[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 7th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
189/01:36:41
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
5
191/04:12:02
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
4
194/19:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
2
198/02:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
2
198/21:41:46
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 213
2
200/04:45:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 213
2
201/00:21:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 213
1
201/08:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
1
202/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 213
1
Coasting Arc #1 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2016/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4604646
86 A = 6777541
26 meter
Y = 1222998
28 meter E =
0007117
Z = 4815848
46 I = 51
40123
XDOT = -4183
531578 Wp = 112
96978
YDOT = 5930
879008 meter/sec RA = 321
08098 deg
ZDOT = 2488
235447 TA = 312
48362
MA = 312
54374
Ha = 220
060 n
mi
Hp = 213
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15107109
11 X = 4567235
85
Y = 4012461
56 feet Y = 1274280
80 meter
Z = 15800027
75 Z = 4838125
57
XDOT = -13725
497304 XDOT = -4261
627798
YDOT = 19458
264461 feet/sec YDOT = 5883
659027 meter/sec
ZDOT = 8163
502122 ZDOT = 2467
724230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 251822
10 X = 76755
38
Y = -15530386
06 feet Y = -4733661
67 meter
Z = 15896828
77 Z = 4845353
41
XDOT = 21088
880389 XDOT = 6427
890743
YDOT = 8624
245901 feet/sec YDOT = 2628
670151 meter/sec
ZDOT = 8072
914229 ZDOT = 2460
624257
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 16188
55253733
00016717 00000-0 10270-3 0 9004
2 25544 51
6433 321
4207 0000849 30
7763 329
3439 15
54750888 7999
Satellite: ISS
Catalog Number: 25544
Epoch time: 16188
55253733 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 321
4207 deg
Eccentricity:
0000849
Arg of perigee: 30
7763 deg
Mean anomaly: 329
3439 deg
Mean motion: 15
54750888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 327
Coasting Arc #2 (Orbit 807)
---------------------------------------
Vector Time (GMT): 2016/189/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5143282
98 A = 6787613
02 meter
Y = -4415552
31 meter E =
0013825
Z = 166702
62 I = 51
41972
XDOT = 2999
689685 Wp = 44
64627
YDOT = 3731
411341 meter/sec RA = 318
22954 deg
ZDOT = 5993
532201 TA = 317
15592
MA = 317
26357
Ha = 220
348 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16874287
98 X = 5191466
78
Y = -14486720
17 feet Y = -4357767
29 meter
Z = 546924
60 Z = 191803
55
XDOT = 9841
501591 XDOT = 2928
627680
YDOT = 12242
163192 feet/sec YDOT = 3764
557937 meter/sec
ZDOT = 19663
819557 ZDOT = 6007
931466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21859459
27 X = 6662763
19
Y = 4078961
39 feet Y = 1243267
43 meter
Z = 657188
76 Z = 200311
13
XDOT = -3163
720537 XDOT = -964
302020
YDOT = 13647
548434 feet/sec YDOT = 4159
772763 meter/sec
ZDOT = 19725
783830 ZDOT = 6012
418911
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 16189
13103654
00016717 00000-0 10270-3 0 9016
2 25544 51
6427 318
5393 0001452 23
9861 336
1360 15
54714276 8080
Satellite: ISS
Catalog Number: 25544
Epoch time: 16189
13103654 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 318
5393 deg
Eccentricity:
0001452
Arg of perigee: 23
9861 deg
Mean anomaly: 336
1360 deg
Mean motion: 15
54714276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 808
Checksum: 300
Coasting Arc #3 (Orbit 822)
---------------------------------------
Vector Time (GMT): 2016/190/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5479039
80 A = 6785734
65 meter
Y = 3436467
52 meter E =
0006061
Z = -2050332
19 I = 51
39127
XDOT = -1186
275709 Wp = 126
34088
YDOT = -5179
030234 meter/sec RA = 313
23988 deg
ZDOT = -5525
227683 TA = 76
40997
MA = 76
34247
Ha = 220
301 n
mi
Hp = 213
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17975852
38 X = -5507100
58
Y = 11274499
75 feet Y = 3375040
51 meter
Z = -6726811
63 Z = -2077015
42
XDOT = -3891
980672 XDOT = -1101
435602
YDOT = -16991
569008 feet/sec YDOT = -5191
821146 meter/sec
ZDOT = -18127
387412 ZDOT = -5530
784571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20135768
94 X = -6137382
37
Y = -6573385
13 feet Y = -2003567
79 meter
Z = -6843758
10 Z = -2085977
47
XDOT = 10168
848729 XDOT = 3099
465093
YDOT = -12302
554263 feet/sec YDOT = -3749
818539 meter/sec
ZDOT = -18150
540879 ZDOT = -5532
284860
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 16190
09519587
00016717 00000-0 10270-3 0 9020
2 25544 51
6437 313
7295 0001403 25
6285 334
4937 15
54728837 8230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16190
09519587 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 313
7295 deg
Eccentricity:
0001403
Arg of perigee: 25
6285 deg
Mean anomaly: 334
4937 deg
Mean motion: 15
54728837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 823
Checksum: 324
Coasting Arc #4 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2016/191/01:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 879562
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5330792
00 A = 6781847
59 meter
Y = -2069227
00 meter E =
0012480
Z = 3634996
38 I = 51
35684
XDOT = -531
999579 Wp = 88
38030
YDOT = 6297
119243 meter/sec RA = 308
23895 deg
ZDOT = 4352
220671 TA = 315
00083
MA = 315
10188
Ha = 220
238 n
mi
Hp = 213
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17489475
08 X = 5335877
45
Y = -6788802
49 feet Y = -2009586
33 meter
Z = 11925841
14 Z = 3660903
86
XDOT = -1745
405443 XDOT = -623
516908
YDOT = 20659
840037 feet/sec YDOT = 6290
658081 meter/sec
ZDOT = 14278
939210 ZDOT = 4349
414519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16507839
04 X = 5031589
34
Y = 8760482
50 feet Y = 2670195
07 meter
Z = 12039122
11 Z = 3669524
42
XDOT = -16213
111802 XDOT = -4941
756477
YDOT = 10890
562015 feet/sec YDOT = 3319
443302 meter/sec
ZDOT = 14265
444163 ZDOT = 4348
107381
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 16191
12362746
00016717 00000-0 10270-3 0 9039
2 25544 51
6435 308
5986 0001445 29
0703 331
0530 15
54735267 8390
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
12362746 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 308
5986 deg
Eccentricity:
0001445
Arg of perigee: 29
0703 deg
Mean anomaly: 331
0530 deg
Mean motion: 15
54735267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 839
Checksum: 303
Coasting Arc #5 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2016/191/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1940823
23 A = 6776660
73 meter
Y = -4096887
95 meter E =
0013376
Z = -5049044
56 I = 51
33839
XDOT = 5608
341127 Wp = 97
49225
YDOT = -4890
558446 meter/sec RA = 307
65857 deg
ZDOT = 1814
907797 TA = 190
15961
MA = 190
18667
Ha = 220
253 n
mi
Hp = 213
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6367530
27 X = -1870340
83
Y = -13441233
43 feet Y = -4118197
12 meter
Z = -16565106
81 Z = -5058301
52
XDOT = 18400
069315 XDOT = 5653
795851
YDOT = -16045
139260 feet/sec YDOT = -4827
588199 meter/sec
ZDOT = 5954
421906 ZDOT = 1842
261406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3754102
00 X = -1144250
29
Y = -14346033
00 feet Y = -4372670
86 meter
Z = -16604608
30 Z = -5061084
61
XDOT = 19889
673225 XDOT = 6062
372399
YDOT = -12226
484722 feet/sec YDOT = -3726
632543 meter/sec
ZDOT = 6074
570413 ZDOT = 1851
529062
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 16191
18790262
00016717 00000-0 10270-3 0 9044
2 25544 51
6445 308
2785 0001425 21
9191 338
2023 15
54756440 8409
Satellite: ISS
Catalog Number: 25544
Epoch time: 16191
18790262 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 308
2785 deg
Eccentricity:
0001425
Arg of perigee: 21
9191 deg
Mean anomaly: 338
2023 deg
Mean motion: 15
54756440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 840
Checksum: 297
Coasting Arc #6 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2016/192/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 505523
23 A = 6780135
78 meter
Y = 5345034
29 meter E =
0011420
Z = 4134192
58 I = 51
33083
XDOT = -5751
626635 Wp = 69
35493
YDOT = 3440
996424 meter/sec RA = 302
63841 deg
ZDOT = -3733
176684 TA = 59
25420
MA = 59
14179
Ha = 220
229 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1658540
77 X = 425634
25
Y = 17536201
73 feet Y = 5350240
46 meter
Z = 13563623
94 Z = 4136454
52
XDOT = -18870
166126 XDOT = -5771
543307
YDOT = 11289
358348 feet/sec YDOT = 3376
566752 meter/sec
ZDOT = -12247
955000 ZDOT = -3761
164490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1290531
80 X = -393354
09
Y = 17560330
76 feet Y = 5352388
82 meter
Z = 13572410
78 Z = 4136870
81
XDOT = -19090
512187 XDOT = -5818
788115
YDOT = 8189
500350 feet/sec YDOT = 2496
159707 meter/sec
ZDOT = -12370
564141 ZDOT = -3770
547950
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 16192
21632745
00016717 00000-0 10270-3 0 9051
2 25544 51
6440 303
1473 0001578 22
5408 337
5814 15
54790922 8569
Satellite: ISS
Catalog Number: 25544
Epoch time: 16192
21632745 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 303
1473 deg
Eccentricity:
0001578
Arg of perigee: 22
5408 deg
Mean anomaly: 337
5814 deg
Mean motion: 15
54790922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 304
Coasting Arc #7 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2016/193/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 785951
60 A = 6784433
42 meter
Y = -6170931
13 meter E =
0006195
Z = -2705559
94 I = 51
32704
XDOT = 5463
960917 Wp = 48
83563
YDOT = -1555
556366 meter/sec RA = 297
62959 deg
ZDOT = 5146
926560 TA = 280
44385
MA = 280
51365
Ha = 220
308 n
mi
Hp = 213
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2578581
35 X = 868040
41
Y = -20245837
03 feet Y = -6161682
95 meter
Z = -8876509
00 Z = -2701542
99
XDOT = 17926
380960 XDOT = 5455
948130
YDOT = -5103
531386 feet/sec YDOT = -1494
499807 meter/sec
ZDOT = 16886
241995 ZDOT = 5173
449318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5543397
27 X = 1689627
49
Y = -19650590
75 feet Y = -5989500
06 meter
Z = -8857789
84 Z = -2699854
34
XDOT = 16935
500302 XDOT = 5161
940492
YDOT = -2869
110989 feet/sec YDOT = -874
505029 meter/sec
ZDOT = 17002
087126 ZDOT = 5182
236156
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 16193
18047398
00016717 00000-0 10270-3 0 9063
2 25544 51
6428 298
3369 0001470 25
3442 334
7783 15
54747615 8716
Satellite: ISS
Catalog Number: 25544
Epoch time: 16193
18047398 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 298
3369 deg
Eccentricity:
0001470
Arg of perigee: 25
3442 deg
Mean anomaly: 334
7783 deg
Mean motion: 15
54747615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 333
Coasting Arc #8 (Orbit 886)
---------------------------------------
Vector Time (GMT): 2016/194/04:12:02
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1917418
26 A = 6787208
10 meter
Y = 6444056
64 meter E =
0013402
Z = 886770
88 I = 51
32291
XDOT = -4858
185900 Wp = 119
17869
YDOT = -624
934674 meter/sec RA = 292
63098 deg
ZDOT = -5902
084084 TA = 51
17886
MA = 51
05929
Ha = 220
345 n
mi
Hp = 213
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6290742
33 X = -1993642
34
Y = 21141918
12 feet Y = 6422188
54 meter
Z = 2909353
28 Z = 877271
87
XDOT = -15938
930118 XDOT = -4822
167074
YDOT = -2050
310611 feet/sec YDOT = -679
060390 meter/sec
ZDOT = -19363
792927 ZDOT = -5925
596326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8962509
00 X = -2731772
74
Y = 20161197
39 feet Y = 6145132
96 meter
Z = 2866710
61 Z = 873773
39
XDOT = -13950
903313 XDOT = -4252
235330
YDOT = -3404
924521 feet/sec YDOT = -1037
820994 meter/sec
ZDOT = -19466
091928 ZDOT = -5933
264820
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 16194
20889170
00016717 00000-0 10270-3 0 9070
2 25544 51
6435 293
2055 0001459 31
4832 328
6408 15
54747496 8878
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
20889170 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 293
2055 deg
Eccentricity:
0001459
Arg of perigee: 31
4832 deg
Mean anomaly: 328
6408 deg
Mean motion: 15
54747496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 887
Checksum: 332
Coasting Arc #9 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2016/194/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3692953
87 A = 6785385
83 meter
Y = -5263940
60 meter E =
0015155
Z = 2143448
29 I = 51
30718
XDOT = 3086
485884 Wp = 68
09119
YDOT = 4404
165635 meter/sec RA = 289
56665 deg
ZDOT = 5472
555194 TA = 315
81037
MA = 315
93132
Ha = 220
279 n
mi
Hp = 213
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12115990
40 X = 3741130
23
Y = -17270146
34 feet Y = -5222374
30 meter
Z = 7032310
65 Z = 2161504
29
XDOT = 10126
266025 XDOT = 3010
424844
YDOT = 14449
362318 feet/sec YDOT = 4438
255131 meter/sec
ZDOT = 17954
577409 ZDOT = 5487
364035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 109403
83 X = 33346
29
Y = 21069318
38 feet Y = 6421928
24 meter
Z = 7111991
60 Z = 2167735
04
XDOT = -14978
523674 XDOT = -4565
454016
YDOT = -6032
347988 feet/sec YDOT = -1838
659667 meter/sec
ZDOT = 18018
226326 ZDOT = 5491
955384
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 16194
85164813
00016717 00000-0 10270-3 0 9082
2 25544 51
6407 289
9980 0001389 44
1508 315
9755 15
54800687 8976
Satellite: ISS
Catalog Number: 25544
Epoch time: 16194
85164813 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 289
9980 deg
Eccentricity:
0001389
Arg of perigee: 44
1508 deg
Mean anomaly: 315
9755 deg
Mean motion: 15
54800687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 352
Coasting Arc #10 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2016/195/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110525
29 A = 6781470
91 meter
Y = 3891695
33 meter E =
0007378
Z = -3742723
59 I = 51
28312
XDOT = -1920
917290 Wp = 70
31610
YDOT = -6092
535005 meter/sec RA = 284
55844 deg
ZDOT = -4229
736741 TA = 154
66514
MA = 154
62895
Ha = 220
454 n
mi
Hp = 213
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13485975
36 X = -4135557
25
Y = 12768029
29 feet Y = 3845589
02 meter
Z = -12279276
87 Z = -3762751
90
XDOT = -6302
222079 XDOT = -1832
100124
YDOT = -19988
631906 feet/sec YDOT = -6113
519053 meter/sec
ZDOT = -13877
089045 ZDOT = -4238
852774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3267328
47 X = 995881
72
Y = -18222233
36 feet Y = -5554136
73 meter
Z = -12367276
17 Z = -3769545
78
XDOT = 15498
097686 XDOT = 4723
820175
YDOT = 12213
590465 feet/sec YDOT = 3722
702374 meter/sec
ZDOT = -13915
619721 ZDOT = -4241
480891
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 16195
81578451
00016717 00000-0 10270-3 0 9097
2 25544 51
6399 285
1867 0001632 45
2093 314
9193 15
54760163 9127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16195
81578451 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 285
1867 deg
Eccentricity:
0001632
Arg of perigee: 45
2093 deg
Mean anomaly: 314
9193 deg
Mean motion: 15
54760163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 328
Coasting Arc #11 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2016/196/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4272964
73 A = 6777442
47 meter
Y = -2096329
19 meter E =
0007520
Z = 4819795
86 I = 51
26272
XDOT = 777
804031 Wp = 108
88965
YDOT = 7229
965162 meter/sec RA = 279
53786 deg
ZDOT = 2449
518280 TA = 316
92264
MA = 316
98147
Ha = 220
245 n
mi
Hp = 213
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14018913
16 X = 4272676
46
Y = -6877720
45 feet Y = -2048548
09 meter
Z = 15812978
54 Z = 4840551
87
XDOT = 2551
850496 XDOT = 685
000286
YDOT = 23720
358143 feet/sec YDOT = 7238
143971 meter/sec
ZDOT = 8036
477298 ZDOT = 2453
071875
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6922720
84 X = -2110045
31
Y = 13893464
92 feet Y = 4234728
11 meter
Z = 15903799
03 Z = 4847477
94
XDOT = -15325
954326 XDOT = -4671
350879
YDOT = -16872
616584 feet/sec YDOT = -5142
773535 meter/sec
ZDOT = 8050
568552 ZDOT = 2453
813295
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 16196
84419147
00016717 00000-0 10270-3 0 9109
2 25544 51
6400 280
0559 0001507 43
1605 316
9666 15
54781149 9280
Satellite: ISS
Catalog Number: 25544
Epoch time: 16196
84419147 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 280
0559 deg
Eccentricity:
0001507
Arg of perigee: 43
1605 deg
Mean anomaly: 316
9666 deg
Mean motion: 15
54781149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 313
Coasting Arc #12 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2016/197/19:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4257549
52 A = 6775528
13 meter
Y = 43735
86 meter E =
0016131
Z = -5284613
89 I = 51
25262
XDOT = 334
910998 Wp = 83
67405
YDOT = -7643
148878 meter/sec RA = 274
50603 deg
ZDOT = -332
208198 TA = 183
13219
MA = 183
14231
Ha = 220
472 n
mi
Hp = 213
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13968338
32 X = -4232051
94
Y = 143490
37 feet Y = -3731
79 meter
Z = -17337972
09 Z = -5305233
95
XDOT = 1098
789364 XDOT = 421
967437
YDOT = -25075
947764 feet/sec YDOT = -7638
916885 meter/sec
ZDOT = -1089
921908 ZDOT = -330
370621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10800339
44 X = 3291943
46
Y = -8681270
85 feet Y = -2646051
35 meter
Z = -17427809
55 Z = -5311996
35
XDOT = 14007
181357 XDOT = 4269
388878
YDOT = 19601
019346 feet/sec YDOT = 5974
390697 meter/sec
ZDOT = -1080
460609 ZDOT = -329
324394
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 16197
80831966
00016717 00000-0 10270-3 0 9114
2 25544 51
6409 275
2449 0001647 48
0535 312
0758 15
54769681 9437
Satellite: ISS
Catalog Number: 25544
Epoch time: 16197
80831966 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 275
2449 deg
Eccentricity:
0001647
Arg of perigee: 48
0535 deg
Mean anomaly: 312
0758 deg
Mean motion: 15
54769681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 335
Coasting Arc #13 (Orbit 947)
---------------------------------------
Vector Time (GMT): 2016/198/02:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2485540
07 A = 6782255
76 meter
Y = 5284684
53 meter E =
0013390
Z = 3438642
96 I = 51
27801
XDOT = -3897
100154 Wp = 83
40796
YDOT = 4799
632350 meter/sec RA = 272
98138 deg
ZDOT = -4542
621079 TA = 56
02508
MA = 55
89791
Ha = 220
280 n
mi
Hp = 213
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8154659
04 X = 2409557
34
Y = 17338203
85 feet Y = 5312054
30 meter
Z = 11281637
01 Z = 3450533
02
XDOT = -12785
761660 XDOT = -3928
415264
YDOT = 15746
825296 feet/sec YDOT = 4755
877760 meter/sec
ZDOT = -14903
612465 ZDOT = -4561
627650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2996029
76 X = -913189
87
Y = 18894097
31 feet Y = 5758920
86 meter
Z = 11332431
46 Z = 3454125
11
XDOT = -17946
839870 XDOT = -5470
196792
YDOT = 6176
244749 feet/sec YDOT = 1882
519399 meter/sec
ZDOT = -14987
325724 ZDOT = -4568
136881
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 16198
12969304
00016717 00000-0 10270-3 0 9129
2 25544 51
6440 273
6425 0001672 35
8582 324
2683 15
54819921 9482
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
12969304 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 273
6425 deg
Eccentricity:
0001672
Arg of perigee: 35
8582 deg
Mean anomaly: 324
2683 deg
Mean motion: 15
54819921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 948
Checksum: 325
Coasting Arc #14 (Orbit 960)
---------------------------------------
Vector Time (GMT): 2016/198/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1110653
00 A = 6786431
58 meter
Y = -6508455
92 meter E =
0015555
Z = 1535783
39 I = 51
28861
XDOT = 4630
738144 Wp = 60
66928
YDOT = 2150
230407 meter/sec RA = 268
93973 deg
ZDOT = 5727
119330 TA = 316
20923
MA = 316
33248
Ha = 220
445 n
mi
Hp = 213
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3643874
67 X = 1175889
54
Y = -21353201
84 feet Y = -6495671
27 meter
Z = 5038659
42 Z = 1541336
34
XDOT = 15192
710447 XDOT = 4578
529930
YDOT = 7054
561702 feet/sec YDOT = 2201
721856 meter/sec
ZDOT = 18789
761581 ZDOT = 5749
487537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20368531
38 X = 6208328
37
Y = 7355485
90 feet Y = 2241952
10 meter
Z = 5064079
05 Z = 1543531
29
XDOT = -9090
658673 XDOT = -2770
832764
YDOT = 12088
548095 feet/sec YDOT = 3684
589459 meter/sec
ZDOT = 18886
806953 ZDOT = 5756
698759
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 16198
96526992
00016717 00000-0 10270-3 0 9134
2 25544 51
6419 269
4731 0001703 47
0078 313
1218 15
54779453 9612
Satellite: ISS
Catalog Number: 25544
Epoch time: 16198
96526992 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 269
4731 deg
Eccentricity:
0001703
Arg of perigee: 47
0078 deg
Mean anomaly: 313
1218 deg
Mean motion: 15
54779453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 961
Checksum: 330
Coasting Arc #15 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2016/199/21:41:46
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2036824
20 A = 6782827
96 meter
Y = 5590106
56 meter E =
0005911
Z = -3262887
02 I = 51
27915
XDOT = -4253
487853 Wp = 84
26958
YDOT = -4294
802423 meter/sec RA = 263
93543 deg
ZDOT = -4709
631797 TA = 133
77831
MA = 133
72939
Ha = 220
435 n
mi
Hp = 213
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6682494
08 X = -2083333
29
Y = 18340244
61 feet Y = 5567069
75 meter
Z = -10705009
92 Z = -3272893
62
XDOT = -13955
012640 XDOT = -4182
269080
YDOT = -14090
559132 feet/sec YDOT = -4341
969018 meter/sec
ZDOT = -15451
547891 ZDOT = -4730
121439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17034297
27 X = -5192053
81
Y = -9481310
32 feet Y = -2889903
38 meter
Z = -10749651
55 Z = -3276493
79
XDOT = 15448
594026 XDOT = 4708
731459
YDOT = -10161
581858 feet/sec YDOT = -3097
250150 meter/sec
ZDOT = -15540
019413 ZDOT = -4736
597917
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 16199
92939218
00016717 00000-0 10270-3 0 9141
2 25544 51
6427 264
6629 0001690 48
7726 311
3573 15
54798665 9763
Satellite: ISS
Catalog Number: 25544
Epoch time: 16199
92939218 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 264
6629 deg
Eccentricity:
0001690
Arg of perigee: 48
7726 deg
Mean anomaly: 311
3573 deg
Mean motion: 15
54798665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 976
Checksum: 358
Coasting Arc #16 (Orbit 980)
---------------------------------------
Vector Time (GMT): 2016/200/04:45:26
000
Vector Time (MET): N/A
Weight (LBS) : 894794
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3469223
16 A = 6777468
76 meter
Y = -3258216
25 meter E =
0007800
Z = 4819914
14 I = 51
25840
XDOT = 2867
154705 Wp = 110
43415
YDOT = 6683
118438 meter/sec RA = 262
45041 deg
ZDOT = 2448
132529 TA = 315
38927
MA = 315
45202
Ha = 220
315 n
mi
Hp = 213
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11381965
76 X = 3481986
76
Y = -10689685
87 feet Y = -3219350
26 meter
Z = 15813366
60 Z = 4836797
17
XDOT = 9406
675540 XDOT = 2780
317482
YDOT = 21926
241596 feet/sec YDOT = 6714
695063 meter/sec
ZDOT = 8031
930871 ZDOT = 2461
850109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9906383
18 X = 3019465
59
Y = -11972090
45 feet Y = -3649093
17 meter
Z = 15887533
31 Z = 4842520
15
XDOT = 11061
002873 XDOT = 3371
393676
YDOT = 19914
503749 feet/sec YDOT = 6069
940743 meter/sec
ZDOT = 8090
456595 ZDOT = 2465
971170
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 16200
25076514
00016717 00000-0 10270-3 0 9152
2 25544 51
6391 263
0556 0001457 55
2216 304
9074 15
54779154 9815
Satellite: ISS
Catalog Number: 25544
Epoch time: 16200
25076514 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 263
0556 deg
Eccentricity:
0001457
Arg of perigee: 55
2216 deg
Mean anomaly: 304
9074 deg
Mean motion: 15
54779154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 981
Checksum: 301
Coasting Arc #17 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2016/201/00:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 909228
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3791669
71 A = 6782052
15 meter
Y = -4385945
26 meter E =
0006323
Z = -3523832
60 I = 51
28228
XDOT = 2471
985486 Wp = 84
59105
YDOT = -5717
570133 meter/sec RA = 258
31625 deg
ZDOT = 4464
029966 TA = 233
67449
MA = 233
73288
Ha = 220
364 n
mi
Hp = 213
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12439861
25 X = -3725226
17
Y = -14389584
18 feet Y = -4427974
35 meter
Z = -11561130
59 Z = -3542090
38
XDOT = 8110
188602 XDOT = 2514
053087
YDOT = -18758
432195 feet/sec YDOT = -5689
692004 meter/sec
ZDOT = 14645
767606 ZDOT = 4476
139629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5767724
65 X = 1758002
47
Y = -18075303
36 feet Y = -5509352
46 meter
Z = -11639878
95 Z = -3547835
10
XDOT = 18856
112298 XDOT = 5747
343028
YDOT = -3433
377022 feet/sec YDOT = -1046
493316 meter/sec
ZDOT = 14699
586593 ZDOT = 4480
433993
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 16201
02205899
00016717 00000-0 10270-3 0 9169
2 25544 51
6434 259
2118 0001580 44
9054 315
2227 15
54795106 9939
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
02205899 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 259
2118 deg
Eccentricity:
0001580
Arg of perigee: 44
9054 deg
Mean anomaly: 315
2227 deg
Mean motion: 15
54795106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 302
Coasting Arc #18 (Orbit 998)
---------------------------------------
Vector Time (GMT): 2016/201/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 909228
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4162135
61 A = 6775300
37 meter
Y = -810845
40 meter E =
0003755
Z = 5281145
75 I = 51
26199
XDOT = 1656
424906 Wp = 76
87609
YDOT = 7490
433750 meter/sec RA = 256
60480 deg
ZDOT = -154
466861 TA = 14
60824
MA = 14
59740
Ha = 220
203 n
mi
Hp = 213
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13655300
56 X = 4145240
26
Y = -2660253
94 feet Y = -764396
63 meter
Z = 17326593
66 Z = 5301322
90
XDOT = 5434
464914 XDOT = 1573
292200
YDOT = 24574
913878 feet/sec YDOT = 7508
492191 meter/sec
ZDOT = -506
781040 ZDOT = -146
621646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3027479
59 X = 922775
78
Y = -13465469
52 feet Y = -4104275
11 meter
Z = 17414664
22 Z = 5307989
66
XDOT = 23699
348286 XDOT = 7223
561358
YDOT = 4711
483600 feet/sec YDOT = 1436
060201 meter/sec
ZDOT = -473
968562 ZDOT = -144
465618
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 16201
40770514
00016717 00000-0 10270-3 0 9173
2 25544 51
6431 257
2827 0001363 65
5410 294
5885 15
54832727 9991
Satellite: ISS
Catalog Number: 25544
Epoch time: 16201
40770514 = yrday
fracday
Element set: 917
Inclination: 51
6431 deg
RA of node: 257
2827 deg
Eccentricity:
0001363
Arg of perigee: 65
5410 deg
Mean anomaly: 294
5885 deg
Mean motion: 15
54832727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 999
Checksum: 318
Coasting Arc #19 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2016/202/08:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 909228
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4541492
05 A = 6777055
51 meter
Y = -1220164
59 meter E =
0013403
Z = -4892452
71 I = 51
27545
XDOT = -498
963709 Wp = 103
13502
YDOT = -7293
370397 meter/sec RA = 251
57499 deg
ZDOT = 2284
428817 TA = 189
32951
MA = 189
35443
Ha = 220
410 n
mi
Hp = 212
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14899908
29 X = -4503745
37
Y = -4003164
67 feet Y = -1270739
10 meter
Z = -16051354
02 Z = -4914422
13
XDOT = -1637
020043 XDOT = -428
466871
YDOT = -23928
380567 feet/sec YDOT = -7298
556171 meter/sec
ZDOT = 7494
845200 ZDOT = 2282
175609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9423737
16 X = -2872355
09
Y = 12089260
57 feet Y = 3684806
62 meter
Z = -16146873
29 Z = -4921566
98
XDOT = -21830
670285 XDOT = -6653
988303
YDOT = -7028
317242 feet/sec YDOT = -2142
231095 meter/sec
ZDOT = 7486
344609 ZDOT = 2281
837837
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 16202
37182148
00016717 00000-0 10270-3 0 9181
2 25544 51
6424 252
4736 0001467 71
5655 288
5658 15
54823565 10142
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
37182148 = yrday
fracday
Element set: 918
Inclination: 51
6424 deg
RA of node: 252
4736 deg
Eccentricity:
0001467
Arg of perigee: 71
5655 deg
Mean anomaly: 288
5658 deg
Mean motion: 15
54823565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 317
Coasting Arc #20 (Orbit 1015)
---------------------------------------
Vector Time (GMT): 2016/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930194
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4544607
78 A = 6779188
54 meter
Y = 2540995
71 meter E =
0010911
Z = 4334726
14 I = 51
28315
XDOT = -553
072730 Wp = 69
80953
YDOT = 6845
096949 meter/sec RA = 251
07561 deg
ZDOT = -3421
986518 TA = 55
10383
MA = 55
00133
Ha = 220
233 n
mi
Hp = 213
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14910130
51 X = 4494800
15
Y = 8336600
10 feet Y = 2591537
68 meter
Z = 14221542
46 Z = 4356681
52
XDOT = -1814
543078 XDOT = -612
953019
YDOT = 22457
667154 feet/sec YDOT = 6838
577604 meter/sec
ZDOT = -11226
989890 ZDOT = -3424
818005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4846371
88 X = 1477174
15
Y = -16297427
29 feet Y = -4967455
84 meter
Z = 14316763
12 Z = 4363749
40
XDOT = 21095
776090 XDOT = 6429
992552
YDOT = -3631
918852 feet/sec YDOT = -1107
008866 meter/sec
ZDOT = -11240
565013 ZDOT = -3426
124216
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 16202
50036856
00016717 00000-0 10270-3 0 9191
2 25544 51
6419 251
8332 0001396 60
1602 299
9690 15
54833680 10161
Satellite: ISS
Catalog Number: 25544
Epoch time: 16202
50036856 = yrday
fracday
Element set: 919
Inclination: 51
6419 deg
RA of node: 251
8332 deg
Eccentricity:
0001396
Arg of perigee: 60
1602 deg
Mean anomaly: 299
9690 deg
Mean motion: 15
54833680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1016
Checksum: 306
Coasting Arc #21 (Orbit 1030)
---------------------------------------
Vector Time (GMT): 2016/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930194
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4456061
28 A = 6783493
52 meter
Y = -4160122
49 meter E =
0006001
Z = -2977563
73 I = 51
30761
XDOT = 1875
631594 Wp = 69
64826
YDOT = -5543
862186 meter/sec RA = 246
06216 deg
ZDOT = 4948
850363 TA = 256
13702
MA = 256
20379
Ha = 220
393 n
mi
Hp = 213
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14619623
63 X = -4394747
14
Y = -13648695
84 feet Y = -4209610
11 meter
Z = -9768909
87 Z = -2999061
07
XDOT = 6153
646963 XDOT = 1913
446183
YDOT = -18188
524233 feet/sec YDOT = -5522
676523 meter/sec
ZDOT = 16236
385705 ZDOT = 4958
052991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9786269
87 X = -2982855
06
Y = 17390357
11 feet Y = 5300580
85 meter
Z = -9861860
62 Z = -3005895
12
XDOT = -17836
464981 XDOT = -5436
554526
YDOT = -825
306934 feet/sec YDOT = -251
553553 meter/sec
ZDOT = 16277
479459 ZDOT = 4961
375739
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 16203
46448279
00016717 00000-0 10270-3 0 9205
2 25544 51
6408 247
0228 0001474 68
5931 291
5379 15
54816555 10315
Satellite: ISS
Catalog Number: 25544
Epoch time: 16203
46448279 = yrday
fracday
Element set: 920
Inclination: 51
6408 deg
RA of node: 247
0228 deg
Eccentricity:
0001474
Arg of perigee: 68
5931 deg
Mean anomaly: 291
5379 deg
Mean motion: 15
54816555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1031
Checksum: 314
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list