[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 10th 2021
- *
- !!! The status of spaceflight nasa gov has been updated !!! *
- *
- spaceflight nasa gov will be taken offline by February 20, 2021 *
- *
- 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 are provided in xml and txt formats at the following links: *
- https://nasa-public-data s3 amazonaws com/iss-coords/current/ISS_OEM/ISS OEM_J2K_EPH xml *
- https://nasa-public-data s3 amazonaws com/iss-coords/current/ISS_OEM/ISS OEM_J2K_EPH txt *
- *
- The above links are permanent links to the most current posted ISS ephemeris data *
- Older archived ephemeris data can be found by searching on data nasa gov *
- *
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15144 822 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 84 1 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
040/05:21:30
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
9
040/09:30:00
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
8
040/14:00:36
808 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
046/21:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 222
4
050/19:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 222
2
053/09:36:25
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
1
054/01:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
1
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2021/039/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 957119
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4164993
95 A = 6792603
13 meter
Y = -857743
60 meter E =
0003289
Z = 5295113
10 I = 51
23391
XDOT = 1588
214814 Wp = 37
48003
YDOT = 7495
426455 meter/sec RA = 257
84129 deg
ZDOT = -32
504051 TA = 52
84673
MA = 52
81670
Ha = 229
160 n
mi
Hp = 223
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13664678
31 X = 4148556
08
Y = -2814119
44 feet Y = -811259
87 meter
Z = 17372418
32 Z = 5315304
44
XDOT = 5210
678525 XDOT = 1504
438511
YDOT = 24591
294143 feet/sec YDOT = 7512
718596 meter/sec
ZDOT = -106
640587 ZDOT = -24
992369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13833910
95 X = 4216576
06
Y = 30223
65 feet Y = 9212
17 meter
Z = 17466127
61 Z = 5323675
70
XDOT = 48
640210 XDOT = 14
825536
YDOT = 24128
577289 feet/sec YDOT = 7354
390358 meter/sec
ZDOT = -71
872593 ZDOT = -21
906766
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 21039
63213375
00016717 00000-0 10270-3 0 9002
2 25544 51
6398 258
5773 0002602 350
9235 9
1867 15
48903546 28666
Satellite: ISS
Catalog Number: 25544
Epoch time: 21039
63213375 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 258
5773 deg
Eccentricity:
0002602
Arg of perigee: 350
9235 deg
Mean anomaly: 9
1867 deg
Mean motion: 15
48903546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 322
Coasting Arc #2 (Orbit 2875)
---------------------------------------
Vector Time (GMT): 2021/040/05:21:30
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2566946
77 A = 6795658
44 meter
Y = -4368362
71 meter E =
0007760
Z = 4522399
40 I = 51
25094
XDOT = 4134
949986 Wp = 95
86032
YDOT = 5653
790844 meter/sec RA = 254
68661 deg
ZDOT = 3108
790661 TA = 322
77006
MA = 322
82384
Ha = 229
124 n
mi
Hp = 222
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8421741
36 X = 2593637
84
Y = -14331898
65 feet Y = -4339508
26 meter
Z = 14837268
39 Z = 4534932
82
XDOT = 13566
108878 XDOT = 4056
320022
YDOT = 18549
182558 feet/sec YDOT = 5699
591021 meter/sec
ZDOT = 10199
444427 ZDOT = 3128
685306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2551470
54 X = 777688
22
Y = 16373402
67 feet Y = 4990613
13 meter
Z = 14895477
93 Z = 4540141
67
XDOT = -20967
030297 XDOT = -6390
750834
YDOT = -6111
503585 feet/sec YDOT = -1862
786293 meter/sec
ZDOT = 10291
715375 ZDOT = 3136
914846
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 21040
27730988
00016717 00000-0 10270-3 0 9019
2 25544 51
6409 255
3885 0002633 351
9254 8
1853 15
48973703 28761
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
27730988 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 255
3885 deg
Eccentricity:
0002633
Arg of perigee: 351
9254 deg
Mean anomaly: 8
1853 deg
Mean motion: 15
48973703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2876
Checksum: 324
Coasting Arc #3 (Orbit 2877)
---------------------------------------
Vector Time (GMT): 2021/040/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4477015
84 A = 6795728
75 meter
Y = -2400923
95 meter E =
0008821
Z = -4521750
90 I = 51
25500
XDOT = 584
662725 Wp = 94
21425
YDOT = -6962
116045 meter/sec RA = 253
78432 deg
ZDOT = 3122
472870 TA = 207
30642
MA = 207
35282
Ha = 229
255 n
mi
Hp = 222
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14688372
18 X = -4427871
89
Y = -7877047
08 feet Y = -2450714
16 meter
Z = -14835140
74 Z = -4543378
53
XDOT = 1918
184794 XDOT = 647
305098
YDOT = -22841
588073 feet/sec YDOT = -6955
227826 meter/sec
ZDOT = 10244
333564 ZDOT = 3125
464629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4870245
98 X = 1484450
97
Y = -15845800
36 feet Y = -4829799
95 meter
Z = -14935490
07 Z = -4552337
37
XDOT = 21605
464144 XDOT = 6585
345471
YDOT = -3014
154980 feet/sec YDOT = -918
714438 meter/sec
ZDOT = 10258
284119 ZDOT = 3126
724999
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 21040
40634637
00016717 00000-0 10270-3 0 9029
2 25544 51
6434 254
7516 0002790 352
1639 7
9467 15
48942294 28788
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
40634637 = yrday
fracday
Element set: 902
Inclination: 51
6434 deg
RA of node: 254
7516 deg
Eccentricity:
0002790
Arg of perigee: 352
1639 deg
Mean anomaly: 7
9467 deg
Mean motion: 15
48942294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2878
Checksum: 321
Coasting Arc #4 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2021/040/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4075601
38 A = 6792503
80 meter
Y = 1235039
92 meter E =
0014841
Z = -5304464
83 I = 51
24153
XDOT = -2238
405680 Wp = 80
48153
YDOT = -7314
380184 meter/sec RA = 252
86843 deg
ZDOT = 19
288333 TA = 189
68942
MA = 189
71807
Ha = 229
309 n
mi
Hp = 222
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13371395
61 X = -4063343
90
Y = 4051968
25 feet Y = 1189532
40 meter
Z = -17403099
84 Z = -5324232
01
XDOT = -7343
850656 XDOT = -2156
541375
YDOT = -23997
310314 feet/sec YDOT = -7338
953917 meter/sec
ZDOT = 63
281931 ZDOT = 8
613885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13777666
84 X = -4199432
85
Y = 1478734
69 feet Y = 450718
33 meter
Z = -17494850
43 Z = -5332430
41
XDOT = -2577
574436 XDOT = -785
644688
YDOT = -23947
179449 feet/sec YDOT = -7299
100296 meter/sec
ZDOT = 13
806676 ZDOT = 4
208275
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 21040
59989920
00016717 00000-0 10270-3 0 9038
2 25544 51
6390 253
7901 0002505 355
5322 4
5805 15
48941640 28813
Satellite: ISS
Catalog Number: 25544
Epoch time: 21040
59989920 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 253
7901 deg
Eccentricity:
0002505
Arg of perigee: 355
5322 deg
Mean anomaly: 4
5805 deg
Mean motion: 15
48941640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 305
Coasting Arc #5 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2021/041/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3944362
20 A = 6792608
18 meter
Y = -1583602
98 meter E =
0003507
Z = 5296379
17 I = 51
25290
XDOT = 2873
200047 Wp = 43
20659
YDOT = 7103
111370 meter/sec RA = 247
89617 deg
ZDOT = -13
424906 TA = 46
93681
MA = 46
90745
Ha = 229
300 n
mi
Hp = 222
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12940820
87 X = 3936051
55
Y = -5195547
85 feet Y = -1539540
88 meter
Z = 17376572
08 Z = 5315518
41
XDOT = 9426
509340 XDOT = 2793
622555
YDOT = 23304
171163 feet/sec YDOT = 7134
796618 meter/sec
ZDOT = -44
044966 ZDOT =
338369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13522572
51 X = 4121680
10
Y = -2916015
38 feet Y = -888801
49 meter
Z = 17465414
59 Z = 5323458
37
XDOT = 5072
143205 XDOT = 1545
989249
YDOT = 23590
657340 feet/sec YDOT = 7190
432357 meter/sec
ZDOT = 19
797830 ZDOT = 6
034379
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 21041
63218235
00016717 00000-0 10270-3 0 9049
2 25544 51
6391 248
6837 0002575 359
6846
4302 15
48901723 28970
Satellite: ISS
Catalog Number: 25544
Epoch time: 21041
63218235 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 248
6837 deg
Eccentricity:
0002575
Arg of perigee: 359
6846 deg
Mean anomaly:
4302 deg
Mean motion: 15
48901723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2897
Checksum: 313
Coasting Arc #6 (Orbit 2911)
---------------------------------------
Vector Time (GMT): 2021/042/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3790204
77 A = 6792486
79 meter
Y = 1936883
94 meter E =
0015345
Z = -5306648
25 I = 51
26713
XDOT = -3480
024764 Wp = 80
65140
YDOT = -6811
356784 meter/sec RA = 242
92528 deg
ZDOT = 1
920994 TA = 189
35273
MA = 189
38134
Ha = 229
470 n
mi
Hp = 222
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12435055
03 X = -3785806
22
Y = 6354606
09 feet Y = 1894523
72 meter
Z = -17410263
30 Z = -5325048
21
XDOT = -11417
404081 XDOT = -3403
608783
YDOT = -22346
971077 feet/sec YDOT = -6849
845661 meter/sec
ZDOT = 6
302474 ZDOT = -14
797368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13149879
90 X = -4008083
39
Y = 4371592
06 feet Y = 1332461
26 meter
Z = -17495677
23 Z = -5332682
42
XDOT = -7502
705572 XDOT = -2286
824658
YDOT = -22885
665847 feet/sec YDOT = -6975
550950 meter/sec
ZDOT = -71
288456 ZDOT = -21
728721
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 21042
59994461
00016717 00000-0 10270-3 0 9058
2 25544 51
6394 243
8970 0002524 6
9426 353
1758 15
48947609 29122
Satellite: ISS
Catalog Number: 25544
Epoch time: 21042
59994461 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 243
8970 deg
Eccentricity:
0002524
Arg of perigee: 6
9426 deg
Mean anomaly: 353
1758 deg
Mean motion: 15
48947609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2912
Checksum: 334
Coasting Arc #7 (Orbit 2927)
---------------------------------------
Vector Time (GMT): 2021/043/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598970
05 A = 6792612
11 meter
Y = -2255626
71 meter E =
0003793
Z = 5298314
81 I = 51
28253
XDOT = 4068
095386 Wp = 50
45699
YDOT = 6493
569177 meter/sec RA = 237
95478 deg
ZDOT = 3
524112 TA = 39
52306
MA = 39
49541
Ha = 229
474 n
mi
Hp = 222
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11807644
51 X = 3598190
43
Y = -7400350
09 feet Y = -2215384
65 meter
Z = 17382922
61 Z = 5315794
73
XDOT = 13346
769638 XDOT = 3995
162848
YDOT = 21304
360816 feet/sec YDOT = 6538
653761 meter/sec
ZDOT = 11
562047 ZDOT = 23
107301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12595536
32 X = 3839119
47
Y = -5719311
99 feet Y = -1743246
29 meter
Z = 17464065
50 Z = 5323047
17
XDOT = 9867
840348 XDOT = 3007
717738
YDOT = 22021
059744 feet/sec YDOT = 6712
019010 meter/sec
ZDOT = 102
480979 ZDOT = 31
236202
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 21043
63222641
00016717 00000-0 10270-3 0 9069
2 25544 51
6382 238
7904 0002539 11
4932 348
6276 15
48900439 29289
Satellite: ISS
Catalog Number: 25544
Epoch time: 21043
63222641 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 238
7904 deg
Eccentricity:
0002539
Arg of perigee: 11
4932 deg
Mean anomaly: 348
6276 deg
Mean motion: 15
48900439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2928
Checksum: 312
Coasting Arc #8 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2021/044/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3384962
85 A = 6792471
74 meter
Y = 2575233
96 meter E =
0015613
Z = -5309460
30 I = 51
30335
XDOT = -4613
962258 Wp = 81
10003
YDOT = -6100
246853 meter/sec RA = 232
98712 deg
ZDOT = -14
898659 TA = 188
74335
MA = 188
77058
Ha = 229
544 n
mi
Hp = 222
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11105521
15 X = -3387718
87
Y = 8448930
33 feet Y = 2537365
21 meter
Z = -17419489
16 Z = -5325909
38
XDOT = -15137
671450 XDOT = -4545
332151
YDOT = -20013
933245 feet/sec YDOT = -6151
459772 meter/sec
ZDOT = -48
880116 ZDOT = -37
143762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11924601
57 X = -3634618
56
Y = 7060803
10 feet Y = 2152132
79 meter
Z = -17495844
17 Z = -5332733
30
XDOT = -12096
323841 XDOT = -3686
959507
YDOT = -20824
760182 feet/sec YDOT = -6347
386903 meter/sec
ZDOT = -152
182341 ZDOT = -46
385178
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 21044
59998751
00016717 00000-0 10270-3 0 9078
2 25544 51
6399 234
0045 0002471 13
7496 346
3721 15
48952972 29433
Satellite: ISS
Catalog Number: 25544
Epoch time: 21044
59998751 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 234
0045 deg
Eccentricity:
0002471
Arg of perigee: 13
7496 deg
Mean anomaly: 346
3721 deg
Mean motion: 15
48952972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 335
Coasting Arc #9 (Orbit 2958)
---------------------------------------
Vector Time (GMT): 2021/045/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3140243
25 A = 6792560
22 meter
Y = -2853895
49 meter E =
0003958
Z = 5301265
64 I = 51
32527
XDOT = 5137
431997 Wp = 53
98096
YDOT = 5685
597516 meter/sec RA = 228
01840 deg
ZDOT = 19
876658 TA = 35
84195
MA = 35
81539
Ha = 229
550 n
mi
Hp = 222
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10302635
34 X = 3146173
24
Y = -9363174
18 feet Y = -2818745
56 meter
Z = 17392603
80 Z = 5316533
83
XDOT = 16855
091855 XDOT = 5073
375541
YDOT = 18653
535159 feet/sec YDOT = 5742
689826 meter/sec
ZDOT = 65
212133 ZDOT = 44
675649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11097714
54 X = 3382583
39
Y = -8257350
63 feet Y = -2516840
47 meter
Z = 17463472
88 Z = 5322866
53
XDOT = 14229
315889 XDOT = 4337
095483
YDOT = 19489
713663 feet/sec YDOT = 5940
464725 meter/sec
ZDOT = 180
393012 ZDOT = 54
983790
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 21045
63226694
00016717 00000-0 10270-3 0 9085
2 25544 51
6403 228
8970 0002574 17
6304 342
4935 15
48918069 29592
Satellite: ISS
Catalog Number: 25544
Epoch time: 21045
63226694 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 228
8970 deg
Eccentricity:
0002574
Arg of perigee: 17
6304 deg
Mean anomaly: 342
4935 deg
Mean motion: 15
48918069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2959
Checksum: 331
Coasting Arc #10 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2021/046/14:00:36
808
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2874789
12 A = 6792448
49 meter
Y = 3128979
91 meter E =
0015984
Z = -5313041
82 I = 51
34988
XDOT = -5604
908800 Wp = 81
20071
YDOT = -5204
015891 meter/sec RA = 223
05411 deg
ZDOT = -29
741275 TA = 188
50044
MA = 188
52755
Ha = 229
659 n
mi
Hp = 222
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9431722
85 X = -2883757
60
Y = 10265682
11 feet Y = 3096781
47 meter
Z = -17431239
56 Z = -5327028
04
XDOT = -18388
808400 XDOT = -5546
154876
YDOT = -17073
542950 feet/sec YDOT = -5266
365513 meter/sec
ZDOT = -97
576362 ZDOT = -56
824030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10164165
72 X = -3098037
71
Y = 9421470
67 feet Y = 2871664
26 meter
Z = -17496152
81 Z = -5332827
38
XDOT = -16155
717264 XDOT = -4924
262622
YDOT = -17858
167228 feet/sec YDOT = -5443
169371 meter/sec
ZDOT = -223
378711 ZDOT = -68
085831
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 21046
60002538
00016717 00000-0 10270-3 0 9093
2 25544 51
6413 224
1115 0002589 21
6782 338
4477 15
48961153 29749
Satellite: ISS
Catalog Number: 25544
Epoch time: 21046
60002538 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 224
1115 deg
Eccentricity:
0002589
Arg of perigee: 21
6782 deg
Mean anomaly: 338
4477 deg
Mean motion: 15
48961153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 306
Coasting Arc #11 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2021/046/21:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2902293
64 A = 6801248
48 meter
Y = 5504133
50 meter E =
0005084
Z = -2750050
76 I = 51
38906
XDOT = -5672
467476 Wp = 89
60967
YDOT = 437
358873 meter/sec RA = 221
52990 deg
ZDOT = -5119
342274 TA = 121
54324
MA = 121
49358
Ha = 229
737 n
mi
Hp = 222
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9521960
77 X = 2853886
89
Y = 18058180
77 feet Y = 5536318
22 meter
Z = -9022476
23 Z = -2736070
78
XDOT = -18610
457598 XDOT = -5652
070323
YDOT = 1434
904439 feet/sec YDOT = 374
038991 meter/sec
ZDOT = -16795
742369 ZDOT = -5146
846730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14290590
96 X = 4355772
12
Y = -14618919
09 feet Y = -4455846
54 meter
Z = -8957506
44 Z = -2730247
96
XDOT = 5921
537564 XDOT = 1804
884649
YDOT = 16141
501778 feet/sec YDOT = 4919
929742 meter/sec
ZDOT = -16923
453115 ZDOT = -5158
268509
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 21046
92261087
00016717 00000-0 10270-3 0 9106
2 25544 51
6433 222
5189 0002888 20
8991 339
2276 15
48961858 29792
Satellite: ISS
Catalog Number: 25544
Epoch time: 21046
92261087 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 222
5189 deg
Eccentricity:
0002888
Arg of perigee: 20
8991 deg
Mean anomaly: 339
2276 deg
Mean motion: 15
48961858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 342
Coasting Arc #12 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2021/047/21:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 942685
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3383655
25 A = 6801397
59 meter
Y = -5220483
60 meter E =
0015514
Z = 2728518
51 I = 51
41387
XDOT = 5610
141526 Wp = 69
88105
YDOT = -941
705796 meter/sec RA = 216
56667 deg
ZDOT = 5136
815327 TA = 321
03900
MA = 321
15068
Ha = 229
908 n
mi
Hp = 222
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11101231
14 X = -3338280
05
Y = -17127570
85 feet Y = -5258068
22 meter
Z = 8951832
37 Z = 2712192
85
XDOT = 18405
976135 XDOT = 5595
303802
YDOT = -3089
585945 feet/sec YDOT = -879
051839 meter/sec
ZDOT = 16853
068658 ZDOT = 5164
030663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12649781
26 X = -3855653
33
Y = 16060097
31 feet Y = 4895117
66 meter
Z = 8875957
84 Z = 2705391
95
XDOT = -7612
888553 XDOT = -2320
408431
YDOT = -15414
366986 feet/sec YDOT = -4698
299057 meter/sec
ZDOT = 16979
441981 ZDOT = 5175
333916
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 21047
95488880
00016717 00000-0 10270-3 0 9113
2 25544 51
6417 217
4132 0003032 26
1826 333
9476 15
48931211 29954
Satellite: ISS
Catalog Number: 25544
Epoch time: 21047
95488880 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 217
4132 deg
Eccentricity:
0003032
Arg of perigee: 26
1826 deg
Mean anomaly: 333
9476 deg
Mean motion: 15
48931211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 311
Coasting Arc #13 (Orbit 3009)
---------------------------------------
Vector Time (GMT): 2021/048/21:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3820562
97 A = 6801318
12 meter
Y = 4916418
82 meter E =
0005335
Z = -2741207
56 I = 51
44273
XDOT = -5499
274528 Wp = 91
67723
YDOT = 1417
767015 meter/sec RA = 211
60582 deg
ZDOT = -5130
661938 TA = 119
33842
MA = 119
28512
Ha = 229
827 n
mi
Hp = 222
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12534655
41 X = 3778617
11
Y = 16129983
02 feet Y = 4958908
47 meter
Z = -8993463
12 Z = -2722751
16
XDOT = -18042
239265 XDOT = -5489
798326
YDOT = 4651
466585 feet/sec YDOT = 1356
322934 meter/sec
ZDOT = -16832
880373 ZDOT = -5157
351840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10949774
70 X = 3337491
33
Y = -17289648
70 feet Y = -5269884
92 meter
Z = -8907682
03 Z = -2715061
48
XDOT = 9151
363475 XDOT = 2789
335587
YDOT = 14516
813747 feet/sec YDOT = 4424
724830 meter/sec
ZDOT = -16956
819410 ZDOT = -5168
438556
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 21048
92264620
00016717 00000-0 10270-3 0 9126
2 25544 51
6426 212
6271 0002874 26
5640 333
5657 15
48949905 30101
Satellite: ISS
Catalog Number: 25544
Epoch time: 21048
92264620 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 212
6271 deg
Eccentricity:
0002874
Arg of perigee: 26
5640 deg
Mean anomaly: 333
5657 deg
Mean motion: 15
48949905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3010
Checksum: 301
Coasting Arc #14 (Orbit 3025)
---------------------------------------
Vector Time (GMT): 2021/049/21:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4244743
58 A = 6801364
56 meter
Y = -4553026
09 meter E =
0015692
Z = 2720022
87 I = 51
47216
XDOT = 5350
640727 Wp = 70
22744
YDOT = -1901
398837 meter/sec RA = 206
64637 deg
ZDOT = 5148
168555 TA = 320
55847
MA = 320
67260
Ha = 229
942 n
mi
Hp = 222
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13926324
08 X = -4206726
88
Y = -14937749
65 feet Y = -4600281
24 meter
Z = 8923959
53 Z = 2699496
35
XDOT = 17554
595562 XDOT = 5346
498618
YDOT = -6238
185162 feet/sec YDOT = -1841
587134 meter/sec
ZDOT = 16890
316782 ZDOT = 5174
149453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9044493
39 X = -2756761
59
Y = 18356734
85 feet Y = 5595132
78 meter
Z = 8828552
86 Z = 2690942
91
XDOT = -10648
094125 XDOT = -3245
539089
YDOT = -13458
106627 feet/sec YDOT = -4102
030900 meter/sec
ZDOT = 17010
969429 ZDOT = 5184
943482
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 21049
95492017
00016717 00000-0 10270-3 0 9134
2 25544 51
6422 207
5213 0003061 29
9664 330
1661 15
48953766 30263
Satellite: ISS
Catalog Number: 25544
Epoch time: 21049
95492017 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 207
5213 deg
Eccentricity:
0003061
Arg of perigee: 29
9664 deg
Mean anomaly: 330
1661 deg
Mean motion: 15
48953766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3026
Checksum: 301
Coasting Arc #15 (Orbit 3039)
---------------------------------------
Vector Time (GMT): 2021/050/19:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 766252
98 A = 6792655
08 meter
Y = -4215369
93 meter E =
0004590
Z = 5267013
84 I = 51
47160
XDOT = 7272
980342 Wp = 78
60972
YDOT = 2288
955766 meter/sec RA = 202
10703 deg
ZDOT = 774
159032 TA = 3
97309
MA = 3
96945
Ha = 229
874 n
mi
Hp = 222
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2513953
36 X = 787749
85
Y = -13829953
83 feet Y = -4206680
87 meter
Z = 17280229
13 Z = 5270788
20
XDOT = 23861
484062 XDOT = 7243
083636
YDOT = 7509
697394 feet/sec YDOT = 2370
120325 meter/sec
ZDOT = 2539
891838 ZDOT = 809
415125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13207446
66 X = -4025629
74
Y = -4748343
78 feet Y = -1447295
18 meter
Z = 17297701
80 Z = 5272339
51
XDOT = 11170
218407 XDOT = 3404
682571
YDOT = -21224
233012 feet/sec YDOT = -6469
146222 meter/sec
ZDOT = 2703
706670 ZDOT = 824
089793
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 21050
85815918
00016717 00000-0 10270-3 0 9145
2 25544 51
6423 203
0536 0003027 32
9551 327
1787 15
48961492 30400
Satellite: ISS
Catalog Number: 25544
Epoch time: 21050
85815918 = yrday
fracday
Element set: 914
Inclination: 51
6423 deg
RA of node: 203
0536 deg
Eccentricity:
0003027
Arg of perigee: 32
9551 deg
Mean anomaly: 327
1787 deg
Mean motion: 15
48961492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3040
Checksum: 299
Coasting Arc #16 (Orbit 3054)
---------------------------------------
Vector Time (GMT): 2021/051/19:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -388982
17 A = 6792733
66 meter
Y = 4274277
25 meter E =
0016616
Z = -5279497
84 I = 51
50404
XDOT = -7428
239193 Wp = 76
49079
YDOT = -1642
655928 meter/sec RA = 197
15205 deg
ZDOT = -780
880572 TA = 186
00290
MA = 186
02284
Ha = 229
966 n
mi
Hp = 222
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1276188
23 X = -411105
20
Y = 14023219
31 feet Y = 4269803
67 meter
Z = -17321187
15 Z = -5281441
06
XDOT = -24370
863495 XDOT = -7405
525428
YDOT = -5389
291104 feet/sec YDOT = -1725
596856 meter/sec
ZDOT = -2561
944133 ZDOT = -816
908265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13670968
54 X = 4166911
21
Y = 3327664
55 feet Y = 1014272
15 meter
Z = -17330150
84 Z = -5282229
98
XDOT = -8875
291565 XDOT = -2705
188869
YDOT = 22218
622405 feet/sec YDOT = 6772
236109 meter/sec
ZDOT = -2729
360062 ZDOT = -831
908947
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 21051
82591564
00016717 00000-0 10270-3 0 9152
2 25544 51
6427 198
2672 0002964 36
1345 324
0005 15
48941852 30559
Satellite: ISS
Catalog Number: 25544
Epoch time: 21051
82591564 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 198
2672 deg
Eccentricity:
0002964
Arg of perigee: 36
1345 deg
Mean anomaly: 324
0005 deg
Mean motion: 15
48941852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3055
Checksum: 305
Coasting Arc #17 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2021/052/19:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 957811
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 13146
85 A = 6792657
25 meter
Y = -4280392
77 meter E =
0004961
Z = 5269960
91 I = 51
53597
XDOT = 7558
515289 Wp = 81
94719
YDOT = 993
503186 meter/sec RA = 192
19900 deg
ZDOT = 788
135121 TA =
50641
MA =
50591
Ha = 230
015 n
mi
Hp = 222
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 43132
70 X = 35412
59
Y = -14043283
36 feet Y = -4280121
31 meter
Z = 17289897
98 Z = 5270078
80
XDOT = 24798
278507 XDOT = 7543
015639
YDOT = 3259
524890 feet/sec YDOT = 1077
941284 meter/sec
ZDOT = 2585
745148 ZDOT = 824
813059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13917166
23 X = -4241952
27
Y = -1873913
46 feet Y = -571168
82 meter
Z = 17290378
04 Z = 5270107
23
XDOT = 6530
760940 XDOT = 1990
575934
YDOT = -23072
780374 feet/sec YDOT = -7032
583458 meter/sec
ZDOT = 2756
200392 ZDOT = 840
089880
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 21052
85818722
00016717 00000-0 10270-3 0 9165
2 25544 51
6418 193
1613 0003123 40
8627 319
2756 15
48963750 30719
Satellite: ISS
Catalog Number: 25544
Epoch time: 21052
85818722 = yrday
fracday
Element set: 916
Inclination: 51
6418 deg
RA of node: 193
1613 deg
Eccentricity:
0003123
Arg of perigee: 40
8627 deg
Mean anomaly: 319
2756 deg
Mean motion: 15
48963750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3071
Checksum: 308
Coasting Arc #18 (Orbit 3079)
---------------------------------------
Vector Time (GMT): 2021/053/09:36:25
000
Vector Time (MET): N/A
Weight (LBS) : 972941
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5919841
31 A = 6800473
97 meter
Y = -1451458
66 meter E =
0014733
Z = 3003946
29 I = 51
57990
XDOT = 3644
670522 Wp = 87
23950
YDOT = 4571
694012 meter/sec RA = 189
23427 deg
ZDOT = -4951
804880 TA = 58
41100
MA = 58
26727
Ha = 229
843 n
mi
Hp = 222
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19422051
53 X = 5921040
86
Y = -4762003
46 feet Y = -1385252
05 meter
Z = 9855466
83 Z = 3032704
82
XDOT = 11957
580452 XDOT = 3617
330066
YDOT = 14998
996103 feet/sec YDOT = 4612
298533 meter/sec
ZDOT = -16246
079003 ZDOT = -4934
167241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12686038
88 X = 3866704
65
Y = 15372227
74 feet Y = 4685455
01 meter
Z = 9989095
10 Z = 3044676
19
XDOT = -7156
918259 XDOT = -2181
428685
YDOT = 16455
637822 feet/sec YDOT = 5015
678408 meter/sec
ZDOT = -16164
035643 ZDOT = -4926
798064
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 21053
43883860
00016717 00000-0 10270-3 0 9176
2 25544 51
6397 190
2862 0002858 37
6291 322
5059 15
48966118 30808
Satellite: ISS
Catalog Number: 25544
Epoch time: 21053
43883860 = yrday
fracday
Element set: 917
Inclination: 51
6397 deg
RA of node: 190
2862 deg
Eccentricity:
0002858
Arg of perigee: 37
6291 deg
Mean anomaly: 322
5059 deg
Mean motion: 15
48966118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3080
Checksum: 328
Coasting Arc #19 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2021/054/01:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 972941
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 287329
76 A = 6792592
89 meter
Y = 4256978
01 meter E =
0017030
Z = -5300108
17 I = 51
57872
XDOT = -7615
243177 Wp = 77
29900
YDOT = -285
563505 meter/sec RA = 185
96882 deg
ZDOT = -640
287036 TA = 186
55515
MA = 186
57745
Ha = 230
055 n
mi
Hp = 221
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 942682
95 X = 265449
83
Y = 13966463
30 feet Y = 4260068
85 meter
Z = -17388806
33 Z = -5298765
57
XDOT = -24984
393626 XDOT = -7608
373872
YDOT = -936
888140 feet/sec YDOT = -370
684232 meter/sec
ZDOT = -2100
679253 ZDOT = -677
261307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -149620
14 X = -45604
22
Y = -14005278
63 feet Y = -4268808
93 meter
Z = -17382494
58 Z = -5298184
35
XDOT = 23833
863601 XDOT = 7264
561625
YDOT = 2573
701510 feet/sec YDOT = 784
464220 meter/sec
ZDOT = -2272
536985 ZDOT = -692
669273
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 21054
08400856
00016717 00000-0 10270-3 0 9189
2 25544 51
6426 187
0986 0003261 39
3272 320
8115 15
48966004 30908
Satellite: ISS
Catalog Number: 25544
Epoch time: 21054
08400856 = yrday
fracday
Element set: 918
Inclination: 51
6426 deg
RA of node: 187
0986 deg
Eccentricity:
0003261
Arg of perigee: 39
3272 deg
Mean anomaly: 320
8115 deg
Mean motion: 15
48966004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 301
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