[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 30th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1552 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
304/00:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
1
304/02:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 212
2
307/03:37:45
968 -0
4 4
5 4
5
N/A 4
3 -0
5 222
6
000/00:01:27
935 1
4 -0
1 215
1
308/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 215
2
311/14:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 215
4
314/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2016/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908899
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1427295
78 A = 6787666
31 meter
Y = -6470251
18 meter E =
0020372
Z = 1428424
13 I = 51
99710
XDOT = 4992
955451 Wp = 118
56798
YDOT = -196
165393 meter/sec RA = 112
13762 deg
ZDOT = -5824
354802 TA = 45
91958
MA = 45
75206
Ha = 222
856 n
mi
Hp = 212
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4682728
93 X = 1492602
88
Y = -21227858
21 feet Y = -6453924
92 meter
Z = 4686430
88 Z = 1435516
93
XDOT = 16381
087438 XDOT = 5023
070745
YDOT = -643
587247 feet/sec YDOT = -140
162950 meter/sec
ZDOT = -19108
775597 ZDOT = -5800
026594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8854744
71 X = 2698926
19
Y = 19845433
95 feet Y = 6048888
27 meter
Z = 4718558
69 Z = 1438216
69
XDOT = -11452
968484 XDOT = -3490
864794
YDOT = 9669
448160 feet/sec YDOT = 2947
247799 meter/sec
ZDOT = -19002
215271 ZDOT = -5791
875214
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 16302
53500896
00016717 00000-0 10270-3 0 9005
2 25544 51
6382 112
9465 0006512 117
2860 242
8957 15
54400916 25722
Satellite: ISS
Catalog Number: 25544
Epoch time: 16302
53500896 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 112
9465 deg
Eccentricity:
0006512
Arg of perigee: 117
2860 deg
Mean anomaly: 242
8957 deg
Mean motion: 15
54400916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 301
Coasting Arc #2 (Orbit 2587)
---------------------------------------
Vector Time (GMT): 2016/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 908899
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2249001
35 A = 6788560
35 meter
Y = 6392518
29 meter E =
0016053
Z = 331902
30 I = 52
01069
XDOT = -4355
164405 Wp = 73
02315
YDOT = -1857
547911 meter/sec RA = 107
19063 deg
ZDOT = 6030
340789 TA = 290
53549
MA = 290
70768
Ha = 222
978 n
mi
Hp = 212
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7378613
36 X = -2321929
25
Y = 20972829
03 feet Y = 6366960
71 meter
Z = 1088918
32 Z = 320799
31
XDOT = -14288
597129 XDOT = -4363
362651
YDOT = -6094
317293 feet/sec YDOT = -1906
295641 meter/sec
ZDOT = 19784
582642 ZDOT = 6009
164216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6868716
88 X = -2093584
91
Y = -21147812
45 feet Y = -6445853
24 meter
Z = 1039226
94 Z = 316756
37
XDOT = 13611
459559 XDOT = 4148
772874
YDOT = -3413
468390 feet/sec YDOT = -1040
425165 meter/sec
ZDOT = 19692
162907 ZDOT = 6002
171254
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 16303
56368456
00016717 00000-0 10270-3 0 9014
2 25544 51
6378 107
8164 0006893 122
3593 237
8227 15
54378377 25884
Satellite: ISS
Catalog Number: 25544
Epoch time: 16303
56368456 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 107
8164 deg
Eccentricity:
0006893
Arg of perigee: 122
3593 deg
Mean anomaly: 237
8227 deg
Mean motion: 15
54378377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2588
Checksum: 342
Coasting Arc #3 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2016/304/00:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4344832
05 A = 6779670
24 meter
Y = 2429707
17 meter E =
0015138
Z = 4594482
57 I = 51
98646
XDOT = -654
258695 Wp = 117
53195
YDOT = -7002
525074 meter/sec RA = 104
61209 deg
ZDOT = 3069
915272 TA = 301
87946
MA = 302
02667
Ha = 222
931 n
mi
Hp = 212
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14254698
33 X = -4393997
33
Y = 7971480
22 feet Y = 2380845
78 meter
Z = 15073761
71 Z = 4573256
33
XDOT = -2146
518028 XDOT = -590
818750
YDOT = -22974
163629 feet/sec YDOT = -7009
486496 meter/sec
ZDOT = 10071
900498 ZDOT = 3066
891568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4051651
74 X = -1234943
45
Y = 15910088
83 feet Y = 4849395
08 meter
Z = 14980400
70 Z = 4566026
13
XDOT = -17066
034581 XDOT = -5201
727340
YDOT = -13863
203654 feet/sec YDOT = -4225
504474 meter/sec
ZDOT = 10059
842855 ZDOT = 3066
240102
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 16304
07801780
00016717 00000-0 10270-3 0 9024
2 25544 51
6382 105
2557 0006565 122
6562 237
5225 15
54403819 25966
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
07801780 = yrday
fracday
Element set: 902
Inclination: 51
6382 deg
RA of node: 105
2557 deg
Eccentricity:
0006565
Arg of perigee: 122
6562 deg
Mean anomaly: 237
5225 deg
Mean motion: 15
54403819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 304
Coasting Arc #4 (Orbit 2596)
---------------------------------------
Vector Time (GMT): 2016/304/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3225647
83 A = 6786421
30 meter
Y = -5517439
12 meter E =
0012420
Z = -2276449
22 I = 52
01130
XDOT = 3345
749707 Wp = 128
44837
YDOT = 4201
532567 meter/sec RA = 104
16068 deg
ZDOT = -5470
076321 TA = 76
74902
MA = 76
61051
Ha = 222
891 n
mi
Hp = 212
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10582834
10 X = 3298163
80
Y = -18101834
37 feet Y = -5480962
46 meter
Z = -7468665
43 Z = -2260602
90
XDOT = 10976
869118 XDOT = 3325
090388
YDOT = 13784
555667 feet/sec YDOT = 4238
831082 meter/sec
ZDOT = -17946
444624 ZDOT = -5453
873573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15801575
22 X = -4816320
13
Y = -13821307
27 feet Y = -4212734
46 meter
Z = -7398339
97 Z = -2255014
02
XDOT = 14602
470817 XDOT = 4450
833105
YDOT = -7174
751646 feet/sec YDOT = -2186
864302 meter/sec
ZDOT = -17876
202814 ZDOT = -5448
666618
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 16304
14231080
00016717 00000-0 10270-3 0 9033
2 25544 51
6399 104
9344 0006552 121
1295 239
0502 15
54385178 25970
Satellite: ISS
Catalog Number: 25544
Epoch time: 16304
14231080 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 104
9344 deg
Eccentricity:
0006552
Arg of perigee: 121
1295 deg
Mean anomaly: 239
0502 deg
Mean motion: 15
54385178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2597
Checksum: 297
Coasting Arc #5 (Orbit 2612)
---------------------------------------
Vector Time (GMT): 2016/305/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3653785
33 A = 6782695
08 meter
Y = 4317507
54 meter E =
0017660
Z = 3733286
86 I = 52
00661
XDOT = -2469
569162 Wp = 106
33556
YDOT = -5841
828349 meter/sec RA = 99
20504 deg
ZDOT = 4317
338582 TA = 298
01153
MA = 298
19007
Ha = 222
837 n
mi
Hp = 212
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11987484
67 X = -3719928
43
Y = 14165050
99 feet Y = 4276278
84 meter
Z = 12248316
46 Z = 3715376
30
XDOT = -8102
261031 XDOT = -2425
033141
YDOT = -19166
103508 feet/sec YDOT = -5869
195471 meter/sec
ZDOT = 14164
496659 ZDOT = 4305
450213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11914166
28 X = 3631437
88
Y = 14294557
68 feet Y = 4356981
18 meter
Z = 12169140
36 Z = 3709153
98
XDOT = -19234
583317 XDOT = -5862
700995
YDOT = 3955
613389 feet/sec YDOT = 1205
670961 meter/sec
ZDOT = 14113
438501 ZDOT = 4301
776055
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16305
17097248
00016717 00000-0 10270-3 0 9044
2 25544 51
6405 99
8052 0006528 126
0896 234
0862 15
54402735 26132
Satellite: ISS
Catalog Number: 25544
Epoch time: 16305
17097248 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 99
8052 deg
Eccentricity:
0006528
Arg of perigee: 126
0896 deg
Mean anomaly: 234
0862 deg
Mean motion: 15
54402735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2613
Checksum: 310
Coasting Arc #6 (Orbit 2627)
---------------------------------------
Vector Time (GMT): 2016/306/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3968774
55 A = 6778803
98 meter
Y = -2677900
57 meter E =
0015881
Z = -4812449
00 I = 51
99869
XDOT = 1546
996704 Wp = 91
35637
YDOT = 7020
040085 meter/sec RA = 94
23709 deg
ZDOT = -2638
392896 TA = 152
75642
MA = 152
67302
Ha = 222
748 n
mi
Hp = 212
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13020913
88 X = 4021802
00
Y = -8785763
03 feet Y = -2633222
77 meter
Z = -15788874
67 Z = -4793040
25
XDOT = 5075
448503 XDOT = 1481
198373
YDOT = 23031
627574 feet/sec YDOT = 7036
971634 meter/sec
ZDOT = -8656
144671 ZDOT = -2631
037869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6681112
59 X = -2036403
12
Y = -14310418
65 feet Y = -4361815
61 meter
Z = -15703408
74 Z = -4786398
99
XDOT = 22500
700751 XDOT = 6858
213589
YDOT = -1068
638060 feet/sec YDOT = -325
720881 meter/sec
ZDOT = -8625
158929 ZDOT = -2628
948441
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16306
13533551
00016717 00000-0 10270-3 0 9054
2 25544 51
6412 94
9954 0006500 127
4645 232
7100 15
54415209 26280
Satellite: ISS
Catalog Number: 25544
Epoch time: 16306
13533551 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 94
9954 deg
Eccentricity:
0006500
Arg of perigee: 127
4645 deg
Mean anomaly: 232
7100 deg
Mean motion: 15
54415209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2628
Checksum: 288
Coasting Arc #7 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2016/307/02:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 893668
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4132810
72 A = 6776557
13 meter
Y = 821090
65 meter E =
0009284
Z = 5301505
61 I = 51
99298
XDOT = -630
888829 Wp = 127
39804
YDOT = -7618
167731 meter/sec RA = 89
26260 deg
ZDOT = 681
772499 TA = 316
09156
MA = 316
16531
Ha = 222
696 n
mi
Hp = 212
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13559090
30 X = -4167438
33
Y = 2693866
96 feet Y = 774681
30 meter
Z = 17393391
10 Z = 5281344
78
XDOT = -2069
845239 XDOT = -548
965487
YDOT = -24993
988619 feet/sec YDOT = -7624
764676 meter/sec
ZDOT = 2236
786415 ZDOT = 678
906893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 816419
53 X = 248844
67
Y = 13910718
21 feet Y = 4239986
91 meter
Z = 17304949
61 Z = 5274548
64
XDOT = -24031
156552 XDOT = -7324
696517
YDOT = -1384
119950 feet/sec YDOT = -421
879761 meter/sec
ZDOT = 2225
585641 ZDOT = 678
358503
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16307
16398046
00016717 00000-0 10270-3 0 9067
2 25544 51
6412 89
8669 0006345 132
8013 227
3674 15
54451004 26449
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
16398046 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 89
8669 deg
Eccentricity:
0006345
Arg of perigee: 132
8013 deg
Mean anomaly: 227
3674 deg
Mean motion: 15
54451004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 310
Coasting Arc #8 (Orbit 2643)
---------------------------------------
Vector Time (GMT): 2016/307/03:38:29
935
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3928143
38 A = 6780599
37 meter
Y = 2434303
42 meter E =
0014754
Z = -4975507
66 I = 51
99928
XDOT = -1616
145203 Wp = 116
39215
YDOT = 7146
707620 meter/sec RA = 89
05343 deg
ZDOT = 2219
346649 TA = 175
19958
MA = 175
18542
Ha = 222
644 n
mi
Hp = 215
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12887609
53 X = 3924799
95
Y = 7986559
78 feet Y = 2478211
74 meter
Z = -16323844
02 Z = -4956433
39
XDOT = -5302
313658 XDOT = -1706
722315
YDOT = 23447
203477 feet/sec YDOT = 7128
128406 meter/sec
ZDOT = 7281
321028 ZDOT = 2211
275432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6675024
12 X = 2034547
35
Y = -13712256
71 feet Y = -4179495
85 meter
Z = -16240737
94 Z = -4950176
92
XDOT = 22858
940768 XDOT = 6967
405146
YDOT = 2541
916983 feet/sec YDOT = 774
776296 meter/sec
ZDOT = 7244
705738 ZDOT = 2208
186309
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16307
16398163
00016717 00000-0 10270-3 0 9078
2 25544 51
6426 89
8653 0003414 156
3626 203
7684 15
53570542 26449
Satellite: ISS
Catalog Number: 25544
Epoch time: 16307
16398163 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 89
8653 deg
Eccentricity:
0003414
Arg of perigee: 156
3626 deg
Mean anomaly: 203
7684 deg
Mean motion: 15
53570542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2644
Checksum: 321
Coasting Arc #9 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/03:38:29
935
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3693094
49 A = 6783531
54 meter
Y = -3829738
86 meter E =
0011084
Z = 4198454
91 I = 52
00785
XDOT = 2280
519273 Wp = 93
05719
YDOT = -6302
166482 meter/sec RA = 84
09184 deg
ZDOT = -3734
790175 TA = 35
12510
MA = 35
05207
Ha = 222
690 n
mi
Hp = 215
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12116451
75 X = -3670389
69
Y = -12564760
03 feet Y = -3870910
52 meter
Z = 13774458
36 Z = 4180569
53
XDOT = 7482
018611 XDOT = 2368
964668
YDOT = -20676
399220 feet/sec YDOT = -6276
169699 meter/sec
ZDOT = -12253
248606 ZDOT = -3723
496809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11076794
48 X = -3376206
96
Y = 13569054
76 feet Y = 4135847
89 meter
Z = 13696812
69 Z = 4174788
51
XDOT = -20420
294134 XDOT = -6224
105652
YDOT = -4325
823126 feet/sec YDOT = -1318
510889 meter/sec
ZDOT = -12202
653272 ZDOT = -3719
368717
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16308
19318120
00016717 00000-0 10270-3 0 9088
2 25544 51
6428 84
7402 0003414 160
7245 199
4037 15
53578117 26600
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19318120 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 84
7402 deg
Eccentricity:
0003414
Arg of perigee: 160
7245 deg
Mean anomaly: 199
4037 deg
Mean motion: 15
53578117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 302
Coasting Arc #10 (Orbit 2659)
---------------------------------------
Vector Time (GMT): 2016/308/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4158427
12 A = 6780249
08 meter
Y = 1831580
95 meter E =
0014834
Z = -5045810
14 I = 51
99788
XDOT = -798
787069 Wp = 115
86051
YDOT = 7345
231708 meter/sec RA = 83
95748 deg
ZDOT = 2006
227517 TA = 173
57253
MA = 173
55348
Ha = 222
497 n
mi
Hp = 215
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13643133
59 X = 4162147
83
Y = 6009123
85 feet Y = 1878104
02 meter
Z = -16554495
20 Z = -5025600
02
XDOT = -2620
692484 XDOT = -890
609590
YDOT = 24098
529225 feet/sec YDOT = 7335
785746 meter/sec
ZDOT = 6582
111277 ZDOT = 2002
124002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1723367
97 X = 525282
56
Y = -14905927
01 feet Y = -4543326
55 meter
Z = -16466308
57 Z = -5018930
85
XDOT = 22737
324276 XDOT = 6930
336439
YDOT = -4627
264587 feet/sec YDOT = -1410
390246 meter/sec
ZDOT = 6562
817931 ZDOT = 2000
346905
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16308
19318016
00016717 00000-0 10270-3 0 9093
2 25544 51
6437 84
7400 0003351 163
0036 197
1229 15
53591240 26602
Satellite: ISS
Catalog Number: 25544
Epoch time: 16308
19318016 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 84
7400 deg
Eccentricity:
0003351
Arg of perigee: 163
0036 deg
Mean anomaly: 197
1229 deg
Mean motion: 15
53591240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2660
Checksum: 289
Coasting Arc #11 (Orbit 2675)
---------------------------------------
Vector Time (GMT): 2016/309/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4072364
00 A = 6782974
38 meter
Y = -3272159
20 meter E =
0010208
Z = 4317499
50 I = 52
00354
XDOT = 1542
336499 Wp = 90
86835
YDOT = -6621
041974 meter/sec RA = 78
99405 deg
ZDOT = -3556
128158 TA = 35
19259
MA = 35
12522
Ha = 222
501 n
mi
Hp = 215
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13360774
29 X = -4056444
23
Y = -10735430
43 feet Y = -3317610
08 meter
Z = 14165024
62 Z = 4297755
21
XDOT = 5060
159119 XDOT = 1633
534576
YDOT = -21722
578656 feet/sec YDOT = -6603
284621 meter/sec
ZDOT = -11667
087134 ZDOT = -3548
414179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6054100
58 X = -1845289
86
Y = 16110038
03 feet Y = 4910339
59 meter
Z = 14079141
29 Z = 4291322
27
XDOT = -21072
897707 XDOT = -6423
019221
YDOT = 2267
000670 feet/sec YDOT = 690
981804 meter/sec
ZDOT = -11632
094191 ZDOT = -3545
462309
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16309
22237014
00016717 00000-0 10270-3 0 9108
2 25544 51
6443 79
6143 0003199 165
2992 194
8254 15
53625489 26763
Satellite: ISS
Catalog Number: 25544
Epoch time: 16309
22237014 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 79
6143 deg
Eccentricity:
0003199
Arg of perigee: 165
2992 deg
Mean anomaly: 194
8254 deg
Mean motion: 15
53625489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2676
Checksum: 325
Coasting Arc #12 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2016/310/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3924320
96 A = 6786445
54 meter
Y = 4487204
14 meter E =
0005648
Z = -3250636
09 I = 52
00739
XDOT = -2322
502422 Wp = 114
94302
YDOT = 5502
599151 meter/sec RA = 74
03762 deg
ZDOT = 4796
193378 TA = 207
64938
MA = 207
67942
Ha = 222
337 n
mi
Hp = 215
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12875068
75 X = 3889642
72
Y = 14721798
37 feet Y = 4530894
64 meter
Z = -10664816
57 Z = -3231656
58
XDOT = -7619
758603 XDOT = -2407
159570
YDOT = 18053
146820 feet/sec YDOT = 5476
154017 meter/sec
ZDOT = 15735
542579 ZDOT = 4784
705406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9711403
64 X = 2960035
83
Y = -17027511
97 feet Y = -5189985
65 meter
Z = -10582510
61 Z = -3225549
23
XDOT = 18342
591714 XDOT = 5590
821954
YDOT = 722
407070 feet/sec YDOT = 220
189675 meter/sec
ZDOT = 15684
210167 ZDOT = 4780
547259
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16310
18722994
00016717 00000-0 10270-3 0 9112
2 25544 51
6438 74
8086 0003174 169
3054 190
8166 15
53604820 26918
Satellite: ISS
Catalog Number: 25544
Epoch time: 16310
18722994 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 74
8086 deg
Eccentricity:
0003174
Arg of perigee: 169
3054 deg
Mean anomaly: 190
8166 deg
Mean motion: 15
53604820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 314
Coasting Arc #13 (Orbit 2706)
---------------------------------------
Vector Time (GMT): 2016/311/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3637322
50 A = 6789423
10 meter
Y = -5404717
88 meter E =
0015945
Z = 1880432
35 I = 52
00739
XDOT = 3162
019696 Wp = 123
54312
YDOT = -4105
401594 meter/sec RA = 69
08943 deg
ZDOT = -5657
597929 TA = 35
85373
MA = 35
74681
Ha = 222
391 n
mi
Hp = 215
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11933472
76 X = -3585749
71
Y = -17732014
04 feet Y = -5445104
50 meter
Z = 6169397
46 Z = 1862888
13
XDOT = 10374
080366 XDOT = 3235
174964
YDOT = -13469
165336 feet/sec YDOT = -4069
632740 meter/sec
ZDOT = -18561
672994 ZDOT = -5642
059680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12578204
13 X = -3833836
62
Y = 17307539
59 feet Y = 5275338
07 meter
Z = 6093555
06 Z = 1857315
58
XDOT = -14982
177804 XDOT = -4566
567795
YDOT = -4347
204738 feet/sec YDOT = -1325
028004 meter/sec
ZDOT = -18492
848016 ZDOT = -5636
620075
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16311
21640802
00016717 00000-0 10270-3 0 9125
2 25544 51
6437 69
6831 0003298 171
7134 188
4074 15
53594810 27076
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
21640802 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 69
6831 deg
Eccentricity:
0003298
Arg of perigee: 171
7134 deg
Mean anomaly: 188
4074 deg
Mean motion: 15
53594810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2707
Checksum: 305
Coasting Arc #14 (Orbit 2712)
---------------------------------------
Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3985930
25 A = 6778884
81 meter
Y = -1298943
45 meter E =
0015570
Z = -5340231
03 I = 51
96738
XDOT = 2751
014621 Wp = 105
72837
YDOT = 7138
312899 meter/sec RA = 67
08589 deg
ZDOT = 313
699817 TA = 167
27301
MA = 167
23366
Ha = 222
288 n
mi
Hp = 215
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13077199
00 X = 4026100
07
Y = -4261625
50 feet Y = -1254145
52 meter
Z = -17520443
00 Z = -5320770
50
XDOT = 9025
638521 XDOT = 2669
463877
YDOT = 23419
661742 feet/sec YDOT = 7168
620615 meter/sec
ZDOT = 1029
198874 ZDOT = 326
865655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1093538
16 X = 333310
43
Y = 13819077
89 feet Y = 4212054
94 meter
Z = -17434958
24 Z = -5314175
27
XDOT = -23863
769749 XDOT = -7273
677019
YDOT = 3271
885644 feet/sec YDOT = 997
270744 meter/sec
ZDOT = 1085
536097 ZDOT = 330
871402
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16311
60234579
00016717 00000-0 10270-3 0 9139
2 25544 51
6434 67
7572 0003605 177
3012 182
8161 15
53616574 27137
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
60234579 = yrday
fracday
Element set: 913
Inclination: 51
6434 deg
RA of node: 67
7572 deg
Eccentricity:
0003605
Arg of perigee: 177
3012 deg
Mean anomaly: 182
8161 deg
Mean motion: 15
53616574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2713
Checksum: 300
Coasting Arc #15 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4543458
68 A = 6780070
40 meter
Y = -179922
74 meter E =
0004970
Z = 5024995
30 I = 51
95917
XDOT = -1970
524924 Wp = 91
44426
YDOT = -7128
816002 meter/sec RA = 62
11419 deg
ZDOT = -2035
334453 TA = 18
25219
MA = 18
23436
Ha = 222
249 n
mi
Hp = 215
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14906360
49 X = -4565518
66
Y = -590297
70 feet Y = -230854
02 meter
Z = 16486205
06 Z = 5002870
43
XDOT = -6464
976784 XDOT = -1880
775309
YDOT = -23388
503945 feet/sec YDOT = -7150
349944 meter/sec
ZDOT = -6677
606473 ZDOT = -2044
688807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3799100
32 X = 1157965
78
Y = -14536156
32 feet Y = -4430620
45 meter
Z = 16389325
42 Z = 4995466
39
XDOT = 23162
462198 XDOT = 7059
918478
YDOT = -1525
958837 feet/sec YDOT = -465
112253 meter/sec
ZDOT = -6717
239780 ZDOT = -2047
414685
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16312
63150987
00016717 00000-0 10270-3 0 9144
2 25544 51
6442 62
6306 0003457 181
0434 179
0712 15
53668652 27291
Satellite: ISS
Catalog Number: 25544
Epoch time: 16312
63150987 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 62
6306 deg
Eccentricity:
0003457
Arg of perigee: 181
0434 deg
Mean anomaly: 179
0712 deg
Mean motion: 15
53668652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 309
Coasting Arc #16 (Orbit 2743)
---------------------------------------
Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5016025
70 A = 6782953
66 meter
Y = 1562951
19 meter E =
0009934
Z = -4300752
31 I = 51
95157
XDOT = 986
032932 Wp = 129
30467
YDOT = 6696
195748 meter/sec RA = 57
14792 deg
ZDOT = 3582
912692 TA = 177
14695
MA = 177
14128
Ha = 222
082 n
mi
Hp = 215
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16456777
22 X = 5019067
07
Y = 5127792
61 feet Y = 1619060
64 meter
Z = -14110079
77 Z = -4276378
03
XDOT = 3235
016180 XDOT = 893
676584
YDOT = 21969
146156 feet/sec YDOT = 6706
705935 meter/sec
ZDOT = 11754
962899 ZDOT = 3587
478148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8300249
39 X = -2529916
01
Y = 15205883
06 feet Y = 4634753
16 meter
Z = -14003610
43 Z = -4268300
46
XDOT = -21051
956501 XDOT = -6416
636341
YDOT = -646
762601 feet/sec YDOT = -197
133241 meter/sec
ZDOT = 11773
691636 ZDOT = 3588
621211
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16313
59634576
00016717 00000-0 10270-3 0 9152
2 25544 51
6429 57
8256 0003479 181
4699 178
6443 15
53671304 27448
Satellite: ISS
Catalog Number: 25544
Epoch time: 16313
59634576 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 57
8256 deg
Eccentricity:
0003479
Arg of perigee: 181
4699 deg
Mean anomaly: 178
6443 deg
Mean motion: 15
53671304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2744
Checksum: 344
Coasting Arc #17 (Orbit 2759)
---------------------------------------
Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5305024
47 A = 6786417
67 meter
Y = -2767292
89 meter E =
0013183
Z = 3186578
30 I = 51
94524
XDOT = 185
059790 Wp = 108
78014
YDOT = -5946
766812 meter/sec RA = 52
18775 deg
ZDOT = -4844
017041 TA = 34
56706
MA = 34
48142
Ha = 222
049 n
mi
Hp = 215
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17404935
93 X = -5289164
88
Y = -9079044
90 feet Y = -2826528
43 meter
Z = 10454653
22 Z = 3160846
06
XDOT = 607
151542 XDOT = 275
074817
YDOT = -19510
389803 feet/sec YDOT = -5944
194241 meter/sec
ZDOT = -15892
444360 ZDOT = -4842
899173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12091107
82 X = 3685369
66
Y = -15540239
40 feet Y = -4736664
97 meter
Z = 10342470
50 Z = 3152385
01
XDOT = 17927
683807 XDOT = 5464
358024
YDOT = 3348
888048 feet/sec YDOT = 1020
741077 meter/sec
ZDOT = -15886
413131 ZDOT = -4842
178722
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16314
62549496
00016717 00000-0 10270-3 0 9164
2 25544 51
6432 52
6992 0003339 187
0414 173
0692 15
53680563 27604
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
62549496 = yrday
fracday
Element set: 916
Inclination: 51
6432 deg
RA of node: 52
6992 deg
Eccentricity:
0003339
Arg of perigee: 187
0414 deg
Mean anomaly: 173
0692 deg
Mean motion: 15
53680563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2760
Checksum: 322
Coasting Arc #18 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5334427
12 A = 6787877
08 meter
Y = -3267068
04 meter E =
0014328
Z = 2614924
79 I = 51
94211
XDOT = 794
812885 Wp = 115
25128
YDOT = -5524
272627 meter/sec RA = 50
58912 deg
ZDOT = -5264
075154 TA = 35
41942
MA = 35
32435
Ha = 222
020 n
mi
Hp = 215
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17501401
30 X = -5310199
84
Y = -10718727
16 feet Y = -3326585
61 meter
Z = 8579149
56 Z = 2589070
04
XDOT = 2607
653823 XDOT = 882
098669
YDOT = -18124
254027 feet/sec YDOT = -5514
896683 meter/sec
ZDOT = -17270
587774 ZDOT = -5260
001837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19843941
81 X = -6048433
46
Y = -5415518
14 feet Y = -1650649
93 meter
Z = 8466528
42 Z = 2580597
86
XDOT = -2820
847011 XDOT = -859
794169
YDOT = -16720
390830 feet/sec YDOT = -5096
375125 meter/sec
ZDOT = -17251
689736 ZDOT = -5258
315032
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16314
94710409
00016717 00000-0 10270-3 0 9174
2 25544 51
6418 51
0980 0003030 186
3845 173
7269 15
53657661 27651
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
94710409 = yrday
fracday
Element set: 917
Inclination: 51
6418 deg
RA of node: 51
0980 deg
Eccentricity:
0003030
Arg of perigee: 186
3845 deg
Mean anomaly: 173
7269 deg
Mean motion: 15
53657661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 319
Coasting Arc #19 (Orbit 2779)
---------------------------------------
Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5284322
98 A = 6790106
36 meter
Y = 4098045
24 meter E =
0006921
Z = -1165132
34 I = 51
92885
XDOT = -2132
794999 Wp = 49
43102
YDOT = 4416
842106 meter/sec RA = 45
63789 deg
ZDOT = 5889
313700 TA = 297
97523
MA = 298
04525
Ha = 221
843 n
mi
Hp = 215
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17337017
66 X = 5243764
67
Y = 13445030
30 feet Y = 4156911
25 meter
Z = -3822612
68 Z = -1139560
64
XDOT = -6997
358921 XDOT = -2210
635054
YDOT = 14490
951791 feet/sec YDOT = 4392
556820 meter/sec
ZDOT = 19321
895342 ZDOT = 5878
763628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20550481
79 X = 6263786
85
Y = 7736703
98 feet Y = 2358147
37 meter
Z = -3711401
17 Z = -1131235
08
XDOT = -1975
215984 XDOT = -602
045832
YDOT = 14448
803858 feet/sec YDOT = 4403
995416 meter/sec
ZDOT = 19274
836196 ZDOT = 5874
970073
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16315
91191945
00016717 00000-0 10270-3 0 9181
2 25544 51
6421 46
2920 0002944 189
9741 170
1353 15
53672882 27806
Satellite: ISS
Catalog Number: 25544
Epoch time: 16315
91191945 = yrday
fracday
Element set: 918
Inclination: 51
6421 deg
RA of node: 46
2920 deg
Eccentricity:
0002944
Arg of perigee: 189
9741 deg
Mean anomaly: 170
1353 deg
Mean motion: 15
53672882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2780
Checksum: 321
Coasting Arc #20 (Orbit 2795)
---------------------------------------
Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893219
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4912539
73 A = 6790544
28 meter
Y = -4658836
73 meter E =
0012983
Z = -420778
94 I = 51
90772
XDOT = 3529
300060 Wp = 148
32409
YDOT = -3186
537607 meter/sec RA = 40
68918 deg
ZDOT = -6017
689549 TA = 36
19649
MA = 36
10869
Ha = 221
729 n
mi
Hp = 215
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16117256
33 X = -4858034
30
Y = -15284897
42 feet Y = -4713467
31 meter
Z = -1380508
33 Z = -444510
79
XDOT = 11579
068438 XDOT = 3593
902467
YDOT = -10454
519709 feet/sec YDOT = -3146
709658 meter/sec
ZDOT = -19743
075947 ZDOT = -6000
387631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20061212
14 X = -6114657
46
Y = -9520857
12 feet Y = -2901957
25 meter
Z = -1483540
24 Z = -452183
07
XDOT = 7182
339656 XDOT = 2189
177127
YDOT = -12114
356319 feet/sec YDOT = -3692
455806 meter/sec
ZDOT = -19666
680436 ZDOT = -5994
404197
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16316
94104704
00016717 00000-0 10270-3 0 9193
2 25544 51
6426 41
1656 0002879 193
9610 166
1463 15
53681174 27966
Satellite: ISS
Catalog Number: 25544
Epoch time: 16316
94104704 = yrday
fracday
Element set: 919
Inclination: 51
6426 deg
RA of node: 41
1656 deg
Eccentricity:
0002879
Arg of perigee: 193
9610 deg
Mean anomaly: 166
1463 deg
Mean motion: 15
53681174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2796
Checksum: 323
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