[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 23rd 2018
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) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
238/15:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
242/21:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
249/00:35:06
517 0
6 0
7 0
7
N/A -0
2 -0
0 223
0
000/00:00:13
035 0
1 -0
0 213
7
Coasting Arc #1 (Orbit 881)
---------------------------------------
Vector Time (GMT): 2018/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5363886
75 A = 6788744
39 meter
Y = 3730842
59 meter E =
0011991
Z = -1836892
05 I = 51
93554
XDOT = -1502
161743 Wp = 58
26170
YDOT = 4934
474938 meter/sec RA = 47
53880 deg
ZDOT = 5669
034909 TA = 281
63244
MA = 281
76701
Ha = 223
541 n
mi
Hp = 213
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17598053
64 X = 5330691
30
Y = 12240297
22 feet Y = 3790639
69 meter
Z = -6026548
73 Z = -1810917
16
XDOT = -4928
352176 XDOT = -1584
765515
YDOT = 16189
222238 feet/sec YDOT = 4917
214826 meter/sec
ZDOT = 18599
195895 ZDOT = 5661
537444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9110129
08 X = -2776767
34
Y = -19439854
09 feet Y = -5925267
53 meter
Z = -5910438
13 Z = -1801501
54
XDOT = 11079
083910 XDOT = 3376
904776
YDOT = -10802
587556 feet/sec YDOT = -3292
628687 meter/sec
ZDOT = 18564
836199 ZDOT = 5658
562073
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 18234
50353964
00016717 00000-0 10270-3 0 9000
2 25544 51
6369 48
2166 0005669 84
9941 275
1858 15
53854335 8826
Satellite: ISS
Catalog Number: 25544
Epoch time: 18234
50353964 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 48
2166 deg
Eccentricity:
0005669
Arg of perigee: 84
9941 deg
Mean anomaly: 275
1858 deg
Mean motion: 15
53854335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 882
Checksum: 340
Coasting Arc #2 (Orbit 897)
---------------------------------------
Vector Time (GMT): 2018/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5100231
78 A = 6789947
96 meter
Y = -4468820
84 meter E =
0016737
Z = 205901
03 I = 51
91780
XDOT = 2972
384476 Wp = 118
19859
YDOT = -3687
036651 meter/sec RA = 42
58821 deg
ZDOT = -6031
169642 TA = 59
59164
MA = 59
42634
Ha = 223
385 n
mi
Hp = 212
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16733043
89 X = -5050881
27
Y = -14661485
70 feet Y = -4525579
23 meter
Z = 675528
30 Z = 181246
19
XDOT = 9751
917573 XDOT = 3042
688753
YDOT = -12096
576939 feet/sec YDOT = -3653
404324 meter/sec
ZDOT = -19787
301975 ZDOT = -6016
560312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7477259
03 X = 2279068
55
Y = 20956648
52 feet Y = 6387586
47 meter
Z = 565455
28 Z = 172350
77
XDOT = -12995
769996 XDOT = -3961
110695
YDOT = 5207
503825 feet/sec YDOT = 1587
247166 meter/sec
ZDOT = -19721
181508 ZDOT = -6011
016124
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 18235
53254842
00016717 00000-0 10270-3 0 9010
2 25544 51
6377 43
0882 0005606 85
5056 274
6737 15
53911514 8988
Satellite: ISS
Catalog Number: 25544
Epoch time: 18235
53254842 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 43
0882 deg
Eccentricity:
0005606
Arg of perigee: 85
5056 deg
Mean anomaly: 274
6737 deg
Mean motion: 15
53911514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 898
Checksum: 322
Coasting Arc #3 (Orbit 913)
---------------------------------------
Vector Time (GMT): 2018/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4522030
52 A = 6789224
98 meter
Y = 4860159
52 meter E =
0019008
Z = 1386293
38 I = 51
89006
XDOT = -4377
710133 Wp = 69
58385
YDOT = 2394
837454 meter/sec RA = 37
63655 deg
ZDOT = 5825
901814 TA = 305
47422
MA = 305
65146
Ha = 223
509 n
mi
Hp = 212
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14836058
14 X = 4460613
03
Y = 15945405
24 feet Y = 4910384
62 meter
Z = 4548206
61 Z = 1408110
15
XDOT = -14362
566052 XDOT = -4432
463138
YDOT = 7857
078261 feet/sec YDOT = 2345
576842 meter/sec
ZDOT = 19113
851097 ZDOT = 5804
503785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5527520
65 X = -1684788
30
Y = -21045589
44 feet Y = -6414695
66 meter
Z = 4645474
55 Z = 1415940
64
XDOT = 14948
213222 XDOT = 4556
215390
YDOT = 312
857349 feet/sec YDOT = 95
358920 meter/sec
ZDOT = 19017
432887 ZDOT = 5796
513544
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 18236
56155726
00016717 00000-0 10270-3 0 9026
2 25544 51
6377 37
9602 0005779 92
7172 267
4642 15
53874018 9141
Satellite: ISS
Catalog Number: 25544
Epoch time: 18236
56155726 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 37
9602 deg
Eccentricity:
0005779
Arg of perigee: 92
7172 deg
Mean anomaly: 267
4642 deg
Mean motion: 15
53874018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 914
Checksum: 331
Coasting Arc #4 (Orbit 928)
---------------------------------------
Vector Time (GMT): 2018/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3562124
38 A = 6786407
01 meter
Y = -4995845
71 meter E =
0010240
Z = -2905186
92 I = 51
85410
XDOT = 5648
699401 Wp = 103
08642
YDOT = -1096
234025 meter/sec RA = 32
67924 deg
ZDOT = -5058
145303 TA = 109
88009
MA = 109
76970
Ha = 223
487 n
mi
Hp = 212
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11686759
79 X = -3491883
11
Y = -16390569
93 feet Y = -5035287
22 meter
Z = -9531453
13 Z = -2922319
37
XDOT = 18532
478349 XDOT = 5685
107318
YDOT = -3596
568325 feet/sec YDOT = -1032
862979 meter/sec
ZDOT = -16594
964906 ZDOT = -5030
617926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2854177
36 X = 869953
26
Y = 19890354
70 feet Y = 6062580
11 meter
Z = -9607663
46 Z = -2928415
82
XDOT = -16777
233681 XDOT = -5113
700826
YDOT = -5521
539924 feet/sec YDOT = -1682
965369 meter/sec
ZDOT = -16471
216015 ZDOT = -5020
426641
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 18237
52625013
00016717 00000-0 10270-3 0 9035
2 25544 51
6378 33
1532 0005807 95
2297 264
9518 15
53882639 9298
Satellite: ISS
Catalog Number: 25544
Epoch time: 18237
52625013 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 33
1532 deg
Eccentricity:
0005807
Arg of perigee: 95
2297 deg
Mean anomaly: 264
9518 deg
Mean motion: 15
53882639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 929
Checksum: 327
Coasting Arc #5 (Orbit 944)
---------------------------------------
Vector Time (GMT): 2018/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2329376
19 A = 6782813
58 meter
Y = 4865993
15 meter E =
0016136
Z = 4100049
52 I = 51
81473
XDOT = -6641
025195 Wp = 101
96190
YDOT = -73
268979 meter/sec RA = 27
71077 deg
ZDOT = 3843
920359 TA = 308
37498
MA = 308
51983
Ha = 223
383 n
mi
Hp = 212
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7642310
33 X = 2254874
65
Y = 15964544
47 feet Y = 4891625
51 meter
Z = 13451606
04 Z = 4111183
41
XDOT = -21788
140402 XDOT = -6658
383727
YDOT = -240
383790 feet/sec YDOT = -147
630368 meter/sec
ZDOT = 12611
287268 ZDOT = 3811
618964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 268753
76 X = 81916
15
Y = -17659864
35 feet Y = -5382726
65 meter
Z = 13500898
30 Z = 4115073
80
XDOT = 18232
695868 XDOT = 5557
325700
YDOT = 9847
944477 feet/sec YDOT = 3001
653477 meter/sec
ZDOT = 12466
279949 ZDOT = 3799
722128
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 18238
55525296
00016717 00000-0 10270-3 0 9042
2 25544 51
6388 28
0250 0005659 100
4718 259
7073 15
53896942 9459
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
55525296 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 28
0250 deg
Eccentricity:
0005659
Arg of perigee: 100
4718 deg
Mean anomaly: 259
7073 deg
Mean motion: 15
53896942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 945
Checksum: 335
Coasting Arc #6 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1532001
63 A = 6778000
74 meter
Y = 3911701
92 meter E =
0008097
Z = 5312344
12 I = 51
79779
XDOT = -6955
220594 Wp = 101
46842
YDOT = -3223
535190 meter/sec RA = 27
01843 deg
ZDOT = 365
798051 TA = 345
04231
MA = 345
06624
Ha = 223
416 n
mi
Hp = 212
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5026252
06 X = -1601433
63
Y = 12833667
72 feet Y = 3894182
10 meter
Z = 17428950
53 Z = 5304733
45
XDOT = -22818
965202 XDOT = -6920
434032
YDOT = -10575
902854 feet/sec YDOT = -3301
118759 meter/sec
ZDOT = 1200
124839 ZDOT = 332
097251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -177838
34 X = -54205
13
Y = -13825478
70 feet Y = -4214005
91 meter
Z = 17394225
07 Z = 5301759
80
XDOT = 24129
126760 XDOT = 7354
557837
YDOT = 1018
211411 feet/sec YDOT = 310
350838 meter/sec
ZDOT = 1049
285501 ZDOT = 319
822221
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 18238
68387708
00016717 00000-0 10270-3 0 9051
2 25544 51
6418 27
3853 0005548 100
8413 259
3364 15
53913471 9475
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
68387708 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 27
3853 deg
Eccentricity:
0005548
Arg of perigee: 100
8413 deg
Mean anomaly: 259
3364 deg
Mean motion: 15
53913471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 330
Coasting Arc #7 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3069162
77 A = 6778792
58 meter
Y = -3154186
26 meter E =
0019344
Z = -5173113
78 I = 51
77034
XDOT = 6443
819509 Wp = 101
33158
YDOT = 3858
252188 meter/sec RA = 22
03233 deg
ZDOT = 1471
543250 TA = 182
83100
MA = 182
84197
Ha = 223
413 n
mi
Hp = 213
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10069431
65 X = 3129333
55
Y = -10348380
11 feet Y = -3119528
69 meter
Z = -16972158
07 Z = -5158058
69
XDOT = 21141
140122 XDOT = 6393
048670
YDOT = 12658
307702 feet/sec YDOT = 3930
027670 meter/sec
ZDOT = 4827
897802 ZDOT = 1502
721055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5197662
31 X = -1584247
47
Y = 13556233
49 feet Y = 4131939
97 meter
Z = -16904124
18 Z = -5152377
05
XDOT = -23419
980338 XDOT = -7138
410007
YDOT = -2789
470701 feet/sec YDOT = -850
230670 meter/sec
ZDOT = 4967
308028 ZDOT = 1514
035487
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 18239
64856528
00016717 00000-0 10270-3 0 9060
2 25544 51
6420 22
5792 0005664 102
5158 257
6628 15
53897458 9628
Satellite: ISS
Catalog Number: 25544
Epoch time: 18239
64856528 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 22
5792 deg
Eccentricity:
0005664
Arg of perigee: 102
5158 deg
Mean anomaly: 257
6628 deg
Mean motion: 15
53897458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 962
Checksum: 342
Coasting Arc #8 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2018/240/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4468784
53 A = 6781456
61 meter
Y = 2352775
91 meter E =
0013913
Z = 4514892
08 I = 51
74804
XDOT = -5495
258772 Wp = 82
11302
YDOT = -4309
838310 meter/sec RA = 17
04776 deg
ZDOT = -3182
971801 TA = 39
81608
MA = 39
71407
Ha = 223
518 n
mi
Hp = 213
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14661366
58 X = -4516692
53
Y = 7719081
06 feet Y = 2302535
36 meter
Z = 14812638
05 Z = 4493067
95
XDOT = -18029
064212 XDOT = -5431
195513
YDOT = -14139
889469 feet/sec YDOT = -4370
932161 meter/sec
ZDOT = -10442
820869 ZDOT = -3209
509630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10219810
27 X = 3114998
17
Y = -13152862
91 feet Y = -4008992
62 meter
Z = 14714340
06 Z = 4484930
85
XDOT = 21250
969088 XDOT = 6477
295378
YDOT = 4659
053314 feet/sec YDOT = 1420
079450 meter/sec
ZDOT = -10561
325975 ZDOT = -3219
092157
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 18240
67756303
00016717 00000-0 10270-3 0 9076
2 25544 51
6419 17
4517 0005645 105
8529 254
3246 15
53896294 9785
Satellite: ISS
Catalog Number: 25544
Epoch time: 18240
67756303 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 17
4517 deg
Eccentricity:
0005645
Arg of perigee: 105
8529 deg
Mean anomaly: 254
3246 deg
Mean motion: 15
53896294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 335
Coasting Arc #9 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2018/241/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5616325
12 A = 6785046
39 meter
Y = -1596153
67 meter E =
0010291
Z = -3466953
04 I = 51
72773
XDOT = 4112
833731 Wp = 100
52825
YDOT = 4566
534774 meter/sec RA = 12
07037 deg
ZDOT = 4569
936951 TA = 218
90503
MA = 218
97913
Ha = 223
367 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18426263
53 X = 5650596
86
Y = -5236724
62 feet Y = -1533156
69 meter
Z = -11374517
84 Z = -3439587
68
XDOT = 13493
548985 XDOT = 4039
265600
YDOT = 14982
069469 feet/sec YDOT = 4612
116371 meter/sec
ZDOT = 14993
231466 ZDOT = 4589
736470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14438576
33 X = -4400878
07
Y = 12698903
40 feet Y = 3870625
76 meter
Z = -11251466
33 Z = -3429446
94
XDOT = -17616
799605 XDOT = -5369
600520
YDOT = -6696
263655 feet/sec YDOT = -2041
021162 meter/sec
ZDOT = 15081
444230 ZDOT = 4596
824201
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 18241
64224597
00016717 00000-0 10270-3 0 9080
2 25544 51
6416 12
6456 0005541 110
1690 250
0059 15
53888339 9937
Satellite: ISS
Catalog Number: 25544
Epoch time: 18241
64224597 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 12
6456 deg
Eccentricity:
0005541
Arg of perigee: 110
1690 deg
Mean anomaly: 250
0059 deg
Mean motion: 15
53888339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 311
Coasting Arc #10 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2018/242/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6409293
07 A = 6788310
59 meter
Y = 830086
08 meter E =
0019554
Z = 2046480
55 I = 51
70638
XDOT = -2396
529579 Wp = 111
25295
YDOT = -4718
999747 meter/sec RA = 7
09931 deg
ZDOT = -5555
715064 TA = 46
12581
MA = 45
96446
Ha = 223
399 n
mi
Hp = 213
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21027864
41 X = -6428039
67
Y = 2723379
53 feet Y = 758308
27 meter
Z = 6714175
02 Z = 2015300
91
XDOT = -7862
629851 XDOT = -2316
595636
YDOT = -15482
282633 feet/sec YDOT = -4745
352905 meter/sec
ZDOT = -18227
411627 ZDOT = -5567
162021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17640326
47 X = 5376771
51
Y = -11843469
39 feet Y = -3609889
47 meter
Z = 6574126
48 Z = 2003793
75
XDOT = 12975
198817 XDOT = 3954
840600
YDOT = 9113
545736 feet/sec YDOT = 2777
808740 meter/sec
ZDOT = -18278
107736 ZDOT = -5571
167238
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 18242
67123787
00016717 00000-0 10270-3 0 9094
2 25544 51
6418 7
5180 0005615 112
1011 248
0738 15
53895132 10096
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
67123787 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 7
5180 deg
Eccentricity:
0005615
Arg of perigee: 112
1011 deg
Mean anomaly: 248
0738 deg
Mean motion: 15
53895132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1009
Checksum: 294
Coasting Arc #11 (Orbit 1012)
---------------------------------------
Vector Time (GMT): 2018/242/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -466573
55 A = 6778263
84 meter
Y = -4244730
87 meter E =
0019873
Z = -5281125
92 I = 51
66095
XDOT = 7611
467420 Wp = 90
79379
YDOT = 140
141304 meter/sec RA = 5
74999 deg
ZDOT = -787
928076 TA = 171
68054
MA = 171
64755
Ha = 223
412 n
mi
Hp = 213
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1530753
12 X = -393420
23
Y = -13926282
39 feet Y = -4249539
80 meter
Z = -17326528
61 Z = -5283214
36
XDOT = 24972
005972 XDOT = 7613
161956
YDOT = 459
781182 feet/sec YDOT = 225
267421 meter/sec
ZDOT = -2585
065866 ZDOT = -750
950167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10409707
13 X = 3172878
73
Y = -9360489
76 feet Y = -2853077
28 meter
Z = -17335292
58 Z = -5283797
18
XDOT = 13690
147378 XDOT = 4172
756921
YDOT = 19687
613334 feet/sec YDOT = 6000
784544 meter/sec
ZDOT = -2419
138707 ZDOT = -737
353478
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 18242
92848581
00016717 00000-0 10270-3 0 9100
2 25544 51
6390 6
2371 0005676 109
5367 250
6399 15
53880308 10130
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
92848581 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 6
2371 deg
Eccentricity:
0005676
Arg of perigee: 109
5367 deg
Mean anomaly: 250
6399 deg
Mean motion: 15
53880308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1013
Checksum: 314
Coasting Arc #12 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2018/243/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1250298
63 A = 6778445
32 meter
Y = 4122227
94 meter E =
0008323
Z = 5226478
38 I = 51
62787
XDOT = -7542
559990 Wp = 89
90440
YDOT = -939
864743 meter/sec RA =
75368 deg
ZDOT = -1061
596502 TA = 10
26630
MA = 10
24931
Ha = 223
376 n
mi
Hp = 213
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4102029
63 X = -1321689
10
Y = 13524369
89 feet Y = 4107847
40 meter
Z = 17147238
79 Z = 5220231
20
XDOT = -24745
931727 XDOT = -7526
332903
YDOT = -3083
545744 feet/sec YDOT = -1024
120210 meter/sec
ZDOT = -3482
928155 ZDOT = -1098
196203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13327171
03 X = -4062121
73
Y = 4806518
51 feet Y = 1465026
84 meter
Z = 17118613
21 Z = 5217753
31
XDOT = -12119
154689 XDOT = -3693
918349
YDOT = -20596
828634 feet/sec YDOT = -6277
913368 meter/sec
ZDOT = -3647
028953 ZDOT = -1111
614425
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 18243
95747409
00016717 00000-0 10270-3 0 9112
2 25544 51
6383 1
1098 0005559 113
0996 247
0743 15
53890033 10296
Satellite: ISS
Catalog Number: 25544
Epoch time: 18243
95747409 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 1
1098 deg
Eccentricity:
0005559
Arg of perigee: 113
0996 deg
Mean anomaly: 247
0743 deg
Mean motion: 15
53890033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 312
Coasting Arc #13 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2018/244/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2890247
25 A = 6780768
20 meter
Y = -3953728
26 meter E =
0016129
Z = -4705400
35 I = 51
60260
XDOT = 6912
228049 Wp = 111
32706
YDOT = 1716
691220 meter/sec RA = 355
75797 deg
ZDOT = 2805
348282 TA = 186
54219
MA = 186
56327
Ha = 223
306 n
mi
Hp = 213
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9482438
48 X = 2957100
52
Y = -12971549
40 feet Y = -3921033
93 meter
Z = -15437665
20 Z = -4691197
95
XDOT = 22677
913545 XDOT = 6878
890873
YDOT = 5632
189042 feet/sec YDOT = 1793
802271 meter/sec
ZDOT = 9203
898562 ZDOT = 2838
844500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16122577
94 X = 4914161
76
Y = -470352
80 feet Y = -143363
53 meter
Z = -15373369
47 Z = -4685803
01
XDOT = 9499
060051 XDOT = 2895
313504
YDOT = 20092
603643 feet/sec YDOT = 6124
225590 meter/sec
ZDOT = 9353
949815 ZDOT = 2851
083904
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 18244
92214752
00016717 00000-0 10270-3 0 9121
2 25544 51
6386 356
3028 0005506 116
3816 243
7902 15
53882370 10448
Satellite: ISS
Catalog Number: 25544
Epoch time: 18244
92214752 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 356
3028 deg
Eccentricity:
0005506
Arg of perigee: 116
3816 deg
Mean anomaly: 243
7902 deg
Mean motion: 15
53882370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 303
Coasting Arc #14 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2018/245/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322253
53 A = 6784223
67 meter
Y = 3677238
68 meter E =
0016591
Z = 3702122
77 I = 51
58233
XDOT = -5836
454811 Wp = 95
19783
YDOT = -2510
574720 meter/sec RA = 350
76740 deg
ZDOT = -4305
257988 TA = 40
58638
MA = 40
46280
Ha = 223
285 n
mi
Hp = 213
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14180621
83 X = -4381035
17
Y = 12064431
36 feet Y = 3628575
68 meter
Z = 12146072
08 Z = 3680983
87
XDOT = -19148
473790 XDOT = -5787
034403
YDOT = -8236
793700 feet/sec YDOT = -2575
565794 meter/sec
ZDOT = -14124
862166 ZDOT = -4333
489378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18358243
81 X = -5595592
71
Y = -3452997
32 feet Y = -1052473
58 meter
Z = 12050697
07 Z = 3673052
47
XDOT = -5881
208542 XDOT = -1792
592364
YDOT = -18642
148511 feet/sec YDOT = -5682
126866 meter/sec
ZDOT = -14251
168110 ZDOT = -4343
756040
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 18245
95112806
00016717 00000-0 10270-3 0 9133
2 25544 51
6394 351
1747 0005428 119
1305 241
0391 15
53914545 10606
Satellite: ISS
Catalog Number: 25544
Epoch time: 18245
95112806 = yrday
fracday
Element set: 913
Inclination: 51
6394 deg
RA of node: 351
1747 deg
Eccentricity:
0005428
Arg of perigee: 119
1305 deg
Mean anomaly: 241
0391 deg
Mean motion: 15
53914545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 293
Coasting Arc #15 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2018/246/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5418792
86 A = 6787663
46 meter
Y = -3324523
60 meter E =
0008752
Z = -2383778
92 I = 51
56062
XDOT = 4369
298381 Wp = 82
07224
YDOT = 3286
931654 meter/sec RA = 345
78447 deg
ZDOT = 5366
257502 TA = 251
29667
MA = 251
39169
Ha = 223
227 n
mi
Hp = 213
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17778191
80 X = 5467144
99
Y = -10907229
65 feet Y = -3263656
59 meter
Z = -7820796
98 Z = -2357338
87
XDOT = 14334
968440 XDOT = 4306
151870
YDOT = 10783
896501 feet/sec YDOT = 3335
439183 meter/sec
ZDOT = 17605
831701 ZDOT = 5387
328572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19828285
57 X = 6043661
44
Y = 6612082
34 feet Y = 2015362
70 meter
Z = -7701693
73 Z = -2347476
25
XDOT = 1390
550708 XDOT = 423
839856
YDOT = 16376
488093 feet/sec YDOT = 4991
553571 meter/sec
ZDOT = 17699
895862 ZDOT = 5394
928259
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 18246
91579420
00016717 00000-0 10270-3 0 9140
2 25544 51
6387 346
3677 0005423 122
0426 238
1253 15
53896286 10759
Satellite: ISS
Catalog Number: 25544
Epoch time: 18246
91579420 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 346
3677 deg
Eccentricity:
0005423
Arg of perigee: 122
0426 deg
Mean anomaly: 238
1253 deg
Mean motion: 15
53896286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 323
Coasting Arc #16 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2018/247/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6126133
97 A = 6789738
28 meter
Y = 2797270
99 meter E =
0018697
Z = 790268
96 I = 51
53674
XDOT = -2639
041377 Wp = 126
34617
YDOT = -4077
090736 meter/sec RA = 340
80672 deg
ZDOT = -5939
234871 TA = 45
09391
MA = 44
94231
Ha = 223
136 n
mi
Hp = 213
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20098864
74 X = -6160797
21
Y = 9177398
26 feet Y = 2728570
51 meter
Z = 2592745
94 Z = 760426
28
XDOT = -8658
272233 XDOT = -2564
404582
YDOT = -13376
281942 feet/sec YDOT = -4106
185076 meter/sec
ZDOT = -19485
678710 ZDOT = -5951
873014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20137271
14 X = -6137840
24
Y = -9130039
74 feet Y = -2782836
11 meter
Z = 2458458
74 Z = 749338
23
XDOT = 3812
276527 XDOT = 1161
981885
YDOT = -13751
539869 feet/sec YDOT = -4191
469352 meter/sec
ZDOT = -19541
795457 ZDOT = -5956
339255
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 18247
94476918
00016717 00000-0 10270-3 0 9153
2 25544 51
6396 341
2396 0005413 126
5482 233
6170 15
53907673 10910
Satellite: ISS
Catalog Number: 25544
Epoch time: 18247
94476918 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 341
2396 deg
Eccentricity:
0005413
Arg of perigee: 126
5482 deg
Mean anomaly: 233
6170 deg
Mean motion: 15
53907673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 327
Coasting Arc #17 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2018/248/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6384220
89 A = 6789592
63 meter
Y = -2142573
94 meter E =
0015606
Z = 829010
90 I = 51
50592
XDOT = 827
944147 Wp = 73
34724
YDOT = 4794
095243 meter/sec RA = 335
82966 deg
ZDOT = 5926
070620 TA = 295
63394
MA = 295
79509
Ha = 223
046 n
mi
Hp = 213
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20945606
58 X = 6403678
40
Y = -7029442
07 feet Y = -2071072
35 meter
Z = 2719852
03 Z = 860070
22
XDOT = 2716
352188 XDOT = 745
488276
YDOT = 15728
658933 feet/sec YDOT = 4802
892969 meter/sec
ZDOT = 19442
488910 ZDOT = 5929
892078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19240323
45 X = 5864450
59
Y = 10824154
23 feet Y = 3299202
21 meter
Z = 2859497
28 Z = 871574
77
XDOT = -9153
642337 XDOT = -2790
030184
YDOT = 11057
571141 feet/sec YDOT = 3370
347684 meter/sec
ZDOT = 19458
953325 ZDOT = 5931
088973
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 18248
97373903
00016717 00000-0 10270-3 0 9168
2 25544 51
6398 336
1121 0005345 130
5740 229
5878 15
53927814 11073
Satellite: ISS
Catalog Number: 25544
Epoch time: 18248
97373903 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 336
1121 deg
Eccentricity:
0005345
Arg of perigee: 130
5740 deg
Mean anomaly: 229
5878 deg
Mean motion: 15
53927814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 325
Coasting Arc #18 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2018/249/00:35:13
035
Vector Time (MET): N/A
Weight (LBS) : 907815
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -267904
69 A = 6778986
30 meter
Y = -4403846
85 meter E =
0018042
Z = -5162779
90 I = 51
46827
XDOT = 7225
645626 Wp = 108
84574
YDOT = -2095
036869 meter/sec RA = 335
24450 deg
ZDOT = 1410
461622 TA = 174
78832
MA = 174
76951
Ha = 223
022 n
mi
Hp = 213
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -878952
38 X = -193561
94
Y = -14448316
44 feet Y = -4406427
18 meter
Z = -16938254
26 Z = -5163900
61
XDOT = 23706
186438 XDOT = 7241
684680
YDOT = -6873
480541 feet/sec YDOT = -2014
144983 meter/sec
ZDOT = 4627
498759 ZDOT = 1445
599932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1003279
32 X = 305799
54
Y = -14435048
10 feet Y = -4399802
66 meter
Z = -16942658
57 Z = -5164122
33
XDOT = 23284
258894 XDOT = 7097
042111
YDOT = -4004
784310 feet/sec YDOT = -1220
658258 meter/sec
ZDOT = 4785
435938 ZDOT = 1458
600874
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 18249
03804957
00016717 00000-0 10270-3 0 9175
2 25544 51
6423 335
7926 0004834 133
2628 226
8928 15
53812438 11089
Satellite: ISS
Catalog Number: 25544
Epoch time: 18249
03804957 = yrday
fracday
Element set: 917
Inclination: 51
6423 deg
RA of node: 335
7926 deg
Eccentricity:
0004834
Arg of perigee: 133
2628 deg
Mean anomaly: 226
8928 deg
Mean motion: 15
53812438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 328
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