[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 11th 2020
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ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 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
280/09:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 222
6
281/08:29:26
464 -1
6 -2
3 2
3
N/A -0
8 0
2 228
7
000/00:06:52
927 1
5 -0
0 222
3
283/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 222
2
288/05:45:05
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 222
1
288/08:50:45
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
1
289/02:17:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 222
0
291/11:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 910)
---------------------------------------
Vector Time (GMT): 2020/279/12:10:00
045
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -715423
78 A = 6793862
79 meter
Y = 4467392
66 meter E =
0014171
Z = -5081119
70 I = 51
74857
XDOT = -7361
123049 Wp = 104
31988
YDOT = 932
485149 meter/sec RA = 161
39933 deg
ZDOT = 1857
237667 TA = 183
68571
MA = 183
69616
Ha = 229
686 n
mi
Hp = 222
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2347190
89 X = -740644
65
Y = 14656800
05 feet Y = 4459250
99 meter
Z = -16670340
23 Z = -5084656
52
XDOT = -24150
666170 XDOT = -7380
024871
YDOT = 3059
334479 feet/sec YDOT = 850
062202 meter/sec
ZDOT = 6093
299432 ZDOT = 1821
433500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1950852
76 X = -594619
92
Y = -14696266
51 feet Y = -4479422
03 meter
Z = -16686679
14 Z = -5086099
80
XDOT = 21301
724703 XDOT = 6492
765690
YDOT = -9554
887566 feet/sec YDOT = -2912
329730 meter/sec
ZDOT = 5927
826762 ZDOT = 1806
801597
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 20279
51995191
00016717 00000-0 10270-3 0 9007
2 25544 51
6433 162
5507 0001038 107
7963 252
3301 15
48846094 9111
Satellite: ISS
Catalog Number: 25544
Epoch time: 20279
51995191 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 162
5507 deg
Eccentricity:
0001038
Arg of perigee: 107
7963 deg
Mean anomaly: 252
3301 deg
Mean motion: 15
48846094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 911
Checksum: 302
Coasting Arc #2 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2020/280/09:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 938748
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3536901
35 A = 6799257
55 meter
Y = 4574583
60 meter E =
0006453
Z = -3583404
22 I = 51
79443
XDOT = -6095
008723 Wp = 100
46478
YDOT = -1220
237382 meter/sec RA = 156
90321 deg
ZDOT = 4463
855851 TA = 217
44112
MA = 217
48610
Ha = 229
701 n
mi
Hp = 222
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11604007
05 X = -3570386
35
Y = 15008476
38 feet Y = 4534844
08 meter
Z = -11756575
54 Z = -3600666
96
XDOT = -19996
747778 XDOT = -6102
593983
YDOT = -4003
403485 feet/sec YDOT = -1288
438395 meter/sec
ZDOT = 14645
196361 ZDOT = 4434
229678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15165357
78 X = 4622401
05
Y = -11315333
15 feet Y = -3448913
54 meter
Z = -11836366
44 Z = -3607724
49
XDOT = 17429
550935 XDOT = 5312
527125
YDOT = 8203
051465 feet/sec YDOT = 2500
290086 meter/sec
ZDOT = 14508
257930 ZDOT = 4422
117017
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 20280
42326282
00016717 00000-0 10270-3 0 9019
2 25544 51
6423 158
0830 0001135 111
9633 248
1638 15
48843547 9259
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42326282 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 158
0830 deg
Eccentricity:
0001135
Arg of perigee: 111
9633 deg
Mean anomaly: 248
1638 deg
Mean motion: 15
48843547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 292
Coasting Arc #3 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2020/281/08:32:52
927
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5354342
89 A = 6802738
22 meter
Y = -3976677
76 meter E =
0013295
Z = 1309618
01 I = 51
83873
XDOT = 3803
097349 Wp = 115
83801
YDOT = 3184
491410 meter/sec RA = 152
27508 deg
ZDOT = -5838
665295 TA = 49
97707
MA = 49
86048
Ha = 228
737 n
mi
Hp = 222
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17566741
77 X = 5392051
85
Y = -13046843
06 feet Y = -3916590
79 meter
Z = 4296647
02 Z = 1335719
50
XDOT = 12477
353507 XDOT = 3795
566211
YDOT = 10447
806462 feet/sec YDOT = 3226
978150 meter/sec
ZDOT = -19155
726032 ZDOT = -5820
209323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21857125
46 X = -6662051
84
Y = 158451
17 feet Y = 48295
92 meter
Z = 4417314
28 Z = 1346397
39
XDOT = -3983
764878 XDOT = -1214
251535
YDOT = -14285
059793 feet/sec YDOT = -4354
086225 meter/sec
ZDOT = -19070
411651 ZDOT = -5812
661471
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 20281
39108114
00016717 00000-0 10270-3 0 9029
2 25544 51
6421 153
2961 0001204 4
7894 355
3267 15
49266217 9404
Satellite: ISS
Catalog Number: 25544
Epoch time: 20281
39108114 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 153
2961 deg
Eccentricity:
0001204
Arg of perigee: 4
7894 deg
Mean anomaly: 355
3267 deg
Mean motion: 15
49266217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 287
Coasting Arc #4 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2020/282/08:32:52
927
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5046746
64 A = 6802814
14 meter
Y = 4384665
51 meter E =
0010106
Z = -1233092
56 I = 51
86839
XDOT = -3966
380699 Wp = 34
50038
YDOT = -2925
111065 meter/sec RA = 147
34053 deg
ZDOT = 5863
843445 TA = 312
16747
MA = 312
25326
Ha = 228
742 n
mi
Hp = 222
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16557567
71 X = -5089412
44
Y = 14385385
52 feet Y = 4327990
60 meter
Z = -4045579
27 Z = -1257711
76
XDOT = -13013
060036 XDOT = -3961
860119
YDOT = -9596
821079 feet/sec YDOT = -2969
440663 meter/sec
ZDOT = 19238
331511 ZDOT = 5844
586990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21800891
09 X = 6644911
61
Y = -2208951
02 feet Y = -673288
27 meter
Z = -4159418
17 Z = -1267790
66
XDOT = 5035
845688 XDOT = 1534
925766
YDOT = 13832
577852 feet/sec YDOT = 4216
169729 meter/sec
ZDOT = 19149
308115 ZDOT = 5836
709114
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 20282
35863641
00016717 00000-0 10270-3 0 9030
2 25544 51
6421 148
5082 0001307 6
9311 353
1857 15
49268004 9550
Satellite: ISS
Catalog Number: 25544
Epoch time: 20282
35863641 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 148
5082 deg
Eccentricity:
0001307
Arg of perigee: 6
9311 deg
Mean anomaly: 353
1857 deg
Mean motion: 15
49268004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 294
Coasting Arc #5 (Orbit 970)
---------------------------------------
Vector Time (GMT): 2020/283/08:32:52
927
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4732055
36 A = 6802946
31 meter
Y = -4749633
71 meter E =
0013290
Z = 1118149
07 I = 51
89722
XDOT = 4094
634279 Wp = 117
52040
YDOT = 2680
699361 meter/sec RA = 142
40848 deg
ZDOT = -5894
033092 TA = 50
41296
MA = 50
29567
Ha = 228
827 n
mi
Hp = 222
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15525116
01 X = 4779384
10
Y = -15582787
75 feet Y = -4696451
84 meter
Z = 3668468
08 Z = 1141250
81
XDOT = 13433
839498 XDOT = 4092
983797
YDOT = 8794
945410 feet/sec YDOT = 2726
479260 meter/sec
ZDOT = -19337
378910 ZDOT = -5874
146705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21582618
10 X = -6578382
00
Y = 4153041
45 feet Y = 1265847
04 meter
Z = 3775314
79 Z = 1150715
95
XDOT = -5958
348970 XDOT = -1816
104766
YDOT = -13331
340714 feet/sec YDOT = -4063
392650 meter/sec
ZDOT = -19245
433017 ZDOT = -5866
007984
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 20283
39069422
00016717 00000-0 10270-3 0 9041
2 25544 51
6427 143
4012 0001290 14
3420 345
7767 15
49265370 9716
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
39069422 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 143
4012 deg
Eccentricity:
0001290
Arg of perigee: 14
3420 deg
Mean anomaly: 345
7767 deg
Mean motion: 15
49265370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 971
Checksum: 291
Coasting Arc #6 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2020/283/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3003636
34 A = 6791462
04 meter
Y = -2941552
33 meter E =
0002650
Z = 5331509
24 I = 51
87336
XDOT = 5673
026193 Wp = 89
65624
YDOT = -5138
994829 meter/sec RA = 139
94637 deg
ZDOT = 360
562700 TA = 356
91385
MA = 356
91548
Ha = 228
772 n
mi
Hp = 222
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9854449
92 X = -2996417
50
Y = -9650762
24 feet Y = -2975100
77 meter
Z = 17491828
21 Z = 5316936
12
XDOT = 18612
290661 XDOT = 5728
318923
YDOT = -16860
219255 feet/sec YDOT = -5075
245820 meter/sec
ZDOT = 1182
948491 ZDOT = 388
254671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3053051
00 X = -930569
94
Y = -13538052
42 feet Y = -4126398
38 meter
Z = 17424450
22 Z = 5310972
43
XDOT = 23814
295030 XDOT = 7258
597125
YDOT = -3682
523545 feet/sec YDOT = -1122
433177 meter/sec
ZDOT = 1311
035529 ZDOT = 399
603629
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 20283
90672020
00016717 00000-0 10270-3 0 9053
2 25544 51
6435 140
8449 0000842 9
2454 350
8712 15
49310729 9796
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
90672020 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 140
8449 deg
Eccentricity:
0000842
Arg of perigee: 9
2454 deg
Mean anomaly: 350
8712 deg
Mean motion: 15
49310729 rev/day
Decay rate: 1
67170E-04 rev/day^2
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