[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 26th 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) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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
311/18:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 221
3
Coasting Arc #1 (Orbit 1236)
---------------------------------------
Vector Time (GMT): 2020/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3577675
88 A = 6791277
87 meter
Y = 2168936
92 meter E =
0003828
Z = 5346306
74 I = 51
95750
XDOT = -4029
614388 Wp = 77
56436
YDOT = -6518
928943 meter/sec RA = 57
97933 deg
ZDOT = -51
073679 TA = 12
92537
MA = 12
91556
Ha = 229
158 n
mi
Hp = 221
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11737781
74 X = -3627633
25
Y = 7115934
77 feet Y = 2128649
62 meter
Z = 17540376
44 Z = 5328806
20
XDOT = -13220
519647 XDOT = -3956
170177
YDOT = -21387
562148 feet/sec YDOT = -6563
580332 meter/sec
ZDOT = -167
564563 ZDOT = -70
469581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5759665
78 X = 1755546
13
Y = -12572844
38 feet Y = -3832202
97 meter
Z = 17459286
58 Z = 5321590
55
XDOT = 22076
471593 XDOT = 6728
908542
YDOT = 9752
520358 feet/sec YDOT = 2972
568205 meter/sec
ZDOT = -257
069251 ZDOT = -78
354708
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 20300
54826550
00016717 00000-0 10270-3 0 9007
2 25544 51
6437 58
4861 0001477 64
0789 296
0513 15
49355937 12373
Satellite: ISS
Catalog Number: 25544
Epoch time: 20300
54826550 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 58
4861 deg
Eccentricity:
0001477
Arg of perigee: 64
0789 deg
Mean anomaly: 296
0513 deg
Mean motion: 15
49355937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1237
Checksum: 314
Coasting Arc #2 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2020/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3474235
57 A = 6791294
91 meter
Y = -2354204
56 meter E =
0016278
Z = -5353429
32 I = 51
93973
XDOT = 4480
486314 Wp = 89
05213
YDOT = 6196
276805 meter/sec RA = 53
05226 deg
ZDOT = 183
610162 TA = 182
69061
MA = 182
69938
Ha = 229
060 n
mi
Hp = 221
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11398410
68 X = 3526307
04
Y = -7723768
25 feet Y = -2315062
23 meter
Z = -17563744
48 Z = -5336426
04
XDOT = 14699
758248 XDOT = 4409
972789
YDOT = 20328
992143 feet/sec YDOT = 6245
986560 meter/sec
ZDOT = 602
395544 ZDOT = 205
203389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4913937
84 X = -1497768
25
Y = 12969011
99 feet Y = 3952954
85 meter
Z = -17484948
53 Z = -5329412
31
XDOT = -22809
236882 XDOT = -6952
255402
YDOT = -7699
153634 feet/sec YDOT = -2346
702028 meter/sec
ZDOT = 702
067871 ZDOT = 213
990287
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 20301
51578119
00016717 00000-0 10270-3 0 9011
2 25544 51
6448 53
6989 0001594 67
4236 292
7082 15
49359494 12520
Satellite: ISS
Catalog Number: 25544
Epoch time: 20301
51578119 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 53
6989 deg
Eccentricity:
0001594
Arg of perigee: 67
4236 deg
Mean anomaly: 292
7082 deg
Mean motion: 15
49359494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 325
Coasting Arc #3 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2020/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3355568
69 A = 6791244
66 meter
Y = 2520585
99 meter E =
0004189
Z = 5335915
16 I = 51
91884
XDOT = -4921
084885 Wp = 71
04763
YDOT = -5866
707860 meter/sec RA = 48
12225 deg
ZDOT = -321
843234 TA = 22
01952
MA = 22
00153
Ha = 229
163 n
mi
Hp = 221
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11009083
64 X = -3409424
54
Y = 8269639
07 feet Y = 2482760
71 meter
Z = 17506283
34 Z = 5319483
92
XDOT = -16145
291618 XDOT = -4853
552480
YDOT = -19247
729200 feet/sec YDOT = -5921
361380 meter/sec
ZDOT = -1055
916123 ZDOT = -345
584082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4052570
06 X = 1235223
35
Y = -13259868
91 feet Y = -4041608
04 meter
Z = 17430127
98 Z = 5312703
01
XDOT = 23442
850063 XDOT = 7145
380699
YDOT = 5626
045792 feet/sec YDOT = 1714
818757 meter/sec
ZDOT = -1165
524264 ZDOT = -355
251796
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 20302
54779199
00016717 00000-0 10270-3 0 9027
2 25544 51
6452 48
5909 0001604 67
1519 292
9800 15
49380731 12688
Satellite: ISS
Catalog Number: 25544
Epoch time: 20302
54779199 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 48
5909 deg
Eccentricity:
0001604
Arg of perigee: 67
1519 deg
Mean anomaly: 292
9800 deg
Mean motion: 15
49380731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 319
Coasting Arc #4 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2020/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3241624
65 A = 6791341
23 meter
Y = -2697798
67 meter E =
0016250
Z = -5337213
91 I = 51
89547
XDOT = 5314
409722 Wp = 91
16892
YDOT = 5481
770871 meter/sec RA = 43
19297 deg
ZDOT = 457
788861 TA = 183
18813
MA = 183
19850
Ha = 229
083 n
mi
Hp = 221
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10635251
49 X = 3297477
03
Y = -8851045
51 feet Y = -2661236
41 meter
Z = -17510544
32 Z = -5321331
26
XDOT = 17435
727434 XDOT = 5250
492198
YDOT = 17984
812569 feet/sec YDOT = 5540
843047 meter/sec
ZDOT = 1501
931959 ZDOT = 483
449293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3173915
57 X = -967409
46
Y = 13562773
67 feet Y = 4133933
41 meter
Z = -17436919
84 Z = -5314773
17
XDOT = -23775
502535 XDOT = -7246
773173
YDOT = -3484
314752 feet/sec YDOT = -1062
019136 meter/sec
ZDOT = 1620
421488 ZDOT = 493
904469
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 20303
51530073
00016717 00000-0 10270-3 0 9032
2 25544 51
6452 43
8044 0001660 70
7995 289
3335 15
49365996 12832
Satellite: ISS
Catalog Number: 25544
Epoch time: 20303
51530073 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 43
8044 deg
Eccentricity:
0001660
Arg of perigee: 70
7995 deg
Mean anomaly: 289
3335 deg
Mean motion: 15
49365996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 308
Coasting Arc #5 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2020/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3114836
90 A = 6791285
90 meter
Y = 2855033
79 meter E =
0004500
Z = 5313352
17 I = 51
87061
XDOT = -5696
036997 Wp = 67
08524
YDOT = -5092
510432 meter/sec RA = 38
26013 deg
ZDOT = -600
697489 TA = 28
64547
MA = 28
62076
Ha = 229
119 n
mi
Hp = 221
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10219281
17 X = -3172341
13
Y = 9366908
77 feet Y = 2819880
06 meter
Z = 17432257
79 Z = 5298081
38
XDOT = -18687
785423 XDOT = -5635
749743
YDOT = -16707
711392 feet/sec YDOT = -5155
870535 meter/sec
ZDOT = -1970
792287 ZDOT = -628
220752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2293423
43 X = 699035
46
Y = -13761407
26 feet Y = -4194476
93 meter
Z = 17361456
69 Z = 5291772
00
XDOT = 24008
002565 XDOT = 7317
639182
YDOT = 1345
585269 feet/sec YDOT = 410
134390 meter/sec
ZDOT = -2097
900151 ZDOT = -639
439966
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 20304
54730444
00016717 00000-0 10270-3 0 9041
2 25544 51
6457 38
6967 0001550 72
8040 287
3279 15
49398675 12997
Satellite: ISS
Catalog Number: 25544
Epoch time: 20304
54730444 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 38
6967 deg
Eccentricity:
0001550
Arg of perigee: 72
8040 deg
Mean anomaly: 287
3279 deg
Mean motion: 15
49398675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 332
Coasting Arc #6 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2020/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2990759
83 A = 6791433
80 meter
Y = -3024860
95 meter E =
0016039
Z = -5308192
16 I = 51
84367
XDOT = 6022
562408 Wp = 93
32233
YDOT = 4656
628976 meter/sec RA = 33
32680 deg
ZDOT = 740
712318 TA = 183
74588
MA = 183
75791
Ha = 229
066 n
mi
Hp = 221
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9812204
16 X = 3050147
35
Y = -9924084
48 feet Y = -2991084
12 meter
Z = -17415328
61 Z = -5293519
54
XDOT = 19759
063018 XDOT = 5966
444904
YDOT = 15277
654120 feet/sec YDOT = 4723
663825 meter/sec
ZDOT = 2430
158525 ZDOT = 769
832052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1388237
93 X = -423134
92
Y = 13971576
64 feet Y = 4258536
56 meter
Z = -17347285
54 Z = -5287452
63
XDOT = -23934
423051 XDOT = -7295
212146
YDOT = 801
938922 feet/sec YDOT = 244
430983 meter/sec
ZDOT = 2564
655080 ZDOT = 781
706868
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 20305
51480459
00016717 00000-0 10270-3 0 9058
2 25544 51
6459 33
9097 0001639 72
9671 287
1659 15
49375732 13147
Satellite: ISS
Catalog Number: 25544
Epoch time: 20305
51480459 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 33
9097 deg
Eccentricity:
0001639
Arg of perigee: 72
9671 deg
Mean anomaly: 287
1659 deg
Mean motion: 15
49375732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 329
Coasting Arc #7 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2020/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2857931
52 A = 6791393
08 meter
Y = 3173178
54 meter E =
0005062
Z = 5277135
69 I = 51
81529
XDOT = -6335
370948 Wp = 63
03695
YDOT = -4220
258209 meter/sec RA = 28
39048 deg
ZDOT = -890
472318 TA = 35
48017
MA = 35
44652
Ha = 229
108 n
mi
Hp = 221
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9376415
73 X = -2918836
62
Y = 10410690
73 feet Y = 3140878
50 meter
Z = 17313437
29 Z = 5263104
66
XDOT = -20785
337755 XDOT = -6283
382350
YDOT = -13845
991499 feet/sec YDOT = -4290
814178 meter/sec
ZDOT = -2921
497105 ZDOT = -921
121752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 500041
98 X = 152412
80
Y = -14081869
20 feet Y = -4292153
73 meter
Z = 17248353
03 Z = 5257298
00
XDOT = 23763
888837 XDOT = 7243
233317
YDOT = -2919
678926 feet/sec YDOT = -889
918137 meter/sec
ZDOT = -3063
075242 ZDOT = -933
625334
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 20306
54679756
00016717 00000-0 10270-3 0 9063
2 25544 51
6462 28
8022 0001619 73
6629 286
4699 15
49414526 13300
Satellite: ISS
Catalog Number: 25544
Epoch time: 20306
54679756 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 28
8022 deg
Eccentricity:
0001619
Arg of perigee: 73
6629 deg
Mean anomaly: 286
4699 deg
Mean motion: 15
49414526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 327
Coasting Arc #8 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2020/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2722474
13 A = 6791606
27 meter
Y = -3337697
61 meter E =
0015843
Z = -5264946
40 I = 51
78388
XDOT = 6588
468066 Wp = 95
49720
YDOT = 3745
504306 meter/sec RA = 23
45335 deg
ZDOT = 1033
610996 TA = 184
39960
MA = 184
41354
Ha = 229
098 n
mi
Hp = 221
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8932001
75 X = 2785169
79
Y = -10950451
49 feet Y = -3306902
24 meter
Z = -17273446
19 Z = -5251569
11
XDOT = 21615
708877 XDOT = 6541
074193
YDOT = 12288
399955 feet/sec YDOT = 3818
916257 meter/sec
ZDOT = 3391
112192 ZDOT = 1065
501141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 432599
64 X = 131856
37
Y = 14200225
80 feet Y = 4328228
82 meter
Z = -17211375
05 Z = -5246027
11
XDOT = -23294
944497 XDOT = -7100
299083
YDOT = 4993
626557 feet/sec YDOT = 1522
057374 meter/sec
ZDOT = 3538
439667 ZDOT = 1078
516410
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 20307
51428984
00016717 00000-0 10270-3 0 9077
2 25544 51
6448 24
0153 0001723 76
3768 283
7574 15
49379299 13452
Satellite: ISS
Catalog Number: 25544
Epoch time: 20307
51428984 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 24
0153 deg
Eccentricity:
0001723
Arg of perigee: 76
3768 deg
Mean anomaly: 283
7574 deg
Mean motion: 15
49379299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 333
Coasting Arc #9 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2020/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2580874
40 A = 6791588
52 meter
Y = 3480168
82 meter E =
0005594
Z = 5226211
03 I = 51
75312
XDOT = -6827
341399 Wp = 62
04829
YDOT = -3273
693621 meter/sec RA = 18
51287 deg
ZDOT = -1188
060597 TA = 39
35583
MA = 39
31520
Ha = 229
084 n
mi
Hp = 221
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8467435
70 X = -2644985
53
Y = 11417876
70 feet Y = 3450948
90 meter
Z = 17146361
64 Z = 5213518
25
XDOT = -22399
414038 XDOT = -6784
455462
YDOT = -10740
464637 feet/sec YDOT = -3349
802003 meter/sec
ZDOT = -3897
836603 ZDOT = -1221
122071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1335619
16 X = -407096
72
Y = -14223163
49 feet Y = -4335220
23 meter
Z = 17087446
71 Z = 5208253
76
XDOT = 22738
522784 XDOT = 6930
701745
YDOT = -7015
522518 feet/sec YDOT = -2138
331263 meter/sec
ZDOT = -4050
595561 ZDOT = -1234
621527
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 20308
54627477
00016717 00000-0 10270-3 0 9080
2 25544 51
6452 18
9078 0001594 80
1633 279
9697 15
49421891 13612
Satellite: ISS
Catalog Number: 25544
Epoch time: 20308
54627477 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 18
9078 deg
Eccentricity:
0001594
Arg of perigee: 80
1633 deg
Mean anomaly: 279
9697 deg
Mean motion: 15
49421891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 336
Coasting Arc #10 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2020/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2432905
38 A = 6791830
64 meter
Y = -3639491
99 meter E =
0015488
Z = -5206386
01 I = 51
72044
XDOT = 7002
351380 Wp = 97
68741
YDOT = 2773
693258 meter/sec RA = 13
57034 deg
ZDOT = 1334
604184 TA = 185
14694
MA = 185
16288
Ha = 229
102 n
mi
Hp = 221
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7981973
03 X = 2498712
73
Y = -11940590
50 feet Y = -3611917
21 meter
Z = -17081318
92 Z = -5194408
00
XDOT = 22973
593768 XDOT = 6964
331767
YDOT = 9100
043498 feet/sec YDOT = 2851
785909 meter/sec
ZDOT = 4378
622652 ZDOT = 1368
527548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2292171
76 X = 698653
95
Y = 14245439
91 feet Y = 4342010
08 meter
Z = -17025699
44 Z = -5189433
19
XDOT = -21901
860212 XDOT = -6675
686993
YDOT = 8939
212513 feet/sec YDOT = 2724
671974 meter/sec
ZDOT = 4535
386439 ZDOT = 1382
385787
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 20309
51375782
00016717 00000-0 10270-3 0 9098
2 25544 51
6446 14
1198 0001752 79
2269 280
9079 15
49387131 13766
Satellite: ISS
Catalog Number: 25544
Epoch time: 20309
51375782 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 14
1198 deg
Eccentricity:
0001752
Arg of perigee: 79
2269 deg
Mean anomaly: 280
9079 deg
Mean motion: 15
49387131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 328
Coasting Arc #11 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2020/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2282426
91 A = 6791849
09 meter
Y = 3776467
43 meter E =
0006401
Z = 5158954
34 I = 51
68794
XDOT = -7162
788166 Wp = 61
45740
YDOT = -2281
052549 meter/sec RA = 8
62542 deg
ZDOT = -1494
786173 TA = 42
95975
MA = 42
90978
Ha = 229
110 n
mi
Hp = 221
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7488277
26 X = -2349546
65
Y = 12389985
01 feet Y = 3750568
04 meter
Z = 16925703
20 Z = 5147704
21
XDOT = -23499
961174 XDOT = -7129
487422
YDOT = -7483
768206 feet/sec YDOT = -2360
965682 meter/sec
ZDOT = -4904
154110 ZDOT = -1529
500209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3204828
54 X = -976831
74
Y = -14180320
26 feet Y = -4322161
62 meter
Z = 16873442
01 Z = 5143025
12
XDOT = 20992
638561 XDOT = 6398
556233
YDOT = -10788
131321 feet/sec YDOT = -3288
222427 meter/sec
ZDOT = -5064
595462 ZDOT = -1543
688697
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 20310
54573258
00016717 00000-0 10270-3 0 9103
2 25544 51
6448 9
0124 0001736 81
7332 278
4015 15
49430316 13925
Satellite: ISS
Catalog Number: 25544
Epoch time: 20310
54573258 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 9
0124 deg
Eccentricity:
0001736
Arg of perigee: 81
7332 deg
Mean anomaly: 278
4015 deg
Mean motion: 15
49430316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 282
Coasting Arc #12 (Orbit 1406)
---------------------------------------
Vector Time (GMT): 2020/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2118533
49 A = 6792130
62 meter
Y = -3931283
98 meter E =
0015166
Z = -5131192
44 I = 51
65374
XDOT = 7258
113842 Wp = 99
91235
YDOT = 1768
991638 meter/sec RA = 3
67843 deg
ZDOT = 1642
965750 TA = 185
97344
MA = 185
99155
Ha = 229
157 n
mi
Hp = 221
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6950569
19 X = 2187261
66
Y = -12897913
31 feet Y = -3907208
37 meter
Z = -16834620
86 Z = -5120734
60
XDOT = 23812
709455 XDOT = 7229
812280
YDOT = 5803
778340 feet/sec YDOT = 1849
998714 meter/sec
ZDOT = 5390
307578 ZDOT = 1678
154812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4187971
52 X = 1276493
72
Y = 14098283
15 feet Y = 4297156
71 meter
Z = -16786016
38 Z = -5116377
79
XDOT = -19830
329822 XDOT = -6044
284530
YDOT = 12496
029028 feet/sec YDOT = 3808
789648 meter/sec
ZDOT = 5552
969002 ZDOT = 1692
544952
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 20311
51320825
00016717 00000-0 10270-3 0 9112
2 25544 51
6437 4
2244 0001909 83
8943 276
2425 15
49392513 14070
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
51320825 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 4
2244 deg
Eccentricity:
0001909
Arg of perigee: 83
8943 deg
Mean anomaly: 276
2425 deg
Mean motion: 15
49392513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1407
Checksum: 286
Coasting Arc #13 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2020/311/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6792618
80 A = 6803041
40 meter
Y = 92143
70 meter E =
0013347
Z = -236005
81 I = 51
67966
XDOT = 136
160688 Wp = 48
64409
YDOT = 4755
363379 meter/sec RA = 2
35055 deg
ZDOT = 6004
812091 TA = 308
81947
MA = 308
93856
Ha = 229
168 n
mi
Hp = 221
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22285494
76 X = 6792229
98
Y = 302308
71 feet Y = 168101
47 meter
Z = -774297
28 Z = -203010
34
XDOT = 446
721416 XDOT = 53
806252
YDOT = 15601
585888 feet/sec YDOT = 4756
425139 meter/sec
ZDOT = 19700
827071 ZDOT = 6005
273818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17625707
64 X = 5372315
69
Y = 13648521
59 feet Y = 4160069
38 meter
Z = -621685
01 Z = -189489
59
XDOT = -8140
159009 XDOT = -2481
120466
YDOT = 11366
984329 feet/sec YDOT = 3464
656824 meter/sec
ZDOT = 19702
681896 ZDOT = 6005
377442
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 20311
77120129
00016717 00000-0 10270-3 0 9126
2 25544 51
6420 2
9480 0001996 80
8108 279
3268 15
49417454 14111
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
77120129 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 2
9480 deg
Eccentricity:
0001996
Arg of perigee: 80
8108 deg
Mean anomaly: 279
3268 deg
Mean motion: 15
49417454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 291
Coasting Arc #14 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2020/312/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6787551
94 A = 6803075
30 meter
Y = 361277
72 meter E =
0013367
Z = 67378
32 I = 51
64728
XDOT = -320
203233 Wp = 127
07821
YDOT = -4743
433797 meter/sec RA = 357
40262 deg
ZDOT = -6007
059831 TA = 52
19757
MA = 52
07661
Ha = 229
112 n
mi
Hp = 221
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22268871
20 X = -6791414
68
Y = 1185294
34 feet Y = 285352
84 meter
Z = 221057
49 Z = 34397
26
XDOT = -1050
535542 XDOT = -237
957689
YDOT = -15562
446840 feet/sec YDOT = -4746
554326 meter/sec
ZDOT = -19708
201545 ZDOT = -6008
415788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18715522
01 X = -5704491
11
Y = -12127693
87 feet Y = -3696521
09 meter
Z = 68492
70 Z = 20876
58
XDOT = 7520
571942 XDOT = 2292
270328
YDOT = -11765
899164 feet/sec YDOT = -3586
246065 meter/sec
ZDOT = -19714
194652 ZDOT = -6008
886530
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 20312
80316873
00016717 00000-0 10270-3 0 9135
2 25544 51
6435 357
8400 0001928 81
4336 278
7033 15
49411399 14278
Satellite: ISS
Catalog Number: 25544
Epoch time: 20312
80316873 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 357
8400 deg
Eccentricity:
0001928
Arg of perigee: 81
4336 deg
Mean anomaly: 278
7033 deg
Mean motion: 15
49411399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 307
Coasting Arc #15 (Orbit 1442)
---------------------------------------
Vector Time (GMT): 2020/313/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6743830
64 A = 6803027
29 meter
Y = -846369
43 meter E =
0013888
Z = 59007
76 I = 51
61335
XDOT = 532
595218 Wp = 50
97942
YDOT = 4728
066120 meter/sec RA = 352
45255 deg
ZDOT = 6004
787538 TA = 309
65518
MA = 309
77762
Ha = 229
136 n
mi
Hp = 221
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22125428
60 X = 6752507
15
Y = -2776802
60 feet Y = -770906
57 meter
Z = 193595
00 Z = 91788
06
XDOT = 1747
359640 XDOT = 450
516812
YDOT = 15512
027953 feet/sec YDOT = 4733
562800 meter/sec
ZDOT = 19700
746516 ZDOT = 6007
175551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19714486
55 X = 6008975
50
Y = 10416454
53 feet Y = 3174935
34 meter
Z = 345250
15 Z = 105232
25
XDOT = -6818
527592 XDOT = -2078
287210
YDOT = 12194
127409 feet/sec YDOT = 3716
770034 meter/sec
ZDOT = 19711
516992 ZDOT = 6008
070379
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 20313
83513096
00016717 00000-0 10270-3 0 9146
2 25544 51
6433 352
7325 0001962 83
9105 276
2269 15
49426897 14436
Satellite: ISS
Catalog Number: 25544
Epoch time: 20313
83513096 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 352
7325 deg
Eccentricity:
0001962
Arg of perigee: 83
9105 deg
Mean anomaly: 276
2269 deg
Mean motion: 15
49426897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1443
Checksum: 316
Coasting Arc #16 (Orbit 1457)
---------------------------------------
Vector Time (GMT): 2020/314/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6670217
43 A = 6803024
92 meter
Y = 1290131
83 meter E =
0012843
Z = -232112
15 I = 51
58006
XDOT = -711
112439 Wp = 129
14593
YDOT = -4713
838368 meter/sec RA = 347
50040 deg
ZDOT = -5996
311620 TA = 53
35190
MA = 53
23389
Ha = 229
129 n
mi
Hp = 221
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21883915
44 X = -6683020
84
Y = 4232715
99 feet Y = 1215469
09 meter
Z = -761522
79 Z = -264544
91
XDOT = -2333
046059 XDOT = -629
221016
YDOT = -15465
348975 feet/sec YDOT = -4721
332511 meter/sec
ZDOT = -19672
938387 ZDOT = -5999
567179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20501864
27 X = -6248968
23
Y = -8731788
61 feet Y = -2661449
17 meter
Z = -911584
28 Z = -277850
89
XDOT = 6194
061332 XDOT = 1887
949894
YDOT = -12554
120580 feet/sec YDOT = -3826
495953 meter/sec
ZDOT = -19687
725887 ZDOT = -6000
818850
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 20314
80259338
00016717 00000-0 10270-3 0 9151
2 25544 51
6435 347
9442 0002011 84
8868 275
2512 15
49417269 14585
Satellite: ISS
Catalog Number: 25544
Epoch time: 20314
80259338 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 347
9442 deg
Eccentricity:
0002011
Arg of perigee: 84
8868 deg
Mean anomaly: 275
2512 deg
Mean motion: 15
49417269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1458
Checksum: 320
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