[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 15th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15438 0847 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
227/05:57:52
433 -0
9 1
8 1
8
N/A 0
8 0
0 224
2
000/00:09:44
866 1
4 -0
1 222
4
227/08:59:52
374 -0
6 1
8 1
8
N/A 1
2 0
0 225
5
000/00:09:44
748 1
3 -0
0 223
5
227/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
6
000/00:00:00
000 0
0 0
0 223
7
234/03:38:33
000 0
0 0
0 0
0
N/A 0
0 0
0 226
8
000/00:00:00
000 0
0 0
0 222
3
235/16:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
9
000/00:00:00
000 0
0 0
0 222
2
236/05:30:59
000 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 221
9
239/14:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
6
000/00:00:00
000 0
0 0
0 221
5
Coasting Arc #1 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2019/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4496317
82 A = 6790256
58 meter
Y = -2610755
01 meter E =
0003673
Z = 4366094
17 I = 52
00130
XDOT = 557
072066 Wp = 55
84043
YDOT = -6799
891592 meter/sec RA = 71
14051 deg
ZDOT = -3488
285937 TA = 69
46709
MA = 69
42767
Ha = 223
895 n
mi
Hp = 221
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14751698
89 X = -4487997
00
Y = -8565469
18 feet Y = -2660989
61 meter
Z = 14324455
95 Z = 4344273
39
XDOT = 1827
664258 XDOT = 650
012766
YDOT = -22309
355616 feet/sec YDOT = -6793
142244 meter/sec
ZDOT = -11444
507666 ZDOT = -3485
354440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6352957
93 X = 1936381
58
Y = 15920097
71 feet Y = 4852445
78 meter
Z = 14225341
30 Z = 4335884
03
XDOT = -14152
050856 XDOT = -4313
545101
YDOT = 15873
216749 feet/sec YDOT = 4838
156465 meter/sec
ZDOT = -11430
529171 ZDOT = -3484
025291
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 19226
54198608
00016717 00000-0 10270-3 0 9008
2 25544 51
6416 71
7524 0006223 261
3850 98
6597 15
51081975 24304
Satellite: ISS
Catalog Number: 25544
Epoch time: 19226
54198608 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 71
7524 deg
Eccentricity:
0006223
Arg of perigee: 261
3850 deg
Mean anomaly: 98
6597 deg
Mean motion: 15
51081975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2430
Checksum: 316
Coasting Arc #2 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2019/227/06:02:44
866
Vector Time (MET): N/A
Weight (LBS) : 937363
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2150771
77 A = 6799161
18 meter
Y = 6414894
86 meter E =
0009678
Z = 605453
87 I = 52
01794
XDOT = -4661
055058 Wp = 23
95140
YDOT = 993
942076 meter/sec RA = 67
45834 deg
ZDOT = 6001
663995 TA = 342
54154
MA = 342
57479
Ha = 224
247 n
mi
Hp = 222
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7056337
81 X = 2075937
83
Y = 21046242
97 feet Y = 6438527
87 meter
Z = 1986397
21 Z = 615719
62
XDOT = -15292
175386 XDOT = -4700
975249
YDOT = 3260
964817 feet/sec YDOT = 941
595569 meter/sec
ZDOT = 19690
498672 ZDOT = 5978
925932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21066422
99 X = 6421045
73
Y = 6982594
33 feet Y = 2128294
75 meter
Z = 2032540
11 Z = 619518
22
XDOT = -6128
254909 XDOT = -1867
892096
YDOT = 12764
132717 feet/sec YDOT = 3890
507652 meter/sec
ZDOT = 19586
872224 ZDOT = 5970
078654
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 19227
31515998
00016717 00000-0 10270-3 0 9010
2 25544 51
6409 67
9166 0006349 276
6704 83
3724 15
50697373 24421
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
31515998 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 67
9166 deg
Eccentricity:
0006349
Arg of perigee: 276
6704 deg
Mean anomaly: 83
3724 deg
Mean motion: 15
50697373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 335
Coasting Arc #3 (Orbit 2442)
---------------------------------------
Vector Time (GMT): 2019/227/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3150901
30 A = 6800110
13 meter
Y = 5977842
19 meter E =
0010160
Z = -696658
82 I = 52
01844
XDOT = -3906
880348 Wp = 358
62017
YDOT = 2756
381591 meter/sec RA = 66
82336 deg
ZDOT = 5989
490695 TA = 353
90403
MA = 353
91639
Ha = 225
479 n
mi
Hp = 223
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10337602
68 X = 3087205
07
Y = 19612343
14 feet Y = 6012721
65 meter
Z = -2285626
05 Z = -681507
90
XDOT = -12817
848912 XDOT = -3966
505569
YDOT = 9043
246691 feet/sec YDOT = 2712
358633 meter/sec
ZDOT = 19650
560022 ZDOT = 5970
368207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17801189
80 X = 5425802
65
Y = -13226329
32 feet Y = -4031385
18 meter
Z = -2217199
51 Z = -675802
41
XDOT = 9951
506536 XDOT = 3033
219192
YDOT = 10118
716289 feet/sec YDOT = 3084
184725 meter/sec
ZDOT = 19563
231199 ZDOT = 5962
872869
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 19227
37960322
00016717 00000-0 10270-3 0 9022
2 25544 51
6431 67
5982 0007375 286
5776 73
4565 15
50361002 24438
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
37960322 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 67
5982 deg
Eccentricity:
0007375
Arg of perigee: 286
5776 deg
Mean anomaly: 73
4565 deg
Mean motion: 15
50361002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 314
Coasting Arc #4 (Orbit 2444)
---------------------------------------
Vector Time (GMT): 2019/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4676310
09 A = 6793798
79 meter
Y = 2928482
94 meter E =
0000829
Z = -3962958
37 I = 51
99265
XDOT = -612
394750 Wp = 284
53730
YDOT = 6468
779048 meter/sec RA = 66
20203 deg
ZDOT = 4057
059136 TA = 27
69956
MA = 27
69515
Ha = 225
576 n
mi
Hp = 223
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15342224
70 X = 4662464
80
Y = 9607883
66 feet Y = 2980699
36 meter
Z = -13001831
92 Z = -3940276
73
XDOT = -2009
169126 XDOT = -704
391462
YDOT = 21223
028373 feet/sec YDOT = 6461
416383 meter/sec
ZDOT = 13310
561469 ZDOT = 4053
861064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6457137
93 X = -1968135
64
Y = -16990246
00 feet Y = -5178626
98 meter
Z = -12898830
61 Z = -3931563
57
XDOT = 13287
185017 XDOT = 4049
933993
YDOT = -15144
794510 feet/sec YDOT = -4616
133367 meter/sec
ZDOT = 13295
392630 ZDOT = 4052
435674
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 19227
50852013
00016717 00000-0 10270-3 0 9035
2 25544 51
6401 66
9569 0007416 286
1475 73
8859 15
50354204 24455
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
50852013 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 66
9569 deg
Eccentricity:
0007416
Arg of perigee: 286
1475 deg
Mean anomaly: 73
8859 deg
Mean motion: 15
50354204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2445
Checksum: 314
Coasting Arc #5 (Orbit 2460)
---------------------------------------
Vector Time (GMT): 2019/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4889419
09 A = 6794779
01 meter
Y = -3005842
59 meter E =
0005884
Z = 3635960
10 I = 51
98258
XDOT = 531
524629 Wp = 54
90870
YDOT = -6228
803688 meter/sec RA = 61
26833 deg
ZDOT = -4426
234740 TA = 82
30385
MA = 82
23703
Ha = 225
672 n
mi
Hp = 223
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16041401
22 X = -4873104
59
Y = -9861688
29 feet Y = -3060428
27 meter
Z = 11929002
95 Z = 3612249
30
XDOT = 1743
847209 XDOT = 622
637118
YDOT = -20435
707637 feet/sec YDOT = -6222
350390 meter/sec
ZDOT = -14521
767520 ZDOT = -4423
431522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7155826
43 X = 2181095
90
Y = 17490880
55 feet Y = 5331220
39 meter
Z = 11821328
44 Z = 3603140
91
XDOT = -12306
633904 XDOT = -3751
062014
YDOT = 14859
141360 feet/sec YDOT = 4529
066287 meter/sec
ZDOT = -14508
412728 ZDOT = -4422
164200
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 19228
53986236
00016717 00000-0 10270-3 0 9045
2 25544 51
6410 61
8442 0007613 290
6552 69
3782 15
50377469 24615
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
53986236 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 61
8442 deg
Eccentricity:
0007613
Arg of perigee: 290
6552 deg
Mean anomaly: 69
3782 deg
Mean motion: 15
50377469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2461
Checksum: 324
Coasting Arc #6 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2019/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5111526
47 A = 6795853
44 meter
Y = 3032535
06 meter E =
0004173
Z = -3289587
78 I = 51
96746
XDOT = -487
521331 Wp = 328
89695
YDOT = 5984
091928 meter/sec RA = 56
33365 deg
ZDOT = 4759
737437 TA = 353
16522
MA = 353
17091
Ha = 225
974 n
mi
Hp = 223
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16770099
97 X = 5093214
58
Y = 9949262
01 feet Y = 3089593
29 meter
Z = -10792610
83 Z = -3264802
92
XDOT = -1599
479432 XDOT = -577
520651
YDOT = 19632
847532 feet/sec YDOT = 5978
137005 meter/sec
ZDOT = 15615
936473 ZDOT = 4757
150572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7993351
05 X = -2436373
40
Y = -17853494
16 feet Y = -5441745
02 meter
Z = -10680056
25 Z = -3255281
15
XDOT = 11437
788873 XDOT = 3486
238048
YDOT = -14453
507157 feet/sec YDOT = -4405
428982 meter/sec
ZDOT = 15603
583997 ZDOT = 4755
972402
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 19229
50674670
00016717 00000-0 10270-3 0 9050
2 25544 51
6396 57
0504 0007336 293
8790 66
1592 15
50352361 24769
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
50674670 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 57
0504 deg
Eccentricity:
0007336
Arg of perigee: 293
8790 deg
Mean anomaly: 66
1592 deg
Mean motion: 15
50352361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2476
Checksum: 323
Coasting Arc #7 (Orbit 2491)
---------------------------------------
Vector Time (GMT): 2019/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5337594
45 A = 6796779
18 meter
Y = -3036814
49 meter E =
0006598
Z = 2909093
35 I = 51
95131
XDOT = 495
020426 Wp = 77
41136
YDOT = -5728
557920 meter/sec RA = 51
39984 deg
ZDOT = -5060
736445 TA = 69
65692
MA = 69
58603
Ha = 226
028 n
mi
Hp = 223
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17511792
83 X = -5317369
76
Y = -9963302
15 feet Y = -3096390
05 meter
Z = 9544269
52 Z = 2883214
95
XDOT = 1624
082764 XDOT = 583
623880
YDOT = -18794
481364 feet/sec YDOT = -5722
527005 meter/sec
ZDOT = -16603
466026 ZDOT = -5058
116475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8896878
53 X = 2711768
58
Y = 18138505
01 feet Y = 5528616
33 meter
Z = 9426746
35 Z = 2873272
29
XDOT = -10709
568268 XDOT = -3264
276408
YDOT = 13894
598361 feet/sec YDOT = 4235
073580 meter/sec
ZDOT = -16590
981363 ZDOT = -5056
931120
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 19230
53808705
00016717 00000-0 10270-3 0 9064
2 25544 51
6396 51
9384 0007540 297
7166 62
3220 15
50375310 24928
Satellite: ISS
Catalog Number: 25544
Epoch time: 19230
53808705 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 51
9384 deg
Eccentricity:
0007540
Arg of perigee: 297
7166 deg
Mean anomaly: 62
3220 deg
Mean motion: 15
50375310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2492
Checksum: 306
Coasting Arc #8 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2019/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5557398
12 A = 6797736
85 meter
Y = 2985744
31 meter E =
0007557
Z = -2518197
84 I = 51
93225
XDOT = -537
230786 Wp = 342
78454
YDOT = 5486
715881 meter/sec RA = 46
46451 deg
ZDOT = 5322
751974 TA = 349
12352
MA = 349
13985
Ha = 226
276 n
mi
Hp = 222
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18232933
46 X = 5535829
49
Y = 9795749
06 feet Y = 3047770
36 meter
Z = -8261803
93 Z = -2491254
90
XDOT = -1762
568196 XDOT = -624
399564
YDOT = 18001
036354 feet/sec YDOT = 5480
220999 meter/sec
ZDOT = 17463
097029 ZDOT = 5319
930417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9894842
02 X = -3015947
85
Y = -18234461
03 feet Y = -5557863
72 meter
Z = -8139440
94 Z = -2480901
60
XDOT = 10135
099979 XDOT = 3089
178474
YDOT = -13284
531693 feet/sec YDOT = -4049
125260 meter/sec
ZDOT = 17449
711936 ZDOT = 5318
672198
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 19231
50497148
00016717 00000-0 10270-3 0 9078
2 25544 51
6392 47
1452 0007247 300
6877 59
3559 15
50349375 25074
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
50497148 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 47
1452 deg
Eccentricity:
0007247
Arg of perigee: 300
6877 deg
Mean anomaly: 59
3559 deg
Mean motion: 15
50349375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 326
Coasting Arc #9 (Orbit 2522)
---------------------------------------
Vector Time (GMT): 2019/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5770010
87 A = 6798461
95 meter
Y = -2916392
67 meter E =
0006886
Z = 2095318
74 I = 51
91191
XDOT = 632
226333 Wp = 95
38914
YDOT = -5245
802992 meter/sec RA = 41
52896 deg
ZDOT = -5545
391422 TA = 61
54948
MA = 61
48012
Ha = 226
356 n
mi
Hp = 222
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18930481
86 X = -5747147
91
Y = -9568217
43 feet Y = -2980789
09 meter
Z = 6874405
31 Z = 2067346
05
XDOT = 2074
233376 XDOT = 717
775645
YDOT = -17210
639736 feet/sec YDOT = -5238
254858 meter/sec
ZDOT = -18193
541410 ZDOT = -5542
112354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10910104
43 X = 3325399
83
Y = 18237711
59 feet Y = 5558854
49 meter
Z = 6747360
53 Z = 2056595
49
XDOT = -9736
713883 XDOT = -2967
750391
YDOT = 12568
562996 feet/sec YDOT = 3830
898001 meter/sec
ZDOT = -18178
090991 ZDOT = -5540
682134
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 19232
53631022
00016717 00000-0 10270-3 0 9084
2 25544 51
6400 42
0329 0007474 305
0968 54
9481 15
50380302 25231
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
53631022 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 42
0329 deg
Eccentricity:
0007474
Arg of perigee: 305
0968 deg
Mean anomaly: 54
9481 deg
Mean motion: 15
50380302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2523
Checksum: 279
Coasting Arc #10 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2019/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5961215
26 A = 6799195
62 meter
Y = 2794232
99 meter E =
0010706
Z = -1670114
34 I = 51
88903
XDOT = -757
245773 Wp = 355
90701
YDOT = 5034
932811 meter/sec RA = 36
59190 deg
ZDOT = 5729
099261 TA = 345
88233
MA = 345
91223
Ha = 226
584 n
mi
Hp = 222
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19557792
86 X = 5937638
75
Y = 9167431
08 feet Y = 2860763
63 meter
Z = -5479377
76 Z = -1641214
47
XDOT = -2484
402143 XDOT = -841
320215
YDOT = 16518
808436 feet/sec YDOT = 5025
994825 meter/sec
ZDOT = 18796
257417 ZDOT = 5725
216523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11958371
72 X = -3644911
70
Y = -18026859
49 feet Y = -5494586
77 meter
Z = -5348113
47 Z = -1630104
99
XDOT = 9514
137225 XDOT = 2899
909026
YDOT = -11874
208036 feet/sec YDOT = -3619
258609 meter/sec
ZDOT = 18778
073876 ZDOT = 5723
556917
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 19233
50319201
00016717 00000-0 10270-3 0 9095
2 25544 51
6406 37
2401 0007111 308
9581 51
0936 15
50355863 25388
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
50319201 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 37
2401 deg
Eccentricity:
0007111
Arg of perigee: 308
9581 deg
Mean anomaly: 51
0936 deg
Mean motion: 15
50355863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 287
Coasting Arc #11 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2019/234/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4396704
01 A = 6798609
08 meter
Y = 4774937
77 meter E =
0012725
Z = 1993989
18 I = 51
87102
XDOT = -4808
504796 Wp = 35
96576
YDOT = 2088
248599 meter/sec RA = 33
40845 deg
ZDOT = 5593
941090 TA = 345
95430
MA = 345
98966
Ha = 226
766 n
mi
Hp = 222
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14424881
91 X = 4333296
84
Y = 15665806
32 feet Y = 4823750
31 meter
Z = 6541959
27 Z = 2015192
56
XDOT = -15775
934371 XDOT = -4858
670987
YDOT = 6851
209315 feet/sec YDOT = 2034
196121 meter/sec
ZDOT = 18352
825099 ZDOT = 5570
461371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19496115
00 X = 5942415
85
Y = 8492976
17 feet Y = 2588659
14 meter
Z = 6637981
04 Z = 2023256
62
XDOT = -11137
925538 XDOT = -3394
839704
YDOT = 11286
804273 feet/sec YDOT = 3440
217943 meter/sec
ZDOT = 18245
740494 ZDOT = 5561
301702
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 19234
21223786
00016717 00000-0 10270-3 0 9108
2 25544 51
6421 33
7300 0007476 314
0013 46
0521 15
50350247 25493
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
21223786 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 33
7300 deg
Eccentricity:
0007476
Arg of perigee: 314
0013 deg
Mean anomaly: 46
0521 deg
Mean motion: 15
50350247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 265
Coasting Arc #12 (Orbit 2563)
---------------------------------------
Vector Time (GMT): 2019/235/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4424482
67 A = 6797774
94 meter
Y = -4560482
72 meter E =
0002150
Z = -2417928
09 I = 51
84091
XDOT = 5056
437454 Wp = 329
41792
YDOT = -2057
074957 meter/sec RA = 28
46902 deg
ZDOT = -5368
822878 TA = 237
47426
MA = 237
49504
Ha = 226
930 n
mi
Hp = 222
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14516019
25 X = -4361412
28
Y = -14962213
65 feet Y = -4609607
76 meter
Z = -7932834
93 Z = -2439267
32
XDOT = 16589
361726 XDOT = 5105
143150
YDOT = -6748
933586 feet/sec YDOT = -2000
257994 meter/sec
ZDOT = -17614
248289 ZDOT = -5344
142361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19417324
28 X = -5918400
44
Y = -7483810
44 feet Y = -2281065
42 meter
Z = -8029484
49 Z = -2447386
87
XDOT = 11767
556655 XDOT = 3586
751269
YDOT = -11740
437575 feet/sec YDOT = -3578
485373 meter/sec
ZDOT = -17501
705211 ZDOT = -5334
519748
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 19235
17911755
00016717 00000-0 10270-3 0 9115
2 25544 51
6431 28
9382 0007531 317
2235 42
8329 15
50360968 25641
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
17911755 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 28
9382 deg
Eccentricity:
0007531
Arg of perigee: 317
2235 deg
Mean anomaly: 42
8329 deg
Mean motion: 15
50360968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 310
Coasting Arc #13 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2019/235/16:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4291329
02 A = 6790568
08 meter
Y = -2133805
96 meter E =
0005897
Z = -4814899
32 I = 51
80158
XDOT = 5325
927840 Wp = 73
06997
YDOT = 4848
802050 meter/sec RA = 25
79828 deg
ZDOT = 2602
266707 TA = 222
52626
MA = 222
57195
Ha = 226
877 n
mi
Hp = 222
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14079163
44 X = 4338258
95
Y = -7000675
74 feet Y = -2085554
87 meter
Z = -15796913
78 Z = -4793939
74
XDOT = 17473
516536 XDOT = 5258
670974
YDOT = 15908
143208 feet/sec YDOT = 4907
984248 meter/sec
ZDOT = 8537
620430 ZDOT = 2627
974677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7168550
23 X = -2184974
11
Y = 14101626
55 feet Y = 4298175
77 meter
Z = -15701299
47 Z = -4785756
08
XDOT = -22445
924521 XDOT = -6841
517794
YDOT = -1790
372699 feet/sec YDOT = -545
705599 meter/sec
ZDOT = 8654
116902 ZDOT = 2637
774832
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 19235
69478492
00016717 00000-0 10270-3 0 9129
2 25544 51
6435 26
3802 0007252 316
3392 43
7192 15
50385853 25725
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
69478492 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 26
3802 deg
Eccentricity:
0007252
Arg of perigee: 316
3392 deg
Mean anomaly: 43
7192 deg
Mean motion: 15
50385853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 318
Coasting Arc #14 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2019/236/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3500100
23 A = 6789408
54 meter
Y = 2850736
27 meter E =
0009106
Z = 5074196
30 I = 51
78252
XDOT = -6128
150480 Wp = 357
91088
YDOT = -4203
708720 meter/sec RA = 23
10321 deg
ZDOT = -1856
644237 TA = 110
10771
MA = 110
00970
Ha = 227
102 n
mi
Hp = 221
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11483268
47 X = -3556365
39
Y = 9352809
30 feet Y = 2811281
01 meter
Z = 16647625
64 Z = 5057057
57
XDOT = -20105
480576 XDOT = -6071
669427
YDOT = -13791
695277 feet/sec YDOT = -4271
922176 meter/sec
ZDOT = -6091
352484 ZDOT = -1886
275275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 769537
20 X = 234554
94
Y = 14877808
13 feet Y = 4534755
92 meter
Z = 16569326
29 Z = 5050330
65
XDOT = -21856
836400 XDOT = -6661
963735
YDOT = 8096
310554 feet/sec YDOT = 2467
755457 meter/sec
ZDOT = -6225
764695 ZDOT = -1897
613079
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 19236
27491077
00016717 00000-0 10270-3 0 9139
2 25544 51
6446 23
5075 0007722 320
3374 39
7212 15
50406474 25816
Satellite: ISS
Catalog Number: 25544
Epoch time: 19236
27491077 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 23
5075 deg
Eccentricity:
0007722
Arg of perigee: 320
3374 deg
Mean anomaly: 39
7212 deg
Mean motion: 15
50406474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 299
Coasting Arc #15 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2019/237/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3713451
84 A = 6790163
72 meter
Y = -2861372
29 meter E =
0007468
Z = -4917086
02 I = 51
75310
XDOT = 6130
489071 Wp = 67
72812
YDOT = 3948
970498 meter/sec RA = 18
15266 deg
ZDOT = 2337
429825 TA = 225
11298
MA = 225
17364
Ha = 227
319 n
mi
Hp = 221
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12183240
93 X = 3769056
86
Y = -9387704
36 feet Y = -2819534
81 meter
Z = -16132171
98 Z = -4898912
60
XDOT = 20113
153121 XDOT = 6074
521051
YDOT = 12955
939955 feet/sec YDOT = 4017
212938 meter/sec
ZDOT = 7668
733021 ZDOT = 2367
073437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -654958
04 X = -199631
21
Y = -15453242
68 feet Y = -4710148
37 meter
Z = -16049163
40 Z = -4891785
00
XDOT = 20984
580779 XDOT = 6396
100221
YDOT = -8974
343453 feet/sec YDOT = -2735
379884 meter/sec
ZDOT = 7803
219883 ZDOT = 2378
421420
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 19237
24178856
00016717 00000-0 10270-3 0 9145
2 25544 51
6441 18
7148 0007705 324
7012 35
3627 15
50376565 25961
Satellite: ISS
Catalog Number: 25544
Epoch time: 19237
24178856 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 18
7148 deg
Eccentricity:
0007705
Arg of perigee: 324
7012 deg
Mean anomaly: 35
3627 deg
Mean motion: 15
50376565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 320
Coasting Arc #16 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2019/238/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3953426
88 A = 6790919
45 meter
Y = 2888392
45 meter E =
0010640
Z = 4707798
04 I = 51
72326
XDOT = -6079
980627 Wp = 16
68194
YDOT = -3710
099697 meter/sec RA = 13
20082 deg
ZDOT = -2817
929408 TA = 101
32328
MA = 101
20371
Ha = 227
430 n
mi
Hp = 221
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12970560
64 X = -4008299
53
Y = 9476353
19 feet Y = 2843875
48 meter
Z = 15445531
63 Z = 4688460
79
XDOT = -19947
443003 XDOT = -6024
353550
YDOT = -12172
243102 feet/sec YDOT = -3777
779196 meter/sec
ZDOT = -9245
175224 ZDOT = -2847
328397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 556937
25 X = 169754
47
Y = 16138358
21 feet Y = 4918971
58 meter
Z = 15357225
52 Z = 4680882
34
XDOT = -20027
725249 XDOT = -6104
450656
YDOT = 9651
995664 feet/sec YDOT = 2941
928278 meter/sec
ZDOT = -9378
567700 ZDOT = -2858
587435
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 19238
27312235
00016717 00000-0 10270-3 0 9151
2 25544 51
6435 13
6030 0007813 328
2609 31
8070 15
50409331 26129
Satellite: ISS
Catalog Number: 25544
Epoch time: 19238
27312235 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 13
6030 deg
Eccentricity:
0007813
Arg of perigee: 328
2609 deg
Mean anomaly: 31
8070 deg
Mean motion: 15
50409331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 274
Coasting Arc #17 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2019/239/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4150838
43 A = 6791894
73 meter
Y = -2974492
90 meter E =
0006102
Z = -4480244
10 I = 51
69335
XDOT = 5998
850218 Wp = 53
45727
YDOT = 3471
369153 meter/sec RA = 8
24693 deg
ZDOT = 3259
735836 TA = 249
35516
MA = 249
42061
Ha = 227
609 n
mi
Hp = 221
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13618236
33 X = 4205553
80
Y = -9758834
98 feet Y = -2927769
25 meter
Z = -14698963
59 Z = -4459948
36
XDOT = 19681
267119 XDOT = 5943
752765
YDOT = 11389
006407 feet/sec YDOT = 3538
144362 meter/sec
ZDOT = 10694
671378 ZDOT = 3288
741856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -721614
24 X = -219948
02
Y = -16819224
62 feet Y = -5126499
66 meter
Z = -14606290
01 Z = -4451997
20
XDOT = 19001
039480 XDOT = 5791
516833
YDOT = -10198
067001 feet/sec YDOT = -3108
370822 meter/sec
ZDOT = 10826
296821 ZDOT = 3299
855271
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 19239
23999948
00016717 00000-0 10270-3 0 9161
2 25544 51
6434 8
8102 0007781 331
4286 28
6438 15
50375780 26273
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
23999948 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 8
8102 deg
Eccentricity:
0007781
Arg of perigee: 331
4286 deg
Mean anomaly: 28
6438 deg
Mean motion: 15
50375780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 338
Coasting Arc #18 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2019/239/14:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 928586
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6279970
85 A = 6798186
29 meter
Y = -1147640
52 meter E =
0010859
Z = -2317662
11 I = 51
70131
XDOT = 2839
327862 Wp = 2
15281
YDOT = 4618
388234 meter/sec RA = 6
30426 deg
ZDOT = 5418
001543 TA = 332
07267
MA = 332
13091
Ha = 227
613 n
mi
Hp = 221
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20603578
90 X = 6303595
09
Y = -3765224
79 feet Y = -1077281
32 meter
Z = -7603878
33 Z = -2287099
51
XDOT = 9315
380125 XDOT = 2761
155472
YDOT = 15152
192369 feet/sec YDOT = 4649
702394 meter/sec
ZDOT = 17775
595615 ZDOT = 5431
603945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18362821
73 X = -5596988
06
Y = 10177851
66 feet Y = 3102209
19 meter
Z = -7464680
88 Z = -2275234
73
XDOT = -12819
272923 XDOT = -3907
314387
YDOT = -10074
345135 feet/sec YDOT = -3070
660397 meter/sec
ZDOT = 17837
003661 ZDOT = 5436
718716
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 19239
62674949
00016717 00000-0 10270-3 0 9176
2 25544 51
6437 6
8905 0007525 331
2710 28
8025 15
50336601 26331
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
62674949 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 6
8905 deg
Eccentricity:
0007525
Arg of perigee: 331
2710 deg
Mean anomaly: 28
8025 deg
Mean motion: 15
50336601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 311
Coasting Arc #19 (Orbit 2648)
---------------------------------------
Vector Time (GMT): 2019/240/14:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 928586
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6396256
69 A = 6798852
16 meter
Y = 1331995
61 meter E =
0009803
Z = 1875417
22 I = 51
67067
XDOT = -2594
761654 Wp = 82
68127
YDOT = -4507
181236 meter/sec RA = 1
35319 deg
ZDOT = -5621
980959 TA = 76
72651
MA = 76
61720
Ha = 227
643 n
mi
Hp = 221
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20985094
12 X = -6419785
63
Y = 4370064
33 feet Y = 1260336
61 meter
Z = 6152943
63 Z = 1844290
06
XDOT = -8512
997554 XDOT = -2516
860281
YDOT = -14787
340012 feet/sec YDOT = -4535
762122 meter/sec
ZDOT = -18444
819418 ZDOT = -5634
395880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18331746
24 X = 5587516
26
Y = -11186747
73 feet Y = -3409720
71 meter
Z = 6011165
27 Z = 1832203
17
XDOT = 12057
452588 XDOT = 3675
111549
YDOT = 9769
423671 feet/sec YDOT = 2977
720335 meter/sec
ZDOT = -18500
837108 ZDOT = -5639
055150
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 19240
65808175
00016717 00000-0 10270-3 0 9182
2 25544 51
6438 1
7787 0007446 336
4757 23
6052 15
50372769 26499
Satellite: ISS
Catalog Number: 25544
Epoch time: 19240
65808175 = yrday
fracday
Element set: 918
Inclination: 51
6438 deg
RA of node: 1
7787 deg
Eccentricity:
0007446
Arg of perigee: 336
4757 deg
Mean anomaly: 23
6052 deg
Mean motion: 15
50372769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2649
Checksum: 335
- 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