[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 13th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15904 8079 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
225/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 222
0
227/05:57:52
433 -0
9 1
8 1
8
N/A 0
8 0
0 224
2
000/00:09:44
866 1
4 -0
1 222
4
227/08:59:52
374 -0
6 1
8 1
8
N/A 1
2 0
0 225
5
000/00:09:44
748 1
3 -0
0 223
5
234/03:38:33
000 0
0 0
0 0
0
N/A 0
0 0
0 226
8
000/00:00:00
000 0
0 0
0 222
3
235/16:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
9
000/00:00:00
000 0
0 0
0 222
2
236/05:30:59
000 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 221
9
Coasting Arc #1 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2019/224/12:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3024750
26 A = 6795071
01 meter
Y = -5427468
03 meter E =
0008476
Z = 2738152
40 I = 52
03438
XDOT = 3385
735654 Wp = 121
05860
YDOT = -4509
643617 meter/sec RA = 80
98200 deg
ZDOT = -5191
137996 TA = 28
17705
MA = 28
13121
Ha = 224
199 n
mi
Hp = 221
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9923721
31 X = -2977134
11
Y = -17806653
64 feet Y = -5461026
85 meter
Z = 8983439
63 Z = 2723574
89
XDOT = 11108
056607 XDOT = 3461
127327
YDOT = -14795
418691 feet/sec YDOT = -4471
360070 meter/sec
ZDOT = -17031
292638 ZDOT = -5174
508858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3000769
15 X = -914634
44
Y = 20192373
22 feet Y = 6154635
36 meter
Z = 8917555
41 Z = 2718070
89
XDOT = -16458
234294 XDOT = -5016
469813
YDOT = 5053
164463 feet/sec YDOT = 1540
204528 meter/sec
ZDOT = -16955
173105 ZDOT = -5167
936762
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 19224
54466459
00016717 00000-0 10270-3 0 9008
2 25544 51
6432 81
6641 0006199 254
0576 105
9892 15
51084622 23994
Satellite: ISS
Catalog Number: 25544
Epoch time: 19224
54466459 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 81
6641 deg
Eccentricity:
0006199
Arg of perigee: 254
0576 deg
Mean anomaly: 105
9892 deg
Mean motion: 15
51084622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2399
Checksum: 326
Coasting Arc #2 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2019/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4352013
54 A = 6788913
89 meter
Y = 2191550
88 meter E =
0006463
Z = -4733018
22 I = 52
00635
XDOT = -508
055982 Wp = 140
41572
YDOT = 7102
146885 meter/sec RA = 76
08005 deg
ZDOT = 2818
654799 TA = 157
44140
MA = 157
41298
Ha = 223
989 n
mi
Hp = 221
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14278259
64 X = 4350173
40
Y = 7190127
57 feet Y = 2240208
11 meter
Z = -15528275
01 Z = -4711882
60
XDOT = -1666
850336 XDOT = -601
127631
YDOT = 23301
006839 feet/sec YDOT = 7095
944908 meter/sec
ZDOT = 9247
555115 ZDOT = 2815
961215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6588148
81 X = -2008067
76
Y = -14667522
61 feet Y = -4470660
89 meter
Z = -15432240
06 Z = -4703746
77
XDOT = 15013
538011 XDOT = 4576
126386
YDOT = -16469
143323 feet/sec YDOT = -5019
794885 meter/sec
ZDOT = 9234
641109 ZDOT = 2814
718610
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 19225
51111137
00016717 00000-0 10270-3 0 9017
2 25544 51
6422 76
8674 0006198 256
6236 103
4225 15
51064780 24149
Satellite: ISS
Catalog Number: 25544
Epoch time: 19225
51111137 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 76
8674 deg
Eccentricity:
0006198
Arg of perigee: 256
6236 deg
Mean anomaly: 103
4225 deg
Mean motion: 15
51064780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2414
Checksum: 290
Coasting Arc #3 (Orbit 2429)
---------------------------------------
Vector Time (GMT): 2019/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937553
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4496281
72 A = 6790256
47 meter
Y = -2610994
96 meter E =
0003673
Z = 4365991
84 I = 52
00140
XDOT = 557
280290 Wp = 55
77737
YDOT = -6799
780190 meter/sec RA = 71
14080 deg
ZDOT = -3488
463335 TA = 69
53218
MA = 69
49275
Ha = 223
892 n
mi
Hp = 221
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14751580
46 X = -4487957
72
Y = -8566256
44 feet Y = -2661229
14 meter
Z = 14324120
22 Z = 4344171
24
XDOT = 1828
347407 XDOT = 650
220591
YDOT = -22308
990126 feet/sec YDOT = -6793
028517 meter/sec
ZDOT = -11445
089683 ZDOT = -3485
530828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6352375
59 X = 1936204
08
Y = 15920641
08 feet Y = 4852611
40 meter
Z = 14225006
42 Z = 4335781
96
XDOT = -14152
324313 XDOT = -4313
628451
YDOT = 15872
546769 feet/sec YDOT = 4837
952255 meter/sec
ZDOT = -11431
106598 ZDOT = -3484
201291
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 19226
54198571
00016717 00000-0 10270-3 0 9029
2 25544 51
6417 71
7526 0006225 261
4209 98
6237 15
51082143 24307
Satellite: ISS
Catalog Number: 25544
Epoch time: 19226
54198571 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 71
7526 deg
Eccentricity:
0006225
Arg of perigee: 261
4209 deg
Mean anomaly: 98
6237 deg
Mean motion: 15
51082143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2430
Checksum: 300
Coasting Arc #4 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2019/227/06:02:44
866
Vector Time (MET): N/A
Weight (LBS) : 937363
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2150541
60 A = 6799160
06 meter
Y = 6414944
51 meter E =
0009680
Z = 605707
18 I = 52
01804
XDOT = -4661
167613 Wp = 23
93114
YDOT = 993
572422 meter/sec RA = 67
45864 deg
ZDOT = 6001
641877 TA = 342
56452
MA = 342
59773
Ha = 224
247 n
mi
Hp = 222
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7055582
67 X = 2075705
89
Y = 21046405
87 feet Y = 6438574
93 meter
Z = 1987228
28 Z = 615971
81
XDOT = -15292
544662 XDOT = -4701
083555
YDOT = 3259
752042 feet/sec YDOT = 941
224680 meter/sec
ZDOT = 19690
426105 ZDOT = 5978
903278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21066097
28 X = 6420946
45
Y = 6983300
85 feet Y = 2128510
10 meter
Z = 2033366
06 Z = 619769
98
XDOT = -6129
395106 XDOT = -1868
239628
YDOT = 12763
724445 feet/sec YDOT = 3890
383211 meter/sec
ZDOT = 19586
797249 ZDOT = 5970
055801
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 19227
31515948
00016717 00000-0 10270-3 0 9037
2 25544 51
6410 67
9169 0006353 276
7014 83
3414 15
50697714 24421
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
31515948 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 67
9169 deg
Eccentricity:
0006353
Arg of perigee: 276
7014 deg
Mean anomaly: 83
3414 deg
Mean motion: 15
50697714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 312
Coasting Arc #5 (Orbit 2442)
---------------------------------------
Vector Time (GMT): 2019/227/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3150693
39 A = 6800109
22 meter
Y = 5977978
23 meter E =
0010165
Z = -696393
31 I = 52
01853
XDOT = -3907
065067 Wp = 358
60883
YDOT = 2756
021944 meter/sec RA = 66
82366 deg
ZDOT = 5989
540720 TA = 353
91824
MA = 353
93057
Ha = 225
481 n
mi
Hp = 223
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10336920
58 X = 3086994
37
Y = 19612789
48 feet Y = 6012855
35 meter
Z = -2284754
95 Z = -681243
40
XDOT = -12818
454944 XDOT = -3966
686495
YDOT = 9042
066746 feet/sec YDOT = 2711
996942 meter/sec
ZDOT = 19650
724148 ZDOT = 5970
417345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17801736
01 X = 5425969
13
Y = -13225717
61 feet Y = -4031198
73 meter
Z = -2216333
05 Z = -675538
32
XDOT = 9950
477762 XDOT = 3032
905622
YDOT = 10119
456651 feet/sec YDOT = 3084
410387 meter/sec
ZDOT = 19563
391314 ZDOT = 5962
921673
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 19227
37960270
00016717 00000-0 10270-3 0 9046
2 25544 51
6433 67
5984 0007379 286
6002 73
4338 15
50361369 24433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
37960270 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 67
5984 deg
Eccentricity:
0007379
Arg of perigee: 286
6002 deg
Mean anomaly: 73
4338 deg
Mean motion: 15
50361369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 323
Coasting Arc #6 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2019/228/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3360816
97 A = 6800411
21 meter
Y = -5902452
41 meter E =
0006403
Z = 235579
07 I = 52
00541
XDOT = 3996
216100 Wp = 158
71687
YDOT = -2517
952214 meter/sec RA = 61
89559 deg
ZDOT = -6031
209520 TA = 18
76218
MA = 18
73859
Ha = 225
637 n
mi
Hp = 223
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11026302
40 X = -3295708
56
Y = -19365001
35 feet Y = -5939671
39 meter
Z = 772897
22 Z = 219412
00
XDOT = 13110
945210 XDOT = 4053
371175
YDOT = -8260
998076 feet/sec YDOT = -2472
944163 meter/sec
ZDOT = -19787
432809 ZDOT = -6011
659008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17212252
35 X = -5246294
52
Y = 14157280
06 feet Y = 4315138
96 meter
Z = 699844
56 Z = 213312
62
XDOT = -9357
379131 XDOT = -2852
129159
YDOT = -10394
692218 feet/sec YDOT = -3168
302188 meter/sec
ZDOT = -19698
176496 ZDOT = -6004
004196
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 19228
41094684
00016717 00000-0 10270-3 0 9050
2 25544 51
6437 62
4869 0007319 289
5482 70
4878 15
50316650 24597
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
41094684 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 62
4869 deg
Eccentricity:
0007319
Arg of perigee: 289
5482 deg
Mean anomaly: 70
4878 deg
Mean motion: 15
50316650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2459
Checksum: 341
Coasting Arc #7 (Orbit 2474)
---------------------------------------
Vector Time (GMT): 2019/229/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3555022
79 A = 6800245
20 meter
Y = 5783515
44 meter E =
0011774
Z = 220831
29 I = 51
98872
XDOT = -4126
971340 Wp = 11
91423
YDOT = 2304
624457 meter/sec RA = 56
96482 deg
ZDOT = 6033
964279 TA = 350
45072
MA = 350
47308
Ha = 225
901 n
mi
Hp = 223
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11663460
61 X = 3489012
99
Y = 18974788
19 feet Y = 5822901
13 meter
Z = 724512
12 Z = 237939
48
XDOT = -13539
932217 XDOT = -4181
744660
YDOT = 7561
103861 feet/sec YDOT = 2258
167621 meter/sec
ZDOT = 19796
470731 ZDOT = 6013
784319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16465897
10 X = 5018805
44
Y = -14994501
80 feet Y = -4570324
15 meter
Z = 801851
99 Z = 244404
49
XDOT = 8887
644891 XDOT = 2708
954163
YDOT = 10820
791199 feet/sec YDOT = 3298
177158 meter/sec
ZDOT = 19704
369637 ZDOT = 6005
891865
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 19229
44228594
00016717 00000-0 10270-3 0 9064
2 25544 51
6437 57
3737 0007481 294
8078 65
2294 15
50373352 24758
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
44228594 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 57
3737 deg
Eccentricity:
0007481
Arg of perigee: 294
8078 deg
Mean anomaly: 65
2294 deg
Mean motion: 15
50373352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2475
Checksum: 336
Coasting Arc #8 (Orbit 2489)
---------------------------------------
Vector Time (GMT): 2019/230/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3726085
08 A = 6800210
39 meter
Y = -5643648
59 meter E =
0004585
Z = -683142
51 I = 51
96810
XDOT = 4290
896232 Wp = 176
93147
YDOT = -2109
392512 meter/sec RA = 52
03433 deg
ZDOT = -5983
936108 TA = 10
39930
MA = 10
38982
Ha = 226
090 n
mi
Hp = 223
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12224688
59 X = -3659380
98
Y = -18515907
46 feet Y = -5684943
35 meter
Z = -2241281
22 Z = -701079
96
XDOT = 14077
743542 XDOT = 4343
231326
YDOT = -6920
579108 feet/sec YDOT = -2061
116255 meter/sec
ZDOT = -19632
336311 ZDOT = -5962
965706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15644227
09 X = -4768360
42
Y = 15721634
83 feet Y = 4791954
30 meter
Z = -2322399
33 Z = -707867
32
XDOT = -8522
003119 XDOT = -2597
506551
YDOT = -11363
049491 feet/sec YDOT = -3463
457485 meter/sec
ZDOT = -19536
657653 ZDOT = -5954
773253
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 19230
40916955
00016717 00000-0 10270-3 0 9078
2 25544 51
6428 52
5815 0007402 297
7719 62
2681 15
50319198 24901
Satellite: ISS
Catalog Number: 25544
Epoch time: 19230
40916955 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 52
5815 deg
Eccentricity:
0007402
Arg of perigee: 297
7719 deg
Mean anomaly: 62
2681 deg
Mean motion: 15
50319198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2490
Checksum: 323
Coasting Arc #9 (Orbit 2505)
---------------------------------------
Vector Time (GMT): 2019/231/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3868429
80 A = 6799689
72 meter
Y = 5465896
28 meter E =
0012359
Z = 1132804
42 I = 51
94530
XDOT = -4489
394190 Wp = 24
14719
YDOT = 1952
366950 meter/sec RA = 47
10149 deg
ZDOT = 5898
811438 TA = 348
08231
MA = 348
11153
Ha = 226
222 n
mi
Hp = 222
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12691698
81 X = 3801518
59
Y = 17932730
58 feet Y = 5508781
70 meter
Z = 3716549
93 Z = 1151432
85
XDOT = -14728
983564 XDOT = -4539
545259
YDOT = 6405
403378 feet/sec YDOT = 1901
883194 meter/sec
ZDOT = 19353
055898 ZDOT = 5876
882034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14702028
75 X = 4481178
36
Y = -16305793
87 feet Y = -4970005
97 meter
Z = 3800818
96 Z = 1158489
62
XDOT = 8333
568065 XDOT = 2540
071546
YDOT = 12010
484906 feet/sec YDOT = 3660
795799 meter/sec
ZDOT = 19253
030232 ZDOT = 5868
323615
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 19231
44050835
00016717 00000-0 10270-3 0 9080
2 25544 51
6426 47
4690 0007532 301
8469 58
1948 15
50378293 25065
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
44050835 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 47
4690 deg
Eccentricity:
0007532
Arg of perigee: 301
8469 deg
Mean anomaly: 58
1948 deg
Mean motion: 15
50378293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2506
Checksum: 319
Coasting Arc #10 (Orbit 2520)
---------------------------------------
Vector Time (GMT): 2019/232/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3980953
39 A = 6799276
39 meter
Y = -5278109
45 meter E =
0002334
Z = -1582163
34 I = 51
92050
XDOT = 4707
663663 Wp = 215
44934
YDOT = -1823
779690 meter/sec RA = 42
16734 deg
ZDOT = -5758
619702 TA = 341
74907
MA = 341
75745
Ha = 226
462 n
mi
Hp = 222
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13060870
71 X = -3913950
97
Y = -17316632
07 feet Y = -5322252
70 meter
Z = -5190824
60 Z = -1601338
22
XDOT = 15445
090758 XDOT = 4755
679754
YDOT = -5983
529166 feet/sec YDOT = -1770
867020 meter/sec
ZDOT = -18893
109259 ZDOT = -5735
635141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13735767
55 X = -4186661
95
Y = 16759251
79 feet Y = 5108219
94 meter
Z = -5277586
50 Z = -1608608
36
XDOT = -8283
261391 XDOT = -2524
738072
YDOT = -12707
892003 feet/sec YDOT = -3873
365482 meter/sec
ZDOT = -18788
297393 ZDOT = -5726
673045
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 19232
40738983
00016717 00000-0 10270-3 0 9095
2 25544 51
6431 42
6767 0007623 305
1699 54
8737 15
50337632 25214
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
40738983 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 42
6767 deg
Eccentricity:
0007623
Arg of perigee: 305
1699 deg
Mean anomaly: 54
8737 deg
Mean motion: 15
50337632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2521
Checksum: 323
Coasting Arc #11 (Orbit 2536)
---------------------------------------
Vector Time (GMT): 2019/233/09:04:44
748
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052842
87 A = 6798481
66 meter
Y = 5062784
85 meter E =
0012101
Z = 2013242
44 I = 51
89212
XDOT = -4952
570968 Wp = 35
25480
YDOT = 1740
145842 meter/sec RA = 37
22991 deg
ZDOT = 5586
871300 TA = 346
88045
MA = 346
91190
Ha = 226
552 n
mi
Hp = 222
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13296728
58 X = 3986148
97
Y = 16610186
51 feet Y = 5107733
74 meter
Z = 6605126
12 Z = 2032767
40
XDOT = -16248
592415 XDOT = -4998
799478
YDOT = 5709
139903 feet/sec YDOT = 1684
504390 meter/sec
ZDOT = 18329
630250 ZDOT = 5562
701359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12704786
02 X = 3872418
78
Y = -17032750
50 feet Y = -5191582
35 meter
Z = 6693489
39 Z = 2040175
57
XDOT = 8435
185494 XDOT = 2571
044539
YDOT = 13460
688714 feet/sec YDOT = 4102
817920 meter/sec
ZDOT = 18219
435861 ZDOT = 5553
284051
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 19233
43872599
00016717 00000-0 10270-3 0 9103
2 25544 51
6424 37
5634 0007622 309
3841 50
6635 15
50383847 25373
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
43872599 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 37
5634 deg
Eccentricity:
0007622
Arg of perigee: 309
3841 deg
Mean anomaly: 50
6635 deg
Mean motion: 15
50383847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2537
Checksum: 320
Coasting Arc #12 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2019/234/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4394322
04 A = 6798598
51 meter
Y = 4775973
54 meter E =
0012724
Z = 1996721
23 I = 51
87110
XDOT = -4811
250248 Wp = 35
97342
YDOT = 2085
244572 meter/sec RA = 33
40878 deg
ZDOT = 5592
709232 TA = 345
97825
MA = 346
01354
Ha = 226
766 n
mi
Hp = 222
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14417067
05 X = 4330890
20
Y = 15669204
54 feet Y = 4824759
31 meter
Z = 6550922
66 Z = 2017912
97
XDOT = -15784
941759 XDOT = -4861
376659
YDOT = 6841
353582 feet/sec YDOT = 2031
161615 meter/sec
ZDOT = 18348
783570 ZDOT = 5569
216274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19490293
41 X = 5940641
43
Y = 8499275
16 feet Y = 2590579
07 meter
Z = 6646891
40 Z = 2025972
50
XDOT = -11149
670293 XDOT = -3398
419505
YDOT = 11281
858444 feet/sec YDOT = 3438
710454 meter/sec
ZDOT = 18241
639009 ZDOT = 5560
051570
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 19234
21223213
00016717 00000-0 10270-3 0 9114
2 25544 51
6422 33
7303 0007482 314
0264 46
0270 15
50352274 25495
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
21223213 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 33
7303 deg
Eccentricity:
0007482
Arg of perigee: 314
0264 deg
Mean anomaly: 46
0270 deg
Mean motion: 15
50352274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 263
Coasting Arc #13 (Orbit 2563)
---------------------------------------
Vector Time (GMT): 2019/235/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4421387
44 A = 6797761
49 meter
Y = -4561750
03 meter E =
0002168
Z = -2421186
33 I = 51
84098
XDOT = 5059
852526 Wp = 329
60608
YDOT = -2053
523181 meter/sec RA = 28
46935 deg
ZDOT = -5366
960159 TA = 237
32526
MA = 237
34617
Ha = 226
929 n
mi
Hp = 222
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14505864
32 X = -4358287
28
Y = -14966371
48 feet Y = -4610840
28 meter
Z = -7943524
72 Z = -2442510
46
XDOT = 16600
566030 XDOT = 5108
509203
YDOT = -6737
280778 feet/sec YDOT = -1996
668303 meter/sec
ZDOT = -17608
137004 ZDOT = -5342
263172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19409798
64 X = -5916106
62
Y = -7491887
75 feet Y = -2283527
39 meter
Z = -8040105
39 Z = -2450624
12
XDOT = 11781
998962 XDOT = 3591
153284
YDOT = -11735
115519 feet/sec YDOT = -3576
863210 meter/sec
ZDOT = -17495
519333 ZDOT = -5332
634293
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 19235
17911048
00016717 00000-0 10270-3 0 9121
2 25544 51
6432 28
9384 0007538 317
2505 42
8059 15
50363291 25643
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
17911048 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 28
9384 deg
Eccentricity:
0007538
Arg of perigee: 317
2505 deg
Mean anomaly: 42
8059 deg
Mean motion: 15
50363291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 308
Coasting Arc #14 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2019/235/16:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4294930
95 A = 6790568
07 meter
Y = -2130491
44 meter E =
0005886
Z = -4813137
66 I = 51
80170
XDOT = 5322
221636 Wp = 72
96750
YDOT = 4850
664421 meter/sec RA = 25
79855 deg
ZDOT = 2606
416342 TA = 222
67243
MA = 222
71816
Ha = 226
876 n
mi
Hp = 222
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14090980
81 X = 4341815
00
Y = -6989801
32 feet Y = -2082200
32 meter
Z = -15791134
04 Z = -4792160
69
XDOT = 17461
357073 XDOT = 5254
924063
YDOT = 15914
253350 feet/sec YDOT = 4909
804946 meter/sec
ZDOT = 8551
234718 ZDOT = 2632
106210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7184495
16 X = -2189834
12
Y = 14099969
49 feet Y = 4297670
70 meter
Z = -15695440
95 Z = -4783970
40
XDOT = -22439
892724 XDOT = -6839
679302
YDOT = -1801
439990 feet/sec YDOT = -549
078909 meter/sec
ZDOT = 8667
648609 ZDOT = 2641
899296
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 19235
69477706
00016717 00000-0 10270-3 0 9137
2 25544 51
6436 26
3805 0007259 316
3685 43
6899 15
50388301 25725
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
69477706 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 26
3805 deg
Eccentricity:
0007259
Arg of perigee: 316
3685 deg
Mean anomaly: 43
6899 deg
Mean motion: 15
50388301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 336
Coasting Arc #15 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2019/236/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3504731
95 A = 6789407
05 meter
Y = 2847534
16 meter E =
0009119
Z = 5072797
11 I = 51
78264
XDOT = -6124
777911 Wp = 357
97306
YDOT = -4206
467947 meter/sec RA = 23
10347 deg
ZDOT = -1861
513572 TA = 110
09431
MA = 109
99616
Ha = 227
101 n
mi
Hp = 221
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11498464
39 X = -3560954
16
Y = 9342303
69 feet Y = 2808027
35 meter
Z = 16643035
13 Z = 5055635
99
XDOT = -20094
415717 XDOT = -6068
242602
YDOT = -13800
747857 feet/sec YDOT = -4274
643385 meter/sec
ZDOT = -6107
327992 ZDOT = -1891
128096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 752131
40 X = 229249
65
Y = 14883921
94 feet Y = 4536619
41 meter
Z = 16564634
19 Z = 5048900
50
XDOT = -21857
165165 XDOT = -6662
063942
YDOT = 8083
220654 feet/sec YDOT = 2463
765655 meter/sec
ZDOT = -6241
664756 ZDOT = -1902
459418
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 19236
27490198
00016717 00000-0 10270-3 0 9143
2 25544 51
6447 23
5078 0007729 320
3660 39
6925 15
50409068 25817
Satellite: ISS
Catalog Number: 25544
Epoch time: 19236
27490198 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 23
5078 deg
Eccentricity:
0007729
Arg of perigee: 320
3660 deg
Mean anomaly: 39
6925 deg
Mean motion: 15
50409068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 324
Coasting Arc #16 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2019/237/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3718989
69 A = 6790164
31 meter
Y = -2857773
29 meter E =
0007455
Z = -4914972
74 I = 51
75322
XDOT = 6126
217749 Wp = 67
64035
YDOT = 3952
281698 meter/sec RA = 18
15291 deg
ZDOT = 2343
081063 TA = 225
25907
MA = 225
31978
Ha = 227
318 n
mi
Hp = 221
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12201409
74 X = 3774543
79
Y = -9375896
62 feet Y = -2815874
17 meter
Z = -16125238
65 Z = -4896772
55
XDOT = 20099
139598 XDOT = 6070
185569
YDOT = 12966
803470 feet/sec YDOT = 4020
476013 meter/sec
ZDOT = 7687
273829 ZDOT = 2372
703771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -634898
68 X = -193517
12
Y = -15461332
87 feet Y = -4712614
26 meter
Z = -16042108
60 Z = -4889634
70
XDOT = 20984
797931 XDOT = 6396
166410
YDOT = -8957
993992 feet/sec YDOT = -2730
396569 meter/sec
ZDOT = 7821
665209 ZDOT = 2384
043556
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 19237
24177808
00016717 00000-0 10270-3 0 9152
2 25544 51
6442 18
7151 0007713 324
7281 35
3359 15
50379372 25964
Satellite: ISS
Catalog Number: 25544
Epoch time: 19237
24177808 = yrday
fracday
Element set: 915
Inclination: 51
6442 deg
RA of node: 18
7151 deg
Eccentricity:
0007713
Arg of perigee: 324
7281 deg
Mean anomaly: 35
3359 deg
Mean motion: 15
50379372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 320
Coasting Arc #17 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2019/238/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3959943
07 A = 6790922
37 meter
Y = 2884386
12 meter E =
0010652
Z = 4704780
65 I = 51
72340
XDOT = -6074
588572 Wp = 16
76622
YDOT = -3714
050800 meter/sec RA = 13
20106 deg
ZDOT = -2824
342437 TA = 101
30822
MA = 101
18850
Ha = 227
428 n
mi
Hp = 221
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12991939
21 X = -4014755
78
Y = 9463209
06 feet Y = 2839796
62 meter
Z = 15435632
07 Z = 4685411
89
XDOT = -19929
752533 XDOT = -6018
886562
YDOT = -12185
206036 feet/sec YDOT = -3781
669581 meter/sec
ZDOT = -9266
215343 ZDOT = -2853
715051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 534129
58 X = 162802
69
Y = 16148691
19 feet Y = 4922121
07 meter
Z = 15347183
00 Z = 4677821
38
XDOT = -20027
763133 XDOT = -6104
462203
YDOT = 9631
626626 feet/sec YDOT = 2935
719796 meter/sec
ZDOT = -9399
487377 ZDOT = -2864
963752
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 19238
27310990
00016717 00000-0 10270-3 0 9168
2 25544 51
6436 13
6033 0007821 328
2914 31
7765 15
50412467 26125
Satellite: ISS
Catalog Number: 25544
Epoch time: 19238
27310990 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 13
6033 deg
Eccentricity:
0007821
Arg of perigee: 328
2914 deg
Mean anomaly: 31
7765 deg
Mean motion: 15
50412467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 297
Coasting Arc #18 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2019/239/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952598
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4158332
07 A = 6791900
35 meter
Y = -2970118
44 meter E =
0006094
Z = -4476166
82 I = 51
69349
XDOT = 5992
250907 Wp = 53
20606
YDOT = 3476
115762 meter/sec RA = 8
24716 deg
ZDOT = 3266
865211 TA = 249
68710
MA = 249
75259
Ha = 227
607 n
mi
Hp = 221
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13642821
75 X = 4212978
16
Y = -9744483
06 feet Y = -2923311
38 meter
Z = -14685586
67 Z = -4455834
84
XDOT = 19659
615837 XDOT = 5937
066237
YDOT = 11404
579273 feet/sec YDOT = 3542
816685 meter/sec
ZDOT = 10718
061717 ZDOT = 3295
838963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -696241
65 X = -212214
46
Y = -16831961
42 feet Y = -5130381
84 meter
Z = -14592748
67 Z = -4447869
79
XDOT = 19001
306174 XDOT = 5791
598122
YDOT = -10173
145309 feet/sec YDOT = -3100
774690 meter/sec
ZDOT = 10849
539817 ZDOT = 3306
939736
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 19239
23998500
00016717 00000-0 10270-3 0 9175
2 25544 51
6435 8
8105 0007789 331
4569 28
6155 15
50379133 26271
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
23998500 = yrday
fracday
Element set: 917
Inclination: 51
6435 deg
RA of node: 8
8105 deg
Eccentricity:
0007789
Arg of perigee: 331
4569 deg
Mean anomaly: 28
6155 deg
Mean motion: 15
50379133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 330
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