[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 15th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
261/10:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 216
1
265/22:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 215
0
267/18:16:53
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 214
7
269/19:33:04
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 214
4
Coasting Arc #1 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2016/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3617888
26 A = 6779064
89 meter
Y = 2655302
77 meter E =
0001512
Z = 5080651
47 I = 51
45650
XDOT = -5834
943550 Wp = 355
64491
YDOT = 4670
392944 meter/sec RA = 331
86300 deg
ZDOT = 1715
635921 TA = 77
74181
MA = 77
72487
Ha = 221
005 n
mi
Hp = 216
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11869712
14 X = 3563247
69
Y = 8711623
28 feet Y = 2695455
49 meter
Z = 16668804
04 Z = 5098093
10
XDOT = -19143
515584 XDOT = -5895
069158
YDOT = 15322
811497 feet/sec YDOT = 4604
806707 meter/sec
ZDOT = 5628
726775 ZDOT = 1687
144900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10619207
94 X = -3236734
58
Y = -10074036
25 feet Y = -3070566
25 meter
Z = 16744482
40 Z = 5103718
24
XDOT = 20160
301600 XDOT = 6144
859928
YDOT = -12112
084542 feet/sec YDOT = -3691
763368 meter/sec
ZDOT = 5503
397447 ZDOT = 1677
435542
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 16258
55114486
00016717 00000-0 10270-3 0 9003
2 25544 51
6445 332
1878 0006179 316
1696 43
8966 15
53857578 18889
Satellite: ISS
Catalog Number: 25544
Epoch time: 16258
55114486 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 332
1878 deg
Eccentricity:
0006179
Arg of perigee: 316
1696 deg
Mean anomaly: 43
8966 deg
Mean motion: 15
53857578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1888
Checksum: 356
Coasting Arc #2 (Orbit 1902)
---------------------------------------
Vector Time (GMT): 2016/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2228141
93 A = 6778230
20 meter
Y = -3597752
36 meter E =
0011871
Z = -5304291
86 I = 51
42471
XDOT = 6453
321281 Wp = 66
67862
YDOT = -4126
120435 meter/sec RA = 326
85356 deg
ZDOT = 92
593996 TA = 204
17940
MA = 204
23517
Ha = 221
308 n
mi
Hp = 216
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7310176
95 X = -2161979
55
Y = -11803649
49 feet Y = -3622299
71 meter
Z = -17402532
34 Z = -5314954
37
XDOT = 21172
313914 XDOT = 6498
531206
YDOT = -13537
140535 feet/sec YDOT = -4053
702274 meter/sec
ZDOT = 303
786077 ZDOT = 124
052758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5929710
75 X = 1807375
84
Y = 12490154
03 feet Y = 3806998
95 meter
Z = -17448425
23 Z = -5318280
01
XDOT = -21553
024344 XDOT = -6569
361820
YDOT = 10827
916832 feet/sec YDOT = 3300
349050 meter/sec
ZDOT = 441
959370 ZDOT = 134
709216
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 16259
51585638
00016717 00000-0 10270-3 0 9012
2 25544 51
6439 327
3817 0006276 321
2591 38
8111 15
53829329 19037
Satellite: ISS
Catalog Number: 25544
Epoch time: 16259
51585638 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 327
3817 deg
Eccentricity:
0006276
Arg of perigee: 321
2591 deg
Mean anomaly: 38
8111 deg
Mean motion: 15
53829329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1903
Checksum: 323
Coasting Arc #3 (Orbit 1918)
---------------------------------------
Vector Time (GMT): 2016/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 776898
27 A = 6779318
27 meter
Y = 4488228
26 meter E =
0008491
Z = 5022565
25 I = 51
40227
XDOT = -6655
211349 Wp = 7
64026
YDOT = 3294
450515 meter/sec RA = 321
84210 deg
ZDOT = -1905
894664 TA = 100
95446
MA = 100
85892
Ha = 221
410 n
mi
Hp = 216
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2548878
84 X = 702254
63
Y = 14725158
33 feet Y = 4496499
42 meter
Z = 16478232
43 Z = 5026157
27
XDOT = -21834
682905 XDOT = -6682
298114
YDOT = 10808
564683 feet/sec YDOT = 3219
875754 meter/sec
ZDOT = -6252
935249 ZDOT = -1938
290179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1152448
22 X = -351266
22
Y = -14883187
67 feet Y = -4536395
60 meter
Z = 16493083
49 Z = 5027091
85
XDOT = 21565
704759 XDOT = 6573
226811
YDOT = -8788
012590 feet/sec YDOT = -2678
586237 meter/sec
ZDOT = -6395
028437 ZDOT = -1949
204668
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 16260
54487297
00016717 00000-0 10270-3 0 9020
2 25544 51
6437 322
2548 0006318 325
2331 34
8408 15
53886475 19190
Satellite: ISS
Catalog Number: 25544
Epoch time: 16260
54487297 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 322
2548 deg
Eccentricity:
0006318
Arg of perigee: 325
2331 deg
Mean anomaly: 34
8408 deg
Mean motion: 15
53886475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1919
Checksum: 324
Coasting Arc #4 (Orbit 1932)
---------------------------------------
Vector Time (GMT): 2016/261/10:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3018432
70 A = 6787537
50 meter
Y = -5531957
62 meter E =
0008889
Z = -2507631
23 I = 51
40554
XDOT = 5524
608627 Wp = 4
41902
YDOT = 624
493809 meter/sec RA = 317
13579 deg
ZDOT = 5282
241562 TA = 327
34881
MA = 327
40374
Ha = 221
611 n
mi
Hp = 216
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9902994
44 X = 3092249
14
Y = -18149467
26 feet Y = -5497791
12 meter
Z = -8227136
57 Z = -2492788
31
XDOT = 18125
356387 XDOT = 5491
555880
YDOT = 2048
864204 feet/sec YDOT = 686
089656 meter/sec
ZDOT = 17330
188853 ZDOT = 5308
998392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16812994
29 X = -5124600
66
Y = 12077860
89 feet Y = 3681332
00 meter
Z = -8161295
00 Z = -2487562
71
XDOT = -14484
354723 XDOT = -4414
831320
YDOT = -8395
877315 feet/sec YDOT = -2559
063406 meter/sec
ZDOT = 17446
919361 ZDOT = 5317
821021
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 16261
44525952
00016717 00000-0 10270-3 0 9032
2 25544 51
6433 317
7684 0006286 328
3647 31
7127 15
53841276 19334
Satellite: ISS
Catalog Number: 25544
Epoch time: 16261
44525952 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 317
7684 deg
Eccentricity:
0006286
Arg of perigee: 328
3647 deg
Mean anomaly: 31
7127 deg
Mean motion: 15
53841276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1933
Checksum: 320
Coasting Arc #5 (Orbit 1948)
---------------------------------------
Vector Time (GMT): 2016/262/10:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3912459
00 A = 6789686
71 meter
Y = 5462778
44 meter E =
0008536
Z = 957909
91 I = 51
38993
XDOT = -4420
245897 Wp = 104
32269
YDOT = -2125
589350 meter/sec RA = 312
14740 deg
ZDOT = -5889
998731 TA = 65
27180
MA = 65
18298
Ha = 221
700 n
mi
Hp = 215
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12836151
57 X = -3977907
54
Y = 17922501
44 feet Y = 5418660
89 meter
Z = 3142749
04 Z = 938744
31
XDOT = -14502
119086 XDOT = -4367
537235
YDOT = -6973
718341 feet/sec YDOT = -2174
725621 meter/sec
ZDOT = -19324
142818 ZDOT = -5911
342986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19145642
74 X = 5835591
91
Y = -10952277
30 feet Y = -3338254
12 meter
Z = 3058055
31 Z = 932095
26
XDOT = 9374
681323 XDOT = 2857
402867
YDOT = 10926
694168 feet/sec YDOT = 3330
456382 meter/sec
ZDOT = -19416
955747 ZDOT = -5918
288112
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 16262
47426479
00016717 00000-0 10270-3 0 9041
2 25544 51
6431 312
6411 0006225 333
4750 26
6083 15
53878166 19498
Satellite: ISS
Catalog Number: 25544
Epoch time: 16262
47426479 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 312
6411 deg
Eccentricity:
0006225
Arg of perigee: 333
4750 deg
Mean anomaly: 26
6083 deg
Mean motion: 15
53878166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1949
Checksum: 313
Coasting Arc #6 (Orbit 1964)
---------------------------------------
Vector Time (GMT): 2016/263/10:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4483835
83 A = 6789936
83 meter
Y = -5042291
53 meter E =
0016198
Z = 660240
90 I = 51
36943
XDOT = 3207
017185 Wp = 29
74731
YDOT = 3636
953891 meter/sec RA = 307
16000 deg
ZDOT = 5947
111039 TA = 337
41389
MA = 337
48510
Ha = 221
905 n
mi
Hp = 215
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14710747
48 X = 4536679
57
Y = -16542951
23 feet Y = -4991854
73 meter
Z = 2166144
68 Z = 682151
44
XDOT = 10521
709923 XDOT = 3137
220704
YDOT = 11932
263422 feet/sec YDOT = 3672
427403 meter/sec
ZDOT = 19511
519157 ZDOT = 5962
520085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20088562
73 X = -6122993
92
Y = 9278856
38 feet Y = 2828195
42 meter
Z = 2262737
61 Z = 689682
42
XDOT = -4073
981646 XDOT = -1241
749606
YDOT = -13631
904559 feet/sec YDOT = -4155
004510 meter/sec
ZDOT = 19578
137537 ZDOT = 5967
416321
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 16263
50326416
00016717 00000-0 10270-3 0 9057
2 25544 51
6429 307
5132 0006410 338
6693 21
4191 15
53852472 19650
Satellite: ISS
Catalog Number: 25544
Epoch time: 16263
50326416 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 307
5132 deg
Eccentricity:
0006410
Arg of perigee: 338
6693 deg
Mean anomaly: 21
4191 deg
Mean motion: 15
53852472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1965
Checksum: 301
Coasting Arc #7 (Orbit 1979)
---------------------------------------
Vector Time (GMT): 2016/264/10:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4793289
48 A = 6787820
65 meter
Y = 4254735
95 meter E =
0002787
Z = -2240302
16 I = 51
34310
XDOT = -1948
606111 Wp = 52
17448
YDOT = -5048
946342 meter/sec RA = 302
16970 deg
ZDOT = -5422
627228 TA = 152
82088
MA = 152
80629
Ha = 221
975 n
mi
Hp = 215
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15726015
34 X = -4829628
22
Y = 13959107
45 feet Y = 4200930
75 meter
Z = -7350072
70 Z = -2263675
73
XDOT = -6393
064670 XDOT = -1865
661608
YDOT = -16564
784587 feet/sec YDOT = -5070
273774 meter/sec
ZDOT = -17790
771746 ZDOT = -5431
891164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19838939
29 X = 6046908
70
Y = -6859922
22 feet Y = -2090904
29 meter
Z = -7452902
99 Z = -2271644
83
XDOT = -1072
315827 XDOT = -326
841864
YDOT = 16260
041651 feet/sec YDOT = 4956
060695 meter/sec
ZDOT = -17830
303251 ZDOT = -5434
676431
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 16264
46794482
00016717 00000-0 10270-3 0 9066
2 25544 51
6418 302
7066 0006268 342
3853 17
7081 15
53894248 19802
Satellite: ISS
Catalog Number: 25544
Epoch time: 16264
46794482 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 302
7066 deg
Eccentricity:
0006268
Arg of perigee: 342
3853 deg
Mean anomaly: 17
7081 deg
Mean motion: 15
53894248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1980
Checksum: 332
Coasting Arc #8 (Orbit 1995)
---------------------------------------
Vector Time (GMT): 2016/265/10:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4830057
01 A = 6784402
12 meter
Y = -3117432
17 meter E =
0011616
Z = 3588836
77 I = 51
31574
XDOT = 755
623154 Wp = 62
59033
YDOT = 6241
633225 meter/sec RA = 297
16984 deg
ZDOT = 4399
100666 TA = 340
12857
MA = 340
17378
Ha = 221
926 n
mi
Hp = 215
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15846643
75 X = 4847124
75
Y = -10227795
83 feet Y = -3063323
48 meter
Z = 11774398
84 Z = 3612341
94
XDOT = 2479
078590 XDOT = 664
402313
YDOT = 20477
799293 feet/sec YDOT = 6249
573457 meter/sec
ZDOT = 14432
744968 ZDOT = 4402
549206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18428640
88 X = -5617049
74
Y = 3697076
33 feet Y = 1126868
87 meter
Z = 11877593
00 Z = 3620290
35
XDOT = 5596
973323 XDOT = 1705
957469
YDOT = -18573
563539 feet/sec YDOT = -5661
222167 meter/sec
ZDOT = 14446
674016 ZDOT = 4403
346240
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 16265
49693122
00016717 00000-0 10270-3 0 9070
2 25544 51
6420 297
5785 0006303 345
7124 14
3849 15
53909447 19962
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
49693122 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 297
5785 deg
Eccentricity:
0006303
Arg of perigee: 345
7124 deg
Mean anomaly: 14
3849 deg
Mean motion: 15
53909447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1996
Checksum: 336
Coasting Arc #9 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2889029
25 A = 6778941
95 meter
Y = -3455430
46 meter E =
0012032
Z = -5075366
59 I = 51
29211
XDOT = 4307
116683 Wp = 72
65843
YDOT = -6100
235258 meter/sec RA = 294
66046 deg
ZDOT = 1708
345448 TA = 213
90867
MA = 213
98565
Ha = 222
145 n
mi
Hp = 214
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9478442
42 X = -2825520
86
Y = -11336714
10 feet Y = -3487382
84 meter
Z = -16651465
21 Z = -5089246
36
XDOT = 14130
960247 XDOT = 4366
712469
YDOT = -20013
895205 feet/sec YDOT = -6051
736832 meter/sec
ZDOT = 5604
807900 ZDOT = 1729
413783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4101205
41 X = -1250047
41
Y = -14125895
88 feet Y = -4305573
06 meter
Z = -16711446
09 Z = -5093648
77
XDOT = 19849
485248 XDOT = 6050
123104
YDOT = -12477
154197 feet/sec YDOT = -3803
036599 meter/sec
ZDOT = 5697
897894 ZDOT = 1736
719278
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 16265
94711120
00016717 00000-0 10270-3 0 9080
2 25544 51
6438 295
3374 0006714 347
3542 12
7441 15
53923827 20037
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
94711120 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 295
3374 deg
Eccentricity:
0006714
Arg of perigee: 347
3542 deg
Mean anomaly: 12
7441 deg
Mean motion: 15
53923827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 301
Coasting Arc #10 (Orbit 2018)
---------------------------------------
Vector Time (GMT): 2016/266/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1992370
89 A = 6781727
12 meter
Y = 4800907
24 meter E =
0012663
Z = 4354910
07 I = 51
28889
XDOT = -4683
582556 Wp = 38
63982
YDOT = 5034
308807 meter/sec RA = 289
64354 deg
ZDOT = -3392
066826 TA = 85
97171
MA = 85
82697
Ha = 222
269 n
mi
Hp = 214
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6536649
89 X = 1917383
44
Y = 15751008
00 feet Y = 4822768
31 meter
Z = 14287762
68 Z = 4364406
07
XDOT = -15366
084500 XDOT = -4723
052085
YDOT = 16516
761179 feet/sec YDOT = 4981
712908 meter/sec
ZDOT = -11128
828170 ZDOT = -3414
914873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -43959
20 X = -13398
76
Y = 17019346
25 feet Y = 5187496
74 meter
Z = 14328367
94 Z = 4367286
55
XDOT = -19191
851984 XDOT = -5849
676485
YDOT = 9445
926455 feet/sec YDOT = 2879
118384 meter/sec
ZDOT = -11229
491397 ZDOT = -3422
748978
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 16266
97608772
00016717 00000-0 10270-3 0 9093
2 25544 51
6435 290
2096 0006864 351
0512 9
0517 15
53962645 20195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16266
97608772 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 290
2096 deg
Eccentricity:
0006864
Arg of perigee: 351
0512 deg
Mean anomaly: 9
0517 deg
Mean motion: 15
53962645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 322
Coasting Arc #11 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2016/267/18:16:53
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4375004
97 A = 6778362
70 meter
Y = -262984
54 meter E =
0005084
Z = 5167556
51 I = 51
26767
XDOT = -1034
056086 Wp = 32
32007
YDOT = 7495
893194 meter/sec RA = 285
53322 deg
ZDOT = 1260
588252 TA = 45
53991
MA = 45
49834
Ha = 222
200 n
mi
Hp = 214
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14353690
86 X = 4352518
73
Y = -862810
16 feet Y = -214185
64 meter
Z = 16953925
56 Z = 5188754
65
XDOT = -3392
572462 XDOT = -1123
923631
YDOT = 24592
825438 feet/sec YDOT = 7483
827300 meter/sec
ZDOT = 4135
788229 ZDOT = 1255
346214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2441154
21 X = 744063
80
Y = 14059336
02 feet Y = 4285285
62 meter
Z = 17046533
70 Z = 5195783
47
XDOT = -23795
724203 XDOT = -7252
936737
YDOT = -839
016663 feet/sec YDOT = -255
732279 meter/sec
ZDOT = 4111
570150 ZDOT = 1253
206582
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 16267
81212963
00016717 00000-0 10270-3 0 9102
2 25544 51
6419 286
0433 0006663 354
2920 5
8155 15
53956321 20321
Satellite: ISS
Catalog Number: 25544
Epoch time: 16267
81212963 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 286
0433 deg
Eccentricity:
0006663
Arg of perigee: 354
2920 deg
Mean anomaly: 5
8155 deg
Mean motion: 15
53956321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 297
Coasting Arc #12 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2016/268/18:16:53
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4035223
58 A = 6778041
22 meter
Y = -1423666
44 meter E =
0015522
Z = -5268731
21 I = 51
25928
XDOT = 1854
042086 Wp = 68
98782
YDOT = -7406
831809 meter/sec RA = 280
50906 deg
ZDOT = 588
299085 TA = 206
62456
MA = 206
70435
Ha = 222
479 n
mi
Hp = 214
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13238922
50 X = -3993410
65
Y = -4670821
65 feet Y = -1468557
66 meter
Z = -17285863
53 Z = -5288231
63
XDOT = 6082
815244 XDOT = 1933
871664
YDOT = -24300
629293 feet/sec YDOT = -7385
652265 meter/sec
ZDOT = 1930
115107 ZDOT = 597
500062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2948619
71 X = 898739
29
Y = -13617961
74 feet Y = -4150754
74 meter
Z = -17370765
15 Z = -5294609
22
XDOT = 23885
594410 XDOT = 7280
329176
YDOT = 2685
514127 feet/sec YDOT = 818
544706 meter/sec
ZDOT = 1971
589976 ZDOT = 600
940625
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 16268
77678820
00016717 00000-0 10270-3 0 9117
2 25544 51
6425 281
2359 0006730 358
8252 1
2884 15
53933571 20472
Satellite: ISS
Catalog Number: 25544
Epoch time: 16268
77678820 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 281
2359 deg
Eccentricity:
0006730
Arg of perigee: 358
8252 deg
Mean anomaly: 1
2884 deg
Mean motion: 15
53933571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 323
Coasting Arc #13 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2016/269/18:16:53
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3604101
49 A = 6779815
52 meter
Y = 3088376
12 meter E =
0012132
Z = 4839757
79 I = 51
26019
XDOT = -2589
916594 Wp = 31
42128
YDOT = 6806
898069 meter/sec RA = 275
48708 deg
ZDOT = -2402
072423 TA = 82
32404
MA = 82
18629
Ha = 222
560 n
mi
Hp = 214
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11824479
95 X = 3545789
20
Y = 10132467
59 feet Y = 3128354
02 meter
Z = 15878470
45 Z = 4857123
65
XDOT = -8497
101686 XDOT = -2654
172362
YDOT = 22332
342746 feet/sec YDOT = 6777
576380 meter/sec
ZDOT = -7880
815035 ZDOT = -2414
810282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8321753
10 X = -2536470
34
Y = 13070452
67 feet Y = 3983873
98 meter
Z = 15953768
88 Z = 4862708
76
XDOT = -22369
297008 XDOT = -6818
161728
YDOT = -4502
082066 feet/sec YDOT = -1372
234614 meter/sec
ZDOT = -7937
614929 ZDOT = -2419
385030
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 16269
80574861
00016717 00000-0 10270-3 0 9123
2 25544 51
6423 276
1089 0006822 2
9497 357
1694 15
53950526 20632
Satellite: ISS
Catalog Number: 25544
Epoch time: 16269
80574861 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 276
1089 deg
Eccentricity:
0006822
Arg of perigee: 2
9497 deg
Mean anomaly: 357
1694 deg
Mean motion: 15
53950526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 329
Coasting Arc #14 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2016/269/19:33:04
000
Vector Time (MET): N/A
Weight (LBS) : 908286
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3624035
02 A = 6782901
54 meter
Y = -4060682
88 meter E =
0011708
Z = 4035136
61 I = 51
27147
XDOT = 2548
918848 Wp = 67
34660
YDOT = 6120
376423 meter/sec RA = 275
26595 deg
ZDOT = 3865
339035 TA = 342
42056
MA = 342
46105
Ha = 222
548 n
mi
Hp = 214
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11889878
67 X = 3649572
34
Y = -13322450
40 feet Y = -4020013
31 meter
Z = 13238637
18 Z = 4052803
65
XDOT = 8362
594647 XDOT = 2461
513686
YDOT = 20079
975140 feet/sec YDOT = 6148
391804 meter/sec
ZDOT = 12681
558515 ZDOT = 3877
508132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17263476
28 X = 5261907
57
Y = 4331511
29 feet Y = 1320244
64 meter
Z = 13316486
41 Z = 4058865
06
XDOT = -13684
747471 XDOT = -4171
111029
YDOT = 15348
286749 feet/sec YDOT = 4678
157801 meter/sec
ZDOT = 12733
640521 ZDOT = 3881
213631
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 16269
87005865
00016717 00000-0 10270-3 0 9134
2 25544 51
6436 275
7880 0006801 3
4370 356
6828 15
53932075 20646
Satellite: ISS
Catalog Number: 25544
Epoch time: 16269
87005865 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 275
7880 deg
Eccentricity:
0006801
Arg of perigee: 3
4370 deg
Mean anomaly: 356
6828 deg
Mean motion: 15
53932075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 324
Coasting Arc #15 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2016/270/19:33:04
000
Vector Time (MET): N/A
Weight (LBS) : 908286
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3942895
98 A = 6779538
44 meter
Y = 2558423
84 meter E =
0016083
Z = -4900140
77 I = 51
25781
XDOT = -1784
364401 Wp = 50
35101
YDOT = -7093
068553 meter/sec RA = 270
25031 deg
ZDOT = -2262
492615 TA = 197
35684
MA = 197
41188
Ha = 222
681 n
mi
Hp = 214
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12936010
42 X = -3947409
16
Y = 8393779
00 feet Y = 2514305
95 meter
Z = -16076577
33 Z = -4919305
58
XDOT = -5854
213913 XDOT = -1693
925094
YDOT = -23271
222288 feet/sec YDOT = -7112
517090 meter/sec
ZDOT = -7422
876033 ZDOT = -2270
940128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13491059
89 X = -4112075
06
Y = -7285272
97 feet Y = -2220551
20 meter
Z = -16160703
30 Z = -4925782
37
XDOT = 17165
731020 XDOT = 5232
114815
YDOT = -15205
949841 feet/sec YDOT = -4634
773511 meter/sec
ZDOT = -7458
556940 ZDOT = -2273
368155
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 16270
83470243
00016717 00000-0 10270-3 0 9149
2 25544 51
6428 270
9816 0006825 6
0686 354
0549 15
53969655 20790
Satellite: ISS
Catalog Number: 25544
Epoch time: 16270
83470243 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 270
9816 deg
Eccentricity:
0006825
Arg of perigee: 6
0686 deg
Mean anomaly: 354
0549 deg
Mean motion: 15
53969655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 333
Coasting Arc #16 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2016/271/19:33:04
000
Vector Time (MET): N/A
Weight (LBS) : 908286
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4173152
33 A = 6777843
76 meter
Y = -845649
84 meter E =
0006775
Z = 5269912
18 I = 51
25332
XDOT = 989
192704 Wp = 32
10422
YDOT = 7594
983205 meter/sec RA = 265
22659 deg
ZDOT = 440
806773 TA = 53
70215
MA = 53
63960
Ha = 222
576 n
mi
Hp = 214
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13691444
66 X = 4156699
50
Y = -2774441
74 feet Y = -799074
18 meter
Z = 17289738
13 Z = 5290144
44
XDOT = 3245
382888 XDOT = 902
048902
YDOT = 24917
923902 feet/sec YDOT = 7605
557828 meter/sec
ZDOT = 1446
216447 ZDOT = 445
399390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9087425
56 X = 2769847
31
Y = 10464412
30 feet Y = 3189552
87 meter
Z = 17378233
53 Z = 5296885
58
XDOT = -19349
393328 XDOT = -5897
695086
YDOT = 14399
515764 feet/sec YDOT = 4388
972405 meter/sec
ZDOT = 1464
996840 ZDOT = 446
531037
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 16271
86365042
00016717 00000-0 10270-3 0 9154
2 25544 51
6430 265
8536 0006714 9
3053 350
8223 15
53978767 20951
Satellite: ISS
Catalog Number: 25544
Epoch time: 16271
86365042 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 265
8536 deg
Eccentricity:
0006714
Arg of perigee: 9
3053 deg
Mean anomaly: 350
8223 deg
Mean motion: 15
53978767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2095
Checksum: 319
Coasting Arc #17 (Orbit 2109)
---------------------------------------
Vector Time (GMT): 2016/272/19:33:04
000
Vector Time (MET): N/A
Weight (LBS) : 908286
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4340233
23 A = 6778423
82 meter
Y = -879215
07 meter E =
0015612
Z = -5144129
53 I = 51
25888
XDOT = -145
930006 Wp = 74
81744
YDOT = -7524
310677 meter/sec RA = 260
20143 deg
ZDOT = 1416
776451 TA = 208
86039
MA = 208
94683
Ha = 222
774 n
mi
Hp = 213
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14239610
32 X = -4305091
03
Y = -2884563
88 feet Y = -927554
70 meter
Z = -16877065
40 Z = -5165127
85
XDOT = -478
772986 XDOT = -68
662505
YDOT = -24686
058651 feet/sec YDOT = -7525
510338 meter/sec
ZDOT = 4648
216702 ZDOT = 1416
256282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4664803
68 X = -1421832
16
Y = -13646541
07 feet Y = -4159465
72 meter
Z = -16968620
18 Z = -5172035
43
XDOT = 20035
523375 XDOT = 6106
827525
YDOT = -12596
305855 feet/sec YDOT = -3839
354025 meter/sec
ZDOT = 4647
191383 ZDOT = 1416
463934
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 16272
82828287
00016717 00000-0 10270-3 0 9167
2 25544 51
6429 261
0458 0006852 12
4060 347
7260 15
53988164 21102
Satellite: ISS
Catalog Number: 25544
Epoch time: 16272
82828287 = yrday
fracday
Element set: 916
Inclination: 51
6429 deg
RA of node: 261
0458 deg
Eccentricity:
0006852
Arg of perigee: 12
4060 deg
Mean anomaly: 347
7260 deg
Mean motion: 15
53988164 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2110
Checksum: 313
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