[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 3rd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
011/02:13:29
648 -0
2 4
9 4
9
N/A 4
4 -0
6 221
9
000/00:16:59
296 -2
2 -0
4 214
0
Coasting Arc #1 (Orbit 1890)
---------------------------------------
Vector Time (GMT): 2016/001/13:32:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3831218
94 A = 6778927
15 meter
Y = -3769807
71 meter E =
0013488
Z = 4131046
64 I = 51
67403
XDOT = 6287
659929 Wp = 38
31673
YDOT = 2227
041971 meter/sec RA = 172
87570 deg
ZDOT = -3782
037544 TA = 90
71589
MA = 90
56134
Ha = 220
633 n
mi
Hp = 212
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12569615
94 X = 3853022
27
Y = -12368135
54 feet Y = -3726842
69 meter
Z = 13553302
61 Z = 4149710
59
XDOT = 20628
805540 XDOT = 6280
660791
YDOT = 7306
568146 feet/sec YDOT = 2297
315710 meter/sec
ZDOT = -12408
259658 ZDOT = -3751
510610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17164733
12 X = 5231810
66
Y = 3758094
45 feet Y = 1145467
19 meter
Z = 13634760
58 Z = 4155875
03
XDOT = 5394
624264 XDOT = 1644
281476
YDOT = 20101
698067 feet/sec YDOT = 6126
997571 meter/sec
ZDOT = -12276
469761 ZDOT = -3741
867983
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 16001
60556047
00016717 00000-0 10270-3 0 9008
2 25544 51
6392 173
8287 0008272 347
9072 12
1881 15
55186618 18911
Satellite: ISS
Catalog Number: 25544
Epoch time: 16001
60556047 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 173
8287 deg
Eccentricity:
0008272
Arg of perigee: 347
9072 deg
Mean anomaly: 12
1881 deg
Mean motion: 15
55186618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1891
Checksum: 313
Coasting Arc #2 (Orbit 1905)
---------------------------------------
Vector Time (GMT): 2016/002/13:32:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5387989
24 A = 6783304
87 meter
Y = 3219700
70 meter E =
0011722
Z = -2556855
61 I = 51
72199
XDOT = -4474
531890 Wp = 14
35830
YDOT = -3304
600667 meter/sec RA = 167
88981 deg
ZDOT = 5284
029752 TA = 316
91885
MA = 317
01054
Ha = 220
704 n
mi
Hp = 212
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17677130
05 X = -5411172
15
Y = 10563322
50 feet Y = 3159319
09 meter
Z = -8388633
89 Z = -2583085
38
XDOT = -14680
222737 XDOT = -4462
914066
YDOT = -10841
865706 feet/sec YDOT = -3354
573042 meter/sec
ZDOT = 17336
055617 ZDOT = 5262
321671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18596558
72 X = -5668231
10
Y = -8735263
00 feet Y = -2662508
16 meter
Z = -8502768
46 Z = -2591643
83
XDOT = 110
077164 XDOT = 33
551519
YDOT = -16966
788635 feet/sec YDOT = -5171
477176 meter/sec
ZDOT = 17242
624733 ZDOT = 5255
552019
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 16002
56941713
00016717 00000-0 10270-3 0 9013
2 25544 51
6406 169
0160 0008342 351
6259 8
4754 15
55218639 19064
Satellite: ISS
Catalog Number: 25544
Epoch time: 16002
56941713 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 169
0160 deg
Eccentricity:
0008342
Arg of perigee: 351
6259 deg
Mean anomaly: 8
4754 deg
Mean motion: 15
55218639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1906
Checksum: 301
Coasting Arc #3 (Orbit 1921)
---------------------------------------
Vector Time (GMT): 2016/003/13:32:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6322252
31 A = 6785939
56 meter
Y = -2400444
06 meter E =
0009498
Z = 555126
36 I = 51
76129
XDOT = 2155
846920 Wp = 89
08606
YDOT = 4273
013140 meter/sec RA = 162
91799 deg
ZDOT = -5986
888692 TA = 84
93510
MA = 84
82669
Ha = 220
876 n
mi
Hp = 212
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20742297
61 X = 6345928
21
Y = -7875472
62 feet Y = -2329612
09 meter
Z = 1821280
71 Z = 585895
81
XDOT = 7072
988584 XDOT = 2136
986640
YDOT = 14019
071983 feet/sec YDOT = 4297
016013 meter/sec
ZDOT = -19642
023268 ZDOT = -5976
461741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18317059
61 X = 5583039
77
Y = 12499861
88 feet Y = 3809957
90 meter
Z = 1954948
32 Z = 595868
25
XDOT = -6468
870937 XDOT = -1971
711862
YDOT = 12586
745499 feet/sec YDOT = 3836
440028 meter/sec
ZDOT = -19597
606159 ZDOT = -5973
350357
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 16003
59752299
00016717 00000-0 10270-3 0 9027
2 25544 51
6399 163
8816 0008433 355
1019 5
0050 15
55241835 19223
Satellite: ISS
Catalog Number: 25544
Epoch time: 16003
59752299 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 163
8816 deg
Eccentricity:
0008433
Arg of perigee: 355
1019 deg
Mean anomaly: 5
0050 deg
Mean motion: 15
55241835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1922
Checksum: 304
Coasting Arc #4 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2016/004/13:36:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6155948
46 A = 6782713
97 meter
Y = 97899
34 meter E =
0016905
Z = 2820077
69 I = 51
78241
XDOT = 2263
538145 Wp = 50
88658
YDOT = -5261
401809 meter/sec RA = 157
94716 deg
ZDOT = 5113
659674 TA = 341
12205
MA = 341
18465
Ha = 221
012 n
mi
Hp = 212
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20196681
28 X = -6170284
45
Y = 321192
06 feet Y = 28979
16 meter
Z = 9252223
40 Z = 2790138
69
XDOT = 7426
306250 XDOT = 2297
364139
YDOT = -17261
816958 feet/sec YDOT = -5235
900540 meter/sec
ZDOT = 16777
098668 ZDOT = 5124
737333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12412855
17 X = -3783438
26
Y = -16009782
06 feet Y = -4879781
57 meter
Z = 9122534
84 Z = 2780548
62
XDOT = 17031
367665 XDOT = 5191
160864
YDOT = -3598
210416 feet/sec YDOT = -1096
734535 meter/sec
ZDOT = 16825
992356 ZDOT = 5128
562470
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16004
62561991
00016717 00000-0 10270-3 0 9030
2 25544 51
6413 158
7477 0008354 358
9775 1
1359 15
55275045 19384
Satellite: ISS
Catalog Number: 25544
Epoch time: 16004
62561991 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 158
7477 deg
Eccentricity:
0008354
Arg of perigee: 358
9775 deg
Mean anomaly: 1
1359 deg
Mean motion: 15
55275045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 328
Coasting Arc #5 (Orbit 1952)
---------------------------------------
Vector Time (GMT): 2016/005/13:36:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5055077
65 A = 6778186
27 meter
Y = 1263460
43 meter E =
0014156
Z = -4349401
19 I = 51
79629
XDOT = -4319
206593 Wp = 36
41727
YDOT = 5279
751488 meter/sec RA = 152
96518 deg
ZDOT = -3480
969611 TA = 198
21718
MA = 198
26794
Ha = 221
103 n
mi
Hp = 212
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16584900
44 X = 5061701
23
Y = 4145211
37 feet Y = 1320026
95 meter
Z = -14269688
95 Z = -4324828
62
XDOT = -14170
625305 XDOT = -4361
015942
YDOT = 17322
019316 feet/sec YDOT = 5231
217709 meter/sec
ZDOT = -11420
503972 ZDOT = -3502
052545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6963614
93 X = 2122509
83
Y = 15708913
41 feet Y = 4788076
81 meter
Z = -14163468
12 Z = -4317025
08
XDOT = -21181
486126 XDOT = -6456
116971
YDOT = -1006
354322 feet/sec YDOT = -306
736797 meter/sec
ZDOT = -11512
752772 ZDOT = -3509
087045
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16005
58945503
00016717 00000-0 10270-3 0 9042
2 25544 51
6412 153
9349 0008485 2
2954 357
8236 15
55248497 19534
Satellite: ISS
Catalog Number: 25544
Epoch time: 16005
58945503 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 153
9349 deg
Eccentricity:
0008485
Arg of perigee: 2
2954 deg
Mean anomaly: 357
8236 deg
Mean motion: 15
55248497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1953
Checksum: 330
Coasting Arc #6 (Orbit 1968)
---------------------------------------
Vector Time (GMT): 2016/006/13:36:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3420032
74 A = 6774523
95 meter
Y = -2678644
28 meter E =
0007482
Z = 5193291
10 I = 51
81350
XDOT = 5798
025601 Wp = 36
77047
YDOT = -4852
269864 meter/sec RA = 147
96998 deg
ZDOT = 1320
401463 TA = 40
61417
MA = 40
55838
Ha = 221
226 n
mi
Hp = 211
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11220579
86 X = -3415052
12
Y = -8788203
03 feet Y = -2716861
90 meter
Z = 17038356
62 Z = 5176689
29
XDOT = 19022
393703 XDOT = 5845
439998
YDOT = -15919
520550 feet/sec YDOT = -4787
167500 meter/sec
ZDOT = 4332
025796 ZDOT = 1348
681681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -263391
25 X = -80281
65
Y = -14335072
73 feet Y = -4369330
17 meter
Z = 16966904
14 Z = 5171512
38
XDOT = 23266
903744 XDOT = 7091
752261
YDOT = 4826
883770 feet/sec YDOT = 1471
234173 meter/sec
ZDOT = 4455
398549 ZDOT = 1358
005478
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16006
61753504
00016717 00000-0 10270-3 0 9056
2 25544 51
6419 148
8003 0008567 5
9234 354
2019 15
55305502 19691
Satellite: ISS
Catalog Number: 25544
Epoch time: 16006
61753504 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 148
8003 deg
Eccentricity:
0008567
Arg of perigee: 5
9234 deg
Mean anomaly: 354
2019 deg
Mean motion: 15
55305502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1969
Checksum: 301
Coasting Arc #7 (Orbit 1983)
---------------------------------------
Vector Time (GMT): 2016/007/13:36:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1555044
30 A = 6774257
33 meter
Y = 3999183
17 meter E =
0017128
Z = -5254696
52 I = 51
83959
XDOT = -6515
691882 Wp = 67
60857
YDOT = 3889
956855 meter/sec RA = 142
97168 deg
ZDOT = 1041
369918 TA = 212
29588
MA = 212
40086
Ha = 221
317 n
mi
Hp = 211
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5101851
37 X = 1535733
90
Y = 13120679
69 feet Y = 4016465
18 meter
Z = -17239817
97 Z = -5247189
07
XDOT = -21376
941869 XDOT = -6563
764598
YDOT = 12762
325640 feet/sec YDOT = 3816
825202 meter/sec
ZDOT = 3416
567974 ZDOT = 1009
601912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6735485
53 X = -2052975
99
Y = 12406066
82 feet Y = 3781369
17 meter
Z = -17207997
77 Z = -5244997
72
XDOT = -22602
805563 XDOT = -6889
335136
YDOT = -7765
691233 feet/sec YDOT = -2366
982688 meter/sec
ZDOT = 3278
230819 ZDOT = 999
204754
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16007
58135457
00016717 00000-0 10270-3 0 9065
2 25544 51
6422 143
9882 0008686 10
3147 349
8183 15
55305587 19843
Satellite: ISS
Catalog Number: 25544
Epoch time: 16007
58135457 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 143
9882 deg
Eccentricity:
0008686
Arg of perigee: 10
3147 deg
Mean anomaly: 349
8183 deg
Mean motion: 15
55305587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1984
Checksum: 332
Coasting Arc #8 (Orbit 1999)
---------------------------------------
Vector Time (GMT): 2016/008/13:36:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 384435
54 A = 6777451
33 meter
Y = -5073408
22 meter E =
0015850
Z = 4474660
59 I = 51
87566
XDOT = 6507
276564 Wp = 42
31192
YDOT = -2408
014567 meter/sec RA = 137
97842 deg
ZDOT = -3271
134149 TA = 80
60228
MA = 80
42313
Ha = 221
444 n
mi
Hp = 211
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1261271
47 X = 419403
20
Y = -16645040
10 feet Y = -5068914
09 meter
Z = 14680644
98 Z = 4476612
56
XDOT = 21349
332559 XDOT = 6549
609626
YDOT = -7900
310258 feet/sec YDOT = -2335
008912 meter/sec
ZDOT = -10732
067419 ZDOT = -3239
420965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13358457
78 X = 4071657
93
Y = -9996236
98 feet Y = -3046853
03 meter
Z = 14690008
67 Z = 4477514
64
XDOT = 19250
757278 XDOT = 5867
630818
YDOT = 10069
469210 feet/sec YDOT = 3069
174215 meter/sec
ZDOT = -10594
208478 ZDOT = -3229
114744
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
60942018
00016717 00000-0 10270-3 0 9079
2 25544 51
6427 138
8536 0008749 14
5886 345
5518 15
55285960 20000
Satellite: ISS
Catalog Number: 25544
Epoch time: 16008
60942018 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 138
8536 deg
Eccentricity:
0008749
Arg of perigee: 14
5886 deg
Mean anomaly: 345
5518 deg
Mean motion: 15
55285960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2000
Checksum: 323
Coasting Arc #9 (Orbit 2014)
---------------------------------------
Vector Time (GMT): 2016/009/13:36:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2068151
04 A = 6782023
55 meter
Y = 5700329
39 meter E =
0012006
Z = -3030848
70 I = 51
91476
XDOT = -5816
065460 Wp = 34
88349
YDOT = 523
283278 meter/sec RA = 133
00167 deg
ZDOT = 4972
149930 TA = 290
50442
MA = 290
63324
Ha = 221
525 n
mi
Hp = 211
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6785272
44 X = -2117017
39
Y = 18701868
08 feet Y = 5676928
98 meter
Z = -9943729
34 Z = -3041013
40
XDOT = -19081
579593 XDOT = -5845
637028
YDOT = 1716
808655 feet/sec YDOT = 458
078437 meter/sec
ZDOT = 16312
827853 ZDOT = 4943
825404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18420497
07 X = -5614567
51
Y = 7455641
02 feet Y = 2272479
38 meter
Z = -9988806
22 Z = -3044588
14
XDOT = -13526
325677 XDOT = -4122
824066
YDOT = -11812
833436 feet/sec YDOT = -3600
551631 meter/sec
ZDOT = 16189
972380 ZDOT = 4934
703581
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
57322239
00016717 00000-0 10270-3 0 9084
2 25544 51
6433 134
0409 0008845 16
5548 343
5893 15
55286054 20153
Satellite: ISS
Catalog Number: 25544
Epoch time: 16009
57322239 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 134
0409 deg
Eccentricity:
0008845
Arg of perigee: 16
5548 deg
Mean anomaly: 343
5893 deg
Mean motion: 15
55286054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2015
Checksum: 311
Coasting Arc #10 (Orbit 2030)
---------------------------------------
Vector Time (GMT): 2016/010/13:36:27
741
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3441182
89 A = 6785390
69 meter
Y = -5748751
29 meter E =
0014654
Z = 1063288
71 I = 51
94706
XDOT = 4593
049340 Wp = 87
41716
YDOT = 1642
407962 meter/sec RA = 128
04067 deg
ZDOT = -5914
154656 TA = 81
10156
MA = 80
93569
Ha = 221
601 n
mi
Hp = 211
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11289970
10 X = 3500046
15
Y = -18860732
58 feet Y = -5709940
66 meter
Z = 3488480
01 Z = 1080147
48
XDOT = 15069
059513 XDOT = 4603
070220
YDOT = 5388
477565 feet/sec YDOT = 1693
826914 meter/sec
ZDOT = -19403
394540 ZDOT = -5891
818596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21494723
99 X = 6551591
87
Y = -4543668
98 feet Y = -1384910
31 meter
Z = 3562592
31 Z = 1085878
14
XDOT = 6036
676085 XDOT = 1839
978871
YDOT = 13241
266930 feet/sec YDOT = 4035
938160 meter/sec
ZDOT = -19306
870782 ZDOT = -5884
734214
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
60127123
00016717 00000-0 10270-3 0 9096
2 25544 51
6431 128
9071 0008811 21
5723 338
5800 15
55311493 20318
Satellite: ISS
Catalog Number: 25544
Epoch time: 16010
60127123 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 128
9071 deg
Eccentricity:
0008811
Arg of perigee: 21
5723 deg
Mean anomaly: 338
5800 deg
Mean motion: 15
55311493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2031
Checksum: 268
Coasting Arc #11 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2016/011/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3623793
21 A = 6776852
69 meter
Y = 2116566
24 meter E =
0016588
Z = -5334465
68 I = 51
91917
XDOT = -4220
069087 Wp = 66
05031
YDOT = 6381
105822 meter/sec RA = 125
41027 deg
ZDOT = -329
177013 TA = 200
78526
MA = 200
85279
Ha = 221
867 n
mi
Hp = 214
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11889085
33 X = 3625768
09
Y = 6944114
97 feet Y = 2157101
26 meter
Z = -17501527
82 Z = -5316857
52
XDOT = -13845
371021 XDOT = -4289
511562
YDOT = 20935
386554 feet/sec YDOT = 6333
525962 meter/sec
ZDOT = -1079
977077 ZDOT = -349
845049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5781824
90 X = -1762300
23
Y = -12601358
69 feet Y = -3840894
13 meter
Z = -17425579
44 Z = -5311316
61
XDOT = 22473
229577 XDOT = 6849
840375
YDOT = -8666
203058 feet/sec YDOT = -2641
458692 meter/sec
ZDOT = -1170
723069 ZDOT = -356
836391
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
11530088
00016717 00000-0 10270-3 0 9103
2 25544 51
6431 126
3411 0006095 3
1882 356
9309 15
54316681 20391
Satellite: ISS
Catalog Number: 25544
Epoch time: 16011
11530088 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 126
3411 deg
Eccentricity:
0006095
Arg of perigee: 3
1882 deg
Mean anomaly: 356
9309 deg
Mean motion: 15
54316681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 278
Coasting Arc #12 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2016/012/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2502982
66 A = 6777597
28 meter
Y = -3660174
21 meter E =
0010199
Z = 5123976
20 I = 51
93986
XDOT = 4864
318774 Wp = 27
75969
YDOT = -5688
662269 meter/sec RA = 120
42819 deg
ZDOT = -1677
265726 TA = 78
42167
MA = 78
30719
Ha = 221
926 n
mi
Hp = 213
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8211885
36 X = -2486757
34
Y = -12008445
57 feet Y = -3688073
71 meter
Z = 16810945
53 Z = 5111856
78
XDOT = 15959
051095 XDOT = 4935
716577
YDOT = -18663
590122 feet/sec YDOT = -5633
866961 meter/sec
ZDOT = -5502
840307 ZDOT = -1653
463273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 101802
01 X = 31029
25
Y = 14607157
84 feet Y = 4452261
71 meter
Z = 16759065
97 Z = 5108163
31
XDOT = -22667
252093 XDOT = -6908
978438
YDOT = 6390
169474 feet/sec YDOT = 1947
723656 meter/sec
ZDOT = -5398
617278 ZDOT = -1645
498546
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
14401635
00016717 00000-0 10270-3 0 9113
2 25544 51
6431 121
2113 0006174 5
5118 354
6101 15
54352418 20551
Satellite: ISS
Catalog Number: 25544
Epoch time: 16012
14401635 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 121
2113 deg
Eccentricity:
0006174
Arg of perigee: 5
5118 deg
Mean anomaly: 354
6101 deg
Mean motion: 15
54352418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 248
Coasting Arc #13 (Orbit 2069)
---------------------------------------
Vector Time (GMT): 2016/013/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1404319
26 A = 6780700
96 meter
Y = 4998619
31 meter E =
0009700
Z = -4367232
52 I = 51
96560
XDOT = -5149
308787 Wp = 71
77636
YDOT = 4480
734181 meter/sec RA = 115
45311 deg
ZDOT = 3482
004863 TA = 233
41362
MA = 233
50291
Ha = 222
045 n
mi
Hp = 213
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4607346
66 X = 1369532
90
Y = 16399669
64 feet Y = 5014128
93 meter
Z = -14328190
68 Z = -4360495
17
XDOT = -16894
057699 XDOT = -5215
944572
YDOT = 14700
571459 feet/sec YDOT = 4422
778542 meter/sec
ZDOT = 11423
900469 ZDOT = 3456
829449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5084875
66 X = 1549870
10
Y = -16282846
70 feet Y = -4963011
68 meter
Z = -14299888
06 Z = -4358605
88
XDOT = 21067
007589 XDOT = 6421
223913
YDOT = -3330
421965 feet/sec YDOT = -1015
112615 meter/sec
ZDOT = 11313
931461 ZDOT = 3448
486309
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
10843175
00016717 00000-0 10270-3 0 9120
2 25544 51
6433 116
4021 0006218 9
2034 350
9232 15
54326706 20706
Satellite: ISS
Catalog Number: 25544
Epoch time: 16013
10843175 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 116
4021 deg
Eccentricity:
0006218
Arg of perigee: 9
2034 deg
Mean anomaly: 350
9232 deg
Mean motion: 15
54326706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2070
Checksum: 260
Coasting Arc #14 (Orbit 2085)
---------------------------------------
Vector Time (GMT): 2016/014/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -322575
50 A = 6784677
97 meter
Y = -6029600
09 meter E =
0015250
Z = 3087201
49 I = 51
99168
XDOT = 5160
502837 Wp = 71
56793
YDOT = -2811
030458 meter/sec RA = 110
48913 deg
ZDOT = -4926
427242 TA = 73
13907
MA = 72
97188
Ha = 222
126 n
mi
Hp = 213
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1058318
57 X = -270123
15
Y = -19782152
53 feet Y = -6032914
08 meter
Z = 10128613
80 Z = 3085761
88
XDOT = 16930
783585 XDOT = 5215
483071
YDOT = -9222
540873 feet/sec YDOT = -2753
014856 meter/sec
ZDOT = -16162
819036 ZDOT = -4901
225629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9635030
77 X = -2936757
38
Y = 17312535
32 feet Y = 5276860
76 meter
Z = 10123473
59 Z = 3085634
75
XDOT = -18063
628065 XDOT = -5505
793834
YDOT = -618
891891 feet/sec YDOT = -188
638248 meter/sec
ZDOT = -16053
030370 ZDOT = -4892
963657
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
13713294
00016717 00000-0 10270-3 0 9133
2 25544 51
6430 111
2720 0006300 13
8867 346
2458 15
54340826 20863
Satellite: ISS
Catalog Number: 25544
Epoch time: 16014
13713294 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 111
2720 deg
Eccentricity:
0006300
Arg of perigee: 13
8867 deg
Mean anomaly: 346
2458 deg
Mean motion: 15
54340826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2086
Checksum: 280
Coasting Arc #15 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2016/015/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -617606
44 A = 6787721
45 meter
Y = 6584710
35 meter E =
0014363
Z = -1496374
75 I = 52
01214
XDOT = -4941
561474 Wp = 28
40351
YDOT = 847
886682 meter/sec RA = 105
53558 deg
ZDOT = 5805
691637 TA = 315
33634
MA = 315
45195
Ha = 222
178 n
mi
Hp = 213
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2026267
86 X = -683923
73
Y = 21603380
41 feet Y = 6577433
06 meter
Z = -4909365
97 Z = -1499535
99
XDOT = -16212
472027 XDOT = -4978
876741
YDOT = 2781
780453 feet/sec YDOT = 792
418248 meter/sec
ZDOT = 19047
544742 ZDOT = 5781
596382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12946353
07 X = 3946048
42
Y = -17408533
38 feet Y = -5306120
97 meter
Z = -4924285
61 Z = -1500922
25
XDOT = 14127
051486 XDOT = 4305
925293
YDOT = 5180
115470 feet/sec YDOT = 1578
899195 meter/sec
ZDOT = 18942
905891 ZDOT = 5773
797716
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
10153184
00016717 00000-0 10270-3 0 9148
2 25544 51
6429 106
4621 0006335 15
9894 344
1458 15
54352100 21011
Satellite: ISS
Catalog Number: 25544
Epoch time: 16015
10153184 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 106
4621 deg
Eccentricity:
0006335
Arg of perigee: 15
9894 deg
Mean anomaly: 344
1458 deg
Mean motion: 15
54352100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2101
Checksum: 273
Coasting Arc #16 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2016/016/02:21:59
296
Vector Time (MET): N/A
Weight (LBS) : 922092
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1483731
17 A = 6788720
54 meter
Y = -6615877
56 meter E =
0010296
Z = -310840
65 I = 52
02258
XDOT = 4547
845745 Wp = 104
70683
YDOT = 1295
383842 meter/sec RA = 100
58946 deg
ZDOT = -6031
433214 TA = 78
62390
MA = 78
50826
Ha = 222
248 n
mi
Hp = 213
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4867884
41 X = 1559111
19
Y = -21705635
04 feet Y = -6598864
02 meter
Z = -1019818
39 Z = -303449
99
XDOT = 14920
753756 XDOT = 4562
320337
YDOT = 4249
946987 feet/sec YDOT = 1346
321776 meter/sec
ZDOT = -19788
166711 ZDOT = -6009
305920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15181263
22 X = -4627249
03
Y = 16261208
58 feet Y = 4956416
37 meter
Z = -986541
26 Z = -300697
78
XDOT = -9647
768235 XDOT = -2940
639758
YDOT = -10166
998591 feet/sec YDOT = -3098
901171 meter/sec
ZDOT = -19692
454075 ZDOT = -6002
260002
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
13021777
00016717 00000-0 10270-3 0 9155
2 25544 51
6426 101
3319 0006177 20
2018 339
9378 15
54322873 21171
Satellite: ISS
Catalog Number: 25544
Epoch time: 16016
13021777 = yrday
fracday
Element set: 915
Inclination: 51
6426 deg
RA of node: 101
3319 deg
Eccentricity:
0006177
Arg of perigee: 20
2018 deg
Mean anomaly: 339
9378 deg
Mean motion: 15
54322873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 290
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