[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 21st 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
294/08:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
3
299/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 212
8
303/19:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 212
6
306/03:16:27
095 0
6 1
1 1
1
N/A 1
0 -0
1 222
6
000/00:02:54
191 -0
1 0
0 213
3
307/06:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
2
Coasting Arc #1 (Orbit 123)
---------------------------------------
Vector Time (GMT): 2017/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4463721
43 A = 6778643
28 meter
Y = -944136
29 meter E =
0008216
Z = 5006063
42 I = 51
89611
XDOT = 3680
849818 Wp = 84
24406
YDOT = -6407
516202 meter/sec RA = 132
57517 deg
ZDOT = 2071
521390 TA = 345
68281
MA = 345
70607
Ha = 222
566 n
mi
Hp = 213
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14644755
34 X = -4477149
72
Y = -3097560
00 feet Y = -994127
30 meter
Z = 16424092
58 Z = 4984346
96
XDOT = 12076
278929 XDOT = 3742
164110
YDOT = -21022
034783 feet/sec YDOT = -6366
011411 meter/sec
ZDOT = 6796
330021 ZDOT = 2089
551776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14459036
25 X = 4407114
25
Y = -4260395
42 feet Y = -1298568
52 meter
Z = 16327885
83 Z = 4976739
60
XDOT = -950
284557 XDOT = -289
646733
YDOT = 23158
188771 feet/sec YDOT = 7058
615937 meter/sec
ZDOT = 6877
170669 ZDOT = 2096
161620
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 17293
55189421
00016717 00000-0 10270-3 0 9004
2 25544 51
6380 133
3720 0005197 35
8378 324
3123 15
54181626 1244
Satellite: ISS
Catalog Number: 25544
Epoch time: 17293
55189421 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 133
3720 deg
Eccentricity:
0005197
Arg of perigee: 35
8378 deg
Mean anomaly: 324
3123 deg
Mean motion: 15
54181626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 124
Checksum: 292
Coasting Arc #2 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3330068
65 A = 6777048
83 meter
Y = 2540471
77 meter E =
0018660
Z = -5343459
76 I = 51
91221
XDOT = -4703
107471 Wp = 77
01735
YDOT = 6039
867976 meter/sec RA = 128
23274 deg
ZDOT = -55
514602 TA = 192
43168
MA = 192
47777
Ha = 222
405 n
mi
Hp = 213
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10925422
09 X = 3327369
53
Y = 8334881
15 feet Y = 2577695
39 meter
Z = -17531035
95 Z = -5327289
63
XDOT = -15430
142623 XDOT = -4770
027670
YDOT = 19815
839816 feet/sec YDOT = 5986
900439 meter/sec
ZDOT = -182
134520 ZDOT = -78
524443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8097902
32 X = -2468240
63
Y = -11214144
67 feet Y = -3418071
30 meter
Z = -17459646
34 Z = -5321700
21
XDOT = 19760
490240 XDOT = 6022
997425
YDOT = -13805
492284 feet/sec YDOT = -4207
914048 meter/sec
ZDOT = -285
033701 ZDOT = -86
878272
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 17294
38777368
00016717 00000-0 10270-3 0 9010
2 25544 51
6401 129
2064 0005264 38
7494 321
4036 15
54236441 1370
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
38777368 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 129
2064 deg
Eccentricity:
0005264
Arg of perigee: 38
7494 deg
Mean anomaly: 321
4036 deg
Mean motion: 15
54236441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 304
Coasting Arc #3 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2137025
34 A = 6778117
83 meter
Y = -3966187
93 meter E =
0010680
Z = 5059182
42 I = 51
93530
XDOT = 5241
079136 Wp = 49
06881
YDOT = -5269
126260 meter/sec RA = 123
25204 deg
ZDOT = -1907
477288 TA = 59
39065
MA = 59
28537
Ha = 222
424 n
mi
Hp = 213
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7011238
00 X = -2117091
24
Y = -13012427
58 feet Y = -3989973
86 meter
Z = 16598367
52 Z = 5048849
78
XDOT = 17195
141521 XDOT = 5308
876222
YDOT = -17287
159646 feet/sec YDOT = -5210
137965 meter/sec
ZDOT = -6258
127585 ZDOT = -1881
852093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3223923
11 X = 982651
76
Y = 14477174
98 feet Y = 4412642
93 meter
Z = 16553073
99 Z = 5045376
95
XDOT = -20305
367163 XDOT = -6189
075911
YDOT = 11581
968632 feet/sec YDOT = 3530
184039 meter/sec
ZDOT = -6143
708568 ZDOT = -1872
602371
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 17295
41654521
00016717 00000-0 10270-3 0 9021
2 25544 51
6398 124
0772 0005168 41
4959 318
6586 15
54263929 1531
Satellite: ISS
Catalog Number: 25544
Epoch time: 17295
41654521 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 124
0772 deg
Eccentricity:
0005168
Arg of perigee: 41
4959 deg
Mean anomaly: 318
6586 deg
Mean motion: 15
54263929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 326
Coasting Arc #4 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 993643
09 A = 6781347
35 meter
Y = 5188781
40 meter E =
0011340
Z = -4260774
56 I = 51
96325
XDOT = -5403
665488 Wp = 85
82447
YDOT = 4022
148608 meter/sec RA = 118
27854 deg
ZDOT = 3647
153912 TA = 221
32566
MA = 221
41153
Ha = 222
453 n
mi
Hp = 213
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3259983
88 X = 956244
19
Y = 17023561
02 feet Y = 5199683
71 meter
Z = -13978919
17 Z = -4256038
68
XDOT = -17728
561311 XDOT = -5465
957160
YDOT = 13196
025616 feet/sec YDOT = 3961
372987 meter/sec
ZDOT = 11965
728059 ZDOT = 3620
752431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1213210
21 X = 369786
47
Y = -17306758
79 feet Y = -5275100
08 meter
Z = -13958636
29 Z = -4254592
34
XDOT = 19374
636656 XDOT = 5905
389253
YDOT = -8173
525718 feet/sec YDOT = -2491
290639 meter/sec
ZDOT = 11848
017500 ZDOT = 3611
275734
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 17296
38101740
00016717 00000-0 10270-3 0 9039
2 25544 51
6401 119
2683 0005168 44
4352 315
7214 15
54237005 1681
Satellite: ISS
Catalog Number: 25544
Epoch time: 17296
38101740 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 119
2683 deg
Eccentricity:
0005168
Arg of perigee: 44
4352 deg
Mean anomaly: 315
7214 deg
Mean motion: 15
54237005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 284
Coasting Arc #5 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 107087
30 A = 6785210
42 meter
Y = -6097529
94 meter E =
0017101
Z = 2962256
09 I = 51
99147
XDOT = 5293
415725 Wp = 83
77634
YDOT = -2360
878496 meter/sec RA = 113
31607 deg
ZDOT = -5024
389409 TA = 62
54565
MA = 62
37186
Ha = 222
493 n
mi
Hp = 212
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 351336
28 X = 160874
01
Y = -20005019
50 feet Y = -6096031
59 meter
Z = 9718687
96 Z = 2962907
13
XDOT = 17366
849493 XDOT = 5343
828892
YDOT = -7745
664356 feet/sec YDOT = -2301
402181 meter/sec
ZDOT = -16484
217222 ZDOT = -4998
552493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5173511
76 X = -1576886
38
Y = 19325783
04 feet Y = 5890498
67 meter
Z = 9722449
49 Z = 2963402
61
XDOT = -17429
805576 XDOT = -5312
604739
YDOT = 3613
023812 feet/sec YDOT = 1101
249658 meter/sec
ZDOT = -16369
229909 ZDOT = -4989
341276
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 17297
40978182
00016717 00000-0 10270-3 0 9046
2 25544 51
6405 114
1384 0005339 47
2134 312
9467 15
54265249 1844
Satellite: ISS
Catalog Number: 25544
Epoch time: 17297
40978182 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 114
1384 deg
Eccentricity:
0005339
Arg of perigee: 47
2134 deg
Mean anomaly: 312
9467 deg
Mean motion: 15
54265249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 314
Coasting Arc #6 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1035042
65 A = 6788219
84 meter
Y = 6558511
84 meter E =
0013790
Z = -1388084
16 I = 52
01171
XDOT = -4951
899659 Wp = 42
78419
YDOT = 444
926306 meter/sec RA = 108
36477 deg
ZDOT = 5838
376283 TA = 302
16688
MA = 302
30058
Ha = 222
573 n
mi
Hp = 212
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3395809
22 X = -1101561
97
Y = 21517427
29 feet Y = 6546565
32 meter
Z = -4554081
88 Z = -1393273
90
XDOT = -16246
389957 XDOT = -4984
867501
YDOT = 1459
731975 feet/sec YDOT = 389
366585 meter/sec
ZDOT = 19154
777830 ZDOT = 5814
240873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8182444
26 X = 2494009
01
Y = -20183155
75 feet Y = -6151825
87 meter
Z = -4578066
10 Z = -1395394
55
XDOT = 14802
029058 XDOT = 4511
658457
YDOT = 1712
749613 feet/sec YDOT = 522
046082 meter/sec
ZDOT = 19047
605006 ZDOT = 5805
710006
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 17298
37424668
00016717 00000-0 10270-3 0 9059
2 25544 51
6391 109
3298 0005272 50
8004 309
3617 15
54224730 1993
Satellite: ISS
Catalog Number: 25544
Epoch time: 17298
37424668 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 109
3298 deg
Eccentricity:
0005272
Arg of perigee: 50
8004 deg
Mean anomaly: 309
3617 deg
Mean motion: 15
54224730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 316
Coasting Arc #7 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1866736
87 A = 6789002
58 meter
Y = -6512390
56 meter E =
0013037
Z = -389824
81 I = 52
02431
XDOT = 4448
978544 Wp = 114
90399
YDOT = 1626
326633 meter/sec RA = 103
42020 deg
ZDOT = -6027
331196 TA = 69
27524
MA = 69
13556
Ha = 222
571 n
mi
Hp = 212
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6124464
79 X = 1941315
03
Y = -21366110
76 feet Y = -6491098
45 meter
Z = -1278952
79 Z = -380575
32
XDOT = 14596
386298 XDOT = 4459
740261
YDOT = 5335
717301 feet/sec YDOT = 1676
138194 meter/sec
ZDOT = -19774
708649 ZDOT = -6005
692908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10506681
51 X = -3202436
53
Y = 19589157
60 feet Y = 5970775
24 meter
Z = -1236942
34 Z = -377020
02
XDOT = -11838
789376 XDOT = -3608
463002
YDOT = -7557
528975 feet/sec YDOT = -2303
534832 meter/sec
ZDOT = -19678
914534 ZDOT = -5998
133150
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 17299
40300614
00016717 00000-0 10270-3 0 9069
2 25544 51
6398 104
2007 0005095 55
5843 304
5791 15
54218921 2152
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
40300614 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 104
2007 deg
Eccentricity:
0005095
Arg of perigee: 55
5843 deg
Mean anomaly: 304
5791 deg
Mean motion: 15
54218921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 215
Checksum: 295
Coasting Arc #8 (Orbit 216)
---------------------------------------
Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2968209
52 A = 6787100
76 meter
Y = -5738587
09 meter E =
0009062
Z = -2082127
82 I = 52
01722
XDOT = 3579
987301 Wp = 104
47011
YDOT = 3862
916565 meter/sec RA = 102
77565 deg
ZDOT = -5565
537017 TA = 98
43233
MA = 98
32960
Ha = 222
577 n
mi
Hp = 212
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9738220
20 X = 3042273
48
Y = -18827385
45 feet Y = -5704980
47 meter
Z = -6831128
02 Z = -2067528
89
XDOT = 11745
365160 XDOT = 3563
560235
YDOT = 12673
610777 feet/sec YDOT = 3902
858460 meter/sec
ZDOT = -18259
635884 ZDOT = -5548
186194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2946377
66 X = 898055
91
Y = 21012251
60 feet Y = 6404534
29 meter
Z = -6765487
93 Z = -2062120
72
XDOT = -15482
231607 XDOT = -4718
984194
YDOT = -3659
760675 feet/sec YDOT = -1115
495054 meter/sec
ZDOT = -18183
200119 ZDOT = -5542
239396
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 17299
53160086
00016717 00000-0 10270-3 0 9071
2 25544 51
6375 103
5550 0005255 58
9769 301
1899 15
54273006 2173
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
53160086 = yrday
fracday
Element set: 907
Inclination: 51
6375 deg
RA of node: 103
5550 deg
Eccentricity:
0005255
Arg of perigee: 58
9769 deg
Mean anomaly: 301
1899 deg
Mean motion: 15
54273006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 217
Checksum: 318
Coasting Arc #9 (Orbit 232)
---------------------------------------
Vector Time (GMT): 2017/300/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3434146
32 A = 6783649
09 meter
Y = 4639046
42 meter E =
0016889
Z = 3548091
54 I = 52
01193
XDOT = -2799
026091 Wp = 84
04248
YDOT = -5538
730775 meter/sec RA = 97
82149 deg
ZDOT = 4515
954051 TA = 317
59871
MA = 317
72909
Ha = 222
662 n
mi
Hp = 212
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11266884
26 X = -3503001
33
Y = 15219968
58 feet Y = 4600258
55 meter
Z = 11640720
28 Z = 3531241
88
XDOT = -9183
156466 XDOT = -2758
819161
YDOT = -18171
688894 feet/sec YDOT = -5569
806471 meter/sec
ZDOT = 14816
122215 ZDOT = 4502
454815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 89709
66 X = 27343
51
Y = -18982456
98 feet Y = -5785852
89 meter
Z = 11565239
82 Z = 3525085
10
XDOT = 16871
834407 XDOT = 5142
535127
YDOT = 9104
134918 feet/sec YDOT = 2774
940323 meter/sec
ZDOT = 14757
034601 ZDOT = 4497
944146
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 17300
56035485
00016717 00000-0 10270-3 0 9082
2 25544 51
6376 98
4251 0005143 64
6694 295
4991 15
54267769 2336
Satellite: ISS
Catalog Number: 25544
Epoch time: 17300
56035485 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 98
4251 deg
Eccentricity:
0005143
Arg of perigee: 64
6694 deg
Mean anomaly: 295
4991 deg
Mean motion: 15
54267769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 233
Checksum: 332
Coasting Arc #10 (Orbit 247)
---------------------------------------
Vector Time (GMT): 2017/301/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3809130
39 A = 6779812
78 meter
Y = -3128668
15 meter E =
0015692
Z = -4670174
55 I = 52
00284
XDOT = 1965
646695 Wp = 69
47761
YDOT = 6787
171400 meter/sec RA = 92
85847 deg
ZDOT = -2946
304552 TA = 171
30301
MA = 171
27579
Ha = 222
656 n
mi
Hp = 212
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12497146
96 X = 3866518
67
Y = -10264659
27 feet Y = -3085751
14 meter
Z = -15322094
98 Z = -4651531
18
XDOT = 6448
972097 XDOT = 1903
916568
YDOT = 22267
622703 feet/sec YDOT = 6808
807345 meter/sec
ZDOT = -9666
353517 ZDOT = -2936
906075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3769758
33 X = -1149022
34
Y = 15807412
36 feet Y = 4818099
29 meter
Z = -15238869
49 Z = -4644807
42
XDOT = -17547
329094 XDOT = -5348
425908
YDOT = -13455
740762 feet/sec YDOT = -4101
309784 meter/sec
ZDOT = -9625
663629 ZDOT = -2933
902274
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 17301
52480916
00016717 00000-0 10270-3 0 9093
2 25544 51
6379 93
6175 0005288 68
0067 292
1648 15
54264810 2486
Satellite: ISS
Catalog Number: 25544
Epoch time: 17301
52480916 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 93
6175 deg
Eccentricity:
0005288
Arg of perigee: 68
0067 deg
Mean anomaly: 292
1648 deg
Mean motion: 15
54264810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 248
Checksum: 323
Coasting Arc #11 (Orbit 263)
---------------------------------------
Vector Time (GMT): 2017/302/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4055416
53 A = 6777328
05 meter
Y = 1358812
39 meter E =
0008020
Z = 5250481
78 I = 51
99534
XDOT = -1120
500381 Wp = 92
43119
YDOT = -7515
887907 meter/sec RA = 87
88438 deg
ZDOT = 1077
886503 TA = 347
29183
MA = 347
31204
Ha = 222
779 n
mi
Hp = 212
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13305172
35 X = -4095814
39
Y = 4458045
90 feet Y = 1313236
33 meter
Z = 17225990
08 Z = 5230683
33
XDOT = -3676
182351 XDOT = -1041
608361
YDOT = -24658
424891 feet/sec YDOT = -7527
976942 meter/sec
ZDOT = 3536
373041 ZDOT = 1072
635368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7746631
38 X = 2361173
24
Y = -11828719
22 feet Y = -3605393
62 meter
Z = 17137900
18 Z = 5223631
97
XDOT = 17351
409555 XDOT = 5288
709632
YDOT = 16463
308078 feet/sec YDOT = 5018
016302 meter/sec
ZDOT = 3514
214175 ZDOT = 1071
132480
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 17302
55355632
00016717 00000-0 10270-3 0 9105
2 25544 51
6380 88
4871 0005154 70
9138 289
2572 15
54263905 2641
Satellite: ISS
Catalog Number: 25544
Epoch time: 17302
55355632 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 88
4871 deg
Eccentricity:
0005154
Arg of perigee: 70
9138 deg
Mean anomaly: 289
2572 deg
Mean motion: 15
54263905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 264
Checksum: 310
Coasting Arc #12 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2017/303/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4228236
48 A = 6777201
03 meter
Y = 512229
21 meter E =
0019411
Z = -5288382
37 I = 51
99389
XDOT = 223
161967 Wp = 91
09713
YDOT = 7595
980370 meter/sec RA = 82
90801 deg
ZDOT = 916
705076 TA = 187
63055
MA = 187
66013
Ha = 222
660 n
mi
Hp = 212
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13872166
93 X = 4247883
14
Y = 1680542
04 feet Y = 559621
76 meter
Z = -17350335
87 Z = -5267794
88
XDOT = 732
158684 XDOT = 133
752121
YDOT = 24921
195441 feet/sec YDOT = 7597
976058 meter/sec
ZDOT = 3007
562586 ZDOT = 917
571494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11875630
36 X = -3619692
13
Y = 7575664
98 feet Y = 2309062
69 meter
Z = -17259029
39 Z = -5260552
16
XDOT = -15810
086161 XDOT = -4818
914262
YDOT = -17945
026918 feet/sec YDOT = -5469
644205 meter/sec
ZDOT = 3010
233247 ZDOT = 917
519094
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 17303
51800243
00016717 00000-0 10270-3 0 9116
2 25544 51
6391 83
6790 0005265 74
7725 285
4009 15
54279015 2795
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
51800243 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 83
6790 deg
Eccentricity:
0005265
Arg of perigee: 74
7725 deg
Mean anomaly: 285
4009 deg
Mean motion: 15
54279015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 305
Coasting Arc #13 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2017/303/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2304926
47 A = 6782532
77 meter
Y = -5065951
07 meter E =
0011794
Z = -3888800
47 I = 52
01241
XDOT = 4035
438348 Wp = 73
77898
YDOT = 5015
054736 meter/sec RA = 81
39561 deg
ZDOT = -4148
493285 TA = 152
83254
MA = 152
77078
Ha = 222
716 n
mi
Hp = 212
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7562094
72 X = 2380294
20
Y = -16620574
37 feet Y = -5039754
66 meter
Z = -12758531
73 Z = -3877420
26
XDOT = 13239
627125 XDOT = 3999
210439
YDOT = 16453
591655 feet/sec YDOT = 5059
978921 meter/sec
ZDOT = -13610
542275 ZDOT = -4128
978371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14541888
31 X = 4432367
56
Y = -11102643
99 feet Y = -3384085
89 meter
Z = -12707229
50 Z = -3873163
55
XDOT = 3257
886491 XDOT = 993
003803
YDOT = 19719
224764 feet/sec YDOT = 6010
419708 meter/sec
ZDOT = -13524
696074 ZDOT = -4122
327363
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 17303
83948254
00016717 00000-0 10270-3 0 9127
2 25544 51
6410 82
0792 0005444 72
8573 287
3175 15
54281985 2841
Satellite: ISS
Catalog Number: 25544
Epoch time: 17303
83948254 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 82
0792 deg
Eccentricity:
0005444
Arg of perigee: 72
8573 deg
Mean anomaly: 287
3175 deg
Mean motion: 15
54281985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 322
Coasting Arc #14 (Orbit 299)
---------------------------------------
Vector Time (GMT): 2017/304/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3030929
45 A = 6778953
34 meter
Y = 3618406
30 meter E =
0011773
Z = 4856593
50 I = 51
99257
XDOT = -3540
551089 Wp = 100
82187
YDOT = -6333
786020 meter/sec RA = 76
42825 deg
ZDOT = 2502
107809 TA = 324
70008
MA = 324
77798
Ha = 222
893 n
mi
Hp = 212
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9943994
27 X = -3094757
61
Y = 11871411
76 feet Y = 3584155
86 meter
Z = 15933705
72 Z = 4841714
59
XDOT = -11615
981262 XDOT = -3481
616120
YDOT = -20780
137861 feet/sec YDOT = -6373
049169 meter/sec
ZDOT = 8209
015123 ZDOT = 2485
052179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14338153
38 X = -4370269
15
Y = 6029028
07 feet Y = 1837647
76 meter
Z = 15867091
59 Z = 4836289
52
XDOT = -544
682735 XDOT = -166
019297
YDOT = -22766
150479 feet/sec YDOT = -6939
122666 meter/sec
ZDOT = 8134
302654 ZDOT = 2479
335449
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 17304
86822042
00016717 00000-0 10270-3 0 9138
2 25544 51
6391 76
9494 0005565 76
4648 283
7124 15
54275877 3003
Satellite: ISS
Catalog Number: 25544
Epoch time: 17304
86822042 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 76
9494 deg
Eccentricity:
0005565
Arg of perigee: 76
4648 deg
Mean anomaly: 283
7124 deg
Mean motion: 15
54275877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 300
Checksum: 325
Coasting Arc #15 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2017/305/19:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 920041
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3747125
45 A = 6777061
82 meter
Y = -1924251
65 meter E =
0020029
Z = -5326258
03 I = 51
97827
XDOT = 2840
128974 Wp = 83
94698
YDOT = 7085
164188 meter/sec RA = 71
45287 deg
ZDOT = -561
374969 TA = 180
70936
MA = 180
71221
Ha = 222
719 n
mi
Hp = 212
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12293718
67 X = 3794237
44
Y = -6313161
58 feet Y = -1882085
70 meter
Z = -17474599
84 Z = -5307940
64
XDOT = 9318
008444 XDOT = 2763
416640
YDOT = 23245
289331 feet/sec YDOT = 7116
495485 meter/sec
ZDOT = -1841
781395 ZDOT = -547
765002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13920395
10 X = 4242936
43
Y = -244510
77 feet Y = -74526
88 meter
Z = -17392986
58 Z = -5301382
31
XDOT = -1807
153959 XDOT = -550
820527
YDOT = 23968
542141 feet/sec YDOT = 7305
611644 meter/sec
ZDOT = -1782
497984 ZDOT = -543
305385
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 17305
83265877
00016717 00000-0 10270-3 0 9144
2 25544 51
6399 72
1412 0005332 79
4922 280
6832 15
54265195 3159
Satellite: ISS
Catalog Number: 25544
Epoch time: 17305
83265877 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 72
1412 deg
Eccentricity:
0005332
Arg of perigee: 79
4922 deg
Mean anomaly: 280
6832 deg
Mean motion: 15
54265195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 317
Coasting Arc #16 (Orbit 319)
---------------------------------------
Vector Time (GMT): 2017/306/03:17:54
191
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3775641
88 A = 6777518
37 meter
Y = -1829997
13 meter E =
0019115
Z = -5339109
85 I = 51
97643
XDOT = 2903
160742 Wp = 84
77158
YDOT = 7072
636352 meter/sec RA = 69
85519 deg
ZDOT = -370
596111 TA = 181
70145
MA = 181
70796
Ha = 222
634 n
mi
Hp = 213
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12387276
53 X = 3821760
24
Y = -6003927
60 feet Y = -1787517
83 meter
Z = -17516764
61 Z = -5320656
34
XDOT = 9524
805584 XDOT = 2825
657082
YDOT = 23204
187505 feet/sec YDOT = 7104
668103 meter/sec
ZDOT = -1215
866507 ZDOT = -356
681827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6049506
44 X = -1843889
56
Y = -12480719
07 feet Y = -3804123
17 meter
Z = -17434561
43 Z = -5314054
32
XDOT = 22260
161833 XDOT = 6784
897327
YDOT = -9173
361318 feet/sec YDOT = -2796
040530 meter/sec
ZDOT = -1155
235999 ZDOT = -352
115933
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 17306
15413878
00016717 00000-0 10270-3 0 9157
2 25544 51
6416 70
5389 0004359 77
0557 283
1082 15
54088470 3200
Satellite: ISS
Catalog Number: 25544
Epoch time: 17306
15413878 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 70
5389 deg
Eccentricity:
0004359
Arg of perigee: 77
0557 deg
Mean anomaly: 283
1082 deg
Mean motion: 15
54088470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 320
Checksum: 311
Coasting Arc #17 (Orbit 335)
---------------------------------------
Vector Time (GMT): 2017/307/03:17:54
191
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4389970
48 A = 6778167
96 meter
Y = 138121
38 meter E =
0008933
Z = 5156412
50 I = 51
96736
XDOT = -2052
663695 Wp = 66
15950
YDOT = -7230
359058 meter/sec RA = 64
87864 deg
ZDOT = -1548
255898 TA = 38
71402
MA = 38
65003
Ha = 222
721 n
mi
Hp = 213
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14402790
30 X = -4416236
79
Y = 453154
14 feet Y = 88883
14 meter
Z = 16917363
83 Z = 5135022
94
XDOT = -6734
460943 XDOT = -1964
138435
YDOT = -23721
650453 feet/sec YDOT = -7252
818452 meter/sec
ZDOT = -5079
579718 ZDOT = -1558
011999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 755373
99 X = 230237
99
Y = 14501005
06 feet Y = 4419906
34 meter
Z = 16822401
10 Z = 5127467
86
XDOT = -22520
613462 XDOT = -6864
282983
YDOT = 7136
284255 feet/sec YDOT = 2175
139441 meter/sec
ZDOT = -5121
708933 ZDOT = -1561
096883
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 17307
18300613
00016717 00000-0 10270-3 0 9164
2 25544 51
6422 65
4103 0004296 79
4988 280
6649 15
54122929 3364
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
18300613 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 65
4103 deg
Eccentricity:
0004296
Arg of perigee: 79
4988 deg
Mean anomaly: 280
6649 deg
Mean motion: 15
54122929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 336
Checksum: 312
Coasting Arc #18 (Orbit 337)
---------------------------------------
Vector Time (GMT): 2017/307/06:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 624694
61 A = 6786320
29 meter
Y = 6183435
43 meter E =
0017714
Z = 2705579
45 I = 51
99062
XDOT = -5356
198224 Wp = 78
62790
YDOT = -1748
920162 meter/sec RA = 64
33982 deg
ZDOT = 5208
398100 TA = 311
80957
MA = 311
96073
Ha = 222
591 n
mi
Hp = 213
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2049522
99 X = 542360
57
Y = 20286861
65 feet Y = 6189960
97 meter
Z = 8876573
01 Z = 2708413
83
XDOT = -17572
828819 XDOT = -5361
543854
YDOT = -5737
927041 feet/sec YDOT = -1808
846458 meter/sec
ZDOT = 17087
920274 ZDOT = 5182
365666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13525818
93 X = 4122669
61
Y = -15251357
50 feet Y = -4648613
77 meter
Z = 8888147
46 Z = 2709107
35
XDOT = 6702
108423 XDOT = 2042
802647
YDOT = 15883
521054 feet/sec YDOT = 4841
297217 meter/sec
ZDOT = 16972
656788 ZDOT = 5173
265789
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 17307
31161393
00016717 00000-0 10270-3 0 9170
2 25544 51
6401 64
7677 0004205 80
0445 280
1182 15
54094067 3385
Satellite: ISS
Catalog Number: 25544
Epoch time: 17307
31161393 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 64
7677 deg
Eccentricity:
0004205
Arg of perigee: 80
0445 deg
Mean anomaly: 280
1182 deg
Mean motion: 15
54094067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 338
Checksum: 289
Coasting Arc #19 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2017/308/06:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 919921
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 449844
71 A = 6782584
99 meter
Y = -5440507
20 meter E =
0011303
Z = -4036645
22 I = 51
96171
XDOT = 5608
215121 Wp = 76
20810
YDOT = 3395
640919 meter/sec RA = 59
38101 deg
ZDOT = -3958
254018 TA = 152
80768
MA = 152
74844
Ha = 222
642 n
mi
Hp = 213
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1475868
46 X = 530257
16
Y = -17849433
08 feet Y = -5435027
22 meter
Z = -13243586
69 Z = -4034264
49
XDOT = 18399
655909 XDOT = 5589
055220
YDOT = 11140
554195 feet/sec YDOT = 3458
248577 meter/sec
ZDOT = -12986
397697 ZDOT = -3931
056791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13963223
29 X = -4255990
46
Y = 11229979
35 feet Y = 3422897
71 meter
Z = -13232119
87 Z = -4033150
14
XDOT = -3939
235673 XDOT = -1200
679033
YDOT = -20032
336716 feet/sec YDOT = -6105
856231 meter/sec
ZDOT = -12866
243728 ZDOT = -3921
631088
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 17308
27617560
00016717 00000-0 10270-3 0 9189
2 25544 51
6388 59
9599 0004292 83
9224 276
2418 15
54080325 3538
Satellite: ISS
Catalog Number: 25544
Epoch time: 17308
27617560 = yrday
fracday
Element set: 918
Inclination: 51
6388 deg
RA of node: 59
9599 deg
Eccentricity:
0004292
Arg of perigee: 83
9224 deg
Mean anomaly: 276
2418 deg
Mean motion: 15
54080325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 331
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