 ZDOT =     -17963
430119                 ZDOT =       -5475
253500


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   09097
51538089  
00010596  00000-0  82463-4 0  9082
2 25544  51
6424 309
1484 0008980 210
9197 149
1437 15
71988817 34839


Satellite: ISS
Catalog Number: 25544
Epoch time:      09097
51538089   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:       309
1484  deg
Eccentricity:     
0008980     
Arg of perigee:   210
9197  deg
Mean anomaly:     149
1437  deg
Mean motion:   15
71988817  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3483
Checksum:              351


Coasting Arc #10 (Orbit 3498)
---------------------------------------

Vector Time (GMT): 2009/098/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4952687
84                 A    =         6729336
71  meter
 Y    =       -1038639
10  meter          E    =           
0011198
 Z    =        4438797
37                 I    =           51
35643
 XDOT =      -1459
018076                 Wp   =          162
99977
 YDOT =       6836
197631  meter/sec      RA   =          303
62303  deg
 ZDOT =       3214
942061                 TA   =          254
59540
                                          MA   =          254
71913
                                          Ha   =            193
868  n
mi
                                          Hp   =            187
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16248975
85                 X    =         4942370
96
 Y    =       -3407608
60  feet           Y    =         -983312
56  meter
 Z    =       14562983
49                 Z    =         4462832
71
 XDOT =      -4786
804711                 XDOT =       -1550
970858
 YDOT =      22428
469919  feet/sec       YDOT =        6819
368179  meter/sec
 ZDOT =      10547
710173                 ZDOT =        3207
630167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15473493
58                 X    =         4716320
84
 Y    =       -5785498
86  feet           Y    =        -1763420
05  meter
 Z    =       14656756
12                 Z    =         4467379
26
 XDOT =      -1862
455529                 XDOT =        -567
676445
 YDOT =      21772
879193  feet/sec       YDOT =        6636
373578  meter/sec
 ZDOT =      10519
631231                 ZDOT =        3206
383599


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   09098
53251839  
00010596  00000-0  82463-4 0  9091
2 25544  51
6411 303
9393 0008947 215
2420 144
8152 15
71960706 34996


Satellite: ISS
Catalog Number: 25544
Epoch time:      09098
53251839   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       303
9393  deg
Eccentricity:     
0008947     
Arg of perigee:   215
2420  deg
Mean anomaly:     144
8152  deg
Mean motion:   15
71960706  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3499
Checksum:              327


Coasting Arc #11 (Orbit 3513)
---------------------------------------

Vector Time (GMT): 2009/099/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         146817
50                 A    =         6733023
52  meter
 Y    =       -5856249
08  meter          E    =           
0006901
 Z    =       -3325465
50                 I    =           51
35290
 XDOT =       5587
447729                 Wp   =          188
21529
 YDOT =      -2506
269093  meter/sec      RA   =          298
43223  deg
 ZDOT =       4652
381141                 TA   =          132
57962
                                          MA   =          132
52137
                                          Ha   =            193
693  n
mi
                                          Hp   =            188
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         481684
71                 X    =          228446
84
 Y    =      -19213415
62  feet           Y    =        -5854151
11  meter
 Z    =      -10910319
88                 Z    =        -3324553
55
 XDOT =      18331
521420                 XDOT =        5592
457290
 YDOT =      -8222
667628  feet/sec       YDOT =       -2443
758649  meter/sec
 ZDOT =      15263
717653                 ZDOT =        4679
537615

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2661277
86                 X    =         -811157
49
 Y    =      -19036119
55  feet           Y    =        -5802209
24  meter
 Z    =      -10907162
44                 Z    =        -3324503
11
 XDOT =      15231
448911                 XDOT =        4642
545628
 YDOT =     -10950
606043  feet/sec       YDOT =       -3337
744722  meter/sec
 ZDOT =      15369
572686                 ZDOT =        4684
645755


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   09099
48606922  
00010596  00000-0  82463-4 0  9105
2 25544  51
6400 299
0556 0009121 219
1631 140
8872 15
72021306 35140


Satellite: ISS
Catalog Number: 25544
Epoch time:      09099
48606922   =   yrday
fracday
Element set:     910
Inclination:       51
6400  deg
RA of node:       299
0556  deg
Eccentricity:     
0009121     
Arg of perigee:   219
1631  deg
Mean anomaly:     140
8872  deg
Mean motion:   15
72021306  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3514
Checksum:              295


Coasting Arc #12 (Orbit 3529)
---------------------------------------

Vector Time (GMT): 2009/100/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 685930
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4598525
12                 A    =         6731904
70  meter
 Y    =        3291104
51  meter          E    =           
0005519
 Z    =       -3647104
19                 I    =           51
33560
 XDOT =      -1063
246949                 Wp   =          185
86753
 YDOT =      -6276
751287  meter/sec      RA   =          293
34205  deg
 ZDOT =      -4328
284751                 TA   =           38
09141
                                          MA   =           38
05241
                                          Ha   =            193
355  n
mi
                                          Hp   =            188
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15087024
68                 X    =        -4617267
80
 Y    =       10797586
97  feet           Y    =         3239576
13  meter
 Z    =      -11965564
92                 Z    =        -3669489
84
 XDOT =      -3488
343007                 XDOT =        -971
953911
 YDOT =     -20593
016032  feet/sec       YDOT =       -6288
130911  meter/sec
 ZDOT =     -14200
409289                 ZDOT =       -4333
228002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12782505
87                 X    =        -3896107
79
 Y    =       13368618
98  feet           Y    =         4074755
06  meter
 Z    =      -12052738
78                 Z    =        -3673674
78
 XDOT =      -6150
420556                 XDOT =       -1874
648186
 YDOT =     -18687
021560  feet/sec       YDOT =       -5695
804171  meter/sec
 ZDOT =     -14220
140506                 ZDOT =       -4334
298826


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   09100
50317794  
00010596  00000-0  82463-4 0  9118
2 25544  51
6391 293
8475 0009049 223
3383 136
7068 15
72037926 35305


Satellite: ISS
Catalog Number: 25544
Epoch time:      09100
50317794   =   yrday
fracday
Element set:     911
Inclination:       51
6391  deg
RA of node:       293
8475  deg
Eccentricity:     
0009049     
Arg of perigee:   223
3383  deg
Mean anomaly:     136
7068  deg
Mean motion:   15
72037926  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            3530
Checksum:              313

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