[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 1st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6283 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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
307/03:22:44
976 2
3 4
6 4
6
N/A 3
4 -0
5 223
7
000/00:01:29
951 -2
0 -0
1 214
4
308/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 214
7
311/14:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
2
314/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2016/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3428736
97 A = 6783044
79 meter
Y = 4600802
70 meter E =
0017999
Z = 3607324
16 I = 52
00900
XDOT = -2791
149988 Wp = 106
29948
YDOT = -5589
450051 meter/sec RA = 97
28748 deg
ZDOT = 4452
584536 TA = 296
18092
MA = 296
36591
Ha = 222
878 n
mi
Hp = 212
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11249137
03 X = -3497452
79
Y = 15094497
05 feet Y = 4562076
23 meter
Z = 11835053
02 Z = 3590500
62
XDOT = -9157
316233 XDOT = -2750
069214
YDOT = -18338
090718 feet/sec YDOT = -5620
432644 meter/sec
ZDOT = 14608
216981 ZDOT = 4439
125520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -818205
77 X = -249389
12
Y = -18854035
10 feet Y = -5746709
90 meter
Z = 11760582
67 Z = 3584625
60
XDOT = 17408
015113 XDOT = 5305
963006
YDOT = 8368
464055 feet/sec YDOT = 2550
707844 meter/sec
ZDOT = 14550
242085 ZDOT = 4434
913787
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 16305
55671803
00016717 00000-0 10270-3 0 9007
2 25544 51
6396 97
8765 0006846 129
8843 230
2912 15
54415558 26193
Satellite: ISS
Catalog Number: 25544
Epoch time: 16305
55671803 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 97
8765 deg
Eccentricity:
0006846
Arg of perigee: 129
8843 deg
Mean anomaly: 230
2912 deg
Mean motion: 15
54415558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2619
Checksum: 334
Coasting Arc #2 (Orbit 2633)
---------------------------------------
Vector Time (GMT): 2016/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3824203
71 A = 6779111
43 meter
Y = -3005638
99 meter E =
0015379
Z = -4734815
35 I = 51
99970
XDOT = 1920
554765 Wp = 93
78890
YDOT = 6859
250655 meter/sec RA = 92
32211 deg
ZDOT = -2811
869448 TA = 148
48467
MA = 148
39245
Ha = 222
836 n
mi
Hp = 212
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12546600
10 X = 3880529
63
Y = -9861020
31 feet Y = -2962559
40 meter
Z = -15534171
08 Z = -4716100
90
XDOT = 6301
032692 XDOT = 1857
369354
YDOT = 22504
103198 feet/sec YDOT = 6880
374201 meter/sec
ZDOT = -9225
293465 ZDOT = -2802
693326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3252861
80 X = -991472
28
Y = 15704512
49 feet Y = 4786735
41 meter
Z = -15451684
19 Z = -4709673
34
XDOT = -18272
121232 XDOT = -5569
342551
YDOT = -12794
427873 feet/sec YDOT = -3899
741616 meter/sec
ZDOT = -9186
310763 ZDOT = -2799
987520
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 16306
52107948
00016717 00000-0 10270-3 0 9010
2 25544 51
6403 93
0681 0006879 131
8023 228
3719 15
54414638 26344
Satellite: ISS
Catalog Number: 25544
Epoch time: 16306
52107948 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 93
0681 deg
Eccentricity:
0006879
Arg of perigee: 131
8023 deg
Mean anomaly: 228
3719 deg
Mean motion: 15
54414638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2634
Checksum: 308
Coasting Arc #3 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2016/307/03:23:29
951
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3292463
68 A = 6783191
50 meter
Y = -4098115
13 meter E =
0010568
Z = -4292937
40 I = 52
00734
XDOT = 2907
766677 Wp = 110
67383
YDOT = 6102
266490 meter/sec RA = 89
14676 deg
ZDOT = -3606
002226 TA = 122
70495
MA = 122
60300
Ha = 223
660 n
mi
Hp = 214
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10802046
18 X = 3358898
94
Y = -13445259
61 feet Y = -4060925
23 meter
Z = -14084440
28 Z = -4276781
54
XDOT = 9539
916920 XDOT = 2856
830333
YDOT = 20020
559349 feet/sec YDOT = 6134
498198 meter/sec
ZDOT = -11830
715964 ZDOT = -3592
000517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13792408
27 X = -4203926
04
Y = -10451657
59 feet Y = -3185665
23 meter
Z = -14012958
06 Z = -4271149
62
XDOT = 18935
261249 XDOT = 5771
467629
YDOT = -9254
196451 feet/sec YDOT = -2820
679078 meter/sec
ZDOT = -11770
475451 ZDOT = -3587
640918
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 16307
16399036
00016717 00000-0 10270-3 0 9023
2 25544 51
6418 89
8654 0006925 162
2648 197
8748 15
53582679 26449
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
16399036 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 89
8654 deg
Eccentricity:
0006925
Arg of perigee: 162
2648 deg
Mean anomaly: 197
8748 deg
Mean motion: 15
53582679 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 356
Coasting Arc #4 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/03:23:29
951
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3654499
70 A = 6780340
21 meter
Y = 2740368
70 meter E =
0012132
Z = 5008293
27 I = 51
99668
XDOT = -2356
590415 Wp = 146
76444
YDOT = -6991
605130 meter/sec RA = 84
18413 deg
ZDOT = 2093
718144 TA = 282
89731
MA = 283
03280
Ha = 223
577 n
mi
Hp = 214
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11989828
41 X = -3709200
33
Y = 8990710
96 feet Y = 2699195
84 meter
Z = 16431408
36 Z = 4990407
29
XDOT = -7731
595851 XDOT = -2288
403986
YDOT = -22938
337040 feet/sec YDOT = -7017
576829 meter/sec
ZDOT = 6869
154015 ZDOT = 2082
435832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9580948
37 X = 2920273
06
Y = 11635232
29 feet Y = 3546418
80 meter
Z = 16352579
23 Z = 4984266
15
XDOT = -21675
450746 XDOT = -6606
677387
YDOT = 8205
157502 feet/sec YDOT = 2500
932006 meter/sec
ZDOT = 6820
996467 ZDOT = 2079
039723
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 16308
19319066
00016717 00000-0 10270-3 0 9033
2 25544 51
6420 84
7397 0006981 167
5630 192
5696 15
53595502 26602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19319066 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 84
7397 deg
Eccentricity:
0006981
Arg of perigee: 167
5630 deg
Mean anomaly: 192
5696 deg
Mean motion: 15
53595502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 329
Coasting Arc #5 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4159381
10 A = 6780259
84 meter
Y = 1829932
44 meter E =
0017049
Z = -5047103
57 I = 51
99710
XDOT = -795
801150 Wp = 125
87362
YDOT = 7345
315330 meter/sec RA = 83
95747 deg
ZDOT = 2002
383978 TA = 163
54238
MA = 163
48697
Ha = 223
459 n
mi
Hp = 214
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13646263
45 X = 4163126
46
Y = 6003715
34 feet Y = 1876466
31 meter
Z = -16558738
73 Z = -5026888
75
XDOT = -2610
896162 XDOT = -887
606158
YDOT = 24098
803576 feet/sec YDOT = 7335
902857 meter/sec
ZDOT = 6569
501239 ZDOT = 1998
295010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1717272
16 X = 523424
56
Y = -14907364
27 feet Y = -4543764
63 meter
Z = -16470531
24 Z = -5020217
92
XDOT = 22734
591719 XDOT = 6929
503556
YDOT = -4636
345862 feet/sec YDOT = -1413
158219 meter/sec
ZDOT = 6550
271595 ZDOT = 1996
522782
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 16308
19319068
00016717 00000-0 10270-3 0 9046
2 25544 51
6429 84
7400 0006881 167
9378 192
1941 15
53587477 26609
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19319068 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 84
7400 deg
Eccentricity:
0006881
Arg of perigee: 167
9378 deg
Mean anomaly: 192
1941 deg
Mean motion: 15
53587477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 339
Coasting Arc #6 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2016/309/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4073858
88 A = 6782965
86 meter
Y = -3261277
24 meter E =
0011051
Z = 4321908
64 I = 52
00270
XDOT = 1536
015610 Wp = 109
48903
YDOT = -6627
933669 meter/sec RA = 78
99406 deg
ZDOT = -3549
760618 TA = 16
47267
MA = 16
43679
Ha = 223
411 n
mi
Hp = 214
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13365678
74 X = -4058082
10
Y = -10699728
47 feet Y = -3306745
64 meter
Z = 14179490
30 Z = 4302156
74
XDOT = 5039
421294 XDOT = 1627
260290
YDOT = -21745
189204 feet/sec YDOT = -6610
246740 meter/sec
ZDOT = -11646
196252 ZDOT = -3542
077231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6018599
37 X = -1834469
09
Y = 16103763
59 feet Y = 4908427
14 meter
Z = 14093571
67 Z = 4295720
64
XDOT = -21088
411153 XDOT = -6427
747719
YDOT = 2291
247352 feet/sec YDOT = 698
372193 meter/sec
ZDOT = -11611
336050 ZDOT = -3539
135228
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 16309
22238282
00016717 00000-0 10270-3 0 9050
2 25544 51
6434 79
6143 0006721 171
1383 188
9890 15
53621139 26765
Satellite: ISS
Catalog Number: 25544
Epoch time: 16309
22238282 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 79
6143 deg
Eccentricity:
0006721
Arg of perigee: 171
1383 deg
Mean anomaly: 188
9890 deg
Mean motion: 15
53621139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 319
Coasting Arc #7 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2016/310/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3927630
05 A = 6786446
49 meter
Y = 4483390
47 meter E =
0007866
Z = -3255940
13 I = 52
00657
XDOT = -2316
337935 Wp = 139
19664
YDOT = 5507
403626 meter/sec RA = 74
03749 deg
ZDOT = 4790
169494 TA = 183
33625
MA = 183
34150
Ha = 223
201 n
mi
Hp = 214
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12885925
36 X = 3893019
98
Y = 14709286
32 feet Y = 4527118
35 meter
Z = -10682218
29 Z = -3236944
38
XDOT = -7599
533907 XDOT = -2401
020004
YDOT = 18068
909534 feet/sec YDOT = 5481
027289 meter/sec
ZDOT = 15715
779179 ZDOT = 4778
711407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9696003
05 X = 2955341
73
Y = -17033815
49 feet Y = -5191906
96 meter
Z = -10599840
49 Z = -3230831
38
XDOT = 18350
417829 XDOT = 5593
207354
YDOT = 699
158604 feet/sec YDOT = 213
103542 meter/sec
ZDOT = 15664
576786 ZDOT = 4774
563004
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 16310
18724502
00016717 00000-0 10270-3 0 9063
2 25544 51
6430 74
8085 0006700 174
9237 185
1984 15
53600493 26919
Satellite: ISS
Catalog Number: 25544
Epoch time: 16310
18724502 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 74
8085 deg
Eccentricity:
0006700
Arg of perigee: 174
9237 deg
Mean anomaly: 185
1984 deg
Mean motion: 15
53600493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 306
Coasting Arc #8 (Orbit 2706)
---------------------------------------
Vector Time (GMT): 2016/311/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3642046
43 A = 6789427
45 meter
Y = -5395340
60 meter E =
0017981
Z = 1890281
80 I = 52
00657
XDOT = 3155
063287 Wp = 133
29554
YDOT = -4118
684843 meter/sec RA = 69
08923 deg
ZDOT = -5655
192969 TA = 25
98118
MA = 25
89102
Ha = 223
242 n
mi
Hp = 214
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11948971
24 X = -3590626
00
Y = -17701248
70 feet Y = -5435780
90 meter
Z = 6201711
93 Z = 1872714
26
XDOT = 10351
257502 XDOT = 3228
355926
YDOT = -13512
745548 feet/sec YDOT = -4082
993012 meter/sec
ZDOT = -18553
782708 ZDOT = -5639
688181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12543921
88 X = -3823387
39
Y = 17311798
56 feet Y = 5276636
20 meter
Z = 6125765
64 Z = 1867133
37
XDOT = -15015
018825 XDOT = -4576
577738
YDOT = -4313
326854 feet/sec YDOT = -1314
702025 meter/sec
ZDOT = -18485
101821 ZDOT = -5634
259035
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 16311
21642614
00016717 00000-0 10270-3 0 9072
2 25544 51
6429 69
6830 0006817 177
9633 182
1548 15
53588197 27076
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
21642614 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 69
6830 deg
Eccentricity:
0006817
Arg of perigee: 177
9633 deg
Mean anomaly: 182
1548 deg
Mean motion: 15
53588197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2707
Checksum: 332
Coasting Arc #9 (Orbit 2712)
---------------------------------------
Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3982936
09 A = 6778900
74 meter
Y = -1306782
69 meter E =
0016597
Z = -5340456
01 I = 51
96660
XDOT = 2758
208802 Wp = 117
81800
YDOT = 7136
052557 meter/sec RA = 67
08575 deg
ZDOT = 304
119473 TA = 155
11263
MA = 155
03250
Ha = 223
185 n
mi
Hp = 215
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13067375
61 X = 4023194
88
Y = -4287344
77 feet Y = -1262017
74 meter
Z = -17521181
13 Z = -5321009
81
XDOT = 9049
241477 XDOT = 2676
729336
YDOT = 23412
245923 feet/sec YDOT = 7166
441122 meter/sec
ZDOT = 997
767301 ZDOT = 317
320433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1120831
86 X = 341629
55
Y = 13815480
77 feet Y = 4210958
54 meter
Z = -17435757
68 Z = -5314418
94
XDOT = -23862
326529 XDOT = -7273
237126
YDOT = 3294
772226 feet/sec YDOT = 1004
246574 meter/sec
ZDOT = 1054
258786 ZDOT = 321
338078
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 16311
60236511
00016717 00000-0 10270-3 0 9081
2 25544 51
6426 67
7570 0007142 181
2479 178
8656 15
53610659 27139
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
60236511 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 67
7570 deg
Eccentricity:
0007142
Arg of perigee: 181
2479 deg
Mean anomaly: 178
8656 deg
Mean motion: 15
53610659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2713
Checksum: 314
Coasting Arc #10 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4537914
51 A = 6780065
47 meter
Y = -160707
99 meter E =
0005711
Z = 5030063
26 I = 51
95832
XDOT = -1984
458319 Wp = 129
75821
YDOT = -7129
805793 meter/sec RA = 62
11415 deg
ZDOT = -2020
130213 TA = 339
76387
MA = 339
78650
Ha = 223
067 n
mi
Hp = 215
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14888170
96 X = -4560214
39
Y = -527257
19 feet Y = -211578
61 meter
Z = 16502832
23 Z = 5007964
74
XDOT = -6510
690022 XDOT = -1894
770457
YDOT = -23391
751290 feet/sec YDOT = -7151
495893 meter/sec
ZDOT = -6627
723797 ZDOT = -2029
552403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3733646
13 X = 1138015
34
Y = -14532035
09 feet Y = -4429364
30 meter
Z = 16406064
40 Z = 5000568
43
XDOT = 23175
816072 XDOT = 7063
988739
YDOT = -1565
450875 feet/sec YDOT = -477
149427 meter/sec
ZDOT = -6667
654060 ZDOT = -2032
300957
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 16312
63153285
00016717 00000-0 10270-3 0 9092
2 25544 51
6434 62
6304 0006994 185
1103 174
9979 15
53662003 27290
Satellite: ISS
Catalog Number: 25544
Epoch time: 16312
63153285 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 62
6304 deg
Eccentricity:
0006994
Arg of perigee: 185
1103 deg
Mean anomaly: 174
9979 deg
Mean motion: 15
53662003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 316
Coasting Arc #11 (Orbit 2743)
---------------------------------------
Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5014959
91 A = 6782951
63 meter
Y = 1550527
08 meter E =
0012003
Z = -4308065
27 I = 51
95071
XDOT = 999
714025 Wp = 144
56188
YDOT = 6699
525463 meter/sec RA = 57
14767 deg
ZDOT = 3570
459519 TA = 161
76821
MA = 161
72514
Ha = 222
859 n
mi
Hp = 215
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16453280
53 X = 5018175
81
Y = 5087031
09 feet Y = 1606625
59 meter
Z = -14134072
40 Z = -4283695
74
XDOT = 3279
901656 XDOT = 907
379919
YDOT = 21980
070418 feet/sec YDOT = 6710
188765 meter/sec
ZDOT = 11714
106032 ZDOT = 3575
091490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8259630
80 X = -2517535
47
Y = 15210675
90 feet Y = 4636214
01 meter
Z = -14027621
54 Z = -4275619
04
XDOT = -21071
247461 XDOT = -6422
516226
YDOT = -607
629793 feet/sec YDOT = -185
205561 meter/sec
ZDOT = 11733
125489 ZDOT = 3576
256649
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 16313
59637261
00016717 00000-0 10270-3 0 9101
2 25544 51
6421 57
8252 0006999 187
0989 173
0066 15
53664268 27441
Satellite: ISS
Catalog Number: 25544
Epoch time: 16313
59637261 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 57
8252 deg
Eccentricity:
0006999
Arg of perigee: 187
0989 deg
Mean anomaly: 173
0066 deg
Mean motion: 15
53664268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2744
Checksum: 336
Coasting Arc #12 (Orbit 2759)
---------------------------------------
Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5304547
60 A = 6786398
28 meter
Y = -2746503
01 meter E =
0013764
Z = 3202239
67 I = 51
94433
XDOT = 163
833477 Wp = 123
50609
YDOT = -5959
130533 meter/sec RA = 52
18747 deg
ZDOT = -4832
149171 TA = 19
62157
MA = 19
56866
Ha = 222
787 n
mi
Hp = 215
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17403371
40 X = -5288996
60
Y = -9010836
66 feet Y = -2805734
95 meter
Z = 10506035
67 Z = 3176508
99
XDOT = 537
511409 XDOT = 253
930686
YDOT = -19550
953192 feet/sec YDOT = -5956
794869 meter/sec
ZDOT = -15853
507778 ZDOT = -4831
134217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12023799
01 X = 3664853
94
Y = -15551376
69 feet Y = -4740059
61 meter
Z = 10393855
85 Z = 3168047
26
XDOT = 17979
413697 XDOT = 5480
125295
YDOT = 3292
402554 feet/sec YDOT = 1003
524298 meter/sec
ZDOT = -15847
924967 ZDOT = -4830
447530
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 16314
62552648
00016717 00000-0 10270-3 0 9112
2 25544 51
6424 52
6989 0006871 191
8837 168
2154 15
53671956 27602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
62552648 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 52
6989 deg
Eccentricity:
0006871
Arg of perigee: 191
8837 deg
Mean anomaly: 168
2154 deg
Mean motion: 15
53671956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2760
Checksum: 338
Coasting Arc #13 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5335930
63 A = 6787863
58 meter
Y = -3246933
01 meter E =
0015196
Z = 2632606
50 I = 51
94121
XDOT = 772
762625 Wp = 128
41315
YDOT = -5539
246871 meter/sec RA = 50
58878 deg
ZDOT = -5254
316254 TA = 22
03134
MA = 21
96609
Ha = 222
698 n
mi
Hp = 215
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17506334
09 X = -5312014
29
Y = -10652667
36 feet Y = -3306469
13 meter
Z = 8637160
44 Z = 2606743
70
XDOT = 2535
310449 XDOT = 860
170088
YDOT = -18173
382123 feet/sec YDOT = -5530
116826 meter/sec
ZDOT = -17238
570388 ZDOT = -5250
349758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19830677
65 X = -6044390
55
Y = -5350581
00 feet Y = -1630857
09 meter
Z = 8524500
14 Z = 2598267
64
XDOT = -2899
456976 XDOT = -883
754486
YDOT = -16748
381449 feet/sec YDOT = -5104
906666 meter/sec
ZDOT = -17220
137370 ZDOT = -5248
697871
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 16314
94713717
00016717 00000-0 10270-3 0 9124
2 25544 51
6410 51
0976 0006554 192
4411 167
6581 15
53648523 27655
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
94713717 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 51
0976 deg
Eccentricity:
0006554
Arg of perigee: 192
4411 deg
Mean anomaly: 167
6581 deg
Mean motion: 15
53648523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 313
Coasting Arc #14 (Orbit 2779)
---------------------------------------
Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5292676
74 A = 6790110
93 meter
Y = 4085196
80 meter E =
0004111
Z = -1184119
03 I = 51
92801
XDOT = -2109
638335 Wp = 73
88516
YDOT = 4433
037891 meter/sec RA = 45
63741 deg
ZDOT = 5882
476090 TA = 273
31619
MA = 273
36323
Ha = 222
431 n
mi
Hp = 215
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17364425
00 X = 5252353
71
Y = 13402876
65 feet Y = 4144157
55 meter
Z = -3884904
96 Z = -1158506
17
XDOT = -6921
385613 XDOT = -2187
628001
YDOT = 14544
087568 feet/sec YDOT = 4409
010722 meter/sec
ZDOT = 19299
462238 ZDOT = 5872
038145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20564645
79 X = 6268104
04
Y = 7688225
07 feet Y = 2343371
00 meter
Z = -3773510
73 Z = -1150166
07
XDOT = -1890
363475 XDOT = -576
182787
YDOT = 14476
137076 feet/sec YDOT = 4412
326581 meter/sec
ZDOT = 19252
891079 ZDOT = 5868
281201
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 16315
91195751
00016717 00000-0 10270-3 0 9135
2 25544 51
6413 46
2915 0006470 196
1138 163
9810 15
53664508 27803
Satellite: ISS
Catalog Number: 25544
Epoch time: 16315
91195751 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 46
2915 deg
Eccentricity:
0006470
Arg of perigee: 196
1138 deg
Mean anomaly: 163
9810 deg
Mean motion: 15
53664508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2780
Checksum: 312
Coasting Arc #15 (Orbit 2795)
---------------------------------------
Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925979
05 A = 6790590
38 meter
Y = -4643601
91 meter E =
0015294
Z = -394933
03 I = 51
90700
XDOT = 3504
293174 Wp = 159
29959
YDOT = -3212
458135 meter/sec RA = 40
68866 deg
ZDOT = -6021
800407 TA = 24
94425
MA = 24
87041
Ha = 222
280 n
mi
Hp = 215
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16161348
58 X = -4871768
53
Y = -15234914
41 feet Y = -4698384
43 meter
Z = -1295712
03 Z = -418730
88
XDOT = 11497
024848 XDOT = 3569
207259
YDOT = -10539
560810 feet/sec YDOT = -3172
908087 meter/sec
ZDOT = -19756
563014 ZDOT = -6004
619211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20088102
50 X = -6122853
64
Y = -9459466
75 feet Y = -2883245
47 meter
Z = -1399035
98 Z = -426426
17
XDOT = 7082
487151 XDOT = 2158
742084
YDOT = -12167
750347 feet/sec YDOT = -3708
730306 meter/sec
ZDOT = -19680
691188 ZDOT = -5998
674674
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 16316
94109109
00016717 00000-0 10270-3 0 9142
2 25544 51
6418 41
1651 0006408 200
0739 160
0162 15
53669562 27962
Satellite: ISS
Catalog Number: 25544
Epoch time: 16316
94109109 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 41
1651 deg
Eccentricity:
0006408
Arg of perigee: 200
0739 deg
Mean anomaly: 160
0162 deg
Mean motion: 15
53669562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2796
Checksum: 298
Coasting Arc #16 (Orbit 2811)
---------------------------------------
Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4263997
68 A = 6788995
51 meter
Y = 4920265
78 meter E =
0010259
Z = 1915688
95 I = 51
87699
XDOT = -4816
788290 Wp = 92
64482
YDOT = 1973
465296 meter/sec RA = 35
73721 deg
ZDOT = 5626
264672 TA = 288
38199
MA = 288
49353
Ha = 222
107 n
mi
Hp = 215
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13989493
71 X = 4199355
25
Y = 16142604
25 feet Y = 4967587
28 meter
Z = 6285068
75 Z = 1936245
80
XDOT = -15803
111187 XDOT = -4865
828802
YDOT = 6474
623673 feet/sec YDOT = 1919
326691 meter/sec
ZDOT = 18458
873597 ZDOT = 5602
746112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18462078
06 X = 5627241
39
Y = 10691764
56 feet Y = 3258849
84 meter
Z = 6374130
53 Z = 1942834
99
XDOT = -12147
944160 XDOT = -3702
693380
YDOT = 9982
548998 feet/sec YDOT = 3042
680935 meter/sec
ZDOT = 18355
488919 ZDOT = 5594
753023
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 16317
97021547
00016717 00000-0 10270-3 0 9156
2 25544 51
6419 36
0392 0006441 204
4383 155
6465 15
53693820 28127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16317
97021547 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 36
0392 deg
Eccentricity:
0006441
Arg of perigee: 204
4383 deg
Mean anomaly: 155
6465 deg
Mean motion: 15
53693820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2812
Checksum: 307
Coasting Arc #17 (Orbit 2826)
---------------------------------------
Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3252244
38 A = 6785842
00 meter
Y = -4954795
17 meter E =
0006129
Z = -3299721
27 I = 51
84129
XDOT = 5977
600659 Wp = 163
22698
YDOT = -773
307470 meter/sec RA = 30
77748 deg
ZDOT = -4738
320686 TA = 54
98979
MA = 54
93228
Ha = 221
865 n
mi
Hp = 216
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10670093
11 X = -3180567
79
Y = -16255889
67 feet Y = -4990763
19 meter
Z = -10825857
18 Z = -3315346
20
XDOT = 19611
550717 XDOT = 6008
821095
YDOT = -2537
097998 feet/sec YDOT = -706
287376 meter/sec
ZDOT = -15545
671543 ZDOT = -4709
206323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15537116
08 X = -4735712
98
Y = -11629189
50 feet Y = -3544576
96 meter
Z = -10893300
48 Z = -3320277
99
XDOT = 16793
951610 XDOT = 5118
796451
YDOT = -8019
250492 feet/sec YDOT = -2444
267550 meter/sec
ZDOT = -15418
020023 ZDOT = -4699
412503
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 16318
93501034
00016717 00000-0 10270-3 0 9168
2 25544 51
6431 31
2331 0006277 208
2832 151
7980 15
53719642 28275
Satellite: ISS
Catalog Number: 25544
Epoch time: 16318
93501034 = yrday
fracday
Element set: 916
Inclination: 51
6431 deg
RA of node: 31
2331 deg
Eccentricity:
0006277
Arg of perigee: 208
2832 deg
Mean anomaly: 151
7980 deg
Mean motion: 15
53719642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2827
Checksum: 297
Coasting Arc #18 (Orbit 2842)
---------------------------------------
Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893386
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1994793
35 A = 6782349
80 meter
Y = 4786176
80 meter E =
0010206
Z = 4372046
89 I = 51
80095
XDOT = -6843
786520 Wp = 145
90981
YDOT = -301
938136 meter/sec RA = 25
80803 deg
ZDOT = 3440
952590 TA = 269
20069
MA = 269
31764
Ha = 221
746 n
mi
Hp = 216
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6544597
60 X = 1919886
73
Y = 15702679
78 feet Y = 4808064
98 meter
Z = 14343985
87 Z = 4381555
54
XDOT = -22453
367847 XDOT = -6856
616649
YDOT = -990
610684 feet/sec YDOT = -378
541773 meter/sec
ZDOT = 11289
214534 ZDOT = 3407
675093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11665158
65 X = 3555540
36
Y = 12335365
88 feet Y = 3759819
52 meter
Z = 14384667
63 Z = 4384446
69
XDOT = -20476
687742 XDOT = -6241
294424
YDOT = 6322
989379 feet/sec YDOT = 1927
247163 meter/sec
ZDOT = 11143
549645 ZDOT = 3396
553932
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 16319
96411570
00016717 00000-0 10270-3 0 9178
2 25544 51
6426 26
1071 0006291 211
6181 148
4594 15
53727919 28432
Satellite: ISS
Catalog Number: 25544
Epoch time: 16319
96411570 = yrday
fracday
Element set: 917
Inclination: 51
6426 deg
RA of node: 26
1071 deg
Eccentricity:
0006291
Arg of perigee: 211
6181 deg
Mean anomaly: 148
4594 deg
Mean motion: 15
53727919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2843
Checksum: 314
- 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