[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 10th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
011/02:13:29
747 -0
2 4
9 4
9
N/A 4
4 -0
6 221
8
000/00:16:59
494 -2
2 -0
4 213
9
Coasting Arc #1 (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 = -1119331
31 A = 6775035
57 meter
Y = -4340601
01 meter E =
0013325
Z = 5077429
12 I = 51
86462
XDOT = 6413
789923 Wp = 30
34673
YDOT = -3797
627772 meter/sec RA = 138
32252 deg
ZDOT = -1819
287755 TA = 77
27311
MA = 77
12420
Ha = 221
493 n
mi
Hp = 211
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3672346
82 X = -1095374
30
Y = -14240816
97 feet Y = -4352984
61 meter
Z = 16658232
01 Z = 5072049
51
XDOT = 21042
617857 XDOT = 6464
616521
YDOT = -12459
408702 feet/sec YDOT = -3725
620185 meter/sec
ZDOT = -5968
791847 ZDOT = -1788
008188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12561121
63 X = 3828629
87
Y = -7697767
09 feet Y = -2346279
41 meter
Z = 16635693
49 Z = 5070559
38
XDOT = 17412
636207 XDOT = 5307
371516
YDOT = 15714
507250 feet/sec YDOT = 4789
781810 meter/sec
ZDOT = -5832
565735 ZDOT = -1777
766036
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
54515867
00016717 00000-0 10270-3 0 9003
2 25544 51
6413 139
1769 0008776 14
9781 345
1631 15
55285411 19994
Satellite: ISS
Catalog Number: 25544
Epoch time: 16008
54515867 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 139
1769 deg
Eccentricity:
0008776
Arg of perigee: 14
9781 deg
Mean anomaly: 345
1631 deg
Mean motion: 15
55285411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1999
Checksum: 331
Coasting Arc #2 (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 = -678790
10 A = 6778796
64 meter
Y = 5376479
22 meter E =
0011328
Z = -4076305
76 I = 51
90175
XDOT = -6237
804223 Wp = 57
84630
YDOT = 2157
518537 meter/sec RA = 133
33597 deg
ZDOT = 3898
173309 TA = 252
34763
MA = 252
47137
Ha = 221
501 n
mi
Hp = 211
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2227001
65 X = -719060
00
Y = 17639367
51 feet Y = 5368663
71 meter
Z = -13373706
57 Z = -4079700
49
XDOT = -20465
236952 XDOT = -6280
402003
YDOT = 7078
472890 feet/sec YDOT = 2087
524786 meter/sec
ZDOT = 12789
282511 ZDOT = 3867
768589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17458581
26 X = -5321375
57
Y = 3299273
92 feet Y = 1005618
69 meter
Z = -13389383
19 Z = -4081084
00
XDOT = -12727
440284 XDOT = -3879
323799
YDOT = -16166
052791 feet/sec YDOT = -4927
412891 meter/sec
ZDOT = 12657
119597 ZDOT = 3857
890053
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
50894764
00016717 00000-0 10270-3 0 9017
2 25544 51
6422 134
3644 0008831 17
2531 342
8921 15
55319402 20147
Satellite: ISS
Catalog Number: 25544
Epoch time: 16009
50894764 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 134
3644 deg
Eccentricity:
0008831
Arg of perigee: 17
2531 deg
Mean anomaly: 342
8921 deg
Mean motion: 15
55319402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2014
Checksum: 288
Coasting Arc #3 (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 = 2299047
84 A = 6783355
09 meter
Y = -5915828
72 meter E =
0017068
Z = 2387137
38 I = 51
93897
XDOT = 5447
959036 Wp = 75
41296
YDOT = -74
858557 meter/sec RA = 128
36485 deg
ZDOT = -5396
078585 TA = 78
02841
MA = 77
83714
Ha = 221
550 n
mi
Hp = 210
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7542807
87 X = 2353433
68
Y = -19408886
88 feet Y = -5889815
33 meter
Z = 7831815
54 Z = 2398437
12
XDOT = 17873
881352 XDOT = 5474
602722
YDOT = -245
598940 feet/sec YDOT = -13
786526 meter/sec
ZDOT = -17703
669899 ZDOT = -5369
549378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20784340
33 X = 6335066
93
Y = 907548
22 feet Y = 276620
70 meter
Z = 7881860
71 Z = 2402391
14
XDOT = 6040
219411 XDOT = 1841
058877
YDOT = 15452
166076 feet/sec YDOT = 4709
820220 meter/sec
ZDOT = -17588
661989 ZDOT = -5361
024174
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
53697731
00016717 00000-0 10270-3 0 9028
2 25544 51
6427 129
2297 0008818 21
7491 338
4046 15
55342913 20309
Satellite: ISS
Catalog Number: 25544
Epoch time: 16010
53697731 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 129
2297 deg
Eccentricity:
0008818
Arg of perigee: 21
7491 deg
Mean anomaly: 338
4046 deg
Mean motion: 15
55342913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2030
Checksum: 301
Coasting Arc #4 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2016/011/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3602692
29 A = 6776732
34 meter
Y = 2148261
51 meter E =
0016639
Z = -5335948
36 I = 51
91924
XDOT = -4243
208366 Wp = 66
05988
YDOT = 6367
461274 meter/sec RA = 125
41316 deg
ZDOT = -295
510315 TA = 201
09560
MA = 201
16430
Ha = 221
839 n
mi
Hp = 213
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11819856
60 X = 3604321
52
Y = 7048102
07 feet Y = 2188558
63 meter
Z = -17506392
27 Z = -5318443
54
XDOT = -13921
287289 XDOT = -4312
660080
YDOT = 20890
620979 feet/sec YDOT = 6319
622603 meter/sec
ZDOT = -969
522030 ZDOT = -316
290777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5665441
12 X = -1726826
45
Y = -12646150
01 feet Y = -3854546
52 meter
Z = -17430897
57 Z = -5312937
58
XDOT = 22506
500055 XDOT = 6859
981217
YDOT = -8594
221787 feet/sec YDOT = -2619
518801 meter/sec
ZDOT = -1060
752914 ZDOT = -323
317488
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
11524544
00016717 00000-0 10270-3 0 9035
2 25544 51
6431 126
3448 0006181 3
4484 356
6710 15
54355401 20394
Satellite: ISS
Catalog Number: 25544
Epoch time: 16011
11524544 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 126
3448 deg
Eccentricity:
0006181
Arg of perigee: 3
4484 deg
Mean anomaly: 356
6710 deg
Mean motion: 15
54355401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 273
Coasting Arc #5 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2016/012/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2466846
06 A = 6777514
79 meter
Y = -3701945
26 meter E =
0010400
Z = 5111358
50 I = 51
94013
XDOT = 4888
020680 Wp = 28
06752
YDOT = -5653
898927 meter/sec RA = 120
43069 deg
ZDOT = -1725
461686 TA = 78
59135
MA = 78
47455
Ha = 221
888 n
mi
Hp = 213
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8093326
98 X = -2450095
05
Y = -12145489
70 feet Y = -3729437
72 meter
Z = 16769548
90 Z = 5099415
90
XDOT = 16036
813256 XDOT = 4959
262102
YDOT = -18549
537163 feet/sec YDOT = -5598
839441 meter/sec
ZDOT = -5660
963537 ZDOT = -1701
544476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -73389
80 X = -22369
21
Y = 14653357
78 feet Y = 4466343
45 meter
Z = 16718443
45 Z = 5095781
57
XDOT = -22664
559719 XDOT = -6908
157802
YDOT = 6264
688796 feet/sec YDOT = 1909
477145 meter/sec
ZDOT = -5556
249290 ZDOT = -1693
544784
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
14393245
00016717 00000-0 10270-3 0 9042
2 25544 51
6431 121
2148 0006271 5
8278 354
2947 15
54399136 20559
Satellite: ISS
Catalog Number: 25544
Epoch time: 16012
14393245 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 121
2148 deg
Eccentricity:
0006271
Arg of perigee: 5
8278 deg
Mean anomaly: 354
2947 deg
Mean motion: 15
54399136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 295
Coasting Arc #6 (Orbit 2069)
---------------------------------------
Vector Time (GMT): 2016/013/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1351714
07 A = 6780671
78 meter
Y = 5043661
03 meter E =
0009641
Z = -4331544
38 I = 51
96614
XDOT = -5167
429996 Wp = 70
53778
YDOT = 4415
578977 meter/sec RA = 115
45540 deg
ZDOT = 3538
467903 TA = 235
30873
MA = 235
39961
Ha = 222
000 n
mi
Hp = 213
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4434757
44 X = 1316254
60
Y = 16547444
32 feet Y = 5058578
62 meter
Z = -14211103
62 Z = -4325064
21
XDOT = -16953
510485 XDOT = -5233
610121
YDOT = 14486
807666 feet/sec YDOT = 4357
423241 meter/sec
ZDOT = 11609
146663 ZDOT = 3513
205567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5310670
18 X = 1618692
27
Y = -16311147
39 feet Y = -4971637
72 meter
Z = -14183924
22 Z = -4323260
10
XDOT = 20998
113247 XDOT = 6400
224918
YDOT = -3135
302643 feet/sec YDOT = -955
640245 meter/sec
ZDOT = 11498
812634 ZDOT = 3504
838091
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
10831624
00016717 00000-0 10270-3 0 9058
2 25544 51
6432 116
4054 0006325 9
5400 350
5871 15
54381137 20704
Satellite: ISS
Catalog Number: 25544
Epoch time: 16013
10831624 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 116
4054 deg
Eccentricity:
0006325
Arg of perigee: 9
5400 deg
Mean anomaly: 350
5871 deg
Mean motion: 15
54381137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2070
Checksum: 266
Coasting Arc #7 (Orbit 2085)
---------------------------------------
Vector Time (GMT): 2016/014/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -252892
62 A = 6784672
74 meter
Y = -6066549
31 meter E =
0015337
Z = 3020591
03 I = 51
99235
XDOT = 5165
615391 Wp = 72
30921
YDOT = -2707
026541 meter/sec RA = 110
49146 deg
ZDOT = -4979
030697 TA = 73
26858
MA = 73
10032
Ha = 222
074 n
mi
Hp = 213
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -829700
19 X = -199708
71
Y = -19903376
99 feet Y = -6069079
97 meter
Z = 9910075
55 Z = 3019491
69
XDOT = 16947
557057 XDOT = 5219
687770
YDOT = -8881
320674 feet/sec YDOT = -2648
958843 meter/sec
ZDOT = -16335
402550 ZDOT = -4953
806453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9893974
75 X = -3015683
50
Y = 17292037
79 feet Y = 5270613
12 meter
Z = 9906417
52 Z = 3019476
06
XDOT = -17897
689486 XDOT = -5455
215755
YDOT = -897
555130 feet/sec YDOT = -273
574804 meter/sec
ZDOT = -16225
534766 ZDOT = -4945
542997
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
13697858
00016717 00000-0 10270-3 0 9062
2 25544 51
6430 111
2751 0006409 14
2836 345
8497 15
54401521 20866
Satellite: ISS
Catalog Number: 25544
Epoch time: 16014
13697858 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 111
2751 deg
Eccentricity:
0006409
Arg of perigee: 14
2836 deg
Mean anomaly: 345
8497 deg
Mean motion: 15
54401521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2086
Checksum: 302
Coasting Arc #8 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2016/015/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -702221
97 A = 6787636
34 meter
Y = 6597686
73 meter E =
0014786
Z = -1396812
68 I = 52
01265
XDOT = -4927
251746 Wp = 28
67420
YDOT = 703
397617 meter/sec RA = 105
53800 deg
ZDOT = 5837
591731 TA = 316
17369
MA = 316
29092
Ha = 222
113 n
mi
Hp = 213
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2303877
84 X = -769161
69
Y = 21645953
84 feet Y = 6589459
73 meter
Z = -4582718
75 Z = -1400386
47
XDOT = -16165
524101 XDOT = -4963
107320
YDOT = 2307
734964 feet/sec YDOT = 648
097365 meter/sec
ZDOT = 19152
203843 ZDOT = 5813
569534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13207110
70 X = 4025527
34
Y = -17299536
27 feet Y = -5272898
66 meter
Z = -4599429
69 Z = -1401906
17
XDOT = 13848
871168 XDOT = 4221
135932
YDOT = 5541
576622 feet/sec YDOT = 1689
072554 meter/sec
ZDOT = 19047
908379 ZDOT = 5805
802474
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
10133612
00016717 00000-0 10270-3 0 9074
2 25544 51
6429 106
4648 0006454 16
4264 343
7097 15
54423465 21016
Satellite: ISS
Catalog Number: 25544
Epoch time: 16015
10133612 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 106
4648 deg
Eccentricity:
0006454
Arg of perigee: 16
4264 deg
Mean anomaly: 343
7097 deg
Mean motion: 15
54423465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2101
Checksum: 284
Coasting Arc #9 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2016/016/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1580172
97 A = 6788453
44 meter
Y = -6586233
78 meter E =
0010001
Z = -438915
22 I = 52
02254
XDOT = 4506
254290 Wp = 104
03506
YDOT = 1474
615615 meter/sec RA = 100
59171 deg
ZDOT = -6021
277534 TA = 80
67066
MA = 80
55758
Ha = 222
174 n
mi
Hp = 213
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5184294
54 X = 1655836
47
Y = -21608378
53 feet Y = -6568140
18 meter
Z = -1440010
58 Z = -431055
40
XDOT = 14784
298852 XDOT = 4518
678428
YDOT = 4837
977741 feet/sec YDOT = 1525
076982 meter/sec
ZDOT = -19754
847553 ZDOT = -5999
357261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15407165
47 X = -4696104
04
Y = 16016198
70 feet Y = 4881737
36 meter
Z = -1404704
41 Z = -428153
91
XDOT = -9250
544281 XDOT = -2819
565897
YDOT = -10588
576985 feet/sec YDOT = -3227
398265 meter/sec
ZDOT = -19660
065916 ZDOT = -5992
388091
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
12997281
00016717 00000-0 10270-3 0 9088
2 25544 51
6426 101
3343 0006305 20
5581 339
5825 15
54401085 21175
Satellite: ISS
Catalog Number: 25544
Epoch time: 16016
12997281 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 101
3343 deg
Eccentricity:
0006305
Arg of perigee: 20
5581 deg
Mean anomaly: 339
5825 deg
Mean motion: 15
54401085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 287
Coasting Arc #10 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2016/017/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2306974
12 A = 6786353
58 meter
Y = 5983403
11 meter E =
0018888
Z = 2187107
59 I = 52
02059
XDOT = -3976
951104 Wp = 55
92414
YDOT = -3558
813985 meter/sec RA = 95
64260 deg
ZDOT = 5517
554927 TA = 328
25072
MA = 328
36448
Ha = 222
236 n
mi
Hp = 212
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7568812
72 X = -2384334
52
Y = 19630587
62 feet Y = 5957172
43 meter
Z = 7175549
83 Z = 2175713
08
XDOT = -13047
739843 XDOT = -3963
661777
YDOT = -11675
898900 feet/sec YDOT = -3603
212615 meter/sec
ZDOT = 18102
214329 ZDOT = 5498
268237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16268696
21 X = 4958698
60
Y = -13367838
57 feet Y = -4074517
19 meter
Z = 7125014
22 Z = 2171704
33
XDOT = 4765
543557 XDOT = 1452
537676
YDOT = 15445
433640 feet/sec YDOT = 4707
768174 meter/sec
ZDOT = 18019
243607 ZDOT = 5492
265451
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
15859416
00016717 00000-0 10270-3 0 9090
2 25544 51
6421 96
2028 0006508 23
0191 337
1252 15
54465526 21338
Satellite: ISS
Catalog Number: 25544
Epoch time: 16017
15859416 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 96
2028 deg
Eccentricity:
0006508
Arg of perigee: 23
0191 deg
Mean anomaly: 337
1252 deg
Mean motion: 15
54465526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 292
Coasting Arc #11 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2016/018/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2964633
95 A = 6782549
11 meter
Y = -4844097
96 meter E =
0010906
Z = -3721332
52 I = 52
00948
XDOT = 3323
644758 Wp = 50
87333
YDOT = 5364
825731 meter/sec RA = 90
68591 deg
ZDOT = -4337
447656 TA = 173
18737
MA = 173
17254
Ha = 222
244 n
mi
Hp = 212
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9726489
35 X = 3036658
07
Y = -15892709
83 feet Y = -4810542
66 meter
Z = -12209096
18 Z = -3706756
29
XDOT = 10904
346319 XDOT = 3284
476307
YDOT = 17601
134288 feet/sec YDOT = 5401
774017 meter/sec
ZDOT = -14230
471313 ZDOT = -4321
397301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16184788
33 X = -4933123
48
Y = 9316508
92 feet Y = 2839671
92 meter
Z = -12144963
51 Z = -3701784
88
XDOT = -620
310642 XDOT = -189
070684
YDOT = -19531
206703 feet/sec YDOT = -5953
111803 meter/sec
ZDOT = -14161
882527 ZDOT = -4316
541794
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
12291635
00016717 00000-0 10270-3 0 9103
2 25544 51
6414 91
3926 0006487 26
4070 333
7412 15
54465510 21481
Satellite: ISS
Catalog Number: 25544
Epoch time: 16018
12291635 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 91
3926 deg
Eccentricity:
0006487
Arg of perigee: 26
4070 deg
Mean anomaly: 333
7412 deg
Mean motion: 15
54465510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 288
Coasting Arc #12 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2016/019/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3508702
25 A = 6778697
10 meter
Y = 3257666
79 meter E =
0010261
Z = 4789144
69 I = 51
99622
XDOT = -2591
990030 Wp = 77
87705
YDOT = -6715
119800 meter/sec RA = 85
71695 deg
ZDOT = 2666
064653 TA = 345
95434
MA = 345
98286
Ha = 222
526 n
mi
Hp = 212
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11511490
33 X = -3568132
99
Y = 10687883
18 feet Y = 3218097
69 meter
Z = 15712416
97 Z = 4771956
15
XDOT = -8503
904297 XDOT = -2529
657791
YDOT = -22031
232938 feet/sec YDOT = -6743
756726 meter/sec
ZDOT = 8746
931276 ZDOT = 2653
624625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15229934
67 X = 4642084
09
Y = -4141369
67 feet Y = -1262289
48 meter
Z = 15637245
62 Z = 4766232
47
XDOT = -2848
450084 XDOT = -868
207586
YDOT = 22386
770506 feet/sec YDOT = 6823
487650 meter/sec
ZDOT = 8694
267772 ZDOT = 2650
012817
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
15151523
00016717 00000-0 10270-3 0 9119
2 25544 51
6416 86
2612 0006665 30
9105 329
2439 15
54461324 21641
Satellite: ISS
Catalog Number: 25544
Epoch time: 16019
15151523 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 86
2612 deg
Eccentricity:
0006665
Arg of perigee: 30
9105 deg
Mean anomaly: 329
2439 deg
Mean motion: 15
54461324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 284
Coasting Arc #13 (Orbit 2178)
---------------------------------------
Vector Time (GMT): 2016/020/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3981409
93 A = 6776370
34 meter
Y = -1406511
97 meter E =
0019500
Z = -5316316
84 I = 51
98452
XDOT = 1734
665433 Wp = 69
71302
YDOT = 7426
563905 meter/sec RA = 80
73836 deg
ZDOT = -661
102544 TA = 193
96670
MA = 194
02071
Ha = 222
342 n
mi
Hp = 212
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13062368
54 X = 4022666
15
Y = -4614540
57 feet Y = -1361758
27 meter
Z = -17441984
38 Z = -5296876
17
XDOT = 5691
159558 XDOT = 1654
702168
YDOT = 24365
367141 feet/sec YDOT = 7445
515012 meter/sec
ZDOT = -2168
971601 ZDOT = -652
869904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13851620
19 X = -4221973
83
Y = -1730833
98 feet Y = -527558
20 meter
Z = -17357393
46 Z = -5290533
53
XDOT = 5611
416053 XDOT = 1710
359613
YDOT = -23347
417235 feet/sec YDOT = -7116
292773 meter/sec
ZDOT = -2134
705195 ZDOT = -650
658143
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16020
11581248
00016717 00000-0 10270-3 0 9129
2 25544 51
6405 81
4503 0006585 34
2475 325
9102 15
54517482 21796
Satellite: ISS
Catalog Number: 25544
Epoch time: 16020
11581248 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 81
4503 deg
Eccentricity:
0006585
Arg of perigee: 34
2475 deg
Mean anomaly: 325
9102 deg
Mean motion: 15
54517482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2179
Checksum: 289
Coasting Arc #14 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2016/021/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4324026
21 A = 6776885
99 meter
Y = -567064
34 meter E =
0010985
Z = 5182226
27 I = 51
98072
XDOT = -746
870959 Wp = 44
72482
YDOT = -7501
231320 meter/sec RA = 75
75754 deg
ZDOT = -1434
562894 TA = 59
05651
MA = 58
94859
Ha = 222
508 n
mi
Hp = 212
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14186437
70 X = -4342536
50
Y = -1860447
31 feet Y = -615522
23 meter
Z = 17002054
70 Z = 5161176
51
XDOT = -2450
364040 XDOT = -655
966432
YDOT = -24610
338975 feet/sec YDOT = -7509
074972 meter/sec
ZDOT = -4706
571173 ZDOT = -1437
970561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12109591
68 X = 3691003
54
Y = 7820909
39 feet Y = 2383813
18 meter
Z = 16910863
63 Z = 5154431
23
XDOT = -7819
172684 XDOT = -2383
283834
YDOT = 22379
890045 feet/sec YDOT = 6821
390486 meter/sec
ZDOT = -4719
883640 ZDOT = -1438
620533
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16021
14438546
00016717 00000-0 10270-3 0 9136
2 25544 51
6410 76
3196 0006541 37
9543 322
2070 15
54522901 21955
Satellite: ISS
Catalog Number: 25544
Epoch time: 16021
14438546 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 76
3196 deg
Eccentricity:
0006541
Arg of perigee: 37
9543 deg
Mean anomaly: 322
2070 deg
Mean motion: 15
54522901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 285
Coasting Arc #15 (Orbit 2209)
---------------------------------------
Vector Time (GMT): 2016/022/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4523925
53 A = 6779805
73 meter
Y = 2398658
23 meter E =
0013087
Z = -4453885
87 I = 51
98081
XDOT = -368
209847 Wp = 82
59839
YDOT = 6882
433047 meter/sec RA = 70
78032 deg
ZDOT = 3342
590972 TA = 220
98752
MA = 221
08596
Ha = 222
449 n
mi
Hp = 212
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14842275
37 X = 4518401
62
Y = 7869613
62 feet Y = 2449217
10 meter
Z = -14612486
45 Z = -4431923
43
XDOT = -1208
037556 XDOT = -461
380141
YDOT = 22580
160916 feet/sec YDOT = 6877
794369 meter/sec
ZDOT = 10966
505813 ZDOT = 3340
576376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10336934
50 X = -3150697
64
Y = -13346649
81 feet Y = -4068058
86 meter
Z = -14517694
06 Z = -4424993
15
XDOT = 9540
917910 XDOT = 2908
071779
YDOT = -19271
117225 feet/sec YDOT = -5873
836530 meter/sec
ZDOT = 10956
410200 ZDOT = 3339
513829
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16022
10866104
00016717 00000-0 10270-3 0 9149
2 25544 51
6398 71
5082 0006578 42
3957 317
7703 15
54551516 22104
Satellite: ISS
Catalog Number: 25544
Epoch time: 16022
10866104 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 71
5082 deg
Eccentricity:
0006578
Arg of perigee: 42
3957 deg
Mean anomaly: 317
7703 deg
Mean motion: 15
54551516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2210
Checksum: 297
Coasting Arc #16 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2016/023/02:21:59
494
Vector Time (MET): N/A
Weight (LBS) : 922092
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4486382
27 A = 6783865
66 meter
Y = -3994175
67 meter E =
0017852
Z = 3141920
77 I = 51
98362
XDOT = 1627
869421 Wp = 78
36496
YDOT = -5689
299896 meter/sec RA = 65
81431 deg
ZDOT = -4881
199415 TA = 65
59804
MA = 65
41185
Ha = 222
409 n
mi
Hp = 212
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14719101
95 X = -4456646
77
Y = -13104250
90 feet Y = -4044179
23 meter
Z = 10308139
03 Z = 3120199
55
XDOT = 5340
778941 XDOT = 1715
077876
YDOT = -18665
682074 feet/sec YDOT = -5670
608177 meter/sec
ZDOT = -16014
433777 ZDOT = -4873
080204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8341213
92 X = 2542402
00
Y = 17908516
52 feet Y = 5458515
83 meter
Z = 10214708
54 Z = 3113443
16
XDOT = -11123
331831 XDOT = -3390
391542
YDOT = 14345
291144 feet/sec YDOT = 4372
444741 meter/sec
ZDOT = -15978
085997 ZDOT = -4870
120612
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16023
13720784
00016717 00000-0 10270-3 0 9157
2 25544 51
6401 66
3769 0006550 44
4522 315
7156 15
54594365 22260
Satellite: ISS
Catalog Number: 25544
Epoch time: 16023
13720784 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 66
3769 deg
Eccentricity:
0006550
Arg of perigee: 44
4522 deg
Mean anomaly: 315
7156 deg
Mean motion: 15
54594365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2226
Checksum: 301
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