[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 28th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16466 6302 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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
089/03:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 221
3
093/12:44:33
314 1
5 1
5 1
5
N/A -0
0 0
0 231
0
000/00:07:06
628 -0
2 -0
0 222
0
096/03:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
1
000/00:00:00
000 0
0 0
0 221
8
097/14:00:43
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 222
0
100/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
0
000/00:00:00
000 0
0 0
0 222
0
100/08:05:06
000 0
0 0
0 0
0
N/A 0
0 0
0 230
8
000/00:00:00
000 0
0 0
0 221
9
100/14:16:50
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 1934)
---------------------------------------
Vector Time (GMT): 2020/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2379380
55 A = 6792533
25 meter
Y = 3457858
90 meter E =
0007412
Z = 5334741
74 I = 51
83086
XDOT = -6429
693633 Wp = 64
30776
YDOT = -4170
445973 meter/sec RA = 32
02071 deg
ZDOT = -161
250515 TA = 27
24490
MA = 27
20604
Ha = 231
008 n
mi
Hp = 221
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7806366
63 X = -2443783
77
Y = 11344681
44 feet Y = 3430891
32 meter
Z = 17502433
53 Z = 5323026
87
XDOT = -21094
795383 XDOT = -6381
797339
YDOT = -13682
565527 feet/sec YDOT = -4242
079589 meter/sec
ZDOT = -529
037122 ZDOT = -192
366930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7014518
55 X = -2138025
25
Y = 11930009
61 feet Y = 3636266
93 meter
Z = 17448430
77 Z = 5318281
70
XDOT = -21225
160498 XDOT = -6469
428920
YDOT = -11481
741988 feet/sec YDOT = -3499
634958 meter/sec
ZDOT = -671
525558 ZDOT = -204
680990
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 20087
54807131
00016717 00000-0 10270-3 0 9003
2 25544 51
6426 32
4250 0005074 57
3311 302
8328 15
48930609 19357
Satellite: ISS
Catalog Number: 25544
Epoch time: 20087
54807131 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 32
4250 deg
Eccentricity:
0005074
Arg of perigee: 57
3311 deg
Mean anomaly: 302
8328 deg
Mean motion: 15
48930609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1935
Checksum: 284
Coasting Arc #2 (Orbit 1949)
---------------------------------------
Vector Time (GMT): 2020/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2049076
16 A = 6792597
89 meter
Y = -3677819
46 meter E =
0019328
Z = -5347071
41 I = 51
80180
XDOT = 6757
481125 Wp = 83
42484
YDOT = 3574
342404 meter/sec RA = 27
08829 deg
ZDOT = 133
632541 TA = 187
83441
MA = 187
86465
Ha = 230
950 n
mi
Hp = 221
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6722690
82 X = 2116023
53
Y = -12066336
81 feet Y = -3654531
26 meter
Z = -17542885
20 Z = -5336954
89
XDOT = 22170
213665 XDOT = 6716
360428
YDOT = 11726
845156 feet/sec YDOT = 3649
679452 meter/sec
ZDOT = 438
426971 ZDOT = 166
357848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5661079
96 X = 1725497
17
Y = -12664087
19 feet Y = -3860013
77 meter
Z = -17496198
06 Z = -5332841
17
XDOT = 22259
486716 XDOT = 6784
691551
YDOT = 9149
270340 feet/sec YDOT = 2788
697600 meter/sec
ZDOT = 588
323380 ZDOT = 179
320966
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 20088
51584914
00016717 00000-0 10270-3 0 9013
2 25544 51
6426 27
6385 0005031 61
2618 298
9037 15
48913846 19502
Satellite: ISS
Catalog Number: 25544
Epoch time: 20088
51584914 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 27
6385 deg
Eccentricity:
0005031
Arg of perigee: 61
2618 deg
Mean anomaly: 298
9037 deg
Mean motion: 15
48913846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1950
Checksum: 319
Coasting Arc #3 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2020/089/03:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2227996
95 A = 6792721
18 meter
Y = -3601066
56 meter E =
0018997
Z = -5327591
23 I = 51
78325
XDOT = 6801
709948 Wp = 87
01036
YDOT = 3454
680784 meter/sec RA = 23
89798 deg
ZDOT = 511
901580 TA = 187
86308
MA = 187
89290
Ha = 230
905 n
mi
Hp = 221
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7309701
28 X = 2293978
12
Y = -11814522
84 feet Y = -3575782
88 meter
Z = -17478973
84 Z = -5316607
97
XDOT = 22315
321353 XDOT = 6760
086628
YDOT = 11334
254542 feet/sec YDOT = 3530
509639 meter/sec
ZDOT = 1679
467126 ZDOT = 544
840568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6215457
02 X = 1894471
30
Y = 12496046
80 feet Y = 3808795
06 meter
Z = -17428313
67 Z = -5312150
01
XDOT = -20382
937219 XDOT = -6212
719264
YDOT = 12679
467325 feet/sec YDOT = 3864
701641 meter/sec
ZDOT = 1830
342592 ZDOT = 557
888422
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 20089
16103214
00016717 00000-0 10270-3 0 9026
2 25544 51
6433 24
4471 0004767 65
9697 294
1952 15
48902988 19604
Satellite: ISS
Catalog Number: 25544
Epoch time: 20089
16103214 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 24
4471 deg
Eccentricity:
0004767
Arg of perigee: 65
9697 deg
Mean anomaly: 294
1952 deg
Mean motion: 15
48902988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 324
Coasting Arc #4 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2020/090/03:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1891939
88 A = 6792559
52 meter
Y = 3777952
66 meter E =
0007619
Z = 5312604
23 I = 51
75271
XDOT = -7097
918028 Wp = 67
93842
YDOT = -2852
248539 meter/sec RA = 18
96238 deg
ZDOT = -496
048094 TA = 26
80766
MA = 26
76830
Ha = 230
940 n
mi
Hp = 221
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6207151
82 X = -1959851
18
Y = 12394857
82 feet Y = 3756416
12 meter
Z = 17429803
91 Z = 5303248
80
XDOT = -23287
132639 XDOT = -7063
086280
YDOT = -9357
770796 feet/sec YDOT = -2931
427766 meter/sec
ZDOT = -1627
454376 ZDOT = -530
442488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7488250
87 X = -2282418
87
Y = -11729946
92 feet Y = -3575287
82 meter
Z = 17386596
64 Z = 5299434
65
XDOT = 18997
323871 XDOT = 5790
384316
YDOT = -14789
904538 feet/sec YDOT = -4507
962903 meter/sec
ZDOT = -1785
038789 ZDOT = -544
079823
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 20090
19332297
00016717 00000-0 10270-3 0 9037
2 25544 51
6439 19
3416 0004800 69
1166 291
0497 15
48950351 19761
Satellite: ISS
Catalog Number: 25544
Epoch time: 20090
19332297 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 19
3416 deg
Eccentricity:
0004800
Arg of perigee: 69
1166 deg
Mean anomaly: 291
0497 deg
Mean motion: 15
48950351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 312
Coasting Arc #5 (Orbit 1990)
---------------------------------------
Vector Time (GMT): 2020/091/03:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1536320
46 A = 6792698
70 meter
Y = -3948603
83 meter E =
0019382
Z = -5326057
23 I = 51
72024
XDOT = 7304
483470 Wp = 88
00477
YDOT = 2208
393436 meter/sec RA = 14
02454 deg
ZDOT = 471
902975 TA = 186
49233
MA = 186
51748
Ha = 231
006 n
mi
Hp = 221
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5040421
45 X = 1606231
74
Y = -12954736
98 feet Y = -3931032
83 meter
Z = -17473941
05 Z = -5318424
47
XDOT = 23964
840782 XDOT = 7276
953438
YDOT = 7245
385288 feet/sec YDOT = 2289
923444 meter/sec
ZDOT = 1548
238106 ZDOT = 507
318477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8749621
37 X = 2666884
59
Y = 10858556
92 feet Y = 3309688
15 meter
Z = -17438622
12 Z = -5315292
02
XDOT = -17287
480427 XDOT = -5269
224034
YDOT = 16665
702083 feet/sec YDOT = 5079
705995 meter/sec
ZDOT = 1710
545184 ZDOT = 521
374172
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 20091
16109611
00016717 00000-0 10270-3 0 9048
2 25544 51
6436 14
5552 0004970 71
9270 288
2421 15
48906343 19915
Satellite: ISS
Catalog Number: 25544
Epoch time: 20091
16109611 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 14
5552 deg
Eccentricity:
0004970
Arg of perigee: 71
9270 deg
Mean anomaly: 288
2421 deg
Mean motion: 15
48906343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1991
Checksum: 297
Coasting Arc #6 (Orbit 2006)
---------------------------------------
Vector Time (GMT): 2020/092/03:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1174436
73 A = 6792551
70 meter
Y = 4061308
93 meter E =
0007736
Z = 5310255
84 I = 51
68660
XDOT = -7490
715537 Wp = 72
89288
YDOT = -1564
051829 meter/sec RA = 9
08501 deg
ZDOT = -457
706633 TA = 21
48749
MA = 21
45504
Ha = 231
013 n
mi
Hp = 221
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3853138
88 X = -1245558
37
Y = 13324504
37 feet Y = 4047777
97 meter
Z = 17422099
23 Z = 5304378
09
XDOT = -24575
838377 XDOT = -7470
445848
YDOT = -5131
403637 feet/sec YDOT = -1647
705008 meter/sec
ZDOT = -1501
662183 ZDOT = -494
044310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9825840
57 X = -2994916
21
Y = -9838275
31 feet Y = -2998706
31 meter
Z = 17394822
03 Z = 5301941
76
XDOT = 15493
840159 XDOT = 4722
522480
YDOT = -18439
954544 feet/sec YDOT = -5620
498145 meter/sec
ZDOT = -1668
240446 ZDOT = -508
479688
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 20092
19338426
00016717 00000-0 10270-3 0 9051
2 25544 51
6428 9
4502 0004980 76
2031 283
9673 15
48948725 20078
Satellite: ISS
Catalog Number: 25544
Epoch time: 20092
19338426 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 9
4502 deg
Eccentricity:
0004980
Arg of perigee: 76
2031 deg
Mean anomaly: 283
9673 deg
Mean motion: 15
48948725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2007
Checksum: 313
Coasting Arc #7 (Orbit 2021)
---------------------------------------
Vector Time (GMT): 2020/093/03:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 797480
96 A = 6792670
35 meter
Y = -4164542
16 meter E =
0019568
Z = -5323641
38 I = 51
65424
XDOT = 7580
254920 Wp = 89
59157
YDOT = 895
300213 meter/sec RA = 4
14211 deg
ZDOT = 436
680905 TA = 184
57583
MA = 184
59374
Ha = 231
029 n
mi
Hp = 221
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2616407
36 X = 869849
93
Y = -13663196
07 feet Y = -4155219
62 meter
Z = -17466015
01 Z = -5319591
70
XDOT = 24869
602757 XDOT = 7567
558894
YDOT = 2937
336656 feet/sec YDOT = 979
997033 meter/sec
ZDOT = 1432
680136 ZDOT = 473
471800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10864210
49 X = 3311411
36
Y = 8726811
54 feet Y = 2659932
16 meter
Z = -17447116
82 Z = -5317881
21
XDOT = -13431
669243 XDOT = -4093
972785
YDOT = 19912
926467 feet/sec YDOT = 6069
459987 meter/sec
ZDOT = 1601
381047 ZDOT = 488
100943
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 20093
16115430
00016717 00000-0 10270-3 0 9068
2 25544 51
6438 4
6632 0004983 79
1781 280
9930 15
48912334 20224
Satellite: ISS
Catalog Number: 25544
Epoch time: 20093
16115430 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 4
6632 deg
Eccentricity:
0004983
Arg of perigee: 79
1781 deg
Mean anomaly: 280
9930 deg
Mean motion: 15
48912334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2022
Checksum: 296
Coasting Arc #8 (Orbit 2027)
---------------------------------------
Vector Time (GMT): 2020/093/12:48:06
628
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 965428
07 A = 6793518
01 meter
Y = -4159502
89 meter E =
0018059
Z = -5299476
68 I = 51
64292
XDOT = 7565
025934 Wp = 91
31265
YDOT = 855
179671 meter/sec RA = 2
22536 deg
ZDOT = 708
623198 TA = 185
46497
MA = 185
48471
Ha = 230
952 n
mi
Hp = 221
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3167414
92 X = 1037610
79
Y = -13646663
04 feet Y = -4148303
30 meter
Z = -17386734
51 Z = -5294611
63
XDOT = 24819
638892 XDOT = 7551
458750
YDOT = 2805
707582 feet/sec YDOT = 939
701326 meter/sec
ZDOT = 2324
879260 ZDOT = 745
337954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2176375
20 X = -663359
16
Y = -13867731
65 feet Y = -4226884
61 meter
Z = -17364097
33 Z = -5292576
87
XDOT = 22983
203694 XDOT = 7005
280486
YDOT = -6721
810686 feet/sec YDOT = -2048
807897 meter/sec
ZDOT = 2493
230800 ZDOT = 759
936748
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 20093
54826209
00016717 00000-0 10270-3 0 9074
2 25544 51
6451 2
7504 0003712 75
7633 284
3929 15
48660634 20288
Satellite: ISS
Catalog Number: 25544
Epoch time: 20093
54826209 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 2
7504 deg
Eccentricity:
0003712
Arg of perigee: 75
7633 deg
Mean anomaly: 284
3929 deg
Mean motion: 15
48660634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2028
Checksum: 306
Coasting Arc #9 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2020/094/12:48:06
628
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -468161
96 A = 6793364
42 meter
Y = 4222751
60 meter E =
0006574
Z = 5295608
07 I = 51
60956
XDOT = -7641
161565 Wp = 71
89647
YDOT = -104
814924 meter/sec RA = 357
28272 deg
ZDOT = -589
342235 TA = 23
74856
MA = 23
71823
Ha = 230
921 n
mi
Hp = 221
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1535964
45 X = -541070
05
Y = 13854171
90 feet Y = 4217108
81 meter
Z = 17374042
23 Z = 5293156
72
XDOT = -25069
427708 XDOT = -7636
558925
YDOT = -343
880983 feet/sec YDOT = -190
238112 meter/sec
ZDOT = -1933
537518 ZDOT = -626
448523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3993996
80 X = 1217370
22
Y = 13369631
12 feet Y = 4075063
57 meter
Z = 17362475
70 Z = 5292082
59
XDOT = -22149
928193 XDOT = -6751
298113
YDOT = 9360
090783 feet/sec YDOT = 2852
955671 meter/sec
ZDOT = -2103
733268 ZDOT = -641
217900
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 20094
58073802
00016717 00000-0 10270-3 0 9083
2 25544 51
6455 357
6459 0003659 78
7517 281
4044 15
48688518 20442
Satellite: ISS
Catalog Number: 25544
Epoch time: 20094
58073802 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 357
6459 deg
Eccentricity:
0003659
Arg of perigee: 78
7517 deg
Mean anomaly: 281
4044 deg
Mean motion: 15
48688518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 339
Coasting Arc #10 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2020/095/12:48:06
628
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -41192
05 A = 6793395
44 meter
Y = -4249544
42 meter E =
0018372
Z = -5315948
58 I = 51
57533
XDOT = 7603
951221 Wp = 90
92703
YDOT = -652
013738 meter/sec RA = 352
33819 deg
ZDOT = 463
396490 TA = 183
50345
MA = 183
51633
Ha = 230
972 n
mi
Hp = 221
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -135144
51 X = 32152
29
Y = -13942074
87 feet Y = -4249595
26 meter
Z = -17440776
19 Z = -5315970
30
XDOT = 24947
346524 XDOT = 7608
426196
YDOT = -2139
152685 feet/sec YDOT = -566
955900 meter/sec
ZDOT = 1520
329690 ZDOT = 500
344090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5780820
01 X = -1761993
94
Y = -12688164
57 feet Y = -3867352
56 meter
Z = -17440555
89 Z = -5315881
44
XDOT = 20894
808309 XDOT = 6368
737573
YDOT = -11837
639920 feet/sec YDOT = -3608
112647 meter/sec
ZDOT = 1689
842778 ZDOT = 515
064079
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 20095
54868513
00016717 00000-0 10270-3 0 9092
2 25544 51
6449 352
8610 0003754 81
3647 278
7928 15
48667408 20592
Satellite: ISS
Catalog Number: 25544
Epoch time: 20095
54868513 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 352
8610 deg
Eccentricity:
0003754
Arg of perigee: 81
3647 deg
Mean anomaly: 278
7928 deg
Mean motion: 15
48667408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 348
Coasting Arc #11 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2020/096/03:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4403070
64 A = 6799907
85 meter
Y = 3730257
54 meter E =
0016071
Z = 3583728
42 I = 51
57419
XDOT = -5733
715195 Wp = 86
74891
YDOT = -2491
051135 meter/sec RA = 349
24479 deg
ZDOT = -4433
597373 TA = 50
92001
MA = 50
77716
Ha = 231
128 n
mi
Hp = 221
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14445769
82 X = -4461863
81
Y = 12238377
75 feet Y = 3680690
79 meter
Z = 11757639
17 Z = 3562197
14
XDOT = -18811
401560 XDOT = -5683
897672
YDOT = -8172
739945 feet/sec YDOT = -2554
891382 meter/sec
ZDOT = -14545
923139 ZDOT = -4461
328126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6066972
15 X = -1849213
11
Y = -17999135
48 feet Y = -5486136
50 meter
Z = 11658610
77 Z = 3553544
56
XDOT = 13147
784483 XDOT = 4007
444710
YDOT = -13974
643282 feet/sec YDOT = -4259
471272 meter/sec
ZDOT = -14672
920825 ZDOT = -4472
306267
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 20096
19398170
00016717 00000-0 10270-3 0 9103
2 25544 51
6427 349
6698 0003989 86
3821 273
7784 15
48674788 20692
Satellite: ISS
Catalog Number: 25544
Epoch time: 20096
19398170 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 349
6698 deg
Eccentricity:
0003989
Arg of perigee: 86
3821 deg
Mean anomaly: 273
7784 deg
Mean motion: 15
48674788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2069
Checksum: 369
Coasting Arc #12 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2020/097/03:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3944257
30 A = 6799675
97 meter
Y = -4146253
35 meter E =
0009354
Z = -3681253
35 I = 51
54125
XDOT = 6017
169028 Wp = 94
64729
YDOT = 1883
932063 meter/sec RA = 344
29569 deg
ZDOT = 4333
955868 TA = 221
65180
MA = 221
72307
Ha = 231
074 n
mi
Hp = 221
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12940476
71 X = 4008210
14
Y = -13603193
40 feet Y = -4101788
61 meter
Z = -12077602
86 Z = -3661938
07
XDOT = 19741
368201 XDOT = 5974
603343
YDOT = 6180
879472 feet/sec YDOT = 1950
982722 meter/sec
ZDOT = 14219
015314 ZDOT = 4363
081239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8180545
44 X = 2493430
25
Y = 16962327
72 feet Y = 5170117
49 meter
Z = -11988720
25 Z = -3654161
93
XDOT = -11434
090779 XDOT = -3485
110869
YDOT = 15637
944197 feet/sec YDOT = 4766
445391 meter/sec
ZDOT = 14352
444203 ZDOT = 4374
624993
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 20097
16192608
00016717 00000-0 10270-3 0 9110
2 25544 51
6434 344
8851 0003894 89
6199 270
5397 15
48652741 20844
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
16192608 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 344
8851 deg
Eccentricity:
0003894
Arg of perigee: 89
6199 deg
Mean anomaly: 270
5397 deg
Mean motion: 15
48652741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2084
Checksum: 338
Coasting Arc #13 (Orbit 2090)
---------------------------------------
Vector Time (GMT): 2020/097/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6598700
92 A = 6804637
81 meter
Y = 1076725
01 meter E =
0011355
Z = -1248264
72 I = 51
54439
XDOT = 286
259056 Wp = 127
48306
YDOT = -4955
098617 meter/sec RA = 342
20584 deg
ZDOT = -5830
690427 TA = 66
07106
MA = 65
95217
Ha = 230
901 n
mi
Hp = 222
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21649281
22 X = -6604187
40
Y = 3532562
37 feet Y = 1002902
84 meter
Z = -4095356
69 Z = -1280331
99
XDOT = 939
170130 XDOT = 369
969264
YDOT = -16256
885227 feet/sec YDOT = -4951
429972 meter/sec
ZDOT = -19129
561770 ZDOT = -5829
096104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12914989
67 X = -3936488
85
Y = 17695950
52 feet Y = 5393725
72 meter
Z = -4242487
20 Z = -1293110
10
XDOT = -9363
530160 XDOT = -2854
003993
YDOT = -11385
243608 feet/sec YDOT = -3470
222252 meter/sec
ZDOT = -19121
889536 ZDOT = -5828
351931
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 20097
61363271
00016717 00000-0 10270-3 0 9127
2 25544 51
6438 342
6522 0003498 89
5949 270
5601 15
48634627 20910
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
61363271 = yrday
fracday
Element set: 912
Inclination: 51
6438 deg
RA of node: 342
6522 deg
Eccentricity:
0003498
Arg of perigee: 89
5949 deg
Mean anomaly: 270
5601 deg
Mean motion: 15
48634627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2091
Checksum: 321
Coasting Arc #14 (Orbit 2106)
---------------------------------------
Vector Time (GMT): 2020/098/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6472739
36 A = 6804647
20 meter
Y = -1748557
62 meter E =
0016704
Z = 1119935
68 I = 51
51225
XDOT = 305
734500 Wp = 64
23967
YDOT = 4924
850374 meter/sec RA = 337
25096 deg
ZDOT = 5860
943119 TA = 307
91096
MA = 308
06186
Ha = 230
877 n
mi
Hp = 221
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21236021
51 X = 6486371
15
Y = -5736737
60 feet Y = -1676098
51 meter
Z = 3674329
67 Z = 1151411
12
XDOT = 1003
065945 XDOT = 222
171416
YDOT = 16157
645583 feet/sec YDOT = 4927
802664 meter/sec
ZDOT = 19228
816006 ZDOT = 5862
224816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10747062
69 X = 3275704
71
Y = -19164995
14 feet Y = -5841490
52 meter
Z = 3818778
79 Z = 1163963
78
XDOT = 10754
789064 XDOT = 3278
059707
YDOT = 9902
017115 feet/sec YDOT = 3018
134817 meter/sec
ZDOT = 19234
338441 ZDOT = 5862
626357
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 20098
64610188
00016717 00000-0 10270-3 0 9134
2 25544 51
6428 337
5468 0003566 92
4992 267
6566 15
48680018 21078
Satellite: ISS
Catalog Number: 25544
Epoch time: 20098
64610188 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 337
5468 deg
Eccentricity:
0003566
Arg of perigee: 92
4992 deg
Mean anomaly: 267
6566 deg
Mean motion: 15
48680018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2107
Checksum: 336
Coasting Arc #15 (Orbit 2121)
---------------------------------------
Vector Time (GMT): 2020/099/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6290382
41 A = 6804808
13 meter
Y = 2365691
65 meter E =
0012248
Z = -1042728
77 I = 51
48056
XDOT = -853
317618 Wp = 128
94490
YDOT = -4835
338201 meter/sec RA = 332
29540 deg
ZDOT = -5876
600008 TA = 62
35613
MA = 62
23185
Ha = 230
910 n
mi
Hp = 221
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20637737
56 X = -6311303
73
Y = 7761455
54 feet Y = 2295231
05 meter
Z = -3421026
15 Z = -1073336
29
XDOT = -2799
598483 XDOT = -770
638581
YDOT = -15863
970476 feet/sec YDOT = -4844
418819 meter/sec
ZDOT = -19280
183754 ZDOT = -5880
543904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8535319
53 X = -2601565
39
Y = 20305754
88 feet Y = 6189194
09 meter
Z = -3561525
38 Z = -1085552
94
XDOT = -11875
150141 XDOT = -3619
545763
YDOT = -8346
419325 feet/sec YDOT = -2543
988610 meter/sec
ZDOT = -19297
920603 ZDOT = -5882
006200
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 20099
61404299
00016717 00000-0 10270-3 0 9147
2 25544 51
6414 332
7616 0003591 95
5921 264
5638 15
48647697 21228
Satellite: ISS
Catalog Number: 25544
Epoch time: 20099
61404299 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 332
7616 deg
Eccentricity:
0003591
Arg of perigee: 95
5921 deg
Mean anomaly: 264
5638 deg
Mean motion: 15
48647697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2122
Checksum: 329
Coasting Arc #16 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1820946
12 A = 6797888
77 meter
Y = -5020450
65 meter E =
0011518
Z = -4217698
70 I = 51
43668
XDOT = 6693
092486 Wp = 105
17732
YDOT = -633
098138 meter/sec RA = 328
95879 deg
ZDOT = 3648
686420 TA = 202
38956
MA = 202
43988
Ha = 231
007 n
mi
Hp = 221
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5974232
67 X = 1897438
36
Y = -16471294
78 feet Y = -4999660
13 meter
Z = -13837594
15 Z = -4208667
02
XDOT = 21958
964850 XDOT = 6681
951089
YDOT = -2077
093627 feet/sec YDOT = -558
313260 meter/sec
ZDOT = 11970
755972 ZDOT = 3681
172208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17527208
94 X = 5342293
29
Y = 972637
62 feet Y = 296459
95 meter
Z = -13795830
61 Z = -4204969
17
XDOT = 8469
532091 XDOT = 2581
513381
YDOT = 19029
157818 feet/sec YDOT = 5800
087303 meter/sec
ZDOT = 12119
734899 ZDOT = 3694
095197
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 20100
25933742
00016717 00000-0 10270-3 0 9151
2 25544 51
6404 329
5714 0003726 96
9838 263
1736 15
48643895 21323
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
25933742 = yrday
fracday
Element set: 915
Inclination: 51
6404 deg
RA of node: 329
5714 deg
Eccentricity:
0003726
Arg of perigee: 96
9838 deg
Mean anomaly: 263
1736 deg
Mean motion: 15
48643895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 318
Coasting Arc #17 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3869179
65 A = 6794274
18 meter
Y = 2360876
27 meter E =
0008766
Z = 5055419
54 I = 51
42448
XDOT = -5471
027220 Wp = 113
76818
YDOT = 5048
389851 meter/sec RA = 328
56831 deg
ZDOT = 1823
694817 TA = 318
47915
MA = 318
54571
Ha = 230
753 n
mi
Hp = 221
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12694158
96 X = 3817935
43
Y = 7745657
07 feet Y = 2403858
00 meter
Z = 16586022
10 Z = 5074090
10
XDOT = -17949
564370 XDOT = -5535
931763
YDOT = 16562
958830 feet/sec YDOT = 4986
846148 meter/sec
ZDOT = 5983
250711 ZDOT = 1796
960414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4266934
64 X = 1300561
68
Y = 14145282
13 feet Y = 4311481
99 meter
Z = 16671450
64 Z = 5081458
15
XDOT = -23417
968718 XDOT = -7137
796865
YDOT = 134
144045 feet/sec YDOT = 40
887105 meter/sec
ZDOT = 5860
326306 ZDOT = 1786
227458
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 20100
38839500
00016717 00000-0 10270-3 0 9163
2 25544 51
6420 328
9341 0003608 98
8413 261
3145 15
48693770 21342
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
38839500 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 328
9341 deg
Eccentricity:
0003608
Arg of perigee: 98
8413 deg
Mean anomaly: 261
3145 deg
Mean motion: 15
48693770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 299
Coasting Arc #18 (Orbit 2137)
---------------------------------------
Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931488
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3906085
93 A = 6794457
50 meter
Y = 2289406
94 meter E =
0008758
Z = 5060159
42 I = 51
41515
XDOT = -5370
868168 Wp = 113
96407
YDOT = 5161
305210 meter/sec RA = 327
28614 deg
ZDOT = 1804
793909 TA = 318
47032
MA = 318
53683
Ha = 230
870 n
mi
Hp = 222
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12815242
54 X = 3855615
12
Y = 7511177
61 feet Y = 2332805
66 meter
Z = 16601572
91 Z = 5079011
18
XDOT = -17620
958558 XDOT = -5436
951002
YDOT = 16933
416042 feet/sec YDOT = 5100
874953 meter/sec
ZDOT = 5921
239859 ZDOT = 1778
543203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13777521
73 X = 4199388
62
Y = -5287388
93 feet Y = -1611596
15 meter
Z = 16687835
90 Z = 5086452
38
XDOT = 1913
330580 XDOT = 583
183161
YDOT = 23354
490042 feet/sec YDOT = 7118
448565 meter/sec
ZDOT = 5800
527528 ZDOT = 1768
000791
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 20100
64651300
00016717 00000-0 10270-3 0 9173
2 25544 51
6401 327
6559 0003634 99
4808 260
6753 15
48624055 21383
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
64651300 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 327
6559 deg
Eccentricity:
0003634
Arg of perigee: 99
4808 deg
Mean anomaly: 260
6753 deg
Mean motion: 15
48624055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2138
Checksum: 300
Coasting Arc #19 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931488
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4175919
84 A = 6794472
39 meter
Y = -1861758
00 meter E =
0016340
Z = -5040732
01 I = 51
38755
XDOT = 4807
240125 Wp = 81
68046
YDOT = -5633
797184 meter/sec RA = 322
32638 deg
ZDOT = -1904
691887 TA = 169
74814
MA = 169
71478
Ha = 230
923 n
mi
Hp = 221
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13700524
42 X = -4130305
45
Y = -6108129
92 feet Y = -1908201
20 meter
Z = -16537834
67 Z = -5060906
40
XDOT = 15771
785186 XDOT = 4879
133645
YDOT = -18483
586563 feet/sec YDOT = -5579
637277 meter/sec
ZDOT = -6248
989131 ZDOT = -1881
165131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13108398
42 X = -3995439
84
Y = 7079572
74 feet Y = 2157853
77 meter
Z = -16630187
51 Z = -5068881
15
XDOT = -4554
745552 XDOT = -1388
286444
YDOT = -22835
261024 feet/sec YDOT = -6960
187560 meter/sec
ZDOT = -6140
739016 ZDOT = -1871
697252
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 20101
61444970
00016717 00000-0 10270-3 0 9185
2 25544 51
6397 322
8691 0003671 104
0942 256
0616 15
48665346 21536
Satellite: ISS
Catalog Number: 25544
Epoch time: 20101
61444970 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 322
8691 deg
Eccentricity:
0003671
Arg of perigee: 104
0942 deg
Mean anomaly: 256
0616 deg
Mean motion: 15
48665346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 305
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