[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 2nd 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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
334/13:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
6
340/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 215
1
341/18:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
7
000/00:00:00
000 0
0 0
0 215
2
342/18:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
4
344/22:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
4
348/01:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 215
5
348/05:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 748)
---------------------------------------
Vector Time (GMT): 2017/333/16:38:16
467
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3250065
88 A = 6778064
93 meter
Y = 2958894
78 meter E =
0003455
Z = 5156786
18 I = 51
27771
XDOT = -3837
719457 Wp = 101
47276
YDOT = 6510
452899 meter/sec RA = 292
48730 deg
ZDOT = -1316
811674 TA = 1
23778
MA = 1
23692
Ha = 221
216 n
mi
Hp = 214
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10662945
79 X = 3191687
57
Y = 9707660
04 feet Y = 2994912
73 meter
Z = 16918589
82 Z = 5172432
55
XDOT = -12590
943101 XDOT = -3903
839313
YDOT = 21359
753605 feet/sec YDOT = 6467
167223 meter/sec
ZDOT = -4320
248275 ZDOT = -1335
614948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1208691
26 X = 368409
10
Y = 14287763
62 feet Y = 4354910
35 meter
Z = 16987484
64 Z = 5177785
32
XDOT = -22655
937021 XDOT = -6905
529604
YDOT = 7153
912973 feet/sec YDOT = 2180
512674 meter/sec
ZDOT = -4404
725695 ZDOT = -1342
560392
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 17333
73918845
00016717 00000-0 10270-3 0 9009
2 25544 51
6421 293
0212 0003179 183
3839 176
7293 15
54085708 7493
Satellite: ISS
Catalog Number: 25544
Epoch time: 17333
73918845 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 293
0212 deg
Eccentricity:
0003179
Arg of perigee: 183
3839 deg
Mean anomaly: 176
7293 deg
Mean motion: 15
54085708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 749
Checksum: 326
Coasting Arc #2 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2017/334/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4047735
48 A = 6777610
02 meter
Y = -1286879
91 meter E =
0014983
Z = -5294377
03 I = 51
26307
XDOT = 2359
210895 Wp = 101
83935
YDOT = -7285
066460 meter/sec RA = 288
16055 deg
ZDOT = -36
055982 TA = 167
83291
MA = 167
79668
Ha = 221
382 n
mi
Hp = 214
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13279972
03 X = -4007326
37
Y = -4222046
96 feet Y = -1331918
35 meter
Z = -17370003
39 Z = -5313941
99
XDOT = 7740
193225 XDOT = 2440
674264
YDOT = -23901
136681 feet/sec YDOT = -7258
228661 meter/sec
ZDOT = -118
293904 ZDOT = -24
397781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4225991
96 X = 1288082
35
Y = -13164724
54 feet Y = -4012608
04 meter
Z = -17456556
79 Z = -5320758
51
XDOT = 22939
708258 XDOT = 6992
023077
YDOT = 7437
106417 feet/sec YDOT = 2266
830036 meter/sec
ZDOT = -65
383570 ZDOT = -19
928912
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 17334
57516154
00016717 00000-0 10270-3 0 9010
2 25544 51
6397 288
8530 0003160 184
0271 176
0857 15
54041882 7627
Satellite: ISS
Catalog Number: 25544
Epoch time: 17334
57516154 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 288
8530 deg
Eccentricity:
0003160
Arg of perigee: 184
0271 deg
Mean anomaly: 176
0857 deg
Mean motion: 15
54041882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 311
Coasting Arc #3 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2017/335/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3452766
59 A = 6778711
15 meter
Y = 2953076
07 meter E =
0004103
Z = 5027213
88 I = 51
25827
XDOT = -3100
603788 Wp = 89
63836
YDOT = 6769
586516 meter/sec RA = 283
13678 deg
ZDOT = -1845
701332 TA = 18
33623
MA = 18
32144
Ha = 221
150 n
mi
Hp = 214
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11327974
38 X = 3395067
58
Y = 9688569
79 feet Y = 2991364
38 meter
Z = 16493483
86 Z = 5043846
76
XDOT = -10172
584607 XDOT = -3167
106953
YDOT = 22209
929516 feet/sec YDOT = 6734
541703 meter/sec
ZDOT = -6055
450564 ZDOT = -1860
924627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9497688
58 X = -2894895
48
Y = 11382561
73 feet Y = 3469404
82 meter
Z = 16566761
85 Z = 5049549
01
XDOT = -21548
563197 XDOT = -6568
002062
YDOT = -9060
631534 feet/sec YDOT = -2761
680492 meter/sec
ZDOT = -6124
078297 ZDOT = -1866
619065
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 17335
60404517
00016717 00000-0 10270-3 0 9025
2 25544 51
6403 283
7256 0003167 189
1906 170
9189 15
54055462 7789
Satellite: ISS
Catalog Number: 25544
Epoch time: 17335
60404517 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 283
7256 deg
Eccentricity:
0003167
Arg of perigee: 189
1906 deg
Mean anomaly: 170
9189 deg
Mean motion: 15
54055462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 318
Coasting Arc #4 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2017/336/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2819638
11 A = 6781733
72 meter
Y = -4464745
30 meter E =
0009317
Z = -4265349
37 I = 51
26280
XDOT = 3682
292560 Wp = 129
61885
YDOT = -5707
701091 meter/sec RA = 278
11626 deg
ZDOT = 3539
668220 TA = 176
71605
MA = 176
70993
Ha = 221
197 n
mi
Hp = 214
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9250781
19 X = -2748783
11
Y = -14648114
51 feet Y = -4495879
91 meter
Z = -13993928
38 Z = -4278874
87
XDOT = 12081
012336 XDOT = 3728
649558
YDOT = -18726
053449 feet/sec YDOT = -5666
264265 meter/sec
ZDOT = 11613
084712 ZDOT = 3557
668211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14327417
88 X = 4366996
97
Y = -9654396
35 feet Y = -2942660
01 meter
Z = -14053183
66 Z = -4283410
38
XDOT = 18420
763850 XDOT = 5614
648821
YDOT = 10312
015874 feet/sec YDOT = 3143
102438 meter/sec
ZDOT = 11693
848110 ZDOT = 3564
284904
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 17336
56861697
00016717 00000-0 10270-3 0 9038
2 25544 51
6411 278
9168 0003131 192
1153 167
9925 15
54070329 7935
Satellite: ISS
Catalog Number: 25544
Epoch time: 17336
56861697 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 278
9168 deg
Eccentricity:
0003131
Arg of perigee: 192
1153 deg
Mean anomaly: 167
9925 deg
Mean motion: 15
54070329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 327
Coasting Arc #5 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2017/337/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2139307
77 A = 6785532
45 meter
Y = 5664654
91 meter E =
0012919
Z = 3046529
49 I = 51
27189
XDOT = -4155
421158 Wp = 109
57446
YDOT = 4205
934135 meter/sec RA = 273
10693 deg
ZDOT = -4889
730354 TA = 35
24708
MA = 35
16172
Ha = 221
068 n
mi
Hp = 214
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7018726
27 X = 2061006
24
Y = 18584825
82 feet Y = 5688139
98 meter
Z = 9995175
50 Z = 3056732
20
XDOT = -13633
271515 XDOT = -4178
391819
YDOT = 13798
996506 feet/sec YDOT = 4159
337450 meter/sec
ZDOT = -16042
422421 ZDOT = -4909
971860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18203765
02 X = -5548507
58
Y = 7898925
98 feet Y = 2407592
64 meter
Z = 10039507
44 Z = 3060041
87
XDOT = -13898
652672 XDOT = -4236
309334
YDOT = -11473
041333 feet/sec YDOT = -3496
982998 meter/sec
ZDOT = -16132
881627 ZDOT = -4917
302320
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 17337
59748847
00016717 00000-0 10270-3 0 9044
2 25544 51
6411 273
7892 0003095 195
3300 164
7760 15
54068253 8093
Satellite: ISS
Catalog Number: 25544
Epoch time: 17337
59748847 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 273
7892 deg
Eccentricity:
0003095
Arg of perigee: 195
3300 deg
Mean anomaly: 164
7760 deg
Mean motion: 15
54068253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 331
Coasting Arc #6 (Orbit 823)
---------------------------------------
Vector Time (GMT): 2017/338/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1446440
76 A = 6788445
51 meter
Y = -6450318
17 meter E =
0005225
Z = -1537372
74 I = 51
28116
XDOT = 4512
349519 Wp = 47
71380
YDOT = -2372
140335 meter/sec RA = 268
10630 deg
ZDOT = 5723
244438 TA = 295
40870
MA = 295
46277
Ha = 221
004 n
mi
Hp = 215
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4745540
56 X = -1366736
17
Y = -21162461
17 feet Y = -6466047
42 meter
Z = -5043873
82 Z = -1544206
38
XDOT = 14804
296321 XDOT = 4510
738955
YDOT = -7782
612647 feet/sec YDOT = -2321
689846 meter/sec
ZDOT = 18777
048682 ZDOT = 5745
160153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20789977
36 X = 6336785
10
Y = -6152283
82 feet Y = -1875216
11 meter
Z = -5073147
59 Z = -1546295
38
XDOT = 8320
662160 XDOT = 2536
137827
YDOT = 12596
421024 feet/sec YDOT = 3839
389128 meter/sec
ZDOT = 18874
640256 ZDOT = 5752
990350
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 17338
56205064
00016717 00000-0 10270-3 0 9052
2 25544 51
6413 268
9815 0003135 200
8273 159
2753 15
54082036 8245
Satellite: ISS
Catalog Number: 25544
Epoch time: 17338
56205064 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 268
9815 deg
Eccentricity:
0003135
Arg of perigee: 200
8273 deg
Mean anomaly: 159
2753 deg
Mean motion: 15
54082036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 824
Checksum: 301
Coasting Arc #7 (Orbit 839)
---------------------------------------
Vector Time (GMT): 2017/339/13:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 933812
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 685035
65 A = 6789488
30 meter
Y = 6745291
00 meter E =
0013320
Z = -160804
47 I = 51
28737
XDOT = -4787
948909 Wp = 148
81403
YDOT = 349
204159 meter/sec RA = 263
11181 deg
ZDOT = -5982
773914 TA = 32
92729
MA = 32
84439
Ha = 220
934 n
mi
Hp = 215
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2247492
28 X = 610338
20
Y = 22130219
83 feet Y = 6752533
90 meter
Z = -527573
73 Z = -157657
38
XDOT = -15708
493797 XDOT = -4762
436352
YDOT = 1145
682937 feet/sec YDOT = 295
805410 meter/sec
ZDOT = -19628
523339 ZDOT = -6005
970460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21855777
73 X = -6661641
05
Y = 4139597
04 feet Y = 1261749
18 meter
Z = -514685
47 Z = -156876
13
XDOT = -2173
333405 XDOT = -662
432022
YDOT = -13829
947086 feet/sec YDOT = -4215
367872 meter/sec
ZDOT = -19731
480109 ZDOT = -6014
155137
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 17339
59091108
00016717 00000-0 10270-3 0 9069
2 25544 51
6420 263
8534 0003215 204
2909 155
8092 15
54070917 8409
Satellite: ISS
Catalog Number: 25544
Epoch time: 17339
59091108 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 263
8534 deg
Eccentricity:
0003215
Arg of perigee: 204
2909 deg
Mean anomaly: 155
8092 deg
Mean motion: 15
54070917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 840
Checksum: 302
Coasting Arc #8 (Orbit 854)
---------------------------------------
Vector Time (GMT): 2017/340/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3666662
11 A = 6784761
62 meter
Y = -4680043
69 meter E =
0003933
Z = -3274204
68 I = 51
27671
XDOT = 2712
086703 Wp = 124
88270
YDOT = -5410
613017 meter/sec RA = 258
12686 deg
ZDOT = 4698
409898 TA = 196
92355
MA = 196
93667
Ha = 220
808 n
mi
Hp = 215
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12029731
35 X = -3598151
58
Y = -15354474
05 feet Y = -4720663
39 meter
Z = -10742141
33 Z = -3291850
33
XDOT = 8897
922253 XDOT = 2749
565438
YDOT = -17751
355044 feet/sec YDOT = -5380
075561 meter/sec
ZDOT = 15414
730636 ZDOT = 4711
674855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14897544
13 X = 4540771
45
Y = -12524589
21 feet Y = -3817494
79 meter
Z = -10819692
87 Z = -3297842
39
XDOT = 17153
191574 XDOT = 5228
292792
YDOT = 7040
228674 feet/sec YDOT = 2145
861700 meter/sec
ZDOT = 15474
428655 ZDOT = 4716
605854
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 17340
55546129
00016717 00000-0 10270-3 0 9076
2 25544 51
6418 259
0454 0003038 207
8401 152
2590 15
54114218 8556
Satellite: ISS
Catalog Number: 25544
Epoch time: 17340
55546129 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 259
0454 deg
Eccentricity:
0003038
Arg of perigee: 207
8401 deg
Mean anomaly: 152
2590 deg
Mean motion: 15
54114218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 855
Checksum: 296
Coasting Arc #9 (Orbit 870)
---------------------------------------
Vector Time (GMT): 2017/341/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3212901
17 A = 6788101
41 meter
Y = 5701660
94 meter E =
0013965
Z = 1771616
57 I = 51
29427
XDOT = -3577
491083 Wp = 127
52007
YDOT = 3775
240834 meter/sec RA = 253
12656 deg
ZDOT = -5639
814580 TA = 32
91738
MA = 32
83049
Ha = 220
749 n
mi
Hp = 215
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10541014
33 X = 3140299
24
Y = 18706236
68 feet Y = 5737183
70 meter
Z = 5812390
32 Z = 1787048
00
XDOT = -11737
175469 XDOT = -3592
045525
YDOT = 12385
960741 feet/sec YDOT = 3735
153998 meter/sec
ZDOT = -18503
328674 ZDOT = -5657
227930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18105716
21 X = -5518622
30
Y = 11507781
67 feet Y = 3507571
85 meter
Z = 5879979
29 Z = 1792217
69
XDOT = -12160
622905 XDOT = -3706
557862
YDOT = -9601
804318 feet/sec YDOT = -2926
629956 meter/sec
ZDOT = -18581
172535 ZDOT = -5663
541389
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 17341
58431155
00016717 00000-0 10270-3 0 9083
2 25544 51
6409 253
9179 0003141 210
8032 149
2937 15
54083451 8715
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
58431155 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 253
9179 deg
Eccentricity:
0003141
Arg of perigee: 210
8032 deg
Mean anomaly: 149
2937 deg
Mean motion: 15
54083451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 871
Checksum: 302
Coasting Arc #10 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2017/341/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1562056
15 A = 6782891
54 meter
Y = 5332132
12 meter E =
0004677
Z = -3893750
18 I = 51
27512
XDOT = -4820
972298 Wp = 101
29644
YDOT = -4367
422294 meter/sec RA = 252
13804 deg
ZDOT = -4051
802879 TA = 126
06279
MA = 126
01946
Ha = 220
689 n
mi
Hp = 215
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5124856
13 X = -1602651
48
Y = 17493871
78 feet Y = 5314437
48 meter
Z = -12774770
94 Z = -3901436
32
XDOT = -15816
838248 XDOT = -4752
094661
YDOT = -14328
813301 feet/sec YDOT = -4420
948246 meter/sec
ZDOT = -13293
316531 ZDOT = -4075
054711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8824276
37 X = -2689639
44
Y = 15922888
04 feet Y = 4853296
27 meter
Z = -12809693
82 Z = -3904394
68
XDOT = -10965
781249 XDOT = -3342
370125
YDOT = -16840
518392 feet/sec YDOT = -5132
990006 meter/sec
ZDOT = -13395
814005 ZDOT = -4083
044109
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 17341
77721835
00016717 00000-0 10270-3 0 9092
2 25544 51
6369 252
9524 0003158 211
7956 148
3006 15
54120291 8740
Satellite: ISS
Catalog Number: 25544
Epoch time: 17341
77721835 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 252
9524 deg
Eccentricity:
0003158
Arg of perigee: 211
7956 deg
Mean anomaly: 148
3006 deg
Mean motion: 15
54120291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 316
Coasting Arc #11 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2017/342/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2482263
82 A = 6779476
02 meter
Y = -4065230
34 meter E =
0007411
Z = 4823015
83 I = 51
27467
XDOT = 4530
075528 Wp = 145
61013
YDOT = 5682
126809 meter/sec RA = 247
12139 deg
ZDOT = 2450
001662 TA = 280
17441
MA = 280
25799
Ha = 220
574 n
mi
Hp = 215
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8143910
18 X = 2504110
03
Y = -13337369
89 feet Y = -4037350
12 meter
Z = 15823542
75 Z = 4835126
69
XDOT = 14862
452519 XDOT = 4454
298891
YDOT = 18642
148323 feet/sec YDOT = 5732
361365 meter/sec
ZDOT = 8038
063196 ZDOT = 2471
823635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10623624
23 X = 3238080
67
Y = -11385261
96 feet Y = -3470227
85 meter
Z = 15877897
59 Z = 4839583
19
XDOT = 9803
844853 XDOT = 2988
211911
YDOT = 20527
580941 feet/sec YDOT = 6256
806671 meter/sec
ZDOT = 8134
037225 ZDOT = 2479
254546
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 17342
80606201
00016717 00000-0 10270-3 0 9108
2 25544 51
6370 247
8229 0003215 217
7128 142
3799 15
54099423 8901
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
80606201 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 247
8229 deg
Eccentricity:
0003215
Arg of perigee: 217
7128 deg
Mean anomaly: 142
3799 deg
Mean motion: 15
54099423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 303
Coasting Arc #12 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2017/342/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4715103
63 A = 6781189
97 meter
Y = 2138768
08 meter E =
0006878
Z = 4373566
13 I = 51
28066
XDOT = -4
449274 Wp = 86
31633
YDOT = 6895
011227 meter/sec RA = 247
02584 deg
ZDOT = -3361
994743 TA = 37
88345
MA = 37
83507
Ha = 220
533 n
mi
Hp = 215
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15469500
09 X = 4669592
31
Y = 7016955
63 feet Y = 2191240
85 meter
Z = 14348970
26 Z = 4396360
20
XDOT = -14
597355 XDOT = -65
219914
YDOT = 22621
427911 feet/sec YDOT = 6894
621891 meter/sec
ZDOT = -11030
166479 ZDOT = -3362
163531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14220778
27 X = 4334493
22
Y = 9132851
78 feet Y = 2783693
22 meter
Z = 14449793
45 Z = 4404297
04
XDOT = -2492
804296 XDOT = -759
806749
YDOT = 21361
928680 feet/sec YDOT = 6511
115862 meter/sec
ZDOT = -11031
956978 ZDOT = -3362
540487
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 17342
80606173
00016717 00000-0 10270-3 0 9117
2 25544 51
6371 247
8226 0003340 215
9329 144
1599 15
54095378 8904
Satellite: ISS
Catalog Number: 25544
Epoch time: 17342
80606173 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 247
8226 deg
Eccentricity:
0003340
Arg of perigee: 215
9329 deg
Mean anomaly: 144
1599 deg
Mean motion: 15
54095378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 315
Coasting Arc #13 (Orbit 904)
---------------------------------------
Vector Time (GMT): 2017/343/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 919378
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4803450
00 A = 6784886
44 meter
Y = -3563139
26 meter E =
0003313
Z = -3208569
19 I = 51
30749
XDOT = 1188
555930 Wp = 126
73009
YDOT = -5886
412321 meter/sec RA = 242
01547 deg
ZDOT = 4759
032706 TA = 195
99136
MA = 196
00182
Ha = 220
633 n
mi
Hp = 215
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15759350
39 X = -4747663
37
Y = -11690089
42 feet Y = -3616542
65 meter
Z = -10526801
81 Z = -3231767
53
XDOT = 3899
461714 XDOT = 1231
173994
YDOT = -19312
376380 feet/sec YDOT = -5872
883005 meter/sec
ZDOT = 15613
624364 ZDOT = 4764
909581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14103563
24 X = -4298766
07
Y = -13562376
40 feet Y = -4133812
33 meter
Z = -10629220
22 Z = -3239786
32
XDOT = 5194
265369 XDOT = 1583
212084
YDOT = -17655
733769 feet/sec YDOT = -5381
467653 meter/sec
ZDOT = 15640
579395 ZDOT = 4767
248600
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 17343
77059780
00016717 00000-0 10270-3 0 9121
2 25544 51
6375 243
0137 0003243 215
5933 144
5003 15
54126440 9052
Satellite: ISS
Catalog Number: 25544
Epoch time: 17343
77059780 = yrday
fracday
Element set: 912
Inclination: 51
6375 deg
RA of node: 243
0137 deg
Eccentricity:
0003243
Arg of perigee: 215
5933 deg
Mean anomaly: 144
5003 deg
Mean motion: 15
54126440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 905
Checksum: 287
Coasting Arc #14 (Orbit 920)
---------------------------------------
Vector Time (GMT): 2017/344/18:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4630894
39 A = 6788054
68 meter
Y = 4656595
39 meter E =
0013354
Z = 1686522
04 I = 51
33331
XDOT = -2477
014915 Wp = 129
34911
YDOT = 4527
178747 meter/sec RA = 237
01711 deg
ZDOT = -5676
534637 TA = 32
07454
MA = 31
99335
Ha = 220
406 n
mi
Hp = 215
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15193223
07 X = 4570286
60
Y = 15277543
94 feet Y = 4708042
28 meter
Z = 5533208
79 Z = 1708870
52
XDOT = -8126
689355 XDOT = -2499
881057
YDOT = 14852
948646 feet/sec YDOT = 4499
351441 meter/sec
ZDOT = -18623
801301 ZDOT = -5688
622601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13417051
12 X = 4089517
18
Y = 16826180
61 feet Y = 5128619
85 meter
Z = 5631710
28 Z = 1716545
29
XDOT = -8334
813160 XDOT = -2540
451051
YDOT = 12921
228215 feet/sec YDOT = 3938
390360 meter/sec
ZDOT = -18678
111960 ZDOT = -5693
088525
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 17344
79943165
00016717 00000-0 10270-3 0 9134
2 25544 51
6365 237
8851 0003293 222
6332 137
4566 15
54138173 9211
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
79943165 = yrday
fracday
Element set: 913
Inclination: 51
6365 deg
RA of node: 237
8851 deg
Eccentricity:
0003293
Arg of perigee: 222
6332 deg
Mean anomaly: 137
4566 deg
Mean motion: 15
54138173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 921
Checksum: 319
Coasting Arc #15 (Orbit 923)
---------------------------------------
Vector Time (GMT): 2017/344/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 564433
84 A = 6781588
91 meter
Y = -5259274
38 meter E =
0009083
Z = 4241192
86 I = 51
31930
XDOT = 5801
067854 Wp = 126
84125
YDOT = 3515
714662 meter/sec RA = 236
18949 deg
ZDOT = 3576
942337 TA = 286
41704
MA = 286
51686
Ha = 220
431 n
mi
Hp = 215
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1851817
07 X = 602600
81
Y = -17254837
20 feet Y = -5252749
25 meter
Z = 13914674
73 Z = 4244027
21
XDOT = 19032
374850 XDOT = 5743
947958
YDOT = 11534
496923 feet/sec YDOT = 3580
266656 meter/sec
ZDOT = 11735
375121 ZDOT = 3604
983612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13409964
77 X = -4087357
26
Y = -10998173
59 feet Y = -3352243
31 meter
Z = 13928023
15 Z = 4245261
45
XDOT = 19284
337763 XDOT = 5877
866150
YDOT = -8450
317852 feet/sec YDOT = -2575
656881 meter/sec
ZDOT = 11859
311509 ZDOT = 3614
718148
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 17344
99233670
00016717 00000-0 10270-3 0 9140
2 25544 51
6409 236
9249 0003494 221
9389 138
1497 15
54161806 9241
Satellite: ISS
Catalog Number: 25544
Epoch time: 17344
99233670 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 236
9249 deg
Eccentricity:
0003494
Arg of perigee: 221
9389 deg
Mean anomaly: 138
1497 deg
Mean motion: 15
54161806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 924
Checksum: 335
Coasting Arc #16 (Orbit 938)
---------------------------------------
Vector Time (GMT): 2017/345/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1827023
88 A = 6778555
48 meter
Y = 4161390
49 meter E =
0010085
Z = -5038229
96 I = 51
32792
XDOT = -5720
727347 Wp = 85
56985
YDOT = -4747
743053 meter/sec RA = 231
17428 deg
ZDOT = -1849
383149 TA = 166
43231
MA = 166
40517
Ha = 220
337 n
mi
Hp = 215
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5994172
83 X = -1848948
48
Y = 13652855
94 feet Y = 4140837
07 meter
Z = -16529625
86 Z = -5047158
22
XDOT = -18768
790507 XDOT = -5658
228182
YDOT = -15576
584819 feet/sec YDOT = -4811
366611 meter/sec
ZDOT = -6067
530018 ZDOT = -1877
021224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8341461
85 X = 2542477
57
Y = 12305243
60 feet Y = 3750638
25 meter
Z = -16569855
42 Z = -5050491
93
XDOT = -22309
042266 XDOT = -6799
796083
YDOT = 6798
985734 feet/sec YDOT = 2072
330852 meter/sec
ZDOT = -6189
514237 ZDOT = -1886
563939
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 17345
95686579
00016717 00000-0 10270-3 0 9158
2 25544 51
6410 232
1172 0003487 227
9645 132
1212 15
54119938 9393
Satellite: ISS
Catalog Number: 25544
Epoch time: 17345
95686579 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 232
1172 deg
Eccentricity:
0003487
Arg of perigee: 227
9645 deg
Mean anomaly: 132
1212 deg
Mean motion: 15
54119938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 325
Coasting Arc #17 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2017/346/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3100731
76 A = 6777216
55 meter
Y = -2882523
50 meter E =
0002008
Z = 5292397
00 I = 51
34592
XDOT = 5276
234826 Wp = 187
69773
YDOT = 5565
011693 meter/sec RA = 226
15402 deg
ZDOT = -62
215564 TA = 262
88608
MA = 262
90892
Ha = 220
090 n
mi
Hp = 215
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10173004
46 X = 3107026
37
Y = -9457098
08 feet Y = -2847814
05 meter
Z = 17363507
23 Z = 5307474
68
XDOT = 17310
481713 XDOT = 5213
915445
YDOT = 18257
912379 feet/sec YDOT = 5623
665712 meter/sec
ZDOT = -204
119303 ZDOT = -36
736134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2792404
80 X = -851124
98
Y = -13519841
80 feet Y = -4120847
78 meter
Z = 17430847
95 Z = 5312922
46
XDOT = 23632
231991 XDOT = 7203
104311
YDOT = -4991
162219 feet/sec YDOT = -1521
306244 meter/sec
ZDOT = -91
817283 ZDOT = -27
985908
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 17346
98569058
00016717 00000-0 10270-3 0 9165
2 25544 51
6415 226
9885 0003359 232
6580 127
4267 15
54173350 9552
Satellite: ISS
Catalog Number: 25544
Epoch time: 17346
98569058 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 226
9885 deg
Eccentricity:
0003359
Arg of perigee: 232
6580 deg
Mean anomaly: 127
4267 deg
Mean motion: 15
54173350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 341
Coasting Arc #18 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2017/347/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4317159
83 A = 6778526
83 meter
Y = 1538665
47 meter E =
0011047
Z = -5004358
01 I = 51
37228
XDOT = -4408
675005 Wp = 117
47143
YDOT = -5944
983738 meter/sec RA = 221
13622 deg
ZDOT = 1973
761792 TA = 171
79633
MA = 171
77825
Ha = 220
163 n
mi
Hp = 215
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14163910
22 X = -4309735
79
Y = 5048115
06 feet Y = 1490429
85 meter
Z = -16418497
42 Z = -5025311
53
XDOT = -14464
156840 XDOT = -4351
456600
YDOT = -19504
539824 feet/sec YDOT = -5993
964747 meter/sec
ZDOT = 6475
596429 ZDOT = 1952
484221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2804506
53 X = -854813
59
Y = 14668477
00 feet Y = 4470951
79 meter
Z = -16511735
27 Z = -5032776
91
XDOT = -23101
512079 XDOT = -7041
340882
YDOT = 2773
130461 feet/sec YDOT = 845
250164 meter/sec
ZDOT = 6381
985040 ZDOT = 1945
229040
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 17347
95021360
00016717 00000-0 10270-3 0 9173
2 25544 51
6402 222
1813 0003220 235
8645 124
2203 15
54157011 9709
Satellite: ISS
Catalog Number: 25544
Epoch time: 17347
95021360 = yrday
fracday
Element set: 917
Inclination: 51
6402 deg
RA of node: 222
1813 deg
Eccentricity:
0003220
Arg of perigee: 235
8645 deg
Mean anomaly: 124
2203 deg
Mean motion: 15
54157011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 266
Coasting Arc #19 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2017/348/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 940547
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -793675
07 A = 6778816
96 meter
Y = 4549114
87 meter E =
0009706
Z = -4971486
00 I = 51
37603
XDOT = -6537
655759 Wp = 80
41928
YDOT = -3409
979180 meter/sec RA = 220
56168 deg
ZDOT = -2078
455851 TA = 169
27064
MA = 169
24992
Ha = 220
209 n
mi
Hp = 215
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2603920
83 X = -820336
22
Y = 14924917
56 feet Y = 4540090
69 meter
Z = -16310649
61 Z = -4975405
94
XDOT = -21449
001835 XDOT = -6488
942344
YDOT = -11187
595734 feet/sec YDOT = -3482
815215 meter/sec
ZDOT = -6819
080876 ZDOT = -2110
095969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15097681
83 X = 4601773
42
Y = -1002229
20 feet Y = -305479
46 meter
Z = -16328698
62 Z = -4976987
34
XDOT = -6039
300696 XDOT = -1840
778852
YDOT = 22301
999960 feet/sec YDOT = 6797
649588 meter/sec
ZDOT = -6959
057553 ZDOT = -2121
120742
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 17348
07881714
00016717 00000-0 10270-3 0 9185
2 25544 51
6403 221
5410 0003036 236
0672 124
0193 15
54137237 9720
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
07881714 = yrday
fracday
Element set: 918
Inclination: 51
6403 deg
RA of node: 221
5410 deg
Eccentricity:
0003036
Arg of perigee: 236
0672 deg
Mean anomaly: 124
0193 deg
Mean motion: 15
54137237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 972
Checksum: 289
Coasting Arc #20 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2017/348/05:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 925316
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 528711
94 A = 6779046
44 meter
Y = -4653212
21 meter E =
0005804
Z = 4900546
18 I = 51
37785
XDOT = 6615
318947 Wp = 148
91543
YDOT = 3146
798475 meter/sec RA = 219
76127 deg
ZDOT = 2268
177487 TA = 278
80651
MA = 278
87223
Ha = 220
085 n
mi
Hp = 215
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1734619
22 X = 556901
42
Y = -15266444
26 feet Y = -4647142
49 meter
Z = 16077907
42 Z = 4903182
70
XDOT = 21703
802318 XDOT = 6568
621131
YDOT = 10324
141978 feet/sec YDOT = 3220
514245 meter/sec
ZDOT = 7441
527187 ZDOT = 2300
199762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6460569
02 X = -1969181
44
Y = 13926108
06 feet Y = 4244677
74 meter
Z = 16090273
26 Z = 4904315
29
XDOT = -16157
200865 XDOT = -4924
714824
YDOT = -16280
359609 feet/sec YDOT = -4962
253609 meter/sec
ZDOT = 7583
240727 ZDOT = 2311
371774
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 17348
27172080
00016717 00000-0 10270-3 0 9197
2 25544 51
6373 220
5800 0003050 241
5346 118
5499 15
54154809 9757
Satellite: ISS
Catalog Number: 25544
Epoch time: 17348
27172080 = yrday
fracday
Element set: 919
Inclination: 51
6373 deg
RA of node: 220
5800 deg
Eccentricity:
0003050
Arg of perigee: 241
5346 deg
Mean anomaly: 118
5499 deg
Mean motion: 15
54154809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 308
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