[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 4th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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
011/02:13:29
648 -0
2 4
9 4
9
N/A 4
4 -0
6 221
9
000/00:16:59
296 -2
2 -0
4 214
0
Coasting Arc #1 (Orbit 1936)
---------------------------------------
Vector Time (GMT): 2016/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6472412
62 A = 6785108
17 meter
Y = 1286038
34 meter E =
0019262
Z = 1525753
20 I = 51
78631
XDOT = 366
016970 Wp = 39
17183
YDOT = -5043
082855 meter/sec RA = 158
27363 deg
ZDOT = 5778
343526 TA = 337
48913
MA = 337
57352
Ha = 221
007 n
mi
Hp = 212
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21234949
54 X = -6493723
86
Y = 4219285
89 feet Y = 1213540
31 meter
Z = 5005751
96 Z = 1494259
99
XDOT = 1200
843077 XDOT = 394
313934
YDOT = -16545
547426 feet/sec YDOT = -5038
831864 meter/sec
ZDOT = 18957
819966 ZDOT = 5780
190046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8790147
21 X = -2679236
87
Y = -19819382
59 feet Y = -6040947
81 meter
Z = 4869126
59 Z = 1484109
79
XDOT = 14931
255997 XDOT = 4551
046828
YDOT = -1941
766549 feet/sec YDOT = -591
850444 meter/sec
ZDOT = 18966
693481 ZDOT = 5781
048173
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 16004
56136692
00016717 00000-0 10270-3 0 9006
2 25544 51
6392 159
0703 0008424 359
0998 1
0138 15
55262162 19372
Satellite: ISS
Catalog Number: 25544
Epoch time: 16004
56136692 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 159
0703 deg
Eccentricity:
0008424
Arg of perigee: 359
0998 deg
Mean anomaly: 1
0138 deg
Mean motion: 15
55262162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1937
Checksum: 302
Coasting Arc #2 (Orbit 1951)
---------------------------------------
Vector Time (GMT): 2016/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5884547
19 A = 6781272
03 meter
Y = 20315
42 meter E =
0009792
Z = -3383303
49 I = 51
80311
XDOT = -2695
368399 Wp = 32
23401
YDOT = 5454
015482 meter/sec RA = 153
30097 deg
ZDOT = -4653
409980 TA = 187
12880
MA = 187
14274
Ha = 221
118 n
mi
Hp = 212
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19306257
19 X = 5900317
36
Y = 66651
64 feet Y = 86208
70 meter
Z = -11100077
05 Z = -3354679
40
XDOT = -8843
072174 XDOT = -2733
551864
YDOT = 17893
751582 feet/sec YDOT = 5423
660877 meter/sec
ZDOT = -15267
093110 ZDOT = -4666
595871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4519083
21 X = 1377416
56
Y = 18842798
58 feet Y = 5743285
01 meter
Z = -10976089
83 Z = -3345512
18
XDOT = -18078
919080 XDOT = -5510
454536
YDOT = -4594
768659 feet/sec YDOT = -1400
485487 meter/sec
ZDOT = -15325
163576 ZDOT = -4671
109858
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 16005
52519987
00016717 00000-0 10270-3 0 9016
2 25544 51
6394 154
2570 0008592 2
9628 357
1575 15
55269058 19521
Satellite: ISS
Catalog Number: 25544
Epoch time: 16005
52519987 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 154
2570 deg
Eccentricity:
0008592
Arg of perigee: 2
9628 deg
Mean anomaly: 357
1575 deg
Mean motion: 15
55269058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1952
Checksum: 331
Coasting Arc #3 (Orbit 1967)
---------------------------------------
Vector Time (GMT): 2016/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4642751
06 A = 6776636
86 meter
Y = -1478497
73 meter E =
0009475
Z = 4700515
16 I = 51
81651
XDOT = 4601
089419 Wp = 59
11795
YDOT = -5454
940052 meter/sec RA = 148
31460 deg
ZDOT = 2829
286755 TA = 2
92316
MA = 2
91763
Ha = 221
255 n
mi
Hp = 211
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15232122
91 X = -4648706
21
Y = -4850714
34 feet Y = -1530449
69 meter
Z = 15421637
65 Z = 4677947
20
XDOT = 15095
437726 XDOT = 4648
002449
YDOT = -17896
784949 feet/sec YDOT = -5403
225535 meter/sec
ZDOT = 9282
436861 ZDOT = 2851
751288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 809731
03 X = 246806
02
Y = -16058933
91 feet Y = -4894763
05 meter
Z = 15324127
49 Z = 4670794
06
XDOT = 19948
587819 XDOT = 6080
329567
YDOT = 9955
662047 feet/sec YDOT = 3034
485792 meter/sec
ZDOT = 9380
719048 ZDOT = 2859
243166
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 16006
55327889
00016717 00000-0 10270-3 0 9029
2 25544 51
6398 149
1221 0008518 5
9507 354
1746 15
55299685 19681
Satellite: ISS
Catalog Number: 25544
Epoch time: 16006
55327889 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 149
1221 deg
Eccentricity:
0008518
Arg of perigee: 5
9507 deg
Mean anomaly: 354
1746 deg
Mean motion: 15
55299685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1968
Checksum: 344
Coasting Arc #4 (Orbit 1982)
---------------------------------------
Vector Time (GMT): 2016/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3002555
96 A = 6774066
54 meter
Y = 2968959
96 meter E =
0018901
Z = -5311779
76 I = 51
83553
XDOT = -5852
886781 Wp = 59
48015
YDOT = 4906
467912 meter/sec RA = 143
31950 deg
ZDOT = -558
135593 TA = 205
15474
MA = 205
24693
Ha = 221
319 n
mi
Hp = 211
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9850905
38 X = 2994935
48
Y = 9740682
29 feet Y = 3002494
37 meter
Z = -17427098
94 Z = -5297212
35
XDOT = -19202
384453 XDOT = -5904
605933
YDOT = 16097
335668 feet/sec YDOT = 4840
727932 meter/sec
ZDOT = -1831
153520 ZDOT = -586
692638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6690133
14 X = -2039152
58
Y = 12220517
21 feet Y = 3724813
64 meter
Z = -17364506
43 Z = -5292701
56
XDOT = -19786
464677 XDOT = -6030
914434
YDOT = -13647
947351 feet/sec YDOT = -4159
894353 meter/sec
ZDOT = -1955
756495 ZDOT = -596
114580
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 16007
51709693
00016717 00000-0 10270-3 0 9034
2 25544 51
6406 144
3101 0008659 10
5043 349
6290 15
55301383 19837
Satellite: ISS
Catalog Number: 25544
Epoch time: 16007
51709693 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 144
3101 deg
Eccentricity:
0008659
Arg of perigee: 10
5043 deg
Mean anomaly: 349
6290 deg
Mean motion: 15
55301383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1983
Checksum: 295
Coasting Arc #5 (Orbit 1998)
---------------------------------------
Vector Time (GMT): 2016/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1121003
28 A = 6775074
48 meter
Y = -4339735
36 meter E =
0013236
Z = 5077895
60 I = 51
86443
XDOT = 6413
284791 Wp = 30
20623
YDOT = -3799
076767 meter/sec RA = 138
32052 deg
ZDOT = -1817
793897 TA = 77
39846
MA = 77
25048
Ha = 221
481 n
mi
Hp = 211
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3677832
27 X = -1097058
09
Y = -14237976
89 feet Y = -4352137
72 meter
Z = 16659762
46 Z = 5072507
85
XDOT = 21040
960601 XDOT = 6464
120373
YDOT = -12464
162621 feet/sec YDOT = -3727
074778 meter/sec
ZDOT = -5963
890738 ZDOT = -1786
516762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12556826
97 X = 3827320
86
Y = -7702218
99 feet Y = -2347636
35 meter
Z = 16637188
48 Z = 5071015
05
XDOT = 17416
382542 XDOT = 5308
513399
YDOT = 15711
841487 feet/sec YDOT = 4788
969285 meter/sec
ZDOT = -5827
674902 ZDOT = -1776
275310
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 16008
54516147
00016717 00000-0 10270-3 0 9049
2 25544 51
6412 139
1747 0008701 14
6352 345
5052 15
55271433 19998
Satellite: ISS
Catalog Number: 25544
Epoch time: 16008
54516147 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 139
1747 deg
Eccentricity:
0008701
Arg of perigee: 14
6352 deg
Mean anomaly: 345
5052 deg
Mean motion: 15
55271433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1999
Checksum: 301
Coasting Arc #6 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2016/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -671036
59 A = 6778845
36 meter
Y = 5373933
07 meter E =
0011238
Z = -4081050
88 I = 51
90150
XDOT = -6238
772374 Wp = 58
03484
YDOT = 2166
099186 meter/sec RA = 133
33409 deg
ZDOT = 3891
771774 TA = 252
08050
MA = 252
20307
Ha = 221
499 n
mi
Hp = 211
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2201563
63 X = -711255
55
Y = 17631014
02 feet Y = 5366204
56 meter
Z = -13389274
53 Z = -4084407
82
XDOT = -20468
413299 XDOT = -6281
434937
YDOT = 7106
624625 feet/sec YDOT = 2096
094247 meter/sec
ZDOT = 12768
280097 ZDOT = 3861
362194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17442886
91 X = -5316591
93
Y = 3321083
27 feet Y = 1012266
18 meter
Z = -13404786
92 Z = -4085779
05
XDOT = -12753
599427 XDOT = -3887
297105
YDOT = -16161
573688 feet/sec YDOT = -4926
047660 meter/sec
ZDOT = 12636
094580 ZDOT = 3851
481628
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 16009
50896185
00016717 00000-0 10270-3 0 9050
2 25544 51
6420 134
3623 0008746 16
9069 343
2374 15
55297103 20149
Satellite: ISS
Catalog Number: 25544
Epoch time: 16009
50896185 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 134
3623 deg
Eccentricity:
0008746
Arg of perigee: 16
9069 deg
Mean anomaly: 343
2374 deg
Mean motion: 15
55297103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2014
Checksum: 303
Coasting Arc #7 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2016/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2284030
68 A = 6783414
55 meter
Y = -5915739
73 meter E =
0016988
Z = 2401835
56 I = 51
93867
XDOT = 5455
900783 Wp = 75
40502
YDOT = -95
554199 meter/sec RA = 128
36305 deg
ZDOT = -5387
708496 TA = 77
85992
MA = 77
66966
Ha = 221
558 n
mi
Hp = 211
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7493538
97 X = 2338345
24
Y = -19408594
92 feet Y = -5889894
67 meter
Z = 7880037
93 Z = 2413062
18
XDOT = 17899
936952 XDOT = 5482
734645
YDOT = -313
498028 feet/sec YDOT = -34
392295 meter/sec
ZDOT = -17676
208975 ZDOT = -5361
140250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20768239
18 X = 6330159
30
Y = 860657
59 feet Y = 262328
43 meter
Z = 7929766
13 Z = 2416992
72
XDOT = 6109
404994 XDOT = 1862
146642
YDOT = 15456
200301 feet/sec YDOT = 4711
049852 meter/sec
ZDOT = -17561
028118 ZDOT = -5352
601370
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 16010
53700898
00016717 00000-0 10270-3 0 9061
2 25544 51
6425 129
2277 0008723 21
4184 338
7333 15
55312169 20308
Satellite: ISS
Catalog Number: 25544
Epoch time: 16010
53700898 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 129
2277 deg
Eccentricity:
0008723
Arg of perigee: 21
4184 deg
Mean anomaly: 338
7333 deg
Mean motion: 15
55312169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2030
Checksum: 293
Coasting Arc #8 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2016/011/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3619707
47 A = 6776841
94 meter
Y = 2122726
68 meter E =
0016546
Z = -5334738
03 I = 51
91906
XDOT = -4224
647598 Wp = 66
04122
YDOT = 6378
455649 meter/sec RA = 125
41182 deg
ZDOT = -322
716477 TA = 200
85585
MA = 200
92343
Ha = 221
851 n
mi
Hp = 214
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11875680
69 X = 3621615
09
Y = 6964326
38 feet Y = 2163215
63 meter
Z = -17502421
35 Z = -5317149
88
XDOT = -13860
392382 XDOT = -4294
091480
YDOT = 20926
691763 feet/sec YDOT = 6330
824582 meter/sec
ZDOT = -1058
781093 ZDOT = -343
406757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5759209
85 X = -1755407
16
Y = -12610109
70 feet Y = -3843561
44 meter
Z = -17426560
82 Z = -5311615
74
XDOT = 22479
937234 XDOT = 6851
884869
YDOT = -8651
998525 feet/sec YDOT = -2637
129150 meter/sec
ZDOT = -1149
623031 ZDOT = -350
405100
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 16011
11528977
00016717 00000-0 10270-3 0 9073
2 25544 51
6429 126
3428 0006090 2
7923 357
3262 15
54319857 20393
Satellite: ISS
Catalog Number: 25544
Epoch time: 16011
11528977 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 126
3428 deg
Eccentricity:
0006090
Arg of perigee: 2
7923 deg
Mean anomaly: 357
3262 deg
Mean motion: 15
54319857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 310
Coasting Arc #9 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2016/012/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2497413
90 A = 6777596
19 meter
Y = -3666662
32 meter E =
0010195
Z = 5122090
18 I = 51
93978
XDOT = 4868
066276 Wp = 27
59830
YDOT = -5683
228225 meter/sec RA = 120
42970 deg
ZDOT = -1684
655396 TA = 78
65616
MA = 78
54163
Ha = 221
910 n
mi
Hp = 213
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8193615
15 X = -2481107
28
Y = -12029732
03 feet Y = -3694499
09 meter
Z = 16804757
82 Z = 5109998
01
XDOT = 15971
346050 XDOT = 4939
438932
YDOT = -18645
761893 feet/sec YDOT = -5628
391150 meter/sec
ZDOT = -5527
084634 ZDOT = -1660
834801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 74678
37 X = 22761
97
Y = 14614416
28 feet Y = 4454474
08 meter
Z = 16752997
56 Z = 5106313
66
XDOT = -22666
955397 XDOT = -6908
888005
YDOT = 6370
405289 feet/sec YDOT = 1941
699532 meter/sec
ZDOT = -5422
783934 ZDOT = -1652
864543
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 16012
14400312
00016717 00000-0 10270-3 0 9080
2 25544 51
6429 121
2130 0006171 5
1211 355
0004 15
54355599 20554
Satellite: ISS
Catalog Number: 25544
Epoch time: 16012
14400312 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 121
2130 deg
Eccentricity:
0006171
Arg of perigee: 5
1211 deg
Mean anomaly: 355
0004 deg
Mean motion: 15
54355599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 248
Coasting Arc #10 (Orbit 2069)
---------------------------------------
Vector Time (GMT): 2016/013/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1397434
78 A = 6780708
42 meter
Y = 5004498
64 meter E =
0009642
Z = -4362640
22 I = 51
96556
XDOT = -5151
796202 Wp = 71
57740
YDOT = 4472
272334 meter/sec RA = 115
45461 deg
ZDOT = 3489
309703 TA = 233
69738
MA = 233
78646
Ha = 222
030 n
mi
Hp = 213
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4584759
77 X = 1362560
88
Y = 16418958
80 feet Y = 5019930
79 meter
Z = -14313124
09 Z = -4355936
53
XDOT = -16902
218509 XDOT = -5218
372663
YDOT = 14672
809496 feet/sec YDOT = 4414
289211 meter/sec
ZDOT = 11447
866479 ZDOT = 3464
122350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5114427
39 X = 1558877
47
Y = -16286499
32 feet Y = -4964124
99 meter
Z = -14284968
45 Z = -4354058
38
XDOT = 21058
433683 XDOT = 6418
610587
YDOT = -3304
815162 feet/sec YDOT = -1007
307661 meter/sec
ZDOT = 11337
847247 ZDOT = 3455
775841
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 16013
10841653
00016717 00000-0 10270-3 0 9095
2 25544 51
6431 116
4038 0006215 8
8147 351
3114 15
54329870 20708
Satellite: ISS
Catalog Number: 25544
Epoch time: 16013
10841653 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 116
4038 deg
Eccentricity:
0006215
Arg of perigee: 8
8147 deg
Mean anomaly: 351
3114 deg
Mean motion: 15
54329870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2070
Checksum: 277
Coasting Arc #11 (Orbit 2085)
---------------------------------------
Vector Time (GMT): 2016/014/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -314786
09 A = 6784688
19 meter
Y = -6033766
92 meter E =
0015212
Z = 3079915
52 I = 51
99165
XDOT = 5161
179938 Wp = 71
60953
YDOT = -2799
464155 meter/sec RA = 110
49065 deg
ZDOT = -4932
261909 TA = 73
19327
MA = 73
02646
Ha = 222
112 n
mi
Hp = 213
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1032762
76 X = -262252
33
Y = -19795823
23 feet Y = -6036993
35 meter
Z = 10104709
72 Z = 3078513
95
XDOT = 16933
005046 XDOT = 5216
059127
YDOT = -9184
593685 feet/sec YDOT = -2741
441547 meter/sec
ZDOT = -16181
961644 ZDOT = -4907
057252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9664065
62 X = -2945607
20
Y = 17310331
01 feet Y = 5276188
89 meter
Z = 10099735
19 Z = 3078399
29
XDOT = -18045
466447 XDOT = -5500
258173
YDOT = -650
085884 feet/sec YDOT = -198
146177 meter/sec
ZDOT = -16072
161897 ZDOT = -4898
794946
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 16014
13711561
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 111
2737 0006296 13
5092 346
6228 15
54343821 20867
Satellite: ISS
Catalog Number: 25544
Epoch time: 16014
13711561 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 111
2737 deg
Eccentricity:
0006296
Arg of perigee: 13
5092 deg
Mean anomaly: 346
6228 deg
Mean motion: 15
54343821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2086
Checksum: 286
Coasting Arc #12 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2016/015/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -626022
84 A = 6787724
17 meter
Y = 6586074
55 meter E =
0014380
Z = -1486680
12 I = 52
01208
XDOT = -4940
282074 Wp = 28
25852
YDOT = 833
719377 meter/sec RA = 105
53712 deg
ZDOT = 5808
886800 TA = 315
58946
MA = 315
70469
Ha = 222
164 n
mi
Hp = 213
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2053880
71 X = -692401
84
Y = 21607856
14 feet Y = 6578702
80 meter
Z = -4877559
44 Z = -1489882
39
XDOT = -16208
274520 XDOT = -4977
454535
YDOT = 2735
299792 feet/sec YDOT = 778
266048 meter/sec
ZDOT = 19058
027560 ZDOT = 5784
798107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12972436
22 X = 3953998
56
Y = -17397880
97 feet Y = -5302874
12 meter
Z = -4892657
26 Z = -1491281
93
XDOT = 14100
111574 XDOT = 4297
714008
YDOT = 5215
752814 feet/sec YDOT = 1589
761458 meter/sec
ZDOT = 18953
419771 ZDOT = 5777
002346
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 16015
10151252
00016717 00000-0 10270-3 0 9119
2 25544 51
6427 106
4637 0006332 15
6111 344
5236 15
54355393 21017
Satellite: ISS
Catalog Number: 25544
Epoch time: 16015
10151252 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 106
4637 deg
Eccentricity:
0006332
Arg of perigee: 15
6111 deg
Mean anomaly: 344
5236 deg
Mean motion: 15
54355393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2101
Checksum: 260
Coasting Arc #13 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2016/016/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1492238
35 A = 6788708
34 meter
Y = -6613446
68 meter E =
0010223
Z = -321891
83 I = 52
02247
XDOT = 4544
332179 Wp = 104
71217
YDOT = 1311
012269 meter/sec RA = 100
59099 deg
ZDOT = -6030
679997 TA = 78
73712
MA = 78
62225
Ha = 222
234 n
mi
Hp = 213
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4895795
11 X = 1567644
23
Y = -21697659
70 feet Y = -6596337
86 meter
Z = -1056075
55 Z = -314459
79
XDOT = 14909
226310 XDOT = 4558
628613
YDOT = 4301
221356 feet/sec YDOT = 1361
909917 meter/sec
ZDOT = -19785
695528 ZDOT = -6008
570204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15201511
33 X = -4633420
65
Y = 16240099
89 feet Y = 4949982
45 meter
Z = -1022619
39 Z = -311694
39
XDOT = -9613
420699 XDOT = -2930
170629
YDOT = -10203
920816 feet/sec YDOT = -3110
155065 meter/sec
ZDOT = -19690
061684 ZDOT = -6001
530801
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 16016
13019633
00016717 00000-0 10270-3 0 9120
2 25544 51
6424 101
3335 0006174 19
8039 340
3353 15
54326077 21170
Satellite: ISS
Catalog Number: 25544
Epoch time: 16016
13019633 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 101
3335 deg
Eccentricity:
0006174
Arg of perigee: 19
8039 deg
Mean anomaly: 340
3353 deg
Mean motion: 15
54326077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 274
Coasting Arc #14 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2016/017/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2211736
84 A = 6786822
17 meter
Y = 6066094
41 meter E =
0018859
Z = 2055337
11 I = 52
02119
XDOT = -4045
727648 Wp = 54
66000
YDOT = -3375
042191 meter/sec RA = 95
64263 deg
ZDOT = 5582
200324 TA = 327
97239
MA = 328
08686
Ha = 222
293 n
mi
Hp = 213
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7256354
47 X = -2289388
92
Y = 19901884
54 feet Y = 6040927
11 meter
Z = 6743231
97 Z = 2044404
52
XDOT = -13273
384673 XDOT = -4034
802210
YDOT = -11072
973066 feet/sec YDOT = -3420
223143 meter/sec
ZDOT = 18314
305524 ZDOT = 5562
573795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16127357
93 X = 4915618
70
Y = -13758648
11 feet Y = -4193635
94 meter
Z = 6694684
04 Z = 2040539
70
XDOT = 5230
491803 XDOT = 1594
253901
YDOT = 15041
883305 feet/sec YDOT = 4584
766031 meter/sec
ZDOT = 18229
826592 ZDOT = 5556
451145
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 16017
15886987
00016717 00000-0 10270-3 0 9138
2 25544 51
6419 96
2023 0006360 22
1595 337
9832 15
54385220 21338
Satellite: ISS
Catalog Number: 25544
Epoch time: 16017
15886987 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 96
2023 deg
Eccentricity:
0006360
Arg of perigee: 22
1595 deg
Mean anomaly: 337
9832 deg
Mean motion: 15
54385220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 310
Coasting Arc #15 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2016/018/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2868155
49 A = 6783197
29 meter
Y = -4995044
22 meter E =
0010176
Z = -3595474
86 I = 52
01060
XDOT = 3429
747047 Wp = 51
49581
YDOT = 5185
841052 meter/sec RA = 90
68741 deg
ZDOT = -4470
898115 TA = 170
71643
MA = 170
69761
Ha = 222
320 n
mi
Hp = 213
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9409958
94 X = 2941263
33
Y = -16387940
36 feet Y = -4962561
76 meter
Z = -11796177
37 Z = -3581364
67
XDOT = 11252
450941 XDOT = 3393
220403
YDOT = 17013
914214 feet/sec YDOT = 5223
990619 meter/sec
ZDOT = -14668
300901 ZDOT = -4454
325930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16139739
92 X = -4919392
73
Y = 9903680
36 feet Y = 3018641
77 meter
Z = -11734037
16 Z = -3576534
53
XDOT = -1165
214473 XDOT = -355
157371
YDOT = -19184
878118 feet/sec YDOT = -5847
550850 meter/sec
ZDOT = -14597
415103 ZDOT = -4449
292123
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 16018
12324597
00016717 00000-0 10270-3 0 9141
2 25544 51
6413 91
3925 0006340 25
5052 334
6413 15
54375008 21480
Satellite: ISS
Catalog Number: 25544
Epoch time: 16018
12324597 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 91
3925 deg
Eccentricity:
0006340
Arg of perigee: 25
5052 deg
Mean anomaly: 334
6413 deg
Mean motion: 15
54375008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 285
Coasting Arc #16 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2016/019/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3418777
06 A = 6779355
25 meter
Y = 3482423
71 meter E =
0010674
Z = 4695798
76 I = 51
99727
XDOT = -2741
850201 Wp = 78
57444
YDOT = -6568
932996 meter/sec RA = 85
72032 deg
ZDOT = 2871
903754 TA = 343
05966
MA = 343
09527
Ha = 222
607 n
mi
Hp = 212
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11216460
17 X = -3480274
34
Y = 11425274
64 feet Y = 3443848
66 meter
Z = 15406163
92 Z = 4679042
04
XDOT = -8995
571526 XDOT = -2682
141394
YDOT = -21551
617442 feet/sec YDOT = -6599
260435 meter/sec
ZDOT = 9422
256410 ZDOT = 2858
729379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15305925
66 X = 4665246
14
Y = -4932440
35 feet Y = -1503407
82 meter
Z = 15332822
24 Z = 4673444
22
XDOT = -2245
313346 XDOT = -684
371508
YDOT = 22183
804467 feet/sec YDOT = 6761
623602 meter/sec
ZDOT = 9366
380005 ZDOT = 2854
872626
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 16019
15190724
00016717 00000-0 10270-3 0 9159
2 25544 51
6414 86
2614 0006517 29
9008 330
2516 15
54363774 21645
Satellite: ISS
Catalog Number: 25544
Epoch time: 16019
15190724 = yrday
fracday
Element set: 915
Inclination: 51
6414 deg
RA of node: 86
2614 deg
Eccentricity:
0006517
Arg of perigee: 29
9008 deg
Mean anomaly: 330
2516 deg
Mean motion: 15
54363774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 298
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