[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 12th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
048/10:49:56
623 1
5 2
9 2
9
N/A -2
3 -0
4 222
1
000/00:09:53
245 0
8 0
2 213
2
Coasting Arc #1 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2016/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2360510
86 A = 6775827
48 meter
Y = -3518121
42 meter E =
0021176
Z = -5306312
78 I = 51
41132
XDOT = 6265
592107 Wp = 94
61517
YDOT = -4393
802513 meter/sec RA = 324
21494 deg
ZDOT = 124
637340 TA = 176
58585
MA = 176
57137
Ha = 222
485 n
mi
Hp = 211
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7744458
21 X = -2295219
49
Y = -11542393
13 feet Y = -3544153
66 meter
Z = -17409162
66 Z = -5317620
47
XDOT = 20556
404550 XDOT = 6313
653597
YDOT = -14415
362577 feet/sec YDOT = -4323
467767 meter/sec
ZDOT = 408
915157 ZDOT = 155
190743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1301108
36 X = 396577
83
Y = -13777732
74 feet Y = -4199452
94 meter
Z = -17457480
18 Z = -5321039
96
XDOT = 24044
096466 XDOT = 7328
640603
YDOT = 1578
456506 feet/sec YDOT = 481
113543 meter/sec
ZDOT = 542
216145 ZDOT = 165
267481
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 16043
51582261
00016717 00000-0 10270-3 0 9001
2 25544 51
6429 324
7451 0006414 103
6899 256
4968 15
54658685 25433
Satellite: ISS
Catalog Number: 25544
Epoch time: 16043
51582261 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 324
7451 deg
Eccentricity:
0006414
Arg of perigee: 103
6899 deg
Mean anomaly: 256
4968 deg
Mean motion: 15
54658685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 328
Coasting Arc #2 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2016/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 660163
94 A = 6777374
61 meter
Y = 4612351
04 meter E =
0011745
Z = 4912205
80 I = 51
39099
XDOT = -6557
358347 Wp = 81
81791
YDOT = 3314
413742 meter/sec RA = 319
19396 deg
ZDOT = -2224
628151 TA = 29
98337
MA = 29
91616
Ha = 222
345 n
mi
Hp = 211
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2165892
18 X = 584677
30
Y = 15132385
30 feet Y = 4619311
78 meter
Z = 16116160
77 Z = 4915228
94
XDOT = -21513
642870 XDOT = -6583
127419
YDOT = 10874
060834 feet/sec YDOT = 3240
940739 meter/sec
ZDOT = -7298
648790 ZDOT = -2256
544675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7664641
96 X = -2336182
87
Y = 13211365
68 feet Y = 4026824
26 meter
Z = 16128356
78 Z = 4915923
15
XDOT = -22656
274327 XDOT = -6905
632415
YDOT = -4039
503777 feet/sec YDOT = -1231
240751 meter/sec
ZDOT = -7437
634274 ZDOT = -2266
990927
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 16044
54429414
00016717 00000-0 10270-3 0 9016
2 25544 51
6424 319
6140 0006341 107
2950 252
8897 15
54702407 25593
Satellite: ISS
Catalog Number: 25544
Epoch time: 16044
54429414 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 319
6140 deg
Eccentricity:
0006341
Arg of perigee: 107
2950 deg
Mean anomaly: 252
8897 deg
Mean motion: 15
54702407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 303
Coasting Arc #3 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2016/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 940384
16 A = 6781111
28 meter
Y = -5462100
22 meter E =
0012882
Z = -3920809
43 I = 51
38057
XDOT = 6252
895378 Wp = 108
18099
YDOT = -1812
794174 meter/sec RA = 314
17874 deg
ZDOT = 4032
134325 TA = 204
15858
MA = 204
21905
Ha = 222
329 n
mi
Hp = 211
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3085249
86 X = 1020438
24
Y = -17920276
31 feet Y = -5451136
89 meter
Z = -12863548
00 Z = -3916046
50
XDOT = 20514
748616 XDOT = 6253
115584
YDOT = -5947
487448 feet/sec YDOT = -1742
868637 meter/sec
ZDOT = 13228
787155 ZDOT = 4062
509686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13292533
09 X = 4051564
09
Y = -12430677
63 feet Y = -3788870
54 meter
Z = -12841836
11 Z = -3914191
65
XDOT = 19001
524464 XDOT = 5791
664657
YDOT = 6540
005264 feet/sec YDOT = 1993
393604 meter/sec
ZDOT = 13360
791172 ZDOT = 4072
369149
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 16045
50846845
00016717 00000-0 10270-3 0 9025
2 25544 51
6430 314
8025 0006364 111
0521 249
1313 15
54723810 25741
Satellite: ISS
Catalog Number: 25544
Epoch time: 16045
50846845 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 314
8025 deg
Eccentricity:
0006364
Arg of perigee: 111
0521 deg
Mean anomaly: 249
1313 deg
Mean motion: 15
54723810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 280
Coasting Arc #4 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2354104
73 A = 6785234
56 meter
Y = 5892853
23 meter E =
0020150
Z = 2374631
51 I = 51
37250
XDOT = -5498
691745 Wp = 109
10098
YDOT = -26
244905 meter/sec RA = 309
17497 deg
ZDOT = -5355
285268 TA = 44
24337
MA = 44
08244
Ha = 222
309 n
mi
Hp = 211
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7723440
73 X = -2431359
93
Y = 19333507
98 feet Y = 5866096
24 meter
Z = 7790785
80 Z = 2363008
02
XDOT = -18040
327246 XDOT = -5471
976202
YDOT = -86
105333 feet/sec YDOT = -87
585843 meter/sec
ZDOT = -17569
833557 ZDOT = -5381
931360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17635561
51 X = -5375319
15
Y = 11100594
59 feet Y = 3383461
23 meter
Z = 7739262
30 Z = 2358927
15
XDOT = -13659
092536 XDOT = -4163
291405
YDOT = -9299
377739 feet/sec YDOT = -2834
450335 meter/sec
ZDOT = -17685
312753 ZDOT = -5390
483327
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 16046
53690216
00016717 00000-0 10270-3 0 9039
2 25544 51
6427 309
6705 0006395 115
4524 244
7291 15
54726308 25908
Satellite: ISS
Catalog Number: 25544
Epoch time: 16046
53690216 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 309
6705 deg
Eccentricity:
0006395
Arg of perigee: 115
4524 deg
Mean anomaly: 244
7291 deg
Mean motion: 15
54726308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 311
Coasting Arc #5 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2016/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3419768
48 A = 6787308
44 meter
Y = -5832891
74 meter E =
0013717
Z = -560107
06 I = 51
36111
XDOT = 4388
116433 Wp = 67
26865
YDOT = 2012
544302 meter/sec RA = 304
17964 deg
ZDOT = 5955
490911 TA = 286
66434
MA = 286
81488
Ha = 222
139 n
mi
Hp = 211
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11219712
86 X = 3487459
88
Y = -19136783
93 feet Y = -5794271
16 meter
Z = -1837621
60 Z = -543330
23
XDOT = 14396
707457 XDOT = 4336
356704
YDOT = 6602
835637 feet/sec YDOT = 2061
325993 meter/sec
ZDOT = 19539
012174 ZDOT = 5976
681192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20164315
93 X = 6146083
49
Y = -9260925
62 feet Y = -2822730
13 meter
Z = -1763782
56 Z = -537600
93
XDOT = 7244
581075 XDOT = 2208
148312
YDOT = 12114
726535 feet/sec YDOT = 3692
568648 meter/sec
ZDOT = 19630
461713 ZDOT = 5983
364730
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 16047
50103925
00016717 00000-0 10270-3 0 9044
2 25544 51
6433 304
8592 0006218 118
7206 241
4572 15
54779802 26053
Satellite: ISS
Catalog Number: 25544
Epoch time: 16047
50103925 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 304
8592 deg
Eccentricity:
0006218
Arg of perigee: 118
7206 deg
Mean anomaly: 241
4572 deg
Mean motion: 15
54779802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 301
Coasting Arc #6 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2016/048/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1389771
33 A = 6780351
15 meter
Y = -4885294
58 meter E =
0013471
Z = -4505441
74 I = 51
31609
XDOT = 5389
431160 Wp = 116
45760
YDOT = -4435
357565 meter/sec RA = 299
37540 deg
ZDOT = 3148
293494 TA = 185
31959
MA = 185
33392
Ha = 222
071 n
mi
Hp = 213
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4559617
22 X = -1313154
33
Y = -16027869
34 feet Y = -4900407
72 meter
Z = -14781632
99 Z = -4512006
49
XDOT = 17681
860761 XDOT = 5423
335073
YDOT = -14551
698048 feet/sec YDOT = -4374
899670 meter/sec
ZDOT = 10329
046895 ZDOT = 3174
556101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9471684
40 X = 2886969
40
Y = -13680486
82 feet Y = -4169812
38 meter
Z = -14809147
64 Z = -4513828
20
XDOT = 21452
643858 XDOT = 6538
765848
YDOT = 3552
507993 feet/sec YDOT = 1082
804436 meter/sec
ZDOT = 10443
721631 ZDOT = 3183
246353
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 16048
46516015
00016717 00000-0 10270-3 0 9059
2 25544 51
6432 300
0467 0004038 131
8477 228
3021 15
54252646 26207
Satellite: ISS
Catalog Number: 25544
Epoch time: 16048
46516015 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 300
0467 deg
Eccentricity:
0004038
Arg of perigee: 131
8477 deg
Mean anomaly: 228
3021 deg
Mean motion: 15
54252646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 280
Coasting Arc #7 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2016/049/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 255028
16 A = 6784224
67 meter
Y = 5896793
25 meter E =
0015767
Z = 3328117
32 I = 51
31391
XDOT = -5388
115992 Wp = 101
57572
YDOT = 2867
524560 meter/sec RA = 294
36471 deg
ZDOT = -4652
198889 TA = 39
43094
MA = 39
31628
Ha = 221
999 n
mi
Hp = 213
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 836706
55 X = 172903
57
Y = 19346434
56 feet Y = 5899186
12 meter
Z = 10919020
07 Z = 3329156
41
XDOT = -17677
545904 XDOT = -5397
182983
YDOT = 9407
888978 feet/sec YDOT = 2807
220158 meter/sec
ZDOT = -15263
119713 ZDOT = -4678
394637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14162365
25 X = -4316688
93
Y = 13203716
09 feet Y = 4024492
66 meter
Z = 10922403
54 Z = 3329148
60
XDOT = -17634
998298 XDOT = -5375
147481
YDOT = -6152
617800 feet/sec YDOT = -1875
317906 meter/sec
ZDOT = -15377
200476 ZDOT = -4686
970705
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 16049
49390278
00016717 00000-0 10270-3 0 9065
2 25544 51
6429 294
9173 0004083 135
6829 224
4651 15
54266131 26368
Satellite: ISS
Catalog Number: 25544
Epoch time: 16049
49390278 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 294
9173 deg
Eccentricity:
0004083
Arg of perigee: 135
6829 deg
Mean anomaly: 224
4651 deg
Mean motion: 15
54266131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 327
Coasting Arc #8 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2016/050/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 747120
70 A = 6787383
40 meter
Y = -6498563
82 meter E =
0007611
Z = -1810443
98 I = 51
31325
XDOT = 5114
751306 Wp = 68
96271
YDOT = -972
496298 meter/sec RA = 289
36301 deg
ZDOT = 5623
342983 TA = 271
05540
MA = 271
14260
Ha = 221
846 n
mi
Hp = 213
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2451183
40 X = 828527
88
Y = -21320747
43 feet Y = -6489753
95 meter
Z = -5939776
83 Z = -1806616
63
XDOT = 16780
680139 XDOT = 5097
930710
YDOT = -3190
604653 feet/sec YDOT = -915
393478 meter/sec
ZDOT = 18449
288003 ZDOT = 5648
147797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17572993
77 X = 5356248
50
Y = -12328166
96 feet Y = -3757625
29 meter
Z = -5921968
35 Z = -1805015
95
XDOT = 12567
814299 XDOT = 3830
669798
YDOT = 9035
108398 feet/sec YDOT = 2753
901040 meter/sec
ZDOT = 18556
980367 ZDOT = 5656
167616
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 16050
45833035
00016717 00000-0 10270-3 0 9077
2 25544 51
6434 290
1079 0003950 140
1702 219
9741 15
54320476 26519
Satellite: ISS
Catalog Number: 25544
Epoch time: 16050
45833035 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 290
1079 deg
Eccentricity:
0003950
Arg of perigee: 140
1702 deg
Mean anomaly: 219
9741 deg
Mean motion: 15
54320476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 290
Coasting Arc #9 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2016/051/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1650321
18 A = 6788836
59 meter
Y = 6576763
77 meter E =
0016118
Z = 41610
80 I = 51
30791
XDOT = -4662
641107 Wp = 136
82337
YDOT = -1123
483383 meter/sec RA = 284
36811 deg
ZDOT = -5987
574037 TA = 42
72615
MA = 42
60094
Ha = 221
801 n
mi
Hp = 213
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5414439
58 X = -1723943
65
Y = 21577308
94 feet Y = 6557897
14 meter
Z = 136518
36 Z = 33414
84
XDOT = -15297
378960 XDOT = -4620
647155
YDOT = -3685
969104 feet/sec YDOT = -1175
389771 meter/sec
ZDOT = -19644
271776 ZDOT = -6010
121347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19530598
28 X = -5952926
36
Y = 10651799
37 feet Y = 3246668
45 meter
Z = 99776
18 Z = 30411
78
XDOT = -6800
401632 XDOT = -2072
762417
YDOT = -12226
527299 feet/sec YDOT = -3726
645521 meter/sec
ZDOT = -19741
790775 ZDOT = -6017
297828
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 16051
48703651
00016717 00000-0 10270-3 0 9082
2 25544 51
6432 284
9781 0004006 145
5685 214
5728 15
54298849 26671
Satellite: ISS
Catalog Number: 25544
Epoch time: 16051
48703651 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 284
9781 deg
Eccentricity:
0004006
Arg of perigee: 145
5685 deg
Mean anomaly: 214
5728 deg
Mean motion: 15
54298849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 337
Coasting Arc #10 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2016/052/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2387559
31 A = 6787426
45 meter
Y = -6117303
08 meter E =
0014861
Z = 1696755
32 I = 51
29633
XDOT = 4077
839799 Wp = 78
81649
YDOT = 3174
224925 meter/sec RA = 279
37190 deg
ZDOT = 5666
486075 TA = 299
88098
MA = 300
02855
Ha = 221
612 n
mi
Hp = 213
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7833199
84 X = 2447545
16
Y = -20069891
98 feet Y = -6090268
24 meter
Z = 5566782
54 Z = 1708499
46
XDOT = 13378
739497 XDOT = 4014
517082
YDOT = 10414
123770 feet/sec YDOT = 3219
472502 meter/sec
ZDOT = 18590
833578 ZDOT = 5686
140619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19899143
92 X = 6065259
07
Y = -8222029
55 feet Y = -2506074
61 meter
Z = 5618803
50 Z = 1712611
31
XDOT = 1025
209987 XDOT = 312
484004
YDOT = 15331
411992 feet/sec YDOT = 4673
014375 meter/sec
ZDOT = 18675
444022 ZDOT = 5692
275338
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 16052
51572228
00016717 00000-0 10270-3 0 9092
2 25544 51
6427 279
8477 0003722 147
8288 212
3092 15
54356478 26839
Satellite: ISS
Catalog Number: 25544
Epoch time: 16052
51572228 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 279
8477 deg
Eccentricity:
0003722
Arg of perigee: 147
8288 deg
Mean anomaly: 212
3092 deg
Mean motion: 15
54356478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 335
Coasting Arc #11 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2016/053/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3035713
18 A = 6783978
12 meter
Y = 5097416
31 meter E =
0007266
Z = -3291199
00 I = 51
28028
XDOT = -3383
505235 Wp = 120
80859
YDOT = -5033
423236 meter/sec RA = 274
36862 deg
ZDOT = -4686
303405 TA = 97
63522
MA = 97
55269
Ha = 221
445 n
mi
Hp = 213
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9959688
92 X = -3076501
28
Y = 16723806
78 feet Y = 5063240
52 meter
Z = -10797896
97 Z = -3306045
02
XDOT = -11100
738961 XDOT = -3304
205267
YDOT = -16513
855762 feet/sec YDOT = -5070
816966 meter/sec
ZDOT = -15375
011170 ZDOT = -4702
546077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18845936
22 X = -5744241
36
Y = 4722081
56 feet Y = 1439290
46 meter
Z = -10863163
86 Z = -3311092
35
XDOT = 4355
911198 XDOT = 1327
681733
YDOT = -18060
219713 feet/sec YDOT = -5504
754969 meter/sec
ZDOT = -15444
507484 ZDOT = -4707
485881
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 16053
48009814
00016717 00000-0 10270-3 0 9107
2 25544 51
6423 275
0381 0003688 155
0076 205
1256 15
54369225 26986
Satellite: ISS
Catalog Number: 25544
Epoch time: 16053
48009814 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 275
0381 deg
Eccentricity:
0003688
Arg of perigee: 155
0076 deg
Mean anomaly: 205
1256 deg
Mean motion: 15
54369225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2698
Checksum: 307
Coasting Arc #12 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2016/054/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3548879
28 A = 6779952
56 meter
Y = -3647057
46 meter E =
0011849
Z = 4475262
07 I = 51
26525
XDOT = 2623
504682 Wp = 123
95460
YDOT = 6469
666137 meter/sec RA = 269
35326 deg
ZDOT = 3179
355004 TA = 293
88906
MA = 294
01317
Ha = 221
341 n
mi
Hp = 213
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11643304
71 X = 3567659
37
Y = -11965411
61 feet Y = -3607265
96 meter
Z = 14682618
34 Z = 4492547
35
XDOT = 8607
298824 XDOT = 2535
520672
YDOT = 21225
938769 feet/sec YDOT = 6498
512362 meter/sec
ZDOT = 10430
954738 ZDOT = 3191
884550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16621653
99 X = 5066280
14
Y = -483108
76 feet Y = -147251
55 meter
Z = 14758188
42 Z = 4498295
83
XDOT = -8765
713351 XDOT = -2671
789430
YDOT = 19937
229258 feet/sec YDOT = 6076
867478 meter/sec
ZDOT = 10484
114716 ZDOT = 3195
558165
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 16054
50874862
00016717 00000-0 10270-3 0 9115
2 25544 51
6420 269
9073 0003612 155
1700 204
9627 15
54398806 27140
Satellite: ISS
Catalog Number: 25544
Epoch time: 16054
50874862 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 269
9073 deg
Eccentricity:
0003612
Arg of perigee: 155
1700 deg
Mean anomaly: 204
9627 deg
Mean motion: 15
54398806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 309
Coasting Arc #13 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/055/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3987018
93 A = 6776933
46 meter
Y = 1847310
92 meter E =
0014954
Z = -5172058
09 I = 51
25609
XDOT = -1756
428752 Wp = 93
53029
YDOT = -7344
507254 meter/sec RA = 264
32654 deg
ZDOT = -1273
359027 TA = 164
18405
MA = 164
13730
Ha = 221
167 n
mi
Hp = 213
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13080770
76 X = -3982256
50
Y = 6060731
37 feet Y = 1802751
35 meter
Z = -16968694
52 Z = -5191414
37
XDOT = -5762
561523 XDOT = -1667
984790
YDOT = -24096
152409 feet/sec YDOT = -7363
654460 meter/sec
ZDOT = -4177
687095 ZDOT = -1281
675353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13590984
55 X = -4142532
09
Y = -4500971
22 feet Y = -1371896
03 meter
Z = -17052918
21 Z = -5197729
47
XDOT = 12046
457953 XDOT = 3671
760384
YDOT = -20466
037696 feet/sec YDOT = -6238
048290 meter/sec
ZDOT = -4212
446922 ZDOT = -1283
953822
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 16055
47308891
00016717 00000-0 10270-3 0 9127
2 25544 51
6410 265
0964 0003481 161
5351 198
5929 15
54460734 27291
Satellite: ISS
Catalog Number: 25544
Epoch time: 16055
47308891 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 265
0964 deg
Eccentricity:
0003481
Arg of perigee: 161
5351 deg
Mean anomaly: 198
5929 deg
Mean motion: 15
54460734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 322
Coasting Arc #14 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2016/056/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4293264
17 A = 6776515
28 meter
Y = 82019
07 meter E =
0004099
Z = 5238980
47 I = 51
25931
XDOT = 800
834480 Wp = 117
32474
YDOT = 7590
914152 meter/sec RA = 259
29604 deg
ZDOT = -776
493509 TA = 340
12260
MA = 340
13857
Ha = 220
945 n
mi
Hp = 213
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14085512
38 X = 4266579
58
Y = 269091
44 feet Y = 129880
72 meter
Z = 17188256
14 Z = 5259770
95
XDOT = 2627
409711 XDOT = 719
663296
YDOT = 24904
573989 feet/sec YDOT = 7599
415652 meter/sec
ZDOT = -2547
550884 ZDOT = -772
801515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10141318
44 X = 3091073
86
Y = 9618844
42 feet Y = 2931823
78 meter
Z = 17278359
60 Z = 5266444
01
XDOT = -14130
890927 XDOT = -4307
095555
YDOT = 19440
135160 feet/sec YDOT = 5925
353197 meter/sec
ZDOT = -2532
862468 ZDOT = -772
016480
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 16056
50170151
00016717 00000-0 10270-3 0 9139
2 25544 51
6413 259
9658 0003493 166
0398 194
0852 15
54480593 27459
Satellite: ISS
Catalog Number: 25544
Epoch time: 16056
50170151 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 259
9658 deg
Eccentricity:
0003493
Arg of perigee: 166
0398 deg
Mean anomaly: 194
0852 deg
Mean motion: 15
54480593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 322
Coasting Arc #15 (Orbit 2759)
---------------------------------------
Vector Time (GMT): 2016/057/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4475798
79 A = 6778747
07 meter
Y = -1981902
18 meter E =
0012938
Z = -4702040
78 I = 51
27283
XDOT = 276
111640 Wp = 122
58371
YDOT = -7143
451355 meter/sec RA = 254
26688 deg
ZDOT = 2746
826891 TA = 174
79439
MA = 174
78092
Ha = 220
950 n
mi
Hp = 213
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14684379
23 X = -4430463
77
Y = -6502303
75 feet Y = -2031700
69 meter
Z = -15426642
98 Z = -4723672
47
XDOT = 905
878085 XDOT = 342
628204
YDOT = -23436
520194 feet/sec YDOT = -7139
991404 meter/sec
ZDOT = 9011
899249 ZDOT = 2748
330683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6641837
85 X = -2024432
18
Y = -14522592
68 feet Y = -4426486
25 meter
Z = -15520069
36 Z = -4730517
14
XDOT = 15072
497052 XDOT = 4594
097102
YDOT = -16537
013529 feet/sec YDOT = -5040
481724 meter/sec
ZDOT = 9019
641823 ZDOT = 2749
186828
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 16057
46600801
00016717 00000-0 10270-3 0 9146
2 25544 51
6402 255
1541 0003418 170
4893 189
6325 15
54511672 27607
Satellite: ISS
Catalog Number: 25544
Epoch time: 16057
46600801 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 255
1541 deg
Eccentricity:
0003418
Arg of perigee: 170
4893 deg
Mean anomaly: 189
6325 deg
Mean motion: 15
54511672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2760
Checksum: 297
Coasting Arc #16 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2016/058/10:54:53
245
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4447488
38 A = 6782525
48 meter
Y = 3653616
81 meter E =
0012415
Z = 3575024
75 I = 51
29623
XDOT = -1464
284472 Wp = 101
77440
YDOT = 6107
365499 meter/sec RA = 249
24956 deg
ZDOT = -4409
470498 TA = 35
68551
MA = 35
60259
Ha = 220
600 n
mi
Hp = 213
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14591497
31 X = 4388936
40
Y = 11986931
80 feet Y = 3703024
66 meter
Z = 11729083
84 Z = 3596486
67
XDOT = -4804
082914 XDOT = -1511
050586
YDOT = 20037
288382 feet/sec YDOT = 6090
728848 meter/sec
ZDOT = -14466
766726 ZDOT = -4416
697935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3283200
20 X = 1000719
42
Y = 18537598
11 feet Y = 5650259
90 meter
Z = 11821496
87 Z = 3603192
25
XDOT = -15222
580592 XDOT = -4639
842564
YDOT = 11964
072156 feet/sec YDOT = 3646
649193 meter/sec
ZDOT = -14499
132974 ZDOT = -4419
335731
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 16058
49458144
00016717 00000-0 10270-3 0 9152
2 25544 51
6407 250
0232 0003240 176
5699 183
5476 15
54572147 27768
Satellite: ISS
Catalog Number: 25544
Epoch time: 16058
49458144 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 250
0232 deg
Eccentricity:
0003240
Arg of perigee: 176
5699 deg
Mean anomaly: 183
5476 deg
Mean motion: 15
54572147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2776
Checksum: 324
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