[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 29th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25305 95 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
334/23:22:31
341 2
1 3
3 3
3
N/A 2
3 -0
3 224
4
000/00:01:02
681 0
9 -0
0 198
2
341/20:07:18
799 1
5 2
0 2
0
N/A 0
8 -0
2 223
6
000/00:00:37
598 1
0 -0
0 199
7
Coasting Arc #1 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2011/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4144179
60 A = 6773036
35 meter
Y = -4564557
10 meter E =
0043895
Z = 2762754
81 I = 51
97529
XDOT = 2266
970375 Wp = 93
71180
YDOT = -5226
312215 meter/sec RA = 68
27676 deg
ZDOT = -5166
828049 TA = 55
01452
MA = 54
60319
Ha = 225
131 n
mi
Hp = 196
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13596389
76 X = -4106251
03
Y = -14975581
03 feet Y = -4610688
08 meter
Z = 9064156
21 Z = 2742713
64
XDOT = 7437
566846 XDOT = 2350
343542
YDOT = -17146
693619 feet/sec YDOT = -5200
494850 meter/sec
ZDOT = -16951
535593 ZDOT = -5155
612930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19512796
89 X = 5947500
49
Y = -5463659
27 feet Y = -1665323
35 meter
Z = 8982647
40 Z = 2737910
93
XDOT = 11530
683632 XDOT = 3514
552371
YDOT = 13019
661454 feet/sec YDOT = 3968
392811 meter/sec
ZDOT = -16905
329960 ZDOT = -5152
744572
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 11329
53775178
00016717 00000-0 10270-3 0 9006
2 25544 51
6430 68
8042 0030534 90
9002 269
5652 15
58646930 26105
Satellite: ISS
Catalog Number: 25544
Epoch time: 11329
53775178 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 68
8042 deg
Eccentricity:
0030534
Arg of perigee: 90
9002 deg
Mean anomaly: 269
5652 deg
Mean motion: 15
58646930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 305
Coasting Arc #2 (Orbit 2625)
---------------------------------------
Vector Time (GMT): 2011/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2850665
91 A = 6776024
70 meter
Y = 6134951
50 meter E =
0040351
Z = 267537
40 I = 51
97456
XDOT = -4405
089189 Wp = 80
78464
YDOT = 1750
159027 meter/sec RA = 63
30536 deg
ZDOT = 6038
098522 TA = 282
09082
MA = 282
54267
Ha = 224
973 n
mi
Hp = 196
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9352578
44 X = 2780552
13
Y = 20127793
64 feet Y = 6166437
34 meter
Z = 877747
38 Z = 281216
53
XDOT = -14452
392353 XDOT = -4453
664795
YDOT = 5741
991560 feet/sec YDOT = 1700
626310 meter/sec
ZDOT = 19810
034520 ZDOT = 6016
580523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22190067
60 X = -6763532
60
Y = -315253
20 feet Y = -96089
17 meter
Z = 933143
19 Z = 284422
05
XDOT = 1127
668200 XDOT = 343
713267
YDOT = -14002
315218 feet/sec YDOT = -4267
905678 meter/sec
ZDOT = 19722
003118 ZDOT = 6011
266550
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 11330
56356888
00016717 00000-0 10270-3 0 9015
2 25544 51
6438 63
6561 0030476 94
2124 266
2515 15
58706143 26261
Satellite: ISS
Catalog Number: 25544
Epoch time: 11330
56356888 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 63
6561 deg
Eccentricity:
0030476
Arg of perigee: 94
2124 deg
Mean anomaly: 266
2515 deg
Mean motion: 15
58706143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2626
Checksum: 310
Coasting Arc #3 (Orbit 2640)
---------------------------------------
Vector Time (GMT): 2011/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -539853
94 A = 6771102
78 meter
Y = -5872922
52 meter E =
0035159
Z = -3351925
90 I = 51
94363
XDOT = 5649
680194 Wp = 96
85656
YDOT = 2140
368040 meter/sec RA = 58
32836 deg
ZDOT = -4706
364959 TA = 122
01133
MA = 121
66922
Ha = 224
842 n
mi
Hp = 196
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1771174
34 X = -457858
46
Y = -19268118
49 feet Y = -5878500
64 meter
Z = -10997132
23 Z = -3354350
04
XDOT = 18535
696176 XDOT = 5648
189117
YDOT = 7022
204857 feet/sec YDOT = 2203
538435 meter/sec
ZDOT = -15440
829917 ZDOT = -4678
921974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18213822
69 X = 5551573
16
Y = 6515098
12 feet Y = 1985801
91 meter
Z = -11006567
37 Z = -3354801
73
XDOT = -13697
426166 XDOT = -4174
975495
YDOT = 12652
791853 feet/sec YDOT = 3856
570957 meter/sec
ZDOT = -15328
896747 ZDOT = -4672
247729
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 11331
52523981
00016717 00000-0 10270-3 0 9023
2 25544 51
6432 58
8283 0030411 97
8874 262
5735 15
58760067 26417
Satellite: ISS
Catalog Number: 25544
Epoch time: 11331
52523981 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 58
8283 deg
Eccentricity:
0030411
Arg of perigee: 97
8874 deg
Mean anomaly: 262
5735 deg
Mean motion: 15
58760067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 314
Coasting Arc #4 (Orbit 2656)
---------------------------------------
Vector Time (GMT): 2011/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2070244
43 A = 6764523
80 meter
Y = 3905250
71 meter E =
0035034
Z = 5093763
44 I = 51
90582
XDOT = -5480
448189 Wp = 104
41687
YDOT = -5136
366389 meter/sec RA = 53
31702 deg
ZDOT = 1692
311221 TA = 329
26332
MA = 329
46804
Ha = 224
748 n
mi
Hp = 196
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6792140
53 X = -2138504
51
Y = 12812502
32 feet Y = 3881717
78 meter
Z = 16711822
32 Z = 5083540
76
XDOT = -17980
473060 XDOT = -5430
825969
YDOT = -16851
595765 feet/sec YDOT = -5197
374842 meter/sec
ZDOT = 5552
202167 ZDOT = 1665
807115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8951678
92 X = -2728471
73
Y = -11470196
07 feet Y = -3496115
76 meter
Z = 16669746
26 Z = 5080938
66
XDOT = 21843
103816 XDOT = 6657
778043
YDOT = -9047
695967 feet/sec YDOT = -2757
737731 meter/sec
ZDOT = 5444
342694 ZDOT = 1659
435653
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 11332
55098690
00016717 00000-0 10270-3 0 9032
2 25544 51
6434 53
6790 0030330 101
5120 258
9444 15
58853294 26570
Satellite: ISS
Catalog Number: 25544
Epoch time: 11332
55098690 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 53
6790 deg
Eccentricity:
0030330
Arg of perigee: 101
5120 deg
Mean anomaly: 258
9444 deg
Mean motion: 15
58853294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2657
Checksum: 306
Coasting Arc #5 (Orbit 2671)
---------------------------------------
Vector Time (GMT): 2011/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4452588
60 A = 6764935
73 meter
Y = -950023
51 meter E =
0043159
Z = -5042879
84 I = 51
88752
XDOT = 3627
916707 Wp = 104
39747
YDOT = 6423
988509 meter/sec RA = 48
28575 deg
ZDOT = 1996
914632 TA = 184
97524
MA = 185
01827
Ha = 224
621 n
mi
Hp = 196
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14608230
30 X = 4487378
44
Y = -3116875
05 feet Y = -900036
99 meter
Z = -16544881
37 Z = -5021164
72
XDOT = 11902
613867 XDOT = 3546
112099
YDOT = 21076
077785 feet/sec YDOT = 6464
100534 meter/sec
ZDOT = 6551
557193 ZDOT = 2014
340911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2816799
57 X = -858560
51
Y = 14768584
40 feet Y = 4501464
52 meter
Z = -16456091
80 Z = -5015816
78
XDOT = -22948
055202 XDOT = -6994
567226
YDOT = 2987
813175 feet/sec YDOT = 910
685456 meter/sec
ZDOT = 6622
225818 ZDOT = 2018
454429
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 11333
51259538
00016717 00000-0 10270-3 0 9040
2 25544 51
6427 48
8516 0030381 104
6013 255
8515 15
58877067 26721
Satellite: ISS
Catalog Number: 25544
Epoch time: 11333
51259538 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 48
8516 deg
Eccentricity:
0030381
Arg of perigee: 104
6013 deg
Mean anomaly: 255
8515 deg
Mean motion: 15
58877067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 315
Coasting Arc #6 (Orbit 2687)
---------------------------------------
Vector Time (GMT): 2011/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5667050
13 A = 6771595
97 meter
Y = -2092863
56 meter E =
0043385
Z = 3009777
96 I = 51
88953
XDOT = -511
684356 Wp = 104
40554
YDOT = -5846
994124 meter/sec RA = 43
27339 deg
ZDOT = -4980
135047 TA = 41
07041
MA = 40
74458
Ha = 224
574 n
mi
Hp = 196
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18592684
17 X = -5657847
09
Y = -6866350
28 feet Y = -2156184
73 meter
Z = 9874599
60 Z = 2982269
63
XDOT = -1678
754450 XDOT = -422
071471
YDOT = -19183
051587 feet/sec YDOT = -5852
214716 meter/sec
ZDOT = -16339
025746 ZDOT = -4982
403521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13296683
31 X = 4052829
07
Y = -14772823
78 feet Y = -4502756
69 meter
Z = 9762391
03 Z = 2975576
79
XDOT = 17323
393218 XDOT = 5280
170253
YDOT = 4681
647626 feet/sec YDOT = 1426
966197 meter/sec
ZDOT = -16347
813952 ZDOT = -4982
813692
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 11334
53827631
00016717 00000-0 10270-3 0 9059
2 25544 51
6428 43
7007 0030355 108
1665 252
2799 15
58940753 26889
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
53827631 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 43
7007 deg
Eccentricity:
0030355
Arg of perigee: 108
1665 deg
Mean anomaly: 252
2799 deg
Mean motion: 15
58940753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2688
Checksum: 322
Coasting Arc #7 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2011/334/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266871
45 A = 6766428
91 meter
Y = -1553801
80 meter E =
0040528
Z = -5053297
80 I = 51
85685
XDOT = 4458
843289 Wp = 107
54336
YDOT = 5893
607443 meter/sec RA = 40
90777 deg
ZDOT = 1953
780355 TA = 181
41557
MA = 181
42708
Ha = 224
448 n
mi
Hp = 198
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13998922
08 X = 4308477
27
Y = -5097774
94 feet Y = -1505854
11 meter
Z = -16579061
04 Z = -5032468
35
XDOT = 14628
750949 XDOT = 4383
117289
YDOT = 19335
982426 feet/sec YDOT = 5943
045447 meter/sec
ZDOT = 6410
040536 ZDOT = 1975
257832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2776015
02 X = 846129
38
Y = -14733275
89 feet Y = -4490702
49 meter
Z = -16493838
73 Z = -5027322
04
XDOT = 22993
744209 XDOT = 7008
493235
YDOT = -2937
446352 feet/sec YDOT = -895
333648 meter/sec
ZDOT = 6497
297794 ZDOT = 1980
376368
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 11334
98700179
00016717 00000-0 10270-3 0 9066
2 25544 51
6438 41
4481 0027703 109
3670 251
0483 15
58344461 26952
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
98700179 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 41
4481 deg
Eccentricity:
0027703
Arg of perigee: 109
3670 deg
Mean anomaly: 251
0483 deg
Mean motion: 15
58344461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 312
Coasting Arc #8 (Orbit 2710)
---------------------------------------
Vector Time (GMT): 2011/335/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5840552
62 A = 6772743
04 meter
Y = -1135131
46 meter E =
0040248
Z = 3189419
54 I = 51
85448
XDOT = -1533
091317 Wp = 106
63419
YDOT = -5792
661365 meter/sec RA = 35
89665 deg
ZDOT = -4830
256259 TA = 36
44256
MA = 36
16926
Ha = 224
494 n
mi
Hp = 198
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19161918
05 X = -5842918
94
Y = -3724184
57 feet Y = -1200457
47 meter
Z = 10463974
86 Z = 3161040
26
XDOT = -5029
827155 XDOT = -1444
738110
YDOT = -19004
794503 feet/sec YDOT = -5809
311116 meter/sec
ZDOT = -15847
297437 ZDOT = -4837
489674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12724970
71 X = -3878571
07
Y = 14884041
26 feet Y = 4536655
78 meter
Z = 10348133
17 Z = 3154110
99
XDOT = -17880
001647 XDOT = -5449
824502
YDOT = -4158
746640 feet/sec YDOT = -1267
585976 meter/sec
ZDOT = -15876
367413 ZDOT = -4839
116787
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 11336
01303138
00016717 00000-0 10270-3 0 9077
2 25544 51
6435 36
3000 0027809 113
0419 247
3672 15
58381751 27119
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
01303138 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 36
3000 deg
Eccentricity:
0027809
Arg of perigee: 113
0419 deg
Mean anomaly: 247
3672 deg
Mean motion: 15
58381751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2711
Checksum: 280
Coasting Arc #9 (Orbit 2725)
---------------------------------------
Vector Time (GMT): 2011/336/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5938721
05 A = 6776723
45 meter
Y = 3255688
10 meter E =
0032822
Z = -328212
10 I = 51
84419
XDOT = -2045
147588 Wp = 96
51927
YDOT = 4285
531515 meter/sec RA = 30
91423 deg
ZDOT = 6017
023135 TA = 259
95149
MA = 260
32199
Ha = 224
197 n
mi
Hp = 198
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19483992
93 X = 5903468
32
Y = 10681391
40 feet Y = 3321901
42 meter
Z = -1076811
35 Z = -299447
15
XDOT = -6709
801798 XDOT = -2122
147021
YDOT = 14060
142767 feet/sec YDOT = 4262
230674 meter/sec
ZDOT = 19740
889551 ZDOT = 6006
900876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18703851
72 X = 5700934
00
Y = -12005114
35 feet Y = -3659158
85 meter
Z = -959575
85 Z = -292478
72
XDOT = 8205
285880 XDOT = 2500
971136
YDOT = 11359
879239 feet/sec YDOT = 3462
491192 meter/sec
ZDOT = 19699
180487 ZDOT = 6004
310213
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 11336
97490269
00016717 00000-0 10270-3 0 9085
2 25544 51
6441 31
4740 0027624 116
6093 243
7897 15
58457927 27269
Satellite: ISS
Catalog Number: 25544
Epoch time: 11336
97490269 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 31
4740 deg
Eccentricity:
0027624
Arg of perigee: 116
6093 deg
Mean anomaly: 243
7897 deg
Mean motion: 15
58457927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2726
Checksum: 338
Coasting Arc #10 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2011/337/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4243230
64 A = 6773408
59 meter
Y = -4491724
36 meter E =
0032213
Z = -2775773
07 I = 51
80687
XDOT = 5351
123089 Wp = 119
99136
YDOT = -1907
020017 meter/sec RA = 25
93307 deg
ZDOT = -5154
449993 TA = 91
43410
MA = 91
06506
Ha = 224
048 n
mi
Hp = 198
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13921360
37 X = -4179203
60
Y = -14736628
46 feet Y = -4538816
67 meter
Z = -9106867
01 Z = -2796231
50
XDOT = 17556
178112 XDOT = 5397
089654
YDOT = -6256
627354 feet/sec YDOT = -1846
923269 meter/sec
ZDOT = -16910
925174 ZDOT = -5128
342431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19483757
50 X = -5938649
29
Y = 5462007
77 feet Y = 1664819
97 meter
Z = -9190059
00 Z = -2801129
98
XDOT = 3032
299983 XDOT = 924
245035
YDOT = -17127
210792 feet/sec YDOT = -5220
373849 meter/sec
ZDOT = -16804
115539 ZDOT = -5121
894416
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 11338
00086847
00016717 00000-0 10270-3 0 9095
2 25544 51
6443 26
3250 0027494 120
6026 239
7846 15
58460775 27428
Satellite: ISS
Catalog Number: 25544
Epoch time: 11338
00086847 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 26
3250 deg
Eccentricity:
0027494
Arg of perigee: 120
6026 deg
Mean anomaly: 239
7846 deg
Mean motion: 15
58460775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 317
Coasting Arc #11 (Orbit 2757)
---------------------------------------
Vector Time (GMT): 2011/338/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1304004
30 A = 6766625
06 meter
Y = 4557651
42 meter E =
0034690
Z = 4810716
14 I = 51
75705
XDOT = -7234
323995 Wp = 122
51630
YDOT = -632
260719 meter/sec RA = 20
92190 deg
ZDOT = 2528
452068 TA = 302
56597
MA = 302
90051
Ha = 223
947 n
mi
Hp = 198
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4278229
33 X = 1229572
96
Y = 14952924
62 feet Y = 4571817
21 meter
Z = 15783189
44 Z = 4816870
48
XDOT = -23734
658776 XDOT = -7238
999156
YDOT = -2074
346190 feet/sec YDOT = -713
185624 meter/sec
ZDOT = 8295
446418 ZDOT = 2493
295936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15243345
36 X = 4646171
66
Y = 2958339
53 feet Y = 901701
89 meter
Z = 15807938
49 Z = 4818259
65
XDOT = -12291
838839 XDOT = -3746
552478
YDOT = 19224
583379 feet/sec YDOT = 5859
653014 meter/sec
ZDOT = 8151
894466 ZDOT = 2484
697433
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 11339
02680251
00016717 00000-0 10270-3 0 9109
2 25544 51
6443 21
1773 0027558 123
9026 236
4756 15
58528783 27583
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
02680251 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 21
1773 deg
Eccentricity:
0027558
Arg of perigee: 123
9026 deg
Mean anomaly: 236
4756 deg
Mean motion: 15
58528783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2758
Checksum: 316
Coasting Arc #12 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2011/339/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2275040
25 A = 6764804
10 meter
Y = -3659191
84 meter E =
0040451
Z = -5248950
91 I = 51
72211
XDOT = 7017
947153 Wp = 117
17257
YDOT = 2851
602465 meter/sec RA = 15
88163 deg
ZDOT = 1042
022109 TA = 162
89274
MA = 162
75599
Ha = 223
749 n
mi
Hp = 198
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7464042
83 X = 2341287
77
Y = -12005222
58 feet Y = -3633380
23 meter
Z = -17220967
57 Z = -5237737
92
XDOT = 23024
761002 XDOT = 6980
476351
YDOT = 9355
651133 feet/sec YDOT = 2929
871885 meter/sec
ZDOT = 3418
707706 ZDOT = 1076
024906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7552432
33 X = -2301981
37
Y = -12016004
70 feet Y = -3662478
23 meter
Z = -17174848
63 Z = -5234893
86
XDOT = 17507
820876 XDOT = 5336
383803
YDOT = -16144
406569 feet/sec YDOT = -4920
815122 meter/sec
ZDOT = 3557
350674 ZDOT = 1084
280486
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 11339
98858571
00016717 00000-0 10270-3 0 9117
2 25544 51
6438 16
3494 0027368 127
5361 232
8287 15
58592626 27737
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
98858571 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 16
3494 deg
Eccentricity:
0027368
Arg of perigee: 127
5361 deg
Mean anomaly: 232
8287 deg
Mean motion: 15
58592626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 348
Coasting Arc #13 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2011/340/23:23:02
681
Vector Time (MET): N/A
Weight (LBS) : 871714
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5223588
14 A = 6770191
31 meter
Y = 2021828
05 meter E =
0036187
Z = 3761181
23 I = 51
71164
XDOT = -4745
006645 Wp = 116
90288
YDOT = -4325
426362 meter/sec RA = 10
85237 deg
ZDOT = -4249
540314 TA = 17
84245
MA = 17
71572
Ha = 223
629 n
mi
Hp = 198
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17137756
36 X = -5264079
79
Y = 6633294
14 feet Y = 1963188
00 meter
Z = 12339833
42 Z = 3735706
46
XDOT = -15567
607104 XDOT = -4675
642411
YDOT = -14191
031373 feet/sec YDOT = -4378
099782 meter/sec
ZDOT = -13942
061396 ZDOT = -4272
423727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1145621
14 X = -349185
32
Y = 18410659
09 feet Y = 5611568
89 meter
Z = 12235602
03 Z = 3729411
50
XDOT = -18011
976744 XDOT = -5490
050512
YDOT = 8240
414762 feet/sec YDOT = 2511
678420 meter/sec
ZDOT = -14035
150102 ZDOT = -4277
913751
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
01445759
00016717 00000-0 10270-3 0 9125
2 25544 51
6440 11
2010 0027250 131
1256 229
2258 15
58670540 27899
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
01445759 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 11
2010 deg
Eccentricity:
0027250
Arg of perigee: 131
1256 deg
Mean anomaly: 229
2258 deg
Mean motion: 15
58670540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 278
Coasting Arc #14 (Orbit 2801)
---------------------------------------
Vector Time (GMT): 2011/341/20:07:37
598
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4487989
58 A = 6769740
33 meter
Y = -2849883
43 meter E =
0033283
Z = -4227414
68 I = 51
68071
XDOT = 5700
209306 Wp = 128
38306
YDOT = 3557
019363 meter/sec RA = 6
51805 deg
ZDOT = 3652
997513 TA = 179
12332
MA = 179
11747
Ha = 223
561 n
mi
Hp = 199
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14724375
26 X = 4540060
29
Y = -9350011
25 feet Y = -2799404
45 meter
Z = -13869470
74 Z = -4205485
49
XDOT = 18701
474102 XDOT = 5642
264501
YDOT = 11670
011033 feet/sec YDOT = 3620
438281 meter/sec
ZDOT = 11984
899978 ZDOT = 3680
549099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11343730
04 X = 3457568
92
Y = -13342910
84 feet Y = -4066919
22 meter
Z = -13779647
13 Z = -4200036
45
XDOT = 20289
226946 XDOT = 6184
156373
YDOT = 4754
053577 feet/sec YDOT = 1449
035530 meter/sec
ZDOT = 12097
119030 ZDOT = 3687
201880
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
84795815
00016717 00000-0 10270-3 0 9138
2 25544 51
6440 7
0171 0025944 134
5415 225
7865 15
58308552 28024
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
84795815 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 7
0171 deg
Eccentricity:
0025944
Arg of perigee: 134
5415 deg
Mean anomaly: 225
7865 deg
Mean motion: 15
58308552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2802
Checksum: 306
Coasting Arc #15 (Orbit 2817)
---------------------------------------
Vector Time (GMT): 2011/342/20:07:37
598
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6435274
98 A = 6776034
35 meter
Y = 1162951
76 meter E =
0039352
Z = 1685382
87 I = 51
67144
XDOT = -2342
890694 Wp = 130
23282
YDOT = -4584
983126 meter/sec RA = 1
51245 deg
ZDOT = -5719
407944 TA = 31
21690
MA = 30
98377
Ha = 223
532 n
mi
Hp = 199
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21113106
89 X = -6455988
44
Y = 3815458
54 feet Y = 1090872
57 meter
Z = 5529471
35 Z = 1654069
72
XDOT = -7686
649259 XDOT = -2263
662176
YDOT = -15042
595557 feet/sec YDOT = -4610
739153 meter/sec
ZDOT = -18764
461758 ZDOT = -5730
597902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18870644
19 X = -5751772
35
Y = 10277110
11 feet Y = 3132463
16 meter
Z = 5401467
90 Z = 1646367
42
XDOT = -11173
400276 XDOT = -3405
652404
YDOT = -10519
676758 feet/sec YDOT = -3206
397476 meter/sec
ZDOT = -18809
755474 ZDOT = -5733
213469
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
87401508
00016717 00000-0 10270-3 0 9146
2 25544 51
6437 1
8693 0026050 138
4572 221
8569 15
58319485 28189
Satellite: ISS
Catalog Number: 25544
Epoch time: 11342
87401508 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 1
8693 deg
Eccentricity:
0026050
Arg of perigee: 138
4572 deg
Mean anomaly: 221
8569 deg
Mean motion: 15
58319485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2818
Checksum: 319
Coasting Arc #16 (Orbit 2833)
---------------------------------------
Vector Time (GMT): 2011/343/20:07:37
598
Vector Time (MET): N/A
Weight (LBS) : 871530
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6609006
20 A = 6776140
17 meter
Y = 672703
14 meter E =
0031110
Z = 1354888
10 I = 51
64251
XDOT = -1693
836332 Wp = 115
24839
YDOT = 4707
481769 meter/sec RA = 356
52345 deg
ZDOT = 5807
686018 TA = 259
51607
MA = 259
86676
Ha = 223
251 n
mi
Hp = 199
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21683091
21 X = 6594410
84
Y = 2207031
30 feet Y = 746527
33 meter
Z = 4445170
93 Z = 1386959
59
XDOT = -5557
205813 XDOT = -1774
563391
YDOT = 15444
493994 feet/sec YDOT = 4688
088163 meter/sec
ZDOT = 19054
087985 ZDOT = 5799
261777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21165663
44 X = 6451294
22
Y = -5085362
00 feet Y = -1550018
34 meter
Z = 4576107
60 Z = 1394797
60
XDOT = -610
825002 XDOT = -186
179461
YDOT = 14909
041157 feet/sec YDOT = 4544
275745 meter/sec
ZDOT = 19019
252743 ZDOT = 5797
068236
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
90003974
00016717 00000-0 10270-3 0 9157
2 25544 51
6438 356
7216 0025834 142
0952 218
2028 15
58390371 28346
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
90003974 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 356
7216 deg
Eccentricity:
0025834
Arg of perigee: 142
0952 deg
Mean anomaly: 218
2028 deg
Mean motion: 15
58390371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2834
Checksum: 307
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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