[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 7th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
159/13:07:16
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
3
164/10:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 214
7
172/07:16:24
783 1
0 1
1 1
1
N/A 0
2 -0
0 220
2
000/00:02:49
566 0
4 0
0 215
8
Coasting Arc #1 (Orbit 3684)
---------------------------------------
Vector Time (GMT): 2018/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 411434
34 A = 6785482
28 meter
Y = -6072012
19 meter E =
0007129
Z = -2999609
47 I = 52
00906
XDOT = 5081
668360 Wp = 129
76628
YDOT = 2809
892868 meter/sec RA = 71
23568 deg
ZDOT = -5003
259067 TA = 84
35567
MA = 84
27438
Ha = 221
694 n
mi
Hp = 214
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1349850
20 X = 493873
21
Y = -19921299
82 feet Y = -6066950
02 meter
Z = -9841238
43 Z = -2997411
19
XDOT = 16672
140288 XDOT = 5074
172918
YDOT = 9218
808623 feet/sec YDOT = 2866
678135 meter/sec
ZDOT = -16414
891952 ZDOT = -4978
591991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18757476
96 X = -5717278
98
Y = -6859215
48 feet Y = -2090688
88 meter
Z = -9830487
13 Z = -2996332
48
XDOT = 12991
203812 XDOT = 3959
718922
YDOT = -12216
298285 feet/sec YDOT = -3723
527717 meter/sec
ZDOT = -16304
898058 ZDOT = -4969
732928
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 18157
52607057
00016717 00000-0 10270-3 0 9001
2 25544 51
6411 71
8659 0003216 157
6093 202
5200 15
54141383 36857
Satellite: ISS
Catalog Number: 25544
Epoch time: 18157
52607057 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 71
8659 deg
Eccentricity:
0003216
Arg of perigee: 157
6093 deg
Mean anomaly: 202
5200 deg
Mean motion: 15
54141383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3685
Checksum: 292
Coasting Arc #2 (Orbit 3700)
---------------------------------------
Vector Time (GMT): 2018/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1372159
28 A = 6781703
81 meter
Y = 5109916
10 meter E =
0012191
Z = 4236942
55 I = 51
98471
XDOT = -5079
221389 Wp = 118
47725
YDOT = -4420
860079 meter/sec RA = 66
27599 deg
ZDOT = 3673
134294 TA = 294
02649
MA = 294
15404
Ha = 221
651 n
mi
Hp = 214
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4501834
91 X = -1449778
69
Y = 16764816
59 feet Y = 5094137
31 meter
Z = 13900730
14 Z = 4230088
95
XDOT = -16664
112167 XDOT = -5047
250842
YDOT = -14504
134119 feet/sec YDOT = -4477
480986 meter/sec
ZDOT = 12050
965533 ZDOT = 3648
538372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14999840
39 X = 4571951
35
Y = 8786571
75 feet Y = 2678147
07 meter
Z = 13869276
71 Z = 4227355
54
XDOT = -17710
078652 XDOT = -5398
031973
YDOT = 11313
283086 feet/sec YDOT = 3448
288685 meter/sec
ZDOT = 11941
540737 ZDOT = 3639
781617
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 18158
55489335
00016717 00000-0 10270-3 0 9013
2 25544 51
6409 66
7373 0003245 162
2935 197
8331 15
54143414 37016
Satellite: ISS
Catalog Number: 25544
Epoch time: 18158
55489335 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 66
7373 deg
Eccentricity:
0003245
Arg of perigee: 162
2935 deg
Mean anomaly: 197
8331 deg
Mean motion: 15
54143414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3701
Checksum: 313
Coasting Arc #3 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2018/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2430796
19 A = 6778391
46 meter
Y = -3809916
94 meter E =
0013350
Z = -5063513
88 I = 51
96112
XDOT = 4811
045256 Wp = 89
17751
YDOT = 5635
957829 meter/sec RA = 61
30498 deg
ZDOT = -1935
252631 TA = 162
13255
MA = 162
08557
Ha = 221
481 n
mi
Hp = 214
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7975053
11 X = 2497815
12
Y = -12499727
48 feet Y = -3782358
94 meter
Z = -16612578
36 Z = -5051543
38
XDOT = 15784
269213 XDOT = 4757
065367
YDOT = 18490
675293 feet/sec YDOT = 5689
456597 meter/sec
ZDOT = -6349
254038 ZDOT = -1912
012702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10163841
47 X = -3097938
88
Y = -10878314
64 feet Y = -3315710
30 meter
Z = -16558412
25 Z = -5047004
05
XDOT = 20986
296755 XDOT = 6396
623251
YDOT = -10121
551389 feet/sec YDOT = -3085
048863 meter/sec
ZDOT = -6246
096207 ZDOT = -1903
810124
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 18159
51940548
00016717 00000-0 10270-3 0 9029
2 25544 51
6423 61
9291 0003139 166
2584 193
8654 15
54183840 37161
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
51940548 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 61
9291 deg
Eccentricity:
0003139
Arg of perigee: 166
2584 deg
Mean anomaly: 193
8654 deg
Mean motion: 15
54183840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 324
Coasting Arc #4 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2018/159/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4586604
78 A = 6786821
99 meter
Y = -4356322
99 meter E =
0015628
Z = 2435400
01 I = 51
98812
XDOT = 1980
257388 Wp = 116
06959
YDOT = -5102
576400 meter/sec RA = 61
03807 deg
ZDOT = -5377
836949 TA = 36
79967
MA = 36
69250
Ha = 221
615 n
mi
Hp = 214
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15047915
96 X = -4549380
27
Y = -14292398
26 feet Y = -4407405
64 meter
Z = 7990157
51 Z = 2413209
75
XDOT = 6496
907441 XDOT = 2063
291502
YDOT = -16740
736221 feet/sec YDOT = -5079
967066 meter/sec
ZDOT = -17643
822011 ZDOT = -5368
016233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13534250
78 X = -4125239
64
Y = 15783006
38 feet Y = 4810660
35 meter
Z = 7891502
07 Z = 2405329
83
XDOT = -15895
341967 XDOT = -4844
900232
YDOT = -4797
877924 feet/sec YDOT = -1462
393191 meter/sec
ZDOT = -17599
079378 ZDOT = -5364
199394
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 18159
58370677
00016717 00000-0 10270-3 0 9037
2 25544 51
6423 61
6093 0003221 166
2288 193
8953 15
54147770 37176
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
58370677 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 61
6093 deg
Eccentricity:
0003221
Arg of perigee: 166
2288 deg
Mean anomaly: 193
8953 deg
Mean motion: 15
54147770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 327
Coasting Arc #5 (Orbit 3731)
---------------------------------------
Vector Time (GMT): 2018/160/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4263818
30 A = 6788884
42 meter
Y = 5218278
79 meter E =
0008574
Z = -802069
52 I = 51
97854
XDOT = -3236
114907 Wp = 55
07894
YDOT = 3554
311786 meter/sec RA = 56
08785 deg
ZDOT = 5970
999036 TA = 296
29248
MA = 296
38054
Ha = 221
363 n
mi
Hp = 214
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13988905
20 X = 4209045
26
Y = 17120337
22 feet Y = 5265653
56 meter
Z = -2631461
67 Z = -781489
69
XDOT = -10617
174891 XDOT = -3304
623941
YDOT = 11661
127907 feet/sec YDOT = 3517
739698 meter/sec
ZDOT = 19589
891851 ZDOT = 5955
112885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16155376
91 X = 4924158
88
Y = -15108652
72 feet Y = -4605117
35 meter
Z = -2540160
54 Z = -774240
93
XDOT = 11246
799864 XDOT = 3428
024599
YDOT = 8772
926956 feet/sec YDOT = 2673
988136 meter/sec
ZDOT = 19518
232749 ZDOT = 5949
157342
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 18160
54821138
00016717 00000-0 10270-3 0 9049
2 25544 51
6422 56
8006 0003110 172
0513 188
0690 15
54192261 37324
Satellite: ISS
Catalog Number: 25544
Epoch time: 18160
54821138 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 56
8006 deg
Eccentricity:
0003110
Arg of perigee: 172
0513 deg
Mean anomaly: 188
0690 deg
Mean motion: 15
54192261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3732
Checksum: 277
Coasting Arc #6 (Orbit 3747)
---------------------------------------
Vector Time (GMT): 2018/161/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3605726
83 A = 6788878
77 meter
Y = -5664758
72 meter E =
0012581
Z = -953884
08 I = 51
95879
XDOT = 4477
224600 Wp = 149
79963
YDOT = -1856
378222 meter/sec RA = 51
14092 deg
ZDOT = -5944
294464 TA = 40
48726
MA = 40
39372
Ha = 221
356 n
mi
Hp = 214
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11829812
44 X = -3537480
44
Y = -18585166
39 feet Y = -5704698
74 meter
Z = -3129540
96 Z = -971234
55
XDOT = 14689
057088 XDOT = 4526
524985
YDOT = -6090
479731 feet/sec YDOT = -1806
034494 meter/sec
ZDOT = -19502
278426 ZDOT = -5922
425844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17536433
67 X = -5345104
98
Y = 13316906
98 feet Y = 4058993
25 meter
Z = -3206303
38 Z = -977281
27
XDOT = -6334
882638 XDOT = -1930
872228
YDOT = -12979
720445 feet/sec YDOT = -3956
218792 meter/sec
ZDOT = -19404
105402 ZDOT = -5914
371326
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 18161
57701190
00016717 00000-0 10270-3 0 9059
2 25544 51
6421 51
6725 0003260 177
7293 182
3875 15
54144025 37481
Satellite: ISS
Catalog Number: 25544
Epoch time: 18161
57701190 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 51
6725 deg
Eccentricity:
0003260
Arg of perigee: 177
7293 deg
Mean anomaly: 182
3875 deg
Mean motion: 15
54144025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3748
Checksum: 304
Coasting Arc #7 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2018/162/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2657277
59 A = 6786289
09 meter
Y = 5683355
56 meter E =
0013131
Z = 2575209
86 I = 51
92934
XDOT = -5553
518515 Wp = 88
95503
YDOT = 191
285601 meter/sec RA = 46
18732 deg
ZDOT = 5285
363781 TA = 299
88321
MA = 300
01361
Ha = 221
130 n
mi
Hp = 214
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8718102
32 X = 2581018
07
Y = 18646179
67 feet Y = 5712644
33 meter
Z = 8448851
26 Z = 2587933
71
XDOT = -18220
205102 XDOT = -5580
918628
YDOT = 627
577430 feet/sec YDOT = 129
028420 meter/sec
ZDOT = 17340
432352 ZDOT = 5258
319818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17682107
00 X = 5389506
21
Y = -10491824
09 feet Y = -3197907
98 meter
Z = 8504888
66 Z = 2592290
06
XDOT = 1703
025501 XDOT = 519
082173
YDOT = 16889
225488 feet/sec YDOT = 5147
835929 meter/sec
ZDOT = 17219
360814 ZDOT = 5248
461176
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 18162
60580283
00016717 00000-0 10270-3 0 9063
2 25544 51
6423 46
5431 0002966 182
7876 177
3261 15
54195268 37641
Satellite: ISS
Catalog Number: 25544
Epoch time: 18162
60580283 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 46
5431 deg
Eccentricity:
0002966
Arg of perigee: 182
7876 deg
Mean anomaly: 177
3261 deg
Mean motion: 15
54195268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 328
Coasting Arc #8 (Orbit 3778)
---------------------------------------
Vector Time (GMT): 2018/163/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1380226
24 A = 6782455
33 meter
Y = -5335926
37 meter E =
0006176
Z = -3957321
58 I = 51
89196
XDOT = 6363
560301 Wp = 98
72775
YDOT = 1352
612875 meter/sec RA = 41
22337 deg
ZDOT = -4049
588218 TA = 129
10873
MA = 129
05380
Ha = 221
053 n
mi
Hp = 214
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4528301
31 X = -1301233
06
Y = -17506320
11 feet Y = -5350918
71 meter
Z = -12983338
53 Z = -3963835
30
XDOT = 20877
822510 XDOT = 6367
633058
YDOT = 4437
706284 feet/sec YDOT = 1423
797999 meter/sec
ZDOT = -13286
050584 ZDOT = -4018
665764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16863595
58 X = -5140023
93
Y = 6469976
58 feet Y = 1972048
86 meter
Z = -13011624
92 Z = -3965943
28
XDOT = 2412
508431 XDOT = 735
332570
YDOT = -20111
865295 feet/sec YDOT = -6130
096542 meter/sec
ZDOT = -13147
871980 ZDOT = -4007
471380
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 18163
57028776
00016717 00000-0 10270-3 0 9075
2 25544 51
6412 41
7343 0002983 187
3113 172
7997 15
54199865 37790
Satellite: ISS
Catalog Number: 25544
Epoch time: 18163
57028776 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 41
7343 deg
Eccentricity:
0002983
Arg of perigee: 187
3113 deg
Mean anomaly: 172
7997 deg
Mean motion: 15
54199865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3779
Checksum: 349
Coasting Arc #9 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2018/164/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3081491
60 A = 6777216
01 meter
Y = -2901217
17 meter E =
0014780
Z = -5305810
41 I = 51
85238
XDOT = 5798
802104 Wp = 106
67595
YDOT = 4958
901379 meter/sec RA = 36
67746 deg
ZDOT = 653
657655 TA = 169
57046
MA = 169
53977
Ha = 220
997 n
mi
Hp = 214
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10109880
58 X = 3139477
83
Y = -9518429
05 feet Y = -2866432
66 meter
Z = -17407514
47 Z = -5290701
13
XDOT = 19024
941286 XDOT = 5739
744180
YDOT = 16269
361480 feet/sec YDOT = 5023
417250 meter/sec
ZDOT = 2144
546112 ZDOT = 681
683895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4267598
09 X = -1300763
90
Y = -13302783
83 feet Y = -4054688
51 meter
Z = -17339414
23 Z = -5285053
46
XDOT = 21839
583658 XDOT = 6656
705099
YDOT = -9975
243640 feet/sec YDOT = -3040
454261 meter/sec
ZDOT = 2269
167787 ZDOT = 691
642342
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 18164
47046994
00016717 00000-0 10270-3 0 9088
2 25544 51
6421 37
2474 0003002 188
3818 171
7285 15
54231601 37931
Satellite: ISS
Catalog Number: 25544
Epoch time: 18164
47046994 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 37
2474 deg
Eccentricity:
0003002
Arg of perigee: 188
3818 deg
Mean anomaly: 171
7285 deg
Mean motion: 15
54231601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 313
Coasting Arc #10 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2018/165/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4439032
43 A = 6779148
40 meter
Y = 1714951
79 meter E =
0005701
Z = 4823562
73 I = 51
83250
XDOT = -4854
793127 Wp = 82
28497
YDOT = -5360
954198 meter/sec RA = 31
69313 deg
ZDOT = -2558
429896 TA = 32
83130
MA = 32
79589
Ha = 220
921 n
mi
Hp = 214
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14563754
68 X = -4481309
96
Y = 5626482
25 feet Y = 1665074
19 meter
Z = 15825337
03 Z = 4801897
01
XDOT = -15927
798972 XDOT = -4782
057115
YDOT = -17588
432407 feet/sec YDOT = -5414
836672 meter/sec
ZDOT = -8393
798873 ZDOT = -2581
837198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -874919
89 X = -266675
58
Y = 15686409
15 feet Y = 4781217
51 meter
Z = 15728084
06 Z = 4793920
02
XDOT = -21403
563632 XDOT = -6523
806195
YDOT = 7337
472536 feet/sec YDOT = 2236
461629 meter/sec
ZDOT = -8497
674691 ZDOT = -2590
091246
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 18165
49924108
00016717 00000-0 10270-3 0 9094
2 25544 51
6425 32
1187 0002962 195
9938 164
1121 15
54272280 38092
Satellite: ISS
Catalog Number: 25544
Epoch time: 18165
49924108 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 32
1187 deg
Eccentricity:
0002962
Arg of perigee: 195
9938 deg
Mean anomaly: 164
1121 deg
Mean motion: 15
54272280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 320
Coasting Arc #11 (Orbit 3823)
---------------------------------------
Vector Time (GMT): 2018/166/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5567845
96 A = 6782899
44 meter
Y = -577442
75 meter E =
0006460
Z = -3838316
89 I = 51
81566
XDOT = 3444
511428 Wp = 129
82686
YDOT = 5415
932924 meter/sec RA = 26
71397 deg
ZDOT = 4182
447183 TA = 184
16292
MA = 184
16829
Ha = 220
775 n
mi
Hp = 214
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18267211
15 X = 5592533
72
Y = -1894497
20 feet Y = -515040
52 meter
Z = -12592903
17 Z = -3811210
45
XDOT = 11300
890513 XDOT = 3363
376928
YDOT = 17768
808806 feet/sec YDOT = 5453
997410 meter/sec
ZDOT = 13721
939576 ZDOT = 4198
983300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5485791
98 X = 1672069
39
Y = -17613331
42 feet Y = -5368543
42 meter
Z = -12471486
51 Z = -3801309
09
XDOT = 19464
407032 XDOT = 5932
751263
YDOT = -3704
058719 feet/sec YDOT = -1128
997098 meter/sec
ZDOT = 13795
048687 ZDOT = 4204
730840
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 18166
46371017
00016717 00000-0 10270-3 0 9109
2 25544 51
6421 27
3095 0002913 199
3652 160
7391 15
54234926 38242
Satellite: ISS
Catalog Number: 25544
Epoch time: 18166
46371017 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 27
3095 deg
Eccentricity:
0002913
Arg of perigee: 199
3652 deg
Mean anomaly: 160
7391 deg
Mean motion: 15
54234926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3824
Checksum: 305
Coasting Arc #12 (Orbit 3839)
---------------------------------------
Vector Time (GMT): 2018/167/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6316355
74 A = 6786614
12 meter
Y = -472839
74 meter E =
0013924
Z = 2415259
50 I = 51
79748
XDOT = -1670
093367 Wp = 117
77451
YDOT = -5217
489194 meter/sec RA = 21
74430 deg
ZDOT = -5371
752734 TA = 35
26379
MA = 35
17175
Ha = 220
829 n
mi
Hp = 214
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20722951
89 X = -6322330
83
Y = -1551311
47 feet Y = -543507
39 meter
Z = 7924079
72 Z = 2384562
48
XDOT = -5479
308948 XDOT = -1585
532920
YDOT = -17117
746699 feet/sec YDOT = -5235
691624 meter/sec
ZDOT = -17623
860675 ZDOT = -5379
660896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9289097
43 X = -2831316
90
Y = 18647177
95 feet Y = 5683659
84 meter
Z = 7786768
59 Z = 2373407
07
XDOT = -16516
217628 XDOT = -5034
143133
YDOT = -829
587367 feet/sec YDOT = -252
858229 meter/sec
ZDOT = -17658
384768 ZDOT = -5382
275677
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 18167
49247177
00016717 00000-0 10270-3 0 9113
2 25544 51
6414 22
1803 0002839 199
8239 160
2804 15
54241329 38404
Satellite: ISS
Catalog Number: 25544
Epoch time: 18167
49247177 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 22
1803 deg
Eccentricity:
0002839
Arg of perigee: 199
8239 deg
Mean anomaly: 160
2804 deg
Mean motion: 15
54241329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3840
Checksum: 311
Coasting Arc #13 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2018/168/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6602756
53 A = 6788724
70 meter
Y = 1370759
34 meter E =
0007684
Z = -753965
21 I = 51
77374
XDOT = -322
147023 Wp = 44
56679
YDOT = 4808
023422 meter/sec RA = 16
78055 deg
ZDOT = 5962
296609 TA = 307
30190
MA = 307
37192
Ha = 220
598 n
mi
Hp = 214
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21662587
03 X = 6590599
92
Y = 4497241
92 feet Y = 1444528
05 meter
Z = -2473639
13 Z = -721920
96
XDOT = -1056
912804 XDOT = -404
849104
YDOT = 15774
355059 feet/sec YDOT = 4803
957677 meter/sec
ZDOT = 19561
340582 ZDOT = 5960
531572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12040570
90 X = 3669966
01
Y = -18579704
00 feet Y = -5663093
78 meter
Z = -2330451
49 Z = -710321
61
XDOT = 12921
292242 XDOT = 3938
409875
YDOT = 5939
563385 feet/sec YDOT = 1810
378920 meter/sec
ZDOT = 19552
639586 ZDOT = 5959
644546
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 18168
45692969
00016717 00000-0 10270-3 0 9124
2 25544 51
6413 17
3713 0002934 207
2666 152
8334 15
54261314 38550
Satellite: ISS
Catalog Number: 25544
Epoch time: 18168
45692969 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 17
3713 deg
Eccentricity:
0002934
Arg of perigee: 207
2666 deg
Mean anomaly: 152
8334 deg
Mean motion: 15
54261314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 318
Coasting Arc #14 (Orbit 3870)
---------------------------------------
Vector Time (GMT): 2018/169/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6351083
64 A = 6788552
07 meter
Y = -2150596
74 meter E =
0010945
Z = -1019950
21 I = 51
74141
XDOT = 2387
812661 Wp = 156
21334
YDOT = -4263
083969 meter/sec RA = 11
81778 deg
ZDOT = -5911
574249 TA = 34
82777
MA = 34
75619
Ha = 220
490 n
mi
Hp = 215
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20836888
58 X = -6321608
72
Y = -7055763
60 feet Y = -2221454
01 meter
Z = -3346293
35 Z = -1050729
93
XDOT = 7834
031041 XDOT = 2464
021182
YDOT = -13986
495960 feet/sec YDOT = -4235
954984 meter/sec
ZDOT = -19394
928638 ZDOT = -5899
790616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13821178
53 X = -4212695
22
Y = 17087901
02 feet Y = 5208392
23 meter
Z = -3483685
95 Z = -1061827
48
XDOT = -9123
594107 XDOT = -2780
871484
YDOT = -11302
077362 feet/sec YDOT = -3444
873180 meter/sec
ZDOT = -19341
483429 ZDOT = -5895
284149
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 18169
48567974
00016717 00000-0 10270-3 0 9136
2 25544 51
6417 12
2415 0003015 212
4174 147
6794 15
54231185 38713
Satellite: ISS
Catalog Number: 25544
Epoch time: 18169
48567974 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 12
2415 deg
Eccentricity:
0003015
Arg of perigee: 212
4174 deg
Mean anomaly: 147
6794 deg
Mean motion: 15
54231185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3871
Checksum: 313
Coasting Arc #15 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2018/170/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5585948
86 A = 6785831
58 meter
Y = 2782345
90 meter E =
0011493
Z = 2654452
11 I = 51
69895
XDOT = -4295
112161 Wp = 87
30166
YDOT = 3631
207040 meter/sec RA = 6
84812 deg
ZDOT = 5213
387787 TA = 302
61710
MA = 302
72798
Ha = 220
331 n
mi
Hp = 215
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18326603
86 X = 5541526
92
Y = 9128431
44 feet Y = 2844563
19 meter
Z = 8708832
37 Z = 2681478
88
XDOT = -14091
575330 XDOT = -4360
721774
YDOT = 11913
408924 feet/sec YDOT = 3582
808760 meter/sec
ZDOT = 17104
290639 ZDOT = 5192
364803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14642824
95 X = 4463133
04
Y = -14236125
20 feet Y = -4339170
96 meter
Z = 8829317
49 Z = 2691175
97
XDOT = 5525
976004 XDOT = 1684
317486
YDOT = 16271
331628 feet/sec YDOT = 4959
501880 meter/sec
ZDOT = 17009
608374 ZDOT = 5184
528632
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 18170
51442299
00016717 00000-0 10270-3 0 9145
2 25544 51
6403 7
1114 0002909 217
4865 142
6085 15
54276139 38873
Satellite: ISS
Catalog Number: 25544
Epoch time: 18170
51442299 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 7
1114 deg
Eccentricity:
0002909
Arg of perigee: 217
4865 deg
Mean anomaly: 142
6085 deg
Mean motion: 15
54276139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 312
Coasting Arc #16 (Orbit 3901)
---------------------------------------
Vector Time (GMT): 2018/171/10:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4331782
51 A = 6781956
18 meter
Y = -3326808
88 meter E =
0004844
Z = -4024562
32 I = 51
65226
XDOT = 5893
360583 Wp = 89
07196
YDOT = -2920
781725 meter/sec RA = 1
86776 deg
ZDOT = -3932
860825 TA = 140
07452
MA = 140
03888
Ha = 220
250 n
mi
Hp = 215
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14211884
88 X = -4274710
17
Y = -10914727
29 feet Y = -3374930
38 meter
Z = -13203944
62 Z = -4045466
20
XDOT = 19335
172515 XDOT = 5944
687231
YDOT = -9582
617207 feet/sec YDOT = -2854
590757 meter/sec
ZDOT = -12903
086695 ZDOT = -3904
108661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14793189
71 X = -4508964
22
Y = 9990305
77 feet Y = 3045045
20 meter
Z = -13296932
95 Z = -4052905
16
XDOT = -2284
241203 XDOT = -696
236719
YDOT = -20366
888150 feet/sec YDOT = -6207
827508 meter/sec
ZDOT = -12773
943955 ZDOT = -3893
498118
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 18171
47886654
00016717 00000-0 10270-3 0 9159
2 25544 51
6395 2
3030 0002968 221
6761 138
4166 15
54269814 39027
Satellite: ISS
Catalog Number: 25544
Epoch time: 18171
47886654 = yrday
fracday
Element set: 915
Inclination: 51
6395 deg
RA of node: 2
3030 deg
Eccentricity:
0002968
Arg of perigee: 221
6761 deg
Mean anomaly: 138
4166 deg
Mean motion: 15
54269814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3902
Checksum: 320
Coasting Arc #17 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2018/172/07:17:49
566
Vector Time (MET): N/A
Weight (LBS) : 923113
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3222782
91 A = 6780532
80 meter
Y = -3792617
12 meter E =
0008476
Z = -4613318
80 I = 51
62030
XDOT = 6737
432744 Wp = 127
04839
YDOT = 2086
741611 meter/sec RA = 357
59113 deg
ZDOT = 2989
942263 TA = 172
81738
MA = 172
80523
Ha = 220
224 n
mi
Hp = 215
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10573434
74 X = 3287362
50
Y = -12442969
54 feet Y = -3756216
23 meter
Z = -15135560
37 Z = -4597507
16
XDOT = 22104
438136 XDOT = 6699
073951
YDOT = 6846
265128 feet/sec YDOT = 2161
869479 meter/sec
ZDOT = 9809
521860 ZDOT = 3022
577347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6299331
02 X = 1920036
10
Y = -15136016
45 feet Y = -4613457
81 meter
Z = -15064183
87 Z = -4591563
24
XDOT = 21972
298048 XDOT = 6697
156445
YDOT = -767
411073 feet/sec YDOT = -233
906895 meter/sec
ZDOT = 9955
200450 ZDOT = 3034
345097
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 18172
31471444
00016717 00000-0 10270-3 0 9161
2 25544 51
6424 358
1366 0003246 238
5566 121
5270 15
54084302 39154
Satellite: ISS
Catalog Number: 25544
Epoch time: 18172
31471444 = yrday
fracday
Element set: 916
Inclination: 51
6424 deg
RA of node: 358
1366 deg
Eccentricity:
0003246
Arg of perigee: 238
5566 deg
Mean anomaly: 121
5270 deg
Mean motion: 15
54084302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 299
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