[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 30th 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) : 19920 769 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
335/15:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 221
8
338/19:32:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
9
340/16:39:40
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 222
0
341/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 221
7
341/22:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 221
9
Coasting Arc #1 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2020/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4254822
88 A = 6794939
68 meter
Y = 2584348
99 meter E =
0010027
Z = 4618586
27 I = 51
24650
XDOT = -1074
755877 Wp = 67
64235
YDOT = 7003
773320 meter/sec RA = 259
40776 deg
ZDOT = -2920
027875 TA = 51
64965
MA = 51
55958
Ha = 229
494 n
mi
Hp = 221
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13959392
65 X = 4203172
76
Y = 8478835
27 feet Y = 2631640
35 meter
Z = 15152842
08 Z = 4639129
70
XDOT = -3526
101960 XDOT = -1138
810190
YDOT = 22978
258924 feet/sec YDOT = 6991
396688 meter/sec
ZDOT = -9580
143948 ZDOT = -2925
403804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13389065
14 X = -4080987
06
Y = 9197981
03 feet Y = 2803544
62 meter
Z = 15247753
73 Z = 4647515
34
XDOT = -18903
326446 XDOT = -5761
733901
YDOT = -11546
021779 feet/sec YDOT = -3519
227438 meter/sec
ZDOT = -9605
189097 ZDOT = -2927
661637
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 20332
54318786
00016717 00000-0 10270-3 0 9009
2 25544 51
6437 260
1794 0001835 80
0152 280
1205 15
49076550 17334
Satellite: ISS
Catalog Number: 25544
Epoch time: 20332
54318786 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 260
1794 deg
Eccentricity:
0001835
Arg of perigee: 80
0152 deg
Mean anomaly: 280
1205 deg
Mean motion: 15
49076550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 287
Coasting Arc #2 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2020/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4467905
46 A = 6794940
78 meter
Y = -2244093
31 meter E =
0012037
Z = -4613132
12 I = 51
25464
XDOT = 495
105019 Wp = 105
60021
YDOT = -7041
448135 meter/sec RA = 254
43370 deg
ZDOT = 2949
137717 TA = 194
00496
MA = 194
03836
Ha = 229
611 n
mi
Hp = 221
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14658482
47 X = -4420070
81
Y = -7362510
87 feet Y = -2293788
76 meter
Z = -15134947
91 Z = -4634719
96
XDOT = 1624
360297 XDOT = 559
482286
YDOT = -23101
863960 feet/sec YDOT = -7035
551828 meter/sec
ZDOT = 9675
648677 ZDOT = 2951
698518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12475596
27 X = 3802561
74
Y = -10507498
30 feet Y = -3202685
48 meter
Z = -15234707
09 Z = -4643538
72
XDOT = 19879
177128 XDOT = 6059
173189
YDOT = 9572
132561 feet/sec YDOT = 2917
586005 meter/sec
ZDOT = 9687
668536 ZDOT = 2952
801370
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 20333
51086124
00016717 00000-0 10270-3 0 9016
2 25544 51
6442 255
3919 0001911 81
3902 278
7465 15
49093513 17482
Satellite: ISS
Catalog Number: 25544
Epoch time: 20333
51086124 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 255
3919 deg
Eccentricity:
0001911
Arg of perigee: 81
3902 deg
Mean anomaly: 278
7465 deg
Mean motion: 15
49093513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 302
Coasting Arc #3 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2020/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4637275
85 A = 6795050
78 meter
Y = 1908741
48 meter E =
0010298
Z = 4578759
64 I = 51
26492
XDOT = 70
430929 Wp = 69
31396
YDOT = 7051
340595 meter/sec RA = 249
46192 deg
ZDOT = -3001
739749 TA = 50
87132
MA = 50
77982
Ha = 229
514 n
mi
Hp = 221
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15214159
63 X = 4593345
60
Y = 6262275
19 feet Y = 1960352
69 meter
Z = 15022177
28 Z = 4601179
71
XDOT = 231
072602 XDOT = 6
156519
YDOT = 23134
319537 feet/sec YDOT = 7051
769157 meter/sec
ZDOT = -9848
227522 ZDOT = -3001
552944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11482518
22 X = -3499871
55
Y = 11649651
30 feet Y = 3550813
72 meter
Z = 15125804
24 Z = 4610345
13
XDOT = -20700
896073 XDOT = -6309
633123
YDOT = -7579
568876 feet/sec YDOT = -2310
252593 meter/sec
ZDOT = -9847
532641 ZDOT = -3001
527949
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 20334
54304296
00016717 00000-0 10270-3 0 9024
2 25544 51
6439 250
2869 0001947 84
3370 275
8003 15
49088145 17646
Satellite: ISS
Catalog Number: 25544
Epoch time: 20334
54304296 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 250
2869 deg
Eccentricity:
0001947
Arg of perigee: 84
3370 deg
Mean anomaly: 275
8003 deg
Mean motion: 15
49088145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1764
Checksum: 314
Coasting Arc #4 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2020/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4796468
29 A = 6795056
26 meter
Y = -1540599
47 meter E =
0011850
Z = -4571607
23 I = 51
27861
XDOT = -642
190773 Wp = 106
80800
YDOT = -6993
528299 meter/sec RA = 244
48962 deg
ZDOT = 3033
752076 TA = 193
72521
MA = 193
75746
Ha = 229
585 n
mi
Hp = 221
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15736444
53 X = -4756677
67
Y = -5054460
20 feet Y = -1594013
94 meter
Z = -14998711
39 Z = -4594810
62
XDOT = -2106
925107 XDOT = -578
675814
YDOT = -22944
646650 feet/sec YDOT = -7000
354996 meter/sec
ZDOT = 9953
254841 ZDOT = 3030
785863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10341472
73 X = 3152080
89
Y = -12767452
17 feet Y = -3891519
42 meter
Z = -15105982
42 Z = -4604303
44
XDOT = 21259
174879 XDOT = 6479
796503
YDOT = 5471
727053 feet/sec YDOT = 1667
782406 meter/sec
ZDOT = 9939
694289 ZDOT = 3029
618819
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 20335
51070959
00016717 00000-0 10270-3 0 9039
2 25544 51
6444 245
4997 0001882 87
8343 272
3023 15
49106064 17797
Satellite: ISS
Catalog Number: 25544
Epoch time: 20335
51070959 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 245
4997 deg
Eccentricity:
0001882
Arg of perigee: 87
8343 deg
Mean anomaly: 272
3023 deg
Mean motion: 15
49106064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 320
Coasting Arc #5 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2020/335/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4554317
77 A = 6793084
60 meter
Y = -83390
50 meter E =
0014778
Z = -5053019
25 I = 51
27377
XDOT = -1892
728800 Wp = 101
92706
YDOT = -7182
504382 meter/sec RA = 243
86734 deg
ZDOT = 1826
024068 TA = 185
88314
MA = 185
90051
Ha = 229
520 n
mi
Hp = 221
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14941987
43 X = -4528501
63
Y = -273590
87 feet Y = -134175
13 meter
Z = -16578147
13 Z = -5075080
08
XDOT = -6209
740159 XDOT = -1821
141141
YDOT = -23564
646922 feet/sec YDOT = -7203
270202 meter/sec
ZDOT = 5990
892610 ZDOT = 1817
002681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5937844
69 X = -1809855
06
Y = -13589951
47 feet Y = -4142217
21 meter
Z = -16680168
53 Z = -5084115
37
XDOT = 17815
739260 XDOT = 5430
237326
YDOT = -15080
111375 feet/sec YDOT = -4596
417947 meter/sec
ZDOT = 5949
331771 ZDOT = 1813
356324
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 20335
63972992
00016717 00000-0 10270-3 0 9041
2 25544 51
6442 244
8617 0001714 87
2733 272
8613 15
49114415 17810
Satellite: ISS
Catalog Number: 25544
Epoch time: 20335
63972992 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 244
8617 deg
Eccentricity:
0001714
Arg of perigee: 87
2733 deg
Mean anomaly: 272
8613 deg
Mean motion: 15
49114415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 315
Coasting Arc #6 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2020/336/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4556198
78 A = 6793076
34 meter
Y = -248438
57 meter E =
0006925
Z = 5027945
05 I = 51
29048
XDOT = 2465
618514 Wp = 63
10147
YDOT = 7007
856740 meter/sec RA = 238
89641 deg
ZDOT = -1882
923004 TA = 45
27869
MA = 45
22232
Ha = 229
279 n
mi
Hp = 221
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14948158
73 X = 4534215
00
Y = -815087
17 feet Y = -197611
53 meter
Z = 16495882
72 Z = 5050024
21
XDOT = 8089
299586 XDOT = 2396
217595
YDOT = 22991
655972 feet/sec YDOT = 7035
041284 meter/sec
ZDOT = -6177
568912 ZDOT = -1871
113347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7155058
03 X = 2180861
69
Y = 13020646
33 feet Y = 3968693
00 meter
Z = 16598008
23 Z = 5059072
91
XDOT = -16257
003250 XDOT = -4955
134591
YDOT = 16760
028334 feet/sec YDOT = 5108
456636 meter/sec
ZDOT = -6123
091404 ZDOT = -1866
318260
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 20336
67190209
00016717 00000-0 10270-3 0 9050
2 25544 51
6447 239
7558 0001558 89
2359 270
8969 15
49135839 17976
Satellite: ISS
Catalog Number: 25544
Epoch time: 20336
67190209 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 239
7558 deg
Eccentricity:
0001558
Arg of perigee: 89
2359 deg
Mean anomaly: 270
8969 deg
Mean motion: 15
49135839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 360
Coasting Arc #7 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2020/337/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4546124
68 A = 6793170
23 meter
Y = 595926
96 meter E =
0014570
Z = -5025802
65 I = 51
30782
XDOT = -3015
217508 Wp = 103
13498
YDOT = -6760
218755 meter/sec RA = 233
92504 deg
ZDOT = 1927
351341 TA = 185
69099
MA = 185
70756
Ha = 229
484 n
mi
Hp = 221
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14915107
22 X = -4528037
88
Y = 1955140
95 feet Y = 545190
83 meter
Z = -16488853
82 Z = -5047842
18
XDOT = -9892
445891 XDOT = -2948
760675
YDOT = -22179
195392 feet/sec YDOT = -6793
565791 meter/sec
ZDOT = 6323
331171 ZDOT = 1912
864804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8382260
02 X = -2554912
85
Y = -12355073
48 feet Y = -3765826
40 meter
Z = -16590816
02 Z = -5056880
72
XDOT = 14470
719666 XDOT = 4410
675354
YDOT = -18212
424052 feet/sec YDOT = -5551
146851 meter/sec
ZDOT = 6256
446202 ZDOT = 1906
964803
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 20337
63956113
00016717 00000-0 10270-3 0 9062
2 25544 51
6433 234
9674 0001659 92
1374 267
9966 15
49124646 18125
Satellite: ISS
Catalog Number: 25544
Epoch time: 20337
63956113 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 234
9674 deg
Eccentricity:
0001659
Arg of perigee: 92
1374 deg
Mean anomaly: 267
9966 deg
Mean motion: 15
49124646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 331
Coasting Arc #8 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2020/338/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4500732
30 A = 6793219
59 meter
Y = -923630
38 meter E =
0007135
Z = 4999111
28 I = 51
32822
XDOT = 3546
761696 Wp = 64
99803
YDOT = 6496
594374 meter/sec RA = 228
95685 deg
ZDOT = -1987
672212 TA = 44
43234
MA = 44
37512
Ha = 229
318 n
mi
Hp = 221
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14766182
08 X = 4486443
11
Y = -3030283
40 feet Y = -873380
61 meter
Z = 16401283
72 Z = 5020939
39
XDOT = 11636
357270 XDOT = 3483
506250
YDOT = 21314
286004 feet/sec YDOT = 6535
903425 meter/sec
ZDOT = -6521
234290 ZDOT = -1970
595959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9477414
17 X = 2888715
84
Y = 11579205
88 feet Y = 3529341
95 meter
Z = 16502286
81 Z = 5029897
02
XDOT = -12625
799812 XDOT = -3848
343783
YDOT = 19539
588000 feet/sec YDOT = 5955
666422 meter/sec
ZDOT = -6442
340378 ZDOT = -1963
625347
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 20338
67172690
00016717 00000-0 10270-3 0 9078
2 25544 51
6425 229
8616 0001630 96
3859 263
7477 15
49129333 18284
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
67172690 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 229
8616 deg
Eccentricity:
0001630
Arg of perigee: 96
3859 deg
Mean anomaly: 263
7477 deg
Mean motion: 15
49129333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 336
Coasting Arc #9 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2020/338/19:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1934943
89 A = 6792681
78 meter
Y = -3996487
79 meter E =
0006572
Z = 5136391
34 I = 51
32964
XDOT = 5843
671631 Wp = 121
75458
YDOT = 4733
407111 meter/sec RA = 228
04957 deg
ZDOT = 1476
758518 TA = 313
92995
MA = 313
98417
Ha = 229
436 n
mi
Hp = 221
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6348241
11 X = 1954540
21
Y = -13111836
57 feet Y = -3974741
05 meter
Z = 16851677
62 Z = 5145837
60
XDOT = 19172
151021 XDOT = 5783
133632
YDOT = 15529
550889 feet/sec YDOT = 4798
416530 meter/sec
ZDOT = 4845
008261 ZDOT = 1504
998648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4993945
56 X = 1522154
61
Y = -13630987
63 feet Y = -4154725
03 meter
Z = 16895447
50 Z = 5149732
40
XDOT = 19498
059247 XDOT = 5943
008459
YDOT = 13330
067898 feet/sec YDOT = 4063
004695 meter/sec
ZDOT = 4975
586797 ZDOT = 1516
558856
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 20338
86525937
00016717 00000-0 10270-3 0 9086
2 25544 51
6416 228
9001 0001865 112
4839 247
6508 15
49137020 18312
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
86525937 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 228
9001 deg
Eccentricity:
0001865
Arg of perigee: 112
4839 deg
Mean anomaly: 247
6508 deg
Mean motion: 15
49137020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1831
Checksum: 312
Coasting Arc #10 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2020/339/19:32:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1643148
76 A = 6792656
53 meter
Y = 4114949
33 meter E =
0015326
Z = -5162155
41 I = 51
35341
XDOT = -6200
359549 Wp = 83
52163
YDOT = -4249
113643 meter/sec RA = 223
08326 deg
ZDOT = -1415
456789 TA = 172
78305
MA = 172
76096
Ha = 229
527 n
mi
Hp = 221
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5390907
99 X = -1663966
39
Y = 13500489
93 feet Y = 4096458
78 meter
Z = -16936205
42 Z = -5170187
20
XDOT = -20342
386971 XDOT = -6145
508353
YDOT = -13940
661558 feet/sec YDOT = -4318
143624 meter/sec
ZDOT = -4643
887103 ZDOT = -1445
443160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3764026
14 X = -1147275
17
Y = 13996248
51 feet Y = 4266056
55 meter
Z = -16973429
41 Z = -5173501
28
XDOT = -20694
421917 XDOT = -6307
659800
YDOT = -11357
555674 feet/sec YDOT = -3461
782969 meter/sec
ZDOT = -4782
582596 ZDOT = -1457
731175
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 20339
83291284
00016717 00000-0 10270-3 0 9090
2 25544 51
6419 224
1137 0001924 115
0672 245
0678 15
49129383 18462
Satellite: ISS
Catalog Number: 25544
Epoch time: 20339
83291284 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 224
1137 deg
Eccentricity:
0001924
Arg of perigee: 115
0672 deg
Mean anomaly: 245
0678 deg
Mean motion: 15
49129383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 316
Coasting Arc #11 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2020/340/16:39:40
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5311112
86 A = 6796280
46 meter
Y = -77480
87 meter E =
0011347
Z = 4231405
81 I = 51
38585
XDOT = 2972
565521 Wp = 79
50865
YDOT = 6072
444137 meter/sec RA = 218
67756 deg
ZDOT = -3609
568783 TA = 47
60618
MA = 47
51021
Ha = 229
381 n
mi
Hp = 221
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17424910
95 X = 5291030
79
Y = -254202
32 feet Y = -18201
00 meter
Z = 13882565
00 Z = 4257156
35
XDOT = 9752
511552 XDOT = 2921
973908
YDOT = 19922
716986 feet/sec YDOT = 6105
403074 meter/sec
ZDOT = -11842
417266 ZDOT = -3595
251335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14159712
57 X = 4315880
39
Y = 9993581
19 feet Y = 3046043
55 meter
Z = 14001736
55 Z = 4267729
30
XDOT = -3045
488169 XDOT = -928
264794
YDOT = 20861
395453 feet/sec YDOT = 6358
553334 meter/sec
ZDOT = -11776
231784 ZDOT = -3589
395448
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 20340
73605221
00016717 00000-0 10270-3 0 9103
2 25544 51
6399 219
6454 0001761 113
1882 246
9454 15
49107121 18605
Satellite: ISS
Catalog Number: 25544
Epoch time: 20340
73605221 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 219
6454 deg
Eccentricity:
0001761
Arg of perigee: 113
1882 deg
Mean anomaly: 246
9454 deg
Mean motion: 15
49107121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1860
Checksum: 292
Coasting Arc #12 (Orbit 1874)
---------------------------------------
Vector Time (GMT): 2020/341/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2374972
40 A = 6791942
45 meter
Y = 3517896
21 meter E =
0016701
Z = -5316807
14 I = 51
39905
XDOT = -6350
352861 Wp = 92
87909
YDOT = -4261
990428 meter/sec RA = 213
77214 deg
ZDOT = 15
900305 TA = 177
27789
MA = 177
26879
Ha = 229
562 n
mi
Hp = 221
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7791904
21 X = -2388308
07
Y = 11541654
24 feet Y = 3491263
56 meter
Z = -17443592
97 Z = -5328375
84
XDOT = -20834
491015 XDOT = -6302
299256
YDOT = -13982
908228 feet/sec YDOT = -4332
735951 meter/sec
ZDOT = 52
166354 ZDOT = -14
830956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13111451
57 X = -3996370
44
Y = 4487897
52 feet Y = 1367911
16 meter
Z = -17497174
15 Z = -5333138
68
XDOT = -7693
909275 XDOT = -2345
103547
YDOT = -22818
951060 feet/sec YDOT = -6955
216283 meter/sec
ZDOT = -90
031258 ZDOT = -27
441528
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 20341
70369966
00016717 00000-0 10270-3 0 9115
2 25544 51
6404 214
8582 0002011 112
6759 247
4604 15
49133847 18750
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
70369966 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 214
8582 deg
Eccentricity:
0002011
Arg of perigee: 112
6759 deg
Mean anomaly: 247
4604 deg
Mean motion: 15
49133847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1875
Checksum: 309
Coasting Arc #13 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2020/341/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1675194
29 A = 6792154
06 meter
Y = 3937260
93 meter E =
0016036
Z = -5288920
95 I = 51
40935
XDOT = -6680
883848 Wp = 88
51227
YDOT = -3671
698824 meter/sec RA = 212
50460 deg
ZDOT = -618
487696 TA = 175
55654
MA = 175
54228
Ha = 229
461 n
mi
Hp = 221
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5496044
26 X = -1693406
88
Y = 12917522
74 feet Y = 3918426
40 meter
Z = -17352102
85 Z = -5297102
23
XDOT = -21918
910262 XDOT = -6636
325003
YDOT = -12046
255983 feet/sec YDOT = -3746
160058 meter/sec
ZDOT = -2029
159109 ZDOT = -650
832960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7550983
06 X = 2301539
64
Y = 11778566
35 feet Y = 3590107
02 meter
Z = -17390008
60 Z = -5300474
62
XDOT = -21521
730072 XDOT = -6559
823326
YDOT = 10586
166422 feet/sec YDOT = 3226
663526 meter/sec
ZDOT = -2178
840120 ZDOT = -664
110469
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 20341
96173740
00016717 00000-0 10270-3 0 9127
2 25544 51
6430 213
5837 0001672 117
6512 242
4808 15
49110800 18791
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
96173740 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 213
5837 deg
Eccentricity:
0001672
Arg of perigee: 117
6512 deg
Mean anomaly: 242
4808 deg
Mean motion: 15
49110800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 292
Coasting Arc #14 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2020/342/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1382558
03 A = 6791985
10 meter
Y = -4030973
81 meter E =
0004607
Z = 5285374
89 I = 51
43864
XDOT = 6972
253037 Wp = 117
58799
YDOT = 3131
197757 meter/sec RA = 207
54368 deg
ZDOT = 561
774077 TA = 327
01854
MA = 327
04727
Ha = 229
335 n
mi
Hp = 221
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4535951
55 X = 1401857
47
Y = -13224979
69 feet Y = -4015405
58 meter
Z = 17340468
81 Z = 5292137
37
XDOT = 22874
845921 XDOT = 6933
992060
YDOT = 10272
958521 feet/sec YDOT = 3208
952521 meter/sec
ZDOT = 1843
090805 ZDOT = 595
549954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8541466
93 X = -2603439
12
Y = -11019553
16 feet Y = -3358759
80 meter
Z = 17371804
56 Z = 5294926
03
XDOT = 20439
549381 XDOT = 6229
974651
YDOT = -12678
345778 feet/sec YDOT = -3864
359793 meter/sec
ZDOT = 1999
424612 ZDOT = 609
424622
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 20342
99389097
00016717 00000-0 10270-3 0 9136
2 25544 51
6431 208
4777 0001701 122
0222 238
1094 15
49155956 18957
Satellite: ISS
Catalog Number: 25544
Epoch time: 20342
99389097 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 208
4777 deg
Eccentricity:
0001701
Arg of perigee: 122
0222 deg
Mean anomaly: 238
1094 deg
Mean motion: 15
49155956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 317
Coasting Arc #15 (Orbit 1909)
---------------------------------------
Vector Time (GMT): 2020/343/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1100583
07 A = 6792100
01 meter
Y = 4116212
28 meter E =
0016029
Z = -5303360
88 I = 51
46859
XDOT = -7189
593985 Wp = 89
98453
YDOT = -2561
464397 meter/sec RA = 202
58428 deg
ZDOT = -497
363167 TA = 175
25471
MA = 175
23950
Ha = 229
433 n
mi
Hp = 221
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3610836
83 X = -1120769
17
Y = 13504633
45 feet Y = 4103792
28 meter
Z = -17399477
94 Z = -5308755
84
XDOT = -23587
906774 XDOT = -7158
000648
YDOT = -8403
754583 feet/sec YDOT = -2641
686916 meter/sec
ZDOT = -1631
768919 ZDOT = -532
211047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9465788
34 X = 2885172
29
Y = 10244092
02 feet Y = 3122399
25 meter
Z = -17424480
75 Z = -5310981
73
XDOT = -19079
014575 XDOT = -5815
283643
YDOT = 14586
806197 feet/sec YDOT = 4446
058529 meter/sec
ZDOT = -1793
092933 ZDOT = -546
534726
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 20343
96153475
00016717 00000-0 10270-3 0 9144
2 25544 51
6425 203
6905 0001685 124
4038 235
7272 15
49113211 19109
Satellite: ISS
Catalog Number: 25544
Epoch time: 20343
96153475 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 203
6905 deg
Eccentricity:
0001685
Arg of perigee: 124
4038 deg
Mean anomaly: 235
7272 deg
Mean motion: 15
49113211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1910
Checksum: 287
Coasting Arc #16 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2020/344/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 803219
93 A = 6791927
66 meter
Y = -4167512
96 meter E =
0004382
Z = 5299259
08 I = 51
50101
XDOT = 7389
719997 Wp = 116
38223
YDOT = 1983
063184 meter/sec RA = 197
62719 deg
ZDOT = 437
283121 TA = 329
42397
MA = 329
44951
Ha = 229
327 n
mi
Hp = 221
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2635235
99 X = 824021
61
Y = -13672942
79 feet Y = -4158414
86 meter
Z = 17386020
60 Z = 5303211
06
XDOT = 24244
488178 XDOT = 7364
871471
YDOT = 6506
112807 feet/sec YDOT = 2065
561372 meter/sec
ZDOT = 1434
655909 ZDOT = 473
119633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10297416
80 X = -3138652
64
Y = -9339145
97 feet Y = -2846571
69 meter
Z = 17404341
56 Z = 5304843
31
XDOT = 17612
614549 XDOT = 5368
324915
YDOT = -16423
615704 feet/sec YDOT = -5005
918067 meter/sec
ZDOT = 1600
582552 ZDOT = 487
857562
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 20344
99368219
00016717 00000-0 10270-3 0 9153
2 25544 51
6433 198
5841 0001667 124
6641 235
4666 15
49160425 19261
Satellite: ISS
Catalog Number: 25544
Epoch time: 20344
99368219 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 198
5841 deg
Eccentricity:
0001667
Arg of perigee: 124
6641 deg
Mean anomaly: 235
4666 deg
Mean motion: 15
49160425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 328
Coasting Arc #17 (Orbit 1940)
---------------------------------------
Vector Time (GMT): 2020/345/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -516913
98 A = 6792030
41 meter
Y = 4213022
41 meter E =
0016153
Z = -5316356
18 I = 51
53319
XDOT = -7512
344184 Wp = 90
82260
YDOT = -1387
551392 meter/sec RA = 192
67215 deg
ZDOT = -370
357290 TA = 175
63871
MA = 175
62462
Ha = 229
433 n
mi
Hp = 221
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1695912
00 X = -538162
69
Y = 13822252
01 feet Y = 4207123
56 meter
Z = -17442113
46 Z = -5318918
42
XDOT = -24646
798504 XDOT = -7494
470821
YDOT = -4552
333963 feet/sec YDOT = -1471
459853 meter/sec
ZDOT = -1215
082973 ZDOT = -406
806519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11065866
47 X = 3372876
10
Y = 8429861
80 feet Y = 2569421
88 meter
Z = -17454000
10 Z = -5319979
23
XDOT = -15909
179836 XDOT = -4849
118014
YDOT = 18026
827507 feet/sec YDOT = 5494
577024 meter/sec
ZDOT = -1383
872127 ZDOT = -421
804224
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 20345
96132018
00016717 00000-0 10270-3 0 9168
2 25544 51
6428 193
7969 0001715 123
1273 237
0042 15
49123351 19412
Satellite: ISS
Catalog Number: 25544
Epoch time: 20345
96132018 = yrday
fracday
Element set: 916
Inclination: 51
6428 deg
RA of node: 193
7969 deg
Eccentricity:
0001715
Arg of perigee: 123
1273 deg
Mean anomaly: 237
0042 deg
Mean motion: 15
49123351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1941
Checksum: 294
Coasting Arc #18 (Orbit 1956)
---------------------------------------
Vector Time (GMT): 2020/346/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 219636
00 A = 6791898
99 meter
Y = -4223551
46 meter E =
0004290
Z = 5311133
35 I = 51
56541
XDOT = 7617
077211 Wp = 114
46826
YDOT = 785
891094 meter/sec RA = 187
71996 deg
ZDOT = 308
030694 TA = 332
57918
MA = 332
60182
Ha = 229
376 n
mi
Hp = 221
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 720590
55 X = 241049
87
Y = -13856796
14 feet Y = -4220976
20 meter
Z = 17424978
17 Z = 5312251
81
XDOT = 24990
410797 XDOT = 7606
226759
YDOT = 2578
382855 feet/sec YDOT = 871
010019 meter/sec
ZDOT = 1010
599390 ZDOT = 345
005778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11723966
51 X = -3573464
99
Y = -7409272
85 feet Y = -2258346
37 meter
Z = 17430180
70 Z = 5312719
08
XDOT = 14115
895705 XDOT = 4302
525011
YDOT = -19540
892305 feet/sec YDOT = -5956
063975 meter/sec
ZDOT = 1181
851566 ZDOT = 360
228357
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 20346
99346381
00016717 00000-0 10270-3 0 9173
2 25544 51
6418 188
6910 0001751 125
8891 234
2421 15
49158071 19579
Satellite: ISS
Catalog Number: 25544
Epoch time: 20346
99346381 = yrday
fracday
Element set: 917
Inclination: 51
6418 deg
RA of node: 188
6910 deg
Eccentricity:
0001751
Arg of perigee: 125
8891 deg
Mean anomaly: 234
2421 deg
Mean motion: 15
49158071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1957
Checksum: 326
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