[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 15th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15140 5164 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 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
346/03:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 219
4
349/11:36:38
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 219
1
355/13:08:55
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
5
356/04:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
4
359/09:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
Coasting Arc #1 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2019/345/11:24:50
319
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6399283
94 A = 6798920
68 meter
Y = -602810
93 meter E =
0013218
Z = -2200498
82 I = 51
51020
XDOT = -1380
382922 Wp = 31
27778
YDOT = -5193
050920 meter/sec RA = 201
17770 deg
ZDOT = 5462
719944 TA = 304
27792
MA = 304
40301
Ha = 229
240 n
mi
Hp = 219
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20995026
05 X = -6381378
58
Y = -1977726
16 feet Y = -674271
82 meter
Z = -7219484
33 Z = -2231541
17
XDOT = -4528
815362 XDOT = -1348
745339
YDOT = -17037
568635 feet/sec YDOT = -5208
311217 meter/sec
ZDOT = 17922
309527 ZDOT = 5456
090572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8954552
79 X = 2729347
69
Y = -19038202
55 feet Y = -5802844
14 meter
Z = -7361134
52 Z = -2243673
80
XDOT = 16216
206503 XDOT = 4942
699742
YDOT = 741
273929 feet/sec YDOT = 225
940294 meter/sec
ZDOT = 17892
343173 ZDOT = 5453
586199
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 19345
48004270
00016717 00000-0 10270-3 0 9004
2 25544 51
6415 202
3564 0007472 20
6419 339
5032 15
50105232 2751
Satellite: ISS
Catalog Number: 25544
Epoch time: 19345
48004270 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 202
3564 deg
Eccentricity:
0007472
Arg of perigee: 20
6419 deg
Mean anomaly: 339
5032 deg
Mean motion: 15
50105232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 275
Checksum: 269
Coasting Arc #2 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2019/346/03:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1641370
35 A = 6791396
06 meter
Y = -4526873
26 meter E =
0010303
Z = 4779377
42 I = 51
50241
XDOT = 7208
116440 Wp = 72
73258
YDOT = 147
996477 meter/sec RA = 197
93686 deg
ZDOT = 2613
976319 TA = 351
44008
MA = 351
45764
Ha = 229
409 n
mi
Hp = 219
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5385073
33 X = -1613843
36
Y = -14851946
41 feet Y = -4545075
04 meter
Z = 15680372
10 Z = 4771470
33
XDOT = 23648
675984 XDOT = 7193
228391
YDOT = 485
552747 feet/sec YDOT = 228
519085 meter/sec
ZDOT = 8576
037791 ZDOT = 2648
954909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8169567
64 X = -2490084
22
Y = 13563192
39 feet Y = 4134061
04 meter
Z = 15644531
72 Z = 4768453
27
XDOT = -13363
771133 XDOT = -4073
277441
YDOT = -18132
008758 feet/sec YDOT = -5526
636269 meter/sec
ZDOT = 8735
697525 ZDOT = 2662
640605
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 19346
18919882
00016717 00000-0 10270-3 0 9017
2 25544 51
6382 198
8411 0007407 25
3533 334
7979 15
50116406 2865
Satellite: ISS
Catalog Number: 25544
Epoch time: 19346
18919882 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 198
8411 deg
Eccentricity:
0007407
Arg of perigee: 25
3533 deg
Mean anomaly: 334
7979 deg
Mean motion: 15
50116406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 286
Checksum: 326
Coasting Arc #3 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2019/347/03:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1571307
75 A = 6790802
06 meter
Y = 4396333
37 meter E =
0018312
Z = -4948152
08 I = 51
53198
XDOT = -7319
066685 Wp = 57
35471
YDOT = 119
505889 meter/sec RA = 192
97175 deg
ZDOT = -2214
369270 TA = 190
92112
MA = 190
96093
Ha = 229
518 n
mi
Hp = 219
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5155209
15 X = 1546065
41
Y = 14423665
91 feet Y = 4413764
50 meter
Z = -16234094
74 Z = -4940579
81
XDOT = -24012
685976 XDOT = -7309
102822
YDOT = 392
079688 feet/sec YDOT = 37
714983 meter/sec
ZDOT = -7264
991043 ZDOT = -2249
898571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7749409
31 X = 2362019
96
Y = -13254370
80 feet Y = -4039932
22 meter
Z = -16199767
33 Z = -4937689
08
XDOT = 14620
116096 XDOT = 4456
211386
YDOT = 17640
291386 feet/sec YDOT = 5376
760814 meter/sec
ZDOT = -7427
209154 ZDOT = -2263
813350
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 19347
15622863
00016717 00000-0 10270-3 0 9026
2 25544 51
6376 194
0491 0007510 29
3424 330
8147 15
50106213 3019
Satellite: ISS
Catalog Number: 25544
Epoch time: 19347
15622863 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 194
0491 deg
Eccentricity:
0007510
Arg of perigee: 29
3424 deg
Mean anomaly: 330
8147 deg
Mean motion: 15
50106213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 279
Coasting Arc #4 (Orbit 316)
---------------------------------------
Vector Time (GMT): 2019/348/03:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1466564
31 A = 6790183
02 meter
Y = -4266788
95 meter E =
0009098
Z = 5066213
47 I = 51
56256
XDOT = 7440
388659 Wp = 69
80222
YDOT = -405
770630 meter/sec RA = 188
00938 deg
ZDOT = 1812
526679 TA = 2
63772
MA = 2
63293
Ha = 229
547 n
mi
Hp = 219
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4811562
70 X = -1443351
71
Y = -13998651
42 feet Y = -4283060
13 meter
Z = 16621435
28 Z = 5059145
14
XDOT = 24410
723946 XDOT = 7435
568863
YDOT = -1331
268470 feet/sec YDOT = -322
594188 meter/sec
ZDOT = 5946
609839 ZDOT = 1848
657576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7419639
61 X = -2261506
15
Y = 12850154
77 feet Y = 3916727
18 meter
Z = 16589392
94 Z = 5056446
97
XDOT = -15938
335166 XDOT = -4858
004558
YDOT = -17090
951018 feet/sec YDOT = -5209
321870 meter/sec
ZDOT = 6111
621333 ZDOT = 1862
822182
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 19348
18772651
00016717 00000-0 10270-3 0 9032
2 25544 51
6372 188
9384 0007460 31
9076 328
2525 15
50121158 3177
Satellite: ISS
Catalog Number: 25544
Epoch time: 19348
18772651 = yrday
fracday
Element set: 903
Inclination: 51
6372 deg
RA of node: 188
9384 deg
Eccentricity:
0007460
Arg of perigee: 31
9076 deg
Mean anomaly: 328
2525 deg
Mean motion: 15
50121158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 317
Checksum: 313
Coasting Arc #5 (Orbit 331)
---------------------------------------
Vector Time (GMT): 2019/349/03:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1365885
39 A = 6789787
22 meter
Y = 4188106
91 meter E =
0019868
Z = -5184077
05 I = 51
59518
XDOT = -7485
243238 Wp = 64
48786
YDOT = 709
035394 meter/sec RA = 183
04786 deg
ZDOT = -1395
213168 TA = 192
02504
MA = 192
07254
Ha = 229
620 n
mi
Hp = 219
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4481251
29 X = 1344132
52
Y = 13740508
22 feet Y = 4203260
35 meter
Z = -17008126
81 Z = -5177494
32
XDOT = -24557
884640 XDOT = -7485
838417
YDOT = 2326
231606 feet/sec YDOT = 625
326998 meter/sec
ZDOT = -4577
471025 ZDOT = -1431
574885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7222028
28 X = 2201274
22
Y = -12559441
46 feet Y = -3828117
76 meter
Z = -16978288
92 Z = -5174982
46
XDOT = 17108
239555 XDOT = 5214
591416
YDOT = 16268
745917 feet/sec YDOT = 4958
713755 meter/sec
ZDOT = -4743
583557 ZDOT = -1445
844268
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 19349
15475490
00016717 00000-0 10270-3 0 9042
2 25544 51
6380 184
1461 0007489 35
7278 324
4373 15
50109295 3321
Satellite: ISS
Catalog Number: 25544
Epoch time: 19349
15475490 = yrday
fracday
Element set: 904
Inclination: 51
6380 deg
RA of node: 184
1461 deg
Eccentricity:
0007489
Arg of perigee: 35
7278 deg
Mean anomaly: 324
4373 deg
Mean motion: 15
50109295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 332
Checksum: 317
Coasting Arc #6 (Orbit 337)
---------------------------------------
Vector Time (GMT): 2019/349/11:36:38
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5295817
84 A = 6796557
36 meter
Y = -2709512
92 meter E =
0018175
Z = 3265254
23 I = 51
63075
XDOT = 4799
397472 Wp = 68
68417
YDOT = -3645
183114 meter/sec RA = 181
33755 deg
ZDOT = 4744
398089 TA = 329
17538
MA = 329
28197
Ha = 229
588 n
mi
Hp = 219
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17374730
45 X = -5280986
39
Y = -8889478
09 feet Y = -2768652
04 meter
Z = 10712776
36 Z = 3239564
89
XDOT = 15746
054699 XDOT = 4816
756743
YDOT = -11959
262186 feet/sec YDOT = -3591
416485 meter/sec
ZDOT = 15565
610529 ZDOT = 4767
753283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12558263
83 X = 3827758
82
Y = -15023023
88 feet Y = -4579017
68 meter
Z = 10595584
91 Z = 3229534
28
XDOT = 7070
690956 XDOT = 2155
146603
YDOT = 16998
953516 feet/sec YDOT = 5181
281032 meter/sec
ZDOT = 15672
483503 ZDOT = 4776
972972
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 19349
54156356
00016717 00000-0 10270-3 0 9053
2 25544 51
6391 182
2292 0007334 34
6572 325
5055 15
50135080 3384
Satellite: ISS
Catalog Number: 25544
Epoch time: 19349
54156356 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 182
2292 deg
Eccentricity:
0007334
Arg of perigee: 34
6572 deg
Mean anomaly: 325
5055 deg
Mean motion: 15
50135080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 338
Checksum: 301
Coasting Arc #7 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2019/350/11:36:38
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5213253
00 A = 6795684
90 meter
Y = 2507721
74 meter E =
0011744
Z = -3580369
13 I = 51
66039
XDOT = -4898
733104 Wp = 58
00785
YDOT = 3836
459437 meter/sec RA = 176
38285 deg
ZDOT = -4450
460625 TA = 164
13323
MA = 164
09641
Ha = 229
664 n
mi
Hp = 219
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17103848
44 X = 5202214
78
Y = 8227433
53 feet Y = 2565958
74 meter
Z = -11746617
89 Z = -3555071
80
XDOT = -16071
959001 XDOT = -4919
651735
YDOT = 12586
809177 feet/sec YDOT = 3781
561927 meter/sec
ZDOT = -14601
248769 ZDOT = -4474
306986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11595678
94 X = -3534362
94
Y = 15115260
76 feet Y = 4607131
48 meter
Z = -11631184
29 Z = -3545184
97
XDOT = -7916
413385 XDOT = -2412
922800
YDOT = -17380
803724 feet/sec YDOT = -5297
668975 meter/sec
ZDOT = -14710
390893 ZDOT = -4483
727144
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 19350
50858993
00016717 00000-0 10270-3 0 9068
2 25544 51
6382 177
4369 0007538 39
2886 320
8810 15
50130234 3530
Satellite: ISS
Catalog Number: 25544
Epoch time: 19350
50858993 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 177
4369 deg
Eccentricity:
0007538
Arg of perigee: 39
2886 deg
Mean anomaly: 320
8810 deg
Mean motion: 15
50130234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 322
Coasting Arc #8 (Orbit 368)
---------------------------------------
Vector Time (GMT): 2019/351/11:36:38
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5100785
15 A = 6794846
03 meter
Y = -2298305
05 meter E =
0016798
Z = 3838790
78 I = 51
69063
XDOT = 4982
703185 Wp = 76
79966
YDOT = -4079
717037 meter/sec RA = 171
43044 deg
ZDOT = 4166
610988 TA = 329
33993
MA = 329
43798
Ha = 229
745 n
mi
Hp = 218
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16734859
42 X = -5093352
30
Y = -7540370
88 feet Y = -2355304
45 meter
Z = 12594457
96 Z = 3814031
10
XDOT = 16347
451394 XDOT = 5007
714530
YDOT = -13384
898416 feet/sec YDOT = -4023
857492 meter/sec
ZDOT = 13669
983556 ZDOT = 4190
875245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10590461
65 X = 3227972
71
Y = -15086039
93 feet Y = -4598224
97 meter
Z = 12481450
45 Z = 3804346
10
XDOT = 8961
014489 XDOT = 2731
317216
YDOT = 17724
206781 feet/sec YDOT = 5402
338227 meter/sec
ZDOT = 13781
061921 ZDOT = 4200
467674
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 19351
54008334
00016717 00000-0 10270-3 0 9070
2 25544 51
6378 172
3255 0007343 42
7724 317
3997 15
50134307 3696
Satellite: ISS
Catalog Number: 25544
Epoch time: 19351
54008334 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 172
3255 deg
Eccentricity:
0007343
Arg of perigee: 42
7724 deg
Mean anomaly: 317
3997 deg
Mean motion: 15
50134307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 369
Checksum: 310
Coasting Arc #9 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2019/352/11:36:38
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4976139
54 A = 6793949
85 meter
Y = 2143434
30 meter E =
0014427
Z = -4114970
96 I = 51
72046
XDOT = -5022
327221 Wp = 59
74327
YDOT = 4315
217778 meter/sec RA = 166
47945 deg
ZDOT = -3828
611715 TA = 170
65325
MA = 170
62638
Ha = 229
759 n
mi
Hp = 218
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16325917
12 X = 4971789
32
Y = 7032264
78 feet Y = 2199057
01 meter
Z = -13500560
91 Z = -4090809
28
XDOT = -16477
451512 XDOT = -5051
610820
YDOT = 14157
538641 feet/sec YDOT = 4258
891126 meter/sec
ZDOT = -12561
062058 ZDOT = -3853
078945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9759340
72 X = -2974647
05
Y = 14956925
61 feet Y = 4558870
93 meter
Z = -13390261
67 Z = -4081351
76
XDOT = -10024
490098 XDOT = -3055
464582
YDOT = -17877
806570 feet/sec YDOT = -5449
155443 meter/sec
ZDOT = -12673
093973 ZDOT = -3862
759043
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 19352
50710908
00016717 00000-0 10270-3 0 9085
2 25544 51
6377 167
5335 0007504 47
5482 312
6302 15
50137109 3841
Satellite: ISS
Catalog Number: 25544
Epoch time: 19352
50710908 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 167
5335 deg
Eccentricity:
0007504
Arg of perigee: 47
5482 deg
Mean anomaly: 312
6302 deg
Mean motion: 15
50137109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 300
Coasting Arc #10 (Orbit 399)
---------------------------------------
Vector Time (GMT): 2019/353/11:36:38
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4825879
08 A = 6793125
87 meter
Y = -1989642
02 meter E =
0015100
Z = 4333284
32 I = 51
75044
XDOT = 5045
930962 Wp = 83
79111
YDOT = -4595
063920 meter/sec RA = 161
53000 deg
ZDOT = 3500
817611 TA = 330
63244
MA = 330
71721
Ha = 229
858 n
mi
Hp = 218
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15832936
61 X = -4824320
29
Y = -6527696
90 feet Y = -2043599
98 meter
Z = 14216812
08 Z = 4309845
72
XDOT = 16554
891606 XDOT = 5079
934297
YDOT = -15075
669029 feet/sec YDOT = -4538
446860 meter/sec
ZDOT = 11485
622082 ZDOT = 3525
411080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8926192
12 X = 2720703
36
Y = -14718940
41 feet Y = -4486333
04 meter
Z = 14109795
95 Z = 4300665
80
XDOT = 11253
791548 XDOT = 3430
155664
YDOT = 17971
185615 feet/sec YDOT = 5477
617375 meter/sec
ZDOT = 11598
260153 ZDOT = 3535
149695
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 19353
53859985
00016717 00000-0 10270-3 0 9099
2 25544 51
6381 162
4216 0007338 50
5654 309
6145 15
50139283 4003
Satellite: ISS
Catalog Number: 25544
Epoch time: 19353
53859985 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 162
4216 deg
Eccentricity:
0007338
Arg of perigee: 50
5654 deg
Mean anomaly: 309
6145 deg
Mean motion: 15
50139283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 400
Checksum: 316
Coasting Arc #11 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2019/354/11:36:38
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4675429
66 A = 6792297
01 meter
Y = 1893569
82 meter E =
0017189
Z = -4565972
39 I = 51
77929
XDOT = -5015
766674 Wp = 63
99161
YDOT = 4854
004734 meter/sec RA = 156
58267 deg
ZDOT = -3124
805665 TA = 174
67867
MA = 174
66037
Ha = 229
896 n
mi
Hp = 218
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15339336
15 X = 4676086
72
Y = 6212499
40 feet Y = 1945857
76 meter
Z = -14980224
39 Z = -4543259
15
XDOT = -16455
927409 XDOT = -5054
494195
YDOT = 15925
212383 feet/sec YDOT = 4797
698558 meter/sec
ZDOT = -10251
987090 ZDOT = -3149
264155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8291785
24 X = -2527336
14
Y = 14430292
25 feet Y = 4398353
08 meter
Z = -14876507
26 Z = -4534359
41
XDOT = -12447
319935 XDOT = -3793
943116
YDOT = -17830
668885 feet/sec YDOT = -5434
787876 meter/sec
ZDOT = -10364
038674 ZDOT = -3158
958988
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 19354
50562238
00016717 00000-0 10270-3 0 9101
2 25544 51
6383 157
6299 0007641 55
8764 304
3110 15
50143100 4152
Satellite: ISS
Catalog Number: 25544
Epoch time: 19354
50562238 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 157
6299 deg
Eccentricity:
0007641
Arg of perigee: 55
8764 deg
Mean anomaly: 304
3110 deg
Mean motion: 15
50143100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 287
Coasting Arc #12 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2019/355/11:36:38
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4506436
94 A = 6791572
11 meter
Y = -1803736
02 meter E =
0013429
Z = 4738486
32 I = 51
80583
XDOT = 4969
549615 Wp = 89
30081
YDOT = -5149
936863 meter/sec RA = 151
63659 deg
ZDOT = 2759
238516 TA = 333
42435
MA = 333
49314
Ha = 229
999 n
mi
Hp = 218
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14784898
11 X = -4508949
15
Y = -5917769
10 feet Y = -1854144
62 meter
Z = 15546214
97 Z = 4716589
39
XDOT = 16304
296637 XDOT = 5013
365454
YDOT = -16896
118317 feet/sec YDOT = -5094
119079 meter/sec
ZDOT = 9052
619802 ZDOT = 2783
484846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7682831
34 X = 2341726
99
Y = -14060105
49 feet Y = -4285520
15 meter
Z = 15446214
41 Z = 4708006
15
XDOT = 13770
652972 XDOT = 4197
295026
YDOT = 17615
708580 feet/sec YDOT = 5369
267975 meter/sec
ZDOT = 9163
737402 ZDOT = 2793
107160
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 19355
53711116
00016717 00000-0 10270-3 0 9117
2 25544 51
6370 152
5181 0007430 59
2814 300
9068 15
50138333 4316
Satellite: ISS
Catalog Number: 25544
Epoch time: 19355
53711116 = yrday
fracday
Element set: 911
Inclination: 51
6370 deg
RA of node: 152
5181 deg
Eccentricity:
0007430
Arg of perigee: 59
2814 deg
Mean anomaly: 300
9068 deg
Mean motion: 15
50138333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 277
Coasting Arc #13 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2019/355/13:08:55
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4676743
18 A = 6791893
78 meter
Y = -1605650
83 meter E =
0013993
Z = 4644063
01 I = 51
81094
XDOT = 4746
879913 Wp = 89
96979
YDOT = -5248
717880 meter/sec RA = 151
32047 deg
ZDOT = 2957
892667 TA = 330
60770
MA = 330
68633
Ha = 229
933 n
mi
Hp = 218
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15343645
60 X = -4680999
12
Y = -5267883
31 feet Y = -1657973
66 meter
Z = 15236427
21 Z = 4621334
57
XDOT = 15573
752996 XDOT = 4790
851942
YDOT = -17220
203020 feet/sec YDOT = -5195
389292 meter/sec
ZDOT = 9704
372267 ZDOT = 2981
057715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 762003
81 X = 232258
76
Y = -16301843
76 feet Y = -4968801
98 meter
Z = 15132614
09 Z = 4612420
78
XDOT = 19665
239630 XDOT = 5993
965039
YDOT = 10049
689929 feet/sec YDOT = 3063
145490 meter/sec
ZDOT = 9810
553669 ZDOT = 2990
256758
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 19355
60157885
00016717 00000-0 10270-3 0 9123
2 25544 51
6389 152
1983 0007293 60
6799 299
5079 15
50157663 4320
Satellite: ISS
Catalog Number: 25544
Epoch time: 19355
60157885 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 152
1983 deg
Eccentricity:
0007293
Arg of perigee: 60
6799 deg
Mean anomaly: 299
5079 deg
Mean motion: 15
50157663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 347
Coasting Arc #14 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2019/356/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 560224
02 A = 6789860
30 meter
Y = 4412944
26 meter E =
0019811
Z = -5146605
40 I = 51
82393
XDOT = -6933
341354 Wp = 87
18274
YDOT = 2781
334781 meter/sec RA = 148
22349 deg
ZDOT = 1636
524654 TA = 198
57719
MA = 198
64962
Ha = 229
949 n
mi
Hp = 218
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1838005
31 X = 535835
04
Y = 14478163
58 feet Y = 4419073
20 meter
Z = -16885188
31 Z = -5143942
84
XDOT = -22747
182919 XDOT = -6971
877124
YDOT = 9125
114112 feet/sec YDOT = 2703
585635 meter/sec
ZDOT = 5369
175373 ZDOT = 1602
751546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5510229
27 X = 1679517
88
Y = -13529062
52 feet Y = -4123658
26 meter
Z = -16873260
19 Z = -5142969
71
XDOT = 23316
434829 XDOT = 7106
849336
YDOT = 3019
082744 feet/sec YDOT = 920
216420 meter/sec
ZDOT = 5214
619269 ZDOT = 1589
415953
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 19356
18179226
00016717 00000-0 10270-3 0 9131
2 25544 51
6408 149
3280 0007638 59
0244 301
1656 15
50130330 4413
Satellite: ISS
Catalog Number: 25544
Epoch time: 19356
18179226 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 149
3280 deg
Eccentricity:
0007638
Arg of perigee: 59
0244 deg
Mean anomaly: 301
1656 deg
Mean motion: 15
50130330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 288
Coasting Arc #15 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2019/357/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -484011
20 A = 6790274
64 meter
Y = -4548436
27 meter E =
0013542
Z = 5010515
55 I = 51
85376
XDOT = 6745
018515 Wp = 59
91502
YDOT = -3006
233290 meter/sec RA = 143
28028 deg
ZDOT = -2066
639255 TA = 50
18523
MA = 50
06611
Ha = 229
930 n
mi
Hp = 218
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1587963
25 X = -457451
72
Y = -14922691
19 feet Y = -4553700
91 meter
Z = 16438699
31 Z = 5008228
37
XDOT = 22129
325837 XDOT = 6788
172430
YDOT = -9862
970112 feet/sec YDOT = -2930
564196 meter/sec
ZDOT = -6780
312515 ZDOT = -2033
769833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5712866
26 X = -1741281
64
Y = 13889083
96 feet Y = 4233392
79 meter
Z = 16428502
07 Z = 5007407
43
XDOT = -23168
780674 XDOT = -7061
844349
YDOT = -1645
873463 feet/sec YDOT = -501
662232 meter/sec
ZDOT = -6629
849029 ZDOT = -2020
777984
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 19357
21327804
00016717 00000-0 10270-3 0 9144
2 25544 51
6410 144
2171 0007601 61
9986 298
1933 15
50162595 4572
Satellite: ISS
Catalog Number: 25544
Epoch time: 19357
21327804 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 144
2171 deg
Eccentricity:
0007601
Arg of perigee: 61
9986 deg
Mean anomaly: 298
1933 deg
Mean motion: 15
50162595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 310
Coasting Arc #16 (Orbit 471)
---------------------------------------
Vector Time (GMT): 2019/358/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 476730
11 A = 6790923
71 meter
Y = 4707891
01 meter E =
0018287
Z = -4886809
65 I = 51
88291
XDOT = -6497
424579 Wp = 91
43413
YDOT = 3200
669454 meter/sec RA = 138
33873 deg
ZDOT = 2457
134794 TA = 202
62598
MA = 202
70670
Ha = 230
011 n
mi
Hp = 218
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1564075
16 X = 447787
14
Y = 15445836
65 feet Y = 4713060
98 meter
Z = -16032840
07 Z = -4884563
52
XDOT = -21317
009775 XDOT = -6544
667930
YDOT = 10500
884037 feet/sec YDOT = 3127
746170 meter/sec
ZDOT = 8061
465861 ZDOT = 2425
458328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5741204
49 X = 1749919
13
Y = -14435341
49 feet Y = -4399892
09 meter
Z = -16022847
71 Z = -4883763
98
XDOT = 22748
657032 XDOT = 6933
790663
YDOT = 287
889967 feet/sec YDOT = 87
748862 meter/sec
ZDOT = 7916
418039 ZDOT = 2412
924218
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 19358
18029536
00016717 00000-0 10270-3 0 9153
2 25544 51
6420 139
4250 0007689 65
5685 294
6267 15
50138599 4724
Satellite: ISS
Catalog Number: 25544
Epoch time: 19358
18029536 = yrday
fracday
Element set: 915
Inclination: 51
6420 deg
RA of node: 139
4250 deg
Eccentricity:
0007689
Arg of perigee: 65
5685 deg
Mean anomaly: 294
6267 deg
Mean motion: 15
50138599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 341
Coasting Arc #17 (Orbit 487)
---------------------------------------
Vector Time (GMT): 2019/359/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -454384
58 A = 6791552
69 meter
Y = -4876454
46 meter E =
0015646
Z = 4695726
46 I = 51
90923
XDOT = 6269
251386 Wp = 66
49013
YDOT = -3358
397120 meter/sec RA = 133
40007 deg
ZDOT = -2867
368366 TA = 51
94631
MA = 51
80523
Ha = 230
004 n
mi
Hp = 218
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1490763
05 X = -422630
08
Y = -15998866
33 feet Y = -4881358
87 meter
Z = 15405926
71 Z = 4693595
62
XDOT = 20568
410060 XDOT = 6320
268089
YDOT = -11018
363255 feet/sec YDOT = -3288
004232 meter/sec
ZDOT = -9407
376529 ZDOT = -2836
791314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5811295
68 X = -1771282
92
Y = 14990194
51 feet Y = 4569011
29 meter
Z = 15396479
70 Z = 4692847
01
XDOT = -22291
302340 XDOT = -6794
388953
YDOT = 922
741904 feet/sec YDOT = 281
251732 meter/sec
ZDOT = -9267
318922 ZDOT = -2824
678808
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 19359
21177914
00016717 00000-0 10270-3 0 9163
2 25544 51
6417 134
3145 0007677 68
8854 291
3117 15
50168072 4882
Satellite: ISS
Catalog Number: 25544
Epoch time: 19359
21177914 = yrday
fracday
Element set: 916
Inclination: 51
6417 deg
RA of node: 134
3145 deg
Eccentricity:
0007677
Arg of perigee: 68
8854 deg
Mean anomaly: 291
3117 deg
Mean motion: 15
50168072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 488
Checksum: 329
Coasting Arc #18 (Orbit 491)
---------------------------------------
Vector Time (GMT): 2019/359/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4880055
21 A = 6800830
30 meter
Y = 4688061
49 meter E =
0020225
Z = 588119
38 I = 51
94127
XDOT = -2901
048715 Wp = 59
39688
YDOT = -3790
202009 meter/sec RA = 132
24786 deg
ZDOT = 5997
645778 TA = 306
91634
MA = 307
10147
Ha = 230
023 n
mi
Hp = 218
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16010679
83 X = -4934972
54
Y = 15380779
18 feet Y = 4633182
11 meter
Z = 1929525
53 Z = 564281
28
XDOT = -9517
876361 XDOT = -2887
583128
YDOT = -12435
045962 feet/sec YDOT = -3822
569222 meter/sec
ZDOT = 19677
315544 ZDOT = 5983
585715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4922276
70 X = -1500309
94
Y = -21658517
03 feet Y = -6601515
99 meter
Z = 1820202
65 Z = 554797
77
XDOT = 14049
815265 XDOT = 4282
383693
YDOT = -1502
959077 feet/sec YDOT = -458
101927 meter/sec
ZDOT = 19613
239915 ZDOT = 5978
115526
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 19359
46965046
00016717 00000-0 10270-3 0 9172
2 25544 51
6377 133
0319 0007574 73
2246 286
9735 15
50137610 4922
Satellite: ISS
Catalog Number: 25544
Epoch time: 19359
46965046 = yrday
fracday
Element set: 917
Inclination: 51
6377 deg
RA of node: 133
0319 deg
Eccentricity:
0007574
Arg of perigee: 73
2246 deg
Mean anomaly: 286
9735 deg
Mean motion: 15
50137610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 328
Coasting Arc #19 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2019/360/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4673667
80 A = 6800422
03 meter
Y = -4833465
40 meter E =
0014625
Z = -1005793
75 I = 51
96338
XDOT = 2821
513278 Wp = 112
93547
YDOT = 3945
990985 meter/sec RA = 127
31636 deg
ZDOT = -5926
089495 TA = 77
89139
MA = 77
72756
Ha = 229
998 n
mi
Hp = 218
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15333555
79 X = 4732255
22
Y = -15857826
13 feet Y = -4780873
40 meter
Z = -3299848
28 Z = -982949
45
XDOT = 9256
933327 XDOT = 2805
963802
YDOT = 12946
164650 feet/sec YDOT = 3977
457140 meter/sec
ZDOT = -19442
550837 ZDOT = -5912
420873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6041457
64 X = 1841436
29
Y = 21231347
24 feet Y = 6471314
64 meter
Z = -3195037
62 Z = -973847
47
XDOT = -14357
698605 XDOT = -4376
226535
YDOT = 1206
794408 feet/sec YDOT = 367
830936 meter/sec
ZDOT = -19380
272653 ZDOT = -5907
107105
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 19360
43666493
00016717 00000-0 10270-3 0 9186
2 25544 51
6391 128
2399 0007622 74
8643 285
3350 15
50181162 5078
Satellite: ISS
Catalog Number: 25544
Epoch time: 19360
43666493 = yrday
fracday
Element set: 918
Inclination: 51
6391 deg
RA of node: 128
2399 deg
Eccentricity:
0007622
Arg of perigee: 74
8643 deg
Mean anomaly: 285
3350 deg
Mean motion: 15
50181162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 318
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