[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 16th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15478 5032 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
137/14:37:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
4
138/21:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
4
140/09:04:46
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
4
142/00:19:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
5
144/09:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
6
146/20:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
148/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
8
Coasting Arc #1 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2018/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6754335
36 A = 6789498
94 meter
Y = 39260
89 meter E =
0016425
Z = 619984
16 I = 51
68211
XDOT = 530
876263 Wp = 60
12587
YDOT = -4778
523106 meter/sec RA = 175
50724 deg
ZDOT = 5975
575213 TA = 306
56434
MA = 306
71541
Ha = 222
623 n
mi
Hp = 213
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22159892
91 X = -6757284
00
Y = 128808
69 feet Y = -36287
28 meter
Z = 2034068
76 Z = 587166
11
XDOT = 1741
720024 XDOT = 555
244782
YDOT = -15677
569245 feet/sec YDOT = -4772
450781 meter/sec
ZDOT = 19604
905555 ZDOT = 5978
212825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13154403
58 X = -4009462
21
Y = 17849763
33 feet Y = 5440607
86 meter
Z = 1887457
77 Z = 575297
13
XDOT = -10299
597319 XDOT = -3139
317263
YDOT = -9705
999921 feet/sec YDOT = -2958
388776 meter/sec
ZDOT = 19617
250105 ZDOT = 5979
337832
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 18136
56320018
00016717 00000-0 10270-3 0 9001
2 25544 51
6384 176
3617 0003998 88
6223 271
5387 15
54023084 33593
Satellite: ISS
Catalog Number: 25544
Epoch time: 18136
56320018 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 176
3617 deg
Eccentricity:
0003998
Arg of perigee: 88
6223 deg
Mean anomaly: 271
5387 deg
Mean motion: 15
54023084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 318
Coasting Arc #2 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2018/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6347951
17 A = 6787358
34 meter
Y = 763915
92 meter E =
0009370
Z = -2276024
17 I = 51
70860
XDOT = -2517
709081 Wp = 120
48951
YDOT = 4774
400427 meter/sec RA = 170
53934 deg
ZDOT = -5440
884706 TA = 84
80576
MA = 84
69884
Ha = 222
576 n
mi
Hp = 213
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20826611
47 X = 6349992
96
Y = 2506285
84 feet Y = 834914
75 meter
Z = -7467270
91 Z = -2245182
49
XDOT = -8260
200398 XDOT = -2544
481245
YDOT = 15664
043395 feet/sec YDOT = 4746
096580 meter/sec
ZDOT = -17850
671607 ZDOT = -5453
179557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14226313
24 X = 4336180
28
Y = -15481566
52 feet Y = -4718781
48 meter
Z = -7329560
57 Z = -2234050
06
XDOT = 6829
340825 XDOT = 2081
583083
YDOT = 14719
331873 feet/sec YDOT = 4486
452355 meter/sec
ZDOT = -17906
170386 ZDOT = -5457
800734
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 18137
52776996
00016717 00000-0 10270-3 0 9019
2 25544 51
6388 171
5536 0003983 94
2653 265
8955 15
54077042 33745
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
52776996 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 171
5536 deg
Eccentricity:
0003983
Arg of perigee: 94
2653 deg
Mean anomaly: 265
8955 deg
Mean motion: 15
54077042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 348
Coasting Arc #3 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2018/137/14:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 146473
03 A = 6777713
30 meter
Y = -4254702
70 meter E =
0006724
Z = 5268257
07 I = 51
67636
XDOT = 7599
958445 Wp = 80
05190
YDOT = -713
670683 meter/sec RA = 169
96890 deg
ZDOT = -785
680509 TA = 17
45857
MA = 17
43547
Ha = 222
514 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 480554
55 X = 168448
59
Y = -13958998
37 feet Y = -4252942
46 meter
Z = 17284307
99 Z = 5269021
50
XDOT = 24934
246866 XDOT = 7611
190539
YDOT = -2341
439249 feet/sec YDOT = -628
619826 meter/sec
ZDOT = -2577
691960 ZDOT = -748
734777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13951710
56 X = -4252481
38
Y = 546647
01 feet Y = 166618
01 meter
Z = 17288227
79 Z = 5269451
83
XDOT = -3927
222767 XDOT = -1197
017499
YDOT = -23727
027287 feet/sec YDOT = -7231
997917 meter/sec
ZDOT = -2412
530461 ZDOT = -735
339285
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 18137
65637892
00016717 00000-0 10270-3 0 9025
2 25544 51
6352 170
9128 0003860 93
5508 266
6086 15
54063280 33766
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
65637892 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 170
9128 deg
Eccentricity:
0003860
Arg of perigee: 93
5508 deg
Mean anomaly: 266
6086 deg
Mean motion: 15
54063280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 325
Coasting Arc #4 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2018/138/14:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1871517
17 A = 6779788
69 meter
Y = 4424094
34 meter E =
0015286
Z = -4798830
63 I = 51
71575
XDOT = -7192
203500 Wp = 105
64595
YDOT = -207
799746 meter/sec RA = 164
97641 deg
ZDOT = 2616
267782 TA = 190
14591
MA = 190
17680
Ha = 222
551 n
mi
Hp = 213
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6140148
18 X = -1897539
09
Y = 14514745
20 feet Y = 4403020
82 meter
Z = -15744194
99 Z = -4807984
58
XDOT = -23596
468175 XDOT = -7202
053860
YDOT = -681
757698 feet/sec YDOT = -288
283303 meter/sec
ZDOT = 8583
555715 ZDOT = 2581
306251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14961971
44 X = 4560408
90
Y = 4817905
89 feet Y = 1468497
71 meter
Z = -15785630
09 Z = -4811460
05
XDOT = 1623
963256 XDOT = 494
984000
YDOT = 22537
240596 feet/sec YDOT = 6869
350934 meter/sec
ZDOT = 8427
341720 ZDOT = 2568
653756
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 18138
62094793
00016717 00000-0 10270-3 0 9031
2 25544 51
6355 166
1050 0003906 96
3630 263
7967 15
54044157 33913
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
62094793 = yrday
fracday
Element set: 903
Inclination: 51
6355 deg
RA of node: 166
1050 deg
Eccentricity:
0003906
Arg of perigee: 96
3630 deg
Mean anomaly: 263
7967 deg
Mean motion: 15
54044157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 318
Coasting Arc #5 (Orbit 3394)
---------------------------------------
Vector Time (GMT): 2018/138/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5870065
44 A = 6788331
47 meter
Y = 3017372
99 meter E =
0010330
Z = -1578529
67 I = 51
75728
XDOT = -3446
790631 Wp = 56
04977
YDOT = -3713
473591 meter/sec RA = 163
66047 deg
ZDOT = 5751
806668 TA = 286
72295
MA = 286
83629
Ha = 222
374 n
mi
Hp = 213
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19258744
88 X = -5895702
52
Y = 9899517
68 feet Y = 2951586
72 meter
Z = -5178903
11 Z = -1607106
57
XDOT = -11308
368212 XDOT = -3432
948860
YDOT = -12183
312305 feet/sec YDOT = -3751
941263 meter/sec
ZDOT = 18870
756784 ZDOT = 5735
096389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17070618
13 X = 5203124
40
Y = -13272179
51 feet Y = -4045360
32 meter
Z = -5306975
57 Z = -1617566
15
XDOT = 12514
188883 XDOT = 3814
324772
YDOT = 8621
494663 feet/sec YDOT = 2627
831573 meter/sec
ZDOT = 18796
520088 ZDOT = 5729
179323
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 18138
87816585
00016717 00000-0 10270-3 0 9040
2 25544 51
6396 164
8239 0003685 96
6163 263
5409 15
54088133 33955
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
87816585 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 164
8239 deg
Eccentricity:
0003685
Arg of perigee: 96
6163 deg
Mean anomaly: 263
5409 deg
Mean motion: 15
54088133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3395
Checksum: 349
Coasting Arc #6 (Orbit 3410)
---------------------------------------
Vector Time (GMT): 2018/139/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6355725
62 A = 6789577
67 meter
Y = -2366962
82 meter E =
0015212
Z = -131459
40 I = 51
79276
XDOT = 1555
093059 Wp = 127
81078
YDOT = 4483
417124 meter/sec RA = 158
69976 deg
ZDOT = -6024
502979 TA = 53
60244
MA = 53
46222
Ha = 222
518 n
mi
Hp = 213
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20852118
19 X = 6382359
84
Y = -7765626
06 feet Y = -2295739
79 meter
Z = -431297
25 Z = -100520
93
XDOT = 5102
011349 XDOT = 1534
106659
YDOT = 14709
373765 feet/sec YDOT = 4500
690562 meter/sec
ZDOT = -19765
429722 ZDOT = -6016
999327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18866076
20 X = -5750380
03
Y = 11802003
20 feet Y = 3597250
58 meter
Z = -292724
32 Z = -89222
37
XDOT = -7223
692752 XDOT = -2201
781551
YDOT = -11978
803407 feet/sec YDOT = -3651
139278 meter/sec
ZDOT = -19732
426185 ZDOT = -6014
443501
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 18139
90703452
00016717 00000-0 10270-3 0 9054
2 25544 51
6402 159
6954 0003761 101
7764 258
3810 15
54042039 34111
Satellite: ISS
Catalog Number: 25544
Epoch time: 18139
90703452 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 159
6954 deg
Eccentricity:
0003761
Arg of perigee: 101
7764 deg
Mean anomaly: 258
3810 deg
Mean motion: 15
54042039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3411
Checksum: 299
Coasting Arc #7 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1530636
70 A = 6780133
50 meter
Y = -4681113
91 meter E =
0011140
Z = 4651733
84 I = 51
77631
XDOT = 7068
716332 Wp = 76
87975
YDOT = -603
601745 meter/sec RA = 156
17073 deg
ZDOT = -2924
996700 TA = 42
18821
MA = 42
10253
Ha = 222
299 n
mi
Hp = 213
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5021773
94 X = 1560272
71
Y = -15357985
28 feet Y = -4663832
04 meter
Z = 15261593
97 Z = 4659240
67
XDOT = 23191
326548 XDOT = 7089
148735
YDOT = -1980
320686 feet/sec YDOT = -524
439952 meter/sec
ZDOT = -9596
445865 ZDOT = -2890
609674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1257998
12 X = 383437
83
Y = -16076716
54 feet Y = -4900183
20 meter
Z = 15295711
88 Z = 4662132
98
XDOT = 21003
464872 XDOT = 6401
856093
YDOT = -7366
437124 feet/sec YDOT = -2245
290035 meter/sec
ZDOT = -9442
657327 ZDOT = -2878
121953
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 18140
42146430
00016717 00000-0 10270-3 0 9061
2 25544 51
6390 157
1285 0003635 104
9329 255
2226 15
54114473 34196
Satellite: ISS
Catalog Number: 25544
Epoch time: 18140
42146430 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 157
1285 deg
Eccentricity:
0003635
Arg of perigee: 104
9329 deg
Mean anomaly: 255
2226 deg
Mean motion: 15
54114473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 291
Coasting Arc #8 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3001272
95 A = 6783772
52 meter
Y = 4897951
83 meter E =
0009388
Z = -3618513
98 I = 51
81731
XDOT = -6226
021489 Wp = 103
31269
YDOT = -549
839051 meter/sec RA = 151
19410 deg
ZDOT = 4427
293083 TA = 213
99431
MA = 214
05449
Ha = 222
419 n
mi
Hp = 213
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9846696
03 X = -3038243
28
Y = 16069395
76 feet Y = 4864183
11 meter
Z = -11871765
02 Z = -3633182
54
XDOT = -20426
579689 XDOT = -6240
915783
YDOT = -1803
933893 feet/sec YDOT = -619
546347 meter/sec
ZDOT = 14525
239775 ZDOT = 4397
012978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5503254
90 X = -1677392
09
Y = 17981146
38 feet Y = 5480653
42 meter
Z = -11937933
99 Z = -3638682
28
XDOT = -19021
706537 XDOT = -5797
816153
YDOT = 3715
596493 feet/sec YDOT = 1132
513811 meter/sec
ZDOT = 14389
929146 ZDOT = 4386
050404
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 18141
38602568
00016717 00000-0 10270-3 0 9077
2 25544 51
6381 152
3212 0003949 108
5350 251
6232 15
54110973 34340
Satellite: ISS
Catalog Number: 25544
Epoch time: 18141
38602568 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 152
3212 deg
Eccentricity:
0003949
Arg of perigee: 108
5350 deg
Mean anomaly: 251
6232 deg
Mean motion: 15
54110973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 291
Coasting Arc #9 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2018/142/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2044966
31 A = 6777481
27 meter
Y = 3669717
89 meter E =
0018518
Z = -5334368
85 I = 51
81164
XDOT = -6568
541256 Wp = 95
27836
YDOT = 3926
407165 meter/sec RA = 148
05931 deg
ZDOT = 181
916282 TA = 176
46087
MA = 176
44775
Ha = 222
409 n
mi
Hp = 213
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6709207
04 X = 2029690
11
Y = 12039756
87 feet Y = 3692501
06 meter
Z = -17501210
12 Z = -5324471
95
XDOT = -21550
332204 XDOT = -6612
842882
YDOT = 12881
913271 feet/sec YDOT = 3852
705495 meter/sec
ZDOT = 596
838197 ZDOT = 149
901209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13819257
72 X = -4212109
75
Y = 727191
12 feet Y = 221647
85 meter
Z = -17457401
57 Z = -5321016
00
XDOT = -1841
706948 XDOT = -561
352278
YDOT = -24030
680240 feet/sec YDOT = -7324
551337 meter/sec
ZDOT = 453
220539 ZDOT = 138
141620
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 18142
02906365
00016717 00000-0 10270-3 0 9082
2 25544 51
6357 149
1135 0003818 109
8296 250
3269 15
54089779 34445
Satellite: ISS
Catalog Number: 25544
Epoch time: 18142
02906365 = yrday
fracday
Element set: 908
Inclination: 51
6357 deg
RA of node: 149
1135 deg
Eccentricity:
0003818
Arg of perigee: 109
8296 deg
Mean anomaly: 250
3269 deg
Mean motion: 15
54089779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3444
Checksum: 331
Coasting Arc #10 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2018/143/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -491426
57 A = 6778900
29 meter
Y = -4544230
66 meter E =
0008659
Z = 4999436
43 I = 51
84414
XDOT = 6740
252745 Wp = 78
33599
YDOT = -3021
872137 meter/sec RA = 143
07356 deg
ZDOT = -2079
436859 TA = 31
84828
MA = 31
79595
Ha = 222
453 n
mi
Hp = 213
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1612291
90 X = -464859
92
Y = -14908893
23 feet Y = -4549577
84 meter
Z = 16402350
49 Z = 4997113
53
XDOT = 22113
690107 XDOT = 6783
644038
YDOT = -9914
278666 feet/sec YDOT = -2946
255266 meter/sec
ZDOT = -6822
299405 ZDOT = -2046
589701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14191746
75 X = 4325644
41
Y = 4877652
70 feet Y = 1486708
54 meter
Z = 16392513
91 Z = 4996438
24
XDOT = -256
854645 XDOT = -78
289296
YDOT = 23232
804864 feet/sec YDOT = 7081
358923 meter/sec
ZDOT = -6675
052103 ZDOT = -2034
555881
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 18143
05792176
00016717 00000-0 10270-3 0 9090
2 25544 51
6361 143
9843 0003780 113
4318 246
7233 15
54065601 34608
Satellite: ISS
Catalog Number: 25544
Epoch time: 18143
05792176 = yrday
fracday
Element set: 909
Inclination: 51
6361 deg
RA of node: 143
9843 deg
Eccentricity:
0003780
Arg of perigee: 113
4318 deg
Mean anomaly: 246
7233 deg
Mean motion: 15
54065601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3460
Checksum: 302
Coasting Arc #11 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2018/144/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -956631
44 A = 6782004
06 meter
Y = 5264694
55 meter E =
0011788
Z = -4179440
23 I = 51
88042
XDOT = -6425
088269 Wp = 112
52514
YDOT = 1808
837006 meter/sec RA = 138
09598 deg
ZDOT = 3753
210734 TA = 195
99120
MA = 196
02845
Ha = 222
414 n
mi
Hp = 213
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3138554
60 X = -995129
95
Y = 17272619
93 feet Y = 5253781
77 meter
Z = -13712074
24 Z = -4184180
52
XDOT = -21079
685922 XDOT = -6463
068895
YDOT = 5934
504612 feet/sec YDOT = 1736
774717 meter/sec
ZDOT = 12313
683509 ZDOT = 3721
907499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14440983
69 X = -4401611
83
Y = -9952508
32 feet Y = -3033524
54 meter
Z = -13733916
87 Z = -4186097
86
XDOT = 2673
614132 XDOT = 814
917587
YDOT = -20659
828351 feet/sec YDOT = -6297
115682 meter/sec
ZDOT = 12173
471824 ZDOT = 3710
474212
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 18144
02247281
00016717 00000-0 10270-3 0 9102
2 25544 51
6359 139
1756 0003987 117
0849 243
0711 15
54097960 34753
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
02247281 = yrday
fracday
Element set: 910
Inclination: 51
6359 deg
RA of node: 139
1756 deg
Eccentricity:
0003987
Arg of perigee: 117
0849 deg
Mean anomaly: 243
0711 deg
Mean motion: 15
54097960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 319
Coasting Arc #12 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2018/144/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4275458
87 A = 6778664
00 meter
Y = 1424087
72 meter E =
0016131
Z = -5078094
82 I = 51
88137
XDOT = -4245
209254 Wp = 85
29528
YDOT = 6090
944326 meter/sec RA = 136
27297 deg
ZDOT = -1869
910697 TA = 166
64037
MA = 166
59761
Ha = 222
405 n
mi
Hp = 213
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14027096
03 X = 4283883
48
Y = 4672203
81 feet Y = 1471946
17 meter
Z = -16660416
08 Z = -5057305
43
XDOT = -13927
851884 XDOT = -4303
921233
YDOT = 19983
413143 feet/sec YDOT = 6043
143273 meter/sec
ZDOT = -6134
877615 ZDOT = -1890
674962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14871271
02 X = 4532763
41
Y = -719561
40 feet Y = -219322
31 meter
Z = -16567616
15 Z = -5049809
40
XDOT = -5833
652849 XDOT = -1778
097388
YDOT = 22553
303622 feet/sec YDOT = 6874
246944 meter/sec
ZDOT = -6228
487859 ZDOT = -1898
443099
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 18144
40829230
00016717 00000-0 10270-3 0 9115
2 25544 51
6392 137
2557 0003883 117
0076 243
1474 15
54089317 34816
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
40829230 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 137
2557 deg
Eccentricity:
0003883
Arg of perigee: 117
0076 deg
Mean anomaly: 243
1474 deg
Mean motion: 15
54089317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 305
Coasting Arc #13 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2018/145/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3116200
79 A = 6777397
83 meter
Y = -2785390
60 meter E =
0006178
Z = 5330106
87 I = 51
89927
XDOT = 5083
411203 Wp = 108
27848
YDOT = -5748
059918 meter/sec RA = 131
29134 deg
ZDOT = -33
688412 TA = 342
03026
MA = 342
05209
Ha = 222
502 n
mi
Hp = 213
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10223755
88 X = -3110713
34
Y = -9138420
61 feet Y = -2820207
68 meter
Z = 17487227
26 Z = 5314982
46
XDOT = 16677
858277 XDOT = 5147
473414
YDOT = -18858
464298 feet/sec YDOT = -5690
855516 meter/sec
ZDOT = -110
526285 ZDOT = -8
839351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13012320
26 X = -3966155
22
Y = -4589623
02 feet Y = -1398917
10 meter
Z = 17419928
67 Z = 5309594
26
XDOT = 8048
288044 XDOT = 2453
118196
YDOT = -22789
927845 feet/sec YDOT = -6946
370007 meter/sec
ZDOT = 1
329113 ZDOT =
405114
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 18145
43714245
00016717 00000-0 10270-3 0 9129
2 25544 51
6379 132
1269 0003958 118
8921 241
2629 15
54109746 34973
Satellite: ISS
Catalog Number: 25544
Epoch time: 18145
43714245 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 132
1269 deg
Eccentricity:
0003958
Arg of perigee: 118
8921 deg
Mean anomaly: 241
2629 deg
Mean motion: 15
54109746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 326
Coasting Arc #14 (Orbit 3511)
---------------------------------------
Vector Time (GMT): 2018/146/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1899316
22 A = 6778669
09 meter
Y = 4109598
73 meter E =
0016575
Z = -5060296
85 I = 51
92600
XDOT = -5517
096378 Wp = 108
49161
YDOT = 4939
792644 meter/sec RA = 126
31110 deg
ZDOT = 1941
052525 TA = 180
29680
MA = 180
29779
Ha = 222
301 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6231352
44 X = 1877801
02
Y = 13482935
47 feet Y = 4130718
21 meter
Z = -16602023
79 Z = -5051122
50
XDOT = -18100
709900 XDOT = -5581
353194
YDOT = 16206
668778 feet/sec YDOT = 4877
737269 meter/sec
ZDOT = 6368
282562 ZDOT = 1914
096228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11108994
93 X = 3386021
65
Y = 9927396
23 feet Y = 3025870
37 meter
Z = -16561507
54 Z = -5047947
50
XDOT = -9634
057080 XDOT = -2936
460598
YDOT = 21202
033296 feet/sec YDOT = 6462
379749 meter/sec
ZDOT = 6247
082635 ZDOT = 1904
110787
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 18146
40168526
00016717 00000-0 10270-3 0 9133
2 25544 51
6396 127
3187 0003733 122
2717 237
8798 15
54091349 35125
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
40168526 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 127
3187 deg
Eccentricity:
0003733
Arg of perigee: 122
2717 deg
Mean anomaly: 237
8798 deg
Mean motion: 15
54091349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3512
Checksum: 322
Coasting Arc #15 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2018/146/20:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1058099
36 A = 6780380
19 meter
Y = -4869115
73 meter E =
0010742
Z = 4590065
22 I = 51
93994
XDOT = 5682
437391 Wp = 81
83543
YDOT = -4140
390285 meter/sec RA = 123
89909 deg
ZDOT = -3074
574833 TA = 38
79140
MA = 38
71433
Ha = 222
160 n
mi
Hp = 213
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3471454
58 X = -1025869
39
Y = -15974789
14 feet Y = -4880768
24 meter
Z = 15059269
09 Z = 4585003
20
XDOT = 18643
167292 XDOT = 5743
248929
YDOT = -13583
957628 feet/sec YDOT = -4076
505120 meter/sec
ZDOT = -10087
187772 ZDOT = -3046
823684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8302183
08 X = 2530505
40
Y = 14106076
77 feet Y = 4299532
20 meter
Z = 15037247
91 Z = 4583353
16
XDOT = -12607
235197 XDOT = -3842
685288
YDOT = 18066
879741 feet/sec YDOT = 5506
784945 meter/sec
ZDOT = -9962
523967 ZDOT = -3036
577305
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 18146
91610550
00016717 00000-0 10270-3 0 9149
2 25544 51
6380 124
7535 0003402 123
8796 236
2681 15
54136171 35209
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
91610550 = yrday
fracday
Element set: 914
Inclination: 51
6380 deg
RA of node: 124
7535 deg
Eccentricity:
0003402
Arg of perigee: 123
8796 deg
Mean anomaly: 236
2681 deg
Mean motion: 15
54136171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 292
Coasting Arc #16 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2018/147/20:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -76432
00 A = 6784135
55 meter
Y = 5811397
76 meter E =
0008267
Z = -3508834
24 I = 51
96824
XDOT = -5548
125633 Wp = 108
53846
YDOT = 2673
211627 meter/sec RA = 118
93246 deg
ZDOT = 4554
491413 TA = 210
45326
MA = 210
50130
Ha = 222
142 n
mi
Hp = 213
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -250761
15 X = -124366
62
Y = 19066265
62 feet Y = 5810275
35 meter
Z = -11511923
36 Z = -3509321
42
XDOT = -18202
511920 XDOT = -5599
729542
YDOT = 8770
379355 feet/sec YDOT = 2610
879716 meter/sec
ZDOT = 14942
557129 ZDOT = 4527
415007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5998738
93 X = -1828415
63
Y = -18097869
58 feet Y = -5516230
65 meter
Z = -11514859
68 Z = -3509729
23
XDOT = 13162
500821 XDOT = 4011
930250
YDOT = -13779
874748 feet/sec YDOT = -4200
105823 meter/sec
ZDOT = 14821
081795 ZDOT = 4517
465731
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 18147
88064513
00016717 00000-0 10270-3 0 9159
2 25544 51
6363 119
9447 0003559 128
9234 231
2236 15
54120141 35351
Satellite: ISS
Catalog Number: 25544
Epoch time: 18147
88064513 = yrday
fracday
Element set: 915
Inclination: 51
6363 deg
RA of node: 119
9447 deg
Eccentricity:
0003559
Arg of perigee: 128
9234 deg
Mean anomaly: 231
2236 deg
Mean motion: 15
54120141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 304
Coasting Arc #17 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2018/148/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3817913
84 A = 6777474
23 meter
Y = 1719994
56 meter E =
0017696
Z = -5344167
48 I = 51
95340
XDOT = -3355
207647 Wp = 96
99737
YDOT = 6878
609903 meter/sec RA = 117
09033 deg
ZDOT = -185
760442 TA = 171
25239
MA = 171
22151
Ha = 222
202 n
mi
Hp = 213
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12525964
06 X = 3824356
20
Y = 5643026
78 feet Y = 1762725
65 meter
Z = -17533357
86 Z = -5325605
26
XDOT = -11007
899105 XDOT = -3430
974438
YDOT = 22567
617791 feet/sec YDOT = 6840
666040 meter/sec
ZDOT = -609
450268 ZDOT = -202
242489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9047323
46 X = 2757624
19
Y = 10477913
96 feet Y = 3193668
18 meter
Z = -17450542
17 Z = -5318925
25
XDOT = -18784
819344 XDOT = -5725
612936
YDOT = 15095
128610 feet/sec YDOT = 4600
995200 meter/sec
ZDOT = -684
088233 ZDOT = -208
510093
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 18148
26646072
00016717 00000-0 10270-3 0 9169
2 25544 51
6382 118
0219 0003704 132
6271 227
5194 15
54094285 35411
Satellite: ISS
Catalog Number: 25544
Epoch time: 18148
26646072 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 118
0219 deg
Eccentricity:
0003704
Arg of perigee: 132
6271 deg
Mean anomaly: 227
5194 deg
Mean motion: 15
54094285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 304
Coasting Arc #18 (Orbit 3556)
---------------------------------------
Vector Time (GMT): 2018/149/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2966938
07 A = 6778253
00 meter
Y = -3313258
29 meter E =
0006808
Z = 5109347
92 I = 51
97166
XDOT = 4027
624212 Wp = 87
03200
YDOT = -6295
095237 meter/sec RA = 112
11323 deg
ZDOT = -1741
050088 TA = 19
72203
MA = 19
69572
Ha = 222
175 n
mi
Hp = 213
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9734048
78 X = -2954486
69
Y = -10870269
98 feet Y = -3346367
62 meter
Z = 16762952
48 Z = 5094965
19
XDOT = 13213
990197 XDOT = 4106
175577
YDOT = -20653
199598 feet/sec YDOT = -6249
616156 meter/sec
ZDOT = -5712
106587 ZDOT = -1721
294945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4535117
64 X = -1382303
86
Y = -13945809
75 feet Y = -4250682
81 meter
Z = 16699046
36 Z = 5089869
33
XDOT = 19525
905577 XDOT = 5951
496020
YDOT = -13091
920707 feet/sec YDOT = -3990
417432 meter/sec
ZDOT = -5622
877822 ZDOT = -1713
853160
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 18149
29529516
00016717 00000-0 10270-3 0 9177
2 25544 51
6391 112
8932 0003629 135
9685 224
1757 15
54150280 35579
Satellite: ISS
Catalog Number: 25544
Epoch time: 18149
29529516 = yrday
fracday
Element set: 917
Inclination: 51
6391 deg
RA of node: 112
8932 deg
Eccentricity:
0003629
Arg of perigee: 135
9685 deg
Mean anomaly: 224
1757 deg
Mean motion: 15
54150280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 330
Coasting Arc #19 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2018/150/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2107982
78 A = 6781270
01 meter
Y = 4750090
39 meter E =
0012224
Z = -4369234
78 I = 51
99352
XDOT = -4443
642815 Wp = 117
78301
YDOT = 5173
425668 meter/sec RA = 107
14244 deg
ZDOT = 3482
389493 TA = 187
45895
MA = 187
47715
Ha = 222
113 n
mi
Hp = 213
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6915954
00 X = 2075933
00
Y = 15584286
07 feet Y = 4773484
69 meter
Z = -14334759
77 Z = -4359072
01
XDOT = -14578
880627 XDOT = -4518
079040
YDOT = 16973
181327 feet/sec YDOT = 5123
317131 meter/sec
ZDOT = 11425
162380 ZDOT = 3460
623436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 314006
22 X = 95709
10
Y = 17084639
52 feet Y = 5207398
12 meter
Z = -14289934
30 Z = -4355571
97
XDOT = -18904
900709 XDOT = -5762
213736
YDOT = 9816
440679 feet/sec YDOT = 2992
051119 meter/sec
ZDOT = 11327
064422 ZDOT = 3452
489236
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 18150
25982614
00016717 00000-0 10270-3 0 9188
2 25544 51
6395 108
0850 0003724 134
6092 225
5365 15
54140353 35720
Satellite: ISS
Catalog Number: 25544
Epoch time: 18150
25982614 = yrday
fracday
Element set: 918
Inclination: 51
6395 deg
RA of node: 108
0850 deg
Eccentricity:
0003724
Arg of perigee: 134
6092 deg
Mean anomaly: 225
5365 deg
Mean motion: 15
54140353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 302
Coasting Arc #20 (Orbit 3587)
---------------------------------------
Vector Time (GMT): 2018/151/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1244430
59 A = 6785055
59 meter
Y = -5872587
77 meter E =
0015704
Z = 3144815
98 I = 52
01481
XDOT = 4683
654545 Wp = 104
19434
YDOT = -3617
486911 meter/sec RA = 102
18264 deg
ZDOT = -4885
304277 TA = 39
73574
MA = 39
62081
Ha = 222
040 n
mi
Hp = 213
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4082777
53 X = -1193945
22
Y = -19267020
23 feet Y = -5886222
01 meter
Z = 10317637
73 Z = 3138892
69
XDOT = 15366
320686 XDOT = 4747
488632
YDOT = -11868
395376 feet/sec YDOT = -3564
753447 meter/sec
ZDOT = -16027
901170 ZDOT = -4862
397954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3430820
61 X = 1045714
12
Y = -19407372
12 feet Y = -5915367
02 meter
Z = 10291946
67 Z = 3136985
35
XDOT = 17393
316042 XDOT = 5301
482730
YDOT = -5399
293223 feet/sec YDOT = -1645
704574 meter/sec
ZDOT = -15924
895263 ZDOT = -4853
908076
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 18151
28865430
00016717 00000-0 10270-3 0 9199
2 25544 51
6392 102
9567 0003634 139
9033 220
2389 15
54162425 35887
Satellite: ISS
Catalog Number: 25544
Epoch time: 18151
28865430 = yrday
fracday
Element set: 919
Inclination: 51
6392 deg
RA of node: 102
9567 deg
Eccentricity:
0003634
Arg of perigee: 139
9033 deg
Mean anomaly: 220
2389 deg
Mean motion: 15
54162425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 320
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