[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 15th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 7 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
080/17:44:26
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
4
082/19:41:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
3
086/11:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
4
087/13:50:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2018/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3470854
70 A = 6777461
40 meter
Y = -2352267
24 meter E =
0003196
Z = 5323726
21 I = 51
90825
XDOT = 4672
184582 Wp = 152
60333
YDOT = -6071
967638 meter/sec RA = 129
69002 deg
ZDOT = 360
350177 TA = 293
95758
MA = 293
99104
Ha = 220
957 n
mi
Hp = 215
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11387318
56 X = -3470152
51
Y = -7717412
21 feet Y = -2391076
20 meter
Z = 17466293
35 Z = 5306868
23
XDOT = 15328
689573 XDOT = 4737
985365
YDOT = -19921
153667 feet/sec YDOT = -6019
352101 meter/sec
ZDOT = 1182
251236 ZDOT = 383
206178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10184035
70 X = -3104094
08
Y = -9387630
23 feet Y = -2861349
69 meter
Z = 17391339
62 Z = 5300880
32
XDOT = 17507
888401 XDOT = 5336
404385
YDOT = -16595
262947 feet/sec YDOT = -5058
236146 meter/sec
ZDOT = 1284
972820 ZDOT = 391
659715
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
54891040
00016717 00000-0 10270-3 0 9007
2 25544 51
6403 130
5100 0002284 206
7497 153
3539 15
54106564 23799
Satellite: ISS
Catalog Number: 25544
Epoch time: 18073
54891040 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 130
5100 deg
Eccentricity:
0002284
Arg of perigee: 206
7497 deg
Mean anomaly: 153
3539 deg
Mean motion: 15
54106564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 290
Coasting Arc #2 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2018/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2322442
83 A = 6778280
54 meter
Y = 3746317
01 meter E =
0013199
Z = -5161131
31 I = 51
93063
XDOT = -5216
884832 Wp = 110
43293
YDOT = 5385
263714 meter/sec RA = 124
70999 deg
ZDOT = 1560
217907 TA = 174
57175
MA = 174
55742
Ha = 220
845 n
mi
Hp = 215
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7619563
10 X = 2305447
60
Y = 12291066
32 feet Y = 3772192
48 meter
Z = -16932845
51 Z = -5149891
60
XDOT = -17115
763883 XDOT = -5284
295197
YDOT = 17668
188038 feet/sec YDOT = 5326
548204 meter/sec
ZDOT = 5118
825153 ZDOT = 1534
712038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5984909
70 X = 1824200
48
Y = 13228381
95 feet Y = 4032010
82 meter
Z = -16883129
95 Z = -5145978
01
XDOT = -18431
627036 XDOT = -5617
959921
YDOT = 14731
249476 feet/sec YDOT = 4490
084840 meter/sec
ZDOT = 5004
345702 ZDOT = 1525
324570
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
51346497
00016717 00000-0 10270-3 0 9017
2 25544 51
6400 125
7021 0002062 208
8885 151
2154 15
54076222 23946
Satellite: ISS
Catalog Number: 25544
Epoch time: 18074
51346497 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 125
7021 deg
Eccentricity:
0002062
Arg of perigee: 208
8885 deg
Mean anomaly: 151
2154 deg
Mean motion: 15
54076222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 287
Coasting Arc #3 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2018/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1172115
63 A = 6780958
44 meter
Y = -4972856
47 meter E =
0007574
Z = 4452927
13 I = 51
95703
XDOT = 5436
885086 Wp = 78
94871
YDOT = -4267
245979 meter/sec RA = 119
73690 deg
ZDOT = -3328
182805 TA = 44
51037
MA = 44
44955
Ha = 220
772 n
mi
Hp = 215
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3845523
71 X = -1138050
41
Y = -16315145
89 feet Y = -4985772
78 meter
Z = 14609340
98 Z = 4447316
89
XDOT = 17837
549494 XDOT = 5500
364886
YDOT = -14000
150851 feet/sec YDOT = -4206
092515 meter/sec
ZDOT = -10919
234926 ZDOT = -3301
617839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1969719
97 X = -600370
65
Y = -16667505
61 feet Y = -5080255
71 meter
Z = 14584901
16 Z = 4445477
87
XDOT = 18234
662999 XDOT = 5557
925282
YDOT = -11623
410894 feet/sec YDOT = -3542
815640 meter/sec
ZDOT = -10800
150562 ZDOT = -3291
885891
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 18075
54231947
00016717 00000-0 10270-3 0 9025
2 25544 51
6391 120
5741 0002119 213
5411 146
5608 15
54121716 24107
Satellite: ISS
Catalog Number: 25544
Epoch time: 18075
54231947 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 120
5741 deg
Eccentricity:
0002119
Arg of perigee: 213
5411 deg
Mean anomaly: 146
5608 deg
Mean motion: 15
54121716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 276
Coasting Arc #4 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2018/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 111754
24 A = 6784694
77 meter
Y = 5925974
45 meter E =
0003850
Z = -3306415
90 I = 51
98567
XDOT = -5352
699479 Wp = 109
51739
YDOT = 2746
686815 meter/sec RA = 114
77289 deg
ZDOT = 4745
109923 TA = 212
28643
MA = 212
31000
Ha = 220
735 n
mi
Hp = 215
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 366647
76 X = 61540
78
Y = 19442173
40 feet Y = 5926942
93 meter
Z = -10847821
21 Z = -3305995
86
XDOT = -17561
349998 XDOT = -5406
064921
YDOT = 9011
439683 feet/sec YDOT = 2686
531550 meter/sec
ZDOT = 15567
945941 ZDOT = 4718
978561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1548407
16 X = -471954
50
Y = 19384528
29 feet Y = 5908404
22 meter
Z = -10846670
46 Z = -3306065
16
XDOT = -17077
866709 XDOT = -5205
333773
YDOT = 7275
542255 feet/sec YDOT = 2217
585279 meter/sec
ZDOT = 15450
971545 ZDOT = 4709
456127
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 18076
50686994
00016717 00000-0 10270-3 0 9039
2 25544 51
6397 115
7654 0001973 211
4532 148
6503 15
54129033 24253
Satellite: ISS
Catalog Number: 25544
Epoch time: 18076
50686994 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 115
7654 deg
Eccentricity:
0001973
Arg of perigee: 211
4532 deg
Mean anomaly: 148
6503 deg
Mean motion: 15
54129033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 316
Coasting Arc #5 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2018/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 847116
02 A = 6787987
08 meter
Y = -6483859
94 meter E =
0013602
Z = 1794502
86 I = 52
00912
XDOT = 5058
479164 Wp = 122
15422
YDOT = -921
466234 meter/sec RA = 109
82032 deg
ZDOT = -5692
967424 TA = 38
22455
MA = 38
12818
Ha = 220
689 n
mi
Hp = 215
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2779252
02 X = 910840
62
Y = -21272506
38 feet Y = -6474030
34 meter
Z = 5887476
59 Z = 1798773
56
XDOT = 16596
060249 XDOT = 5096
060634
YDOT = -3023
183184 feet/sec YDOT = -864
689532 meter/sec
ZDOT = -18677
714646 ZDOT = -5668
303767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4537335
81 X = 1382979
96
Y = -20962395
58 feet Y = -6389338
17 meter
Z = 5907343
33 Z = 1800558
25
XDOT = 15386
898642 XDOT = 4689
926706
YDOT = -1924
390523 feet/sec YDOT = -586
554231 meter/sec
ZDOT = -18567
509235 ZDOT = -5659
376815
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 18077
53571902
00016717 00000-0 10270-3 0 9046
2 25544 51
6395 110
6366 0001865 219
0955 141
0063 15
54118338 24410
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
53571902 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 110
6366 deg
Eccentricity:
0001865
Arg of perigee: 219
0955 deg
Mean anomaly: 141
0063 deg
Mean motion: 15
54118338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 300
Coasting Arc #6 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2018/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1647365
56 A = 6789401
91 meter
Y = 6580452
14 meter E =
0010037
Z = -124393
89 I = 52
02368
XDOT = -4603
210236 Wp = 44
63442
YDOT = -1043
853608 meter/sec RA = 104
87490 deg
ZDOT = 6042
524267 TA = 314
03279
MA = 314
11544
Ha = 220
660 n
mi
Hp = 215
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5404742
64 X = -1720223
28
Y = 21589409
90 feet Y = 6561622
77 meter
Z = -408116
44 Z = -132574
09
XDOT = -15102
395786 XDOT = -4620
546881
YDOT = -3424
716561 feet/sec YDOT = -1095
425975 meter/sec
ZDOT = 19824
554681 ZDOT = 6020
121494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6853079
58 X = -2088818
66
Y = 21173504
36 feet Y = 6453684
13 meter
Z = -445460
86 Z = -135776
47
XDOT = -13421
842459 XDOT = -4090
977582
YDOT = -3948
243627 feet/sec YDOT = -1203
424658 meter/sec
ZDOT = 19724
684306 ZDOT = 6012
083777
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 18078
50026423
00016717 00000-0 10270-3 0 9058
2 25544 51
6393 105
8286 0001804 223
7142 136
3868 15
54099966 24569
Satellite: ISS
Catalog Number: 25544
Epoch time: 18078
50026423 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 105
8286 deg
Eccentricity:
0001804
Arg of perigee: 223
7142 deg
Mean anomaly: 136
3868 deg
Mean motion: 15
54099966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 321
Coasting Arc #7 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2018/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2339380
63 A = 6788362
16 meter
Y = -6166285
87 meter E =
0008490
Z = -1589892
14 I = 52
02731
XDOT = 4045
376643 Wp = 155
46779
YDOT = 3018
242035 meter/sec RA = 99
93045 deg
ZDOT = -5772
153917 TA = 41
82726
MA = 41
76241
Ha = 220
647 n
mi
Hp = 215
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7675133
31 X = 2415882
74
Y = -20230596
68 feet Y = -6139697
75 meter
Z = -5216181
58 Z = -1578341
62
XDOT = 13272
233082 XDOT = 4039
363375
YDOT = 9902
368882 feet/sec YDOT = 3063
445879 meter/sec
ZDOT = -18937
512852 ZDOT = -5752
517787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8723606
48 X = 2658955
25
Y = -19814813
35 feet Y = -6039555
11 meter
Z = -5163828
57 Z = -1573934
95
XDOT = 11433
692331 XDOT = 3484
989422
YDOT = 9930
229261 feet/sec YDOT = 3026
733879 meter/sec
ZDOT = -18850
246172 ZDOT = -5745
555033
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 18079
52910982
00016717 00000-0 10270-3 0 9064
2 25544 51
6390 100
6995 0001935 226
1407 133
9586 15
54099059 24723
Satellite: ISS
Catalog Number: 25544
Epoch time: 18079
52910982 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 100
6995 deg
Eccentricity:
0001935
Arg of perigee: 226
1407 deg
Mean anomaly: 133
9586 deg
Mean motion: 15
54099059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 331
Coasting Arc #8 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2899186
70 A = 6785324
45 meter
Y = 5280559
22 meter E =
0011554
Z = 3112481
89 I = 52
02194
XDOT = -3431
583219 Wp = 89
01161
YDOT = -4788
156520 meter/sec RA = 94
98030 deg
ZDOT = 4911
559299 TA = 306
60342
MA = 306
70966
Ha = 220
609 n
mi
Hp = 215
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9511767
39 X = -2973138
76
Y = 17324669
35 feet Y = 5247725
36 meter
Z = 10211554
75 Z = 3098218
39
XDOT = -11258
475129 XDOT = -3401
643611
YDOT = -15709
174936 feet/sec YDOT = -4826
362922 meter/sec
ZDOT = 16114
039694 ZDOT = 4894
962991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10152863
02 X = -3094592
65
Y = 16995518
88 feet Y = 5180234
15 meter
Z = 10147189
16 Z = 3092863
26
XDOT = -9593
766726 XDOT = -2924
180098
YDOT = -15338
741383 feet/sec YDOT = -4675
248373 meter/sec
ZDOT = 16040
580331 ZDOT = 4889
168885
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 18080
55795227
00016717 00000-0 10270-3 0 9073
2 25544 51
6390 95
5703 0001724 234
1143 125
9849 15
54111402 24881
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
55795227 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 95
5703 deg
Eccentricity:
0001724
Arg of perigee: 234
1143 deg
Mean anomaly: 125
9849 deg
Mean motion: 15
54111402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 308
Coasting Arc #9 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2018/080/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3599132
96 A = 6779472
71 meter
Y = 3086168
06 meter E =
0010467
Z = -4855854
56 I = 52
00357
XDOT = -2426
878742 Wp = 114
92969
YDOT = 6810
533776 meter/sec RA = 93
75100 deg
ZDOT = 2529
657061 TA = 179
84668
MA = 179
84636
Ha = 220
481 n
mi
Hp = 215
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11808178
99 X = 3587942
41
Y = 10125223
28 feet Y = 3126352
98 meter
Z = -15931281
36 Z = -4838398
61
XDOT = -7962
200598 XDOT = -2515
143423
YDOT = 22344
270920 feet/sec YDOT = 6782
901486 meter/sec
ZDOT = 8299
399807 ZDOT = 2517
652993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11232845
44 X = 3423771
29
Y = -10873837
92 feet Y = -3314345
80 meter
Z = -15853762
82 Z = -4832226
91
XDOT = 20668
021356 XDOT = 6299
612909
YDOT = 9329
382604 feet/sec YDOT = 2843
595818 meter/sec
ZDOT = 8244
914962 ZDOT = 2513
050080
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 18080
75086107
00016717 00000-0 10270-3 0 9086
2 25544 51
6394 94
6090 0001753 241
2976 118
8001 15
54119718 24912
Satellite: ISS
Catalog Number: 25544
Epoch time: 18080
75086107 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 94
6090 deg
Eccentricity:
0001753
Arg of perigee: 241
2976 deg
Mean anomaly: 118
8001 deg
Mean motion: 15
54119718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2491
Checksum: 312
Coasting Arc #10 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2018/081/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3131650
99 A = 6783032
35 meter
Y = -4587760
41 meter E =
0009597
Z = 3885428
90 I = 52
01660
XDOT = 3119
023932 Wp = 84
53460
YDOT = -5649
264105 meter/sec RA = 88
78685 deg
ZDOT = -4146
837970 TA = 48
81245
MA = 48
72972
Ha = 220
544 n
mi
Hp = 215
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10274445
51 X = -3098990
11
Y = -15051707
38 feet Y = -4622597
75 meter
Z = 12747470
15 Z = 3870296
05
XDOT = 10233
018149 XDOT = 3202
106973
YDOT = -18534
331052 feet/sec YDOT = -5613
920819 meter/sec
ZDOT = -13605
111451 ZDOT = -4131
484519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15830778
98 X = -4825221
43
Y = 9121772
12 feet Y = 2780316
14 meter
Z = 12680529
60 Z = 3865025
42
XDOT = -16985
477190 XDOT = -5177
173447
YDOT = -10617
247240 feet/sec YDOT = -3236
136959 meter/sec
ZDOT = -13535
809852 ZDOT = -4125
714843
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 18081
77970156
00016717 00000-0 10270-3 0 9096
2 25544 51
6395 89
4813 0001774 245
3303 114
7665 15
54114117 25077
Satellite: ISS
Catalog Number: 25544
Epoch time: 18081
77970156 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 89
4813 deg
Eccentricity:
0001774
Arg of perigee: 245
3303 deg
Mean anomaly: 114
7665 deg
Mean motion: 15
54114117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 317
Coasting Arc #11 (Orbit 2521)
---------------------------------------
Vector Time (GMT): 2018/082/17:44:26
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2607983
71 A = 6786646
80 meter
Y = 5729487
28 meter E =
0003592
Z = -2533283
09 I = 52
02781
XDOT = -3740
507693 Wp = 39
64922
YDOT = 4053
010057 meter/sec RA = 83
83154 deg
ZDOT = 5322
655737 TA = 292
08406
MA = 292
12219
Ha = 220
398 n
mi
Hp = 215
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8556377
00 X = 2556026
57
Y = 18797530
44 feet Y = 5758360
87 meter
Z = -8311296
23 Z = -2520740
95
XDOT = -12272
006866 XDOT = -3811
406249
YDOT = 13297
277090 feet/sec YDOT = 4010
785047 meter/sec
ZDOT = 17462
781291 ZDOT = 5304
313163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19300568
45 X = 5882813
26
Y = -7413600
60 feet Y = -2259665
46 meter
Z = -8256086
64 Z = -2516455
21
XDOT = 11953
851728 XDOT = 3643
534007
YDOT = 11790
339264 feet/sec YDOT = 3593
695408 meter/sec
ZDOT = 17380
336266 ZDOT = 5297
526494
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 18082
74423741
00016717 00000-0 10270-3 0 9109
2 25544 51
6402 84
6729 0001854 249
6787 110
4167 15
54126581 25226
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
74423741 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 84
6729 deg
Eccentricity:
0001854
Arg of perigee: 249
6787 deg
Mean anomaly: 110
4167 deg
Mean motion: 15
54126581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2522
Checksum: 309
Coasting Arc #12 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2018/082/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3428733
77 A = 6779529
86 meter
Y = 3281987
17 meter E =
0006222
Z = 4838619
24 I = 52
00508
XDOT = -2774
525126 Wp = 132
20179
YDOT = -6677
357949 meter/sec RA = 83
47152 deg
ZDOT = 2556
942898 TA = 292
73846
MA = 292
80420
Ha = 220
521 n
mi
Hp = 215
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11249126
53 X = -3488682
50
Y = 10767674
43 feet Y = 3243309
82 meter
Z = 15874735
06 Z = 4821817
81
XDOT = -9102
772724 XDOT = -2712
071184
YDOT = -21907
342352 feet/sec YDOT = -6708
035236 meter/sec
ZDOT = 8388
920270 ZDOT = 2543
617308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14619551
03 X = 4456039
15
Y = 5580726
01 feet Y = 1701005
29 meter
Z = 15799275
24 Z = 4815619
09
XDOT = -15385
743570 XDOT = -4689
574640
YDOT = 16664
188123 feet/sec YDOT = 5079
244540 meter/sec
ZDOT = 8330
343755 ZDOT = 2539
088777
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 18082
87284162
00016717 00000-0 10270-3 0 9116
2 25544 51
6416 84
0325 0001827 250
4887 109
6068 15
54113615 25244
Satellite: ISS
Catalog Number: 25544
Epoch time: 18082
87284162 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 84
0325 deg
Eccentricity:
0001827
Arg of perigee: 250
4887 deg
Mean anomaly: 109
6068 deg
Mean motion: 15
54113615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 304
Coasting Arc #13 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2018/083/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3915905
87 A = 6777440
40 meter
Y = -1577742
86 meter E =
0012765
Z = -5312943
58 I = 51
99368
XDOT = 2038
849793 Wp = 85
67499
YDOT = 7351
366587 meter/sec RA = 78
49802 deg
ZDOT = -680
811689 TA = 177
85039
MA = 177
84490
Ha = 220
292 n
mi
Hp = 215
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12847460
20 X = 3959064
99
Y = -5176321
72 feet Y = -1533711
49 meter
Z = -17430917
26 Z = -5293816
61
XDOT = 6689
139741 XDOT = 1959
800297
YDOT = 24118
656780 feet/sec YDOT = 7373
724376 meter/sec
ZDOT = -2233
634149 ZDOT = -671
100105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10434660
12 X = -3180484
41
Y = -9270749
36 feet Y = -2825724
40 meter
Z = -17345301
70 Z = -5286847
96
XDOT = 17886
061456 XDOT = 5451
671532
YDOT = -16034
632134 feet/sec YDOT = -4887
355874 meter/sec
ZDOT = -2191
298778 ZDOT = -667
907867
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 18083
83737310
00016717 00000-0 10270-3 0 9122
2 25544 51
6417 79
2242 0001894 258
5708 101
5232 15
54150074 25394
Satellite: ISS
Catalog Number: 25544
Epoch time: 18083
83737310 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 79
2242 deg
Eccentricity:
0001894
Arg of perigee: 258
5708 deg
Mean anomaly: 101
5232 deg
Mean motion: 15
54150074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 300
Coasting Arc #14 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2018/084/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4315713
58 A = 6777787
08 meter
Y = -201411
30 meter E =
0002577
Z = 5221388
02 I = 51
98677
XDOT = -1181
281996 Wp = 35
85918
YDOT = -7472
170488 meter/sec RA = 73
52224 deg
ZDOT = -1262
269554 TA = 66
21193
MA = 66
18492
Ha = 220
399 n
mi
Hp = 215
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14159165
30 X = -4338503
18
Y = -660798
23 feet Y = -249799
68 meter
Z = 17130538
13 Z = 5200368
59
XDOT = -3875
597101 XDOT = -1091
506961
YDOT = -24514
995039 feet/sec YDOT = -7484
878512 meter/sec
ZDOT = -4141
304312 ZDOT = -1267
789259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6025929
28 X = 1836703
24
Y = 12954241
03 feet Y = 3948452
67 meter
Z = 17036718
25 Z = 5192791
72
XDOT = -19000
132574 XDOT = -5791
240409
YDOT = 14325
927044 feet/sec YDOT = 4366
542563 meter/sec
ZDOT = -4164
895012 ZDOT = -1269
460000
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 18084
86620476
00016717 00000-0 10270-3 0 9131
2 25544 51
6411 74
0956 0001951 261
9005 98
1927 15
54160747 25553
Satellite: ISS
Catalog Number: 25544
Epoch time: 18084
86620476 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 74
0956 deg
Eccentricity:
0001951
Arg of perigee: 261
9005 deg
Mean anomaly: 98
1927 deg
Mean motion: 15
54160747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 318
Coasting Arc #15 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2018/085/19:41:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4611304
53 A = 6780425
33 meter
Y = 1896770
07 meter E =
0008222
Z = -4603005
05 I = 51
98459
XDOT = 178
019376 Wp = 115
65450
YDOT = 7016
509443 meter/sec RA = 68
54954 deg
ZDOT = 3070
445380 TA = 184
91982
MA = 184
92791
Ha = 220
258 n
mi
Hp = 215
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15128951
87 X = 4612110
37
Y = 6222998
92 feet Y = 1948341
00 meter
Z = -15101722
59 Z = -4580603
33
XDOT = 584
053070 XDOT = 84
631163
YDOT = 23020
044104 feet/sec YDOT = 7017
978252 meter/sec
ZDOT = 10073
639697 ZDOT = 3071
082758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1820652
61 X = -554934
92
Y = -16349281
78 feet Y = -4983261
09 meter
Z = -15001971
04 Z = -4572600
77
XDOT = 18776
425456 XDOT = 5723
054479
YDOT = -11333
709148 feet/sec YDOT = -3454
514548 meter/sec
ZDOT = 10075
485928 ZDOT = 3071
008111
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 18085
83073425
00016717 00000-0 10270-3 0 9146
2 25544 51
6406 69
2871 0001983 266
1025 93
9901 15
54145999 25707
Satellite: ISS
Catalog Number: 25544
Epoch time: 18085
83073425 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 69
2871 deg
Eccentricity:
0001983
Arg of perigee: 266
1025 deg
Mean anomaly: 93
9901 deg
Mean motion: 15
54145999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 327
Coasting Arc #16 (Orbit 2579)
---------------------------------------
Vector Time (GMT): 2018/086/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4734514
85 A = 6781299
50 meter
Y = 2072402
88 meter E =
0007308
Z = -4397955
83 I = 51
97662
XDOT = 189
323041 Wp = 116
05002
YDOT = 6847
104252 meter/sec RA = 65
35336 deg
ZDOT = 3431
592913 TA = 188
59606
MA = 188
60858
Ha = 220
418 n
mi
Hp = 215
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15533185
19 X = 4732351
53
Y = 6799222
04 feet Y = 2125334
98 meter
Z = -14428988
93 Z = -4374962
87
XDOT = 621
138586 XDOT = 96
074086
YDOT = 22464
252794 feet/sec YDOT = 6848
700317 meter/sec
ZDOT = 11258
506934 ZDOT = 3432
285465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14366213
66 X = 4378821
92
Y = 9168682
05 feet Y = 2794614
29 meter
Z = -14326624
13 Z = -4366755
03
XDOT = -2320
395543 XDOT = -707
256561
YDOT = 21224
509088 feet/sec YDOT = 6469
230370 meter/sec
ZDOT = 11260
618309 ZDOT = 3432
236461
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 18086
47375230
00016717 00000-0 10270-3 0 9157
2 25544 51
6381 66
0807 0001698 265
0831 95
0128 15
54112967 25803
Satellite: ISS
Catalog Number: 25544
Epoch time: 18086
47375230 = yrday
fracday
Element set: 915
Inclination: 51
6381 deg
RA of node: 66
0807 deg
Eccentricity:
0001698
Arg of perigee: 265
0831 deg
Mean anomaly: 95
0128 deg
Mean motion: 15
54112967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2580
Checksum: 314
Coasting Arc #17 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2018/087/11:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 919900
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4855493
63 A = 6785014
82 meter
Y = -3495938
86 meter E =
0011096
Z = 3189376
55 I = 51
97445
XDOT = 1027
352770 Wp = 94
20663
YDOT = -5858
129770 meter/sec RA = 60
39019 deg
ZDOT = -4843
503311 TA = 49
12667
MA = 49
03057
Ha = 220
375 n
mi
Hp = 215
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15930097
20 X = -4831532
39
Y = -11469615
68 feet Y = -3550102
00 meter
Z = 10463833
83 Z = 3165849
06
XDOT = 3370
579954 XDOT = 1116
310583
YDOT = -19219
585859 feet/sec YDOT = -5846
144349 meter/sec
ZDOT = -15890
758893 ZDOT = -4838
296122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14234614
35 X = -4338710
45
Y = -13596790
86 feet Y = -4144301
85 meter
Z = 10359292
05 Z = 3157512
22
XDOT = 5142
059981 XDOT = 1567
299882
YDOT = -17506
482650 feet/sec YDOT = -5335
975912 meter/sec
ZDOT = -15866
663966 ZDOT = -4836
159177
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 18087
50257710
00016717 00000-0 10270-3 0 9165
2 25544 51
6377 60
9511 0001799 273
8067 86
2880 15
54158322 25962
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
50257710 = yrday
fracday
Element set: 916
Inclination: 51
6377 deg
RA of node: 60
9511 deg
Eccentricity:
0001799
Arg of perigee: 273
8067 deg
Mean anomaly: 86
2880 deg
Mean motion: 15
54158322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 331
Coasting Arc #18 (Orbit 2597)
---------------------------------------
Vector Time (GMT): 2018/087/13:50:30
000
Vector Time (MET): N/A
Weight (LBS) : 904774
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1007009
26 A = 6781118
42 meter
Y = 5080813
07 meter E =
0007755
Z = 4372300
11 I = 51
96153
XDOT = -5497
306928 Wp = 112
98011
YDOT = -4076
359214 meter/sec RA = 59
87868 deg
ZDOT = 3462
983995 TA = 302
00458
MA = 302
07991
Ha = 220
280 n
mi
Hp = 215
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3303836
14 X = -1084987
58
Y = 16669334
23 feet Y = 5069116
49 meter
Z = 14344816
64 Z = 4367218
49
XDOT = -18035
783886 XDOT = -5468
136600
YDOT = -13373
881937 feet/sec YDOT = -4137
670390 meter/sec
ZDOT = 11361
496048 ZDOT = 3436
351544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6141741
73 X = 1872002
88
Y = 15866079
57 feet Y = 4835981
05 meter
Z = 14321394
11 Z = 4365160
92
XDOT = -21307
370975 XDOT = -6494
486673
YDOT = -1923
691166 feet/sec YDOT = -586
341067 meter/sec
ZDOT = 11243
175750 ZDOT = 3426
919968
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 18087
63118010
00016717 00000-0 10270-3 0 9179
2 25544 51
6393 60
3103 0001897 271
2439 88
8496 15
54171297 25984
Satellite: ISS
Catalog Number: 25544
Epoch time: 18087
63118010 = yrday
fracday
Element set: 917
Inclination: 51
6393 deg
RA of node: 60
3103 deg
Eccentricity:
0001897
Arg of perigee: 271
2439 deg
Mean anomaly: 88
8496 deg
Mean motion: 15
54171297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2598
Checksum: 327
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