[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 6th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
280/14:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
284/08:40:17
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
284/14:44:01
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
7
287/02:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 216
5
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
Coasting Arc #1 (Orbit 1566)
---------------------------------------
Vector Time (GMT): 2018/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5522268
65 A = 6787439
28 meter
Y = -2896402
95 meter E =
0009858
Z = 2669517
01 I = 51
59342
XDOT = 4381
579854 Wp = 80
15658
YDOT = -3553
314060 meter/sec RA = 187
83727 deg
ZDOT = 5193
887106 TA = 309
99052
MA = 310
07703
Ha = 220
412 n
mi
Hp = 216
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18117679
30 X = -5502436
98
Y = -9502634
36 feet Y = -2958045
68 meter
Z = 8758257
89 Z = 2642740
10
XDOT = 14375
261987 XDOT = 4395
759133
YDOT = -11657
854527 feet/sec YDOT = -3504
236469 meter/sec
ZDOT = 17040
312029 ZDOT = 5215
206085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19868240
08 X = 6055839
58
Y = 5088318
67 feet Y = 1550919
53 meter
Z = 8638257
55 Z = 2632940
90
XDOT = -10842
962205 XDOT = -3304
934880
YDOT = 13163
391424 feet/sec YDOT = 4012
201706 meter/sec
ZDOT = 17136
376722 ZDOT = 5223
167625
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 18278
55901809
00016717 00000-0 10270-3 0 9000
2 25544 51
6403 188
7005 0003756 251
4085 108
6660 15
53768783 15675
Satellite: ISS
Catalog Number: 25544
Epoch time: 18278
55901809 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 188
7005 deg
Eccentricity:
0003756
Arg of perigee: 251
4085 deg
Mean anomaly: 108
6660 deg
Mean motion: 15
53768783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1567
Checksum: 329
Coasting Arc #2 (Orbit 1581)
---------------------------------------
Vector Time (GMT): 2018/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4416362
59 A = 6783858
42 meter
Y = 3334673
03 meter E =
0002719
Z = -3926726
89 I = 51
61620
XDOT = -5809
859245 Wp = 72
19779
YDOT = 2924
234612 meter/sec RA = 182
85604 deg
ZDOT = -4052
476614 TA = 155
38471
MA = 155
37173
Ha = 220
283 n
mi
Hp = 216
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14489378
56 X = 4397819
16
Y = 10940528
32 feet Y = 3383955
76 meter
Z = -12882962
24 Z = -3905319
04
XDOT = -19061
217997 XDOT = -5822
442175
YDOT = 9593
945576 feet/sec YDOT = 2859
193948 meter/sec
ZDOT = -13295
526950 ZDOT = -4080
729874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16815544
47 X = -5125377
95
Y = -7023923
55 feet Y = -2140891
90 meter
Z = -12787100
12 Z = -3897508
12
XDOT = 15522
160925 XDOT = 4731
154650
YDOT = -12733
581750 feet/sec YDOT = -3881
195718 meter/sec
ZDOT = -13422
690243 ZDOT = -4091
235986
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 18279
52376313
00016717 00000-0 10270-3 0 9015
2 25544 51
6418 183
8943 0003751 256
1491 103
9244 15
53796732 15824
Satellite: ISS
Catalog Number: 25544
Epoch time: 18279
52376313 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 183
8943 deg
Eccentricity:
0003751
Arg of perigee: 256
1491 deg
Mean anomaly: 103
9244 deg
Mean motion: 15
53796732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1582
Checksum: 323
Coasting Arc #3 (Orbit 1597)
---------------------------------------
Vector Time (GMT): 2018/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3020892
19 A = 6780575
11 meter
Y = -3699263
58 meter E =
0005160
Z = 4812393
37 I = 51
63777
XDOT = 6862
683334 Wp = 146
72938
YDOT = -2276
952163 meter/sec RA = 177
86783 deg
ZDOT = 2552
124296 TA = 278
12335
MA = 278
18188
Ha = 220
323 n
mi
Hp = 216
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9911063
63 X = -3002677
74
Y = -12136691
52 feet Y = -3732942
87 meter
Z = 15788692
15 Z = 4797763
49
XDOT = 22515
365270 XDOT = 6875
237825
YDOT = -7470
315494 feet/sec YDOT = -2200
138371 meter/sec
ZDOT = 8373
111207 ZDOT = 2585
491851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12848309
46 X = 3916164
72
Y = 9083507
33 feet Y = 2768653
03 meter
Z = 15723298
06 Z = 4792461
25
XDOT = -19051
130706 XDOT = -5806
784639
YDOT = 12162
276870 feet/sec YDOT = 3707
061990 meter/sec
ZDOT = 8523
203167 ZDOT = 2597
872325
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 18280
55282242
00016717 00000-0 10270-3 0 9028
2 25544 51
6413 178
7672 0003696 259
0341 101
0396 15
53789450 15988
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
55282242 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 178
7672 deg
Eccentricity:
0003696
Arg of perigee: 259
0341 deg
Mean anomaly: 101
0396 deg
Mean motion: 15
53789450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1598
Checksum: 320
Coasting Arc #4 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2018/280/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6136339
31 A = 6788355
78 meter
Y = 1972673
37 meter E =
0004083
Z = -2121904
24 I = 51
66641
XDOT = -3258
866237 Wp = 4
59943
YDOT = -4210
121918 meter/sec RA = 177
26665 deg
ZDOT = 5515
004616 TA = 331
90784
MA = 331
92987
Ha = 220
117 n
mi
Hp = 216
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20132346
83 X = -6147635
05
Y = 6472025
49 feet Y = 1903989
15 meter
Z = -6961628
09 Z = -2151740
37
XDOT = -10691
818363 XDOT = -3238
334487
YDOT = -13812
735953 feet/sec YDOT = -4246
449359 meter/sec
ZDOT = 18093
847164 ZDOT = 5499
224420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5886844
39 X = 1794310
17
Y = -20264674
01 feet Y = -6176672
64 meter
Z = -7095831
09 Z = -2162809
32
XDOT = 16019
660676 XDOT = 4882
792574
YDOT = -1652
019394 feet/sec YDOT = -503
535511 meter/sec
ZDOT = 18023
329567 ZDOT = 5493
510852
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 18280
61713686
00016717 00000-0 10270-3 0 9037
2 25544 51
6400 178
4464 0003939 261
8250 98
2456 15
53780424 15997
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
61713686 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 178
4464 deg
Eccentricity:
0003939
Arg of perigee: 261
8250 deg
Mean anomaly: 98
2456 deg
Mean motion: 15
53780424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 328
Coasting Arc #5 (Orbit 1614)
---------------------------------------
Vector Time (GMT): 2018/281/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6626176
64 A = 6790182
64 meter
Y = -1342169
56 meter E =
0010655
Z = 560164
24 I = 51
70596
XDOT = 1436
718390 Wp = 144
05745
YDOT = 4574
470046 meter/sec RA = 172
30038 deg
ZDOT = -5985
075735 TA = 29
90333
MA = 29
84250
Ha = 220
126 n
mi
Hp = 216
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21739424
67 X = 6637971
66
Y = -4403443
44 feet Y = -1268005
03 meter
Z = 1837809
18 Z = 592381
14
XDOT = 4713
643013 XDOT = 1414
531344
YDOT = 15008
103826 feet/sec YDOT = 4590
411635 meter/sec
ZDOT = -19636
075245 ZDOT = -5978
151017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8166073
36 X = -2489019
16
Y = 20609578
48 feet Y = 6281799
52 meter
Z = 1982665
46 Z = 604316
43
XDOT = -13715
954820 XDOT = -4180
623029
YDOT = -3534
153641 feet/sec YDOT = -1077
210030 meter/sec
ZDOT = -19605
367523 ZDOT = -5975
716021
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 18281
64619308
00016717 00000-0 10270-3 0 9048
2 25544 51
6405 173
3199 0003941 264
0544 96
0159 15
53782177 16157
Satellite: ISS
Catalog Number: 25544
Epoch time: 18281
64619308 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 173
3199 deg
Eccentricity:
0003941
Arg of perigee: 264
0544 deg
Mean anomaly: 96
0159 deg
Mean motion: 15
53782177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1615
Checksum: 319
Coasting Arc #6 (Orbit 1630)
---------------------------------------
Vector Time (GMT): 2018/282/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6671520
05 A = 6789821
28 meter
Y = 660616
71 meter E =
0010386
Z = 1037207
57 I = 51
73669
XDOT = 440
008177 Wp = 44
25575
YDOT = -4872
574889 meter/sec RA = 167
33612 deg
ZDOT = 5905
284377 TA = 326
97288
MA = 327
03770
Ha = 220
032 n
mi
Hp = 216
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21888189
13 X = -6683449
70
Y = 2167377
66 feet Y = 585944
56 meter
Z = 3402911
97 Z = 1004770
01
XDOT = 1443
596380 XDOT = 465
776689
YDOT = -15986
138087 feet/sec YDOT = -4867
509648 meter/sec
ZDOT = 19374
292574 ZDOT = 5907
484974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9802079
95 X = 2987673
97
Y = -19714984
72 feet Y = -6009127
34 meter
Z = 3257109
99 Z = 992767
13
XDOT = 11407
098765 XDOT = 3476
883704
YDOT = 8890
080613 feet/sec YDOT = 2709
696571 meter/sec
ZDOT = 19384
611646 ZDOT = 5908
429630
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 18282
67524338
00016717 00000-0 10270-3 0 9051
2 25544 51
6395 168
1912 0004008 268
4610 91
6084 15
53816395 16313
Satellite: ISS
Catalog Number: 25544
Epoch time: 18282
67524338 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 168
1912 deg
Eccentricity:
0004008
Arg of perigee: 268
4610 deg
Mean anomaly: 91
6084 deg
Mean motion: 15
53816395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1631
Checksum: 318
Coasting Arc #7 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2018/283/14:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6282862
10 A = 6787595
23 meter
Y = 120971
23 meter E =
0003211
Z = -2560609
47 I = 51
75927
XDOT = -2248
641499 Wp = 179
17289
YDOT = 5081
031259 meter/sec RA = 162
37215 deg
ZDOT = -5280
570258 TA = 29
54193
MA = 29
52379
Ha = 220
104 n
mi
Hp = 216
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20613064
63 X = 6293480
76
Y = 396887
24 feet Y = 191289
67 meter
Z = -8400949
69 Z = -2530063
08
XDOT = -7377
432738 XDOT = -2279
641109
YDOT = 16670
050062 feet/sec YDOT = 5055
711533 meter/sec
ZDOT = -17324
705571 ZDOT = -5291
569408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11015416
13 X = -3357498
84
Y = 17492963
62 feet Y = 5331855
31 meter
Z = -8263700
14 Z = -2518775
80
XDOT = -9246
144181 XDOT = -2818
224747
YDOT = -14025
061106 feet/sec YDOT = -4274
838625 meter/sec
ZDOT = -17374
586161 ZDOT = -5295
773862
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 18283
63997708
00016717 00000-0 10270-3 0 9064
2 25544 51
6377 163
3846 0003963 272
8323 87
2376 15
53799518 16463
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
63997708 = yrday
fracday
Element set: 906
Inclination: 51
6377 deg
RA of node: 163
3846 deg
Eccentricity:
0003963
Arg of perigee: 272
8323 deg
Mean anomaly: 87
2376 deg
Mean motion: 15
53799518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 361
Coasting Arc #8 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2018/284/08:40:17
000
Vector Time (MET): N/A
Weight (LBS) : 914032
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2798630
94 A = 6778735
55 meter
Y = -3314601
56 meter E =
0002099
Z = 5209666
27 I = 51
75477
XDOT = 6630
924101 Wp = 193
53716
YDOT = -3644
195718 meter/sec RA = 158
63966 deg
ZDOT = 1241
653361 TA = 244
55270
MA = 244
57442
Ha = 220
103 n
mi
Hp = 216
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9181860
05 X = -2786664
53
Y = -10874677
04 feet Y = -3345830
45 meter
Z = 17092080
92 Z = 5196100
53
XDOT = 21755
000331 XDOT = 6665
150252
YDOT = -11956
022697 feet/sec YDOT = -3569
852647 meter/sec
ZDOT = 4073
665884 ZDOT = 1273
948246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2387879
18 X = 727825
57
Y = 14104367
51 feet Y = 4299011
22 meter
Z = 17031419
06 Z = 5191176
53
XDOT = -23754
523727 XDOT = -7240
378832
YDOT = -1080
575127 feet/sec YDOT = -329
359299 meter/sec
ZDOT = 4219
126136 ZDOT = 1285
989646
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 18284
41176263
00016717 00000-0 10270-3 0 9077
2 25544 51
6389 159
5403 0003965 275
2123 84
8577 15
53840662 16585
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
41176263 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 159
5403 deg
Eccentricity:
0003965
Arg of perigee: 275
2123 deg
Mean anomaly: 84
8577 deg
Mean motion: 15
53840662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 336
Coasting Arc #9 (Orbit 1661)
---------------------------------------
Vector Time (GMT): 2018/284/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5129321
81 A = 6782951
53 meter
Y = -1442436
52 meter E =
0006335
Z = 4193707
25 I = 51
77439
XDOT = 4452
080338 Wp = 110
19690
YDOT = -5020
506713 meter/sec RA = 157
39573 deg
ZDOT = 3711
843091 TA = 301
73588
MA = 301
79761
Ha = 220
175 n
mi
Hp = 216
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16828483
63 X = -5133182
14
Y = -4732403
27 feet Y = -1499817
41 meter
Z = 13758882
04 Z = 4168780
96
XDOT = 14606
562790 XDOT = 4489
859567
YDOT = -16471
478717 feet/sec YDOT = -4970
508932 meter/sec
ZDOT = 12177
962896 ZDOT = 3733
562394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12500287
47 X = 3810087
62
Y = -12345148
52 feet Y = -3762801
27 meter
Z = 13646994
47 Z = 4159603
91
XDOT = 6197
451279 XDOT = 1888
983150
YDOT = 19870
337646 feet/sec YDOT = 6056
478915 meter/sec
ZDOT = 12276
027459 ZDOT = 3741
733170
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 18284
66902382
00016717 00000-0 10270-3 0 9084
2 25544 51
6371 158
2564 0004071 276
3079 83
7610 15
53798704 16621
Satellite: ISS
Catalog Number: 25544
Epoch time: 18284
66902382 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 158
2564 deg
Eccentricity:
0004071
Arg of perigee: 276
3079 deg
Mean anomaly: 83
7610 deg
Mean motion: 15
53798704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1662
Checksum: 329
Coasting Arc #10 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2018/285/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3936043
34 A = 6779805
44 meter
Y = 2375962
54 meter E =
0009075
Z = -4991117
14 I = 51
79367
XDOT = -5583
552035 Wp = 64
17544
YDOT = 4798
250218 meter/sec RA = 152
41498 deg
ZDOT = -2118
232407 TA = 185
21720
MA = 185
22667
Ha = 220
113 n
mi
Hp = 216
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12913528
00 X = 3933426
88
Y = 7795152
69 feet Y = 2419963
19 meter
Z = -16375056
22 Z = -4972003
27
XDOT = -18318
740271 XDOT = -5626
502936
YDOT = 15742
290743 feet/sec YDOT = 4735
570788 meter/sec
ZDOT = -6949
581389 ZDOT = -2145
460564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13096559
73 X = -3991831
41
Y = 7668290
72 feet Y = 2337295
01 meter
Z = -16289368
24 Z = -4964999
44
XDOT = -4453
799282 XDOT = -1357
518021
YDOT = -22636
163496 feet/sec YDOT = -6899
502634 meter/sec
ZDOT = -7072
405323 ZDOT = -2155
669142
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
63375187
00016717 00000-0 10270-3 0 9090
2 25544 51
6365 153
4484 0003892 279
2110 80
8602 15
53815897 16778
Satellite: ISS
Catalog Number: 25544
Epoch time: 18285
63375187 = yrday
fracday
Element set: 909
Inclination: 51
6365 deg
RA of node: 153
4484 deg
Eccentricity:
0003892
Arg of perigee: 279
2110 deg
Mean anomaly: 80
8602 deg
Mean motion: 15
53815897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 342
Coasting Arc #11 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2018/286/14:44:01
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2569187
14 A = 6778422
08 meter
Y = -3323960
20 meter E =
0001223
Z = 5320588
15 I = 51
81736
XDOT = 6310
253006 Wp = 276
41493
YDOT = -4342
712838 meter/sec RA = 147
43066 deg
ZDOT = 334
225488 TA = 170
40727
MA = 170
40493
Ha = 220
333 n
mi
Hp = 216
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8429091
68 X = -2557671
88
Y = -10905381
23 feet Y = -3352626
02 meter
Z = 17455997
86 Z = 5308135
79
XDOT = 20702
929809 XDOT = 6356
721912
YDOT = -14247
745532 feet/sec YDOT = -4271
887371 meter/sec
ZDOT = 1096
540316 ZDOT = 364
992178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13629272
72 X = 4154202
33
Y = -2481933
80 feet Y = -756493
42 meter
Z = 17400336
70 Z = 5303622
63
XDOT = 2786
219200 XDOT = 849
239612
YDOT = 23955
723049 feet/sec YDOT = 7301
704385 meter/sec
ZDOT = 1235
251160 ZDOT = 376
504553
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
66279330
00016717 00000-0 10270-3 0 9109
2 25544 51
6363 148
3203 0003822 283
5214 76
5512 15
53776313 16933
Satellite: ISS
Catalog Number: 25544
Epoch time: 18286
66279330 = yrday
fracday
Element set: 910
Inclination: 51
6363 deg
RA of node: 148
3203 deg
Eccentricity:
0003822
Arg of perigee: 283
5214 deg
Mean anomaly: 76
5512 deg
Mean motion: 15
53776313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 306
Coasting Arc #12 (Orbit 1699)
---------------------------------------
Vector Time (GMT): 2018/287/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 600286
54 A = 6779379
18 meter
Y = 4455866
49 meter E =
0009452
Z = -5082470
53 I = 51
83579
XDOT = -6803
840702 Wp = 102
86427
YDOT = 3005
849551 meter/sec RA = 145
00080 deg
ZDOT = 1832
487390 TA = 184
84372
MA = 184
85288
Ha = 220
279 n
mi
Hp = 216
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1969444
02 X = 575103
62
Y = 14618984
54 feet Y = 4462438
31 meter
Z = -16674772
08 Z = -5079615
82
XDOT = -22322
312016 XDOT = -6845
848698
YDOT = 9861
711126 feet/sec YDOT = 2929
529470 meter/sec
ZDOT = 6012
097735 ZDOT = 1799
333921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13468691
15 X = 4105257
06
Y = 6049913
12 feet Y = 1844013
52 meter
Z = -16662363
36 Z = -5078688
35
XDOT = -3166
947285 XDOT = -965
285532
YDOT = 23190
015274 feet/sec YDOT = 7068
316655 meter/sec
ZDOT = 5862
772375 ZDOT = 1786
973020
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
11299631
00016717 00000-0 10270-3 0 9117
2 25544 51
6378 146
0800 0003765 285
7956 74
2782 15
53796193 17001
Satellite: ISS
Catalog Number: 25544
Epoch time: 18287
11299631 = yrday
fracday
Element set: 911
Inclination: 51
6378 deg
RA of node: 146
0800 deg
Eccentricity:
0003765
Arg of perigee: 285
7956 deg
Mean anomaly: 74
2782 deg
Mean motion: 15
53796193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1700
Checksum: 332
Coasting Arc #13 (Orbit 1715)
---------------------------------------
Vector Time (GMT): 2018/288/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 799769
07 A = 6782098
65 meter
Y = -5133585
28 meter E =
0006959
Z = 4357289
59 I = 51
87097
XDOT = 6555
021773 Wp = 51
10820
YDOT = -1935
610475 meter/sec RA = 140
02410 deg
ZDOT = -3475
630802 TA = 74
11611
MA = 74
03942
Ha = 220
231 n
mi
Hp = 216
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2623914
26 X = 835949
05
Y = -16842471
40 feet Y = -5124439
27 meter
Z = 14295569
52 Z = 4361262
70
XDOT = 21505
976945 XDOT = 6593
062180
YDOT = -6350
428068 feet/sec YDOT = -1862
095088 meter/sec
ZDOT = -11402
988195 ZDOT = -3443
695805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13076033
59 X = -3985575
04
Y = -10910813
03 feet Y = -3325615
81 meter
Z = 14313929
64 Z = 4362885
75
XDOT = 4990
485272 XDOT = 1521
099911
YDOT = -20786
166664 feet/sec YDOT = -6335
623599 meter/sec
ZDOT = -11259
220691 ZDOT = -3431
810467
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
14203298
00016717 00000-0 10270-3 0 9126
2 25544 51
6369 140
9521 0003886 290
0721 70
0013 15
53839522 17169
Satellite: ISS
Catalog Number: 25544
Epoch time: 18288
14203298 = yrday
fracday
Element set: 912
Inclination: 51
6369 deg
RA of node: 140
9521 deg
Eccentricity:
0003886
Arg of perigee: 290
0721 deg
Mean anomaly: 70
0013 deg
Mean motion: 15
53839522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1716
Checksum: 299
Coasting Arc #14 (Orbit 1730)
---------------------------------------
Vector Time (GMT): 2018/289/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2017183
22 A = 6785728
95 meter
Y = 5606862
68 meter E =
0002519
Z = -3245179
15 I = 51
90830
XDOT = -5949
334304 Wp = 29
78329
YDOT = 630
801822 meter/sec RA = 135
05847 deg
ZDOT = 4791
659809 TA = 292
79261
MA = 292
81922
Ha = 220
425 n
mi
Hp = 216
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6618055
18 X = -2063967
21
Y = 18395218
77 feet Y = 5584043
44 meter
Z = -10646913
22 Z = -3255091
88
XDOT = -19518
813333 XDOT = -5979
221614
YDOT = 2069
559782 feet/sec YDOT = 564
105286 meter/sec
ZDOT = 15720
668666 ZDOT = 4762
686999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12574011
58 X = 3832558
73
Y = 14937002
89 feet Y = 4552798
48 meter
Z = -10692037
52 Z = -3258933
04
XDOT = -7028
674169 XDOT = -2142
339887
YDOT = 17067
747960 feet/sec YDOT = 5202
249578 meter/sec
ZDOT = 15590
328437 ZDOT = 4751
932108
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
10675319
00016717 00000-0 10270-3 0 9131
2 25544 51
6376 136
1456 0003710 295
6538 64
4231 15
53817957 17318
Satellite: ISS
Catalog Number: 25544
Epoch time: 18289
10675319 = yrday
fracday
Element set: 913
Inclination: 51
6376 deg
RA of node: 136
1456 deg
Eccentricity:
0003710
Arg of perigee: 295
6538 deg
Mean anomaly: 64
4231 deg
Mean motion: 15
53817957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1731
Checksum: 323
Coasting Arc #15 (Orbit 1746)
---------------------------------------
Vector Time (GMT): 2018/290/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3025197
22 A = 6788710
96 meter
Y = -5795497
27 meter E =
0010052
Z = 1812676
17 I = 51
94067
XDOT = 5079
735234 Wp = 111
47034
YDOT = 869
023415 meter/sec RA = 130
10238 deg
ZDOT = -5677
529994 TA = 48
69271
MA = 48
60622
Ha = 220
466 n
mi
Hp = 216
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9925187
72 X = 3080974
11
Y = -19014098
64 feet Y = -5761355
47 meter
Z = 5947100
29 Z = 1827507
40
XDOT = 16665
798011 XDOT = 5097
218807
YDOT = 2851
126689 feet/sec YDOT = 925
926076 meter/sec
ZDOT = -18627
066910 ZDOT = -5652
811682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11733602
18 X = -3576401
95
Y = -17932182
56 feet Y = -5465729
24 meter
Z = 6014375
18 Z = 1833181
55
XDOT = 9401
285116 XDOT = 2865
511703
YDOT = -12385
308037 feet/sec YDOT = -3775
041890 meter/sec
ZDOT = -18515
993314 ZDOT = -5643
674762
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
13578384
00016717 00000-0 10270-3 0 9141
2 25544 51
6370 131
0175 0003940 301
1971 58
8795 15
53851693 17477
Satellite: ISS
Catalog Number: 25544
Epoch time: 18290
13578384 = yrday
fracday
Element set: 914
Inclination: 51
6370 deg
RA of node: 131
0175 deg
Eccentricity:
0003940
Arg of perigee: 301
1971 deg
Mean anomaly: 58
8795 deg
Mean motion: 15
53851693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1747
Checksum: 322
Coasting Arc #16 (Orbit 1761)
---------------------------------------
Vector Time (GMT): 2018/291/02:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3753164
18 A = 6790067
22 meter
Y = 5645460
00 meter E =
0011421
Z = -232662
08 I = 51
96533
XDOT = -4049
998202 Wp = 24
97183
YDOT = -2448
606297 meter/sec RA = 125
15482 deg
ZDOT = 6035
268142 TA = 332
53228
MA = 332
59260
Ha = 220
496 n
mi
Hp = 216
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12313530
77 X = -3814884
18
Y = 18521850
40 feet Y = 5603144
40 meter
Z = -763327
03 Z = -251044
02
XDOT = -13287
395677 XDOT = -4051
632665
YDOT = -8033
485225 feet/sec YDOT = -2493
905036 meter/sec
ZDOT = 19800
748497 ZDOT = 6015
590595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10457107
32 X = 3187326
31
Y = 19626433
06 feet Y = 5982136
80 meter
Z = -846570
75 Z = -258034
76
XDOT = -12008
991566 XDOT = -3660
340629
YDOT = 7233
746078 feet/sec YDOT = 2204
845805 meter/sec
ZDOT = 19712
495574 ZDOT = 6008
368651
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
10049954
00016717 00000-0 10270-3 0 9156
2 25544 51
6366 126
2114 0003736 301
6189 58
4599 15
53864957 17622
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
10049954 = yrday
fracday
Element set: 915
Inclination: 51
6366 deg
RA of node: 126
2114 deg
Eccentricity:
0003736
Arg of perigee: 301
6189 deg
Mean anomaly: 58
4599 deg
Mean motion: 15
53864957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1762
Checksum: 332
Coasting Arc #17 (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 = 477205
86 A = 6782879
74 meter
Y = 5338608
06 meter E =
0003979
Z = -4160678
60 I = 51
95418
XDOT = -5693
338049 Wp = 100
60521
YDOT = 3458
971912 meter/sec RA = 122
29972 deg
ZDOT = 3787
603186 TA = 208
25847
MA = 208
28006
Ha = 220
494 n
mi
Hp = 216
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1565636
02 X = 437683
19
Y = 17515118
31 feet Y = 5343723
29 meter
Z = -13650520
35 Z = -4158456
77
XDOT = -18678
930608 XDOT = -5749
992469
YDOT = 11348
333045 feet/sec YDOT = 3394
988488 meter/sec
ZDOT = 12426
519639 ZDOT = 3759
808838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17570238
91 X = -5355408
82
Y = 880445
07 feet Y = 268359
66 meter
Z = -13641070
80 Z = -4157798
38
XDOT = -10444
435826 XDOT = -3183
464040
YDOT = -17963
382859 feet/sec YDOT = -5475
239095 meter/sec
ZDOT = 12301
155331 ZDOT = 3749
392145
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
67932771
00016717 00000-0 10270-3 0 9167
2 25544 51
6390 123
3232 0003817 298
9817 61
0953 15
53827758 17716
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
67932771 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 123
3232 deg
Eccentricity:
0003817
Arg of perigee: 298
9817 deg
Mean anomaly: 61
0953 deg
Mean motion: 15
53827758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1771
Checksum: 337
Coasting Arc #18 (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 = 548316
83 A = 6786504
09 meter
Y = -6082837
36 meter E =
0009978
Z = 2950596
66 I = 51
98357
XDOT = 5442
605563 Wp = 88
70282
YDOT = -1958
377906 meter/sec RA = 117
34027 deg
ZDOT = -5033
857357 TA = 57
78225
MA = 57
68556
Ha = 220
584 n
mi
Hp = 216
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1798939
73 X = 601963
45
Y = -19956815
49 feet Y = -6076405
54 meter
Z = 9680435
24 Z = 2953390
94
XDOT = 17856
317463 XDOT = 5488
552284
YDOT = -6425
124363 feet/sec YDOT = -1897
258356 meter/sec
ZDOT = -16515
280043 ZDOT = -5007
307039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19901958
13 X = 6066116
84
Y = 2273114
38 feet Y = 692845
26 meter
Z = 9693632
38 Z = 2954619
15
XDOT = 6104
252004 XDOT = 1860
576011
YDOT = 16681
614938 feet/sec YDOT = 5084
556233 meter/sec
ZDOT = -16395
652204 ZDOT = -4997
394792
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
70835221
00016717 00000-0 10270-3 0 9175
2 25544 51
6395 118
1952 0003716 303
2029 56
8767 15
53828079 17874
Satellite: ISS
Catalog Number: 25544
Epoch time: 18292
70835221 = yrday
fracday
Element set: 917
Inclination: 51
6395 deg
RA of node: 118
1952 deg
Eccentricity:
0003716
Arg of perigee: 303
2029 deg
Mean anomaly: 56
8767 deg
Mean motion: 15
53828079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 333
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