[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 13th 2020
- spaceflight nasa gov will be taken offline by October 2020 *
- Do you use any data hosted on this site? *
- Please let us know how you use the data at the survey link below *
- *
- https://www surveymonkey com/r/KRLJMCN *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13864 993 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
263/20:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
7
267/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
7
Coasting Arc #1 (Orbit 538)
---------------------------------------
Vector Time (GMT): 2020/255/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3172700
16 A = 6795009
56 meter
Y = -3723120
64 meter E =
0011611
Z = -4727622
54 I = 51
24714
XDOT = 3372
664425 Wp = 107
82774
YDOT = -6310
155047 meter/sec RA = 280
43774 deg
ZDOT = 2708
050892 TA = 189
15635
MA = 189
17754
Ha = 229
431 n
mi
Hp = 222
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10409121
27 X = -3107867
24
Y = -12214962
73 feet Y = -3758237
54 meter
Z = -15510572
63 Z = -4742876
79
XDOT = 11065
171998 XDOT = 3429
821663
YDOT = -20702
608422 feet/sec YDOT = -6272
119914 meter/sec
ZDOT = 8884
681403 ZDOT = 2724
572776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8644366
48 X = 2634802
90
Y = 13440498
11 feet Y = 4096663
82 meter
Z = -15580786
95 Z = -4749023
86
XDOT = -12597
853160 XDOT = -3839
825643
YDOT = 18482
772752 feet/sec YDOT = 5633
549135 meter/sec
ZDOT = 8961
090105 ZDOT = 2731
340264
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 20255
51832687
00016717 00000-0 10270-3 0 9001
2 25544 51
6436 281
2497 0000676 91
0501 269
0727 15
48928011 5394
Satellite: ISS
Catalog Number: 25544
Epoch time: 20255
51832687 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 281
2497 deg
Eccentricity:
0000676
Arg of perigee: 91
0501 deg
Mean anomaly: 269
0727 deg
Mean motion: 15
48928011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 539
Checksum: 309
Coasting Arc #2 (Orbit 554)
---------------------------------------
Vector Time (GMT): 2020/256/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3477825
74 A = 6794895
83 meter
Y = 3429226
90 meter E =
0008377
Z = 4718859
95 I = 51
24007
XDOT = -2815
350065 Wp = 65
41727
YDOT = 6592
435293 meter/sec RA = 275
46540 deg
ZDOT = -2708
604191 TA = 51
57498
MA = 51
49981
Ha = 229
298 n
mi
Hp = 222
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11410189
45 X = 3416299
21
Y = 11250744
44 feet Y = 3467774
43 meter
Z = 15481823
98 Z = 4735604
35
XDOT = -9236
712811 XDOT = -2875
702628
YDOT = 21628
724714 feet/sec YDOT = 6560
614575 meter/sec
ZDOT = -8886
496688 ZDOT = -2722
426588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9976929
87 X = -3040968
22
Y = -12443433
35 feet Y = -3792758
48 meter
Z = 15558932
62 Z = 4742362
66
XDOT = 10626
203893 XDOT = 3238
866947
YDOT = -19740
837977 feet/sec YDOT = -6017
007415 meter/sec
ZDOT = -8950
451829 ZDOT = -2728
097717
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 20256
55060863
00016717 00000-0 10270-3 0 9016
2 25544 51
6415 276
1444 0000759 96
2151 263
9085 15
48963693 5559
Satellite: ISS
Catalog Number: 25544
Epoch time: 20256
55060863 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 276
1444 deg
Eccentricity:
0000759
Arg of perigee: 96
2151 deg
Mean anomaly: 263
9085 deg
Mean motion: 15
48963693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 555
Checksum: 319
Coasting Arc #3 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2020/257/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3774659
66 A = 6794988
54 meter
Y = -3101095
25 meter E =
0011611
Z = -4734248
04 I = 51
23850
XDOT = 2219
853493 Wp = 108
23931
YDOT = -6808
338771 meter/sec RA = 270
49292 deg
ZDOT = 2691
691202 TA = 188
57279
MA = 188
59264
Ha = 229
409 n
mi
Hp = 222
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12384054
01 X = -3716705
66
Y = -10174197
03 feet Y = -3142982
23 meter
Z = -15532309
83 Z = -4752442
90
XDOT = 7282
983902 XDOT = 2282
746811
YDOT = -22337
069460 feet/sec YDOT = -6783
163083 meter/sec
ZDOT = 8831
007880 ZDOT = 2702
627141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11260424
71 X = 3432177
45
Y = 11290305
48 feet Y = 3441285
11 meter
Z = -15616131
56 Z = -4759796
90
XDOT = -8478
928540 XDOT = -2584
377419
YDOT = 20732
488930 feet/sec YDOT = 6319
262626 meter/sec
ZDOT = 8881
640571 ZDOT = 2707
124046
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 20257
51837327
00016717 00000-0 10270-3 0 9021
2 25544 51
6420 271
3583 0000591 97
1328 262
9889 15
48920527 5703
Satellite: ISS
Catalog Number: 25544
Epoch time: 20257
51837327 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 271
3583 deg
Eccentricity:
0000591
Arg of perigee: 97
1328 deg
Mean anomaly: 262
9889 deg
Mean motion: 15
48920527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 318
Coasting Arc #4 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2020/258/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4022181
65 A = 6794859
53 meter
Y = 2759260
80 meter E =
0008232
Z = 4725660
67 I = 51
23836
XDOT = -1621
457532 Wp = 64
78559
YDOT = 6988
473624 meter/sec RA = 265
51922 deg
ZDOT = -2693
266293 TA = 52
04241
MA = 51
96806
Ha = 229
247 n
mi
Hp = 222
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13196134
01 X = 3968073
51
Y = 9052692
91 feet Y = 2803937
34 meter
Z = 15504136
07 Z = 4745067
14
XDOT = -5319
742559 XDOT = -1686
402025
YDOT = 22928
063072 feet/sec YDOT = 6969
978104 meter/sec
ZDOT = -8836
175503 ZDOT = -2701
300593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12349607
00 X = -3764160
21
Y = -10039683
60 feet Y = -3060095
56 meter
Z = 15593569
09 Z = 4752919
86
XDOT = 6286
413423 XDOT = 1916
098811
YDOT = -21551
105443 feet/sec YDOT = -6568
776939 meter/sec
ZDOT = -8873
410116 ZDOT = -2704
615403
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 20258
55065329
00016717 00000-0 10270-3 0 9032
2 25544 51
6410 266
2518 0000650 94
4392 265
6832 15
48961721 5866
Satellite: ISS
Catalog Number: 25544
Epoch time: 20258
55065329 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 266
2518 deg
Eccentricity:
0000650
Arg of perigee: 94
4392 deg
Mean anomaly: 265
6832 deg
Mean motion: 15
48961721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 312
Coasting Arc #5 (Orbit 600)
---------------------------------------
Vector Time (GMT): 2020/259/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4255782
18 A = 6794956
57 meter
Y = -2385421
79 meter E =
0011740
Z = -4740959
05 I = 51
24132
XDOT = 997
427945 Wp = 107
78694
YDOT = -7096
645923 meter/sec RA = 260
54682 deg
ZDOT = 2677
325228 TA = 188
86933
MA = 188
89009
Ha = 229
446 n
mi
Hp = 222
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13962539
98 X = -4205762
76
Y = -7826186
98 feet Y = -2432733
60 meter
Z = -15554327
58 Z = -4761510
12
XDOT = 3272
401393 XDOT = 1063
705867
YDOT = -23282
959065 feet/sec YDOT = -7085
121226 meter/sec
ZDOT = 8783
875420 ZDOT = 2682
331688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13359035
12 X = 4071833
91
Y = 8647651
59 feet Y = 2635804
21 meter
Z = -15649061
77 Z = -4769834
03
XDOT = -3978
854088 XDOT = -1212
754726
YDOT = 22072
509064 feet/sec YDOT = 6727
700763 meter/sec
ZDOT = 8807
124589 ZDOT = 2684
411575
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 20259
51841675
00016717 00000-0 10270-3 0 9046
2 25544 51
6402 261
4657 0000678 90
6789 269
4438 15
48917805 6012
Satellite: ISS
Catalog Number: 25544
Epoch time: 20259
51841675 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 261
4657 deg
Eccentricity:
0000678
Arg of perigee: 90
6789 deg
Mean anomaly: 269
4438 deg
Mean motion: 15
48917805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 601
Checksum: 332
Coasting Arc #6 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2020/260/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438652
53 A = 6794862
40 meter
Y = 2005605
48 meter E =
0008092
Z = 4732908
54 I = 51
24652
XDOT = -375
804189 Wp = 64
28940
YDOT = 7169
620236 meter/sec RA = 255
57374 deg
ZDOT = -2678
696167 TA = 52
37881
MA = 52
30539
Ha = 229
224 n
mi
Hp = 222
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14562508
31 X = 4392905
78
Y = 6580070
46 feet Y = 2054986
28 meter
Z = 15527915
17 Z = 4754358
33
XDOT = -1232
953377 XDOT = -442
937641
YDOT = 23522
376102 feet/sec YDOT = 7165
042132 meter/sec
ZDOT = -8788
373251 ZDOT = -2680
685315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14159070
40 X = -4315684
66
Y = -7197468
64 feet Y = -2193788
44 meter
Z = 15626813
35 Z = 4763052
71
XDOT = 1660
263712 XDOT = 506
048379
YDOT = -22417
107923 feet/sec YDOT = -6832
734495 meter/sec
ZDOT = -8797
683395 ZDOT = -2681
533899
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 20260
55069733
00016717 00000-0 10270-3 0 9050
2 25544 51
6386 256
3593 0000554 93
7238 266
3975 15
48946940 6172
Satellite: ISS
Catalog Number: 25544
Epoch time: 20260
55069733 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 256
3593 deg
Eccentricity:
0000554
Arg of perigee: 93
7238 deg
Mean anomaly: 266
3975 deg
Mean motion: 15
48946940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 336
Coasting Arc #7 (Orbit 631)
---------------------------------------
Vector Time (GMT): 2020/261/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4601960
29 A = 6794915
96 meter
Y = -1596807
21 meter E =
0011762
Z = -4748736
43 I = 51
25661
XDOT = -258
665025 Wp = 107
89043
YDOT = -7167
200948 meter/sec RA = 250
60166 deg
ZDOT = 2662
638936 TA = 188
60227
MA = 188
62245
Ha = 229
428 n
mi
Hp = 222
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15098294
92 X = -4560695
71
Y = -5238868
79 feet Y = -1648039
38 meter
Z = -15579843
94 Z = -4770990
50
XDOT = -848
638533 XDOT = -191
433540
YDOT = -23514
438805 feet/sec YDOT = -7169
717343 meter/sec
ZDOT = 8735
692047 ZDOT = 2661
546456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14850744
01 X = 4526506
77
Y = 5625958
02 feet Y = 1714792
00 meter
Z = -15682467
65 Z = -4780016
14
XDOT = 709
518773 XDOT = 216
261322
YDOT = 22446
739299 feet/sec YDOT = 6841
766138 meter/sec
ZDOT = 8730
766237 ZDOT = 2661
137549
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 20261
51846115
00016717 00000-0 10270-3 0 9065
2 25544 51
6392 251
5725 0000630 91
6389 268
4833 15
48917738 6328
Satellite: ISS
Catalog Number: 25544
Epoch time: 20261
51846115 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 251
5725 deg
Eccentricity:
0000630
Arg of perigee: 91
6389 deg
Mean anomaly: 268
4833 deg
Mean motion: 15
48917738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 632
Checksum: 317
Coasting Arc #8 (Orbit 647)
---------------------------------------
Vector Time (GMT): 2020/262/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4714450
17 A = 6794824
47 meter
Y = 1192337
47 meter E =
0008060
Z = 4740963
86 I = 51
26938
XDOT = 883
574980 Wp = 63
87142
YDOT = 7130
077597 meter/sec RA = 245
62979 deg
ZDOT = -2664
796610 TA = 52
63871
MA = 52
56533
Ha = 229
220 n
mi
Hp = 222
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15467356
19 X = 4677737
74
Y = 3911868
34 feet Y = 1244853
05 meter
Z = 15554343
38 Z = 4763775
59
XDOT = 2898
868044 XDOT = 816
722736
YDOT = 23392
643036 feet/sec YDOT = 7139
584296 meter/sec
ZDOT = -8742
771031 ZDOT = -2660
667644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15326065
99 X = -4671384
92
Y = -4045929
10 feet Y = -1233199
19 meter
Z = 15659552
29 Z = 4773031
54
XDOT = -3050
209669 XDOT = -929
703907
YDOT = -22299
476366 feet/sec YDOT = -6796
880396 meter/sec
ZDOT = -8723
819871 ZDOT = -2659
020297
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 20262
55074038
00016717 00000-0 10270-3 0 9078
2 25544 51
6396 246
4660 0000559 88
7156 271
4058 15
48946185 6480
Satellite: ISS
Catalog Number: 25544
Epoch time: 20262
55074038 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 246
4660 deg
Eccentricity:
0000559
Arg of perigee: 88
7156 deg
Mean anomaly: 271
4058 deg
Mean motion: 15
48946185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 648
Checksum: 332
Coasting Arc #9 (Orbit 662)
---------------------------------------
Vector Time (GMT): 2020/263/12:10:07
837
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4802944
19 A = 6794864
49 meter
Y = -762831
03 meter E =
0011785
Z = -4756844
50 I = 51
28454
XDOT = -1507
678493 Wp = 107
42288
YDOT = -7016
596557 meter/sec RA = 240
65964 deg
ZDOT = 2649
506778 TA = 188
91744
MA = 188
93839
Ha = 229
417 n
mi
Hp = 222
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15757690
91 X = -4770950
79
Y = -2502726
48 feet Y = -816362
55 meter
Z = -15606445
23 Z = -4780097
75
XDOT = -4946
451748 XDOT = -1441
974644
YDOT = -23020
329910 feet/sec YDOT = -7033
088881 meter/sec
ZDOT = 8692
607538 ZDOT = 2642
343232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15671360
68 X = 4776630
74
Y = 2370146
05 feet Y = 722420
52 meter
Z = -15713702
85 Z = -4789536
63
XDOT = 5374
356752 XDOT = 1638
103938
YDOT = 21833
717815 feet/sec YDOT = 6654
917190 meter/sec
ZDOT = 8659
641902 ZDOT = 2639
458852
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 20263
51850247
00016717 00000-0 10270-3 0 9080
2 25544 51
6398 241
6795 0000629 82
5041 277
6181 15
48922219 6635
Satellite: ISS
Catalog Number: 25544
Epoch time: 20263
51850247 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 241
6795 deg
Eccentricity:
0000629
Arg of perigee: 82
5041 deg
Mean anomaly: 277
6181 deg
Mean motion: 15
48922219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 663
Checksum: 319
Coasting Arc #10 (Orbit 668)
---------------------------------------
Vector Time (GMT): 2020/263/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 30262
47 A = 6798724
46 meter
Y = -5699611
96 meter E =
0012131
Z = 3696477
53 I = 51
30486
XDOT = 5695
090598 Wp = 94
14850
YDOT = 2816
974814 meter/sec RA = 239
00629 deg
ZDOT = 4283
811468 TA = 310
05160
MA = 310
15795
Ha = 229
325 n
mi
Hp = 222
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 99286
30 X = 76039
44
Y = -18699514
30 feet Y = -5699017
27 meter
Z = 12127550
94 Z = 3696736
20
XDOT = 18684
680440 XDOT = 5642
358552
YDOT = 9242
043354 feet/sec YDOT = 2880
366922 meter/sec
ZDOT = 14054
499567 ZDOT = 4311
347943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15526395
08 X = 4732445
22
Y = -10420283
66 feet Y = -3176102
46 meter
Z = 12128805
75 Z = 3696859
99
XDOT = 1942
159402 XDOT = 591
970186
YDOT = 19450
456766 feet/sec YDOT = 5928
499222 meter/sec
ZDOT = 14181
496247 ZDOT = 4322
520056
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 20263
90560697
00016717 00000-0 10270-3 0 9091
2 25544 51
6416 239
7648 0000463 62
9253 297
1945 15
48929404 6698
Satellite: ISS
Catalog Number: 25544
Epoch time: 20263
90560697 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 239
7648 deg
Eccentricity:
0000463
Arg of perigee: 62
9253 deg
Mean anomaly: 297
1945 deg
Mean motion: 15
48929404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 669
Checksum: 343
Coasting Arc #11 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2020/264/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 459140
13 A = 6798679
78 meter
Y = 5685035
54 meter E =
0005970
Z = -3706305
56 I = 51
32257
XDOT = -5909
025482 Wp = 79
46565
YDOT = -2309
993027 meter/sec RA = 234
03780 deg
ZDOT = -4280
107360 TA = 144
79832
MA = 144
75888
Ha = 229
280 n
mi
Hp = 222
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1506365
27 X = 413537
56
Y = 18651691
40 feet Y = 5689914
77 meter
Z = -12159795
13 Z = -3704186
32
XDOT = -19386
566542 XDOT = -5861
964705
YDOT = -7578
717281 feet/sec YDOT = -2375
809116 meter/sec
ZDOT = -14042
346980 ZDOT = -4308
696994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14386798
56 X = -4385096
20
Y = 11975438
47 feet Y = 3650113
65 meter
Z = -12150071
88 Z = -3703341
91
XDOT = -3948
184328 XDOT = -1203
406583
YDOT = -19107
994742 feet/sec YDOT = -5824
116797 meter/sec
ZDOT = -14174
220573 ZDOT = -4320
302431
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 20264
87336869
00016717 00000-0 10270-3 0 9102
2 25544 51
6408 234
9784 0000309 75
8258 284
2927 15
48940532 6843
Satellite: ISS
Catalog Number: 25544
Epoch time: 20264
87336869 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 234
9784 deg
Eccentricity:
0000309
Arg of perigee: 75
8258 deg
Mean anomaly: 284
2927 deg
Mean motion: 15
48940532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 684
Checksum: 339
Coasting Arc #12 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2020/265/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -971002
18 A = 6798720
84 meter
Y = -5622283
67 meter E =
0011971
Z = 3687721
17 I = 51
34402
XDOT = 6090
332356 Wp = 94
56807
YDOT = 1775
801634 meter/sec RA = 229
06986 deg
ZDOT = 4297
970007 TA = 309
46881
MA = 309
57464
Ha = 229
239 n
mi
Hp = 222
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3185702
69 X = -925972
99
Y = -18445812
58 feet Y = -5632890
20 meter
Z = 12098822
72 Z = 3683113
94
XDOT = 19981
405367 XDOT = 6049
144836
YDOT = 5826
120848 feet/sec YDOT = 1843
677963 meter/sec
ZDOT = 14100
951465 ZDOT = 4327
454696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13027709
65 X = 3970845
90
Y = -13460619
71 feet Y = -4102796
89 meter
Z = 12077612
06 Z = 3681256
16
XDOT = 5954
234105 XDOT = 1814
850555
YDOT = 18575
380676 feet/sec YDOT = 5661
776030 meter/sec
ZDOT = 14236
975267 ZDOT = 4339
430061
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 20265
90564784
00016717 00000-0 10270-3 0 9117
2 25544 51
6413 229
8719 0000223 65
2175 294
8998 15
48947312 7003
Satellite: ISS
Catalog Number: 25544
Epoch time: 20265
90564784 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 229
8719 deg
Eccentricity:
0000223
Arg of perigee: 65
2175 deg
Mean anomaly: 294
8998 deg
Mean motion: 15
48947312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 700
Checksum: 324
Coasting Arc #13 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2020/266/20:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1450008
22 A = 6798688
05 meter
Y = 5521623
04 meter E =
0006049
Z = -3698204
61 I = 51
36589
XDOT = -6212
232284 Wp = 79
82744
YDOT = -1241
314537 meter/sec RA = 224
10351 deg
ZDOT = -4294
043939 TA = 144
28074
MA = 144
24025
Ha = 229
312 n
mi
Hp = 222
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4757244
82 X = 1406119
93
Y = 18115561
16 feet Y = 5537592
60 meter
Z = -12133217
22 Z = -3691267
68
XDOT = -20381
339513 XDOT = -6177
031626
YDOT = -4072
554254 feet/sec YDOT = -1310
587436 meter/sec
ZDOT = -14088
070667 ZDOT = -4324
135283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11586917
91 X = -3531692
58
Y = 14741881
46 feet Y = 4493325
47 meter
Z = -12101246
17 Z = -3688459
83
XDOT = -7838
445367 XDOT = -2389
158148
YDOT = -17826
004787 feet/sec YDOT = -5433
366259 meter/sec
ZDOT = -14226
916638 ZDOT = -4336
364191
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 20266
87340863
00016717 00000-0 10270-3 0 9125
2 25544 51
6401 225
0847 0000441 75
1252 284
9947 15
48953507 7151
Satellite: ISS
Catalog Number: 25544
Epoch time: 20266
87340863 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 225
0847 deg
Eccentricity:
0000441
Arg of perigee: 75
1252 deg
Mean anomaly: 284
9947 deg
Mean motion: 15
48953507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 715
Checksum: 310
Coasting Arc #14 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2020/267/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1945656
78 A = 6798949
03 meter
Y = 5412167
80 meter E =
0005761
Z = -3631811
58 I = 51
39081
XDOT = -6247
279689 Wp = 81
92563
YDOT = -681
877665 meter/sec RA = 219
94378 deg
ZDOT = -4368
152778 TA = 141
17527
MA = 141
13387
Ha = 229
318 n
mi
Hp = 222
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6383388
39 X = 1902633
05
Y = 17756456
05 feet Y = 5433684
92 meter
Z = -11915392
32 Z = -3622464
85
XDOT = -20496
324440 XDOT = -6217
972304
YDOT = -2237
131448 feet/sec YDOT = -751
575411 meter/sec
ZDOT = -14331
209902 ZDOT = -4398
428605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18895651
10 X = -5759394
46
Y = -138077
94 feet Y = -42086
15 meter
Z = -11872289
46 Z = -3618673
83
XDOT = 9205
394480 XDOT = 2805
804237
YDOT = -16956
641074 feet/sec YDOT = -5168
384199 meter/sec
ZDOT = -14470
928099 ZDOT = -4410
738885
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 20267
71213549
00016717 00000-0 10270-3 0 9130
2 25544 51
6434 220
9393 0000383 73
6297 286
4895 15
48937493 7283
Satellite: ISS
Catalog Number: 25544
Epoch time: 20267
71213549 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 220
9393 deg
Eccentricity:
0000383
Arg of perigee: 73
6297 deg
Mean anomaly: 286
4895 deg
Mean motion: 15
48937493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 337
Coasting Arc #15 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2020/268/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2427274
33 A = 6799033
21 meter
Y = -5216197
43 meter E =
0012461
Z = 3612768
87 I = 51
41717
XDOT = 6281
984775 Wp = 92
69209
YDOT = 124
414516 meter/sec RA = 214
98123 deg
ZDOT = 4386
536893 TA = 310
17475
MA = 310
28379
Ha = 229
400 n
mi
Hp = 222
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7963498
47 X = -2386313
64
Y = -17113508
63 feet Y = -5243111
88 meter
Z = 11852916
24 Z = 3601077
65
XDOT = 20610
186271 XDOT = 6258
819318
YDOT = 408
184108 feet/sec YDOT = 194
534701 meter/sec
ZDOT = 14391
525240 ZDOT = 4416
996106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18814650
61 X = 5734705
51
Y = -1890551
27 feet Y = -576240
03 meter
Z = 11798976
52 Z = 3596328
04
XDOT = -7349
648542 XDOT = -2240
172876
YDOT = 17834
007448 feet/sec YDOT = 5435
805470 meter/sec
ZDOT = 14532
113758 ZDOT = 4429
388274
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 20268
74441466
00016717 00000-0 10270-3 0 9146
2 25544 51
6429 215
8335 0000515 70
4784 289
6422 15
48929698 7446
Satellite: ISS
Catalog Number: 25544
Epoch time: 20268
74441466 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 215
8335 deg
Eccentricity:
0000515
Arg of perigee: 70
4784 deg
Mean anomaly: 289
6422 deg
Mean motion: 15
48929698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 336
Coasting Arc #16 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2020/269/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2867047
97 A = 6798994
92 meter
Y = 4991792
20 meter E =
0005584
Z = -3623283
90 I = 51
44588
XDOT = -6260
005796 Wp = 82
47799
YDOT = 417
493073 meter/sec RA = 210
02086 deg
ZDOT = -4383
375411 TA = 140
45684
MA = 140
41609
Ha = 229
276 n
mi
Hp = 222
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9406325
36 X = 2828614
97
Y = 16377271
01 feet Y = 5023638
62 meter
Z = -11887414
38 Z = -3609450
38
XDOT = -20538
076758 XDOT = -6242
917178
YDOT = 1369
727931 feet/sec YDOT = 347
584657 meter/sec
ZDOT = -14381
152924 ZDOT = -4413
742521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18537734
51 X = -5650301
48
Y = 3815786
98 feet Y = 1163051
87 meter
Z = -11823567
64 Z = -3603823
42
XDOT = 5449
303607 XDOT = 1660
947739
YDOT = -18469
843204 feet/sec YDOT = -5629
608209 meter/sec
ZDOT = -14521
338513 ZDOT = -4426
103979
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 20269
71217384
00016717 00000-0 10270-3 0 9155
2 25544 51
6432 211
0472 0000254 69
7119 290
4058 15
48937173 7591
Satellite: ISS
Catalog Number: 25544
Epoch time: 20269
71217384 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 211
0472 deg
Eccentricity:
0000254
Arg of perigee: 69
7119 deg
Mean anomaly: 290
4058 deg
Mean motion: 15
48937173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 310
- 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