[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 15th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
291/16:05:00
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
4
295/18:32:00
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
2
300/09:45:00
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
5
Coasting Arc #1 (Orbit 1674)
---------------------------------------
Vector Time (GMT): 2018/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4414771
51 A = 6787497
63 meter
Y = 4488538
90 meter E =
0004094
Z = -2529857
62 I = 51
81952
XDOT = -5134
728058 Wp = 1
40016
YDOT = -2062
349840 meter/sec RA = 152
94583 deg
ZDOT = 5305
541451 TA = 330
28408
MA = 330
30732
Ha = 220
084 n
mi
Hp = 216
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14484158
51 X = -4452346
50
Y = 14726177
49 feet Y = 4438959
61 meter
Z = -8300057
80 Z = -2551395
06
XDOT = -16846
220662 XDOT = -5137
056759
YDOT = -6766
239631 feet/sec YDOT = -2119
782635 meter/sec
ZDOT = 17406
632057 ZDOT = 5280
592638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8477916
63 X = 2584068
99
Y = -18792361
16 feet Y = -5727911
68 meter
Z = -8397273
51 Z = -2559488
97
XDOT = 16883
367423 XDOT = 5146
050390
YDOT = -105
303274 feet/sec YDOT = -32
096438 meter/sec
ZDOT = 17294
690476 ZDOT = 5271
421657
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18285
50514150
00016717 00000-0 10270-3 0 9002
2 25544 51
6399 154
0925 0004050 282
0263 78
0435 15
53802565 16759
Satellite: ISS
Catalog Number: 25544
Epoch time: 18285
50514150 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 154
0925 deg
Eccentricity:
0004050
Arg of perigee: 282
0263 deg
Mean anomaly: 78
0435 deg
Mean motion: 15
53802565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1675
Checksum: 295
Coasting Arc #2 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2018/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5235042
87 A = 6789857
79 meter
Y = -4198240
22 meter E =
0010005
Z = 999154
61 I = 51
85604
XDOT = 3687
368073 Wp = 131
47098
YDOT = 3180
733195 meter/sec RA = 147
98724 deg
ZDOT = -5923
223298 TA = 37
73626
MA = 37
66613
Ha = 220
234 n
mi
Hp = 216
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17175337
50 X = 5276746
21
Y = -13773754
01 feet Y = -4139465
12 meter
Z = 3278066
32 Z = 1024686
63
XDOT = 12097
664281 XDOT = 3680
298661
YDOT = 10435
476362 feet/sec YDOT = 3221
928117 meter/sec
ZDOT = -19433
147303 ZDOT = -5905
328287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11037966
03 X = -3364372
04
Y = 19029018
10 feet Y = 5800044
72 meter
Z = 3393230
43 Z = 1034256
64
XDOT = -13777
394860 XDOT = -4199
349953
YDOT = -4522
701319 feet/sec YDOT = -1378
519362 meter/sec
ZDOT = -19353
007549 ZDOT = -5898
796701
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18286
53418432
00016717 00000-0 10270-3 0 9013
2 25544 51
6397 148
9646 0003866 284
7913 75
2811 15
53791057 16912
Satellite: ISS
Catalog Number: 25544
Epoch time: 18286
53418432 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 148
9646 deg
Eccentricity:
0003866
Arg of perigee: 284
7913 deg
Mean anomaly: 75
2811 deg
Mean motion: 15
53791057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1691
Checksum: 339
Coasting Arc #3 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2018/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5670516
58 A = 6790040
49 meter
Y = 3672855
56 meter E =
0011401
Z = 605884
56 I = 51
88330
XDOT = -2129
330314 Wp = 34
36811
YDOT = -4283
907092 meter/sec RA = 143
03375 deg
ZDOT = 5994
690500 TA = 332
15082
MA = 332
21180
Ha = 220
208 n
mi
Hp = 216
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18604057
01 X = -5714109
14
Y = 12050051
05 feet Y = 3609200
19 meter
Z = 1987810
25 Z = 578232
66
XDOT = -6985
991845 XDOT = -2110
387784
YDOT = -14054
813295 feet/sec YDOT = -4307
612620 meter/sec
ZDOT = 19667
619750 ZDOT = 5984
392924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12713642
84 X = 3875118
34
Y = -18170251
38 feet Y = -5538292
62 meter
Z = 1863144
49 Z = 567886
44
XDOT = 10557
069776 XDOT = 3217
794868
YDOT = 9415
107753 feet/sec YDOT = 2869
724843 meter/sec
ZDOT = 19621
735915 ZDOT = 5980
705107
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18287
56322227
00016717 00000-0 10270-3 0 9024
2 25544 51
6385 143
8366 0003987 288
6492 71
4227 15
53837897 17071
Satellite: ISS
Catalog Number: 25544
Epoch time: 18287
56322227 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 143
8366 deg
Eccentricity:
0003987
Arg of perigee: 288
6492 deg
Mean anomaly: 71
4227 deg
Mean motion: 15
53837897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1707
Checksum: 349
Coasting Arc #4 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2018/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5751345
84 A = 6788322
36 meter
Y = -2870710
42 meter E =
0003213
Z = -2176392
01 I = 51
90324
XDOT = 562
108182 Wp = 174
20556
YDOT = 5299
759573 meter/sec RA = 138
08080 deg
ZDOT = -5508
892698 TA = 29
84291
MA = 29
82459
Ha = 220
279 n
mi
Hp = 216
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18869244
90 X = 5793591
40
Y = -9418341
26 feet Y = -2806158
73 meter
Z = -7140393
74 Z = -2148350
85
XDOT = 1844
186950 XDOT = 529
562721
YDOT = 17387
662642 feet/sec YDOT = 5305
863306 meter/sec
ZDOT = -18073
794941 ZDOT = -5506
241350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13706682
95 X = -4177796
96
Y = 16083188
16 feet Y = 4902155
75 meter
Z = -7014034
42 Z = -2137877
69
XDOT = -7453
101990 XDOT = -2271
705486
YDOT = -14223
426444 feet/sec YDOT = -4335
300380 meter/sec
ZDOT = -18062
389956 ZDOT = -5505
416459
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18288
52794544
00016717 00000-0 10270-3 0 9037
2 25544 51
6387 139
0299 0004154 291
5955 68
4755 15
53807828 17229
Satellite: ISS
Catalog Number: 25544
Epoch time: 18288
52794544 = yrday
fracday
Element set: 903
Inclination: 51
6387 deg
RA of node: 139
0299 deg
Eccentricity:
0004154
Arg of perigee: 291
5955 deg
Mean anomaly: 68
4755 deg
Mean motion: 15
53807828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 350
Coasting Arc #5 (Orbit 1737)
---------------------------------------
Vector Time (GMT): 2018/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5494907
79 A = 6785030
92 meter
Y = 1818955
78 meter E =
0008664
Z = 3531503
59 I = 51
91604
XDOT = 883
475592 Wp = 79
84298
YDOT = -6130
124368 meter/sec RA = 133
12112 deg
ZDOT = 4524
153608 TA = 321
58755
MA = 321
64921
Ha = 220
516 n
mi
Hp = 216
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18027912
71 X = -5531993
87
Y = 5967702
69 feet Y = 1757300
67 meter
Z = 11586297
86 Z = 3504720
75
XDOT = 2898
541968 XDOT = 929
982452
YDOT = -20111
956587 feet/sec YDOT = -6119
984536 meter/sec
ZDOT = 14843
023648 ZDOT = 4528
558455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14094496
52 X = 4296002
54
Y = -12835292
05 feet Y = -3912197
02 meter
Z = 11465681
66 Z = 3494739
77
XDOT = 4712
409541 XDOT = 1436
342428
YDOT = 18475
592397 feet/sec YDOT = 5631
360563 meter/sec
ZDOT = 14863
437117 ZDOT = 4530
375633
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18289
55697895
00016717 00000-0 10270-3 0 9043
2 25544 51
6384 133
9010 0004169 297
2983 62
7745 15
53825669 17386
Satellite: ISS
Catalog Number: 25544
Epoch time: 18289
55697895 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 133
9010 deg
Eccentricity:
0004169
Arg of perigee: 297
2983 deg
Mean anomaly: 62
7745 deg
Mean motion: 15
53825669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1738
Checksum: 363
Coasting Arc #6 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2018/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4982507
83 A = 6781460
40 meter
Y = -538506
54 meter E =
0007906
Z = -4576450
86 I = 51
92430
XDOT = -2138
362092 Wp = 46
63720
YDOT = 6666
250946 meter/sec RA = 128
15517 deg
ZDOT = -3110
589778 TA = 192
30170
MA = 192
32102
Ha = 220
476 n
mi
Hp = 216
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16346810
47 X = 5010389
49
Y = -1766753
74 feet Y = -482632
98 meter
Z = -15014602
57 Z = -4552179
55
XDOT = -7015
623660 XDOT = -2197
637263
YDOT = 21870
902053 feet/sec YDOT = 6642
006737 meter/sec
ZDOT = -10205
347040 ZDOT = -3121
121567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14148959
92 X = -4312602
98
Y = 8568201
64 feet Y = 2611587
86 meter
Z = -14905394
18 Z = -4543164
15
XDOT = -2346
167025 XDOT = -715
111709
YDOT = -21722
273895 feet/sec YDOT = -6620
949083 meter/sec
ZDOT = -10253
379374 ZDOT = -3125
230033
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18290
52169564
00016717 00000-0 10270-3 0 9050
2 25544 51
6367 129
0940 0004044 300
6166 59
4588 15
53830449 17536
Satellite: ISS
Catalog Number: 25544
Epoch time: 18290
52169564 = yrday
fracday
Element set: 905
Inclination: 51
6367 deg
RA of node: 129
0940 deg
Eccentricity:
0004044
Arg of perigee: 300
6166 deg
Mean anomaly: 59
4588 deg
Mean motion: 15
53830449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 320
Coasting Arc #7 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2018/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4271207
63 A = 6778994
87 meter
Y = -891412
79 meter E =
0000511
Z = 5187902
28 I = 51
93588
XDOT = 3150
737649 Wp = 132
69173
YDOT = -6845
940015 meter/sec RA = 123
18227 deg
ZDOT = 1417
275229 TA = 303
72901
MA = 303
73389
Ha = 220
766 n
mi
Hp = 216
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14013148
38 X = -4286122
51
Y = -2924582
63 feet Y = -939259
51 meter
Z = 17020676
78 Z = 5167117
84
XDOT = 10337
065778 XDOT = 3220
172238
YDOT = -22460
433121 feet/sec YDOT = -6810
317971 meter/sec
ZDOT = 4649
853112 ZDOT = 1432
749589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13974937
20 X = 4259560
86
Y = -3576741
99 feet Y = -1090190
96 meter
Z = 16927285
55 Z = 5159436
64
XDOT = 342
964401 XDOT = 104
535549
YDOT = 23685
238226 feet/sec YDOT = 7219
260611 meter/sec
ZDOT = 4720
147418 ZDOT = 1438
700933
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18291
55072585
00016717 00000-0 10270-3 0 9061
2 25544 51
6371 123
9662 0004054 304
2835 55
7933 15
53798462 17697
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
55072585 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 123
9662 deg
Eccentricity:
0004054
Arg of perigee: 304
2835 deg
Mean anomaly: 55
7933 deg
Mean motion: 15
53798462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 332
Coasting Arc #8 (Orbit 1770)
---------------------------------------
Vector Time (GMT): 2018/291/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 490379
71 A = 6782851
89 meter
Y = 5330664
70 meter E =
0004061
Z = -4169367
13 I = 51
95374
XDOT = -5691
879636 Wp = 100
74067
YDOT = 3474
630244 meter/sec RA = 122
29918 deg
ZDOT = 3775
348554 TA = 207
97415
MA = 207
99599
Ha = 220
508 n
mi
Hp = 216
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1608857
30 X = 450987
08
Y = 17489057
41 feet Y = 5335927
98 meter
Z = -13679026
01 Z = -4167080
98
XDOT = -18674
145789 XDOT = -5748
649733
YDOT = 11399
705525 feet/sec YDOT = 3410
662481 meter/sec
ZDOT = 12386
314155 ZDOT = 3747
561010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17546120
74 X = -5348057
60
Y = 924964
91 feet Y = 281929
30 meter
Z = -13669286
39 Z = -4166398
49
XDOT = -10492
732098 XDOT = -3198
184744
YDOT = -17962
365530 feet/sec YDOT = -5474
929014 meter/sec
ZDOT = 12260
978849 ZDOT = 3737
146353
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18291
67935436
00016717 00000-0 10270-3 0 9078
2 25544 51
6386 123
3227 0003781 299
2799 60
7975 15
53826946 17716
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
67935436 = yrday
fracday
Element set: 907
Inclination: 51
6386 deg
RA of node: 123
3227 deg
Eccentricity:
0003781
Arg of perigee: 299
2799 deg
Mean anomaly: 60
7975 deg
Mean motion: 15
53826946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1771
Checksum: 358
Coasting Arc #9 (Orbit 1786)
---------------------------------------
Vector Time (GMT): 2018/292/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 535537
53 A = 6786476
86 meter
Y = -6078254
43 meter E =
0010010
Z = 2962296
71 I = 51
98314
XDOT = 5444
234179 Wp = 88
46326
YDOT = -1976
561125 meter/sec RA = 117
33961 deg
ZDOT = -5025
009333 TA = 57
87083
MA = 57
77373
Ha = 220
597 n
mi
Hp = 216
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1757012
89 X = 589077
02
Y = -19941779
64 feet Y = -6071966
12 meter
Z = 9718821
24 Z = 2965028
66
XDOT = 17861
660693 XDOT = 5490
341130
YDOT = -6484
780594 feet/sec YDOT = -1915
422466 meter/sec
ZDOT = -16486
251093 ZDOT = -4998
450713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19888064
83 X = 6061882
16
Y = 2230542
12 feet Y = 679869
24 meter
Z = 9731737
51 Z = 2966233
59
XDOT = 6160
640769 XDOT = 1877
763306
YDOT = 16689
388122 feet/sec YDOT = 5086
925500 meter/sec
ZDOT = -16366
584034 ZDOT = -4988
534814
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 18292
70837935
00016717 00000-0 10270-3 0 9089
2 25544 51
6391 118
1947 0003681 303
5226 56
5575 15
53827417 17876
Satellite: ISS
Catalog Number: 25544
Epoch time: 18292
70837935 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 118
1947 deg
Eccentricity:
0003681
Arg of perigee: 303
5226 deg
Mean anomaly: 56
5575 deg
Mean motion: 15
53827417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 339
Coasting Arc #10 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2018/293/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1396921
21 A = 6789211
57 meter
Y = 6466735
62 meter E =
0009186
Z = -1500004
84 I = 52
00672
XDOT = -5008
076515 Wp = 13
71620
YDOT = 260
148431 meter/sec RA = 112
39019 deg
ZDOT = 5801
369096 TA = 329
98934
MA = 330
04196
Ha = 220
739 n
mi
Hp = 216
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4583074
85 X = -1461843
90
Y = 21216324
22 feet Y = 6450751
15 meter
Z = -4921275
71 Z = -1506948
91
XDOT = -16430
697227 XDOT = -5038
793721
YDOT = 853
505350 feet/sec YDOT = 203
973371 meter/sec
ZDOT = 19033
363175 ZDOT = 5776
966649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21170246
88 X = -6452691
25
Y = -4758412
89 feet Y = -1450364
25 meter
Z = -4953190
59 Z = -1509732
49
XDOT = -1039
183561 XDOT = -316
743149
YDOT = -15020
803910 feet/sec YDOT = -4578
341032 meter/sec
ZDOT = 18923
565362 ZDOT = 5767
902722
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 18293
67308696
00016717 00000-0 10270-3 0 9094
2 25544 51
6392 113
3880 0003756 309
6300 50
4521 15
53835882 18020
Satellite: ISS
Catalog Number: 25544
Epoch time: 18293
67308696 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 113
3880 deg
Eccentricity:
0003756
Arg of perigee: 309
6300 deg
Mean anomaly: 50
4521 deg
Mean motion: 15
53835882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 318
Coasting Arc #11 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2018/294/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2128535
31 A = 6790117
46 meter
Y = -6442430
17 meter E =
0008144
Z = -126906
38 I = 52
02105
XDOT = 4446
152964 Wp = 137
34869
YDOT = 1583
415725 meter/sec RA = 107
44653 deg
ZDOT = -6041
226282 TA = 44
01077
MA = 43
94596
Ha = 220
751 n
mi
Hp = 216
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6983383
57 X = 2201034
62
Y = -21136581
92 feet Y = -6418222
05 meter
Z = -416359
52 Z = -116389
85
XDOT = 14587
116023 XDOT = 4457
461893
YDOT = 5194
933482 feet/sec YDOT = 1633
198378 meter/sec
ZDOT = -19820
296202 ZDOT = -6019
600739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21187583
69 X = 6457975
51
Y = 6829839
09 feet Y = 2081734
95 meter
Z = -368363
44 Z = -112277
18
XDOT = -4586
718096 XDOT = -1398
031676
YDOT = 13211
560520 feet/sec YDOT = 4026
883647 meter/sec
ZDOT = -19723
182044 ZDOT = -6011
625887
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 18294
70210625
00016717 00000-0 10270-3 0 9105
2 25544 51
6387 108
2604 0003754 311
6712 48
4119 15
53854833 18183
Satellite: ISS
Catalog Number: 25544
Epoch time: 18294
70210625 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 108
2604 deg
Eccentricity:
0003754
Arg of perigee: 311
6712 deg
Mean anomaly: 48
4119 deg
Mean motion: 15
53854833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 302
Coasting Arc #12 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2018/295/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2700830
75 A = 6788883
58 meter
Y = 5977315
18 meter E =
0013347
Z = 1720365
15 I = 52
02712
XDOT = -3826
470692 Wp = 48
79951
YDOT = -3382
327776 meter/sec RA = 102
50265 deg
ZDOT = 5724
300323 TA = 329
97436
MA = 330
05083
Ha = 220
944 n
mi
Hp = 216
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8860993
28 X = -2775826
82
Y = 19610614
12 feet Y = 5946693
44 meter
Z = 5644242
63 Z = 1707062
49
XDOT = -12554
037705 XDOT = -3816
170366
YDOT = -11096
875907 feet/sec YDOT = -3425
059918 meter/sec
ZDOT = 18780
512871 ZDOT = 5705
737606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19823804
21 X = -6042295
52
Y = -8413643
87 feet Y = -2564478
65 meter
Z = 5583748
43 Z = 1701926
52
XDOT = 10167
013073 XDOT = 3098
905585
YDOT = -11502
021167 feet/sec YDOT = -3505
816052 meter/sec
ZDOT = 18697
373597 ZDOT = 5698
959472
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 18295
73112202
00016717 00000-0 10270-3 0 9112
2 25544 51
6400 103
1326 0003766 317
7986 42
2876 15
53860835 18346
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
73112202 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 103
1326 deg
Eccentricity:
0003766
Arg of perigee: 317
7986 deg
Mean anomaly: 42
2876 deg
Mean motion: 15
53860835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 302
Coasting Arc #13 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2018/295/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4045404
40 A = 6783083
08 meter
Y = -3575708
44 meter E =
0006786
Z = -4113458
85 I = 52
00724
XDOT = 1722
383309 Wp = 39
25375
YDOT = 6389
705068 meter/sec RA = 102
00821 deg
ZDOT = -3858
855351 TA = 191
00876
MA = 191
02361
Ha = 220
912 n
mi
Hp = 216
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13272324
15 X = 4105069
73
Y = -11731326
91 feet Y = -3530136
68 meter
Z = -13495599
91 Z = -4093662
04
XDOT = 5650
863875 XDOT = 1669
548508
YDOT = 20963
599304 feet/sec YDOT = 6408
670189 meter/sec
ZDOT = -12660
286586 ZDOT = -3850
617344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17486299
51 X = 5329824
09
Y = 3227116
37 feet Y = 983625
07 meter
Z = -13406151
04 Z = -4086194
84
XDOT = -12673
790128 XDOT = -3862
971231
YDOT = 16208
554865 feet/sec YDOT = 4940
367523 meter/sec
ZDOT = -12623
923130 ZDOT = -3847
771770
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 18295
79543513
00016717 00000-0 10270-3 0 9122
2 25544 51
6389 102
8143 0003942 317
7159 42
3689 15
53846138 18357
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
79543513 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 102
8143 deg
Eccentricity:
0003942
Arg of perigee: 317
7159 deg
Mean anomaly: 42
3689 deg
Mean motion: 15
53846138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 333
Coasting Arc #14 (Orbit 1850)
---------------------------------------
Vector Time (GMT): 2018/296/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4148438
58 A = 6779802
51 meter
Y = 2065914
12 meter E =
0003162
Z = 4945940
39 I = 52
00269
XDOT = -897
705552 Wp = 95
01958
YDOT = -7267
461099 meter/sec RA = 97
04317 deg
ZDOT = 2281
135923 TA = 332
79842
MA = 332
81498
Ha = 221
161 n
mi
Hp = 215
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13610362
79 X = -4195257
25
Y = 6777933
46 feet Y = 2019262
01 meter
Z = 16226838
56 Z = 4925674
34
XDOT = -2945
228189 XDOT = -827
452887
YDOT = -23843
376308 feet/sec YDOT = -7277
106877 meter/sec
ZDOT = 7484
041743 ZDOT = 2276
946289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13928557
80 X = -4245424
42
Y = -6335267
42 feet Y = -1930989
51 meter
Z = 16135436
51 Z = 4918081
05
XDOT = 16108
447067 XDOT = 4909
854666
YDOT = -16387
524239 feet/sec YDOT = -4994
917388 meter/sec
ZDOT = 7466
003832 ZDOT = 2275
637968
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 18296
82444641
00016717 00000-0 10270-3 0 9130
2 25544 51
6392 97
6862 0004029 322
7160 37
3712 15
53874051 18519
Satellite: ISS
Catalog Number: 25544
Epoch time: 18296
82444641 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 97
6862 deg
Eccentricity:
0004029
Arg of perigee: 322
7160 deg
Mean anomaly: 37
3712 deg
Mean motion: 15
53874051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 313
Coasting Arc #15 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2018/297/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181950
05 A = 6778278
21 meter
Y = -398626
13 meter E =
0013236
Z = -5330599
39 I = 51
99949
XDOT = 103
946947 Wp = 70
90202
YDOT = 7642
469001 meter/sec RA = 92
07269 deg
ZDOT = -486
735740 TA = 194
45303
MA = 194
49092
Ha = 221
192 n
mi
Hp = 216
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13720308
55 X = 4211990
75
Y = -1307828
50 feet Y = -351693
02 meter
Z = -17488843
16 Z = -5310211
37
XDOT = 341
033292 XDOT = 20
843376
YDOT = 25073
717196 feet/sec YDOT = 7643
166717 meter/sec
ZDOT = -1596
902035 ZDOT = -486
433116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9935795
87 X = 3028430
58
Y = 9717954
39 feet Y = 2962032
50 meter
Z = -17397075
62 Z = -5302628
65
XDOT = -18206
808951 XDOT = -5549
435368
YDOT = 15737
996882 feet/sec YDOT = 4796
941450 meter/sec
ZDOT = -1596
413738 ZDOT = -486
586907
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 18297
78914458
00016717 00000-0 10270-3 0 9145
2 25544 51
6384 92
8795 0004024 326
7344 33
3555 15
53839316 18667
Satellite: ISS
Catalog Number: 25544
Epoch time: 18297
78914458 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 92
8795 deg
Eccentricity:
0004024
Arg of perigee: 326
7344 deg
Mean anomaly: 33
3555 deg
Mean motion: 15
53839316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 346
Coasting Arc #16 (Orbit 1881)
---------------------------------------
Vector Time (GMT): 2018/298/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4137577
31 A = 6778651
39 meter
Y = -1322427
00 meter E =
0006281
Z = 5203870
87 I = 52
00225
XDOT = 683
375536 Wp = 14
48180
YDOT = -7515
769663 meter/sec RA = 87
10029 deg
ZDOT = -1360
313918 TA = 88
56336
MA = 88
49140
Ha = 221
323 n
mi
Hp = 215
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13574728
72 X = -4147760
47
Y = -4338671
25 feet Y = -1368752
98 meter
Z = 17073067
15 Z = 5183746
67
XDOT = 2242
045721 XDOT = 773
976063
YDOT = -24658
036951 feet/sec YDOT = -7507
621160 meter/sec
ZDOT = -4462
972173 ZDOT = -1356
773847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5756245
82 X = -1754503
73
Y = -13154504
39 feet Y = -4009492
94 meter
Z = 16982685
25 Z = 5176322
46
XDOT = 19086
390814 XDOT = 5817
531920
YDOT = -14118
745676 feet/sec YDOT = -4303
393682 meter/sec
ZDOT = -4446
164633 ZDOT = -1355
190980
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 18298
81814987
00016717 00000-0 10270-3 0 9157
2 25544 51
6393 87
7518 0004113 330
7561 29
3361 15
53890981 18821
Satellite: ISS
Catalog Number: 25544
Epoch time: 18298
81814987 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 87
7518 deg
Eccentricity:
0004113
Arg of perigee: 330
7561 deg
Mean anomaly: 29
3361 deg
Mean motion: 15
53890981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1882
Checksum: 342
Coasting Arc #17 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2018/299/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4035920
98 A = 6781182
72 meter
Y = 2921547
17 meter E =
0007909
Z = -4606605
25 I = 52
00841
XDOT = -1471
395669 Wp = 86
75209
YDOT = 6864
259058 meter/sec RA = 82
13189 deg
ZDOT = 3069
222083 TA = 213
77301
MA = 213
82342
Ha = 221
510 n
mi
Hp = 215
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13241210
57 X = 4025328
60
Y = 9585128
50 feet Y = 2966620
33 meter
Z = -15113534
29 Z = -4587025
34
XDOT = -4827
413611 XDOT = -1562
953480
YDOT = 22520
534967 feet/sec YDOT = 6847
293017 meter/sec
ZDOT = 10069
626256 ZDOT = 3061
851823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1862269
52 X = 567619
75
Y = 16321173
32 feet Y = 4974693
63 meter
Z = -15025795
09 Z = -4579862
34
XDOT = -18781
010182 XDOT = -5724
451903
YDOT = 11366
987744 feet/sec YDOT = 3464
657864 meter/sec
ZDOT = 10035
641614 ZDOT = 3058
863564
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 18299
78284123
00016717 00000-0 10270-3 0 9168
2 25544 51
6399 82
9446 0004183 338
6514 21
4463 15
53875216 18972
Satellite: ISS
Catalog Number: 25544
Epoch time: 18299
78284123 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 82
9446 deg
Eccentricity:
0004183
Arg of perigee: 338
6514 deg
Mean anomaly: 21
4463 deg
Mean motion: 15
53875216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 344
Coasting Arc #18 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3396286
82 A = 6779512
28 meter
Y = -3066303
49 meter E =
0013009
Z = -5014110
73 I = 51
99671
XDOT = 2977
330594 Wp = 56
44719
YDOT = 6735
992659 meter/sec RA = 79
02545 deg
ZDOT = -2099
533986 TA = 193
17511
MA = 193
20912
Ha = 221
478 n
mi
Hp = 215
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11142673
29 X = 3454679
27
Y = -10060050
84 feet Y = -3027997
39 meter
Z = -16450494
54 Z = -4997470
43
XDOT = 9768
144993 XDOT = 2911
984289
YDOT = 22099
713447 feet/sec YDOT = 6768
921851 meter/sec
ZDOT = -6888
234863 ZDOT = -2085
229482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11060898
31 X = -3371361
80
Y = 10270840
83 feet Y = 3130552
28 meter
Z = -16375253
24 Z = -4991177
19
XDOT = -9478
208347 XDOT = -2888
957904
YDOT = -21104
388133 feet/sec YDOT = -6432
617503 meter/sec
ZDOT = -6824
699962 ZDOT = -2080
168548
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 18300
42596724
00016717 00000-0 10270-3 0 9176
2 25544 51
6369 79
7377 0004050 341
1610 18
9392 15
53881952 19073
Satellite: ISS
Catalog Number: 25544
Epoch time: 18300
42596724 = yrday
fracday
Element set: 917
Inclination: 51
6369 deg
RA of node: 79
7377 deg
Eccentricity:
0004050
Arg of perigee: 341
1610 deg
Mean anomaly: 18
9392 deg
Mean motion: 15
53881952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 323
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