[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 27th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
333/00:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
7
000/00:00:00
000 0
0 0
0 221
6
333/10:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
6
336/14:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 221
0
338/17:51:57
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 220
6
339/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
5
340/09:34:11
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
4
341/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
3
342/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
1
343/10:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 219
9
346/03:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 219
5
Coasting Arc #1 (Orbit 58)
---------------------------------------
Vector Time (GMT): 2019/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3557566
14 A = 6792980
06 meter
Y = -3786446
97 meter E =
0006118
Z = 4369803
33 I = 51
24778
XDOT = 2624
983286 Wp = 63
30175
YDOT = 6361
765483 meter/sec RA = 270
75422 deg
ZDOT = 3374
450828 TA = 352
32417
MA = 352
33353
Ha = 227
569 n
mi
Hp = 221
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11671804
92 X = 3578416
39
Y = -12422726
29 feet Y = -3746547
68 meter
Z = 14336625
11 Z = 4387135
20
XDOT = 8612
149888 XDOT = 2537
257547
YDOT = 20871
934000 feet/sec YDOT = 6390
629002 meter/sec
ZDOT = 11071
032899 ZDOT = 3386
989932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6427064
45 X = 1958969
25
Y = 15715214
12 feet Y = 4789997
26 meter
Z = 14415924
03 Z = 4393973
65
XDOT = -21383
025517 XDOT = -6517
546178
YDOT = -1465
542667 feet/sec YDOT = -446
697405 meter/sec
ZDOT = 11127
670906 ZDOT = 3391
714092
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 19331
55452230
00016717 00000-0 10270-3 0 9000
2 25544 51
6422 271
3490 0006802 329
9577 30
1183 15
50075299 599
Satellite: ISS
Catalog Number: 25544
Epoch time: 19331
55452230 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 271
3490 deg
Eccentricity:
0006802
Arg of perigee: 329
9577 deg
Mean anomaly: 30
1183 deg
Mean motion: 15
50075299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 59
Checksum: 293
Coasting Arc #2 (Orbit 73)
---------------------------------------
Vector Time (GMT): 2019/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3401992
27 A = 6792313
22 meter
Y = 3714168
93 meter E =
0011686
Z = -4567742
48 I = 51
24571
XDOT = -2910
312609 Wp = 33
98540
YDOT = -6396
905662 meter/sec RA = 265
77200 deg
ZDOT = -3028
220225 TA = 205
49257
MA = 205
55025
Ha = 227
929 n
mi
Hp = 221
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11161391
95 X = -3421084
45
Y = 12185593
62 feet Y = 3676019
29 meter
Z = -14986031
75 Z = -4584314
22
XDOT = -9548
269714 XDOT = -2823
854616
YDOT = -20987
223299 feet/sec YDOT = -6428
967026 meter/sec
ZDOT = -9935
105725 ZDOT = -3042
148475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6687106
74 X = -2038230
13
Y = -15035607
47 feet Y = -4582853
16 meter
Z = -15061859
82 Z = -4590854
87
XDOT = 21932
574975 XDOT = 6685
048852
YDOT = 279
757954 feet/sec YDOT = 85
270224 meter/sec
ZDOT = -9998
089129 ZDOT = -3047
417567
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 19332
52159737
00016717 00000-0 10270-3 0 9015
2 25544 51
6418 266
5582 0006883 335
2802 24
8018 15
50059554 742
Satellite: ISS
Catalog Number: 25544
Epoch time: 19332
52159737 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 266
5582 deg
Eccentricity:
0006883
Arg of perigee: 335
2802 deg
Mean anomaly: 24
8018 deg
Mean motion: 15
50059554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 74
Checksum: 311
Coasting Arc #3 (Orbit 81)
---------------------------------------
Vector Time (GMT): 2019/333/00:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4190222
72 A = 6789257
00 meter
Y = 773039
04 meter E =
0013515
Z = -5296323
05 I = 51
23856
XDOT = -1096
274399 Wp = 62
33663
YDOT = -7570
452135 meter/sec RA = 263
15531 deg
ZDOT = -231
939133 TA = 205
40262
MA = 205
46911
Ha = 227
742 n
mi
Hp = 221
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13747449
88 X = -4172828
73
Y = 2536217
32 feet Y = 726278
96 meter
Z = -17376387
96 Z = -5316635
49
XDOT = -3596
700785 XDOT = -1010
411277
YDOT = -24837
441389 feet/sec YDOT = -7582
231328 meter/sec
ZDOT = -760
955162 ZDOT = -237
056929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1266889
38 X = -386147
88
Y = 13805481
26 feet Y = 4207910
69 meter
Z = -17469038
71 Z = -5324563
00
XDOT = -23871
420785 XDOT = -7276
009055
YDOT = -3205
821515 feet/sec YDOT = -977
134398 meter/sec
ZDOT = -783
696604 ZDOT = -238
870725
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 19333
03736893
00016717 00000-0 10270-3 0 9027
2 25544 51
6434 264
0008 0006459 333
9780 26
1045 15
50056672 827
Satellite: ISS
Catalog Number: 25544
Epoch time: 19333
03736893 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 264
0008 deg
Eccentricity:
0006459
Arg of perigee: 333
9780 deg
Mean anomaly: 26
1045 deg
Mean motion: 15
50056672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 82
Checksum: 298
Coasting Arc #4 (Orbit 88)
---------------------------------------
Vector Time (GMT): 2019/333/10:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3350381
12 A = 6791320
78 meter
Y = -3453367
32 meter E =
0004535
Z = 4788550
83 I = 51
24533
XDOT = 3092
786305 Wp = 53
47731
YDOT = 6533
286675 meter/sec RA = 261
10897 deg
ZDOT = 2548
671446 TA = 11
28786
MA = 11
27769
Ha = 227
791 n
mi
Hp = 221
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10992064
05 X = 3365488
32
Y = -11329945
28 feet Y = -3415817
14 meter
Z = 15710468
60 Z = 4804862
14
XDOT = 10146
936696 XDOT = 3007
119172
YDOT = 21434
667569 feet/sec YDOT = 6567
393069 meter/sec
ZDOT = 8361
782960 ZDOT = 2563
487977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 40414
26 X = 12318
27
Y = 15711184
07 feet Y = 4788768
91 meter
Z = 15785088
44 Z = 4811294
96
XDOT = -21003
352996 XDOT = -6401
821993
YDOT = -8411
281567 feet/sec YDOT = -2563
758622 meter/sec
ZDOT = 8428
823483 ZDOT = 2569
105397
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 19333
48866816
00016717 00000-0 10270-3 0 9036
2 25544 51
6412 261
7675 0006844 336
4519 23
6318 15
50087208 894
Satellite: ISS
Catalog Number: 25544
Epoch time: 19333
48866816 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 261
7675 deg
Eccentricity:
0006844
Arg of perigee: 336
4519 deg
Mean anomaly: 23
6318 deg
Mean motion: 15
50087208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 89
Checksum: 324
Coasting Arc #5 (Orbit 103)
---------------------------------------
Vector Time (GMT): 2019/334/10:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3252568
87 A = 6790833
90 meter
Y = 3357553
59 meter E =
0013859
Z = -4937552
74 I = 51
25008
XDOT = -3402
037070 Wp = 44
12541
YDOT = -6500
229651 meter/sec RA = 256
12558 deg
ZDOT = -2173
057381 TA = 204
48634
MA = 204
55222
Ha = 228
139 n
mi
Hp = 221
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10671157
70 X = -3265888
24
Y = 11015595
76 feet Y = 3321107
20 meter
Z = -16199320
01 Z = -4953384
54
XDOT = -11161
538942 XDOT = -3318
541193
YDOT = -21326
212766 feet/sec YDOT = -6537
806512 meter/sec
ZDOT = -7129
453350 ZDOT = -2189
381300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -317693
72 X = -96833
05
Y = -15256614
97 feet Y = -4650216
24 meter
Z = -16271745
32 Z = -4959627
97
XDOT = 21824
559197 XDOT = 6652
125643
YDOT = 7249
335122 feet/sec YDOT = 2209
597345 meter/sec
ZDOT = -7203
390748 ZDOT = -2195
593500
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 19334
45573940
00016717 00000-0 10270-3 0 9048
2 25544 51
6415 256
9760 0006917 341
3944 18
6954 15
50059529 1049
Satellite: ISS
Catalog Number: 25544
Epoch time: 19334
45573940 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 256
9760 deg
Eccentricity:
0006917
Arg of perigee: 341
3944 deg
Mean anomaly: 18
6954 deg
Mean motion: 15
50059529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 104
Checksum: 321
Coasting Arc #6 (Orbit 119)
---------------------------------------
Vector Time (GMT): 2019/335/10:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3182589
65 A = 6790200
29 meter
Y = -3226490
15 meter E =
0004455
Z = 5053223
33 I = 51
25728
XDOT = 3719
336739 Wp = 35
25794
YDOT = 6459
511662 meter/sec RA = 251
14339 deg
ZDOT = 1784
701402 TA = 37
38732
MA = 37
35634
Ha = 228
086 n
mi
Hp = 221
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10441567
09 X = 3193886
83
Y = -10585597
61 feet Y = -3190837
57 meter
Z = 16578816
70 Z = 5068710
30
XDOT = 12202
548356 XDOT = 3638
159053
YDOT = 21192
623564 feet/sec YDOT = 6500
649827 meter/sec
ZDOT = 5855
319560 ZDOT = 1802
572139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 432220
22 X = 131740
72
Y = 14783112
81 feet Y = 4505892
78 meter
Z = 16649658
39 Z = 5074815
88
XDOT = -22613
313436 XDOT = -6892
537935
YDOT = -6014
472837 feet/sec YDOT = -1833
211321 meter/sec
ZDOT = 5936
336406 ZDOT = 1809
395336
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 19335
48727640
00016717 00000-0 10270-3 0 9051
2 25544 51
6413 251
8659 0006987 344
3312 15
7621 15
50093502 1203
Satellite: ISS
Catalog Number: 25544
Epoch time: 19335
48727640 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 251
8659 deg
Eccentricity:
0006987
Arg of perigee: 344
3312 deg
Mean anomaly: 15
7621 deg
Mean motion: 15
50093502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 120
Checksum: 298
Coasting Arc #7 (Orbit 134)
---------------------------------------
Vector Time (GMT): 2019/336/10:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3141264
90 A = 6789888
02 meter
Y = 3125548
55 meter E =
0015483
Z = -5157170
85 I = 51
26726
XDOT = -4027
921159 Wp = 52
44263
YDOT = -6354
465331 meter/sec RA = 246
16101 deg
ZDOT = -1391
375937 TA = 204
04016
MA = 204
11252
Ha = 228
409 n
mi
Hp = 220
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10305987
19 X = -3150931
50
Y = 10254424
39 feet Y = 3090367
14 meter
Z = -16919851
88 Z = -5172453
17
XDOT = -13214
964434 XDOT = -3949
805768
YDOT = -20847
983368 feet/sec YDOT = -6399
071491 meter/sec
ZDOT = -4564
881682 ZDOT = -1410
752971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -538488
53 X = -164131
30
Y = -14446673
12 feet Y = -4403345
97 meter
Z = -16989751
18 Z = -5178476
16
XDOT = 23182
209110 XDOT = 7065
937337
YDOT = 4632
224504 feet/sec YDOT = 1411
902029 meter/sec
ZDOT = -4652
798799 ZDOT = -1418
173074
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 19336
45434415
00016717 00000-0 10270-3 0 9065
2 25544 51
6408 247
0747 0007014 349
3719 10
7282 15
50064519 1350
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
45434415 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 247
0747 deg
Eccentricity:
0007014
Arg of perigee: 349
3719 deg
Mean anomaly: 10
7282 deg
Mean motion: 15
50064519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 135
Checksum: 299
Coasting Arc #8 (Orbit 137)
---------------------------------------
Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4727879
66 A = 6791517
15 meter
Y = 1220767
78 meter E =
0011806
Z = 4720303
69 I = 51
27726
XDOT = 881
319114 Wp = 27
11845
YDOT = 7111
696021 meter/sec RA = 245
29172 deg
ZDOT = -2708
951458 TA = 89
90026
MA = 89
76498
Ha = 228
266 n
mi
Hp = 220
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15511416
22 X = 4690948
64
Y = 4005143
63 feet Y = 1273431
35 meter
Z = 15486560
68 Z = 4743180
43
XDOT = 2891
466909 XDOT = 814
887166
YDOT = 23332
336026 feet/sec YDOT = 7121
180352 meter/sec
ZDOT = -8887
636018 ZDOT = -2704
831045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 882008
19 X = 268836
10
Y = 15894277
38 feet Y = 4844575
75 meter
Z = 15590791
46 Z = 4752073
24
XDOT = -20161
928525 XDOT = -6145
355814
YDOT = 9860
411574 feet/sec YDOT = 3005
453448 meter/sec
ZDOT = -8869
334295 ZDOT = -2703
373093
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 19336
64775487
00016717 00000-0 10270-3 0 9074
2 25544 51
6426 246
1179 0007117 348
2964 11
8020 15
50106953 1387
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
64775487 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 246
1179 deg
Eccentricity:
0007117
Arg of perigee: 348
2964 deg
Mean anomaly: 11
8020 deg
Mean motion: 15
50106953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 138
Checksum: 315
Coasting Arc #9 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2019/337/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4893737
31 A = 6792252
18 meter
Y = -1209798
99 meter E =
0009113
Z = -4557679
43 I = 51
29428
XDOT = -1128
278992 Wp = 67
29589
YDOT = -6927
642464 meter/sec RA = 240
31135 deg
ZDOT = 3058
720865 TA = 233
45486
MA = 233
53879
Ha = 228
404 n
mi
Hp = 220
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16055568
62 X = -4857706
54
Y = -3969156
78 feet Y = -1264322
41 meter
Z = -14953016
51 Z = -4581364
03
XDOT = -3701
702729 XDOT = -1065
585828
YDOT = -22728
485775 feet/sec YDOT = -6939
909369 meter/sec
ZDOT = 10035
173442 ZDOT = 3053
391839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1365346
42 X = -416157
59
Y = -16383893
96 feet Y = -4993810
88 meter
Z = -15060944
19 Z = -4590575
79
XDOT = 19117
678656 XDOT = 5827
068454
YDOT = -10771
069416 feet/sec YDOT = -3283
021958 meter/sec
ZDOT = 10011
328090 ZDOT = 3051
452802
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 19337
61482038
00016717 00000-0 10270-3 0 9080
2 25544 51
6424 241
3264 0007079 351
6127 8
4904 15
50075378 1539
Satellite: ISS
Catalog Number: 25544
Epoch time: 19337
61482038 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 241
3264 deg
Eccentricity:
0007079
Arg of perigee: 351
6127 deg
Mean anomaly: 8
4904 deg
Mean motion: 15
50075378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 303
Coasting Arc #10 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2019/338/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5075269
52 A = 6792934
46 meter
Y = 1220814
74 meter E =
0013236
Z = 4345843
95 I = 51
31503
XDOT = 1323
313067 Wp = 39
02833
YDOT = 6726
637613 meter/sec RA = 235
33221 deg
ZDOT = -3419
233154 TA = 85
92105
MA = 85
76977
Ha = 228
504 n
mi
Hp = 220
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16651146
73 X = 5040131
02
Y = 4005297
72 feet Y = 1277373
24 meter
Z = 14258018
20 Z = 4370412
56
XDOT = 4341
578305 XDOT = 1264
604307
YDOT = 22069
021039 feet/sec YDOT = 6741
107794 meter/sec
ZDOT = -11217
956543 ZDOT = -3412
947122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1815563
29 X = 553383
69
Y = 16935209
82 feet Y = 5161851
95 meter
Z = 14369988
81 Z = 4379972
59
XDOT = -18048
000976 XDOT = -5501
030697
YDOT = 11473
303480 feet/sec YDOT = 3497
062901 meter/sec
ZDOT = -11189
715410 ZDOT = -3410
625257
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 19338
64635180
00016717 00000-0 10270-3 0 9093
2 25544 51
6429 236
2152 0007264 354
6808 5
4265 15
50113395 1694
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
64635180 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 236
2152 deg
Eccentricity:
0007264
Arg of perigee: 354
6808 deg
Mean anomaly: 5
4265 deg
Mean motion: 15
50113395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 311
Coasting Arc #11 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2019/338/17:51:57
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3412307
34 A = 6800795
80 meter
Y = 5835965
99 meter E =
0006490
Z = -740067
26 I = 51
34035
XDOT = -4477
882400 Wp = 98
72133
YDOT = 1873
244131 meter/sec RA = 234
66082 deg
ZDOT = -5920
422324 TA = 89
28944
MA = 89
21508
Ha = 228
599 n
mi
Hp = 220
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11195234
07 X = 3350389
12
Y = 19146870
05 feet Y = 5873778
66 meter
Z = -2428042
19 Z = -723641
48
XDOT = -14691
215224 XDOT = -4469
738489
YDOT = 6145
814079 feet/sec YDOT = 1823
215197 meter/sec
ZDOT = -19423
957757 ZDOT = -5942
154411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4119540
49 X = 1255635
94
Y = 21801874
21 feet Y = 6645211
26 meter
Z = -2353498
34 Z = -717346
29
XDOT = -14188
176994 XDOT = -4324
556348
YDOT = 590
072023 feet/sec YDOT = 179
853953 meter/sec
ZDOT = -19523
188987 ZDOT = -5950
668003
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 19338
77529430
00016717 00000-0 10270-3 0 9109
2 25544 51
6394 235
5721 0007058 357
3821 2
7291 15
50115432 1711
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
77529430 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 235
5721 deg
Eccentricity:
0007058
Arg of perigee: 357
3821 deg
Mean anomaly: 2
7291 deg
Mean motion: 15
50115432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 294
Coasting Arc #12 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/17:51:57
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3637888
52 A = 6800684
08 meter
Y = -5629140
01 meter E =
0018257
Z = 1085442
96 I = 51
35921
XDOT = 4592
806938 Wp = 39
36162
YDOT = -1830
073159 meter/sec RA = 229
68797 deg
ZDOT = 5861
649670 TA = 332
44886
MA = 332
54551
Ha = 228
652 n
mi
Hp = 220
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11935329
80 X = -3579943
98
Y = -18468307
13 feet Y = -5669497
53 meter
Z = 3561164
56 Z = 1067911
73
XDOT = 15068
264232 XDOT = 4584
457143
YDOT = -6004
177031 feet/sec YDOT = -1778
760170 meter/sec
ZDOT = 19231
134088 ZDOT = 5883
939595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5419552
61 X = -1651879
64
Y = -21324156
09 feet Y = -6499602
78 meter
Z = 3481547
82 Z = 1061175
78
XDOT = 14518
476204 XDOT = 4425
231547
YDOT = -511
284231 feet/sec YDOT = -155
839434 meter/sec
ZDOT = 19332
911685 ZDOT = 5892
671482
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 19339
80682708
00016717 00000-0 10270-3 0 9113
2 25544 51
6389 230
4609 0006700 1
7500 358
3673 15
50070194 1877
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80682708 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 230
4609 deg
Eccentricity:
0006700
Arg of perigee: 1
7500 deg
Mean anomaly: 358
3673 deg
Mean motion: 15
50070194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 304
Coasting Arc #13 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -302588
27 A = 6792781
52 meter
Y = 5132205
80 meter E =
0013317
Z = -4453051
07 I = 51
33490
XDOT = -6146
422055 Wp = 42
18191
YDOT = -3188
576977 meter/sec RA = 229
50116 deg
ZDOT = -3253
246782 TA = 194
80061
MA = 194
83963
Ha = 228
678 n
mi
Hp = 220
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -992743
66 X = -338324
98
Y = 16837945
54 feet Y = 5128622
48 meter
Z = -14609747
60 Z = -4454607
44
XDOT = -20165
426688 XDOT = -6094
507052
YDOT = -10461
210555 feet/sec YDOT = -3257
020151 meter/sec
ZDOT = -10673
381832 ZDOT = -3282
978126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2099353
69 X = -639883
01
Y = 16729555
44 feet Y = 5099168
50 meter
Z = -14617159
91 Z = -4455310
34
XDOT = -18070
724188 XDOT = -5507
956732
YDOT = -11723
054605 feet/sec YDOT = -3573
187044 meter/sec
ZDOT = -10808
794031 ZDOT = -3294
520421
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 19339
80682729
00016717 00000-0 10270-3 0 9127
2 25544 51
6400 230
4615 0006689 2
1819 357
9359 15
50077444 1873
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80682729 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 230
4615 deg
Eccentricity:
0006689
Arg of perigee: 2
1819 deg
Mean anomaly: 357
9359 deg
Mean motion: 15
50077444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 324
Coasting Arc #14 (Orbit 196)
---------------------------------------
Vector Time (GMT): 2019/340/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 872822
41 A = 6791192
72 meter
Y = -4687555
01 meter E =
0007406
Z = 4828782
81 I = 51
34461
XDOT = 6243
460500 Wp = 62
22179
YDOT = 3703
266631 meter/sec RA = 226
44690 deg
ZDOT = 2466
905246 TA = 3
44824
MA = 3
44314
Ha = 228
706 n
mi
Hp = 220
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2863590
59 X = 901719
37
Y = -15379117
48 feet Y = -4677633
19 meter
Z = 15842463
30 Z = 4833092
62
XDOT = 20483
794292 XDOT = 6189
602493
YDOT = 12149
824905 feet/sec YDOT = 3772
784139 meter/sec
ZDOT = 8093
521149 ZDOT = 2497
103336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7183936
70 X = 2189663
91
Y = 13873581
64 feet Y = 4228667
68 meter
Z = 15862403
19 Z = 4834860
49
XDOT = -22590
240705 XDOT = -6885
505367
YDOT = 2288
354774 feet/sec YDOT = 697
490535 meter/sec
ZDOT = 8231
042218 ZDOT = 2508
821668
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 19340
45153319
00016717 00000-0 10270-3 0 9139
2 25544 51
6412 227
2714 0007047 2
6899 357
4288 15
50095581 1971
Satellite: ISS
Catalog Number: 25544
Epoch time: 19340
45153319 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 227
2714 deg
Eccentricity:
0007047
Arg of perigee: 2
6899 deg
Mean anomaly: 357
4288 deg
Mean motion: 15
50095581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 197
Checksum: 314
Coasting Arc #15 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2019/341/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 917861
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -856739
43 A = 6790656
65 meter
Y = 4553519
03 meter E =
0016614
Z = -4978951
12 I = 51
36751
XDOT = -6474
490244 Wp = 51
16501
YDOT = -3501
160158 meter/sec RA = 221
47124 deg
ZDOT = -2082
428044 TA = 198
40953
MA = 198
46973
Ha = 228
938 n
mi
Hp = 220
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2810824
89 X = -883409
24
Y = 14939366
90 feet Y = 4543789
56 meter
Z = -16335141
49 Z = -4983177
39
XDOT = -21241
765891 XDOT = -6424
742643
YDOT = -11486
745926 feet/sec YDOT = -3573
284197 meter/sec
ZDOT = -6832
113004 ZDOT = -2113
758488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7191494
69 X = -2191967
58
Y = -13368951
40 feet Y = -4074856
39 meter
Z = -16354687
70 Z = -4984908
81
XDOT = 22761
794925 XDOT = 6937
795093
YDOT = -3689
583990 feet/sec YDOT = -1124
585200 meter/sec
ZDOT = -6974
829799 ZDOT = -2125
928123
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 19341
41859371
00016717 00000-0 10270-3 0 9148
2 25544 51
6421 222
4801 0007183 6
9120 353
2129 15
50086676 2121
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
41859371 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 222
4801 deg
Eccentricity:
0007183
Arg of perigee: 6
9120 deg
Mean anomaly: 353
2129 deg
Mean motion: 15
50086676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 283
Coasting Arc #16 (Orbit 212)
---------------------------------------
Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940461
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1894424
95 A = 6795768
66 meter
Y = 5461824
02 meter E =
0009673
Z = -3584861
11 I = 51
38702
XDOT = -6205
210664 Wp = 38
05095
YDOT = -745
377785 meter/sec RA = 221
18441 deg
ZDOT = -4413
726506 TA = 184
36093
MA = 184
36937
Ha = 228
910 n
mi
Hp = 220
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6215304
95 X = 1850621
93
Y = 17919370
15 feet Y = 5482764
13 meter
Z = -11761355
36 Z = -3575764
63
XDOT = -20358
302705 XDOT = -6174
974738
YDOT = -2445
465173 feet/sec YDOT = -814
599496 meter/sec
ZDOT = -14480
730005 ZDOT = -4443
796097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18667554
49 X = -5689870
61
Y = -3496160
30 feet Y = -1065629
66 meter
Z = -11720178
94 Z = -3572310
54
XDOT = 11983
305391 XDOT = 3652
511483
YDOT = -14968
952447 feet/sec YDOT = -4562
536706 meter/sec
ZDOT = -14617
857468 ZDOT = -4455
522956
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 19341
48306375
00016717 00000-0 10270-3 0 9157
2 25544 51
6432 222
1616 0007121 5
7488 354
3743 15
50073842 2136
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
48306375 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 222
1616 deg
Eccentricity:
0007121
Arg of perigee: 5
7488 deg
Mean anomaly: 354
3743 deg
Mean motion: 15
50073842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 213
Checksum: 287
Coasting Arc #17 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2019/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940461
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1969800
78 A = 6794984
48 meter
Y = -5238405
84 meter E =
0013796
Z = 3838112
00 I = 51
41054
XDOT = 6428
855199 Wp = 66
29490
YDOT = 617
237748 meter/sec RA = 216
21274 deg
ZDOT = 4135
483089 TA = 340
05625
MA = 340
11012
Ha = 229
097 n
mi
Hp = 220
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6462600
98 X = -1929720
70
Y = -17186370
87 feet Y = -5260209
74 meter
Z = 12592230
96 Z = 3828640
23
XDOT = 21092
044616 XDOT = 6401
387071
YDOT = 2025
058227 feet/sec YDOT = 688
975842 meter/sec
ZDOT = 13567
857904 ZDOT = 4166
645874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18206181
80 X = 5549244
21
Y = 2598144
74 feet Y = 791914
52 meter
Z = 12549319
64 Z = 3825032
63
XDOT = -11756
715698 XDOT = -3583
446945
YDOT = 16061
659304 feet/sec YDOT = 4895
593756 meter/sec
ZDOT = 13709
995683 ZDOT = 4178
806684
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 19342
51459186
00016717 00000-0 10270-3 0 9162
2 25544 51
6435 217
0504 0007255 10
5676 349
5626 15
50064256 2291
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
51459186 = yrday
fracday
Element set: 916
Inclination: 51
6435 deg
RA of node: 217
0504 deg
Eccentricity:
0007255
Arg of perigee: 10
5676 deg
Mean anomaly: 349
5626 deg
Mean motion: 15
50064256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 229
Checksum: 307
Coasting Arc #18 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2019/342/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 940461
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -301310
63 A = 6791380
85 meter
Y = -4803754
33 meter E =
0008491
Z = 4783095
78 I = 51
41097
XDOT = 6890
267342 Wp = 69
34541
YDOT = 2147
049731 meter/sec RA = 213
94545 deg
ZDOT = 2589
578481 TA = 355
05071
MA = 355
05910
Ha = 228
862 n
mi
Hp = 220
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -988551
95 X = -270805
25
Y = -15760348
87 feet Y = -4806953
65 meter
Z = 15692571
45 Z = 4781705
77
XDOT = 22605
863984 XDOT = 6853
167370
YDOT = 7044
126414 feet/sec YDOT = 2223
893904 meter/sec
ZDOT = 8495
992392 ZDOT = 2622
959437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11934724
14 X = -3637703
92
Y = -10349810
09 feet Y = -3154622
11 meter
Z = 15686504
42 Z = 4781246
55
XDOT = 20152
209038 XDOT = 6142
393315
YDOT = -10126
803252 feet/sec YDOT = -3086
649631 meter/sec
ZDOT = 8648
170978 ZDOT = 2635
962514
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 19342
96588218
00016717 00000-0 10270-3 0 9171
2 25544 51
6431 214
8116 0006753 11
6277 348
5028 15
50105241 2365
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
96588218 = yrday
fracday
Element set: 917
Inclination: 51
6431 deg
RA of node: 214
8116 deg
Eccentricity:
0006753
Arg of perigee: 11
6277 deg
Mean anomaly: 348
5028 deg
Mean motion: 15
50105241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 300
Coasting Arc #19 (Orbit 243)
---------------------------------------
Vector Time (GMT): 2019/343/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 956863
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6023693
69 A = 6797184
89 meter
Y = 831482
39 meter E =
0015837
Z = 3031409
17 I = 51
44441
XDOT = 1710
623440 Wp = 69
38252
YDOT = 5621
909948 meter/sec RA = 211
27064 deg
ZDOT = -4914
842342 TA = 75
83052
MA = 75
65462
Ha = 229
133 n
mi
Hp = 219
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19762774
57 X = 5999222
97
Y = 2727960
58 feet Y = 898706
46 meter
Z = 9945568
14 Z = 3060611
15
XDOT = 5612
281627 XDOT = 1671
504434
YDOT = 18444
586444 feet/sec YDOT = 5640
821106 meter/sec
ZDOT = -16124
810834 ZDOT = -4906
627094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13147738
96 X = -4007430
83
Y = 14915723
86 feet Y = 4546312
63 meter
Z = 10078764
57 Z = 3072007
44
XDOT = -17449
182482 XDOT = -5318
510821
YDOT = -4452
599519 feet/sec YDOT = -1357
152333 meter/sec
ZDOT = -16087
645838 ZDOT = -4903
514451
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 19343
48164811
00016717 00000-0 10270-3 0 9189
2 25544 51
6425 212
2600 0007246 14
7904 345
3457 15
50067013 2441
Satellite: ISS
Catalog Number: 25544
Epoch time: 19343
48164811 = yrday
fracday
Element set: 918
Inclination: 51
6425 deg
RA of node: 212
2600 deg
Eccentricity:
0007246
Arg of perigee: 14
7904 deg
Mean anomaly: 345
3457 deg
Mean motion: 15
50067013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 244
Checksum: 284
Coasting Arc #20 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2019/344/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 956863
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6184479
24 A = 6797828
02 meter
Y = -619392
67 meter E =
0011214
Z = -2744981
36 I = 51
47580
XDOT = -1728
603902 Wp = 33
77057
YDOT = -5415
531134 meter/sec RA = 206
30456 deg
ZDOT = 5135
799414 TA = 295
13899
MA = 295
25528
Ha = 229
108 n
mi
Hp = 219
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20290286
21 X = -6163759
56
Y = -2032128
17 feet Y = -688435
70 meter
Z = -9005844
36 Z = -2774973
48
XDOT = -5671
272644 XDOT = -1692
864640
YDOT = -17767
490598 feet/sec YDOT = -5434
662398 meter/sec
ZDOT = 16849
735610 ZDOT = 5127
488514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12589469
02 X = 3837270
16
Y = -15963934
64 feet Y = -4865807
28 meter
Z = -9142677
54 Z = -2786688
12
XDOT = 16926
479134 XDOT = 5159
190840
YDOT = 3755
726539 feet/sec YDOT = 1144
745449 meter/sec
ZDOT = 16812
114813 ZDOT = 5124
332595
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 19344
44870276
00016717 00000-0 10270-3 0 9196
2 25544 51
6424 207
4688 0007261 16
6363 343
5024 15
50084633 2592
Satellite: ISS
Catalog Number: 25544
Epoch time: 19344
44870276 = yrday
fracday
Element set: 919
Inclination: 51
6424 deg
RA of node: 207
4688 deg
Eccentricity:
0007261
Arg of perigee: 16
6363 deg
Mean anomaly: 343
5024 deg
Mean motion: 15
50084633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 259
Checksum: 312
Coasting Arc #21 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2019/345/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 956863
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6343540
15 A = 6798635
34 meter
Y = 430683
47 meter E =
0016112
Z = 2398716
34 I = 51
50871
XDOT = 1680
188525 Wp = 79
33252
YDOT = 5221
641030 meter/sec RA = 201
34151 deg
ZDOT = -5347
313132 TA = 73
86100
MA = 73
68372
Ha = 229
286 n
mi
Hp = 219
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20812139
60 X = 6326600
86
Y = 1413003
52 feet Y = 501526
37 meter
Z = 7869804
27 Z = 2429490
23
XDOT = 5512
429543 XDOT = 1647
648369
YDOT = 17131
368208 feet/sec YDOT = 5240
248898 meter/sec
ZDOT = -17543
678253 ZDOT = -5339
229587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12062219
67 X = -3676564
56
Y = 16953303
39 feet Y = 5167366
87 meter
Z = 8010238
04 Z = 2441520
56
XDOT = -16309
217727 XDOT = -4971
049563
YDOT = -3280
935403 feet/sec YDOT = -1000
029111 meter/sec
ZDOT = -17507
076597 ZDOT = -5336
156947
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 19345
48022800
00016717 00000-0 10270-3 0 9205
2 25544 51
6423 202
3584 0007265 21
0423 339
1025 15
50072270 2755
Satellite: ISS
Catalog Number: 25544
Epoch time: 19345
48022800 = yrday
fracday
Element set: 920
Inclination: 51
6423 deg
RA of node: 202
3584 deg
Eccentricity:
0007265
Arg of perigee: 21
0423 deg
Mean anomaly: 339
1025 deg
Mean motion: 15
50072270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 275
Checksum: 264
Coasting Arc #22 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2019/346/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 956863
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6438457
46 A = 6800976
75 meter
Y = -2157526
29 meter E =
0018953
Z = 81983
03 I = 51
53489
XDOT = 1592
672976 Wp = 39
02980
YDOT = -4496
537785 meter/sec RA = 197
97642 deg
ZDOT = 6002
416630 TA = 321
85366
MA = 321
98766
Ha = 229
224 n
mi
Hp = 219
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21123548
08 X = -6414251
08
Y = -7078498
34 feet Y = -2229390
34 meter
Z = 268973
21 Z = 50765
53
XDOT = 5225
305039 XDOT = 1613
679470
YDOT = -14752
420554 feet/sec YDOT = -4478
610847 meter/sec
ZDOT = 19692
967946 ZDOT = 6010
203666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6182454
74 X = 1884412
20
Y = 21404275
19 feet Y = 6524023
08 meter
Z = 126594
54 Z = 38586
02
XDOT = -13470
282726 XDOT = -4105
742175
YDOT = 3743
492442 feet/sec YDOT = 1141
016496 meter/sec
ZDOT = 19728
765169 ZDOT = 6013
327623
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 19346
18939669
00016717 00000-0 10270-3 0 9214
2 25544 51
6388 198
8433 0007074 26
0069 334
1436 15
50132086 2861
Satellite: ISS
Catalog Number: 25544
Epoch time: 19346
18939669 = yrday
fracday
Element set: 921
Inclination: 51
6388 deg
RA of node: 198
8433 deg
Eccentricity:
0007074
Arg of perigee: 26
0069 deg
Mean anomaly: 334
1436 deg
Mean motion: 15
50132086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 286
Checksum: 329
- 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