[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 20th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 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
265/22:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 215
0
278/01:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 213
3
Coasting Arc #1 (Orbit 1964)
---------------------------------------
Vector Time (GMT): 2016/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2775657
22 A = 6788889
09 meter
Y = -5953296
88 meter E =
0012363
Z = -1686511
49 I = 51
36392
XDOT = 5095
868529 Wp = 11
43321
YDOT = 771
859414 meter/sec RA = 306
83970 deg
ZDOT = 5681
192030 TA = 330
00233
MA = 330
07310
Ha = 221
938 n
mi
Hp = 215
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9106486
96 X = 2850214
64
Y = -19531813
92 feet Y = -5921840
96 meter
Z = -5533174
17 Z = -1672846
07
XDOT = 16718
728771 XDOT = 5059
261608
YDOT = 2532
347158 feet/sec YDOT = 828
640862 meter/sec
ZDOT = 18639
081462 ZDOT = 5705
857709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9828735
81 X = -2995798
67
Y = 19195949
50 feet Y = 5850925
41 meter
Z = -5472417
34 Z = -1667992
80
XDOT = -15097
732247 XDOT = -4601
788789
YDOT = -2404
043908 feet/sec YDOT = -732
752583 meter/sec
ZDOT = 18746
641898 ZDOT = 5713
976450
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
50326586
00016717 00000-0 10270-3 0 9000
2 25544 51
6420 307
5138 0006396 339
2539 20
8353 15
53873653 19653
Satellite: ISS
Catalog Number: 25544
Epoch time: 16263
50326586 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 307
5138 deg
Eccentricity:
0006396
Arg of perigee: 339
2539 deg
Mean anomaly: 20
8353 deg
Mean motion: 15
53873653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1965
Checksum: 317
Coasting Arc #2 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2016/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3539287
10 A = 6789975
37 meter
Y = 5792324
50 meter E =
0007330
Z = 62831
97 I = 51
34949
XDOT = -4116
218017 Wp = 108
49505
YDOT = -2443
999406 meter/sec RA = 301
85034 deg
ZDOT = -5984
666249 TA = 70
82588
MA = 70
74655
Ha = 222
025 n
mi
Hp = 215
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11611834
31 X = -3604100
51
Y = 19003689
32 feet Y = 5752383
44 meter
Z = 206141
64 Z = 45480
77
XDOT = -13504
652286 XDOT = -4059
511417
YDOT = -8018
370755 feet/sec YDOT = -2489
713286 meter/sec
ZDOT = -19634
731787 ZDOT = -6004
524026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11957853
88 X = 3644753
86
Y = -18788571
07 feet Y = -5726756
46 meter
Z = 129327
96 Z = 39419
16
XDOT = 11858
626786 XDOT = 3614
509444
YDOT = 7390
962718 feet/sec YDOT = 2252
765437 meter/sec
ZDOT = -19720
993123 ZDOT = -6010
958704
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
53226248
00016717 00000-0 10270-3 0 9019
2 25544 51
6421 302
3860 0006380 343
6254 16
4692 15
53904398 19811
Satellite: ISS
Catalog Number: 25544
Epoch time: 16264
53226248 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 302
3860 deg
Eccentricity:
0006380
Arg of perigee: 343
6254 deg
Mean anomaly: 16
4692 deg
Mean motion: 15
53904398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1981
Checksum: 304
Coasting Arc #3 (Orbit 1996)
---------------------------------------
Vector Time (GMT): 2016/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030396
66 A = 6789060
04 meter
Y = -5227645
80 meter E =
0016926
Z = 1541527
57 I = 51
32963
XDOT = 3079
318926 Wp = 40
76890
YDOT = 4070
753429 meter/sec RA = 296
85972 deg
ZDOT = 5730
715059 TA = 336
16531
MA = 336
24359
Ha = 222
218 n
mi
Hp = 215
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13223086
16 X = 4081065
83
Y = -17151068
89 feet Y = -5182291
76 meter
Z = 5057505
15 Z = 1561229
95
XDOT = 10102
752382 XDOT = 3005
732241
YDOT = 13355
490252 feet/sec YDOT = 4104
777497 meter/sec
ZDOT = 18801
558592 ZDOT = 5745
494671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13208106
60 X = -4025830
89
Y = 17136738
72 feet Y = 5223277
96 meter
Z = 5144476
27 Z = 1568036
37
XDOT = -8717
205907 XDOT = -2657
004361
YDOT = -12404
492424 feet/sec YDOT = -3780
889291 meter/sec
ZDOT = 18865
355167 ZDOT = 5750
160255
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
56125491
00016717 00000-0 10270-3 0 9022
2 25544 51
6418 297
2582 0006511 349
1450 10
9561 15
53864632 19972
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
56125491 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 297
2582 deg
Eccentricity:
0006511
Arg of perigee: 349
1450 deg
Mean anomaly: 10
9561 deg
Mean motion: 15
53864632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1997
Checksum: 318
Coasting Arc #4 (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 = -2893390
44 A = 6778953
36 meter
Y = -3449341
07 meter E =
0012043
Z = -5077050
16 I = 51
29166
XDOT = 4303
413024 Wp = 72
61564
YDOT = -6104
638662 meter/sec RA = 294
66020 deg
ZDOT = 1701
867475 TA = 213
88681
MA = 213
96381
Ha = 222
155 n
mi
Hp = 214
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9492750
79 X = -2829941
64
Y = -11316735
80 feet Y = -3481342
56 meter
Z = -16656988
72 Z = -5090951
26
XDOT = 14118
809135 XDOT = 4363
089793
YDOT = -20028
342066 feet/sec YDOT = -6056
181199 meter/sec
ZDOT = 5583
554708 ZDOT = 1722
918016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4122234
17 X = -1256456
97
Y = -14113222
94 feet Y = -4301710
35 meter
Z = -16717063
85 Z = -5095361
06
XDOT = 19845
116847 XDOT = 6048
791615
YDOT = -12493
650610 feet/sec YDOT = -3808
064706 meter/sec
ZDOT = 5676
567799 ZDOT = 1730
217865
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
94712279
00016717 00000-0 10270-3 0 9031
2 25544 51
6434 295
3371 0006719 347
3179 12
7804 15
53917397 20039
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
94712279 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 295
3371 deg
Eccentricity:
0006719
Arg of perigee: 347
3179 deg
Mean anomaly: 12
7804 deg
Mean motion: 15
53917397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 324
Coasting Arc #5 (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 = 1998841
33 A = 6781729
87 meter
Y = 4794033
85 meter E =
0012656
Z = 4359532
79 I = 51
28841
XDOT = -4680
079253 Wp = 38
49330
YDOT = 5042
692249 meter/sec RA = 289
64326 deg
ZDOT = -3384
414413 TA = 86
02959
MA = 85
88493
Ha = 222
280 n
mi
Hp = 214
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6557878
39 X = 1923907
81
Y = 15728457
50 feet Y = 4815967
58 meter
Z = 14302929
11 Z = 4369060
36
XDOT = -15354
590726 XDOT = -4719
679961
YDOT = 16544
265910 feet/sec YDOT = 4990
134793 meter/sec
ZDOT = -11103
721829 ZDOT = -3407
245761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15831
52 X = -4825
45
Y = 17006548
96 feet Y = 5183596
12 meter
Z = 14343673
42 Z = 4371951
66
XDOT = -19192
789526 XDOT = -5849
962248
YDOT = 9473
624738 feet/sec YDOT = 2887
560820 meter/sec
ZDOT = -11204
313640 ZDOT = -3415
074798
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
97610371
00016717 00000-0 10270-3 0 9046
2 25544 51
6431 290
2093 0006870 351
0088 9
0940 15
53955767 20190
Satellite: ISS
Catalog Number: 25544
Epoch time: 16266
97610371 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 290
2093 deg
Eccentricity:
0006870
Arg of perigee: 351
0088 deg
Mean anomaly: 9
0940 deg
Mean motion: 15
53955767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2019
Checksum: 310
Coasting Arc #6 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2016/267/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1167058
53 A = 6785446
91 meter
Y = -5838613
27 meter E =
0008304
Z = -3249546
54 I = 51
28949
XDOT = 4852
322962 Wp = 27
99587
YDOT = -3593
070615 meter/sec RA = 284
63475 deg
ZDOT = 4725
275670 TA = 294
12963
MA = 294
21645
Ha = 222
391 n
mi
Hp = 214
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3828932
17 X = -1085897
99
Y = -19155555
36 feet Y = -5851210
55 meter
Z = -10661241
92 Z = -3255018
26
XDOT = 15919
694757 XDOT = 4869
187545
YDOT = -11788
289418 feet/sec YDOT = -3538
714034 meter/sec
ZDOT = 15502
872932 ZDOT = 4748
888329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3492886
28 X = 1064631
74
Y = -19206973
41 feet Y = -5854285
50 meter
Z = -10684101
25 Z = -3256514
06
XDOT = 17629
599660 XDOT = 5373
501976
YDOT = -5453
247140 feet/sec YDOT = -1662
149728 meter/sec
ZDOT = 15606
613537 ZDOT = 4756
895806
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
94077115
00016717 00000-0 10270-3 0 9058
2 25544 51
6421 285
4023 0006762 354
3482 5
7593 15
53915749 20342
Satellite: ISS
Catalog Number: 25544
Epoch time: 16267
94077115 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 285
4023 deg
Eccentricity:
0006762
Arg of perigee: 354
3482 deg
Mean anomaly: 5
7593 deg
Mean motion: 15
53915749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2034
Checksum: 314
Coasting Arc #7 (Orbit 2049)
---------------------------------------
Vector Time (GMT): 2016/268/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 346670
04 A = 6788509
18 meter
Y = 6536345
01 meter E =
0012537
Z = 1791710
00 I = 51
29342
XDOT = -4880
550179 Wp = 85
02435
YDOT = 1810
768079 meter/sec RA = 279
63494 deg
ZDOT = -5626
375635 TA = 75
20057
MA = 75
06171
Ha = 222
534 n
mi
Hp = 214
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1137368
90 X = 264849
85
Y = 21444701
47 feet Y = 6539764
37 meter
Z = 5878313
63 Z = 1793194
75
XDOT = -16012
303737 XDOT = -4873
105418
YDOT = 5940
840154 feet/sec YDOT = 1756
231646 meter/sec
ZDOT = -18459
237647 ZDOT = -5650
066182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6454003
99 X = -1967180
42
Y = 20480523
53 feet Y = 6242463
57 meter
Z = 5883654
36 Z = 1793337
85
XDOT = -15472
546023 XDOT = -4716
032028
YDOT = 490
069253 feet/sec YDOT = 149
373108 meter/sec
ZDOT = -18563
002320 ZDOT = -5658
003107
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
96974250
00016717 00000-0 10270-3 0 9068
2 25544 51
6427 280
2746 0006849 358
3943 1
7186 15
53942057 20509
Satellite: ISS
Catalog Number: 25544
Epoch time: 16268
96974250 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 280
2746 deg
Eccentricity:
0006849
Arg of perigee: 358
3943 deg
Mean anomaly: 1
7186 deg
Mean motion: 15
53942057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2050
Checksum: 331
Coasting Arc #8 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2016/269/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 393398
23 A = 6789897
16 meter
Y = -6765526
94 meter E =
0017425
Z = -193580
78 I = 51
29195
XDOT = 4801
971213 Wp = 28
60934
YDOT = 114
833177 meter/sec RA = 274
63954 deg
ZDOT = 5984
071199 TA = 329
29373
MA = 329
39558
Ha = 222
610 n
mi
Hp = 214
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1290676
62 X = 469963
17
Y = -22196610
70 feet Y = -6760699
62 meter
Z = -635107
56 Z = -191483
13
XDOT = 15754
498731 XDOT = 4771
262248
YDOT = 376
749267 feet/sec YDOT = 168
360923 meter/sec
ZDOT = 19632
779523 ZDOT = 6007
323319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8608430
54 X = 2623849
63
Y = -20500324
57 feet Y = -6248498
93 meter
Z = -624780
65 Z = -190433
14
XDOT = 13115
337785 XDOT = 3997
554957
YDOT = 4930
184785 feet/sec YDOT = 1502
720322 meter/sec
ZDOT = 19734
296303 ZDOT = 6015
013513
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
93439694
00016717 00000-0 10270-3 0 9075
2 25544 51
6412 275
4665 0006849 1
8494 358
2683 15
53929160 20658
Satellite: ISS
Catalog Number: 25544
Epoch time: 16269
93439694 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 275
4665 deg
Eccentricity:
0006849
Arg of perigee: 1
8494 deg
Mean anomaly: 358
2683 deg
Mean motion: 15
53929160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2065
Checksum: 347
Coasting Arc #9 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2016/270/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1131297
07 A = 6788978
21 meter
Y = 6533692
11 meter E =
0005736
Z = -1461670
76 I = 51
28611
XDOT = -4619
244087 Wp = 89
25420
YDOT = -2081
064361 meter/sec RA = 269
64637 deg
ZDOT = -5746
762161 TA = 106
76039
MA = 106
69744
Ha = 222
703 n
mi
Hp = 214
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3711604
54 X = -1197174
24
Y = 21435997
74 feet Y = 6520672
68 meter
Z = -4795507
76 Z = -1467327
06
XDOT = -15155
000285 XDOT = -4567
714546
YDOT = -6827
638979 feet/sec YDOT = -2132
432383 meter/sec
ZDOT = -18854
206566 ZDOT = -5769
075845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10276646
40 X = -3132321
82
Y = 19168211
25 feet Y = 5842470
79 meter
Z = -4821319
15 Z = -1469538
08
XDOT = -10700
033791 XDOT = -3261
370300
YDOT = -10487
316135 feet/sec YDOT = -3196
533958 meter/sec
ZDOT = -18951
293728 ZDOT = -5776
354328
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
96335663
00016717 00000-0 10270-3 0 9082
2 25544 51
6400 270
3392 0006740 5
3968 354
7256 15
53932215 20811
Satellite: ISS
Catalog Number: 25544
Epoch time: 16270
96335663 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 270
3392 deg
Eccentricity:
0006740
Arg of perigee: 5
3968 deg
Mean anomaly: 354
7256 deg
Mean motion: 15
53932215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2081
Checksum: 307
Coasting Arc #10 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2016/271/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1825299
52 A = 6786069
93 meter
Y = -5823628
72 meter E =
0016286
Z = 2944306
02 I = 51
27764
XDOT = 4367
762082 Wp = 59
24740
YDOT = 3888
559800 meter/sec RA = 264
64613 deg
ZDOT = 4971
213029 TA = 334
59681
MA = 334
67678
Ha = 222
602 n
mi
Hp = 214
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5988515
47 X = 1875982
99
Y = -19106393
42 feet Y = -5802933
22 meter
Z = 9659796
64 Z = 2953296
71
XDOT = 14329
928089 XDOT = 4299
806594
YDOT = 12757
742125 feet/sec YDOT = 3937
023725 meter/sec
ZDOT = 16309
754032 ZDOT = 4992
264951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11387788
62 X = 3470997
97
Y = -16445541
94 feet Y = -5012601
18 meter
Z = 9700034
99 Z = 2956570
66
XDOT = 8538
707181 XDOT = 2602
597949
YDOT = 15610
196650 feet/sec YDOT = 4757
987939 meter/sec
ZDOT = 16401
035098 ZDOT = 4999
035498
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
99230909
00016717 00000-0 10270-3 0 9094
2 25544 51
6397 265
2102 0006655 8
0322 352
0936 15
53974140 20973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16271
99230909 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 265
2102 deg
Eccentricity:
0006655
Arg of perigee: 8
0322 deg
Mean anomaly: 352
0936 deg
Mean motion: 15
53974140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 311
Coasting Arc #11 (Orbit 2111)
---------------------------------------
Vector Time (GMT): 2016/272/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2535935
38 A = 6782385
99 meter
Y = 4722646
76 meter E =
0012865
Z = -4169383
55 I = 51
26827
XDOT = -3990
492086 Wp = 44
18210
YDOT = -5396
882365 meter/sec RA = 259
63698 deg
ZDOT = -3683
741977 TA = 187
72728
MA = 187
74712
Ha = 222
864 n
mi
Hp = 213
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8319997
96 X = -2568303
62
Y = 15494247
91 feet Y = 4694106
66 meter
Z = -13679079
88 Z = -4181781
80
XDOT = -13092
165638 XDOT = -3911
952118
YDOT = -17706
306972 feet/sec YDOT = -5441
068100 meter/sec
ZDOT = -12085
767640 ZDOT = -3702
935304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12288905
18 X = -3745658
30
Y = 12520832
15 feet Y = 3816349
64 meter
Z = -13734004
61 Z = -4186124
61
XDOT = -6541
637972 XDOT = -1993
891254
YDOT = -19775
953467 feet/sec YDOT = -6027
710617 meter/sec
ZDOT = -12168
693146 ZDOT = -3709
017671
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
95694749
00016717 00000-0 10270-3 0 9109
2 25544 51
6387 260
4018 0006796 13
6360 346
4975 15
53968615 21123
Satellite: ISS
Catalog Number: 25544
Epoch time: 16272
95694749 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 260
4018 deg
Eccentricity:
0006796
Arg of perigee: 13
6360 deg
Mean anomaly: 346
4975 deg
Mean motion: 15
53968615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2112
Checksum: 336
Coasting Arc #12 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2016/273/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3224000
98 A = 6779330
65 meter
Y = -3293982
27 meter E =
0007778
Z = 4964222
28 I = 51
26406
XDOT = 3498
592205 Wp = 66
23423
YDOT = 6514
639017 meter/sec RA = 254
61911 deg
ZDOT = 2051
130731 TA = 3
72958
MA = 3
72379
Ha = 222
879 n
mi
Hp = 213
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10577431
03 X = 3236481
32
Y = -10807028
45 feet Y = -3257858
81 meter
Z = 16286818
50 Z = 4979914
55
XDOT = 11478
320884 XDOT = 3415
520262
YDOT = 21373
487588 feet/sec YDOT = 6553
298441 meter/sec
ZDOT = 6729
431533 ZDOT = 2067
923378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12978285
78 X = 3955781
51
Y = -7614685
55 feet Y = -2320956
16 meter
Z = 16355886
71 Z = 4985274
27
XDOT = 4752
421021 XDOT = 1448
537927
YDOT = 22705
845272 feet/sec YDOT = 6920
741639 meter/sec
ZDOT = 6801
702949 ZDOT = 2073
159059
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 16273
98588931
00016717 00000-0 10270-3 0 9119
2 25544 51
6383 255
2731 0006794 17
5899 342
5488 15
53933786 21285
Satellite: ISS
Catalog Number: 25544
Epoch time: 16273
98588931 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 255
2731 deg
Eccentricity:
0006794
Arg of perigee: 17
5899 deg
Mean anomaly: 342
5488 deg
Mean motion: 15
53933786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2128
Checksum: 358
Coasting Arc #13 (Orbit 2142)
---------------------------------------
Vector Time (GMT): 2016/274/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3894023
76 A = 6777803
82 meter
Y = 1708540
09 meter E =
0018544
Z = -5293163
28 I = 51
26874
XDOT = -2825
783048 Wp = 69
23271
YDOT = -7111
542774 meter/sec RA = 249
59542 deg
ZDOT = -210
784299 TA = 198
71039
MA = 198
77864
Ha = 222
955 n
mi
Hp = 213
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12775668
49 X = -3887127
52
Y = 5605446
49 feet Y = 1665032
28 meter
Z = -17366021
25 Z = -5312063
15
XDOT = -9270
941759 XDOT = -2745
026037
YDOT = -23331
833249 feet/sec YDOT = -7142
691068 meter/sec
ZDOT = -691
549539 ZDOT = -224
314172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13663234
41 X = -4164553
85
Y = 2252005
43 feet Y = 686411
26 meter
Z = -17448837
41 Z = -5318405
64
XDOT = -2959
869077 XDOT = -902
168095
YDOT = -23913
125007 feet/sec YDOT = -7288
720502 meter/sec
ZDOT = -749
488453 ZDOT = -228
444081
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 16274
95051441
00016717 00000-0 10270-3 0 9129
2 25544 51
6381 250
4651 0006640 22
0292 338
1144 15
53982473 21433
Satellite: ISS
Catalog Number: 25544
Epoch time: 16274
95051441 = yrday
fracday
Element set: 912
Inclination: 51
6381 deg
RA of node: 250
4651 deg
Eccentricity:
0006640
Arg of perigee: 22
0292 deg
Mean anomaly: 338
1144 deg
Mean motion: 15
53982473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2143
Checksum: 286
Coasting Arc #14 (Orbit 2158)
---------------------------------------
Vector Time (GMT): 2016/275/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4487943
80 A = 6778741
98 meter
Y = -37190
72 meter E =
0011337
Z = 5076306
93 I = 51
28464
XDOT = 1957
222612 Wp = 38
40890
YDOT = 7227
968613 meter/sec RA = 244
57131 deg
ZDOT = -1666
673755 TA = 67
81824
MA = 67
69798
Ha = 222
946 n
mi
Hp = 213
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14724225
07 X = 4463367
29
Y = -122016
79 feet Y = 12859
79 meter
Z = 16654550
29 Z = 5098048
82
XDOT = 6421
334029 XDOT = 1884
348249
YDOT = 23713
807785 feet/sec YDOT = 7249
447887 meter/sec
ZDOT = -5468
089747 ZDOT = -1657
343969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14238904
27 X = 4340018
02
Y = 3301396
18 feet Y = 1006265
56 meter
Z = 16749511
21 Z = 5105251
02
XDOT = 971
881617 XDOT = 296
229517
YDOT = 23527
411568 feet/sec YDOT = 7171
155046 meter/sec
ZDOT = -5428
500306 ZDOT = -1654
606893
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 16275
97944184
00016717 00000-0 10270-3 0 9138
2 25544 51
6388 245
3362 0006645 25
6223 334
5258 15
53962693 21595
Satellite: ISS
Catalog Number: 25544
Epoch time: 16275
97944184 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 245
3362 deg
Eccentricity:
0006645
Arg of perigee: 25
6223 deg
Mean anomaly: 334
5258 deg
Mean motion: 15
53962693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2159
Checksum: 337
Coasting Arc #15 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2016/276/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4957565
55 A = 6781435
46 meter
Y = -1504485
15 meter E =
0012172
Z = -4384619
20 I = 51
30917
XDOT = -890
904623 Wp = 78
29698
YDOT = -6826
122610 meter/sec RA = 239
55400 deg
ZDOT = 3359
917491 TA = 225
84378
MA = 225
94391
Ha = 223
050 n
mi
Hp = 213
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16264978
85 X = -4919074
63
Y = -4935974
91 feet Y = -1559709
34 meter
Z = -14385233
61 Z = -4408608
50
XDOT = -2922
915430 XDOT = -830
828257
YDOT = -22395
415387 feet/sec YDOT = -6835
748951 meter/sec
ZDOT = 11023
351349 ZDOT = 3355
736456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14713669
78 X = -4484726
55
Y = -8330836
22 feet Y = -2539238
88 meter
Z = -14489769
51 Z = -4416481
75
XDOT = 1332
320935 XDOT = 406
091421
YDOT = -21437
361538 feet/sec YDOT = -6534
107797 meter/sec
ZDOT = 11006
174793 ZDOT = 3354
682077
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 16276
94405382
00016717 00000-0 10270-3 0 9149
2 25544 51
6392 240
5283 0006646 30
8782 329
2760 15
54002812 21743
Satellite: ISS
Catalog Number: 25544
Epoch time: 16276
94405382 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 240
5283 deg
Eccentricity:
0006646
Arg of perigee: 30
8782 deg
Mean anomaly: 329
2760 deg
Mean motion: 15
54002812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 306
Coasting Arc #16 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2016/277/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5220530
29 A = 6785218
31 meter
Y = 2895883
11 meter E =
0017023
Z = 3215927
45 I = 51
33816
XDOT = -389
409206 Wp = 73
81137
YDOT = 6007
322036 meter/sec RA = 234
54745 deg
ZDOT = -4751
692660 TA = 68
78986
MA = 68
60809
Ha = 223
059 n
mi
Hp = 213
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17127724
05 X = 5172137
92
Y = 9500928
84 feet Y = 2953992
39 meter
Z = 10550943
08 Z = 3241170
03
XDOT = -1277
589258 XDOT = -433
473585
YDOT = 19709
061799 feet/sec YDOT = 6002
720453 meter/sec
ZDOT = -15589
542848 ZDOT = -4753
692094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14810009
16 X = 4514090
79
Y = 12726397
88 feet Y = 3879006
07 meter
Z = 10660741
32 Z = 3249393
95
XDOT = -4172
440419 XDOT = -1271
759840
YDOT = 17992
600420 feet/sec YDOT = 5484
144608 meter/sec
ZDOT = -15599
224084 ZDOT = -4754
643501
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 16277
97296669
00016717 00000-0 10270-3 0 9150
2 25544 51
6384 235
4003 0006529 33
6641 326
4925 15
54003876 21903
Satellite: ISS
Catalog Number: 25544
Epoch time: 16277
97296669 = yrday
fracday
Element set: 915
Inclination: 51
6384 deg
RA of node: 235
4003 deg
Eccentricity:
0006529
Arg of perigee: 33
6641 deg
Mean anomaly: 326
4925 deg
Mean motion: 15
54003876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 327
Coasting Arc #17 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2016/278/01:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1211208
52 A = 6780271
62 meter
Y = 4737369
05 meter E =
0016408
Z = -4713047
00 I = 51
32851
XDOT = -5782
327959 Wp = 57
77124
YDOT = -4203
292656 meter/sec RA = 233
86082 deg
ZDOT = -2737
412963 TA = 184
96031
MA = 184
97659
Ha = 223
064 n
mi
Hp = 213
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3973781
24 X = -1241198
61
Y = 15542549
37 feet Y = 4723656
26 meter
Z = -15462752
62 Z = -4719004
25
XDOT = -18970
892253 XDOT = -5721
598501
YDOT = -13790
330237 feet/sec YDOT = -4267
615291 meter/sec
ZDOT = -8981
013659 ZDOT = -2765
354558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7356861
93 X = 2242371
52
Y = 14227081
34 feet Y = 4336414
39 meter
Z = -15489520
20 Z = -4721205
76
XDOT = -22271
436993 XDOT = -6788
333995
YDOT = 1600
934003 feet/sec YDOT = 487
964684 meter/sec
ZDOT = -9102
396097 ZDOT = -2774
410330
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 16278
10158048
00016717 00000-0 10270-3 0 9165
2 25544 51
6428 234
7603 0006347 34
3143 325
8419 15
54005015 21923
Satellite: ISS
Catalog Number: 25544
Epoch time: 16278
10158048 = yrday
fracday
Element set: 916
Inclination: 51
6428 deg
RA of node: 234
7603 deg
Eccentricity:
0006347
Arg of perigee: 34
3143 deg
Mean anomaly: 325
8419 deg
Mean motion: 15
54005015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 292
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