[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 5th 2017
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) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
156/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
5
160/01:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 216
6
165/09:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
7
167/11:41:11
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
6
167/16:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
6
Coasting Arc #1 (Orbit 1994)
---------------------------------------
Vector Time (GMT): 2017/156/15:02:17
595
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2571226
70 A = 6786906
75 meter
Y = -5697995
75 meter E =
0005402
Z = -2634306
63 I = 52
02422
XDOT = 3755
649782 Wp = 182
09188
YDOT = 4124
443127 meter/sec RA = 95
08229 deg
ZDOT = -5260
346751 TA = 27
42219
MA = 27
39370
Ha = 220
230 n
mi
Hp = 216
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8435783
12 X = 2647548
41
Y = -18694211
78 feet Y = -5668815
59 meter
Z = -8642738
28 Z = -2621631
35
XDOT = 12321
685638 XDOT = 3734
802559
YDOT = 13531
637557 feet/sec YDOT = 4166
325230 meter/sec
ZDOT = -17258
355481 ZDOT = -5242
153018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20469718
92 X = -6239170
33
Y = 1614832
71 feet Y = 492201
01 meter
Z = -8585792
82 Z = -2616949
65
XDOT = 5941
454194 XDOT = 1810
955238
YDOT = -15935
920871 feet/sec YDOT = -4857
268681 meter/sec
ZDOT = -17178
723711 ZDOT = -5236
074987
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 17156
65350387
00016717 00000-0 10270-3 0 9004
2 25544 51
6415 95
8203 0004840 240
9023 119
1645 15
53962388 19958
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
65350387 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 95
8203 deg
Eccentricity:
0004840
Arg of perigee: 240
9023 deg
Mean anomaly: 119
1645 deg
Mean motion: 15
53962388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1995
Checksum: 316
Coasting Arc #2 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2017/156/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1541726
25 A = 6788970
17 meter
Y = 6467657
43 meter E =
0008927
Z = 1350483
75 I = 52
02840
XDOT = -4406
074128 Wp = 59
04213
YDOT = -2276
303986 meter/sec RA = 94
28616 deg
ZDOT = 5847
469403 TA = 315
58340
MA = 315
65497
Ha = 220
098 n
mi
Hp = 216
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5058156
99 X = -1620494
78
Y = 21219348
52 feet Y = 6449976
26 meter
Z = 4430720
97 Z = 1342803
67
XDOT = -14455
623781 XDOT = -4408
696936
YDOT = -7468
188930 feet/sec YDOT = -2325
590867 meter/sec
ZDOT = 19184
610902 ZDOT = 5826
059211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6546543
22 X = 1995386
37
Y = -20815801
74 feet Y = -6344656
37 meter
Z = 4395698
13 Z = 1339808
79
XDOT = 12509
702943 XDOT = 3812
957457
YDOT = 7982
437806 feet/sec YDOT = 2433
047043 meter/sec
ZDOT = 19090
460198 ZDOT = 5818
772268
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 17156
84642591
00016717 00000-0 10270-3 0 9017
2 25544 51
6380 94
8560 0004880 241
5625 118
5036 15
53990708 19980
Satellite: ISS
Catalog Number: 25544
Epoch time: 17156
84642591 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 94
8560 deg
Eccentricity:
0004880
Arg of perigee: 241
5625 deg
Mean anomaly: 118
5036 deg
Mean motion: 15
53990708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1998
Checksum: 331
Coasting Arc #3 (Orbit 2012)
---------------------------------------
Vector Time (GMT): 2017/157/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2192734
20 A = 6786190
89 meter
Y = -5730697
59 meter E =
0004002
Z = -2893318
90 I = 52
02096
XDOT = 4015
732165 Wp = 183
35932
YDOT = 4100
932974 meter/sec RA = 89
33795 deg
ZDOT = -5082
740097 TA = 29
39821
MA = 29
37570
Ha = 219
993 n
mi
Hp = 216
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7194009
83 X = 2270707
90
Y = -18801501
27 feet Y = -5705740
67 meter
Z = -9492516
06 Z = -2882478
33
XDOT = 13174
974296 XDOT = 3994
265790
YDOT = 13454
504507 feet/sec YDOT = 4145
720113 meter/sec
ZDOT = -16675
656486 ZDOT = -5063
284360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8227262
67 X = -2507669
66
Y = 18398036
98 feet Y = 5607721
67 meter
Z = -9443647
22 Z = -2878423
67
XDOT = -11221
779219 XDOT = -3420
398306
YDOT = -13528
019018 feet/sec YDOT = -4123
340197 meter/sec
ZDOT = -16590
456346 ZDOT = -5056
771094
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 17157
81104384
00016717 00000-0 10270-3 0 9029
2 25544 51
6383 90
0480 0004783 246
1571 113
9080 15
53999135 20135
Satellite: ISS
Catalog Number: 25544
Epoch time: 17157
81104384 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 90
0480 deg
Eccentricity:
0004783
Arg of perigee: 246
1571 deg
Mean anomaly: 113
9080 deg
Mean motion: 15
53999135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2013
Checksum: 298
Coasting Arc #4 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2017/158/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2794508
26 A = 6782504
62 meter
Y = 4590275
18 meter E =
0007015
Z = 4136019
21 I = 52
00734
XDOT = -3553
522683 Wp = 126
56298
YDOT = -5616
227508 meter/sec RA = 84
38059 deg
ZDOT = 3823
560460 TA = 284
14350
MA = 284
22143
Ha = 219
853 n
mi
Hp = 216
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9168334
18 X = -2865721
24
Y = 15059957
93 feet Y = 4558626
42 meter
Z = 13569616
82 Z = 4122271
76
XDOT = -11658
538986 XDOT = -3509
029669
YDOT = -18425
943267 feet/sec YDOT = -5655
717088 meter/sec
ZDOT = 12544
489698 ZDOT = 3806
405715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9778304
50 X = 2980427
21
Y = -14727908
74 feet Y = -4489066
58 meter
Z = 13508095
74 Z = 4117267
58
XDOT = 10014
099620 XDOT = 3052
297564
YDOT = 18111
450904 feet/sec YDOT = 5520
370236 meter/sec
ZDOT = 12469
725800 ZDOT = 3800
772424
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 17158
83996570
00016717 00000-0 10270-3 0 9039
2 25544 51
6383 84
9191 0004884 249
4503 110
6126 15
54004041 20295
Satellite: ISS
Catalog Number: 25544
Epoch time: 17158
83996570 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 84
9191 deg
Eccentricity:
0004884
Arg of perigee: 249
4503 deg
Mean anomaly: 110
6126 deg
Mean motion: 15
54004041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 308
Coasting Arc #5 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2017/159/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3380171
71 A = 6779264
25 meter
Y = -3122320
66 meter E =
0007823
Z = -4985511
32 I = 51
99199
XDOT = 2986
632432 Wp = 76
15623
YDOT = 6711
003501 meter/sec RA = 79
41439 deg
ZDOT = -2179
064707 TA = 172
69105
MA = 172
67964
Ha = 219
854 n
mi
Hp = 216
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11089802
20 X = 3439052
54
Y = -10243834
18 feet Y = -3084191
40 meter
Z = -16356664
44 Z = -4968948
71
XDOT = 9798
662835 XDOT = 2921
951204
YDOT = 22017
728022 feet/sec YDOT = 6744
040684 meter/sec
ZDOT = -7149
162423 ZDOT = -2164
712611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11377082
74 X = -3467734
82
Y = 10044278
22 feet Y = 3061496
00 meter
Z = -16282960
00 Z = -4963046
21
XDOT = -8719
055277 XDOT = -2657
568048
YDOT = -21359
299016 feet/sec YDOT = -6510
314340 meter/sec
ZDOT = -7086
982781 ZDOT = -2160
112352
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 17159
80457937
00016717 00000-0 10270-3 0 9047
2 25544 51
6379 80
1119 0004642 250
7027 109
3623 15
54002635 20447
Satellite: ISS
Catalog Number: 25544
Epoch time: 17159
80457937 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 80
1119 deg
Eccentricity:
0004642
Arg of perigee: 250
7027 deg
Mean anomaly: 109
3623 deg
Mean motion: 15
54002635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 298
Coasting Arc #6 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2017/160/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3526078
60 A = 6778589
67 meter
Y = 2687363
69 meter E =
0004539
Z = 5129349
52 I = 51
99196
XDOT = -2822
010829 Wp = 186
50872
YDOT = -6926
742392 meter/sec RA = 77
97316 deg
ZDOT = 1684
867939 TA = 247
27236
MA = 247
32034
Ha = 219
800 n
mi
Hp = 216
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11568499
33 X = -3580783
46
Y = 8816809
99 feet Y = 2647626
11 meter
Z = 16828574
54 Z = 5112088
23
XDOT = -9258
565711 XDOT = -2752
528789
YDOT = -22725
532781 feet/sec YDOT = -6957
911760 meter/sec
ZDOT = 5527
781951 ZDOT = 1671
327152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11343868
51 X = -3457611
12
Y = -9244407
98 feet Y = -2817695
55 meter
Z = 16751859
74 Z = 5105966
85
XDOT = 19186
558708 XDOT = 5848
063094
YDOT = -13607
767697 feet/sec YDOT = -4147
647594 meter/sec
ZDOT = 5469
227986 ZDOT = 1667
020690
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 17160
12611502
00016717 00000-0 10270-3 0 9055
2 25544 51
6417 78
5110 0004960 251
5475 108
5139 15
54019377 20490
Satellite: ISS
Catalog Number: 25544
Epoch time: 17160
12611502 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 78
5110 deg
Eccentricity:
0004960
Arg of perigee: 251
5475 deg
Mean anomaly: 108
5139 deg
Mean motion: 15
54019377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 289
Coasting Arc #7 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2017/161/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060138
02 A = 6777780
40 meter
Y = -1004817
01 meter E =
0010182
Z = -5341986
90 I = 51
98077
XDOT = 2088
846492 Wp = 98
90636
YDOT = 7368
017803 meter/sec RA = 72
99905 deg
ZDOT = 200
495348 TA = 173
00447
MA = 172
99025
Ha = 219
631 n
mi
Hp = 216
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13320662
80 X = 4097021
35
Y = -3296643
73 feet Y = -959206
80 meter
Z = -17526203
75 Z = -5322174
41
XDOT = 6853
170907 XDOT = 2005
326221
YDOT = 24173
286754 feet/sec YDOT = 7390
909679 meter/sec
ZDOT = 657
793138 ZDOT = 210
440606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6610340
21 X = 2014831
70
Y = 12152250
61 feet Y = 3704005
99 meter
Z = -17438518
94 Z = -5315260
57
XDOT = -20746
593854 XDOT = -6323
561807
YDOT = 12296
074269 feet/sec YDOT = 3747
843437 meter/sec
ZDOT = 700
373962 ZDOT = 213
473984
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 17161
09072487
00016717 00000-0 10270-3 0 9066
2 25544 51
6413 73
7039 0004933 256
3440 103
7163 15
53987140 20640
Satellite: ISS
Catalog Number: 25544
Epoch time: 17161
09072487 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 73
7039 deg
Eccentricity:
0004933
Arg of perigee: 256
3440 deg
Mean anomaly: 103
7163 deg
Mean motion: 15
53987140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 300
Coasting Arc #8 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2017/162/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4507187
03 A = 6779031
09 meter
Y = -683880
50 meter E =
0002584
Z = 5017860
78 I = 51
97564
XDOT = -1197
729326 Wp = 5
14145
YDOT = -7286
100298 meter/sec RA = 68
02503 deg
ZDOT = -2066
265003 TA = 104
87719
MA = 104
84857
Ha = 219
584 n
mi
Hp = 216
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14787359
03 X = -4523579
14
Y = -2243702
42 feet Y = -734375
31 meter
Z = 16462797
83 Z = 4995926
23
XDOT = -3929
558156 XDOT = -1106
128274
YDOT = -23904
528536 feet/sec YDOT = -7298
981641 meter/sec
ZDOT = -6779
084654 ZDOT = -2071
861818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1881533
91 X = -573491
54
Y = -14944438
90 feet Y = -4555064
98 meter
Z = 16366046
43 Z = 4988370
95
XDOT = 20865
599712 XDOT = 6359
834792
YDOT = -10085
924169 feet/sec YDOT = -3074
189687 meter/sec
ZDOT = -6802
461961 ZDOT = -2073
390406
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 17162
11963584
00016717 00000-0 10270-3 0 9078
2 25544 51
6419 68
5761 0004911 261
2328 98
8269 15
54039885 20800
Satellite: ISS
Catalog Number: 25544
Epoch time: 17162
11963584 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 68
5761 deg
Eccentricity:
0004911
Arg of perigee: 261
2328 deg
Mean anomaly: 98
8269 deg
Mean motion: 15
54039885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 332
Coasting Arc #9 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2017/163/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4829229
06 A = 6782222
74 meter
Y = 2242759
09 meter E =
0004104
Z = -4205274
70 I = 51
97206
XDOT = 135
122023 Wp = 137
88514
YDOT = 6695
448499 meter/sec RA = 63
05664 deg
ZDOT = 3725
128603 TA = 170
22474
MA = 170
21675
Ha = 219
495 n
mi
Hp = 216
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15843927
36 X = 4824218
22
Y = 7358133
49 feet Y = 2296735
39 meter
Z = -13796833
00 Z = -4181827
60
XDOT = 443
313724 XDOT = 42
146840
YDOT = 21966
694552 feet/sec YDOT = 6696
439131 meter/sec
ZDOT = 12221
550535 ZDOT = 3725
560131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2461051
80 X = -750128
59
Y = 17376733
51 feet Y = 5296428
37 meter
Z = -13693689
06 Z = -4173836
43
XDOT = -19667
050592 XDOT = -5994
517021
YDOT = 6848
499475 feet/sec YDOT = 2087
422640 meter/sec
ZDOT = 12222
212018 ZDOT = 3725
330223
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 17163
08424021
00016717 00000-0 10270-3 0 9084
2 25544 51
6408 63
7691 0004607 264
4670 95
5957 15
54034206 20950
Satellite: ISS
Catalog Number: 25544
Epoch time: 17163
08424021 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 63
7691 deg
Eccentricity:
0004607
Arg of perigee: 264
4670 deg
Mean anomaly: 95
5957 deg
Mean motion: 15
54034206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 308
Coasting Arc #10 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2017/164/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4949667
69 A = 6785905
34 meter
Y = -3565478
23 meter E =
0008503
Z = 2963139
80 I = 51
96908
XDOT = 1085
835604 Wp = 102
43657
YDOT = -5691
312051 meter/sec RA = 58
09637 deg
ZDOT = -5024
093848 TA = 43
87305
MA = 43
80555
Ha = 219
428 n
mi
Hp = 216
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16239067
21 X = -4923823
17
Y = -11697763
23 feet Y = -3620684
67 meter
Z = 9721587
26 Z = 2939158
14
XDOT = 3562
452770 XDOT = 1173
801210
YDOT = -18672
283632 feet/sec YDOT = -5678
676971 meter/sec
ZDOT = -16483
247532 ZDOT = -5018
606320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6184055
79 X = 1884900
20
Y = -19087636
15 feet Y = -5817911
50 meter
Z = 9616331
29 Z = 2931057
78
XDOT = 17513
393355 XDOT = 5338
082295
YDOT = -2634
739766 feet/sec YDOT = -803
068681 meter/sec
ZDOT = -16457
944002 ZDOT = -5016
381332
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 17164
11314567
00016717 00000-0 10270-3 0 9093
2 25544 51
6410 58
6410 0004814 269
9446 90
1155 15
54053429 21114
Satellite: ISS
Catalog Number: 25544
Epoch time: 17164
11314567 = yrday
fracday
Element set: 909
Inclination: 51
6410 deg
RA of node: 58
6410 deg
Eccentricity:
0004814
Arg of perigee: 269
9446 deg
Mean anomaly: 90
1155 deg
Mean motion: 15
54053429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 291
Coasting Arc #11 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2017/165/01:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4819365
94 A = 6788794
53 meter
Y = 4553155
06 meter E =
0007165
Z = -1438105
36 I = 51
96086
XDOT = -2404
512199 Wp = 4
31672
YDOT = 4379
457354 meter/sec RA = 53
14373 deg
ZDOT = 5816
556616 TA = 340
06973
MA = 340
09771
Ha = 219
516 n
mi
Hp = 216
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15811568
04 X = 4775078
77
Y = 14938172
78 feet Y = 4606801
03 meter
Z = -4718193
43 Z = -1414801
43
XDOT = -7888
819551 XDOT = -2481
559641
YDOT = 14368
298405 feet/sec YDOT = 4352
136949 meter/sec
ZDOT = 19083
190996 ZDOT = 5804
689674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9072187
97 X = -2765202
89
Y = 19794011
07 feet Y = 6033214
57 meter
Z = -4616120
72 Z = -1406993
59
XDOT = -14736
868746 XDOT = -4491
797594
YDOT = -2323
316986 feet/sec YDOT = -708
147017 meter/sec
ZDOT = 19029
950878 ZDOT = 5800
329028
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 17165
07774288
00016717 00000-0 10270-3 0 9101
2 25544 51
6414 53
8332 0004668 274
3973 85
6647 15
54022875 21262
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
07774288 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 53
8332 deg
Eccentricity:
0004668
Arg of perigee: 274
3973 deg
Mean anomaly: 85
6647 deg
Mean motion: 15
54022875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 327
Coasting Arc #12 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5028113
57 A = 6781131
32 meter
Y = 657683
05 meter E =
0004932
Z = -4507176
10 I = 51
92871
XDOT = 2032
668162 Wp = 122
38568
YDOT = 6641
865980 meter/sec RA = 51
57561 deg
ZDOT = 3236
784345 TA = 180
06257
MA = 180
06264
Ha = 219
523 n
mi
Hp = 216
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16496435
58 X = 5042279
07
Y = 2157752
79 feet Y = 713990
57 meter
Z = -14787323
17 Z = -4482716
66
XDOT = 6668
858800 XDOT = 1942
523335
YDOT = 21790
898886 feet/sec YDOT = 6664
092235 meter/sec
ZDOT = 10619
371212 ZDOT = 3246
440240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13764189
50 X = 4195324
96
Y = -9513943
76 feet Y = -2899850
06 meter
Z = -14679413
21 Z = -4474285
15
XDOT = 18803
884742 XDOT = 5731
424069
YDOT = 10755
449304 feet/sec YDOT = 3278
260948 meter/sec
ZDOT = 10660
766370 ZDOT = 3249
401589
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 17165
39927505
00016717 00000-0 10270-3 0 9119
2 25544 51
6409 52
2313 0004716 277
7809 82
2808 15
54031058 21318
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
39927505 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 52
2313 deg
Eccentricity:
0004716
Arg of perigee: 277
7809 deg
Mean anomaly: 82
2808 deg
Mean motion: 15
54031058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2131
Checksum: 301
Coasting Arc #13 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5530542
60 A = 6784875
08 meter
Y = -1994568
05 meter E =
0007927
Z = 3380626
25 I = 51
92016
XDOT = -680
124662 Wp = 84
56896
YDOT = -6044
744034 meter/sec RA = 46
61005 deg
ZDOT = -4668
926910 TA = 56
13927
MA = 56
06387
Ha = 219
616 n
mi
Hp = 216
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18144824
79 X = -5524249
15
Y = -6543858
44 feet Y = -2056379
50 meter
Z = 11091293
46 Z = 3353775
73
XDOT = -2231
380126 XDOT = -589
800903
YDOT = -19831
837381 feet/sec YDOT = -6051
844124 meter/sec
ZDOT = -15318
001673 ZDOT = -4672
011994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17779491
99 X = -5419189
16
Y = 7652107
46 feet Y = 2332362
35 meter
Z = 10973078
72 Z = 3344594
39
XDOT = -14536
708418 XDOT = -4430
788726
YDOT = -11743
748834 feet/sec YDOT = -3579
494645 meter/sec
ZDOT = -15330
481174 ZDOT = -4672
730662
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 17166
42817403
00016717 00000-0 10270-3 0 9120
2 25544 51
6409 47
1038 0004753 281
7970 78
2649 15
54029399 21470
Satellite: ISS
Catalog Number: 25544
Epoch time: 17166
42817403 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 47
1038 deg
Eccentricity:
0004753
Arg of perigee: 281
7970 deg
Mean anomaly: 78
2649 deg
Mean motion: 15
54029399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2147
Checksum: 324
Coasting Arc #14 (Orbit 2161)
---------------------------------------
Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5731359
46 A = 6788080
05 meter
Y = 3073926
58 meter E =
0006755
Z = -1929162
98 I = 51
90836
XDOT = -862
610398 Wp = 357
79579
YDOT = 5136
401783 meter/sec RA = 41
65144 deg
ZDOT = 5627
524328 TA = 341
02195
MA = 341
04712
Ha = 219
675 n
mi
Hp = 216
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18803672
77 X = 5705930
96
Y = 10085060
95 feet Y = 3137876
53 meter
Z = -6329274
87 Z = -1901383
31
XDOT = -2830
086609 XDOT = -947
318605
YDOT = 16851
711888 feet/sec YDOT = 5126
281329 meter/sec
ZDOT = 18463
006327 ZDOT = 5623
128777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20558056
94 X = 6266095
76
Y = -5846678
24 feet Y = -1782067
53 meter
Z = -6207167
84 Z = -1891944
76
XDOT = 9165
533266 XDOT = 2793
654540
YDOT = 12669
087480 feet/sec YDOT = 3861
537864 meter/sec
ZDOT = 18442
613843 ZDOT = 5621
308699
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 17167
39276404
00016717 00000-0 10270-3 0 9138
2 25544 51
6413 42
2958 0004851 285
1303 74
9313 15
54035293 21627
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
39276404 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 42
2958 deg
Eccentricity:
0004851
Arg of perigee: 285
1303 deg
Mean anomaly: 74
9313 deg
Mean motion: 15
54035293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2162
Checksum: 299
Coasting Arc #15 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2017/167/11:41:11
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5596942
10 A = 6789098
79 meter
Y = -3638958
40 meter E =
0009251
Z = 1206261
56 I = 51
91051
XDOT = 1726
192701 Wp = 130
97126
YDOT = -4611
355059 meter/sec RA = 41
17254 deg
ZDOT = -5878
395907 TA = 35
97180
MA = 35
90957
Ha = 219
641 n
mi
Hp = 216
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18362670
95 X = -5561693
76
Y = -11938839
88 feet Y = -3701350
22 meter
Z = 3957551
07 Z = 1179158
65
XDOT = 5663
361879 XDOT = 1806
184130
YDOT = -15129
117646 feet/sec YDOT = -4591
603796 meter/sec
ZDOT = -19286
075811 ZDOT = -5869
816745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15126487
93 X = -4610553
52
Y = 15869491
32 feet Y = 4837020
95 meter
Z = 3838541
48 Z = 1169987
44
XDOT = -12645
558873 XDOT = -3854
366344
YDOT = -7378
767071 feet/sec YDOT = -2249
048203 meter/sec
ZDOT = -19247
305623 ZDOT = -5866
578754
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 17167
52137591
00016717 00000-0 10270-3 0 9147
2 25544 51
6427 41
6561 0004788 284
4969 75
5653 15
54008328 21649
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
52137591 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 41
6561 deg
Eccentricity:
0004788
Arg of perigee: 284
4969 deg
Mean anomaly: 75
5653 deg
Mean motion: 15
54008328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 330
Coasting Arc #16 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2017/167/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3532590
79 A = 6777959
68 meter
Y = -2424219
21 meter E =
0009737
Z = -5260609
16 I = 51
86532
XDOT = 5263
627273 Wp = 95
84384
YDOT = 5473
817872 meter/sec RA = 40
11134 deg
ZDOT = 1012
789340 TA = 183
82803
MA = 183
83548
Ha = 219
587 n
mi
Hp = 216
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11589864
78 X = 3584989
94
Y = -7953475
11 feet Y = -2384421
93 meter
Z = -17259216
42 Z = -5243321
89
XDOT = 17269
118349 XDOT = 5197
106769
YDOT = 17958
720052 feet/sec YDOT = 5532
307288 meter/sec
ZDOT = 3322
799673 ZDOT = 1038
197337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13913802
63 X = -4240927
04
Y = 2575733
23 feet Y = 785083
49 meter
Z = -17182403
16 Z = -5237196
48
XDOT = -8378
290655 XDOT = -2553
702992
YDOT = -22365
050887 feet/sec YDOT = -6816
867510 meter/sec
ZDOT = 3433
971508 ZDOT = 1046
674516
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 17167
71429297
00016717 00000-0 10270-3 0 9156
2 25544 51
6396 40
6892 0004586 282
0011 78
0627 15
54044916 21673
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
71429297 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 40
6892 deg
Eccentricity:
0004586
Arg of perigee: 282
0011 deg
Mean anomaly: 78
0627 deg
Mean motion: 15
54044916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 323
Coasting Arc #17 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2017/168/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4729216
09 A = 6780393
96 meter
Y = 1195945
36 meter E =
0005576
Z = 4709072
09 I = 51
84701
XDOT = -4263
359357 Wp = 30
85525
YDOT = -5712
795056 meter/sec RA = 35
12946 deg
ZDOT = -2824
591816 TA = 87
11143
MA = 87
04762
Ha = 219
847 n
mi
Hp = 216
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15515800
83 X = -4765112
41
Y = 3923705
26 feet Y = 1142858
95 meter
Z = 15449711
59 Z = 4686011
88
XDOT = -13987
399465 XDOT = -4185
440003
YDOT = -18742
765932 feet/sec YDOT = -5760
034914 meter/sec
ZDOT = -9267
033516 ZDOT = -2845
113189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15920055
58 X = 4852432
94
Y = 2414725
92 feet Y = 736008
46 meter
Z = 15347640
07 Z = 4677960
69
XDOT = 5777
366817 XDOT = 1760
941406
YDOT = 21508
383420 feet/sec YDOT = 6555
755266 meter/sec
ZDOT = -9356
567597 ZDOT = -2851
881804
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 17168
74318527
00016717 00000-0 10270-3 0 9164
2 25544 51
6390 35
5598 0004517 285
8207 74
2448 15
54009682 21833
Satellite: ISS
Catalog Number: 25544
Epoch time: 17168
74318527 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 35
5598 deg
Eccentricity:
0004517
Arg of perigee: 285
8207 deg
Mean anomaly: 74
2448 deg
Mean motion: 15
54009682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 331
Coasting Arc #18 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2017/169/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5688406
99 A = 6783903
38 meter
Y = -55275
42 meter E =
0001306
Z = -3696430
71 I = 51
83273
XDOT = 2876
921090 Wp = 61
98763
YDOT = 5621
129349 meter/sec RA = 30
15584 deg
ZDOT = 4344
981501 TA = 254
14233
MA = 254
15673
Ha = 219
848 n
mi
Hp = 216
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18662752
60 X = 5706557
87
Y = -181349
79 feet Y = 8438
02 meter
Z = -12127397
34 Z = -3668753
94
XDOT = 9438
717487 XDOT = 2792
744415
YDOT = 18442
025422 feet/sec YDOT = 5652
829986 meter/sec
ZDOT = 14255
188650 ZDOT = 4358
752819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17475240
47 X = -5326453
30
Y = -6774733
78 feet Y = -2064938
86 meter
Z = -12005163
10 Z = -3659173
71
XDOT = -2340
571549 XDOT = -713
406208
YDOT = -19318
922271 feet/sec YDOT = -5888
407508 meter/sec
ZDOT = 14314
920126 ZDOT = 4363
187654
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 17169
70776846
00016717 00000-0 10270-3 0 9174
2 25544 51
6399 30
7529 0004577 289
5463 70
5195 15
54042088 21985
Satellite: ISS
Catalog Number: 25544
Epoch time: 17169
70776846 = yrday
fracday
Element set: 917
Inclination: 51
6399 deg
RA of node: 30
7529 deg
Eccentricity:
0004577
Arg of perigee: 289
5463 deg
Mean anomaly: 70
5195 deg
Mean motion: 15
54042088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 353
Coasting Arc #19 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2017/170/16:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6308490
76 A = 6787426
27 meter
Y = -971355
85 meter E =
0009199
Z = 2296291
24 I = 51
81593
XDOT = -1172
470421 Wp = 105
47020
YDOT = -5277
568877 meter/sec RA = 25
18927 deg
ZDOT = -5437
818358 TA = 49
01965
MA = 48
94010
Ha = 219
866 n
mi
Hp = 216
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20697148
17 X = -6308314
30
Y = -3186863
03 feet Y = -1041900
91 meter
Z = 7533763
90 Z = 2265646
61
XDOT = -3846
687732 XDOT = -1086
953638
YDOT = -17314
858521 feet/sec YDOT = -5290
201544 meter/sec
ZDOT = -17840
611412 ZDOT = -5443
306720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18269219
64 X = 5568458
15
Y = 10333514
59 feet Y = 3149655
25 meter
Z = 7398630
06 Z = 2255102
44
XDOT = -1897
186586 XDOT = -578
262472
YDOT = 16181
960938 feet/sec YDOT = 4932
261694 meter/sec
ZDOT = -17863
822868 ZDOT = -5444
893210
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 17170
73665593
00016717 00000-0 10270-3 0 9186
2 25544 51
6399 25
6242 0004678 292
8076 67
2582 15
54041868 22146
Satellite: ISS
Catalog Number: 25544
Epoch time: 17170
73665593 = yrday
fracday
Element set: 918
Inclination: 51
6399 deg
RA of node: 25
6242 deg
Eccentricity:
0004678
Arg of perigee: 292
8076 deg
Mean anomaly: 67
2582 deg
Mean motion: 15
54041868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 336
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