[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 30th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
306/13:59:44
828 0
0 0
0 0
0
N/A 0
0 0
0 227
0
000/00:00:00
000 0
0 0
0 222
0
308/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
308/09:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
2
311/22:40:58
115 1
0 1
3 1
3
N/A 0
6 -0
0 225
9
000/00:05:52
230 0
6 0
0 223
7
312/03:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
9
000/00:00:00
000 0
0 0
0 223
5
Coasting Arc #1 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2019/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4719838
52 A = 6790821
10 meter
Y = 510086
60 meter E =
0013262
Z = -4867263
46 I = 51
96483
XDOT = 1839
360723 Wp = 138
31541
YDOT = 6990
595420 meter/sec RA = 59
49341 deg
ZDOT = 2510
561326 TA = 156
33207
MA = 156
27101
Ha = 227
831 n
mi
Hp = 221
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15485034
51 X = 4737426
94
Y = 1673512
48 feet Y = 562965
35 meter
Z = -15968712
14 Z = -4844292
89
XDOT = 6034
648042 XDOT = 1748
857883
YDOT = 22935
024343 feet/sec YDOT = 7010
658504 meter/sec
ZDOT = 8236
749757 ZDOT = 2519
276446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13644728
80 X = -4158913
34
Y = 7729347
47 feet Y = 2355905
11 meter
Z = -15863961
32 Z = -4835335
41
XDOT = -17663
125083 XDOT = -5383
720525
YDOT = -14156
611311 feet/sec YDOT = -4314
935127 meter/sec
ZDOT = 8275
908157 ZDOT = 2522
496806
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 19301
51168225
00016717 00000-0 10270-3 0 9001
2 25544 51
6430 60
1970 0006754 198
9844 161
1056 15
50238400 35937
Satellite: ISS
Catalog Number: 25544
Epoch time: 19301
51168225 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 60
1970 deg
Eccentricity:
0006754
Arg of perigee: 198
9844 deg
Mean anomaly: 161
1056 deg
Mean motion: 15
50238400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 292
Coasting Arc #2 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2019/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4891114
70 A = 6791664
77 meter
Y = -565009
02 meter E =
0005706
Z = 4672456
54 I = 51
94945
XDOT = -2016
196301 Wp = 118
56200
YDOT = -6789
543741 meter/sec RA = 54
55797 deg
ZDOT = -2931
508283 TA =
49383
MA =
49327
Ha = 227
922 n
mi
Hp = 221
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16046964
22 X = -4907129
95
Y = -1853704
12 feet Y = -619794
43 meter
Z = 15329581
84 Z = 4648657
75
XDOT = -6614
817261 XDOT = -1925
883745
YDOT = -22275
405973 feet/sec YDOT = -6811
585323 meter/sec
ZDOT = -9617
809327 ZDOT = -2941
083089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14064741
29 X = 4286933
15
Y = -8151055
24 feet Y = -2484441
64 meter
Z = 15221061
39 Z = 4639379
51
XDOT = 17954
766629 XDOT = 5472
612868
YDOT = 12940
343338 feet/sec YDOT = 3944
216650 meter/sec
ZDOT = -9660
886175 ZDOT = -2944
638106
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 19302
54310737
00016717 00000-0 10270-3 0 9013
2 25544 51
6430 55
0859 0006740 201
9648 158
1215 15
50203702 36096
Satellite: ISS
Catalog Number: 25544
Epoch time: 19302
54310737 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 55
0859 deg
Eccentricity:
0006740
Arg of perigee: 201
9648 deg
Mean anomaly: 158
1215 deg
Mean motion: 15
50203702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3609
Checksum: 283
Coasting Arc #3 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2019/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5097167
88 A = 6792401
75 meter
Y = 603611
01 meter E =
0010675
Z = -4458723
19 I = 51
93301
XDOT = 2143
462735 Wp = 149
05576
YDOT = 6548
061062 meter/sec RA = 49
62228 deg
ZDOT = 3331
484868 TA = 154
53829
MA = 154
48566
Ha = 227
540 n
mi
Hp = 221
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16722991
73 X = 5111697
88
Y = 1980351
09 feet Y = 660692
46 meter
Z = -14628356
93 Z = -4433927
08
XDOT = 7032
358055 XDOT = 2053
898164
YDOT = 21483
139967 feet/sec YDOT = 6571
529929 meter/sec
ZDOT = 10930
068464 ZDOT = 3341
679864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14531470
17 X = -4429192
11
Y = 8701247
25 feet Y = 2652140
16 meter
Z = -14515293
32 Z = -4424261
40
XDOT = -17992
205660 XDOT = -5484
024285
YDOT = -11708
250749 feet/sec YDOT = -3568
674828 meter/sec
ZDOT = 10975
977480 ZDOT = 3345
477936
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 19303
51006382
00016717 00000-0 10270-3 0 9020
2 25544 51
6441 50
2949 0006739 206
9439 153
1362 15
50244524 36248
Satellite: ISS
Catalog Number: 25544
Epoch time: 19303
51006382 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 50
2949 deg
Eccentricity:
0006739
Arg of perigee: 206
9439 deg
Mean anomaly: 153
1362 deg
Mean motion: 15
50244524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 292
Coasting Arc #4 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2019/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5294282
73 A = 6793358
42 meter
Y = -599646
24 meter E =
0007404
Z = 4206451
20 I = 51
91378
XDOT = -2241
397630 Wp = 114
77451
YDOT = -6316
778686 meter/sec RA = 44
68499 deg
ZDOT = -3719
423289 TA = 13
29438
MA = 13
27488
Ha = 227
581 n
mi
Hp = 221
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17369694
00 X = -5307616
91
Y = -1967343
29 feet Y = -658925
34 meter
Z = 13800692
92 Z = 4180700
55
XDOT = -7353
666766 XDOT = -2152
527674
YDOT = -20724
339521 feet/sec YDOT = -6341
346547 meter/sec
ZDOT = -12202
832314 ZDOT = -3730
095776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14872530
82 X = 4533147
39
Y = -9360106
70 feet Y = -2852960
52 meter
Z = 13683276
79 Z = 4170662
77
XDOT = 17931
933169 XDOT = 5465
653230
YDOT = 10573
077754 feet/sec YDOT = 3222
674099 meter/sec
ZDOT = -12250
925337 ZDOT = -3734
082043
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 19304
54148262
00016717 00000-0 10270-3 0 9039
2 25544 51
6444 45
1836 0006590 209
8141 150
2635 15
50221938 36409
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
54148262 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 45
1836 deg
Eccentricity:
0006590
Arg of perigee: 209
8141 deg
Mean anomaly: 150
2635 deg
Mean motion: 15
50221938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 292
Coasting Arc #5 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2019/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5513687
89 A = 6794231
35 meter
Y = 569437
70 meter E =
0007515
Z = -3936724
52 I = 51
89221
XDOT = 2287
956355 Wp = 160
68422
YDOT = 6061
113821 meter/sec RA = 39
74740 deg
ZDOT = 4076
508307 TA = 151
93311
MA = 151
89257
Ha = 227
196 n
mi
Hp = 222
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18089527
20 X = 5526033
27
Y = 1868233
91 feet Y = 631164
83 meter
Z = -12915762
85 Z = -3909910
57
XDOT = 7506
418488 XDOT = 2200
207381
YDOT = 19885
544031 feet/sec YDOT = 6086
208566 meter/sec
ZDOT = 13374
371085 ZDOT = 4087
409666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15196257
21 X = -4631819
20
Y = 10145859
26 feet Y = 3092457
90 meter
Z = -12793495
57 Z = -3899457
45
XDOT = -17649
443772 XDOT = -5379
550462
YDOT = -9488
948746 feet/sec YDOT = -2892
231578 meter/sec
ZDOT = 13423
520098 ZDOT = 4091
488926
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 19305
50843338
00016717 00000-0 10270-3 0 9043
2 25544 51
6442 40
3926 0006559 214
9757 145
0963 15
50246505 36558
Satellite: ISS
Catalog Number: 25544
Epoch time: 19305
50843338 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 40
3926 deg
Eccentricity:
0006559
Arg of perigee: 214
9757 deg
Mean anomaly: 145
0963 deg
Mean motion: 15
50246505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 315
Coasting Arc #6 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2019/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5714281
60 A = 6795204
45 meter
Y = -500405
91 meter E =
0009159
Z = 3631957
33 I = 51
86854
XDOT = -2301
436733 Wp = 118
82198
YDOT = -5825
247914 meter/sec RA = 34
80840 deg
ZDOT = -4419
399236 TA = 18
32760
MA = 18
29462
Ha = 227
226 n
mi
Hp = 222
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18747643
06 X = -5725903
52
Y = -1641751
67 feet Y = -564372
15 meter
Z = 11915870
51 Z = 3604170
82
XDOT = -7550
645450 XDOT = -2214
658755
YDOT = -19111
705755 feet/sec YDOT = -5850
498837 meter/sec
ZDOT = -14499
341325 ZDOT = -4430
368366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15366892
47 X = 4683828
83
Y = -11001440
43 feet Y = -3353239
04 meter
Z = 11789162
95 Z = 3593336
87
XDOT = 17291
081224 XDOT = 5270
321557
YDOT = 8547
122072 feet/sec YDOT = 2605
162808 meter/sec
ZDOT = -14548
812795 ZDOT = -4434
478140
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 19306
53984715
00016717 00000-0 10270-3 0 9053
2 25544 51
6438 35
2817 0006503 217
9030 142
1664 15
50239076 36710
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
53984715 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 35
2817 deg
Eccentricity:
0006503
Arg of perigee: 217
9030 deg
Mean anomaly: 142
1664 deg
Mean motion: 15
50239076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 307
Coasting Arc #7 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2019/306/13:59:44
828
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -576500
87 A = 6791348
02 meter
Y = -4872269
08 meter E =
0006237
Z = -4700440
91 I = 51
85230
XDOT = 6827
150215 Wp = 103
08986
YDOT = 1952
767428 meter/sec RA = 34
44490 deg
ZDOT = -2866
066099 TA = 138
51391
MA = 138
46655
Ha = 227
047 n
mi
Hp = 222
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1891407
06 X = -499142
42
Y = -15985134
78 feet Y = -4878283
22 meter
Z = -15421394
07 Z = -4703053
66
XDOT = 22398
786794 XDOT = 6818
728360
YDOT = 6406
717284 feet/sec YDOT = 2029
066453 meter/sec
ZDOT = -9403
104000 ZDOT = -2832
922246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15672069
63 X = 4776846
82
Y = 3624237
55 feet Y = 1104667
60 meter
Z = -15432837
90 Z = -4703928
99
XDOT = -13239
170623 XDOT = -4035
299206
YDOT = 17915
648498 feet/sec YDOT = 5460
689662 meter/sec
ZDOT = -9252
099212 ZDOT = -2820
039840
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 19306
60431011
00016717 00000-0 10270-3 0 9068
2 25544 51
6425 34
9632 0006447 219
1409 140
9276 15
50232024 36720
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
60431011 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 34
9632 deg
Eccentricity:
0006447
Arg of perigee: 219
1409 deg
Mean anomaly: 140
9276 deg
Mean motion: 15
50232024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 282
Coasting Arc #8 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2019/307/13:59:44
828
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 512604
51 A = 6790541
65 meter
Y = 4697419
88 meter E =
0008264
Z = 4878513
38 I = 51
82207
XDOT = -7039
699654 Wp = 168
92780
YDOT = -1776
841917 meter/sec RA = 29
50080 deg
ZDOT = 2441
981526 TA = 257
10126
MA = 257
19358
Ha = 226
774 n
mi
Hp = 222
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1681773
34 X = 436341
10
Y = 15411482
53 feet Y = 4702725
64 meter
Z = 16005621
32 Z = 4880818
34
XDOT = -23096
127474 XDOT = -7031
169223
YDOT = -5829
533850 feet/sec YDOT = -1855
517176 meter/sec
ZDOT = 8011
750415 ZDOT = 2407
805550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15120379
33 X = -4608691
62
Y = -3375561
04 feet Y = -1028871
00 meter
Z = 16015673
12 Z = 4881577
17
XDOT = 12597
241584 XDOT = 3839
639235
YDOT = -19020
347986 feet/sec YDOT = -5797
402066 meter/sec
ZDOT = 7856
026880 ZDOT = 2394
516993
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 19307
63571845
00016717 00000-0 10270-3 0 9073
2 25544 51
6429 29
8515 0006373 223
9232 136
1413 15
50260854 36881
Satellite: ISS
Catalog Number: 25544
Epoch time: 19307
63571845 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 29
8515 deg
Eccentricity:
0006373
Arg of perigee: 223
9232 deg
Mean anomaly: 136
1413 deg
Mean motion: 15
50260854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 318
Coasting Arc #9 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1158259
04 A = 6791027
81 meter
Y = 4719323
67 meter E =
0008391
Z = 4745444
77 I = 51
80125
XDOT = -7072
694935 Wp = 163
79894
YDOT = -1040
111129 meter/sec RA = 25
99675 deg
ZDOT = 2751
645176 TA = 258
95384
MA = 259
04822
Ha = 226
695 n
mi
Hp = 222
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3800062
46 X = 1082349
11
Y = 15483345
36 feet Y = 4731851
61 meter
Z = 15569044
53 Z = 4750886
93
XDOT = -23204
379708 XDOT = -7073
904569
YDOT = -3412
438088 feet/sec YDOT = -1119
209809 meter/sec
ZDOT = 9027
707269 ZDOT = 2717
285324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5243670
82 X = 1598270
86
Y = -15030613
51 feet Y = -4581331
00 meter
Z = 15593401
80 Z = 4752868
87
XDOT = 16650
887263 XDOT = 5075
190438
YDOT = 15042
854104 feet/sec YDOT = 4585
061931 meter/sec
ZDOT = 8871
077857 ZDOT = 2703
904531
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 19308
34481070
00016717 00000-0 10270-3 0 9083
2 25544 51
6413 26
3338 0006391 225
2984 134
7647 15
50273826 36996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
34481070 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 26
3338 deg
Eccentricity:
0006391
Arg of perigee: 225
2984 deg
Mean anomaly: 134
7647 deg
Mean motion: 15
50273826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 323
Coasting Arc #10 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4634572
13 A = 6798033
25 meter
Y = -4332078
10 meter E =
0008190
Z = -2428590
67 I = 51
82412
XDOT = 4961
844002 Wp = 182
87057
YDOT = -2304
157942 meter/sec RA = 25
55094 deg
ZDOT = -5365
944511 TA = 24
18068
MA = 24
14226
Ha = 226
709 n
mi
Hp = 222
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15205289
14 X = -4573988
24
Y = -14212854
64 feet Y = -4383566
37 meter
Z = -7967817
17 Z = -2450956
87
XDOT = 16279
015753 XDOT = 5013
306064
YDOT = -7559
573299 feet/sec YDOT = -2248
383268 meter/sec
ZDOT = -17604
804825 ZDOT = -5341
716502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15135225
25 X = 4613216
66
Y = 14230310
22 feet Y = 4337398
55 meter
Z = -8069410
94 Z = -2459556
46
XDOT = -15368
248595 XDOT = -4684
242172
YDOT = 6438
579093 feet/sec YDOT = 1962
478907 meter/sec
ZDOT = -17494
061031 ZDOT = -5332
189802
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 19308
40927396
00016717 00000-0 10270-3 0 9097
2 25544 51
6436 26
0148 0006423 224
7883 135
2750 15
50263229 37005
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
40927396 = yrday
fracday
Element set: 909
Inclination: 51
6436 deg
RA of node: 26
0148 deg
Eccentricity:
0006423
Arg of perigee: 224
7883 deg
Mean anomaly: 135
2750 deg
Mean motion: 15
50263229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 306
Coasting Arc #11 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4648137
00 A = 6797161
18 meter
Y = 4095857
65 meter E =
0008635
Z = 2791913
41 I = 51
79099
XDOT = -5174
723188 Wp = 103
01321
YDOT = 2366
655034 meter/sec RA = 20
60820 deg
ZDOT = 5127
928397 TA = 288
51259
MA = 288
60640
Ha = 226
573 n
mi
Hp = 222
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15249793
30 X = 4588428
75
Y = 13437853
17 feet Y = 4147502
54 meter
Z = 9159820
89 Z = 2814347
57
XDOT = -16977
438281 XDOT = -5225
712128
YDOT = 7764
616254 feet/sec YDOT = 2308
502508 meter/sec
ZDOT = 16823
912064 ZDOT = 5102
667410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15401754
51 X = -4694454
78
Y = -13192442
54 feet Y = -4021056
49 meter
Z = 9261740
12 Z = 2822978
39
XDOT = 16001
520479 XDOT = 4877
263442
YDOT = -6916
345035 feet/sec YDOT = -2108
101967 meter/sec
ZDOT = 16708
455796 ZDOT = 5092
737327
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 19309
44067621
00016717 00000-0 10270-3 0 9100
2 25544 51
6438 20
9037 0006411 228
2373 131
8230 15
50286397 37160
Satellite: ISS
Catalog Number: 25544
Epoch time: 19309
44067621 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 20
9037 deg
Eccentricity:
0006411
Arg of perigee: 228
2373 deg
Mean anomaly: 131
8230 deg
Mean motion: 15
50286397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 294
Coasting Arc #12 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4602388
01 A = 6796299
29 meter
Y = -3873947
34 meter E =
0004868
Z = -3156126
32 I = 51
75630
XDOT = 5394
920497 Wp = 186
69498
YDOT = -2459
278784 meter/sec RA = 15
66321 deg
ZDOT = -4852
435338 TA = 29
57130
MA = 29
54378
Ha = 226
387 n
mi
Hp = 222
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15099698
18 X = -4543395
43
Y = -12709800
97 feet Y = -3925084
66 meter
Z = -10354745
14 Z = -3178339
97
XDOT = 17699
870397 XDOT = 5445
590644
YDOT = -8068
499949 feet/sec YDOT = -2398
665697 meter/sec
ZDOT = -15920
063445 ZDOT = -4826
105410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15444105
56 X = 4707363
37
Y = 12203245
39 feet Y = 3719549
20 meter
Z = -10455672
06 Z = -3186888
84
XDOT = -16638
664544 XDOT = -5071
464953
YDOT = 7531
358897 feet/sec YDOT = 2295
558192 meter/sec
ZDOT = -15799
730230 ZDOT = -4815
757774
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 19310
40761586
00016717 00000-0 10270-3 0 9110
2 25544 51
6438 16
1125 0006429 232
1818 127
8751 15
50263487 37317
Satellite: ISS
Catalog Number: 25544
Epoch time: 19310
40761586 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 16
1125 deg
Eccentricity:
0006429
Arg of perigee: 232
1818 deg
Mean anomaly: 127
8751 deg
Mean motion: 15
50263487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 301
Coasting Arc #13 (Orbit 3746)
---------------------------------------
Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4542867
64 A = 6795276
22 meter
Y = 3658132
20 meter E =
0007921
Z = 3484493
11 I = 51
72162
XDOT = -5589
129634 Wp = 119
39523
YDOT = 2596
316549 meter/sec RA = 10
71466 deg
ZDOT = 4549
472027 TA = 281
39710
MA = 281
48606
Ha = 226
202 n
mi
Hp = 222
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14904421
38 X = 4484697
71
Y = 12001746
07 feet Y = 3708608
57 meter
Z = 11432064
00 Z = 3506419
65
XDOT = -18337
039483 XDOT = -5639
846154
YDOT = 8518
098913 feet/sec YDOT = 2533
531457 meter/sec
ZDOT = 14926
089328 ZDOT = 4522
198485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15413715
82 X = -4698100
58
Y = -11238913
57 feet Y = -3425620
86 meter
Z = 11531693
67 Z = 3514860
23
XDOT = 17164
427380 XDOT = 5231
717465
YDOT = -8314
588459 feet/sec YDOT = -2534
286562 meter/sec
ZDOT = 14801
448501 ZDOT = 4511
481503
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 19311
43901238
00016717 00000-0 10270-3 0 9125
2 25544 51
6447 11
0011 0006403 236
2504 123
8037 15
50298392 37477
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
43901238 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 11
0011 deg
Eccentricity:
0006403
Arg of perigee: 236
2504 deg
Mean anomaly: 123
8037 deg
Mean motion: 15
50298392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3747
Checksum: 276
Coasting Arc #14 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/311/22:43:54
230
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5344444
14 A = 6795842
35 meter
Y = -2141012
05 meter E =
0002893
Z = -3612342
51 I = 51
70250
XDOT = 4660
383104 Wp = 199
31778
YDOT = 4168
356217 meter/sec RA = 7
86956 deg
ZDOT = 4420
779291 TA = 118
05593
MA = 118
02668
Ha = 225
910 n
mi
Hp = 223
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17534265
57 X = 5385535
41
Y = -7024317
74 feet Y = -2081017
02 meter
Z = -11851517
42 Z = -3586280
91
XDOT = 15289
970814 XDOT = 4591
950901
YDOT = 13675
709372 feet/sec YDOT = 4220
089374 meter/sec
ZDOT = 14503
869066 ZDOT = 4443
251779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12523261
27 X = 3817090
04
Y = -14239641
79 feet Y = -4340242
82 meter
Z = -11732455
10 Z = -3576052
32
XDOT = 18699
707679 XDOT = 5699
670901
YDOT = 4401
435540 feet/sec YDOT = 1341
557553 meter/sec
ZDOT = 14605
931512 ZDOT = 4451
887925
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 19311
95471110
00016717 00000-0 10270-3 0 9134
2 25544 51
6451 8
4494 0006565 251
0987 108
9453 15
50042014 37559
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
95471110 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 8
4494 deg
Eccentricity:
0006565
Arg of perigee: 251
0987 deg
Mean anomaly: 108
9453 deg
Mean motion: 15
50042014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 297
Coasting Arc #15 (Orbit 3757)
---------------------------------------
Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1842350
57 A = 6790655
76 meter
Y = -4211593
01 meter E =
0006148
Z = -5003724
43 I = 51
67517
XDOT = 7333
246798 Wp = 78
79163
YDOT = -747
948261 meter/sec RA = 7
01099 deg
ZDOT = -2071
525349 TA = 171
04057
MA = 171
02960
Ha = 225
911 n
mi
Hp = 223
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6044457
25 X = -1770812
63
Y = -13817562
37 feet Y = -4231795
59 meter
Z = -16416418
75 Z = -5012500
20
XDOT = 24059
208654 XDOT = 7351
128048
YDOT = -2453
898495 feet/sec YDOT = -665
842778 meter/sec
ZDOT = -6796
343010 ZDOT = -2035
859103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13560413
58 X = -4133214
06
Y = 6501848
60 feet Y = 1981763
45 meter
Z = -16456015
50 Z = -5015793
53
XDOT = -2978
388545 XDOT = -907
812828
YDOT = -22993
081976 feet/sec YDOT = -7008
291386 meter/sec
ZDOT = -6633
623283 ZDOT = -2021
928377
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 19312
14812674
00016717 00000-0 10270-3 0 9141
2 25544 51
6410 7
4885 0006606 251
1617 108
8817 15
50033027 37584
Satellite: ISS
Catalog Number: 25544
Epoch time: 19312
14812674 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 7
4885 deg
Eccentricity:
0006606
Arg of perigee: 251
1617 deg
Mean anomaly: 108
8817 deg
Mean motion: 15
50033027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3758
Checksum: 299
Coasting Arc #16 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1774301
49 A = 6790325
41 meter
Y = 4109802
48 meter E =
0005071
Z = 5108898
33 I = 51
63985
XDOT = -7390
812000 Wp = 205
02045
YDOT = 1077
738083 meter/sec RA = 2
05661 deg
ZDOT = 1695
953784 TA = 228
55481
MA = 228
59838
Ha = 225
715 n
mi
Hp = 223
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5821199
13 X = 1703395
89
Y = 13483603
93 feet Y = 4129247
62 meter
Z = 16761477
45 Z = 5117345
10
XDOT = -24248
070865 XDOT = -7410
552456
YDOT = 3535
886098 feet/sec YDOT = 994
978460 meter/sec
ZDOT = 5564
152835 ZDOT = 1660
003250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13126442
38 X = 4000939
64
Y = -6489353
24 feet Y = -1977954
87 meter
Z = 16799579
33 Z = 5120511
78
XDOT = 4481
953083 XDOT = 1366
099300
YDOT = 23078
534225 feet/sec YDOT = 7034
337232 meter/sec
ZDOT = 5400
118727 ZDOT = 1645
956188
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 19313
17968285
00016717 00000-0 10270-3 0 9156
2 25544 51
6405 2
3780 0006545 255
2519 104
7906 15
49990827 37744
Satellite: ISS
Catalog Number: 25544
Epoch time: 19313
17968285 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 2
3780 deg
Eccentricity:
0006545
Arg of perigee: 255
2519 deg
Mean anomaly: 104
7906 deg
Mean motion: 15
49990827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 334
Coasting Arc #17 (Orbit 3788)
---------------------------------------
Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1684971
87 A = 6789810
95 meter
Y = -4039027
34 meter E =
0007517
Z = -5197856
39 I = 51
60443
XDOT = 7410
749829 Wp = 82
65250
YDOT = -1411
754961 meter/sec RA = 357
09950 deg
ZDOT = -1305
989997 TA = 174
78058
MA = 174
77274
Ha = 225
552 n
mi
Hp = 223
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5528122
95 X = -1614432
13
Y = -13251402
04 feet Y = -4057475
53 meter
Z = -17053334
63 Z = -5205870
18
XDOT = 24313
483692 XDOT = 7432
329631
YDOT = -4631
741997 feet/sec YDOT = -1328
762076 meter/sec
ZDOT = -4284
744086 ZDOT = -1269
938020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12803737
71 X = -3902579
25
Y = 6402384
39 feet Y = 1951446
76 meter
Z = -17089464
47 Z = -5208868
77
XDOT = -5997
937313 XDOT = -1828
171293
YDOT = -22986
778747 feet/sec YDOT = -7006
370162 meter/sec
ZDOT = -4120
228599 ZDOT = -1255
845677
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 19314
14676307
00016717 00000-0 10270-3 0 9166
2 25544 51
6398 357
5869 0006524 257
3010 102
7411 15
50038156 37899
Satellite: ISS
Catalog Number: 25544
Epoch time: 19314
14676307 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 357
5869 deg
Eccentricity:
0006524
Arg of perigee: 257
3010 deg
Mean anomaly: 102
7411 deg
Mean motion: 15
50038156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3789
Checksum: 319
Coasting Arc #18 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1596724
11 A = 6789655
85 meter
Y = 3991525
82 meter E =
0004416
Z = 5258664
03 I = 51
57038
XDOT = -7399
445589 Wp = 233
14363
YDOT = 1753
448429 meter/sec RA = 352
13941 deg
ZDOT = 913
752655 TA = 208
08452
MA = 208
10836
Ha = 225
308 n
mi
Hp = 223
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5238596
18 X = 1526426
66
Y = 13095557
16 feet Y = 4008988
43 meter
Z = 17252834
73 Z = 5266249
81
XDOT = -24276
396291 XDOT = -7422
941840
YDOT = 5752
783561 feet/sec YDOT = 1670
571222 meter/sec
ZDOT = 2997
876165 ZDOT = 877
750858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12563604
95 X = 3829386
79
Y = -6317579
78 feet Y = -1925598
32 meter
Z = 17287013
33 Z = 5269081
66
XDOT = 7526
479960 XDOT = 2294
071092
YDOT = 22739
740589 feet/sec YDOT = 6931
072932 meter/sec
ZDOT = 2833
568454 ZDOT = 863
671665
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 19315
17831500
00016717 00000-0 10270-3 0 9179
2 25544 51
6400 352
4757 0006526 261
8932 98
1478 15
49996866 38057
Satellite: ISS
Catalog Number: 25544
Epoch time: 19315
17831500 = yrday
fracday
Element set: 917
Inclination: 51
6400 deg
RA of node: 352
4757 deg
Eccentricity:
0006526
Arg of perigee: 261
8932 deg
Mean anomaly: 98
1478 deg
Mean motion: 15
49996866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 340
Coasting Arc #19 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 934263
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1500312
50 A = 6789320
65 meter
Y = -3977278
93 meter E =
0008356
Z = -5301150
13 I = 51
53750
XDOT = 7347
364020 Wp = 87
34693
YDOT = -2089
504033 meter/sec RA = 347
17734 deg
ZDOT = -512
059827 TA = 177
75480
MA = 177
75105
Ha = 225
188 n
mi
Hp = 223
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4922285
11 X = -1429975
10
Y = -13048815
38 feet Y = -3993663
06 meter
Z = -17392224
84 Z = -5308267
57
XDOT = 24105
525000 XDOT = 7372
670762
YDOT = -6855
328192 feet/sec YDOT = -2007
199107 meter/sec
ZDOT = -1679
986309 ZDOT = -476
306619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12441557
68 X = -3792186
78
Y = 6212291
42 feet Y = 1893506
43 meter
Z = -17424265
73 Z = -5310916
19
XDOT = -9015
860540 XDOT = -2748
034293
YDOT = -22307
701597 feet/sec YDOT = -6799
387447 meter/sec
ZDOT = -1516
789261 ZDOT = -462
317367
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 19316
14538979
00016717 00000-0 10270-3 0 9182
2 25544 51
6406 347
6846 0006382 264
6259 95
4164 15
50051620 38202
Satellite: ISS
Catalog Number: 25544
Epoch time: 19316
14538979 = yrday
fracday
Element set: 918
Inclination: 51
6406 deg
RA of node: 347
6846 deg
Eccentricity:
0006382
Arg of perigee: 264
6259 deg
Mean anomaly: 95
4164 deg
Mean motion: 15
50051620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 328
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