[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 20th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
141/08:41:36
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
5
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 3389)
---------------------------------------
Vector Time (GMT): 2018/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5488079
65 A = 6783990
71 meter
Y = -1565279
25 meter E =
0016057
Z = 3655334
21 I = 51
72788
XDOT = 4251
904634 Wp = 94
97442
YDOT = -4656
237299 meter/sec RA = 165
56523 deg
ZDOT = 4372
000916 TA = 308
41950
MA = 308
56356
Ha = 222
717 n
mi
Hp = 213
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18005510
66 X = -5487924
25
Y = -5135430
62 feet Y = -1626650
30 meter
Z = 11992566
31 Z = 3628674
93
XDOT = 13949
818354 XDOT = 4282
418847
YDOT = -15276
369091 feet/sec YDOT = -4608
519478 meter/sec
ZDOT = 14343
835025 ZDOT = 4392
728976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14526886
77 X = -4427795
09
Y = 11932286
60 feet Y = 3636960
96 meter
Z = 11873618
06 Z = 3619078
78
XDOT = -3783
472368 XDOT = -1153
202378
YDOT = -19031
155287 feet/sec YDOT = -5800
696131 meter/sec
ZDOT = 14437
018852 ZDOT = 4400
403346
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
55664498
00016717 00000-0 10270-3 0 9005
2 25544 51
6373 166
4245 0004118 96
7998 263
3623 15
54053453 33902
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
55664498 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 166
4245 deg
Eccentricity:
0004118
Arg of perigee: 96
7998 deg
Mean anomaly: 263
3623 deg
Mean motion: 15
54053453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 331
Coasting Arc #2 (Orbit 3404)
---------------------------------------
Vector Time (GMT): 2018/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4244771
10 A = 6780234
35 meter
Y = 2436929
11 meter E =
0014132
Z = -4705225
29 I = 51
74918
XDOT = -5629
785418 Wp = 79
01902
YDOT = 4350
233591 meter/sec RA = 160
58395 deg
ZDOT = -2830
372438 TA = 162
92509
MA = 162
87749
Ha = 222
516 n
mi
Hp = 213
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13926414
38 X = 4240060
84
Y = 7995174
26 feet Y = 2484371
27 meter
Z = -15437090
84 Z = -4684616
71
XDOT = -18470
424600 XDOT = -5664
263971
YDOT = 14272
419918 feet/sec YDOT = 4287
084997 meter/sec
ZDOT = -9285
998812 ZDOT = -2857
803384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14442250
73 X = 4401998
02
Y = -7219117
16 feet Y = -2200386
91 meter
Z = -15345271
06 Z = -4677238
62
XDOT = 1106
761594 XDOT = 337
340934
YDOT = 22182
375337 feet/sec YDOT = 6761
188003 meter/sec
ZDOT = -9409
122983 ZDOT = -2867
900685
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
52120960
00016717 00000-0 10270-3 0 9015
2 25544 51
6393 161
6167 0003925 101
0238 259
1356 15
54074805 34053
Satellite: ISS
Catalog Number: 25544
Epoch time: 18139
52120960 = yrday
fracday
Element set: 901
Inclination: 51
6393 deg
RA of node: 161
6167 deg
Eccentricity:
0003925
Arg of perigee: 101
0238 deg
Mean anomaly: 259
1356 deg
Mean motion: 15
54074805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 292
Coasting Arc #3 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2018/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2754766
76 A = 6777845
91 meter
Y = -3285923
79 meter E =
0007638
Z = 5243475
35 I = 51
77089
XDOT = 6554
322576 Wp = 112
80735
YDOT = -3857
683121 meter/sec RA = 155
59600 deg
ZDOT = 1021
880585 TA = 327
40903
MA = 327
45615
Ha = 222
617 n
mi
Hp = 213
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9037948
70 X = -2743288
01
Y = -10780589
87 feet Y = -3316665
83 meter
Z = 17203003
12 Z = 5230121
17
XDOT = 21503
682993 XDOT = 6592
009346
YDOT = -12656
440687 feet/sec YDOT = -3784
177555 meter/sec
ZDOT = 3352
626591 ZDOT = 1053
810436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14017448
20 X = -4272518
21
Y = 1858395
01 feet Y = 566438
80 meter
Z = 17143700
44 Z = 5225399
89
XDOT = 1124
572621 XDOT = 342
769735
YDOT = -23890
377812 feet/sec YDOT = -7281
787157 meter/sec
ZDOT = 3495
823773 ZDOT = 1065
527086
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
55007613
00016717 00000-0 10270-3 0 9020
2 25544 51
6380 156
4879 0004017 102
7201 257
4401 15
54085553 34214
Satellite: ISS
Catalog Number: 25544
Epoch time: 18140
55007613 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 156
4879 deg
Eccentricity:
0004017
Arg of perigee: 102
7201 deg
Mean anomaly: 257
4401 deg
Mean motion: 15
54085553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 278
Coasting Arc #4 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2018/141/08:41:36
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5513726
01 A = 6783079
28 meter
Y = 505039
93 meter E =
0009842
Z = -3927215
74 I = 51
81398
XDOT = -3404
419564 Wp = 87
65792
YDOT = 5518
289229 meter/sec RA = 151
32434 deg
ZDOT = -4078
507575 TA = 139
73778
MA = 139
66485
Ha = 222
485 n
mi
Hp = 213
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18089652
25 X = 5526745
08
Y = 1656955
14 feet Y = 566771
32 meter
Z = -12884566
09 Z = -3900400
28
XDOT = -11169
355524 XDOT = -3446
062303
YDOT = 18104
623454 feet/sec YDOT = 5479
986157 meter/sec
ZDOT = -13380
930365 ZDOT = -4095
145778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18220163
88 X = 5553505
95
Y = -1039277
43 feet Y = -316771
76 meter
Z = -12764740
22 Z = -3890692
82
XDOT = -8368
802644 XDOT = -2550
811046
YDOT = 18209
626365 feet/sec YDOT = 5550
294116 meter/sec
ZDOT = -13455
979490 ZDOT = -4101
382548
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
38602970
00016717 00000-0 10270-3 0 9030
2 25544 51
6382 152
3207 0003848 109
1141 251
0429 15
54073270 34348
Satellite: ISS
Catalog Number: 25544
Epoch time: 18141
38602970 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 152
3207 deg
Eccentricity:
0003848
Arg of perigee: 109
1141 deg
Mean anomaly: 251
0429 deg
Mean motion: 15
54073270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 282
Coasting Arc #5 (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 = 2047707
10 A = 6777488
67 meter
Y = 3668075
94 meter E =
0018511
Z = -5334450
85 I = 51
81170
XDOT = -6567
451979 Wp = 95
20258
YDOT = 3928
359079 meter/sec RA = 148
05915 deg
ZDOT = 179
106216 TA = 176
50978
MA = 176
49685
Ha = 222
410 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6718199
14 X = 2032449
46
Y = 12034369
89 feet Y = 3690889
86 meter
Z = -17501479
15 Z = -5324540
59
XDOT = -21546
758462 XDOT = -6611
761864
YDOT = 12888
317188 feet/sec YDOT = 3854
669544 meter/sec
ZDOT = 587
618819 ZDOT = 147
096414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13818456
56 X = -4211865
56
Y = 737644
08 feet Y = 224833
91 meter
Z = -17457610
67 Z = -5321079
73
XDOT = -1848
297170 XDOT = -563
360977
YDOT = -24030
347813 feet/sec YDOT = -7324
450013 meter/sec
ZDOT = 444
024495 ZDOT = 135
338666
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
02906844
00016717 00000-0 10270-3 0 9040
2 25544 51
6357 149
1134 0003806 109
5841 250
5723 15
54087140 34441
Satellite: ISS
Catalog Number: 25544
Epoch time: 18142
02906844 = yrday
fracday
Element set: 904
Inclination: 51
6357 deg
RA of node: 149
1134 deg
Eccentricity:
0003806
Arg of perigee: 109
5841 deg
Mean anomaly: 250
5723 deg
Mean motion: 15
54087140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3444
Checksum: 295
Coasting Arc #6 (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 = -495271
41 A = 6778904
43 meter
Y = -4542517
28 meter E =
0008649
Z = 5000633
37 I = 51
84418
XDOT = 6739
869851 Wp = 78
20761
YDOT = -3025
204072 meter/sec RA = 143
07343 deg
ZDOT = -2075
778780 TA = 31
93973
MA = 31
88733
Ha = 222
455 n
mi
Hp = 213
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1624906
21 X = -468729
45
Y = -14903271
92 feet Y = -4547907
60 meter
Z = 16406277
46 Z = 4998291
74
XDOT = 22112
433894 XDOT = 6783
280662
YDOT = -9925
210209 feet/sec YDOT = -2949
591373 meter/sec
ZDOT = -6810
297836 ZDOT = -2042
933436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14192127
01 X = 4325760
31
Y = 4863824
17 feet Y = 1482493
61 meter
Z = 16396356
90 Z = 4997609
58
XDOT = -247
425455 XDOT = -75
415279
YDOT = 23236
286892 feet/sec YDOT = 7082
420245 meter/sec
ZDOT = -6663
058235 ZDOT = -2030
900150
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
05792846
00016717 00000-0 10270-3 0 9050
2 25544 51
6362 143
9842 0003768 113
1759 246
9791 15
54062486 34609
Satellite: ISS
Catalog Number: 25544
Epoch time: 18143
05792846 = yrday
fracday
Element set: 905
Inclination: 51
6362 deg
RA of node: 143
9842 deg
Eccentricity:
0003768
Arg of perigee: 113
1759 deg
Mean anomaly: 246
9791 deg
Mean motion: 15
54062486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3460
Checksum: 333
Coasting Arc #7 (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 = -951742
90 A = 6782004
43 meter
Y = 5263320
00 meter E =
0011792
Z = -4182289
78 I = 51
88044
XDOT = -6426
004346 Wp = 112
44859
YDOT = 1813
931794 meter/sec RA = 138
09586 deg
ZDOT = 3749
177273 TA = 196
01869
MA = 196
05601
Ha = 222
417 n
mi
Hp = 213
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3122516
08 X = -990212
55
Y = 17268110
25 feet Y = 5252462
04 meter
Z = -13721423
16 Z = -4187006
26
XDOT = -21082
691425 XDOT = -6464
022283
YDOT = 5951
219796 feet/sec YDOT = 1741
859052 meter/sec
ZDOT = 12300
450370 ZDOT = 3717
869498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14443575
14 X = -4402401
70
Y = -9935990
48 feet Y = -3028489
90 meter
Z = -13743159
11 Z = -4188914
90
XDOT = 2660
830592 XDOT = 811
021165
YDOT = -20669
242027 feet/sec YDOT = -6299
984970 meter/sec
ZDOT = 12160
217757 ZDOT = 3706
434372
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
02248158
00016717 00000-0 10270-3 0 9061
2 25544 51
6360 139
1755 0003975 116
8375 243
3184 15
54094408 34753
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
02248158 = yrday
fracday
Element set: 906
Inclination: 51
6360 deg
RA of node: 139
1755 deg
Eccentricity:
0003975
Arg of perigee: 116
8375 deg
Mean anomaly: 243
3184 deg
Mean motion: 15
54094408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 318
Coasting Arc #8 (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 = 4279014
76 A = 6778681
55 meter
Y = 1418982
58 meter E =
0016119
Z = -5076543
90 I = 51
88145
XDOT = -4240
655420 Wp = 85
19786
YDOT = 6092
454044 meter/sec RA = 136
27289 deg
ZDOT = -1875
305317 TA = 166
68374
MA = 166
64114
Ha = 222
409 n
mi
Hp = 213
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14038762
33 X = 4287488
66
Y = 4655454
67 feet Y = 1466881
07 meter
Z = -16655327
76 Z = -5055737
12
XDOT = -13912
911482 XDOT = -4299
358415
YDOT = 19988
366285 feet/sec YDOT = 6044
703965 meter/sec
ZDOT = -6152
576500 ZDOT = -1896
047439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14876109
99 X = 4534238
32
Y = -739370
91 feet Y = -225360
25 meter
Z = -16562449
42 Z = -5048234
58
XDOT = -5819
266484 XDOT = -1773
712424
YDOT = 22552
162744 feet/sec YDOT = 6873
899204 meter/sec
ZDOT = -6246
087901 ZDOT = -1903
807592
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
40830198
00016717 00000-0 10270-3 0 9075
2 25544 51
6393 137
2556 0003872 116
7471 243
4078 15
54085605 34818
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
40830198 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 137
2556 deg
Eccentricity:
0003872
Arg of perigee: 116
7471 deg
Mean anomaly: 243
4078 deg
Mean motion: 15
54085605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 317
Coasting Arc #9 (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 = -3121546
68 A = 6777410
23 meter
Y = -2779345
39 meter E =
0006175
Z = 5330152
81 I = 51
89933
XDOT = 5079
194939 Wp = 108
21666
YDOT = -5751
811022 meter/sec RA = 131
29131 deg
ZDOT = -26
495441 TA = 342
02383
MA = 342
04566
Ha = 222
507 n
mi
Hp = 213
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10241294
88 X = -3116126
65
Y = -9118587
24 feet Y = -2814222
63 meter
Z = 17487377
99 Z = 5315002
27
XDOT = 16664
025392 XDOT = 5143
264470
YDOT = -18870
771071 feet/sec YDOT = -5694
653729 meter/sec
ZDOT = -86
927301 ZDOT = -1
666845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13021135
85 X = -3968842
21
Y = -4564657
32 feet Y = -1391307
55 meter
Z = 17419961
76 Z = 5309604
34
XDOT = 8032
524723 XDOT = 2448
313536
YDOT = -22795
441558 feet/sec YDOT = -6948
050587 meter/sec
ZDOT = 24
837037 ZDOT = 7
570329
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
43715479
00016717 00000-0 10270-3 0 9084
2 25544 51
6380 132
1268 0003947 118
6217 241
5333 15
54105495 34970
Satellite: ISS
Catalog Number: 25544
Epoch time: 18145
43715479 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 132
1268 deg
Eccentricity:
0003947
Arg of perigee: 118
6217 deg
Mean anomaly: 241
5333 deg
Mean motion: 15
54105495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 318
Coasting Arc #10 (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 = 1906538
01 A = 6778672
33 meter
Y = 4103131
42 meter E =
0016585
Z = -5062841
40 I = 51
92602
XDOT = -5513
925648 Wp = 108
37166
YDOT = 4946
616074 meter/sec RA = 126
31112 deg
ZDOT = 1932
631664 TA = 180
33217
MA = 180
33327
Ha = 222
306 n
mi
Hp = 213
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6255045
97 X = 1885106
95
Y = 13461717
25 feet Y = 4124332
13 meter
Z = -16610372
04 Z = -5053631
76
XDOT = -18090
307244 XDOT = -5578
218097
YDOT = 16229
055361 feet/sec YDOT = 4884
595958 meter/sec
ZDOT = 6340
655065 ZDOT = 1905
690683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11122551
87 X = 3390153
81
Y = 9898579
06 feet Y = 3017086
90 meter
Z = -16569697
14 Z = -5050443
69
XDOT = -9617
661256 XDOT = -2931
463151
YDOT = 21217
505600 feet/sec YDOT = 6467
095707 meter/sec
ZDOT = 6219
522784 ZDOT = 1895
710544
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
40170040
00016717 00000-0 10270-3 0 9092
2 25544 51
6396 127
3187 0003721 121
9846 238
1669 15
54086597 35121
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
40170040 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 127
3187 deg
Eccentricity:
0003721
Arg of perigee: 121
9846 deg
Mean anomaly: 238
1669 deg
Mean motion: 15
54086597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3512
Checksum: 317
Coasting Arc #11 (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 = -1066244
83 A = 6780378
12 meter
Y = -4863190
33 meter E =
0010722
Z = 4594480
68 I = 51
93994
XDOT = 5680
466832 Wp = 81
67390
YDOT = -4149
322322 meter/sec RA = 123
89911 deg
ZDOT = -3066
120689 TA = 38
85991
MA = 38
78287
Ha = 222
167 n
mi
Hp = 213
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3498178
57 X = -1034101
96
Y = -15955348
85 feet Y = -4874934
42 meter
Z = 15073755
52 Z = 4589378
88
XDOT = 18636
702204 XDOT = 5741
337330
YDOT = -13613
262211 feet/sec YDOT = -4085
458864 meter/sec
ZDOT = -10059
451079 ZDOT = -3038
378970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8321739
24 X = 2536466
12
Y = 14079341
06 feet Y = 4291383
15 meter
Z = 15051555
65 Z = 4587714
16
XDOT = -12593
862074 XDOT = -3838
609160
YDOT = 18091
300251 feet/sec YDOT = 5514
228316 meter/sec
ZDOT = -9934
828315 ZDOT = -3028
135670
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
91612227
00016717 00000-0 10270-3 0 9108
2 25544 51
6380 124
7534 0003391 123
5570 236
5906 15
54131055 35201
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
91612227 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 124
7534 deg
Eccentricity:
0003391
Arg of perigee: 123
5570 deg
Mean anomaly: 236
5906 deg
Mean motion: 15
54131055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 283
Coasting Arc #12 (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 = -66811
66 A = 6784128
44 meter
Y = 5806757
23 meter E =
0008290
Z = -3516726
72 I = 51
96822
XDOT = -5548
277863 Wp = 108
53354
YDOT = 2686
029259 meter/sec RA = 118
93247 deg
ZDOT = 4546
729480 TA = 210
34610
MA = 210
39412
Ha = 222
149 n
mi
Hp = 213
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -219198
36 X = -114656
76
Y = 19051040
79 feet Y = 5805742
90 meter
Z = -11537817
32 Z = -3517166
95
XDOT = -18203
011360 XDOT = -5599
987386
YDOT = 8812
431951 feet/sec YDOT = 2623
695055 meter/sec
ZDOT = 14917
091469 ZDOT = 4519
652079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6023845
15 X = -1836068
00
Y = -18073200
83 feet Y = -5508711
61 meter
Z = -11540543
00 Z = -3517557
51
XDOT = 13151
017638 XDOT = 4008
430176
YDOT = -13817
943165 feet/sec YDOT = -4211
709077 meter/sec
ZDOT = 14795
610015 ZDOT = 4509
701933
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
88066519
00016717 00000-0 10270-3 0 9113
2 25544 51
6364 119
9447 0003547 128
6010 231
5461 15
54114601 35355
Satellite: ISS
Catalog Number: 25544
Epoch time: 18147
88066519 = yrday
fracday
Element set: 911
Inclination: 51
6364 deg
RA of node: 119
9447 deg
Eccentricity:
0003547
Arg of perigee: 128
6010 deg
Mean anomaly: 231
5461 deg
Mean motion: 15
54114601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 302
Coasting Arc #13 (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 = 3824132
34 A = 6777492
93 meter
Y = 1707240
69 meter E =
0017691
Z = -5343831
50 I = 51
95346
XDOT = -3346
211339 Wp = 96
84354
YDOT = 6882
630584 meter/sec RA = 117
09048 deg
ZDOT = -198
360039 TA = 171
28635
MA = 171
25560
Ha = 222
210 n
mi
Hp = 213
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12546365
94 X = 3830715
22
Y = 5601183
38 feet Y = 1750042
11 meter
Z = -17532255
58 Z = -5325238
73
XDOT = -10978
383657 XDOT = -3421
962555
YDOT = 22580
809001 feet/sec YDOT = 6844
787412 meter/sec
ZDOT = -650
787529 ZDOT = -214
798347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9083562
42 X = 2768669
83
Y = 10448698
89 feet Y = 3184763
42 meter
Z = -17449301
55 Z = -5318547
11
XDOT = -18765
586121 XDOT = -5719
750650
YDOT = 15117
079953 feet/sec YDOT = 4607
685970 meter/sec
ZDOT = -725
230343 ZDOT = -221
050209
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
26648220
00016717 00000-0 10270-3 0 9122
2 25544 51
6382 118
0219 0003691 132
3286 227
8180 15
54088465 35410
Satellite: ISS
Catalog Number: 25544
Epoch time: 18148
26648220 = yrday
fracday
Element set: 912
Inclination: 51
6382 deg
RA of node: 118
0219 deg
Eccentricity:
0003691
Arg of perigee: 132
3286 deg
Mean anomaly: 227
8180 deg
Mean motion: 15
54088465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 306
Coasting Arc #14 (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 = -2975725
56 A = 6778255
43 meter
Y = -3299514
14 meter E =
0006784
Z = 5113150
91 I = 51
97166
XDOT = 4019
310499 Wp = 86
96702
YDOT = -6304
327964 meter/sec RA = 112
11343 deg
ZDOT = -1726
725124 TA = 19
64521
MA = 19
61909
Ha = 222
185 n
mi
Hp = 213
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9762879
13 X = -2963445
69
Y = -10825177
61 feet Y = -3332722
69 meter
Z = 16775429
51 Z = 5098725
09
XDOT = 13186
714234 XDOT = 4097
896140
YDOT = -20683
490695 feet/sec YDOT = -6258
941662 meter/sec
ZDOT = -5665
108676 ZDOT = -1707
010285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4579950
96 X = -1395969
05
Y = -13916495
84 feet Y = -4241747
93 meter
Z = 16711328
70 Z = 5093612
99
XDOT = 19515
266052 XDOT = 5948
253093
YDOT = -13127
575375 feet/sec YDOT = -4001
284974 meter/sec
ZDOT = -5576
058998 ZDOT = -1699
582783
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
29532067
00016717 00000-0 10270-3 0 9138
2 25544 51
6391 112
8932 0003617 135
6466 224
4977 15
54143900 35578
Satellite: ISS
Catalog Number: 25544
Epoch time: 18149
29532067 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 112
8932 deg
Eccentricity:
0003617
Arg of perigee: 135
6466 deg
Mean anomaly: 224
4977 deg
Mean motion: 15
54143900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 320
Coasting Arc #15 (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 = 2119343
38 A = 6781258
45 meter
Y = 4736843
38 meter E =
0012267
Z = -4378139
35 I = 51
99347
XDOT = -4436
765709 Wp = 117
65087
YDOT = 5188
843561 meter/sec RA = 107
14264 deg
ZDOT = 3468
131196 TA = 187
42564
MA = 187
44382
Ha = 222
124 n
mi
Hp = 213
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6953226
31 X = 2087484
15
Y = 15540824
73 feet Y = 4760365
78 meter
Z = -14363974
26 Z = -4367920
93
XDOT = -14556
317942 XDOT = -4511
305592
YDOT = 17023
764965 feet/sec YDOT = 5138
811350 meter/sec
ZDOT = 11378
383188 ZDOT = 3446
398295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 365550
20 X = 111419
70
Y = 17059422
02 feet Y = 5199711
83 meter
Z = -14318897
99 Z = -4364400
11
XDOT = -18905
613310 XDOT = -5762
430937
YDOT = 9868
181340 feet/sec YDOT = 3007
821672 meter/sec
ZDOT = 11280
431491 ZDOT = 3438
275518
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
25985576
00016717 00000-0 10270-3 0 9144
2 25544 51
6396 108
0850 0003711 134
2712 225
8746 15
54133178 35725
Satellite: ISS
Catalog Number: 25544
Epoch time: 18150
25985576 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 108
0850 deg
Eccentricity:
0003711
Arg of perigee: 134
2712 deg
Mean anomaly: 225
8746 deg
Mean motion: 15
54133178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 313
Coasting Arc #16 (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 = -1258232
17 A = 6785039
00 meter
Y = -5861915
83 meter E =
0015674
Z = 3159219
75 I = 52
01474
XDOT = 4678
910907 Wp = 103
92287
YDOT = -3639
641741 meter/sec RA = 102
18280 deg
ZDOT = -4873
350179 TA = 39
81584
MA = 39
70093
Ha = 222
052 n
mi
Hp = 213
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4128058
31 X = -1207935
08
Y = -19232007
33 feet Y = -5875705
47 meter
Z = 10364894
20 Z = 3153228
97
XDOT = 15350
757569 XDOT = 4742
935021
YDOT = -11941
081829 feet/sec YDOT = -3586
960264 meter/sec
ZDOT = -15988
681691 ZDOT = -4850
466442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3375381
38 X = 1028816
24
Y = -19392162
30 feet Y = -5910731
07 meter
Z = 10338899
61 Z = 3151296
60
XDOT = 17407
217789 XDOT = 5305
719982
YDOT = -5468
527787 feet/sec YDOT = -1666
807270 meter/sec
ZDOT = -15885
773774 ZDOT = -4841
983846
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
28868867
00016717 00000-0 10270-3 0 9152
2 25544 51
6393 102
9568 0003622 139
5513 220
5910 15
54154981 35886
Satellite: ISS
Catalog Number: 25544
Epoch time: 18151
28868867 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 102
9568 deg
Eccentricity:
0003622
Arg of perigee: 139
5513 deg
Mean anomaly: 220
5910 deg
Mean motion: 15
54154981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 332
Coasting Arc #17 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2018/152/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 460777
52 A = 6788114
76 meter
Y = 6568872
10 meter E =
0007803
Z = -1645482
54 I = 52
03188
XDOT = -4747
781141 Wp = 65
35201
YDOT = 1767
340408 meter/sec RA = 97
23261 deg
ZDOT = 5750
328732 TA = 276
73858
MA = 276
82737
Ha = 222
010 n
mi
Hp = 213
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1511737
26 X = 395281
28
Y = 21551417
66 feet Y = 6573658
86 meter
Z = -5398564
76 Z = -1643402
36
XDOT = -15576
709779 XDOT = -4795
123398
YDOT = 5798
360917 feet/sec YDOT = 1713
981915 meter/sec
ZDOT = 18865
907914 ZDOT = 5727
150774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6350020
55 X = -1935486
26
Y = 20652279
18 feet Y = 6294814
69 meter
Z = -5390181
64 Z = -1642927
36
XDOT = -15230
032431 XDOT = -4642
113885
YDOT = 192
975037 feet/sec YDOT = 58
818791 meter/sec
ZDOT = 18761
930557 ZDOT = 5718
636434
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 18152
25321783
00016717 00000-0 10270-3 0 9162
2 25544 51
6402 98
1488 0003708 142
3031 217
8382 15
54150466 36030
Satellite: ISS
Catalog Number: 25544
Epoch time: 18152
25321783 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 98
1488 deg
Eccentricity:
0003708
Arg of perigee: 142
3031 deg
Mean anomaly: 217
8382 deg
Mean motion: 15
54150466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 296
Coasting Arc #18 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2018/153/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 335475
44 A = 6789286
77 meter
Y = -6772796
47 meter E =
0015569
Z = -82931
62 I = 52
03954
XDOT = 4709
844039 Wp = 137
42406
YDOT = 299
123879 meter/sec RA = 92
28901 deg
ZDOT = -6047
404700 TA = 43
46466
MA = 43
34203
Ha = 221
991 n
mi
Hp = 213
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1100641
20 X = 411588
61
Y = -22220460
85 feet Y = -6768619
36 meter
Z = -272085
37 Z = -81118
07
XDOT = 15452
244222 XDOT = 4735
524308
YDOT = 981
377557 feet/sec YDOT = 351
937032 meter/sec
ZDOT = -19840
566602 ZDOT = -6024
463414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8711816
73 X = 2655361
74
Y = -20471184
68 feet Y = -6239617
09 meter
Z = -263000
04 Z = -80162
41
XDOT = 12792
263934 XDOT = 3899
082047
YDOT = 5668
254913 feet/sec YDOT = 1727
684097 meter/sec
ZDOT = -19737
932785 ZDOT = -6016
121913
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 18153
28204342
00016717 00000-0 10270-3 0 9178
2 25544 51
6409 93
0200 0003655 144
9309 215
2085 15
54142952 36190
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
28204342 = yrday
fracday
Element set: 917
Inclination: 51
6409 deg
RA of node: 93
0200 deg
Eccentricity:
0003655
Arg of perigee: 144
9309 deg
Mean anomaly: 215
2085 deg
Mean motion: 15
54142952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 292
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