[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 18th 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
143/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 210
7
145/00:25:31
964 -2
4 3
4 3
4
N/A -0
5 -0
1 220
3
000/00:06:59
927 -2
2 -0
1 212
2
Coasting Arc #1 (Orbit 1319)
---------------------------------------
Vector Time (GMT): 2012/138/06:05:13
762
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4225472
88 A = 6771476
22 meter
Y = 338710
25 meter E =
0010129
Z = 5283768
11 I = 51
27384
XDOT = -749
857451 Wp = 336
94965
YDOT = 7631
747997 meter/sec RA = 276
32868 deg
ZDOT = 119
683094 TA = 111
95804
MA = 111
85035
Ha = 219
181 n
mi
Hp = 212
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13863099
99 X = 4195703
53
Y = 1111254
09 feet Y = 385795
46 meter
Z = 17335197
20 Z = 5304223
30
XDOT = -2460
162242 XDOT = -835
722882
YDOT = 25038
543296 feet/sec YDOT = 7622
882522 meter/sec
ZDOT = 392
661069 ZDOT = 115
831970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10761024
69 X = 3279960
32
Y = 8642976
32 feet Y = 2634379
18 meter
Z = 17419207
70 Z = 5309374
51
XDOT = -15462
661537 XDOT = -4713
019237
YDOT = 18554
677451 feet/sec YDOT = 5655
465687 meter/sec
ZDOT = 376
137095 ZDOT = 114
646587
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
30200765
00016717 00000-0 10270-3 0 9005
2 25544 51
6403 276
8515 0011479 326
4736 33
5690 15
56149200 13203
Satellite: ISS
Catalog Number: 25544
Epoch time: 12138
30200765 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 276
8515 deg
Eccentricity:
0011479
Arg of perigee: 326
4736 deg
Mean anomaly: 33
5690 deg
Mean motion: 15
56149200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1320
Checksum: 282
Coasting Arc #2 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2012/139/06:05:13
762
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3788722
82 A = 6773462
04 meter
Y = -2907498
16 meter E =
0008306
Z = -4805272
77 I = 51
27762
XDOT = 2157
410314 Wp = 38
95978
YDOT = -6923
483382 meter/sec RA = 271
28216 deg
ZDOT = 2496
842472 TA = 255
65652
MA = 255
74875
Ha = 219
322 n
mi
Hp = 211
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12430192
97 X = -3732585
64
Y = -9539035
96 feet Y = -2949551
87 meter
Z = -15765330
61 Z = -4823542
35
XDOT = 7078
117828 XDOT = 2222
540451
YDOT = -22714
840493 feet/sec YDOT = -6898
993855 meter/sec
ZDOT = 8191
740395 ZDOT = 2507
481102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5106538
90 X = -1556473
06
Y = -14733029
25 feet Y = -4490627
32 meter
Z = -15840128
25 Z = -4828071
09
XDOT = 17234
109848 XDOT = 5252
956682
YDOT = -14797
845535 feet/sec YDOT = -4510
383319 meter/sec
ZDOT = 8236
083854 ZDOT = 2510
358359
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
26528133
00016717 00000-0 10270-3 0 9014
2 25544 51
6395 272
0333 0011609 329
7781 30
2702 15
56178503 13352
Satellite: ISS
Catalog Number: 25544
Epoch time: 12139
26528133 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 272
0333 deg
Eccentricity:
0011609
Arg of perigee: 329
7781 deg
Mean anomaly: 30
2702 deg
Mean motion: 15
56178503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 290
Coasting Arc #3 (Orbit 1350)
---------------------------------------
Vector Time (GMT): 2012/140/06:05:13
762
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3015577
70 A = 6778439
02 meter
Y = 5071358
84 meter E =
0012675
Z = 3341608
09 I = 51
29556
XDOT = -3388
111710 Wp = 35
08221
YDOT = 5080
524591 meter/sec RA = 266
25130 deg
ZDOT = -4633
882909 TA = 105
75730
MA = 105
61748
Ha = 219
564 n
mi
Hp = 211
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9893627
63 X = 2942411
52
Y = 16638316
41 feet Y = 5104671
57 meter
Z = 10963281
13 Z = 3356080
54
XDOT = -11115
852067 XDOT = -3422
160573
YDOT = 16668
387765 feet/sec YDOT = 5042
446579 meter/sec
ZDOT = -15203
027918 ZDOT = -4650
424863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -543425
51 X = -165636
10
Y = 19316441
59 feet Y = 5887651
40 meter
Z = 11022284
10 Z = 3359592
19
XDOT = -16797
430019 XDOT = -5119
856670
YDOT = 8276
935319 feet/sec YDOT = 2522
809885 meter/sec
ZDOT = -15271
458130 ZDOT = -4654
740438
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
29275971
00016717 00000-0 10270-3 0 9029
2 25544 51
6400 266
8950 0011806 333
6965 26
3588 15
56229508 13510
Satellite: ISS
Catalog Number: 25544
Epoch time: 12140
29275971 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 266
8950 deg
Eccentricity:
0011806
Arg of perigee: 333
6965 deg
Mean anomaly: 26
3588 deg
Mean motion: 15
56229508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1351
Checksum: 313
Coasting Arc #4 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2012/141/06:05:13
762
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1964616
02 A = 6782707
95 meter
Y = -6364931
67 meter E =
0018071
Z = -1213983
55 I = 51
31125
XDOT = 4349
828556 Wp = 3
23414
YDOT = -2451
256970 meter/sec RA = 261
23867 deg
ZDOT = 5834
512347 TA = 343
48647
MA = 343
54525
Ha = 219
714 n
mi
Hp = 211
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6445590
62 X = -1887398
68
Y = -20882321
74 feet Y = -6386469
37 meter
Z = -3982885
66 Z = -1223340
74
XDOT = 14271
091062 XDOT = 4348
572454
YDOT = -8042
181661 feet/sec YDOT = -2402
622031 meter/sec
ZDOT = 19142
100876 ZDOT = 5855
640743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5321995
59 X = 1622144
26
Y = -21189389
97 feet Y = -6458526
06 meter
Z = -4020757
88 Z = -1225527
00
XDOT = 14727
422524 XDOT = 4488
918385
YDOT = 63
736854 feet/sec YDOT = 19
426993 meter/sec
ZDOT = 19229
140334 ZDOT = 5861
041974
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
25601050
00016717 00000-0 10270-3 0 9038
2 25544 51
6388 262
0768 0011778 337
0821 22
9806 15
56190089 13669
Satellite: ISS
Catalog Number: 25544
Epoch time: 12141
25601050 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 262
0768 deg
Eccentricity:
0011778
Arg of perigee: 337
0821 deg
Mean anomaly: 22
9806 deg
Mean motion: 15
56190089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 301
Coasting Arc #5 (Orbit 1381)
---------------------------------------
Vector Time (GMT): 2012/142/06:05:13
762
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 650428
71 A = 6782668
75 meter
Y = 6649129
47 meter E =
0004197
Z = -1186691
24 I = 51
31668
XDOT = -4942
011545 Wp = 26
01365
YDOT = -556
284876 meter/sec RA = 256
23669 deg
ZDOT = -5829
799583 TA = 166
93274
MA = 166
92186
Ha = 219
876 n
mi
Hp = 211
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2133952
47 X = 581793
23
Y = 21814729
23 feet Y = 6656019
32 meter
Z = -3893343
96 Z = -1183697
47
XDOT = -16213
948640 XDOT = -4907
103431
YDOT = -1825
081613 feet/sec YDOT = -611
353725 meter/sec
ZDOT = -19126
639052 ZDOT = -5853
723319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9110285
94 X = -2776815
15
Y = 19938150
51 feet Y = 6077148
27 meter
Z = -3881640
91 Z = -1183124
15
XDOT = -11538
878499 XDOT = -3517
050167
YDOT = -9012
546608 feet/sec YDOT = -2747
024206 meter/sec
ZDOT = -19224
899391 ZDOT = -5859
749334
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
28346456
00016717 00000-0 10270-3 0 9049
2 25544 51
6385 256
9386 0011708 340
9390 19
1324 15
56214837 13820
Satellite: ISS
Catalog Number: 25544
Epoch time: 12142
28346456 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 256
9386 deg
Eccentricity:
0011708
Arg of perigee: 340
9390 deg
Mean anomaly: 19
1324 deg
Mean motion: 15
56214837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1382
Checksum: 313
Coasting Arc #6 (Orbit 1397)
---------------------------------------
Vector Time (GMT): 2012/143/06:05:13
762
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 839970
70 A = 6778396
12 meter
Y = -5829059
57 meter E =
0014844
Z = 3335695
22 I = 51
31027
XDOT = 5085
320300 Wp = 39
10599
YDOT = 3392
841426 meter/sec RA = 251
22455 deg
ZDOT = 4648
392043 TA =
04787
MA =
04772
Ha = 219
894 n
mi
Hp = 210
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2755809
37 X = 888885
72
Y = -19124211
19 feet Y = -5819393
38 meter
Z = 10943881
96 Z = 3339893
97
XDOT = 16684
121720 XDOT = 5024
421750
YDOT = 11131
369509 feet/sec YDOT = 3449
367591 meter/sec
ZDOT = 15250
630063 ZDOT = 4672
949111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11682342
84 X = 3560778
10
Y = -15377365
99 feet Y = -4687021
15 meter
Z = 10961659
20 Z = 3341113
72
XDOT = 7924
042932 XDOT = 2415
248286
YDOT = 16962
972945 feet/sec YDOT = 5170
314154 meter/sec
ZDOT = 15351
248092 ZDOT = 4679
060418
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
31090436
00016717 00000-0 10270-3 0 9059
2 25544 51
6378 251
7986 0011749 344
2935 15
7853 15
56256056 13983
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
31090436 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 251
7986 deg
Eccentricity:
0011749
Arg of perigee: 344
2935 deg
Mean anomaly: 15
7853 deg
Mean motion: 15
56256056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1398
Checksum: 326
Coasting Arc #7 (Orbit 1401)
---------------------------------------
Vector Time (GMT): 2012/143/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945769
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4238907
81 A = 6771272
58 meter
Y = -643456
96 meter E =
0012426
Z = 5242395
45 I = 51
29230
XDOT = 2058
011459 Wp = 359
65219
YDOT = 7351
876871 meter/sec RA = 249
84926 deg
ZDOT = -749
486637 TA = 97
61085
MA = 97
46969
Ha = 219
735 n
mi
Hp = 210
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13907177
87 X = 4220321
33
Y = -2111079
27 feet Y = -596159
41 meter
Z = 17199460
15 Z = 5262942
93
XDOT = 6752
006099 XDOT = 1979
289202
YDOT = 24120
330940 feet/sec YDOT = 7374
450754 meter/sec
ZDOT = -2458
945658 ZDOT = -739
679140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3394912
37 X = 1034769
29
Y = -13543517
40 feet Y = -4128064
10 meter
Z = 17283963
31 Z = 5268152
02
XDOT = 23872
108581 XDOT = 7276
218695
YDOT = 2845
628664 feet/sec YDOT = 867
347617 meter/sec
ZDOT = -2419
295469 ZDOT = -737
401259
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
56776320
00016717 00000-0 10270-3 0 9060
2 25544 51
6407 250
5128 0011337 345
4944 14
5882 15
56280962 14025
Satellite: ISS
Catalog Number: 25544
Epoch time: 12143
56776320 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 250
5128 deg
Eccentricity:
0011337
Arg of perigee: 345
4944 deg
Mean anomaly: 14
5882 deg
Mean motion: 15
56280962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1402
Checksum: 299
Coasting Arc #8 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2012/144/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945769
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4786204
69 A = 6774622
84 meter
Y = -1857798
03 meter E =
0010291
Z = -4421330
12 I = 51
31472
XDOT = -342
832627 Wp = 40
52645
YDOT = -6919
314683 meter/sec RA = 244
80944 deg
ZDOT = 3290
550955 TA = 262
75704
MA = 262
87403
Ha = 219
857 n
mi
Hp = 210
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15702771
29 X = -4743596
66
Y = -6095137
88 feet Y = -1911081
56 meter
Z = -14505676
26 Z = -4444478
25
XDOT = -1124
778961 XDOT = -281
418870
YDOT = -22701
163657 feet/sec YDOT = -6922
805461 meter/sec
ZDOT = 10795
770851 ZDOT = 3289
033817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11454063
66 X = -3491198
60
Y = 12237960
23 feet Y = 3730130
28 meter
Z = -14600655
15 Z = -4450279
69
XDOT = -20629
556485 XDOT = -6287
888816
YDOT = -6481
482712 feet/sec YDOT = -1975
555931 meter/sec
ZDOT = 10790
146849 ZDOT = 3288
836759
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
53097468
00016717 00000-0 10270-3 0 9078
2 25544 51
6403 245
6967 0011310 349
4717 10
6198 15
56291671 14172
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53097468 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 245
6967 deg
Eccentricity:
0011310
Arg of perigee: 349
4717 deg
Mean anomaly: 10
6198 deg
Mean motion: 15
56291671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 314
Coasting Arc #9 (Orbit 1424)
---------------------------------------
Vector Time (GMT): 2012/145/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -239544
96 A = 6779415
03 meter
Y = 5748027
78 meter E =
0010361
Z = -3598124
07 I = 51
33052
XDOT = -5526
481584 Wp = 13
67851
YDOT = -2981
783277 meter/sec RA = 242
35202 deg
ZDOT = -4388
207332 TA = 209
09946
MA = 209
15725
Ha = 220
250 n
mi
Hp = 212
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -785908
67 X = -286323
76
Y = 18858358
85 feet Y = 5745087
91 meter
Z = -11804868
99 Z = -3599400
72
XDOT = -18131
501261 XDOT = -5471
410842
YDOT = -9782
753533 feet/sec YDOT = -3043
275372 meter/sec
ZDOT = -14397
005683 ZDOT = -4414
921541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17280050
26 X = -5266959
32
Y = -7584151
88 feet Y = -2311649
49 meter
Z = -11810621
76 Z = -3599877
51
XDOT = 15169
295413 XDOT = 4623
601242
YDOT = -11934
440691 feet/sec YDOT = -3637
617523 meter/sec
ZDOT = -14506
549540 ZDOT = -4421
596300
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
04469180
00016717 00000-0 10270-3 0 9080
2 25544 51
6398 243
1291 0009807 342
9369 17
1453 15
55650510 14252
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
04469180 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 243
1291 deg
Eccentricity:
0009807
Arg of perigee: 342
9369 deg
Mean anomaly: 17
1453 deg
Mean motion: 15
55650510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1425
Checksum: 306
Coasting Arc #10 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2012/146/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1847195
86 A = 6774748
50 meter
Y = -4331895
59 meter E =
0006978
Z = 4864968
53 I = 51
32946
XDOT = 5393
209347 Wp = 31
00023
YDOT = 4930
391239 meter/sec RA = 237
32662 deg
ZDOT = 2346
759721 TA = 35
96661
MA = 35
91966
Ha = 220
276 n
mi
Hp = 211
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6060353
87 X = 1871865
67
Y = -14212255
86 feet Y = -4311101
71 meter
Z = 15961182
84 Z = 4874001
61
XDOT = 17694
256389 XDOT = 5326
275785
YDOT = 16175
824276 feet/sec YDOT = 4990
326933 meter/sec
ZDOT = 7699
342917 ZDOT = 2372
797798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11215139
41 X = 3418374
49
Y = 10570618
21 feet Y = 3221924
43 meter
Z = 15998691
89 Z = 4876401
29
XDOT = -20569
266995 XDOT = -6269
512580
YDOT = 10030
754727 feet/sec YDOT = 3057
374041 meter/sec
ZDOT = 7805
953203 ZDOT = 2379
254536
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
07251959
00016717 00000-0 10270-3 0 9098
2 25544 51
6392 237
9928 0009794 346
6331 13
4562 15
55662688 14416
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
07251959 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 237
9928 deg
Eccentricity:
0009794
Arg of perigee: 346
6331 deg
Mean anomaly: 13
4562 deg
Mean motion: 15
55662688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 338
Coasting Arc #11 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3419387
92 A = 6772814
23 meter
Y = 2502510
27 meter E =
0016326
Z = -5294923
51 I = 51
34088
XDOT = -4619
479441 Wp = 54
17808
YDOT = -6111
375600 meter/sec RA = 232
29030 deg
ZDOT = 104
411370 TA = 216
76585
MA = 216
87793
Ha = 220
440 n
mi
Hp = 211
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11218464
29 X = -3421395
74
Y = 8210335
53 feet Y = 2464261
86 meter
Z = -17371796
28 Z = -5311539
42
XDOT = -15155
772445 XDOT = -4551
304671
YDOT = -20050
444883 feet/sec YDOT = -6162
652302 meter/sec
ZDOT = 342
556987 ZDOT = 82
135062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4015825
07 X = -1224023
48
Y = -13219348
51 feet Y = -4029257
43 meter
Z = -17440321
97 Z = -5315810
14
XDOT = 23003
635790 XDOT = 7011
508189
YDOT = -7278
537818 feet/sec YDOT = -2218
498327 meter/sec
ZDOT = 251
495866 ZDOT = 76
655940
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
03609710
00016717 00000-0 10270-3 0 9109
2 25544 51
6395 233
1777 0009909 350
2125 9
8834 15
55690230 14560
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03609710 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 233
1777 deg
Eccentricity:
0009909
Arg of perigee: 350
2125 deg
Mean anomaly: 9
8834 deg
Mean motion: 15
55690230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 303
Coasting Arc #12 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2012/148/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4779793
25 A = 6774858
51 meter
Y = -457403
23 meter E =
0014507
Z = 4780432
63 I = 51
36720
XDOT = 3200
133203 Wp = 21
25868
YDOT = 6481
445409 meter/sec RA = 227
25504 deg
ZDOT = -2563
815078 TA = 94
16037
MA = 93
99456
Ha = 220
493 n
mi
Hp = 211
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15681736
40 X = 4761330
47
Y = -1500666
78 feet Y = -404056
27 meter
Z = 15683834
09 Z = 4803607
82
XDOT = 10499
124681 XDOT = 3139
872980
YDOT = 21264
584674 feet/sec YDOT = 6516
894564 meter/sec
ZDOT = -8411
466792 ZDOT = -2548
414757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3542292
71 X = -1079690
82
Y = 15251943
28 feet Y = 4648792
31 meter
Z = 15779160
23 Z = 4809488
04
XDOT = -22404
677037 XDOT = -6828
945561
YDOT = 3486
822320 feet/sec YDOT = 1062
783443 meter/sec
ZDOT = -8348
691456 ZDOT = -2544
681156
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 12148
06390065
00016717 00000-0 10270-3 0 9114
2 25544 51
6391 228
0412 0010046 353
4746 6
6275 15
55727417 14723
Satellite: ISS
Catalog Number: 25544
Epoch time: 12148
06390065 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 228
0412 deg
Eccentricity:
0010046
Arg of perigee: 353
4746 deg
Mean anomaly: 6
6275 deg
Mean motion: 15
55727417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 291
Coasting Arc #13 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2012/149/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5658942
48 A = 6779581
04 meter
Y = -1422790
63 meter E =
0010767
Z = -3445828
61 I = 51
40459
XDOT = -1246
245426 Wp = 24
97860
YDOT = -6043
829063 meter/sec RA = 222
23449 deg
ZDOT = 4556
950597 TA = 294
43426
MA = 294
54656
Ha = 220
622 n
mi
Hp = 211
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18566084
26 X = -5625872
85
Y = -4667948
25 feet Y = -1485887
28 meter
Z = -11305211
98 Z = -3473239
37
XDOT = -4088
731714 XDOT = -1200
706186
YDOT = -19828
835510 feet/sec YDOT = -6057
511051 meter/sec
ZDOT = 14950
625319 ZDOT = 4551
006557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10038980
28 X = 3059881
19
Y = -16221886
83 feet Y = -4944431
10 meter
Z = -11417806
54 Z = -3480147
43
XDOT = 18981
175265 XDOT = 5785
462221
YDOT = 1274
199706 feet/sec YDOT = 388
376070 meter/sec
ZDOT = 14926
684297 ZDOT = 4549
653374
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 12149
02745713
00016717 00000-0 10270-3 0 9126
2 25544 51
6394 223
2256 0010075 356
9572 3
1518 15
55710402 14870
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
02745713 = yrday
fracday
Element set: 912
Inclination: 51
6394 deg
RA of node: 223
2256 deg
Eccentricity:
0010075
Arg of perigee: 356
9572 deg
Mean anomaly: 3
1518 deg
Mean motion: 15
55710402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 290
Coasting Arc #14 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2012/150/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5896684
51 A = 6783811
91 meter
Y = 3018786
97 meter E =
0012906
Z = 1460679
38 I = 51
44169
XDOT = -1090
031624 Wp = 75
17595
YDOT = 4938
665290 meter/sec RA = 217
23277 deg
ZDOT = -5760
408011 TA = 88
84058
MA = 88
69272
Ha = 220
839 n
mi
Hp = 211
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19346077
80 X = 5855393
87
Y = 9904156
72 feet Y = 3084496
39 meter
Z = 4792255
19 Z = 1489225
28
XDOT = -3576
219239 XDOT = -1117
192838
YDOT = 16202
970110 feet/sec YDOT = 4926
324365 meter/sec
ZDOT = -18898
976413 ZDOT = -5765
769043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15010206
46 X = -4575110
93
Y = 15681845
42 feet Y = 4779826
48 meter
Z = 4909397
38 Z = 1496384
32
XDOT = -13394
208600 XDOT = -4082
554781
YDOT = -6850
903588 feet/sec YDOT = -2088
155413 meter/sec
ZDOT = -18921
426877 ZDOT = -5767
250912
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 12150
05523978
00016717 00000-0 10270-3 0 9139
2 25544 51
6394 218
0889 0009959 1
3651 358
7528 15
55700309 15036
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
05523978 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 218
0889 deg
Eccentricity:
0009959
Arg of perigee: 1
3651 deg
Mean anomaly: 358
7528 deg
Mean motion: 15
55700309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 319
Coasting Arc #15 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2012/151/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5348537
40 A = 6784393
49 meter
Y = -4083289
71 meter E =
0021365
Z = 753862
65 I = 51
46896
XDOT = 3456
063501 Wp = 32
17616
YDOT = -3418
167741 meter/sec RA = 212
24126 deg
ZDOT = 5945
942664 TA = 336
00609
MA = 336
10550
Ha = 220
879 n
mi
Hp = 210
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17547694
88 X = -5306141
84
Y = -13396619
80 feet Y = -4142863
37 meter
Z = 2473302
67 Z = 727982
18
XDOT = 11338
791015 XDOT = 3465
144949
YDOT = -11214
461094 feet/sec YDOT = -3379
469467 meter/sec
ZDOT = 19507
685907 ZDOT = 5962
754096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17629233
14 X = 5373390
26
Y = -13308446
78 feet Y = -4056414
58 meter
Z = 2367198
17 Z = 721522
00
XDOT = 6808
992296 XDOT = 2075
380852
YDOT = 12538
319341 feet/sec YDOT = 3821
679735 meter/sec
ZDOT = 19577
102457 ZDOT = 5967
100829
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 12151
08300815
00016717 00000-0 10270-3 0 9147
2 25544 51
6395 212
9517 0010146 4
2025 355
9212 15
55755437 15193
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
08300815 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 212
9517 deg
Eccentricity:
0010146
Arg of perigee: 4
2025 deg
Mean anomaly: 355
9212 deg
Mean motion: 15
55755437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 284
Coasting Arc #16 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2012/152/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4028181
59 A = 6781200
19 meter
Y = 4646571
01 meter E =
0009488
Z = -2873160
76 I = 51
48402
XDOT = -5520
473238 Wp = 34
76068
YDOT = 1669
434067 meter/sec RA = 207
24757 deg
ZDOT = -5040
461351 TA = 177
99077
MA = 177
98695
Ha = 220
993 n
mi
Hp = 210
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13215818
85 X = 3989880
66
Y = 15244655
54 feet Y = 4691402
67 meter
Z = -9426380
46 Z = -2853684
49
XDOT = -18111
788838 XDOT = -5514
245123
YDOT = 5477
145888 feet/sec YDOT = 1607
735870 meter/sec
ZDOT = -16536
946688 ZDOT = -5067
264705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18102075
34 X = -5517512
56
Y = 8992718
68 feet Y = 2740980
65 meter
Z = -9346652
76 Z = -2848859
76
XDOT = -94
083724 XDOT = -28
676719
YDOT = -17489
840858 feet/sec YDOT = -5330
903494 meter/sec
ZDOT = -16647
322318 ZDOT = -5074
103843
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 12152
04653260
00016717 00000-0 10270-3 0 9150
2 25544 51
6391 208
1364 0010083 7
1716 352
9579 15
55741243 15345
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
04653260 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 208
1364 deg
Eccentricity:
0010083
Arg of perigee: 7
1716 deg
Mean anomaly: 352
9579 deg
Mean motion: 15
55741243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 289
Coasting Arc #17 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2012/153/00:29:01
927
Vector Time (MET): N/A
Weight (LBS) : 945461
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2046991
60 A = 6776201
55 meter
Y = -4665685
22 meter E =
0012644
Z = 4454444
97 I = 51
49462
XDOT = 6957
359712 Wp = 57
77300
YDOT = 50
937678 meter/sec RA = 202
23876 deg
ZDOT = 3250
399061 TA = 359
48287
MA = 359
48418
Ha = 221
196 n
mi
Hp = 210
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6715851
71 X = -2016305
88
Y = -15307366
22 feet Y = -4688404
75 meter
Z = 14614320
77 Z = 4444574
75
XDOT = 22825
983307 XDOT = 6940
483045
YDOT = 167
118365 feet/sec YDOT = 128
644544 meter/sec
ZDOT = 10664
038915 ZDOT = 3284
157205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16479626
32 X = 5022990
10
Y = -3002329
06 feet Y = -915109
90 meter
Z = 14574101
44 Z = 4442186
12
XDOT = -5750
676155 XDOT = -1752
806092
YDOT = 20877
066457 feet/sec YDOT = 6363
329856 meter/sec
ZDOT = 10802
891863 ZDOT = 3292
721440
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 12153
07428137
00016717 00000-0 10270-3 0 9168
2 25544 51
6388 202
9990 0010294 11
7834 348
3559 15
55752352 15502
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
07428137 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 202
9990 deg
Eccentricity:
0010294
Arg of perigee: 11
7834 deg
Mean anomaly: 348
3559 deg
Mean motion: 15
55752352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 314
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:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
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]
- 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