[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 24th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 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
146/12:06:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 209
7
147/00:13:09
849 -2
6 3
0 3
1
N/A -0
2 -0
5 220
3
000/00:06:15
698 -1
7 -0
1 211
2
Coasting Arc #1 (Orbit 1416)
---------------------------------------
Vector Time (GMT): 2012/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2330057
77 A = 6782599
98 meter
Y = 6332402
91 meter E =
0005775
Z = -713688
47 I = 51
34167
XDOT = -4732
998169 Wp = 57
68476
YDOT = 1076
851643 meter/sec RA = 244
94477 deg
ZDOT = -5929
889732 TA = 130
05645
MA = 130
00578
Ha = 219
872 n
mi
Hp = 210
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7644546
49 X = 2262541
35
Y = 20775600
09 feet Y = 6358081
64 meter
Z = -2341497
61 Z = -702532
28
XDOT = -15528
209216 XDOT = -4715
881628
YDOT = 3532
977830 feet/sec YDOT = 1024
020745 meter/sec
ZDOT = -19455
018806 ZDOT = -5952
840948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21865721
54 X = 6664671
92
Y = 3487826
20 feet Y = 1063089
43 meter
Z = -2296203
68 Z = -699882
88
XDOT = -4206
543284 XDOT = -1282
154393
YDOT = 13572
089111 feet/sec YDOT = 4136
772761 meter/sec
ZDOT = -19549
447553 ZDOT = -5958
671614
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
53078356
00016717 00000-0 10270-3 0 9006
2 25544 51
6402 245
6982 0011334 350
2744 9
8189 15
56371387 14177
Satellite: ISS
Catalog Number: 25544
Epoch time: 12144
53078356 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 245
6982 deg
Eccentricity:
0011334
Arg of perigee: 350
2744 deg
Mean anomaly: 9
8189 deg
Mean motion: 15
56371387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1417
Checksum: 307
Coasting Arc #2 (Orbit 1432)
---------------------------------------
Vector Time (GMT): 2012/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -727432
40 A = 6778895
39 meter
Y = -6027950
44 meter E =
0017628
Z = 2987961
68 I = 51
34359
XDOT = 5601
187959 Wp = 42
77015
YDOT = 1778
284401 meter/sec RA = 239
93762 deg
ZDOT = 4946
727072 TA = 351
66171
MA = 351
69096
Ha = 219
938 n
mi
Hp = 210
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2386589
25 X = -674487
51
Y = -19776740
30 feet Y = -6035789
36 meter
Z = 9803023
90 Z = 2984555
73
XDOT = 18376
600916 XDOT = 5556
856286
YDOT = 5834
266406 feet/sec YDOT = 1840
671900 meter/sec
ZDOT = 16229
419526 ZDOT = 4973
830099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18570496
87 X = -5660287
45
Y = -7226057
08 feet Y = -2202502
20 meter
Z = 9789549
92 Z = 2983854
82
XDOT = 13279
101842 XDOT = 4047
470241
YDOT = -11969
030079 feet/sec YDOT = -3648
160368 meter/sec
ZDOT = 16340
673847 ZDOT = 4980
637389
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
55812224
00016717 00000-0 10270-3 0 9010
2 25544 51
6403 240
5587 0011418 354
4252 5
6773 15
56416361 14339
Satellite: ISS
Catalog Number: 25544
Epoch time: 12145
55812224 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 240
5587 deg
Eccentricity:
0011418
Arg of perigee: 354
4252 deg
Mean anomaly: 5
6773 deg
Mean motion: 15
56416361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1433
Checksum: 283
Coasting Arc #3 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2012/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924885
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1163139
19 A = 6773502
75 meter
Y = 4806822
99 meter E =
0017678
Z = -4643677
34 I = 51
34108
XDOT = -5742
407155 Wp = 32
17803
YDOT = -4175
102089 meter/sec RA = 234
91311 deg
ZDOT = -2873
817082 TA = 209
05532
MA = 209
15381
Ha = 220
089 n
mi
Hp = 209
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3816073
44 X = -1194245
59
Y = 15770416
64 feet Y = 4793642
62 meter
Z = -15235161
87 Z = -4649402
88
XDOT = -18839
918488 XDOT = -5681
333114
YDOT = -13697
841500 feet/sec YDOT = -4238
975448 meter/sec
ZDOT = -9428
533734 ZDOT = -2901
565648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12300276
80 X = 3749124
37
Y = 10547097
11 feet Y = 3214755
20 meter
Z = -15259113
61 Z = -4650977
83
XDOT = -20023
004320 XDOT = -6103
011717
YDOT = 9500
368941 feet/sec YDOT = 2895
712453 meter/sec
ZDOT = -9542
249183 ZDOT = -2908
477551
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
52123273
00016717 00000-0 10270-3 0 9028
2 25544 51
6397 235
7416 0011481 357
4859 2
6235 15
56422547 14483
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
52123273 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 235
7416 deg
Eccentricity:
0011481
Arg of perigee: 357
4859 deg
Mean anomaly: 2
6235 deg
Mean motion: 15
56422547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1448
Checksum: 305
Coasting Arc #4 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2012/146/12:06:00
000
Vector Time (MET): N/A
Weight (LBS) : 941309
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3079246
06 A = 6770803
25 meter
Y = 2953357
98 meter E =
0019016
Z = -5270686
64 I = 51
33220
XDOT = -4755
677879 Wp = 48
21267
YDOT = -5979
890528 meter/sec RA = 234
87557 deg
ZDOT = -561
260079 TA = 216
33857
MA = 216
46785
Ha = 220
086 n
mi
Hp = 209
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10102513
32 X = -3086438
35
Y = 9689494
67 feet Y = 2918884
29 meter
Z = -17292279
02 Z = -5285662
70
XDOT = -15602
617712 XDOT = -4685
729585
YDOT = -19619
063412 feet/sec YDOT = -6032
680298 meter/sec
ZDOT = -1841
404459 ZDOT = -584
193776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4366215
88 X = 1330822
60
Y = 13218977
27 feet Y = 4029144
27 meter
Z = -17354100
23 Z = -5289529
75
XDOT = -23487
571305 XDOT = -7159
011734
YDOT = 5169
657511 feet/sec YDOT = 1575
711609 meter/sec
ZDOT = -1935
170581 ZDOT = -589
839993
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
52123250
00016717 00000-0 10270-3 0 9034
2 25544 51
6397 235
7417 0011565 357
3881 2
7211 15
56423223 14488
Satellite: ISS
Catalog Number: 25544
Epoch time: 12146
52123250 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 235
7417 deg
Eccentricity:
0011565
Arg of perigee: 357
3881 deg
Mean anomaly: 2
7211 deg
Mean motion: 15
56423223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1448
Checksum: 286
Coasting Arc #5 (Orbit 1455)
---------------------------------------
Vector Time (GMT): 2012/147/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 262373
97 A = 6777604
05 meter
Y = 5510737
47 meter E =
0013004
Z = -3950588
56 I = 51
35818
XDOT = -6012
381538 Wp = 23
18019
YDOT = -2576
330570 meter/sec RA = 232
34981 deg
ZDOT = -3985
826734 TA = 205
01294
MA = 205
07600
Ha = 220
318 n
mi
Hp = 211
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 860806
99 X = 219923
41
Y = 18079847
34 feet Y = 5513434
54 meter
Z = -12961248
57 Z = -3949416
52
XDOT = -19725
661213 XDOT = -5963
763326
YDOT = -8452
528117 feet/sec YDOT = -2643
292503 meter/sec
ZDOT = -13076
859365 ZDOT = -4014
916868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17035915
25 X = -5192546
97
Y = -6124716
02 feet Y = -1866813
44 meter
Z = -12956900
80 Z = -3949263
36
XDOT = 14946
244183 XDOT = 4555
615227
YDOT = -13605
962146 feet/sec YDOT = -4147
097262 meter/sec
ZDOT = -13196
235509 ZDOT = -4022
212583
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
03489059
00016717 00000-0 10270-3 0 9044
2 25544 51
6391 233
1729 0010138 352
4515 7
6485 15
55890020 14563
Satellite: ISS
Catalog Number: 25544
Epoch time: 12147
03489059 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 233
1729 deg
Eccentricity:
0010138
Arg of perigee: 352
4515 deg
Mean anomaly: 7
6485 deg
Mean motion: 15
55890020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1456
Checksum: 301
Coasting Arc #6 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2012/148/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1656348
87 A = 6773161
65 meter
Y = -4175404
45 meter E =
0007968
Z = 5064285
29 I = 51
36265
XDOT = 5997
809700 Wp = 27
76707
YDOT = 4467
430274 meter/sec RA = 227
32040 deg
ZDOT = 1727
467072 TA = 45
51980
MA = 45
45468
Ha = 220
320 n
mi
Hp = 210
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5434215
46 X = 1678314
78
Y = -13698833
51 feet Y = -4156759
75 meter
Z = 16615109
21 Z = 5072384
77
XDOT = 19677
853348 XDOT = 5939
016548
YDOT = 14656
923472 feet/sec YDOT = 4534
172616 meter/sec
ZDOT = 5667
542888 ZDOT = 1756
461805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10743979
86 X = 3274765
06
Y = 10031759
51 feet Y = 3057680
30 meter
Z = 16648762
39 Z = 5074542
78
XDOT = -20164
351748 XDOT = -6146
094413
YDOT = 12024
517345 feet/sec YDOT = 3665
072887 meter/sec
ZDOT = 5786
382502 ZDOT = 1763
689387
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
06255511
00016717 00000-0 10270-3 0 9053
2 25544 51
6387 228
0351 0010130 356
2976 3
8101 15
55918104 14722
Satellite: ISS
Catalog Number: 25544
Epoch time: 12148
06255511 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 228
0351 deg
Eccentricity:
0010130
Arg of perigee: 356
2976 deg
Mean anomaly: 3
8101 deg
Mean motion: 15
55918104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 279
Coasting Arc #7 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2012/149/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3531329
20 A = 6772262
16 meter
Y = 2451229
83 meter E =
0016763
Z = -5244462
96 I = 51
38171
XDOT = -5149
724562 Wp = 59
28619
YDOT = -5608
102284 meter/sec RA = 222
28254 deg
ZDOT = 856
783007 TA = 218
88197
MA = 219
00266
Ha = 220
440 n
mi
Hp = 210
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11585725
73 X = -3533000
39
Y = 8042092
61 feet Y = 2411731
35 meter
Z = -17206243
30 Z = -5261621
94
XDOT = -16895
421790 XDOT = -5090
792950
YDOT = -18399
285710 feet/sec YDOT = -5665
360248 meter/sec
ZDOT = 2810
967871 ZDOT = 831
908535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3445112
87 X = -1050070
40
Y = -13586590
46 feet Y = -4141192
77 meter
Z = -17277003
78 Z = -5266030
75
XDOT = 22211
420372 XDOT = 6770
040929
YDOT = -9033
730771 feet/sec YDOT = -2753
481139 meter/sec
ZDOT = 2709
149373 ZDOT = 825
748729
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
02597133
00016717 00000-0 10270-3 0 9060
2 25544 51
6390 223
2187 0010251 359
5430
5713 15
55955826 14876
Satellite: ISS
Catalog Number: 25544
Epoch time: 12149
02597133 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 223
2187 deg
Eccentricity:
0010251
Arg of perigee: 359
5430 deg
Mean anomaly:
5713 deg
Mean motion: 15
55955826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1487
Checksum: 300
Coasting Arc #8 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2012/150/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5117849
12 A = 6775497
23 meter
Y = -526916
19 meter E =
0016406
Z = 4408585
70 I = 51
41631
XDOT = 3486
947947 Wp = 34
21308
YDOT = 5973
818919 meter/sec RA = 217
25066 deg
ZDOT = -3314
604639 TA = 89
44182
MA = 89
25384
Ha = 220
479 n
mi
Hp = 210
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16790843
57 X = 5101944
79
Y = -1728727
66 feet Y = -469774
43 meter
Z = 14463863
84 Z = 4433409
47
XDOT = 11440
117936 XDOT = 3435
990026
YDOT = 19599
143436 feet/sec YDOT = 6012
527410 meter/sec
ZDOT = -10874
687135 ZDOT = -3297
788510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4030115
02 X = -1228379
06
Y = 16300748
40 feet Y = 4968468
11 meter
Z = 14565989
81 Z = 4439713
69
XDOT = -21148
216588 XDOT = -6445
976416
YDOT = 4483
741043 feet/sec YDOT = 1366
644270 meter/sec
ZDOT = -10806
023260 ZDOT = -3293
675890
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
05359446
00016717 00000-0 10270-3 0 9079
2 25544 51
6390 218
0808 0010388 2
9958 357
1256 15
56007892 15037
Satellite: ISS
Catalog Number: 25544
Epoch time: 12150
05359446 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 218
0808 deg
Eccentricity:
0010388
Arg of perigee: 2
9958 deg
Mean anomaly: 357
1256 deg
Mean motion: 15
56007892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 310
Coasting Arc #9 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2012/151/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6065443
23 A = 6780569
91 meter
Y = -1228038
91 meter E =
0013742
Z = -2757564
26 I = 51
45819
XDOT = -1191
976138 Wp = 22
68225
YDOT = -5581
893283 meter/sec RA = 212
23743 deg
ZDOT = 5128
593648 TA = 305
96018
MA = 306
08757
Ha = 220
572 n
mi
Hp = 210
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19899748
13 X = -6037864
49
Y = -4028999
04 feet Y = -1295712
09 meter
Z = -9047126
82 Z = -2786963
28
XDOT = -3910
682867 XDOT = -1154
383477
YDOT = -18313
298172 feet/sec YDOT = -5595
012803 meter/sec
ZDOT = 16826
094647 ZDOT = 5122
894013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10212006
64 X = 3112619
62
Y = -17485629
07 feet Y = -5329619
74 meter
Z = -9167933
74 Z = -2794386
21
XDOT = 17353
213640 XDOT = 5289
259517
YDOT = 1360
162744 feet/sec YDOT = 414
577604 meter/sec
ZDOT = 16803
107798 ZDOT = 5121
587257
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
01697353
00016717 00000-0 10270-3 0 9089
2 25544 51
6391 213
2640 0010409 6
2214 353
9067 15
55999461 15186
Satellite: ISS
Catalog Number: 25544
Epoch time: 12151
01697353 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 213
2640 deg
Eccentricity:
0010409
Arg of perigee: 6
2214 deg
Mean anomaly: 353
9067 deg
Mean motion: 15
55999461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 299
Coasting Arc #10 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2012/152/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6193109
77 A = 6783756
37 meter
Y = 2719334
15 meter E =
0012161
Z = 524544
28 I = 51
49496
XDOT = -1491
989118 Wp = 81
60604
YDOT = 4572
364312 meter/sec RA = 207
24311 deg
ZDOT = -5968
160232 TA = 92
72367
MA = 92
58447
Ha = 220
740 n
mi
Hp = 210
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20318601
60 X = 6159693
18
Y = 8921699
95 feet Y = 2788402
46 meter
Z = 1720945
82 Z = 554549
57
XDOT = -4894
977421 XDOT = -1514
014956
YDOT = 15001
195248 feet/sec YDOT = 4555
557202 meter/sec
ZDOT = -19580
578190 ZDOT = -5975
461554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14709046
18 X = -4483317
28
Y = 16602622
76 feet Y = 5060479
42 meter
Z = 1844134
85 Z = 562092
30
XDOT = -11607
854731 XDOT = -3538
074122
YDOT = -8064
703468 feet/sec YDOT = -2458
121617 meter/sec
ZDOT = -19610
978719 ZDOT = -5977
426314
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
04455853
00016717 00000-0 10270-3 0 9091
2 25544 51
6390 208
1262 0010243 10
6229 349
5139 15
55999466 15343
Satellite: ISS
Catalog Number: 25544
Epoch time: 12152
04455853 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 208
1262 deg
Eccentricity:
0010243
Arg of perigee: 10
6229 deg
Mean anomaly: 349
5139 deg
Mean motion: 15
55999466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 308
Coasting Arc #11 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2012/153/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5365268
04 A = 6782396
52 meter
Y = -3723483
36 meter E =
0022008
Z = 1779173
67 I = 51
51795
XDOT = 4097
753218 Wp = 43
51108
YDOT = -3186
575283 meter/sec RA = 202
25337 deg
ZDOT = 5662
254333 TA = 336
10904
MA = 336
21102
Ha = 220
778 n
mi
Hp = 209
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17602585
42 X = -5331875
50
Y = -12216152
76 feet Y = -3783294
55 meter
Z = 5837183
94 Z = 1753189
78
XDOT = 13444
072238 XDOT = 4105
575165
YDOT = -10454
643318 feet/sec YDOT = -3140
708411 meter/sec
ZDOT = 18576
949911 ZDOT = 5682
180114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16800756
19 X = 5120870
49
Y = -13343644
35 feet Y = -4067142
80 meter
Z = 5730607
72 Z = 1746689
23
XDOT = 5171
298628 XDOT = 1576
211822
YDOT = 14561
834897 feet/sec YDOT = 4438
447277 meter/sec
ZDOT = 18659
169726 ZDOT = 5687
314932
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
07212050
00016717 00000-0 10270-3 0 9107
2 25544 51
6385 202
9876 0010435 13
4363 346
7066 15
56072043 15503
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
07212050 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 202
9876 deg
Eccentricity:
0010435
Arg of perigee: 13
4363 deg
Mean anomaly: 346
7066 deg
Mean motion: 15
56072043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 274
Coasting Arc #12 (Orbit 1564)
---------------------------------------
Vector Time (GMT): 2012/154/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3666326
41 A = 6777677
37 meter
Y = 4282967
17 meter E =
0014212
Z = -3778995
93 I = 51
52972
XDOT = -6195
092831 Wp = 38
23125
YDOT = 1582
454010 meter/sec RA = 197
25422 deg
ZDOT = -4214
477794 TA = 187
09715
MA = 187
11729
Ha = 220
820 n
mi
Hp = 209
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12028629
94 X = 3636518
75
Y = 14051729
55 feet Y = 4323800
06 meter
Z = -12398280
61 Z = -3761256
67
XDOT = -20325
107714 XDOT = -6191
854353
YDOT = 5191
778247 feet/sec YDOT = 1513
195225 meter/sec
ZDOT = -13827
026883 ZDOT = -4244
565801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16822647
48 X = -5127542
95
Y = 7805965
89 feet Y = 2379258
40 meter
Z = -12325657
47 Z = -3756860
40
XDOT = 1104
003675 XDOT = 336
500320
YDOT = -19661
949035 feet/sec YDOT = -5992
962066 meter/sec
ZDOT = -13950
930602 ZDOT = -4252
243647
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 12154
03544295
00016717 00000-0 10270-3 0 9114
2 25544 51
6374 198
1707 0010387 16
6432 343
5061 15
56081226 15657
Satellite: ISS
Catalog Number: 25544
Epoch time: 12154
03544295 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 198
1707 deg
Eccentricity:
0010387
Arg of perigee: 16
6432 deg
Mean anomaly: 343
5061 deg
Mean motion: 15
56081226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1565
Checksum: 295
Coasting Arc #13 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2012/155/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1297916
11 A = 6772930
23 meter
Y = -4355116
83 meter E =
0010843
Z = 5012609
54 I = 51
54302
XDOT = 7427
764140 Wp = 53
35028
YDOT = 26
476034 meter/sec RA = 192
23690 deg
ZDOT = 1949
698774 TA = 17
75054
MA = 17
71269
Ha = 220
960 n
mi
Hp = 209
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4258254
94 X = -1273470
38
Y = -14288441
03 feet Y = -4369494
95 meter
Z = 16445569
37 Z = 5006362
98
XDOT = 24369
304920 XDOT = 7417
444667
YDOT = 86
863628 feet/sec YDOT = 109
479914 meter/sec
ZDOT = 6396
649522 ZDOT = 1985
758083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14927346
36 X = 4549855
17
Y = -547180
50 feet Y = -166780
62 meter
Z = 16420230
15 Z = 5004886
15
XDOT = -6365
925743 XDOT = -1940
334166
YDOT = 22404
714119 feet/sec YDOT = 6828
956864 meter/sec
ZDOT = 6545
004834 ZDOT = 1994
917473
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 12155
06296790
00016717 00000-0 10270-3 0 9123
2 25544 51
6370 193
0317 0010507 21
1832 338
9755 15
56096105 15811
Satellite: ISS
Catalog Number: 25544
Epoch time: 12155
06296790 = yrday
fracday
Element set: 912
Inclination: 51
6370 deg
RA of node: 193
0317 deg
Eccentricity:
0010507
Arg of perigee: 21
1832 deg
Mean anomaly: 338
9755 deg
Mean motion: 15
56096105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 298
Coasting Arc #14 (Orbit 1595)
---------------------------------------
Vector Time (GMT): 2012/156/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1317061
29 A = 6771587
32 meter
Y = 4054187
47 meter E =
0020605
Z = -5277058
02 I = 51
56753
XDOT = -7473
494266 Wp = 66
95871
YDOT = -1514
594686 meter/sec RA = 187
20904 deg
ZDOT = 711
739077 TA = 209
79600
MA = 209
91349
Ha = 220
887 n
mi
Hp = 209
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4321067
24 X = -1336663
08
Y = 13301140
00 feet Y = 4039350
55 meter
Z = -17313182
47 Z = -5283503
27
XDOT = -24519
338143 XDOT = -7459
459819
YDOT = -4969
142672 feet/sec YDOT = -1598
089569 meter/sec
ZDOT = 2335
101958 ZDOT = 675
466547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11900493
63 X = -3627270
46
Y = -7282815
67 feet Y = -2219802
22 meter
Z = -17340042
73 Z = -5285245
02
XDOT = 10177
842385 XDOT = 3102
206359
YDOT = -21757
049717 feet/sec YDOT = -6631
548754 meter/sec
ZDOT = 2185
971194 ZDOT = 666
284020
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 12156
02625173
00016717 00000-0 10270-3 0 9132
2 25544 51
6353 188
2134 0010445 24
3301 335
8343 15
56163022 15960
Satellite: ISS
Catalog Number: 25544
Epoch time: 12156
02625173 = yrday
fracday
Element set: 913
Inclination: 51
6353 deg
RA of node: 188
2134 deg
Eccentricity:
0010445
Arg of perigee: 24
3301 deg
Mean anomaly: 335
8343 deg
Mean motion: 15
56163022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1596
Checksum: 276
Coasting Arc #15 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2012/157/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3819497
52 A = 6774789
15 meter
Y = -3383898
04 meter E =
0018201
Z = 4451760
73 I = 51
60924
XDOT = 6340
171937 Wp = 46
84133
YDOT = 2832
118456 meter/sec RA = 182
18799 deg
ZDOT = -3266
320682 TA = 76
15187
MA = 75
94943
Ha = 220
813 n
mi
Hp = 208
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12531159
83 X = 3835427
29
Y = -11102027
68 feet Y = -3341097
77 meter
Z = 14605514
22 Z = 4470353
91
XDOT = 20801
089032 XDOT = 6323
898543
YDOT = 9291
727217 feet/sec YDOT = 2902
927766 meter/sec
ZDOT = -10716
275202 ZDOT = -3235
559230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8044821
29 X = 2452061
53
Y = 14605354
00 feet Y = 4451711
90 meter
Z = 14682319
84 Z = 4475171
09
XDOT = -12647
881829 XDOT = -3855
074381
YDOT = 17679
987760 feet/sec YDOT = 5388
860269 meter/sec
ZDOT = -10589
912493 ZDOT = -3227
805328
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 12157
05373512
00016717 00000-0 10270-3 0 9144
2 25544 51
6355 183
0745 0010393 27
4284 332
7417 15
56202043 16123
Satellite: ISS
Catalog Number: 25544
Epoch time: 12157
05373512 = yrday
fracday
Element set: 914
Inclination: 51
6355 deg
RA of node: 183
0745 deg
Eccentricity:
0010393
Arg of perigee: 27
4284 deg
Mean anomaly: 332
7417 deg
Mean motion: 15
56202043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 281
Coasting Arc #16 (Orbit 1626)
---------------------------------------
Vector Time (GMT): 2012/158/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5674316
38 A = 6779940
24 meter
Y = 2467769
68 meter E =
0014681
Z = -2763806
44 I = 51
65570
XDOT = -4174
630294 Wp = 40
96700
YDOT = -3868
126366 meter/sec RA = 177
18575 deg
ZDOT = 5143
342805 TA = 287
70134
MA = 287
86156
Ha = 220
876 n
mi
Hp = 208
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18616523
56 X = -5688063
80
Y = 8096357
23 feet Y = 2404239
58 meter
Z = -9067606
44 Z = -2791405
00
XDOT = -13696
293615 XDOT = -4156
051057
YDOT = -12690
703299 feet/sec YDOT = -3914
706674 meter/sec
ZDOT = 16874
484270 ZDOT = 5123
107080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4091601
11 X = -1247120
02
Y = -19831990
08 feet Y = -6044790
58 meter
Z = -9181416
35 Z = -2798495
70
XDOT = 13817
686196 XDOT = 4211
630752
YDOT = -10585
123790 feet/sec YDOT = -3226
345731 meter/sec
ZDOT = 16791
514608 ZDOT = 5118
053652
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 12158
01698373
00016717 00000-0 10270-3 0 9157
2 25544 51
6341 178
2557 0010355 31
7520 328
4256 15
56212897 16271
Satellite: ISS
Catalog Number: 25544
Epoch time: 12158
01698373 = yrday
fracday
Element set: 915
Inclination: 51
6341 deg
RA of node: 178
2557 deg
Eccentricity:
0010355
Arg of perigee: 31
7520 deg
Mean anomaly: 328
4256 deg
Mean motion: 15
56212897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1627
Checksum: 312
Coasting Arc #17 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2012/159/00:16:17
698
Vector Time (MET): N/A
Weight (LBS) : 941034
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6647697
47 A = 6782972
81 meter
Y = -1267182
06 meter E =
0015977
Z = 447887
62 I = 51
69712
XDOT = 1293
470848 Wp = 89
17134
YDOT = 4601
541107 meter/sec RA = 172
20420 deg
ZDOT = -5994
250163 TA = 86
00134
MA = 85
81872
Ha = 220
960 n
mi
Hp = 208
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21810031
07 X = 6659197
56
Y = -4157421
47 feet Y = -1192779
17 meter
Z = 1469447
57 Z = 480209
45
XDOT = 4243
670762 XDOT = 1271
037946
YDOT = 15096
919644 feet/sec YDOT = 4615
881024 meter/sec
ZDOT = -19666
175074 ZDOT = -5988
020318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -48844
97 X = -14887
95
Y = 22193470
01 feet Y = 6764569
66 meter
Z = 1602618
96 Z = 488478
26
XDOT = -14030
612568 XDOT = -4276
530711
YDOT = 1427
604456 feet/sec YDOT = 435
133838 meter/sec
ZDOT = -19640
914120 ZDOT = -5986
550624
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 12159
04442701
00016717 00000-0 10270-3 0 9164
2 25544 51
6345 173
1164 0010523 34
9458 325
2384 15
56281398 16432
Satellite: ISS
Catalog Number: 25544
Epoch time: 12159
04442701 = yrday
fracday
Element set: 916
Inclination: 51
6345 deg
RA of node: 173
1164 deg
Eccentricity:
0010523
Arg of perigee: 34
9458 deg
Mean anomaly: 325
2384 deg
Mean motion: 15
56281398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 300
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