[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 17th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
107/20:46:03
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
3
109/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
4
114/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
2
116/09:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
5
118/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
4
118/11:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 581)
---------------------------------------
Vector Time (GMT): 2019/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3197009
99 A = 6782054
96 meter
Y = -2850428
47 meter E =
0014323
Z = -5270867
82 I = 51
29417
XDOT = 4476
154759 Wp = 99
64607
YDOT = -6178
816131 meter/sec RA = 302
15391 deg
ZDOT = 625
559191 TA = 176
36979
MA = 176
35939
Ha = 223
334 n
mi
Hp = 217
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10488877
93 X = -3139295
00
Y = -9351799
44 feet Y = -2885857
40 meter
Z = -17292873
43 Z = -5286257
37
XDOT = 14685
547109 XDOT = 4541
876725
YDOT = -20271
706466 feet/sec YDOT = -6128
393109 meter/sec
ZDOT = 2052
359551 ZDOT = 647
462914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13313337
14 X = -4057905
16
Y = -4222279
68 feet Y = -1286950
85 meter
Z = -17362131
00 Z = -5291977
53
XDOT = 4660
028080 XDOT = 1420
376559
YDOT = -23554
838096 feet/sec YDOT = -7179
514652 meter/sec
ZDOT = 2152
026208 ZDOT = 655
937588
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 19107
51498939
00016717 00000-0 10270-3 0 9003
2 25544 51
6369 302
8076 0001260 201
8913 158
2185 15
52565965 5825
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
51498939 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 302
8076 deg
Eccentricity:
0001260
Arg of perigee: 201
8913 deg
Mean anomaly: 158
2185 deg
Mean motion: 15
52565965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 582
Checksum: 322
Coasting Arc #2 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2019/107/20:46:03
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1908313
93 A = 6792354
63 meter
Y = 6235553
02 meter E =
0014035
Z = 1874535
65 I = 51
32495
XDOT = -5240
993928 Wp = 118
71763
YDOT = 86
432376 meter/sec RA = 300
31867 deg
ZDOT = -5597
643508 TA = 40
55778
MA = 40
45329
Ha = 223
291 n
mi
Hp = 217
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6260872
46 X = -1987005
34
Y = 20457851
11 feet Y = 6213773
08 meter
Z = 6150051
35 Z = 1865074
08
XDOT = -17194
861970 XDOT = -5214
380479
YDOT = 283
570786 feet/sec YDOT = 27
972260 meter/sec
ZDOT = -18364
972138 ZDOT = -5623
037838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13988883
13 X = 4263811
58
Y = -16203876
99 feet Y = -4938941
71 meter
Z = 6106623
20 Z = 1861298
75
XDOT = 14565
494382 XDOT = 4439
562688
YDOT = 5578
632898 feet/sec YDOT = 1700
367307 meter/sec
ZDOT = -18479
763462 ZDOT = -5632
631903
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 19107
90119169
00016717 00000-0 10270-3 0 9012
2 25544 51
6396 300
8881 0001322 202
3049 157
8045 15
52585656 5887
Satellite: ISS
Catalog Number: 25544
Epoch time: 19107
90119169 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 300
8881 deg
Eccentricity:
0001322
Arg of perigee: 202
3049 deg
Mean anomaly: 157
8045 deg
Mean motion: 15
52585656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 313
Coasting Arc #3 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2019/108/20:46:03
000
Vector Time (MET): N/A
Weight (LBS) : 930220
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2347743
10 A = 6793772
37 meter
Y = -6328731
96 meter E =
0009243
Z = -731535
10 I = 51
31246
XDOT = 4739
441511 Wp = 41
55426
YDOT = 1078
980784 meter/sec RA = 295
33177 deg
ZDOT = 5925
835261 TA = 310
51183
MA = 310
59232
Ha = 223
349 n
mi
Hp = 217
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7702569
21 X = 2421891
72
Y = -20763556
29 feet Y = -6302063
31 meter
Z = -2400049
54 Z = -719949
94
XDOT = 15549
348788 XDOT = 4698
239029
YDOT = 3539
963201 feet/sec YDOT = 1131
750598 meter/sec
ZDOT = 19441
716737 ZDOT = 5948
757813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15132789
27 X = -4612474
17
Y = 16177306
33 feet Y = 4930842
97 meter
Z = -2347025
59 Z = -715373
40
XDOT = -11678
500823 XDOT = -3559
607051
YDOT = -8113
128159 feet/sec YDOT = -2472
881463 meter/sec
ZDOT = 19545
208980 ZDOT = 5957
379697
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 19108
86669675
00016717 00000-0 10270-3 0 9021
2 25544 51
6387 296
0863 0001281 208
3269 151
7814 15
52525619 6035
Satellite: ISS
Catalog Number: 25544
Epoch time: 19108
86669675 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 296
0863 deg
Eccentricity:
0001281
Arg of perigee: 208
3269 deg
Mean anomaly: 151
7814 deg
Mean motion: 15
52525619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 330
Coasting Arc #4 (Orbit 611)
---------------------------------------
Vector Time (GMT): 2019/109/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4331397
83 A = 6782334
83 meter
Y = 448853
51 meter E =
0003887
Z = 5198086
47 I = 51
26856
XDOT = -2088
501118 Wp = 140
05403
YDOT = 7294
202842 meter/sec RA = 292
69807 deg
ZDOT = 1107
037063 TA = 299
26081
MA = 299
29966
Ha = 223
098 n
mi
Hp = 217
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14210622
81 X = 4300806
93
Y = 1472616
50 feet Y = 497119
53 meter
Z = 17054089
47 Z = 5219052
74
XDOT = -6852
037788 XDOT = -2175
289194
YDOT = 23931
111687 feet/sec YDOT = 7270
362570 meter/sec
ZDOT = 3632
011361 ZDOT = 1096
680494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13542273
82 X = 4127685
06
Y = 4180633
20 feet Y = 1274257
00 meter
Z = 17148804
43 Z = 5226955
59
XDOT = -11083
803088 XDOT = -3378
343181
YDOT = 21154
979738 feet/sec YDOT = 6448
037824 meter/sec
ZDOT = 3584
445681 ZDOT = 1092
539043
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 19109
44599842
00016717 00000-0 10270-3 0 9035
2 25544 51
6401 293
2065 0001146 217
6843 142
4229 15
52552829 6126
Satellite: ISS
Catalog Number: 25544
Epoch time: 19109
44599842 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 293
2065 deg
Eccentricity:
0001146
Arg of perigee: 217
6843 deg
Mean anomaly: 142
4229 deg
Mean motion: 15
52552829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 612
Checksum: 305
Coasting Arc #5 (Orbit 626)
---------------------------------------
Vector Time (GMT): 2019/110/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3961641
67 A = 6781875
83 meter
Y = -1555274
12 meter E =
0014059
Z = -5292410
59 I = 51
25472
XDOT = 2510
566608 Wp = 95
23198
YDOT = -7228
209558 meter/sec RA = 287
68636 deg
ZDOT = 244
160668 TA = 177
11564
MA = 177
10752
Ha = 223
147 n
mi
Hp = 217
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12997512
04 X = -3918247
69
Y = -5102605
37 feet Y = -1599333
56 meter
Z = -17363551
81 Z = -5311549
62
XDOT = 8236
767088 XDOT = 2590
021895
YDOT = -23714
598289 feet/sec YDOT = -7199
690373 meter/sec
ZDOT = 801
052061 ZDOT = 256
549550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11773306
89 X = -3588503
94
Y = -7304470
06 feet Y = -2226402
47 meter
Z = -17449893
81 Z = -5318727
63
XDOT = 11768
623457 XDOT = 3587
076430
YDOT = -21023
228514 feet/sec YDOT = -6407
880051 meter/sec
ZDOT = 857
786270 ZDOT = 261
453255
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 19110
41149768
00016717 00000-0 10270-3 0 9043
2 25544 51
6393 288
4027 0001141 225
9766 134
1292 15
52585861 6277
Satellite: ISS
Catalog Number: 25544
Epoch time: 19110
41149768 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 288
4027 deg
Eccentricity:
0001141
Arg of perigee: 225
9766 deg
Mean anomaly: 134
1292 deg
Mean motion: 15
52585861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 627
Checksum: 314
Coasting Arc #6 (Orbit 642)
---------------------------------------
Vector Time (GMT): 2019/111/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598638
12 A = 6782712
88 meter
Y = 2651478
79 meter E =
0003784
Z = 5099181
77 I = 51
24824
XDOT = -2862
414925 Wp = 56
71569
YDOT = 6935
175913 meter/sec RA = 282
67674 deg
ZDOT = -1583
177686 TA = 48
65262
MA = 48
62007
Ha = 223
001 n
mi
Hp = 217
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11806555
51 X = 3543951
66
Y = 8699077
41 feet Y = 2691415
59 meter
Z = 16729598
99 Z = 5116530
04
XDOT = -9391
125083 XDOT = -2932
062965
YDOT = 22753
201814 feet/sec YDOT = 6902
776936 meter/sec
ZDOT = -5194
152514 ZDOT = -1597
251726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10149842
39 X = 3093671
96
Y = 10460822
16 feet Y = 3188458
60 meter
Z = 16807738
76 Z = 5122998
77
XDOT = -12116
600514 XDOT = -3693
139837
YDOT = 20220
535485 feet/sec YDOT = 6163
219216 meter/sec
ZDOT = -5258
464914 ZDOT = -1602
780106
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 19111
44136280
00016717 00000-0 10270-3 0 9053
2 25544 51
6391 283
2811 0001167 229
0500 131
0551 15
52579332 6436
Satellite: ISS
Catalog Number: 25544
Epoch time: 19111
44136280 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 283
2811 deg
Eccentricity:
0001167
Arg of perigee: 229
0500 deg
Mean anomaly: 131
0551 deg
Mean motion: 15
52579332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 643
Checksum: 273
Coasting Arc #7 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2019/112/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3278189
00 A = 6784558
24 meter
Y = -3693850
79 meter E =
0010011
Z = -4661680
18 I = 51
24731
XDOT = 3154
144724 Wp = 115
39956
YDOT = -6375
761227 meter/sec RA = 277
66797 deg
ZDOT = 2834
578287 TA = 182
93598
MA = 182
94186
Ha = 223
086 n
mi
Hp = 217
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10755213
24 X = -3213995
47
Y = -12118933
05 feet Y = -3730150
82 meter
Z = -15294226
30 Z = -4677448
75
XDOT = 10348
243844 XDOT = 3211
436862
YDOT = -20917
851793 feet/sec YDOT = -6340
169060 meter/sec
ZDOT = 9299
797531 ZDOT = 2850
039263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8807743
15 X = -2684600
11
Y = -13520096
78 feet Y = -4120925
50 meter
Z = -15365127
79 Z = -4683290
95
XDOT = 12188
291925 XDOT = 3714
991379
YDOT = -18587
049099 feet/sec YDOT = -5665
332565 meter/sec
ZDOT = 9370
315141 ZDOT = 2856
072055
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 19112
40686029
00016717 00000-0 10270-3 0 9062
2 25544 51
6382 278
4784 0001244 232
3030 127
8009 15
52583945 6584
Satellite: ISS
Catalog Number: 25544
Epoch time: 19112
40686029 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 278
4784 deg
Eccentricity:
0001244
Arg of perigee: 232
3030 deg
Mean anomaly: 127
8009 deg
Mean motion: 15
52583945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 310
Coasting Arc #8 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2019/113/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2969623
00 A = 6787036
85 meter
Y = 4633373
78 meter E =
0009686
Z = 3964846
68 I = 51
25345
XDOT = -3438
442192 Wp = 81
16404
YDOT = 5597
311361 meter/sec RA = 272
66357 deg
ZDOT = -3955
972834 TA = 50
29001
MA = 50
20467
Ha = 222
899 n
mi
Hp = 217
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9742857
61 X = 2898331
34
Y = 15201357
53 feet Y = 4666183
46 meter
Z = 13008027
17 Z = 3979099
13
XDOT = -11280
978319 XDOT = -3481
561221
YDOT = 18363
882418 feet/sec YDOT = 5558
619302 meter/sec
ZDOT = -12978
913498 ZDOT = -3972
780281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7661235
01 X = 2335144
43
Y = 16298521
55 feet Y = 4967789
37 meter
Z = 13071992
56 Z = 3984343
33
XDOT = -12231
663592 XDOT = -3728
211063
YDOT = 16246
080836 feet/sec YDOT = 4951
805439 meter/sec
ZDOT = -13055
433674 ZDOT = -3979
296184
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 19113
43672022
00016717 00000-0 10270-3 0 9075
2 25544 51
6392 273
3560 0001286 244
4783 115
6236 15
52605276 6743
Satellite: ISS
Catalog Number: 25544
Epoch time: 19113
43672022 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 273
3560 deg
Eccentricity:
0001286
Arg of perigee: 244
4783 deg
Mean anomaly: 115
6236 deg
Mean motion: 15
52605276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 302
Coasting Arc #9 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2019/114/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2698070
44 A = 6789751
54 meter
Y = -5414555
03 meter E =
0003413
Z = -3085043
65 I = 51
25999
XDOT = 3712
789552 Wp = 80
31891
YDOT = -4615
253731 meter/sec RA = 267
66392 deg
ZDOT = 4858
325724 TA = 244
05871
MA = 244
09388
Ha = 223
068 n
mi
Hp = 217
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8851937
14 X = -2622337
27
Y = -17764288
16 feet Y = -5444303
19 meter
Z = -10121534
29 Z = -3097966
20
XDOT = 12181
068085 XDOT = 3740
523448
YDOT = -15141
908567 feet/sec YDOT = -4573
579803 meter/sec
ZDOT = 15939
388857 ZDOT = 4876
428429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6794678
04 X = -2071017
87
Y = -18616762
11 feet Y = -5674389
09 meter
Z = -10179425
33 Z = -3102688
84
XDOT = 12295
239377 XDOT = 3747
588962
YDOT = -13238
694361 feet/sec YDOT = -4035
154041 meter/sec
ZDOT = 16021
663120 ZDOT = 4883
402919
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 19114
40221366
00016717 00000-0 10270-3 0 9085
2 25544 51
6373 268
5535 0001170 237
6162 122
4877 15
52582846 6897
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
40221366 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 268
5535 deg
Eccentricity:
0001170
Arg of perigee: 237
6162 deg
Mean anomaly: 122
4877 deg
Mean motion: 15
52582846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 316
Coasting Arc #10 (Orbit 689)
---------------------------------------
Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4042682
12 A = 6782568
83 meter
Y = 1853082
57 meter E =
0012871
Z = -5132633
36 I = 51
23596
XDOT = -1510
208952 Wp = 81
60701
YDOT = -7360
606928 meter/sec RA = 267
43914 deg
ZDOT = -1469
293478 TA = 174
15245
MA = 174
13741
Ha = 223
168 n
mi
Hp = 217
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13263392
78 X = -4038171
67
Y = 6079667
24 feet Y = 1807899
85 meter
Z = -16839348
30 Z = -5152260
34
XDOT = -4954
753780 XDOT = -1420
651242
YDOT = -24148
972861 feet/sec YDOT = -7376
994347 meter/sec
ZDOT = -4820
516659 ZDOT = -1476
412276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11516471
56 X = -3510220
53
Y = 8789138
07 feet Y = 2678929
28 meter
Z = -16928246
44 Z = -5159729
52
XDOT = -9408
132140 XDOT = -2867
598676
YDOT = -21664
310941 feet/sec YDOT = -6603
281975 meter/sec
ZDOT = -4851
986266 ZDOT = -1478
885414
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 19114
46658098
00016717 00000-0 10270-3 0 9098
2 25544 51
6372 268
2325 0001076 222
6869 137
4199 15
52588548 6903
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
46658098 = yrday
fracday
Element set: 909
Inclination: 51
6372 deg
RA of node: 268
2325 deg
Eccentricity:
0001076
Arg of perigee: 222
6869 deg
Mean anomaly: 137
4199 deg
Mean motion: 15
52588548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 690
Checksum: 345
Coasting Arc #11 (Orbit 705)
---------------------------------------
Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4188624
16 A = 6781975
10 meter
Y = -702896
35 meter E =
0001920
Z = 5285995
67 I = 51
23509
XDOT = 1111
320936 Wp = 121
84768
YDOT = 7585
596656 meter/sec RA = 262
42766 deg
ZDOT = 127
040604 TA = 326
92874
MA = 326
94075
Ha = 223
066 n
mi
Hp = 217
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13742205
24 X = 4170496
28
Y = -2306090
40 feet Y = -656157
73 meter
Z = 17342505
48 Z = 5306298
49
XDOT = 3646
066063 XDOT = 1025
796946
YDOT = 24887
128138 feet/sec YDOT = 7597
546027 meter/sec
ZDOT = 416
799883 ZDOT = 132
231500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12708520
37 X = 3873557
01
Y = -5428224
74 feet Y = -1654522
90 meter
Z = 17434352
31 Z = 5313990
58
XDOT = 8967
758648 XDOT = 2733
372836
YDOT = 22417
800281 feet/sec YDOT = 6832
945526 meter/sec
ZDOT = 439
551162 ZDOT = 133
975194
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 19115
49643898
00016717 00000-0 10270-3 0 9106
2 25544 51
6361 263
1101 0001083 227
0482 133
0579 15
52542608 7064
Satellite: ISS
Catalog Number: 25544
Epoch time: 19115
49643898 = yrday
fracday
Element set: 910
Inclination: 51
6361 deg
RA of node: 263
1101 deg
Eccentricity:
0001083
Arg of perigee: 227
0482 deg
Mean anomaly: 133
0579 deg
Mean motion: 15
52542608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 706
Checksum: 294
Coasting Arc #12 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2019/116/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4082831
17 A = 6781972
81 meter
Y = -1183107
88 meter E =
0001848
Z = 5283220
18 I = 51
24079
XDOT = 1837
086458 Wp = 125
16262
YDOT = 7440
142188 meter/sec RA = 257
60293 deg
ZDOT = 245
328632 TA = 322
47933
MA = 322
49223
Ha = 222
995 n
mi
Hp = 217
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13395115
38 X = 4070094
55
Y = -3881587
55 feet Y = -1137522
13 meter
Z = 17333399
54 Z = 5303022
14
XDOT = 6027
186541 XDOT = 1752
560462
YDOT = 24409
915315 feet/sec YDOT = 7460
213155 meter/sec
ZDOT = 804
883963 ZDOT = 254
047381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13136737
56 X = 4004077
61
Y = -4336669
99 feet Y = -1321817
01 meter
Z = 17423030
65 Z = 5310539
74
XDOT = 6544
805406 XDOT = 1994
856688
YDOT = 23229
513897 feet/sec YDOT = 7080
355836 meter/sec
ZDOT = 843
616486 ZDOT = 257
134305
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 19116
46192637
00016717 00000-0 10270-3 0 9115
2 25544 51
6365 258
3086 0001087 240
1379 119
9665 15
52548885 7210
Satellite: ISS
Catalog Number: 25544
Epoch time: 19116
46192637 = yrday
fracday
Element set: 911
Inclination: 51
6365 deg
RA of node: 258
3086 deg
Eccentricity:
0001087
Arg of perigee: 240
1379 deg
Mean anomaly: 119
9665 deg
Mean motion: 15
52548885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 329
Coasting Arc #13 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2019/117/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4363461
18 A = 6782213
72 meter
Y = 42874
79 meter E =
0013491
Z = -5203938
41 I = 51
25115
XDOT = -1399
127455 Wp = 101
42030
YDOT = -7444
445660 meter/sec RA = 252
59180 deg
ZDOT = 1111
660798 TA = 179
31068
MA = 179
30882
Ha = 223
102 n
mi
Hp = 217
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14315817
52 X = -4338338
42
Y = 140665
31 feet Y = -5779
98 meter
Z = -17073288
74 Z = -5225073
49
XDOT = -4590
313173 XDOT = -1321
177402
YDOT = -24424
034318 feet/sec YDOT = -7459
655846 meter/sec
ZDOT = 3647
181095 ZDOT = 1105
053612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14174862
03 X = -4320497
95
Y = 873808
24 feet Y = 266336
75 meter
Z = -17168848
30 Z = -5233064
96
XDOT = -5807
953492 XDOT = -1770
264224
YDOT = -23118
786942 feet/sec YDOT = -7046
606260 meter/sec
ZDOT = 3617
974618 ZDOT = 1102
758664
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 19117
42741031
00016717 00000-0 10270-3 0 9121
2 25544 51
6373 253
5065 0001003 237
2576 122
8480 15
52600472 7362
Satellite: ISS
Catalog Number: 25544
Epoch time: 19117
42741031 = yrday
fracday
Element set: 912
Inclination: 51
6373 deg
RA of node: 253
5065 deg
Eccentricity:
0001003
Arg of perigee: 237
2576 deg
Mean anomaly: 122
8480 deg
Mean motion: 15
52600472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 277
Coasting Arc #14 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2019/118/09:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 945825
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4633590
65 A = 6783839
63 meter
Y = 1057476
94 meter E =
0005917
Z = 4837365
79 I = 51
26594
XDOT = 881
424371 Wp = 59
77553
YDOT = 7223
140945 meter/sec RA = 247
58309 deg
ZDOT = -2418
165163 TA = 54
09762
MA = 54
04271
Ha = 222
999 n
mi
Hp = 217
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15202069
05 X = 4597923
97
Y = 3469412
53 feet Y = 1109093
58 meter
Z = 15870622
68 Z = 4859787
46
XDOT = 2891
812240 XDOT = 812
333777
YDOT = 23697
968979 feet/sec YDOT = 7232
611332 meter/sec
ZDOT = -7933
612740 ZDOT = -2414
051355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15298591
91 X = 4663010
81
Y = 2422305
96 feet Y = 738318
86 meter
Z = 15971910
04 Z = 4868238
18
XDOT = 4747
086551 XDOT = 1446
911981
YDOT = 22322
671693 feet/sec YDOT = 6803
950332 meter/sec
ZDOT = -7915
640325 ZDOT = -2412
687171
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 19118
45725952
00016717 00000-0 10270-3 0 9130
2 25544 51
6360 248
3839 0001020 238
7577 121
3475 15
52563401 7521
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
45725952 = yrday
fracday
Element set: 913
Inclination: 51
6360 deg
RA of node: 248
3839 deg
Eccentricity:
0001020
Arg of perigee: 238
7577 deg
Mean anomaly: 121
3475 deg
Mean motion: 15
52563401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 305
Coasting Arc #15 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2171610
60 A = 6793612
83 meter
Y = -6405536
03 meter E =
0011894
Z = 572843
86 I = 51
30166
XDOT = 4719
406128 Wp = 50
78071
YDOT = -1061
315959 meter/sec RA = 247
38181 deg
ZDOT = 5947
542146 TA = 315
42701
MA = 315
52261
Ha = 223
049 n
mi
Hp = 217
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7124706
69 X = -2102603
24
Y = -21015538
15 feet Y = -6429434
65 meter
Z = 1879409
00 Z = 562462
60
XDOT = 15483
615905 XDOT = 4702
033380
YDOT = -3482
007739 feet/sec YDOT = -1008
637370 meter/sec
ZDOT = 19512
933549 ZDOT = 5970
425118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13968221
10 X = -4257513
79
Y = -17247471
71 feet Y = -5257029
38 meter
Z = 1833026
46 Z = 558706
46
XDOT = 11941
936231 XDOT = 3639
902163
YDOT = -7559
536172 feet/sec YDOT = -2304
146625 meter/sec
ZDOT = 19616
490956 ZDOT = 5979
106443
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 19118
52162368
00016717 00000-0 10270-3 0 9145
2 25544 51
6381 248
0637 0001135 235
6031 124
5014 15
52611332 7537
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52162368 = yrday
fracday
Element set: 914
Inclination: 51
6381 deg
RA of node: 248
0637 deg
Eccentricity:
0001135
Arg of perigee: 235
6031 deg
Mean anomaly: 124
5014 deg
Mean motion: 15
52611332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 276
Coasting Arc #16 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4517107
93 A = 6788924
95 meter
Y = 3770520
43 meter E =
0011464
Z = 3375789
91 I = 51
28592
XDOT = -1509
191715 Wp = 93
63635
YDOT = 5942
867879 meter/sec RA = 247
23136 deg
ZDOT = -4605
479259 TA = 46
73755
MA = 46
64195
Ha = 223
001 n
mi
Hp = 217
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14819907
89 X = 4458211
42
Y = 12370473
84 feet Y = 3820704
59 meter
Z = 11075426
21 Z = 3397589
32
XDOT = -4951
416387 XDOT = -1553
163471
YDOT = 19497
598029 feet/sec YDOT = 5925
745161 meter/sec
ZDOT = -15109
840089 ZDOT = -4612
917189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18887398
79 X = 5756879
15
Y = 3706579
69 feet Y = 1129765
49 meter
Z = 11173665
15 Z = 3405733
14
XDOT = 5444
355152 XDOT = 1659
439450
YDOT = 18035
818738 feet/sec YDOT = 5497
317551 meter/sec
ZDOT = -15143
986457 ZDOT = -4615
887072
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 19118
52162464
00016717 00000-0 10270-3 0 9153
2 25544 51
6379 248
0637 0001183 235
9063 124
1976 15
52579587 7533
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52162464 = yrday
fracday
Element set: 915
Inclination: 51
6379 deg
RA of node: 248
0637 deg
Eccentricity:
0001183
Arg of perigee: 235
9063 deg
Mean anomaly: 124
1976 deg
Mean motion: 15
52579587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 330
Coasting Arc #17 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4511810
37 A = 6791328
58 meter
Y = -4482953
40 meter E =
0004463
Z = -2377768
75 I = 51
30920
XDOT = 2188
909547 Wp = 41
91541
YDOT = -5033
791278 meter/sec RA = 242
23826 deg
ZDOT = 5346
154739 TA = 291
42828
MA = 291
47588
Ha = 222
989 n
mi
Hp = 217
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14802527
47 X = -4449795
46
Y = -14707852
37 feet Y = -4533060
91 meter
Z = -7801078
58 Z = -2399534
84
XDOT = 7181
461767 XDOT = 2219
067388
YDOT = -16515
063247 feet/sec YDOT = -5009
144659 meter/sec
ZDOT = 17539
877754 ZDOT = 5356
861006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20116619
61 X = -6131545
66
Y = -5405372
92 feet Y = -1647557
66 meter
Z = -7899121
93 Z = -2407652
36
XDOT = -2496
048958 XDOT = -760
795722
YDOT = -16370
876614 feet/sec YDOT = -4989
843192 meter/sec
ZDOT = 17588
714188 ZDOT = 5361
040084
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 19119
48710429
00016717 00000-0 10270-3 0 9160
2 25544 51
6391 243
2619 0001183 246
8682 113
2345 15
52596875 7686
Satellite: ISS
Catalog Number: 25544
Epoch time: 19119
48710429 = yrday
fracday
Element set: 916
Inclination: 51
6391 deg
RA of node: 243
2619 deg
Eccentricity:
0001183
Arg of perigee: 246
8682 deg
Mean anomaly: 113
2345 deg
Mean motion: 15
52596875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 330
Coasting Arc #18 (Orbit 783)
---------------------------------------
Vector Time (GMT): 2019/120/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4396581
86 A = 6793092
80 meter
Y = 5022277
91 meter E =
0013037
Z = 1225655
37 I = 51
33221
XDOT = -2956
235051 Wp = 125
50874
YDOT = 4017
926430 meter/sec RA = 237
25027 deg
ZDOT = -5823
207770 TA = 41
11693
MA = 41
01876
Ha = 222
967 n
mi
Hp = 217
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14424481
18 X = 4334140
97
Y = 16477289
73 feet Y = 5071094
46 meter
Z = 4021179
03 Z = 1246860
70
XDOT = -9698
933893 XDOT = -2972
658828
YDOT = 13182
173328 feet/sec YDOT = 3984
775785 meter/sec
ZDOT = -19105
012369 ZDOT = -5837
608127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20811476
78 X = 6343338
12
Y = 6758119
20 feet Y = 2059874
73 meter
Z = 4116658
11 Z = 1254757
39
XDOT = -960
546063 XDOT = -292
774440
YDOT = 14706
509809 feet/sec YDOT = 4482
544190 meter/sec
ZDOT = -19170
462427 ZDOT = -5843
156948
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 19120
51694615
00016717 00000-0 10270-3 0 9175
2 25544 51
6397 238
1396 0001179 249
9350 110
1675 15
52606682 7846
Satellite: ISS
Catalog Number: 25544
Epoch time: 19120
51694615 = yrday
fracday
Element set: 917
Inclination: 51
6397 deg
RA of node: 238
1396 deg
Eccentricity:
0001179
Arg of perigee: 249
9350 deg
Mean anomaly: 110
1675 deg
Mean motion: 15
52606682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 784
Checksum: 325
Coasting Arc #19 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2019/121/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4177948
81 A = 6793748
93 meter
Y = -5350023
48 meter E =
0011146
Z = -37541
52 I = 51
35396
XDOT = 3756
499910 Wp = 42
31818
YDOT = -2968
194834 meter/sec RA = 232
26633 deg
ZDOT = 5987
189169 TA = 317
27611
MA = 317
36271
Ha = 223
001 n
mi
Hp = 217
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13707181
14 X = -4117630
46
Y = -17552570
48 feet Y = -5396406
97 meter
Z = -123167
70 Z = -57690
01
XDOT = 12324
474771 XDOT = 3760
329177
YDOT = -9738
172027 feet/sec YDOT = -2926
165476 meter/sec
ZDOT = 19643
009084 ZDOT = 6005
446393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20904842
05 X = -6371795
86
Y = -7677015
05 feet Y = -2339954
19 meter
Z = -213856
58 Z = -65183
48
XDOT = 4658
768923 XDOT = 1419
992768
YDOT = -13180
393837 feet/sec YDOT = -4017
384041 meter/sec
ZDOT = 19725
813764 ZDOT = 6012
428035
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 19121
48242001
00016717 00000-0 10270-3 0 9181
2 25544 51
6403 233
3381 0001022 259
6787 100
4250 15
52608178 7993
Satellite: ISS
Catalog Number: 25544
Epoch time: 19121
48242001 = yrday
fracday
Element set: 918
Inclination: 51
6403 deg
RA of node: 233
3381 deg
Eccentricity:
0001022
Arg of perigee: 259
6787 deg
Mean anomaly: 100
4250 deg
Mean motion: 15
52608178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 288
Coasting Arc #20 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2019/122/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 965966
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3792979
52 A = 6793143
48 meter
Y = 5504262
82 meter E =
0008832
Z = -1185243
99 I = 51
37302
XDOT = -4585
981442 Wp = 148
64734
YDOT = 1909
032062 meter/sec RA = 227
28416 deg
ZDOT = -5837
430459 TA = 44
26606
MA = 44
19545
Ha = 222
984 n
mi
Hp = 217
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12444158
54 X = 3736904
73
Y = 18058605
04 feet Y = 5546365
02 meter
Z = -3888595
77 Z = -1166955
15
XDOT = -15045
870873 XDOT = -4578
632548
YDOT = 6263
228551 feet/sec YDOT = 1857
789401 meter/sec
ZDOT = -19151
674734 ZDOT = -5859
689932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20269435
19 X = 6178123
85
Y = 8411506
15 feet Y = 2563827
07 meter
Z = -3806315
33 Z = -1160164
91
XDOT = -8525
016375 XDOT = -2598
424991
YDOT = 11871
985274 feet/sec YDOT = 3618
581112 meter/sec
ZDOT = -19252
498240 ZDOT = -5868
161463
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 19122
51225655
00016717 00000-0 10270-3 0 9193
2 25544 51
6401 228
2164 0001109 259
3496 100
7531 15
52620800 8142
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
51225655 = yrday
fracday
Element set: 919
Inclination: 51
6401 deg
RA of node: 228
2164 deg
Eccentricity:
0001109
Arg of perigee: 259
3496 deg
Mean anomaly: 100
7531 deg
Mean motion: 15
52620800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 279
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