[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 9th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25295 19 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
343/19:50:40
741 3
2 4
3 4
3
N/A 1
3 -0
4 223
3
000/00:01:21
482 2
5 -0
0 201
2
Coasting Arc #1 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2011/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5669799
46 A = 6773440
88 meter
Y = -2771093
65 meter E =
0033699
Z = -2440593
89 I = 51
70737
XDOT = 4079
748025 Wp = 135
55006
YDOT = -3685
008669 meter/sec RA = 8
26799 deg
ZDOT = -5361
819104 TA = 71
80971
MA = 71
44314
Ha = 223
706 n
mi
Hp = 198
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18601704
26 X = -5626535
01
Y = -9091514
60 feet Y = -2834254
72 meter
Z = -8007197
79 Z = -2468033
32
XDOT = 13385
000081 XDOT = 4146
698425
YDOT = -12089
923454 feet/sec YDOT = -3639
011630 meter/sec
ZDOT = -17591
270027 ZDOT = -5341
837087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13551861
79 X = 4130607
47
Y = -15595597
09 feet Y = -4753537
99 meter
Z = -8119030
06 Z = -2474680
36
XDOT = 7083
248622 XDOT = 2158
974180
YDOT = 15155
641125 feet/sec YDOT = 4619
439415 meter/sec
ZDOT = -17509
326401 ZDOT = -5336
842687
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 11341
52723492
00016717 00000-0 10270-3 0 9001
2 25544 51
6438 8
6327 0028341 136
9898 223
3479 15
58702872 27977
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
52723492 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 8
6327 deg
Eccentricity:
0028341
Arg of perigee: 136
9898 deg
Mean anomaly: 223
3479 deg
Mean motion: 15
58702872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 332
Coasting Arc #2 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2011/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984386
98 A = 6766538
72 meter
Y = 3869762
72 meter E =
0035796
Z = 4669856
49 I = 51
65302
XDOT = -6896
901705 Wp = 134
75240
YDOT = 1853
468774 meter/sec RA = 3
25169 deg
ZDOT = 2833
694772 TA = 287
00013
MA = 287
39208
Ha = 223
593 n
mi
Hp = 198
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9791295
87 X = 2918207
10
Y = 12696071
92 feet Y = 3902765
45 meter
Z = 15321051
48 Z = 4684194
48
XDOT = -22627
630267 XDOT = -6930
880721
YDOT = 6080
934298 feet/sec YDOT = 1776
153110 meter/sec
ZDOT = 9296
898858 ZDOT = 2800
106829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14654540
19 X = -4466703
85
Y = 6365286
91 feet Y = 1940139
45 meter
Z = 15379268
83 Z = 4687601
14
XDOT = 8
408363 XDOT = 2
562869
YDOT = -22411
467956 feet/sec YDOT = -6831
015433 meter/sec
ZDOT = 9159
542509 ZDOT = 2791
828557
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 11342
55302635
00016717 00000-0 10270-3 0 9018
2 25544 51
6423 3
4839 0028373 140
4887 219
8344 15
58749979 28134
Satellite: ISS
Catalog Number: 25544
Epoch time: 11342
55302635 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 3
4839 deg
Eccentricity:
0028373
Arg of perigee: 140
4887 deg
Mean anomaly: 219
8344 deg
Mean motion: 15
58749979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 326
Coasting Arc #3 (Orbit 2827)
---------------------------------------
Vector Time (GMT): 2011/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 774455
64 A = 6764118
68 meter
Y = -4203019
91 meter E =
0039475
Z = -5272589
18 I = 51
61554
XDOT = 7599
848455 Wp = 127
96765
YDOT = 386
533537 meter/sec RA = 358
20347 deg
ZDOT = 788
488487 TA = 149
70217
MA = 149
47337
Ha = 223
467 n
mi
Hp = 198
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2540864
95 X = 847010
64
Y = -13789435
39 feet Y = -4193953
16 meter
Z = -17298520
93 Z = -5268651
10
XDOT = 24933
886006 XDOT = 7591
130941
YDOT = 1268
154649 feet/sec YDOT = 471
470867 meter/sec
ZDOT = 2586
904485 ZDOT = 825
387822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12850727
93 X = 3916901
87
Y = 5659741
43 feet Y = 1725089
19 meter
Z = -17282056
24 Z = -5267570
74
XDOT = -6390
885609 XDOT = -1947
941934
YDOT = 23067
401484 feet/sec YDOT = 7030
943972 meter/sec
ZDOT = 2737
586070 ZDOT = 834
416234
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 11343
51467687
00016717 00000-0 10270-3 0 9025
2 25544 51
6433 358
6559 0028199 144
2696 216
0353 15
58773733 28285
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
51467687 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 358
6559 deg
Eccentricity:
0028199
Arg of perigee: 144
2696 deg
Mean anomaly: 216
0353 deg
Mean motion: 15
58773733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2828
Checksum: 344
Coasting Arc #4 (Orbit 2832)
---------------------------------------
Vector Time (GMT): 2011/343/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4660979
62 A = 6772204
33 meter
Y = -3239923
14 meter E =
0028914
Z = -3729102
69 I = 51
62691
XDOT = 5553
013621 Wp = 138
31373
YDOT = 3059
791516 meter/sec RA = 356
54094 deg
ZDOT = 4280
310274 TA = 177
23132
MA = 177
21528
Ha = 223
290 n
mi
Hp = 201
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15291927
90 X = 4714978
15
Y = -10629669
09 feet Y = -3187498
82 meter
Z = -12234588
86 Z = -3706328
66
XDOT = 18218
548624 XDOT = 5497
592538
YDOT = 10038
686076 feet/sec YDOT = 3121
578314 meter/sec
ZDOT = 14043
012709 ZDOT = 4307
152835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12028059
15 X = 3666152
43
Y = -14298018
84 feet Y = -4358036
14 meter
Z = -12141274
18 Z = -3700660
37
XDOT = 19092
969508 XDOT = 5819
537106
YDOT = 4038
682707 feet/sec YDOT = 1230
990489 meter/sec
ZDOT = 14152
375499 ZDOT = 4313
644052
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 11343
83522084
00016717 00000-0 10270-3 0 9034
2 25544 51
6447 357
0464 0024685 146
9159 213
3546 15
58031657 28339
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
83522084 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 357
0464 deg
Eccentricity:
0024685
Arg of perigee: 146
9159 deg
Mean anomaly: 213
3546 deg
Mean motion: 15
58031657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2833
Checksum: 317
Coasting Arc #5 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2011/344/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6422346
29 A = 6777591
12 meter
Y = 1805084
37 meter E =
0037487
Z = 1061054
60 I = 51
61467
XDOT = -2226
440161 Wp = 140
86351
YDOT = -4399
559205 meter/sec RA = 351
53952 deg
ZDOT = -5906
851605 TA = 27
57676
MA = 27
37839
Ha = 223
246 n
mi
Hp = 201
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21070689
94 X = -6447208
22
Y = 5922192
80 feet Y = 1733126
60 meter
Z = 3481150
25 Z = 1029794
51
XDOT = -7304
593703 XDOT = -2148
383366
YDOT = -14434
249359 feet/sec YDOT = -4424
019403 meter/sec
ZDOT = -19379
434399 ZDOT = -5917
478694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18594084
56 X = -5667476
97
Y = 11583615
23 feet Y = 3530685
92 meter
Z = 3353300
91 Z = 1022086
12
XDOT = -10092
209559 XDOT = -3076
105474
YDOT = -10493
995486 feet/sec YDOT = -3198
569824 meter/sec
ZDOT = -19422
442312 ZDOT = -5919
960417
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 11344
86146326
00016717 00000-0 10270-3 0 9040
2 25544 51
6447 351
8998 0024832 150
8571 209
3976 15
58028284 28490
Satellite: ISS
Catalog Number: 25544
Epoch time: 11344
86146326 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 351
8998 deg
Eccentricity:
0024832
Arg of perigee: 150
8571 deg
Mean anomaly: 209
3976 deg
Mean motion: 15
58028284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 344
Coasting Arc #6 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2011/345/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6513007
57 A = 6776208
87 meter
Y = -18942
16 meter E =
0028891
Z = 1887207
09 I = 51
58129
XDOT = -1632
698720 Wp = 124
95907
YDOT = 4963
277010 meter/sec RA = 346
54725 deg
ZDOT = 5607
281106 TA = 255
84778
MA = 256
16896
Ha = 222
929 n
mi
Hp = 201
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21368135
09 X = 6503567
60
Y = -62146
20 feet Y = 53837
25 meter
Z = 6191624
30 Z = 1918824
39
XDOT = -5356
623097 XDOT = -1715
316913
YDOT = 16283
717226 feet/sec YDOT = 4944
556488 meter/sec
ZDOT = 18396
591555 ZDOT = 5599
149419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20355553
69 X = 6204372
77
Y = -6374678
86 feet Y = -1943002
12 meter
Z = 6320773
22 Z = 1926571
68
XDOT = -865
745176 XDOT = -263
879130
YDOT = 15689
166655 feet/sec YDOT = 4782
057997 meter/sec
ZDOT = 18362
925481 ZDOT = 5597
019687
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 11345
88767363
00016717 00000-0 10270-3 0 9054
2 25544 51
6448 346
7532 0024554 154
5379 205
6991 15
58108019 28655
Satellite: ISS
Catalog Number: 25544
Epoch time: 11345
88767363 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 346
7532 deg
Eccentricity:
0024554
Arg of perigee: 154
5379 deg
Mean anomaly: 205
6991 deg
Mean motion: 15
58108019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 343
Coasting Arc #7 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2011/346/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4819320
61 A = 6769606
22 meter
Y = -2004211
49 meter E =
0026145
Z = -4313875
00 I = 51
53068
XDOT = 5027
605355 Wp = 138
40198
YDOT = -4614
503900 meter/sec RA = 341
53192 deg
ZDOT = -3504
109211 TA = 96
05589
MA = 95
75791
Ha = 222
647 n
mi
Hp = 201
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15811419
32 X = -4775594
97
Y = -6575497
03 feet Y = -2057859
08 meter
Z = -14153133
21 Z = -4337181
24
XDOT = 16494
768226 XDOT = 5095
854272
YDOT = -15139
448492 feet/sec YDOT = -4557
900102 meter/sec
ZDOT = -11496
421295 ZDOT = -3479
519954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16993001
54 X = -5179466
87
Y = -1333174
25 feet Y = -406351
51 meter
Z = -14248153
11 Z = -4342837
07
XDOT = 10906
467032 XDOT = 3324
291151
YDOT = -18318
664496 feet/sec YDOT = -5583
528938 meter/sec
ZDOT = -11395
562753 ZDOT = -3473
367527
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 11346
84971878
00016717 00000-0 10270-3 0 9060
2 25544 51
6450 341
9276 0024475 158
4457 201
7734 15
58154458 28809
Satellite: ISS
Catalog Number: 25544
Epoch time: 11346
84971878 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 341
9276 deg
Eccentricity:
0024475
Arg of perigee: 158
4457 deg
Mean anomaly: 201
7734 deg
Mean motion: 15
58154458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 343
Coasting Arc #8 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2011/347/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1996043
01 A = 6765498
78 meter
Y = 3715377
69 meter E =
0025888
Z = 5282126
41 I = 51
48916
XDOT = -6942
643451 Wp = 156
70357
YDOT = 3276
616245 meter/sec RA = 336
48679 deg
ZDOT = 294
959569 TA = 290
34515
MA = 290
62310
Ha = 222
489 n
mi
Hp = 201
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6548697
54 X = 1928689
10
Y = 12189559
34 feet Y = 3737321
50 meter
Z = 17329811
06 Z = 5291659
93
XDOT = -22777
701612 XDOT = -6980
200081
YDOT = 10750
053296 feet/sec YDOT = 3198
769324 meter/sec
ZDOT = 967
715122 ZDOT = 261
141516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10093399
54 X = 3076468
18
Y = 9394379
84 feet Y = 2863406
98 meter
Z = 17368421
37 Z = 5293894
83
XDOT = -17297
286045 XDOT = -5272
212787
YDOT = 16906
872272 feet/sec YDOT = 5153
214668 meter/sec
ZDOT = 829
280509 ZDOT = 252
764699
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 11347
87587219
00016717 00000-0 10270-3 0 9077
2 25544 51
6452 336
7813 0024537 162
0685 198
1340 15
58211730 28969
Satellite: ISS
Catalog Number: 25544
Epoch time: 11347
87587219 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 336
7813 deg
Eccentricity:
0024537
Arg of perigee: 162
0685 deg
Mean anomaly: 198
1340 deg
Mean motion: 15
58211730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 330
Coasting Arc #9 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2011/348/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1319131
98 A = 6768592
59 meter
Y = -4851478
34 meter E =
0031117
Z = -4559104
56 I = 51
47185
XDOT = 6942
225489 Wp = 150
22243
YDOT = -1004
922491 meter/sec RA = 331
43420 deg
ZDOT = 3060
586684 TA = 150
60878
MA = 150
43343
Ha = 222
331 n
mi
Hp = 201
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4327860
84 X = 1395431
29
Y = -15916923
68 feet Y = -4836299
98 meter
Z = -14957692
11 Z = -4552511
35
XDOT = 22776
330343 XDOT = 6938
079095
YDOT = -3296
989800 feet/sec YDOT = -927
313718 meter/sec
ZDOT = 10041
294896 ZDOT = 3094
301624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1344012
15 X = -409654
90
Y = -16464818
64 feet Y = -5018476
72 meter
Z = -14930330
56 Z = -4550764
75
XDOT = 18983
016750 XDOT = 5786
023506
YDOT = -10832
000554 feet/sec YDOT = -3301
593769 meter/sec
ZDOT = 10179
104419 ZDOT = 3102
591027
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 11348
83786356
00016717 00000-0 10270-3 0 9088
2 25544 51
6447 331
9548 0024438 165
8025 194
3822 15
58254665 29119
Satellite: ISS
Catalog Number: 25544
Epoch time: 11348
83786356 = yrday
fracday
Element set: 908
Inclination: 51
6447 deg
RA of node: 331
9548 deg
Eccentricity:
0024438
Arg of perigee: 165
8025 deg
Mean anomaly: 194
3822 deg
Mean motion: 15
58254665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 341
Coasting Arc #10 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2011/349/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4052480
90 A = 6775049
13 meter
Y = 4888236
89 meter E =
0033382
Z = 2297827
36 I = 51
46796
XDOT = -5178
766658 Wp = 147
43218
YDOT = -1741
539977 meter/sec RA = 326
40910 deg
ZDOT = -5419
630227 TA = 6
78210
MA = 6
73704
Ha = 222
150 n
mi
Hp = 202
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13295541
01 X = -4118003
30
Y = 16037522
61 feet Y = 4842553
05 meter
Z = 7538803
66 Z = 2277981
72
XDOT = -16990
704257 XDOT = -5132
580102
YDOT = -5713
713835 feet/sec YDOT = -1799
193507 meter/sec
ZDOT = -17780
939065 ZDOT = -5444
676446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6650313
75 X = -2027015
63
Y = 19772934
72 feet Y = 6026790
50 meter
Z = 7457310
67 Z = 2272988
29
XDOT = -16365
429213 XDOT = -4988
182824
YDOT = 1251
425138 feet/sec YDOT = 381
434382 meter/sec
ZDOT = -17883
096248 ZDOT = -5450
767736
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 11349
86395928
00016717 00000-0 10270-3 0 9094
2 25544 51
6450 326
8083 0024435 169
3390 190
8287 15
58293586 29279
Satellite: ISS
Catalog Number: 25544
Epoch time: 11349
86395928 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 326
8083 deg
Eccentricity:
0024435
Arg of perigee: 169
3390 deg
Mean anomaly: 190
8287 deg
Mean motion: 15
58293586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 357
Coasting Arc #11 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2011/350/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5609518
15 A = 6776800
83 meter
Y = -3752970
22 meter E =
0021168
Z = 710355
41 I = 51
44893
XDOT = 2139
514927 Wp = 140
12559
YDOT = 4342
771594 meter/sec RA = 321
40481 deg
ZDOT = 5934
115752 TA = 227
56614
MA = 227
74536
Ha = 221
921 n
mi
Hp = 202
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18403930
93 X = 5647616
93
Y = -12312894
41 feet Y = -3690028
16 meter
Z = 2330562
36 Z = 737698
67
XDOT = 7019
405929 XDOT = 2061
967442
YDOT = 14247
938301 feet/sec YDOT = 4366
263047 meter/sec
ZDOT = 19468
883702 ZDOT = 5944
321347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12389744
89 X = 3776394
24
Y = -18337709
90 feet Y = -5589333
98 meter
Z = 2442576
68 Z = 744497
37
XDOT = 10427
458079 XDOT = 3178
289223
YDOT = 9691
719797 feet/sec YDOT = 2954
036194 meter/sec
ZDOT = 19510
196156 ZDOT = 5946
707788
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 11350
89002248
00016717 00000-0 10270-3 0 9101
2 25544 51
6439 321
6602 0024512 173
5732 186
5742 15
58362396 29431
Satellite: ISS
Catalog Number: 25544
Epoch time: 11350
89002248 = yrday
fracday
Element set: 910
Inclination: 51
6439 deg
RA of node: 321
6602 deg
Eccentricity:
0024512
Arg of perigee: 173
5732 deg
Mean anomaly: 186
5742 deg
Mean motion: 15
58362396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 306
Coasting Arc #12 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2011/351/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5586357
61 A = 6771585
71 meter
Y = 1425814
51 meter E =
0024650
Z = -3534465
33 I = 51
40749
XDOT = 1248
757654 Wp = 164
40905
YDOT = -6119
868395 meter/sec RA = 316
39039 deg
ZDOT = -4473
021275 TA = 57
55692
MA = 57
31878
Ha = 221
621 n
mi
Hp = 202
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18327944
92 X = -5584716
38
Y = 4677869
13 feet Y = 1363353
78 meter
Z = -11596014
85 Z = -3561599
77
XDOT = 4096
973929 XDOT = 1338
827538
YDOT = -20078
308384 feet/sec YDOT = -6105
400194 meter/sec
ZDOT = -14675
266650 ZDOT = -4466
736334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14951233
22 X = -4557135
89
Y = 11474799
57 feet Y = 3497518
91 meter
Z = -11706971
63 Z = -3568284
95
XDOT = -3203
755201 XDOT = -976
504585
YDOT = -19018
594620 feet/sec YDOT = -5796
867640 meter/sec
ZDOT = -14649
071868 ZDOT = -4465
037105
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 11351
85193190
00016717 00000-0 10270-3 0 9116
2 25544 51
6428 316
8340 0024447 177
2241 182
9054 15
58367578 29586
Satellite: ISS
Catalog Number: 25544
Epoch time: 11351
85193190 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 316
8340 deg
Eccentricity:
0024447
Arg of perigee: 177
2241 deg
Mean anomaly: 182
9054 deg
Mean motion: 15
58367578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 326
Coasting Arc #13 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2011/352/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4196170
82 A = 6765707
37 meter
Y = 1421164
05 meter E =
0027347
Z = 5116242
86 I = 51
36651
XDOT = -4012
026805 Wp = 172
14742
YDOT = 6367
819899 meter/sec RA = 311
34243 deg
ZDOT = 1494
134548 TA = 263
26241
MA = 263
57369
Ha = 221
480 n
mi
Hp = 202
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13766964
65 X = 4155113
36
Y = 4662611
72 feet Y = 1467858
37 meter
Z = 16785573
70 Z = 5136528
27
XDOT = -13162
817602 XDOT = -4090
193105
YDOT = 20891
797570 feet/sec YDOT = 6322
517819 meter/sec
ZDOT = 4902
016233 ZDOT = 1474
454543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14377769
38 X = 4382344
11
Y = -1328382
77 feet Y = -404891
07 meter
Z = 16868310
37 Z = 5141461
00
XDOT = -3598
878438 XDOT = -1096
938148
YDOT = 23410
700624 feet/sec YDOT = 7135
581550 meter/sec
ZDOT = 4821
091387 ZDOT = 1469
468655
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 11352
87793936
00016717 00000-0 10270-3 0 9124
2 25544 51
6427 311
6859 0024427 180
6997 179
4128 15
58388833 29745
Satellite: ISS
Catalog Number: 25544
Epoch time: 11352
87793936 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 311
6859 deg
Eccentricity:
0024427
Arg of perigee: 180
6997 deg
Mean anomaly: 179
4128 deg
Mean motion: 15
58388833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 363
Coasting Arc #14 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2011/353/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1825215
34 A = 6766193
56 meter
Y = -4232623
54 meter E =
0029656
Z = -4971101
07 I = 51
34825
XDOT = 5578
164635 Wp = 159
36611
YDOT = -4835
598744 meter/sec RA = 306
27477 deg
ZDOT = 2045
629613 TA = 130
75758
MA = 130
49979
Ha = 221
281 n
mi
Hp = 202
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5988239
31 X = -1753600
80
Y = -13886560
16 feet Y = -4252633
44 meter
Z = -16309386
70 Z = -4979794
37
XDOT = 18301
065075 XDOT = 5621
885318
YDOT = -15864
825276 feet/sec YDOT = -4772
975974 meter/sec
ZDOT = 6711
383244 ZDOT = 2072
834349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11225713
73 X = -3421597
55
Y = -10076265
25 feet Y = -3071245
65 meter
Z = -16344536
94 Z = -4981814
86
XDOT = 9068
344316 XDOT = 2764
031348
YDOT = -21295
003615 feet/sec YDOT = -6490
717102 meter/sec
ZDOT = 6822
910871 ZDOT = 2079
623233
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 11353
83979114
00016717 00000-0 10270-3 0 9136
2 25544 51
6413 306
8574 0024515 184
3752 175
7193 15
58474002 29899
Satellite: ISS
Catalog Number: 25544
Epoch time: 11353
83979114 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 306
8574 deg
Eccentricity:
0024515
Arg of perigee: 184
3752 deg
Mean anomaly: 175
7193 deg
Mean motion: 15
58474002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 329
Coasting Arc #15 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2011/354/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -722733
76 A = 6772450
86 meter
Y = 5961610
95 meter E =
0027039
Z = 3092586
10 I = 51
35340
XDOT = -5664
985436 Wp = 159
52147
YDOT = 1833
024950 meter/sec RA = 301
22958 deg
ZDOT = -4869
481466 TA = 344
59017
MA = 344
67234
Ha = 220
934 n
mi
Hp = 202
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2371173
75 X = -804367
29
Y = 19559091
04 feet Y = 5953072
16 meter
Z = 10146279
84 Z = 3088877
32
XDOT = -18585
910224 XDOT = -5661
406427
YDOT = 6013
861384 feet/sec YDOT = 1769
696088 meter/sec
ZDOT = -15975
989063 ZDOT = -4896
993286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6418421
56 X = 1956334
89
Y = 18636033
59 feet Y = 5680263
04 meter
Z = 10130627
75 Z = 3087815
34
XDOT = -12600
808714 XDOT = -3840
726496
YDOT = 13064
116743 feet/sec YDOT = 3981
942783 meter/sec
ZDOT = -16088
518024 ZDOT = -4903
780294
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 11354
86573730
00016717 00000-0 10270-3 0 9145
2 25544 51
6420 301
7097 0024432 188
6274 171
4464 15
58541182 30053
Satellite: ISS
Catalog Number: 25544
Epoch time: 11354
86573730 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 301
7097 deg
Eccentricity:
0024432
Arg of perigee: 188
6274 deg
Mean anomaly: 171
4464 deg
Mean motion: 15
58541182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 302
Coasting Arc #16 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2011/355/19:51:21
482
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2909019
48 A = 6776463
08 meter
Y = -6130814
81 meter E =
0015950
Z = -122616
45 I = 51
35105
XDOT = 4366
764926 Wp = 167
61702
YDOT = 1955
012714 meter/sec RA = 296
21188 deg
ZDOT = 5978
860747 TA = 191
05747
MA = 191
09256
Ha = 220
849 n
mi
Hp = 203
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9544027
16 X = 2977954
91
Y = -20114221
82 feet Y = -6097898
91 meter
Z = -402284
95 Z = -108317
67
XDOT = 14326
656582 XDOT = 4315
534662
YDOT = 6414
083708 feet/sec YDOT = 2003
557382 meter/sec
ZDOT = 19615
684866 ZDOT = 5999
950405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -656544
34 X = -200114
71
Y = -22254960
33 feet Y = -6783311
91 meter
Z = -343361
63 Z = -104656
63
XDOT = 13947
694232 XDOT = 4251
257202
YDOT = -707
737857 feet/sec YDOT = -215
718499 meter/sec
ZDOT = 19701
665490 ZDOT = 6005
067641
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 11355
82753656
00016717 00000-0 10270-3 0 9150
2 25544 51
6407 296
8815 0024603 191
7579 168
3004 15
58556563 30204
Satellite: ISS
Catalog Number: 25544
Epoch time: 11355
82753656 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 296
8815 deg
Eccentricity:
0024603
Arg of perigee: 191
7579 deg
Mean anomaly: 168
3004 deg
Mean motion: 15
58556563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
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
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