[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 20th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
170/05:52:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
0
171/22:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 503)
---------------------------------------
Vector Time (GMT): 2016/169/13:24:18
756
Vector Time (MET): N/A
Weight (LBS) : 906675
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3627428
80 A = 6788024
79 meter
Y = -5722482
00 meter E =
0010806
Z = -322176
41 I = 51
97126
XDOT = 4144
996289 Wp = 136
84681
YDOT = -2295
123040 meter/sec RA = 55
49846 deg
ZDOT = -6029
916252 TA = 46
61018
MA = 46
52024
Ha = 220
188 n
mi
Hp = 214
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11901013
12 X = -3561603
96
Y = -18774547
25 feet Y = -5762678
24 meter
Z = -1057009
22 Z = -339638
50
XDOT = 13599
069191 XDOT = 4199
643819
YDOT = -7529
931232 feet/sec YDOT = -2248
464647 meter/sec
ZDOT = -19783
189804 ZDOT = -6009
648288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14636045
84 X = -4461066
77
Y = 16725425
48 feet Y = 5097909
69 meter
Z = -1131950
13 Z = -345018
40
XDOT = -9892
179596 XDOT = -3015
136341
YDOT = -9963
040507 feet/sec YDOT = -3036
734746 meter/sec
ZDOT = -19694
383981 ZDOT = -6002
848237
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 16169
59006500
00016717 00000-0 10270-3 0 9005
2 25544 51
6441 56
0279 0000588 321
3039 38
8071 15
54559593 5041
Satellite: ISS
Catalog Number: 25544
Epoch time: 16169
59006500 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 56
0279 deg
Eccentricity:
0000588
Arg of perigee: 321
3039 deg
Mean anomaly: 38
8071 deg
Mean motion: 15
54559593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 504
Checksum: 300
Coasting Arc #2 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2016/170/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1358880
05 A = 6777791
50 meter
Y = 4489827
41 meter E =
0006303
Z = 4888501
63 I = 51
92156
XDOT = -5811
126076 Wp = 118
13936
YDOT = -4389
983252 meter/sec RA = 52
10422 deg
ZDOT = 2411
361286 TA = 308
29781
MA = 308
35447
Ha = 220
181 n
mi
Hp = 214
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4458267
87 X = -1432731
82
Y = 14730404
90 feet Y = 4474217
94 meter
Z = 16038391
18 Z = 4881721
70
XDOT = -19065
374264 XDOT = -5773
317715
YDOT = -14402
832190 feet/sec YDOT = -4454
756050 meter/sec
ZDOT = 7911
290309 ZDOT = 2383
223355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6031930
72 X = -1838532
48
Y = 14193425
07 feet Y = 4326155
96 meter
Z = 16007918
96 Z = 4879213
70
XDOT = -16522
047524 XDOT = -5035
920085
YDOT = -15826
413480 feet/sec YDOT = -4823
890829 meter/sec
ZDOT = 7789
552928 ZDOT = 2374
255733
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 16170
29717238
00016717 00000-0 10270-3 0 9012
2 25544 51
6407 52
5000 0000612 328
1640 31
9476 15
54617783 5158
Satellite: ISS
Catalog Number: 25544
Epoch time: 16170
29717238 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 52
5000 deg
Eccentricity:
0000612
Arg of perigee: 328
1640 deg
Mean anomaly: 31
9476 deg
Mean motion: 15
54617783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 284
Coasting Arc #3 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2016/171/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2803593
46 A = 6775976
94 meter
Y = -3125067
08 meter E =
0014653
Z = -5331254
88 I = 51
89544
XDOT = 5398
100455 Wp = 85
12169
YDOT = 5422
082708 meter/sec RA = 47
11915 deg
ZDOT = -339
150449 TA = 181
64973
MA = 181
65457
Ha = 220
167 n
mi
Hp = 214
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9198141
27 X = 2864227
42
Y = -10252844
74 feet Y = -3093375
64 meter
Z = -17490993
70 Z = -5317488
84
XDOT = 17710
303329 XDOT = 5338
715620
YDOT = 17788
985263 feet/sec YDOT = 5482
115870 meter/sec
ZDOT = -1112
698325 ZDOT = -313
071176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10141811
64 X = 3091224
19
Y = -9433353
15 feet Y = -2875286
04 meter
Z = -17430346
92 Z = -5312769
74
XDOT = 15467
036586 XDOT = 4714
352751
YDOT = 18479
160801 feet/sec YDOT = 5632
448212 meter/sec
ZDOT = -1000
154823 ZDOT = -304
847190
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 16171
26140197
00016717 00000-0 10270-3 0 9025
2 25544 51
6413 47
6897 0000592 338
8463 21
2665 15
54613209 5300
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
26140197 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 47
6897 deg
Eccentricity:
0000592
Arg of perigee: 338
8463 deg
Mean anomaly: 21
2665 deg
Mean motion: 15
54613209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 299
Coasting Arc #4 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5685774
50 A = 6784407
33 meter
Y = -2314138
93 meter E =
0012975
Z = 2875284
58 I = 51
91150
XDOT = -242
843492 Wp = 97
90448
YDOT = -5740
852936 meter/sec RA = 43
68419 deg
ZDOT = -5082
847629 TA = 49
48503
MA = 49
37207
Ha = 220
137 n
mi
Hp = 214
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18654115
82 X = -5673441
56
Y = -7592319
34 feet Y = -2377652
52 meter
Z = 9433348
35 Z = 2847694
06
XDOT = -796
730618 XDOT = -153
939453
YDOT = -18834
819344 feet/sec YDOT = -5743
070729 meter/sec
ZDOT = -16676
009281 ZDOT = -5083
812217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15325503
50 X = 4671213
47
Y = -13152705
10 feet Y = -4008944
52 meter
Z = 9313576
21 Z = 2838778
03
XDOT = 16097
648679 XDOT = 4906
563317
YDOT = 6904
405020 feet/sec YDOT = 2104
462650 meter/sec
ZDOT = -16679
017907 ZDOT = -5083
764658
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 16171
96849524
00016717 00000-0 10270-3 0 9033
2 25544 51
6442 44
1615 0000481 314
9722 45
1392 15
54645992 5410
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
96849524 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 44
1615 deg
Eccentricity:
0000481
Arg of perigee: 314
9722 deg
Mean anomaly: 45
1392 deg
Mean motion: 15
54645992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 307
Coasting Arc #5 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5730260
26 A = 6787412
58 meter
Y = 3443867
94 meter E =
0009661
Z = -1145180
27 I = 51
89654
XDOT = -1612
321499 Wp = 33
99718
YDOT = 4632
320044 meter/sec RA = 38
72546 deg
ZDOT = 5894
646429 TA = 313
61333
MA = 313
69344
Ha = 220
153 n
mi
Hp = 214
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18800066
47 X = 5696886
96
Y = 11298779
32 feet Y = 3507761
09 meter
Z = -3757153
11 Z = -1117424
68
XDOT = -5289
768696 XDOT = -1692
635043
YDOT = 15197
900408 feet/sec YDOT = 4613
840049 meter/sec
ZDOT = 19339
391171 ZDOT = 5886
619806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18468771
30 X = -5629281
49
Y = 11870069
70 feet Y = 3617997
24 meter
Z = -3636900
49 Z = -1108527
27
XDOT = -10362
256303 XDOT = -3158
415721
YDOT = -10241
287770 feet/sec YDOT = -3121
544512 meter/sec
ZDOT = 19303
436123 ZDOT = 5883
687330
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 16172
93270684
00016717 00000-0 10270-3 0 9047
2 25544 51
6434 39
3519 0000679 324
9728 35
1380 15
54607492 5561
Satellite: ISS
Catalog Number: 25544
Epoch time: 16172
93270684 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 39
3519 deg
Eccentricity:
0000679
Arg of perigee: 324
9728 deg
Mean anomaly: 35
1380 deg
Mean motion: 15
54607492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 322
Coasting Arc #6 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2016/173/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5246853
03 A = 6787499
11 meter
Y = -4230417
19 meter E =
0009800
Z = -764509
02 I = 51
87101
XDOT = 3513
641221 Wp = 139
66114
YDOT = -3287
932277 meter/sec RA = 33
77041 deg
ZDOT = -5970
409972 TA = 48
57661
MA = 48
49244
Ha = 220
045 n
mi
Hp = 213
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17214084
75 X = -5195443
85
Y = -13879321
49 feet Y = -4288803
44 meter
Z = -2508231
68 Z = -789872
55
XDOT = 11527
694296 XDOT = 3579
148102
YDOT = -10787
179386 feet/sec YDOT = -3248
273264 meter/sec
ZDOT = -19587
959226 ZDOT = -5953
183030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19899831
87 X = 6065468
75
Y = -9612223
94 feet Y = -2929805
86 meter
Z = -2617889
87 Z = -797932
83
XDOT = 4069
671120 XDOT = 1240
435757
YDOT = 13696
658911 feet/sec YDOT = 4174
741636 meter/sec
ZDOT = -19512
182835 ZDOT = -5947
313328
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 16173
96119159
00016717 00000-0 10270-3 0 9051
2 25544 51
6426 34
2214 0000494 326
8529 33
2592 15
54664560 5724
Satellite: ISS
Catalog Number: 25544
Epoch time: 16173
96119159 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 34
2214 deg
Eccentricity:
0000494
Arg of perigee: 326
8529 deg
Mean anomaly: 33
2592 deg
Mean motion: 15
54664560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 309
Coasting Arc #7 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2016/174/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4251514
20 A = 6784941
18 meter
Y = 4623683
54 meter E =
0013569
Z = 2548211
19 I = 51
83571
XDOT = -5225
318825 Wp = 73
66588
YDOT = 1875
654656 meter/sec RA = 28
80874 deg
ZDOT = 5295
144154 TA = 314
89771
MA = 315
00777
Ha = 220
045 n
mi
Hp = 213
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13948537
40 X = 4187117
01
Y = 15169565
43 feet Y = 4670866
40 meter
Z = 8360272
95 Z = 2568708
04
XDOT = -17143
434464 XDOT = -5271
625839
YDOT = 6153
722626 feet/sec YDOT = 1816
962030 meter/sec
ZDOT = 17372
520190 ZDOT = 5269
648832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19547010
36 X = -5957928
76
Y = 6411439
20 feet Y = 1954206
67 meter
Z = 8448633
53 Z = 2575143
50
XDOT = 1966
727623 XDOT = 599
458579
YDOT = -16833
314089 feet/sec YDOT = -5130
794134 meter/sec
ZDOT = 17261
002776 ZDOT = 5261
153646
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 16174
98966574
00016717 00000-0 10270-3 0 9066
2 25544 51
6430 29
0900 0000579 338
0802 22
0326 15
54671125 5889
Satellite: ISS
Catalog Number: 25544
Epoch time: 16174
98966574 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 29
0900 deg
Eccentricity:
0000579
Arg of perigee: 338
0802 deg
Mean anomaly: 22
0326 deg
Mean motion: 15
54671125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 309
Coasting Arc #8 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2016/175/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2766067
74 A = 6780743
42 meter
Y = -4698169
42 meter E =
0007294
Z = -4039637
95 I = 51
79302
XDOT = 6558
930888 Wp = 66
38687
YDOT = -484
497853 meter/sec RA = 23
83524 deg
ZDOT = -3930
394853 TA = 162
86938
MA = 162
84475
Ha = 220
086 n
mi
Hp = 213
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9075025
40 X = -2693703
42
Y = -15413941
68 feet Y = -4728696
34 meter
Z = -13253405
35 Z = -4052899
49
XDOT = 21518
802127 XDOT = 6582
953175
YDOT = -1589
559884 feet/sec YDOT = -411
016731 meter/sec
ZDOT = -12894
996237 ZDOT = -3898
475216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17715267
44 X = 5399613
52
Y = -2146152
96 feet Y = -654147
42 meter
Z = -13310212
79 Z = -4056952
86
XDOT = -7254
495497 XDOT = -2211
170227
YDOT = 19172
178613 feet/sec YDOT = 5843
680041 meter/sec
ZDOT = -12755
774677 ZDOT = -3887
960122
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 16175
95385241
00016717 00000-0 10270-3 0 9071
2 25544 51
6428 24
2799 0000615 348
4649 11
6490 15
54682936 6030
Satellite: ISS
Catalog Number: 25544
Epoch time: 16175
95385241 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 24
2799 deg
Eccentricity:
0000615
Arg of perigee: 348
4649 deg
Mean anomaly: 11
6490 deg
Mean motion: 15
54682936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 325
Coasting Arc #9 (Orbit 618)
---------------------------------------
Vector Time (GMT): 2016/176/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 944333
48 A = 6777024
32 meter
Y = 4480936
31 meter E =
0005524
Z = 4992381
62 I = 51
75044
XDOT = -7343
979409 Wp = 118
28879
YDOT = -774
362791 meter/sec RA = 18
84737 deg
ZDOT = 2079
876593 TA = 311
49299
MA = 311
54039
Ha = 220
034 n
mi
Hp = 213
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3098206
94 X = 869905
73
Y = 14701234
60 feet Y = 4491079
81 meter
Z = 16379204
78 Z = 4996788
59
XDOT = -24094
420633 XDOT = -7344
877517
YDOT = -2540
560339 feet/sec YDOT = -856
493298 meter/sec
ZDOT = 6823
742102 ZDOT = 2044
199458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14735948
12 X = -4491516
99
Y = -2824622
87 feet Y = -860945
05 meter
Z = 16397465
44 Z = 4997947
47
XDOT = 11323
927693 XDOT = 3451
533161
YDOT = -20283
166896 feet/sec YDOT = -6182
309270 meter/sec
ZDOT = 6668
415235 ZDOT = 2032
532964
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 16176
98230914
00016717 00000-0 10270-3 0 9082
2 25544 51
6422 19
1491 0000665 347
4559 12
6577 15
54709441 6195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16176
98230914 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 19
1491 deg
Eccentricity:
0000665
Arg of perigee: 347
4559 deg
Mean anomaly: 12
6577 deg
Mean motion: 15
54709441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 619
Checksum: 321
Coasting Arc #10 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2016/177/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1059377
21 A = 6775710
15 meter
Y = -4068694
51 meter E =
0014773
Z = -5326279
17 I = 51
71622
XDOT = 7426
510086 Wp = 87
40348
YDOT = 1870
591925 meter/sec RA = 13
84856 deg
ZDOT = 48
948047 TA = 183
05852
MA = 183
06756
Ha = 220
084 n
mi
Hp = 213
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3475647
01 X = 1130668
20
Y = -13348735
28 feet Y = -4056448
78 meter
Z = -17474669
19 Z = -5320960
22
XDOT = 24365
190572 XDOT = 7404
802938
YDOT = 6137
112615 feet/sec YDOT = 1953
518734 meter/sec
ZDOT = 160
590704 ZDOT = 84
971327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11124990
53 X = 3390897
11
Y = 8206278
76 feet Y = 2501273
77 meter
Z = -17450630
18 Z = -5318952
08
XDOT = -13994
545169 XDOT = -4265
537367
YDOT = 19641
074664 feet/sec YDOT = 5986
599558 meter/sec
ZDOT = 317
186866 ZDOT = 96
678557
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 16177
94647990
00016717 00000-0 10270-3 0 9096
2 25544 51
6434 14
3385 0000754 351
3101 8
8039 15
54695099 6343
Satellite: ISS
Catalog Number: 25544
Epoch time: 16177
94647990 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 14
3385 deg
Eccentricity:
0000754
Arg of perigee: 351
3101 deg
Mean anomaly: 8
8039 deg
Mean motion: 15
54695099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 634
Checksum: 323
Coasting Arc #11 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2016/178/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3027258
30 A = 6777168
44 meter
Y = 3490420
69 meter E =
0006962
Z = 4954869
20 I = 51
68981
XDOT = -6802
586831 Wp = 51
18607
YDOT = -2799
983535 meter/sec RA = 8
84878 deg
ZDOT = -2177
398070 TA = 60
05355
MA = 59
98444
Ha = 220
136 n
mi
Hp = 213
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9931949
80 X = -3090132
57
Y = 11451511
44 feet Y = 3456215
93 meter
Z = 16256132
54 Z = 4940011
16
XDOT = -22318
198264 XDOT = -6760
194321
YDOT = -9186
297687 feet/sec YDOT = -2875
817396 meter/sec
ZDOT = -7143
694455 ZDOT = -2210
340422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7239946
35 X = -2206735
65
Y = -13397338
68 feet Y = -4083508
83 meter
Z = 16190647
90 Z = 4934909
48
XDOT = 15392
225218 XDOT = 4691
550246
YDOT = -17149
077592 feet/sec YDOT = -5227
038850 meter/sec
ZDOT = -7286
658856 ZDOT = -2220
973619
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 16178
97491778
00016717 00000-0 10270-3 0 9103
2 25544 51
6431 9
2081 0000879 359
9361
1791 15
54751796 6501
Satellite: ISS
Catalog Number: 25544
Epoch time: 16178
97491778 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 9
2081 deg
Eccentricity:
0000879
Arg of perigee: 359
9361 deg
Mean anomaly:
1791 deg
Mean motion: 15
54751796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 328
Coasting Arc #12 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2016/179/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4729695
98 A = 6780970
49 meter
Y = -2821175
08 meter E =
0006564
Z = -3962653
34 I = 51
67104
XDOT = 5477
057693 Wp = 97
99417
YDOT = 3550
084711 meter/sec RA = 3
85489 deg
ZDOT = 4014
594149 TA = 213
88664
MA = 213
92860
Ha = 220
130 n
mi
Hp = 213
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15517375
25 X = 4780140
38
Y = -9255823
75 feet Y = -2768002
11 meter
Z = -13000831
15 Z = -3939555
38
XDOT = 17969
349387 XDOT = 5417
451548
YDOT = 11647
259549 feet/sec YDOT = 3610
999234 meter/sec
ZDOT = 13171
240645 ZDOT = 4041
055786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3549881
29 X = 1082003
82
Y = 17789880
07 feet Y = 5422355
45 meter
Z = -12899586
36 Z = -3931793
92
XDOT = -15629
914071 XDOT = -4763
997809
YDOT = 12740
991358 feet/sec YDOT = 3883
454166 meter/sec
ZDOT = 13285
797206 ZDOT = 4049
510988
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 16179
93907259
00016717 00000-0 10270-3 0 9117
2 25544 51
6436 4
3978 0000919 8
9752 351
1417 15
54749306 6651
Satellite: ISS
Catalog Number: 25544
Epoch time: 16179
93907259 = yrday
fracday
Element set: 911
Inclination: 51
6436 deg
RA of node: 4
3978 deg
Eccentricity:
0000919
Arg of perigee: 8
9752 deg
Mean anomaly: 351
1417 deg
Mean motion: 15
54749306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 332
Coasting Arc #13 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2016/180/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5993831
43 A = 6785047
31 meter
Y = 2037056
72 meter E =
0013761
Z = 2425209
59 I = 51
65184
XDOT = -3589
302164 Wp = 101
74700
YDOT = -4163
327413 meter/sec RA = 358
87162 deg
ZDOT = -5350
911824 TA = 51
11357
MA = 50
99091
Ha = 220
143 n
mi
Hp = 213
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19664801
26 X = -6027945
47
Y = 6683256
97 feet Y = 1969838
75 meter
Z = 7956724
38 Z = 2396010
33
XDOT = -11775
925735 XDOT = -3516
487563
YDOT = -13659
210673 feet/sec YDOT = -4203
057788 meter/sec
ZDOT = -17555
484986 ZDOT = -5368
171287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -114337
84 X = -34850
17
Y = -20817599
37 feet Y = -6345204
29 meter
Z = 7829066
27 Z = 2386299
40
XDOT = 15127
179775 XDOT = 4610
764395
YDOT = -6742
065202 feet/sec YDOT = -2054
981474 meter/sec
ZDOT = -17629
807878 ZDOT = -5373
565441
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 16180
96749447
00016717 00000-0 10270-3 0 9126
2 25544 51
6427 359
2668 0000979 12
6991 347
4186 15
54771332 6815
Satellite: ISS
Catalog Number: 25544
Epoch time: 16180
96749447 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 359
2668 deg
Eccentricity:
0000979
Arg of perigee: 12
6991 deg
Mean anomaly: 347
4186 deg
Mean motion: 15
54771332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 345
Coasting Arc #14 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2016/181/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6649639
57 A = 6787257
60 meter
Y = -1188538
26 meter E =
0011769
Z = -599610
57 I = 51
62846
XDOT = 1356
854415 Wp = 38
29871
YDOT = 4613
051235 meter/sec RA = 353
89634 deg
ZDOT = 5975
348067 TA = 315
22586
MA = 315
32078
Ha = 220
082 n
mi
Hp = 213
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21816402
79 X = 6665348
55
Y = -3899403
73 feet Y = -1114089
66 meter
Z = -1967226
29 Z = -567270
15
XDOT = 4451
622096 XDOT = 1276
143520
YDOT = 15134
682528 feet/sec YDOT = 4627
772584 meter/sec
ZDOT = 19604
160326 ZDOT = 5981
743788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2817003
29 X = -858622
60
Y = 21994561
33 feet Y = 6703942
29 meter
Z = -1826067
88 Z = -556585
49
XDOT = -14133
191561 XDOT = -4307
796788
YDOT = -201
381357 feet/sec YDOT = -61
381038 meter/sec
ZDOT = 19631
049465 ZDOT = 5983
543877
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 16181
93163111
00016717 00000-0 10270-3 0 9133
2 25544 51
6438 354
4566 0000985 11
6036 348
5140 15
54795542 6964
Satellite: ISS
Catalog Number: 25544
Epoch time: 16181
93163111 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 354
4566 deg
Eccentricity:
0000985
Arg of perigee: 11
6036 deg
Mean anomaly: 348
5140 deg
Mean motion: 15
54795542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 311
Coasting Arc #15 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2016/182/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6646047
38 A = 6786647
41 meter
Y = 216578
43 meter E =
0008099
Z = -1342704
96 I = 51
59227
XDOT = 1009
721431 Wp = 136
00424
YDOT = -4894
758888 meter/sec RA = 348
92159 deg
ZDOT = -5814
161321 TA = 58
62634
MA = 58
54713
Ha = 220
104 n
mi
Hp = 213
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21804617
39 X = -6641452
97
Y = 710559
15 feet Y = 142283
75 meter
Z = -4405200
01 Z = -1374978
69
XDOT = 3312
734354 XDOT = 1092
623567
YDOT = -16058
920236 feet/sec YDOT = -4883
003264 meter/sec
ZDOT = -19075
332417 ZDOT = -5809
055574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5482300
71 X = 1671005
26
Y = -21086289
02 feet Y = -6427100
89 meter
Z = -4545856
93 Z = -1385577
19
XDOT = 12893
878217 XDOT = 3930
054081
YDOT = 7441
284376 feet/sec YDOT = 2268
103478 meter/sec
ZDOT = -19052
049647 ZDOT = -5807
064732
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 16182
96003568
00016717 00000-0 10270-3 0 9147
2 25544 51
6416 349
3252 0001015 17
7491 342
3698 15
54769801 7120
Satellite: ISS
Catalog Number: 25544
Epoch time: 16182
96003568 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 349
3252 deg
Eccentricity:
0001015
Arg of perigee: 17
7491 deg
Mean anomaly: 342
3698 deg
Mean motion: 15
54769801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 311
Coasting Arc #16 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2016/183/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5982787
70 A = 6783254
58 meter
Y = 818954
84 meter E =
0013312
Z = 3075834
26 I = 51
54936
XDOT = -3203
803031 Wp = 79
96408
YDOT = 4966
038280 meter/sec RA = 343
93781 deg
ZDOT = 4893
697109 TA = 315
45527
MA = 315
56220
Ha = 219
967 n
mi
Hp = 213
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19628568
58 X = 5958244
22
Y = 2686859
72 feet Y = 885720
71 meter
Z = 10091319
76 Z = 3104837
64
XDOT = -10511
164800 XDOT = -3282
867869
YDOT = 16292
776508 feet/sec YDOT = 4929
768467 meter/sec
ZDOT = 16055
436709 ZDOT = 4877
942483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7804162
61 X = -2378708
76
Y = 18139246
59 feet Y = 5528842
36 meter
Z = 10217506
21 Z = 3114295
89
XDOT = -11553
495850 XDOT = -3521
505535
YDOT = -14003
998070 feet/sec YDOT = -4268
418612 meter/sec
ZDOT = 15985
744664 ZDOT = 4872
454973
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 16183
98843048
00016717 00000-0 10270-3 0 9156
2 25544 51
6411 344
1936 0001100 11
0349 349
0828 15
54802532 7286
Satellite: ISS
Catalog Number: 25544
Epoch time: 16183
98843048 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 344
1936 deg
Eccentricity:
0001100
Arg of perigee: 11
0349 deg
Mean anomaly: 349
0828 deg
Mean motion: 15
54802532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 296
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