[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 21st 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
057/06:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 213
9
058/23:08:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 213
9
060/14:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
1
063/17:18:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2018/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -390935
41 A = 6781688
14 meter
Y = 5286866
02 meter E =
0010400
Z = -4239149
53 I = 51
32025
XDOT = -5901
301629 Wp = 83
10306
YDOT = -3309
936565 meter/sec RA = 234
42442 deg
ZDOT = -3590
154077 TA = 150
02755
MA = 149
96797
Ha = 222
015 n
mi
Hp = 213
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1282596
50 X = -429434
15
Y = 17345360
97 feet Y = 5282278
69 meter
Z = -13907970
90 Z = -4241142
51
XDOT = -19361
225817 XDOT = -5846
411499
YDOT = -10859
371931 feet/sec YDOT = -3375
622375 meter/sec
ZDOT = -11778
720725 ZDOT = -3618
686701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9580461
31 X = -2920124
61
Y = 14507101
01 feet Y = 4421764
39 meter
Z = -13917508
28 Z = -4242056
52
XDOT = -10373
081414 XDOT = -3161
715215
YDOT = -18251
780837 feet/sec YDOT = -5563
142799 meter/sec
ZDOT = -11905
330996 ZDOT = -3628
744887
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 18052
52275071
00016717 00000-0 10270-3 0 9002
2 25544 51
6362 235
3312 0003074 119
0394 241
1067 15
54136406 20520
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
52275071 = yrday
fracday
Element set: 900
Inclination: 51
6362 deg
RA of node: 235
3312 deg
Eccentricity:
0003074
Arg of perigee: 119
0394 deg
Mean anomaly: 241
1067 deg
Mean motion: 15
54136406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2052
Checksum: 266
Coasting Arc #2 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2018/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1658503
99 A = 6778645
40 meter
Y = -4237773
71 meter E =
0008676
Z = 5019156
74 I = 51
33020
XDOT = 5884
754125 Wp = 123
94337
YDOT = 4546
729915 meter/sec RA = 229
40877 deg
ZDOT = 1887
256840 TA = 307
65320
MA = 307
73188
Ha = 221
950 n
mi
Hp = 213
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5441286
04 X = 1681388
43
Y = -13903457
06 feet Y = -4219098
88 meter
Z = 16467049
68 Z = 5027268
99
XDOT = 19306
936105 XDOT = 5824
306767
YDOT = 14917
092896 feet/sec YDOT = 4612
199427 meter/sec
ZDOT = 6191
787532 ZDOT = 1915
695574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11324480
94 X = 3451701
79
Y = -9667554
25 feet Y = -2946670
54 meter
Z = 16503695
45 Z = 5030326
37
XDOT = 9097
278570 XDOT = 2772
850508
YDOT = 21481
525169 feet/sec YDOT = 6547
568872 meter/sec
ZDOT = 6317
841164 ZDOT = 1925
677987
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 18053
55158377
00016717 00000-0 10270-3 0 9016
2 25544 51
6366 230
2018 0002952 123
0133 237
1303 15
54105474 20687
Satellite: ISS
Catalog Number: 25544
Epoch time: 18053
55158377 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 230
2018 deg
Eccentricity:
0002952
Arg of perigee: 123
0133 deg
Mean anomaly: 237
1303 deg
Mean motion: 15
54105474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2068
Checksum: 277
Coasting Arc #3 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2018/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2993209
11 A = 6777318
29 meter
Y = 3003693
40 meter E =
0017560
Z = -5301989
07 I = 51
34878
XDOT = -5452
724254 Wp = 96
47892
YDOT = -5373
609470 meter/sec RA = 224
38865 deg
ZDOT = 32
187612 TA = 173
84036
MA = 173
81874
Ha = 222
004 n
mi
Hp = 213
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9820239
86 X = -3000820
73
Y = 9854637
15 feet Y = 2970178
45 meter
Z = -17394977
26 Z = -5316547
55
XDOT = -17889
515270 XDOT = -5392
386191
YDOT = -17629
952330 feet/sec YDOT = -5434
248205 meter/sec
ZDOT = 105
602402 ZDOT = 5
847246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13161500
74 X = -4011625
42
Y = 4248935
66 feet Y = 1295075
59 meter
Z = -17460173
61 Z = -5321860
92
XDOT = -7400
567631 XDOT = -2255
693014
YDOT = -22944
445796 feet/sec YDOT = -6993
467079 meter/sec
ZDOT = -11
024738 ZDOT = -3
360340
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 18054
51610893
00016717 00000-0 10270-3 0 9020
2 25544 51
6370 225
3935 0003200 126
1246 234
0203 15
54143113 20835
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
51610893 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 225
3935 deg
Eccentricity:
0003200
Arg of perigee: 126
1246 deg
Mean anomaly: 234
0203 deg
Mean motion: 15
54143113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 259
Coasting Arc #4 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2018/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4239507
43 A = 6778620
90 meter
Y = -1693920
71 meter E =
0007236
Z = 5004786
80 I = 51
37574
XDOT = 4623
095212 Wp = 81
55429
YDOT = 5806
227536 meter/sec RA = 219
36994 deg
ZDOT = -1947
544508 TA = 27
42281
MA = 27
38463
Ha = 221
891 n
mi
Hp = 213
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13909145
11 X = 4233823
91
Y = -5557482
65 feet Y = -1646543
21 meter
Z = 16419904
21 Z = 5025366
87
XDOT = 15167
635209 XDOT = 4567
284835
YDOT = 19049
302939 feet/sec YDOT = 5857
614028 meter/sec
ZDOT = -6389
581718 ZDOT = -1925
223175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14828524
77 X = 4519734
35
Y = 1199902
95 feet Y = 365730
42 meter
Z = 16511761
61 Z = 5032784
94
XDOT = 5176
042690 XDOT = 1577
657812
YDOT = 22757
549040 feet/sec YDOT = 6936
500947 meter/sec
ZDOT = -6290
884096 ZDOT = -1917
461472
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 18055
54493345
00016717 00000-0 10270-3 0 9036
2 25544 51
6356 220
2642 0003205 130
7876 229
3555 15
54108786 20994
Satellite: ISS
Catalog Number: 25544
Epoch time: 18055
54493345 = yrday
fracday
Element set: 903
Inclination: 51
6356 deg
RA of node: 220
2642 deg
Eccentricity:
0003205
Arg of perigee: 130
7876 deg
Mean anomaly: 229
3555 deg
Mean motion: 15
54108786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2099
Checksum: 314
Coasting Arc #5 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2018/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5311865
44 A = 6781651
63 meter
Y = 433249
55 meter E =
0011055
Z = -4205624
84 I = 51
41426
XDOT = -3364
889210 Wp = 117
27843
YDOT = -5830
116755 meter/sec RA = 214
35964 deg
ZDOT = 3651
831720 TA = 190
30232
MA = 190
32500
Ha = 221
899 n
mi
Hp = 213
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17427380
07 X = -5295887
00
Y = 1421422
41 feet Y = 373937
81 meter
Z = -13797981
77 Z = -4231388
83
XDOT = -11039
662761 XDOT = -3317
183563
YDOT = -19127
679644 feet/sec YDOT = -5867
478386 meter/sec
ZDOT = 11981
075196 ZDOT = 3635
602603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16251009
62 X = -4953307
73
Y = -6201400
65 feet Y = -1890186
92 meter
Z = -13912786
74 Z = -4240617
40
XDOT = -2226
138945 XDOT = -678
527151
YDOT = -20867
295608 feet/sec YDOT = -6360
351701 meter/sec
ZDOT = 11909
493033 ZDOT = 3630
013477
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 18056
50945067
00016717 00000-0 10270-3 0 9047
2 25544 51
6375 215
4558 0003155 134
7342 225
4068 15
54152051 21141
Satellite: ISS
Catalog Number: 25544
Epoch time: 18056
50945067 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 215
4558 deg
Eccentricity:
0003155
Arg of perigee: 134
7342 deg
Mean anomaly: 225
4068 deg
Mean motion: 15
54152051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 292
Coasting Arc #6 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2018/057/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1701033
67 A = 6781536
23 meter
Y = -4965467
57 meter E =
0012320
Z = 4287191
06 I = 51
43795
XDOT = 6776
832365 Wp = 112
17061
YDOT = 729
319199 meter/sec RA = 210
46087 deg
ZDOT = 3520
870822 TA = 301
82939
MA = 301
94928
Ha = 221
812 n
mi
Hp = 213
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5580819
14 X = -1666206
55
Y = -16290904
10 feet Y = -4984294
79 meter
Z = 14065587
46 Z = 4279012
98
XDOT = 22233
701985 XDOT = 6751
071061
YDOT = 2392
779525 feet/sec YDOT = 804
958498 meter/sec
ZDOT = 11551
413458 ZDOT = 3553
727070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17035443
89 X = 5192403
30
Y = -2709172
37 feet Y = -825755
74 meter
Z = 14029750
02 Z = 4276267
81
XDOT = -6464
547288 XDOT = -1970
394013
YDOT = 20144
364715 feet/sec YDOT = 6140
002365 meter/sec
ZDOT = 11697
684826 ZDOT = 3565
454335
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 18057
34536211
00016717 00000-0 10270-3 0 9058
2 25544 51
6402 211
2933 0002596 130
5276 229
6103 15
54139173 21271
Satellite: ISS
Catalog Number: 25544
Epoch time: 18057
34536211 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 211
2933 deg
Eccentricity:
0002596
Arg of perigee: 130
5276 deg
Mean anomaly: 229
6103 deg
Mean motion: 15
54139173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2127
Checksum: 283
Coasting Arc #7 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2018/058/06:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 920932
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 68611
65 A = 6778308
32 meter
Y = 4509209
34 meter E =
0014654
Z = -5073395
05 I = 51
45495
XDOT = -7211
535931 Wp = 85
37376
YDOT = -1873
865208 meter/sec RA = 205
45221 deg
ZDOT = -1766
266297 TA = 167
49202
MA = 167
45561
Ha = 221
665 n
mi
Hp = 213
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 225103
84 X = 42826
65
Y = 14793993
90 feet Y = 4509832
14 meter
Z = -16644996
88 Z = -5073124
65
XDOT = -23659
894787 XDOT = -7181
466501
YDOT = -6147
851732 feet/sec YDOT = -1954
341528 meter/sec
ZDOT = -5794
836932 ZDOT = -1801
223478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14656618
65 X = -4467337
36
Y = -2029516
50 feet Y = -618596
63 meter
Z = -16644321
57 Z = -5073189
22
XDOT = 9690
312274 XDOT = 2953
607181
YDOT = -21268
810026 feet/sec YDOT = -6482
733296 meter/sec
ZDOT = -5950
356019 ZDOT = -1813
668515
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 18058
30987078
00016717 00000-0 10270-3 0 9067
2 25544 51
6387 206
4839 0002546 135
0902 225
0457 15
54175507 21425
Satellite: ISS
Catalog Number: 25544
Epoch time: 18058
30987078 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 206
4839 deg
Eccentricity:
0002546
Arg of perigee: 135
0902 deg
Mean anomaly: 225
0457 deg
Mean motion: 15
54175507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 316
Coasting Arc #8 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2018/058/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1315275
45 A = 6779541
73 meter
Y = -4630944
52 meter E =
0010144
Z = 4768632
89 I = 51
47713
XDOT = 7180
528755 Wp = 124
06028
YDOT = 665
755937 meter/sec RA = 202
09253 deg
ZDOT = 2617
484832 TA = 300
03399
MA = 300
13459
Ha = 221
698 n
mi
Hp = 213
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4315208
17 X = -1286556
15
Y = -15193387
52 feet Y = -4645491
91 meter
Z = 15645121
05 Z = 4762313
99
XDOT = 23558
165206 XDOT = 7159
836378
YDOT = 2184
238640 feet/sec YDOT = 745
938033 meter/sec
ZDOT = 8587
548660 ZDOT = 2652
314178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5359569
50 X = -1633596
78
Y = 14886182
16 feet Y = 4537308
32 meter
Z = 15617504
73 Z = 4760215
44
XDOT = -16638
326293 XDOT = -5071
361854
YDOT = -15195
558571 feet/sec YDOT = -4631
606252 meter/sec
ZDOT = 8742
654893 ZDOT = 2664
761211
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 18059
01717673
00016717 00000-0 10270-3 0 9079
2 25544 51
6365 202
9577 0002693 139
4350 220
7004 15
54185068 21534
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
01717673 = yrday
fracday
Element set: 907
Inclination: 51
6365 deg
RA of node: 202
9577 deg
Eccentricity:
0002693
Arg of perigee: 139
4350 deg
Mean anomaly: 220
7004 deg
Mean motion: 15
54185068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 307
Coasting Arc #9 (Orbit 2167)
---------------------------------------
Vector Time (GMT): 2018/059/23:08:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -436746
47 A = 6777455
85 meter
Y = 4253140
41 meter E =
0016225
Z = -5272673
97 I = 51
50194
XDOT = -7435
407716 Wp = 92
42412
YDOT = -1672
670937 meter/sec RA = 197
08345 deg
ZDOT = -735
984074 TA = 170
53626
MA = 170
50565
Ha = 221
691 n
mi
Hp = 213
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1432895
25 X = -458662
55
Y = 13953872
75 feet Y = 4248133
36 meter
Z = -17298799
10 Z = -5274849
12
XDOT = -24394
382269 XDOT = -7412
575913
YDOT = -5487
765541 feet/sec YDOT = -1755
691187 meter/sec
ZDOT = -2414
645913 ZDOT = -772
046187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9088862
45 X = 2770285
27
Y = -10667898
66 feet Y = -3251575
51 meter
Z = -17308978
06 Z = -5275776
51
XDOT = 16033
462056 XDOT = 4886
999235
YDOT = 17824
472785 feet/sec YDOT = 5432
899305 meter/sec
ZDOT = -2575
150596 ZDOT = -784
905902
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 18059
98168131
00016717 00000-0 10270-3 0 9085
2 25544 51
6376 198
1485 0002723 140
3057 219
8295 15
54165182 21681
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
98168131 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 198
1485 deg
Eccentricity:
0002723
Arg of perigee: 140
3057 deg
Mean anomaly: 219
8295 deg
Mean motion: 15
54165182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2168
Checksum: 330
Coasting Arc #10 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2018/060/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3807270
93 A = 6783005
73 meter
Y = 4092440
45 meter E =
0007513
Z = -3848119
85 I = 51
54404
XDOT = -6173
705735 Wp = 98
71202
YDOT = 1857
552155 meter/sec RA = 193
92302 deg
ZDOT = -4140
718150 TA = 127
68463
MA = 127
61647
Ha = 221
677 n
mi
Hp = 214
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12491046
37 X = 3779916
89
Y = 13426641
89 feet Y = 4134862
59 meter
Z = -12625065
11 Z = -3829692
79
XDOT = -20254
940076 XDOT = -6173
905597
YDOT = 6094
331216 feet/sec YDOT = 1788
511945 meter/sec
ZDOT = -13585
033302 ZDOT = -4170
707856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15572984
72 X = 4746645
74
Y = 9789699
81 feet Y = 2983900
50 meter
Z = -12543410
45 Z = -3823231
50
XDOT = -17240
664263 XDOT = -5254
954467
YDOT = 9881
801696 feet/sec YDOT = 3011
973157 meter/sec
ZDOT = -13718
889825 ZDOT = -4181
517619
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 18060
62468064
00016717 00000-0 10270-3 0 9097
2 25544 51
6410 194
9408 0002970 150
4787 209
6533 15
54172864 21783
Satellite: ISS
Catalog Number: 25544
Epoch time: 18060
62468064 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 194
9408 deg
Eccentricity:
0002970
Arg of perigee: 150
4787 deg
Mean anomaly: 209
6533 deg
Mean motion: 15
54172864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2178
Checksum: 324
Coasting Arc #11 (Orbit 2193)
---------------------------------------
Vector Time (GMT): 2018/061/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2235949
53 A = 6779298
08 meter
Y = -4215955
55 meter E =
0009899
Z = 4810931
28 I = 51
56471
XDOT = 7183
572080 Wp = 128
92277
YDOT = -907
254841 meter/sec RA = 188
92695 deg
ZDOT = 2534
012782 TA = 296
08404
MA = 296
18589
Ha = 221
583 n
mi
Hp = 214
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7335792
41 X = -2212007
89
Y = -13831875
17 feet Y = -4240824
97 meter
Z = 15783895
26 Z = 4800128
74
XDOT = 23568
149868 XDOT = 7180
874703
YDOT = -2976
557878 feet/sec YDOT = -826
937941 meter/sec
ZDOT = 8313
690231 ZDOT = 2568
900949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10906131
36 X = -3324188
84
Y = -11300158
25 feet Y = -3444288
23 meter
Z = 15736222
33 Z = 4796400
56
XDOT = 21005
172948 XDOT = 6402
376714
YDOT = -8434
695289 feet/sec YDOT = -2570
895124 meter/sec
ZDOT = 8469
283102 ZDOT = 2581
437489
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 18061
65347522
00016717 00000-0 10270-3 0 9108
2 25544 51
6414 189
8123 0002893 153
3988 206
7313 15
54218663 21943
Satellite: ISS
Catalog Number: 25544
Epoch time: 18061
65347522 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 189
8123 deg
Eccentricity:
0002893
Arg of perigee: 153
3988 deg
Mean anomaly: 206
7313 deg
Mean motion: 15
54218663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2194
Checksum: 315
Coasting Arc #12 (Orbit 2208)
---------------------------------------
Vector Time (GMT): 2018/062/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 428369
85 A = 6777364
92 meter
Y = 4232818
81 meter E =
0015706
Z = -5289055
82 I = 51
58993
XDOT = -7630
731744 Wp = 95
01573
YDOT = -18
358950 meter/sec RA = 183
92508 deg
ZDOT = -635
689600 TA = 168
91983
MA = 168
88521
Ha = 221
507 n
mi
Hp = 214
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1405412
89 X = 406696
54
Y = 13887200
82 feet Y = 4237487
19 meter
Z = -17352545
33 Z = -5287028
23
XDOT = -25035
209135 XDOT = -7626
871524
YDOT = -60
232775 feet/sec YDOT = -103
669547 meter/sec
ZDOT = -2085
595802 ZDOT = -672
747091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5444311
78 X = 1659426
23
Y = 12864145
15 feet Y = 3920991
44 meter
Z = -17343978
79 Z = -5286444
73
XDOT = -23045
829622 XDOT = -7024
368869
YDOT = 6731
929593 feet/sec YDOT = 2051
892140 meter/sec
ZDOT = -2250
768871 ZDOT = -686
034352
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 18062
61796838
00016717 00000-0 10270-3 0 9114
2 25544 51
6408 185
0048 0002813 157
3498 202
7779 15
54179324 22091
Satellite: ISS
Catalog Number: 25544
Epoch time: 18062
61796838 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 185
0048 deg
Eccentricity:
0002813
Arg of perigee: 157
3498 deg
Mean anomaly: 202
7779 deg
Mean motion: 15
54179324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2209
Checksum: 329
Coasting Arc #13 (Orbit 2224)
---------------------------------------
Vector Time (GMT): 2018/063/14:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1415193
62 A = 6777552
89 meter
Y = -4129734
35 meter E =
0004332
Z = 5180593
51 I = 51
62514
XDOT = 7502
167891 Wp = 92
78100
YDOT = 908
093986 meter/sec RA = 178
92234 deg
ZDOT = -1324
741100 TA = 9
94700
MA = 9
93843
Ha = 221
304 n
mi
Hp = 214
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4643023
67 X = 1436103
93
Y = -13548997
20 feet Y = -4113791
02 meter
Z = 16996697
85 Z = 5187519
33
XDOT = 24613
411717 XDOT = 7497
890588
YDOT = 2979
310978 feet/sec YDOT = 991
964280 meter/sec
ZDOT = -4346
263452 ZDOT = -1288
309099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 202839
20 X = 61825
39
Y = -14283760
00 feet Y = -4353690
05 meter
Z = 17028029
49 Z = 5190143
39
XDOT = 23340
978110 XDOT = 7114
330128
YDOT = -4659
278147 feet/sec YDOT = -1420
147979 meter/sec
ZDOT = -4183
961848 ZDOT = -1275
271571
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 18063
64675266
00016717 00000-0 10270-3 0 9120
2 25544 51
6418 179
8757 0002694 161
1587 198
9665 15
54241518 22252
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
64675266 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 179
8757 deg
Eccentricity:
0002694
Arg of perigee: 161
1587 deg
Mean anomaly: 198
9665 deg
Mean motion: 15
54241518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2225
Checksum: 346
Coasting Arc #14 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2018/063/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3769425
73 A = 6780709
01 meter
Y = -3429541
78 meter E =
0011412
Z = 4467622
44 I = 51
63765
XDOT = 6377
084130 Wp = 120
02414
YDOT = -2757
769286 meter/sec RA = 178
35688 deg
ZDOT = 3251
688735 TA = 297
19305
MA = 297
30932
Ha = 221
599 n
mi
Hp = 214
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12366882
32 X = -3752496
64
Y = -11251777
49 feet Y = -3471598
80 meter
Z = 14657553
94 Z = 4449353
68
XDOT = 20922
192028 XDOT = 6391
653475
YDOT = -9047
799495 feet/sec YDOT = -2686
374421 meter/sec
ZDOT = 10668
270128 ZDOT = 3282
701843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15865991
30 X = -4835954
15
Y = 5493833
45 feet Y = 1674520
44 meter
Z = 14576497
41 Z = 4442916
41
XDOT = 2529
105726 XDOT = 770
871425
YDOT = -21472
546692 feet/sec YDOT = -6544
832232 meter/sec
ZDOT = 10806
824513 ZDOT = 3293
920112
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 18063
77535206
00016717 00000-0 10270-3 0 9134
2 25544 51
6403 179
2356 0002720 151
1650 208
9653 15
54211433 22279
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
77535206 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 179
2356 deg
Eccentricity:
0002720
Arg of perigee: 151
1650 deg
Mean anomaly: 208
9653 deg
Mean motion: 15
54211433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 287
Coasting Arc #15 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2018/064/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2077788
03 A = 6777855
96 meter
Y = 3875002
29 meter E =
0014549
Z = -5170754
98 I = 51
66187
XDOT = -7256
309140 Wp = 89
43813
YDOT = 1984
534113 meter/sec RA = 173
36208 deg
ZDOT = -1431
958309 TA = 166
78886
MA = 166
75072
Ha = 221
441 n
mi
Hp = 214
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6816889
85 X = 2059418
89
Y = 12713262
12 feet Y = 3898134
17 meter
Z = -16964419
24 Z = -5160707
00
XDOT = -23806
788518 XDOT = -7271
005791
YDOT = 6510
938691 feet/sec YDOT = 1903
306715 meter/sec
ZDOT = -4698
025949 ZDOT = -1467
242627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14476338
11 X = 4412387
86
Y = -189525
29 feet Y = -57767
31 meter
Z = -16920054
85 Z = -5157232
72
XDOT = -5361
113807 XDOT = -1634
067488
YDOT = 23007
972594 feet/sec YDOT = 7012
830047 meter/sec
ZDOT = -4855
550797 ZDOT = -1479
971883
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 18064
73983241
00016717 00000-0 10270-3 0 9148
2 25544 51
6412 174
4276 0002641 156
1587 203
9689 15
54205546 22422
Satellite: ISS
Catalog Number: 25544
Epoch time: 18064
73983241 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 174
4276 deg
Eccentricity:
0002641
Arg of perigee: 156
1587 deg
Mean anomaly: 203
9689 deg
Mean motion: 15
54205546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 314
Coasting Arc #16 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2018/065/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -259045
90 A = 6777131
00 meter
Y = -4217745
11 meter E =
0003902
Z = 5295170
66 I = 51
69039
XDOT = 7569
652456 Wp = 112
47788
YDOT = -1130
307684 meter/sec RA = 168
36436 deg
ZDOT = -531
150472 TA = 342
57727
MA = 342
59066
Ha = 221
425 n
mi
Hp = 214
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -849888
11 X = -237583
67
Y = -13837746
43 feet Y = -4220521
34 meter
Z = 17372607
16 Z = 5293964
92
XDOT = 24834
817768 XDOT = 7584
309307
YDOT = -3708
358544 feet/sec YDOT = -1045
576735 meter/sec
ZDOT = -1742
619658 ZDOT = -494
344221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12779678
74 X = -3895246
08
Y = -5390334
87 feet Y = -1642974
07 meter
Z = 17367703
26 Z = 5293675
95
XDOT = 7522
962825 XDOT = 2292
999069
YDOT = -22909
272928 feet/sec YDOT = -6982
746388 meter/sec
ZDOT = -1578
386171 ZDOT = -481
092105
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 18065
76860547
00016717 00000-0 10270-3 0 9156
2 25544 51
6393 169
2987 0002642 156
4899 203
6374 15
54228028 22586
Satellite: ISS
Catalog Number: 25544
Epoch time: 18065
76860547 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 169
2987 deg
Eccentricity:
0002642
Arg of perigee: 156
4899 deg
Mean anomaly: 203
6374 deg
Mean motion: 15
54228028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 346
Coasting Arc #17 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2018/066/17:18:30
000
Vector Time (MET): N/A
Weight (LBS) : 905824
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1545298
85 A = 6779009
99 meter
Y = 4470330
05 meter E =
0013405
Z = -4868917
04 I = 51
72983
XDOT = -7255
620055 Wp = 116
44534
YDOT = 154
662241 meter/sec RA = 163
37051 deg
ZDOT = 2444
178958 TA = 177
54568
MA = 177
53910
Ha = 221
285 n
mi
Hp = 214
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5069878
11 X = -1571521
94
Y = 14666437
19 feet Y = 4452902
37 meter
Z = -15974137
26 Z = -4876487
64
XDOT = -23804
527740 XDOT = -7268
682745
YDOT = 507
422052 feet/sec YDOT = 73
452107 meter/sec
ZDOT = 8018
959835 ZDOT = 2408
902138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11029153
54 X = 3361686
00
Y = 10866002
06 feet Y = 3311957
43 meter
Z = -16008400
18 Z = -4879360
38
XDOT = -9160
592666 XDOT = -2792
148645
YDOT = 20883
298214 feet/sec YDOT = 6365
229296 meter/sec
ZDOT = 7861
636034 ZDOT = 2396
226663
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 18066
73307335
00016717 00000-0 10270-3 0 9166
2 25544 51
6405 164
4905 0002446 163
4615 196
6618 15
54214389 22737
Satellite: ISS
Catalog Number: 25544
Epoch time: 18066
73307335 = yrday
fracday
Element set: 916
Inclination: 51
6405 deg
RA of node: 164
4905 deg
Eccentricity:
0002446
Arg of perigee: 163
4615 deg
Mean anomaly: 196
6618 deg
Mean motion: 15
54214389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 317
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