[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 21st 2020
- spaceflight nasa gov will be taken offline in the next 30 days *
- *
- Current information about the International Space Station can be *
- found at www nasa gov/station *
- *
- Predicted ISS and visiting vehicle sightings opportunities can be *
- found at spotthestation nasa gov *
- *
- Updated ISS trajectory information will be made available as a CCSDS *
- Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
- system *
- Included in the OEM are a sequence of events with ISS maneuver *
- details (in the comment section), predicted post-maneuver state *
- vectors, predicted coasting state vectors at 4-minute intervals, *
- and ISS ballistic details *
- *
- OEMs will be provided in xml and txt formats *
- Links to the OEMs and more details to follow *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14570 0291 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 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
355/04:48:45
000 0
0 -0
0 0
1
N/A 0
0 -0
1 229
1
000/00:07:30
000 0
1 -0
0 222
1
358/10:50:00
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
2
361/14:12:30
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
3
Coasting Arc #1 (Orbit 1995)
---------------------------------------
Vector Time (GMT): 2020/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4076616
39 A = 6796605
23 meter
Y = 3598074
52 meter E =
0008896
Z = -4087468
73 I = 51
66508
XDOT = -6102
125772 Wp = 112
70556
YDOT = -2533
485347 meter/sec RA = 175
04000 deg
ZDOT = 3859
144696 TA = 197
29397
MA = 197
32430
Ha = 229
245 n
mi
Hp = 221
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13374725
69 X = -4096693
44
Y = 11804706
42 feet Y = 3552375
33 meter
Z = -13410330
49 Z = -4107319
62
XDOT = -20020
097678 XDOT = -6092
087697
YDOT = -8311
959799 feet/sec YDOT = -2601
668248 meter/sec
ZDOT = 12661
235879 ZDOT = 3829
526673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10023396
35 X = -3055131
21
Y = -14672752
25 feet Y = -4472254
89 meter
Z = -13502340
98 Z = -4115513
53
XDOT = 9725
303411 XDOT = 2964
272480
YDOT = -18158
537254 feet/sec YDOT = -5534
722155 meter/sec
ZDOT = 12524
008687 ZDOT = 3817
317848
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 20349
50906283
00016717 00000-0 10270-3 0 9008
2 25544 51
6387 176
2393 0001553 128
2424 231
8866 15
49187353 19965
Satellite: ISS
Catalog Number: 25544
Epoch time: 20349
50906283 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 176
2393 deg
Eccentricity:
0001553
Arg of perigee: 128
2424 deg
Mean anomaly: 231
8866 deg
Mean motion: 15
49187353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1996
Checksum: 327
Coasting Arc #2 (Orbit 2011)
---------------------------------------
Vector Time (GMT): 2020/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3830559
70 A = 6796791
17 meter
Y = -3899839
19 meter E =
0011525
Z = 4030021
76 I = 51
69917
XDOT = 6247
140367 Wp = 84
39580
YDOT = 2061
642430 meter/sec RA = 170
09525 deg
ZDOT = -3932
114577 TA = 46
47830
MA = 46
38259
Ha = 229
108 n
mi
Hp = 222
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12567453
07 X = 3854308
64
Y = -12794747
99 feet Y = -3856871
06 meter
Z = 13221856
18 Z = 4048686
11
XDOT = 20495
867345 XDOT = 6242
722127
YDOT = 6763
918734 feet/sec YDOT = 2131
478452 meter/sec
ZDOT = -12900
638375 ZDOT = -3901
778745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11346862
03 X = 3458523
55
Y = 13805774
67 feet Y = 4208000
12 meter
Z = 13308389
89 Z = 4056397
24
XDOT = -7975
727968 XDOT = -2431
001885
YDOT = 18889
420917 feet/sec YDOT = 5757
495495 meter/sec
ZDOT = -12760
054019 ZDOT = -3889
264465
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 20350
54118101
00016717 00000-0 10270-3 0 9019
2 25544 51
6385 171
1323 0001434 135
3519 224
7746 15
49186604 20128
Satellite: ISS
Catalog Number: 25544
Epoch time: 20350
54118101 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 171
1323 deg
Eccentricity:
0001434
Arg of perigee: 135
3519 deg
Mean anomaly: 224
7746 deg
Mean motion: 15
49186604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2012
Checksum: 271
Coasting Arc #3 (Orbit 2026)
---------------------------------------
Vector Time (GMT): 2020/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3547855
40 A = 6796907
98 meter
Y = 4205111
99 meter E =
0008475
Z = -4000292
96 I = 51
73256
XDOT = -6343
482956 Wp = 113
81976
YDOT = -1567
567723 meter/sec RA = 165
15212 deg
ZDOT = 3981
549995 TA = 197
67531
MA = 197
70482
Ha = 229
228 n
mi
Hp = 221
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11639945
52 X = -3575183
53
Y = 13796299
18 feet Y = 4165285
22 meter
Z = -13124320
72 Z = -4017592
60
XDOT = -20811
951957 XDOT = -6344
822459
YDOT = -5142
938723 feet/sec YDOT = -1638
513289 meter/sec
ZDOT = 13062
828068 ZDOT = 3950
732478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12665808
66 X = -3860538
48
Y = -12778544
09 feet Y = -3894900
24 meter
Z = -13204548
44 Z = -4024746
36
XDOT = 6125
539355 XDOT = 1867
064395
YDOT = -19410
906359 feet/sec YDOT = -5916
444258 meter/sec
ZDOT = 12919
979323 ZDOT = 3938
009698
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 20351
50879220
00016717 00000-0 10270-3 0 9023
2 25544 51
6382 166
3439 0001672 137
3771 222
7509 15
49189902 20270
Satellite: ISS
Catalog Number: 25544
Epoch time: 20351
50879220 = yrday
fracday
Element set: 902
Inclination: 51
6382 deg
RA of node: 166
3439 deg
Eccentricity:
0001672
Arg of perigee: 137
3771 deg
Mean anomaly: 222
7509 deg
Mean motion: 15
49189902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2027
Checksum: 307
Coasting Arc #4 (Orbit 2042)
---------------------------------------
Vector Time (GMT): 2020/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3256655
98 A = 6797128
91 meter
Y = -4471147
88 meter E =
0011766
Z = 3940497
20 I = 51
76647
XDOT = 6412
382799 Wp = 87
05971
YDOT = 1087
670469 meter/sec RA = 160
21172 deg
ZDOT = -4054
381150 TA = 45
32329
MA = 45
22748
Ha = 229
127 n
mi
Hp = 222
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10684566
86 X = 3287271
18
Y = -14669120
35 feet Y = -4434559
05 meter
Z = 12928140
42 Z = 3956390
26
XDOT = 21038
001309 XDOT = 6419
437221
YDOT = 3568
472668 feet/sec YDOT = 1159
418414 meter/sec
ZDOT = -13301
775426 ZDOT = -4023
215309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13826151
01 X = 4214210
83
Y = 11673429
96 feet Y = 3558061
45 meter
Z = 13001863
58 Z = 3962968
02
XDOT = -4302
524645 XDOT = -1311
409512
YDOT = 19790
660505 feet/sec YDOT = 6032
193322 meter/sec
ZDOT = -13157
281395 ZDOT = -4010
339369
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 20352
54090679
00016717 00000-0 10270-3 0 9032
2 25544 51
6390 161
2367 0001559 143
3731 216
7526 15
49179333 20437
Satellite: ISS
Catalog Number: 25544
Epoch time: 20352
54090679 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 161
2367 deg
Eccentricity:
0001559
Arg of perigee: 143
3731 deg
Mean anomaly: 216
7526 deg
Mean motion: 15
49179333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2043
Checksum: 303
Coasting Arc #5 (Orbit 2057)
---------------------------------------
Vector Time (GMT): 2020/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2929350
50 A = 6797205
95 meter
Y = 4734817
70 meter E =
0008074
Z = -3908036
39 I = 51
79942
XDOT = -6430
865533 Wp = 113
49477
YDOT = -594
188600 meter/sec RA = 155
27339 deg
ZDOT = 4104
092715 TA = 199
52921
MA = 199
56016
Ha = 229
228 n
mi
Hp = 221
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9610730
00 X = -2963096
19
Y = 15534178
80 feet Y = 4701871
43 meter
Z = -12821641
69 Z = -3922347
19
XDOT = -21098
640200 XDOT = -6443
678271
YDOT = -1949
437664 feet/sec YDOT = -666
175341 meter/sec
ZDOT = 13464
871113 ZDOT = 4072
823267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14951141
60 X = -4557107
96
Y = -10413120
49 feet Y = -3173919
13 meter
Z = -12888041
90 Z = -3928275
17
XDOT = 2423
223985 XDOT = 738
598671
YDOT = -19950
374961 feet/sec YDOT = -6080
874288 meter/sec
ZDOT = 13319
868630 ZDOT = 4059
895959
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 20353
50851279
00016717 00000-0 10270-3 0 9041
2 25544 51
6400 156
4487 0001760 139
6352 220
4929 15
49198114 20582
Satellite: ISS
Catalog Number: 25544
Epoch time: 20353
50851279 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 156
4487 deg
Eccentricity:
0001760
Arg of perigee: 139
6352 deg
Mean anomaly: 220
4929 deg
Mean motion: 15
49198114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2058
Checksum: 307
Coasting Arc #6 (Orbit 2073)
---------------------------------------
Vector Time (GMT): 2020/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2598154
35 A = 6797462
16 meter
Y = -4958504
59 meter E =
0012155
Z = 3845512
42 I = 51
82920
XDOT = 6425
343030 Wp = 89
57571
YDOT = 118
851319 meter/sec RA = 150
33784 deg
ZDOT = -4176
431010 TA = 44
35128
MA = 44
25398
Ha = 229
184 n
mi
Hp = 222
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8524128
45 X = 2634729
69
Y = -16268059
69 feet Y = -4929246
08 meter
Z = 12616510
58 Z = 3858221
38
XDOT = 21080
521753 XDOT = 6443
822919
YDOT = 389
932149 feet/sec YDOT = 190
807909 meter/sec
ZDOT = -13702
201476 ZDOT = -4145
174689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15906027
94 X = 4848157
32
Y = 9100384
55 feet Y = 2773797
21 meter
Z = 12675493
97 Z = 3863490
56
XDOT = -597
683543 XDOT = -182
173944
YDOT = 19980
154101 feet/sec YDOT = 6089
950970 meter/sec
ZDOT = -13557
234855 ZDOT = -4132
245184
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 20354
54062415
00016717 00000-0 10270-3 0 9053
2 25544 51
6389 151
3421 0001745 145
6484 214
4779 15
49177796 20743
Satellite: ISS
Catalog Number: 25544
Epoch time: 20354
54062415 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 151
3421 deg
Eccentricity:
0001745
Arg of perigee: 145
6484 deg
Mean anomaly: 214
4779 deg
Mean motion: 15
49177796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2074
Checksum: 320
Coasting Arc #7 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2020/355/04:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1494652
93 A = 6791817
08 meter
Y = -3987107
31 meter E =
0003572
Z = 5288293
98 I = 51
83541
XDOT = 6711
865340 Wp = 82
10654
YDOT = -3606
316088 meter/sec RA = 146
89262 deg
ZDOT = -821
025322 TA = 15
73065
MA = 15
71955
Ha = 229
068 n
mi
Hp = 222
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4903716
95 X = -1475644
01
Y = -13081060
74 feet Y = -4003715
83 meter
Z = 17350045
85 Z = 5281079
39
XDOT = 22020
555576 XDOT = 6755
681449
YDOT = -11831
745695 feet/sec YDOT = -3531
014114 meter/sec
ZDOT = -2693
652631 ZDOT = -788
316001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 602147
96 X = 183534
70
Y = 13998463
31 feet Y = 4266731
62 meter
Z = 17316614
10 Z = 5278103
98
XDOT = -23636
353779 XDOT = -7204
360632
YDOT = 4165
024480 feet/sec YDOT = 1269
499461 meter/sec
ZDOT = -2541
902482 ZDOT = -774
771877
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 20355
25019835
00016717 00000-0 10270-3 0 9061
2 25544 51
6429 147
8366 0001236 143
8826 216
2407 15
49239204 20854
Satellite: ISS
Catalog Number: 25544
Epoch time: 20355
25019835 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 147
8366 deg
Eccentricity:
0001236
Arg of perigee: 143
8826 deg
Mean anomaly: 216
2407 deg
Mean motion: 15
49239204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 309
Coasting Arc #8 (Orbit 2099)
---------------------------------------
Vector Time (GMT): 2020/356/04:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1756237
31 A = 6791933
30 meter
Y = 3899207
52 meter E =
0015285
Z = -5289917
44 I = 51
86435
XDOT = -6392
342892 Wp = 100
45120
YDOT = 4102
870285 meter/sec RA = 141
95933 deg
ZDOT = 901
512582 TA = 178
16942
MA = 178
16382
Ha = 229
017 n
mi
Hp = 222
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5761933
44 X = 1738199
83
Y = 12792675
58 feet Y = 3918746
63 meter
Z = -17355372
18 Z = -5281429
87
XDOT = -20972
253584 XDOT = -6442
126337
YDOT = 13460
860515 feet/sec YDOT = 4031
108077 meter/sec
ZDOT = 2957
718445 ZDOT = 870
340790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1748100
67 X = -532821
08
Y = -13969985
53 feet Y = -4258051
59 meter
Z = -17316033
54 Z = -5277927
02
XDOT = 23056
117616 XDOT = 7027
504649
YDOT = -6373
887131 feet/sec YDOT = -1942
760798 meter/sec
ZDOT = 2813
075426 ZDOT = 857
425390
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 20356
21779993
00016717 00000-0 10270-3 0 9077
2 25544 51
6440 143
0488 0001220 145
3255 214
7975 15
49219397 21008
Satellite: ISS
Catalog Number: 25544
Epoch time: 20356
21779993 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 143
0488 deg
Eccentricity:
0001220
Arg of perigee: 145
3255 deg
Mean anomaly: 214
7975 deg
Mean motion: 15
49219397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2100
Checksum: 309
Coasting Arc #9 (Orbit 2115)
---------------------------------------
Vector Time (GMT): 2020/357/04:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2003454
52 A = 6791885
33 meter
Y = -3783027
12 meter E =
0003654
Z = 5270048
64 I = 51
89070
XDOT = 6059
427671 Wp = 77
04659
YDOT = -4586
479000 meter/sec RA = 137
02794 deg
ZDOT = -987
419327 TA = 22
38636
MA = 22
37042
Ha = 229
010 n
mi
Hp = 222
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6573013
50 X = -1986601
40
Y = -12411506
28 feet Y = -3805337
39 meter
Z = 17290185
83 Z = 5260357
32
XDOT = 19880
012044 XDOT = 6115
061015
YDOT = -15047
503282 feet/sec YDOT = -4518
406977 meter/sec
ZDOT = -3239
564721 ZDOT = -957
850415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2873805
35 X = 875935
87
Y = 13803720
79 feet Y = 4207374
10 meter
Z = 17245261
85 Z = 5256355
81
XDOT = -22360
399488 XDOT = -6815
449764
YDOT = 8536
676004 feet/sec YDOT = 2601
978846 meter/sec
ZDOT = -3102
332624 ZDOT = -945
590984
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 20357
24990299
00016717 00000-0 10270-3 0 9086
2 25544 51
6442 137
9420 0001129 150
1955 209
9260 15
49249091 21161
Satellite: ISS
Catalog Number: 25544
Epoch time: 20357
24990299 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 137
9420 deg
Eccentricity:
0001129
Arg of perigee: 150
1955 deg
Mean anomaly: 209
9260 deg
Mean motion: 15
49249091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2116
Checksum: 311
Coasting Arc #10 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2020/358/04:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2253953
89 A = 6792021
09 meter
Y = 3664600
03 meter E =
0015018
Z = -5268830
85 I = 51
91417
XDOT = -5668
231602 Wp = 101
57450
YDOT = 5023
837741 meter/sec RA = 132
09824 deg
ZDOT = 1069
039215 TA = 178
65539
MA = 178
65134
Ha = 228
963 n
mi
Hp = 222
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7394861
85 X = 2238400
61
Y = 12022965
97 feet Y = 3689718
85 meter
Z = -17286190
47 Z = -5257919
52
XDOT = -18596
560373 XDOT = -5729
181175
YDOT = 16482
407286 feet/sec YDOT = 4960
110619 meter/sec
ZDOT = 3507
346507 ZDOT = 1041
357619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4006803
41 X = -1221273
68
Y = -13598804
38 feet Y = -4144915
58 meter
Z = -17235606
15 Z = -5253412
75
XDOT = 21372
531313 XDOT = 6514
347544
YDOT = -10581
204935 feet/sec YDOT = -3225
151264 meter/sec
ZDOT = 3378
844756 ZDOT = 1029
871882
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 20358
21750033
00016717 00000-0 10270-3 0 9095
2 25544 51
6435 133
1544 0001122 148
6515 211
4702 15
49226224 21314
Satellite: ISS
Catalog Number: 25544
Epoch time: 20358
21750033 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 133
1544 deg
Eccentricity:
0001122
Arg of perigee: 148
6515 deg
Mean anomaly: 211
4702 deg
Mean motion: 15
49226224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2131
Checksum: 263
Coasting Arc #11 (Orbit 2134)
---------------------------------------
Vector Time (GMT): 2020/358/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5376165
62 A = 6797549
04 meter
Y = -1613112
79 meter E =
0006603
Z = -3839894
79 I = 51
93482
XDOT = -1105
758477 Wp = 90
46474
YDOT = 6301
392637 meter/sec RA = 130
90395 deg
ZDOT = -4201
615925 TA = 135
35593
MA = 135
30274
Ha = 229
109 n
mi
Hp = 222
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17638338
65 X = 5412456
35
Y = -5292364
80 feet Y = -1552789
40 meter
Z = -12598080
03 Z = -3813691
52
XDOT = -3627
816525 XDOT = -1155
731367
YDOT = 20673
860356 feet/sec YDOT = 6288
748198 meter/sec
ZDOT = -13784
829149 ZDOT = -4207
108086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 213184
49 X = 64978
63
Y = 18496590
64 feet Y = 5637760
83 meter
Z = -12476474
79 Z = -3802829
51
XDOT = -17554
992323 XDOT = -5350
761660
YDOT = -9099
105883 feet/sec YDOT = -2773
407473 meter/sec
ZDOT = -13810
391571 ZDOT = -4209
407351
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 20358
47552650
00016717 00000-0 10270-3 0 9100
2 25544 51
6402 131
8728 0001594 152
6231 207
5003 15
49218922 21350
Satellite: ISS
Catalog Number: 25544
Epoch time: 20358
47552650 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 131
8728 deg
Eccentricity:
0001594
Arg of perigee: 152
6231 deg
Mean anomaly: 207
5003 deg
Mean motion: 15
49218922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2135
Checksum: 284
Coasting Arc #12 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2020/359/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5204759
90 A = 6797369
28 meter
Y = 2004016
87 meter E =
0012129
Z = 3878187
14 I = 51
95613
XDOT = 636
847943 Wp = 105
17800
YDOT = -6408
399952 meter/sec RA = 125
97614 deg
ZDOT = 4152
264959 TA = 301
28415
MA = 301
40288
Ha = 229
070 n
mi
Hp = 222
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17075983
93 X = -5245620
63
Y = 6574858
49 feet Y = 1945584
66 meter
Z = 12723711
08 Z = 3852805
38
XDOT = 2089
396137 XDOT = 688
291940
YDOT = -21024
934226 feet/sec YDOT = -6400
991021 meter/sec
ZDOT = 13622
916532 ZDOT = 4155
482847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1915370
62 X = -583804
96
Y = -18279319
72 feet Y = -5571536
65 meter
Z = 12605897
08 Z = 3842277
43
XDOT = 18460
821661 XDOT = 5626
858442
YDOT = 7502
445345 feet/sec YDOT = 2286
745341 meter/sec
ZDOT = 13637
942882 ZDOT = 4156
844990
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 20359
50762666
00016717 00000-0 10270-3 0 9116
2 25544 51
6407 126
7653 0001640 163
1572 196
9632 15
49234553 21517
Satellite: ISS
Catalog Number: 25544
Epoch time: 20359
50762666 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 126
7653 deg
Eccentricity:
0001640
Arg of perigee: 163
1572 deg
Mean anomaly: 196
9632 deg
Mean motion: 15
49234553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 307
Coasting Arc #13 (Orbit 2165)
---------------------------------------
Vector Time (GMT): 2020/360/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5015941
56 A = 6797190
72 meter
Y = -2347151
38 meter E =
0006710
Z = -3947199
35 I = 51
97542
XDOT = -175
306318 Wp = 87
63755
YDOT = 6474
396117 meter/sec RA = 121
05000 deg
ZDOT = -4078
400599 TA = 139
82211
MA = 139
77248
Ha = 229
015 n
mi
Hp = 222
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16456501
20 X = 5060988
61
Y = -7700627
88 feet Y = -2290807
20 meter
Z = -12950129
11 Z = -3922724
66
XDOT = -575
151962 XDOT = -227
881371
YDOT = 21241
457077 feet/sec YDOT = 6472
142206 meter/sec
ZDOT = -13380
579392 ZDOT = -4079
379140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3471317
23 X = 1058057
49
Y = 17916364
21 feet Y = 5460907
81 meter
Z = -12836502
46 Z = -3912565
95
XDOT = -19186
916882 XDOT = -5848
172266
YDOT = -5859
056839 feet/sec YDOT = -1785
840525 meter/sec
ZDOT = -13385
231457 ZDOT = -4079
818548
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 20360
47521918
00016717 00000-0 10270-3 0 9128
2 25544 51
6418 121
9775 0001537 162
4292 197
6912 15
49219789 21666
Satellite: ISS
Catalog Number: 25544
Epoch time: 20360
47521918 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 121
9775 deg
Eccentricity:
0001537
Arg of perigee: 162
4292 deg
Mean anomaly: 197
6912 deg
Mean motion: 15
49219789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2166
Checksum: 328
Coasting Arc #14 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2020/361/10:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4793009
44 A = 6796977
66 meter
Y = 2698648
63 meter E =
0011731
Z = 3985900
90 I = 51
99200
XDOT = -309
109804 Wp = 107
16262
YDOT = -6513
061018 meter/sec RA = 116
12515 deg
ZDOT = 4024
830361 TA = 300
97178
MA = 301
08699
Ha = 229
008 n
mi
Hp = 222
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15725096
58 X = -4842191
59
Y = 8853834
07 feet Y = 2644774
24 meter
Z = 13077102
68 Z = 3962499
17
XDOT = -1014
139778 XDOT = -255
806171
YDOT = -21368
310427 feet/sec YDOT = -6516
220189 meter/sec
ZDOT = 13204
824020 ZDOT = 4023
457442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5067053
23 X = -1544437
82
Y = -17401850
78 feet Y = -5304084
12 meter
Z = 12968431
50 Z = 3952777
92
XDOT = 19798
936349 XDOT = 6034
715799
YDOT = 4103
345800 feet/sec YDOT = 1250
699800 meter/sec
ZDOT = 13198
580431 ZDOT = 4022
927315
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 20361
50731391
00016717 00000-0 10270-3 0 9132
2 25544 51
6424 116
8705 0001547 166
4444 193
6748 15
49244034 21825
Satellite: ISS
Catalog Number: 25544
Epoch time: 20361
50731391 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 116
8705 deg
Eccentricity:
0001547
Arg of perigee: 166
4444 deg
Mean anomaly: 193
6748 deg
Mean motion: 15
49244034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 301
Coasting Arc #15 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2020/361/14:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2334738
58 A = 6793383
54 meter
Y = -4053738
74 meter E =
0006376
Z = 4921714
37 I = 51
98420
XDOT = 4693
088903 Wp = 69
98037
YDOT = -5578
313113 meter/sec RA = 115
39155 deg
ZDOT = -2363
654272 TA = 43
09162
MA = 43
04172
Ha = 228
920 n
mi
Hp = 222
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7659903
46 X = -2313141
84
Y = -13299667
77 feet Y = -4079727
36 meter
Z = 16147356
85 Z = 4910425
01
XDOT = 15397
273304 XDOT = 4766
599798
YDOT = -18301
552209 feet/sec YDOT = -5525
420282 meter/sec
ZDOT = -7754
771232 ZDOT = -2340
679224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5757080
56 X = 1754758
16
Y = -14286292
79 feet Y = -4354462
04 meter
Z = 16095038
94 Z = 4905767
87
XDOT = 22888
274115 XDOT = 6976
345950
YDOT = 590
116985 feet/sec YDOT = 179
867657 meter/sec
ZDOT = -7648
019727 ZDOT = -2331
116413
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 20361
63632468
00016717 00000-0 10270-3 0 9142
2 25544 51
6443 116
2344 0001301 169
8099 190
3077 15
49251775 21841
Satellite: ISS
Catalog Number: 25544
Epoch time: 20361
63632468 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 116
2344 deg
Eccentricity:
0001301
Arg of perigee: 169
8099 deg
Mean anomaly: 190
3077 deg
Mean motion: 15
49251775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2184
Checksum: 307
Coasting Arc #16 (Orbit 2198)
---------------------------------------
Vector Time (GMT): 2020/362/14:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2625729
88 A = 6793545
64 meter
Y = 3917642
50 meter E =
0012518
Z = -4901580
08 I = 51
99715
XDOT = -4232
013582 Wp = 112
92498
YDOT = 5887
902277 meter/sec RA = 110
46857 deg
ZDOT = 2439
140565 TA = 180
94098
MA = 180
94334
Ha = 228
850 n
mi
Hp = 222
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8614599
33 X = 2605535
54
Y = 12853157
80 feet Y = 3946893
12 meter
Z = -16081299
49 Z = -4888873
77
XDOT = -13884
558997 XDOT = -4309
387314
YDOT = 19317
264688 feet/sec YDOT = 5840
143871 meter/sec
ZDOT = 8002
429675 ZDOT = 2418
396043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4565073
81 X = -1391434
50
Y = 14848089
71 feet Y = 4525697
74 meter
Z = -16022406
61 Z = -4883629
53
XDOT = -22707
868207 XDOT = -6921
358229
YDOT = 1548
920018 feet/sec YDOT = 472
110821 meter/sec
ZDOT = 7905
998803 ZDOT = 2409
748435
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 20362
60391366
00016717 00000-0 10270-3 0 9150
2 25544 51
6434 111
4479 0001346 168
8132 191
3048 15
49241943 21994
Satellite: ISS
Catalog Number: 25544
Epoch time: 20362
60391366 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 111
4479 deg
Eccentricity:
0001346
Arg of perigee: 168
8132 deg
Mean anomaly: 191
3048 deg
Mean motion: 15
49241943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2199
Checksum: 308
Coasting Arc #17 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2020/363/14:12:30
000
Vector Time (MET): N/A
Weight (LBS) : 996846
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2893542
27 A = 6793627
25 meter
Y = -3758649
60 meter E =
0006597
Z = 4859025
10 I = 52
00935
XDOT = 3767
704577 Wp = 69
96730
YDOT = -6175
667091 meter/sec RA = 105
54524 deg
ZDOT = -2528
485410 TA = 44
80874
MA = 44
75548
Ha = 228
826 n
mi
Hp = 222
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9493248
93 X = -2874899
15
Y = -12331527
57 feet Y = -3790903
82 meter
Z = 15941683
39 Z = 4845014
11
XDOT = 12361
235488 XDOT = 3848
764635
YDOT = -20261
374969 feet/sec YDOT = -6133
080266 meter/sec
ZDOT = -8295
555807 ZDOT = -2509
987549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3346872
22 X = 1020126
65
Y = -15266086
32 feet Y = -4653103
11 meter
Z = 15876733
66 Z = 4839228
42
XDOT = 22406
846359 XDOT = 6829
606770
YDOT = -3642
573054 feet/sec YDOT = -1110
256267 meter/sec
ZDOT = -8209
521853 ZDOT = -2502
262261
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 20363
63600455
00016717 00000-0 10270-3 0 9167
2 25544 51
6443 106
3409 0001271 181
2196 178
8951 15
49262295 22151
Satellite: ISS
Catalog Number: 25544
Epoch time: 20363
63600455 = yrday
fracday
Element set: 916
Inclination: 51
6443 deg
RA of node: 106
3409 deg
Eccentricity:
0001271
Arg of perigee: 181
2196 deg
Mean anomaly: 178
8951 deg
Mean motion: 15
49262295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 302
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