[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 1st 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) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
060/14:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
1
063/17:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
1
069/22:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 214
4
072/21:25:54
349 -0
6 0
7 0
7
N/A 0
4 -0
0 220
8
000/00:01:48
697 0
2 -0
0 215
0
073/06:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
0
Coasting Arc #1 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2018/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6290521
56 A = 6789136
77 meter
Y = 2510599
34 meter E =
0014479
Z = -351438
50 I = 51
52673
XDOT = -2052
798548 Wp = 139
20444
YDOT = 4325
693803 meter/sec RA = 199
39414 deg
ZDOT = -5992
265712 TA = 44
59061
MA = 44
47422
Ha = 221
734 n
mi
Hp = 213
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20638194
11 X = 6263686
90
Y = 8236874
47 feet Y = 2580794
20 meter
Z = -1153013
46 Z = -320947
49
XDOT = -6734
903373 XDOT = -2071
910525
YDOT = 14191
908801 feet/sec YDOT = 4302
630625 meter/sec
ZDOT = -19659
664411 ZDOT = -6002
284032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15890902
22 X = 4843547
00
Y = 15542028
20 feet Y = 4737210
20 meter
Z = -1017439
39 Z = -310115
53
XDOT = -10420
301870 XDOT = -3176
108010
YDOT = 9400
841379 feet/sec YDOT = 2865
376452 meter/sec
ZDOT = -19704
802424 ZDOT = -6006
023779
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 18059
53159838
00016717 00000-0 10270-3 0 9002
2 25544 51
6375 200
3882 0003034 145
3158 214
8193 15
54181080 21610
Satellite: ISS
Catalog Number: 25544
Epoch time: 18059
53159838 = yrday
fracday
Element set: 900
Inclination: 51
6375 deg
RA of node: 200
3882 deg
Eccentricity:
0003034
Arg of perigee: 145
3158 deg
Mean anomaly: 214
8193 deg
Mean motion: 15
54181080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 296
Coasting Arc #2 (Orbit 2176)
---------------------------------------
Vector Time (GMT): 2018/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5680787
15 A = 6787479
42 meter
Y = -3110357
67 meter E =
0014759
Z = 2013103
23 I = 51
55470
XDOT = 3921
653662 Wp = 80
54660
YDOT = -3545
819207 meter/sec RA = 194
41576 deg
ZDOT = 5555
634726 TA = 301
72420
MA = 301
86797
Ha = 221
702 n
mi
Hp = 213
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18637753
11 X = -5655362
44
Y = -10204585
54 feet Y = -3173741
76 meter
Z = 6604669
39 Z = 1985570
70
XDOT = 12866
317788 XDOT = 3934
026809
YDOT = -11633
265114 feet/sec YDOT = -3501
894779 meter/sec
ZDOT = 18227
148050 ZDOT = 5574
714747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13604676
07 X = -4146705
27
Y = -16371111
22 feet Y = -4989914
70 meter
Z = 6482327
60 Z = 1975813
45
XDOT = 14941
864337 XDOT = 4554
280250
YDOT = -5122
974109 feet/sec YDOT = -1561
482509 meter/sec
ZDOT = 18312
577539 ZDOT = 5581
673634
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 18060
56040556
00016717 00000-0 10270-3 0 9014
2 25544 51
6396 195
2593 0003133 149
3167 210
8169 15
54196812 21773
Satellite: ISS
Catalog Number: 25544
Epoch time: 18060
56040556 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 195
2593 deg
Eccentricity:
0003133
Arg of perigee: 149
3167 deg
Mean anomaly: 210
8169 deg
Mean motion: 15
54196812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2177
Checksum: 311
Coasting Arc #3 (Orbit 2177)
---------------------------------------
Vector Time (GMT): 2018/060/14:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2846232
98 A = 6781106
79 meter
Y = 4308902
12 meter E =
0009786
Z = -4403687
47 I = 51
53737
XDOT = -6801
441232 Wp = 87
47501
YDOT = 1064
982842 meter/sec RA = 193
91227 deg
ZDOT = -3359
955513 TA = 148
48787
MA = 148
42922
Ha = 221
684 n
mi
Hp = 214
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9338034
72 X = 2819228
42
Y = 14136817
97 feet Y = 4340579
16 meter
Z = -14447793
55 Z = -4389927
87
XDOT = -22314
439737 XDOT = -6796
524158
YDOT = 3494
038196 feet/sec YDOT = 988
951562 meter/sec
ZDOT = -11023
476094 ZDOT = -3392
981950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12838162
24 X = 3913071
85
Y = 11134815
96 feet Y = 3393891
90 meter
Z = -14386963
44 Z = -4385146
46
XDOT = -19711
491542 XDOT = -6008
062622
YDOT = 8319
155003 feet/sec YDOT = 2535
678445 meter/sec
ZDOT = -11170
775750 ZDOT = -3404
852449
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 18060
62470634
00016717 00000-0 10270-3 0 9026
2 25544 51
6408 194
9406 0002983 151
3421 208
7896 15
54156065 21784
Satellite: ISS
Catalog Number: 25544
Epoch time: 18060
62470634 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 194
9406 deg
Eccentricity:
0002983
Arg of perigee: 151
3421 deg
Mean anomaly: 208
7896 deg
Mean motion: 15
54156065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2178
Checksum: 314
Coasting Arc #4 (Orbit 2193)
---------------------------------------
Vector Time (GMT): 2018/061/14:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1153228
23 A = 6778030
32 meter
Y = -4290673
90 meter E =
0007726
Z = 5115431
17 I = 51
56019
XDOT = 7502
897325 Wp = 135
75162
YDOT = -105
712046 meter/sec RA = 188
91162 deg
ZDOT = 1595
916939 TA = 298
80713
MA = 298
88468
Ha = 221
588 n
mi
Hp = 214
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3783557
19 X = -1130010
61
Y = -14077014
12 feet Y = -4303439
59 meter
Z = 16782910
66 Z = 5109886
27
XDOT = 24615
804872 XDOT = 7495
769831
YDOT = -346
824299 feet/sec YDOT = -21
849128 meter/sec
ZDOT = 5235
947962 ZDOT = 1632
345379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7695525
37 X = -2345596
13
Y = -12412465
69 feet Y = -3783319
54 meter
Z = 16758678
55 Z = 5108045
22
XDOT = 22586
124922 XDOT = 6884
250876
YDOT = -6683
994242 feet/sec YDOT = -2037
281445 meter/sec
ZDOT = 5398
315851 ZDOT = 1645
406671
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 18061
65350919
00016717 00000-0 10270-3 0 9034
2 25544 51
6412 189
8122 0002901 153
4933 206
6368 15
54202527 21942
Satellite: ISS
Catalog Number: 25544
Epoch time: 18061
65350919 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 189
8122 deg
Eccentricity:
0002901
Arg of perigee: 153
4933 deg
Mean anomaly: 206
6368 deg
Mean motion: 15
54202527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2194
Checksum: 300
Coasting Arc #5 (Orbit 2208)
---------------------------------------
Vector Time (GMT): 2018/062/14:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -689006
92 A = 6777262
73 meter
Y = 4172739
52 meter E =
0016248
Z = -5309665
97 I = 51
58936
XDOT = -7606
399653 Wp = 101
87159
YDOT = -801
550596 meter/sec RA = 183
90782 deg
ZDOT = 354
776428 TA = 171
53218
MA = 171
50473
Ha = 221
527 n
mi
Hp = 214
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2260521
39 X = -709825
25
Y = 13690090
30 feet Y = 4164917
40 meter
Z = -17420163
95 Z = -5313064
05
XDOT = -24955
379438 XDOT = -7598
594468
YDOT = -2629
759173 feet/sec YDOT = -886
566894 meter/sec
ZDOT = 1163
964659 ZDOT = 317
846827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2026787
06 X = 617764
69
Y = 13706806
66 feet Y = 4177834
67 meter
Z = -17435774
34 Z = -5314424
02
XDOT = -23614
086838 XDOT = -7197
573668
YDOT = 4772
881279 feet/sec YDOT = 1454
774214 meter/sec
ZDOT = 999
448714 ZDOT = 304
631968
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 18062
61801092
00016717 00000-0 10270-3 0 9045
2 25544 51
6405 185
0046 0002824 156
8346 203
2934 15
54172113 22092
Satellite: ISS
Catalog Number: 25544
Epoch time: 18062
61801092 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 185
0046 deg
Eccentricity:
0002824
Arg of perigee: 156
8346 deg
Mean anomaly: 203
2934 deg
Mean motion: 15
54172113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2209
Checksum: 281
Coasting Arc #6 (Orbit 2224)
---------------------------------------
Vector Time (GMT): 2018/063/14:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2482165
70 A = 6778704
65 meter
Y = -3942636
71 meter E =
0006410
Z = 4918751
75 I = 51
62865
XDOT = 7138
989079 Wp = 82
51202
YDOT = 1660
200636 meter/sec RA = 178
90656 deg
ZDOT = -2268
483084 TA = 29
66155
MA = 29
62522
Ha = 221
308 n
mi
Hp = 214
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8143588
24 X = 2502176
41
Y = -12935159
79 feet Y = -3914766
83 meter
Z = 16137636
98 Z = 4930858
28
XDOT = 23421
880179 XDOT = 7130
912658
YDOT = 5446
852479 feet/sec YDOT = 1739
988237 meter/sec
ZDOT = -7442
529804 ZDOT = -2233
824595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3568105
49 X = 1087558
55
Y = -14803584
71 feet Y = -4512132
62 meter
Z = 16192041
83 Z = 4935334
35
XDOT = 22913
899121 XDOT = 6984
156452
YDOT = -2460
843725 feet/sec YDOT = -750
065167 meter/sec
ZDOT = -7288
217408 ZDOT = -2221
448666
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 18063
64680620
00016717 00000-0 10270-3 0 9052
2 25544 51
6415 179
8755 0002701 160
9368 199
1887 15
54222760 22257
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
64680620 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 179
8755 deg
Eccentricity:
0002701
Arg of perigee: 160
9368 deg
Mean anomaly: 199
1887 deg
Mean motion: 15
54222760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2225
Checksum: 323
Coasting Arc #7 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2018/063/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3208786
40 A = 6779739
85 meter
Y = -3648532
73 meter E =
0010280
Z = 4723795
13 I = 51
63409
XDOT = 6757
817418 Wp = 126
05375
YDOT = -2371
551190 meter/sec RA = 178
34913 deg
ZDOT = 2748
635601 TA = 296
70087
MA = 296
80607
Ha = 221
615 n
mi
Hp = 214
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10527514
43 X = -3190694
50
Y = -11970251
73 feet Y = -3684313
75 meter
Z = 15498015
52 Z = 4708252
59
XDOT = 22171
316989 XDOT = 6770
483212
YDOT = -7780
679758 feet/sec YDOT = -2295
909419 meter/sec
ZDOT = 9017
833336 ZDOT = 2781
493481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15587565
41 X = -4751089
94
Y = 3643286
56 feet Y = 1110473
74 meter
Z = 15429136
05 Z = 4702800
67
XDOT = 3959
851517 XDOT = 1206
962742
YDOT = -22010
503382 feet/sec YDOT = -6708
801431 meter/sec
ZDOT = 9164
568376 ZDOT = 2793
360441
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 18063
77540677
00016717 00000-0 10270-3 0 9064
2 25544 51
6400 179
2355 0002741 152
0229 208
1071 15
54196933 22273
Satellite: ISS
Catalog Number: 25544
Epoch time: 18063
77540677 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 179
2355 deg
Eccentricity:
0002741
Arg of perigee: 152
0229 deg
Mean anomaly: 208
1071 deg
Mean motion: 15
54196933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2227
Checksum: 301
Coasting Arc #8 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2018/064/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1457772
63 A = 6777474
19 meter
Y = 4024575
38 meter E =
0015394
Z = -5267886
31 I = 51
66018
XDOT = -7445
800273 Wp = 92
97148
YDOT = 1561
119473 meter/sec RA = 173
35238 deg
ZDOT = -870
772226 TA = 168
70951
MA = 168
67494
Ha = 221
470 n
mi
Hp = 214
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4782718
60 X = 1438248
82
Y = 13203987
46 feet Y = 4040767
35 meter
Z = -17283091
56 Z = -5260852
95
XDOT = -24428
478587 XDOT = -7458
474029
YDOT = 5121
783049 feet/sec YDOT = 1477
784439 meter/sec
ZDOT = -2856
864257 ZDOT = -906
972050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13972933
50 X = 4258950
13
Y = 1744771
60 feet Y = 531806
38 meter
Z = -17252183
55 Z = -5258465
55
XDOT = -6586
804945 XDOT = -2007
658147
YDOT = 23000
980706 feet/sec YDOT = 7010
698919 meter/sec
ZDOT = -3018
423505 ZDOT = -920
015484
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 18064
73989883
00016717 00000-0 10270-3 0 9078
2 25544 51
6409 174
4275 0002667 156
8506 203
2767 15
54184350 22422
Satellite: ISS
Catalog Number: 25544
Epoch time: 18064
73989883 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 174
4275 deg
Eccentricity:
0002667
Arg of perigee: 156
8506 deg
Mean anomaly: 203
2767 deg
Mean motion: 15
54184350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 334
Coasting Arc #9 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2018/065/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 370133
97 A = 6777467
38 meter
Y = -4292998
73 meter E =
0004165
Z = 5227718
51 I = 51
69112
XDOT = 7563
684287 Wp = 97
05089
YDOT = -677
988220 meter/sec RA = 168
35467 deg
ZDOT = -1092
043329 TA = 3
40170
MA = 3
39887
Ha = 221
430 n
mi
Hp = 214
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1214350
28 X = 392718
58
Y = -14084641
50 feet Y = -4288732
77 meter
Z = 17151307
44 Z = 5229571
82
XDOT = 24815
237162 XDOT = 7576
008129
YDOT = -2224
370800 feet/sec YDOT = -593
337118 meter/sec
ZDOT = -3582
819320 ZDOT = -1055
271786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12114705
43 X = -3692562
21
Y = -7265374
86 feet Y = -2214486
26 meter
Z = 17160051
29 Z = 5230383
63
XDOT = 8554
441826 XDOT = 2607
393869
YDOT = -22340
897469 feet/sec YDOT = -6809
505548 meter/sec
ZDOT = -3418
791184 ZDOT = -1042
047553
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 18065
76868579
00016717 00000-0 10270-3 0 9081
2 25544 51
6390 169
2987 0002675 157
5534 202
5736 15
54209675 22584
Satellite: ISS
Catalog Number: 25544
Epoch time: 18065
76868579 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 169
2987 deg
Eccentricity:
0002675
Arg of perigee: 157
5534 deg
Mean anomaly: 202
5736 deg
Mean motion: 15
54209675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 359
Coasting Arc #10 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2018/066/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2131374
13 A = 6779947
46 meter
Y = 4464040
29 meter E =
0012150
Z = -4648552
98 I = 51
73252
XDOT = -7064
220146 Wp = 119
59398
YDOT = -310
300548 meter/sec RA = 163
36274 deg
ZDOT = 2940
906265 TA = 179
68894
MA = 179
68819
Ha = 221
325 n
mi
Hp = 214
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6992697
27 X = -2158553
74
Y = 14645801
49 feet Y = 4440053
39 meter
Z = -15251158
06 Z = -4658972
83
XDOT = -23176
575281 XDOT = -7074
510546
YDOT = -1018
046416 feet/sec YDOT = -389
354768 meter/sec
ZDOT = 9648
642601 ZDOT = 2906
565972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10251958
44 X = 3124796
93
Y = 12524369
73 feet Y = 3817427
89 meter
Z = -15298125
69 Z = -4662868
71
XDOT = -10008
257558 XDOT = -3050
516904
YDOT = 19791
176585 feet/sec YDOT = 6032
350623 meter/sec
ZDOT = 9495
547361 ZDOT = 2894
242836
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 18066
73316853
00016717 00000-0 10270-3 0 9093
2 25544 51
6402 164
4905 0002479 163
6756 196
4477 15
54191845 22730
Satellite: ISS
Catalog Number: 25544
Epoch time: 18066
73316853 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 164
4905 deg
Eccentricity:
0002479
Arg of perigee: 163
6756 deg
Mean anomaly: 196
4477 deg
Mean motion: 15
54191845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 337
Coasting Arc #11 (Orbit 2288)
---------------------------------------
Vector Time (GMT): 2018/067/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3670858
37 A = 6783584
87 meter
Y = -4458713
95 meter E =
0012836
Z = 3545633
32 I = 51
77503
XDOT = 6058
913132 Wp = 97
98937
YDOT = 1405
585581 meter/sec RA = 158
38149 deg
ZDOT = -4493
195315 TA = 40
25251
MA = 40
15754
Ha = 221
174 n
mi
Hp = 214
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12043498
58 X = 3703221
39
Y = -14628326
62 feet Y = -4417482
64 meter
Z = 11632655
25 Z = 3563543
93
XDOT = 19878
323923 XDOT = 6064
570609
YDOT = 4611
501250 feet/sec YDOT = 1473
371767 meter/sec
ZDOT = -14741
454447 ZDOT = -4463
749799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8345047
51 X = -2543570
48
Y = -16956336
90 feet Y = -5168291
49 meter
Z = 11713039
19 Z = 3570134
34
XDOT = 11245
142271 XDOT = 3427
519364
YDOT = -15654
086147 feet/sec YDOT = -4771
365458 meter/sec
ZDOT = -14610
294339 ZDOT = -4453
217715
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 18067
76194451
00016717 00000-0 10270-3 0 9107
2 25544 51
6388 159
3612 0002391 163
6274 196
4956 15
54243369 22897
Satellite: ISS
Catalog Number: 25544
Epoch time: 18067
76194451 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 159
3612 deg
Eccentricity:
0002391
Arg of perigee: 163
6274 deg
Mean anomaly: 196
4956 deg
Mean motion: 15
54243369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2289
Checksum: 338
Coasting Arc #12 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/068/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4851662
78 A = 6787081
34 meter
Y = 4262800
69 meter E =
0005339
Z = -2086219
97 I = 51
81634
XDOT = -4628
575284 Wp = 64
61207
YDOT = -2560
528037 meter/sec RA = 153
41380 deg
ZDOT = 5545
441927 TA = 272
36732
MA = 272
42845
Ha = 221
198 n
mi
Hp = 214
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15917528
80 X = -4888836
32
Y = 13985566
56 feet Y = 4208338
05 meter
Z = -6844553
70 Z = -2109878
08
XDOT = -15185
614448 XDOT = -4626
535363
YDOT = -8400
682536 feet/sec YDOT = -2612
276109 meter/sec
ZDOT = 18193
707108 ZDOT = 5522
963263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6487637
23 X = 1977431
83
Y = 20134843
27 feet Y = 6137100
23 meter
Z = -6950565
45 Z = -2118532
35
XDOT = -12341
895267 XDOT = -3761
809677
YDOT = 10207
817063 feet/sec YDOT = 3111
342641 meter/sec
ZDOT = 18093
738281 ZDOT = 5514
971428
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 18068
72641922
00016717 00000-0 10270-3 0 9115
2 25544 51
6383 154
5534 0002523 166
7810 193
3409 15
54245499 23042
Satellite: ISS
Catalog Number: 25544
Epoch time: 18068
72641922 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 154
5534 deg
Eccentricity:
0002523
Arg of perigee: 166
7810 deg
Mean anomaly: 193
3409 deg
Mean motion: 15
54245499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 311
Coasting Arc #13 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2018/069/17:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5615118
01 A = 6788959
02 meter
Y = -3784389
93 meter E =
0014665
Z = 365954
37 I = 51
85079
XDOT = 2927
765833 Wp = 136
93526
YDOT = 3749
437217 meter/sec RA = 148
45444 deg
ZDOT = -6018
041103 TA = 39
12981
MA = 39
02385
Ha = 221
154 n
mi
Hp = 214
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18422303
17 X = 5655241
16
Y = -12415977
45 feet Y = -3721373
45 meter
Z = 1200637
69 Z = 393328
11
XDOT = 9605
530948 XDOT = 2914
853173
YDOT = 12301
303204 feet/sec YDOT = 3782
104846 meter/sec
ZDOT = -19744
229341 ZDOT = -6003
850835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4409371
77 X = -1343976
52
Y = -21766623
50 feet Y = -6634466
84 meter
Z = 1323186
75 Z = 403307
32
XDOT = 13504
806750 XDOT = 4116
265098
YDOT = -3955
940354 feet/sec YDOT = -1205
770620 meter/sec
ZDOT = -19681
361124 ZDOT = -5998
878871
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 18069
75518747
00016717 00000-0 10270-3 0 9128
2 25544 51
6377 149
4234 0002333 171
1804 188
9390 15
54233187 23205
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
75518747 = yrday
fracday
Element set: 912
Inclination: 51
6377 deg
RA of node: 149
4234 deg
Eccentricity:
0002333
Arg of perigee: 171
1804 deg
Mean anomaly: 188
9390 deg
Mean motion: 15
54233187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 317
Coasting Arc #14 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3253
09 A = 6778603
47 meter
Y = 4630582
23 meter E =
0013327
Z = -4962809
08 I = 51
82455
XDOT = -6936
452235 Wp = 115
17988
YDOT = 2375
552196 meter/sec RA = 147
37943 deg
ZDOT = 2211
093807 TA = 176
37286
MA = 176
36319
Ha = 221
039 n
mi
Hp = 214
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10672
88 X = -24421
13
Y = 15192198
91 feet Y = 4630463
49 meter
Z = -16282182
03 Z = -4962860
85
XDOT = -22757
389224 XDOT = -6973
240986
YDOT = 7793
806417 feet/sec YDOT = 2297
778491 meter/sec
ZDOT = 7254
244772 ZDOT = 2177
309769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8715058
32 X = 2656349
78
Y = -12442901
64 feet Y = -3792596
42 meter
Z = -16282949
07 Z = -4963042
88
XDOT = 22190
212837 XDOT = 6763
576873
YDOT = 6242
898353 feet/sec YDOT = 1902
835418 meter/sec
ZDOT = 7103
258247 ZDOT = 2165
073114
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 18069
94808195
00016717 00000-0 10270-3 0 9139
2 25544 51
6400 148
4620 0002184 176
3508 183
7661 15
54234074 23235
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
94808195 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 148
4620 deg
Eccentricity:
0002184
Arg of perigee: 176
3508 deg
Mean anomaly: 183
7661 deg
Mean motion: 15
54234074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 308
Coasting Arc #15 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1550769
70 A = 6782038
14 meter
Y = -5207387
59 meter E =
0010510
Z = 4049833
79 I = 51
86325
XDOT = 6499
458371 Wp = 89
67496
YDOT = -1120
168561 meter/sec RA = 142
40139 deg
ZDOT = -3920
304527 TA = 40
87804
MA = 40
79927
Ha = 221
017 n
mi
Hp = 214
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5087827
10 X = 1589213
16
Y = -17084604
96 feet Y = -5189830
54 meter
Z = 13286856
26 Z = 4057460
58
XDOT = 21323
682321 XDOT = 6530
543875
YDOT = -3675
093704 feet/sec YDOT = -1047
313659 meter/sec
ZDOT = -12861
891492 ZDOT = -3888
657237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13790501
90 X = -4203344
98
Y = 11254785
31 feet Y = 3430458
56 meter
Z = 13321491
12 Z = 4060390
49
XDOT = -18909
589411 XDOT = -5763
642852
YDOT = -8079
338331 feet/sec YDOT = -2462
582323 meter/sec
ZDOT = -12720
564040 ZDOT = -3877
227919
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 18070
97684418
00016717 00000-0 10270-3 0 9145
2 25544 51
6401 143
3337 0002162 177
8891 182
2271 15
54228333 23391
Satellite: ISS
Catalog Number: 25544
Epoch time: 18070
97684418 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 143
3337 deg
Eccentricity:
0002162
Arg of perigee: 177
8891 deg
Mean anomaly: 182
2271 deg
Mean motion: 15
54228333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 310
Coasting Arc #16 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2859379
01 A = 6785785
85 meter
Y = 5521613
18 meter E =
0003978
Z = -2719896
89 I = 51
90188
XDOT = -5625
423768 Wp = 83
93833
YDOT = -359
505398 meter/sec RA = 137
43461 deg
ZDOT = 5191
001133 TA = 245
44783
MA = 245
48929
Ha = 220
914 n
mi
Hp = 214
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9381164
74 X = -2907699
04
Y = 18115528
81 feet Y = 5489367
22 meter
Z = -8923546
21 Z = -2733904
41
XDOT = -18456
114723 XDOT = -5646
200370
YDOT = -1179
479652 feet/sec YDOT = -422
528453 meter/sec
ZDOT = 17030
843612 ZDOT = 5163
624748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17768629
67 X = 5415878
32
Y = -9966111
70 feet Y = -3037670
85 meter
Z = -8986697
40 Z = -2739145
37
XDOT = 14110
238401 XDOT = 4300
800664
YDOT = 9930
505299 feet/sec YDOT = 3026
818015 meter/sec
ZDOT = 16908
730078 ZDOT = 5153
780928
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 18071
94130519
00016717 00000-0 10270-3 0 9152
2 25544 51
6405 138
5249 0002146 182
9591 177
1549 15
54252249 23540
Satellite: ISS
Catalog Number: 25544
Epoch time: 18071
94130519 = yrday
fracday
Element set: 915
Inclination: 51
6405 deg
RA of node: 138
5249 deg
Eccentricity:
0002146
Arg of perigee: 182
9591 deg
Mean anomaly: 177
1549 deg
Mean motion: 15
54252249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2354
Checksum: 316
Coasting Arc #17 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2018/072/21:26:48
697
Vector Time (MET): N/A
Weight (LBS) : 904718
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1089239
79 A = 6779080
92 meter
Y = 4528725
42 meter E =
0012120
Z = -4936732
76 I = 51
90052
XDOT = -6124
826688 Wp = 116
46689
YDOT = 3981
502506 meter/sec RA = 132
68061 deg
ZDOT = 2300
164506 TA = 175
97354
MA = 175
96378
Ha = 220
845 n
mi
Hp = 215
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3573621
35 X = 1062497
07
Y = 14858023
04 feet Y = 4540756
01 meter
Z = -16196629
80 Z = -4931507
12
XDOT = -20094
575747 XDOT = -6180
066540
YDOT = 13062
672265 feet/sec YDOT = 3912
701855 meter/sec
ZDOT = 7546
471475 ZDOT = 2270
278105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8513733
82 X = 2594986
07
Y = -12719492
45 feet Y = -3876901
30 meter
Z = -16173845
66 Z = -4929788
16
XDOT = 22290
538981 XDOT = 6794
156281
YDOT = 5490
570410 feet/sec YDOT = 1673
525861 meter/sec
ZDOT = 7412
632316 ZDOT = 2259
370330
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 18072
90576356
00016717 00000-0 10270-3 0 9163
2 25544 51
6404 133
7161 0002054 204
0936 156
0120 15
54117192 23690
Satellite: ISS
Catalog Number: 25544
Epoch time: 18072
90576356 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 133
7161 deg
Eccentricity:
0002054
Arg of perigee: 204
0936 deg
Mean anomaly: 156
0120 deg
Mean motion: 15
54117192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 287
Coasting Arc #18 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904718
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -634020
64 A = 6782758
81 meter
Y = 5481560
17 meter E =
0006985
Z = -3952273
30 I = 51
92078
XDOT = -6106
943109 Wp = 128
20094
YDOT = 2218
954507 meter/sec RA = 130
73537 deg
ZDOT = 4057
880595 TA = 184
09027
MA = 184
09598
Ha = 220
905 n
mi
Hp = 215
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2080120
21 X = -676072
05
Y = 17984121
31 feet Y = 5474234
56 meter
Z = -12966775
93 Z = -3955455
84
XDOT = -20035
902590 XDOT = -6151
012928
YDOT = 7280
034472 feet/sec YDOT = 2150
416503 meter/sec
ZDOT = 13313
256545 ZDOT = 4028
108364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18059955
22 X = -5504674
35
Y = -1099154
49 feet Y = -335022
29 meter
Z = -12981628
33 Z = -3956800
32
XDOT = -8351
356656 XDOT = -2545
493509
YDOT = -18420
079496 feet/sec YDOT = -5614
440230 meter/sec
ZDOT = 13180
129755 ZDOT = 4017
303549
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 18073
29157857
00016717 00000-0 10270-3 0 9178
2 25544 51
6397 131
7886 0002516 201
4803 158
6244 15
54108190 23750
Satellite: ISS
Catalog Number: 25544
Epoch time: 18073
29157857 = yrday
fracday
Element set: 917
Inclination: 51
6397 deg
RA of node: 131
7886 deg
Eccentricity:
0002516
Arg of perigee: 201
4803 deg
Mean anomaly: 158
6244 deg
Mean motion: 15
54108190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 322
Coasting Arc #19 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904718
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1814722
55 A = 6786506
26 meter
Y = -5993783
34 meter E =
0013421
Z = 2595986
85 I = 51
95382
XDOT = 5534
631043 Wp = 114
00049
YDOT = -616
866452 meter/sec RA = 125
77413 deg
ZDOT = -5277
111536 TA = 36
90475
MA = 36
81247
Ha = 220
894 n
mi
Hp = 215
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5953814
14 X = 1869002
04
Y = -19664643
52 feet Y = -5973186
05 meter
Z = 8517017
21 Z = 2604934
59
XDOT = 18158
238331 XDOT = 5566
750728
YDOT = -2023
840066 feet/sec YDOT = -554
795464 meter/sec
ZDOT = -17313
358058 ZDOT = -5250
148522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20014109
89 X = 6100300
69
Y = 4570276
63 feet Y = 1393020
32 meter
Z = 8557667
13 Z = 2608376
94
XDOT = 3574
914131 XDOT = 1089
633827
YDOT = 16636
520232 feet/sec YDOT = 5070
811367 meter/sec
ZDOT = -17192
947641 ZDOT = -5240
410441
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 18074
32041737
00016717 00000-0 10270-3 0 9183
2 25544 51
6396 126
6598 0002526 202
7237 157
3804 15
54107559 23912
Satellite: ISS
Catalog Number: 25544
Epoch time: 18074
32041737 = yrday
fracday
Element set: 918
Inclination: 51
6396 deg
RA of node: 126
6598 deg
Eccentricity:
0002526
Arg of perigee: 202
7237 deg
Mean anomaly: 157
3804 deg
Mean motion: 15
54107559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 319
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list