[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 17th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14678 7446 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
197/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
7
199/15:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 215
4
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
527 -1
2 1
2 1
2
N/A 0
2 0
0 221
8
000/00:03:15
055 -0
3 0
0 215
4
209/20:18:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 306)
---------------------------------------
Vector Time (GMT): 2018/197/12:04:09
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1204940
49 A = 6780036
80 meter
Y = 4652114
57 meter E =
0010563
Z = -4792670
82 I = 51
32489
XDOT = -5906
073652 Wp = 52
22682
YDOT = -4158
200628 meter/sec RA = 231
55486 deg
ZDOT = -2548
898675 TA = 192
53037
MA = 192
55665
Ha = 220
779 n
mi
Hp = 215
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3953216
84 X = -1233592
39
Y = 15262843
09 feet Y = 4638480
24 meter
Z = -15723985
62 Z = -4798593
13
XDOT = -19376
882062 XDOT = -5846
755618
YDOT = -13642
390513 feet/sec YDOT = -4223
914570 meter/sec
ZDOT = -8362
528460 ZDOT = -2577
443957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15486453
74 X = 4720271
10
Y = -2810669
65 feet Y = -856692
11 meter
Z = -15751060
70 Z = -4800923
30
XDOT = -4631
234758 XDOT = -1411
600354
YDOT = 22105
199968 feet/sec YDOT = 6737
664950 meter/sec
ZDOT = -8489
805728 ZDOT = -2587
692786
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 18197
52353526
00016717 00000-0 10270-3 0 9004
2 25544 51
6384 232
4951 0003857 319
7085 40
3781 15
53970528 3079
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
52353526 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 232
4951 deg
Eccentricity:
0003857
Arg of perigee: 319
7085 deg
Mean anomaly: 40
3781 deg
Mean motion: 15
53970528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 307
Checksum: 317
Coasting Arc #2 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -784413
53 A = 6784191
94 meter
Y = -5660604
90 meter E =
0009836
Z = 3645853
86 I = 51
33795
XDOT = 6011
744638 Wp = 77
30711
YDOT = 1967
452390 meter/sec RA = 231
41847 deg
ZDOT = 4340
342718 TA = 326
22794
MA = 326
29056
Ha = 220
873 n
mi
Hp = 215
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2573535
21 X = -738766
05
Y = -18571538
38 feet Y = -5669121
78 meter
Z = 11961462
80 Z = 3642153
99
XDOT = 19723
571648 XDOT = 5968
214593
YDOT = 6454
896293 feet/sec YDOT = 2034
436167 meter/sec
ZDOT = 14239
969546 ZDOT = 4369
439491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13761625
00 X = -4194543
30
Y = 12748425
56 feet Y = 3885720
11 meter
Z = 11945586
49 Z = 3641014
76
XDOT = -4930
401113 XDOT = -1502
786259
YDOT = -18811
262831 feet/sec YDOT = -5733
672911 meter/sec
ZDOT = 14369
981612 ZDOT = 4379
970395
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 18197
58784401
00016717 00000-0 10270-3 0 9011
2 25544 51
6371 232
1744 0003827 323
7595 36
3298 15
53960835 3089
Satellite: ISS
Catalog Number: 25544
Epoch time: 18197
58784401 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 232
1744 deg
Eccentricity:
0003827
Arg of perigee: 323
7595 deg
Mean anomaly: 36
3298 deg
Mean motion: 15
53960835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 308
Checksum: 324
Coasting Arc #3 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -479417
30 A = 6780526
88 meter
Y = 4907014
66 meter E =
0010187
Z = -4664590
77 I = 51
34864
XDOT = -6293
100709 Wp = 49
14735
YDOT = -3316
785005 meter/sec RA = 226
41083 deg
ZDOT = -2839
910411 TA = 192
49658
MA = 192
52185
Ha = 220
877 n
mi
Hp = 215
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1572891
41 X = -511595
54
Y = 16099129
47 feet Y = 4901473
83 meter
Z = -15303775
50 Z = -4666997
45
XDOT = -20646
655869 XDOT = -6241
749250
YDOT = -10881
840566 feet/sec YDOT = -3386
871518 meter/sec
ZDOT = -9317
291376 ZDOT = -2870
355041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13936153
54 X = 4247739
60
Y = -8190960
44 feet Y = -2496604
74 meter
Z = -15315132
82 Z = -4668052
48
XDOT = 2563
749579 XDOT = 781
430872
YDOT = 22052
260150 feet/sec YDOT = 6721
528894 meter/sec
ZDOT = -9453
192959 ZDOT = -2881
333214
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 18198
55246606
00016717 00000-0 10270-3 0 9020
2 25544 51
6383 227
3673 0003905 324
3018 35
7873 15
53984976 3234
Satellite: ISS
Catalog Number: 25544
Epoch time: 18198
55246606 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 227
3673 deg
Eccentricity:
0003905
Arg of perigee: 324
3018 deg
Mean anomaly: 35
7873 deg
Mean motion: 15
53984976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 328
Coasting Arc #4 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2018/199/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1850221
68 A = 6778150
64 meter
Y = -3920064
30 meter E =
0001813
Z = 5209590
17 I = 51
36376
XDOT = 6224
837074 Wp = 42
59025
YDOT = 4352
082540 meter/sec RA = 221
39514 deg
ZDOT = 1065
114023 TA = 37
17517
MA = 37
16262
Ha = 220
932 n
mi
Hp = 215
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6070281
10 X = 1868614
31
Y = -12861103
36 feet Y = -3899271
28 meter
Z = 17091831
27 Z = 5218622
25
XDOT = 20422
693812 XDOT = 6170
534558
YDOT = 14278
486023 feet/sec YDOT = 4421
389287 meter/sec
ZDOT = 3494
468578 ZDOT = 1095
220045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13872954
83 X = -4228476
63
Y = 2897885
10 feet Y = 883275
38 meter
Z = 17132728
17 Z = 5222055
55
XDOT = -510
776474 XDOT = -155
684669
YDOT = -23877
796486 feet/sec YDOT = -7277
952369 meter/sec
ZDOT = 3628
751119 ZDOT = 1106
043341
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 18199
58139359
00016717 00000-0 10270-3 0 9031
2 25544 51
6377 222
2382 0003971 330
2892 29
8034 15
53991358 3399
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
58139359 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 222
2382 deg
Eccentricity:
0003971
Arg of perigee: 330
2892 deg
Mean anomaly: 29
8034 deg
Mean motion: 15
53991358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 334
Coasting Arc #5 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2018/199/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5109328
16 A = 6781262
53 meter
Y = 288549
26 meter E =
0006848
Z = -4455190
32 I = 51
37524
XDOT = -3174
788088 Wp = 87
97063
YDOT = -6172
494338 meter/sec RA = 220
84229 deg
ZDOT = 3245
723729 TA = 214
83978
MA = 214
88463
Ha = 221
011 n
mi
Hp = 215
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16762887
67 X = -5090534
39
Y = 946683
91 feet Y = 231518
54 meter
Z = -14616766
14 Z = -4479963
67
XDOT = -10415
971417 XDOT = -3121
295403
YDOT = -20250
965677 feet/sec YDOT = -6207
698085 meter/sec
ZDOT = 10648
699897 ZDOT = 3230
431515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16296849
56 X = 4967279
75
Y = 3612135
44 feet Y = 1100978
88 meter
Z = -14727716
65 Z = -4489008
03
XDOT = 4861
474815 XDOT = 1481
777524
YDOT = 21147
461284 feet/sec YDOT = 6445
746199 meter/sec
ZDOT = 10580
953077 ZDOT = 3225
074498
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 18199
64570239
00016717 00000-0 10270-3 0 9045
2 25544 51
6363 221
9182 0004155 330
3012 29
7904 15
53966931 3404
Satellite: ISS
Catalog Number: 25544
Epoch time: 18199
64570239 = yrday
fracday
Element set: 904
Inclination: 51
6363 deg
RA of node: 221
9182 deg
Eccentricity:
0004155
Arg of perigee: 330
3012 deg
Mean anomaly: 29
7904 deg
Mean motion: 15
53966931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 340
Checksum: 303
Coasting Arc #6 (Orbit 355)
---------------------------------------
Vector Time (GMT): 2018/200/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5833507
25 A = 6784905
63 meter
Y = 934800
44 meter E =
0011216
Z = 3330959
83 I = 51
41293
XDOT = 1734
034843 Wp = 71
41703
YDOT = 5838
053994 meter/sec RA = 215
83982 deg
ZDOT = -4658
793376 TA = 69
65711
MA = 69
53665
Ha = 221
085 n
mi
Hp = 215
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19138803
33 X = 5806440
62
Y = 3066930
57 feet Y = 999883
21 meter
Z = 10928345
89 Z = 3359231
01
XDOT = 5689
090693 XDOT = 1691
252971
YDOT = 19153
720453 feet/sec YDOT = 5857
206229 meter/sec
ZDOT = -15284
755171 ZDOT = -4650
473694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17655295
55 X = -5381334
08
Y = -7823677
32 feet Y = -2384656
85 meter
Z = 11054827
55 Z = 3369511
44
XDOT = -1290
650793 XDOT = -393
390362
YDOT = -18708
281239 feet/sec YDOT = -5702
284122 meter/sec
ZDOT = -15248
175405 ZDOT = -4647
643863
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 18200
67462786
00016717 00000-0 10270-3 0 9059
2 25544 51
6359 216
7899 0004253 333
6588 26
4348 15
53995234 3560
Satellite: ISS
Catalog Number: 25544
Epoch time: 18200
67462786 = yrday
fracday
Element set: 905
Inclination: 51
6359 deg
RA of node: 216
7899 deg
Eccentricity:
0004253
Arg of perigee: 333
6588 deg
Mean anomaly: 26
4348 deg
Mean motion: 15
53995234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 356
Checksum: 343
Coasting Arc #7 (Orbit 370)
---------------------------------------
Vector Time (GMT): 2018/201/15:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 944469
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6213341
59 A = 6788131
77 meter
Y = -1946910
78 meter E =
0009618
Z = -1900801
17 I = 51
45130
XDOT = -67
025615 Wp = 17
25459
YDOT = -5238
135722 meter/sec RA = 210
84909 deg
ZDOT = 5600
578545 TA = 321
74870
MA = 321
81689
Ha = 221
152 n
mi
Hp = 215
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20384978
96 X = -6181875
89
Y = -6387502
55 feet Y = -2016216
59 meter
Z = -6236224
32 Z = -1930906
90
XDOT = -219
900313 XDOT = -35
650798
YDOT = -17185
484652 feet/sec YDOT = -5238
710202 meter/sec
ZDOT = 18374
601524 ZDOT = 5600
328807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18237324
95 X = 5558736
65
Y = 11047654
88 feet Y = 3367325
21 meter
Z = -6370820
20 Z = -1941826
00
XDOT = -2953
642638 XDOT = -900
270276
YDOT = 15441
409625 feet/sec YDOT = 4706
541654 meter/sec
ZDOT = 18374
081615 ZDOT = 5600
420076
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
63924358
00016717 00000-0 10270-3 0 9065
2 25544 51
6361 211
9824 0004195 337
3078 22
7888 15
53989432 3716
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
63924358 = yrday
fracday
Element set: 906
Inclination: 51
6361 deg
RA of node: 211
9824 deg
Eccentricity:
0004195
Arg of perigee: 337
3078 deg
Mean anomaly: 22
7888 deg
Mean motion: 15
53989432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 371
Checksum: 325
Coasting Arc #8 (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 = -1691307
74 A = 6777758
22 meter
Y = 3897373
12 meter E =
0013897
Z = -5292513
52 I = 51
42546
XDOT = -6786
251370 Wp = 69
81896
YDOT = -3524
379965 meter/sec RA = 209
97264 deg
ZDOT = -422
883408 TA = 196
10883
MA = 196
15306
Ha = 221
187 n
mi
Hp = 215
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5548909
92 X = -1709055
50
Y = 12786657
22 feet Y = 3878360
89 meter
Z = -17363889
49 Z = -5300772
07
XDOT = -22264
604233 XDOT = -6744
282288
YDOT = -11562
926395 feet/sec YDOT = -3600
033821 meter/sec
ZDOT = -1387
412757 ZDOT = -455
746727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6549500
97 X = -1996287
90
Y = -12251196
89 feet Y = -3734164
81 meter
Z = -17401318
18 Z = -5303921
78
XDOT = 22071
278279 XDOT = 6727
325619
YDOT = -9602
578319 feet/sec YDOT = -2926
865872 meter/sec
ZDOT = -1534
180883 ZDOT = -467
618333
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
83216619
00016717 00000-0 10270-3 0 9072
2 25544 51
6398 211
0222 0004311 336
5121 23
5834 15
54015833 3748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18201
83216619 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 211
0222 deg
Eccentricity:
0004311
Arg of perigee: 336
5121 deg
Mean anomaly: 23
5834 deg
Mean motion: 15
54015833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 274
Coasting Arc #9 (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 = 3232203
42 A = 6778266
72 meter
Y = -3012234
99 meter E =
0007060
Z = 5139993
67 I = 51
45690
XDOT = 6250
031822 Wp = 18
25373
YDOT = 4195
816820 meter/sec RA = 204
96030 deg
ZDOT = -1464
200991 TA = 85
91583
MA = 85
83513
Ha = 221
138 n
mi
Hp = 215
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10604341
93 X = 3240679
64
Y = -9882660
73 feet Y = -2976043
30 meter
Z = 16863496
29 Z = 5155714
81
XDOT = 20505
353746 XDOT = 6209
760793
YDOT = 13765
803216 feet/sec YDOT = 4265
483945 meter/sec
ZDOT = -4803
809024 ZDOT = -1433
938181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1361878
21 X = 415100
48
Y = 14348276
18 feet Y = 4373354
58 meter
Z = 16934249
80 Z = 5161559
34
XDOT = -22425
880006 XDOT = -6835
408226
YDOT = 7666
216078 feet/sec YDOT = 2336
662661 meter/sec
ZDOT = -4668
743229 ZDOT = -1423
032936
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
86108402
00016717 00000-0 10270-3 0 9087
2 25544 51
6400 205
8937 0004406 339
5542 20
5434 15
54044590 3904
Satellite: ISS
Catalog Number: 25544
Epoch time: 18202
86108402 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 205
8937 deg
Eccentricity:
0004406
Arg of perigee: 339
5542 deg
Mean anomaly: 20
5434 deg
Mean motion: 15
54044590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 285
Coasting Arc #10 (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 = 5019647
03 A = 6781998
06 meter
Y = -1733313
86 meter E =
0011068
Z = 4215526
33 I = 51
49745
XDOT = 4730
154516 Wp = 50
73936
YDOT = 4814
994980 meter/sec RA = 200
10963 deg
ZDOT = -3639
363494 TA = 76
65557
MA = 76
53219
Ha = 221
358 n
mi
Hp = 215
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16468658
24 X = 5018179
73
Y = -5686725
27 feet Y = -1677189
31 meter
Z = 13830466
95 Z = 4239906
10
XDOT = 15518
879646 XDOT = 4693
638321
YDOT = 15797
227624 feet/sec YDOT = 4867
687009 meter/sec
ZDOT = -11940
168942 ZDOT = -3616
474461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8406928
80 X = -2562431
90
Y = 15160506
43 feet Y = 4620922
36 meter
Z = 13939869
36 Z = 4248872
18
XDOT = -21052
038769 XDOT = -6416
661417
YDOT = -749
167255 feet/sec YDOT = -228
346179 meter/sec
ZDOT = -11838
182419 ZDOT = -3608
278001
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
82569556
00016717 00000-0 10270-3 0 9096
2 25544 51
6388 201
0863 0004397 345
8124 14
2904 15
54017166 4058
Satellite: ISS
Catalog Number: 25544
Epoch time: 18203
82569556 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 201
0863 deg
Eccentricity:
0004397
Arg of perigee: 345
8124 deg
Mean anomaly: 14
2904 deg
Mean motion: 15
54017166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 405
Checksum: 308
Coasting Arc #11 (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 = -6013191
70 A = 6785680
68 meter
Y = 860336
46 meter E =
0006559
Z = -3020214
18 I = 51
54155
XDOT = -3180
835284 Wp = 30
81069
YDOT = -4924
055246 meter/sec RA = 195
11764 deg
ZDOT = 4940
592890 TA = 294
54018
MA = 294
60854
Ha = 221
394 n
mi
Hp = 214
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19728319
23 X = -6007694
86
Y = 2822626
19 feet Y = 793123
85 meter
Z = -9908839
17 Z = -3049410
43
XDOT = -10435
811298 XDOT = -3149
535274
YDOT = -16155
036896 feet/sec YDOT = -4959
451055 meter/sec
ZDOT = 16209
294259 ZDOT = 4925
217159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12501360
46 X = 3810414
67
Y = -15436274
09 feet Y = -4704976
34 meter
Z = -10039737
10 Z = -3060111
87
XDOT = 17588
165750 XDOT = 5360
872921
YDOT = 3767
676577 feet/sec YDOT = 1148
387821 meter/sec
ZDOT = 16140
961992 ZDOT = 4919
765215
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
79030309
00016717 00000-0 10270-3 0 9104
2 25544 51
6392 196
2783 0004418 347
0281 13
0757 15
54016556 4203
Satellite: ISS
Catalog Number: 25544
Epoch time: 18204
79030309 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 196
2783 deg
Eccentricity:
0004418
Arg of perigee: 347
0281 deg
Mean anomaly: 13
0757 deg
Mean motion: 15
54016556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 420
Checksum: 291
Coasting Arc #12 (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 = 6619117
51 A = 6788735
55 meter
Y = -17712
35 meter E =
0011900
Z = 1491075
47 I = 51
58379
XDOT = 1319
834989 Wp = 101
12601
YDOT = 4879
762878 meter/sec RA = 190
13772 deg
ZDOT = -5764
153432 TA = 62
58520
MA = 62
46419
Ha = 221
612 n
mi
Hp = 214
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21716264
79 X = 6611580
87
Y = -58111
38 feet Y = 56264
89 meter
Z = 4891979
89 Z = 1523210
11
XDOT = 4330
167287 XDOT = 1293
168880
YDOT = 16009
720728 feet/sec YDOT = 4894
373716 meter/sec
ZDOT = -18911
264542 ZDOT = -5757
806450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15606128
56 X = -4756747
99
Y = 15053861
89 feet Y = 4588417
10 meter
Z = 5035970
01 Z = 1534963
66
XDOT = -13200
391086 XDOT = -4023
479203
YDOT = -7328
334270 feet/sec YDOT = -2233
676285 meter/sec
ZDOT = -18883
369341 ZDOT = -5755
650975
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
81921528
00016717 00000-0 10270-3 0 9111
2 25544 51
6394 191
1501 0004317 352
1371 7
9713 15
53989535 4368
Satellite: ISS
Catalog Number: 25544
Epoch time: 18205
81921528 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 191
1501 deg
Eccentricity:
0004317
Arg of perigee: 352
1371 deg
Mean anomaly: 7
9713 deg
Mean motion: 15
53989535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 436
Checksum: 303
Coasting Arc #13 (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 = -897675
38 A = 6777647
73 meter
Y = 4129193
35 meter E =
0014789
Z = -5311437
25 I = 51
55726
XDOT = -7538
978193 Wp = 76
73180
YDOT = -1320
791015 meter/sec RA = 188
44388 deg
ZDOT = 251
252955 TA = 195
64614
MA = 195
69190
Ha = 221
496 n
mi
Hp = 214
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2945129
19 X = -917982
66
Y = 13547222
28 feet Y = 4119041
96 meter
Z = -17425975
21 Z = -5315846
65
XDOT = -24734
180422 XDOT = -7524
868871
YDOT = -4333
303855 feet/sec YDOT = -1405
018212 meter/sec
ZDOT = 824
320719 ZDOT = 214
665867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5825633
96 X = -1775653
23
Y = 12552208
89 feet Y = 3825913
27 meter
Z = -17446193
58 Z = -5317599
80
XDOT = -22198
113394 XDOT = -6765
984962
YDOT = -9402
168642 feet/sec YDOT = -2865
781002 meter/sec
ZDOT = 660
520276 ZDOT = 201
326580
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
14074845
00016717 00000-0 10270-3 0 9120
2 25544 51
6385 189
5427 0003946 353
0296 7
0801 15
54033411 4418
Satellite: ISS
Catalog Number: 25544
Epoch time: 18206
14074845 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 189
5427 deg
Eccentricity:
0003946
Arg of perigee: 353
0296 deg
Mean anomaly: 7
0801 deg
Mean motion: 15
54033411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 292
Coasting Arc #14 (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 = 2626588
59 A = 6779122
58 meter
Y = -3788093
28 meter E =
0008800
Z = 4968738
46 I = 51
59467
XDOT = 7063
613858 Wp = 34
60824
YDOT = 2107
243225 meter/sec RA = 183
44132 deg
ZDOT = -2118
521971 TA = 76
08025
MA = 75
98239
Ha = 221
560 n
mi
Hp = 214
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8617416
65 X = 2644617
80
Y = -12428127
57 feet Y = -3758620
67 meter
Z = 16301635
36 Z = 4981540
68
XDOT = 23174
586149 XDOT = 7049
815586
YDOT = 6913
527640 feet/sec YDOT = 2186
156503 meter/sec
ZDOT = -6950
531402 ZDOT = -2084
243278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10927217
18 X = 3330615
80
Y = -10364675
13 feet Y = -3159152
98 meter
Z = 16359430
73 Z = 4986354
49
XDOT = 20496
832719 XDOT = 6247
434613
YDOT = 10834
707750 feet/sec YDOT = 3302
418922 meter/sec
ZDOT = -6797
136514 ZDOT = -2071
767209
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
16965629
00016717 00000-0 10270-3 0 9133
2 25544 51
6382 184
4137 0003955 357
8768 2
2367 15
54009451 4571
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
16965629 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 184
4137 deg
Eccentricity:
0003955
Arg of perigee: 357
8768 deg
Mean anomaly: 2
2367 deg
Mean motion: 15
54009451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 328
Coasting Arc #15 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2018/207/15:58:15
055
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1572187
35 A = 6779034
65 meter
Y = 4114396
22 meter E =
0014247
Z = -5165485
58 I = 51
61019
XDOT = -7449
454225 Wp = 61
82278
YDOT = 1037
543114 meter/sec RA = 180
77983 deg
ZDOT = -1437
378114 TA = 194
30089
MA = 194
34126
Ha = 221
788 n
mi
Hp = 215
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5158094
96 X = 1551152
91
Y = 13498675
25 feet Y = 4131860
40 meter
Z = -16947131
17 Z = -5157899
26
XDOT = -24440
466619 XDOT = -7453
520773
YDOT = 3404
012841 feet/sec YDOT = 954
215577 meter/sec
ZDOT = -4715
807459 ZDOT = -1473
574067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5965615
51 X = -1818319
61
Y = -13204832
56 feet Y = -4024832
97 meter
Z = -16913582
13 Z = -5155259
83
XDOT = 23235
555209 XDOT = 7082
197228
YDOT = -4234
064665 feet/sec YDOT = -1290
542910 meter/sec
ZDOT = -4878
156298 ZDOT = -1486
862039
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
68410990
00016717 00000-0 10270-3 0 9147
2 25544 51
6384 181
8537 0004251 347
1485 12
9559 15
53805155 4650
Satellite: ISS
Catalog Number: 25544
Epoch time: 18207
68410990 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 181
8537 deg
Eccentricity:
0004251
Arg of perigee: 347
1485 deg
Mean anomaly: 12
9559 deg
Mean motion: 15
53805155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 321
Coasting Arc #16 (Orbit 480)
---------------------------------------
Vector Time (GMT): 2018/208/15:58:15
055
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 112496
84 A = 6778242
33 meter
Y = -4217422
35 meter E =
0005081
Z = 5304092
43 I = 51
64142
XDOT = 7655
734280 Wp = 18
26825
YDOT = -269
432960 meter/sec RA = 175
78310 deg
ZDOT = -371
791254 TA = 75
30426
MA = 75
24795
Ha = 221
734 n
mi
Hp = 215
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 369084
11 X = 133884
92
Y = -13836687
50 feet Y = -4216045
20 meter
Z = 17401878
05 Z = 5304690
47
XDOT = 25117
238452 XDOT = 7659
984096
YDOT = -883
966404 feet/sec YDOT = -183
797457 meter/sec
ZDOT = -1219
787579 ZDOT = -334
592838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 704472
90 X = 214723
34
Y = 13819712
92 feet Y = 4212248
50 meter
Z = 17405021
01 Z = 5305050
40
XDOT = -23995
616176 XDOT = -7313
863810
YDOT = 2569
284927 feet/sec YDOT = 783
118046 meter/sec
ZDOT = -1053
004937 ZDOT = -320
955905
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
71316438
00016717 00000-0 10270-3 0 9155
2 25544 51
6388 176
7266 0004292 347
7428 12
3619 15
53832932 4816
Satellite: ISS
Catalog Number: 25544
Epoch time: 18208
71316438 = yrday
fracday
Element set: 915
Inclination: 51
6388 deg
RA of node: 176
7266 deg
Eccentricity:
0004292
Arg of perigee: 347
7428 deg
Mean anomaly: 12
3619 deg
Mean motion: 15
53832932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 481
Checksum: 325
Coasting Arc #17 (Orbit 495)
---------------------------------------
Vector Time (GMT): 2018/209/15:58:15
055
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1752895
23 A = 6779743
67 meter
Y = 4268742
46 meter E =
0011689
Z = -4976687
93 I = 51
68035
XDOT = -7335
894876 Wp = 85
69172
YDOT = -523
680019 meter/sec RA = 170
78927 deg
ZDOT = 2139
865129 TA = 205
13983
MA = 205
19678
Ha = 221
941 n
mi
Hp = 215
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5750968
61 X = -1776325
62
Y = 14005060
57 feet Y = 4249009
72 meter
Z = -16327716
30 Z = -4985259
31
XDOT = -24067
896576 XDOT = -7339
887832
YDOT = -1718
110298 feet/sec YDOT = -605
737539 meter/sec
ZDOT = 7020
554884 ZDOT = 2104
220950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4412126
59 X = 1344816
19
Y = -14438728
57 feet Y = -4400924
47 meter
Z = -16366610
44 Z = -4988542
86
XDOT = 23119
313478 XDOT = 7046
766748
YDOT = -692
900596 feet/sec YDOT = -211
196102 meter/sec
ZDOT = 6860
803054 ZDOT = 2091
172771
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
67790175
00016717 00000-0 10270-3 0 9166
2 25544 51
6401 171
9195 0004354 353
3888 6
7206 15
53803840 4963
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
67790175 = yrday
fracday
Element set: 916
Inclination: 51
6401 deg
RA of node: 171
9195 deg
Eccentricity:
0004354
Arg of perigee: 353
3888 deg
Mean anomaly: 6
7206 deg
Mean motion: 15
53803840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 496
Checksum: 323
Coasting Arc #18 (Orbit 498)
---------------------------------------
Vector Time (GMT): 2018/209/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5554255
79 A = 6785284
97 meter
Y = 1795101
43 meter E =
0006179
Z = -3467659
93 I = 51
70097
XDOT = -4277
780045 Wp = 45
33169
YDOT = 4420
475084 meter/sec RA = 169
93132 deg
ZDOT = -4564
269563 TA = 175
27045
MA = 175
26461
Ha = 221
938 n
mi
Hp = 215
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18222624
00 X = 5550613
36
Y = 5889440
39 feet Y = 1857192
82 meter
Z = -11376837
03 Z = -3440688
60
XDOT = -14034
711434 XDOT = -4304
722767
YDOT = 14502
871009 feet/sec YDOT = 4372
487651 meter/sec
ZDOT = -14974
637674 ZDOT = -4585
114215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11773366
65 X = -3588522
15
Y = 15194403
47 feet Y = 4631254
18 meter
Z = -11256104
79 Z = -3430860
74
XDOT = -7774
802811 XDOT = -2369
759897
YDOT = -17185
310708 feet/sec YDOT = -5238
082704 meter/sec
ZDOT = -15068
576640 ZDOT = -4592
902160
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
87084720
00016717 00000-0 10270-3 0 9171
2 25544 51
6365 170
9563 0004352 352
9227 7
1863 15
53805582 4992
Satellite: ISS
Catalog Number: 25544
Epoch time: 18209
87084720 = yrday
fracday
Element set: 917
Inclination: 51
6365 deg
RA of node: 170
9563 deg
Eccentricity:
0004352
Arg of perigee: 352
9227 deg
Mean anomaly: 7
1863 deg
Mean motion: 15
53805582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 499
Checksum: 327
Coasting Arc #19 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2018/210/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4397064
15 A = 6781807
05 meter
Y = -2502335
80 meter E =
0008103
Z = 4508855
00 I = 51
72140
XDOT = 5626
333495 Wp = 83
41909
YDOT = -4123
139030 meter/sec RA = 164
95174 deg
ZDOT = 3194
550506 TA = 334
52697
MA = 334
56688
Ha = 222
134 n
mi
Hp = 215
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14426063
48 X = -4390656
70
Y = -8209763
14 feet Y = -2551471
21 meter
Z = 14792831
36 Z = 4487511
49
XDOT = 18459
099394 XDOT = 5656
504314
YDOT = -13527
359023 feet/sec YDOT = -4060
052943 meter/sec
ZDOT = 10480
808748 ZDOT = 3221
953762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12479404
96 X = 3803722
63
Y = -11072055
48 feet Y = -3374762
51 meter
Z = 14697394
91 Z = 4479765
97
XDOT = 6016
028215 XDOT = 1833
685400
YDOT = 20874
579790 feet/sec YDOT = 6362
571920 meter/sec
ZDOT = 10604
135242 ZDOT = 3232
140422
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
89989746
00016717 00000-0 10270-3 0 9188
2 25544 51
6364 165
8285 0004324 355
4309 4
6803 15
53784861 5154
Satellite: ISS
Catalog Number: 25544
Epoch time: 18210
89989746 = yrday
fracday
Element set: 918
Inclination: 51
6364 deg
RA of node: 165
8285 deg
Eccentricity:
0004324
Arg of perigee: 355
4309 deg
Mean anomaly: 4
6803 deg
Mean motion: 15
53784861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 336
Coasting Arc #20 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2018/211/20:18:00
000
Vector Time (MET): N/A
Weight (LBS) : 944337
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3007013
44 A = 6779093
95 meter
Y = 3232263
84 meter E =
0015055
Z = -5157677
74 I = 51
74428
XDOT = -6549
550193 Wp = 62
83769
YDOT = 3663
449860 meter/sec RA = 159
96578 deg
ZDOT = -1519
361450 TA = 192
50626
MA = 192
54366
Ha = 222
067 n
mi
Hp = 215
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9865529
64 X = 2995698
65
Y = 10604540
16 feet Y = 3265827
25 meter
Z = -16921514
89 Z = -5143098
38
XDOT = -21488
025568 XDOT = -6582
649021
YDOT = 12019
192453 feet/sec YDOT = 3590
023245 meter/sec
ZDOT = -4984
781661 ZDOT = -1551
256522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13163181
03 X = -4012137
58
Y = 6221925
17 feet Y = 1896442
79 meter
Z = -16856480
23 Z = -5137855
17
XDOT = -4363
947730 XDOT = -1330
131268
YDOT = -23155
180112 feet/sec YDOT = -7057
698898 meter/sec
ZDOT = -5128
216320 ZDOT = -1563
080334
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
86462820
00016717 00000-0 10270-3 0 9196
2 25544 51
6364 161
0211 0004187
5464 359
5692 15
53811703 5309
Satellite: ISS
Catalog Number: 25544
Epoch time: 18211
86462820 = yrday
fracday
Element set: 919
Inclination: 51
6364 deg
RA of node: 161
0211 deg
Eccentricity:
0004187
Arg of perigee:
5464 deg
Mean anomaly: 359
5692 deg
Mean motion: 15
53811703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 289
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