[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 20th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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
201/19:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 215
3
203/18:49:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 215
1
206/03:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
8
207/15:56:37
126 -1
2 1
3 1
3
N/A 0
4 -0
1 221
8
000/00:03:14
253 -0
3 -0
0 215
4
209/20:18:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 215
3
212/23:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
9
215/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
7
216/02:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
6
Coasting Arc #1 (Orbit 368)
---------------------------------------
Vector Time (GMT): 2018/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4871209
72 A = 6780891
55 meter
Y = 1269310
69 meter E =
0007773
Z = -4549777
70 I = 51
42537
XDOT = -4315
320413 Wp = 87
75127
YDOT = -5530
342155 meter/sec RA = 211
52096 deg
ZDOT = 3082
182402 TA = 213
19122
MA = 213
24000
Ha = 221
173 n
mi
Hp = 215
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15981659
18 X = -4862941
22
Y = 4164405
15 feet Y = 1214883
99 meter
Z = -14927092
21 Z = -4573420
00
XDOT = -14157
875370 XDOT = -4268
129376
YDOT = -18144
167174 feet/sec YDOT = -5578
335391 meter/sec
ZDOT = 10112
146989 ZDOT = 3061
334491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10993110
53 X = 3350700
09
Y = 12195528
36 feet Y = 3717197
04 meter
Z = -15033109
83 Z = -4582091
88
XDOT = -8693
289894 XDOT = -2649
714760
YDOT = 20167
315928 feet/sec YDOT = 6146
997895 meter/sec
ZDOT = 10019
420676 ZDOT = 3053
919422
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 18201
51062806
00016717 00000-0 10270-3 0 9007
2 25544 51
6384 212
6239 0004169 336
3803 23
7158 15
53971967 3697
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
51062806 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 212
6239 deg
Eccentricity:
0004169
Arg of perigee: 336
3803 deg
Mean anomaly: 23
7158 deg
Mean motion: 15
53971967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 369
Checksum: 308
Coasting Arc #2 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2018/201/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1690498
22 A = 6777766
53 meter
Y = 3897769
54 meter E =
0013916
Z = -5292496
72 I = 51
42577
XDOT = -6786
491616 Wp = 69
63737
YDOT = -3523
804916 meter/sec RA = 209
97251 deg
ZDOT = -423
641289 TA = 196
28290
MA = 196
32765
Ha = 221
205 n
mi
Hp = 215
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5546254
01 X = -1708250
55
Y = 12787957
80 feet Y = 3878766
33 meter
Z = -17363834
39 Z = -5300751
36
XDOT = -22265
392442 XDOT = -6744
525265
YDOT = -11561
039751 feet/sec YDOT = -3599
461474 meter/sec
ZDOT = -1389
899243 ZDOT = -456
505782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6552179
51 X = -1997104
31
Y = -12249944
46 feet Y = -3733783
07 meter
Z = -17401245
56 Z = -5303899
65
XDOT = 22070
384408 XDOT = 6727
053168
YDOT = -9604
167258 feet/sec YDOT = -2927
350180 meter/sec
ZDOT = -1536
672691 ZDOT = -468
377836
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 18201
83216750
00016717 00000-0 10270-3 0 9012
2 25544 51
6401 211
0223 0004352 336
7904 23
3052 15
54013035 3742
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
83216750 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 211
0223 deg
Eccentricity:
0004352
Arg of perigee: 336
7904 deg
Mean anomaly: 23
3052 deg
Mean motion: 15
54013035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 248
Coasting Arc #3 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2018/202/19:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3230333
18 A = 6778277
23 meter
Y = -3013471
91 meter E =
0007104
Z = 5140463
76 I = 51
45721
XDOT = 6251
278637 Wp = 18
15866
YDOT = 4194
631344 meter/sec RA = 204
96024 deg
ZDOT = -1462
217536 TA = 85
99157
MA = 85
91037
Ha = 221
160 n
mi
Hp = 215
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10598205
97 X = 3238821
09
Y = -9886718
85 feet Y = -2977301
06 meter
Z = 16865038
59 Z = 5156175
85
XDOT = 20509
444348 XDOT = 6211
011138
YDOT = 13761
913858 feet/sec YDOT = 4264
312431 meter/sec
ZDOT = -4797
301626 ZDOT = -1431
948661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1368854
13 X = 417226
74
Y = 14345914
39 feet Y = 4372634
71 meter
Z = 16935751
68 Z = 5162017
11
XDOT = -22425
465975 XDOT = -6835
282029
YDOT = 7671
289536 feet/sec YDOT = 2338
209051 meter/sec
ZDOT = -4662
208532 ZDOT = -1421
041161
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 18202
86108773
00016717 00000-0 10270-3 0 9022
2 25544 51
6403 205
8938 0004449 339
8396 20
2580 15
54040308 3907
Satellite: ISS
Catalog Number: 25544
Epoch time: 18202
86108773 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 205
8938 deg
Eccentricity:
0004449
Arg of perigee: 339
8396 deg
Mean anomaly: 20
2580 deg
Mean motion: 15
54040308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 303
Coasting Arc #4 (Orbit 404)
---------------------------------------
Vector Time (GMT): 2018/203/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5016972
54 A = 6782006
97 meter
Y = -1736040
18 meter E =
0011101
Z = 4217631
32 I = 51
49773
XDOT = 4733
815142 Wp = 50
51845
YDOT = 4813
688809 meter/sec RA = 200
10963 deg
ZDOT = -3636
276485 TA = 76
83963
MA = 76
71578
Ha = 221
382 n
mi
Hp = 215
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16459883
65 X = 5015525
69
Y = -5695669
88 feet Y = -1679945
42 meter
Z = 13837373
11 Z = 4241998
15
XDOT = 15530
889572 XDOT = 4697
298286
YDOT = 15792
942287 feet/sec YDOT = 4866
421770 meter/sec
ZDOT = -11930
040961 ZDOT = -3613
369672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8394391
42 X = -2558610
50
Y = 15161285
36 feet Y = 4621159
78 meter
Z = 13946717
85 Z = 4250959
60
XDOT = -21058
020376 XDOT = -6418
484611
YDOT = -738
922757 feet/sec YDOT = -225
223656 meter/sec
ZDOT = -11827
974646 ZDOT = -3605
166672
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 18203
82570242
00016717 00000-0 10270-3 0 9034
2 25544 51
6391 201
0865 0004443 346
0748 14
0281 15
54011537 4053
Satellite: ISS
Catalog Number: 25544
Epoch time: 18203
82570242 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 201
0865 deg
Eccentricity:
0004443
Arg of perigee: 346
0748 deg
Mean anomaly: 14
0281 deg
Mean motion: 15
54011537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 271
Coasting Arc #5 (Orbit 419)
---------------------------------------
Vector Time (GMT): 2018/204/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6010158
78 A = 6785690
52 meter
Y = 864999
55 meter E =
0006595
Z = -3024921
98 I = 51
54182
XDOT = -3188
117419 Wp = 30
79689
YDOT = -4922
996507 meter/sec RA = 195
11769 deg
ZDOT = 4936
956520 TA = 294
49240
MA = 294
56117
Ha = 221
423 n
mi
Hp = 214
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19718368
69 X = -6004691
44
Y = 2837925
02 feet Y = 797820
69 meter
Z = -9924284
70 Z = -3054103
57
XDOT = -10459
702819 XDOT = -3156
811044
YDOT = -16151
563343 feet/sec YDOT = -4958
473714 meter/sec
ZDOT = 16197
363910 ZDOT = 4921
545430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12483588
28 X = 3804997
71
Y = -15440658
84 feet Y = -4706312
82 meter
Z = -10055117
46 Z = -3064799
80
XDOT = 17602
948246 XDOT = 5365
378625
YDOT = 3750
237948 feet/sec YDOT = 1143
072526 meter/sec
ZDOT = 16128
873116 ZDOT = 4916
080526
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 18204
79031410
00016717 00000-0 10270-3 0 9041
2 25544 51
6395 196
2785 0004464 347
3207 12
7833 15
54008981 4204
Satellite: ISS
Catalog Number: 25544
Epoch time: 18204
79031410 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 196
2785 deg
Eccentricity:
0004464
Arg of perigee: 347
3207 deg
Mean anomaly: 12
7833 deg
Mean motion: 15
54008981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 299
Coasting Arc #6 (Orbit 435)
---------------------------------------
Vector Time (GMT): 2018/205/18:49:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6617302
04 A = 6788752
03 meter
Y = -24579
99 meter E =
0011916
Z = 1499226
57 I = 51
58406
XDOT = 1331
776821 Wp = 100
75339
YDOT = 4879
664251 meter/sec RA = 190
13782 deg
ZDOT = -5761
431696 TA = 62
86644
MA = 62
74497
Ha = 221
645 n
mi
Hp = 214
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21710308
53 X = 6609802
74
Y = -80643
01 feet Y = 49377
16 meter
Z = 4918722
36 Z = 1531352
48
XDOT = 4369
346525 XDOT = 1305
097706
YDOT = 16009
397148 feet/sec YDOT = 4894
408557 meter/sec
ZDOT = -18902
334960 ZDOT = -5755
026736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15586104
67 X = -4750644
70
Y = 15065872
07 feet Y = 4592077
81 meter
Z = 5062674
14 Z = 1543103
08
XDOT = -13227
519038 XDOT = -4031
747803
YDOT = -7302
477768 feet/sec YDOT = -2225
795224 meter/sec
ZDOT = -18874
179966 ZDOT = -5752
850054
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 18205
81923194
00016717 00000-0 10270-3 0 9055
2 25544 51
6397 191
1504 0004367 352
4363 7
6723 15
53980215 4367
Satellite: ISS
Catalog Number: 25544
Epoch time: 18205
81923194 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 191
1504 deg
Eccentricity:
0004367
Arg of perigee: 352
4363 deg
Mean anomaly: 7
6723 deg
Mean motion: 15
53980215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 306
Coasting Arc #7 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2018/206/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -885536
61 A = 6777675
78 meter
Y = 4131308
42 meter E =
0014826
Z = -5311886
86 I = 51
55756
XDOT = -7540
769033 Wp = 76
46937
YDOT = -1312
366845 meter/sec RA = 188
44418 deg
ZDOT = 240
376326 TA = 195
80430
MA = 195
85062
Ha = 221
529 n
mi
Hp = 214
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2905303
83 X = -905866
26
Y = 13554161
50 feet Y = 4121292
65 meter
Z = -17427450
33 Z = -5316237
35
XDOT = -24740
055882 XDOT = -7526
700948
YDOT = -4305
665503 feet/sec YDOT = -1396
614298 meter/sec
ZDOT = 788
636239 ZDOT = 203
780439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5788408
66 X = -1764306
96
Y = 12567994
87 feet Y = 3830724
84 meter
Z = -17447404
95 Z = -5317969
03
XDOT = -22208
716984 XDOT = -6769
216937
YDOT = -9379
244437 feet/sec YDOT = -2858
793705 meter/sec
ZDOT = 624
795434 ZDOT = 190
437648
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 18206
14076715
00016717 00000-0 10270-3 0 9061
2 25544 51
6388 189
5430 0003996 353
3535 6
7564 15
54023275 4418
Satellite: ISS
Catalog Number: 25544
Epoch time: 18206
14076715 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 189
5430 deg
Eccentricity:
0003996
Arg of perigee: 353
3535 deg
Mean anomaly: 6
7564 deg
Mean motion: 15
54023275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 313
Coasting Arc #8 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2018/207/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2611032
21 A = 6779137
16 meter
Y = -3792710
62 meter E =
0008828
Z = 4973439
94 I = 51
59491
XDOT = 7070
980309 Wp = 34
36905
YDOT = 2096
553321 meter/sec RA = 183
44174 deg
ZDOT = -2104
456116 TA = 76
17637
MA = 76
07815
Ha = 221
598 n
mi
Hp = 214
779
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8566378
64 X = 2629091
37
Y = -12443276
31 feet Y = -3763411
80 meter
Z = 16317060
17 Z = 4986166
67
XDOT = 23198
754296 XDOT = 7057
232704
YDOT = 6878
455776 feet/sec YDOT = 2175
549257 meter/sec
ZDOT = -6904
383582 ZDOT = -2070
141517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10880394
98 X = 3316344
39
Y = -10390216
33 feet Y = -3166937
94 meter
Z = 16374517
71 Z = 4990953
00
XDOT = 20525
658971 XDOT = 6256
220854
YDOT = 10808
841562 feet/sec YDOT = 3294
534908 meter/sec
ZDOT = -6750
826595 ZDOT = -2057
651946
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 18207
16968232
00016717 00000-0 10270-3 0 9079
2 25544 51
6385 184
4141 0004009 358
1890 1
9247 15
53997775 4577
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
16968232 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 184
4141 deg
Eccentricity:
0004009
Arg of perigee: 358
1890 deg
Mean anomaly: 1
9247 deg
Mean motion: 15
53997775 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 330
Coasting Arc #9 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2018/207/15:58:14
253
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1597496
45 A = 6779108
80 meter
Y = 4110858
68 meter E =
0014249
Z = -5160628
75 I = 51
61048
XDOT = -7442
580118 Wp = 61
50293
YDOT = 1055
274655 meter/sec RA = 180
78011 deg
ZDOT = -1459
698742 TA = 194
40102
MA = 194
44167
Ha = 221
828 n
mi
Hp = 215
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5241130
07 X = 1576476
10
Y = 13487069
15 feet Y = 4128605
97 meter
Z = -16931196
67 Z = -5152919
45
XDOT = -24417
913772 XDOT = -7446
737035
YDOT = 3462
187188 feet/sec YDOT = 972
023486 meter/sec
ZDOT = -4789
037866 ZDOT = -1495
861521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6047055
53 X = -1843142
53
Y = -13189282
15 feet Y = -4020093
20 meter
Z = -16897096
06 Z = -5150234
88
XDOT = 23210
931705 XDOT = 7074
691984
YDOT = -4283
603359 feet/sec YDOT = -1305
642304 meter/sec
ZDOT = -4951
239970 ZDOT = -1509
137943
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 18207
68414010
00016717 00000-0 10270-3 0 9087
2 25544 51
6386 181
8539 0004289 347
3404 12
7640 15
53787298 4654
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
68414010 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 181
8539 deg
Eccentricity:
0004289
Arg of perigee: 347
3404 deg
Mean anomaly: 12
7640 deg
Mean motion: 15
53787298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 325
Coasting Arc #10 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2018/208/15:58:14
253
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 78580
55 A = 6778293
63 meter
Y = -4216189
23 meter E =
0005062
Z = 5305730
18 I = 51
64160
XDOT = 7656
247937 Wp = 18
29209
YDOT = -293
301413 meter/sec RA = 175
78362 deg
ZDOT = -341
675216 TA = 74
99284
MA = 74
93682
Ha = 221
779 n
mi
Hp = 215
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 257810
21 X = 99949
41
Y = -13832641
85 feet Y = -4215191
47 meter
Z = 17407251
26 Z = 5306163
43
XDOT = 25118
923679 XDOT = 7660
618334
YDOT = -962
274978 feet/sec YDOT = -207
659495 meter/sec
ZDOT = -1120
981680 ZDOT = -304
474014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 814425
62 X = 248236
93
Y = 13808021
40 feet Y = 4208684
92 meter
Z = 17409655
34 Z = 5306462
95
XDOT = -23992
234831 XDOT = -7312
833176
YDOT = 2637
989426 feet/sec YDOT = 804
059177 meter/sec
ZDOT = -954
183936 ZDOT = -290
835264
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 18208
71320711
00016717 00000-0 10270-3 0 9097
2 25544 51
6390 176
7268 0004330 347
9675 12
1373 15
53813173 4811
Satellite: ISS
Catalog Number: 25544
Epoch time: 18208
71320711 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 176
7268 deg
Eccentricity:
0004330
Arg of perigee: 347
9675 deg
Mean anomaly: 12
1373 deg
Mean motion: 15
53813173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 302
Coasting Arc #11 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2018/209/15:58:14
253
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1711843
57 A = 6779756
94 meter
Y = 4271602
77 meter E =
0011794
Z = -4988619
76 I = 51
68040
XDOT = -7348
181571 Wp = 85
38464
YDOT = -493
320326 meter/sec RA = 170
78996 deg
ZDOT = 2104
327326 TA = 205
08477
MA = 205
14211
Ha = 221
990 n
mi
Hp = 215
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5616284
68 X = -1735251
04
Y = 14014444
79 feet Y = 4252329
22 meter
Z = -16366862
74 Z = -4996991
67
XDOT = -24108
207254 XDOT = -7352
340484
YDOT = -1618
505007 feet/sec YDOT = -575
516170 meter/sec
ZDOT = 6903
961042 ZDOT = 2068
623063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4277724
07 X = 1303850
30
Y = -14436172
02 feet Y = -4400145
23 meter
Z = -16404862
89 Z = -5000202
21
XDOT = 23150
315400 XDOT = 7056
216134
YDOT = -784
322599 feet/sec YDOT = -239
061528 meter/sec
ZDOT = 6743
936524 ZDOT = 2055
551853
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 18209
67795735
00016717 00000-0 10270-3 0 9107
2 25544 51
6402 171
9199 0004396 353
6097 6
4999 15
53782501 4965
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
67795735 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 171
9199 deg
Eccentricity:
0004396
Arg of perigee: 353
6097 deg
Mean anomaly: 6
4999 deg
Mean motion: 15
53782501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 346
Coasting Arc #12 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2018/209/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5575652
86 A = 6785415
36 meter
Y = 1772967
55 meter E =
0006123
Z = -3444810
52 I = 51
70141
XDOT = -4242
299907 Wp = 45
36894
YDOT = 4431
774382 meter/sec RA = 169
93171 deg
ZDOT = -4586
326744 TA = 174
90943
MA = 174
90321
Ha = 221
988 n
mi
Hp = 215
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18292824
35 X = 5572145
36
Y = 5816822
67 feet Y = 1835298
97 meter
Z = -11301871
80 Z = -3417734
94
XDOT = -13918
306782 XDOT = -4269
264478
YDOT = 14539
942199 feet/sec YDOT = 4384
183593 meter/sec
ZDOT = -15047
003753 ZDOT = -4606
999102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11728864
43 X = -3574957
88
Y = 15284682
51 feet Y = 4658771
23 meter
Z = -11180669
69 Z = -3407868
12
XDOT = -7842
909069 XDOT = -2390
518684
YDOT = -17091
309652 feet/sec YDOT = -5209
431182 meter/sec
ZDOT = -15140
171456 ZDOT = -4614
724260
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 18209
87090552
00016717 00000-0 10270-3 0 9115
2 25544 51
6367 170
9566 0004395 353
1446 6
9646 15
53783651 4998
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
87090552 = yrday
fracday
Element set: 911
Inclination: 51
6367 deg
RA of node: 170
9566 deg
Eccentricity:
0004395
Arg of perigee: 353
1446 deg
Mean anomaly: 6
9646 deg
Mean motion: 15
53783651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 337
Coasting Arc #13 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2018/210/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4432241
07 A = 6781951
06 meter
Y = -2476442
54 meter E =
0008237
Z = 4488753
82 I = 51
72187
XDOT = 5590
944348 Wp = 82
96849
YDOT = -4143
059822 meter/sec RA = 164
95252 deg
ZDOT = 3230
737746 TA = 334
57057
MA = 334
61108
Ha = 222
186 n
mi
Hp = 215
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14541473
33 X = -4426022
92
Y = -8124811
48 feet Y = -2525972
37 meter
Z = 14726882
60 Z = 4467238
98
XDOT = 18342
993269 XDOT = 5621
164782
YDOT = -13592
715952 feet/sec YDOT = -4080
369205 meter/sec
ZDOT = 10599
533286 ZDOT = 3257
969217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12436387
14 X = 3790610
80
Y = -11208376
38 feet Y = -3416313
12 meter
Z = 14630675
07 Z = 4459429
76
XDOT = 6105
846285 XDOT = 1861
061948
YDOT = 20788
373761 feet/sec YDOT = 6336
296322 meter/sec
ZDOT = 10722
091625 ZDOT = 3268
093527
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 18210
89997094
00016717 00000-0 10270-3 0 9127
2 25544 51
6366 165
8290 0004368 355
6469 4
4645 15
53761978 5155
Satellite: ISS
Catalog Number: 25544
Epoch time: 18210
89997094 = yrday
fracday
Element set: 912
Inclination: 51
6366 deg
RA of node: 165
8290 deg
Eccentricity:
0004368
Arg of perigee: 355
6469 deg
Mean anomaly: 4
4645 deg
Mean motion: 15
53761978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 346
Coasting Arc #14 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2018/211/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3057103
50 A = 6779221
65 meter
Y = 3204120
93 meter E =
0015039
Z = -5145930
98 I = 51
74466
XDOT = -6520
018669 Wp = 62
31607
YDOT = 3694
680271 meter/sec RA = 159
96700 deg
ZDOT = -1569
624738 TA = 192
53220
MA = 192
56964
Ha = 222
125 n
mi
Hp = 215
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10029867
12 X = 3046042
64
Y = 10512207
78 feet Y = 3238245
90 meter
Z = -16882975
65 Z = -5131107
69
XDOT = -21391
137365 XDOT = -6553
224771
YDOT = 12121
654434 feet/sec YDOT = 3621
583300 meter/sec
ZDOT = -5149
687459 ZDOT = -1601
376618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13125944
21 X = -4000787
80
Y = 6406477
97 feet Y = 1952694
49 meter
Z = -16816844
00 Z = -5125774
05
XDOT = -4478
159550 XDOT = -1364
943031
YDOT = -23096
279523 feet/sec YDOT = -7039
745998 meter/sec
ZDOT = -5292
483318 ZDOT = -1613
148915
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 18211
86471718
00016717 00000-0 10270-3 0 9136
2 25544 51
6366 161
0217 0004236
8198 359
2961 15
53785972 5303
Satellite: ISS
Catalog Number: 25544
Epoch time: 18211
86471718 = yrday
fracday
Element set: 913
Inclination: 51
6366 deg
RA of node: 161
0217 deg
Eccentricity:
0004236
Arg of perigee:
8198 deg
Mean anomaly: 359
2961 deg
Mean motion: 15
53785972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 313
Coasting Arc #15 (Orbit 545)
---------------------------------------
Vector Time (GMT): 2018/212/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1530455
52 A = 6778458
83 meter
Y = -3909608
51 meter E =
0005427
Z = 5319363
17 I = 51
77285
XDOT = 7023
389333 Wp = 31
72049
YDOT = -3074
497690 meter/sec RA = 154
97894 deg
ZDOT = -234
340942 TA = 60
53542
MA = 60
48129
Ha = 222
314 n
mi
Hp = 214
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5021179
52 X = -1512461
66
Y = -12826799
58 feet Y = -3926622
61 meter
Z = 17451978
91 Z = 5311972
51
XDOT = 23042
615923 XDOT = 7058
385510
YDOT = -10086
934679 feet/sec YDOT = -2995
761615 meter/sec
ZDOT = -768
835110 ZDOT = -200
139410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13766410
65 X = 4196001
96
Y = -1168830
34 feet Y = -356259
49 meter
Z = 17419252
93 Z = 5309388
29
XDOT = 2833
876958 XDOT = 863
765697
YDOT = 23984
133701 feet/sec YDOT = 7310
363952 meter/sec
ZDOT = -615
103682 ZDOT = -187
483602
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 18212
89377838
00016717 00000-0 10270-3 0 9149
2 25544 51
6368 155
8938 0004275 5
3571 354
7627 15
53750617 5468
Satellite: ISS
Catalog Number: 25544
Epoch time: 18212
89377838 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node: 155
8938 deg
Eccentricity:
0004275
Arg of perigee: 5
3571 deg
Mean anomaly: 354
7627 deg
Mean motion: 15
53750617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 546
Checksum: 341
Coasting Arc #16 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2018/212/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1879290
39 A = 6778323
58 meter
Y = -3748118
44 meter E =
0004728
Z = 5323433
54 I = 51
77918
XDOT = 6891
623887 Wp = 37
13422
YDOT = -3367
563640 meter/sec RA = 154
34314 deg
ZDOT = 65
515452 TA = 52
26429
MA = 52
22145
Ha = 222
211 n
mi
Hp = 214
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6165650
90 X = -1863096
22
Y = -12296976
52 feet Y = -3769043
51 meter
Z = 17465333
13 Z = 5314344
02
XDOT = 22610
314589 XDOT = 6928
450482
YDOT = -11048
437139 feet/sec YDOT = -3290
290828 meter/sec
ZDOT = 214
945709 ZDOT = 99
081382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7653229
62 X = 2332704
39
Y = -11492051
74 feet Y = -3502777
37 meter
Z = 17424969
64 Z = 5311130
75
XDOT = 19855
377360 XDOT = 6051
919019
YDOT = 13759
396714 feet/sec YDOT = 4193
864118 meter/sec
ZDOT = 365
860091 ZDOT = 111
514156
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 18213
02241056
00016717 00000-0 10270-3 0 9158
2 25544 51
6394 155
2515 0004035 6
0275 354
0925 15
53793887 5487
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
02241056 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 155
2515 deg
Eccentricity:
0004035
Arg of perigee: 6
0275 deg
Mean anomaly: 354
0925 deg
Mean motion: 15
53793887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 299
Coasting Arc #17 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2018/213/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 378739
54 A = 6779230
35 meter
Y = 4449553
40 meter E =
0013840
Z = -5112287
88 I = 51
81127
XDOT = -7003
929795 Wp = 86
48689
YDOT = 2572
057710 meter/sec RA = 149
35968 deg
ZDOT = 1724
598014 TA = 200
13581
MA = 200
19045
Ha = 222
218 n
mi
Hp = 214
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1242583
81 X = 353787
72
Y = 14598272
32 feet Y = 4453649
27 meter
Z = -16772598
02 Z = -5110508
67
XDOT = -22978
772293 XDOT = -7040
547784
YDOT = 8438
509546 feet/sec YDOT = 2493
530161 meter/sec
ZDOT = 5658
129967 ZDOT = 1690
486909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11925463
23 X = -3634881
19
Y = 8525747
08 feet Y = 2598647
71 meter
Z = -16765099
96 Z = -5110002
47
XDOT = -18266
363645 XDOT = -5567
587639
YDOT = -14756
781153 feet/sec YDOT = -4497
866895 meter/sec
ZDOT = 5504
840046 ZDOT = 1677
875246
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 18213
98715276
00016717 00000-0 10270-3 0 9164
2 25544 51
6389 150
4462 0003950 10
5489 349
5746 15
53804058 5631
Satellite: ISS
Catalog Number: 25544
Epoch time: 18213
98715276 = yrday
fracday
Element set: 916
Inclination: 51
6389 deg
RA of node: 150
4462 deg
Eccentricity:
0003950
Arg of perigee: 10
5489 deg
Mean anomaly: 349
5746 deg
Mean motion: 15
53804058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 329
Coasting Arc #18 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2018/214/23:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 944334
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1074126
90 A = 6782086
42 meter
Y = -5033392
28 meter E =
0011973
Z = 4412384
70 I = 51
84894
XDOT = 6710
111206 Wp = 54
69009
YDOT = -1541
923076 meter/sec RA = 144
38079 deg
ZDOT = -3379
204178 TA = 69
44962
MA = 69
32119
Ha = 222
307 n
mi
Hp = 214
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3524038
38 X = 1108899
03
Y = -16513754
19 feet Y = -5021186
28 meter
Z = 14476327
74 Z = 4417686
77
XDOT = 22014
800545 XDOT = 6743
268934
YDOT = -5058
802742 feet/sec YDOT = -1466
700532 meter/sec
ZDOT = -11086
627879 ZDOT = -3346
528601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15895315
94 X = 4844892
30
Y = -5635305
24 feet Y = -1717641
04 meter
Z = 14500663
95 Z = 4419802
37
XDOT = 15372
733826 XDOT = 4685
609270
YDOT = 15099
778035 feet/sec YDOT = 4602
412345 meter/sec
ZDOT = -10939
873858 ZDOT = -3334
473552
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 18215
01620966
00016717 00000-0 10270-3 0 9172
2 25544 51
6394 145
3182 0003914 14
7217 345
4049 15
53769920 5790
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
01620966 = yrday
fracday
Element set: 917
Inclination: 51
6394 deg
RA of node: 145
3182 deg
Eccentricity:
0003914
Arg of perigee: 14
7217 deg
Mean anomaly: 345
4049 deg
Mean motion: 15
53769920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 316
Coasting Arc #19 (Orbit 586)
---------------------------------------
Vector Time (GMT): 2018/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919627
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5661403
05 A = 6790062
09 meter
Y = -3660239
29 meter E =
0008513
Z = -795954
59 I = 51
88974
XDOT = 1999
860877 Wp = 115
22985
YDOT = 4378
452546 meter/sec RA = 141
80253 deg
ZDOT = -5963
386897 TA = 73
34026
MA = 73
24682
Ha = 222
459 n
mi
Hp = 214
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18574156
98 X = 5705778
38
Y = -12008659
07 feet Y = -3596681
43 meter
Z = -2611399
56 Z = -768345
97
XDOT = 6561
223350 XDOT = 1979
717921
YDOT = 14365
001792 feet/sec YDOT = 4400
703849 meter/sec
ZDOT = -19564
917641 ZDOT = -5953
721198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21275194
65 X = -6484679
33
Y = -6099742
08 feet Y = -1859201
39 meter
Z = -2487136
26 Z = -758079
13
XDOT = 5970
001486 XDOT = 1819
656453
YDOT = -12937
527471 feet/sec YDOT = -3943
358373 meter/sec
ZDOT = -19522
036054 ZDOT = -5950
316589
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 18215
53073623
00016717 00000-0 10270-3 0 9182
2 25544 51
6395 142
7583 0004525 13
7220 346
4055 15
53790899 5875
Satellite: ISS
Catalog Number: 25544
Epoch time: 18215
53073623 = yrday
fracday
Element set: 918
Inclination: 51
6395 deg
RA of node: 142
7583 deg
Eccentricity:
0004525
Arg of perigee: 13
7220 deg
Mean anomaly: 346
4055 deg
Mean motion: 15
53790899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 587
Checksum: 321
Coasting Arc #20 (Orbit 596)
---------------------------------------
Vector Time (GMT): 2018/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 919627
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5461932
25 A = 6783722
87 meter
Y = 661665
20 meter E =
0012324
Z = 3956305
04 I = 51
88464
XDOT = 2191
527135 Wp = 80
03772
YDOT = -6141
937554 meter/sec RA = 138
74979 deg
ZDOT = 4044
134532 TA = 327
86783
MA = 327
94289
Ha = 222
511 n
mi
Hp = 214
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17919725
23 X = -5488142
74
Y = 2170817
57 feet Y = 600439
45 meter
Z = 12980003
40 Z = 3929709
41
XDOT = 7190
049654 XDOT = 2240
400962
YDOT = -20150
713759 feet/sec YDOT = -6117
157209 meter/sec
ZDOT = 13268
157913 ZDOT = 4054
898694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18132475
50 X = -5526778
53
Y = 357224
34 feet Y = 108881
98 meter
Z = 12860607
00 Z = 3919913
01
XDOT = 9110
594473 XDOT = 2776
909195
YDOT = -18014
695050 feet/sec YDOT = -5490
879051 meter/sec
ZDOT = 13317
133148 ZDOT = 4059
062183
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 18216
17389155
00016717 00000-0 10270-3 0 9194
2 25544 51
6396 139
5523 0004219 16
1732 343
9555 15
53813140 5972
Satellite: ISS
Catalog Number: 25544
Epoch time: 18216
17389155 = yrday
fracday
Element set: 919
Inclination: 51
6396 deg
RA of node: 139
5523 deg
Eccentricity:
0004219
Arg of perigee: 16
1732 deg
Mean anomaly: 343
9555 deg
Mean motion: 15
53813140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 597
Checksum: 320
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