[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 13th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10 7639 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 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
077/03:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
2
078/21:26:42
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 215
0
079/03:12:07
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
0
080/10:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 214
9
084/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 214
6
Coasting Arc #1 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2016/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -43641
53 A = 6777628
37 meter
Y = -4218832
24 meter E =
0001003
Z = 5303778
08 I = 51
59108
XDOT = 7657
273706 Wp = 138
60514
YDOT = 303
876718 meter/sec RA = 184
07465 deg
ZDOT = 303
953274 TA = 308
49125
MA = 308
50024
Ha = 220
459 n
mi
Hp = 215
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -143180
87 X = -22225
67
Y = -13841313
11 feet Y = -4219199
72 meter
Z = 17400846
71 Z = 5303618
73
XDOT = 25122
289062 XDOT = 7651
830106
YDOT = 996
970861 feet/sec YDOT = 389
475051 meter/sec
ZDOT = 997
222028 ZDOT = 341
137038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2454427
19 X = 748109
41
Y = -13622766
18 feet Y = -4152219
13 meter
Z = 17400802
98 Z = 5303764
75
XDOT = 23442
918073 XDOT = 7145
401429
YDOT = 5706
810647 feet/sec YDOT = 1739
435885 meter/sec
ZDOT = 1158
550112 ZDOT = 353
126074
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 16071
54884717
00016717 00000-0 10270-3 0 9006
2 25544 51
6432 184
9669 0001818 268
9830 91
1114 15
54045661 29791
Satellite: ISS
Catalog Number: 25544
Epoch time: 16071
54884717 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 184
9669 deg
Eccentricity:
0001818
Arg of perigee: 268
9830 deg
Mean anomaly: 91
1114 deg
Mean motion: 15
54045661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 331
Coasting Arc #2 (Orbit 2993)
---------------------------------------
Vector Time (GMT): 2016/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1723577
19 A = 6778329
88 meter
Y = 4092258
87 meter E =
0011968
Z = -5132097
80 I = 51
62558
XDOT = -7407
431861 Wp = 103
32404
YDOT = -1134
548371 meter/sec RA = 179
07567 deg
ZDOT = 1583
475128 TA = 181
96380
MA = 181
96851
Ha = 220
477 n
mi
Hp = 215
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5654780
81 X = -1744280
22
Y = 13426046
16 feet Y = 4072868
24 meter
Z = -16837591
21 Z = -5140521
34
XDOT = -24302
597970 XDOT = -7401
886364
YDOT = -3722
271559 feet/sec YDOT = -1217
351978 meter/sec
ZDOT = 5195
128372 ZDOT = 1547
505308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7853879
73 X = -2393862
54
Y = 12218757
19 feet Y = 3724277
19 meter
Z = -16874782
53 Z = -5143433
71
XDOT = -22389
160060 XDOT = -6824
215986
YDOT = -7433
624864 feet/sec YDOT = -2265
768859 meter/sec
ZDOT = 5039
181153 ZDOT = 1535
942415
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 16072
51344366
00016717 00000-0 10270-3 0 9016
2 25544 51
6431 180
1610 0001705 273
1618 86
9340 15
54061832 29949
Satellite: ISS
Catalog Number: 25544
Epoch time: 16072
51344366 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 180
1610 deg
Eccentricity:
0001705
Arg of perigee: 273
1618 deg
Mean anomaly: 86
9340 deg
Mean motion: 15
54061832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2994
Checksum: 289
Coasting Arc #3 (Orbit 3009)
---------------------------------------
Vector Time (GMT): 2016/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3376017
91 A = 6781136
98 meter
Y = -3868158
69 meter E =
0007808
Z = 4425842
45 I = 51
66718
XDOT = 6624
489186 Wp = 63
33543
YDOT = 1961
224296 meter/sec RA = 174
08169 deg
ZDOT = -3331
074791 TA = 60
32242
MA = 60
24471
Ha = 220
436 n
mi
Hp = 215
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11076174
25 X = 3397522
87
Y = -12690809
34 feet Y = -3830285
06 meter
Z = 14520480
46 Z = 4442294
97
XDOT = 21733
888405 XDOT = 6618
246870
YDOT = 6434
462912 feet/sec YDOT = 2035
268450 meter/sec
ZDOT = -10928
723069 ZDOT = -3298
910074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12888530
63 X = 3928424
14
Y = -10748369
64 feet Y = -3276103
07 meter
Z = 14592496
66 Z = 4447792
98
XDOT = 19693
997315 XDOT = 6002
730382
YDOT = 8931
853592 feet/sec YDOT = 2722
428975 meter/sec
ZDOT = -10789
403910 ZDOT = -3288
610312
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 16073
54232770
00016717 00000-0 10270-3 0 9026
2 25544 51
6433 175
0324 0001665 280
6957 79
4008 15
54058758 30101
Satellite: ISS
Catalog Number: 25544
Epoch time: 16073
54232770 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 175
0324 deg
Eccentricity:
0001665
Arg of perigee: 280
6957 deg
Mean anomaly: 79
4008 deg
Mean motion: 15
54058758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3010
Checksum: 301
Coasting Arc #4 (Orbit 3024)
---------------------------------------
Vector Time (GMT): 2016/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4756353
64 A = 6784804
97 meter
Y = 3555421
01 meter E =
0003089
Z = -3283205
45 I = 51
71123
XDOT = -5344
758580 Wp = 72
07026
YDOT = -2779
480213 meter/sec RA = 169
10003 deg
ZDOT = 4737
571966 TA = 249
87202
MA = 249
90525
Ha = 220
415 n
mi
Hp = 215
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15604834
76 X = -4779809
36
Y = 11664767
10 feet Y = 3502100
83 meter
Z = -10771671
41 Z = -3306367
90
XDOT = -17535
297178 XDOT = -5336
293554
YDOT = -9119
029570 feet/sec YDOT = -2839
201052 meter/sec
ZDOT = 15543
215111 ZDOT = 4711
629352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17058284
20 X = -5199365
02
Y = 9295382
20 feet Y = 2833232
50 meter
Z = -10872781
35 Z = -3314023
76
XDOT = -15453
636502 XDOT = -4710
268406
YDOT = -10327
361317 feet/sec YDOT = -3147
779729 meter/sec
ZDOT = 15431
019383 ZDOT = 4703
374708
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 16074
50688777
00016717 00000-0 10270-3 0 9036
2 25544 51
6431 170
2253 0001847 288
8910 71
2043 15
54082866 30250
Satellite: ISS
Catalog Number: 25544
Epoch time: 16074
50688777 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 170
2253 deg
Eccentricity:
0001847
Arg of perigee: 288
8910 deg
Mean anomaly: 71
2043 deg
Mean motion: 15
54082866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3025
Checksum: 310
Coasting Arc #5 (Orbit 3040)
---------------------------------------
Vector Time (GMT): 2016/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5769954
64 A = 6787997
96 meter
Y = -3092659
11 meter E =
0012266
Z = 1772208
55 I = 51
75250
XDOT = 3684
672706 Wp = 115
07295
YDOT = 3605
879280 meter/sec RA = 164
13015 deg
ZDOT = -5678
324421 TA = 45
49272
MA = 45
39254
Ha = 220
448 n
mi
Hp = 215
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18930297
39 X = 5795500
10
Y = -10146519
39 feet Y = -3027992
65 meter
Z = 5814332
52 Z = 1800299
75
XDOT = 12088
821215 XDOT = 3671
659748
YDOT = 11830
312599 feet/sec YDOT = 3647
010456 meter/sec
ZDOT = -18629
673296 ZDOT = -5660
457225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20032150
55 X = 6105799
49
Y = -7653887
15 feet Y = -2332904
80 meter
Z = 5936786
48 Z = 1809532
52
XDOT = 10042
054395 XDOT = 3060
818180
YDOT = 11828
161858 feet/sec YDOT = 3605
223734 meter/sec
ZDOT = -18552
656517 ZDOT = -5654
849706
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 16075
53573653
00016717 00000-0 10270-3 0 9047
2 25544 51
6422 165
0973 0001688 291
6330 68
4642 15
54109666 30411
Satellite: ISS
Catalog Number: 25544
Epoch time: 16075
53573653 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 165
0973 deg
Eccentricity:
0001688
Arg of perigee: 291
6330 deg
Mean anomaly: 68
4642 deg
Mean motion: 15
54109666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3041
Checksum: 312
Coasting Arc #6 (Orbit 3055)
---------------------------------------
Vector Time (GMT): 2016/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6312028
69 A = 6789340
00 meter
Y = 2481724
98 meter E =
0011572
Z = -94938
63 I = 51
78826
XDOT = -1809
592302 Wp = 35
75368
YDOT = -4386
539980 meter/sec RA = 159
16795 deg
ZDOT = 6025
148810 TA = 323
22564
MA = 323
30498
Ha = 220
453 n
mi
Hp = 215
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20708755
54 X = -6338849
66
Y = 8142142
32 feet Y = 2410989
71 meter
Z = -311478
43 Z = -125666
02
XDOT = -5936
982617 XDOT = -1789
673784
YDOT = -14391
535367 feet/sec YDOT = -4406
664113 meter/sec
ZDOT = 19767
548589 ZDOT = 6016
407119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21478902
54 X = -6546769
49
Y = 5805386
10 feet Y = 1769481
68 meter
Z = -445302
48 Z = -135728
20
XDOT = -4014
203523 XDOT = -1223
529234
YDOT = -13405
192645 feet/sec YDOT = -4085
902718 meter/sec
ZDOT = 19730
273564 ZDOT = 6013
787382
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 16076
50026406
00016717 00000-0 10270-3 0 9055
2 25544 51
6429 160
2893 0001871 301
6370 58
4600 15
54121903 30563
Satellite: ISS
Catalog Number: 25544
Epoch time: 16076
50026406 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 160
2893 deg
Eccentricity:
0001871
Arg of perigee: 301
6370 deg
Mean anomaly: 58
4600 deg
Mean motion: 15
54121903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3056
Checksum: 282
Coasting Arc #7 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2016/077/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2218954
99 A = 6781174
57 meter
Y = -4726753
34 meter E =
0008708
Z = 4322723
52 I = 51
78005
XDOT = 6816
258490 Wp = 59
58883
YDOT = -24
059600 meter/sec RA = 155
83356 deg
ZDOT = -3515
677932 TA = 66
15142
MA = 66
06018
Ha = 220
339 n
mi
Hp = 215
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7280036
06 X = 2250648
07
Y = -15507720
93 feet Y = -4701761
88 meter
Z = 14182163
79 Z = 4333579
98
XDOT = 22363
052788 XDOT = 6833
098419
YDOT = -78
935696 feet/sec YDOT = 52
258146 meter/sec
ZDOT = -11534
376416 ZDOT = -3482
525673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8303931
96 X = 2531038
46
Y = 14938955
36 feet Y = 4553393
59 meter
Z = 14230053
76 Z = 4337320
39
XDOT = -12052
945114 XDOT = -3673
737671
YDOT = 17579
427930 feet/sec YDOT = 5358
209633 meter/sec
ZDOT = -11390
394438 ZDOT = -3471
792225
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 16077
20757290
00016717 00000-0 10270-3 0 9066
2 25544 51
6414 156
7637 0002218 310
4968 49
5991 15
54187794 30676
Satellite: ISS
Catalog Number: 25544
Epoch time: 16077
20757290 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 156
7637 deg
Eccentricity:
0002218
Arg of perigee: 310
4968 deg
Mean anomaly: 49
5991 deg
Mean motion: 15
54187794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3067
Checksum: 336
Coasting Arc #8 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2016/078/03:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3623170
00 A = 6785001
63 meter
Y = 4820144
77 meter E =
0003881
Z = -3110111
47 I = 51
81985
XDOT = -5776
662431 Wp = 50
66415
YDOT = -1187
283496 meter/sec RA = 150
85882 deg
ZDOT = 4895
996078 TA = 273
66395
MA = 273
70833
Ha = 220
455 n
mi
Hp = 215
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11887040
67 X = -3661693
37
Y = 15814123
27 feet Y = 4779412
34 meter
Z = -10203777
77 Z = -3127805
80
XDOT = -18952
304564 XDOT = -5786
738965
YDOT = -3895
287059 feet/sec YDOT = -1251
937780 meter/sec
ZDOT = 16062
979259 ZDOT = 4867
910485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6148727
88 X = -1874132
26
Y = -18761435
97 feet Y = -5718485
68 meter
Z = -10281389
86 Z = -3133767
63
XDOT = 12768
479904 XDOT = 3891
832675
YDOT = -12908
956509 feet/sec YDOT = -3934
649944 meter/sec
ZDOT = 15941
177234 ZDOT = 4858
870821
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 16078
17207622
00016717 00000-0 10270-3 0 9073
2 25544 51
6396 151
9550 0001995 314
9497 45
1494 15
54184047 30828
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
17207622 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 151
9550 deg
Eccentricity:
0001995
Arg of perigee: 314
9497 deg
Mean anomaly: 45
1494 deg
Mean motion: 15
54184047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 325
Coasting Arc #9 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2016/078/21:26:42
000
Vector Time (MET): N/A
Weight (LBS) : 890369
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3235316
43 A = 6777439
28 meter
Y = -2822037
77 meter E =
0001874
Z = 5242809
19 I = 51
81720
XDOT = 5899
291120 Wp = 105
90107
YDOT = -4785
322887 meter/sec RA = 147
27545 deg
ZDOT = 1063
825003 TA = 333
93133
MA = 333
94076
Ha = 220
539 n
mi
Hp = 214
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10614555
21 X = -3228986
25
Y = -9258654
09 feet Y = -2858181
20 meter
Z = 17200817
55 Z = 5227108
74
XDOT = 19354
629658 XDOT = 5947
195802
YDOT = -15699
878239 feet/sec YDOT = -4719
085115 meter/sec
ZDOT = 3490
239510 ZDOT = 1092
598853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1700629
61 X = 518351
91
Y = 14065049
48 feet Y = 4287027
08 meter
Z = 17133062
31 Z = 5222157
39
XDOT = -23838
586591 XDOT = -7266
001193
YDOT = -1525
645872 feet/sec YDOT = -465
016862 meter/sec
ZDOT = 3615
980589 ZDOT = 1102
150883
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 16078
94366965
00016717 00000-0 10270-3 0 9085
2 25544 51
6418 148
1113 0002113 319
2021 40
8973 15
54234519 30947
Satellite: ISS
Catalog Number: 25544
Epoch time: 16078
94366965 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 148
1113 deg
Eccentricity:
0002113
Arg of perigee: 319
2021 deg
Mean anomaly: 40
8973 deg
Mean motion: 15
54234519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 306
Coasting Arc #10 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2016/079/03:12:07
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4682089
46 A = 6788008
19 meter
Y = 4647343
31 meter E =
0008573
Z = -1580469
10 I = 51
85754
XDOT = -4407
076871 Wp = 24
01653
YDOT = -2487
156853 meter/sec RA = 146
05754 deg
ZDOT = 5760
972851 TA = 318
75182
MA = 318
81656
Ha = 220
436 n
mi
Hp = 215
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15361185
90 X = -4726032
08
Y = 15247189
33 feet Y = 4594739
18 meter
Z = -5185266
07 Z = -1603320
54
XDOT = -14458
913620 XDOT = -4406
921308
YDOT = -8159
963430 feet/sec YDOT = -2536
438135 meter/sec
ZDOT = 18900
829565 ZDOT = 5739
565326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 327403
41 X = 99792
56
Y = -21616859
29 feet Y = -6588818
71 meter
Z = -5285262
58 Z = -1610948
03
XDOT = 14557
650635 XDOT = 4437
171914
YDOT = -4363
442730 feet/sec YDOT = -1329
977344 meter/sec
ZDOT = 18808
229115 ZDOT = 5732
748234
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 16079
13656610
00016717 00000-0 10270-3 0 9097
2 25544 51
6405 147
1480 0002131 317
6972 42
4016 15
54203255 30978
Satellite: ISS
Catalog Number: 25544
Epoch time: 16079
13656610 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 147
1480 deg
Eccentricity:
0002131
Arg of perigee: 317
6972 deg
Mean anomaly: 42
4016 deg
Mean motion: 15
54203255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 289
Coasting Arc #11 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2016/080/03:12:07
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5360094
99 A = 6788985
08 meter
Y = -4155979
01 meter E =
0009663
Z = -167344
39 I = 51
88762
XDOT = 2787
400455 Wp = 133
71184
YDOT = 3828
800738 meter/sec RA = 141
10259 deg
ZDOT = -6029
879152 TA = 48
08461
MA = 48
00225
Ha = 220
511 n
mi
Hp = 214
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17585613
50 X = 5406982
69
Y = -13635101
75 feet Y = -4095776
73 meter
Z = -549030
16 Z = -141192
24
XDOT = 9145
014616 XDOT = 2773
668913
YDOT = 12561
682212 feet/sec YDOT = 3859
893689 meter/sec
ZDOT = -19783
068083 ZDOT = -6016
372698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2691821
47 X = -820467
18
Y = 22091544
00 feet Y = 6733502
61 meter
Z = -434760
67 Z = -132515
05
XDOT = -13837
310972 XDOT = -4217
612384
YDOT = -2056
028559 feet/sec YDOT = -626
677505 meter/sec
ZDOT = -19724
997068 ZDOT = -6012
179106
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 16080
16534108
00016717 00000-0 10270-3 0 9101
2 25544 51
6410 142
0188 0002224 325
5296 34
5712 15
54243792 31137
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
16534108 = yrday
fracday
Element set: 910
Inclination: 51
6410 deg
RA of node: 142
0188 deg
Eccentricity:
0002224
Arg of perigee: 325
5296 deg
Mean anomaly: 34
5712 deg
Mean motion: 15
54243792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 272
Coasting Arc #12 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2016/080/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4651466
01 A = 6779189
55 meter
Y = -1014676
97 meter E =
0005667
Z = 4822565
58 I = 51
86526
XDOT = 3982
639227 Wp = 113
22496
YDOT = -6032
253681 meter/sec RA = 139
62629 deg
ZDOT = 2567
573399 TA = 311
56549
MA = 311
61406
Ha = 220
553 n
mi
Hp = 214
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15260715
24 X = -4663199
62
Y = -3328992
67 feet Y = -1066757
67 meter
Z = 15822065
56 Z = 4799941
82
XDOT = 13066
401665 XDOT = 4037
325359
YDOT = -19790
858533 feet/sec YDOT = -5987
411026 meter/sec
ZDOT = 8423
797242 ZDOT = 2587
053536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12312320
28 X = -3752795
22
Y = -9771073
51 feet Y = -2978223
21 meter
Z = 15723939
47 Z = 4792656
75
XDOT = 19702
873079 XDOT = 6005
435715
YDOT = -11109
316628 feet/sec YDOT = -3386
119708 meter/sec
ZDOT = 8509
381172 ZDOT = 2593
659381
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 16080
48682981
00016717 00000-0 10270-3 0 9110
2 25544 51
6437 140
4153 0001861 317
8140 42
2869 15
54261084 31186
Satellite: ISS
Catalog Number: 25544
Epoch time: 16080
48682981 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 140
4153 deg
Eccentricity:
0001861
Arg of perigee: 317
8140 deg
Mean anomaly: 42
2869 deg
Mean motion: 15
54261084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3118
Checksum: 300
Coasting Arc #13 (Orbit 3132)
---------------------------------------
Vector Time (GMT): 2016/081/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3480657
42 A = 6777211
03 meter
Y = 2402296
97 meter E =
0013747
Z = -5307571
82 I = 51
88088
XDOT = -4985
346329 Wp = 78
04358
YDOT = 5777
004756 meter/sec RA = 134
64444 deg
ZDOT = -653
229981 TA = 185
72457
MA = 185
74030
Ha = 220
524 n
mi
Hp = 215
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11419479
72 X = 3479317
33
Y = 7881551
73 feet Y = 2441211
68 meter
Z = -17413293
36 Z = -5290667
43
XDOT = -16356
123127 XDOT = -5046
402629
YDOT = 18953
427677 feet/sec YDOT = 5720
913811 meter/sec
ZDOT = -2143
142983 ZDOT = -677
596527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7072711
66 X = 2155762
51
Y = 12043226
68 feet Y = 3670775
49 meter
Z = -17340230
71 Z = -5285302
32
XDOT = -21983
340131 XDOT = -6700
522072
YDOT = 9664
415960 feet/sec YDOT = 2945
713985 meter/sec
ZDOT = -2249
927142 ZDOT = -685
777793
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 16081
45129141
00016717 00000-0 10270-3 0 9123
2 25544 51
6424 135
6078 0001940 324
1291 35
9731 15
54232008 31338
Satellite: ISS
Catalog Number: 25544
Epoch time: 16081
45129141 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 135
6078 deg
Eccentricity:
0001940
Arg of perigee: 324
1291 deg
Mean anomaly: 35
9731 deg
Mean motion: 15
54232008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3133
Checksum: 275
Coasting Arc #14 (Orbit 3148)
---------------------------------------
Vector Time (GMT): 2016/082/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2177438
68 A = 6777411
38 meter
Y = -3760583
92 meter E =
0004726
Z = 5199645
14 I = 51
90417
XDOT = 5581
246103 Wp = 31
29661
YDOT = -5088
175673 meter/sec RA = 129
66082 deg
ZDOT = -1338
244557 TA = 71
53809
MA = 71
48673
Ha = 220
518 n
mi
Hp = 214
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7143827
70 X = -2160482
58
Y = -12337873
76 feet Y = -3784837
84 meter
Z = 17059203
23 Z = 5189109
54
XDOT = 18311
174877 XDOT = 5644
229121
YDOT = -16693
489740 feet/sec YDOT = -5025
410525 meter/sec
ZDOT = -4390
566132 ZDOT = -1310
978607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1548455
04 X = -471969
10
Y = -14226698
23 feet Y = -4336297
62 meter
Z = 17014028
41 Z = 5185875
86
XDOT = 22538
849030 XDOT = 6869
841184
YDOT = -7578
908100 feet/sec YDOT = -2310
051189 meter/sec
ZDOT = -4271
281996 ZDOT = -1301
886752
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 16082
48003717
00016717 00000-0 10270-3 0 9138
2 25544 51
6425 130
4789 0001951 327
0447 33
0584 15
54299492 31490
Satellite: ISS
Catalog Number: 25544
Epoch time: 16082
48003717 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 130
4789 deg
Eccentricity:
0001951
Arg of perigee: 327
0447 deg
Mean anomaly: 33
0584 deg
Mean motion: 15
54299492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3149
Checksum: 312
Coasting Arc #15 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2016/083/10:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 887836
79 A = 6780109
83 meter
Y = 4964797
17 meter E =
0008582
Z = -4539405
21 I = 51
93222
XDOT = -5752
730688 Wp = 100
99831
YDOT = 3934
429714 meter/sec RA = 124
68303 deg
ZDOT = 3181
480599 TA = 200
81879
MA = 200
85376
Ha = 220
591 n
mi
Hp = 214
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2912850
37 X = 854303
65
Y = 16288704
64 feet Y = 4974537
32 meter
Z = -14893061
72 Z = -4535174
59
XDOT = -18873
788345 XDOT = -5811
753145
YDOT = 12908
233970 feet/sec YDOT = 3869
769358 meter/sec
ZDOT = 10437
928474 ZDOT = 3153
391324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3667023
52 X = -1117708
77
Y = 16151869
91 feet Y = 4923089
95 meter
Z = -14875480
51 Z = -4534046
46
XDOT = -21320
867627 XDOT = -6498
600453
YDOT = 4648
948250 feet/sec YDOT = 1416
999427 meter/sec
ZDOT = 10315
240183 ZDOT = 3144
085208
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 16083
44447708
00016717 00000-0 10270-3 0 9148
2 25544 51
6417 125
6704 0001938 338
0668 22
0402 15
54304743 31646
Satellite: ISS
Catalog Number: 25544
Epoch time: 16083
44447708 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 125
6704 deg
Eccentricity:
0001938
Arg of perigee: 338
0668 deg
Mean anomaly: 22
0402 deg
Mean motion: 15
54304743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 298
Coasting Arc #16 (Orbit 3175)
---------------------------------------
Vector Time (GMT): 2016/084/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2203755
26 A = 6787635
53 meter
Y = -6195295
01 meter E =
0012758
Z = 1661517
28 I = 51
96797
XDOT = 5080
389431 Wp = 110
31289
YDOT = 259
546005 meter/sec RA = 120
98036 deg
ZDOT = -5739
349723 TA = 51
56637
MA = 51
45192
Ha = 220
637 n
mi
Hp = 214
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7230168
16 X = 2264797
85
Y = -20325771
03 feet Y = -6170309
58 meter
Z = 5451172
16 Z = 1672371
83
XDOT = 16667
944329 XDOT = 5104
988865
YDOT = 851
528889 feet/sec YDOT = 316
494926 meter/sec
ZDOT = -18829
887542 ZDOT = -5714
610730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15700819
16 X = 4785609
68
Y = 14777315
10 feet Y = 4504125
64 meter
Z = 5499346
67 Z = 1676200
87
XDOT = -6467
359404 XDOT = -1971
251146
YDOT = 13876
883343 feet/sec YDOT = 4229
674043 meter/sec
ZDOT = -18722
430701 ZDOT = -5706
596878
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 16084
21602104
00016717 00000-0 10270-3 0 9158
2 25544 51
6391 121
8197 0001811 342
5783 17
5307 15
54302046 31769
Satellite: ISS
Catalog Number: 25544
Epoch time: 16084
21602104 = yrday
fracday
Element set: 915
Inclination: 51
6391 deg
RA of node: 121
8197 deg
Eccentricity:
0001811
Arg of perigee: 342
5783 deg
Mean anomaly: 17
5307 deg
Mean motion: 15
54302046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3176
Checksum: 281
Coasting Arc #17 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2016/085/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3032781
24 A = 6788769
30 meter
Y = 6065377
31 meter E =
0013201
Z = 80774
77 I = 51
98839
XDOT = -4190
134432 Wp = 40
07468
YDOT = -2182
752729 meter/sec RA = 116
03232 deg
ZDOT = 6042
631748 TA = 320
79149
MA = 320
88704
Ha = 220
673 n
mi
Hp = 214
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9950069
69 X = -3100772
77
Y = 19899531
87 feet Y = 6031082
59 meter
Z = 265009
09 Z = 65876
16
XDOT = -13747
160210 XDOT = -4194
767566
YDOT = -7161
262233 feet/sec YDOT = -2229
634592 meter/sec
ZDOT = 19824
907310 ZDOT = 6022
266113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14492608
06 X = -4417346
94
Y = -16881649
47 feet Y = -5145526
76 meter
Z = 199268
78 Z = 60737
12
XDOT = 10742
993432 XDOT = 3274
464398
YDOT = -8962
056034 feet/sec YDOT = -2731
634679 meter/sec
ZDOT = 19736
767451 ZDOT = 6015
766719
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 16085
24473572
00016717 00000-0 10270-3 0 9168
2 25544 51
6399 116
6906 0001693 348
2296 11
8817 15
54321611 31927
Satellite: ISS
Catalog Number: 25544
Epoch time: 16085
24473572 = yrday
fracday
Element set: 916
Inclination: 51
6399 deg
RA of node: 116
6906 deg
Eccentricity:
0001693
Arg of perigee: 348
2296 deg
Mean anomaly: 11
8817 deg
Mean motion: 15
54321611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3192
Checksum: 319
Coasting Arc #18 (Orbit 3206)
---------------------------------------
Vector Time (GMT): 2016/086/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 905478
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3640934
83 A = 6787270
70 meter
Y = -5418105
51 meter E =
0005759
Z = -1853264
83 I = 51
99686
XDOT = 3177
003729 Wp = 132
60227
YDOT = 4068
087602 meter/sec RA = 111
08407 deg
ZDOT = -5666
632238 TA = 67
67700
MA = 67
61596
Ha = 220
677 n
mi
Hp = 214
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11945324
23 X = 3710253
25
Y = -17775936
73 feet Y = -5377002
83 meter
Z = -6080265
20 Z = -1835408
85
XDOT = 10423
240580 XDOT = 3158
803490
YDOT = 13346
744101 feet/sec YDOT = 4103
512422 meter/sec
ZDOT = -18591
313118 ZDOT = -5651
243816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12054769
48 X = 3674293
74
Y = 17728667
94 feet Y = 5403697
99 meter
Z = -6001765
42 Z = -1829338
10
XDOT = -15013
063115 XDOT = -4575
981638
YDOT = 3953
699548 feet/sec YDOT = 1205
087622 meter/sec
ZDOT = -18525
117951 ZDOT = -5646
455951
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 16086
20914506
00016717 00000-0 10270-3 0 9173
2 25544 51
6399 111
8812 0001812 350
7736 9
3383 15
54347148 32070
Satellite: ISS
Catalog Number: 25544
Epoch time: 16086
20914506 = yrday
fracday
Element set: 917
Inclination: 51
6399 deg
RA of node: 111
8812 deg
Eccentricity:
0001812
Arg of perigee: 350
7736 deg
Mean anomaly: 9
3383 deg
Mean motion: 15
54347148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3207
Checksum: 307
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