[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 11th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
257/13:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 1178)
---------------------------------------
Vector Time (GMT): 2018/253/13:16:40
263
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4269466
63 A = 6779090
95 meter
Y = 1363541
36 meter E =
0009820
Z = 5081616
24 I = 51
34506
XDOT = -4011
696944 Wp = 133
46550
YDOT = 6323
845686 meter/sec RA = 312
63356 deg
ZDOT = 1665
012099 TA = 300
35021
MA = 300
44728
Ha = 222
755 n
mi
Hp = 213
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14007436
45 X = 4229218
17
Y = 4473560
88 feet Y = 1411061
05 meter
Z = 16671969
30 Z = 5102257
77
XDOT = -13161
735379 XDOT = -4090
201481
YDOT = 20747
525215 feet/sec YDOT = 6278
545360 meter/sec
ZDOT = 5462
638119 ZDOT = 1645
333376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14375726
88 X = -4381721
55
Y = -2543601
90 feet Y = -775289
86 meter
Z = 16764371
43 Z = 5109780
41
XDOT = 10068
399251 XDOT = 3068
848092
YDOT = -21301
525687 feet/sec YDOT = -6492
705029 meter/sec
ZDOT = 5373
540969 ZDOT = 1637
855287
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 18253
60432267
00016717 00000-0 10270-3 0 9006
2 25544 51
6399 313
0383 0004908 142
9832 217
1660 15
53835740 11798
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
60432267 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 313
0383 deg
Eccentricity:
0004908
Arg of perigee: 142
9832 deg
Mean anomaly: 217
1660 deg
Mean motion: 15
53835740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1179
Checksum: 308
Coasting Arc #2 (Orbit 1193)
---------------------------------------
Vector Time (GMT): 2018/254/13:16:40
263
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3253988
62 A = 6778297
84 meter
Y = -2727357
28 meter E =
0018055
Z = -5299099
26 I = 51
32073
XDOT = 4766
574901 Wp = 104
06060
YDOT = -5987
946697 meter/sec RA = 307
61551 deg
ZDOT = 151
044010 TA = 167
41033
MA = 167
36517
Ha = 222
849 n
mi
Hp = 213
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10675815
67 X = -3197508
51
Y = -8948022
58 feet Y = -2763430
48 meter
Z = -17385496
26 Z = -5314768
47
XDOT = 15638
369098 XDOT = 4832
445830
YDOT = -19645
494414 feet/sec YDOT = -5934
275226 meter/sec
ZDOT = 495
551214 ZDOT = 174
359048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11804947
66 X = 3598148
05
Y = 7228226
22 feet Y = 2203163
35 meter
Z = -17455417
07 Z = -5320411
12
XDOT = -11917
792554 XDOT = -3632
543171
YDOT = 20945
439782 feet/sec YDOT = 6384
170046 meter/sec
ZDOT = 600
895512 ZDOT = 183
152952
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 18254
56903990
00016717 00000-0 10270-3 0 9019
2 25544 51
6402 308
2311 0004883 147
3088 212
8368 15
53810383 11944
Satellite: ISS
Catalog Number: 25544
Epoch time: 18254
56903990 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 308
2311 deg
Eccentricity:
0004883
Arg of perigee: 147
3088 deg
Mean anomaly: 212
8368 deg
Mean motion: 15
53810383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1194
Checksum: 307
Coasting Arc #3 (Orbit 1209)
---------------------------------------
Vector Time (GMT): 2018/255/13:16:40
263
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2187253
68 A = 6779431
53 meter
Y = 4013754
59 meter E =
0007400
Z = 4999994
93 I = 51
30499
XDOT = -5223
119048 Wp = 96
65958
YDOT = 5273
486765 meter/sec RA = 302
59704 deg
ZDOT = -1946
800677 TA = 12
31900
MA = 12
30091
Ha = 222
646 n
mi
Hp = 214
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7176029
14 X = 2117920
80
Y = 13168486
20 feet Y = 4037826
87 meter
Z = 16404182
85 Z = 5010451
03
XDOT = -17136
217349 XDOT = -5272
243890
YDOT = 17301
465763 feet/sec YDOT = 5214
803334 meter/sec
ZDOT = -6387
141330 ZDOT = -1972
292745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9202549
34 X = -2804937
04
Y = -11776833
16 feet Y = -3589578
75 meter
Z = 16450559
99 Z = 5014130
68
XDOT = 13045
100461 XDOT = 3976
146621
YDOT = -19283
650551 feet/sec YDOT = -5877
656688 meter/sec
ZDOT = -6502
141619 ZDOT = -1981
852765
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 18255
59806716
00016717 00000-0 10270-3 0 9022
2 25544 51
6396 303
1037 0004834 149
2647 210
8790 15
53857709 12102
Satellite: ISS
Catalog Number: 25544
Epoch time: 18255
59806716 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 303
1037 deg
Eccentricity:
0004834
Arg of perigee: 149
2647 deg
Mean anomaly: 210
8790 deg
Mean motion: 15
53857709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1210
Checksum: 318
Coasting Arc #4 (Orbit 1224)
---------------------------------------
Vector Time (GMT): 2018/256/13:16:40
263
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1153865
05 A = 6782485
56 meter
Y = -5161381
39 meter E =
0012189
Z = -4259462
69 I = 51
29916
XDOT = 5374
245452 Wp = 124
94771
YDOT = -4135
382816 meter/sec RA = 297
58255 deg
ZDOT = 3555
581530 TA = 181
56489
MA = 181
56871
Ha = 222
699 n
mi
Hp = 214
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3785646
48 X = -1075372
96
Y = -16933665
98 feet Y = -5173846
24 meter
Z = -13974615
13 Z = -4264876
66
XDOT = 17632
038884 XDOT = 5402
817793
YDOT = -13567
528924 feet/sec YDOT = -4075
124178 meter/sec
ZDOT = 11665
293732 ZDOT = 3581
757677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6792750
19 X = 2070430
26
Y = 15946092
64 feet Y = 4860369
04 meter
Z = -13998239
37 Z = -4266663
36
XDOT = -13546
334405 XDOT = -4128
922727
YDOT = 16113
184855 feet/sec YDOT = 4911
298744 meter/sec
ZDOT = 11783
205133 ZDOT = 3591
520924
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 18256
56277900
00016717 00000-0 10270-3 0 9038
2 25544 51
6407 298
2965 0004737 151
9677 208
1731 15
53835028 12255
Satellite: ISS
Catalog Number: 25544
Epoch time: 18256
56277900 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 298
2965 deg
Eccentricity:
0004737
Arg of perigee: 151
9677 deg
Mean anomaly: 208
1731 deg
Mean motion: 15
53835028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1225
Checksum: 327
Coasting Arc #5 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2018/257/13:16:40
263
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 179642
19 A = 6786048
55 meter
Y = 6026667
83 meter E =
0015962
Z = 3094474
85 I = 51
29487
XDOT = -5317
071096 Wp = 110
05802
YDOT = 2658
283605 meter/sec RA = 292
57632 deg
ZDOT = -4853
458065 TA = 34
13083
MA = 34
02831
Ha = 222
592 n
mi
Hp = 214
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 589377
27 X = 97205
55
Y = 19772532
25 feet Y = 6028216
02 meter
Z = 10152476
56 Z = 3095146
80
XDOT = -17444
458977 XDOT = -5322
825902
YDOT = 8721
402903 feet/sec YDOT = 2598
791870 meter/sec
ZDOT = -15923
418848 ZDOT = -4879
300892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4540199
26 X = -1383852
73
Y = -19252042
48 feet Y = -5868022
55 meter
Z = 10154734
28 Z = 3095163
01
XDOT = 13793
620612 XDOT = 4204
295562
YDOT = -11739
263711 feet/sec YDOT = -3578
127579 meter/sec
ZDOT = -16039
641915 ZDOT = -4888
882856
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 18257
59180314
00016717 00000-0 10270-3 0 9045
2 25544 51
6387 293
1691 0004772 154
8413 205
2973 15
53859183 12413
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59180314 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 293
1691 deg
Eccentricity:
0004772
Arg of perigee: 154
8413 deg
Mean anomaly: 205
2973 deg
Mean motion: 15
53859183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 322
Coasting Arc #6 (Orbit 1240)
---------------------------------------
Vector Time (GMT): 2018/257/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3749161
91 A = 6778307
16 meter
Y = -2026877
27 meter E =
0017408
Z = -5285516
82 I = 51
26841
XDOT = 3205
791764 Wp = 107
16870
YDOT = -6941
332821 meter/sec RA = 292
48143 deg
ZDOT = 383
898140 TA = 166
54028
MA = 166
49379
Ha = 222
629 n
mi
Hp = 214
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12300399
98 X = -3700543
75
Y = -6649859
80 feet Y = -2068531
57 meter
Z = -17340934
45 Z = -5303610
81
XDOT = 10517
689516 XDOT = 3281
308627
YDOT = -22773
401644 feet/sec YDOT = -6905
061164 meter/sec
ZDOT = 1259
508334 ZDOT = 399
654819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13728926
46 X = 4184576
78
Y = 2055529
55 feet Y = 626525
41 meter
Z = -17421821
35 Z = -5310171
15
XDOT = -1887
304726 XDOT = -575
250481
YDOT = 23997
153738 feet/sec YDOT = 7314
332459 meter/sec
ZDOT = 1331
037761 ZDOT = 405
700309
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 18257
59180304
00016717 00000-0 10270-3 0 9055
2 25544 51
6387 293
1693 0004755 157
1224 203
0141 15
53822244 12413
Satellite: ISS
Catalog Number: 25544
Epoch time: 18257
59180304 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 293
1693 deg
Eccentricity:
0004755
Arg of perigee: 157
1224 deg
Mean anomaly: 203
0141 deg
Mean motion: 15
53822244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1241
Checksum: 292
Coasting Arc #7 (Orbit 1256)
---------------------------------------
Vector Time (GMT): 2018/258/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3032392
51 A = 6779742
06 meter
Y = 3528326
89 meter E =
0007038
Z = 4925185
77 I = 51
26126
XDOT = -3805
304552 Wp = 97
99490
YDOT = 6300
013004 meter/sec RA = 287
45929 deg
ZDOT = -2168
637642 TA = 13
25893
MA = 13
24045
Ha = 222
396 n
mi
Hp = 214
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9948794
34 X = 2968788
33
Y = 11575875
64 feet Y = 3561881
89 meter
Z = 16158745
98 Z = 4939761
45
XDOT = -12484
594988 XDOT = -3864
936073
YDOT = 20669
334001 feet/sec YDOT = 6257
125889 meter/sec
ZDOT = -7114
952893 ZDOT = -2187
267829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13348852
87 X = -4068730
35
Y = -7258446
57 feet Y = -2212374
52 meter
Z = 16223672
75 Z = 4944975
45
XDOT = 3633
853070 XDOT = 1107
598416
YDOT = -22786
797519 feet/sec YDOT = -6945
415884 meter/sec
ZDOT = -7199
277787 ZDOT = -2194
339869
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 18258
62082454
00016717 00000-0 10270-3 0 9068
2 25544 51
6381 288
0412 0004691 160
4929 199
6404 15
53852290 12570
Satellite: ISS
Catalog Number: 25544
Epoch time: 18258
62082454 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 288
0412 deg
Eccentricity:
0004691
Arg of perigee: 160
4929 deg
Mean anomaly: 199
6404 deg
Mean motion: 15
53852290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1257
Checksum: 322
Coasting Arc #8 (Orbit 1271)
---------------------------------------
Vector Time (GMT): 2018/259/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2314872
35 A = 6782953
92 meter
Y = -4870897
78 meter E =
0010988
Z = -4126178
54 I = 51
26301
XDOT = 4219
200858 Wp = 128
60258
YDOT = -5177
663318 meter/sec RA = 282
44363 deg
ZDOT = 3745
156499 TA = 180
22744
MA = 180
22794
Ha = 222
492 n
mi
Hp = 214
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7594725
56 X = -2240189
71
Y = -15980635
75 feet Y = -4896366
94 meter
Z = -13537331
18 Z = -4137241
76
XDOT = 13842
522499 XDOT = 4258
593287
YDOT = -16987
084376 feet/sec YDOT = -5130
260822 meter/sec
ZDOT = 12287
258855 ZDOT = 3765
747950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12962526
62 X = 3950978
11
Y = 11987656
35 feet Y = 3653837
65 meter
Z = -13586350
14 Z = -4141119
52
XDOT = -5490
624171 XDOT = -1673
542247
YDOT = 19968
213863 feet/sec YDOT = 6086
311586 meter/sec
ZDOT = 12380
232066 ZDOT = 3773
494734
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 18259
58553037
00016717 00000-0 10270-3 0 9075
2 25544 51
6383 283
2346 0004588 162
1582 197
9733 15
53826832 12720
Satellite: ISS
Catalog Number: 25544
Epoch time: 18259
58553037 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 283
2346 deg
Eccentricity:
0004588
Arg of perigee: 162
1582 deg
Mean anomaly: 197
9733 deg
Mean motion: 15
53826832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1272
Checksum: 339
Coasting Arc #9 (Orbit 1287)
---------------------------------------
Vector Time (GMT): 2018/260/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1586927
56 A = 6786449
75 meter
Y = 5909260
57 meter E =
0015381
Z = 2915343
65 I = 51
26765
XDOT = -4517
887313 Wp = 113
66158
YDOT = 3682
983740 meter/sec RA = 277
43584 deg
ZDOT = -4991
104579 TA = 32
87492
MA = 32
77935
Ha = 222
220 n
mi
Hp = 214
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5206455
25 X = 1506569
41
Y = 19387337
81 feet Y = 5926557
53 meter
Z = 9564775
77 Z = 2922856
92
XDOT = -14822
464938 XDOT = -4534
491500
YDOT = 12083
279986 feet/sec YDOT = 3632
368488 meter/sec
ZDOT = -16375
015024 ZDOT = -5013
091454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12328670
08 X = -3757778
64
Y = -15822384
38 feet Y = -4822662
76 meter
Z = 9597761
50 Z = 2925397
70
XDOT = 7648
530563 XDOT = 2331
272116
YDOT = -15982
236077 feet/sec YDOT = -4871
385556 meter/sec
ZDOT = -16474
058979 ZDOT = -5021
293177
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 18260
61454724
00016717 00000-0 10270-3 0 9085
2 25544 51
6369 278
1067 0004430 167
5120 192
6143 15
53870664 12886
Satellite: ISS
Catalog Number: 25544
Epoch time: 18260
61454724 = yrday
fracday
Element set: 908
Inclination: 51
6369 deg
RA of node: 278
1067 deg
Eccentricity:
0004430
Arg of perigee: 167
5120 deg
Mean anomaly: 192
6143 deg
Mean motion: 15
53870664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1288
Checksum: 315
Coasting Arc #10 (Orbit 1302)
---------------------------------------
Vector Time (GMT): 2018/261/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -892277
37 A = 6789165
68 meter
Y = -6569746
87 meter E =
0006321
Z = -1460069
70 I = 51
27343
XDOT = 4694
296376 Wp = 70
85203
YDOT = -1909
851444 meter/sec RA = 272
43724 deg
ZDOT = 5747
299691 TA = 273
14564
MA = 273
21796
Ha = 222
302 n
mi
Hp = 214
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2927419
20 X = -811654
08
Y = -21554287
62 feet Y = -6579274
22 meter
Z = -4790254
91 Z = -1464207
89
XDOT = 15401
234830 XDOT = 4687
386658
YDOT = -6265
916810 feet/sec YDOT = -1857
394887 meter/sec
ZDOT = 18855
970114 ZDOT = 5770
086246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11430070
31 X = 3483885
43
Y = 18502428
79 feet Y = 5639540
29 meter
Z = -4808041
38 Z = -1465491
01
XDOT = -10046
172290 XDOT = -3062
073314
YDOT = 11113
555259 feet/sec YDOT = 3387
411643 meter/sec
ZDOT = 18958
387171 ZDOT = 5778
516410
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 18261
57925032
00016717 00000-0 10270-3 0 9097
2 25544 51
6368 273
3004 0004655 169
4896 190
6354 15
53869422 13033
Satellite: ISS
Catalog Number: 25544
Epoch time: 18261
57925032 = yrday
fracday
Element set: 909
Inclination: 51
6368 deg
RA of node: 273
3004 deg
Eccentricity:
0004655
Arg of perigee: 169
4896 deg
Mean anomaly: 190
6354 deg
Mean motion: 15
53869422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1303
Checksum: 324
Coasting Arc #11 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2018/262/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 167621
80 A = 6790087
69 meter
Y = 6777407
85 meter E =
0015476
Z = -168397
47 I = 51
27684
XDOT = -4802
434343 Wp = 145
90936
YDOT = -22
903851 meter/sec RA = 267
44202 deg
ZDOT = -5982
211112 TA = 35
91457
MA = 35
81064
Ha = 222
119 n
mi
Hp = 214
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 549940
28 X = 92640
47
Y = 22235590
07 feet Y = 6778863
06 meter
Z = -552485
15 Z = -167765
76
XDOT = -15756
018185 XDOT = -4772
762961
YDOT = -75
143869 feet/sec YDOT = -76
442468 meter/sec
ZDOT = -19626
676878 ZDOT = -6005
467530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9913064
44 X = -3021502
04
Y = -19911235
98 feet Y = -6068944
73 meter
Z = -550431
66 Z = -167771
57
XDOT = 12736
994698 XDOT = 3882
235984
YDOT = -5821
326431 feet/sec YDOT = -1774
340296 meter/sec
ZDOT = -19730
978384 ZDOT = -6014
002211
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 18262
60826286
00016717 00000-0 10270-3 0 9105
2 25544 51
6375 268
1718 0004388 173
7903 186
3305 15
53864586 13196
Satellite: ISS
Catalog Number: 25544
Epoch time: 18262
60826286 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 268
1718 deg
Eccentricity:
0004388
Arg of perigee: 173
7903 deg
Mean anomaly: 186
3305 deg
Mean motion: 15
53864586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 335
Coasting Arc #12 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2018/263/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 545412
95 A = 6788686
11 meter
Y = -6533986
70 meter E =
0012790
Z = 1745183
54 I = 51
27420
XDOT = 4820
331447 Wp = 84
14167
YDOT = 1919
193752 meter/sec RA = 262
44774 deg
ZDOT = 5644
507027 TA = 295
10868
MA = 295
24134
Ha = 222
028 n
mi
Hp = 214
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1789412
57 X = 609960
12
Y = -21436964
24 feet Y = -6527526
48 meter
Z = 5725667
77 Z = 1747990
20
XDOT = 15814
735720 XDOT = 4771
094309
YDOT = 6296
567428 feet/sec YDOT = 1972
823154 meter/sec
ZDOT = 18518
723842 ZDOT = 5667
802696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7832333
60 X = 2387295
28
Y = 20031156
86 feet Y = 6105496
61 meter
Z = 5738990
30 Z = 1749244
24
XDOT = -15402
791886 XDOT = -4694
770967
YDOT = 654
704305 feet/sec YDOT = 199
553872 meter/sec
ZDOT = 18622
992997 ZDOT = 5676
288266
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 18263
63727125
00016717 00000-0 10270-3 0 9112
2 25544 51
6366 263
0449 0004584 179
1626 180
9535 15
53904537 13355
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
63727125 = yrday
fracday
Element set: 911
Inclination: 51
6366 deg
RA of node: 263
0449 deg
Eccentricity:
0004584
Arg of perigee: 179
1626 deg
Mean anomaly: 180
9535 deg
Mean motion: 15
53904537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 321
Coasting Arc #13 (Orbit 1349)
---------------------------------------
Vector Time (GMT): 2018/264/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1324868
56 A = 6785743
01 meter
Y = 5837244
44 meter E =
0006701
Z = -3194335
65 I = 51
26953
XDOT = -4739
078466 Wp = 140
03559
YDOT = -3680
250423 meter/sec RA = 257
44641 deg
ZDOT = -4770
265761 TA = 77
08759
MA = 77
01275
Ha = 221
910 n
mi
Hp = 214
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4346681
64 X = -1374527
45
Y = 19151064
44 feet Y = 5822150
90 meter
Z = -10480103
82 Z = -3200892
50
XDOT = -15548
157696 XDOT = -4674
401326
YDOT = -12074
312410 feet/sec YDOT = -3732
884877 meter/sec
ZDOT = -15650
478218 ZDOT = -4793
129045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4887288
23 X = -1489645
45
Y = -19003698
99 feet Y = -5792327
45 meter
Z = -10510153
42 Z = -3203494
76
XDOT = 17857
653367 XDOT = 5443
012746
YDOT = 4100
328673 feet/sec YDOT = 1249
780179 meter/sec
ZDOT = -15752
624854 ZDOT = -4801
400056
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 18264
60196873
00016717 00000-0 10270-3 0 9121
2 25544 51
6367 258
2370 0004330 182
5054 177
6077 15
53864823 13501
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
60196873 = yrday
fracday
Element set: 912
Inclination: 51
6367 deg
RA of node: 258
2370 deg
Eccentricity:
0004330
Arg of perigee: 182
5054 deg
Mean anomaly: 177
6077 deg
Mean motion: 15
53864823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1350
Checksum: 316
Coasting Arc #14 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2018/265/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2111495
11 A = 6782043
52 meter
Y = -4788302
70 meter E =
0011340
Z = 4311039
73 I = 51
26672
XDOT = 4533
519099 Wp = 130
90681
YDOT = 5126
344595 meter/sec RA = 252
43777 deg
ZDOT = 3460
120424 TA = 283
68964
MA = 283
81587
Ha = 221
743 n
mi
Hp = 215
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6927477
38 X = 2143941
61
Y = -15709654
52 feet Y = -4764508
62 meter
Z = 14143831
15 Z = 4321375
93
XDOT = 14873
750325 XDOT = 4459
050557
YDOT = 16818
715862 feet/sec YDOT = 5176
625536 meter/sec
ZDOT = 11352
101127 ZDOT = 3481
961209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1340612
20 X = 408618
60
Y = 17077990
55 feet Y = 5205371
52 meter
Z = 14190706
30 Z = 4325327
28
XDOT = -19716
438957 XDOT = -6009
570594
YDOT = -8002
179095 feet/sec YDOT = -2439
064188 meter/sec
ZDOT = 11449
521180 ZDOT = 3489
814056
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 18265
63097264
00016717 00000-0 10270-3 0 9130
2 25544 51
6377 253
1098 0004453 188
4941 171
6137 15
53906164 13662
Satellite: ISS
Catalog Number: 25544
Epoch time: 18265
63097264 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 253
1098 deg
Eccentricity:
0004453
Arg of perigee: 188
4941 deg
Mean anomaly: 171
6137 deg
Mean motion: 15
53906164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 326
Coasting Arc #15 (Orbit 1380)
---------------------------------------
Vector Time (GMT): 2018/266/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2953052
97 A = 6779222
85 meter
Y = 3443390
83 meter E =
0012033
Z = -5048015
50 I = 51
26775
XDOT = -4139
583569 Wp = 95
17642
YDOT = -6186
956140 meter/sec RA = 247
41900 deg
ZDOT = -1803
457679 TA = 157
28235
MA = 157
22905
Ha = 221
698 n
mi
Hp = 215
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9688494
01 X = -2966817
86
Y = 11297214
02 feet Y = 3410290
18 meter
Z = -16561730
63 Z = -5062394
24
XDOT = -13581
310921 XDOT = -4061
331399
YDOT = -20298
412532 feet/sec YDOT = -6232
810516 meter/sec
ZDOT = -5916
855901 ZDOT = -1823
375533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2905086
15 X = 885470
26
Y = -14522461
98 feet Y = -4426446
41 meter
Z = -16626588
79 Z = -5067784
26
XDOT = 20622
623960 XDOT = 6285
775783
YDOT = 10983
131714 feet/sec YDOT = 3347
658546 meter/sec
ZDOT = -6005
556953 ZDOT = -1830
493759
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 18266
59566406
00016717 00000-0 10270-3 0 9146
2 25544 51
6375 248
3014 0004229 190
6159 169
4905 15
53867149 13815
Satellite: ISS
Catalog Number: 25544
Epoch time: 18266
59566406 = yrday
fracday
Element set: 914
Inclination: 51
6375 deg
RA of node: 248
3014 deg
Eccentricity:
0004229
Arg of perigee: 190
6159 deg
Mean anomaly: 169
4905 deg
Mean motion: 15
53867149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1381
Checksum: 335
Coasting Arc #16 (Orbit 1396)
---------------------------------------
Vector Time (GMT): 2018/267/13:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3759209
16 A = 6778066
78 meter
Y = -1959843
67 meter E =
0004286
Z = 5287501
70 I = 51
27806
XDOT = 3548
678080 Wp = 162
51510
YDOT = 6799
225168 meter/sec RA = 242
39804 deg
ZDOT = -6
817121 TA = 287
52676
MA = 287
57359
Ha = 221
478 n
mi
Hp = 215
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12333363
37 X = 3755161
29
Y = -6429933
31 feet Y = -1917827
54 meter
Z = 17347446
51 Z = 5305753
11
XDOT = 11642
644621 XDOT = 3472
416625
YDOT = 22307
169186 feet/sec YDOT = 6838
482544 meter/sec
ZDOT = -22
365884 ZDOT = 10
235089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7372894
07 X = -2247258
11
Y = 11672276
73 feet Y = 3557709
95 meter
Z = 17429520
46 Z = 5312517
84
XDOT = -20377
824726 XDOT = -6211
160976
YDOT = -12971
208989 feet/sec YDOT = -3953
624500 meter/sec
ZDOT = 53
435977 ZDOT = 16
287286
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 18267
62466499
00016717 00000-0 10270-3 0 9153
2 25544 51
6377 243
1746 0004194 195
4476 164
6549 15
53881371 13979
Satellite: ISS
Catalog Number: 25544
Epoch time: 18267
62466499 = yrday
fracday
Element set: 915
Inclination: 51
6377 deg
RA of node: 243
1746 deg
Eccentricity:
0004194
Arg of perigee: 195
4476 deg
Mean anomaly: 164
6549 deg
Mean motion: 15
53881371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 356
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