[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 24th 2020
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ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14262 1813 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 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
267/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
7
274/02:26:58
371 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 222
7
277/05:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 222
5
277/09:15:00
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
6
280/09:58:30
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
6
Coasting Arc #1 (Orbit 693)
---------------------------------------
Vector Time (GMT): 2020/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2256800
91 A = 6793114
48 meter
Y = 3791686
30 meter E =
0014440
Z = -5177794
29 I = 51
31691
XDOT = -5537
901808 Wp = 80
14995
YDOT = -5106
823629 meter/sec RA = 230
78733 deg
ZDOT = -1326
713178 TA = 177
01644
MA = 177
00782
Ha = 229
378 n
mi
Hp = 222
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7404202
47 X = -2273881
89
Y = 12439915
67 feet Y = 3766353
39 meter
Z = -16987514
08 Z = -5188798
74
XDOT = -18168
969186 XDOT = -5473
939688
YDOT = -16754
670700 feet/sec YDOT = -5168
394842 meter/sec
ZDOT = -4352
733522 ZDOT = -1353
458875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7305387
36 X = 2226682
07
Y = -12428852
78 feet Y = -3788314
33 meter
Z = -17038318
13 Z = -5193279
37
XDOT = 17208
845430 XDOT = 5245
256087
YDOT = 16247
685950 feet/sec YDOT = 4952
294678 meter/sec
ZDOT = -4476
085744 ZDOT = -1364
310935
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 20265
51851063
00016717 00000-0 10270-3 0 9001
2 25544 51
6405 231
7858 0000580 85
6499 274
4718 15
48943378 6945
Satellite: ISS
Catalog Number: 25544
Epoch time: 20265
51851063 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 231
7858 deg
Eccentricity:
0000580
Arg of perigee: 85
6499 deg
Mean anomaly: 274
4718 deg
Mean motion: 15
48943378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 694
Checksum: 330
Coasting Arc #2 (Orbit 709)
---------------------------------------
Vector Time (GMT): 2020/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1906692
15 A = 6793033
60 meter
Y = -3970782
30 meter E =
0004744
Z = 5168275
35 I = 51
34006
XDOT = 5972
036519 Wp = 120
78748
YDOT = 4611
566258 meter/sec RA = 225
82185 deg
ZDOT = 1336
546197 TA = 316
28683
MA = 316
32438
Ha = 229
216 n
mi
Hp = 222
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6255551
68 X = 1925848
14
Y = -13027500
98 feet Y = -3949353
06 meter
Z = 16956283
97 Z = 5177584
04
XDOT = 19593
295667 XDOT = 5913
532500
YDOT = 15129
810557 feet/sec YDOT = 4678
022767 meter/sec
ZDOT = 4384
994085 ZDOT = 1365
414094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5932961
43 X = -1808366
65
Y = 13122049
81 feet Y = 3999600
78 meter
Z = 16999266
22 Z = 5181376
34
XDOT = -18842
493409 XDOT = -5743
191991
YDOT = -14386
531383 feet/sec YDOT = -4385
014765 meter/sec
ZDOT = 4518
162745 ZDOT = 1377
136005
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 20266
55078232
00016717 00000-0 10270-3 0 9016
2 25544 51
6413 226
6808 0000474 75
8488 284
2714 15
48971132 7106
Satellite: ISS
Catalog Number: 25544
Epoch time: 20266
55078232 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 226
6808 deg
Eccentricity:
0000474
Arg of perigee: 75
8488 deg
Mean anomaly: 284
2714 deg
Mean motion: 15
48971132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 710
Checksum: 306
Coasting Arc #3 (Orbit 724)
---------------------------------------
Vector Time (GMT): 2020/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1557500
15 A = 6793117
61 meter
Y = 4126509
59 meter E =
0014420
Z = -5179343
43 I = 51
36397
XDOT = -6337
663530 Wp = 79
74011
YDOT = -4068
879287 meter/sec RA = 220
85651 deg
ZDOT = -1336
626756 TA = 177
33689
MA = 177
32921
Ha = 229
368 n
mi
Hp = 222
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5109908
62 X = -1578369
81
Y = 13538417
30 feet Y = 4108975
75 meter
Z = -16992596
55 Z = -5186959
95
XDOT = -20792
859352 XDOT = -6285
200457
YDOT = -13349
341494 feet/sec YDOT = -4139
458261 meter/sec
ZDOT = -4385
258386 ZDOT = -1367
285370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4544264
64 X = 1385091
86
Y = -13694995
79 feet Y = -4174234
72 meter
Z = -17027771
31 Z = -5190064
69
XDOT = 20192
834761 XDOT = 6154
776035
YDOT = 12325
956821 feet/sec YDOT = 3756
951639 meter/sec
ZDOT = -4526
718296 ZDOT = -1379
743737
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 20267
51853762
00016717 00000-0 10270-3 0 9023
2 25544 51
6407 221
8935 0000580 76
5742 283
5473 15
48947091 7253
Satellite: ISS
Catalog Number: 25544
Epoch time: 20267
51853762 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 221
8935 deg
Eccentricity:
0000580
Arg of perigee: 76
5742 deg
Mean anomaly: 283
5473 deg
Mean motion: 15
48947091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 725
Checksum: 320
Coasting Arc #4 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2020/267/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1920251
25 A = 6798865
28 meter
Y = 5409279
03 meter E =
0005866
Z = -3649620
67 I = 51
39067
XDOT = -6257
268187 Wp = 81
20312
YDOT = -709
693049 meter/sec RA = 219
94217 deg
ZDOT = -4349
272940 TA = 142
16125
MA = 142
12000
Ha = 229
319 n
mi
Hp = 222
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6300036
92 X = 1877348
23
Y = 17746978
45 feet Y = 5430512
72 meter
Z = -11973821
10 Z = -3640397
06
XDOT = -20529
095103 XDOT = -6227
740727
YDOT = -2328
389268 feet/sec YDOT = -779
501262 meter/sec
ZDOT = -14269
268176 ZDOT = -4379
596753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18857819
27 X = -5747863
31
Y = -212504
60 feet Y = -64771
40 meter
Z = -11931286
39 Z = -3636656
09
XDOT = 9297
068825 XDOT = 2833
746578
YDOT = -16958
660746 feet/sec YDOT = -5168
999795 meter/sec
ZDOT = -14409
207665 ZDOT = -4391
926496
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 20267
71208821
00016717 00000-0 10270-3 0 9036
2 25544 51
6435 220
9383 0000433 72
4108 287
7089 15
48947400 7285
Satellite: ISS
Catalog Number: 25544
Epoch time: 20267
71208821 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 220
9383 deg
Eccentricity:
0000433
Arg of perigee: 72
4108 deg
Mean anomaly: 287
7089 deg
Mean motion: 15
48947400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 305
Coasting Arc #5 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2020/268/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2398357
38 A = 6798942
64 meter
Y = -5215445
23 meter E =
0012457
Z = 3632937
66 I = 51
41702
XDOT = 6296
182457 Wp = 92
95931
YDOT = 154
863658 meter/sec RA = 214
97956 deg
ZDOT = 4365
252825 TA = 310
20598
MA = 310
31494
Ha = 229
402 n
mi
Hp = 222
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7868626
57 X = -2357505
22
Y = -17111040
77 feet Y = -5242036
91 meter
Z = 11919086
81 Z = 3621386
65
XDOT = 20656
766590 XDOT = 6272
778839
YDOT = 508
082866 feet/sec YDOT = 225
141280 meter/sec
ZDOT = 14321
695621 ZDOT = 4395
780426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18780898
11 X = 5724417
74
Y = -1802338
59 feet Y = -549352
80 meter
Z = 11865794
22 Z = 3616694
08
XDOT = -7453
077729 XDOT = -2271
698092
YDOT = 17847
597457 feet/sec YDOT = 5439
947705 meter/sec
ZDOT = 14462
599666 ZDOT = 4408
200378
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 20268
74436096
00016717 00000-0 10270-3 0 9048
2 25544 51
6430 215
8325 0000565 70
4425 289
6786 15
48939435 7447
Satellite: ISS
Catalog Number: 25544
Epoch time: 20268
74436096 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 215
8325 deg
Eccentricity:
0000565
Arg of perigee: 70
4425 deg
Mean anomaly: 289
6786 deg
Mean motion: 15
48939435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 329
Coasting Arc #6 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2020/269/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2834703
46 A = 6798895
23 meter
Y = 4993793
84 meter E =
0005704
Z = -3645928
91 I = 51
44570
XDOT = -6278
665242 Wp = 81
63719
YDOT = 384
925943 meter/sec RA = 210
01911 deg
ZDOT = -4359
479564 TA = 141
63174
MA = 141
59115
Ha = 229
277 n
mi
Hp = 222
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9300208
20 X = 2796360
48
Y = 16383838
05 feet Y = 5025279
06 meter
Z = -11961709
03 Z = -3632252
29
XDOT = -20599
295415 XDOT = -6261
327134
YDOT = 1262
880392 feet/sec YDOT = 314
810260 meter/sec
ZDOT = -14302
754476 ZDOT = -4389
936708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18510532
54 X = -5642010
32
Y = 3713532
97 feet Y = 1131884
85 meter
Z = -11898586
59 Z = -3626689
19
XDOT = 5562
744295 XDOT = 1695
524461
YDOT = -18496
585203 feet/sec YDOT = -5637
759170 meter/sec
ZDOT = -14443
355607 ZDOT = -4402
334789
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 20269
71211390
00016717 00000-0 10270-3 0 9055
2 25544 51
6433 211
0461 0000303 70
0064 290
1119 15
48947523 7594
Satellite: ISS
Catalog Number: 25544
Epoch time: 20269
71211390 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 211
0461 deg
Eccentricity:
0000303
Arg of perigee: 70
0064 deg
Mean anomaly: 290
1119 deg
Mean motion: 15
48947523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 273
Coasting Arc #7 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2020/270/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3270685
92 A = 6798952
02 meter
Y = -4719700
94 meter E =
0012377
Z = 3630186
61 I = 51
47586
XDOT = 6221
363541 Wp = 92
47094
YDOT = -935
955299 meter/sec RA = 205
05973 deg
ZDOT = 4374
933019 TA = 310
60978
MA = 310
71739
Ha = 229
376 n
mi
Hp = 222
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10730596
84 X = -3235299
02
Y = -15484583
15 feet Y = -4756078
11 meter
Z = 11910061
07 Z = 3614385
08
XDOT = 20411
297706 XDOT = 6210
116450
YDOT = -3070
719486 feet/sec YDOT = -866
446281 meter/sec
ZDOT = 14353
454786 ZDOT = 4405
126567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18015379
20 X = 5491087
58
Y = -5665379
09 feet Y = -1726807
55 meter
Z = 11837109
89 Z = 3607951
10
XDOT = -3581
900419 XDOT = -1091
763248
YDOT = 18983
784756 feet/sec YDOT = 5786
257593 meter/sec
ZDOT = 14492
858533 ZDOT = 4417
423281
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 20270
74438377
00016717 00000-0 10270-3 0 9067
2 25544 51
6435 205
9396 0000514 57
5362 302
5837 15
48945318 7753
Satellite: ISS
Catalog Number: 25544
Epoch time: 20270
74438377 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 205
9396 deg
Eccentricity:
0000514
Arg of perigee: 57
5362 deg
Mean anomaly: 302
5837 deg
Mean motion: 15
48945318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 324
Coasting Arc #8 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2020/271/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3661352
03 A = 6798914
79 meter
Y = 4425639
94 meter E =
0005735
Z = -3643508
29 I = 51
50585
XDOT = -6111
144257 Wp = 81
33245
YDOT = 1463
141452 meter/sec RA = 200
10305 deg
ZDOT = -4368
910745 TA = 141
85533
MA = 141
81473
Ha = 229
297 n
mi
Hp = 222
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12012309
79 X = 3629289
07
Y = 14519816
07 feet Y = 4466404
33 meter
Z = -11953767
35 Z = -3625801
07
XDOT = -20049
685884 XDOT = -6105
829773
YDOT = 4800
332849 feet/sec YDOT = 1394
831732 meter/sec
ZDOT = -14333
696670 ZDOT = -4398
583336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17353861
18 X = -5289456
89
Y = 7477455
59 feet Y = 2279128
46 meter
Z = -11871998
96 Z = -3618585
28
XDOT = 1603
326977 XDOT = 488
694063
YDOT = -19227
632396 feet/sec YDOT = -5860
582354 meter/sec
ZDOT = -14470
711207 ZDOT = -4410
672776
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 20271
71213516
00016717 00000-0 10270-3 0 9072
2 25544 51
6424 201
1529 0000374 62
6172 297
5016 15
48949292 7901
Satellite: ISS
Catalog Number: 25544
Epoch time: 20271
71213516 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 201
1529 deg
Eccentricity:
0000374
Arg of perigee: 62
6172 deg
Mean anomaly: 297
5016 deg
Mean motion: 15
48949292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 297
Coasting Arc #9 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2020/272/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4043557
11 A = 6798975
63 meter
Y = -4079773
20 meter E =
0012355
Z = 3627269
59 I = 51
53824
XDOT = 5959
017639 Wp = 92
59026
YDOT = -1995
383127 meter/sec RA = 195
14884 deg
ZDOT = 4385
110632 TA = 310
40070
MA = 310
50845
Ha = 229
375 n
mi
Hp = 222
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13266263
48 X = -4015254
48
Y = -13385082
68 feet Y = -4124832
64 meter
Z = 11900490
79 Z = 3607696
67
XDOT = 19550
582805 XDOT = 5959
587427
YDOT = -6546
532570 feet/sec YDOT = -1928
741611 meter/sec
ZDOT = 14386
845907 ZDOT = 4414
058654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16464122
73 X = 5018264
61
Y = -9286026
77 feet Y = -2830380
96 meter
Z = 11810090
42 Z = 3599715
56
XDOT = 433
620051 XDOT = 132
167392
YDOT = 19292
932967 feet/sec YDOT = 5880
485968 meter/sec
ZDOT = 14520
527496 ZDOT = 4425
856781
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 20272
74440514
00016717 00000-0 10270-3 0 9087
2 25544 51
6424 196
0472 0000451 59
7321 300
3873 15
48945835 8060
Satellite: ISS
Catalog Number: 25544
Epoch time: 20272
74440514 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 196
0472 deg
Eccentricity:
0000451
Arg of perigee: 59
7321 deg
Mean anomaly: 300
3873 deg
Mean motion: 15
48945835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 301
Coasting Arc #10 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2020/273/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4377179
49 A = 6798918
55 meter
Y = 3721999
58 meter E =
0005603
Z = -3640432
09 I = 51
57116
XDOT = -5759
501941 Wp = 81
77680
YDOT = 2494
638250 meter/sec RA = 190
19641 deg
ZDOT = -4379
581559 TA = 141
31772
MA = 141
27758
Ha = 229
252 n
mi
Hp = 222
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14360825
11 X = 4352916
79
Y = 12211284
70 feet Y = 3770812
35 meter
Z = -11943674
84 Z = -3619228
72
XDOT = -18896
003743 XDOT = -5765
696172
YDOT = 8184
508694 feet/sec YDOT = 2430
196347 meter/sec
ZDOT = -14368
705903 ZDOT = -4407
574232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15439928
95 X = -4706090
34
Y = 10921877
66 feet Y = 3328988
31 meter
Z = -11845730
17 Z = -3610578
55
XDOT = -2416
391081 XDOT = -736
516001
YDOT = -19122
336955 feet/sec YDOT = -5828
488304 meter/sec
ZDOT = -14497
985991 ZDOT = -4418
986130
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 20273
71215561
00016717 00000-0 10270-3 0 9098
2 25544 51
6425 191
2603 0000268 58
5722 301
5454 15
48956274 8216
Satellite: ISS
Catalog Number: 25544
Epoch time: 20273
71215561 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 191
2603 deg
Eccentricity:
0000268
Arg of perigee: 58
5722 deg
Mean anomaly: 301
5454 deg
Mean motion: 15
48956274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 821
Checksum: 298
Coasting Arc #11 (Orbit 827)
---------------------------------------
Vector Time (GMT): 2020/274/02:26:58
371
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6295794
35 A = 6803587
11 meter
Y = -2087713
62 meter E =
0014224
Z = 1484147
29 I = 51
60109
XDOT = 2766
994930 Wp = 62
77810
YDOT = -4220
185215 meter/sec RA = 188
13095 deg
ZDOT = 5765
011841 TA = 313
39972
MA = 313
51806
Ha = 229
378 n
mi
Hp = 222
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20655493
28 X = -6279190
14
Y = -6849454
12 feet Y = -2158024
73 meter
Z = 4869249
64 Z = 1453605
26
XDOT = 9078
067355 XDOT = 2785
977482
YDOT = -13845
752019 feet/sec YDOT = -4189
136020 meter/sec
ZDOT = 18914
080843 ZDOT = 5778
499338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19447878
26 X = -5927713
30
Y = 9833536
62 feet Y = 2997261
96 meter
Z = 4728171
41 Z = 1441146
65
XDOT = -2784
808585 XDOT = -848
809657
YDOT = -14690
629375 feet/sec YDOT = -4477
703833 meter/sec
ZDOT = 18976
361283 ZDOT = 5783
994919
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 20274
16377395
00016717 00000-0 10270-3 0 9104
2 25544 51
6431 189
0252 0000506 97
7824 262
3383 15
48938366 8285
Satellite: ISS
Catalog Number: 25544
Epoch time: 20274
16377395 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 189
0252 deg
Eccentricity:
0000506
Arg of perigee: 97
7824 deg
Mean anomaly: 262
3383 deg
Mean motion: 15
48938366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 828
Checksum: 323
Coasting Arc #12 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2020/275/02:26:58
371
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6449551
06 A = 6803462
00 meter
Y = 1547740
56 meter E =
0008822
Z = -1499863
04 I = 51
63477
XDOT = -2398
816422 Wp = 139
99154
YDOT = 4435
826767 meter/sec RA = 183
18251 deg
ZDOT = -5763
194401 TA = 56
34664
MA = 56
26252
Ha = 229
375 n
mi
Hp = 222
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21159944
41 X = 6439049
93
Y = 5077888
99 feet Y = 1619805
21 meter
Z = -4920810
50 Z = -1468559
11
XDOT = -7870
132618 XDOT = -2420
246413
YDOT = 14553
237423 feet/sec YDOT = 4408
881091 meter/sec
ZDOT = -18908
118114 ZDOT = -5774
899467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18348635
42 X = 5592664
08
Y = -11758319
56 feet Y = -3583935
80 meter
Z = -4776199
27 Z = -1455785
54
XDOT = 4268
167711 XDOT = 1300
937518
YDOT = 14327
789273 feet/sec YDOT = 4367
110170 meter/sec
ZDOT = -18962
168033 ZDOT = -5779
668817
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 20275
13152297
00016717 00000-0 10270-3 0 9115
2 25544 51
6432 184
2389 0000591 95
8913 264
2304 15
48972576 8438
Satellite: ISS
Catalog Number: 25544
Epoch time: 20275
13152297 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 184
2389 deg
Eccentricity:
0000591
Arg of perigee: 95
8913 deg
Mean anomaly: 264
2304 deg
Mean motion: 15
48972576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 317
Coasting Arc #13 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2020/276/02:26:58
371
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6563449
65 A = 6803621
66 meter
Y = -966898
66 meter E =
0014392
Z = 1477768
93 I = 51
66776
XDOT = 1989
811264 Wp = 62
63142
YDOT = -4627
861012 meter/sec RA = 178
23652 deg
ZDOT = 5772
896043 TA = 313
45988
MA = 313
57950
Ha = 229
448 n
mi
Hp = 222
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21533627
45 X = -6559327
92
Y = -3172239
70 feet Y = -1040272
67 meter
Z = 4848323
25 Z = 1445896
02
XDOT = 6528
252177 XDOT = 2013
371781
YDOT = -15183
271038 feet/sec YDOT = -4605
477223 meter/sec
ZDOT = 18939
947647 ZDOT = 5782
619541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17001394
51 X = -5182025
05
Y = 13642542
66 feet Y = 4158247
00 meter
Z = 4701070
98 Z = 1432886
43
XDOT = -5774
464291 XDOT = -1760
056716
YDOT = -13781
012242 feet/sec YDOT = -4200
452531 meter/sec
ZDOT = 18984
847430 ZDOT = 5786
581497
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 20276
16379081
00016717 00000-0 10270-3 0 9122
2 25544 51
6423 179
1339 0000648 87
9386 272
1838 15
48929996 8590
Satellite: ISS
Catalog Number: 25544
Epoch time: 20276
16379081 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 179
1339 deg
Eccentricity:
0000648
Arg of perigee: 87
9386 deg
Mean anomaly: 272
1838 deg
Mean motion: 15
48929996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 356
Coasting Arc #14 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2020/277/02:26:58
371
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6621532
01 A = 6803454
40 meter
Y = 408527
25 meter E =
0008882
Z = -1493188
96 I = 51
70215
XDOT = -1590
303889 Wp = 140
06107
YDOT = 4775
948034 meter/sec RA = 173
29226 deg
ZDOT = -5771
242873 TA = 56
18696
MA = 56
10242
Ha = 229
375 n
mi
Hp = 222
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21724186
38 X = 6623724
77
Y = 1340312
51 feet Y = 482586
10 meter
Z = -4898913
93 Z = -1461018
38
XDOT = -5217
532444 XDOT = -1615
557961
YDOT = 15669
120845 feet/sec YDOT = 4758
022399 meter/sec
ZDOT = -18934
523861 ZDOT = -5779
029823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15528227
90 X = 4733003
87
Y = -15298532
95 feet Y = -4662992
84 meter
Z = -4750273
36 Z = -1447883
32
XDOT = 7148
029221 XDOT = 2178
719306
YDOT = 13118
756525 feet/sec YDOT = 3998
596989 meter/sec
ZDOT = -18970
482179 ZDOT = -5782
202968
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 20277
13153874
00016717 00000-0 10270-3 0 9131
2 25544 51
6430 174
3471 0000612 98
9440 261
1779 15
48978485 8742
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
13153874 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 174
3471 deg
Eccentricity:
0000612
Arg of perigee: 98
9440 deg
Mean anomaly: 261
1779 deg
Mean motion: 15
48978485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 327
Coasting Arc #15 (Orbit 875)
---------------------------------------
Vector Time (GMT): 2020/277/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2439904
79 A = 6794675
96 meter
Y = 4150897
39 meter E =
0011980
Z = -4805631
03 I = 51
67502
XDOT = -7097
973704 Wp = 107
60240
YDOT = -1151
403510 meter/sec RA = 172
53383 deg
ZDOT = 2611
082787 TA = 188
17728
MA = 188
19683
Ha = 229
382 n
mi
Hp = 222
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8004936
98 X = -2462796
66
Y = 13618429
74 feet Y = 4123484
21 meter
Z = -15766505
99 Z = -4817539
28
XDOT = -23287
315302 XDOT = -7097
254172
YDOT = -3777
570572 feet/sec YDOT = -1230
773894 meter/sec
ZDOT = 8566
544577 ZDOT = 2576
604920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14885453
25 X = 4537086
15
Y = 5121177
00 feet Y = 1560934
75 meter
Z = -15821510
16 Z = -4822396
30
XDOT = 1171
409789 XDOT = 357
045704
YDOT = 22550
025372 feet/sec YDOT = 6873
247734 meter/sec
ZDOT = 8407
237992 ZDOT = 2562
526140
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 20277
26057179
00016717 00000-0 10270-3 0 9147
2 25544 51
6404 173
7099 0000594 86
8058 273
3160 15
48941376 8762
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
26057179 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 173
7099 deg
Eccentricity:
0000594
Arg of perigee: 86
8058 deg
Mean anomaly: 273
3160 deg
Mean motion: 15
48941376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 876
Checksum: 333
Coasting Arc #16 (Orbit 877)
---------------------------------------
Vector Time (GMT): 2020/277/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937176
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5972408
55 A = 6802527
04 meter
Y = 2507042
11 meter E =
0006801
Z = -2072365
79 I = 51
70722
XDOT = -3557
757286 Wp = 44
03008
YDOT = -3909
398163 meter/sec RA = 171
86088 deg
ZDOT = 5539
520522 TA = 293
12362
MA = 293
19527
Ha = 229
277 n
mi
Hp = 222
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19594516
24 X = -5989932
64
Y = 8225203
76 feet Y = 2440156
19 meter
Z = -6799100
37 Z = -2101420
66
XDOT = -11672
432041 XDOT = -3540
685057
YDOT = -12826
109459 feet/sec YDOT = -3949
087627 meter/sec
ZDOT = 18174
279929 ZDOT = 5522
279852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21058403
43 X = 6418601
37
Y = 2509836
81 feet Y = 764998
26 meter
Z = -6933337
84 Z = -2113281
38
XDOT = 4100
222286 XDOT = 1249
747753
YDOT = 15443
797214 feet/sec YDOT = 4707
269391 meter/sec
ZDOT = 18094
604161 ZDOT = 5515
235348
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 20277
38960558
00016717 00000-0 10270-3 0 9155
2 25544 51
6417 173
0717 0000467 72
6153 287
5048 15
48953987 8789
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
38960558 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 173
0717 deg
Eccentricity:
0000467
Arg of perigee: 72
6153 deg
Mean anomaly: 287
5048 deg
Mean motion: 15
48953987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 878
Checksum: 348
Coasting Arc #17 (Orbit 893)
---------------------------------------
Vector Time (GMT): 2020/278/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937176
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5739818
80 A = 6802524
45 meter
Y = -3000319
93 meter E =
0014283
Z = 2058668
58 I = 51
74140
XDOT = 3876
712219 Wp = 109
46478
YDOT = 3591
084762 meter/sec RA = 166
91940 deg
ZDOT = -5548
313810 TA = 47
84304
MA = 47
72180
Ha = 229
282 n
mi
Hp = 222
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18831426
51 X = 5762942
66
Y = -9843569
32 feet Y = -2936003
72 meter
Z = 6754162
00 Z = 2086607
28
XDOT = 12718
872109 XDOT = 3863
218557
YDOT = 11781
774153 feet/sec YDOT = 3634
361094 meter/sec
ZDOT = -18203
129297 ZDOT = -5529
514929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21204420
21 X = -6463107
28
Y = -361261
40 feet Y = -110112
47 meter
Z = 6883257
91 Z = 2098017
01
XDOT = -5654
082782 XDOT = -1723
364432
YDOT = -14948
109353 feet/sec YDOT = -4556
183731 meter/sec
ZDOT = -18116
248591 ZDOT = -5521
832570
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 20278
42186956
00016717 00000-0 10270-3 0 9164
2 25544 51
6425 167
9656 0000537 69
2380 290
8828 15
48966576 8943
Satellite: ISS
Catalog Number: 25544
Epoch time: 20278
42186956 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 167
9656 deg
Eccentricity:
0000537
Arg of perigee: 69
2380 deg
Mean anomaly: 290
8828 deg
Mean motion: 15
48966576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 894
Checksum: 361
Coasting Arc #18 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2020/279/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937176
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5449298
92 A = 6802500
22 meter
Y = 3496287
53 meter E =
0006890
Z = -2080907
47 I = 51
77287
XDOT = -4182
143422 Wp = 44
07813
YDOT = -3229
603842 meter/sec RA = 161
98049 deg
ZDOT = 5541
402014 TA = 292
99779
MA = 293
07046
Ha = 229
299 n
mi
Hp = 222
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17878277
30 X = -5477882
38
Y = 11470759
60 feet Y = 3435189
62 meter
Z = -6827124
25 Z = -2107448
20
XDOT = -13720
942986 XDOT = -4172
635720
YDOT = -10595
813131 feet/sec YDOT = -3276
318107 meter/sec
ZDOT = 18180
452801 ZDOT = 5521
109641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21117739
37 X = 6436686
96
Y = -1887437
07 feet Y = -575290
82 meter
Z = -6949778
11 Z = -2118292
37
XDOT = 7210
792969 XDOT = 2197
849697
YDOT = 14269
484682 feet/sec YDOT = 4349
338931 meter/sec
ZDOT = 18086
664361 ZDOT = 5512
815297
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 20279
38961607
00016717 00000-0 10270-3 0 9175
2 25544 51
6415 163
1794 0000561 67
4365 292
6845 15
48960098 9092
Satellite: ISS
Catalog Number: 25544
Epoch time: 20279
38961607 = yrday
fracday
Element set: 917
Inclination: 51
6415 deg
RA of node: 163
1794 deg
Eccentricity:
0000561
Arg of perigee: 67
4365 deg
Mean anomaly: 292
6845 deg
Mean motion: 15
48960098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 909
Checksum: 341
Coasting Arc #19 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2020/280/09:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937176
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5135400
29 A = 6802526
83 meter
Y = -3941826
03 meter E =
0014309
Z = 2067563
11 I = 51
80511
XDOT = 4441
117969 Wp = 109
54922
YDOT = 2860
916749 meter/sec RA = 157
04392 deg
ZDOT = -5549
841561 TA = 47
67602
MA = 47
55488
Ha = 229
297 n
mi
Hp = 222
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16848426
14 X = 5169054
05
Y = -12932500
08 feet Y = -3884210
05 meter
Z = 6783343
55 Z = 2092591
29
XDOT = 14570
597011 XDOT = 4435
754790
YDOT = 9386
209808 feet/sec YDOT = 2910
550329 meter/sec
ZDOT = -18208
141603 ZDOT = -5528
281020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20817932
85 X = -6345305
93
Y = 4018689
44 feet Y = 1224896
54 meter
Z = 6899027
35 Z = 2102823
54
XDOT = -8628
451288 XDOT = -2629
951952
YDOT = -13462
897582 feet/sec YDOT = -4103
491183 meter/sec
ZDOT = -18108
484025 ZDOT = -5519
465931
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 20280
42187977
00016717 00000-0 10270-3 0 9183
2 25544 51
6419 158
0738 0000531 74
6762 285
4447 15
48962856 9255
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42187977 = yrday
fracday
Element set: 918
Inclination: 51
6419 deg
RA of node: 158
0738 deg
Eccentricity:
0000531
Arg of perigee: 74
6762 deg
Mean anomaly: 285
4447 deg
Mean motion: 15
48962856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 342
Coasting Arc #20 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2020/280/09:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 937176
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4229329
03 A = 6800429
24 meter
Y = 4388166
52 meter E =
0005031
Z = -3019295
37 I = 51
79976
XDOT = -5508
060705 Wp = 72
54344
YDOT = -1897
858877 meter/sec RA = 156
88943 deg
ZDOT = 4965
509810 TA = 253
06193
MA = 253
11708
Ha = 229
275 n
mi
Hp = 222
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13875751
41 X = -4263418
18
Y = 14396871
79 feet Y = 4340680
42 meter
Z = -9905824
70 Z = -3039923
18
XDOT = -18071
065304 XDOT = -5510
549021
YDOT = -6226
571120 feet/sec YDOT = -1959
467700 meter/sec
ZDOT = 16291
042684 ZDOT = 4938
747264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17197853
50 X = 5241905
75
Y = -10106542
26 feet Y = -3080474
08 meter
Z = -10001169
73 Z = -3048356
53
XDOT = 15071
624174 XDOT = 4593
831048
YDOT = 9674
626257 feet/sec YDOT = 2948
826083 meter/sec
ZDOT = 16167
340327 ZDOT = 4927
805332
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 20280
42187956
00016717 00000-0 10270-3 0 9191
2 25544 51
6424 158
0739 0000517 76
2380 283
8827 15
48977161 9259
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42187956 = yrday
fracday
Element set: 919
Inclination: 51
6424 deg
RA of node: 158
0739 deg
Eccentricity:
0000517
Arg of perigee: 76
2380 deg
Mean anomaly: 283
8827 deg
Mean motion: 15
48977161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 334
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