[list_settings.list_name] Current ISS TLEs @ 06:30 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
Epoch rev: 979
Checksum: 303
Coasting Arc #7 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2020/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3163688
14 A = 6791572
93 meter
Y = 2766966
00 meter E =
0014996
Z = -5347777
19 I = 51
89777
XDOT = -5267
929115 Wp = 84
86281
YDOT = 5540
931297 meter/sec RA = 135
01567 deg
ZDOT = -248
841421 TA = 182
76379
MA = 182
77209
Ha = 228
734 n
mi
Hp = 222
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10379554
25 X = 3158488
62
Y = 9077972
44 feet Y = 2802315
50 meter
Z = -17545200
74 Z = -5332421
75
XDOT = -17283
232004 XDOT = -5328
289216
YDOT = 18178
908455 feet/sec YDOT = 5481
684039 meter/sec
ZDOT = -816
408862 ZDOT = -274
577835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4035525
68 X = 1230028
23
Y = 13279523
13 feet Y = 4047598
65 meter
Z = -17474198
03 Z = -5326135
56
XDOT = -23344
159317 XDOT = -7115
299760
YDOT = 5860
050278 feet/sec YDOT = 1786
143325 meter/sec
ZDOT = -935
477797 ZDOT = -285
133632
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 20284
87427374
00016717 00000-0 10270-3 0 9061
2 25544 51
6429 136
0579 0000875 9
6709 350
4458 15
49268503 9945
Satellite: ISS
Catalog Number: 25544
Epoch time: 20284
87427374 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 136
0579 deg
Eccentricity:
0000875
Arg of perigee: 9
6709 deg
Mean anomaly: 350
4458 deg
Mean motion: 15
49268503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 340
Coasting Arc #8 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2020/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3301012
01 A = 6791410
24 meter
Y = -2579177
66 meter E =
0002670
Z = 5343238
22 I = 51
92173
XDOT = 4851
946453 Wp = 78
30651
YDOT = -5929
834036 meter/sec RA = 130
08566 deg
ZDOT = 135
638145 TA = 10
40779
MA = 10
40227
Ha = 228
802 n
mi
Hp = 222
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10830091
90 X = -3297880
09
Y = -8461868
95 feet Y = -2616074
29 meter
Z = 17530309
12 Z = 5327210
77
XDOT = 15918
459491 XDOT = 4917
236181
YDOT = -19454
836076 feet/sec YDOT = -5875
211029 meter/sec
ZDOT = 445
007038 ZDOT = 159
365880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4968130
17 X = -1514286
08
Y = -12915298
30 feet Y = -3936582
92 meter
Z = 17456191
08 Z = 5320647
04
XDOT = 22759
125030 XDOT = 6936
981309
YDOT = -8006
974212 feet/sec YDOT = -2440
525740 meter/sec
ZDOT = 554
808338 ZDOT = 169
105582
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 20285
90632619
00016717 00000-0 10270-3 0 9077
2 25544 51
6438 130
9506 0000913 11
5667 348
5504 15
49313534 10101
Satellite: ISS
Catalog Number: 25544
Epoch time: 20285
90632619 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 130
9506 deg
Eccentricity:
0000913
Arg of perigee: 11
5667 deg
Mean anomaly: 348
5504 deg
Mean motion: 15
49313534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1010
Checksum: 292
Coasting Arc #9 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2020/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3443012
61 A = 6791540
21 meter
Y = 2393336
17 meter E =
0015189
Z = -5355608
78 I = 51
94161
XDOT = -4390
419732 Wp = 86
01616
YDOT = 6263
931691 meter/sec RA = 125
15752 deg
ZDOT = -22
290193 TA = 183
76607
MA = 183
77751
Ha = 228
802 n
mi
Hp = 222
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11295973
12 X = 3442008
35
Y = 7852152
78 feet Y = 2431832
54 meter
Z = -17570894
94 Z = -5338886
42
XDOT = -14404
264213 XDOT = -4460
030327
YDOT = 20550
956993 feet/sec YDOT = 6214
445649 meter/sec
ZDOT = -73
130554 ZDOT = -43
786622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5899546
75 X = 1798181
85
Y = 12536447
14 feet Y = 3821109
09 meter
Z = -17493556
02 Z = -5332035
87
XDOT = -21886
605695 XDOT = -6671
037416
YDOT = 10054
298096 feet/sec YDOT = 3064
550060 meter/sec
ZDOT = -172
630353 ZDOT = -52
617732
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 20286
87387524
00016717 00000-0 10270-3 0 9087
2 25544 51
6429 126
1631 0001072 17
1251 342
9935 15
49270802 10257
Satellite: ISS
Catalog Number: 25544
Epoch time: 20286
87387524 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 126
1631 deg
Eccentricity:
0001072
Arg of perigee: 17
1251 deg
Mean anomaly: 342
9935 deg
Mean motion: 15
49270802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 298
Coasting Arc #10 (Orbit 1040)
---------------------------------------
Vector Time (GMT): 2020/287/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3560978
72 A = 6791404
68 meter
Y = -2197835
29 meter E =
0003015
Z = 5346626
33 I = 51
95987
XDOT = 3921
082700 Wp = 68
51772
YDOT = -6583
389557 meter/sec RA = 120
23064 deg
ZDOT = -93
581181 TA = 22
37729
MA = 22
36414
Ha = 228
893 n
mi
Hp = 222
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11683001
03 X = -3562108
26
Y = -7210745
71 feet Y = -2237662
67 meter
Z = 17541424
96 Z = 5329325
75
XDOT = 12864
444554 XDOT = 3994
863292
YDOT = -21599
047103 feet/sec YDOT = -6539
128669 meter/sec
ZDOT = -307
024872 ZDOT = -74
354303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6765507
86 X = -2062126
80
Y = -12063007
88 feet Y = -3676804
80 meter
Z = 17461406
04 Z = 5322236
56
XDOT = 20909
651036 XDOT = 6373
261636
YDOT = -12048
020364 feet/sec YDOT = -3672
236607 meter/sec
ZDOT = -218
006076 ZDOT = -66
448252
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 20287
90592444
00016717 00000-0 10270-3 0 9092
2 25544 51
6427 121
0563 0001055 21
5754 338
5440 15
49312807 10413
Satellite: ISS
Catalog Number: 25544
Epoch time: 20287
90592444 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 121
0563 deg
Eccentricity:
0001055
Arg of perigee: 21
5754 deg
Mean anomaly: 338
5440 deg
Mean motion: 15
49312807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1041
Checksum: 289
Coasting Arc #11 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2020/288/05:45:05
000
Vector Time (MET): N/A
Weight (LBS) : 938498
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747894
02 A = 6793934
24 meter
Y = 960759
10 meter E =
0007844
Z = 4758195
48 I = 51
97359
XDOT = 1345
229551 Wp = 107
43448
YDOT = -7024
122832 meter/sec RA = 118
37184 deg
ZDOT = 2754
582984 TA = 315
38680
MA = 315
44991
Ha = 228
982 n
mi
Hp = 222
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15577080
13 X = -4781397
46
Y = 3152096
80 feet Y = 907477
77 meter
Z = 15610877
55 Z = 4735050
40
XDOT = 4413
482778 XDOT = 1410
295115
YDOT = -23045
022416 feet/sec YDOT = -7008
715502 meter/sec
ZDOT = 9037
345747 ZDOT = 2761
276195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7991172
12 X = 2435709
26
Y = 13858371
97 feet Y = 4224031
78 meter
Z = 15503784
44 Z = 4725553
50
XDOT = -22218
200181 XDOT = -6772
107415
YDOT = 2644
374792 feet/sec YDOT = 806
005437 meter/sec
ZDOT = 9068
386775 ZDOT = 2764
044289
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 20288
29294416
00016717 00000-0 10270-3 0 9105
2 25544 51
6416 119
1425 0001343 23
1504 336
9706 15
49314033 10473
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
29294416 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 119
1425 deg
Eccentricity:
0001343
Arg of perigee: 23
1504 deg
Mean anomaly: 336
9706 deg
Mean motion: 15
49314033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 282
Coasting Arc #12 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2020/288/08:50:45
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4744366
98 A = 6794113
07 meter
Y = 1056594
94 meter E =
0008017
Z = 4741428
09 I = 51
97742
XDOT = 1230
516766 Wp = 106
23474
YDOT = -7030
482501 meter/sec RA = 117
73761 deg
ZDOT = 2791
886942 TA = 316
18949
MA = 316
25306
Ha = 229
089 n
mi
Hp = 222
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15565508
48 X = -4778860
91
Y = 3466518
83 feet Y = 1003347
51 meter
Z = 15555866
42 Z = 4718297
72
XDOT = 4037
128499 XDOT = 1295
480762
YDOT = -23065
887471 feet/sec YDOT = -7016
358531 meter/sec
ZDOT = 9159
734061 ZDOT = 2798
022689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15677430
79 X = 4778480
90
Y = 3440685
15 feet Y = 1048720
83 meter
Z = 15448839
33 Z = 4708806
23
XDOT = -13049
826912 XDOT = -3977
587243
YDOT = 18115
600397 feet/sec YDOT = 5521
635001 meter/sec
ZDOT = 9188
197661 ZDOT = 2800
562647
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 20288
42195110
00016717 00000-0 10270-3 0 9112
2 25544 51
6431 118
5047 0001479 25
3523 334
7699 15
49275731 10498
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
42195110 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 118
5047 deg
Eccentricity:
0001479
Arg of perigee: 25
3523 deg
Mean anomaly: 334
7699 deg
Mean motion: 15
49275731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 304
Coasting Arc #13 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2020/289/02:17:30
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1266938
93 A = 6801901
06 meter
Y = -6408878
86 meter E =
0014084
Z = 1872621
22 I = 52
01114
XDOT = 5128
755466 Wp = 107
52149
YDOT = -647
496889 meter/sec RA = 114
11827 deg
ZDOT = -5655
068253 TA = 52
01431
MA = 51
88720
Ha = 228
902 n
mi
Hp = 222
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4156623
78 X = 1329414
54
Y = -21026505
45 feet Y = -6394361
56 meter
Z = 6143770
42 Z = 1878927
88
XDOT = 16826
625545 XDOT = 5163
084257
YDOT = -2124
333626 feet/sec YDOT = -589
951993 meter/sec
ZDOT = -18553
373535 ZDOT = -5630
070995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15535587
68 X = -4735247
12
Y = -14753867
70 feet Y = -4496978
88 meter
Z = 6173027
69 Z = 1881538
84
XDOT = 6227
150454 XDOT = 1898
035458
YDOT = -14313
570313 feet/sec YDOT = -4362
776232 meter/sec
ZDOT = -18437
708301 ZDOT = -5619
813490
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 20289
13148332
00016717 00000-0 10270-3 0 9126
2 25544 51
6396 114
9915 0001475 27
0955 333
0272 15
49303817 10605
Satellite: ISS
Catalog Number: 25544
Epoch time: 20289
13148332 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 114
9915 deg
Eccentricity:
0001475
Arg of perigee: 27
0955 deg
Mean anomaly: 333
0272 deg
Mean motion: 15
49303817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 295
Coasting Arc #14 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2020/290/02:17:30
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -783276
40 A = 6802029
20 meter
Y = 6510729
24 meter E =
0008845
Z = -1794628
21 I = 52
02473
XDOT = -5036
162360 Wp = 38
12112
YDOT = 956
588191 meter/sec RA = 109
19478 deg
ZDOT = 5690
146590 TA = 302
31486
MA = 302
40049
Ha = 228
966 n
mi
Hp = 221
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2569804
46 X = -847305
67
Y = 21360660
24 feet Y = 6501611
92 meter
Z = -5887887
83 Z = -1798589
19
XDOT = -16522
842387 XDOT = -5074
124943
YDOT = 3138
412699 feet/sec YDOT = 900
058413 meter/sec
ZDOT = 18668
459942 ZDOT = 5665
590120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16899437
79 X = 5150948
64
Y = 13306894
41 feet Y = 4055941
42 meter
Z = -5906309
12 Z = -1800243
02
XDOT = -5042
755217 XDOT = -1537
031790
YDOT = 14608
329404 feet/sec YDOT = 4452
618802 meter/sec
ZDOT = 18554
823900 ZDOT = 5655
510325
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 20290
09902599
00016717 00000-0 10270-3 0 9137
2 25544 51
6401 110
2035 0001495 34
6492 325
4755 15
49300674 10751
Satellite: ISS
Catalog Number: 25544
Epoch time: 20290
09902599 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 110
2035 deg
Eccentricity:
0001495
Arg of perigee: 34
6492 deg
Mean anomaly: 325
4755 deg
Mean motion: 15
49300674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 292
Coasting Arc #15 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2020/291/02:17:30
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 323762
49 A = 6802213
67 meter
Y = -6578389
41 meter E =
0014149
Z = 1676195
90 I = 52
03548
XDOT = 4929
771333 Wp = 109
63615
YDOT = -1227
528852 meter/sec RA = 104
27153 deg
ZDOT = -5735
085841 TA = 52
13391
MA = 52
00600
Ha = 228
977 n
mi
Hp = 221
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1062212
90 X = 389157
76
Y = -21582642
43 feet Y = -6574403
11 meter
Z = 5499330
37 Z = 1677927
91
XDOT = 16173
790461 XDOT = 4970
990003
YDOT = -4027
325629 feet/sec YDOT = -1172
170515 meter/sec
ZDOT = -18815
898428 ZDOT = -5711
038150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18080463
23 X = -5510925
19
Y = -11829883
12 feet Y = -3605748
37 meter
Z = 5507458
56 Z = 1678673
37
XDOT = 3934
471664 XDOT = 1199
226963
YDOT = -14774
229180 feet/sec YDOT = -4503
185054 meter/sec
ZDOT = -18704
605162 ZDOT = -5701
163653
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 20291
13106933
00016717 00000-0 10270-3 0 9142
2 25544 51
6403 105
0953 0001596 31
9789 328
1458 15
49300965 10916
Satellite: ISS
Catalog Number: 25544
Epoch time: 20291
13106933 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 105
0953 deg
Eccentricity:
0001596
Arg of perigee: 31
9789 deg
Mean anomaly: 328
1458 deg
Mean motion: 15
49300965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 302
Coasting Arc #16 (Orbit 1096)
---------------------------------------
Vector Time (GMT): 2020/291/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4321779
76 A = 6793607
81 meter
Y = 1930142
47 meter E =
0007338
Z = 4868281
76 I = 52
00830
XDOT = -402
501109 Wp = 108
26981
YDOT = -7231
941607 meter/sec RA = 102
48362 deg
ZDOT = 2504
626505 TA = 317
20272
MA = 317
25983
Ha = 229
133 n
mi
Hp = 222
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14179067
46 X = -4366689
95
Y = 6332488
42 feet Y = 1881562
39 meter
Z = 15972053
01 Z = 4847178
50
XDOT = -1320
541697 XDOT = -333
767806
YDOT = -23726
842543 feet/sec YDOT = -7236
058212 meter/sec
ZDOT = 8217
278560 ZDOT = 2502
838605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12495354
46 X = 3808584
04
Y = -9387405
75 feet Y = -2861281
27 meter
Z = 15874368
38 Z = 4838507
48
XDOT = 5998
589991 XDOT = 1828
370229
YDOT = 21896
199332 feet/sec YDOT = 6673
961556 meter/sec
ZDOT = 8209
139368 ZDOT = 2502
145679
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 20291
51808538
00016717 00000-0 10270-3 0 9155
2 25544 51
6392 103
1783 0001467 31
1563 328
9673 15
49269461 10970
Satellite: ISS
Catalog Number: 25544
Epoch time: 20291
51808538 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 103
1783 deg
Eccentricity:
0001467
Arg of perigee: 31
1563 deg
Mean anomaly: 328
9673 deg
Mean motion: 15
49269461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1097
Checksum: 319
Coasting Arc #17 (Orbit 1111)
---------------------------------------
Vector Time (GMT): 2020/292/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4165162
91 A = 6793320
21 meter
Y = -2165532
24 meter E =
0013098
Z = -4922589
22 I = 52
01363
XDOT = 925
232607 Wp = 69
74017
YDOT = 7208
267308 meter/sec RA = 97
55975 deg
ZDOT = -2388
916567 TA = 176
92225
MA = 176
91418
Ha = 228
972 n
mi
Hp = 222
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13665232
66 X = 4212980
77
Y = -7104764
55 feet Y = -2118687
15 meter
Z = -16150227
10 Z = -4902239
73
XDOT = 3035
540049 XDOT = 856
163135
YDOT = 23649
170958 feet/sec YDOT = 7218
227671 meter/sec
ZDOT = -7837
652780 ZDOT = -2384
589966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11647858
94 X = -3550267
41
Y = 10226333
00 feet Y = 3116986
30 meter
Z = -16056014
26 Z = -4893873
15
XDOT = -7971
482691 XDOT = -2429
707924
YDOT = -21350
156293 feet/sec YDOT = -6507
527638 meter/sec
ZDOT = -7817
789748 ZDOT = -2382
862315
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 20292
48562408
00016717 00000-0 10270-3 0 9166
2 25544 51
6390 98
3898 0001395 41
8407 318
2850 15
49304919 11120
Satellite: ISS
Catalog Number: 25544
Epoch time: 20292
48562408 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 98
3898 deg
Eccentricity:
0001395
Arg of perigee: 41
8407 deg
Mean anomaly: 318
2850 deg
Mean motion: 15
49304919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1112
Checksum: 320
Coasting Arc #18 (Orbit 1127)
---------------------------------------
Vector Time (GMT): 2020/293/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3981342
48 A = 6793198
04 meter
Y = 2391574
61 meter E =
0006901
Z = 4952760
41 I = 52
01710
XDOT = -1456
601585 Wp = 110
21706
YDOT = -7168
663861 meter/sec RA = 92
63598 deg
ZDOT = 2285
780847 TA = 317
52179
MA = 317
57518
Ha = 229
128 n
mi
Hp = 221
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13062147
25 X = -4031848
19
Y = 7846373
38 feet Y = 2346769
97 meter
Z = 16249213
95 Z = 4933297
44
XDOT = -4778
876590 XDOT = -1387
434469
YDOT = -23519
238389 feet/sec YDOT = -7184
565895 meter/sec
ZDOT = 7499
280995 ZDOT = 2278
873035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10696594
84 X = 3260322
11
Y = -10985856
74 feet Y = -3348489
13 meter
Z = 16159085
07 Z = 4925289
13
XDOT = 9944
882316 XDOT = 3031
200130
YDOT = 20690
711434 feet/sec YDOT = 6306
528845 meter/sec
ZDOT = 7467
495790 ZDOT = 2276
092717
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 20293
51766416
00016717 00000-0 10270-3 0 9177
2 25544 51
6398 93
2817 0001384 39
2115 320
9135 15
49287004 11286
Satellite: ISS
Catalog Number: 25544
Epoch time: 20293
51766416 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 93
2817 deg
Eccentricity:
0001384
Arg of perigee: 39
2115 deg
Mean anomaly: 320
9135 deg
Mean motion: 15
49287004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1128
Checksum: 307
Coasting Arc #19 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2020/294/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 953607
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3806337
68 A = 6792931
25 meter
Y = -2596986
39 meter E =
0013848
Z = -5003908
68 I = 52
01811
XDOT = 1974
571877 Wp = 71
80014
YDOT = 7065
890104 meter/sec RA = 87
71309 deg
ZDOT = -2165
850543 TA = 177
15207
MA = 177
14418
Ha = 229
041 n
mi
Hp = 221
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12487984
51 X = 3859401
73
Y = -8520296
55 feet Y = -2554124
38 meter
Z = -16417023
23 Z = -4985289
75
XDOT = 6478
254191 XDOT = 1905
932901
YDOT = 23182
054148 feet/sec YDOT = 7087
587447 meter/sec
ZDOT = -7105
808868 ZDOT = -2156
425189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9769756
67 X = -2977821
83
Y = 11658529
16 feet Y = 3553519
69 meter
Z = -16330781
20 Z = -4977622
11
XDOT = -11801
996344 XDOT = -3597
248486
YDOT = -19779
373385 feet/sec YDOT = -6028
753008 meter/sec
ZDOT = -7062
390875 ZDOT = -2152
616739
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 20294
48519856
00016717 00000-0 10270-3 0 9189
2 25544 51
6411 88
4938 0001523 52
1168 308
0119 15
49319551 11438
Satellite: ISS
Catalog Number: 25544
Epoch time: 20294
48519856 = yrday
fracday
Element set: 918
Inclination: 51
6411 deg
RA of node: 88
4938 deg
Eccentricity:
0001523
Arg of perigee: 52
1168 deg
Mean anomaly: 308
0119 deg
Mean motion: 15
49319551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 311
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