[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 14th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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
286/19:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
287/08:46:53
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
9
289/11:09:57
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
7
290/03:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
7
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
5
000/00:00:00
000 0
0 0
0 212
8
Coasting Arc #1 (Orbit 14)
---------------------------------------
Vector Time (GMT): 2017/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2359486
05 A = 6779774
99 meter
Y = -4308312
00 meter E =
0011717
Z = 4669865
29 I = 51
70738
XDOT = 7071
400624 Wp = 44
15826
YDOT = 740
852767 meter/sec RA = 167
35078 deg
ZDOT = -2876
824957 TA = 74
45387
MA = 74
32455
Ha = 221
808 n
mi
Hp = 213
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7741095
96 X = 2384803
27
Y = -14134881
87 feet Y = -4281784
77 meter
Z = 15321080
34 Z = 4681388
79
XDOT = 23200
133280 XDOT = 7076
564976
YDOT = 2430
619315 feet/sec YDOT = 819
958697 meter/sec
ZDOT = -9438
402089 ZDOT = -2842
461487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1964475
23 X = -598772
05
Y = 15946016
56 feet Y = 4860345
85 meter
Z = 15372714
40 Z = 4685603
35
XDOT = -21384
682885 XDOT = -6518
051343
YDOT = 6357
402622 feet/sec YDOT = 1937
736319 meter/sec
ZDOT = -9286
161121 ZDOT = -2830
421910
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 17286
54323982
00016717 00000-0 10270-3 0 9007
2 25544 51
6417 168
3158 0005003 10
6567 349
4691 15
54209732 151
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
54323982 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 168
3158 deg
Eccentricity:
0005003
Arg of perigee: 10
6567 deg
Mean anomaly: 349
4691 deg
Mean motion: 15
54209732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 15
Checksum: 302
Coasting Arc #2 (Orbit 19)
---------------------------------------
Vector Time (GMT): 2017/286/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 264904
82 A = 6777694
06 meter
Y = -4315897
40 meter E =
0007863
Z = 5216385
94 I = 51
70859
XDOT = 7521
391993 Wp = 35
11151
YDOT = -957
017412 meter/sec RA = 165
77128 deg
ZDOT = -1166
609768 TA = 66
10190
MA = 66
01953
Ha = 221
909 n
mi
Hp = 214
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 869110
31 X = 287807
79
Y = -14159768
38 feet Y = -4312806
66 meter
Z = 17114127
09 Z = 5217728
69
XDOT = 24676
482917 XDOT = 7537
201476
YDOT = -3139
820907 feet/sec YDOT = -872
819754 meter/sec
ZDOT = -3827
459868 ZDOT = -1130
034416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10327103
67 X = 3147701
20
Y = -9715075
12 feet Y = -2961154
90 meter
Z = 17120630
39 Z = 5218368
14
XDOT = 19321
804497 XDOT = 5889
286011
YDOT = 14038
576694 feet/sec YDOT = 4278
958176 meter/sec
ZDOT = -3665
189988 ZDOT = -1117
149908
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 17286
86474550
00016717 00000-0 10270-3 0 9011
2 25544 51
6403 166
7073 0004523 16
2452 343
8845 15
54151771 209
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
86474550 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 166
7073 deg
Eccentricity:
0004523
Arg of perigee: 16
2452 deg
Mean anomaly: 343
8845 deg
Mean motion: 15
54151771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 20
Checksum: 294
Coasting Arc #3 (Orbit 27)
---------------------------------------
Vector Time (GMT): 2017/287/08:46:53
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -643725
66 A = 6778133
78 meter
Y = 4415003
92 meter E =
0014701
Z = -5114720
14 I = 51
72731
XDOT = -7418
954273 Wp = 82
76260
YDOT = 868
362517 meter/sec RA = 163
04582 deg
ZDOT = 1689
267843 TA = 203
52186
MA = 203
58916
Ha = 222
061 n
mi
Hp = 213
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2111960
82 X = -668202
57
Y = 14484920
99 feet Y = 4407668
09 meter
Z = -16780577
89 Z = -5117906
97
XDOT = -24340
401157 XDOT = -7436
318841
YDOT = 2848
958390 feet/sec YDOT = 785
301743 meter/sec
ZDOT = 5542
217332 ZDOT = 1653
186341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8159809
12 X = 2487109
82
Y = -12132498
85 feet Y = -3697985
65 meter
Z = -16795270
04 Z = -5119198
31
XDOT = 22265
935526 XDOT = 6786
657148
YDOT = 7551
621461 feet/sec YDOT = 2301
734221 meter/sec
ZDOT = 5382
136977 ZDOT = 1640
475350
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 17287
37914935
00016717 00000-0 10270-3 0 9025
2 25544 51
6401 164
1471 0005056 16
1207 344
0105 15
54166171 280
Satellite: ISS
Catalog Number: 25544
Epoch time: 17287
37914935 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 164
1471 deg
Eccentricity:
0005056
Arg of perigee: 16
1207 deg
Mean anomaly: 344
0105 deg
Mean motion: 15
54166171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 28
Checksum: 279
Coasting Arc #4 (Orbit 43)
---------------------------------------
Vector Time (GMT): 2017/288/08:46:53
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2343374
33 A = 6781132
94 meter
Y = -4639249
03 meter E =
0013287
Z = 4350804
90 I = 51
76812
XDOT = 6839
434982 Wp = 54
35048
YDOT = 189
441502 meter/sec RA = 158
05972 deg
ZDOT = -3466
774846 TA = 70
84856
MA = 70
70478
Ha = 222
087 n
mi
Hp = 213
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7688236
00 X = 2373943
22
Y = -15220633
30 feet Y = -4612872
49 meter
Z = 14274294
31 Z = 4362263
07
XDOT = 22439
091147 XDOT = 6853
648316
YDOT = 621
527236 feet/sec YDOT = 266
003881 meter/sec
ZDOT = -11373
933222 ZDOT = -3433
516198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13327506
22 X = -4062223
90
Y = 10568076
05 feet Y = 3221149
58 meter
Z = 14325692
85 Z = 4366471
18
XDOT = -19358
973280 XDOT = -5900
615056
YDOT = -9129
147354 feet/sec YDOT = -2782
564114 meter/sec
ZDOT = -11226
486216 ZDOT = -3421
832999
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 17288
40795562
00016717 00000-0 10270-3 0 9034
2 25544 51
6399 159
0194 0005039 20
1249 340
0101 15
54165100 444
Satellite: ISS
Catalog Number: 25544
Epoch time: 17288
40795562 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 159
0194 deg
Eccentricity:
0005039
Arg of perigee: 20
1249 deg
Mean anomaly: 340
0101 deg
Mean motion: 15
54165100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 44
Checksum: 282
Coasting Arc #5 (Orbit 58)
---------------------------------------
Vector Time (GMT): 2017/289/08:46:53
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3750214
14 A = 6784868
53 meter
Y = 4689648
65 meter E =
0008429
Z = -3157865
94 I = 51
81133
XDOT = -5772
663287 Wp = 49
73504
YDOT = -1354
608801 meter/sec RA = 153
08422 deg
ZDOT = 4857
650817 TA = 273
95184
MA = 274
04819
Ha = 222
102 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12303852
18 X = -3787036
78
Y = 15385986
40 feet Y = 4647504
97 meter
Z = -10360452
57 Z = -3176173
47
XDOT = -18939
184011 XDOT = -5780
683010
YDOT = -4444
254598 feet/sec YDOT = -1419
206987 meter/sec
ZDOT = 15937
174596 ZDOT = 4829
589356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17448568
60 X = 5318323
71
Y = -9053146
12 feet Y = -2759398
94 meter
Z = -10442237
92 Z = -3182794
12
XDOT = 14912
627215 XDOT = 4545
368775
YDOT = 10554
618094 feet/sec YDOT = 3217
047595 meter/sec
ZDOT = 15812
909280 ZDOT = 4819
774749
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 17289
37245749
00016717 00000-0 10270-3 0 9049
2 25544 51
6404 154
2109 0004999 22
6605 337
4767 15
54184005 590
Satellite: ISS
Catalog Number: 25544
Epoch time: 17289
37245749 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 154
2109 deg
Eccentricity:
0004999
Arg of perigee: 22
6605 deg
Mean anomaly: 337
4767 deg
Mean motion: 15
54184005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 59
Checksum: 323
Coasting Arc #6 (Orbit 60)
---------------------------------------
Vector Time (GMT): 2017/289/11:09:57
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5012447
65 A = 6787799
22 meter
Y = -4198542
83 meter E =
0014789
Z = 1807022
73 I = 51
82476
XDOT = 4366
384890 Wp = 94
61459
YDOT = 2756
480630 meter/sec RA = 152
59927 deg
ZDOT = -5668
480486 TA = 65
57847
MA = 65
42424
Ha = 222
168 n
mi
Hp = 213
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16445038
22 X = 5050246
60
Y = -13774746
81 feet Y = -4142278
67 meter
Z = 5928552
27 Z = 1831464
19
XDOT = 14325
409745 XDOT = 4362
771694
YDOT = 9043
571622 feet/sec YDOT = 2805
287715 meter/sec
ZDOT = -18597
376923 ZDOT = -5647
278768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13247648
55 X = -4037883
28
Y = 16833874
89 feet Y = 5130965
07 meter
Z = 6037476
93 Z = 1840222
97
XDOT = -14761
484389 XDOT = -4499
300442
YDOT = -4935
628634 feet/sec YDOT = -1504
379608 meter/sec
ZDOT = -18503
709980 ZDOT = -5639
930802
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 17289
50105737
00016717 00000-0 10270-3 0 9057
2 25544 51
6415 153
5710 0004974 23
6522 336
4859 15
54161821 619
Satellite: ISS
Catalog Number: 25544
Epoch time: 17289
50105737 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 153
5710 deg
Eccentricity:
0004974
Arg of perigee: 23
6522 deg
Mean anomaly: 336
4859 deg
Mean motion: 15
54161821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 61
Checksum: 300
Coasting Arc #7 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2205098
61 A = 6777257
18 meter
Y = 3572493
88 meter E =
0017790
Z = -5335230
42 I = 51
80546
XDOT = -6558
740122 Wp = 75
31341
YDOT = 3948
523934 meter/sec RA = 149
31973 deg
ZDOT = -62
617927 TA = 194
06548
MA = 194
11508
Ha = 222
256 n
mi
Hp = 213
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7234575
51 X = 2190902
45
Y = 11720780
46 feet Y = 3597072
83 meter
Z = -17504036
81 Z = -5324553
47
XDOT = -21518
176253 XDOT = -6602
101938
YDOT = 12954
474850 feet/sec YDOT = 3874
937165 meter/sec
ZDOT = -205
439394 ZDOT = -94
584468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13476430
06 X = 4107615
88
Y = -3121051
32 feet Y = -951296
44 meter
Z = -17457146
20 Z = -5320938
16
XDOT = 4993
444292 XDOT = 1522
001820
YDOT = 23583
773049 feet/sec YDOT = 7188
334025 meter/sec
ZDOT = -347
712432 ZDOT = -105
982749
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 17290
14405468
00016717 00000-0 10270-3 0 9064
2 25544 51
6384 150
3636 0004984 27
6565 332
4852 15
54165257 715
Satellite: ISS
Catalog Number: 25544
Epoch time: 17290
14405468 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 150
3636 deg
Eccentricity:
0004984
Arg of perigee: 27
6565 deg
Mean anomaly: 332
4852 deg
Mean motion: 15
54165257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 71
Checksum: 313
Coasting Arc #8 (Orbit 86)
---------------------------------------
Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -590278
76 A = 6778299
05 meter
Y = -4469267
07 meter E =
0010294
Z = 5057875
78 I = 51
83564
XDOT = 6784
676110 Wp = 43
56269
YDOT = -3043
304191 meter/sec RA = 144
33216 deg
ZDOT = -1887
773328 TA = 64
72855
MA = 64
62191
Ha = 222
274 n
mi
Hp = 213
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1936610
10 X = -564827
48
Y = -14662949
71 feet Y = -4475725
09 meter
Z = 16594080
63 Z = 5055070
66
XDOT = 22259
436056 XDOT = 6827
372940
YDOT = -9984
593801 feet/sec YDOT = -2967
194791 meter/sec
ZDOT = -6193
482046 ZDOT = -1854
710827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14573044
94 X = -4441864
10
Y = -2602388
42 feet Y = -793207
99 meter
Z = 16582219
41 Z = 5054260
48
XDOT = -2766
753830 XDOT = -843
306567
YDOT = -23234
094757 feet/sec YDOT = -7081
752082 meter/sec
ZDOT = -6046
449935 ZDOT = -1842
957940
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 17291
17284810
00016717 00000-0 10270-3 0 9075
2 25544 51
6371 145
2343 0005041 29
7025 330
4413 15
54189785 878
Satellite: ISS
Catalog Number: 25544
Epoch time: 17291
17284810 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 145
2343 deg
Eccentricity:
0005041
Arg of perigee: 29
7025 deg
Mean anomaly: 330
4413 deg
Mean motion: 15
54189785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 87
Checksum: 297
Coasting Arc #9 (Orbit 101)
---------------------------------------
Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -906595
69 A = 6781459
57 meter
Y = 5196099
89 meter E =
0010691
Z = -4270539
52 I = 51
87158
XDOT = -6497
823629 Wp = 82
85294
YDOT = 1833
867650 meter/sec RA = 139
35345 deg
ZDOT = 3619
804043 TA = 224
02290
MA = 224
10809
Ha = 222
368 n
mi
Hp = 213
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2974395
30 X = -943887
84
Y = 17047571
83 feet Y = 5185752
75 meter
Z = -14010956
42 Z = -4275034
71
XDOT = -21318
318994 XDOT = -6535
431111
YDOT = 6016
626147 feet/sec YDOT = 1760
994664 meter/sec
ZDOT = 11875
997517 ZDOT = 3588
147401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15447820
76 X = 4708495
77
Y = 7762300
65 feet Y = 2365949
24 meter
Z = -14031577
06 Z = -4276824
69
XDOT = 33
566952 XDOT = 10
231207
YDOT = 21093
068306 feet/sec YDOT = 6429
167220 meter/sec
ZDOT = 11735
343981 ZDOT = 3576
932845
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 17292
13733941
00016717 00000-0 10270-3 0 9087
2 25544 51
6367 140
4263 0005111 33
2755 326
8718 15
54170491 1028
Satellite: ISS
Catalog Number: 25544
Epoch time: 17292
13733941 = yrday
fracday
Element set: 908
Inclination: 51
6367 deg
RA of node: 140
4263 deg
Eccentricity:
0005111
Arg of perigee: 33
2755 deg
Mean anomaly: 326
8718 deg
Mean motion: 15
54170491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 102
Checksum: 289
Coasting Arc #10 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2254660
11 A = 6785249
82 meter
Y = -5653139
41 meter E =
0016231
Z = 2989030
46 I = 51
90899
XDOT = 5809
947762 Wp = 81
14662
YDOT = -337
723934 meter/sec RA = 134
38512 deg
ZDOT = -4995
713491 TA = 64
78995
MA = 64
62176
Ha = 222
319 n
mi
Hp = 213
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7397178
85 X = 2303187
85
Y = -18547045
31 feet Y = -5627654
64 meter
Z = 9806530
38 Z = 3000101
58
XDOT = 19061
508407 XDOT = 5837
559802
YDOT = -1108
018157 feet/sec YDOT = -272
599220 meter/sec
ZDOT = -16390
136126 ZDOT = -4967
422769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15786260
06 X = -4811652
07
Y = -12187070
66 feet Y = -3714619
14 meter
Z = 9856393
08 Z = 3004228
61
XDOT = 3359
852493 XDOT = 1024
083040
YDOT = -17573
645606 feet/sec YDOT = -5356
447181 meter/sec
ZDOT = -16264
598253 ZDOT = -4957
449548
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
16612469
00016717 00000-0 10270-3 0 9093
2 25544 51
6368 135
2963 0005117 35
7243 324
4251 15
54216276 1188
Satellite: ISS
Catalog Number: 25544
Epoch time: 17293
16612469 = yrday
fracday
Element set: 909
Inclination: 51
6368 deg
RA of node: 135
2963 deg
Eccentricity:
0005117
Arg of perigee: 35
7243 deg
Mean anomaly: 324
4251 deg
Mean motion: 15
54216276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 118
Checksum: 305
Coasting Arc #11 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3286977
68 A = 6788170
03 meter
Y = 5758598
43 meter E =
0013600
Z = -1428599
50 I = 51
94100
XDOT = -4817
429275 Wp = 39
09129
YDOT = -1315
917472 meter/sec RA = 129
42906 deg
ZDOT = 5820
082236 TA = 305
39336
MA = 305
52033
Ha = 222
404 n
mi
Hp = 213
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10784047
52 X = -3344187
95
Y = 18893039
47 feet Y = 5721521
21 meter
Z = -4687006
23 Z = -1444706
45
XDOT = -15805
214156 XDOT = -4830
628151
YDOT = -4317
314541 feet/sec YDOT = -1369
862598 meter/sec
ZDOT = 19094
757993 ZDOT = 5796
648081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15436376
60 X = 4705007
59
Y = 15306161
05 feet Y = 4665317
89 meter
Z = -4759239
41 Z = -1450616
17
XDOT = -7203
025918 XDOT = -2195
482300
YDOT = 13128
763460 feet/sec YDOT = 4001
647103 meter/sec
ZDOT = 18990
977895 ZDOT = 5788
450062
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
13060686
00016717 00000-0 10270-3 0 9101
2 25544 51
6369 130
4880 0005168 40
6948 319
4590 15
54219057 1334
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
13060686 = yrday
fracday
Element set: 910
Inclination: 51
6369 deg
RA of node: 130
4880 deg
Eccentricity:
0005168
Arg of perigee: 40
6948 deg
Mean anomaly: 319
4590 deg
Mean motion: 15
54219057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 309
Coasting Arc #12 (Orbit 136)
---------------------------------------
Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3341067
14 A = 6777065
25 meter
Y = 2526240
42 meter E =
0018566
Z = -5343295
02 I = 51
91247
XDOT = -4693
209288 Wp = 77
06442
YDOT = 6047
457377 meter/sec RA = 128
23368 deg
ZDOT = -71
587623 TA = 192
23223
MA = 192
27737
Ha = 222
374 n
mi
Hp = 213
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10961506
37 X = 3338525
54
Y = 8288190
35 feet Y = 2563587
90 meter
Z = -17530495
49 Z = -5327071
08
XDOT = -15397
668268 XDOT = -4760
137012
YDOT = 19840
739427 feet/sec YDOT = 5994
600485 meter/sec
ZDOT = -234
867529 ZDOT = -94
549400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8146128
13 X = -2482939
85
Y = -11180143
78 feet Y = -3407707
83 meter
Z = -17458865
21 Z = -5321462
12
XDOT = 19738
932645 XDOT = 6016
426670
YDOT = -13835
429045 feet/sec YDOT = -4217
038773 meter/sec
ZDOT = -337
554510 ZDOT = -102
886615
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
38780094
00016717 00000-0 10270-3 0 9111
2 25544 51
6404 129
2067 0005156 38
4789 321
6731 15
54231097 1376
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
38780094 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 129
2067 deg
Eccentricity:
0005156
Arg of perigee: 38
4789 deg
Mean anomaly: 321
6731 deg
Mean motion: 15
54231097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 137
Checksum: 311
Coasting Arc #13 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2150875
97 A = 6778109
41 meter
Y = -3952233
52 meter E =
0010528
Z = 5064284
15 I = 51
93549
XDOT = 5233
842439 Wp = 48
93410
YDOT = -5282
423664 meter/sec RA = 123
25303 deg
ZDOT = -1890
290777 TA = 59
35295
MA = 59
24920
Ha = 222
391 n
mi
Hp = 213
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7056679
68 X = -2131121
66
Y = -12966645
42 feet Y = -3976175
35 meter
Z = 16615105
47 Z = 5053883
78
XDOT = 17171
399078 XDOT = 5301
705272
YDOT = -17330
786299 feet/sec YDOT = -5223
515926 meter/sec
ZDOT = -6201
741393 ZDOT = -1864
700576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3280402
38 X = 999866
65
Y = 14445852
86 feet Y = 4403095
95 meter
Z = 16569509
55 Z = 5050386
51
XDOT = -20296
611098 XDOT = -6186
407063
YDOT = 11626
454443 feet/sec YDOT = 3543
743314 meter/sec
ZDOT = -6087
475795 ZDOT = -1855
462622
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
41657567
00016717 00000-0 10270-3 0 9125
2 25544 51
6401 124
0776 0005061 41
1951 318
9583 15
54259479 1536
Satellite: ISS
Catalog Number: 25544
Epoch time: 17295
41657567 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 124
0776 deg
Eccentricity:
0005061
Arg of perigee: 41
1951 deg
Mean anomaly: 318
9583 deg
Mean motion: 15
54259479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 315
Coasting Arc #14 (Orbit 167)
---------------------------------------
Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1008824
31 A = 6781319
45 meter
Y = 5177373
48 meter E =
0011286
Z = -4271064
78 I = 51
96339
XDOT = -5400
109518 Wp = 86
21817
YDOT = 4040
813209 meter/sec RA = 118
27950 deg
ZDOT = 3631
734379 TA = 220
74904
MA = 220
83351
Ha = 222
417 n
mi
Hp = 213
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3309791
06 X = 971601
84
Y = 16986133
45 feet Y = 5188446
54 meter
Z = -14012679
73 Z = -4266254
72
XDOT = -17716
894745 XDOT = -5462
535265
YDOT = 13257
261183 feet/sec YDOT = 3980
076603 meter/sec
ZDOT = 11915
139038 ZDOT = 3605
349845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1155139
42 X = 352086
50
Y = -17283702
68 feet Y = -5268072
58 meter
Z = -13992066
12 Z = -4264781
75
XDOT = 19380
737900 XDOT = 5907
248912
YDOT = -8231
530224 feet/sec YDOT = -2508
970412 meter/sec
ZDOT = 11797
501052 ZDOT = 3595
878321
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
38105013
00016717 00000-0 10270-3 0 9137
2 25544 51
6404 119
2687 0005061 44
0985 316
0570 15
54234006 1685
Satellite: ISS
Catalog Number: 25544
Epoch time: 17296
38105013 = yrday
fracday
Element set: 913
Inclination: 51
6404 deg
RA of node: 119
2687 deg
Eccentricity:
0005061
Arg of perigee: 44
0985 deg
Mean anomaly: 316
0570 deg
Mean motion: 15
54234006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 168
Checksum: 286
Coasting Arc #15 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 91275
37 A = 6785177
37 meter
Y = -6090407
93 meter E =
0016987
Z = 2977357
71 I = 51
99160
XDOT = 5293
796425 Wp = 83
69823
YDOT = -2384
158964 meter/sec RA = 113
31697 deg
ZDOT = -5012
984563 TA = 62
42887
MA = 62
25642
Ha = 222
454 n
mi
Hp = 212
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 299459
88 X = 144910
26
Y = -19981653
32 feet Y = -6089087
25 meter
Z = 9768233
96 Z = 2977931
57
XDOT = 17368
098507 XDOT = 5344
414491
YDOT = -7822
043845 feet/sec YDOT = -2324
677246 meter/sec
ZDOT = -16446
799747 ZDOT = -4987
145299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5117179
69 X = -1559716
37
Y = 19315895
78 feet Y = 5887485
03 meter
Z = 9771651
99 Z = 2978399
53
XDOT = -17450
187547 XDOT = -5318
817164
YDOT = 3682
725247 feet/sec YDOT = 1122
494655 meter/sec
ZDOT = -16331
798685 ZDOT = -4977
932239
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
40981609
00016717 00000-0 10270-3 0 9145
2 25544 51
6409 114
1389 0005231 46
8319 313
3265 15
54263594 1846
Satellite: ISS
Catalog Number: 25544
Epoch time: 17297
40981609 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 114
1389 deg
Eccentricity:
0005231
Arg of perigee: 46
8319 deg
Mean anomaly: 313
3265 deg
Mean motion: 15
54263594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 315
Coasting Arc #16 (Orbit 198)
---------------------------------------
Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1020080
66 A = 6788201
53 meter
Y = 6557112
77 meter E =
0013636
Z = -1405837
27 I = 52
01190
XDOT = -4955
883164 Wp = 42
58403
YDOT = 470
442566 meter/sec RA = 108
36563 deg
ZDOT = 5832
924919 TA = 302
17006
MA = 302
30226
Ha = 222
533 n
mi
Hp = 212
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3346721
33 X = -1086499
21
Y = 21512837
16 feet Y = 6545334
13 meter
Z = -4612326
99 Z = -1410954
09
XDOT = -16259
459199 XDOT = -4989
109559
YDOT = 1543
446740 feet/sec YDOT = 414
836853 meter/sec
ZDOT = 19136
892778 ZDOT = 5808
769530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8133230
21 X = 2479008
57
Y = -20189959
24 feet Y = -6153899
58 meter
Z = -4635987
36 Z = -1413048
95
XDOT = 14833
227535 XDOT = 4521
167753
YDOT = 1637
781965 feet/sec YDOT = 499
195943 meter/sec
ZDOT = 19029
627580 ZDOT = 5800
230486
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
37428188
00016717 00000-0 10270-3 0 9151
2 25544 51
6394 109
3303 0005165 50
3991 309
7618 15
54223788 1991
Satellite: ISS
Catalog Number: 25544
Epoch time: 17298
37428188 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 109
3303 deg
Eccentricity:
0005165
Arg of perigee: 50
3991 deg
Mean anomaly: 309
7618 deg
Mean motion: 15
54223788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 199
Checksum: 336
Coasting Arc #17 (Orbit 214)
---------------------------------------
Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1853076
65 A = 6789007
10 meter
Y = -6517318
37 meter E =
0013004
Z = -371210
73 I = 52
02459
XDOT = 4456
259797 Wp = 115
18737
YDOT = 1600
772103 meter/sec RA = 103
42106 deg
ZDOT = -6028
878025 TA = 68
79199
MA = 68
65313
Ha = 222
529 n
mi
Hp = 212
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6079647
81 X = 1927620
52
Y = -21382278
13 feet Y = -6496179
21 meter
Z = -1217882
97 Z = -362027
68
XDOT = 14620
274924 XDOT = 4467
314244
YDOT = 5251
876978 feet/sec YDOT = 1650
666724 meter/sec
ZDOT = -19779
783546 ZDOT = -6007
203655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10465897
73 X = -3190005
63
Y = 19614504
61 feet Y = 5978501
00 meter
Z = -1176166
67 Z = -358495
60
XDOT = -11878
029033 XDOT = -3620
423249
YDOT = -7483
605121 feet/sec YDOT = -2281
002841 meter/sec
ZDOT = -19683
825525 ZDOT = -5999
630020
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
40304143
00016717 00000-0 10270-3 0 9161
2 25544 51
6402 104
2013 0004989 55
1977 304
9644 15
54219387 2158
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
40304143 = yrday
fracday
Element set: 916
Inclination: 51
6402 deg
RA of node: 104
2013 deg
Eccentricity:
0004989
Arg of perigee: 55
1977 deg
Mean anomaly: 304
9644 deg
Mean motion: 15
54219387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 215
Checksum: 303
Coasting Arc #18 (Orbit 216)
---------------------------------------
Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2957218
10 A = 6787128
14 meter
Y = -5750369
12 meter E =
0008994
Z = -2064960
48 I = 52
01757
XDOT = 3591
542329 Wp = 105
13730
YDOT = 3840
477458 meter/sec RA = 102
77657 deg
ZDOT = -5573
746750 TA = 97
56584
MA = 97
46367
Ha = 222
534 n
mi
Hp = 212
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9702159
13 X = 3031331
24
Y = -18866040
41 feet Y = -5716885
14 meter
Z = -6774804
74 Z = -2050414
82
XDOT = 11783
275356 XDOT = 3575
405204
YDOT = 12599
991659 feet/sec YDOT = 3880
550190 meter/sec
ZDOT = -18286
570701 ZDOT = -5556
339090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2998469
06 X = 913933
37
Y = 21022618
66 feet Y = 6407694
17 meter
Z = -6709399
35 Z = -2045024
92
XDOT = -15469
818699 XDOT = -4715
200739
YDOT = -3581
493563 feet/sec YDOT = -1091
639238 meter/sec
ZDOT = -18209
879369 ZDOT = -5550
371232
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
53163609
00016717 00000-0 10270-3 0 9176
2 25544 51
6379 103
5556 0005147 58
6387 301
5268 15
54273820 2174
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
53163609 = yrday
fracday
Element set: 917
Inclination: 51
6379 deg
RA of node: 103
5556 deg
Eccentricity:
0005147
Arg of perigee: 58
6387 deg
Mean anomaly: 301
5268 deg
Mean motion: 15
54273820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 217
Checksum: 324
Coasting Arc #19 (Orbit 232)
---------------------------------------
Vector Time (GMT): 2017/300/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3425856
91 A = 6783684
08 meter
Y = 4655538
56 meter E =
0016814
Z = 3534634
60 I = 52
01233
XDOT = -2812
035456 Wp = 83
92035
YDOT = -5520
919944 meter/sec RA = 97
82253 deg
ZDOT = 4529
537094 TA = 317
52702
MA = 317
65701
Ha = 222
617 n
mi
Hp = 212
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11239688
02 X = -3494831
58
Y = 15274076
63 feet Y = 4616842
71 meter
Z = 11596570
21 Z = 3517824
91
XDOT = -9225
838109 XDOT = -2772
092705
YDOT = -18113
254408 feet/sec YDOT = -5552
142596 meter/sec
ZDOT = 14860
686003 ZDOT = 4515
974019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 35468
95 X = 10810
93
Y = -19009672
42 feet Y = -5794148
15 meter
Z = 11521264
72 Z = 3511681
49
XDOT = 16869
730394 XDOT = 5141
893824
YDOT = 9035
552586 feet/sec YDOT = 2754
036428 meter/sec
ZDOT = 14801
312376 ZDOT = 4511
440012
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
56038924
00016717 00000-0 10270-3 0 9184
2 25544 51
6380 98
4258 0005033 64
3607 295
8065 15
54269555 2338
Satellite: ISS
Catalog Number: 25544
Epoch time: 17300
56038924 = yrday
fracday
Element set: 918
Inclination: 51
6380 deg
RA of node: 98
4258 deg
Eccentricity:
0005033
Arg of perigee: 64
3607 deg
Mean anomaly: 295
8065 deg
Mean motion: 15
54269555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 233
Checksum: 316
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