[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 21st 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21814 1409 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
325/21:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
1
331/13:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 212
9
337/11:31:53
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
0
337/17:35:42
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
1
337/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
0
338/16:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 2296)
---------------------------------------
Vector Time (GMT): 2018/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1690976
09 A = 6784919
85 meter
Y = -5634796
18 meter E =
0009988
Z = -3386268
90 I = 51
37012
XDOT = 6045
936927 Wp = 77
53994
YDOT = -947
306068 meter/sec RA = 314
09038 deg
ZDOT = 4609
090029 TA = 242
77362
MA = 242
87543
Ha = 223
123 n
mi
Hp = 213
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5547821
82 X = 1770309
43
Y = -18486864
09 feet Y = -5615442
81 meter
Z = -11109806
10 Z = -3377862
01
XDOT = 19835
751073 XDOT = 6033
691489
YDOT = -3107
959541 feet/sec YDOT = -879
764832 meter/sec
ZDOT = 15121
686446 ZDOT = 4638
430108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13090968
07 X = 3990127
07
Y = 14213531
61 feet Y = 4332284
43 meter
Z = -11071239
18 Z = -3374513
70
XDOT = -6283
497718 XDOT = -1915
210104
YDOT = 17633
688568 feet/sec YDOT = 5374
748275 meter/sec
ZDOT = 15253
693412 ZDOT = 4649
325752
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 18325
50703682
00016717 00000-0 10270-3 0 9007
2 25544 51
6380 314
7496 0005342 68
6513 291
5209 15
53984737 22972
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
50703682 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 314
7496 deg
Eccentricity:
0005342
Arg of perigee: 68
6513 deg
Mean anomaly: 291
5209 deg
Mean motion: 15
53984737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2297
Checksum: 323
Coasting Arc #2 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/325/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4228975
48 A = 6778602
35 meter
Y = 1405510
13 meter E =
0008722
Z = 5100460
55 I = 51
34097
XDOT = -4021
619633 Wp = 95
15022
YDOT = 6341
693237 meter/sec RA = 312
09471 deg
ZDOT = 1583
809583 TA = 339
50805
MA = 339
54302
Ha = 222
911 n
mi
Hp = 213
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13874591
47 X = 4188168
34
Y = 4611253
71 feet Y = 1452573
07 meter
Z = 16733794
47 Z = 5120904
96
XDOT = -13194
290133 XDOT = -4099
928843
YDOT = 20806
080173 feet/sec YDOT = 6296
282766 meter/sec
ZDOT = 5196
225667 ZDOT = 1564
083496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14384940
05 X = 4384529
73
Y = -1940146
68 feet Y = -591356
71 meter
Z = 16825491
29 Z = 5128409
75
XDOT = -2820
721683 XDOT = -859
755969
YDOT = 23460
754627 feet/sec YDOT = 7150
838010 meter/sec
ZDOT = 5106
687074 ZDOT = 1556
518220
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 18325
95718899
00016717 00000-0 10270-3 0 9013
2 25544 51
6392 312
5047 0005116 67
8216 292
3479 15
53971502 23046
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
95718899 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 312
5047 deg
Eccentricity:
0005116
Arg of perigee: 67
8216 deg
Mean anomaly: 292
3479 deg
Mean motion: 15
53971502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 323
Coasting Arc #3 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2018/326/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3181614
07 A = 6777741
90 meter
Y = -2821706
11 meter E =
0019696
Z = -5294649
03 I = 51
31508
XDOT = 4796
493697 Wp = 87
05568
YDOT = -5957
110095 meter/sec RA = 307
07356 deg
ZDOT = 294
431718 TA = 185
75774
MA = 185
78042
Ha = 223
012 n
mi
Hp = 212
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10438366
37 X = -3124105
19
Y = -9257565
99 feet Y = -2856963
21 meter
Z = -17370895
76 Z = -5309965
14
XDOT = 15736
527876 XDOT = 4861
321045
YDOT = -19544
324459 feet/sec YDOT = -5903
109919 meter/sec
ZDOT = 965
983327 ZDOT = 317
889099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13412847
73 X = -4088235
99
Y = -3517769
29 feet Y = -1072216
08 meter
Z = -17439347
90 Z = -5315513
24
XDOT = 4802
238679 XDOT = 1463
722349
YDOT = -23594
492425 feet/sec YDOT = -7191
601291 meter/sec
ZDOT = 1072
233355 ZDOT = 326
816727
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 18326
92179704
00016717 00000-0 10270-3 0 9028
2 25544 51
6374 307
6958 0005118 72
2654 287
9057 15
54010201 23199
Satellite: ISS
Catalog Number: 25544
Epoch time: 18326
92179704 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 307
6958 deg
Eccentricity:
0005118
Arg of perigee: 72
2654 deg
Mean anomaly: 287
9057 deg
Mean motion: 15
54010201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2319
Checksum: 311
Coasting Arc #4 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2018/327/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2055374
66 A = 6779303
68 meter
Y = 4163228
18 meter E =
0011175
Z = 4932565
41 I = 51
30166
XDOT = -5261
263053 Wp = 65
35359
YDOT = 5155
737642 meter/sec RA = 302
05319 deg
ZDOT = -2150
822811 TA = 45
73867
MA = 45
64701
Ha = 222
918 n
mi
Hp = 213
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6743355
20 X = 1984707
13
Y = 13658885
11 feet Y = 4185817
23 meter
Z = 16182957
38 Z = 4942378
70
XDOT = -17261
361722 XDOT = -5308
077100
YDOT = 16915
149743 feet/sec YDOT = 5096
640989 meter/sec
ZDOT = -7056
505285 ZDOT = -2176
494071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12299901
31 X = 3749009
92
Y = 8907263
08 feet Y = 2714933
79 meter
Z = 16226496
34 Z = 4945836
09
XDOT = -6535
948080 XDOT = -1992
156975
YDOT = 22142
044694 feet/sec YDOT = 6748
895223 meter/sec
ZDOT = -7172
591618 ZDOT = -2186
205925
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 18327
95070992
00016717 00000-0 10270-3 0 9032
2 25544 51
6380 302
5675 0004951 76
1528 284
0175 15
54000846 23354
Satellite: ISS
Catalog Number: 25544
Epoch time: 18327
95070992 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 302
5675 deg
Eccentricity:
0004951
Arg of perigee: 76
1528 deg
Mean anomaly: 284
0175 deg
Mean motion: 15
54000846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 310
Coasting Arc #5 (Orbit 2349)
---------------------------------------
Vector Time (GMT): 2018/328/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -986428
27 A = 6782469
90 meter
Y = -5312953
73 meter E =
0012184
Z = -4110559
56 I = 51
29554
XDOT = 5392
699483 Wp = 97
35996
YDOT = -3914
694289 meter/sec RA = 297
03691 deg
ZDOT = 3773
807147 TA = 211
76133
MA = 211
83488
Ha = 223
006 n
mi
Hp = 212
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3236313
21 X = -906976
68
Y = -17430950
57 feet Y = -5323539
98 meter
Z = -13486087
81 Z = -4115158
98
XDOT = 17692
583605 XDOT = 5417
742353
YDOT = -12843
485200 feet/sec YDOT = -3854
249761 meter/sec
ZDOT = 12381
257045 ZDOT = 3800
063953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11242872
93 X = -3426827
67
Y = -13688350
65 feet Y = -4172209
28 meter
Z = -13506042
73 Z = -4116641
82
XDOT = 8120
009867 XDOT = 2474
979007
YDOT = -18976
414975 feet/sec YDOT = -5784
011284 meter/sec
ZDOT = 12499
804159 ZDOT = 3809
940308
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 18328
91531186
00016717 00000-0 10270-3 0 9047
2 25544 51
6378 297
7584 0005081 80
6371 279
5355 15
54020878 23509
Satellite: ISS
Catalog Number: 25544
Epoch time: 18328
91531186 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 297
7584 deg
Eccentricity:
0005081
Arg of perigee: 80
6371 deg
Mean anomaly: 279
5355 deg
Mean motion: 15
54020878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2350
Checksum: 330
Coasting Arc #6 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2018/329/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -40956
36 A = 6786175
97 meter
Y = 6157315
80 meter E =
0018169
Z = 2834862
61 I = 51
29398
XDOT = -5297
271760 Wp = 94
88616
YDOT = 2302
159851 meter/sec RA = 292
03049 deg
ZDOT = -5050
329133 TA = 52
70847
MA = 52
54297
Ha = 222
928 n
mi
Hp = 212
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -134371
26 X = -123576
61
Y = 20201167
31 feet Y = 6156395
51 meter
Z = 9300730
36 Z = 2834463
68
XDOT = -17379
500525 XDOT = -5298
089254
YDOT = 7553
017885 feet/sec YDOT = 2242
918082 meter/sec
ZDOT = -16569
321302 ZDOT = -5076
063550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9977525
35 X = 3041149
73
Y = 17567095
48 feet Y = 5354450
70 meter
Z = 9298115
17 Z = 2834065
50
XDOT = -9857
980981 XDOT = -3004
712603
YDOT = 14476
406865 feet/sec YDOT = 4412
408813 meter/sec
ZDOT = -16685
303420 ZDOT = -5085
680482
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 18329
94421444
00016717 00000-0 10270-3 0 9057
2 25544 51
6378 292
6299 0004955 83
0576 277
1140 15
54042480 23665
Satellite: ISS
Catalog Number: 25544
Epoch time: 18329
94421444 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 292
6299 deg
Eccentricity:
0004955
Arg of perigee: 83
0576 deg
Mean anomaly: 277
1140 deg
Mean motion: 15
54042480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 326
Coasting Arc #7 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2018/330/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 911940
34 A = 6788888
88 meter
Y = -6593268
76 meter E =
0012732
Z = -1321777
09 I = 51
29078
XDOT = 4997
787683 Wp = 56
15530
YDOT = -460
858106 meter/sec RA = 287
03226 deg
ZDOT = 5794
241551 TA = 289
39014
MA = 289
52772
Ha = 223
053 n
mi
Hp = 212
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2991930
26 X = 992020
90
Y = -21631459
20 feet Y = -6582622
91 meter
Z = -4336539
00 Z = -1317153
36
XDOT = 16396
941216 XDOT = 4974
424049
YDOT = -1512
001661 feet/sec YDOT = -405
100633 meter/sec
ZDOT = 19009
978842 ZDOT = 5818
462506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8600123
23 X = -2621317
56
Y = -20077272
24 feet Y = -6119552
58 meter
Z = -4314888
65 Z = -1315178
06
XDOT = 11680
721671 XDOT = 3560
283965
YDOT = -9078
894391 feet/sec YDOT = -2767
247010 meter/sec
ZDOT = 19118
916588 ZDOT = 5827
445776
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 18330
90881032
00016717 00000-0 10270-3 0 9069
2 25544 51
6371 287
8223 0005183 89
2439 270
9307 15
54025767 23813
Satellite: ISS
Catalog Number: 25544
Epoch time: 18330
90881032 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 287
8223 deg
Eccentricity:
0005183
Arg of perigee: 89
2439 deg
Mean anomaly: 270
9307 deg
Mean motion: 15
54025767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2381
Checksum: 316
Coasting Arc #8 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2018/331/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1697061
71 A = 6789594
83 meter
Y = -6567038
62 meter E =
0016527
Z = 99764
28 I = 51
28934
XDOT = 4619
344294 Wp = 58
30402
YDOT = 1295
625829 meter/sec RA = 283
81402 deg
ZDOT = 5982
972441 TA = 302
77592
MA = 302
93505
Ha = 223
014 n
mi
Hp = 212
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5567787
75 X = 1769885
43
Y = -21545402
28 feet Y = -6547653
72 meter
Z = 327310
63 Z = 108184
30
XDOT = 15155
329048 XDOT = 4575
450609
YDOT = 4250
740908 feet/sec YDOT = 1347
036530 meter/sec
ZDOT = 19629
174675 ZDOT = 6005
305282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20882609
39 X = 6365019
34
Y = 7687288
96 feet Y = 2343085
68 meter
Z = 366013
13 Z = 111560
80
XDOT = -5169
394465 XDOT = -1575
631433
YDOT = 13002
216603 feet/sec YDOT = 3963
075621 meter/sec
ZDOT = 19729
399598 ZDOT = 6013
520997
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 18331
61617747
00016717 00000-0 10270-3 0 9079
2 25544 51
6391 284
3003 0005132 88
1499 272
0241 15
54036012 23928
Satellite: ISS
Catalog Number: 25544
Epoch time: 18331
61617747 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 284
3003 deg
Eccentricity:
0005132
Arg of perigee: 88
1499 deg
Mean anomaly: 272
0241 deg
Mean motion: 15
54036012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 291
Coasting Arc #9 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2018/332/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2392005
70 A = 6788203
99 meter
Y = 6095953
34 meter E =
0011330
Z = -1782560
32 I = 51
27886
XDOT = -4068
611073 Wp = 120
57104
YDOT = -3234
200140 meter/sec RA = 278
81859 deg
ZDOT = -5633
051017 TA = 79
10180
MA = 78
97433
Ha = 223
000 n
mi
Hp = 212
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7847787
74 X = -2451335
81
Y = 19999846
91 feet Y = 6068872
67 meter
Z = -5848295
03 Z = -1794323
53
XDOT = -13348
461525 XDOT = -4004
780454
YDOT = -10610
892847 feet/sec YDOT = -3279
340835 meter/sec
ZDOT = -18481
138508 ZDOT = -5652
660221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19285697
21 X = -5878280
51
Y = -9434673
47 feet Y = -2875688
47 meter
Z = -5901950
82 Z = -1798914
61
XDOT = 10980
900242 XDOT = 3346
978394
YDOT = -10896
456085 feet/sec YDOT = -3321
239815 meter/sec
ZDOT = -18568
881030 ZDOT = -5659
794938
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 18332
58076422
00016717 00000-0 10270-3 0 9086
2 25544 51
6401 279
4921 0005159 90
2711 269
9033 15
54041815 24072
Satellite: ISS
Catalog Number: 25544
Epoch time: 18332
58076422 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 279
4921 deg
Eccentricity:
0005159
Arg of perigee: 90
2711 deg
Mean anomaly: 269
9033 deg
Mean motion: 15
54041815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 302
Coasting Arc #10 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2018/333/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2945199
60 A = 6785087
06 meter
Y = -5177266
83 meter E =
0017898
Z = 3233626
74 I = 51
26354
XDOT = 3472
977611 Wp = 89
18159
YDOT = 4944
012500 meter/sec RA = 273
81713 deg
ZDOT = 4730
021915 TA = 308
52774
MA = 308
68805
Ha = 222
975 n
mi
Hp = 212
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9662728
35 X = 2987167
04
Y = -16985783
58 feet Y = -5144097
09 meter
Z = 10609011
62 Z = 3248035
20
XDOT = 11394
283502 XDOT = 3394
458119
YDOT = 16220
513451 feet/sec YDOT = 4982
410454 meter/sec
ZDOT = 15518
444603 ZDOT = 4746
702071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16320414
51 X = 4974462
34
Y = 10683487
17 feet Y = 3256326
89 meter
Z = 10674430
30 Z = 3253566
36
XDOT = -16147
166724 XDOT = -4921
656417
YDOT = 9014
012706 feet/sec YDOT = 2747
471073 meter/sec
ZDOT = 15592
818974 ZDOT = 4752
691223
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 18333
60965267
00016717 00000-0 10270-3 0 9095
2 25544 51
6392 274
3644 0005198 94
1164 266
0582 15
54043782 24235
Satellite: ISS
Catalog Number: 25544
Epoch time: 18333
60965267 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 274
3644 deg
Eccentricity:
0005198
Arg of perigee: 94
1164 deg
Mean anomaly: 266
0582 deg
Mean motion: 15
54043782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 324
Coasting Arc #11 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/334/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3454919
31 A = 6781211
04 meter
Y = 3843569
86 meter E =
0013911
Z = -4403752
50 I = 51
25044
XDOT = -2795
904211 Wp = 79
39183
YDOT = -6308
504403 meter/sec RA = 268
80496 deg
ZDOT = -3318
986789 TA = 156
87420
MA = 156
81153
Ha = 222
958 n
mi
Hp = 212
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11335037
10 X = -3476251
17
Y = 12610137
33 feet Y = 3804815
45 meter
Z = -14448006
87 Z = -4420587
06
XDOT = -9172
914079 XDOT = -2709
030968
YDOT = -20697
192924 feet/sec YDOT = -6339
284280 meter/sec
ZDOT = -10889
064269 ZDOT = -3332
357649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12051396
09 X = -3673265
53
Y = -11834533
99 feet Y = -3607165
96 meter
Z = -14524158
83 Z = -4426963
61
XDOT = 20250
484678 XDOT = 6172
347730
YDOT = -7210
787744 feet/sec YDOT = -2197
848104 meter/sec
ZDOT = -10948
410352 ZDOT = -3337
075475
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 18334
57423192
00016717 00000-0 10270-3 0 9100
2 25544 51
6399 269
5565 0005168 97
2470 262
9270 15
54069753 24382
Satellite: ISS
Catalog Number: 25544
Epoch time: 18334
57423192 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 269
5565 deg
Eccentricity:
0005168
Arg of perigee: 97
2470 deg
Mean anomaly: 262
9270 deg
Mean motion: 15
54069753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 336
Coasting Arc #12 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/335/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3865501
20 A = 6778321
22 meter
Y = -2243251
86 meter E =
0009786
Z = 5089350
59 I = 51
24286
XDOT = 2075
379773 Wp = 113
51169
YDOT = 7213
676339 meter/sec RA = 263
78364 deg
ZDOT = 1597
002386 TA = 320
97564
MA = 321
04621
Ha = 222
750 n
mi
Hp = 212
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12682090
54 X = 3865576
96
Y = -7359750
19 feet Y = -2200024
87 meter
Z = 16697344
47 Z = 5108128
15
XDOT = 6808
988756 XDOT = 1986
802711
YDOT = 23666
917123 feet/sec YDOT = 7236
389364 meter/sec
ZDOT = 5239
509141 ZDOT = 1606
869040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6963716
50 X = 2122540
79
Y = 12793460
58 feet Y = 3899446
78 meter
Z = 16782034
28 Z = 5115164
05
XDOT = -22933
750172 XDOT = -6990
207052
YDOT = 5526
260000 feet/sec YDOT = 1684
404048 meter/sec
ZDOT = 5283
009587 ZDOT = 1610
261322
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 18335
60311058
00016717 00000-0 10270-3 0 9113
2 25544 51
6400 264
4281 0005027 102
1888 257
9828 15
54088379 24543
Satellite: ISS
Catalog Number: 25544
Epoch time: 18335
60311058 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 264
4281 deg
Eccentricity:
0005027
Arg of perigee: 102
1888 deg
Mean anomaly: 257
9828 deg
Mean motion: 15
54088379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 310
Coasting Arc #13 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/336/13:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4231941
39 A = 6777536
35 meter
Y = 485865
67 meter E =
0019888
Z = -5288888
20 I = 51
24557
XDOT = -1249
505654 Wp = 95
36258
YDOT = -7544
795745 meter/sec RA = 258
75671 deg
ZDOT = 305
868336 TA = 177
57972
MA = 177
57008
Ha = 222
930 n
mi
Hp = 212
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13884322
14 X = -4211368
98
Y = 1594047
46 feet Y = 438656
36 meter
Z = -17351995
40 Z = -5309395
79
XDOT = -4099
427999 XDOT = -1166
530538
YDOT = -24753
266880 feet/sec YDOT = -7558
304653 meter/sec
ZDOT = 1003
505041 ZDOT = 299
999873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1400877
94 X = -426987
60
Y = -13789220
53 feet Y = -4202954
42 meter
Z = -17444256
11 Z = -5317009
26
XDOT = 23802
443124 XDOT = 7254
984664
YDOT = -3658
795585 feet/sec YDOT = -1115
200894 meter/sec
ZDOT = 978
003292 ZDOT = 298
095403
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 18336
56768195
00016717 00000-0 10270-3 0 9128
2 25544 51
6408 259
6199 0005138 103
8886 256
2838 15
54078601 24690
Satellite: ISS
Catalog Number: 25544
Epoch time: 18336
56768195 = yrday
fracday
Element set: 912
Inclination: 51
6408 deg
RA of node: 259
6199 deg
Eccentricity:
0005138
Arg of perigee: 103
8886 deg
Mean anomaly: 256
2838 deg
Mean motion: 15
54078601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 352
Coasting Arc #14 (Orbit 2483)
---------------------------------------
Vector Time (GMT): 2018/337/11:31:53
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3217909
79 A = 6778784
61 meter
Y = -3281536
70 meter E =
0010868
Z = 4975929
97 I = 51
25534
XDOT = 3526
542437 Wp = 116
99754
YDOT = 6513
506366 meter/sec RA = 254
12417 deg
ZDOT = 2006
696055 TA = 313
36796
MA = 313
45844
Ha = 222
705 n
mi
Hp = 212
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10557446
82 X = 3230194
86
Y = -10766196
51 feet Y = -3245483
32 meter
Z = 16325229
55 Z = 4991591
40
XDOT = 11570
021120 XDOT = 3443
696861
YDOT = 21369
771543 feet/sec YDOT = 6552
479309 meter/sec
ZDOT = 6583
648473 ZDOT = 2023
626112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5178367
24 X = 1578366
33
Y = 14079723
45 feet Y = 4291499
71 meter
Z = 16396026
68 Z = 4997508
93
XDOT = -23227
105874 XDOT = -7079
621870
YDOT = 756
786060 feet/sec YDOT = 230
668391 meter/sec
ZDOT = 6659
018271 ZDOT = 2029
668769
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 18337
53224840
00016717 00000-0 10270-3 0 9131
2 25544 51
6393 254
8121 0004976 109
0989 251
0703 15
54103919 24848
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
53224840 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 254
8121 deg
Eccentricity:
0004976
Arg of perigee: 109
0989 deg
Mean anomaly: 251
0703 deg
Mean motion: 15
54103919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2484
Checksum: 313
Coasting Arc #15 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/17:35:42
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1435224
74 A = 6783556
25 meter
Y = -5478380
22 meter E =
0016359
Z = 3722750
41 I = 51
27165
XDOT = 4846
665645 Wp = 100
33325
YDOT = 4166
838402 meter/sec RA = 252
86586 deg
ZDOT = 4244
540824 TA = 304
42530
MA = 304
57983
Ha = 222
745 n
mi
Hp = 213
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4708742
60 X = 1478295
40
Y = -17973688
37 feet Y = -5462089
89 meter
Z = 12213748
08 Z = 3729826
71
XDOT = 15901
134007 XDOT = 4779
092598
YDOT = 13670
729666 feet/sec YDOT = 4220
659160 meter/sec
ZDOT = 13925
658870 ZDOT = 4267
920705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11653414
33 X = 3551960
69
Y = -14444029
47 feet Y = -4402540
18 meter
Z = 12246196
14 Z = 3732640
58
XDOT = 7675
436312 XDOT = 2339
472988
YDOT = 18140
192794 feet/sec YDOT = 5529
130764 meter/sec
ZDOT = 14030
302918 ZDOT = 4276
436329
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 18337
78946501
00016717 00000-0 10270-3 0 9144
2 25544 51
6376 253
5281 0004818 110
8173 249
3496 15
54081005 24886
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78946501 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 253
5281 deg
Eccentricity:
0004818
Arg of perigee: 110
8173 deg
Mean anomaly: 249
3496 deg
Mean motion: 15
54081005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 324
Coasting Arc #16 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4159302
41 A = 6784350
45 meter
Y = 4101119
00 meter E =
0016864
Z = 3434707
83 I = 51
27488
XDOT = -1999
130654 Wp = 95
20887
YDOT = 5850
300518 meter/sec RA = 252
72918 deg
ZDOT = -4546
717836 TA = 44
27075
MA = 44
13597
Ha = 222
669 n
mi
Hp = 213
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13646005
28 X = 4096449
15
Y = 13455114
82 feet Y = 4147279
61 meter
Z = 11268726
48 Z = 3454760
15
XDOT = -6558
827605 XDOT = -2042
315851
YDOT = 19193
899338 feet/sec YDOT = 5827
703604 meter/sec
ZDOT = -14917
053269 ZDOT = -4556
533691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8639229
81 X = 2633237
25
Y = 17046637
58 feet Y = 5195815
14 meter
Z = 11358416
55 Z = 3462045
36
XDOT = -10934
898086 XDOT = -3332
956937
YDOT = 15549
710978 feet/sec YDOT = 4739
551906 meter/sec
ZDOT = -14961
861912 ZDOT = -4560
375511
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 18337
78946447
00016717 00000-0 10270-3 0 9154
2 25544 51
6378 253
5270 0004805 110
7827 249
3841 15
54091348 24882
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78946447 = yrday
fracday
Element set: 915
Inclination: 51
6378 deg
RA of node: 253
5270 deg
Eccentricity:
0004805
Arg of perigee: 110
7827 deg
Mean anomaly: 249
3841 deg
Mean motion: 15
54091348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 340
Coasting Arc #17 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2018/338/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2890859
35 A = 6778806
14 meter
Y = 3569013
00 meter E =
0016878
Z = -5000759
18 I = 51
26773
XDOT = -4155
253761 Wp = 85
23304
YDOT = -6120
482645 meter/sec RA = 248
16285 deg
ZDOT = -1970
459426 TA = 165
52550
MA = 165
47710
Ha = 222
747 n
mi
Hp = 212
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9484446
70 X = -2906262
72
Y = 11709360
23 feet Y = 3536599
60 meter
Z = -16406690
24 Z = -5014839
41
XDOT = -13632
722314 XDOT = -4076
932363
YDOT = -20080
323637 feet/sec YDOT = -6166
511530 meter/sec
ZDOT = -6464
761897 ZDOT = -1990
454728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14939469
98 X = -4553550
45
Y = 1334603
06 feet Y = 406787
01 meter
Z = -16470409
90 Z = -5020180
94
XDOT = 5189
333957 XDOT = 1581
708990
YDOT = -22616
723620 feet/sec YDOT = -6893
577359 meter/sec
ZDOT = -6553
976452 ZDOT = -1997
652022
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 18338
68972406
00016717 00000-0 10270-3 0 9169
2 25544 51
6394 249
0415 0004799 112
3616 247
8046 15
54084447 25026
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
68972406 = yrday
fracday
Element set: 916
Inclination: 51
6394 deg
RA of node: 249
0415 deg
Eccentricity:
0004799
Arg of perigee: 112
3616 deg
Mean anomaly: 247
8046 deg
Mean motion: 15
54084447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 329
Coasting Arc #18 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2018/339/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3732031
38 A = 6777528
37 meter
Y = -2007391
81 meter E =
0007261
Z = 5283425
44 I = 51
27664
XDOT = 3532
049879 Wp = 109
21978
YDOT = 6812
394111 meter/sec RA = 243
13887 deg
ZDOT = 90
937154 TA = 339
89565
MA = 339
92423
Ha = 222
684 n
mi
Hp = 213
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12244197
44 X = 3728536
69
Y = -6585931
15 feet Y = -1965677
64 meter
Z = 17334072
96 Z = 5301546
01
XDOT = 11588
090155 XDOT = 3455
167540
YDOT = 22350
374381 feet/sec YDOT = 6851
462064 meter/sec
ZDOT = 298
350244 ZDOT = 107
908769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13216633
89 X = 4028430
01
Y = 3971886
79 feet Y = 1210631
09 meter
Z = 17415787
37 Z = 5308331
99
XDOT = -7416
086447 XDOT = -2260
423149
YDOT = 23002
749077 feet/sec YDOT = 7011
237919 meter/sec
ZDOT = 373
904782 ZDOT = 113
966178
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 18339
71858858
00016717 00000-0 10270-3 0 9179
2 25544 51
6394 243
9130 0004936 115
7751 244
3912 15
54066023 25184
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
71858858 = yrday
fracday
Element set: 917
Inclination: 51
6394 deg
RA of node: 243
9130 deg
Eccentricity:
0004936
Arg of perigee: 115
7751 deg
Mean anomaly: 244
3912 deg
Mean motion: 15
54066023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 327
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