[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 14th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
145/00:25:23
363 -2
4 3
4 3
4
N/A -0
5 -0
1 220
2
000/00:06:46
727 -2
3 -0
1 212
2
Coasting Arc #1 (Orbit 1229)
---------------------------------------
Vector Time (GMT): 2012/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5060701
86 A = 6775545
30 meter
Y = 1100086
44 meter E =
0009182
Z = -4373811
55 I = 51
34629
XDOT = 1456
552005 Wp = 356
50191
YDOT = -6730
792121 meter/sec RA = 305
24377 deg
ZDOT = -3368
827774 TA = 239
21071
MA = 239
30112
Ha = 218
064 n
mi
Hp = 213
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16603352
57 X = -5051380
09
Y = 3609207
49 feet Y = 1043546
92 meter
Z = -14349775
44 Z = -4398373
57
XDOT = 4778
713927 XDOT = 1548
073880
YDOT = -22082
651316 feet/sec YDOT = -6713
992130 meter/sec
ZDOT = -11052
584560 ZDOT = -3361
529984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8144687
27 X = -2482500
68
Y = 14813920
90 feet Y = 4515283
09 meter
Z = -14450798
15 Z = -4404603
28
XDOT = -12367
044265 XDOT = -3769
475092
YDOT = -17580
962717 feet/sec YDOT = -5358
677436 meter/sec
ZDOT = -11021
941152 ZDOT = -3359
487663
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 12132
52211584
00016717 00000-0 10270-3 0 9004
2 25544 51
6369 305
7462 0010804 303
7460 56
2664 15
56038697 12300
Satellite: ISS
Catalog Number: 25544
Epoch time: 12132
52211584 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 305
7462 deg
Eccentricity:
0010804
Arg of perigee: 303
7460 deg
Mean anomaly: 56
2664 deg
Mean motion: 15
56038697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1230
Checksum: 288
Coasting Arc #2 (Orbit 1245)
---------------------------------------
Vector Time (GMT): 2012/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4131745
21 A = 6772157
49 meter
Y = 1223574
06 meter E =
0007478
Z = 5228637
84 I = 51
31730
XDOT = -3186
902350 Wp = 310
32439
YDOT = 6915
529957 meter/sec RA = 300
20602 deg
ZDOT = 905
616402 TA = 131
00622
MA = 130
94153
Ha = 218
289 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13555594
53 X = 4092356
27
Y = 4014350
58 feet Y = 1269557
34 meter
Z = 17154323
63 Z = 5248614
10
XDOT = -10455
716371 XDOT = -3268
395644
YDOT = 22688
746577 feet/sec YDOT = 6879
436352 meter/sec
ZDOT = 2971
182421 ZDOT = 889
936870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11740976
84 X = 3578649
74
Y = -7694159
40 feet Y = -2345179
78 meter
Z = 17236279
96 Z = 5253618
13
XDOT = 10031
839684 XDOT = 3057
704736
YDOT = 21777
307511 feet/sec YDOT = 6637
723329 meter/sec
ZDOT = 2906
093079 ZDOT = 885
777171
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 12133
54969016
00016717 00000-0 10270-3 0 9018
2 25544 51
6364 300
6071 0010826 307
6210 52
3961 15
56002733 12461
Satellite: ISS
Catalog Number: 25544
Epoch time: 12133
54969016 = yrday
fracday
Element set: 901
Inclination: 51
6364 deg
RA of node: 300
6071 deg
Eccentricity:
0010826
Arg of perigee: 307
6210 deg
Mean anomaly: 52
3961 deg
Mean motion: 15
56002733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1246
Checksum: 273
Coasting Arc #3 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2012/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2841535
94 A = 6772733
60 meter
Y = -3490589
84 meter E =
0006241
Z = -5063885
59 I = 51
30606
XDOT = 4374
016302 Wp = 50
21391
YDOT = -6058
011592 meter/sec RA = 295
16293 deg
ZDOT = 1726
769904 TA = 236
52363
MA = 236
58330
Ha = 218
349 n
mi
Hp = 213
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9322624
49 X = -2777692
95
Y = -11452066
41 feet Y = -3522008
56 meter
Z = -16613797
86 Z = -5077534
72
XDOT = 14350
447186 XDOT = 4433
044837
YDOT = -19875
366115 feet/sec YDOT = -6008
768633 meter/sec
ZDOT = 5665
255589 ZDOT = 1748
161991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14703712
18 X = -4481691
47
Y = -81129
16 feet Y = -24728
17 meter
Z = -16669544
03 Z = -5080877
02
XDOT = -6378
591825 XDOT = -1944
194788
YDOT = -22578
249110 feet/sec YDOT = -6881
850329 meter/sec
ZDOT = 5753
724348 ZDOT = 1753
735181
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 12134
51302624
00016717 00000-0 10270-3 0 9023
2 25544 51
6371 295
7905 0010741 310
7448 49
2772 15
56063866 12619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12134
51302624 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 295
7905 deg
Eccentricity:
0010741
Arg of perigee: 310
7448 deg
Mean anomaly: 49
2772 deg
Mean motion: 15
56063866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 296
Coasting Arc #4 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2012/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1356232
68 A = 6777229
94 meter
Y = 5377247
38 meter E =
0009921
Z = 3900332
02 I = 51
30828
XDOT = -4983
997130 Wp = 19
27324
YDOT = 4196
159942 meter/sec RA = 290
12821 deg
ZDOT = -4039
895383 TA = 113
24628
MA = 113
14179
Ha = 218
637 n
mi
Hp = 213
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4449582
29 X = 1277055
34
Y = 17641887
72 feet Y = 5391970
83 meter
Z = 12796364
90 Z = 3906728
36
XDOT = -16351
696621 XDOT = -5010
923977
YDOT = 13766
928942 feet/sec YDOT = 4140
275318 meter/sec
ZDOT = -13254
249943 ZDOT = -4064
172923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16572039
66 X = 5051157
69
Y = 7466069
88 feet Y = 2275658
10 meter
Z = 12822138
73 Z = 3908187
88
XDOT = 1312
072064 XDOT = 399
919565
YDOT = 20090
666014 feet/sec YDOT = 6123
635001 meter/sec
ZDOT = -13354
390722 ZDOT = -4070
418292
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 12135
54057277
00016717 00000-0 10270-3 0 9039
2 25544 51
6363 290
6517 0010805 314
4931 45
5339 15
56062673 12772
Satellite: ISS
Catalog Number: 25544
Epoch time: 12135
54057277 = yrday
fracday
Element set: 903
Inclination: 51
6363 deg
RA of node: 290
6517 deg
Eccentricity:
0010805
Arg of perigee: 314
4931 deg
Mean anomaly: 45
5339 deg
Mean motion: 15
56062673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 305
Coasting Arc #5 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2012/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 113532
49 A = 6781951
83 meter
Y = -6478267
20 meter E =
0013609
Z = -1972505
02 I = 51
31629
XDOT = 5044
365408 Wp = 347
96941
YDOT = -1602
734620 meter/sec RA = 285
11230 deg
ZDOT = 5560
321582 TA = 350
12431
MA = 350
15103
Ha = 218
738 n
mi
Hp = 212
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 372481
93 X = 195547
44
Y = -21254157
48 feet Y = -6476539
00 meter
Z = -6471473
16 Z = -1971754
38
XDOT = 16549
755276 XDOT = 5034
901521
YDOT = -5258
315683 feet/sec YDOT = -1546
378421 meter/sec
ZDOT = 18242
524875 ZDOT = 5584
804131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16684602
29 X = -5085466
78
Y = -13173826
70 feet Y = -4015382
38 meter
Z = -6467785
91 Z = -1971381
15
XDOT = 4785
862882 XDOT = 1458
731007
YDOT = -15057
132370 feet/sec YDOT = -4589
413946 meter/sec
ZDOT = 18343
261665 ZDOT = 5591
026156
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 12136
50388483
00016717 00000-0 10270-3 0 9043
2 25544 51
6377 285
8345 0010800 318
3659 41
6671 15
56099928 12923
Satellite: ISS
Catalog Number: 25544
Epoch time: 12136
50388483 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 285
8345 deg
Eccentricity:
0010800
Arg of perigee: 318
3659 deg
Mean anomaly: 41
6671 deg
Mean motion: 15
56099928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 330
Coasting Arc #6 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2012/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1473567
45 A = 6783401
86 meter
Y = 6611766
61 meter E =
0001027
Z = -362404
30 I = 51
31397
XDOT = -4613
839622 Wp = 71
16674
YDOT = -1354
738408 meter/sec RA = 280
10891 deg
ZDOT = -5969
394637 TA = 112
75765
MA = 112
74680
Ha = 218
953 n
mi
Hp = 212
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4834538
88 X = -1545631
55
Y = 21692147
66 feet Y = 6594885
34 meter
Z = -1188990
47 Z = -369737
79
XDOT = -15137
269100 XDOT = -4569
349363
YDOT = -4444
679817 feet/sec YDOT = -1406
084303 meter/sec
ZDOT = -19584
628073 ZDOT = -5991
700750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14654201
66 X = 4466600
67
Y = 16706357
01 feet Y = 5092097
62 meter
Z = -1219731
04 Z = -371774
02
XDOT = -11238
673746 XDOT = -3425
547758
YDOT = 8424
768110 feet/sec YDOT = 2567
869320 meter/sec
ZDOT = -19676
148506 ZDOT = -5997
290065
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 12137
53140397
00016717 00000-0 10270-3 0 9058
2 25544 51
6369 280
6958 0010969 322
5987 37
4402 15
56147266 13086
Satellite: ISS
Catalog Number: 25544
Epoch time: 12137
53140397 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 280
6958 deg
Eccentricity:
0010969
Arg of perigee: 322
5987 deg
Mean anomaly: 37
4402 deg
Mean motion: 15
56147266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 328
Coasting Arc #7 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2012/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2616552
96 A = 6780433
39 meter
Y = -5666999
73 meter E =
0013859
Z = 2624066
94 I = 51
30138
XDOT = 3811
061011 Wp = 30
95583
YDOT = 4168
239107 meter/sec RA = 275
10254 deg
ZDOT = 5201
118002 TA = 358
81724
MA = 358
82051
Ha = 218
940 n
mi
Hp = 212
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8584491
35 X = 2666980
70
Y = -18592518
79 feet Y = -5637457
96 meter
Z = 8609143
49 Z = 2636900
51
XDOT = 12503
481008 XDOT = 3738
901380
YDOT = 13675
325155 feet/sec YDOT = 4210
453074 meter/sec
ZDOT = 17064
035438 ZDOT = 5219
457169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10270400
09 X = -3130417
95
Y = -17691084
07 feet Y = -5392242
42 meter
Z = 8662391
41 Z = 2640296
90
XDOT = 17033
413733 XDOT = 5191
784506
YDOT = -1495
626490 feet/sec YDOT = -455
866954 meter/sec
ZDOT = 17139
000899 ZDOT = 5223
967474
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 12138
55890972
00016717 00000-0 10270-3 0 9063
2 25544 51
6384 275
5573 0010839 325
7814 34
2640 15
56170997 13243
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
55890972 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 275
5573 deg
Eccentricity:
0010839
Arg of perigee: 325
7814 deg
Mean anomaly: 34
2640 deg
Mean motion: 15
56170997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 330
Coasting Arc #8 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2012/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3505196
44 A = 6775264
82 meter
Y = 3826789
94 meter E =
0012944
Z = -4365825
47 I = 51
28255
XDOT = -2695
765624 Wp = 12
63900
YDOT = -6330
178159 meter/sec RA = 270
07970 deg
ZDOT = -3373
746690 TA = 222
95857
MA = 223
05972
Ha = 219
253 n
mi
Hp = 211
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11499988
33 X = -3526519
29
Y = 12555085
11 feet Y = 3787473
69 meter
Z = -14323574
39 Z = -4382905
45
XDOT = -8844
375407 XDOT = -2608
390723
YDOT = -20768
301048 feet/sec YDOT = -6359
835146 meter/sec
ZDOT = -11068
722737 ZDOT = -3386
630968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3960762
49 X = 1207240
41
Y = 16497482
13 feet Y = 5028432
55 meter
Z = -14394100
21 Z = -4387321
75
XDOT = -20905
839085 XDOT = -6372
099753
YDOT = -4713
980359 feet/sec YDOT = -1436
821213 meter/sec
ZDOT = -11121
082096 ZDOT = -3389
705823
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 12139
52218534
00016717 00000-0 10270-3 0 9070
2 25544 51
6386 270
7406 0010989 329
8158 30
2362 15
56160535 13399
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
52218534 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 270
7406 deg
Eccentricity:
0010989
Arg of perigee: 329
8158 deg
Mean anomaly: 30
2362 deg
Mean motion: 15
56160535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 313
Coasting Arc #9 (Orbit 1354)
---------------------------------------
Vector Time (GMT): 2012/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4093628
64 A = 6771539
11 meter
Y = -1328134
48 meter E =
0008486
Z = 5228766
19 I = 51
27233
XDOT = 1344
944941 Wp = 345
83189
YDOT = 7503
534988 meter/sec RA = 265
03707 deg
ZDOT = 861
360441 TA = 95
94153
MA = 95
84481
Ha = 219
272 n
mi
Hp = 211
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13430540
14 X = 4082775
21
Y = -4357396
60 feet Y = -1282418
07 meter
Z = 17154744
72 Z = 5248626
77
XDOT = 4412
549018 XDOT = 1256
754551
YDOT = 24617
896943 feet/sec YDOT = 7518
081830 meter/sec
ZDOT = 2825
985700 ZDOT = 867
680593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3661283
15 X = 1115959
10
Y = -13533317
83 feet Y = -4124955
28 meter
Z = 17236469
89 Z = 5253676
02
XDOT = 22012
269041 XDOT = 6709
339604
YDOT = 9551
757795 feet/sec YDOT = 2911
375776 meter/sec
ZDOT = 2851
272004 ZDOT = 869
067707
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 12140
54966436
00016717 00000-0 10270-3 0 9086
2 25544 51
6394 265
6015 0011090 333
5493 26
5093 15
56210323 13553
Satellite: ISS
Catalog Number: 25544
Epoch time: 12140
54966436 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 265
6015 deg
Eccentricity:
0011090
Arg of perigee: 333
5493 deg
Mean anomaly: 26
5093 deg
Mean motion: 15
56210323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1355
Checksum: 293
Coasting Arc #10 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2012/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4335028
06 A = 6772333
37 meter
Y = -1317332
75 meter E =
0011203
Z = -5039092
00 I = 51
27905
XDOT = 163
845156 Wp = 50
53232
YDOT = -7447
300410 meter/sec RA = 259
99115 deg
ZDOT = 1815
643242 TA = 237
08293
MA = 237
19075
Ha = 219
434 n
mi
Hp = 211
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14222533
00 X = -4295495
97
Y = -4321957
85 feet Y = -1365588
22 meter
Z = -16532454
06 Z = -5060055
85
XDOT = 537
549725 XDOT = 238
290064
YDOT = -24433
400296 feet/sec YDOT = -7445
052114 meter/sec
ZDOT = 5956
834782 ZDOT = 1816
619354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11192529
02 X = -3411482
85
Y = 9635107
78 feet Y = 2936780
85 meter
Z = -16618477
49 Z = -5065311
94
XDOT = -19692
263651 XDOT = -6002
201961
YDOT = -12647
615626 feet/sec YDOT = -3854
993243 meter/sec
ZDOT = 5961
519799 ZDOT = 1817
071235
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 12141
51291524
00016717 00000-0 10270-3 0 9094
2 25544 51
6396 260
7856 0011052 337
8132 22
2543 15
56226515 13709
Satellite: ISS
Catalog Number: 25544
Epoch time: 12141
51291524 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 260
7856 deg
Eccentricity:
0011052
Arg of perigee: 337
8132 deg
Mean anomaly: 22
2543 deg
Mean motion: 15
56226515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1370
Checksum: 287
Coasting Arc #11 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2012/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166339
33 A = 6777082
61 meter
Y = 3757282
10 meter E =
0014351
Z = 3804976
21 I = 51
30127
XDOT = -1778
470323 Wp = 33
19986
YDOT = 6195
734788 meter/sec RA = 254
95503 deg
ZDOT = -4151
440021 TA = 100
81146
MA = 100
64990
Ha = 219
697 n
mi
Hp = 211
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13669092
28 X = 4105530
97
Y = 12327041
00 feet Y = 3803532
28 meter
Z = 12483517
74 Z = 3825069
12
XDOT = -5834
876387 XDOT = -1827
453029
YDOT = 20327
213870 feet/sec YDOT = 6175
573395 meter/sec
ZDOT = -13620
210043 ZDOT = -4160
198213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17592630
51 X = 5362233
78
Y = -5219149
88 feet Y = -1590796
88 meter
Z = 12565749
68 Z = 3830040
50
XDOT = 14007
339860 XDOT = 4269
437189
YDOT = 14184
253160 feet/sec YDOT = 4323
360363 meter/sec
ZDOT = -13656
758603 ZDOT = -4162
580022
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 12142
54036983
00016717 00000-0 10270-3 0 9106
2 25544 51
6399 255
6468 0011040 341
8625 18
2133 15
56201818 13869
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
54036983 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 255
6468 deg
Eccentricity:
0011040
Arg of perigee: 341
8625 deg
Mean anomaly: 18
2133 deg
Mean motion: 15
56201818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1386
Checksum: 299
Coasting Arc #12 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2012/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3543049
68 A = 6781836
70 meter
Y = -5479613
75 meter E =
0016738
Z = -1809814
68 I = 51
32666
XDOT = 3335
825466 Wp = 5
82611
YDOT = -4010
699890 meter/sec RA = 249
93978 deg
ZDOT = 5633
710377 TA = 334
15497
MA = 334
23849
Ha = 219
855 n
mi
Hp = 210
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11624178
73 X = -3472720
41
Y = -17977735
39 feet Y = -5518840
88 meter
Z = -5937712
20 Z = -1826856
69
XDOT = 10944
309273 XDOT = 3353
058351
YDOT = -13158
464206 feet/sec YDOT = -3973
300926 meter/sec
ZDOT = 18483
301761 ZDOT = 5649
957275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21368335
76 X = -6513068
74
Y = 940192
21 feet Y = 286570
59 meter
Z = -6007261
65 Z = -1831013
35
XDOT = -5830
909572 XDOT = -1777
261237
YDOT = -14430
332831 feet/sec YDOT = -4398
365447 meter/sec
ZDOT = 18550
431017 ZDOT = 5654
171374
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 12143
50359460
00016717 00000-0 10270-3 0 9112
2 25544 51
6404 250
8297 0011359 345
2994 14
7828 15
56217717 14018
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
50359460 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 250
8297 deg
Eccentricity:
0011359
Arg of perigee: 345
2994 deg
Mean anomaly: 14
7828 deg
Mean motion: 15
56217717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1401
Checksum: 304
Coasting Arc #13 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2012/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911697
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2427376
59 A = 6782977
51 meter
Y = 6308513
06 meter E =
0005736
Z = -591749
74 I = 51
34175
XDOT = -4670
478004 Wp = 60
58845
YDOT = 1243
092600 meter/sec RA = 244
93856 deg
ZDOT = -5946
997932 TA = 125
82385
MA = 125
77054
Ha = 219
968 n
mi
Hp = 210
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7963833
95 X = 2359527
71
Y = 20697221
34 feet Y = 6335278
20 meter
Z = -1941436
15 Z = -580121
58
XDOT = -15323
090563 XDOT = -4655
141940
YDOT = 4078
387796 feet/sec YDOT = 1190
950888 meter/sec
ZDOT = -19511
148072 ZDOT = -5969
649730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21952444
11 X = 6691104
96
Y = 3173168
75 feet Y = 967181
84 meter
Z = -1894200
23 Z = -577352
23
XDOT = -3653
307579 XDOT = -1113
528150
YDOT = 13653
493758 feet/sec YDOT = 4161
584898 meter/sec
ZDOT = -19604
360859 ZDOT = -5975
409190
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 12144
53102261
00016717 00000-0 10270-3 0 9122
2 25544 51
6398 245
6915 0011236 349
1836 10
9074 15
56264180 14175
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53102261 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 245
6915 deg
Eccentricity:
0011236
Arg of perigee: 349
1836 deg
Mean anomaly: 10
9074 deg
Mean motion: 15
56264180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 291
Coasting Arc #14 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2012/145/00:28:46
727
Vector Time (MET): N/A
Weight (LBS) : 911399
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -131745
40 A = 6779685
78 meter
Y = 5804543
75 meter E =
0009936
Z = -3512024
97 I = 51
33144
XDOT = -5531
305283 Wp = 12
99584
YDOT = -2838
319166 meter/sec RA = 242
34898 deg
ZDOT = -4476
544636 TA = 208
52513
MA = 208
57954
Ha = 220
233 n
mi
Hp = 212
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -432235
55 X = -179582
43
Y = 19043778
70 feet Y = 5802803
43 meter
Z = -11522391
65 Z = -3512780
50
XDOT = -18147
327043 XDOT = -5477
409301
YDOT = -9312
070753 feet/sec YDOT = -2899
871761 meter/sec
ZDOT = -14686
826233 ZDOT = -4503
285114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17573571
39 X = -5356424
56
Y = -7344289
43 feet Y = -2238539
42 meter
Z = -11526007
35 Z = -3513127
04
XDOT = 14768
937680 XDOT = 4501
572205
YDOT = -12081
875369 feet/sec YDOT = -3682
555612 meter/sec
ZDOT = -14796
490681 ZDOT = -4509
970360
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 12145
04474082
00016717 00000-0 10270-3 0 9133
2 25544 51
6397 243
1249 0009746 342
8405 17
2418 15
55647168 14253
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
04474082 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 243
1249 deg
Eccentricity:
0009746
Arg of perigee: 342
8405 deg
Mean anomaly: 17
2418 deg
Mean motion: 15
55647168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 310
Coasting Arc #15 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2012/146/00:28:46
727
Vector Time (MET): N/A
Weight (LBS) : 911399
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1740956
48 A = 6774954
90 meter
Y = -4427393
55 meter E =
0007078
Z = 4817895
25 I = 51
33016
XDOT = 5438
488262 Wp = 33
79087
YDOT = 4820
273201 meter/sec RA = 237
32449 deg
ZDOT = 2468
402082 TA = 31
90451
MA = 31
86166
Ha = 220
264 n
mi
Hp = 211
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5711799
48 X = 1766930
74
Y = -14525569
38 feet Y = -4407780
41 meter
Z = 15806742
95 Z = 4826415
38
XDOT = 17842
809258 XDOT = 5372
191782
YDOT = 15814
544622 feet/sec YDOT = 4880
718780 meter/sec
ZDOT = 8098
432029 ZDOT = 2494
661659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11619030
82 X = 3541480
59
Y = 10367945
63 feet Y = 3160149
83 meter
Z = 15842151
62 Z = 4828687
81
XDOT = -20309
340639 XDOT = -6190
287027
YDOT = 10241
553605 feet/sec YDOT = 3121
625539 meter/sec
ZDOT = 8205
962410 ZDOT = 2501
177343
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 12146
07257004
00016717 00000-0 10270-3 0 9141
2 25544 51
6391 237
9885 0009736 346
5955 13
4939 15
55659441 14415
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
07257004 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 237
9885 deg
Eccentricity:
0009736
Arg of perigee: 346
5955 deg
Mean anomaly: 13
4939 deg
Mean motion: 15
55659441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 330
Coasting Arc #16 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:28:46
727
Vector Time (MET): N/A
Weight (LBS) : 911399
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3327733
42 A = 6772815
77 meter
Y = 2622025
34 meter E =
0016451
Z = -5295674
77 I = 51
34093
XDOT = -4704
270213 Wp = 53
58979
YDOT = -6046
972971 meter/sec RA = 232
28856 deg
ZDOT = -28
391454 TA = 216
08271
MA = 216
19385
Ha = 220
423 n
mi
Hp = 211
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10917760
56 X = -3331080
85
Y = 8602445
35 feet Y = 2584794
38 meter
Z = -17374261
07 Z = -5311848
67
XDOT = -15433
957392 XDOT = -4636
164176
YDOT = -19839
150167 feet/sec YDOT = -6099
198227 meter/sec
ZDOT = -93
147815 ZDOT = -51
079833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4471489
04 X = -1362909
86
Y = -13072204
12 feet Y = -3984407
82 meter
Z = -17440979
75 Z = -5316010
63
XDOT = 22916
260765 XDOT = 6984
876281
YDOT = -7549
209067 feet/sec YDOT = -2300
998924 meter/sec
ZDOT = -185
908563 ZDOT = -56
664930
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 12147
03614839
00016717 00000-0 10270-3 0 9152
2 25544 51
6394 233
1735 0009851 350
1552 9
9407 15
55689708 14567
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03614839 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 233
1735 deg
Eccentricity:
0009851
Arg of perigee: 350
1552 deg
Mean anomaly: 9
9407 deg
Mean motion: 15
55689708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 323
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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