[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 28th 2018
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) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
242/21:54:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
1
249/00:35:06
532 0
6 0
7 0
7
N/A -0
2 -0
1 223
0
000/00:00:13
064 0
2 -0
0 213
7
249/22:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
8
253/11:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 959)
---------------------------------------
Vector Time (GMT): 2018/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -824202
65 A = 6779632
75 meter
Y = -4573932
20 meter E =
0017679
Z = -4951855
02 I = 51
77534
XDOT = 7233
572772 Wp = 82
43251
YDOT = 1117
229364 meter/sec RA = 22
73139 deg
ZDOT = -2240
528830 TA = 165
71703
MA = 165
66699
Ha = 223
461 n
mi
Hp = 212
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2704076
94 X = -748941
27
Y = -15006339
23 feet Y = -4582728
54 meter
Z = -16246243
51 Z = -4955675
54
XDOT = 23732
194133 XDOT = 7231
425143
YDOT = 3665
450669 feet/sec YDOT = 1198
108020 meter/sec
ZDOT = -7350
816370 ZDOT = -2205
396452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4041805
55 X = -1231942
33
Y = 14684335
41 feet Y = 4475785
43 meter
Z = -16262742
04 Z = -4956883
77
XDOT = -18885
161346 XDOT = -5756
197178
YDOT = -13147
875617 feet/sec YDOT = -4007
472488 meter/sec
ZDOT = -7193
260702 ZDOT = -2192
505862
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 18239
51994555
00016717 00000-0 10270-3 0 9003
2 25544 51
6399 23
2179 0005784 102
3716 257
8084 15
53893573 9601
Satellite: ISS
Catalog Number: 25544
Epoch time: 18239
51994555 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 23
2179 deg
Eccentricity:
0005784
Arg of perigee: 102
3716 deg
Mean anomaly: 257
8084 deg
Mean motion: 15
53893573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 960
Checksum: 338
Coasting Arc #2 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2018/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -795337
68 A = 6778094
08 meter
Y = 4136834
09 meter E =
0008346
Z = 5303269
44 I = 51
73887
XDOT = -7396
665610 Wp = 105
97753
YDOT = -1997
446503 meter/sec RA = 17
74341 deg
ZDOT = 446
000798 TA = 339
76149
MA = 339
79456
Ha = 223
468 n
mi
Hp = 213
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2609375
60 X = -867298
00
Y = 13572290
31 feet Y = 4127538
14 meter
Z = 17399177
96 Z = 5299230
90
XDOT = -24267
275624 XDOT = -7375
946291
YDOT = -6553
302176 feet/sec YDOT = -2080
045258 meter/sec
ZDOT = 1463
257211 ZDOT = 410
121247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8053093
62 X = 2454582
94
Y = -11261199
48 feet Y = -3432413
60 meter
Z = 17380459
37 Z = 5297564
02
XDOT = 18630
565475 XDOT = 5678
596357
YDOT = 15347
648399 feet/sec YDOT = 4677
963232 meter/sec
ZDOT = 1302
487558 ZDOT = 396
998208
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 18240
54893935
00016717 00000-0 10270-3 0 9019
2 25544 51
6396 18
0898 0005716 106
0800 254
0982 15
53888051 9766
Satellite: ISS
Catalog Number: 25544
Epoch time: 18240
54893935 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 18
0898 deg
Eccentricity:
0005716
Arg of perigee: 106
0800 deg
Mean anomaly: 254
0982 deg
Mean motion: 15
53888051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 976
Checksum: 329
Coasting Arc #3 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2018/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2445854
41 A = 6778706
88 meter
Y = -3642843
20 meter E =
0019464
Z = -5184342
49 I = 51
70983
XDOT = 7015
607733 Wp = 103
20290
YDOT = 2720
010711 meter/sec RA = 12
75326 deg
ZDOT = 1398
642918 TA = 180
26074
MA = 180
26175
Ha = 223
392 n
mi
Hp = 213
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8024456
72 X = 2511590
54
Y = -11951585
29 feet Y = -3615124
84 meter
Z = -17008997
68 Z = -5172301
50
XDOT = 23017
085737 XDOT = 6977
876585
YDOT = 8923
919656 feet/sec YDOT = 2798
253248 meter/sec
ZDOT = 4588
723484 ZDOT = 1432
630192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12192372
94 X = -3716235
27
Y = 7773772
83 feet Y = 2369445
96 meter
Z = -16954432
96 Z = -5167711
17
XDOT = -17035
068793 XDOT = -5192
288968
YDOT = -16378
653142 feet/sec YDOT = -4992
213478 meter/sec
ZDOT = 4740
880973 ZDOT = 1445
020521
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 18241
51361784
00016717 00000-0 10270-3 0 9020
2 25544 51
6403 13
2838 0005731 110
1711 250
0058 15
53904099 9918
Satellite: ISS
Catalog Number: 25544
Epoch time: 18241
51361784 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 13
2838 deg
Eccentricity:
0005731
Arg of perigee: 110
1711 deg
Mean anomaly: 250
0058 deg
Mean motion: 15
53904099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 282
Coasting Arc #4 (Orbit 1006)
---------------------------------------
Vector Time (GMT): 2018/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3969607
76 A = 6781401
73 meter
Y = 3081229
50 meter E =
0013558
Z = 4542599
28 I = 51
68688
XDOT = -6169
349087 Wp = 84
93151
YDOT = -3331
086160 meter/sec RA = 7
76348 deg
ZDOT = -3122
512961 TA = 36
34651
MA = 36
25451
Ha = 223
553 n
mi
Hp = 213
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13023647
50 X = -4025833
38
Y = 10109020
67 feet Y = 3036524
58 meter
Z = 14903540
96 Z = 4523179
56
XDOT = -20240
646610 XDOT = -6116
473966
YDOT = -10928
760367 feet/sec YDOT = -3399
780705 meter/sec
ZDOT = -10244
465096 ZDOT = -3152
352730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15973216
18 X = 4868636
29
Y = -4389458
14 feet Y = -1337906
84 meter
Z = 14815945
74 Z = 4515900
26
XDOT = 14212
611946 XDOT = 4332
004121
YDOT = 16588
255161 feet/sec YDOT = 5056
100173 meter/sec
ZDOT = -10377
906141 ZDOT = -3163
185792
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 18242
54260536
00016717 00000-0 10270-3 0 9038
2 25544 51
6412 8
1555 0005799 113
4149 246
7614 15
53874099 10077
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
54260536 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 8
1555 deg
Eccentricity:
0005799
Arg of perigee: 113
4149 deg
Mean anomaly: 246
7614 deg
Mean motion: 15
53874099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1007
Checksum: 309
Coasting Arc #5 (Orbit 1012)
---------------------------------------
Vector Time (GMT): 2018/242/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 456442
06 A = 6778072
40 meter
Y = -4188374
27 meter E =
0020275
Z = -5327025
94 I = 51
66034
XDOT = 7612
313335 Wp = 95
33143
YDOT = 788
720158 meter/sec RA = 5
73546 deg
ZDOT = 30
385466 TA = 174
96881
MA = 174
94841
Ha = 223
388 n
mi
Hp = 213
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1497513
33 X = 529119
54
Y = -13741385
39 feet Y = -4182864
06 meter
Z = -17477119
24 Z = -5324631
87
XDOT = 24974
781282 XDOT = 7602
780290
YDOT = 2587
664560 feet/sec YDOT = 873
793020 meter/sec
ZDOT = 99
689850 ZDOT = 67
340165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11987707
67 X = 3653853
30
Y = -6910823
95 feet Y = -2106419
14 meter
Z = -17465774
90 Z = -5323568
19
XDOT = 12331
020014 XDOT = 3758
494900
YDOT = 20704
509455 feet/sec YDOT = 6310
734482 meter/sec
ZDOT = 265
419835 ZDOT = 80
899966
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 18242
92847315
00016717 00000-0 10270-3 0 9047
2 25544 51
6391 6
2365 0005630 109
6703 250
5057 15
53885427 10136
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
92847315 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 6
2365 deg
Eccentricity:
0005630
Arg of perigee: 109
6703 deg
Mean anomaly: 250
5057 deg
Mean motion: 15
53885427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1013
Checksum: 297
Coasting Arc #6 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2018/243/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2152784
51 A = 6779201
34 meter
Y = 3969375
12 meter E =
0009826
Z = 5048275
84 I = 51
63053
XDOT = -7277
408504 Wp = 83
42590
YDOT = -1570
247083 meter/sec RA =
73969 deg
ZDOT = -1864
500038 TA = 24
64833
MA = 24
60141
Ha = 223
355 n
mi
Hp = 213
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7062941
30 X = -2221533
05
Y = 13022884
25 feet Y = 3944917
11 meter
Z = 16562584
78 Z = 5037651
12
XDOT = -23876
012151 XDOT = -7250
251927
YDOT = -5151
729276 feet/sec YDOT = -1651
476384 meter/sec
ZDOT = -6117
126110 ZDOT = -1899
785138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14693521
18 X = -4478585
25
Y = 2275293
00 feet Y = 693509
31 meter
Z = 16514337
59 Z = 5033570
10
XDOT = -10312
239082 XDOT = -3143
170472
YDOT = -20947
912661 feet/sec YDOT = -6384
923779 meter/sec
ZDOT = -6275
237212 ZDOT = -1912
692302
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 18243
95745486
00016717 00000-0 10270-3 0 9058
2 25544 51
6384 1
1091 0005502 113
1521 247
0211 15
53906563 10299
Satellite: ISS
Catalog Number: 25544
Epoch time: 18243
95745486 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 1
1091 deg
Eccentricity:
0005502
Arg of perigee: 113
1521 deg
Mean anomaly: 247
0211 deg
Mean motion: 15
53906563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 281
Coasting Arc #7 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2018/244/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3704811
38 A = 6782216
32 meter
Y = -3707196
22 meter E =
0013845
Z = -4318961
08 I = 51
60755
XDOT = 6399
624921 Wp = 112
22342
YDOT = 2312
131281 meter/sec RA = 355
74705 deg
ZDOT = 3508
890124 TA = 193
54420
MA = 193
58139
Ha = 223
281 n
mi
Hp = 213
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12154892
97 X = 3766970
20
Y = -12162717
27 feet Y = -3665419
10 meter
Z = -14169819
81 Z = -4300813
21
XDOT = 20996
144753 XDOT = 6356
250025
YDOT = 7585
732550 feet/sec YDOT = 2383
453957 meter/sec
ZDOT = 11512
106706 ZDOT = 3539
871882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17149051
81 X = 5227030
99
Y = 1974648
86 feet Y = 601872
97 meter
Z = -14087856
18 Z = -4293978
56
XDOT = 7277
404137 XDOT = 2218
152781
YDOT = 19827
507043 feet/sec YDOT = 6043
424147 meter/sec
ZDOT = 11650
789756 ZDOT = 3551
160718
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 18244
92212193
00016717 00000-0 10270-3 0 9061
2 25544 51
6386 356
3021 0005478 116
4201 243
7514 15
53893817 10445
Satellite: ISS
Catalog Number: 25544
Epoch time: 18244
92212193 = yrday
fracday
Element set: 906
Inclination: 51
6386 deg
RA of node: 356
3021 deg
Eccentricity:
0005478
Arg of perigee: 116
4201 deg
Mean anomaly: 243
7514 deg
Mean motion: 15
53893817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 300
Coasting Arc #8 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2018/245/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4995149
29 A = 6785840
24 meter
Y = 3334421
95 meter E =
0018067
Z = 3139142
77 I = 51
58789
XDOT = -5102
447355 Wp = 101
66730
YDOT = -3062
882422 meter/sec RA = 350
76054 deg
ZDOT = -4845
794957 TA = 42
09215
MA = 41
95351
Ha = 223
261 n
mi
Hp = 213
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16388285
07 X = -5047312
78
Y = 10939704
55 feet Y = 3278271
15 meter
Z = 10299024
84 Z = 3114751
26
XDOT = -16740
312843 XDOT = -5044
279796
YDOT = -10048
826843 feet/sec YDOT = -3119
616423 meter/sec
ZDOT = -15898
277417 ZDOT = -4870
439529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18921098
21 X = -5767150
74
Y = -5700623
38 feet Y = -1737550
01 meter
Z = 10189105
51 Z = 3105639
36
XDOT = -3280
735564 XDOT = -999
968200
YDOT = -17842
493001 feet/sec YDOT = -5438
391867 meter/sec
ZDOT = -16008
410565 ZDOT = -4879
363540
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 18245
95109493
00016717 00000-0 10270-3 0 9074
2 25544 51
6395 351
1738 0005421 119
1964 240
9731 15
53921579 10602
Satellite: ISS
Catalog Number: 25544
Epoch time: 18245
95109493 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 351
1738 deg
Eccentricity:
0005421
Arg of perigee: 119
1964 deg
Mean anomaly: 240
9731 deg
Mean motion: 15
53921579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 320
Coasting Arc #9 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2018/246/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5904157
06 A = 6788765
34 meter
Y = -2887510
84 meter E =
0009932
Z = -1699684
14 I = 51
56458
XDOT = 3476
211328 Wp = 70
40263
YDOT = 3776
872656 meter/sec RA = 345
78142 deg
ZDOT = 5689
287987 TA = 270
95663
MA = 271
07042
Ha = 223
195 n
mi
Hp = 213
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19370594
02 X = 5944263
35
Y = -9473460
77 feet Y = -2821262
25 meter
Z = -5576391
54 Z = -1670906
40
XDOT = 11404
892807 XDOT = 3406
083429
YDOT = 12391
314488 feet/sec YDOT = 3815
354037 meter/sec
ZDOT = 18665
643001 ZDOT = 5706
003794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19823290
53 X = 6042138
95
Y = 8569209
49 feet Y = 2611895
05 meter
Z = -5446862
91 Z = -1660203
81
XDOT = -1442
744591 XDOT = -439
748551
YDOT = 15184
442053 feet/sec YDOT = 4628
217938 meter/sec
ZDOT = 18740
096500 ZDOT = 5711
981413
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 18246
91575302
00016717 00000-0 10270-3 0 9088
2 25544 51
6388 346
3669 0005426 122
2517 237
9162 15
53918184 10755
Satellite: ISS
Catalog Number: 25544
Epoch time: 18246
91575302 = yrday
fracday
Element set: 908
Inclination: 51
6388 deg
RA of node: 346
3669 deg
Eccentricity:
0005426
Arg of perigee: 122
2517 deg
Mean anomaly: 237
9162 deg
Mean motion: 15
53918184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 327
Coasting Arc #10 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2018/247/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6392548
15 A = 6789931
59 meter
Y = 2264617
64 meter E =
0017449
Z = 46601
28 I = 51
53766
XDOT = -1641
544370 Wp = 131
53923
YDOT = -4480
413434 meter/sec RA = 340
80560 deg
ZDOT = -6006
116885 TA = 47
95797
MA = 47
80961
Ha = 223
074 n
mi
Hp = 213
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20972927
01 X = -6417622
99
Y = 7429847
89 feet Y = 2192991
54 meter
Z = 152891
35 Z = 15487
76
XDOT = -5385
644258 XDOT = -1562
146769
YDOT = -14699
519142 feet/sec YDOT = -4498
326454 meter/sec
ZDOT = -19705
107892 ZDOT = -6013
897995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19478597
78 X = -5937076
60
Y = -10755172
83 feet Y = -3278176
68 meter
Z = 12978
80 Z = 3955
94
XDOT = 6723
314230 XDOT = 2049
266177
YDOT = -12267
745135 feet/sec YDOT = -3739
208717 meter/sec
ZDOT = -19739
376212 ZDOT = -6016
561869
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 18247
94471884
00016717 00000-0 10270-3 0 9093
2 25544 51
6397 341
2387 0005365 126
7115 233
4532 15
53922224 10911
Satellite: ISS
Catalog Number: 25544
Epoch time: 18247
94471884 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 341
2387 deg
Eccentricity:
0005365
Arg of perigee: 126
7115 deg
Mean anomaly: 233
4532 deg
Mean motion: 15
53922224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 318
Coasting Arc #11 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2018/248/21:54:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6423630
55 A = 6788789
01 meter
Y = -1523365
87 meter E =
0016707
Z = 1559781
75 I = 51
50350
XDOT = -197
822976 Wp = 79
67691
YDOT = 5087
722497 meter/sec RA = 335
82784 deg
ZDOT = 5734
206747 TA = 297
40825
MA = 297
57811
Ha = 222
995 n
mi
Hp = 213
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21074903
38 X = 6432611
31
Y = -4997919
53 feet Y = -1451482
14 meter
Z = 5117394
19 Z = 1591007
04
XDOT = -649
025513 XDOT = -282
554067
YDOT = 16692
002943 feet/sec YDOT = 5085
036659 meter/sec
ZDOT = 18813
014263 ZDOT = 5733
039903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17914832
59 X = 5460440
97
Y = 12113376
02 feet Y = 3692157
01 meter
Z = 5257696
27 Z = 1602545
82
XDOT = -11933
512774 XDOT = -3637
334694
YDOT = 9417
296773 feet/sec YDOT = 2870
392056 meter/sec
ZDOT = 18807
058033 ZDOT = 5732
391288
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 18248
97367906
00016717 00000-0 10270-3 0 9108
2 25544 51
6400 336
1112 0005307 130
5406 229
6209 15
53941294 11071
Satellite: ISS
Catalog Number: 25544
Epoch time: 18248
97367906 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 336
1112 deg
Eccentricity:
0005307
Arg of perigee: 130
5406 deg
Mean anomaly: 229
6209 deg
Mean motion: 15
53941294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 293
Coasting Arc #12 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2018/249/00:35:13
064
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -230028
15 A = 6778974
51 meter
Y = -4414720
95 meter E =
0017967
Z = -5155236
08 I = 51
46847
XDOT = 7227
306716 Wp = 109
01484
YDOT = -2065
798497 meter/sec RA = 335
24270 deg
ZDOT = 1444
981061 TA = 174
95884
MA = 174
94073
Ha = 222
985 n
mi
Hp = 213
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -754685
52 X = -155603
26
Y = -14483992
63 feet Y = -4416877
26 meter
Z = -16913504
21 Z = -5156172
61
XDOT = 23711
636207 XDOT = 7242
851019
YDOT = -6777
554124 feet/sec YDOT = -1984
890801 meter/sec
ZDOT = 4740
751511 ZDOT = 1480
126238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1130775
16 X = 344660
27
Y = -14455308
61 feet Y = -4405978
06 meter
Z = -16917080
66 Z = -5156326
18
XDOT = 23275
724111 XDOT = 7094
440709
YDOT = -3918
342282 feet/sec YDOT = -1194
310727 meter/sec
ZDOT = 4898
715350 ZDOT = 1493
128439
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 18249
03798886
00016717 00000-0 10270-3 0 9112
2 25544 51
6424 335
7915 0004800 133
2661 226
8892 15
53828048 11082
Satellite: ISS
Catalog Number: 25544
Epoch time: 18249
03798886 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 335
7915 deg
Eccentricity:
0004800
Arg of perigee: 133
2661 deg
Mean anomaly: 226
8892 deg
Mean motion: 15
53828048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 328
Coasting Arc #13 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2018/249/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3049416
32 A = 6778448
84 meter
Y = 3058572
87 meter E =
0008270
Z = 5219624
33 I = 51
43808
XDOT = -6189
375723 Wp = 129
96134
YDOT = 4417
707896 meter/sec RA = 330
62706 deg
ZDOT = 1021
009525 TA = 310
20386
MA = 310
27622
Ha = 222
778 n
mi
Hp = 213
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10004646
72 X = 2989634
03
Y = 10034687
90 feet Y = 3092339
50 meter
Z = 17124751
74 Z = 5234291
82
XDOT = -20306
350798 XDOT = -6243
275212
YDOT = 14493
792309 feet/sec YDOT = 4348
192678 meter/sec
ZDOT = 3349
768784 ZDOT = 990
813004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3093194
11 X = 942805
56
Y = 13746883
65 feet Y = 4190050
14 meter
Z = 17190124
48 Z = 5239549
94
XDOT = -23914
829025 XDOT = -7289
239887
YDOT = 1336
764484 feet/sec YDOT = 407
445815 meter/sec
ZDOT = 3213
684561 ZDOT = 979
531054
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 18250
00270922
00016717 00000-0 10270-3 0 9128
2 25544 51
6409 330
9846 0004767 136
9027 223
2499 15
53858830 11236
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
00270922 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 330
9846 deg
Eccentricity:
0004767
Arg of perigee: 136
9027 deg
Mean anomaly: 223
2499 deg
Mean motion: 15
53858830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 308
Coasting Arc #14 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2018/250/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1613562
06 A = 6778466
07 meter
Y = -3981346
08 meter E =
0018316
Z = -5259227
38 I = 51
40978
XDOT = 6622
692212 Wp = 106
34529
YDOT = -3752
523072 meter/sec RA = 325
61533 deg
ZDOT = 806
150548 TA = 171
41405
MA = 171
38267
Ha = 222
905 n
mi
Hp = 213
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5293838
78 X = -1543375
45
Y = -13062159
07 feet Y = -3998997
96 meter
Z = -17254683
00 Z = -5266894
65
XDOT = 21727
992822 XDOT = 6660
245960
YDOT = -12311
427401 feet/sec YDOT = -3678
253508 meter/sec
ZDOT = 2644
850880 ZDOT = 838
412270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2268414
01 X = 691412
59
Y = -13868303
65 feet Y = -4227058
95 meter
Z = -17288529
89 Z = -5269543
91
XDOT = 23939
402555 XDOT = 7296
729899
YDOT = 426
484147 feet/sec YDOT = 129
992368 meter/sec
ZDOT = 2790
092405 ZDOT = 850
420165
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 18250
96742952
00016717 00000-0 10270-3 0 9131
2 25544 51
6412 326
1777 0004791 139
1097 221
0416 15
53831404 11388
Satellite: ISS
Catalog Number: 25544
Epoch time: 18250
96742952 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 326
1777 deg
Eccentricity:
0004791
Arg of perigee: 139
1097 deg
Mean anomaly: 221
0416 deg
Mean motion: 15
53831404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 303
Coasting Arc #15 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2018/251/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 189773
71 A = 6780399
07 meter
Y = 4790495
44 meter E =
0009308
Z = 4786560
90 I = 51
38950
XDOT = -6660
078569 Wp = 90
66646
YDOT = 2825
067094 meter/sec RA = 320
60527 deg
ZDOT = -2559
127949 TA = 24
61926
MA = 24
57486
Ha = 222
759 n
mi
Hp = 213
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 622617
14 X = 112940
67
Y = 15716848
54 feet Y = 4792188
46 meter
Z = 15703939
97 Z = 4787295
69
XDOT = -21850
651472 XDOT = -6678
743536
YDOT = 9268
592829 feet/sec YDOT = 2750
484881 meter/sec
ZDOT = -8396
089071 ZDOT = -2591
525456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7393228
42 X = -2253456
02
Y = 13880345
46 feet Y = 4230729
30 meter
Z = 15706587
60 Z = 4787367
90
XDOT = -22499
783700 XDOT = -6857
934072
YDOT = -2303
022894 feet/sec YDOT = -701
961378 meter/sec
ZDOT = -8541
797208 ZDOT = -2603
539789
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 18251
99645926
00016717 00000-0 10270-3 0 9149
2 25544 51
6410 321
0513 0004680 143
2967 216
8506 15
53850066 11542
Satellite: ISS
Catalog Number: 25544
Epoch time: 18251
99645926 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 321
0513 deg
Eccentricity:
0004680
Arg of perigee: 143
2967 deg
Mean anomaly: 216
8506 deg
Mean motion: 15
53850066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 305
Coasting Arc #16 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2018/252/22:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1117354
31 A = 6783747
18 meter
Y = -5449501
30 meter E =
0010434
Z = -3894623
94 I = 51
37647
XDOT = 6286
952325 Wp = 122
10477
YDOT = -1613
016240 meter/sec RA = 315
59887 deg
ZDOT = 4063
277479 TA = 190
66434
MA = 190
68648
Ha = 222
753 n
mi
Hp = 214
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3665860
60 X = 1197126
95
Y = -17878941
28 feet Y = -5436560
67 meter
Z = -12777637
59 Z = -3889001
91
XDOT = 20626
484006 XDOT = 6284
785191
YDOT = -5292
048033 feet/sec YDOT = -1542
722843 meter/sec
ZDOT = 13330
962857 ZDOT = 4093
811931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11935338
55 X = 3637891
19
Y = -13831307
24 feet Y = -4215782
45 meter
Z = -12751695
24 Z = -3886716
71
XDOT = 19524
175152 XDOT = 5950
968586
YDOT = 4438
788175 feet/sec YDOT = 1352
942636 meter/sec
ZDOT = 13468
136996 ZDOT = 4105
088156
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 18252
96117095
00016717 00000-0 10270-3 0 9159
2 25544 51
6417 316
2438 0004695 145
9504 214
1950 15
53850305 11699
Satellite: ISS
Catalog Number: 25544
Epoch time: 18252
96117095 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 316
2438 deg
Eccentricity:
0004695
Arg of perigee: 145
9504 deg
Mean anomaly: 214
1950 deg
Mean motion: 15
53850305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 312
Coasting Arc #17 (Orbit 1176)
---------------------------------------
Vector Time (GMT): 2018/253/11:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2895719
66 A = 6778268
99 meter
Y = -3107250
82 meter E =
0017790
Z = -5297553
25 I = 51
34468
XDOT = 5372
727128 Wp = 105
56847
YDOT = -5447
148957 meter/sec RA = 313
08297 deg
ZDOT = 254
218919 TA = 166
89193
MA = 166
84564
Ha = 222
747 n
mi
Hp = 214
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9500392
58 X = -2835025
76
Y = -10194392
45 feet Y = -3139294
03 meter
Z = -17380424
04 Z = -5311471
77
XDOT = 17627
057506 XDOT = 5432
004495
YDOT = -17871
223613 feet/sec YDOT = -5386
735926 meter/sec
ZDOT = 834
051572 ZDOT = 280
462189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4007248
55 X = 1221409
36
Y = 13265195
64 feet Y = 4043231
63 meter
Z = -17442441
92 Z = -5316456
30
XDOT = -22678
241588 XDOT = -6912
328036
YDOT = 8120
274494 feet/sec YDOT = 2475
059666 meter/sec
ZDOT = 952
478356 ZDOT = 290
315403
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 18253
47568174
00016717 00000-0 10270-3 0 9165
2 25544 51
6403 313
6782 0004864 151
9243 208
2173 15
53826054 11776
Satellite: ISS
Catalog Number: 25544
Epoch time: 18253
47568174 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 313
6782 deg
Eccentricity:
0004864
Arg of perigee: 151
9243 deg
Mean anomaly: 208
2173 deg
Mean motion: 15
53826054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1177
Checksum: 315
Coasting Arc #18 (Orbit 1191)
---------------------------------------
Vector Time (GMT): 2018/254/11:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 909595
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1703883
82 A = 6779507
72 meter
Y = 4276478
18 meter E =
0007152
Z = 4970495
61 I = 51
32737
XDOT = -5736
304415 Wp = 98
52708
YDOT = 4666
937492 meter/sec RA = 308
06621 deg
ZDOT = -2047
416477 TA = 11
46569
MA = 11
44941
Ha = 222
514 n
mi
Hp = 214
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5590170
01 X = 1631792
42
Y = 14030440
23 feet Y = 4295129
70 meter
Z = 16307400
30 Z = 4978596
86
XDOT = -18819
896376 XDOT = -5778
119821
YDOT = 15311
474710 feet/sec YDOT = 4602
556106 meter/sec
ZDOT = -6717
245658 ZDOT = -2075
383519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 918315
23 X = 279902
48
Y = -15036349
38 feet Y = -4583079
29 meter
Z = 16343177
56 Z = 4981400
52
XDOT = 22372
672298 XDOT = 6819
190516
YDOT = -6076
962422 feet/sec YDOT = -1852
258146 meter/sec
ZDOT = -6843
283622 ZDOT = -2085
832848
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 18254
50470279
00016717 00000-0 10270-3 0 9179
2 25544 51
6401 308
5507 0004851 156
4251 203
7124 15
53879586 11928
Satellite: ISS
Catalog Number: 25544
Epoch time: 18254
50470279 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 308
5507 deg
Eccentricity:
0004851
Arg of perigee: 156
4251 deg
Mean anomaly: 203
7124 deg
Mean motion: 15
53879586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1192
Checksum: 311
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