[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 2nd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6283 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 ET - UTC (sec) : 68 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
308/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 214
9
311/14:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 215
3
314/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 215
7
322/07:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 216
8
Coasting Arc #1 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2016/307/12:18:06
508
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2304655
51 A = 6788364
58 meter
Y = -5822444
40 meter E =
0018342
Z = 2591760
32 I = 52
02132
XDOT = 3945
081059 Wp = 125
37088
YDOT = -3922
495953 meter/sec RA = 87
25678 deg
ZDOT = -5288
025846 TA = 25
60576
MA = 25
51503
Ha = 223
928 n
mi
Hp = 214
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7561205
74 X = -2251966
14
Y = -19102507
87 feet Y = -5847921
95 meter
Z = 8503150
65 Z = 2580692
68
XDOT = 12943
179327 XDOT = 4014
337824
YDOT = -12869
081212 feet/sec YDOT = -3877
992272 meter/sec
ZDOT = -17349
166163 ZDOT = -5268
692835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19014211
26 X = 5795531
59
Y = 7832104
20 feet Y = 2387225
36 meter
Z = 8455715
44 Z = 2577302
07
XDOT = 720
523643 XDOT = 219
615607
YDOT = 16945
722034 feet/sec YDOT = 5165
056076 meter/sec
ZDOT = -17263
795200 ZDOT = -5262
004777
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 16307
54995978
00016717 00000-0 10270-3 0 9000
2 25544 51
6396 87
9386 0007638 167
2872 192
8475 15
53492473 26502
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
54995978 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 87
9386 deg
Eccentricity:
0007638
Arg of perigee: 167
2872 deg
Mean anomaly: 192
8475 deg
Mean motion: 15
53492473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 366
Coasting Arc #2 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4162421
23 A = 6780415
53 meter
Y = 1802042
59 meter E =
0017019
Z = -5054742
96 I = 51
99696
XDOT = -775
674606 Wp = 126
48099
YDOT = 7354
108766 meter/sec RA = 83
95824 deg
ZDOT = 1977
818189 TA = 162
68923
MA = 162
63113
Ha = 223
554 n
mi
Hp = 214
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13656237
62 X = 4166515
34
Y = 5912213
22 feet Y = 1848612
41 meter
Z = -16583802
36 Z = -5034512
53
XDOT = -2544
864192 XDOT = -867
460106
YDOT = 24127
653431 feet/sec YDOT = 7344
921470 meter/sec
ZDOT = 6488
904821 ZDOT = 1973
827042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1626804
38 X = 495849
97
Y = -14890294
52 feet Y = -4538561
77 meter
Z = -16495521
46 Z = -5027834
94
XDOT = 22743
952803 XDOT = 6932
356814
YDOT = -4701
827159 feet/sec YDOT = -1433
116918 meter/sec
ZDOT = 6470
102026 ZDOT = 1972
087098
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 16308
19323524
00016717 00000-0 10270-3 0 9015
2 25544 51
6429 84
7405 0006992 169
7016 190
4281 15
53523049 26609
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19323524 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 84
7405 deg
Eccentricity:
0006992
Arg of perigee: 169
7016 deg
Mean anomaly: 190
4281 deg
Mean motion: 15
53523049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 308
Coasting Arc #3 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2016/309/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4085378
72 A = 6783058
92 meter
Y = -3211470
30 meter E =
0010764
Z = 4348608
70 I = 52
00235
XDOT = 1496
907260 Wp = 110
46738
YDOT = -6658
828559 meter/sec RA = 78
99529 deg
ZDOT = -3507
954273 TA = 15
00589
MA = 14
97398
Ha = 223
502 n
mi
Hp = 214
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13403473
49 X = -4070287
74
Y = -10536319
88 feet Y = -3257071
36 meter
Z = 14267088
89 Z = 4328799
17
XDOT = 4911
113057 XDOT = 1588
297239
YDOT = -21846
550392 feet/sec YDOT = -6641
578153 meter/sec
ZDOT = -11509
036330 ZDOT = -3500
460517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5851324
72 X = -1783483
78
Y = 16089772
81 feet Y = 4904162
75 meter
Z = 14180908
78 Z = 4322341
00
XDOT = -21145
918583 XDOT = -6445
275984
YDOT = 2433
230907 feet/sec YDOT = 741
648781 meter/sec
ZDOT = -11475
001077 ZDOT = -3497
580328
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 16309
22247075
00016717 00000-0 10270-3 0 9027
2 25544 51
6434 79
6151 0006830 172
9995 187
1254 15
53555853 26767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16309
22247075 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 79
6151 deg
Eccentricity:
0006830
Arg of perigee: 172
9995 deg
Mean anomaly: 187
1254 deg
Mean motion: 15
53555853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 328
Coasting Arc #4 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2016/310/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3953228
43 A = 6786499
38 meter
Y = 4421692
10 meter E =
0008045
Z = -3309279
30 I = 52
00605
XDOT = -2260
302840 Wp = 141
39469
YDOT = 5570
694248 meter/sec RA = 74
03892 deg
ZDOT = 4743
239865 TA = 180
41620
MA = 180
41687
Ha = 223
295 n
mi
Hp = 215
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12969909
56 X = 3919565
49
Y = 14506863
86 feet Y = 4465711
54 meter
Z = -10857215
55 Z = -3290156
89
XDOT = -7415
691731 XDOT = -2345
468837
YDOT = 18276
555931 feet/sec YDOT = 5544
941827 meter/sec
ZDOT = 15561
810581 ZDOT = 4732
052813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9476888
54 X = 2888555
63
Y = -17048473
16 feet Y = -5196374
62 meter
Z = -10774271
63 Z = -3283997
99
XDOT = 18485
588032 XDOT = 5634
407232
YDOT = 472
825952 feet/sec YDOT = 144
117350 meter/sec
ZDOT = 15511
783697 ZDOT = 4727
991671
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 16310
18737469
00016717 00000-0 10270-3 0 9036
2 25544 51
6429 74
8095 0006813 176
7646 183
3552 15
53532238 26919
Satellite: ISS
Catalog Number: 25544
Epoch time: 16310
18737469 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 74
8095 deg
Eccentricity:
0006813
Arg of perigee: 176
7646 deg
Mean anomaly: 183
3552 deg
Mean motion: 15
53532238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 329
Coasting Arc #5 (Orbit 2706)
---------------------------------------
Vector Time (GMT): 2016/311/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3689081
78 A = 6789487
08 meter
Y = -5332663
77 meter E =
0017799
Z = 1975341
78 I = 52
00607
XDOT = 3084
405029 Wp = 133
19774
YDOT = -4222
049780 meter/sec RA = 69
09069 deg
ZDOT = -5617
728500 TA = 25
10049
MA = 25
01407
Ha = 223
336 n
mi
Hp = 215
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12103286
68 X = -3638771
91
Y = -17495616
03 feet Y = -5373636
25 meter
Z = 6480780
11 Z = 1957543
05
XDOT = 10119
439072 XDOT = 3158
676784
YDOT = -13851
869358 feet/sec YDOT = -4187
142623 meter/sec
ZDOT = -18430
867783 ZDOT = -5602
564579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12297319
66 X = -3748223
03
Y = 17388323
45 feet Y = 5299960
99 meter
Z = 6403809
51 Z = 1951881
14
XDOT = -15248
758568 XDOT = -4647
821612
YDOT = -3996
898229 feet/sec YDOT = -1218
254580 meter/sec
ZDOT = -18363
660751 ZDOT = -5597
243797
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 16311
21660135
00016717 00000-0 10270-3 0 9047
2 25544 51
6429 69
6843 0006921 179
7556 180
3601 15
53520436 27072
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
21660135 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 69
6843 deg
Eccentricity:
0006921
Arg of perigee: 179
7556 deg
Mean anomaly: 180
3601 deg
Mean motion: 15
53520436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2707
Checksum: 303
Coasting Arc #6 (Orbit 2712)
---------------------------------------
Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3936534
66 A = 6779089
08 meter
Y = -1424907
57 meter E =
0016384
Z = -5344610
87 I = 51
96650
XDOT = 2841
582940 Wp = 117
78426
YDOT = 7107
353830 meter/sec RA = 67
08900 deg
ZDOT = 191
103733 TA = 154
07273
MA = 153
99055
Ha = 223
289 n
mi
Hp = 215
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12915139
97 X = 3978137
99
Y = -4674893
59 feet Y = -1380654
00 meter
Z = -17534812
55 Z = -5325386
81
XDOT = 9322
778676 XDOT = 2760
967185
YDOT = 23318
089992 feet/sec YDOT = 7138
679569 meter/sec
ZDOT = 626
980750 ZDOT = 204
711807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1533076
66 X = 467281
77
Y = 13757195
50 feet Y = 4193193
19 meter
Z = -17450340
10 Z = -5318863
66
XDOT = -23838
830398 XDOT = -7266
075505
YDOT = 3554
954353 feet/sec YDOT = 1083
550087 meter/sec
ZDOT = 685
260874 ZDOT = 208
867514
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 16311
60255773
00016717 00000-0 10270-3 0 9059
2 25544 51
6426 67
7584 0007266 182
9900 177
1210 15
53539021 27139
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
60255773 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 67
7584 deg
Eccentricity:
0007266
Arg of perigee: 182
9900 deg
Mean anomaly: 177
1210 deg
Mean motion: 15
53539021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2713
Checksum: 302
Coasting Arc #7 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4496016
36 A = 6780100
15 meter
Y = -13884
44 meter E =
0005467
Z = 5070567
00 I = 51
95772
XDOT = -2103
024310 Wp = 135
25061
YDOT = -7131
921924 meter/sec RA = 62
11793 deg
ZDOT = -1886
806759 TA = 332
93354
MA = 332
96203
Ha = 223
162 n
mi
Hp = 215
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14750709
84 X = -4520157
92
Y = -45552
63 feet Y = -64296
83 meter
Z = 16635718
50 Z = 5048667
53
XDOT = -6899
686056 XDOT = -2013
951610
YDOT = -23398
693978 feet/sec YDOT = -7154
941346 meter/sec
ZDOT = -6190
310890 ZDOT = -1896
806415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3233834
12 X = 985672
64
Y = -14502073
82 feet Y = -4420232
10 meter
Z = 16539794
97 Z = 5041329
51
XDOT = 23268
887198 XDOT = 7092
356818
YDOT = -1910
201995 feet/sec YDOT = -582
229568 meter/sec
ZDOT = -6232
770238 ZDOT = -1899
748369
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 16312
63177258
00016717 00000-0 10270-3 0 9065
2 25544 51
6433 62
6321 0007123 186
8922 173
2133 15
53590902 27292
Satellite: ISS
Catalog Number: 25544
Epoch time: 16312
63177258 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 62
6321 deg
Eccentricity:
0007123
Arg of perigee: 186
8922 deg
Mean anomaly: 173
2133 deg
Mean motion: 15
53590902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 301
Coasting Arc #8 (Orbit 2743)
---------------------------------------
Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4988482
84 A = 6782852
63 meter
Y = 1385328
39 meter E =
0012349
Z = -4394307
54 I = 51
94965
XDOT = 1156
001764 Wp = 144
56307
YDOT = 6745
484902 meter/sec RA = 57
15148 deg
ZDOT = 3433
898300 TA = 160
17647
MA = 160
12844
Ha = 222
958 n
mi
Hp = 215
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16366413
53 X = 4993966
94
Y = 4545040
65 feet Y = 1441143
50 meter
Z = -14417019
48 Z = -4370061
12
XDOT = 3792
656705 XDOT = 1063
805477
YDOT = 22130
855978 feet/sec YDOT = 6757
896685 meter/sec
ZDOT = 11266
070537 ZDOT = 3439
289822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7711507
28 X = -2350467
42
Y = 15234601
43 feet Y = 4643506
52 meter
Z = -14311076
54 Z = -4362016
13
XDOT = -21319
322502 XDOT = -6498
129499
YDOT = -171
987798 feet/sec YDOT = -52
421881 meter/sec
ZDOT = 11288
408320 ZDOT = 3440
706856
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 16313
59665776
00016717 00000-0 10270-3 0 9079
2 25544 51
6420 57
8273 0007110 188
8347 171
2682 15
53590245 27443
Satellite: ISS
Catalog Number: 25544
Epoch time: 16313
59665776 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 57
8273 deg
Eccentricity:
0007110
Arg of perigee: 188
8347 deg
Mean anomaly: 171
2682 deg
Mean motion: 15
53590245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2744
Checksum: 326
Coasting Arc #9 (Orbit 2759)
---------------------------------------
Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5306565
89 A = 6786235
33 meter
Y = -2573503
10 meter E =
0013120
Z = 3340019
66 I = 51
94308
XDOT = -31
687096 Wp = 122
98560
YDOT = -6057
123184 meter/sec RA = 52
19096 deg
ZDOT = -4710
992882 TA = 18
27015
MA = 18
22306
Ha = 222
887 n
mi
Hp = 215
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17409993
08 X = -5293618
55
Y = -8443251
63 feet Y = -2632772
15 meter
Z = 10958069
76 Z = 3314272
85
XDOT = -103
960288 XDOT = 58
931889
YDOT = -19872
451390 feet/sec YDOT = -6056
971040 meter/sec
ZDOT = -15456
013392 ZDOT = -4710
926461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11467280
49 X = 3495227
09
Y = -15663526
06 feet Y = -4774242
74 meter
Z = 10845786
24 Z = 3305795
65
XDOT = 18403
975546 XDOT = 5609
531746
YDOT = 2757
785273 feet/sec YDOT = 840
572951 meter/sec
ZDOT = -15454
566599 ZDOT = -4710
551899
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 16314
62586119
00016717 00000-0 10270-3 0 9088
2 25544 51
6424 52
7013 0006998 193
7326 166
3637 15
53597756 27605
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
62586119 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 52
7013 deg
Eccentricity:
0006998
Arg of perigee: 193
7326 deg
Mean anomaly: 166
3637 deg
Mean motion: 15
53597756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2760
Checksum: 337
Coasting Arc #10 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5356237
25 A = 6787725
17 meter
Y = -3078053
96 meter E =
0014656
Z = 2789888
47 I = 51
93999
XDOT = 566
315850 Wp = 127
51106
YDOT = -5661
352732 meter/sec RA = 50
59207 deg
ZDOT = -5149
086913 TA = 20
97309
MA = 20
91304
Ha = 222
797 n
mi
Hp = 215
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17572956
87 X = -5334971
88
Y = -10098602
24 feet Y = -3137831
98 meter
Z = 9153177
40 Z = 2763920
58
XDOT = 1857
991634 XDOT = 654
592909
YDOT = -18573
991903 feet/sec YDOT = -5654
526447 meter/sec
ZDOT = -16893
329766 ZDOT = -5146
121182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19743863
76 X = -6017929
67
Y = -4798858
00 feet Y = -1462691
92 meter
Z = 9040024
48 Z = 2755399
46
XDOT = -3623
332825 XDOT = -1104
391845
YDOT = -16950
618369 feet/sec YDOT = -5166
548479 meter/sec
ZDOT = -16879
256843 ZDOT = -5144
797486
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 16314
94748771
00016717 00000-0 10270-3 0 9098
2 25544 51
6409 51
1001 0006673 194
3222 165
7742 15
53573237 27653
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
94748771 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 51
1001 deg
Eccentricity:
0006673
Arg of perigee: 194
3222 deg
Mean anomaly: 165
7742 deg
Mean motion: 15
53573237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 315
Coasting Arc #11 (Orbit 2779)
---------------------------------------
Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5361302
19 A = 6790135
51 meter
Y = 3929868
44 meter E =
0003356
Z = -1385794
91 I = 51
92729
XDOT = -1875
782222 Wp = 78
54098
YDOT = 4608
940571 meter/sec RA = 45
64034 deg
ZDOT = 5825
767724 TA = 266
43374
MA = 266
47212
Ha = 222
527 n
mi
Hp = 215
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17589574
12 X = 5323690
66
Y = 12893269
16 feet Y = 3989611
75 meter
Z = -4546571
24 Z = -1359842
09
XDOT = -6154
141147 XDOT = -1955
480787
YDOT = 15121
196098 feet/sec YDOT = 4587
518980 meter/sec
ZDOT = 19113
411168 ZDOT = 5816
461656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20633838
34 X = 6289193
92
Y = 7133597
20 feet Y = 2174320
43 meter
Z = -4433658
07 Z = -1351378
98
XDOT = -1026
517858 XDOT = -312
882643
YDOT = 14796
339490 feet/sec YDOT = 4509
924277 meter/sec
ZDOT = 19071
763612 ZDOT = 5813
073549
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 16315
91235624
00016717 00000-0 10270-3 0 9106
2 25544 51
6412 46
2943 0006589 198
0885 162
0034 15
53582870 27803
Satellite: ISS
Catalog Number: 25544
Epoch time: 16315
91235624 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 46
2943 deg
Eccentricity:
0006589
Arg of perigee: 198
0885 deg
Mean anomaly: 162
0034 deg
Mean motion: 15
53582870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2780
Checksum: 313
Coasting Arc #12 (Orbit 2795)
---------------------------------------
Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5057585
39 A = 6790890
61 meter
Y = -4514374
65 meter E =
0015594
Z = -160020
06 I = 51
90720
XDOT = 3255
570749 Wp = 158
21799
YDOT = -3440
523879 meter/sec RA = 40
69171 deg
ZDOT = -6035
610365 TA = 23
50022
MA = 23
42904
Ha = 222
389 n
mi
Hp = 216
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16593127
93 X = -5005951
28
Y = -14810940
46 feet Y = -4570643
27 meter
Z = -525000
21 Z = -184463
51
XDOT = 10681
006395 XDOT = 3323
120694
YDOT = -11287
808001 feet/sec YDOT = -3403
740475 meter/sec
ZDOT = -19801
871275 ZDOT = -6019
631016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20371421
54 X = -6209209
29
Y = -8920665
75 feet Y = -2719018
92 meter
Z = -631176
73 Z = -192382
67
XDOT = 6113
891480 XDOT = 1863
514123
YDOT = -12604
721545 feet/sec YDOT = -3841
919127 meter/sec
ZDOT = -19731
218801 ZDOT = -6014
075491
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 16316
94154271
00016717 00000-0 10270-3 0 9119
2 25544 51
6418 41
1683 0006542 201
9200 158
1674 15
53587669 27962
Satellite: ISS
Catalog Number: 25544
Epoch time: 16316
94154271 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 41
1683 deg
Eccentricity:
0006542
Arg of perigee: 201
9200 deg
Mean anomaly: 158
1674 deg
Mean motion: 15
53587669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2796
Checksum: 315
Coasting Arc #13 (Orbit 2811)
---------------------------------------
Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4467921
62 A = 6789613
63 meter
Y = 4829151
06 meter E =
0009664
Z = 1669176
03 I = 51
87821
XDOT = -4574
613550 Wp = 88
80552
YDOT = 2243
509066 meter/sec RA = 35
74116 deg
ZDOT = 5725
801836 TA = 289
41041
MA = 289
51483
Ha = 222
208 n
mi
Hp = 216
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14658535
48 X = 4405480
38
Y = 15843671
47 feet Y = 4878765
28 meter
Z = 5476299
31 Z = 1690728
86
XDOT = -15008
574640 XDOT = -4627
175282
YDOT = 7360
594047 feet/sec YDOT = 2192
058936 meter/sec
ZDOT = 18785
439094 ZDOT = 5703
451171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19001427
75 X = 5791635
18
Y = 10188629
59 feet Y = 3105494
30 meter
Z = 5569740
82 Z = 1697657
00
XDOT = -11145
983282 XDOT = -3397
295704
YDOT = 10521
238284 feet/sec YDOT = 3206
873429 meter/sec
ZDOT = 18687
116136 ZDOT = 5695
832998
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 16317
97072139
00016717 00000-0 10270-3 0 9126
2 25544 51
6418 36
0427 0006578 206
3361 153
7458 15
53611089 28121
Satellite: ISS
Catalog Number: 25544
Epoch time: 16317
97072139 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 36
0427 deg
Eccentricity:
0006578
Arg of perigee: 206
3361 deg
Mean anomaly: 153
7458 deg
Mean motion: 15
53611089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2812
Checksum: 311
Coasting Arc #14 (Orbit 2826)
---------------------------------------
Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3535111
57 A = 6786723
24 meter
Y = -4910529
94 meter E =
0006889
Z = -3066633
68 I = 51
84339
XDOT = 5768
852557 Wp = 170
31288
YDOT = -1076
410502 meter/sec RA = 30
78323 deg
ZDOT = -4934
732471 TA = 44
78160
MA = 44
72601
Ha = 221
964 n
mi
Hp = 216
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11598135
09 X = -3465041
22
Y = -16110662
54 feet Y = -4949670
16 meter
Z = -10061134
12 Z = -3083636
65
XDOT = 18926
681618 XDOT = 5804
431995
YDOT = -3531
530518 feet/sec YDOT = -1011
700398 meter/sec
ZDOT = -16190
067162 ZDOT = -4906
621594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16363489
42 X = -4987591
58
Y = -11172389
05 feet Y = -3405344
18 meter
Z = -10134620
94 Z = -3089032
46
XDOT = 15846
505584 XDOT = 4830
014902
YDOT = -8659
314305 feet/sec YDOT = -2639
359000 meter/sec
ZDOT = -16066
750059 ZDOT = -4897
145418
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 16318
93556863
00016717 00000-0 10270-3 0 9135
2 25544 51
6431 31
2369 0006427 210
2646 149
8136 15
53632719 28279
Satellite: ISS
Catalog Number: 25544
Epoch time: 16318
93556863 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 31
2369 deg
Eccentricity:
0006427
Arg of perigee: 210
2646 deg
Mean anomaly: 149
8136 deg
Mean motion: 15
53632719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2827
Checksum: 318
Coasting Arc #15 (Orbit 2842)
---------------------------------------
Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2353038
22 A = 6783302
89 meter
Y = 4794044
35 meter E =
0010219
Z = 4182444
74 I = 51
80325
XDOT = -6696
662072 Wp = 141
31014
YDOT = 21
159691 meter/sec RA = 25
81604 deg
ZDOT = 3730
576001 TA = 270
37042
MA = 270
48751
Ha = 221
849 n
mi
Hp = 216
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7719941
65 X = 2278938
02
Y = 15728491
97 feet Y = 4819943
19 meter
Z = 13721931
55 Z = 4193695
66
XDOT = -21970
676089 XDOT = -6714
523004
YDOT = 69
421559 feet/sec YDOT = -53
826837 meter/sec
ZDOT = 12239
422575 ZDOT = 3698
001006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12774943
22 X = 3893802
69
Y = 11935478
39 feet Y = 3637933
81 meter
Z = 13770241
31 Z = 4197169
55
XDOT = -19680
110133 XDOT = -5998
497568
YDOT = 7060
038275 feet/sec YDOT = 2151
899666 meter/sec
ZDOT = 12096
769346 ZDOT = 3687
095297
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 16319
96473141
00016717 00000-0 10270-3 0 9147
2 25544 51
6426 26
1112 0006406 213
5597 146
5150 15
53635042 28430
Satellite: ISS
Catalog Number: 25544
Epoch time: 16319
96473141 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 26
1112 deg
Eccentricity:
0006406
Arg of perigee: 213
5597 deg
Mean anomaly: 146
5150 deg
Mean motion: 15
53635042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2843
Checksum: 291
Coasting Arc #16 (Orbit 2857)
---------------------------------------
Vector Time (GMT): 2016/320/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -918806
89 A = 6780231
78 meter
Y = -4534132
81 meter E =
0008321
Z = -4963230
02 I = 51
76413
XDOT = 7282
821495 Wp = 100
93481
YDOT = 921
607685 meter/sec RA = 20
83799 deg
ZDOT = -2194
806388 TA = 147
70209
MA = 147
65111
Ha = 221
671 n
mi
Hp = 216
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3014458
31 X = -843926
97
Y = -14875763
80 feet Y = -4543988
61 meter
Z = -16283563
07 Z = -4967511
79
XDOT = 23893
771310 XDOT = 7282
636241
YDOT = 3023
647262 feet/sec YDOT = 1003
048149 meter/sec
ZDOT = -7200
808359 ZDOT = -2159
427825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8281748
63 X = -2524276
98
Y = -12696723
07 feet Y = -3869961
19 meter
Z = -16301398
61 Z = -4968666
30
XDOT = 22397
668999 XDOT = 6826
809511
YDOT = -5582
545698 feet/sec YDOT = -1701
559929 meter/sec
ZDOT = -7046
070553 ZDOT = -2147
642305
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 16320
92956529
00016717 00000-0 10270-3 0 9152
2 25544 51
6429 21
3055 0006341 217
5369 142
5341 15
53662308 28584
Satellite: ISS
Catalog Number: 25544
Epoch time: 16320
92956529 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 21
3055 deg
Eccentricity:
0006341
Arg of perigee: 217
5369 deg
Mean anomaly: 142
5341 deg
Mean motion: 15
53662308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2858
Checksum: 310
Coasting Arc #17 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2016/321/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -614810
84 A = 6778688
35 meter
Y = 4176673
89 meter E =
0005974
Z = 5305549
39 I = 51
72861
XDOT = -7455
417253 Wp = 197
68244
YDOT = -1719
718982 meter/sec RA = 15
85240 deg
ZDOT = 484
455270 TA = 247
66919
MA = 247
73253
Ha = 221
463 n
mi
Hp = 216
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2017095
93 X = -687242
33
Y = 13702998
31 feet Y = 4169393
37 meter
Z = 17406658
11 Z = 5302387
04
XDOT = -24460
030357 XDOT = -7437
986128
YDOT = -5642
122643 feet/sec YDOT = -1802
993025 meter/sec
ZDOT = 1589
420176 ZDOT = 448
280286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3403136
29 X = 1037275
94
Y = 13445105
83 feet Y = 4098068
26 meter
Z = 17391963
03 Z = 5301070
33
XDOT = -23745
762876 XDOT = -7237
708525
YDOT = 4135
828218 feet/sec YDOT = 1260
600441 meter/sec
ZDOT = 1431
359038 ZDOT = 436
278235
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 16321
95871267
00016717 00000-0 10270-3 0 9162
2 25544 51
6429 16
1795 0006508 222
6414 137
4234 15
53690397 28741
Satellite: ISS
Catalog Number: 25544
Epoch time: 16321
95871267 = yrday
fracday
Element set: 916
Inclination: 51
6429 deg
RA of node: 16
1795 deg
Eccentricity:
0006508
Arg of perigee: 222
6414 deg
Mean anomaly: 137
4234 deg
Mean motion: 15
53690397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 327
Coasting Arc #18 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/322/07:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4623497
38 A = 6782861
38 meter
Y = 2389102
30 meter E =
0005445
Z = 4344371
93 I = 51
72921
XDOT = -5421
207587 Wp = 113
87772
YDOT = -4164
338124 meter/sec RA = 13
86412 deg
ZDOT = -3478
134650 TA = 11
41075
MA = 11
39841
Ha = 221
827 n
mi
Hp = 216
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15168954
67 X = -4670972
74
Y = 7838262
16 feet Y = 2337133
56 meter
Z = 14253188
75 Z = 4321796
59
XDOT = -17786
114131 XDOT = -5357
342417
YDOT = -13662
526652 feet/sec YDOT = -4224
604417 meter/sec
ZDOT = -11411
202919 ZDOT = -3504
315068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16774754
80 X = 5112945
26
Y = -3600716
65 feet Y = -1097498
43 meter
Z = 14153846
47 Z = 4314092
40
XDOT = 13286
095303 XDOT = 4049
601848
YDOT = 16576
600428 feet/sec YDOT = 5052
547811 meter/sec
ZDOT = -11525
000348 ZDOT = -3512
820106
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 16322
34464284
00016717 00000-0 10270-3 0 9174
2 25544 51
6425 14
2520 0006774 219
7688 140
2969 15
53636872 28809
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
34464284 = yrday
fracday
Element set: 917
Inclination: 51
6425 deg
RA of node: 14
2520 deg
Eccentricity:
0006774
Arg of perigee: 219
7688 deg
Mean anomaly: 140
2969 deg
Mean motion: 15
53636872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 327
- 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