[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 16th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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
260/08:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
1
261/05:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 215
9
270/16:51:48
829 -0
9 1
4 1
4
N/A -0
9 0
0 220
6
000/00:03:37
658 -0
6 0
0 215
8
Coasting Arc #1 (Orbit 3578)
---------------------------------------
Vector Time (GMT): 2017/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924173
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 642412
21 A = 6783368
52 meter
Y = -5670600
60 meter E =
0001663
Z = -3668574
29 I = 51
34574
XDOT = 5967
516364 Wp = 102
62243
YDOT = -2117
117555 meter/sec RA = 307
40507 deg
ZDOT = 4318
765888 TA = 213
55427
MA = 213
56480
Ha = 219
461 n
mi
Hp = 215
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2107651
61 X = 723594
68
Y = -18604332
68 feet Y = -5662963
01 meter
Z = -12036004
90 Z = -3665256
15
XDOT = 19578
465761 XDOT = 5969
768673
YDOT = -6945
923737 feet/sec YDOT = -2050
371865 meter/sec
ZDOT = 14169
179424 ZDOT = 4347
759687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4191205
80 X = -1277479
53
Y = 18258502
63 feet Y = 5565191
60 meter
Z = -12020385
99 Z = -3663813
65
XDOT = -18791
887923 XDOT = -5727
767439
YDOT = 5096
438369 feet/sec YDOT = 1553
394415 meter/sec
ZDOT = 14297
831636 ZDOT = 4357
979083
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 17258
50778113
00016717 00000-0 10270-3 0 9002
2 25544 51
6407 308
0750 0003906 278
4055 81
6655 15
54221129 35794
Satellite: ISS
Catalog Number: 25544
Epoch time: 17258
50778113 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 308
0750 deg
Eccentricity:
0003906
Arg of perigee: 278
4055 deg
Mean anomaly: 81
6655 deg
Mean motion: 15
54221129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3579
Checksum: 310
Coasting Arc #2 (Orbit 3594)
---------------------------------------
Vector Time (GMT): 2017/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924173
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1792914
97 A = 6786952
80 meter
Y = 6149990
09 meter E =
0009810
Z = 2227420
81 I = 51
33859
XDOT = -5399
657081 Wp = 110
55480
YDOT = 398
717613 meter/sec RA = 302
40482 deg
ZDOT = -5431
146797 TA = 44
57311
MA = 44
49426
Ha = 219
470 n
mi
Hp = 215
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5882266
96 X = -1872372
18
Y = 20177132
83 feet Y = 6129496
39 meter
Z = 7307811
05 Z = 2218517
97
XDOT = -17715
410372 XDOT = -5377
332671
YDOT = 1308
128652 feet/sec YDOT = 338
459362 meter/sec
ZDOT = -17818
723088 ZDOT = -5457
322280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7748002
80 X = 2361591
25
Y = -19551854
07 feet Y = -5959405
12 meter
Z = 7267414
33 Z = 2215107
89
XDOT = 16218
227183 XDOT = 4943
315645
YDOT = -259
035828 feet/sec YDOT = -78
954120 meter/sec
ZDOT = -17934
618446 ZDOT = -5466
471702
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 17259
53656802
00016717 00000-0 10270-3 0 9017
2 25544 51
6405 302
9462 0004087 283
8876 76
1822 15
54230696 35959
Satellite: ISS
Catalog Number: 25544
Epoch time: 17259
53656802 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 302
9462 deg
Eccentricity:
0004087
Arg of perigee: 283
8876 deg
Mean anomaly: 76
1822 deg
Mean motion: 15
54230696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3595
Checksum: 330
Coasting Arc #3 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2017/260/08:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 340526
66 A = 6784926
55 meter
Y = -5998908
71 meter E =
0002042
Z = -3149457
45 I = 51
31813
XDOT = 5543
545472 Wp = 8
56993
YDOT = -2210
078615 meter/sec RA = 298
06202 deg
ZDOT = 4811
400679 TA = 314
93774
MA = 314
95430
Ha = 219
465 n
mi
Hp = 216
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1117213
46 X = 422881
16
Y = -19681459
01 feet Y = -5994640
54 meter
Z = -10332865
65 Z = -3147602
68
XDOT = 18187
485144 XDOT = 5544
475895
YDOT = -7250
914092 feet/sec YDOT = -2148
081242 meter/sec
ZDOT = 15785
435300 ZDOT = 4838
331780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16362597
96 X = -4987319
86
Y = 11002854
36 feet Y = 3353670
01 meter
Z = -10323695
61 Z = -3146662
42
XDOT = -15934
063499 XDOT = -4856
702555
YDOT = -8780
048183 feet/sec YDOT = -2676
158686 meter/sec
ZDOT = 15904
962728 ZDOT = 4847
832639
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 17260
37245434
00016717 00000-0 10270-3 0 9027
2 25544 51
6417 298
7778 0004222 283
6843 76
3840 15
54198094 36089
Satellite: ISS
Catalog Number: 25544
Epoch time: 17260
37245434 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 298
7778 deg
Eccentricity:
0004222
Arg of perigee: 283
6843 deg
Mean anomaly: 76
3840 deg
Mean motion: 15
54198094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 330
Coasting Arc #4 (Orbit 3621)
---------------------------------------
Vector Time (GMT): 2017/261/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1667397
95 A = 6781022
59 meter
Y = 4908450
38 meter E =
0006713
Z = 4369341
16 I = 51
29046
XDOT = -5022
714133 Wp = 51
25881
YDOT = 4713
410769 meter/sec RA = 293
72971 deg
ZDOT = -3370
599193 TA = 73
06092
MA = 72
98734
Ha = 219
601 n
mi
Hp = 215
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5470465
73 X = 1591162
44
Y = 16103839
83 feet Y = 4926670
60 meter
Z = 14335108
78 Z = 4377255
09
XDOT = -16478
720910 XDOT = -5058
674827
YDOT = 15463
946091 feet/sec YDOT = 4657
041901 meter/sec
ZDOT = -11058
396301 ZDOT = -3395
085711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16816499
60 X = 5125669
08
Y = -2341382
29 feet Y = -713653
32 meter
Z = 14369351
64 Z = 4379778
38
XDOT = 12032
337027 XDOT = 3667
456326
YDOT = 17730
040996 feet/sec YDOT = 5404
116496 meter/sec
ZDOT = -11167
495352 ZDOT = -3403
852583
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 17261
27263751
00016717 00000-0 10270-3 0 9030
2 25544 51
6399 294
2875 0003851 286
1776 73
8952 15
54186729 36221
Satellite: ISS
Catalog Number: 25544
Epoch time: 17261
27263751 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 294
2875 deg
Eccentricity:
0003851
Arg of perigee: 286
1776 deg
Mean anomaly: 73
8952 deg
Mean motion: 15
54186729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3622
Checksum: 345
Coasting Arc #5 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2017/262/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -667022
65 A = 6784832
44 meter
Y = -5958144
52 meter E =
0002443
Z = -3174300
09 I = 51
29080
XDOT = 5108
966980 Wp = 16
70304
YDOT = -3121
041569 meter/sec RA = 288
71964 deg
ZDOT = 4787
838503 TA = 306
45255
MA = 306
47506
Ha = 219
647 n
mi
Hp = 215
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2188394
52 X = -584928
37
Y = -19547718
25 feet Y = -5965145
02 meter
Z = -10414370
39 Z = -3177340
11
XDOT = 16761
702691 XDOT = 5120
230683
YDOT = -10239
637693 feet/sec YDOT = -3063
846014 meter/sec
ZDOT = 15708
131573 ZDOT = 4812
683967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19629416
78 X = -5983046
23
Y = -1152100
14 feet Y = -351160
12 meter
Z = -10426894
66 Z = -3178117
49
XDOT = -7417
169693 XDOT = -2260
753323
YDOT = -16694
502703 feet/sec YDOT = -5088
484424 meter/sec
ZDOT = 15818
556282 ZDOT = 4821
495955
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 17262
23711291
00016717 00000-0 10270-3 0 9045
2 25544 51
6396 289
4795 0004016 291
0057 69
0666 15
54201373 36374
Satellite: ISS
Catalog Number: 25544
Epoch time: 17262
23711291 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 289
4795 deg
Eccentricity:
0004016
Arg of perigee: 291
0057 deg
Mean anomaly: 69
0666 deg
Mean motion: 15
54201373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 313
Coasting Arc #6 (Orbit 3652)
---------------------------------------
Vector Time (GMT): 2017/263/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -273820
10 A = 6787964
73 meter
Y = 6582129
07 meter E =
0009962
Z = 1615898
10 I = 51
29210
XDOT = -4991
691250 Wp = 118
11808
YDOT = 1196
451688 meter/sec RA = 283
71841 deg
ZDOT = -5697
132465 TA = 44
10687
MA = 44
02746
Ha = 219
702 n
mi
Hp = 215
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -898359
92 X = -355252
12
Y = 21594911
65 feet Y = 6578611
94 meter
Z = 5301502
95 Z = 1614369
26
XDOT = -16376
939798 XDOT = -4977
025391
YDOT = 3925
366430 feet/sec YDOT = 1140
712396 meter/sec
ZDOT = -18691
379477 ZDOT = -5721
345121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21215684
85 X = 6466540
74
Y = 4138157
14 feet Y = 1261310
30 meter
Z = 5293728
83 Z = 1613528
55
XDOT = 1761
697111 XDOT = 536
965279
YDOT = 15109
993370 feet/sec YDOT = 4605
525979 meter/sec
ZDOT = -18798
698743 ZDOT = -5729
843377
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 17263
26588317
00016717 00000-0 10270-3 0 9051
2 25544 51
6397 284
3500 0003971 293
2443 66
8291 15
54218516 36539
Satellite: ISS
Catalog Number: 25544
Epoch time: 17263
26588317 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 284
3500 deg
Eccentricity:
0003971
Arg of perigee: 293
2443 deg
Mean anomaly: 66
8291 deg
Mean motion: 15
54218516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3653
Checksum: 324
Coasting Arc #7 (Orbit 3668)
---------------------------------------
Vector Time (GMT): 2017/264/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1107910
02 A = 6789030
08 meter
Y = -6689978
71 meter E =
0011850
Z = 100487
23 I = 51
28998
XDOT = 4717
890001 Wp = 27
79967
YDOT = 875
342989 meter/sec RA = 278
72278 deg
ZDOT = 5984
330308 TA = 333
28836
MA = 333
34935
Ha = 219
838 n
mi
Hp = 215
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3634875
40 X = 1182148
68
Y = -21948749
06 feet Y = -6677174
20 meter
Z = 329682
50 Z = 106050
40
XDOT = 15478
641734 XDOT = 4678
681939
YDOT = 2871
860199 feet/sec YDOT = 927
883277 meter/sec
ZDOT = 19633
629618 ZDOT = 6007
153117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21278046
45 X = -6485548
56
Y = -6495158
89 feet Y = -1979724
43 meter
Z = 355309
85 Z = 108298
44
XDOT = 4398
801984 XDOT = 1340
754845
YDOT = -13284
989367 feet/sec YDOT = -4049
264759 meter/sec
ZDOT = 19734
480963 ZDOT = 6015
069798
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 17264
29464798
00016717 00000-0 10270-3 0 9062
2 25544 51
6407 279
2206 0003947 300
7823 59
2941 15
54230802 36693
Satellite: ISS
Catalog Number: 25544
Epoch time: 17264
29464798 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 279
2206 deg
Eccentricity:
0003947
Arg of perigee: 300
7823 deg
Mean anomaly: 59
2941 deg
Mean motion: 15
54230802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3669
Checksum: 329
Coasting Arc #8 (Orbit 3683)
---------------------------------------
Vector Time (GMT): 2017/265/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1876553
03 A = 6787559
05 meter
Y = 6259441
62 meter E =
0003713
Z = -1828241
92 I = 51
28060
XDOT = -4318
743092 Wp = 160
77791
YDOT = -2932
295876 meter/sec RA = 273
72691 deg
ZDOT = -5613
286310 TA = 39
42374
MA = 39
39673
Ha = 219
907 n
mi
Hp = 215
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6156670
04 X = -1937527
52
Y = 20536225
79 feet Y = 6238115
55 meter
Z = -5998169
03 Z = -1837506
66
XDOT = -14169
104633 XDOT = -4258
365559
YDOT = -9620
393293 feet/sec YDOT = -2980
254178 meter/sec
ZDOT = -18416
293668 ZDOT = -5634
118564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19697763
84 X = 6003878
42
Y = 8434127
51 feet Y = 2570722
07 meter
Z = -6040097
70 Z = -1841021
78
XDOT = -10555
895698 XDOT = -3217
437009
YDOT = 11414
245658 feet/sec YDOT = 3479
062077 meter/sec
ZDOT = -18508
030548 ZDOT = -5641
247711
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 17265
25911074
00016717 00000-0 10270-3 0 9074
2 25544 51
6400 274
4122 0003936 302
9107 57
1667 15
54242082 36849
Satellite: ISS
Catalog Number: 25544
Epoch time: 17265
25911074 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 274
4122 deg
Eccentricity:
0003936
Arg of perigee: 302
9107 deg
Mean anomaly: 57
1667 deg
Mean motion: 15
54242082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 297
Coasting Arc #9 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2017/266/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2560198
07 A = 6784133
07 meter
Y = -5314933
47 meter E =
0009704
Z = 3338979
31 I = 51
26919
XDOT = 3827
169845 Wp = 74
84713
YDOT = 4763
001344 meter/sec RA = 268
72338 deg
ZDOT = 4638
334832 TA = 324
30747
MA = 324
37231
Ha = 219
870 n
mi
Hp = 215
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8399599
97 X = 2603221
47
Y = -17437445
78 feet Y = -5286062
62 meter
Z = 10954656
53 Z = 3351521
26
XDOT = 12556
331514 XDOT = 3751
093230
YDOT = 15626
644829 feet/sec YDOT = 4805
374569 meter/sec
ZDOT = 15217
633962 ZDOT = 4656
740884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16539633
98 X = -5041280
44
Y = -9991100
49 feet Y = -3045287
43 meter
Z = 11010936
07 Z = 3356133
31
XDOT = 16041
425149 XDOT = 4889
426385
YDOT = -9663
927140 feet/sec YDOT = -2945
564992 meter/sec
ZDOT = 15298
370219 ZDOT = 4662
943243
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 17266
28786594
00016717 00000-0 10270-3 0 9086
2 25544 51
6409 269
2829 0003929 306
6485 53
4306 15
54272067 37000
Satellite: ISS
Catalog Number: 25544
Epoch time: 17266
28786594 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 269
2829 deg
Eccentricity:
0003929
Arg of perigee: 306
6485 deg
Mean anomaly: 53
4306 deg
Mean motion: 15
54272067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 340
Coasting Arc #10 (Orbit 3714)
---------------------------------------
Vector Time (GMT): 2017/267/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3198823
88 A = 6780336
32 meter
Y = 3943864
67 meter E =
0008498
Z = -4501387
61 I = 51
25820
XDOT = -3219
964476 Wp = 44
98147
YDOT = -6200
701265 meter/sec RA = 263
70959 deg
ZDOT = -3142
246715 TA = 193
28071
MA = 193
30310
Ha = 220
108 n
mi
Hp = 215
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10494828
99 X = -3220821
65
Y = 12939188
56 feet Y = 3907969
76 meter
Z = -14768332
06 Z = -4516980
56
XDOT = -10564
187912 XDOT = -3135
123573
YDOT = -20343
508087 feet/sec YDOT = -6236
235070 meter/sec
ZDOT = -10309
208383 ZDOT = -3157
681769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12058330
73 X = 3675379
21
Y = 11406179
50 feet Y = 3476603
51 meter
Z = -14837904
06 Z = -4522593
16
XDOT = -20292
028106 XDOT = -6185
010167
YDOT = 7944
088689 feet/sec YDOT = 2421
358232 meter/sec
ZDOT = -10376
597324 ZDOT = -3162
786864
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 17267
25232051
00016717 00000-0 10270-3 0 9099
2 25544 51
6411 264
4746 0004062 310
6060 49
4739 15
54243131 37152
Satellite: ISS
Catalog Number: 25544
Epoch time: 17267
25232051 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 264
4746 deg
Eccentricity:
0004062
Arg of perigee: 310
6060 deg
Mean anomaly: 49
4739 deg
Mean motion: 15
54243131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 285
Coasting Arc #11 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2017/268/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3767794
03 A = 6777453
46 meter
Y = -2264748
75 meter E =
0000834
Z = 5157657
13 I = 51
25386
XDOT = 2497
393867 Wp = 55
05121
YDOT = 7132
622640 meter/sec RA = 258
68596 deg
ZDOT = 1307
876621 TA = 22
32102
MA = 22
31739
Ha = 220
032 n
mi
Hp = 215
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12361528
97 X = 3767785
32
Y = -7430278
04 feet Y = -2222614
27 meter
Z = 16921447
28 Z = 5175960
34
XDOT = 8193
549431 XDOT = 2411
096262
YDOT = 23400
992913 feet/sec YDOT = 7160
067805 meter/sec
ZDOT = 4290
933796 ZDOT = 1319
798070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6637293
20 X = -2023046
97
Y = -12696618
05 feet Y = -3869929
18 meter
Z = 17002765
58 Z = 5182442
95
XDOT = 22946
080555 XDOT = 6993
965353
YDOT = -6181
212198 feet/sec YDOT = -1884
033478 meter/sec
ZDOT = 4342
652300 ZDOT = 1323
640421
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 17268
28106525
00016717 00000-0 10270-3 0 9101
2 25544 51
6413 259
3455 0004085 315
9744 44
1083 15
54290813 37317
Satellite: ISS
Catalog Number: 25544
Epoch time: 17268
28106525 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 259
3455 deg
Eccentricity:
0004085
Arg of perigee: 315
9744 deg
Mean anomaly: 44
1083 deg
Mean motion: 15
54290813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 302
Coasting Arc #12 (Orbit 3745)
---------------------------------------
Vector Time (GMT): 2017/269/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4262816
02 A = 6777090
66 meter
Y = 457427
19 meter E =
0012088
Z = -5258835
25 I = 51
25895
XDOT = -1624
601405 Wp = 81
27426
YDOT = -7455
773727 meter/sec RA = 253
65872 deg
ZDOT = 671
508755 TA = 195
16069
MA = 195
19695
Ha = 220
295 n
mi
Hp = 215
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13985616
85 X = -4242069
10
Y = 1500745
38 feet Y = 409873
04 meter
Z = -17253396
48 Z = -5279492
59
XDOT = -5330
057102 XDOT = -1544
370116
YDOT = -24461
199892 feet/sec YDOT = -7473
492472 meter/sec
ZDOT = 2203
112714 ZDOT = 663
812336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 856518
97 X = 261066
98
Y = 13926633
39 feet Y = 4244837
86 meter
Z = -17344874
26 Z = -5286717
68
XDOT = -23666
358241 XDOT = -7213
505992
YDOT = 4145
590684 feet/sec YDOT = 1263
576041 meter/sec
ZDOT = 2170
122991 ZDOT = 661
453488
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 17269
24551122
00016717 00000-0 10270-3 0 9116
2 25544 51
6404 254
5376 0004128 320
1198 39
9651 15
54268704 37468
Satellite: ISS
Catalog Number: 25544
Epoch time: 17269
24551122 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 254
5376 deg
Eccentricity:
0004128
Arg of perigee: 320
1198 deg
Mean anomaly: 39
9651 deg
Mean motion: 15
54268704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3746
Checksum: 308
Coasting Arc #13 (Orbit 3761)
---------------------------------------
Vector Time (GMT): 2017/270/05:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 904865
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4629316
12 A = 6779033
19 meter
Y = 1345192
13 meter E =
0008038
Z = 4765492
43 I = 51
27698
XDOT = 584
646343 Wp = 29
73737
YDOT = 7194
173075 meter/sec RA = 248
63315 deg
ZDOT = -2589
949164 TA = 85
96026
MA = 85
86839
Ha = 220
271 n
mi
Hp = 215
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15188045
01 X = 4590781
08
Y = 4413360
02 feet Y = 1396745
20 meter
Z = 15634817
69 Z = 4787886
76
XDOT = 1918
131045 XDOT = 516
736575
YDOT = 23602
930035 feet/sec YDOT = 7200
331088 meter/sec
ZDOT = -8497
208543 ZDOT = -2587
274586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4850748
20 X = 1478508
05
Y = -14950648
07 feet Y = -4556957
53 meter
Z = 15733732
76 Z = 4795641
74
XDOT = 22559
367118 XDOT = 6876
095097
YDOT = -1641
492862 feet/sec YDOT = -500
327024 meter/sec
ZDOT = -8486
391104 ZDOT = -2586
652008
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 17270
27424592
00016717 00000-0 10270-3 0 9122
2 25544 51
6413 249
4078 0004234 323
9826 36
1041 15
54313450 37626
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
27424592 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 249
4078 deg
Eccentricity:
0004234
Arg of perigee: 323
9826 deg
Mean anomaly: 36
1041 deg
Mean motion: 15
54313450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3762
Checksum: 292
Coasting Arc #14 (Orbit 3768)
---------------------------------------
Vector Time (GMT): 2017/270/16:53:37
658
Vector Time (MET): N/A
Weight (LBS) : 904716
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2440236
13 A = 6779622
77 meter
Y = 4087718
41 meter E =
0010580
Z = -4836589
67 I = 51
28211
XDOT = -4596
866024 Wp = 49
93710
YDOT = -5624
342733 meter/sec RA = 246
30338 deg
ZDOT = -2431
067268 TA = 196
04416
MA = 196
07770
Ha = 220
613 n
mi
Hp = 215
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8006024
03 X = -2462270
70
Y = 13411149
63 feet Y = 4060306
47 meter
Z = -15868076
33 Z = -4848497
51
XDOT = -15081
581444 XDOT = -4521
822424
YDOT = -18452
568022 feet/sec YDOT = -5675
328607 meter/sec
ZDOT = -7975
942481 ZDOT = -2453
214964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11693425
67 X = -3564156
14
Y = -10272563
29 feet Y = -3131077
29 meter
Z = -15921351
74 Z = -4852828
01
XDOT = 20191
496633 XDOT = 6154
368174
YDOT = -10455
835459 feet/sec YDOT = -3186
938648 meter/sec
ZDOT = -8073
168187 ZDOT = -2460
701663
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 17270
72431956
00016717 00000-0 10270-3 0 9135
2 25544 51
6415 247
1666 0004516 316
7542 43
3256 15
54039529 37691
Satellite: ISS
Catalog Number: 25544
Epoch time: 17270
72431956 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 247
1666 deg
Eccentricity:
0004516
Arg of perigee: 316
7542 deg
Mean anomaly: 43
3256 deg
Mean motion: 15
54039529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3769
Checksum: 320
Coasting Arc #15 (Orbit 3784)
---------------------------------------
Vector Time (GMT): 2017/271/16:53:37
658
Vector Time (MET): N/A
Weight (LBS) : 904716
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3372677
48 A = 6777701
51 meter
Y = -2621486
74 meter E =
0002194
Z = 5262195
41 I = 51
28918
XDOT = 4088
197101 Wp = 352
51149
YDOT = 6460
347202 meter/sec RA = 241
28189 deg
ZDOT = 600
309222 TA = 91
74355
MA = 91
71842
Ha = 220
540 n
mi
Hp = 215
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11065214
84 X = 3376179
61
Y = -8600678
29 feet Y = -2583751
21 meter
Z = 17264420
63 Z = 5278587
65
XDOT = 13412
720148 XDOT = 4012
735904
YDOT = 21195
364836 feet/sec YDOT = 6505
642324 meter/sec
ZDOT = 1969
518445 ZDOT = 619
984832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6608698
82 X = 2014331
40
Y = 12256129
30 feet Y = 3735668
21 meter
Z = 17337337
19 Z = 5284420
38
XDOT = -22274
007174 XDOT = -6789
117387
YDOT = 9112
539501 feet/sec YDOT = 2777
502040 meter/sec
ZDOT = 2055
705151 ZDOT = 626
578930
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 17271
75322331
00016717 00000-0 10270-3 0 9146
2 25544 51
6408 242
0384 0004515 319
2833 40
7982 15
54051167 37851
Satellite: ISS
Catalog Number: 25544
Epoch time: 17271
75322331 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 242
0384 deg
Eccentricity:
0004515
Arg of perigee: 319
2833 deg
Mean anomaly: 40
7982 deg
Mean motion: 15
54051167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3785
Checksum: 301
Coasting Arc #16 (Orbit 3799)
---------------------------------------
Vector Time (GMT): 2017/272/16:53:37
658
Vector Time (MET): N/A
Weight (LBS) : 904716
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4255697
29 A = 6778117
34 meter
Y = 1086488
80 meter E =
0011107
Z = -5171856
38 I = 51
30733
XDOT = -3296
417974 Wp = 83
61396
YDOT = -6793
817190 meter/sec RA = 236
25974 deg
ZDOT = 1288
857973 TA = 198
81389
MA = 198
85497
Ha = 220
733 n
mi
Hp = 215
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13962261
45 X = -4242407
91
Y = 3564595
79 feet Y = 1038972
60 meter
Z = -16968032
73 Z = -5192497
16
XDOT = -10815
019600 XDOT = -3226
463383
YDOT = -22289
426477 feet/sec YDOT = -6830
288748 meter/sec
ZDOT = 4228
536656 ZDOT = 1273
015323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1397579
57 X = -425982
25
Y = -14233196
45 feet Y = -4338278
28 meter
Z = -17059546
09 Z = -5199749
65
XDOT = 22649
973644 XDOT = 6903
711967
YDOT = -7195
221601 feet/sec YDOT = -2193
103544 meter/sec
ZDOT = 4159
341320 ZDOT = 1267
767234
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 17272
71781702
00016717 00000-0 10270-3 0 9155
2 25544 51
6409 237
2311 0004606 322
4226 37
6605 15
54048399 38009
Satellite: ISS
Catalog Number: 25544
Epoch time: 17272
71781702 = yrday
fracday
Element set: 915
Inclination: 51
6409 deg
RA of node: 237
2311 deg
Eccentricity:
0004606
Arg of perigee: 322
4226 deg
Mean anomaly: 37
6605 deg
Mean motion: 15
54048399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3800
Checksum: 298
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