[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 3rd 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
186/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 221
2
189/16:57:30
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
1
190/18:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 221
2
191/21:37:03
333 -0
6 0
9 0
9
N/A -0
7 -0
1 229
0
000/00:02:06
667 0
0 -0
1 221
6
192/13:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
7
193/01:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 221
8
195/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 221
9
Coasting Arc #1 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2020/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1017752
60 A = 6802882
87 meter
Y = 6714802
56 meter E =
0013623
Z = -274052
06 I = 51
27559
XDOT = -4707
503816 Wp = 132
13393
YDOT = -948
952595 meter/sec RA = 276
76442 deg
ZDOT = -5969
326236 TA = 50
82847
MA = 50
70752
Ha = 229
151 n
mi
Hp = 221
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3339083
33 X = -1091432
69
Y = 22030192
11 feet Y = 6703009
40 meter
Z = -899120
92 Z = -279173
74
XDOT = -15444
566327 XDOT = -4667
546885
YDOT = -3113
361532 feet/sec YDOT = -1001
370851 meter/sec
ZDOT = -19584
403661 ZDOT = -5992
096579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22279990
74 X = 6790941
18
Y = -192970
38 feet Y = -58817
37 meter
Z = -923057
77 Z = -281348
01
XDOT = -668
033649 XDOT = -203
616656
YDOT = 13985
890687 feet/sec YDOT = 4262
899481 meter/sec
ZDOT = -19689
054111 ZDOT = -6001
223693
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 20183
53175319
00016717 00000-0 10270-3 0 9005
2 25544 51
6434 277
4688 0002345 109
4319 250
7085 15
49465870 34236
Satellite: ISS
Catalog Number: 25544
Epoch time: 20183
53175319 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 277
4688 deg
Eccentricity:
0002345
Arg of perigee: 109
4319 deg
Mean anomaly: 250
7085 deg
Mean motion: 15
49465870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 315
Coasting Arc #2 (Orbit 3438)
---------------------------------------
Vector Time (GMT): 2020/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 548831
79 A = 6802843
58 meter
Y = -6761727
75 meter E =
0014213
Z = 420793
61 I = 51
27349
XDOT = 4755
742687 Wp = 57
45335
YDOT = 765
474541 meter/sec RA = 271
78927 deg
ZDOT = 5957
424048 TA = 307
09818
MA = 307
22801
Ha = 229
160 n
mi
Hp = 221
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1800629
23 X = 622358
68
Y = -22184146
16 feet Y = -6755179
29 meter
Z = 1380556
45 Z = 423636
92
XDOT = 15602
830339 XDOT = 4717
891756
YDOT = 2511
399412 feet/sec YDOT = 818
443885 meter/sec
ZDOT = 19545
354487 ZDOT = 5980
433768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22154966
73 X = -6752833
86
Y = 2121021
94 feet Y = 646487
49 meter
Z = 1394007
90 Z = 424893
61
XDOT = -80
408194 XDOT = -24
508418
YDOT = -14054
610054 feet/sec YDOT = -4283
845144 meter/sec
ZDOT = 19651
123516 ZDOT = 5989
662448
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 20184
56367941
00016717 00000-0 10270-3 0 9014
2 25544 51
6443 272
3610 0002312 106
4149 253
7256 15
49465453 34394
Satellite: ISS
Catalog Number: 25544
Epoch time: 20184
56367941 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 272
3610 deg
Eccentricity:
0002312
Arg of perigee: 106
4149 deg
Mean anomaly: 253
7256 deg
Mean motion: 15
49465453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 302
Coasting Arc #3 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2020/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -115654
05 A = 6802751
22 meter
Y = 6768714
79 meter E =
0012858
Z = -612933
45 I = 51
27201
XDOT = -4802
569575 Wp = 134
34714
YDOT = -611
853455 meter/sec RA = 266
81502 deg
ZDOT = -5936
948470 TA = 52
29031
MA = 52
17381
Ha = 229
146 n
mi
Hp = 221
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -379442
42 X = -188357
98
Y = 22207069
52 feet Y = 6767015
08 meter
Z = -2010936
53 Z = -613670
46
XDOT = -15756
461860 XDOT = -4766
532579
YDOT = -2007
393225 feet/sec YDOT = -665
356509 meter/sec
ZDOT = -19478
177395 ZDOT = -5960
189946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21863961
27 X = 6664135
40
Y = -3905125
53 feet Y = -1190282
26 meter
Z = -2014688
84 Z = -614077
16
XDOT = 744
036774 XDOT = 226
782409
YDOT = 14123
900890 feet/sec YDOT = 4304
964991 meter/sec
ZDOT = -19585
030399 ZDOT = -5969
517266
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 20185
53110985
00016717 00000-0 10270-3 0 9027
2 25544 51
6429 267
5732 0002350 111
7737 248
3664 15
49467599 34546
Satellite: ISS
Catalog Number: 25544
Epoch time: 20185
53110985 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 267
5732 deg
Eccentricity:
0002350
Arg of perigee: 111
7737 deg
Mean anomaly: 248
3664 deg
Mean motion: 15
49467599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 327
Coasting Arc #4 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2020/186/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4187127
07 A = 6793238
08 meter
Y = 2467559
13 meter E =
0009206
Z = 4739717
22 I = 51
24388
XDOT = -1162
975502 Wp = 73
57818
YDOT = 7094
465185 meter/sec RA = 262
03594 deg
ZDOT = -2659
212657 TA = 42
87291
MA = 42
80118
Ha = 228
972 n
mi
Hp = 221
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13737293
55 X = 4136200
31
Y = 8095666
45 feet Y = 2514096
84 meter
Z = 15550253
36 Z = 4759933
26
XDOT = -3815
536423 XDOT = -1229
304696
YDOT = 23275
804413 feet/sec YDOT = 7081
089646 meter/sec
ZDOT = -8724
450973 ZDOT = -2665
021505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9081827
19 X = 2768140
93
Y = -12995269
85 feet Y = -3960958
25 meter
Z = 15643107
27 Z = 4768019
10
XDOT = 21986
438473 XDOT = 6701
466447
YDOT = 4803
693905 feet/sec YDOT = 1464
165902 meter/sec
ZDOT = -8751
532031 ZDOT = -2667
466963
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 20186
49853975
00016717 00000-0 10270-3 0 9037
2 25544 51
6434 262
7837 0002343 114
1103 246
0293 15
49492111 34698
Satellite: ISS
Catalog Number: 25544
Epoch time: 20186
49853975 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 262
7837 deg
Eccentricity:
0002343
Arg of perigee: 114
1103 deg
Mean anomaly: 246
0293 deg
Mean motion: 15
49492111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 309
Coasting Arc #5 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2020/187/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4376732
15 A = 6793498
36 meter
Y = -2293596
18 meter E =
0013014
Z = -4674877
92 I = 51
25031
XDOT = 697
117734 Wp = 110
92382
YDOT = -7076
577809 meter/sec RA = 257
05938 deg
ZDOT = 2821
103506 TA = 187
28630
MA = 187
30523
Ha = 229
066 n
mi
Hp = 221
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14359357
43 X = -4328051
66
Y = -7524921
84 feet Y = -2342266
78 meter
Z = -15337525
98 Z = -4696020
27
XDOT = 2287
131674 XDOT = 762
495235
YDOT = -23217
118795 feet/sec YDOT = -7068
417161 meter/sec
ZDOT = 9255
588931 ZDOT = 2824
647140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8322488
81 X = -2536694
59
Y = 13804440
52 feet Y = 4207593
47 meter
Z = -15434665
52 Z = -4704486
05
XDOT = -22046
374102 XDOT = -6719
734826
YDOT = -2930
901957 feet/sec YDOT = -893
338916 meter/sec
ZDOT = 9272
232858 ZDOT = 2826
176575
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 20187
46596830
00016717 00000-0 10270-3 0 9040
2 25544 51
6430 257
9959 0002338 117
5713 242
5675 15
49504571 34849
Satellite: ISS
Catalog Number: 25544
Epoch time: 20187
46596830 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 257
9959 deg
Eccentricity:
0002338
Arg of perigee: 117
5713 deg
Mean anomaly: 242
5675 deg
Mean motion: 15
49504571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3484
Checksum: 333
Coasting Arc #6 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2020/188/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4544494
87 A = 6793819
12 meter
Y = 2115882
47 meter E =
0009951
Z = 4578301
32 I = 51
26030
XDOT = -250
964800 Wp = 75
84780
YDOT = 7048
942420 meter/sec RA = 252
08213 deg
ZDOT = -3000
692628 TA = 44
31701
MA = 44
23740
Ha = 228
878 n
mi
Hp = 221
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14909760
08 X = 4498258
36
Y = 6941871
63 feet Y = 2166442
88 meter
Z = 15020673
64 Z = 4600264
37
XDOT = -823
375328 XDOT = -315
194163
YDOT = 23126
451509 feet/sec YDOT = 7045
777380 meter/sec
ZDOT = -9844
792085 ZDOT = -3002
066382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7523048
53 X = 2293025
19
Y = -14520733
61 feet Y = -4425919
60 meter
Z = 15121613
68 Z = 4609067
85
XDOT = 22019
025798 XDOT = 6711
399063
YDOT = 1121
948639 feet/sec YDOT = 341
969945 meter/sec
ZDOT = -9851
432880 ZDOT = -3002
716742
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 20188
49788983
00016717 00000-0 10270-3 0 9057
2 25544 51
6431 252
8875 0002201 117
5439 242
5935 15
49509126 35004
Satellite: ISS
Catalog Number: 25544
Epoch time: 20188
49788983 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 252
8875 deg
Eccentricity:
0002201
Arg of perigee: 117
5439 deg
Mean anomaly: 242
5935 deg
Mean motion: 15
49509126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 325
Coasting Arc #7 (Orbit 3514)
---------------------------------------
Vector Time (GMT): 2020/189/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4726758
97 A = 6794148
98 meter
Y = -1908190
91 meter E =
0012005
Z = -4504041
30 I = 51
27121
XDOT = -193
555799 Wp = 112
42854
YDOT = -6966
146219 meter/sec RA = 247
10695 deg
ZDOT = 3156
708030 TA = 189
49244
MA = 189
51515
Ha = 229
052 n
mi
Hp = 221
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15507739
40 X = -4683192
14
Y = -6260468
86 feet Y = -1960804
56 meter
Z = -14777038
37 Z = -4526896
04
XDOT = -635
025586 XDOT = -130
977034
YDOT = -22854
810429 feet/sec YDOT = -6967
961313 meter/sec
ZDOT = 10356
653643 ZDOT = 3155
918683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6604322
81 X = -2012997
59
Y = 15262704
30 feet Y = 4652072
27 meter
Z = -14882106
45 Z = -4536066
05
XDOT = -21751
342792 XDOT = -6629
809283
YDOT = 675
846897 feet/sec YDOT = 205
998134 meter/sec
ZDOT = 10353
317198 ZDOT = 3155
691082
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 20189
46531724
00016717 00000-0 10270-3 0 9065
2 25544 51
6414 248
0997 0002344 120
1657 239
9726 15
49505180 35157
Satellite: ISS
Catalog Number: 25544
Epoch time: 20189
46531724 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 248
0997 deg
Eccentricity:
0002344
Arg of perigee: 120
1657 deg
Mean anomaly: 239
9726 deg
Mean motion: 15
49505180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3515
Checksum: 316
Coasting Arc #8 (Orbit 3518)
---------------------------------------
Vector Time (GMT): 2020/189/16:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3741356
67 A = 6791013
71 meter
Y = 2047780
42 meter E =
0016911
Z = -5299285
98 I = 51
26055
XDOT = -3340
408301 Wp = 91
17561
YDOT = -6873
853984 meter/sec RA = 245
88109 deg
ZDOT = -299
039693 TA = 175
95801
MA = 175
94433
Ha = 229
153 n
mi
Hp = 221
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12274792
23 X = -3738237
17
Y = 6718439
69 feet Y = 2005960
17 meter
Z = -17386108
85 Z = -5317451
73
XDOT = -10959
344820 XDOT = -3261
842021
YDOT = -22552
014382 feet/sec YDOT = -6910
769472 meter/sec
ZDOT = -981
101356 ZDOT = -315
075997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12203541
04 X = 3719639
31
Y = -6630640
06 feet Y = -2021019
09 meter
Z = -17469772
06 Z = -5324786
52
XDOT = 10307
784350 XDOT = 3141
812670
YDOT = 21739
705145 feet/sec YDOT = 6626
262128 meter/sec
ZDOT = -1054
596337 ZDOT = -321
440964
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 20189
72329844
00016717 00000-0 10270-3 0 9073
2 25544 51
6384 246
8236 0002337 113
5442 246
5953 15
49462965 35198
Satellite: ISS
Catalog Number: 25544
Epoch time: 20189
72329844 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 246
8236 deg
Eccentricity:
0002337
Arg of perigee: 113
5442 deg
Mean anomaly: 246
5953 deg
Mean motion: 15
49462965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3519
Checksum: 335
Coasting Arc #9 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2020/190/16:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3649982
43 A = 6790950
77 meter
Y = -2172327
10 meter E =
0004607
Z = 5294823
17 I = 51
27517
XDOT = 3801
984101 Wp = 106
60920
YDOT = 6654
374263 meter/sec RA = 240
90500 deg
ZDOT = 107
848385 TA = 342
34937
MA = 342
36537
Ha = 228
961 n
mi
Hp = 221
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11975007
96 X = 3648284
11
Y = -7127057
42 feet Y = -2131520
60 meter
Z = 17371467
08 Z = 5312548
55
XDOT = 12473
701119 XDOT = 3726
766481
YDOT = 21831
936557 feet/sec YDOT = 6696
470177 meter/sec
ZDOT = 353
833284 ZDOT = 126
134742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11783896
94 X = -3591731
79
Y = 7245160
79 feet Y = 2208325
01 meter
Z = 17453110
03 Z = 5319707
94
XDOT = -12161
904819 XDOT = -3706
948589
YDOT = -20845
965077 feet/sec YDOT = -6353
850155 meter/sec
ZDOT = 437
718183 ZDOT = 133
416502
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 20190
75522032
00016717 00000-0 10270-3 0 9083
2 25544 51
6383 241
7152 0002244 117
4691 242
6688 15
49469497 35351
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
75522032 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 241
7152 deg
Eccentricity:
0002244
Arg of perigee: 117
4691 deg
Mean anomaly: 242
6688 deg
Mean motion: 15
49469497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 318
Coasting Arc #10 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2020/190/18:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 965635
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1404938
61 A = 6794133
64 meter
Y = -4876268
00 meter E =
0010970
Z = 4511263
49 I = 51
28854
XDOT = 5389
391197 Wp = 114
22103
YDOT = 4459
638802 meter/sec RA = 240
63373 deg
ZDOT = 3131
587247 TA = 304
15047
MA = 304
25446
Ha = 228
913 n
mi
Hp = 221
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4609378
63 X = 1437449
42
Y = -15998254
58 feet Y = -4860375
79 meter
Z = 14800733
22 Z = 4518166
29
XDOT = 17681
729648 XDOT = 5323
910513
YDOT = 14631
360898 feet/sec YDOT = 4519
540275 meter/sec
ZDOT = 10274
236376 ZDOT = 3157
607790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1779590
11 X = 542419
06
Y = 16525036
72 feet Y = 5036831
19 meter
Z = 14832681
66 Z = 4521001
37
XDOT = -20591
050158 XDOT = -6276
152088
YDOT = -7142
642408 feet/sec YDOT = -2177
077406 meter/sec
ZDOT = 10393
794106 ZDOT = 3168
028443
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 20190
81971378
00016717 00000-0 10270-3 0 9092
2 25544 51
6397 241
3964 0002128 121
4826 238
6532 15
49519102 35362
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
81971378 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 241
3964 deg
Eccentricity:
0002128
Arg of perigee: 121
4826 deg
Mean anomaly: 238
6532 deg
Mean motion: 15
49519102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 318
Coasting Arc #11 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2020/191/18:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 965635
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1155920
60 A = 6793854
75 meter
Y = 4860712
57 meter E =
0011733
Z = -4614860
68 I = 51
30554
XDOT = -5704
577080 Wp = 78
21279
YDOT = -4156
517636 meter/sec RA = 235
65868 deg
ZDOT = -2953
137193 TA = 162
16925
MA = 162
12805
Ha = 229
012 n
mi
Hp = 221
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3792390
42 X = -1187772
72
Y = 15947219
72 feet Y = 4847608
68 meter
Z = -15140619
03 Z = -4620552
38
XDOT = -18715
804069 XDOT = -5643
329323
YDOT = -13636
868885 feet/sec YDOT = -4219
967489 meter/sec
ZDOT = -9688
770317 ZDOT = -2980
698969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2798619
69 X = -853019
28
Y = -16126523
60 feet Y = -4915364
39 meter
Z = -15166982
27 Z = -4622896
19
XDOT = 21307
422888 XDOT = 6494
502496
YDOT = 5521
213420 feet/sec YDOT = 1682
865850 meter/sec
ZDOT = -9815
454452 ZDOT = -2991
750517
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 20191
78713984
00016717 00000-0 10270-3 0 9108
2 25544 51
6403 236
6065 0002143 118
7252 241
4114 15
49490834 35513
Satellite: ISS
Catalog Number: 25544
Epoch time: 20191
78713984 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 236
6065 deg
Eccentricity:
0002143
Arg of perigee: 118
7252 deg
Mean anomaly: 241
4114 deg
Mean motion: 15
49490834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3551
Checksum: 295
Coasting Arc #12 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2020/191/21:38:06
667
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4024861
41 A = 6791597
32 meter
Y = 1585313
72 meter E =
0015712
Z = -5249578
66 I = 51
30151
XDOT = -3760
137889 Wp = 100
08737
YDOT = -6601
309206 meter/sec RA = 234
95508 deg
ZDOT = 888
969389 TA = 178
47916
MA = 178
47438
Ha = 228
993 n
mi
Hp = 221
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13204925
88 X = -4016790
78
Y = 5201160
48 feet Y = 1540350
56 meter
Z = -17223027
09 Z = -5269109
70
XDOT = -12336
410396 XDOT = -3690
358641
YDOT = -21657
838603 feet/sec YDOT = -6642
967690 meter/sec
ZDOT = 2916
566238 ZDOT = 870
873198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -878868
43 X = -267879
10
Y = -14055028
34 feet Y = -4283972
64 meter
Z = -17312959
56 Z = -5276990
07
XDOT = 23399
131002 XDOT = 7132
055129
YDOT = -4955
152810 feet/sec YDOT = -1510
330577 meter/sec
ZDOT = 2833
522720 ZDOT = 863
657725
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 20191
91612986
00016717 00000-0 10270-3 0 9114
2 25544 51
6426 235
9693 0001511 131
4115 228
7165 15
49335650 35535
Satellite: ISS
Catalog Number: 25544
Epoch time: 20191
91612986 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 235
9693 deg
Eccentricity:
0001511
Arg of perigee: 131
4115 deg
Mean anomaly: 228
7165 deg
Mean motion: 15
49335650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 303
Coasting Arc #13 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2020/192/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1855823
95 A = 6792612
84 meter
Y = 4170338
53 meter E =
0013895
Z = -5042809
18 I = 51
31697
XDOT = -5670
233954 Wp = 82
30038
YDOT = -4782
263593 meter/sec RA = 231
79418 deg
ZDOT = -1870
772596 TA = 169
45746
MA = 169
42830
Ha = 229
062 n
mi
Hp = 221
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6088661
27 X = -1877825
35
Y = 13682213
02 feet Y = 4149462
89 meter
Z = -16544649
54 Z = -5051876
89
XDOT = -18603
129769 XDOT = -5607
248853
YDOT = -15689
841184 feet/sec YDOT = -4845
319825 meter/sec
ZDOT = -6137
705366 ZDOT = -1898
163418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14728264
86 X = 4489175
13
Y = -2442501
68 feet Y = -744474
51 meter
Z = -16586517
94 Z = -5055570
67
XDOT = -3223
542345 XDOT = -982
535707
YDOT = 23038
477139 feet/sec YDOT = 7022
127832 meter/sec
ZDOT = -6263
598885 ZDOT = -1909
144940
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 20192
56114604
00016717 00000-0 10270-3 0 9121
2 25544 51
6422 232
7757 0001740 135
8112 224
3177 15
49315585 35637
Satellite: ISS
Catalog Number: 25544
Epoch time: 20192
56114604 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 232
7757 deg
Eccentricity:
0001740
Arg of perigee: 135
8112 deg
Mean anomaly: 224
3177 deg
Mean motion: 15
49315585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 292
Coasting Arc #14 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2020/193/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5358417
76 A = 6801411
67 meter
Y = -3621696
11 meter E =
0006283
Z = -2102186
22 I = 51
35414
XDOT = 1340
279868 Wp = 56
12266
YDOT = -5162
429177 meter/sec RA = 229
11838 deg
ZDOT = 5492
913183 TA = 280
56238
MA = 280
63315
Ha = 228
947 n
mi
Hp = 221
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17580110
77 X = -5307309
58
Y = -11882205
10 feet Y = -3681331
79 meter
Z = -6896936
41 Z = -2128091
14
XDOT = 4397
243662 XDOT = 1371
227074
YDOT = -16937
103600 feet/sec YDOT = -5147
268729 meter/sec
ZDOT = 18021
368710 ZDOT = 5499
498278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3916880
60 X = -1193865
21
Y = -20814611
35 feet Y = -6344293
54 meter
Z = -7016040
57 Z = -2138489
17
XDOT = 13513
777877 XDOT = 4118
999497
YDOT = -8611
170568 feet/sec YDOT = -2624
684789 meter/sec
ZDOT = 18051
839762 ZDOT = 5502
200760
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 20193
07715898
00016717 00000-0 10270-3 0 9131
2 25544 51
6385 230
2204 0001533 140
2667 219
8595 15
49319818 35715
Satellite: ISS
Catalog Number: 25544
Epoch time: 20193
07715898 = yrday
fracday
Element set: 913
Inclination: 51
6385 deg
RA of node: 230
2204 deg
Eccentricity:
0001533
Arg of perigee: 140
2667 deg
Mean anomaly: 219
8595 deg
Mean motion: 15
49319818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 320
Coasting Arc #15 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2020/194/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5623937
79 A = 6801502
74 meter
Y = 3260361
87 meter E =
0014963
Z = 1975159
74 I = 51
37820
XDOT = -1040
038177 Wp = 114
70447
YDOT = 5175
865451 meter/sec RA = 224
15052 deg
ZDOT = -5555
278005 TA = 43
45025
MA = 43
33243
Ha = 228
740 n
mi
Hp = 221
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18451239
48 X = 5577467
40
Y = 10696725
31 feet Y = 3322992
73 meter
Z = 6480182
88 Z = 2002365
75
XDOT = -3412
198743 XDOT = -1070
854922
YDOT = 16981
185862 feet/sec YDOT = 5164
063240 meter/sec
ZDOT = -18225
977708 ZDOT = -5560
404381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5727500
98 X = 1745742
30
Y = 20504307
48 feet Y = 6249712
92 meter
Z = 6605304
55 Z = 2013296
83
XDOT = -12705
074359 XDOT = -3872
506665
YDOT = 9456
034894 feet/sec YDOT = 2882
199436 meter/sec
ZDOT = -18249
727091 ZDOT = -5562
516817
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 20194
10918452
00016717 00000-0 10270-3 0 9148
2 25544 51
6389 225
1127 0001277 146
6271 213
4960 15
49366195 35875
Satellite: ISS
Catalog Number: 25544
Epoch time: 20194
10918452 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 225
1127 deg
Eccentricity:
0001277
Arg of perigee: 146
6271 deg
Mean anomaly: 213
4960 deg
Mean motion: 15
49366195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 317
Coasting Arc #16 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2020/195/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5879059
53 A = 6801774
20 meter
Y = -2852310
31 meter E =
0006605
Z = -1883646
78 I = 51
40337
XDOT = 722
788521 Wp = 53
13557
YDOT = -5174
439246 meter/sec RA = 219
18341 deg
ZDOT = 5597
029207 TA = 286
10763
MA = 286
18033
Ha = 228
904 n
mi
Hp = 221
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19288253
05 X = -5837577
61
Y = -9357973
47 feet Y = -2917822
02 meter
Z = -6179943
51 Z = -1912104
24
XDOT = 2371
353414 XDOT = 753
410005
YDOT = -16976
506713 feet/sec YDOT = -5166
185865 meter/sec
ZDOT = 18362
956717 ZDOT = 5600
614045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7607750
20 X = -2318842
26
Y = -20002382
89 feet Y = -6096726
31 meter
Z = -6310854
97 Z = -1923548
59
XDOT = 11807
668451 XDOT = 3598
977344
YDOT = -10272
036412 feet/sec YDOT = -3130
916698 meter/sec
ZDOT = 18379
603768 ZDOT = 5602
103228
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 20195
07671106
00016717 00000-0 10270-3 0 9158
2 25544 51
6385 220
3237 0001613 149
2359 210
8886 15
49321557 36029
Satellite: ISS
Catalog Number: 25544
Epoch time: 20195
07671106 = yrday
fracday
Element set: 915
Inclination: 51
6385 deg
RA of node: 220
3237 deg
Eccentricity:
0001613
Arg of perigee: 149
2359 deg
Mean anomaly: 210
8886 deg
Mean motion: 15
49321557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 301
Coasting Arc #17 (Orbit 3603)
---------------------------------------
Vector Time (GMT): 2020/195/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2344579
37 A = 6798416
14 meter
Y = 5384297
99 meter E =
0005976
Z = -3428251
90 I = 51
39667
XDOT = -6134
631535 Wp = 106
48662
YDOT = -235
220098 meter/sec RA = 218
68980 deg
ZDOT = -4573
210638 TA = 113
68808
MA = 113
62536
Ha = 228
981 n
mi
Hp = 221
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7692189
54 X = 2300848
63
Y = 17665019
66 feet Y = 5410272
59 meter
Z = -11247545
59 Z = -3416968
60
XDOT = -20126
743882 XDOT = -6109
331450
YDOT = -771
719483 feet/sec YDOT = -303
679993 meter/sec
ZDOT = -15003
971909 ZDOT = -4602
948599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6394318
31 X = 1948988
22
Y = 18207077
61 feet Y = 5549517
25 meter
Z = -11195758
12 Z = -3412467
07
XDOT = -18578
447021 XDOT = -5662
710652
YDOT = -2768
710828 feet/sec YDOT = -843
903060 meter/sec
ZDOT = -15140
852852 ZDOT = -4614
931949
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 20195
20571498
00016717 00000-0 10270-3 0 9167
2 25544 51
6404 219
6839 0001857 151
4808 208
6444 15
49326833 36043
Satellite: ISS
Catalog Number: 25544
Epoch time: 20195
20571498 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 219
6839 deg
Eccentricity:
0001857
Arg of perigee: 151
4808 deg
Mean anomaly: 208
6444 deg
Mean motion: 15
49326833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3604
Checksum: 324
Coasting Arc #18 (Orbit 3619)
---------------------------------------
Vector Time (GMT): 2020/196/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2694993
00 A = 6798115
93 meter
Y = -5158750
37 meter E =
0013158
Z = 3503360
87 I = 51
42386
XDOT = 6201
245381 Wp = 98
93312
YDOT = -173
826999 meter/sec RA = 213
72507 deg
ZDOT = 4497
896482 TA = 302
34057
MA = 302
46789
Ha = 228
923 n
mi
Hp = 221
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8841840
55 X = -2654123
23
Y = -16925034
01 feet Y = -5188659
58 meter
Z = 11493966
12 Z = 3490368
41
XDOT = 20345
293245 XDOT = 6180
880207
YDOT = -570
298552 feet/sec YDOT = -104
594629 meter/sec
ZDOT = 14756
878221 ZDOT = 4527
970041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7899757
96 X = -2407846
23
Y = -17424034
51 feet Y = -5310845
72 meter
Z = 11434291
56 Z = 3485172
07
XDOT = 18971
701428 XDOT = 5782
574595
YDOT = 1209
143686 feet/sec YDOT = 368
546995 meter/sec
ZDOT = 14895
330568 ZDOT = 4540
096757
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 20196
23773809
00016717 00000-0 10270-3 0 9172
2 25544 51
6412 214
5764 0001860 155
6355 204
4883 15
49356907 36204
Satellite: ISS
Catalog Number: 25544
Epoch time: 20196
23773809 = yrday
fracday
Element set: 917
Inclination: 51
6412 deg
RA of node: 214
5764 deg
Eccentricity:
0001860
Arg of perigee: 155
6355 deg
Mean anomaly: 204
4883 deg
Mean motion: 15
49356907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3620
Checksum: 320
Coasting Arc #19 (Orbit 3634)
---------------------------------------
Vector Time (GMT): 2020/197/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2993413
10 A = 6797906
69 meter
Y = 4924423
63 meter E =
0006098
Z = -3609861
03 I = 51
45088
XDOT = -6238
805185 Wp = 100
52338
YDOT = 573
574900 meter/sec RA = 208
76270 deg
ZDOT = -4398
411806 TA = 122
22466
MA = 122
16554
Ha = 228
950 n
mi
Hp = 221
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9820909
12 X = 2955658
80
Y = 16156245
49 feet Y = 4957687
48 meter
Z = -11843376
08 Z = -3595411
33
XDOT = -20468
520949 XDOT = -6223
390531
YDOT = 1881
807416 feet/sec YDOT = 503
894889 meter/sec
ZDOT = -14430
484928 ZDOT = -4428
679822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9211288
81 X = 2807600
83
Y = 16558838
55 feet Y = 5047133
99 meter
Z = -11776973
53 Z = -3589621
53
XDOT = -19223
336800 XDOT = -5859
273057
YDOT = 348
573256 feet/sec YDOT = 106
245128 meter/sec
ZDOT = -14569
860155 ZDOT = -4440
893375
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 20197
20526177
00016717 00000-0 10270-3 0 9185
2 25544 51
6405 209
7888 0001860 156
4844 203
6391 15
49322741 36351
Satellite: ISS
Catalog Number: 25544
Epoch time: 20197
20526177 = yrday
fracday
Element set: 918
Inclination: 51
6405 deg
RA of node: 209
7888 deg
Eccentricity:
0001860
Arg of perigee: 156
4844 deg
Mean anomaly: 203
6391 deg
Mean motion: 15
49322741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3635
Checksum: 320
Coasting Arc #20 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2020/198/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965539
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3299411
12 A = 6797574
17 meter
Y = -4658665
27 meter E =
0012641
Z = 3682036
54 I = 51
48062
XDOT = 6249
833291 Wp = 102
79746
YDOT = -1000
675405 meter/sec RA = 203
80200 deg
ZDOT = 4318
975427 TA = 301
05249
MA = 301
17652
Ha = 228
862 n
mi
Hp = 221
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10824839
64 X = -3264956
45
Y = -15284334
88 feet Y = -4695369
54 meter
Z = 12080172
38 Z = 3666092
37
XDOT = 20504
702398 XDOT = 6239
579645
YDOT = -3283
055792 feet/sec YDOT = -930
843281 meter/sec
ZDOT = 14169
866886 ZDOT = 4349
309463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10521755
31 X = -3207031
02
Y = -15551411
26 feet Y = -4740070
15 meter
Z = 12006868
20 Z = 3659693
43
XDOT = 19349
175850 XDOT = 5897
628799
YDOT = -2004
174483 feet/sec YDOT = -610
872382 meter/sec
ZDOT = 14309
576200 ZDOT = 4361
558826
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 20198
23728402
00016717 00000-0 10270-3 0 9195
2 25544 51
6409 204
6814 0001881 163
2374 196
8838 15
49362156 36516
Satellite: ISS
Catalog Number: 25544
Epoch time: 20198
23728402 = yrday
fracday
Element set: 919
Inclination: 51
6409 deg
RA of node: 204
6814 deg
Eccentricity:
0001881
Arg of perigee: 163
2374 deg
Mean anomaly: 196
8838 deg
Mean motion: 15
49362156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 325
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