[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 30th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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
212/08:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 222
6
214/23:32:45
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
8
219/03:44:00
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
5
223/13:07:30
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
5
Coasting Arc #1 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2020/211/14:45:07
864
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2696720
41 A = 6800442
14 meter
Y = -5540405
61 meter E =
0012859
Z = 2864231
49 I = 51
91467
XDOT = 5725
406782 Wp = 95
92883
YDOT = 146
016230 meter/sec RA = 137
31740 deg
ZDOT = -5089
790796 TA = 51
69064
MA = 51
57509
Ha = 228
785 n
mi
Hp = 222
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8847507
92 X = 2744561
78
Y = -18177183
77 feet Y = -5509981
79 meter
Z = 9397084
95 Z = 2877446
55
XDOT = 18784
142984 XDOT = 5748
071536
YDOT = 479
055874 feet/sec YDOT = 210
169130 meter/sec
ZDOT = -16698
788702 ZDOT = -5061
924185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12344732
56 X = -3762674
48
Y = 15973220
02 feet Y = 4868637
46 meter
Z = 9458193
89 Z = 2882857
50
XDOT = -17227
551348 XDOT = -5250
957651
YDOT = -3467
062838 feet/sec YDOT = -1056
760753 meter/sec
ZDOT = -16570
217023 ZDOT = -5050
602149
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 20211
65283524
00016717 00000-0 10270-3 0 9008
2 25544 51
6439 138
2843 0000862 338
5612 21
5502 15
49114854 38595
Satellite: ISS
Catalog Number: 25544
Epoch time: 20211
65283524 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 138
2843 deg
Eccentricity:
0000862
Arg of perigee: 338
5612 deg
Mean anomaly: 21
5502 deg
Mean motion: 15
49114854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 297
Coasting Arc #2 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2020/212/08:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5414340
20 A = 6802806
46 meter
Y = -3763814
11 meter E =
0007146
Z = -1662051
11 I = 51
93628
XDOT = 1596
671718 Wp = 139
38076
YDOT = 4819
683002 meter/sec RA = 133
81100 deg
ZDOT = -5732
225933 TA = 58
70437
MA = 58
63442
Ha = 228
881 n
mi
Hp = 222
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17763583
33 X = 5464099
09
Y = -12348471
48 feet Y = -3702988
66 meter
Z = -5452923
60 Z = -1635630
28
XDOT = 5238
424273 XDOT = 1570
501477
YDOT = 15812
608273 feet/sec YDOT = 4837
392521 meter/sec
ZDOT = -18806
515529 ZDOT = -5724
532965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4603344
04 X = -1403099
26
Y = -21169663
26 feet Y = -6452513
36 meter
Z = -5330909
63 Z = -1624861
26
XDOT = 15118
400439 XDOT = 4608
088454
YDOT = 1423
259398 feet/sec YDOT = 433
809464 meter/sec
ZDOT = -18771
141083 ZDOT = -5721
443802
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 20212
36244507
00016717 00000-0 10270-3 0 9016
2 25544 51
6402 134
7716 0000845 348
7699 11
3432 15
49121656 38704
Satellite: ISS
Catalog Number: 25544
Epoch time: 20212
36244507 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 134
7716 deg
Eccentricity:
0000845
Arg of perigee: 348
7699 deg
Mean anomaly: 11
3432 deg
Mean motion: 15
49121656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 294
Coasting Arc #3 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2020/213/08:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5076864
47 A = 6802637
79 meter
Y = 4189651
49 meter E =
0013924
Z = 1689310
85 I = 51
95842
XDOT = -1963
982335 Wp = 61
33834
YDOT = -4699
812297 meter/sec RA = 128
88471 deg
ZDOT = 5724
441804 TA = 317
06101
MA = 317
16962
Ha = 228
764 n
mi
Hp = 222
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16656379
50 X = -5131542
66
Y = 13745575
76 feet Y = 4132572
42 meter
Z = 5542358
42 Z = 1664517
56
XDOT = -6443
511597 XDOT = -1939
087291
YDOT = -15419
331684 feet/sec YDOT = -4721
636514 meter/sec
ZDOT = 18780
977048 ZDOT = 5714
961533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6672232
74 X = 2033696
54
Y = 20569726
57 feet Y = 6269652
66 meter
Z = 5427819
74 Z = 1654399
46
XDOT = -15254
005624 XDOT = -4649
420914
YDOT = -22
159536 feet/sec YDOT = -6
754226 meter/sec
ZDOT = 18737
354067 ZDOT = 5711
145520
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 20213
39460408
00016717 00000-0 10270-3 0 9021
2 25544 51
6400 129
6660 0000661 335
6174 24
4945 15
49167930 38868
Satellite: ISS
Catalog Number: 25544
Epoch time: 20213
39460408 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 129
6660 deg
Eccentricity:
0000661
Arg of perigee: 335
6174 deg
Mean anomaly: 24
4945 deg
Mean motion: 15
49167930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 303
Coasting Arc #4 (Orbit 3900)
---------------------------------------
Vector Time (GMT): 2020/214/08:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4725394
06 A = 6802661
49 meter
Y = -4566307
29 meter E =
0006800
Z = -1750613
47 I = 51
97944
XDOT = 2302
715058 Wp = 138
59821
YDOT = 4562
336929 meter/sec RA = 123
95848 deg
ZDOT = -5702
343446 TA = 60
47485
MA = 60
40706
Ha = 228
868 n
mi
Hp = 222
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15503261
35 X = 4784607
98
Y = -14981323
14 feet Y = -4513133
25 meter
Z = -5743482
52 Z = -1727516
59
XDOT = 7554
839430 XDOT = 2279
224662
YDOT = 14968
297010 feet/sec YDOT = 4587
956925 meter/sec
ZDOT = -18708
475874 ZDOT = -5691
214446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8586037
30 X = -2617024
17
Y = -19806207
75 feet Y = -6036932
12 meter
Z = -5636740
64 Z = -1718078
55
XDOT = 15265
999325 XDOT = 4653
076594
YDOT = -1324
836022 feet/sec YDOT = -403
810019 meter/sec
ZDOT = -18657
239860 ZDOT = -5686
726709
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 20214
36225577
00016717 00000-0 10270-3 0 9036
2 25544 51
6411 124
8782 0000914 348
4502 11
6627 15
49126324 39015
Satellite: ISS
Catalog Number: 25544
Epoch time: 20214
36225577 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 124
8782 deg
Eccentricity:
0000914
Arg of perigee: 348
4502 deg
Mean anomaly: 11
6627 deg
Mean motion: 15
49126324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3901
Checksum: 285
Coasting Arc #5 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2020/214/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4893362
25 A = 6800266
81 meter
Y = -3664121
45 meter E =
0004076
Z = -2980215
19 I = 51
98642
XDOT = 1189
909293 Wp = 110
21897
YDOT = 5661
370440 meter/sec RA = 120
77443 deg
ZDOT = -5013
705834 TA = 103
57422
MA = 103
52881
Ha = 228
793 n
mi
Hp = 222
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16054338
08 X = 4948447
71
Y = -12021395
83 feet Y = -3609092
01 meter
Z = -9777608
88 Z = -2956312
34
XDOT = 3903
901881 XDOT = 1150
866876
YDOT = 18574
050000 feet/sec YDOT = 5674
459163 meter/sec
ZDOT = -16449
166122 ZDOT = -5008
019990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18900396
20 X = 5760840
76
Y = 6868652
86 feet Y = 2093565
39 meter
Z = -9667160
69 Z = -2946550
58
XDOT = -12814
326618 XDOT = -3905
806753
YDOT = 12178
993232 feet/sec YDOT = 3712
157137 meter/sec
ZDOT = -16423
088931 ZDOT = -5005
757506
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 20215
00735385
00016717 00000-0 10270-3 0 9042
2 25544 51
6443 121
6849 0000551 319
9621 40
1488 15
49120618 39114
Satellite: ISS
Catalog Number: 25544
Epoch time: 20215
00735385 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 121
6849 deg
Eccentricity:
0000551
Arg of perigee: 319
9621 deg
Mean anomaly: 40
1488 deg
Mean motion: 15
49120618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 290
Coasting Arc #6 (Orbit 3926)
---------------------------------------
Vector Time (GMT): 2020/215/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4564703
64 A = 6800138
29 meter
Y = 4035508
84 meter E =
0013024
Z = 3006024
39 I = 52
00294
XDOT = -1632
305482 Wp = 80
06833
YDOT = -5578
406069 meter/sec RA = 115
85091 deg
ZDOT = 4993
990772 TA = 314
08854
MA = 314
19566
Ha = 228
869 n
mi
Hp = 222
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14976061
81 X = -4624091
82
Y = 13239858
38 feet Y = 3984130
69 meter
Z = 9862284
73 Z = 2983707
59
XDOT = -5355
332947 XDOT = -1594
062080
YDOT = -18301
857183 feet/sec YDOT = -5596
446354 meter/sec
ZDOT = 16384
484160 ZDOT = 4986
154187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19415017
00 X = -5917697
18
Y = -4965624
90 feet Y = -1513522
47 meter
Z = 9759130
16 Z = 2974582
87
XDOT = 11675
412060 XDOT = 3558
665596
YDOT = -13413
747528 feet/sec YDOT = -4088
510247 meter/sec
ZDOT = 16348
478840 ZDOT = 4983
016350
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 20216
03950922
00016717 00000-0 10270-3 0 9053
2 25544 51
6448 116
5788 0000639 339
9176 20
1949 15
49141180 39272
Satellite: ISS
Catalog Number: 25544
Epoch time: 20216
03950922 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 116
5788 deg
Eccentricity:
0000639
Arg of perigee: 339
9176 deg
Mean anomaly: 20
1949 deg
Mean motion: 15
49141180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 319
Coasting Arc #7 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2020/216/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4226902
37 A = 6800047
78 meter
Y = -4361080
24 meter E =
0004150
Z = -3060946
37 I = 52
01487
XDOT = 2052
882175 Wp = 102
65653
YDOT = 5462
496646 meter/sec RA = 110
92908 deg
ZDOT = -4954
371715 TA = 112
16525
MA = 112
12121
Ha = 228
843 n
mi
Hp = 222
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13867789
92 X = 4290223
04
Y = -14308006
04 feet Y = -4313457
71 meter
Z = -10042474
96 Z = -3040260
85
XDOT = 6735
177738 XDOT = 2015
711172
YDOT = 17921
576922 feet/sec YDOT = 5485
245996 meter/sec
ZDOT = -16254
500378 ZDOT = -4944
489736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19729997
38 X = 6013703
20
Y = 3110267
29 feet Y = 948009
47 meter
Z = -9946827
55 Z = -3031793
04
XDOT = -10446
883541 XDOT = -3184
210103
YDOT = 14501
573178 feet/sec YDOT = 4420
079505 meter/sec
ZDOT = -16209
050328 ZDOT = -4940
518540
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 20217
00715578
00016717 00000-0 10270-3 0 9068
2 25544 51
6436 111
7927 0000628 340
1093 20
0028 15
49122281 39426
Satellite: ISS
Catalog Number: 25544
Epoch time: 20217
00715578 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 111
7927 deg
Eccentricity:
0000628
Arg of perigee: 340
1093 deg
Mean anomaly: 20
0028 deg
Mean motion: 15
49122281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 278
Coasting Arc #8 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2020/217/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3846776
27 A = 6799915
24 meter
Y = 4672442
60 meter E =
0012927
Z = 3086473
78 I = 52
02578
XDOT = -2482
075588 Wp = 81
17154
YDOT = -5312
686065 meter/sec RA = 106
00699 deg
ZDOT = 4933
422217 TA = 314
02072
MA = 314
12717
Ha = 228
877 n
mi
Hp = 222
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12620657
06 X = -3913730
95
Y = 15329536
08 feet Y = 4629050
66 meter
Z = 10126226
31 Z = 3067625
79
XDOT = -8143
292611 XDOT = -2446
446167
YDOT = -17430
072393 feet/sec YDOT = -5340
243463 meter/sec
ZDOT = 16185
768427 ZDOT = 4921
451832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19866696
49 X = -6055369
09
Y = -1161093
86 feet Y = -353901
41 meter
Z = 10039041
40 Z = 3059899
82
XDOT = 9084
226449 XDOT = 2768
872222
YDOT = -15516
924104 feet/sec YDOT = -4729
558467 meter/sec
ZDOT = 16130
673411 ZDOT = 4916
629256
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 20218
03930958
00016717 00000-0 10270-3 0 9074
2 25544 51
6438 106
6863 0000673 344
2689 15
8440 15
49143124 39582
Satellite: ISS
Catalog Number: 25544
Epoch time: 20218
03930958 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 106
6863 deg
Eccentricity:
0000673
Arg of perigee: 344
2689 deg
Mean anomaly: 15
8440 deg
Mean motion: 15
49143124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 320
Coasting Arc #9 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2020/218/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3465700
50 A = 6799801
77 meter
Y = -4937130
82 meter E =
0004271
Z = -3141795
95 I = 52
03292
XDOT = 2883
922872 Wp = 95
56422
YDOT = 5133
278548 meter/sec RA = 101
08572 deg
ZDOT = -4891
487090 TA = 120
30597
MA = 120
26371
Ha = 228
869 n
mi
Hp = 222
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11370408
47 X = 3535912
07
Y = -16197935
76 feet Y = -4897982
19 meter
Z = -10307729
49 Z = -3124791
00
XDOT = 9461
689211 XDOT = 2850
066133
YDOT = 16841
465051 feet/sec YDOT = 5165
339498 meter/sec
ZDOT = -16048
185991 ZDOT = -4877
560521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19818792
69 X = 6040768
01
Y = -700633
91 feet Y = -213553
22 meter
Z = -10229035
52 Z = -3117810
03
XDOT = -7660
755838 XDOT = -2334
998379
YDOT = 16367
868402 feet/sec YDOT = 4988
926289 meter/sec
ZDOT = -15984
056114 ZDOT = -4871
940304
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 20219
00695307
00016717 00000-0 10270-3 0 9089
2 25544 51
6433 101
8992 0000759 351
3989 8
7148 15
49130400 39730
Satellite: ISS
Catalog Number: 25544
Epoch time: 20219
00695307 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 101
8992 deg
Eccentricity:
0000759
Arg of perigee: 351
3989 deg
Mean anomaly: 8
7148 deg
Mean motion: 15
49130400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 313
Coasting Arc #10 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2020/219/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3474829
96 A = 6793215
17 meter
Y = -2933402
14 meter E =
0006596
Z = 5043582
89 I = 52
01119
XDOT = 2828
375360 Wp = 49
86618
YDOT = -6829
682718 meter/sec RA = 100
18788 deg
ZDOT = -2017
705231 TA = 59
68457
MA = 59
61934
Ha = 229
047 n
mi
Hp = 222
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11400360
77 X = -3466267
77
Y = -9624022
78 feet Y = -2972212
46 meter
Z = 16547187
96 Z = 5026724
64
XDOT = 9279
446718 XDOT = 2914
337326
YDOT = -22407
095530 feet/sec YDOT = -6797
573095 meter/sec
ZDOT = -6619
767817 ZDOT = -2003
757860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13040644
64 X = -3974788
49
Y = -7422832
85 feet Y = -2262479
45 meter
Z = 16469444
72 Z = 5019886
75
XDOT = 4650
529583 XDOT = 1417
481417
YDOT = -22757
347154 feet/sec YDOT = -6936
439412 meter/sec
ZDOT = -6555
124785 ZDOT = -1998
002035
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 20219
20048056
00016717 00000-0 10270-3 0 9095
2 25544 51
6422 100
9425 0001007 7
2057 352
9107 15
49147068 39769
Satellite: ISS
Catalog Number: 25544
Epoch time: 20219
20048056 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 100
9425 deg
Eccentricity:
0001007
Arg of perigee: 7
2057 deg
Mean anomaly: 352
9107 deg
Mean motion: 15
49147068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3976
Checksum: 288
Coasting Arc #11 (Orbit 3990)
---------------------------------------
Vector Time (GMT): 2020/220/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3703521
06 A = 6793380
83 meter
Y = 2677737
60 meter E =
0012617
Z = -5037706
93 I = 52
01558
XDOT = -2264
456015 Wp = 100
18693
YDOT = 7010
181991 meter/sec RA = 95
26674 deg
ZDOT = 2063
671468 TA = 189
81411
MA = 189
83877
Ha = 229
023 n
mi
Hp = 222
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12150659
64 X = 3697772
33
Y = 8785228
35 feet Y = 2719120
97 meter
Z = -16527909
89 Z = -5019730
96
XDOT = -7429
317635 XDOT = -2352
701598
YDOT = 22999
284749 feet/sec YDOT = 6984
365774 meter/sec
ZDOT = 6770
575681 ZDOT = 2052
457659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13738879
88 X = 4187610
59
Y = 6228625
38 feet Y = 1898485
01 meter
Z = -16444998
56 Z = -5012435
56
XDOT = -2400
059632 XDOT = -731
538176
YDOT = 23013
078624 feet/sec YDOT = 7014
386365 meter/sec
ZDOT = 6718
536355 ZDOT = 2047
809881
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 20220
16812199
00016717 00000-0 10270-3 0 9101
2 25544 51
6416 96
1556 0001102 10
6285 349
4888 15
49115059 39919
Satellite: ISS
Catalog Number: 25544
Epoch time: 20220
16812199 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 96
1556 deg
Eccentricity:
0001102
Arg of perigee: 10
6285 deg
Mean anomaly: 349
4888 deg
Mean motion: 15
49115059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3991
Checksum: 304
Coasting Arc #12 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2020/221/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3896862
38 A = 6793398
08 meter
Y = -2416743
30 meter E =
0006963
Z = 5009213
34 I = 52
01625
XDOT = 1702
392924 Wp = 50
31902
YDOT = -7162
509125 meter/sec RA = 90
34489 deg
ZDOT = -2124
981999 TA = 60
31584
MA = 60
24654
Ha = 229
093 n
mi
Hp = 222
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12784981
57 X = -3893879
50
Y = -7928947
82 feet Y = -2460304
18 meter
Z = 16434426
97 Z = 4990291
44
XDOT = 5585
278623 XDOT = 1792
681496
YDOT = -23499
045687 feet/sec YDOT = -7142
966888 meter/sec
ZDOT = -6971
725720 ZDOT = -2116
493381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14282176
89 X = -4353207
52
Y = -5020432
98 feet Y = -1530227
97 meter
Z = 16347141
43 Z = 4982608
71
XDOT = 168
007100 XDOT = 51
208564
YDOT = -23117
667805 feet/sec YDOT = -7046
265147 meter/sec
ZDOT = -6932
251086 ZDOT = -2112
950131
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 20221
20027196
00016717 00000-0 10270-3 0 9113
2 25544 51
6400 91
0486 0001106 8
7561 351
3608 15
49138459 40077
Satellite: ISS
Catalog Number: 25544
Epoch time: 20221
20027196 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 91
0486 deg
Eccentricity:
0001106
Arg of perigee: 8
7561 deg
Mean anomaly: 351
3608 deg
Mean motion: 15
49138459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 274
Coasting Arc #13 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2020/222/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4088666
97 A = 6793534
39 meter
Y = 2127438
74 meter E =
0012434
Z = -5002177
05 I = 52
01596
XDOT = -1119
912159 Wp = 100
42651
YDOT = 7250
169254 meter/sec RA = 85
42358 deg
ZDOT = 2170
519809 TA = 190
65765
MA = 190
68403
Ha = 229
058 n
mi
Hp = 222
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13414261
71 X = 4088870
84
Y = 6979785
88 feet Y = 2173162
34 meter
Z = -16411342
02 Z = -4982315
63
XDOT = -3674
252491 XDOT = -1211
445498
YDOT = 23786
644533 feet/sec YDOT = 7237
133771 meter/sec
ZDOT = 7121
127983 ZDOT = 2164
857567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14762195
89 X = 4499517
31
Y = 3706288
96 feet Y = 1129676
87 meter
Z = -16319711
08 Z = -4974247
94
XDOT = 2076
989251 XDOT = 633
066324
YDOT = 22932
193762 feet/sec YDOT = 6989
732659 meter/sec
ZDOT = 7094
685915 ZDOT = 2162
460267
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 20222
16791230
00016717 00000-0 10270-3 0 9127
2 25544 51
6405 86
2614 0001169 14
6268 345
4916 15
49117218 40223
Satellite: ISS
Catalog Number: 25544
Epoch time: 20222
16791230 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 86
2614 deg
Eccentricity:
0001169
Arg of perigee: 14
6268 deg
Mean anomaly: 345
4916 deg
Mean motion: 15
49117218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 284
Coasting Arc #14 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2020/223/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244369
60 A = 6793548
31 meter
Y = -1840363
63 meter E =
0007402
Z = 4971612
52 I = 52
01268
XDOT = 545
410805 Wp = 51
31774
YDOT = -7309
616444 meter/sec RA = 80
50148 deg
ZDOT = -2233
468431 TA = 60
42379
MA = 60
35004
Ha = 229
147 n
mi
Hp = 222
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13925097
11 X = -4247623
68
Y = -6037938
42 feet Y = -1887845
50 meter
Z = 16311064
70 Z = 4950987
29
XDOT = 1789
405529 XDOT = 637
957399
YDOT = -23981
681248 feet/sec YDOT = -7302
999765 meter/sec
ZDOT = -7327
652332 ZDOT = -2230
594434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15087565
27 X = -4598689
89
Y = -2413678
58 feet Y = -735689
23 meter
Z = 16215899
33 Z = 4942606
12
XDOT = -4269
212218 XDOT = -1301
255884
YDOT = -22601
434749 feet/sec YDOT = -6888
917311 meter/sec
ZDOT = -7314
066094 ZDOT = -2229
327345
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 20223
20005913
00016717 00000-0 10270-3 0 9130
2 25544 51
6408 81
1543 0001225 14
2091 345
9093 15
49144393 40386
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
20005913 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 81
1543 deg
Eccentricity:
0001225
Arg of perigee: 14
2091 deg
Mean anomaly: 345
9093 deg
Mean motion: 15
49144393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 270
Coasting Arc #15 (Orbit 4043)
---------------------------------------
Vector Time (GMT): 2020/223/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3830001
85 A = 6797920
17 meter
Y = -4174419
34 meter E =
0011915
Z = 3749435
15 I = 52
02710
XDOT = 2231
730820 Wp = 77
76699
YDOT = -5930
087670 meter/sec RA = 78
56679 deg
ZDOT = -4308
566640 TA = 57
79624
MA = 57
68076
Ha = 228
957 n
mi
Hp = 222
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12565622
87 X = -3801250
05
Y = -13695601
52 feet Y = -4217088
49 meter
Z = 12301296
41 Z = 3730900
38
XDOT = 7321
951510 XDOT = 2318
805347
YDOT = -19455
668208 feet/sec YDOT = -5904
643892 meter/sec
ZDOT = -14135
717323 ZDOT = -4297
514513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5814117
50 X = 1772143
01
Y = 17713112
76 feet Y = 5398956
77 meter
Z = 12215889
10 Z = 3723403
00
XDOT = -13541
221648 XDOT = -4127
364358
YDOT = 14189
968049 feet/sec YDOT = 4325
102261 meter/sec
ZDOT = -14084
419068 ZDOT = -4292
930932
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 20223
58711185
00016717 00000-0 10270-3 0 9147
2 25544 51
6427 79
2384 0001375 1
5325 358
5829 15
49175968 40449
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
58711185 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 79
2384 deg
Eccentricity:
0001375
Arg of perigee: 1
5325 deg
Mean anomaly: 358
5829 deg
Mean motion: 15
49175968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4044
Checksum: 320
Coasting Arc #16 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2020/224/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4168293
15 A = 6798089
17 meter
Y = 3871980
45 meter E =
0005825
Z = -3726061
26 I = 52
01754
XDOT = -1753
162587 Wp = 88
54347
YDOT = 6057
030931 meter/sec RA = 73
64453 deg
ZDOT = 4338
990499 TA = 227
42022
MA = 227
46938
Ha = 229
027 n
mi
Hp = 222
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13675502
45 X = 4142784
66
Y = 12703347
95 feet Y = 3918450
80 meter
Z = -12224610
45 Z = -3705875
27
XDOT = -5751
845758 XDOT = -1841
840016
YDOT = 19872
148725 feet/sec YDOT = 6036
929822 meter/sec
ZDOT = 14235
533132 ZDOT = 4330
259228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7531496
33 X = -2295600
08
Y = -17144590
26 feet Y = -5225671
11 meter
Z = -12131574
71 Z = -3697703
97
XDOT = 12057
183362 XDOT = 3675
029489
YDOT = -15326
997508 feet/sec YDOT = -4671
668840 meter/sec
ZDOT = 14194
931175 ZDOT = 4326
615022
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 20224
55474982
00016717 00000-0 10270-3 0 9157
2 25544 51
6407 74
4505 0001193 13
2323 346
8858 15
49147401 40594
Satellite: ISS
Catalog Number: 25544
Epoch time: 20224
55474982 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 74
4505 deg
Eccentricity:
0001193
Arg of perigee: 13
2323 deg
Mean anomaly: 346
8858 deg
Mean motion: 15
49147401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 305
Coasting Arc #17 (Orbit 4074)
---------------------------------------
Vector Time (GMT): 2020/225/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466737
25 A = 6798214
94 meter
Y = -3566237
92 meter E =
0012157
Z = 3672045
37 I = 52
00802
XDOT = 1286
328480 Wp = 80
14930
YDOT = -6146
641533 meter/sec RA = 68
72212 deg
ZDOT = -4390
449403 TA = 56
54872
MA = 56
43254
Ha = 229
010 n
mi
Hp = 222
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14654649
77 X = -4444363
11
Y = -11700255
66 feet Y = -3616063
27 meter
Z = 12047392
95 Z = 3650402
00
XDOT = 4220
237795 XDOT = 1376
292616
YDOT = -20166
146762 feet/sec YDOT = -6131
753628 meter/sec
ZDOT = -14404
361559 ZDOT = -4383
982794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9113441
50 X = 2777776
97
Y = 16461893
36 feet Y = 5017585
10 meter
Z = 11947621
96 Z = 3641635
17
XDOT = -10531
755646 XDOT = -3210
079121
YDOT = 16297
395037 feet/sec YDOT = 4967
446007 meter/sec
ZDOT = -14374
197549 ZDOT = -4381
255413
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 20225
58689445
00016717 00000-0 10270-3 0 9164
2 25544 51
6413 69
3438 0001214 6
5977 353
5189 15
49162051 40751
Satellite: ISS
Catalog Number: 25544
Epoch time: 20225
58689445 = yrday
fracday
Element set: 916
Inclination: 51
6413 deg
RA of node: 69
3438 deg
Eccentricity:
0001214
Arg of perigee: 6
5977 deg
Mean anomaly: 353
5189 deg
Mean motion: 15
49162051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4075
Checksum: 319
Coasting Arc #18 (Orbit 4089)
---------------------------------------
Vector Time (GMT): 2020/226/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4757243
38 A = 6798331
69 meter
Y = 3211815
79 meter E =
0005756
Z = -3647468
73 I = 51
99451
XDOT = -799
965999 Wp = 86
61730
YDOT = 6197
582595 meter/sec RA = 63
79812 deg
ZDOT = 4420
321751 TA = 230
48741
MA = 230
53831
Ha = 229
070 n
mi
Hp = 222
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15607753
87 X = 4738691
50
Y = 10537453
40 feet Y = 3264911
21 meter
Z = -11966760
91 Z = -3624404
92
XDOT = -2624
560365 XDOT = -890
680989
YDOT = 20333
276230 feet/sec YDOT = 6188
129276 meter/sec
ZDOT = 14502
367951 ZDOT = 4416
215965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10708937
99 X = -3264084
30
Y = -15572165
77 feet Y = -4746396
13 meter
Z = -11860420
39 Z = -3615056
13
XDOT = 8881
674772 XDOT = 2707
134471
YDOT = -17122
853250 feet/sec YDOT = -5219
045671 meter/sec
ZDOT = 14483
088360 ZDOT = 4414
445332
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 20226
55453100
00016717 00000-0 10270-3 0 9170
2 25544 51
6408 64
5556 0001128 22
0792 338
0406 15
49151332 40902
Satellite: ISS
Catalog Number: 25544
Epoch time: 20226
55453100 = yrday
fracday
Element set: 917
Inclination: 51
6408 deg
RA of node: 64
5556 deg
Eccentricity:
0001128
Arg of perigee: 22
0792 deg
Mean anomaly: 338
0406 deg
Mean motion: 15
49151332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4090
Checksum: 276
- 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