[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 6th 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) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
037/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
040/08:25:00
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
5
042/08:58:45
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
6
042/12:24:48
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
043/19:08:00
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
6
048/05:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 1802)
---------------------------------------
Vector Time (GMT): 2018/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -487991
24 A = 6780144
11 meter
Y = -4868482
52 meter E =
0013334
Z = -4706055
49 I = 51
36308
XDOT = 6336
686377 Wp = 99
75758
YDOT = -3297
714427 meter/sec RA = 314
52449 deg
ZDOT = 2758
935659 TA = 197
68632
MA = 197
73279
Ha = 222
203 n
mi
Hp = 213
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1601021
13 X = -410655
12
Y = -15972711
66 feet Y = -4873507
45 meter
Z = -15439814
59 Z = -4708237
81
XDOT = 20789
653468 XDOT = 6359
690122
YDOT = -10819
273055 feet/sec YDOT = -3226
724460 meter/sec
ZDOT = 9051
626177 ZDOT = 2789
772655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10296094
34 X = 3138249
55
Y = -12304694
98 feet Y = -3750471
03 meter
Z = -15448740
52 Z = -4708776
11
XDOT = 21375
691808 XDOT = 6515
310863
YDOT = 6367
368761 feet/sec YDOT = 1940
773998 meter/sec
ZDOT = 9189
395354 ZDOT = 2800
927704
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 18036
51112795
00016717 00000-0 10270-3 0 9006
2 25544 51
6411 315
1495 0003173 67
2917 292
8571 15
54062005 18038
Satellite: ISS
Catalog Number: 25544
Epoch time: 18036
51112795 = yrday
fracday
Element set: 900
Inclination: 51
6411 deg
RA of node: 315
1495 deg
Eccentricity:
0003173
Arg of perigee: 67
2917 deg
Mean anomaly: 292
8571 deg
Mean motion: 15
54062005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1803
Checksum: 288
Coasting Arc #2 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4182632
18 A = 6778308
45 meter
Y = -1493949
85 meter E =
0016567
Z = -5135307
30 I = 51
34599
XDOT = 4078
764442 Wp = 78
10652
YDOT = -6305
487328 meter/sec RA = 312
01882 deg
ZDOT = -1488
456158 TA = 177
48156
MA = 177
47320
Ha = 222
135 n
mi
Hp = 213
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13722546
53 X = -4140671
33
Y = -4901410
26 feet Y = -1540488
58 meter
Z = -16848121
07 Z = -5155522
77
XDOT = 13381
773105 XDOT = 4156
200994
YDOT = -20687
294383 feet/sec YDOT = -6259
442895 meter/sec
ZDOT = -4883
386345 ZDOT = -1468
454800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6771340
42 X = 2063904
56
Y = 12784742
08 feet Y = 3896789
39 meter
Z = -16937845
44 Z = -5162655
29
XDOT = -22910
130135 XDOT = -6983
007665
YDOT = 5786
888415 feet/sec YDOT = 1763
843589 meter/sec
ZDOT = -4793
361224 ZDOT = -1461
016501
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 18037
02556628
00016717 00000-0 10270-3 0 9011
2 25544 51
6417 312
5827 0002805 76
2873 283
8592 15
54045092 18115
Satellite: ISS
Catalog Number: 25544
Epoch time: 18037
02556628 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 312
5827 deg
Eccentricity:
0002805
Arg of perigee: 76
2873 deg
Mean anomaly: 283
8592 deg
Mean motion: 15
54045092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 310
Coasting Arc #3 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3091315
68 A = 6777486
04 meter
Y = 2915058
92 meter E =
0005554
Z = 5275654
50 I = 51
32282
XDOT = -4870
288304 Wp = 74
10696
YDOT = 5914
732047 meter/sec RA = 306
99833 deg
ZDOT = -412
535478 TA = 19
85290
MA = 19
83130
Ha = 221
969 n
mi
Hp = 213
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10142111
80 X = 3032862
94
Y = 9563841
59 feet Y = 2949301
53 meter
Z = 17308577
76 Z = 5290528
74
XDOT = -15978
636168 XDOT = -4934
062616
YDOT = 19405
288869 feet/sec YDOT = 5859
912540 meter/sec
ZDOT = -1353
462854 ZDOT = -436
348483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1220988
02 X = -372157
15
Y = -13804312
99 feet Y = -4207554
60 meter
Z = 17374305
54 Z = 5295688
33
XDOT = 23797
859503 XDOT = 7253
587577
YDOT = -3950
604625 feet/sec YDOT = -1204
144290 meter/sec
ZDOT = -1460
375148 ZDOT = -445
122345
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 18038
05444151
00016717 00000-0 10270-3 0 9023
2 25544 51
6420 307
4541 0002880 78
0648 282
0828 15
54101809 18277
Satellite: ISS
Catalog Number: 25544
Epoch time: 18038
05444151 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 307
4541 deg
Eccentricity:
0002880
Arg of perigee: 78
0648 deg
Mean anomaly: 282
0828 deg
Mean motion: 15
54101809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 294
Coasting Arc #4 (Orbit 1841)
---------------------------------------
Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1968091
11 A = 6779240
12 meter
Y = -4263263
70 meter E =
0014923
Z = -4903481
33 I = 51
30821
XDOT = 5292
222313 Wp = 101
48107
YDOT = -5047
462297 meter/sec RA = 301
97896 deg
ZDOT = 2267
295839 TA = 190
79860
MA = 190
83067
Ha = 222
165 n
mi
Hp = 213
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6456991
82 X = -1896453
66
Y = -13987085
62 feet Y = -4284871
84 meter
Z = -16087537
18 Z = -4912867
38
XDOT = 17362
934098 XDOT = 5337
257894
YDOT = -16559
915674 feet/sec YDOT = -4988
029157 meter/sec
ZDOT = 7438
634642 ZDOT = 2293
112815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4207117
03 X = -1282329
27
Y = 14775233
64 feet Y = 4503491
21 meter
Z = -16128632
84 Z = -4916007
29
XDOT = -22837
719688 XDOT = -6960
936961
YDOT = 1732
842966 feet/sec YDOT = 528
170536 meter/sec
ZDOT = 7554
316395 ZDOT = 2302
555637
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 18039
01901250
00016717 00000-0 10270-3 0 9039
2 25544 51
6407 302
6472 0003038 81
5259 278
6238 15
54084280 18421
Satellite: ISS
Catalog Number: 25544
Epoch time: 18039
01901250 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 302
6472 deg
Eccentricity:
0003038
Arg of perigee: 81
5259 deg
Mean anomaly: 278
6238 deg
Mean motion: 15
54084280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1842
Checksum: 294
Coasting Arc #5 (Orbit 1857)
---------------------------------------
Vector Time (GMT): 2018/040/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 848171
17 A = 6782589
54 meter
Y = 5402732
82 meter E =
0013750
Z = 4001953
75 I = 51
30366
XDOT = -5426
724332 Wp = 79
41408
YDOT = 3758
812830 meter/sec RA = 296
96423 deg
ZDOT = -3910
397844 TA = 51
41645
MA = 51
29336
Ha = 222
070 n
mi
Hp = 213
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2782713
82 X = 768254
22
Y = 17725501
36 feet Y = 5411770
89 meter
Z = 13129769
52 Z = 4005879
59
XDOT = -17804
213688 XDOT = -5449
358694
YDOT = 12332
063089 feet/sec YDOT = 3698
000835 meter/sec
ZDOT = -12829
389251 ZDOT = -3936
813662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9148445
50 X = 2788446
19
Y = -15420958
12 feet Y = -4700308
03 meter
Z = 13146396
39 Z = 4007021
62
XDOT = 20396
782000 XDOT = 6216
939154
YDOT = 1023
574459 feet/sec YDOT = 311
985495 meter/sec
ZDOT = -12947
525620 ZDOT = -3946
405809
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 18040
04788329
00016717 00000-0 10270-3 0 9045
2 25544 51
6414 297
5184 0002909 83
2892 276
8592 15
54102252 18589
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
04788329 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 297
5184 deg
Eccentricity:
0002909
Arg of perigee: 83
2892 deg
Mean anomaly: 276
8592 deg
Mean motion: 15
54102252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1858
Checksum: 328
Coasting Arc #6 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4453260
36 A = 6778277
06 meter
Y = -185536
49 meter E =
0016800
Z = -5121848
97 I = 51
28237
XDOT = 2054
715795 Wp = 78
48842
YDOT = -7215
108104 meter/sec RA = 295
28157 deg
ZDOT = -1526
115274 TA = 176
71430
MA = 176
70325
Ha = 222
211 n
mi
Hp = 213
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14610434
25 X = -4425975
80
Y = -608715
52 feet Y = -235183
44 meter
Z = -16803966
42 Z = -5143414
76
XDOT = 6741
193553 XDOT = 2142
657327
YDOT = -23671
614513 feet/sec YDOT = -7191
639179 meter/sec
ZDOT = -5006
939874 ZDOT = -1515
920599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1931117
50 X = 588604
61
Y = -14383066
51 feet Y = -4383958
67 meter
Z = -16899905
15 Z = -5151091
09
XDOT = 21905
976019 XDOT = 6676
941491
YDOT = 8765
879075 feet/sec YDOT = 2671
839942 meter/sec
ZDOT = -4960
452200 ZDOT = -1511
945830
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 18040
36940670
00016717 00000-0 10270-3 0 9050
2 25544 51
6398 295
9167 0003116 79
5652 280
5851 15
54073332 18638
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
36940670 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 295
9167 deg
Eccentricity:
0003116
Arg of perigee: 79
5652 deg
Mean anomaly: 280
5851 deg
Mean motion: 15
54073332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1863
Checksum: 322
Coasting Arc #7 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3819818
76 A = 6777508
87 meter
Y = 1866549
00 meter E =
0005744
Z = 5273436
68 I = 51
26689
XDOT = -2935
669470 Wp = 76
70255
YDOT = 7079
278112 meter/sec RA = 290
25796 deg
ZDOT = -377
630049 TA = 16
92422
MA = 16
90507
Ha = 222
057 n
mi
Hp = 213
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12532213
78 X = 3773047
47
Y = 6123848
42 feet Y = 1909003
39 meter
Z = 17301301
43 Z = 5291878
09
XDOT = -9631
461515 XDOT = -3012
779393
YDOT = 23225
978058 feet/sec YDOT = 7046
018289 meter/sec
ZDOT = -1238
943731 ZDOT = -392
077654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7029091
08 X = -2142466
96
Y = 11929515
39 feet Y = 3636116
29 meter
Z = 17383080
11 Z = 5298362
82
XDOT = -21578
552242 XDOT = -6577
142723
YDOT = -10806
052173 feet/sec YDOT = -3293
684702 meter/sec
ZDOT = -1304
322824 ZDOT = -397
557597
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 18041
39827341
00016717 00000-0 10270-3 0 9064
2 25544 51
6398 290
7890 0003127 80
8130 279
3376 15
54089565 18792
Satellite: ISS
Catalog Number: 25544
Epoch time: 18041
39827341 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 290
7890 deg
Eccentricity:
0003127
Arg of perigee: 80
8130 deg
Mean anomaly: 279
3376 deg
Mean motion: 15
54089565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 340
Coasting Arc #8 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3132187
50 A = 6779195
25 meter
Y = -3489522
83 meter E =
0015187
Z = -4909958
74 I = 51
26153
XDOT = 3598
318338 Wp = 102
01377
YDOT = -6376
540825 meter/sec RA = 285
23390 deg
ZDOT = 2239
162417 TA = 189
99134
MA = 190
02157
Ha = 222
217 n
mi
Hp = 213
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10276205
70 X = -3069084
40
Y = -11448565
72 feet Y = -3524196
34 meter
Z = -16108788
51 Z = -4925020
20
XDOT = 11805
506357 XDOT = 3658
478653
YDOT = -20920
409530 feet/sec YDOT = -6335
965551 meter/sec
ZDOT = 7346
333388 ZDOT = 2256
787665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12010724
17 X = 3660868
73
Y = -9500828
40 feet Y = -2895852
50 meter
Z = -16175286
47 Z = -4930227
32
XDOT = 19523
136315 XDOT = 5950
651949
YDOT = 12053
822985 feet/sec YDOT = 3674
005246 meter/sec
ZDOT = 7425
733124 ZDOT = 2263
363456
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 18042
36283507
00016717 00000-0 10270-3 0 9073
2 25544 51
6394 285
9811 0003150 85
1273 275
0239 15
54079644 18944
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
36283507 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 285
9811 deg
Eccentricity:
0003150
Arg of perigee: 85
1273 deg
Mean anomaly: 275
0239 deg
Mean motion: 15
54079644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 321
Coasting Arc #9 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2018/042/08:58:45
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4450892
90 A = 6779819
58 meter
Y = -1959564
35 meter E =
0010395
Z = 4716881
02 I = 51
26422
XDOT = 295
494554 Wp = 109
00108
YDOT = 7178
224669 meter/sec RA = 285
15569 deg
ZDOT = 2695
056540 TA = 314
19502
MA = 314
28039
Ha = 222
010 n
mi
Hp = 213
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14602666
99 X = 4449562
81
Y = -6429016
88 feet Y = -1909798
78 meter
Z = 15475331
43 Z = 4738498
29
XDOT = 969
470321 XDOT = 202
112837
YDOT = 23550
605869 feet/sec YDOT = 7181
007002 meter/sec
ZDOT = 8842
049016 ZDOT = 2696
265013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7714108
00 X = 2351260
12
Y = 13858814
26 feet Y = 4224166
59 meter
Z = 15571828
06 Z = 4746293
19
XDOT = -22361
521510 XDOT = -6815
791756
YDOT = 2477
032652 feet/sec YDOT = 754
999552 meter/sec
ZDOT = 8846
341262 ZDOT = 2696
364817
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 18042
42713808
00016717 00000-0 10270-3 0 9083
2 25544 51
6398 285
6612 0003051 87
0168 273
1334 15
54107255 18954
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
42713808 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 285
6612 deg
Eccentricity:
0003051
Arg of perigee: 87
0168 deg
Mean anomaly: 273
1334 deg
Mean motion: 15
54107255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 311
Coasting Arc #10 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2018/042/12:24:48
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1014887
88 A = 6785395
03 meter
Y = 5955953
99 meter E =
0016108
Z = 3073306
74 I = 51
28287
XDOT = -4889
719124 Wp = 93
24589
YDOT = 3355
789100 meter/sec RA = 284
39484 deg
ZDOT = -4867
448718 TA = 51
22722
MA = 51
08342
Ha = 222
163 n
mi
Hp = 213
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3329684
64 X = 933283
16
Y = 19540531
46 feet Y = 5966846
93 meter
Z = 10083027
35 Z = 3078038
32
XDOT = -16042
385578 XDOT = -4903
238030
YDOT = 11009
806757 feet/sec YDOT = 3301
033243 meter/sec
ZDOT = -15969
319940 ZDOT = -4891
233686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7954541
79 X = -2424544
34
Y = 18144903
63 feet Y = 5530566
63 meter
Z = 10103185
02 Z = 3079450
79
XDOT = -18039
563370 XDOT = -5498
458915
YDOT = 1081
369416 feet/sec YDOT = 329
601398 meter/sec
ZDOT = -16075
673524 ZDOT = -4899
865290
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 18042
55574623
00016717 00000-0 10270-3 0 9098
2 25544 51
6413 285
0211 0003138 84
1744 275
9766 15
54098793 18972
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
55574623 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 285
0211 deg
Eccentricity:
0003138
Arg of perigee: 84
1744 deg
Mean anomaly: 275
9766 deg
Mean motion: 15
54098793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 334
Coasting Arc #11 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2018/043/12:24:48
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -188447
16 A = 6788384
49 meter
Y = -6597626
78 meter E =
0010230
Z = -1575440
87 I = 51
28564
XDOT = 4888
420354 Wp = 50
31961
YDOT = -1496
171260 meter/sec RA = 279
39411 deg
ZDOT = 5712
154104 TA = 292
36995
MA = 292
47833
Ha = 222
131 n
mi
Hp = 213
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -618264
95 X = -107004
21
Y = -21645757
16 feet Y = -6599278
79 meter
Z = -5168769
27 Z = -1576158
32
XDOT = 16038
124521 XDOT = 4877
041624
YDOT = -4908
698358 feet/sec YDOT = -1441
569089 meter/sec
ZDOT = 18740
663070 ZDOT = 5735
872214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11029562
46 X = 3361810
64
Y = -18634562
41 feet Y = -5679814
62 meter
Z = -5170983
11 Z = -1576115
65
XDOT = 14725
039402 XDOT = 4488
192010
YDOT = 3514
201595 feet/sec YDOT = 1071
128646 meter/sec
ZDOT = 18846
438267 ZDOT = 5744
394384
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 18043
52030418
00016717 00000-0 10270-3 0 9107
2 25544 51
6413 280
2130 0002957 87
0947 273
0544 15
54089349 19122
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
52030418 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 280
2130 deg
Eccentricity:
0002957
Arg of perigee: 87
0947 deg
Mean anomaly: 273
0544 deg
Mean motion: 15
54089349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 293
Coasting Arc #12 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3606582
02 A = 6779004
31 meter
Y = 2893293
44 meter E =
0008825
Z = 4951115
29 I = 51
25153
XDOT = -2656
409069 Wp = 71
12994
YDOT = 6890
127633 meter/sec RA = 277
98355 deg
ZDOT = -2085
503861 TA = 39
29696
MA = 39
23295
Ha = 222
153 n
mi
Hp = 213
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11832618
16 X = 3549911
03
Y = 9492432
54 feet Y = 2933307
97 meter
Z = 16243816
58 Z = 4968496
70
XDOT = -8715
252852 XDOT = -2723
128869
YDOT = 22605
405620 feet/sec YDOT = 6860
048740 meter/sec
ZDOT = -6842
204270 ZDOT = -2098
569690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13077040
74 X = 3985882
02
Y = -7523500
12 feet Y = -2293162
84 meter
Z = 16320743
13 Z = 4974562
51
XDOT = 17422
154930 XDOT = 5310
272823
YDOT = 15269
786029 feet/sec YDOT = 4654
230782 meter/sec
ZDOT = -6901
369282 ZDOT = -2103
537357
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 18043
84182506
00016717 00000-0 10270-3 0 9119
2 25544 51
6403 278
6050 0003232 99
3118 260
8400 15
54062409 19174
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
84182506 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 278
6050 deg
Eccentricity:
0003232
Arg of perigee: 99
3118 deg
Mean anomaly: 260
8400 deg
Mean motion: 15
54062409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 287
Coasting Arc #13 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3087033
56 A = 6782171
85 meter
Y = -4418735
50 meter E =
0010726
Z = -4127299
54 I = 51
25855
XDOT = 3308
780878 Wp = 107
14738
YDOT = -5804
142210 meter/sec RA = 272
96543 deg
ZDOT = 3744
152912 TA = 201
64336
MA = 201
68873
Ha = 222
178 n
mi
Hp = 213
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10128062
86 X = -3017344
89
Y = -14497163
72 feet Y = -4452867
33 meter
Z = -13541008
98 Z = -4142125
48
XDOT = 10855
580307 XDOT = 3355
251788
YDOT = -19042
461319 feet/sec YDOT = -5766
881178 meter/sec
ZDOT = 12283
966247 ZDOT = 3760
338500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17065458
76 X = -5201551
83
Y = 4443155
32 feet Y = 1354273
74 meter
Z = -13606352
40 Z = -4147216
21
XDOT = -13853
572029 XDOT = -4222
568754
YDOT = -15418
691152 feet/sec YDOT = -4699
617063 meter/sec
ZDOT = 12356
841493 ZDOT = 3766
365287
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 18044
80637867
00016717 00000-0 10270-3 0 9122
2 25544 51
6400 273
7979 0003116 101
9019 258
2483 15
54086552 19322
Satellite: ISS
Catalog Number: 25544
Epoch time: 18044
80637867 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 273
7979 deg
Eccentricity:
0003116
Arg of perigee: 101
9019 deg
Mean anomaly: 258
2483 deg
Mean motion: 15
54086552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 318
Coasting Arc #14 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2483097
05 A = 6786009
81 meter
Y = 5629633
99 meter E =
0016520
Z = 2843764
77 I = 51
26983
XDOT = -3894
066270 Wp = 100
74454
YDOT = 4275
802544 meter/sec RA = 267
95620 deg
ZDOT = -5042
392162 TA = 46
72144
MA = 46
58373
Ha = 222
172 n
mi
Hp = 213
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8146643
86 X = 2406147
26
Y = 18469927
79 feet Y = 5656971
58 meter
Z = 9329936
92 Z = 2855639
29
XDOT = -12775
807974 XDOT = -3917
097390
YDOT = 14028
223571 feet/sec YDOT = 4232
127380 meter/sec
ZDOT = -16543
281373 ZDOT = -5061
363859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20099921
61 X = 6126456
11
Y = -1589091
51 feet Y = -484355
09 meter
Z = 9381988
11 Z = 2859629
98
XDOT = 8988
529760 XDOT = 2739
703871
YDOT = 15096
326271 feet/sec YDOT = 4601
360248 meter/sec
ZDOT = -16628
325543 ZDOT = -5068
313626
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 18045
83523553
00016717 00000-0 10270-3 0 9133
2 25544 51
6393 268
6693 0003214 107
4686 252
6818 15
54077976 19486
Satellite: ISS
Catalog Number: 25544
Epoch time: 18045
83523553 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 268
6693 deg
Eccentricity:
0003214
Arg of perigee: 107
4686 deg
Mean anomaly: 252
6818 deg
Mean motion: 15
54077976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 343
Coasting Arc #15 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2018/046/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1844586
12 A = 6788717
76 meter
Y = -6398931
83 meter E =
0010355
Z = -1304792
05 I = 51
28227
XDOT = 4382
092328 Wp = 54
02712
YDOT = -2437
619418 meter/sec RA = 262
95640 deg
ZDOT = 5797
890789 TA = 291
70651
MA = 291
81673
Ha = 222
158 n
mi
Hp = 213
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6051791
72 X = -1766556
60
Y = -20993870
85 feet Y = -6419123
06 meter
Z = -4280813
82 Z = -1313562
22
XDOT = 14376
943332 XDOT = 4380
862385
YDOT = -7997
439036 feet/sec YDOT = -2388
622324 meter/sec
ZDOT = 19021
951406 ZDOT = 5819
174113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21826194
54 X = -6652624
10
Y = -809926
40 feet Y = -246865
57 meter
Z = -4318959
85 Z = -1316418
96
XDOT = -3222
344373 XDOT = -982
170565
YDOT = -14440
357427 feet/sec YDOT = -4401
420944 meter/sec
ZDOT = 19117
019246 ZDOT = 5826
867466
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 18046
79978509
00016717 00000-0 10270-3 0 9145
2 25544 51
6404 263
8615 0003101 106
9063 253
2429 15
54084225 19635
Satellite: ISS
Catalog Number: 25544
Epoch time: 18046
79978509 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 263
8615 deg
Eccentricity:
0003101
Arg of perigee: 106
9063 deg
Mean anomaly: 253
2429 deg
Mean motion: 15
54084225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 314
Coasting Arc #16 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2018/047/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1084200
16 A = 6789339
10 meter
Y = 6683301
96 meter E =
0014154
Z = -416167
08 I = 51
28884
XDOT = -4800
463508 Wp = 132
23038
YDOT = 415
956882 meter/sec RA = 257
96173 deg
ZDOT = -5966
090264 TA = 52
27905
MA = 52
15083
Ha = 222
141 n
mi
Hp = 213
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3557087
13 X = 1011406
56
Y = 21926843
71 feet Y = 6695019
18 meter
Z = -1365377
57 Z = -411077
91
XDOT = -15749
552193 XDOT = -4775
778641
YDOT = 1364
687933 feet/sec YDOT = 362
412314 meter/sec
ZDOT = -19573
786956 ZDOT = -5989
348775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22003410
87 X = 6706639
63
Y = 3057475
54 feet Y = 931918
55 meter
Z = -1343634
29 Z = -409539
73
XDOT = -3080
014492 XDOT = -938
788417
YDOT = 13723
091842 feet/sec YDOT = 4182
798394 meter/sec
ZDOT = -19677
367597 ZDOT = -5997
661644
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 18047
82863541
00016717 00000-0 10270-3 0 9150
2 25544 51
6397 258
7326 0003166 111
7038 248
4452 15
54100501 19790
Satellite: ISS
Catalog Number: 25544
Epoch time: 18047
82863541 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 258
7326 deg
Eccentricity:
0003166
Arg of perigee: 111
7038 deg
Mean anomaly: 248
4452 deg
Mean motion: 15
54100501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 314
Coasting Arc #17 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2018/048/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4188919
86 A = 6782590
83 meter
Y = 3551243
38 meter E =
0013713
Z = 3969862
21 I = 51
26789
XDOT = -1646
710666 Wp = 83
86108
YDOT = 6370
310326 meter/sec RA = 255
72738 deg
ZDOT = -3947
768555 TA = 47
46123
MA = 47
34553
Ha = 222
010 n
mi
Hp = 213
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13743175
39 X = 4129614
51
Y = 11651060
96 feet Y = 3597755
53 meter
Z = 13024482
31 Z = 3990065
70
XDOT = -5402
594049 XDOT = -1698
647071
YDOT = 20899
968260 feet/sec YDOT = 6351
604922 meter/sec
ZDOT = -12951
996573 ZDOT = -3955
894245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17595593
10 X = -5363136
78
Y = 3560777
51 feet Y = 1085324
98 meter
Z = 13113931
44 Z = 3997126
30
XDOT = -12908
954227 XDOT = -3934
649249
YDOT = -15793
908202 feet/sec YDOT = -4813
983220 meter/sec
ZDOT = -12989
022946 ZDOT = -3959
054194
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 18048
27875693
00016717 00000-0 10270-3 0 9162
2 25544 51
6380 256
4916 0003017 101
6505 258
4987 15
54112957 19864
Satellite: ISS
Catalog Number: 25544
Epoch time: 18048
27875693 = yrday
fracday
Element set: 916
Inclination: 51
6380 deg
RA of node: 256
4916 deg
Eccentricity:
0003017
Arg of perigee: 101
6505 deg
Mean anomaly: 258
4987 deg
Mean motion: 15
54112957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 340
Coasting Arc #18 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2018/049/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3957920
91 A = 6786324
93 meter
Y = -4821930
53 meter E =
0007163
Z = -2674921
89 I = 51
28900
XDOT = 2629
393998 Wp = 74
77283
YDOT = -5014
718459 meter/sec RA = 250
72042 deg
ZDOT = 5162
642442 TA = 254
89298
MA = 254
97224
Ha = 222
086 n
mi
Hp = 213
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12985304
83 X = -3890713
51
Y = -15819982
07 feet Y = -4865815
21 meter
Z = -8775990
46 Z = -2693984
01
XDOT = 8626
620727 XDOT = 2660
197609
YDOT = -16452
488382 feet/sec YDOT = -4985
142015 meter/sec
ZDOT = 16937
803286 ZDOT = 5175
490195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20416116
53 X = 6222832
32
Y = -766133
27 feet Y = -233517
42 meter
Z = -8860203
63 Z = -2700590
07
XDOT = 7928
203444 XDOT = 2416
516410
YDOT = 15226
331211 feet/sec YDOT = 4640
985753 meter/sec
ZDOT = 16995
653982 ZDOT = 5180
275334
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 18049
24330178
00016717 00000-0 10270-3 0 9175
2 25544 51
6377 251
6837 0002976 106
2774 253
8706 15
54097164 20010
Satellite: ISS
Catalog Number: 25544
Epoch time: 18049
24330178 = yrday
fracday
Element set: 917
Inclination: 51
6377 deg
RA of node: 251
6837 deg
Eccentricity:
0002976
Arg of perigee: 106
2774 deg
Mean anomaly: 253
8706 deg
Mean motion: 15
54097164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 319
Coasting Arc #19 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2018/050/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3505630
89 A = 6788901
75 meter
Y = 5707244
35 meter E =
0016518
Z = 1060216
65 I = 51
31091
XDOT = -3645
932189 Wp = 120
99487
YDOT = 3340
056135 meter/sec RA = 245
72270 deg
ZDOT = -5864
832243 TA = 47
45063
MA = 47
31130
Ha = 222
056 n
mi
Hp = 213
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11501413
69 X = 3436400
50
Y = 18724554
97 feet Y = 5746059
75 meter
Z = 3478401
09 Z = 1077076
78
XDOT = -11961
719781 XDOT = -3654
522812
YDOT = 10958
189418 feet/sec YDOT = 3299
236171 meter/sec
ZDOT = -19241
575602 ZDOT = -5882
563851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21891859
08 X = -6672638
65
Y = -1765076
02 feet Y = -537995
17 meter
Z = 3552711
94 Z = 1082866
60
XDOT = -2003
778223 XDOT = -610
751602
YDOT = -14421
994560 feet/sec YDOT = -4395
823942 meter/sec
ZDOT = -19320
939459 ZDOT = -5889
022347
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 18050
27214663
00016717 00000-0 10270-3 0 9181
2 25544 51
6391 246
5543 0002961 109
7458 250
4014 15
54105881 20172
Satellite: ISS
Catalog Number: 25544
Epoch time: 18050
27214663 = yrday
fracday
Element set: 918
Inclination: 51
6391 deg
RA of node: 246
5543 deg
Eccentricity:
0002961
Arg of perigee: 109
7458 deg
Mean anomaly: 250
4014 deg
Mean motion: 15
54105881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 297
Coasting Arc #20 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2018/051/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2859003
69 A = 6789238
31 meter
Y = -6119942
96 meter E =
0014821
Z = 622414
11 I = 51
32619
XDOT = 4595
927059 Wp = 61
60332
YDOT = -1532
143858 meter/sec RA = 240
73030 deg
ZDOT = 5944
836860 TA = 305
14607
MA = 305
28485
Ha = 222
059 n
mi
Hp = 213
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9379933
36 X = -2793379
67
Y = -20078553
03 feet Y = -6151547
32 meter
Z = 2042041
05 Z = 608686
24
XDOT = 15078
500851 XDOT = 4583
841789
YDOT = -5026
718694 feet/sec YDOT = -1480
816017 meter/sec
ZDOT = 19504
057939 ZDOT = 5967
132813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21826110
06 X = 6652598
35
Y = 3872352
23 feet Y = 1180292
96 meter
Z = 1981711
67 Z = 604025
72
XDOT = -4210
792328 XDOT = -1283
449502
YDOT = 13526
329097 feet/sec YDOT = 4122
825109 meter/sec
ZDOT = 19603
506593 ZDOT = 5975
148810
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 18051
30098811
00016717 00000-0 10270-3 0 9192
2 25544 51
6389 241
4256 0002954 111
2309 248
9159 15
54107439 20330
Satellite: ISS
Catalog Number: 25544
Epoch time: 18051
30098811 = yrday
fracday
Element set: 919
Inclination: 51
6389 deg
RA of node: 241
4256 deg
Eccentricity:
0002954
Arg of perigee: 111
2309 deg
Mean anomaly: 248
9159 deg
Mean motion: 15
54107439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 306
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