[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 20th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 ET - UTC (sec) : 67 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
027/19:27:31
970 1
7 1
9 1
9
N/A 0
7 -0
1 222
4
000/00:05:03
941 -0
5 -0
3 212
6
Coasting Arc #1 (Orbit 2184)
---------------------------------------
Vector Time (GMT): 2016/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1814980
27 A = 6787999
93 meter
Y = 6499574
74 meter E =
0017164
Z = -654423
93 I = 52
02264
XDOT = -4414
405703 Wp = 38
91704
YDOT = 1827
269024 meter/sec RA = 78
73956 deg
ZDOT = 6002
997241 TA = 314
04925
MA = 314
19049
Ha = 222
354 n
mi
Hp = 212
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5954659
69 X = 1745344
41
Y = 21324064
12 feet Y = 6519481
73 meter
Z = -2147060
15 Z = -645776
10
XDOT = -14482
958344 XDOT = -4463
670275
YDOT = 5994
977112 feet/sec YDOT = 1777
628459 meter/sec
ZDOT = 19694
872838 ZDOT = 5981
433809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15901427
91 X = -4846755
23
Y = 15410145
70 feet Y = 4697012
41 meter
Z = -2110817
26 Z = -643377
10
XDOT = -11111
059482 XDOT = -3386
650930
YDOT = -8825
191831 feet/sec YDOT = -2689
918470 meter/sec
ZDOT = 19600
989918 ZDOT = 5974
381727
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 16020
50124314
00016717 00000-0 10270-3 0 9006
2 25544 51
6416 79
5333 0006486 36
4346 323
7247 15
54525591 21851
Satellite: ISS
Catalog Number: 25544
Epoch time: 16020
50124314 = yrday
fracday
Element set: 900
Inclination: 51
6416 deg
RA of node: 79
5333 deg
Eccentricity:
0006486
Arg of perigee: 36
4346 deg
Mean anomaly: 323
7247 deg
Mean motion: 15
54525591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2185
Checksum: 291
Coasting Arc #2 (Orbit 2200)
---------------------------------------
Vector Time (GMT): 2016/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -913025
94 A = 6787292
15 meter
Y = -6610369
70 meter E =
0010128
Z = -1240013
72 I = 52
01441
XDOT = 4900
444743 Wp = 102
79027
YDOT = 417
599865 meter/sec RA = 73
79270 deg
ZDOT = -5876
869185 TA = 90
61264
MA = 90
49659
Ha = 222
295 n
mi
Hp = 212
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2995491
93 X = -833015
93
Y = -21687564
64 feet Y = -6620132
33 meter
Z = -4068286
47 Z = -1244254
92
XDOT = 16077
574616 XDOT = 4923
957724
YDOT = 1370
078297 feet/sec YDOT = 472
531656 meter/sec
ZDOT = -19281
066881 ZDOT = -5853
007253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17425544
85 X = 5311306
07
Y = -13248939
69 feet Y = -4038276
82 meter
Z = -4085384
99 Z = -1245225
35
XDOT = 5807
912428 XDOT = 1770
251708
YDOT = 13509
542421 feet/sec YDOT = 4117
708530 meter/sec
ZDOT = -19177
646971 ZDOT = -5845
346797
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 16021
52977777
00016717 00000-0 10270-3 0 9019
2 25544 51
6421 74
4019 0006520 41
6034 318
5614 15
54600769 22013
Satellite: ISS
Catalog Number: 25544
Epoch time: 16021
52977777 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 74
4019 deg
Eccentricity:
0006520
Arg of perigee: 41
6034 deg
Mean anomaly: 318
5614 deg
Mean motion: 15
54600769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2201
Checksum: 286
Coasting Arc #3 (Orbit 2216)
---------------------------------------
Vector Time (GMT): 2016/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -100003
13 A = 6784324
09 meter
Y = 6102674
58 meter E =
0019006
Z = 2938333
94 I = 51
99376
XDOT = -5205
544343 Wp = 69
92399
YDOT = -2524
497668 meter/sec RA = 68
83971 deg
ZDOT = 5046
018466 TA = 323
47789
MA = 323
60736
Ha = 222
447 n
mi
Hp = 212
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -328094
26 X = -182510
21
Y = 20021898
24 feet Y = 6101094
82 meter
Z = 9640203
21 Z = 2937648
05
XDOT = -17078
557557 XDOT = -5201
438844
YDOT = -8282
472664 feet/sec YDOT = -2582
686789 meter/sec
ZDOT = 16555
178694 ZDOT = 5020
741544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17461108
94 X = -5322146
00
Y = 9806851
23 feet Y = 2989128
25 meter
Z = 9636021
83 Z = 2937059
46
XDOT = -850
298395 XDOT = -259
170951
YDOT = -17737
971812 feet/sec YDOT = -5406
533808 meter/sec
ZDOT = 16446
033350 ZDOT = 5012
750965
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 16022
55830037
00016717 00000-0 10270-3 0 9021
2 25544 51
6413 69
2708 0006661 45
8532 314
3167 15
54591150 22173
Satellite: ISS
Catalog Number: 25544
Epoch time: 16022
55830037 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 69
2708 deg
Eccentricity:
0006661
Arg of perigee: 45
8532 deg
Mean anomaly: 314
3167 deg
Mean motion: 15
54591150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2217
Checksum: 288
Coasting Arc #4 (Orbit 2231)
---------------------------------------
Vector Time (GMT): 2016/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1268878
34 A = 6780031
65 meter
Y = -5083806
79 meter E =
0014863
Z = -4318506
97 I = 51
96817
XDOT = 5220
823594 Wp = 60
52088
YDOT = 4324
070361 meter/sec RA = 63
87428 deg
ZDOT = -3558
438150 TA = 173
32703
MA = 173
30722
Ha = 222
395 n
mi
Hp = 211
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4162986
69 X = 1346609
42
Y = -16679156
13 feet Y = -5069182
58 meter
Z = -14168329
95 Z = -4312154
59
XDOT = 17128
686333 XDOT = 5189
367747
YDOT = 14186
582549 feet/sec YDOT = 4382
277307 meter/sec
ZDOT = -11674
665846 ZDOT = -3533
153484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16452007
14 X = 5014571
78
Y = -5066044
47 feet Y = -1544130
35 meter
Z = -14139764
33 Z = -4309800
17
XDOT = -3506
089428 XDOT = -1068
656058
YDOT = 20876
111442 feet/sec YDOT = 6363
038768 meter/sec
ZDOT = -11565
843616 ZDOT = -3525
269134
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 16023
52252807
00016717 00000-0 10270-3 0 9033
2 25544 51
6421 64
4599 0006618 49
3826 310
7902 15
54624338 22323
Satellite: ISS
Catalog Number: 25544
Epoch time: 16023
52252807 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 64
4599 deg
Eccentricity:
0006618
Arg of perigee: 49
3826 deg
Mean anomaly: 310
7902 deg
Mean motion: 15
54624338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2232
Checksum: 300
Coasting Arc #5 (Orbit 2247)
---------------------------------------
Vector Time (GMT): 2016/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2484121
99 A = 6776683
83 meter
Y = 3655585
09 meter E =
0009514
Z = 5128630
86 I = 51
94108
XDOT = -4920
175667 Wp = 82
49404
YDOT = -5657
421136 meter/sec RA = 58
89621 deg
ZDOT = 1647
947905 TA = 351
67658
MA = 351
69235
Ha = 222
547 n
mi
Hp = 211
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8150006
51 X = -2549727
12
Y = 11993389
42 feet Y = 3627439
09 meter
Z = 16826216
72 Z = 5116404
61
XDOT = -16142
308619 XDOT = -4864
552151
YDOT = -18561
092966 feet/sec YDOT = -5712
130815 meter/sec
ZDOT = 5406
653231 ZDOT = 1624
182480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14552502
08 X = -4435602
63
Y = -543253
28 feet Y = -165583
60 meter
Z = 16772451
35 Z = 5112243
17
XDOT = 6960
753556 XDOT = 2121
637684
YDOT = -22543
376142 feet/sec YDOT = -6871
221048 meter/sec
ZDOT = 5304
689170 ZDOT = 1616
869259
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 16024
55102539
00016717 00000-0 10270-3 0 9044
2 25544 51
6409 59
3283 0006736 53
0918 307
0852 15
54651258 22488
Satellite: ISS
Catalog Number: 25544
Epoch time: 16024
55102539 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 59
3283 deg
Eccentricity:
0006736
Arg of perigee: 53
0918 deg
Mean anomaly: 307
0852 deg
Mean motion: 15
54651258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2248
Checksum: 306
Coasting Arc #6 (Orbit 2262)
---------------------------------------
Vector Time (GMT): 2016/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3690494
15 A = 6775944
83 meter
Y = -2023220
89 meter E =
0020424
Z = -5327613
68 I = 51
92218
XDOT = 4190
006115 Wp = 81
97590
YDOT = 6387
826877 meter/sec RA = 53
91038 deg
ZDOT = 480
959584 TA = 192
57687
MA = 192
62791
Ha = 222
466 n
mi
Hp = 211
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12107920
45 X = 3738722
67
Y = -6637863
81 feet Y = -1981681
71 meter
Z = -17479047
52 Z = -5309569
46
XDOT = 13746
739221 XDOT = 4115
928212
YDOT = 20957
437260 feet/sec YDOT = 6434
268108 meter/sec
ZDOT = 1577
951392 ZDOT = 501
133158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12268925
20 X = 3739568
40
Y = 6548336
41 feet Y = 1995932
94 meter
Z = -17400368
98 Z = -5303632
46
XDOT = -9460
186978 XDOT = -2883
464991
YDOT = 22108
587186 feet/sec YDOT = 6738
697374 meter/sec
ZDOT = 1664
184068 ZDOT = 507
243304
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 16025
51523102
00016717 00000-0 10270-3 0 9055
2 25544 51
6420 54
5173 0006685 55
7867 304
3918 15
54643879 22631
Satellite: ISS
Catalog Number: 25544
Epoch time: 16025
51523102 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 54
5173 deg
Eccentricity:
0006685
Arg of perigee: 55
7867 deg
Mean anomaly: 304
3918 deg
Mean motion: 15
54643879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2263
Checksum: 310
Coasting Arc #7 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2016/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4745731
18 A = 6777903
11 meter
Y = 307471
69 meter E =
0014212
Z = 4821709
52 I = 51
90829
XDOT = -3046
893908 Wp = 60
00775
YDOT = -6559
429606 meter/sec RA = 48
92466 deg
ZDOT = -2568
026045 TA = 55
21893
MA = 55
08525
Ha = 222
596 n
mi
Hp = 211
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15569984
18 X = -4772237
96
Y = 1008765
38 feet Y = 254253
69 meter
Z = 15819256
95 Z = 4798592
07
XDOT = -9996
371088 XDOT = -2960
844210
YDOT = -21520
438341 feet/sec YDOT = -6593
020923 meter/sec
ZDOT = -8425
282300 ZDOT = -2582
617603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9682599
39 X = -2951256
29
Y = -12363406
88 feet Y = -3768366
42 meter
Z = 15718916
78 Z = 4791125
84
XDOT = 11246
609289 XDOT = 3427
966511
YDOT = -19651
502684 feet/sec YDOT = -5989
778018 meter/sec
ZDOT = -8487
261062 ZDOT = -2586
917172
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 16026
54370388
00016717 00000-0 10270-3 0 9066
2 25544 51
6406 49
3851 0006828 59
6523 300
5304 15
54701021 22799
Satellite: ISS
Catalog Number: 25544
Epoch time: 16026
54370388 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 49
3851 deg
Eccentricity:
0006828
Arg of perigee: 59
6523 deg
Mean anomaly: 300
5304 deg
Mean motion: 15
54701021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 299
Coasting Arc #8 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2016/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5522906
98 A = 6781856
73 meter
Y = 1250589
74 meter E =
0011902
Z = -3740119
41 I = 51
90080
XDOT = 1514
989056 Wp = 79
69567
YDOT = 6151
735995 meter/sec RA = 43
94805 deg
ZDOT = 4307
800175 TA = 235
85073
MA = 235
96366
Ha = 222
560 n
mi
Hp = 211
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18119773
54 X = 5526679
63
Y = 4102984
72 feet Y = 1312371
49 meter
Z = -12270732
97 Z = -3713281
93
XDOT = 4970
436536 XDOT = 1425
161208
YDOT = 20182
860875 feet/sec YDOT = 6168
175518 meter/sec
ZDOT = 14133
202673 ZDOT = 4314
941047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7187505
75 X = 2190751
75
Y = 17214460
67 feet Y = 5246967
61 meter
Z = -12154574
01 Z = -3704714
16
XDOT = -12380
535262 XDOT = -3773
587148
YDOT = 15137
160428 feet/sec YDOT = 4613
806498 meter/sec
ZDOT = 14162
938657 ZDOT = 4316
863703
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 16027
50788681
00016717 00000-0 10270-3 0 9073
2 25544 51
6417 44
5745 0006884 62
8189 297
3665 15
54697031 22941
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
50788681 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 44
5745 deg
Eccentricity:
0006884
Arg of perigee: 62
8189 deg
Mean anomaly: 297
3665 deg
Mean motion: 15
54697031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 348
Coasting Arc #9 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2016/027/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2480072
34 A = 6776682
23 meter
Y = -3399229
80 meter E =
0019712
Z = -5328969
84 I = 51
87423
XDOT = 5853
721366 Wp = 79
49656
YDOT = 4914
928086 meter/sec RA = 42
42230 deg
ZDOT = -408
619435 TA = 186
59926
MA = 186
62526
Ha = 222
441 n
mi
Hp = 212
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8136720
28 X = 2543784
39
Y = -11152328
75 feet Y = -3371139
98 meter
Z = -17483496
85 Z = -5316767
61
XDOT = 19205
122592 XDOT = 5800
311229
YDOT = 16125
092145 feet/sec YDOT = 4980
089625 meter/sec
ZDOT = -1340
614943 ZDOT = -380
313997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5130341
58 X = -1563728
11
Y = -12889222
34 feet Y = -3928634
97 meter
Z = -17429884
06 Z = -5312628
66
XDOT = 22890
750819 XDOT = 6977
100850
YDOT = -7453
230293 feet/sec YDOT = -2271
744593 meter/sec
ZDOT = -1218
828945 ZDOT = -371
499063
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 16027
82928066
00016717 00000-0 10270-3 0 9082
2 25544 51
6426 42
9704 0005363 59
4615 300
7067 15
54377368 22993
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
82928066 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 42
9704 deg
Eccentricity:
0005363
Arg of perigee: 59
4615 deg
Mean anomaly: 300
7067 deg
Mean motion: 15
54377368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 329
Coasting Arc #10 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2016/028/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3897120
45 A = 6777396
50 meter
Y = 2090497
86 meter E =
0010313
Z = 5129464
44 I = 51
85276
XDOT = -5096
100019 Wp = 58
06764
YDOT = -5504
368868 meter/sec RA = 37
43482 deg
ZDOT = -1620
777289 TA = 47
55394
MA = 47
46678
Ha = 222
489 n
mi
Hp = 212
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12785828
24 X = -3945123
60
Y = 6858588
76 feet Y = 2046649
52 meter
Z = 16828951
56 Z = 5110416
82
XDOT = -16719
488250 XDOT = -5026
297146
YDOT = -18058
952978 feet/sec YDOT = -5560
966621 meter/sec
ZDOT = -5317
510792 ZDOT = -1645
362664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -716064
16 X = -218256
36
Y = 14587422
90 feet Y = 4446246
50 meter
Z = 16745912
92 Z = 5104154
26
XDOT = -22994
353583 XDOT = -7008
678972
YDOT = 5125
897723 feet/sec YDOT = 1562
373626 meter/sec
ZDOT = -5423
032433 ZDOT = -1652
940286
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 16028
85795112
00016717 00000-0 10270-3 0 9091
2 25544 51
6426 37
8400 0005268 61
9314 298
2371 15
54422083 23150
Satellite: ISS
Catalog Number: 25544
Epoch time: 16028
85795112 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 37
8400 deg
Eccentricity:
0005268
Arg of perigee: 61
9314 deg
Mean anomaly: 298
2371 deg
Mean motion: 15
54422083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 305
Coasting Arc #11 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2016/029/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5125839
29 A = 6780553
29 meter
Y = -814792
24 meter E =
0012966
Z = -4374846
39 I = 51
83765
XDOT = 3839
059437 Wp = 93
28497
YDOT = 5656
592146 meter/sec RA = 32
45152 deg
ZDOT = 3452
664023 TA = 211
66101
MA = 211
73907
Ha = 222
457 n
mi
Hp = 212
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16817058
04 X = 5155820
37
Y = -2673202
88 feet Y = -757304
28 meter
Z = -14353170
58 Z = -4349873
83
XDOT = 12595
339360 XDOT = 3758
749373
YDOT = 18558
373181 feet/sec YDOT = 5699
074174 meter/sec
ZDOT = 11327
637872 ZDOT = 3471
117634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6093634
74 X = 1857339
87
Y = -15997786
95 feet Y = -4876125
46 meter
Z = -14244696
87 Z = -4341783
61
XDOT = 21163
099405 XDOT = 6450
512699
YDOT = -2071
600123 feet/sec YDOT = -631
423717 meter/sec
ZDOT = 11406
524052 ZDOT = 3476
708531
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 16029
82232023
00016717 00000-0 10270-3 0 9108
2 25544 51
6432 33
0303 0005303 65
5414 294
6292 15
54402089 23301
Satellite: ISS
Catalog Number: 25544
Epoch time: 16029
82232023 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 33
0303 deg
Eccentricity:
0005303
Arg of perigee: 65
5414 deg
Mean anomaly: 294
6292 deg
Mean motion: 15
54402089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 263
Coasting Arc #12 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2016/030/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6026668
46 A = 6784582
12 meter
Y = -409934
85 meter E =
0018097
Z = 3074046
16 I = 51
82374
XDOT = -2150
453650 Wp = 88
22222
YDOT = -5479
612353 meter/sec RA = 27
47707 deg
ZDOT = -4921
175342 TA = 56
54160
MA = 56
36872
Ha = 222
546 n
mi
Hp = 212
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19772534
33 X = -6036568
78
Y = -1344930
62 feet Y = -477384
28 meter
Z = 10085453
28 Z = 3044746
42
XDOT = -7055
294127 XDOT = -2065
114766
YDOT = -17977
730816 feet/sec YDOT = -5503
183201 meter/sec
ZDOT = -16145
588393 ZDOT = -4931
414081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10750200
97 X = -3276661
26
Y = 16725441
87 feet Y = 5097914
68 meter
Z = 9958468
43 Z = 3035341
18
XDOT = -17882
142119 XDOT = -5450
476918
YDOT = -1804
194889 feet/sec YDOT = -549
918602 meter/sec
ZDOT = -16188
874565 ZDOT = -4934
368967
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 16030
85096772
00016717 00000-0 10270-3 0 9113
2 25544 51
6431 27
8999 0005414 69
8878 290
2857 15
54417718 23467
Satellite: ISS
Catalog Number: 25544
Epoch time: 16030
85096772 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 27
8999 deg
Eccentricity:
0005414
Arg of perigee: 69
8878 deg
Mean anomaly: 290
2857 deg
Mean motion: 15
54417718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 344
Coasting Arc #13 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2016/031/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6467254
47 A = 6787540
21 meter
Y = 1436627
44 meter E =
0013223
Z = -1460252
51 I = 51
80543
XDOT = 185
413479 Wp = 50
40967
YDOT = 5014
295758 meter/sec RA = 22
51090 deg
ZDOT = 5797
449759 TA = 293
69465
MA = 293
83335
Ha = 222
434 n
mi
Hp = 212
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21218026
46 X = 6457802
29
Y = 4713344
62 feet Y = 1508895
66 meter
Z = -4790854
71 Z = -1428859
53
XDOT = 608
311939 XDOT = 101
167371
YDOT = 16451
101569 feet/sec YDOT = 5015
898330 meter/sec
ZDOT = 19020
504459 ZDOT = 5798
145645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14098884
26 X = 4297339
92
Y = -16580859
48 feet Y = -5053845
97 meter
Z = -4655009
67 Z = -1418846
95
XDOT = 13562
821397 XDOT = 4133
947962
YDOT = 6232
990152 feet/sec YDOT = 1899
815398 meter/sec
ZDOT = 19022
495137 ZDOT = 5798
056518
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 16031
81531149
00016717 00000-0 10270-3 0 9123
2 25544 51
6434 23
0899 0005288 72
4953 287
6777 15
54448451 23616
Satellite: ISS
Catalog Number: 25544
Epoch time: 16031
81531149 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 23
0899 deg
Eccentricity:
0005288
Arg of perigee: 72
4953 deg
Mean anomaly: 287
6777 deg
Mean motion: 15
54448451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 323
Coasting Arc #14 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2016/032/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6360731
70 A = 6788404
36 meter
Y = -2327944
99 meter E =
0014551
Z = -383031
14 I = 51
77802
XDOT = 1942
686356 Wp = 119
43596
YDOT = -4348
790660 meter/sec RA = 17
54943 deg
ZDOT = -6008
758165 TA = 64
68523
MA = 64
53457
Ha = 222
410 n
mi
Hp = 212
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20868542
33 X = -6332366
72
Y = -7637614
79 feet Y = -2398916
32 meter
Z = -1256663
83 Z = -413860
73
XDOT = 6373
642900 XDOT = 2020
358902
YDOT = -14267
685894 feet/sec YDOT = -4326
632111 meter/sec
ZDOT = -19713
773508 ZDOT = -5999
132409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16244747
31 X = -4951398
98
Y = 15152057
78 feet Y = 4618347
21 meter
Z = -1389874
97 Z = -423633
89
XDOT = -8683
303777 XDOT = -2646
670991
YDOT = -11065
326063 feet/sec YDOT = -3372
711384 meter/sec
ZDOT = -19671
138045 ZDOT = -5995
762876
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 16032
84393377
00016717 00000-0 10270-3 0 9137
2 25544 51
6432 17
9594 0005211 78
2355 281
9382 15
54419680 23772
Satellite: ISS
Catalog Number: 25544
Epoch time: 16032
84393377 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 17
9594 deg
Eccentricity:
0005211
Arg of perigee: 78
2355 deg
Mean anomaly: 281
9382 deg
Mean motion: 15
54419680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 323
Coasting Arc #15 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2016/033/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5695282
39 A = 6786307
01 meter
Y = 2993336
59 meter E =
0019049
Z = 2131235
73 I = 51
74032
XDOT = -3956
900188 Wp = 72
49264
YDOT = 3575
151662 meter/sec RA = 12
58289 deg
ZDOT = 5517
682534 TA = 311
11412
MA = 311
27843
Ha = 222
288 n
mi
Hp = 212
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18685309
69 X = 5651034
37
Y = 9820658
09 feet Y = 3056777
63 meter
Z = 6992243
20 Z = 2158794
18
XDOT = -12981
955998 XDOT = -4023
386576
YDOT = 11729
500202 feet/sec YDOT = 3530
531307 meter/sec
ZDOT = 18102
632984 ZDOT = 5498
299573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16976369
64 X = 5174397
47
Y = -12478475
50 feet Y = -3803439
33 meter
Z = 7111125
92 Z = 2167471
18
XDOT = 3922
384834 XDOT = 1195
542897
YDOT = 15668
378281 feet/sec YDOT = 4775
721700 meter/sec
ZDOT = 18017
846456 ZDOT = 5491
839600
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 16033
87254056
00016717 00000-0 10270-3 0 9142
2 25544 51
6426 12
8281 0005192 79
4276 280
7462 15
54484510 23933
Satellite: ISS
Catalog Number: 25544
Epoch time: 16033
87254056 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 12
8281 deg
Eccentricity:
0005192
Arg of perigee: 79
4276 deg
Mean anomaly: 280
7462 deg
Mean motion: 15
54484510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 309
Coasting Arc #16 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2016/034/19:30:03
941
Vector Time (MET): N/A
Weight (LBS) : 922299
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4478548
17 A = 6782463
20 meter
Y = -3531620
68 meter E =
0010815
Z = -3681255
05 I = 51
69532
XDOT = 5697
513669 Wp = 80
61032
YDOT = -2703
410703 meter/sec RA = 7
60598 deg
ZDOT = -4347
147322 TA = 143
10370
MA = 143
02925
Ha = 222
283 n
mi
Hp = 212
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14693399
51 X = -4420842
14
Y = -11586682
03 feet Y = -3581380
13 meter
Z = -12077608
43 Z = -3702870
27
XDOT = 18692
630146 XDOT = 5748
436726
YDOT = -8869
457688 feet/sec YDOT = -2639
412616 meter/sec
ZDOT = -14262
294362 ZDOT = -4319
346885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16666114
73 X = -5079831
77
Y = 8374533
99 feet Y = 2552557
96 meter
Z = -12170604
56 Z = -3709600
27
XDOT = 477
578592 XDOT = 145
565955
YDOT = -19557
356361 feet/sec YDOT = -5961
082219 meter/sec
ZDOT = -14141
190313 ZDOT = -4310
234807
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 16034
83684839
00016717 00000-0 10270-3 0 9156
2 25544 51
6417 8
0178 0005108 83
6007 276
5728 15
54485025 24088
Satellite: ISS
Catalog Number: 25544
Epoch time: 16034
83684839 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 8
0178 deg
Eccentricity:
0005108
Arg of perigee: 83
6007 deg
Mean anomaly: 276
5728 deg
Mean motion: 15
54485025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 318
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