[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 3rd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
277/07:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
4
280/14:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
284/08:40:17
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
284/14:44:01
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
7
287/02:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
5
Coasting Arc #1 (Orbit 1534)
---------------------------------------
Vector Time (GMT): 2018/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6542191
64 A = 6790315
43 meter
Y = -1755185
82 meter E =
0007819
Z = -411955
43 I = 51
53748
XDOT = 889
834258 Wp = 32
37222
YDOT = -4707
595147 meter/sec RA = 197
78722 deg
ZDOT = 5985
119029 TA = 323
18126
MA = 323
23493
Ha = 220
545 n
mi
Hp = 216
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21463883
32 X = -6520077
36
Y = -5758483
66 feet Y = -1828221
52 meter
Z = -1351559
80 Z = -443681
49
XDOT = 2919
403734 XDOT = 913
337064
YDOT = -15444
865967 feet/sec YDOT = -4697
512724 meter/sec
ZDOT = 19636
217286 ZDOT = 5989
498850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22165984
62 X = 6756192
11
Y = 1456943
24 feet Y = 444076
30 meter
Z = -1493846
50 Z = -455324
41
XDOT = 387
791054 XDOT = 118
198713
YDOT = 14074
324246 feet/sec YDOT = 4289
854030 meter/sec
ZDOT = 19656
314608 ZDOT = 5991
244692
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 18276
50088036
00016717 00000-0 10270-3 0 9001
2 25544 51
6390 198
9544 0003689 243
3256 116
7519 15
53758023 15350
Satellite: ISS
Catalog Number: 25544
Epoch time: 18276
50088036 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 198
9544 deg
Eccentricity:
0003689
Arg of perigee: 243
3256 deg
Mean anomaly: 116
7519 deg
Mean motion: 15
53758023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1535
Checksum: 325
Coasting Arc #2 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2018/277/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6220926
06 A = 6787349
69 meter
Y = 645632
36 meter E =
0001455
Z = -2635378
29 I = 51
55195
XDOT = -2717
531800 Wp = 33
04862
YDOT = -4916
943403 meter/sec RA = 193
61988 deg
ZDOT = 5212
821049 TA = 297
22828
MA = 297
24310
Ha = 220
537 n
mi
Hp = 216
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20409862
39 X = -6214882
03
Y = 2118216
42 feet Y = 576099
29 meter
Z = -8646254
23 Z = -2665582
83
XDOT = -8915
786747 XDOT = -2687
668406
YDOT = -16131
704079 feet/sec YDOT = -4947
165444 meter/sec
ZDOT = 17102
431263 ZDOT = 5199
693012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15061584
37 X = 4590770
92
Y = 13850384
29 feet Y = 4221597
13 meter
Z = -8781945
51 Z = -2676736
99
XDOT = -5100
585046 XDOT = -1554
658322
YDOT = 16348
232246 feet/sec YDOT = 4982
941188 meter/sec
ZDOT = 17043
926707 ZDOT = 5194
988860
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 18277
33699950
00016717 00000-0 10270-3 0 9017
2 25544 51
6368 194
7886 0003628 243
9466 116
1313 15
53764316 15482
Satellite: ISS
Catalog Number: 25544
Epoch time: 18277
33699950 = yrday
fracday
Element set: 901
Inclination: 51
6368 deg
RA of node: 194
7886 deg
Eccentricity:
0003628
Arg of perigee: 243
9466 deg
Mean anomaly: 116
1313 deg
Mean motion: 15
53764316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 343
Coasting Arc #3 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2018/278/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6686433
76 A = 6789735
82 meter
Y = 106539
06 meter E =
0011791
Z = 1134597
85 I = 51
59332
XDOT = 923
643866 Wp = 136
96389
YDOT = 4848
191262 meter/sec RA = 188
64297 deg
ZDOT = -5870
900000 TA = 30
71071
MA = 30
64176
Ha = 220
351 n
mi
Hp = 216
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21937118
64 X = 6679234
17
Y = 349537
61 feet Y = 181271
24 meter
Z = 3722433
89 Z = 1167060
79
XDOT = 3030
327643 XDOT = 897
879190
YDOT = 15906
139312 feet/sec YDOT = 4858
375552 meter/sec
ZDOT = -19261
482941 ZDOT = -5866
476224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14529605
02 X = -4428623
61
Y = -16405588
53 feet Y = -5000423
39 meter
Z = 3868217
63 Z = 1179032
73
XDOT = 8408
842336 XDOT = 2563
015144
YDOT = -12004
838977 feet/sec YDOT = -3659
074920 meter/sec
ZDOT = -19242
049886 ZDOT = -5864
976805
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 18278
36606709
00016717 00000-0 10270-3 0 9022
2 25544 51
6376 189
6608 0003709 250
0720 110
0033 15
53786811 15642
Satellite: ISS
Catalog Number: 25544
Epoch time: 18278
36606709 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 189
6608 deg
Eccentricity:
0003709
Arg of perigee: 250
0720 deg
Mean anomaly: 110
0033 deg
Mean motion: 15
53786811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 308
Coasting Arc #4 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2018/279/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6723552
97 A = 6790182
21 meter
Y = -790833
01 meter E =
0009449
Z = 452766
65 I = 51
62855
XDOT = 959
361027 Wp = 41
43567
YDOT = -4690
377959 meter/sec RA = 183
67294 deg
ZDOT = 5989
298426 TA = 323
44696
MA = 323
51140
Ha = 220
297 n
mi
Hp = 216
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22058900
81 X = -6716409
25
Y = -2594596
50 feet Y = -865980
46 meter
Z = 1485454
90 Z = 420123
29
XDOT = 3147
509932 XDOT = 982
645879
YDOT = -15388
379129 feet/sec YDOT = -4679
518909 meter/sec
ZDOT = 19649
929220 ZDOT = 5994
015722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13287058
65 X = 4049895
48
Y = 17809969
69 feet Y = 5428478
76 meter
Z = 1338904
11 Z = 408097
97
XDOT = -11949
450999 XDOT = -3642
192665
YDOT = 7418
309586 feet/sec YDOT = 2261
100762 meter/sec
ZDOT = 19671
532972 ZDOT = 5995
883250
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 18279
39512914
00016717 00000-0 10270-3 0 9031
2 25544 51
6383 184
5339 0003741 251
6266 108
4480 15
53811202 15801
Satellite: ISS
Catalog Number: 25544
Epoch time: 18279
39512914 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 184
5339 deg
Eccentricity:
0003741
Arg of perigee: 251
6266 deg
Mean anomaly: 108
4480 deg
Mean motion: 15
53811202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 306
Coasting Arc #5 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2018/280/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6310705
39 A = 6788646
35 meter
Y = 1457123
40 meter E =
0005956
Z = -2022236
33 I = 51
65662
XDOT = -2811
005342 Wp = 173
45542
YDOT = 4464
649711 meter/sec RA = 178
70336 deg
ZDOT = -5562
572949 TA = 28
87857
MA = 28
84561
Ha = 220
287 n
mi
Hp = 216
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20704414
01 X = 6303765
44
Y = 4780588
59 feet Y = 1527655
05 meter
Z = -6634633
63 Z = -1991597
93
XDOT = -9222
458472 XDOT = -2833
701138
YDOT = 14647
800889 feet/sec YDOT = 4433
087542 meter/sec
ZDOT = -18249
911249 ZDOT = -5576
283582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11106336
07 X = -3385211
23
Y = -18165399
07 feet Y = -5536813
64 meter
Z = -6497132
14 Z = -1980325
87
XDOT = 15506
409069 XDOT = 4726
353484
YDOT = -2939
962243 feet/sec YDOT = -896
100492 meter/sec
ZDOT = -18311
893126 ZDOT = -5581
465025
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 18280
35987373
00016717 00000-0 10270-3 0 9045
2 25544 51
6387 179
7271 0003698 259
2842 100
7894 15
53790993 15954
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
35987373 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 179
7271 deg
Eccentricity:
0003698
Arg of perigee: 259
2842 deg
Mean anomaly: 100
7894 deg
Mean motion: 15
53790993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 363
Coasting Arc #6 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2018/280/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6136303
19 A = 6788357
12 meter
Y = 1972736
14 meter E =
0004080
Z = -2121972
58 I = 51
66638
XDOT = -3258
958658 Wp = 4
75547
YDOT = -4210
087668 meter/sec RA = 177
26657 deg
ZDOT = 5514
966279 TA = 331
75101
MA = 331
77313
Ha = 220
122 n
mi
Hp = 216
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20132228
33 X = -6147599
30
Y = 6472231
44 feet Y = 1904052
32 meter
Z = -6961852
29 Z = -2151808
53
XDOT = -10692
121581 XDOT = -3238
427097
YDOT = -13812
623583 feet/sec YDOT = -4246
416143 meter/sec
ZDOT = 18093
721388 ZDOT = 5499
185634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5886606
58 X = 1794237
69
Y = -20264689
92 feet Y = -6176677
49 meter
Z = -7096054
52 Z = -2162877
42
XDOT = 16019
735764 XDOT = 4882
815461
YDOT = -1652
315488 feet/sec YDOT = -503
625761 meter/sec
ZDOT = 18023
201769 ZDOT = 5493
471899
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 18280
61713700
00016717 00000-0 10270-3 0 9056
2 25544 51
6399 178
4463 0003928 261
7444 98
3264 15
53779925 15997
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
61713700 = yrday
fracday
Element set: 905
Inclination: 51
6399 deg
RA of node: 178
4463 deg
Eccentricity:
0003928
Arg of perigee: 261
7444 deg
Mean anomaly: 98
3264 deg
Mean motion: 15
53779925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 347
Coasting Arc #7 (Orbit 1614)
---------------------------------------
Vector Time (GMT): 2018/281/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6626108
97 A = 6790184
78 meter
Y = -1342383
32 meter E =
0010665
Z = 560431
51 I = 51
70593
XDOT = 1437
112250 Wp = 144
02074
YDOT = 4574
394619 meter/sec RA = 172
30030 deg
ZDOT = -5985
042866 TA = 29
93714
MA = 29
87619
Ha = 220
131 n
mi
Hp = 216
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21739202
67 X = 6637905
09
Y = -4404144
77 feet Y = -1268219
55 meter
Z = 1838686
06 Z = 592648
09
XDOT = 4714
935204 XDOT = 1414
925858
YDOT = 15007
856361 feet/sec YDOT = 4590
340616 meter/sec
ZDOT = -19635
967409 ZDOT = -5978
116234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8165361
39 X = -2488802
15
Y = 20609770
24 feet Y = 6281857
97 meter
Z = 1983540
89 Z = 604583
26
XDOT = -13716
438196 XDOT = -4180
770362
YDOT = -3532
988308 feet/sec YDOT = -1076
854836 meter/sec
ZDOT = -19605
251078 ZDOT = -5975
680529
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 18281
64619365
00016717 00000-0 10270-3 0 9063
2 25544 51
6405 173
3197 0003931 263
9738 96
0967 15
53781394 16154
Satellite: ISS
Catalog Number: 25544
Epoch time: 18281
64619365 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 173
3197 deg
Eccentricity:
0003931
Arg of perigee: 263
9738 deg
Mean anomaly: 96
0967 deg
Mean motion: 15
53781394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1615
Checksum: 341
Coasting Arc #8 (Orbit 1630)
---------------------------------------
Vector Time (GMT): 2018/282/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6671568
16 A = 6789824
92 meter
Y = 661113
36 meter E =
0010389
Z = 1036617
10 I = 51
73666
XDOT = 439
155961 Wp = 44
30796
YDOT = -4872
492330 meter/sec RA = 167
33604 deg
ZDOT = 5905
410608 TA = 326
91419
MA = 326
97914
Ha = 220
037 n
mi
Hp = 216
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21888346
99 X = -6683500
50
Y = 2169007
07 feet Y = 586440
65 meter
Z = 3400974
75 Z = 1004179
31
XDOT = 1440
800397 XDOT = 464
923001
YDOT = -15985
867223 feet/sec YDOT = -4867
436626 meter/sec
ZDOT = 19374
706719 ZDOT = 5907
607062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9800776
55 X = 2987276
69
Y = -19715973
00 feet Y = -6009428
57 meter
Z = 3255171
65 Z = 992176
32
XDOT = 11408
283818 XDOT = 3477
244908
YDOT = 8887
660580 feet/sec YDOT = 2708
958945 meter/sec
ZDOT = 19385
007167 ZDOT = 5908
550184
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 18282
67524457
00016717 00000-0 10270-3 0 9075
2 25544 51
6395 168
1911 0003997 268
3864 91
6830 15
53815315 16318
Satellite: ISS
Catalog Number: 25544
Epoch time: 18282
67524457 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 168
1911 deg
Eccentricity:
0003997
Arg of perigee: 268
3864 deg
Mean anomaly: 91
6830 deg
Mean motion: 15
53815315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1631
Checksum: 337
Coasting Arc #9 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2018/283/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6283232
73 A = 6787601
01 meter
Y = 120136
21 meter E =
0003220
Z = -2559749
56 I = 51
75925
XDOT = -2247
318080 Wp = 178
98498
YDOT = 5081
060490 meter/sec RA = 162
37208 deg
ZDOT = -5281
103830 TA = 29
71928
MA = 29
70099
Ha = 220
110 n
mi
Hp = 216
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20614280
60 X = 6293856
52
Y = 394147
67 feet Y = 190458
83 meter
Z = -8398128
47 Z = -2529201
36
XDOT = -7373
090814 XDOT = -2278
315524
YDOT = 16670
145963 feet/sec YDOT = 5055
755575 meter/sec
ZDOT = -17326
456135 ZDOT = -5292
096546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11013688
91 X = -3356972
38
Y = 17495403
71 feet Y = 5332599
05 meter
Z = -8260870
69 Z = -2517913
39
XDOT = -9248
296997 XDOT = -2818
880925
YDOT = -14021
508813 feet/sec YDOT = -4273
755886 meter/sec
ZDOT = -17376
307816 ZDOT = -5296
298622
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 18283
63997903
00016717 00000-0 10270-3 0 9083
2 25544 51
6377 163
3844 0003952 272
7607 87
3093 15
53798162 16464
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
63997903 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 163
3844 deg
Eccentricity:
0003952
Arg of perigee: 272
7607 deg
Mean anomaly: 87
3093 deg
Mean motion: 15
53798162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 351
Coasting Arc #10 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2018/284/08:40:17
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2800136
60 A = 6778741
31 meter
Y = -3313774
46 meter E =
0002104
Z = 5209381
59 I = 51
75474
XDOT = 6630
117015 Wp = 193
14032
YDOT = -3645
161288 meter/sec RA = 158
63961 deg
ZDOT = 1243
157728 TA = 244
93486
MA = 244
95670
Ha = 220
109 n
mi
Hp = 216
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9186799
87 X = -2788177
94
Y = -10871963
47 feet Y = -3345020
23 meter
Z = 17091146
94 Z = 5195808
52
XDOT = 21752
352413 XDOT = 6664
346716
YDOT = -11959
190579 feet/sec YDOT = -3570
827223 meter/sec
ZDOT = 4078
601470 ZDOT = 1275
448700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2393505
87 X = 729540
59
Y = 14104574
37 feet Y = 4299074
27 meter
Z = 17030452
04 Z = 5190881
78
XDOT = -23753
836304 XDOT = -7240
169305
YDOT = -1076
890647 feet/sec YDOT = -328
236269 meter/sec
ZDOT = 4224
044230 ZDOT = 1287
488681
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 18284
41176530
00016717 00000-0 10270-3 0 9096
2 25544 51
6388 159
5401 0003954 275
1405 84
9296 15
53839128 16586
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
41176530 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 159
5401 deg
Eccentricity:
0003954
Arg of perigee: 275
1405 deg
Mean anomaly: 84
9296 deg
Mean motion: 15
53839128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 336
Coasting Arc #11 (Orbit 1661)
---------------------------------------
Vector Time (GMT): 2018/284/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5130433
60 A = 6782959
34 meter
Y = -1441182
58 meter E =
0006350
Z = 4192782
49 I = 51
77438
XDOT = 4450
449707 Wp = 110
18214
YDOT = -5020
971146 meter/sec RA = 157
39568 deg
ZDOT = 3713
173145 TA = 301
73450
MA = 301
79637
Ha = 220
181 n
mi
Hp = 216
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16832131
22 X = -5134303
37
Y = -4728289
31 feet Y = -1498575
96 meter
Z = 13755848
06 Z = 4167850
78
XDOT = 14601
212948 XDOT = 4488
227789
YDOT = -16473
002449 feet/sec YDOT = -4970
991607 meter/sec
ZDOT = 12182
326592 ZDOT = 3734
884524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12498514
47 X = 3809547
21
Y = -12350338
60 feet Y = -3764383
21 meter
Z = 13643936
00 Z = 4158671
69
XDOT = 6201
063413 XDOT = 1890
084128
YDOT = 19866
551987 feet/sec YDOT = 6055
325046 meter/sec
ZDOT = 12280
355588 ZDOT = 3743
052383
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 18284
66902674
00016717 00000-0 10270-3 0 9101
2 25544 51
6371 158
2562 0004060 276
2380 83
8310 15
53797151 16624
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
66902674 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 158
2562 deg
Eccentricity:
0004060
Arg of perigee: 276
2380 deg
Mean anomaly: 83
8310 deg
Mean motion: 15
53797151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1662
Checksum: 309
Coasting Arc #12 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2018/285/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3937952
58 A = 6779813
86 meter
Y = 2374331
06 meter E =
0009078
Z = -4990401
67 I = 51
79365
XDOT = -5581
830760 Wp = 64
21779
YDOT = 4799
283492 meter/sec RA = 152
41494 deg
ZDOT = -2120
401444 TA = 185
15284
MA = 185
16219
Ha = 220
119 n
mi
Hp = 216
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12919791
93 X = 3935350
75
Y = 7789800
06 feet Y = 2418353
14 meter
Z = -16372708
89 Z = -4971278
50
XDOT = -18313
093046 XDOT = -5624
782808
YDOT = 15745
680749 feet/sec YDOT = 4736
623304 meter/sec
ZDOT = -6956
697652 ZDOT = -2147
621242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13094872
25 X = -3991317
06
Y = 7676343
10 feet Y = 2339749
38 meter
Z = -16286978
92 Z = -4964271
18
XDOT = -4458
922650 XDOT = -1359
079624
YDOT = -22632
924296 feet/sec YDOT = -6898
515325 meter/sec
ZDOT = -7079
484113 ZDOT = -2157
826758
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 18285
63375586
00016717 00000-0 10270-3 0 9116
2 25544 51
6365 153
4482 0003881 279
1394 80
9320 15
53814067 16773
Satellite: ISS
Catalog Number: 25544
Epoch time: 18285
63375586 = yrday
fracday
Element set: 911
Inclination: 51
6365 deg
RA of node: 153
4482 deg
Eccentricity:
0003881
Arg of perigee: 279
1394 deg
Mean anomaly: 80
9320 deg
Mean motion: 15
53814067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 333
Coasting Arc #13 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2018/286/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2572040
22 A = 6778428
89 meter
Y = -3321998
62 meter E =
0001211
Z = 5320434
03 I = 51
81733
XDOT = 6308
773454 Wp = 275
85593
YDOT = -4344
632879 meter/sec RA = 147
43065 deg
ZDOT = 337
293141 TA = 170
93699
MA = 170
93480
Ha = 220
339 n
mi
Hp = 216
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8438452
16 X = -2560545
93
Y = -10898945
61 feet Y = -3350696
47 meter
Z = 17455492
23 Z = 5307967
76
XDOT = 20698
075636 XDOT = 6355
249039
YDOT = -14254
044879 feet/sec YDOT = -4273
823920 meter/sec
ZDOT = 1106
604793 ZDOT = 368
052660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13627936
66 X = 4153795
09
Y = -2493211
36 feet Y = -759930
82 meter
Z = 17399768
36 Z = 5303449
40
XDOT = 2793
262652 XDOT = 851
386456
YDOT = 23954
400008 feet/sec YDOT = 7301
301122 meter/sec
ZDOT = 1245
283584 ZDOT = 379
562436
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 18286
66279859
00016717 00000-0 10270-3 0 9127
2 25544 51
6362 148
3201 0003811 283
4533 76
6195 15
53774241 16937
Satellite: ISS
Catalog Number: 25544
Epoch time: 18286
66279859 = yrday
fracday
Element set: 912
Inclination: 51
6362 deg
RA of node: 148
3201 deg
Eccentricity:
0003811
Arg of perigee: 283
4533 deg
Mean anomaly: 76
6195 deg
Mean motion: 15
53774241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 328
Coasting Arc #14 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2018/287/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 603740
14 A = 6779381
64 meter
Y = 4454354
20 meter E =
0009470
Z = -5083406
51 I = 51
83575
XDOT = -6803
438587 Wp = 102
86509
YDOT = 3008
724478 meter/sec RA = 145
00079 deg
ZDOT = 1829
196097 TA = 184
81011
MA = 184
81922
Ha = 220
284 n
mi
Hp = 216
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1980774
73 X = 578578
42
Y = 14614022
98 feet Y = 4460964
77 meter
Z = -16677842
88 Z = -5080534
98
XDOT = -22320
992738 XDOT = -6845
462772
YDOT = 9871
143302 feet/sec YDOT = 2932
408803 meter/sec
ZDOT = 6001
299531 ZDOT = 1796
044542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13470560
04 X = 4105826
70
Y = 6037666
93 feet Y = 1840280
88 meter
Z = -16665358
36 Z = -5079601
23
XDOT = -3159
124190 XDOT = -962
901053
YDOT = 23193
741097 feet/sec YDOT = 7069
452286 meter/sec
ZDOT = 5851
982501 ZDOT = 1783
684266
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 18287
11300221
00016717 00000-0 10270-3 0 9137
2 25544 51
6377 146
0798 0003753 285
7258 74
3480 15
53794027 17008
Satellite: ISS
Catalog Number: 25544
Epoch time: 18287
11300221 = yrday
fracday
Element set: 913
Inclination: 51
6377 deg
RA of node: 146
0798 deg
Eccentricity:
0003753
Arg of perigee: 285
7258 deg
Mean anomaly: 74
3480 deg
Mean motion: 15
53794027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 309
Coasting Arc #15 (Orbit 1715)
---------------------------------------
Vector Time (GMT): 2018/288/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 795598
80 A = 6782097
74 meter
Y = -5132355
93 meter E =
0006956
Z = 4359493
30 I = 51
87091
XDOT = 6555
672644 Wp = 51
12352
YDOT = -1939
777870 meter/sec RA = 140
02409 deg
ZDOT = -3472
088729 TA = 74
05961
MA = 73
98298
Ha = 220
237 n
mi
Hp = 216
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2610232
28 X = 831754
64
Y = -16838438
09 feet Y = -5123256
69 meter
Z = 14302799
54 Z = 4363446
09
XDOT = 21508
112350 XDOT = 6593
742398
YDOT = -6364
100622 feet/sec YDOT = -1866
255040 meter/sec
ZDOT = -11391
367221 ZDOT = -3440
150499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13079720
40 X = -3986698
78
Y = -10896986
03 feet Y = -3321401
34 meter
Z = 14321068
20 Z = 4365061
59
XDOT = 4980
881274 XDOT = 1518
172612
YDOT = -20794
759577 feet/sec YDOT = -6338
242719 meter/sec
ZDOT = -11247
584777 ZDOT = -3428
263840
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 18288
14204040
00016717 00000-0 10270-3 0 9144
2 25544 51
6368 140
9520 0003874 290
0052 70
0684 15
53837068 17168
Satellite: ISS
Catalog Number: 25544
Epoch time: 18288
14204040 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node: 140
9520 deg
Eccentricity:
0003874
Arg of perigee: 290
0052 deg
Mean anomaly: 70
0684 deg
Mean motion: 15
53837068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1716
Checksum: 296
Coasting Arc #16 (Orbit 1730)
---------------------------------------
Vector Time (GMT): 2018/289/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2012561
14 A = 6785726
71 meter
Y = 5606387
03 meter E =
0002507
Z = -3248905
63 I = 51
90824
XDOT = -5951
320545 Wp = 30
34368
YDOT = 636
357644 meter/sec RA = 135
05845 deg
ZDOT = 4788
423483 TA = 292
18193
MA = 292
20853
Ha = 220
431 n
mi
Hp = 216
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6602890
89 X = -2059322
06
Y = 18393658
24 feet Y = 5583619
61 meter
Z = -10659139
19 Z = -3258795
85
XDOT = -19525
329871 XDOT = -5981
254113
YDOT = 2087
787545 feet/sec YDOT = 569
638638 meter/sec
ZDOT = 15710
050797 ZDOT = 4759
440911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12580359
32 X = 3834493
52
Y = 14923054
31 feet Y = 4548546
95 meter
Z = -10704162
24 Z = -3262628
65
XDOT = -7017
210711 XDOT = -2138
845825
YDOT = 17082
050084 feet/sec YDOT = 5206
608866 meter/sec
ZDOT = 15579
666131 ZDOT = 4748
682237
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 18289
10676220
00016717 00000-0 10270-3 0 9155
2 25544 51
6375 136
1455 0003698 295
5944 64
4826 15
53815232 17315
Satellite: ISS
Catalog Number: 25544
Epoch time: 18289
10676220 = yrday
fracday
Element set: 915
Inclination: 51
6375 deg
RA of node: 136
1455 deg
Eccentricity:
0003698
Arg of perigee: 295
5944 deg
Mean anomaly: 64
4826 deg
Mean motion: 15
53815232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1731
Checksum: 324
Coasting Arc #17 (Orbit 1746)
---------------------------------------
Vector Time (GMT): 2018/290/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3020465
82 A = 6788711
23 meter
Y = -5796305
38 meter E =
0010065
Z = 1817955
76 I = 51
94061
XDOT = 5083
335429 Wp = 111
40716
YDOT = 862
130425 meter/sec RA = 130
10235 deg
ZDOT = -5675
366123 TA = 48
69564
MA = 48
60904
Ha = 220
470 n
mi
Hp = 216
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9909664
76 X = 3076226
46
Y = -19016749
93 feet Y = -5762216
58 meter
Z = 5964421
79 Z = 1832763
97
XDOT = 16677
609675 XDOT = 5100
885303
YDOT = 2828
511894 feet/sec YDOT = 919
073717 meter/sec
ZDOT = -18619
967595 ZDOT = -5650
630161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11743572
89 X = -3579441
02
Y = -17919847
65 feet Y = -5461969
56 meter
Z = 6031593
23 Z = 1838429
62
XDOT = 9388
232319 XDOT = 2861
533211
YDOT = -12405
914862 feet/sec YDOT = -3781
322850 meter/sec
ZDOT = -18508
813938 ZDOT = -5641
486488
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 18290
13579470
00016717 00000-0 10270-3 0 9160
2 25544 51
6370 131
0174 0003928 301
1442 58
9325 15
53848800 17471
Satellite: ISS
Catalog Number: 25544
Epoch time: 18290
13579470 = yrday
fracday
Element set: 916
Inclination: 51
6370 deg
RA of node: 131
0174 deg
Eccentricity:
0003928
Arg of perigee: 301
1442 deg
Mean anomaly: 58
9325 deg
Mean motion: 15
53848800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1747
Checksum: 305
Coasting Arc #18 (Orbit 1761)
---------------------------------------
Vector Time (GMT): 2018/291/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3748707
77 A = 6790075
25 meter
Y = 5648167
42 meter E =
0011406
Z = -239307
87 I = 51
96529
XDOT = -4055
273913 Wp = 24
95824
YDOT = -2440
654967 meter/sec RA = 125
15479 deg
ZDOT = 6034
922217 TA = 332
47453
MA = 332
53489
Ha = 220
501 n
mi
Hp = 216
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12298910
01 X = -3810426
10
Y = 18530733
00 feet Y = 5605901
67 meter
Z = -785130
82 Z = -257668
17
XDOT = -13304
704438 XDOT = -4056
995217
YDOT = -8007
398186 feet/sec YDOT = -2486
013188 meter/sec
ZDOT = 19799
613574 ZDOT = 6015
218831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10471934
06 X = 3191845
50
Y = 19617654
67 feet Y = 5979461
14 meter
Z = -868277
43 Z = -264650
96
XDOT = -11994
887000 XDOT = -3656
041558
YDOT = 7260
277237 feet/sec YDOT = 2212
932502 meter/sec
ZDOT = 19711
243635 ZDOT = 6007
987060
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 18291
10051228
00016717 00000-0 10270-3 0 9175
2 25544 51
6365 126
2113 0003723 301
5646 58
5143 15
53861684 17623
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
10051228 = yrday
fracday
Element set: 917
Inclination: 51
6365 deg
RA of node: 126
2113 deg
Eccentricity:
0003723
Arg of perigee: 301
5646 deg
Mean anomaly: 58
5143 deg
Mean motion: 15
53861684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1762
Checksum: 292
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