[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 13th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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
346/16:46:55
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
5
348/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
5
348/05:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
349/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
351/07:21:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
9
000/00:00:00
000 0
0 0
0 215
7
353/08:42:47
000 0
0 0
0 0
0
N/A 0
0 0
0 220
0
000/00:00:00
000 0
0 0
0 215
7
Coasting Arc #1 (Orbit 931)
---------------------------------------
Vector Time (GMT): 2017/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5286256
96 A = 6784773
25 meter
Y = -2759533
49 meter E =
0002623
Z = -3239758
55 I = 51
34069
XDOT = 240
986662 Wp = 120
53580
YDOT = -6019
622041 meter/sec RA = 233
32704 deg
ZDOT = 4735
690106 TA = 201
77697
MA = 201
78812
Ha = 220
312 n
mi
Hp = 215
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17343362
73 X = -5239269
00
Y = -9053587
57 feet Y = -2818385
18 meter
Z = -10629129
10 Z = -3265323
65
XDOT = 790
638655 XDOT = 285
278012
YDOT = -19749
416146 feet/sec YDOT = -6016
679696 meter/sec
ZDOT = 15537
041031 ZDOT = 4736
968099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12044537
62 X = 3671175
07
Y = -15338593
21 feet Y = -4675203
21 meter
Z = -10742194
18 Z = -3274220
79
XDOT = 18175
146534 XDOT = 5539
784663
YDOT = 3389
716319 feet/sec YDOT = 1033
185534 meter/sec
ZDOT = 15543
587567 ZDOT = 4737
685490
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 17345
50679192
00016717 00000-0 10270-3 0 9006
2 25544 51
6415 234
3641 0002987 231
6610 128
4275 15
54132487 9325
Satellite: ISS
Catalog Number: 25544
Epoch time: 17345
50679192 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 234
3641 deg
Eccentricity:
0002987
Arg of perigee: 231
6610 deg
Mean anomaly: 128
4275 deg
Mean motion: 15
54132487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 932
Checksum: 305
Coasting Arc #2 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2017/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5291584
94 A = 6788093
62 meter
Y = 3874167
89 meter E =
0012851
Z = 1723427
80 I = 51
37209
XDOT = -1719
065579 Wp = 126
82869
YDOT = 4877
931006 meter/sec RA = 228
33113 deg
ZDOT = -5665
350906 TA = 34
18521
MA = 34
10253
Ha = 220
298 n
mi
Hp = 215
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17360842
98 X = 5239498
04
Y = 12710524
57 feet Y = 3933050
70 meter
Z = 5654290
67 Z = 1749006
52
XDOT = -5639
978935 XDOT = -1745
964446
YDOT = 16003
710650 feet/sec YDOT = 4858
557082 meter/sec
ZDOT = -18587
109271 ZDOT = -5673
766781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15393644
70 X = -4691982
90
Y = 14990050
54 feet Y = 4568967
40 meter
Z = 5767269
27 Z = 1757863
67
XDOT = -13780
097381 XDOT = -4200
173682
YDOT = -6958
330416 feet/sec YDOT = -2120
899111 meter/sec
ZDOT = -18625
166111 ZDOT = -5676
950631
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 17346
53562724
00016717 00000-0 10270-3 0 9013
2 25544 51
6418 229
2358 0002919 232
7995 127
2891 15
54103759 9487
Satellite: ISS
Catalog Number: 25544
Epoch time: 17346
53562724 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 229
2358 deg
Eccentricity:
0002919
Arg of perigee: 232
7995 deg
Mean anomaly: 127
2891 deg
Mean motion: 15
54103759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 334
Coasting Arc #3 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2017/346/16:46:55
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3519179
90 A = 6788295
74 meter
Y = 5599747
21 meter E =
0008773
Z = -1507530
89 I = 51
37367
XDOT = -4851
515381 Wp = 161
88118
YDOT = 1507
184052 meter/sec RA = 227
35856 deg
ZDOT = -5744
114435 TA = 34
64606
MA = 34
58894
Ha = 220
270 n
mi
Hp = 215
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11545865
82 X = 3463623
38
Y = 18371874
06 feet Y = 5638790
52 meter
Z = -4945967
49 Z = -1490570
36
XDOT = -15917
045212 XDOT = -4840
106229
YDOT = 4944
829567 feet/sec YDOT = 1452
995139 meter/sec
ZDOT = -18845
519800 ZDOT = -5767
654005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1762017
84 X = 537063
04
Y = 21643919
90 feet Y = 6597066
78 meter
Z = -4871487
79 Z = -1484829
48
XDOT = -14709
204157 XDOT = -4483
365427
YDOT = -3054
846441 feet/sec YDOT = -931
117195 meter/sec
ZDOT = -18950
222567 ZDOT = -5776
027838
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 17346
72853156
00016717 00000-0 10270-3 0 9027
2 25544 51
6379 228
2691 0002881 233
3882 126
7006 15
54161857 9511
Satellite: ISS
Catalog Number: 25544
Epoch time: 17346
72853156 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 228
2691 deg
Eccentricity:
0002881
Arg of perigee: 233
3882 deg
Mean anomaly: 126
7006 deg
Mean motion: 15
54161857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 951
Checksum: 322
Coasting Arc #4 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2017/347/16:46:55
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2470082
71 A = 6785421
18 meter
Y = -5536932
48 meter E =
0010578
Z = 3038189
80 I = 51
38556
XDOT = 5893
554109 Wp = 92
47164
YDOT = 71
338200 meter/sec RA = 222
36480 deg
ZDOT = 4906
276114 TA = 302
51369
MA = 302
61586
Ha = 220
295 n
mi
Hp = 215
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8103945
89 X = -2422741
84
Y = -18165788
97 feet Y = -5564290
10 meter
Z = 9967814
30 Z = 3026305
46
XDOT = 19335
807444 XDOT = 5868
485850
YDOT = 234
049214 feet/sec YDOT = 137
103510 meter/sec
ZDOT = 16096
706410 ZDOT = 4934
844570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 822060
28 X = 250563
97
Y = -19900435
95 feet Y = -6065652
88 meter
Z = 9915846
70 Z = 3022350
07
XDOT = 15640
591632 XDOT = 4767
252329
YDOT = 8754
906727 feet/sec YDOT = 2668
495570 meter/sec
ZDOT = 16223
516828 ZDOT = 4944
927929
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 17347
75736400
00016717 00000-0 10270-3 0 9034
2 25544 51
6367 223
1400 0003099 232
6274 127
4596 15
54141234 9675
Satellite: ISS
Catalog Number: 25544
Epoch time: 17347
75736400 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 223
1400 deg
Eccentricity:
0003099
Arg of perigee: 232
6274 deg
Mean anomaly: 127
4596 deg
Mean motion: 15
54141234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 303
Coasting Arc #5 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 919742
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2643991
67 A = 6777399
55 meter
Y = 3311610
80 meter E =
0012448
Z = -5299918
35 I = 51
37119
XDOT = -5886
244194 Wp = 96
29358
YDOT = -4899
424172 meter/sec RA = 220
52844 deg
ZDOT = -126
465286 TA = 172
50469
MA = 172
48607
Ha = 220
244 n
mi
Hp = 215
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8674513
35 X = -2655081
82
Y = 10864864
83 feet Y = 3281982
19 meter
Z = -17388183
56 Z = -5312788
90
XDOT = -19311
824784 XDOT = -5830
405727
YDOT = -16074
226285 feet/sec YDOT = -4964
935959 meter/sec
ZDOT = -414
912355 ZDOT = -154
923803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12665298
57 X = 3860383
01
Y = 5556614
74 feet Y = 1693656
17 meter
Z = -17445791
52 Z = -5317477
25
XDOT = -10303
341039 XDOT = -3140
458349
YDOT = 21803
828158 feet/sec YDOT = 6645
806822 meter/sec
ZDOT = -540
553056 ZDOT = -164
760571
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 17348
07887391
00016717 00000-0 10270-3 0 9047
2 25544 51
6404 221
5409 0002959 236
9186 123
1683 15
54116465 9725
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
07887391 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 221
5409 deg
Eccentricity:
0002959
Arg of perigee: 236
9186 deg
Mean anomaly: 123
1683 deg
Mean motion: 15
54116465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 326
Coasting Arc #6 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2017/348/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -101617
32 A = 6780059
24 meter
Y = -4924778
36 meter E =
0006878
Z = 4657180
24 I = 51
38115
XDOT = 6641
311573 Wp = 136
83785
YDOT = 2565
246378 meter/sec RA = 219
76970 deg
ZDOT = 2850
129496 TA = 284
72076
MA = 284
79698
Ha = 220
118 n
mi
Hp = 215
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -333390
15 X = -69162
10
Y = -16157409
33 feet Y = -4925733
55 meter
Z = 15279462
73 Z = 4656765
12
XDOT = 21789
079963 XDOT = 6598
288031
YDOT = 8416
162657 feet/sec YDOT = 2639
273323 meter/sec
ZDOT = 9350
818555 ZDOT = 2882
286924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4896159
44 X = -1492349
40
Y = 15402453
64 feet Y = 4694667
87 meter
Z = 15278319
64 Z = 4656831
83
XDOT = -16634
484316 XDOT = -5070
190820
YDOT = -14728
667754 feet/sec YDOT = -4489
297931 meter/sec
ZDOT = 9493
214698 ZDOT = 2893
531840
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 17348
27177885
00016717 00000-0 10270-3 0 9050
2 25544 51
6374 220
5800 0003005 241
3071 118
7780 15
54152247 9750
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
27177885 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 220
5800 deg
Eccentricity:
0003005
Arg of perigee: 241
3071 deg
Mean anomaly: 118
7780 deg
Mean motion: 15
54152247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 304
Coasting Arc #7 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2017/349/05:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 904510
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1435701
94 A = 6777726
03 meter
Y = 4082267
20 meter E =
0011599
Z = -5226608
78 I = 51
39948
XDOT = -6663
684919 Wp = 86
41379
YDOT = -3639
182857 meter/sec RA = 214
75512 deg
ZDOT = -1013
184431 TA = 173
84920
MA = 173
83495
Ha = 220
129 n
mi
Hp = 215
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4710308
22 X = -1455855
70
Y = 13393265
10 feet Y = 4066099
93 meter
Z = -17147666
60 Z = -5233631
67
XDOT = -21862
483330 XDOT = -6617
573738
YDOT = -11939
576301 feet/sec YDOT = -3713
442832 meter/sec
ZDOT = -3324
095901 ZDOT = -1045
443166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8547626
92 X = 2605316
68
Y = -11287800
89 feet Y = -3440521
71 meter
Z = -17179425
15 Z = -5236288
79
XDOT = 16199
210842 XDOT = 4937
519465
YDOT = 17536
894957 feet/sec YDOT = 5345
245583 meter/sec
ZDOT = -3466
808693 ZDOT = -1056
683290
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 17349
23630664
00016717 00000-0 10270-3 0 9067
2 25544 51
6379 215
7712 0002853 244
8507 115
2350 15
54128220 9901
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
23630664 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 215
7712 deg
Eccentricity:
0002853
Arg of perigee: 244
8507 deg
Mean anomaly: 115
2350 deg
Mean motion: 15
54128220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 302
Coasting Arc #8 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2017/349/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6082098
58 A = 6788375
79 meter
Y = 2598492
12 meter E =
0012314
Z = 1498218
72 I = 51
44502
XDOT = -722
418883 Wp = 128
88730
YDOT = 5021
895632 meter/sec RA = 213
53520 deg
ZDOT = -5752
900028 TA = 34
70251
MA = 34
62224
Ha = 220
090 n
mi
Hp = 215
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19954391
67 X = 6045311
83
Y = 8525236
62 feet Y = 2666300
49 meter
Z = 4915415
75 Z = 1527674
83
XDOT = -2370
140693 XDOT = -750
576340
YDOT = 16476
035537 feet/sec YDOT = 5013
660096 meter/sec
ZDOT = -18874
343925 ZDOT = -5756
477318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15254099
13 X = -4649449
41
Y = 15390604
65 feet Y = 4691056
30 meter
Z = 5045836
55 Z = 1537970
98
XDOT = -13371
888047 XDOT = -4075
751477
YDOT = -7034
381787 feet/sec YDOT = -2144
079569 meter/sec
ZDOT = -18890
936617 ZDOT = -5757
957481
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 17349
49351412
00016717 00000-0 10270-3 0 9077
2 25544 51
6414 214
4914 0002920 245
9089 114
1758 15
54112354 9948
Satellite: ISS
Catalog Number: 25544
Epoch time: 17349
49351412 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 214
4914 deg
Eccentricity:
0002920
Arg of perigee: 245
9089 deg
Mean anomaly: 114
1758 deg
Mean motion: 15
54112354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 309
Coasting Arc #9 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2017/350/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5880997
68 A = 6789230
50 meter
Y = -3376079
09 meter E =
0009826
Z = 194304
03 I = 51
47551
XDOT = 2531
807121 Wp = 39
61734
YDOT = -4056
060441 meter/sec RA = 208
55151 deg
ZDOT = 5995
054543 TA = 322
48075
MA = 322
54929
Ha = 219
935 n
mi
Hp = 215
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19294611
80 X = -5843752
21
Y = -11076374
97 feet Y = -3441636
19 meter
Z = 637480
43 Z = 165825
86
XDOT = 8306
453810 XDOT = 2547
853641
YDOT = -13307
284910 feet/sec YDOT = -4027
658916 meter/sec
ZDOT = 19668
814119 ZDOT = 6007
391952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17155648
09 X = 5229041
54
Y = -14170272
49 feet Y = -4319099
06 meter
Z = 511492
50 Z = 155902
91
XDOT = 8546
663944 XDOT = 2605
023170
YDOT = 11082
861311 feet/sec YDOT = 3378
056128 meter/sec
ZDOT = 19724
171291 ZDOT = 6011
927410
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 17350
52233701
00016717 00000-0 10270-3 0 9084
2 25544 51
6408 209
3619 0002979 253
8255 106
2570 15
54159278 10103
Satellite: ISS
Catalog Number: 25544
Epoch time: 17350
52233701 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 209
3619 deg
Eccentricity:
0002979
Arg of perigee: 253
8255 deg
Mean anomaly: 106
2570 deg
Mean motion: 15
54159278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1010
Checksum: 301
Coasting Arc #10 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2017/351/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -555052
08 A = 6778776
68 meter
Y = -4586499
24 meter E =
0004823
Z = 4959909
19 I = 51
46317
XDOT = 7232
755934 Wp = 150
17244
YDOT = 1419
601312 meter/sec RA = 204
32967 deg
ZDOT = 2117
136818 TA = 279
13307
MA = 279
18763
Ha = 219
918 n
mi
Hp = 215
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1821037
00 X = -527816
31
Y = -15047569
69 feet Y = -4592554
47 meter
Z = 16272667
93 Z = 4957278
55
XDOT = 23729
514219 XDOT = 7206
059944
YDOT = 4657
484620 feet/sec YDOT = 1500
333435 meter/sec
ZDOT = 6945
986935 ZDOT = 2152
206833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5877757
09 X = 1791540
36
Y = 13984158
31 feet Y = 4262371
45 meter
Z = 16261627
81 Z = 4956544
16
XDOT = -23047
178303 XDOT = -7024
779947
YDOT = 1409
928582 feet/sec YDOT = 429
746232 meter/sec
ZDOT = 7101
542572 ZDOT = 2164
550176
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 17351
35825686
00016717 00000-0 10270-3 0 9096
2 25544 51
6386 205
1945 0002990 255
4180 104
6641 15
54172125 10233
Satellite: ISS
Catalog Number: 25544
Epoch time: 17351
35825686 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 205
1945 deg
Eccentricity:
0002990
Arg of perigee: 255
4180 deg
Mean anomaly: 104
6641 deg
Mean motion: 15
54172125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1023
Checksum: 303
Coasting Arc #11 (Orbit 1037)
---------------------------------------
Vector Time (GMT): 2017/352/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1173899
15 A = 6777297
12 meter
Y = 4062902
42 meter E =
0011990
Z = -5306286
06 I = 51
48894
XDOT = -7279
166999 Wp = 90
22734
YDOT = -2375
578113 meter/sec RA = 199
31898 deg
ZDOT = -209
026534 TA = 177
77678
MA = 177
77145
Ha = 219
923 n
mi
Hp = 215
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3851375
16 X = -1193468
96
Y = 13329732
33 feet Y = 4049666
27 meter
Z = -17409075
00 Z = -5312035
58
XDOT = -23881
781494 XDOT = -7251
046293
YDOT = -7793
891446 feet/sec YDOT = -2456
821476 meter/sec
ZDOT = -685
782592 ZDOT = -244
318549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -197997
64 X = -60349
68
Y = -13840736
62 feet Y = -4218656
52 meter
Z = -17435181
50 Z = -5314243
32
XDOT = 24097
596113 XDOT = 7344
947295
YDOT = 714
331022 feet/sec YDOT = 217
728096 meter/sec
ZDOT = -842
215978 ZDOT = -256
707430
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 17352
32277846
00016717 00000-0 10270-3 0 9105
2 25544 51
6391 200
3858 0002882 260
6811 99
4015 15
54156139 10387
Satellite: ISS
Catalog Number: 25544
Epoch time: 17352
32277846 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 200
3858 deg
Eccentricity:
0002882
Arg of perigee: 260
6811 deg
Mean anomaly: 99
4015 deg
Mean motion: 15
54156139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1038
Checksum: 306
Coasting Arc #12 (Orbit 1053)
---------------------------------------
Vector Time (GMT): 2017/353/07:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 925679
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2884235
03 A = 6778145
69 meter
Y = -3433187
16 meter E =
0003041
Z = 5082673
73 I = 51
52320
XDOT = 6780
352913 Wp = 25
10817
YDOT = 3142
161216 meter/sec RA = 194
31078 deg
ZDOT = -1722
099056 TA = 81
57798
MA = 81
54351
Ha = 219
759 n
mi
Hp = 215
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9462713
34 X = 2897722
37
Y = -11263737
41 feet Y = -3400858
86 meter
Z = 16675438
74 Z = 5096716
80
XDOT = 22245
252339 XDOT = 6753
077599
YDOT = 10308
927875 feet/sec YDOT = 3217
831453 meter/sec
ZDOT = -5649
931285 ZDOT = -1689
228100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5541135
59 X = -1688938
13
Y = 13550275
01 feet Y = 4130123
82 meter
Z = 16738304
72 Z = 5101835
28
XDOT = -23360
559139 XDOT = -7120
298425
YDOT = -2741
088718 feet/sec YDOT = -835
483841 meter/sec
ZDOT = -5504
333607 ZDOT = -1677
720883
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 17353
35159636
00016717 00000-0 10270-3 0 9116
2 25544 51
6390 195
2574 0002934 266
8338 93
2479 15
54175186 10540
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
35159636 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 195
2574 deg
Eccentricity:
0002934
Arg of perigee: 266
8338 deg
Mean anomaly: 93
2479 deg
Mean motion: 15
54175186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1054
Checksum: 330
Coasting Arc #13 (Orbit 1054)
---------------------------------------
Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1895313
97 A = 6779573
03 meter
Y = -4401456
50 meter E =
0005327
Z = 4793967
52 I = 51
53064
XDOT = 7218
278106 Wp = 136
23014
YDOT = -299
757833 meter/sec RA = 194
06085 deg
ZDOT = 2573
078731 TA = 288
36647
MA = 288
42439
Ha = 219
977 n
mi
Hp = 215
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6218221
69 X = -1869241
56
Y = -14440474
08 feet Y = -4422505
98 meter
Z = 15728239
89 Z = 4784823
49
XDOT = 23682
014785 XDOT = 7208
594860
YDOT = -983
457457 feet/sec YDOT = -219
092557 meter/sec
ZDOT = 8441
859354 ZDOT = 2608
119308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13866973
62 X = 4226653
56
Y = 7493841
63 feet Y = 2284122
93 meter
Z = 15688227
52 Z = 4781771
75
XDOT = -17474
423137 XDOT = -5326
204172
YDOT = 14298
914665 feet/sec YDOT = 4358
309190 meter/sec
ZDOT = 8597
575828 ZDOT = 2620
541112
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 17353
41589798
00016717 00000-0 10270-3 0 9120
2 25544 51
6403 194
9366 0002852 265
3771 94
7055 15
54146761 10558
Satellite: ISS
Catalog Number: 25544
Epoch time: 17353
41589798 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 194
9366 deg
Eccentricity:
0002852
Arg of perigee: 265
3771 deg
Mean anomaly: 94
7055 deg
Mean motion: 15
54146761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1055
Checksum: 332
Coasting Arc #14 (Orbit 1069)
---------------------------------------
Vector Time (GMT): 2017/354/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 120357
29 A = 6777406
37 meter
Y = 4262253
76 meter E =
0011667
Z = -5278179
80 I = 51
55511
XDOT = -7600
380656 Wp = 83
08593
YDOT = -650
156556 meter/sec RA = 189
05672 deg
ZDOT = -698
280470 TA = 180
22988
MA = 180
23042
Ha = 219
846 n
mi
Hp = 215
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 394873
00 X = 98325
38
Y = 13983772
18 feet Y = 4263477
09 meter
Z = -17316862
87 Z = -5277648
18
XDOT = -24935
632074 XDOT = -7589
153667
YDOT = -2133
059568 feet/sec YDOT = -735
086355 meter/sec
ZDOT = -2290
946425 ZDOT = -735
173420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9186323
36 X = -2799991
36
Y = -10553419
48 feet Y = -3216682
26 meter
Z = -17315090
21 Z = -5277639
50
XDOT = 19950
637169 XDOT = 6080
954209
YDOT = -13338
379659 feet/sec YDOT = -4065
538120 meter/sec
ZDOT = -2454
787490 ZDOT = -748
219227
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 17354
38041283
00016717 00000-0 10270-3 0 9130
2 25544 51
6397 190
1287 0002942 270
6381 89
4426 15
54174714 10705
Satellite: ISS
Catalog Number: 25544
Epoch time: 17354
38041283 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 190
1287 deg
Eccentricity:
0002942
Arg of perigee: 270
6381 deg
Mean anomaly: 89
4426 deg
Mean motion: 15
54174714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1070
Checksum: 309
Coasting Arc #15 (Orbit 1085)
---------------------------------------
Vector Time (GMT): 2017/355/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1697629
41 A = 6777633
44 meter
Y = -4008942
00 meter E =
0002456
Z = 5194732
45 I = 51
58924
XDOT = 7412
513021 Wp = 5
65405
YDOT = 1517
689981 meter/sec RA = 184
05217 deg
ZDOT = -1248
703653 TA = 96
35379
MA = 96
32582
Ha = 219
696 n
mi
Hp = 215
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5569650
29 X = 1717099
02
Y = -13152696
85 feet Y = -3989849
62 meter
Z = 17043085
46 Z = 5203025
82
XDOT = 24319
268442 XDOT = 7401
056440
YDOT = 4979
297837 feet/sec YDOT = 1600
517841 meter/sec
ZDOT = -4096
796763 ZDOT = -1212
723874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4258584
14 X = 1298016
44
Y = 13586846
10 feet Y = 4141270
69 meter
Z = 17080493
99 Z = 5206134
57
XDOT = -20871
952824 XDOT = -6361
771221
YDOT = 11501
511309 feet/sec YDOT = 3505
660647 meter/sec
ZDOT = -3937
106776 ZDOT = -1200
030145
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 17355
40922705
00016717 00000-0 10270-3 0 9142
2 25544 51
6402 185
0000 0003122 273
6576 86
4220 15
54194508 10867
Satellite: ISS
Catalog Number: 25544
Epoch time: 17355
40922705 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 185
0000 deg
Eccentricity:
0003122
Arg of perigee: 273
6576 deg
Mean anomaly: 86
4220 deg
Mean motion: 15
54194508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1086
Checksum: 283
Coasting Arc #16 (Orbit 1100)
---------------------------------------
Vector Time (GMT): 2017/356/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3398944
79 A = 6780241
61 meter
Y = 3679822
34 meter E =
0007115
Z = -4576342
18 I = 51
63082
XDOT = -6630
242488 Wp = 115
25232
YDOT = -2315
816699 meter/sec RA = 179
05324 deg
ZDOT = 3063
039762 TA = 185
40082
MA = 185
40850
Ha = 219
802 n
mi
Hp = 215
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11151393
68 X = -3417611
51
Y = 12072907
95 feet Y = 3641709
06 meter
Z = -15014246
00 Z = -4592898
06
XDOT = -21752
764069 XDOT = -6618
732246
YDOT = -7597
823815 feet/sec YDOT = -2389
896524 meter/sec
ZDOT = 10049
343052 ZDOT = 3030
860122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 442913
88 X = 135000
15
Y = -16360995
28 feet Y = -4986831
36 meter
Z = -15088337
58 Z = -4598925
30
XDOT = 20268
725478 XDOT = 6177
907526
YDOT = -8585
036723 feet/sec YDOT = -2616
719193 meter/sec
ZDOT = 9906
627869 ZDOT = 3019
540175
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 17356
37373940
00016717 00000-0 10270-3 0 9151
2 25544 51
6404 180
1911 0003119 279
2052 80
8748 15
54173096 11013
Satellite: ISS
Catalog Number: 25544
Epoch time: 17356
37373940 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 180
1911 deg
Eccentricity:
0003119
Arg of perigee: 279
2052 deg
Mean anomaly: 80
8748 deg
Mean motion: 15
54173096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1101
Checksum: 298
Coasting Arc #17 (Orbit 1116)
---------------------------------------
Vector Time (GMT): 2017/357/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4841369
07 A = 6783962
61 meter
Y = -3251678
42 meter E =
0009346
Z = 3458579
88 I = 51
67602
XDOT = 5337
528872 Wp = 83
41349
YDOT = 3075
616043 meter/sec RA = 174
06636 deg
ZDOT = -4568
276688 TA = 56
03071
MA = 55
94193
Ha = 219
782 n
mi
Hp = 215
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15883756
81 X = 4860570
47
Y = -10668236
30 feet Y = -3197431
83 meter
Z = 11347046
84 Z = 3482143
92
XDOT = 17511
577663 XDOT = 5324
930050
YDOT = 10090
603815 feet/sec YDOT = 3135
233844 meter/sec
ZDOT = -14987
784408 ZDOT = -4542
379233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4639118
71 X = -1414003
38
Y = 18498248
05 feet Y = 5638266
00 meter
Z = 11452242
78 Z = 3490643
60
XDOT = -18495
454144 XDOT = -5637
414423
YDOT = 4592
926753 feet/sec YDOT = 1399
924074 meter/sec
ZDOT = -14873
078196 ZDOT = -4533
314234
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 17357
40254923
00016717 00000-0 10270-3 0 9166
2 25544 51
6402 175
0621 0003086 286
0415 74
0398 15
54197071 11176
Satellite: ISS
Catalog Number: 25544
Epoch time: 17357
40254923 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 175
0621 deg
Eccentricity:
0003086
Arg of perigee: 286
0415 deg
Mean anomaly: 74
0398 deg
Mean motion: 15
54197071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1117
Checksum: 296
Coasting Arc #18 (Orbit 1131)
---------------------------------------
Vector Time (GMT): 2017/358/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5879849
40 A = 6787502
52 meter
Y = 2734800
66 meter E =
0006192
Z = -1992803
38 I = 51
71933
XDOT = -3648
522495 Wp = 12
26423
YDOT = -3783
380214 meter/sec RA = 169
09200 deg
ZDOT = 5582
127892 TA = 325
76028
MA = 325
80019
Ha = 219
861 n
mi
Hp = 215
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19290844
48 X = -5900313
69
Y = 8972443
12 feet Y = 2668933
86 meter
Z = -6538068
82 Z = -2021415
15
XDOT = -11970
218159 XDOT = -3633
059557
YDOT = -12412
664745 feet/sec YDOT = -3824
094375 meter/sec
ZDOT = 18314
067887 ZDOT = 5564
441976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7993350
73 X = 2436373
30
Y = -19673922
36 feet Y = -5996611
54 meter
Z = -6665649
48 Z = -2031689
96
XDOT = 15870
607744 XDOT = 4837
361240
YDOT = 279
549177 feet/sec YDOT = 85
206589 meter/sec
ZDOT = 18235
950340 ZDOT = 5558
317664
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 17358
36705807
00016717 00000-0 10270-3 0 9175
2 25544 51
6396 170
2539 0003205 288
2646 71
8157 15
54153717 11320
Satellite: ISS
Catalog Number: 25544
Epoch time: 17358
36705807 = yrday
fracday
Element set: 917
Inclination: 51
6396 deg
RA of node: 170
2539 deg
Eccentricity:
0003205
Arg of perigee: 288
2646 deg
Mean anomaly: 71
8157 deg
Mean motion: 15
54153717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1132
Checksum: 319
Coasting Arc #19 (Orbit 1147)
---------------------------------------
Vector Time (GMT): 2017/359/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6452588
22 A = 6789233
97 meter
Y = -2073978
77 meter E =
0009848
Z = 291969
76 I = 51
75774
XDOT = 1704
867870 Wp = 138
47340
YDOT = 4442
332499 meter/sec RA = 164
12725 deg
ZDOT = -6013
364825 TA = 38
38535
MA = 38
31532
Ha = 219
971 n
mi
Hp = 215
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21169908
85 X = 6473882
20
Y = -6804392
27 feet Y = -2001702
46 meter
Z = 957906
04 Z = 323365
84
XDOT = 5593
398523 XDOT = 1684
275582
YDOT = 14574
581689 feet/sec YDOT = 4461
282665 meter/sec
ZDOT = -19728
887220 ZDOT = -6005
132950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10537073
51 X = -3211700
01
Y = 19574149
07 feet Y = 5966200
64 meter
Z = 1097792
83 Z = 334607
26
XDOT = -12799
289702 XDOT = -3901
223501
YDOT = -5768
128144 feet/sec YDOT = -1758
125458 meter/sec
ZDOT = -19692
887481 ZDOT = -6002
392104
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 17359
39586520
00016717 00000-0 10270-3 0 9189
2 25544 51
6404 165
1248 0003141 289
8550 70
2264 15
54144921 11486
Satellite: ISS
Catalog Number: 25544
Epoch time: 17359
39586520 = yrday
fracday
Element set: 918
Inclination: 51
6404 deg
RA of node: 165
1248 deg
Eccentricity:
0003141
Arg of perigee: 289
8550 deg
Mean anomaly: 70
2264 deg
Mean motion: 15
54144921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1148
Checksum: 309
Coasting Arc #20 (Orbit 1163)
---------------------------------------
Vector Time (GMT): 2017/360/08:42:47
000
Vector Time (MET): N/A
Weight (LBS) : 940911
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6506365
79 A = 6788323
07 meter
Y = 1280299
10 meter E =
0012230
Z = 1419485
41 I = 51
78505
XDOT = 288
079628 Wp = 48
54168
YDOT = -5002
422104 meter/sec RA = 159
16471 deg
ZDOT = 5807
914146 TA = 326
90941
MA = 326
98587
Ha = 219
964 n
mi
Hp = 215
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21346344
47 X = -6527094
01
Y = 4200456
37 feet Y = 1207424
50 meter
Z = 4657104
35 Z = 1387829
34
XDOT = 945
143136 XDOT = 315
784764
YDOT = -16412
146010 feet/sec YDOT = -4999
045957 meter/sec
ZDOT = 19054
836437 ZDOT = 5809
380604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12186721
61 X = 3714512
75
Y = -18057880
75 feet Y = -5504042
05 meter
Z = 4516152
80 Z = 1376523
37
XDOT = 9679
445356 XDOT = 2950
294944
YDOT = 11320
336243 feet/sec YDOT = 3450
438487 meter/sec
ZDOT = 19062
039555 ZDOT = 5810
109656
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 17360
42466704
00016717 00000-0 10270-3 0 9197
2 25544 51
6391 159
9948 0003189 294
5455 65
5365 15
54199470 11644
Satellite: ISS
Catalog Number: 25544
Epoch time: 17360
42466704 = yrday
fracday
Element set: 919
Inclination: 51
6391 deg
RA of node: 159
9948 deg
Eccentricity:
0003189
Arg of perigee: 294
5455 deg
Mean anomaly: 65
5365 deg
Mean motion: 15
54199470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1164
Checksum: 345
- 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