[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 5th 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) : 14538 8138 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
340/16:39:38
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 221
9
341/16:30:00
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
7
341/22:40:00
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
351/15:35:00
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
0
354/02:00:00
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
1
Coasting Arc #1 (Orbit 1840)
---------------------------------------
Vector Time (GMT): 2020/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5139297
94 A = 6795368
29 meter
Y = -65173
77 meter E =
0011039
Z = -4456382
17 I = 51
35688
XDOT = -2739
334241 Wp = 108
93615
YDOT = -6358
585409 meter/sec RA = 224
61251 deg
ZDOT = 3255
249764 TA = 194
05694
MA = 194
08769
Ha = 229
431 n
mi
Hp = 221
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16861213
73 X = -5116540
56
Y = -213824
70 feet Y = -122517
20 meter
Z = -14620676
42 Z = -4481291
70
XDOT = -8987
317063 XDOT = -2683
839216
YDOT = -20861
500687 feet/sec YDOT = -6388
908786 meter/sec
ZDOT = 10679
953293 ZDOT = 3242
076974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5145976
01 X = 1568493
49
Y = -15952479
70 feet Y = -4862315
81 meter
Z = -14735934
00 Z = -4491512
68
XDOT = 21441
605379 XDOT = 6535
401319
YDOT = -2883
185249 feet/sec YDOT = -878
794864 meter/sec
ZDOT = 10619
096454 ZDOT = 3236
700599
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
51029353
00016717 00000-0 10270-3 0 9002
2 25544 51
6437 225
7139 0001645 97
8277 262
3060 15
49146259 18412
Satellite: ISS
Catalog Number: 25544
Epoch time: 20339
51029353 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 225
7139 deg
Eccentricity:
0001645
Arg of perigee: 97
8277 deg
Mean anomaly: 262
3060 deg
Mean motion: 15
49146259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1841
Checksum: 308
Coasting Arc #2 (Orbit 1856)
---------------------------------------
Vector Time (GMT): 2020/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5153808
45 A = 6795373
09 meter
Y = -305456
33 meter E =
0010611
Z = 4411215
19 I = 51
38280
XDOT = 3215
069455 Wp = 73
91324
YDOT = 6111
924406 meter/sec RA = 219
64669 deg
ZDOT = -3323
517002 TA = 49
84469
MA = 49
75181
Ha = 229
209 n
mi
Hp = 221
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16908820
36 X = 5135413
94
Y = -1002153
32 feet Y = -247926
16 meter
Z = 14472490
77 Z = 4436205
68
XDOT = 10548
128133 XDOT = 3162
628868
YDOT = 20052
245427 feet/sec YDOT = 6147
584834 meter/sec
ZDOT = -10903
927173 ZDOT = -3308
026023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3716398
07 X = -1132758
13
Y = 16423761
09 feet Y = 5005962
38 meter
Z = 14588144
62 Z = 4446466
48
XDOT = -21018
283387 XDOT = -6406
372776
YDOT = 4893
220053 feet/sec YDOT = 1491
453472 meter/sec
ZDOT = -10832
315898 ZDOT = -3301
689886
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
54243700
00016717 00000-0 10270-3 0 9012
2 25544 51
6442 220
6075 0001573 98
0856 262
0473 15
49192228 18576
Satellite: ISS
Catalog Number: 25544
Epoch time: 20340
54243700 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 220
6075 deg
Eccentricity:
0001573
Arg of perigee: 98
0856 deg
Mean anomaly: 262
0473 deg
Mean motion: 15
49192228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1857
Checksum: 292
Coasting Arc #3 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2020/340/16:39:38
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5327364
27 A = 6796280
55 meter
Y = -44079
94 meter E =
0011439
Z = 4211366
60 I = 51
38590
XDOT = 2935
391133 Wp = 79
70586
YDOT = 6072
857838 meter/sec RA = 218
67628 deg
ZDOT = -3639
236380 TA = 47
76586
MA = 47
66886
Ha = 229
343 n
mi
Hp = 221
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17478229
23 X = 5307004
83
Y = -144619
24 feet Y = 15380
11 meter
Z = 13816819
56 Z = 4237195
41
XDOT = 9630
548335 XDOT = 2884
941764
YDOT = 19924
074273 feet/sec YDOT = 6105
401863 meter/sec
ZDOT = -11939
751904 ZDOT = -3625
099166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14137218
61 X = 4309024
23
Y = 10115880
14 feet Y = 3083320
27 meter
Z = 13936352
94 Z = 4247800
38
XDOT = -3138
612405 XDOT = -956
649061
YDOT = 20792
181488 feet/sec YDOT = 6337
456917 meter/sec
ZDOT = -11874
400523 ZDOT = -3619
317279
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
73596465
00016717 00000-0 10270-3 0 9023
2 25544 51
6397 219
6448 0001754 112
2617 247
8719 15
49131556 18607
Satellite: ISS
Catalog Number: 25544
Epoch time: 20340
73596465 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 219
6448 deg
Eccentricity:
0001754
Arg of perigee: 112
2617 deg
Mean anomaly: 247
8719 deg
Mean motion: 15
49131556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1860
Checksum: 324
Coasting Arc #4 (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 = -2430914
96 A = 6791872
95 meter
Y = 3480074
14 meter E =
0016713
Z = -5316338
27 I = 51
39886
XDOT = -6323
637913 Wp = 93
19385
YDOT = -4300
946290 meter/sec RA = 213
77012 deg
ZDOT = 75
402436 TA = 177
53311
MA = 177
52486
Ha = 229
526 n
mi
Hp = 221
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7975442
78 X = -2443825
81
Y = 11417566
08 feet Y = 3452818
28 meter
Z = -17442054
70 Z = -5328177
69
XDOT = -20746
843547 XDOT = -6275
439705
YDOT = -14110
716175 feet/sec YDOT = -4371
392265 meter/sec
ZDOT = 247
383319 ZDOT = 44
801293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13181566
46 X = -4017741
46
Y = 4277729
81 feet Y = 1303852
05 meter
Z = -17496888
53 Z = -5333051
62
XDOT = -7562
973539 XDOT = -2305
194335
YDOT = -22862
714557 feet/sec YDOT = -6968
555397 meter/sec
ZDOT = 105
788342 ZDOT = 32
244287
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
70359708
00016717 00000-0 10270-3 0 9039
2 25544 51
6403 214
8576 0002007 111
8598 248
2766 15
49157651 18756
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
70359708 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 214
8576 deg
Eccentricity:
0002007
Arg of perigee: 111
8598 deg
Mean anomaly: 248
2766 deg
Mean motion: 15
49157651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1875
Checksum: 319
Coasting Arc #5 (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 = -1736374
52 A = 6792057
63 meter
Y = 3903347
48 meter E =
0016093
Z = -5294254
88 I = 51
40908
XDOT = -6661
198208 Wp = 88
82684
YDOT = -3717
046739 meter/sec RA = 212
50253 deg
ZDOT = -556
958996 TA = 175
83411
MA = 175
82069
Ha = 229
425 n
mi
Hp = 221
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5696766
78 X = -1754177
42
Y = 12806258
15 feet Y = 3883831
09 meter
Z = -17369602
62 Z = -5302732
36
XDOT = -21854
324830 XDOT = -6616
432603
YDOT = -12195
035234 feet/sec YDOT = -3791
286685 meter/sec
ZDOT = -1827
293293 ZDOT = -589
208137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7345246
61 X = 2238831
17
Y = 11880015
87 feet Y = 3621028
84 meter
Z = -17408879
06 Z = -5306226
34
XDOT = -21600
577847 XDOT = -6583
856128
YDOT = 10464
464007 feet/sec YDOT = 3189
568629 meter/sec
ZDOT = -1976
528962 ZDOT = -602
446028
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
96163083
00016717 00000-0 10270-3 0 9047
2 25544 51
6429 213
5830 0001666 116
5715 243
5606 15
49134950 18798
Satellite: ISS
Catalog Number: 25544
Epoch time: 20341
96163083 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 213
5830 deg
Eccentricity:
0001666
Arg of perigee: 116
5715 deg
Mean anomaly: 243
5606 deg
Mean motion: 15
49134950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 309
Coasting Arc #6 (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 = 1455700
62 A = 6791888
57 meter
Y = -3997758
63 meter E =
0004495
Z = 5290836
33 I = 51
43837
XDOT = 6953
408867 Wp = 115
98044
YDOT = 3184
683684 meter/sec RA = 207
54134 deg
ZDOT = 490
958354 TA = 329
30704
MA = 329
33333
Ha = 229
296 n
mi
Hp = 221
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4775920
68 X = 1474596
68
Y = -13116006
01 feet Y = -3981374
73 meter
Z = 17358386
91 Z = 5297953
13
XDOT = 22813
021218 XDOT = 6914
895178
YDOT = 10448
437283 feet/sec YDOT = 3262
226312 meter/sec
ZDOT = 1610
755754 ZDOT = 524
642083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8317608
37 X = -2535207
03
Y = -11158428
38 feet Y = -3401088
97 meter
Z = 17391362
65 Z = 5300887
34
XDOT = 20541
855172 XDOT = 6261
157456
YDOT = -12547
104939 feet/sec YDOT = -3824
357585 meter/sec
ZDOT = 1766
662592 ZDOT = 538
478758
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
99376858
00016717 00000-0 10270-3 0 9058
2 25544 51
6430 208
4768 0001694 121
0450 239
0867 15
49179686 18953
Satellite: ISS
Catalog Number: 25544
Epoch time: 20342
99376858 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 208
4768 deg
Eccentricity:
0001694
Arg of perigee: 121
0450 deg
Mean anomaly: 239
0867 deg
Mean motion: 15
49179686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 345
Coasting Arc #7 (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 = -1185379
51 A = 6792004
60 meter
Y = 4085576
96 meter E =
0016093
Z = -5308711
07 I = 51
46832
XDOT = -7172
616390 Wp = 90
42639
YDOT = -2622
522920 meter/sec RA = 202
58166 deg
ZDOT = -417
938958 TA = 175
57518
MA = 175
56093
Ha = 229
399 n
mi
Hp = 221
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3889040
39 X = -1205190
75
Y = 13404123
88 feet Y = 4072210
81 meter
Z = -17417031
08 Z = -5314517
04
XDOT = -23532
206004 XDOT = -7140
727340
YDOT = -8604
077820 feet/sec YDOT = -2702
553935 meter/sec
ZDOT = -1371
190807 ZDOT = -452
703653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9230776
14 X = 2813540
57
Y = 10423530
71 feet Y = 3177092
16 meter
Z = -17443936
58 Z = -5316911
87
XDOT = -19205
193671 XDOT = -5853
743031
YDOT = 14450
201987 feet/sec YDOT = 4404
421566 meter/sec
ZDOT = -1532
129328 ZDOT = -466
993019
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
96139765
00016717 00000-0 10270-3 0 9061
2 25544 51
6424 203
6895 0001678 123
3127 236
8184 15
49136741 19102
Satellite: ISS
Catalog Number: 25544
Epoch time: 20343
96139765 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 203
6895 deg
Eccentricity:
0001678
Arg of perigee: 123
3127 deg
Mean anomaly: 236
8184 deg
Mean motion: 15
49136741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1910
Checksum: 317
Coasting Arc #8 (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 = 900051
11 A = 6791832
16 meter
Y = -4141010
00 meter E =
0004262
Z = 5304343
75 I = 51
50075
XDOT = 7375
616937 Wp = 114
18611
YDOT = 2052
155380 meter/sec RA = 197
62431 deg
ZDOT = 348
642122 TA = 332
47020
MA = 332
49276
Ha = 229
289 n
mi
Hp = 221
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2952923
58 X = 920524
53
Y = -13585990
81 feet Y = -4130830
90 meter
Z = 17402702
59 Z = 5308765
31
XDOT = 24198
218296 XDOT = 7350
427420
YDOT = 6732
793243 feet/sec YDOT = 2134
493959 meter/sec
ZDOT = 1143
838984 ZDOT = 384
409303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10056254
22 X = -3065146
29
Y = -9563309
73 feet Y = -2914896
81 meter
Z = 17423197
74 Z = 5310590
67
XDOT = 17765
636663 XDOT = 5414
966055
YDOT = -16284
191235 feet/sec YDOT = -4963
421489 meter/sec
ZDOT = 1309
444248 ZDOT = 399
118607
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
99352958
00016717 00000-0 10270-3 0 9077
2 25544 51
6431 198
5830 0001661 123
6538 236
4771 15
49184111 19261
Satellite: ISS
Catalog Number: 25544
Epoch time: 20344
99352958 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 198
5830 deg
Eccentricity:
0001661
Arg of perigee: 123
6538 deg
Mean anomaly: 236
4771 deg
Mean motion: 15
49184111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 322
Coasting Arc #9 (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 = -624957
63 A = 6791940
59 meter
Y = 4192481
55 meter E =
0016217
Z = -5320935
33 I = 51
53292
XDOT = -7502
019768 Wp = 91
39681
YDOT = -1463
801552 meter/sec RA = 192
66900 deg
ZDOT = -273
339426 TA = 175
99353
MA = 175
98053
Ha = 229
402 n
mi
Hp = 221
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2050385
92 X = -645946
37
Y = 13754860
71 feet Y = 4185375
93 meter
Z = -17457136
89 Z = -5324021
78
XDOT = -24612
925748 XDOT = -7483
765783
YDOT = -4802
498529 feet/sec YDOT = -1547
592438 meter/sec
ZDOT = -896
782894 ZDOT = -309
737585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10826560
43 X = 3299935
62
Y = 8699763
88 feet Y = 2651688
03 meter
Z = -17471451
05 Z = -5325298
28
XDOT = -16088
157540 XDOT = -4903
670418
YDOT = 17888
993349 feet/sec YDOT = 5452
565173 meter/sec
ZDOT = -1065
335174 ZDOT = -324
714161
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
96115319
00016717 00000-0 10270-3 0 9084
2 25544 51
6426 193
7957 0001711 122
0687 238
0629 15
49145893 19417
Satellite: ISS
Catalog Number: 25544
Epoch time: 20345
96115319 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 193
7957 deg
Eccentricity:
0001711
Arg of perigee: 122
0687 deg
Mean anomaly: 238
0629 deg
Mean motion: 15
49145893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1941
Checksum: 325
Coasting Arc #10 (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 = 338964
02 A = 6791808
60 meter
Y = -4210542
49 meter E =
0004173
Z = 5315057
65 I = 51
56516
XDOT = 7611
584385 Wp = 111
70778
YDOT = 869
682947 meter/sec RA = 187
71656 deg
ZDOT = 201
894194 TA = 336
35533
MA = 336
37451
Ha = 229
338 n
mi
Hp = 221
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1112086
69 X = 360204
49
Y = -13814115
77 feet Y = -4206633
78 meter
Z = 17437853
20 Z = 5316755
35
XDOT = 24972
389714 XDOT = 7600
312914
YDOT = 2853
290507 feet/sec YDOT = 954
738105 meter/sec
ZDOT = 662
382527 ZDOT = 238
841582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11492369
73 X = -3502874
29
Y = -7727671
16 feet Y = -2355394
17 meter
Z = 17445738
50 Z = 5317461
10
XDOT = 14323
428538 XDOT = 4365
781018
YDOT = -19407
569452 feet/sec YDOT = -5915
427169 meter/sec
ZDOT = 833
505998 ZDOT = 254
052628
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
99328160
00016717 00000-0 10270-3 0 9099
2 25544 51
6416 188
6897 0001748 125
0373 235
0941 15
49181537 19573
Satellite: ISS
Catalog Number: 25544
Epoch time: 20346
99328160 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 188
6897 deg
Eccentricity:
0001748
Arg of perigee: 125
0373 deg
Mean anomaly: 235
0941 deg
Mean motion: 15
49181537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1957
Checksum: 336
Coasting Arc #11 (Orbit 1971)
---------------------------------------
Vector Time (GMT): 2020/347/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -62417
49 A = 6791885
61 meter
Y = 4226617
98 meter E =
0016180
Z = -5330151
49 I = 51
59946
XDOT = -7642
660186 Wp = 92
95036
YDOT = -269
595441 meter/sec RA = 182
76511 deg
ZDOT = -125
424677 TA = 175
85734
MA = 175
84393
Ha = 229
357 n
mi
Hp = 221
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -204781
81 X = -83784
98
Y = 13866856
89 feet Y = 4225801
26 meter
Z = -17487373
64 Z = -5330506
00
XDOT = -25074
344443 XDOT = -7638
468218
YDOT = -884
499479 feet/sec YDOT = -355
037699 meter/sec
ZDOT = -411
498283 ZDOT = -162
540125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12107363
01 X = 3690324
25
Y = 6759075
93 feet Y = 2060166
34 meter
Z = -17489040
74 Z = -5330659
62
XDOT = -12368
682097 XDOT = -3769
974303
YDOT = 20655
786034 feet/sec YDOT = 6295
883583 meter/sec
ZDOT = -583
431885 ZDOT = -177
830038
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 20347
96090097
00016717 00000-0 10270-3 0 9104
2 25544 51
6421 183
9017 0001712 127
8275 232
3030 15
49156389 19726
Satellite: ISS
Catalog Number: 25544
Epoch time: 20347
96090097 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 183
9017 deg
Eccentricity:
0001712
Arg of perigee: 127
8275 deg
Mean anomaly: 232
3030 deg
Mean motion: 15
49156389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1972
Checksum: 304
Coasting Arc #12 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2020/348/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -218548
24 A = 6791773
39 meter
Y = -4208591
62 meter E =
0004062
Z = 5322841
73 I = 51
63287
XDOT = 7656
447579 Wp = 107
97894
YDOT = -332
009030 meter/sec RA = 177
81649 deg
ZDOT = 50
597186 TA = 341
53123
MA = 341
54597
Ha = 229
359 n
mi
Hp = 221
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -717021
78 X = -197325
83
Y = -13807715
30 feet Y = -4210917
80 meter
Z = 17463391
52 Z = 5321830
95
XDOT = 25119
578671 XDOT = 7659
345385
YDOT = -1089
268472 feet/sec YDOT = -246
372942 meter/sec
ZDOT = 166
001266 ZDOT = 87
796591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12599895
03 X = -3840448
00
Y = -5707218
93 feet Y = -1739560
33 meter
Z = 17458735
99 Z = 5321422
73
XDOT = 10349
519818 XDOT = 3154
533641
YDOT = -21801
073064 feet/sec YDOT = -6644
967070 meter/sec
ZDOT = 338
359856 ZDOT = 103
132084
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 20348
99302362
00016717 00000-0 10270-3 0 9110
2 25544 51
6417 178
7949 0001771 124
9976 235
1340 15
49187399 19885
Satellite: ISS
Catalog Number: 25544
Epoch time: 20348
99302362 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 178
7949 deg
Eccentricity:
0001771
Arg of perigee: 124
9976 deg
Mean anomaly: 235
1340 deg
Mean motion: 15
49187399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 349
Coasting Arc #13 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2020/349/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 491253
55 A = 6791837
43 meter
Y = 4190623
49 meter E =
0016149
Z = -5336213
33 I = 51
66758
XDOT = -7592
025667 Wp = 94
10306
YDOT = 927
211274 meter/sec RA = 172
87007 deg
ZDOT = 28
178318 TA = 176
17222
MA = 176
15986
Ha = 229
313 n
mi
Hp = 222
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1611724
24 X = 470276
59
Y = 13748764
74 feet Y = 4196000
72 meter
Z = -17507261
60 Z = -5333877
20
XDOT = -24908
220693 XDOT = -7601
966644
YDOT = 3042
031740 feet/sec YDOT = 842
256205 meter/sec
ZDOT = 92
448551 ZDOT = -8
724916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13047850
26 X = 3976984
76
Y = 4664514
54 feet Y = 1421744
03 meter
Z = -17496465
45 Z = -5332922
67
XDOT = -8196
255384 XDOT = -2498
218641
YDOT = 22645
266679 feet/sec YDOT = 6902
277284 meter/sec
ZDOT = -78
576563 ZDOT = -23
950136
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
96063685
00016717 00000-0 10270-3 0 9121
2 25544 51
6425 174
0074 0001668 129
6683 230
4614 15
49169313 20031
Satellite: ISS
Catalog Number: 25544
Epoch time: 20349
96063685 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 174
0074 deg
Eccentricity:
0001668
Arg of perigee: 129
6683 deg
Mean anomaly: 230
4614 deg
Mean motion: 15
49169313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 306
Coasting Arc #14 (Orbit 2018)
---------------------------------------
Vector Time (GMT): 2020/350/22:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 997900
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -764873
55 A = 6791764
83 meter
Y = -4138778
50 meter E =
0003939
Z = 5327133
41 I = 51
69936
XDOT = 7510
441942 Wp = 105
32558
YDOT = -1521
801783 meter/sec RA = 167
92596 deg
ZDOT = -104
921902 TA = 345
66844
MA = 345
67961
Ha = 229
362 n
mi
Hp = 221
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2509427
65 X = -744411
73
Y = -13578669
62 feet Y = -4147218
42 meter
Z = 17477471
81 Z = 5323466
91
XDOT = 24640
557552 XDOT = 7527
410649
YDOT = -4992
788001 feet/sec YDOT = -1437
719732 meter/sec
ZDOT = -344
231963 ZDOT = -68
398254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13364641
93 X = -4073542
86
Y = -3557600
77 feet Y = -1084356
72 meter
Z = 17460507
99 Z = 5321962
84
XDOT = 5998
459266 XDOT = 1828
330384
YDOT = -23377
268476 feet/sec YDOT = -7125
391432 meter/sec
ZDOT = -174
926768 ZDOT = -53
317679
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
99275616
00016717 00000-0 10270-3 0 9136
2 25544 51
6408 168
9005 0001783 128
8482 231
2827 15
49189508 20194
Satellite: ISS
Catalog Number: 25544
Epoch time: 20350
99275616 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 168
9005 deg
Eccentricity:
0001783
Arg of perigee: 128
8482 deg
Mean anomaly: 231
2827 deg
Mean motion: 15
49189508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 324
Coasting Arc #15 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2020/351/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 982624
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3826254
30 A = 6793973
29 meter
Y = -2878841
99 meter E =
0009090
Z = 4815403
09 I = 51
73125
XDOT = 6125
685393 Wp = 124
57241
YDOT = -3814
606142 meter/sec RA = 164
45970 deg
ZDOT = 2578
358972 TA = 300
00667
MA = 300
09684
Ha = 229
280 n
mi
Hp = 222
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12553327
76 X = -3817168
16
Y = -9445019
65 feet Y = -2921579
94 meter
Z = 15798566
58 Z = 4796838
33
XDOT = 20097
393021 XDOT = 6155
362093
YDOT = -12515
112013 feet/sec YDOT = -3745
938841 meter/sec
ZDOT = 8459
182980 ZDOT = 2608
186389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3246252
12 X = -989457
65
Y = -15458574
66 feet Y = -4711773
56 meter
Z = 15712525
46 Z = 4789177
76
XDOT = 22178
834161 XDOT = 6760
108652
YDOT = 4109
748678 feet/sec YDOT = 1252
651397 meter/sec
ZDOT = 8597
486592 ZDOT = 2620
513913
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
70233650
00016717 00000-0 10270-3 0 9149
2 25544 51
6420 165
3859 0001815 147
8457 212
2804 15
49214470 20309
Satellite: ISS
Catalog Number: 25544
Epoch time: 20351
70233650 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 165
3859 deg
Eccentricity:
0001815
Arg of perigee: 147
8457 deg
Mean anomaly: 212
2804 deg
Mean motion: 15
49214470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2030
Checksum: 282
Coasting Arc #16 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2020/352/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 982624
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3985663
90 A = 6793914
09 meter
Y = 2599350
41 meter E =
0012023
Z = -4860276
41 I = 51
76432
XDOT = -5830
807601 Wp = 80
67724
YDOT = 4277
953746 meter/sec RA = 159
51997 deg
ZDOT = -2497
013063 TA = 164
78919
MA = 164
75301
Ha = 229
205 n
mi
Hp = 222
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13076325
12 X = 3979909
14
Y = 8528052
52 feet Y = 2643889
53 meter
Z = -15945788
76 Z = -4840929
40
XDOT = -19129
946197 XDOT = -5866
082690
YDOT = 14035
281320 feet/sec YDOT = 4212
552613 meter/sec
ZDOT = -8192
300076 ZDOT = -2525
421573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4505256
38 X = 1373202
14
Y = 15042367
19 feet Y = 4584913
52 meter
Z = -15856102
67 Z = -4832940
09
XDOT = -22523
377190 XDOT = -6865
125368
YDOT = -2016
740753 feet/sec YDOT = -614
702582 meter/sec
ZDOT = -8324
053719 ZDOT = -2537
171574
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
66994486
00016717 00000-0 10270-3 0 9157
2 25544 51
6432 160
5989 0001766 148
8822 211
2433 15
49186055 20455
Satellite: ISS
Catalog Number: 25544
Epoch time: 20352
66994486 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 160
5989 deg
Eccentricity:
0001766
Arg of perigee: 148
8822 deg
Mean anomaly: 211
2433 deg
Mean motion: 15
49186055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 326
Coasting Arc #17 (Orbit 2060)
---------------------------------------
Vector Time (GMT): 2020/353/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 982624
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4131485
59 A = 6793696
85 meter
Y = -2288468
61 meter E =
0008650
Z = 4879340
75 I = 51
79572
XDOT = 5508
612881 Wp = 126
01717
YDOT = -4738
633857 meter/sec RA = 154
58212 deg
ZDOT = 2433
855928 TA = 300
10037
MA = 300
18610
Ha = 229
251 n
mi
Hp = 222
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13554742
75 X = -4129288
93
Y = -7508099
12 feet Y = -2334658
20 meter
Z = 16008335
78 Z = 4859276
89
XDOT = 18072
876907 XDOT = 5549
370181
YDOT = -15546
699006 feet/sec YDOT = -4676
805015 meter/sec
ZDOT = 7985
091626 ZDOT = 2460
712666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5781170
26 X = -1762100
70
Y = -14479311
05 feet Y = -4413294
01 meter
Z = 15915308
35 Z = 4850985
98
XDOT = 22735
206123 XDOT = 6929
690826
YDOT = -134
613843 feet/sec YDOT = -41
030299 meter/sec
ZDOT = 8109
674472 ZDOT = 2471
828779
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
70205575
00016717 00000-0 10270-3 0 9168
2 25544 51
6436 155
4921 0001744 149
1145 211
0108 15
49222820 20612
Satellite: ISS
Catalog Number: 25544
Epoch time: 20353
70205575 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 155
4921 deg
Eccentricity:
0001744
Arg of perigee: 149
1145 deg
Mean anomaly: 211
0108 deg
Mean motion: 15
49222820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2061
Checksum: 274
Coasting Arc #18 (Orbit 2066)
---------------------------------------
Vector Time (GMT): 2020/354/02:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 982624
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4106840
83 A = 6800364
13 meter
Y = 4637716
11 meter E =
0005200
Z = -2807997
50 I = 51
82834
XDOT = -5425
366298 Wp = 75
83468
YDOT = -1708
145234 meter/sec RA = 152
40149 deg
ZDOT = 5122
883181 TA = 252
48691
MA = 252
54373
Ha = 229
142 n
mi
Hp = 222
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13473887
25 X = -4144756
48
Y = 15215604
03 feet Y = 4591578
80 meter
Z = -9212590
22 Z = -2828038
22
XDOT = -17799
758194 XDOT = -5430
745800
YDOT = -5604
151031 feet/sec YDOT = -1768
846266 meter/sec
ZDOT = 16807
359517 ZDOT = 5096
515931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19664890
90 X = 5993858
75
Y = 4962912
19 feet Y = 1512695
63 meter
Z = -9305569
87 Z = -2836337
70
XDOT = 3576
039190 XDOT = 1089
976745
YDOT = 17059
320143 feet/sec YDOT = 5199
680780 meter/sec
ZDOT = 16685
088006 ZDOT = 5085
614824
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
08909836
00016717 00000-0 10270-3 0 9172
2 25544 51
6409 153
5806 0001305 134
9589 225
1666 15
49178737 20678
Satellite: ISS
Catalog Number: 25544
Epoch time: 20354
08909836 = yrday
fracday
Element set: 917
Inclination: 51
6409 deg
RA of node: 153
5806 deg
Eccentricity:
0001305
Arg of perigee: 134
9589 deg
Mean anomaly: 225
1666 deg
Mean motion: 15
49178737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2067
Checksum: 334
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