[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 19th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
263/18:05:08
491 0
1 0
8 0
9
N/A -0
8 0
1 222
0
000/00:00:16
983 0
2 -0
0 215
2
264/18:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 215
5
267/01:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 215
7
268/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
8
271/01:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
1
274/09:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 216
3
277/08:22:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
5
Coasting Arc #1 (Orbit 1317)
---------------------------------------
Vector Time (GMT): 2018/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3969620
58 A = 6780087
74 meter
Y = 2639199
31 meter E =
0006673
Z = 4815358
16 I = 51
24435
XDOT = -1706
857336 Wp = 97
31198
YDOT = 7063
277715 meter/sec RA = 267
80274 deg
ZDOT = -2462
057071 TA = 16
99852
MA = 16
97618
Ha = 221
991 n
mi
Hp = 214
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13023689
57 X = 3916422
89
Y = 8658790
38 feet Y = 2683293
21 meter
Z = 15798419
15 Z = 4834511
77
XDOT = -5599
925643 XDOT = -1773
754671
YDOT = 23173
483318 feet/sec YDOT = 7043
816257 meter/sec
ZDOT = -8077
615063 ZDOT = -2470
511279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12522793
63 X = -3816947
50
Y = -9222732
70 feet Y = -2811088
93 meter
Z = 15884018
06 Z = 4841448
71
XDOT = 5892
869352 XDOT = 1796
146579
YDOT = -21991
796613 feet/sec YDOT = -6703
099608 meter/sec
ZDOT = -8116
345727 ZDOT = -2473
862178
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 18262
54391625
00016717 00000-0 10270-3 0 9001
2 25544 51
6384 268
4917 0004425 173
8677 186
2530 15
53882239 13184
Satellite: ISS
Catalog Number: 25544
Epoch time: 18262
54391625 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 268
4917 deg
Eccentricity:
0004425
Arg of perigee: 173
8677 deg
Mean anomaly: 186
2530 deg
Mean motion: 15
53882239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1318
Checksum: 329
Coasting Arc #2 (Orbit 1332)
---------------------------------------
Vector Time (GMT): 2018/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3704618
48 A = 6783496
82 meter
Y = -4107284
13 meter E =
0009186
Z = -3937817
59 I = 51
25692
XDOT = 2464
344665 Wp = 133
10650
YDOT = -6052
114940 meter/sec RA = 262
78767 deg
ZDOT = 3993
923995 TA = 178
85576
MA = 178
85365
Ha = 222
100 n
mi
Hp = 214
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12154260
10 X = -3639286
59
Y = -13475341
64 feet Y = -4148346
74 meter
Z = -12919349
05 Z = -3955654
29
XDOT = 8085
120291 XDOT = 2512
437642
YDOT = -19856
020144 feet/sec YDOT = -6024
287735 meter/sec
ZDOT = 13103
425181 ZDOT = 4006
012123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11699436
42 X = 3565988
22
Y = 13797556
86 feet Y = 4205495
33 meter
Z = -12998886
99 Z = -3962060
76
XDOT = -7525
451801 XDOT = -2293
757709
YDOT = 18778
497036 feet/sec YDOT = 5723
685897 meter/sec
ZDOT = 13158
323427 ZDOT = 4010
656981
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 18263
50860944
00016717 00000-0 10270-3 0 9014
2 25544 51
6375 263
6853 0004319 176
5026 183
6158 15
53850188 13332
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
50860944 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 263
6853 deg
Eccentricity:
0004319
Arg of perigee: 176
5026 deg
Mean anomaly: 183
6158 deg
Mean motion: 15
53850188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1333
Checksum: 320
Coasting Arc #3 (Orbit 1336)
---------------------------------------
Vector Time (GMT): 2018/263/18:05:16
983
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4272663
34 A = 6780227
39 meter
Y = -1928501
25 meter E =
0013424
Z = -4910979
81 I = 51
24778
XDOT = 723
609142 Wp = 123
46356
YDOT = -7289
521251 meter/sec RA = 261
52504 deg
ZDOT = 2230
137104 TA = 168
48072
MA = 168
44997
Ha = 221
983 n
mi
Hp = 215
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14017924
33 X = -4226925
90
Y = -6327103
82 feet Y = -1976025
77 meter
Z = -16112138
48 Z = -4931623
60
XDOT = 2374
045743 XDOT = 794
236028
YDOT = -23915
752135 feet/sec YDOT = -7281
034283 meter/sec
ZDOT = 7316
722781 ZDOT = 2233
824224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6322958
44 X = 1927237
73
Y = -13912920
80 feet Y = -4240658
26 meter
Z = -16204514
29 Z = -4939135
96
XDOT = 22901
562147 XDOT = 6980
396142
YDOT = 1855
130867 feet/sec YDOT = 565
443888 meter/sec
ZDOT = 7334
075685 ZDOT = 2235
426269
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 18263
76586200
00016717 00000-0 10270-3 0 9023
2 25544 51
6396 262
4037 0003981 188
2178 171
8909 15
53712409 13378
Satellite: ISS
Catalog Number: 25544
Epoch time: 18263
76586200 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 262
4037 deg
Eccentricity:
0003981
Arg of perigee: 188
2178 deg
Mean anomaly: 171
8909 deg
Mean motion: 15
53712409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1337
Checksum: 325
Coasting Arc #4 (Orbit 1352)
---------------------------------------
Vector Time (GMT): 2018/264/18:05:16
983
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4198190
23 A = 6783295
80 meter
Y = 3386561
48 meter E =
0009393
Z = 4104241
55 I = 51
26352
XDOT = -1551
106813 Wp = 98
88203
YDOT = 6499
103223 meter/sec RA = 256
51064 deg
ZDOT = -3770
057440 TA = 30
19446
MA = 30
14036
Ha = 221
775 n
mi
Hp = 215
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13773590
01 X = 4140072
58
Y = 11110766
01 feet Y = 3433183
98 meter
Z = 13465359
42 Z = 4124493
35
XDOT = -5088
933115 XDOT = -1605
353431
YDOT = 21322
517135 feet/sec YDOT = 6481
454012 meter/sec
ZDOT = -12368
954857 ZDOT = -3777
724500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10869417
37 X = -3312998
41
Y = 13877035
74 feet Y = 4229720
49 meter
Z = 13555827
25 Z = 4131816
15
XDOT = -20394
429208 XDOT = -6216
222023
YDOT = -3838
295022 feet/sec YDOT = -1169
912323 meter/sec
ZDOT = -12404
053621 ZDOT = -3780
755544
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 18264
79497072
00016717 00000-0 10270-3 0 9036
2 25544 51
6391 257
2776 0004020 192
2048 167
9008 15
53711304 13538
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
79497072 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 257
2776 deg
Eccentricity:
0004020
Arg of perigee: 192
2048 deg
Mean anomaly: 167
9008 deg
Mean motion: 15
53711304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1353
Checksum: 308
Coasting Arc #5 (Orbit 1352)
---------------------------------------
Vector Time (GMT): 2018/264/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2477813
65 A = 6789982
82 meter
Y = 6196865
34 meter E =
0015613
Z = 1199675
70 I = 51
28599
XDOT = -4135
538505 Wp = 136
33824
YDOT = 2788
791271 meter/sec RA = 256
49029 deg
ZDOT = -5829
435782 TA = 30
55647
MA = 30
46560
Ha = 221
918 n
mi
Hp = 215
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8129309
88 X = 2402507
06
Y = 20330923
03 feet Y = 6224153
01 meter
Z = 3935943
91 Z = 1211528
54
XDOT = -13568
039715 XDOT = -4138
099970
YDOT = 9149
577660 feet/sec YDOT = 2742
529952 meter/sec
ZDOT = -19125
445478 ZDOT = -5849
531187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19807820
24 X = -6037423
61
Y = 9309480
53 feet Y = 2837529
67 meter
Z = 3988432
58 Z = 1215674
25
XDOT = -9260
092576 XDOT = -2822
476217
YDOT = -11422
453300 feet/sec YDOT = -3481
563766 meter/sec
ZDOT = -19215
885394 ZDOT = -5857
001868
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 18264
79497089
00016717 00000-0 10270-3 0 9045
2 25544 51
6395 257
2773 0004165 192
3396 167
7655 15
53689889 13534
Satellite: ISS
Catalog Number: 25544
Epoch time: 18264
79497089 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 257
2773 deg
Eccentricity:
0004165
Arg of perigee: 192
3396 deg
Mean anomaly: 167
7655 deg
Mean motion: 15
53689889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1353
Checksum: 373
Coasting Arc #6 (Orbit 1368)
---------------------------------------
Vector Time (GMT): 2018/265/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1878241
08 A = 6790467
79 meter
Y = -6512167
28 meter E =
0009531
Z = 356387
72 I = 51
29752
XDOT = 4700
388643 Wp = 61
31566
YDOT = -1022
646898 meter/sec RA = 251
49674 deg
ZDOT = 5968
321660 TA = 302
54248
MA = 302
63451
Ha = 221
748 n
mi
Hp = 215
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6162208
26 X = -1807011
76
Y = -21365378
21 feet Y = -6532772
77 meter
Z = 1169251
07 Z = 347437
61
XDOT = 15421
222581 XDOT = 4682
483933
YDOT = -3355
140743 feet/sec YDOT = -970
183356 meter/sec
ZDOT = 19581
107807 ZDOT = 5991
111080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20825034
89 X = 6347470
64
Y = -7801334
80 feet Y = -2377846
85 meter
Z = 1129797
25 Z = 344362
20
XDOT = 3955
634367 XDOT = 1205
677355
YDOT = 13467
467568 feet/sec YDOT = 4104
884115 meter/sec
ZDOT = 19683
440242 ZDOT = 5999
512586
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 18265
82407518
00016717 00000-0 10270-3 0 9059
2 25544 51
6403 252
1495 0003967 198
1651 161
9361 15
53719331 13699
Satellite: ISS
Catalog Number: 25544
Epoch time: 18265
82407518 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 252
1495 deg
Eccentricity:
0003967
Arg of perigee: 198
1651 deg
Mean anomaly: 161
9361 deg
Mean motion: 15
53719331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1369
Checksum: 322
Coasting Arc #7 (Orbit 1383)
---------------------------------------
Vector Time (GMT): 2018/266/18:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1116986
62 A = 6789059
38 meter
Y = 6412166
63 meter E =
0009717
Z = -1912562
65 I = 51
30395
XDOT = -5203
289528 Wp = 162
45228
YDOT = -753
629333 meter/sec RA = 246
50423 deg
ZDOT = -5582
038666 TA = 38
72315
MA = 38
65353
Ha = 221
711 n
mi
Hp = 215
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3664654
25 X = 1054491
20
Y = 21037292
10 feet Y = 6424307
88 meter
Z = -6274811
84 Z = -1907289
28
XDOT = -17071
159870 XDOT = -5167
360904
YDOT = -2472
537183 feet/sec YDOT = -811
615915 meter/sec
ZDOT = -18313
775151 ZDOT = -5607
227091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20593239
12 X = -6276819
28
Y = 5674842
09 feet Y = 1729691
87 meter
Z = -6251822
36 Z = -1905555
46
XDOT = 1277
286176 XDOT = 389
316826
YDOT = -15605
156844 feet/sec YDOT = -4756
451806 meter/sec
ZDOT = -18426
686069 ZDOT = -5616
453914
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 18266
78885976
00016717 00000-0 10270-3 0 9064
2 25544 51
6402 247
3434 0004091 201
4399 158
6583 15
53691296 13848
Satellite: ISS
Catalog Number: 25544
Epoch time: 18266
78885976 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 247
3434 deg
Eccentricity:
0004091
Arg of perigee: 201
4399 deg
Mean anomaly: 158
6583 deg
Mean motion: 15
53691296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1384
Checksum: 346
Coasting Arc #8 (Orbit 1388)
---------------------------------------
Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3932681
89 A = 6778585
66 meter
Y = -1595252
68 meter E =
0003913
Z = 5284668
99 I = 51
27055
XDOT = 3101
498765 Wp = 164
59507
YDOT = 7011
360779 meter/sec RA = 244
96742 deg
ZDOT = -195
232779 TA = 287
25354
MA = 287
29636
Ha = 221
693 n
mi
Hp = 215
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12902499
64 X = 3924557
99
Y = -5233768
63 feet Y = -1551319
47 meter
Z = 17338152
86 Z = 5303753
09
XDOT = 10175
520881 XDOT = 3023
813610
YDOT = 23003
152161 feet/sec YDOT = 7045
609501 meter/sec
ZDOT = -640
527490 ZDOT = -180
356309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9472344
21 X = 2887170
51
Y = -10057828
10 feet Y = -3065626
00 meter
Z = 17423925
07 Z = 5310812
36
XDOT = 18057
827173 XDOT = 5504
025722
YDOT = 16032
158862 feet/sec YDOT = 4886
602021 meter/sec
ZDOT = -574
517039 ZDOT = -175
112793
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 18267
11045516
00016717 00000-0 10270-3 0 9071
2 25544 51
6376 245
7354 0004341 198
6420 161
4574 15
53706611 13896
Satellite: ISS
Catalog Number: 25544
Epoch time: 18267
11045516 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 245
7354 deg
Eccentricity:
0004341
Arg of perigee: 198
6420 deg
Mean anomaly: 161
4574 deg
Mean motion: 15
53706611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1389
Checksum: 311
Coasting Arc #9 (Orbit 1403)
---------------------------------------
Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 909575
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4583537
77 A = 6779749
14 meter
Y = 89577
13 meter E =
0013042
Z = -5006385
02 I = 51
29041
XDOT = -2271
987428 Wp = 124
32240
YDOT = -7048
336166 meter/sec RA = 239
94823 deg
ZDOT = 1950
411557 TA = 164
74699
MA = 164
70763
Ha = 221
669 n
mi
Hp = 215
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15037853
59 X = -4559880
28
Y = 293888
22 feet Y = 38452
46 meter
Z = -16425147
71 Z = -5028592
93
XDOT = -7454
026994 XDOT = -2202
476239
YDOT = -23124
462487 feet/sec YDOT = -7073
354194 meter/sec
ZDOT = 6398
988048 ZDOT = 1939
544711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13354141
91 X = -4070342
46
Y = 6678875
41 feet Y = 2035721
23 meter
Z = -16524781
55 Z = -5036753
42
XDOT = -16218
228557 XDOT = -4943
316064
YDOT = -16685
477367 feet/sec YDOT = -5085
733501 meter/sec
ZDOT = 6350
950265 ZDOT = 1935
769641
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 18268
07523699
00016717 00000-0 10270-3 0 9081
2 25544 51
6383 240
9295 0004435 202
7045 157
3912 15
53734483 14045
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
07523699 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 240
9295 deg
Eccentricity:
0004435
Arg of perigee: 202
7045 deg
Mean anomaly: 157
3912 deg
Mean motion: 15
53734483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1404
Checksum: 320
Coasting Arc #10 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2018/268/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1066274
39 A = 6782074
46 meter
Y = 5004702
72 meter E =
0007023
Z = -4457063
10 I = 51
30420
XDOT = -5627
181864 Wp = 92
38392
YDOT = -4073
333297 meter/sec RA = 237
78307 deg
ZDOT = -3232
330123 TA = 144
91966
MA = 144
87339
Ha = 221
505 n
mi
Hp = 215
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3498275
57 X = -1100508
90
Y = 16419628
34 feet Y = 4992586
91 meter
Z = -14622910
42 Z = -4462326
52
XDOT = -18461
882755 XDOT = -5565
513422
YDOT = -13363
954386 feet/sec YDOT = -4135
915956 meter/sec
ZDOT = -10604
757621 ZDOT = -3259
514910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2063804
21 X = 629047
52
Y = -16639623
18 feet Y = -5071757
14 meter
Z = -14647023
20 Z = -4464412
67
XDOT = 18196
927074 XDOT = 5546
423372
YDOT = 11685
198736 feet/sec YDOT = 3561
648575 meter/sec
ZDOT = -10726
303686 ZDOT = -3269
377363
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 18268
52546799
00016717 00000-0 10270-3 0 9098
2 25544 51
6371 238
6891 0003947 206
3201 153
7751 15
53720964 14117
Satellite: ISS
Catalog Number: 25544
Epoch time: 18268
52546799 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 238
6891 deg
Eccentricity:
0003947
Arg of perigee: 206
3201 deg
Mean anomaly: 153
7751 deg
Mean motion: 15
53720964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 329
Coasting Arc #11 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2018/269/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2141542
32 A = 6779366
24 meter
Y = -3925331
00 meter E =
0006531
Z = 5095401
39 I = 51
31485
XDOT = 5495
534230 Wp = 162
21731
YDOT = 5099
053062 meter/sec RA = 232
76984 deg
ZDOT = 1611
772036 TA = 272
12424
MA = 272
19903
Ha = 221
282 n
mi
Hp = 215
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7026057
48 X = 2160526
23
Y = -12878382
55 feet Y = -3901276
02 meter
Z = 16717196
16 Z = 5105850
97
XDOT = 18029
967946 XDOT = 5430
277531
YDOT = 16729
176711 feet/sec YDOT = 5160
143265 meter/sec
ZDOT = 5287
965998 ZDOT = 1638
308615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5620877
31 X = -1713243
40
Y = 13492272
05 feet Y = 4112444
52 meter
Z = 16764462
46 Z = 5109808
16
XDOT = -18561
916386 XDOT = -5657
672114
YDOT = -14477
678374 feet/sec YDOT = -4412
796369 meter/sec
ZDOT = 5406
516279 ZDOT = 1647
906162
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 18269
55456496
00016717 00000-0 10270-3 0 9108
2 25544 51
6380 233
5626 0003928 212
7844 147
3065 15
53746071 14271
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
55456496 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 233
5626 deg
Eccentricity:
0003928
Arg of perigee: 212
7844 deg
Mean anomaly: 147
3065 deg
Mean motion: 15
53746071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 323
Coasting Arc #12 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2018/270/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3266481
14 A = 6778543
76 meter
Y = 2708346
45 meter E =
0013069
Z = -5297199
96 I = 51
33256
XDOT = -5048
421972 Wp = 105
39077
YDOT = -5756
721649 meter/sec RA = 227
75208 deg
ZDOT = 166
726242 TA = 166
22481
MA = 166
18911
Ha = 221
264 n
mi
Hp = 215
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10716801
62 X = -3270792
45
Y = 8885651
09 feet Y = 2671793
70 meter
Z = -17379264
96 Z = -5313078
40
XDOT = -16563
064213 XDOT = -4984
483381
YDOT = -18886
882052 feet/sec YDOT = -5812
819086 meter/sec
ZDOT = 547
002105 ZDOT = 142
358325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9508947
21 X = 2898327
11
Y = -10044605
07 feet Y = -3061595
62 meter
Z = -17450768
32 Z = -5318994
18
XDOT = 17896
010224 XDOT = 5454
703916
YDOT = 16162
946056 feet/sec YDOT = 4926
465958 meter/sec
ZDOT = 438
231244 ZDOT = 133
572883
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 18270
51934317
00016717 00000-0 10270-3 0 9110
2 25544 51
6377 228
7556 0003846 215
6788 144
4108 15
53723077 14427
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
51934317 = yrday
fracday
Element set: 911
Inclination: 51
6377 deg
RA of node: 228
7556 deg
Eccentricity:
0003846
Arg of perigee: 215
6788 deg
Mean anomaly: 144
4108 deg
Mean motion: 15
53723077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 321
Coasting Arc #13 (Orbit 1450)
---------------------------------------
Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -430685
57 A = 6782707
31 meter
Y = -5256865
94 meter E =
0009593
Z = 4262430
32 I = 51
36102
XDOT = 6370
000401 Wp = 132
74240
YDOT = 2366
750920 meter/sec RA = 225
07434 deg
ZDOT = 3551
067760 TA = 280
83793
MA = 280
94589
Ha = 221
322 n
mi
Hp = 216
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1413010
41 X = -392574
81
Y = -17246935
51 feet Y = -5261468
64 meter
Z = 13984351
43 Z = 4260431
26
XDOT = 20898
951448 XDOT = 6325
811798
YDOT = 7764
930840 feet/sec YDOT = 2437
737973 meter/sec
ZDOT = 11650
484778 ZDOT = 3581
903955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7724792
17 X = -2354516
65
Y = -15492500
54 feet Y = -4722114
17 meter
Z = 13975889
27 Z = 4259851
05
XDOT = 21088
613177 XDOT = 6427
809296
YDOT = 153
520138 feet/sec YDOT = 46
792938 meter/sec
ZDOT = 11788
612343 ZDOT = 3593
169042
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 18271
09820811
00016717 00000-0 10270-3 0 9128
2 25544 51
6398 225
8684 0004391 214
4381 145
6488 15
53760899 14519
Satellite: ISS
Catalog Number: 25544
Epoch time: 18271
09820811 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 225
8684 deg
Eccentricity:
0004391
Arg of perigee: 214
4381 deg
Mean anomaly: 145
6488 deg
Mean motion: 15
53760899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1451
Checksum: 331
Coasting Arc #14 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -878011
67 A = 6779829
41 meter
Y = 4492005
06 meter E =
0009673
Z = -5010050
46 I = 51
37620
XDOT = -6547
253246 Wp = 91
01206
YDOT = -3461
194303 meter/sec RA = 220
06645 deg
ZDOT = -1959
348683 TA = 159
89726
MA = 159
85914
Ha = 221
197 n
mi
Hp = 216
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2880615
73 X = -903840
64
Y = 14737549
41 feet Y = 4482041
69 meter
Z = -16437173
44 Z = -5014378
72
XDOT = -21480
489652 XDOT = -6498
544946
YDOT = -11355
624353 feet/sec YDOT = -3534
138048 meter/sec
ZDOT = -6428
309327 ZDOT = -1991
034948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3078173
94 X = 938227
42
Y = 14675324
80 feet Y = 4473039
00 meter
Z = -16457024
87 Z = -5016101
18
XDOT = -23080
974299 XDOT = -7035
080966
YDOT = -2513
870143 feet/sec YDOT = -766
227619 meter/sec
ZDOT = -6570
161494 ZDOT = -2002
585223
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 18272
06298336
00016717 00000-0 10270-3 0 9138
2 25544 51
6407 221
0626 0004327 218
5822 141
5021 15
53733338 14660
Satellite: ISS
Catalog Number: 25544
Epoch time: 18272
06298336 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 221
0626 deg
Eccentricity:
0004327
Arg of perigee: 218
5822 deg
Mean anomaly: 141
5021 deg
Mean motion: 15
53733338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 292
Coasting Arc #15 (Orbit 1481)
---------------------------------------
Vector Time (GMT): 2018/273/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2236296
25 A = 6778385
19 meter
Y = -3594373
07 meter E =
0003625
Z = 5294449
29 I = 51
39799
XDOT = 6367
218624 Wp = 187
07141
YDOT = 4267
865930 meter/sec RA = 215
05387 deg
ZDOT = 204
498634 TA = 260
95244
MA = 260
99346
Ha = 220
966 n
mi
Hp = 216
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7336929
96 X = 2250605
23
Y = -11792562
56 feet Y = -3569284
92 meter
Z = 17370240
47 Z = 5305347
61
XDOT = 20889
824882 XDOT = 6318
027571
YDOT = 14002
184809 feet/sec YDOT = 4338
793554 meter/sec
ZDOT = 670
927276 ZDOT = 235
309168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1924823
10 X = 586686
08
Y = -13692214
61 feet Y = -4173387
01 meter
Z = 17419490
29 Z = 5309460
64
XDOT = 23736
237841 XDOT = 7234
805294
YDOT = 4380
378426 feet/sec YDOT = 1335
139344 meter/sec
ZDOT = 808
791310 ZDOT = 246
519591
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 18273
09207148
00016717 00000-0 10270-3 0 9144
2 25544 51
6408 215
9353 0004225 222
9549 137
1274 15
53779261 14826
Satellite: ISS
Catalog Number: 25544
Epoch time: 18273
09207148 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 215
9353 deg
Eccentricity:
0004225
Arg of perigee: 222
9549 deg
Mean anomaly: 137
1274 deg
Mean motion: 15
53779261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1482
Checksum: 314
Coasting Arc #16 (Orbit 1496)
---------------------------------------
Vector Time (GMT): 2018/274/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3593731
82 A = 6779188
54 meter
Y = 2636741
22 meter E =
0011851
Z = -5118199
08 I = 51
42788
XDOT = -5765
415545 Wp = 119
01651
YDOT = -4788
662385 meter/sec RA = 210
04404 deg
ZDOT = 1578
341831 TA = 166
28219
MA = 166
24996
Ha = 220
949 n
mi
Hp = 216
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11790458
72 X = -3598087
62
Y = 8650725
78 feet Y = 2596529
03 meter
Z = -16791991
74 Z = -5135667
14
XDOT = -18915
405330 XDOT = -5719
105758
YDOT = -15710
834595 feet/sec YDOT = -4852
876256 meter/sec
ZDOT = 5178
286846 ZDOT = 1550
447722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7047271
60 X = -2148008
38
Y = 12709773
97 feet Y = 3873939
11 meter
Z = -16870642
21 Z = -5142171
74
XDOT = -22827
832159 XDOT = -6957
923242
YDOT = -5937
164954 feet/sec YDOT = -1809
647878 meter/sec
ZDOT = 5053
540559 ZDOT = 1540
319163
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 18274
05684180
00016717 00000-0 10270-3 0 9157
2 25544 51
6403 211
1302 0004144 225
4101 134
6713 15
53769629 14978
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
05684180 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 211
1302 deg
Eccentricity:
0004144
Arg of perigee: 225
4101 deg
Mean anomaly: 134
6713 deg
Mean motion: 15
53769629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1497
Checksum: 289
Coasting Arc #17 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2018/274/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5510002
18 A = 6789942
41 meter
Y = -3843129
11 meter E =
0009541
Z = 956360
23 I = 51
46984
XDOT = 3452
944623 Wp = 58
34851
YDOT = -3473
116290 meter/sec RA = 208
38598 deg
ZDOT = 5898
670310 TA = 312
03087
MA = 312
11204
Ha = 220
862 n
mi
Hp = 216
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18077434
96 X = -5471263
28
Y = -12608691
32 feet Y = -3904529
14 meter
Z = 3137664
79 Z = 929688
43
XDOT = 11328
558473 XDOT = 3462
872325
YDOT = -11394
738483 feet/sec YDOT = -3434
447320 meter/sec
ZDOT = 19352
592880 ZDOT = 5915
467997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7971144
89 X = 2429604
96
Y = 20566194
40 feet Y = 6268576
05 meter
Z = 3018308
93 Z = 919980
56
XDOT = -14153
501217 XDOT = -4313
987171
YDOT = 2615
085669 feet/sec YDOT = 797
078112 meter/sec
ZDOT = 19428
315827 ZDOT = 5921
750664
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 18274
44274721
00016717 00000-0 10270-3 0 9167
2 25544 51
6365 209
2100 0003973 227
9168 132
1647 15
53794538 15032
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
44274721 = yrday
fracday
Element set: 916
Inclination: 51
6365 deg
RA of node: 209
2100 deg
Eccentricity:
0003973
Arg of perigee: 227
9168 deg
Mean anomaly: 132
1647 deg
Mean motion: 15
53794538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 313
Coasting Arc #18 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2018/275/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4729817
88 A = 6787896
23 meter
Y = 4189640
82 meter E =
0005924
Z = -2471332
20 I = 51
49304
XDOT = -4951
257125 Wp = 171
07045
YDOT = 2461
330206 meter/sec RA = 203
40333 deg
ZDOT = -5310
839310 TA = 36
67077
MA = 36
63025
Ha = 220
795 n
mi
Hp = 216
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15517775
19 X = 4694621
16
Y = 13745540
75 feet Y = 4242336
04 meter
Z = -8108045
26 Z = -2448441
80
XDOT = -16244
281906 XDOT = -4952
614916
YDOT = 8075
230336 feet/sec YDOT = 2405
954034 meter/sec
ZDOT = -17424
013484 ZDOT = -5334
894409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5585550
60 X = -1702475
82
Y = -20004809
69 feet Y = -6097465
99 meter
Z = -8005676
05 Z = -2440130
06
XDOT = 16465
990607 XDOT = 5018
833937
YDOT = 2408
808113 feet/sec YDOT = 734
204713 meter/sec
ZDOT = -17532
230104 ZDOT = -5343
823736
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 18275
40751491
00016717 00000-0 10270-3 0 9179
2 25544 51
6374 204
4026 0003765 235
0059 125
0740 15
53752627 15188
Satellite: ISS
Catalog Number: 25544
Epoch time: 18275
40751491 = yrday
fracday
Element set: 917
Inclination: 51
6374 deg
RA of node: 204
4026 deg
Eccentricity:
0003765
Arg of perigee: 235
0059 deg
Mean anomaly: 125
0740 deg
Mean motion: 15
53752627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 301
Coasting Arc #19 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2018/276/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943654
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3620411
48 A = 6784459
84 meter
Y = -4343520
60 meter E =
0008871
Z = 3744681
20 I = 51
51290
XDOT = 6203
656227 Wp = 111
29352
YDOT = -1496
407205 meter/sec RA = 198
41676 deg
ZDOT = 4250
787423 TA = 293
56786
MA = 293
66101
Ha = 220
631 n
mi
Hp = 216
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11877990
43 X = -3589761
74
Y = -14250395
67 feet Y = -4383835
02 meter
Z = 12285699
49 Z = 3727169
04
XDOT = 20353
202844 XDOT = 6199
280204
YDOT = -4909
472458 feet/sec YDOT = -1427
057903 meter/sec
ZDOT = 13946
152963 ZDOT = 4280
912229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2597834
90 X = 791820
08
Y = 18420850
34 feet Y = 5614675
18 meter
Z = 12207471
98 Z = 3720837
46
XDOT = -18441
689204 XDOT = -5621
026869
YDOT = -6755
746716 feet/sec YDOT = -2059
151599 meter/sec
ZDOT = 14081
546467 ZDOT = 4292
055363
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18276
43659295
00016717 00000-0 10270-3 0 9183
2 25544 51
6376 199
2760 0003898 239
2429 120
8340 15
53785406 15348
Satellite: ISS
Catalog Number: 25544
Epoch time: 18276
43659295 = yrday
fracday
Element set: 918
Inclination: 51
6376 deg
RA of node: 199
2760 deg
Eccentricity:
0003898
Arg of perigee: 239
2429 deg
Mean anomaly: 120
8340 deg
Mean motion: 15
53785406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 345
Coasting Arc #20 (Orbit 1548)
---------------------------------------
Vector Time (GMT): 2018/277/08:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 928546
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1856125
33 A = 6780532
11 meter
Y = -4390160
06 meter E =
0005995
Z = 4822192
51 I = 51
52970
XDOT = 7239
907829 Wp = 151
81513
YDOT = -300
448733 meter/sec RA = 193
57869 deg
ZDOT = 2506
753608 TA = 273
46895
MA = 273
53753
Ha = 220
517 n
mi
Hp = 216
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6089650
04 X = -1830319
12
Y = -14403412
28 feet Y = -4410771
97 meter
Z = 15820841
58 Z = 4813239
02
XDOT = 23752
978443 XDOT = 7230
552925
YDOT = -985
724188 feet/sec YDOT = -219
539217 meter/sec
ZDOT = 8224
257244 ZDOT = 2541
899958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5136831
60 X = -1565706
27
Y = 14812597
79 feet Y = 4514879
81 meter
Z = 15781034
79 Z = 4810059
40
XDOT = -17083
983313 XDOT = -5207
198114
YDOT = -14877
252309 feet/sec YDOT = -4534
586504 meter/sec
ZDOT = 8382
108512 ZDOT = 2554
866675
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18277
40135254
00016717 00000-0 10270-3 0 9196
2 25544 51
6369 194
4693 0003887 244
3754 115
6997 15
53779960 15492
Satellite: ISS
Catalog Number: 25544
Epoch time: 18277
40135254 = yrday
fracday
Element set: 919
Inclination: 51
6369 deg
RA of node: 194
4693 deg
Eccentricity:
0003887
Arg of perigee: 244
3754 deg
Mean anomaly: 115
6997 deg
Mean motion: 15
53779960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1549
Checksum: 362
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