[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 8th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
128/07:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 213
4
131/03:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
4
132/22:41:21
823 -1
0 1
0 1
0
N/A -0
1 -0
1 222
0
000/00:02:39
647 -0
0 -0
0 213
8
134/06:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
9
137/14:35:00
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
8
140/09:04:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 213
7
Coasting Arc #1 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2018/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4041321
91 A = 6787930
72 meter
Y = -5184806
25 meter E =
0017050
Z = 1657617
59 I = 51
40714
XDOT = 4781
220975 Wp = 61
84629
YDOT = -1894
667521 meter/sec RA = 220
45559 deg
ZDOT = 5693
631645 TA = 316
38322
MA = 316
51788
Ha = 221
866 n
mi
Hp = 213
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13258930
15 X = -3991095
52
Y = -17010519
19 feet Y = -5229718
32 meter
Z = 5438377
92 Z = 1638107
92
XDOT = 15686
420521 XDOT = 4774
395472
YDOT = -6216
100792 feet/sec YDOT = -1841
238986 meter/sec
ZDOT = 18679
893847 ZDOT = 5716
840666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21400357
36 X = -6522828
92
Y = -2848571
50 feet Y = -868244
59 meter
Z = 5351942
76 Z = 1631272
15
XDOT = 6561
072961 XDOT = 1999
815038
YDOT = -13769
117746 feet/sec YDOT = -4196
827089 meter/sec
ZDOT = 18783
694844 ZDOT = 5725
270188
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 18127
56111127
00016717 00000-0 10270-3 0 9000
2 25544 51
6408 221
2378 0003166 52
9686 307
1756 15
54223339 32194
Satellite: ISS
Catalog Number: 25544
Epoch time: 18127
56111127 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 221
2378 deg
Eccentricity:
0003166
Arg of perigee: 52
9686 deg
Mean anomaly: 307
1756 deg
Mean motion: 15
54223339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 298
Coasting Arc #2 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2018/128/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -232555
99 A = 6778840
13 meter
Y = 4691161
99 meter E =
0015272
Z = -4902235
29 I = 51
39442
XDOT = -6778
676358 Wp = 70
12728
YDOT = -2726
614248 meter/sec RA = 216
39350 deg
ZDOT = -2288
382135 TA = 177
39017
MA = 177
38219
Ha = 221
927 n
mi
Hp = 213
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -762978
98 X = -261183
94
Y = 15390951
41 feet Y = 4688401
45 meter
Z = -16083449
10 Z = -4903434
37
XDOT = -22239
751831 XDOT = -6736
566984
YDOT = -8945
584803 feet/sec YDOT = -2802
182564 meter/sec
ZDOT = -7507
815402 ZDOT = -2321
208599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6445100
98 X = -1964466
78
Y = 13990494
85 feet Y = 4264302
83 meter
Z = -16089362
46 Z = -4904037
68
XDOT = -16117
689597 XDOT = -4912
671789
YDOT = -16224
517288 feet/sec YDOT = -4945
232869 meter/sec
ZDOT = -7653
992370 ZDOT = -2332
936874
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 18128
33268931
00016717 00000-0 10270-3 0 9013
2 25544 51
6375 217
3902 0003326 57
6043 302
5431 15
54239181 32318
Satellite: ISS
Catalog Number: 25544
Epoch time: 18128
33268931 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 217
3902 deg
Eccentricity:
0003326
Arg of perigee: 57
6043 deg
Mean anomaly: 302
5431 deg
Mean motion: 15
54239181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 285
Coasting Arc #3 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2018/129/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1839219
17 A = 6777151
79 meter
Y = -3816874
49 meter E =
0005456
Z = 5284752
64 I = 51
41619
XDOT = 6692
250849 Wp = 81
49286
YDOT = 3735
842579 meter/sec RA = 211
37660 deg
ZDOT = 369
588767 TA = 4
97723
MA = 4
97181
Ha = 221
907 n
mi
Hp = 213
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6034183
63 X = 1856093
09
Y = -12522554
10 feet Y = -3796212
81 meter
Z = 17338427
30 Z = 5293727
92
XDOT = 21956
203573 XDOT = 6648
182975
YDOT = 12256
701376 feet/sec YDOT = 3810
433533 meter/sec
ZDOT = 1212
561573 ZDOT = 401
990652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10064342
22 X = 3067611
51
Y = -9514634
86 feet Y = -2900060
70 meter
Z = 17378939
37 Z = 5297100
72
XDOT = 15300
428650 XDOT = 4663
570652
YDOT = 18659
786899 feet/sec YDOT = 5687
503047 meter/sec
ZDOT = 1356
744336 ZDOT = 413
535674
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 18129
36145554
00016717 00000-0 10270-3 0 9023
2 25544 51
6379 212
2595 0003324 59
9793 300
1689 15
54213782 32474
Satellite: ISS
Catalog Number: 25544
Epoch time: 18129
36145554 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 212
2595 deg
Eccentricity:
0003324
Arg of perigee: 59
9793 deg
Mean anomaly: 300
1689 deg
Mean motion: 15
54213782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 321
Coasting Arc #4 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2018/130/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3427325
90 A = 6777810
67 meter
Y = 2853699
83 meter E =
0016412
Z = -5118298
99 I = 51
44827
XDOT = -6049
461330 Wp = 95
03297
YDOT = -4414
505746 meter/sec RA = 206
36270 deg
ZDOT = 1592
558034 TA = 190
37493
MA = 190
40884
Ha = 221
960 n
mi
Hp = 213
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11244507
53 X = -3434119
80
Y = 9362532
25 feet Y = 2815335
15 meter
Z = -16792319
53 Z = -5134964
39
XDOT = -19847
314076 XDOT = -6007
383389
YDOT = -14483
286569 feet/sec YDOT = -4481
919726 meter/sec
ZDOT = 5224
927933 ZDOT = 1563
273762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13691186
17 X = -4173073
55
Y = 4912445
90 feet Y = 1497313
51 meter
Z = -16867046
32 Z = -5141075
72
XDOT = -13256
533012 XDOT = -4040
591262
YDOT = -19487
315998 feet/sec YDOT = -5939
733916 meter/sec
ZDOT = 5094
721300 ZDOT = 1552
871052
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 18130
32591802
00016717 00000-0 10270-3 0 9033
2 25544 51
6387 207
4519 0003357 64
2623 295
8876 15
54247113 32622
Satellite: ISS
Catalog Number: 25544
Epoch time: 18130
32591802 = yrday
fracday
Element set: 903
Inclination: 51
6387 deg
RA of node: 207
4519 deg
Eccentricity:
0003357
Arg of perigee: 64
2623 deg
Mean anomaly: 295
8876 deg
Mean motion: 15
54247113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 309
Coasting Arc #5 (Orbit 3274)
---------------------------------------
Vector Time (GMT): 2018/131/03:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 870169
89 A = 6778766
69 meter
Y = 4592092
79 meter E =
0015443
Z = -4924334
64 I = 51
47470
XDOT = -7246
439382 Wp = 70
47375
YDOT = -1033
696765 meter/sec RA = 202
25306 deg
ZDOT = -2245
166039 TA = 177
51635
MA = 177
50867
Ha = 221
950 n
mi
Hp = 213
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2854888
08 X = 842675
27
Y = 15065921
22 feet Y = 4601669
90 meter
Z = -16155953
53 Z = -4920174
38
XDOT = -23774
407422 XDOT = -7223
435774
YDOT = -3391
393586 feet/sec YDOT = -1114
602816 meter/sec
ZDOT = -7366
030313 ZDOT = -2280
311260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14416133
72 X = -4394037
56
Y = 5281100
25 feet Y = 1609679
36 meter
Z = -16137914
09 Z = -4918836
21
XDOT = 25
098048 XDOT = 7
649885
YDOT = -22912
484445 feet/sec YDOT = -6983
725259 meter/sec
ZDOT = -7522
809080 ZDOT = -2292
952208
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 18131
16178220
00016717 00000-0 10270-3 0 9042
2 25544 51
6374 203
2872 0003398 58
2478 301
9005 15
54243419 32752
Satellite: ISS
Catalog Number: 25544
Epoch time: 18131
16178220 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 203
2872 deg
Eccentricity:
0003398
Arg of perigee: 58
2478 deg
Mean anomaly: 301
9005 deg
Mean motion: 15
54243419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3275
Checksum: 298
Coasting Arc #6 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2018/132/03:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 908385
99 A = 6777121
32 meter
Y = -4126873
51 meter E =
0005515
Z = 5293647
41 I = 51
50062
XDOT = 7392
778846 Wp = 81
61935
YDOT = 2031
597077 meter/sec RA = 197
24313 deg
ZDOT = 315
723390 TA = 5
36993
MA = 5
36402
Ha = 221
955 n
mi
Hp = 213
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2980269
00 X = 928752
17
Y = -13539611
25 feet Y = -4116601
46 meter
Z = 17367609
60 Z = 5298109
54
XDOT = 24254
523772 XDOT = 7367
977883
YDOT = 6665
344742 feet/sec YDOT = 2114
129550 meter/sec
ZDOT = 1035
837894 ZDOT = 351
575256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13829980
88 X = 4215378
17
Y = 475104
61 feet Y = 144811
89 meter
Z = 17388008
62 Z = 5299865
03
XDOT = -2326
601767 XDOT = -709
148219
YDOT = 24027
008317 feet/sec YDOT = 7323
432135 meter/sec
ZDOT = 1195
672982 ZDOT = 364
441125
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 18132
19053845
00016717 00000-0 10270-3 0 9052
2 25544 51
6381 198
1579 0003351 62
1050 298
0442 15
54219876 32914
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
19053845 = yrday
fracday
Element set: 905
Inclination: 51
6381 deg
RA of node: 198
1579 deg
Eccentricity:
0003351
Arg of perigee: 62
1050 deg
Mean anomaly: 298
0442 deg
Mean motion: 15
54219876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3291
Checksum: 310
Coasting Arc #7 (Orbit 3302)
---------------------------------------
Vector Time (GMT): 2018/132/22:42:41
647
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1219640
52 A = 6777520
75 meter
Y = 4048849
52 meter E =
0017209
Z = -5311459
07 I = 51
52935
XDOT = -7405
160154 Wp = 86
73967
YDOT = -1928
984436 meter/sec RA = 193
22273 deg
ZDOT = 231
574637 TA = 185
46509
MA = 185
48390
Ha = 221
983 n
mi
Hp = 213
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4001445
27 X = -1239024
48
Y = 13283627
04 feet Y = 4035102
35 meter
Z = -17426046
81 Z = -5317430
79
XDOT = -24295
144862 XDOT = -7384
164242
YDOT = -6328
689094 feet/sec YDOT = -2011
676645 meter/sec
ZDOT = 759
759308 ZDOT = 195
653260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3380985
42 X = -1030524
36
Y = -13419721
35 feet Y = -4090331
07 meter
Z = -17453178
38 Z = -5319728
77
XDOT = 23176
797284 XDOT = 7064
287812
YDOT = -6612
155106 feet/sec YDOT = -2015
384876 meter/sec
ZDOT = 599
588186 ZDOT = 182
754479
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 18132
96210313
00016717 00000-0 10270-3 0 9063
2 25544 51
6414 194
3128 0002754 57
4079 302
7339 15
54076753 33030
Satellite: ISS
Catalog Number: 25544
Epoch time: 18132
96210313 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 194
3128 deg
Eccentricity:
0002754
Arg of perigee: 57
4079 deg
Mean anomaly: 302
7339 deg
Mean motion: 15
54076753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3303
Checksum: 297
Coasting Arc #8 (Orbit 3318)
---------------------------------------
Vector Time (GMT): 2018/133/22:42:41
647
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2926799
92 A = 6778826
84 meter
Y = -3559496
73 meter E =
0008820
Z = 4966627
03 I = 51
56582
XDOT = 6868
243398 Wp = 57
74185
YDOT = 2687
167257 meter/sec RA = 188
21860 deg
ZDOT = -2114
204517 TA = 52
89526
MA = 52
81468
Ha = 221
850 n
mi
Hp = 213
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9602361
93 X = 2942259
89
Y = -11678138
89 feet Y = -3526680
96 meter
Z = 16294708
11 Z = 4980882
15
XDOT = 22533
606949 XDOT = 6847
954202
YDOT = 8816
165540 feet/sec YDOT = 2763
859308 meter/sec
ZDOT = -6936
366526 ZDOT = -2080
889463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2011107
18 X = -612985
47
Y = 14914678
51 feet Y = 4545994
01 meter
Z = 16358777
69 Z = 4986155
44
XDOT = -22775
149518 XDOT = -6941
865573
YDOT = 4400
492074 feet/sec YDOT = 1341
269984 meter/sec
ZDOT = -6787
904170 ZDOT = -2068
953191
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 18133
99097890
00016717 00000-0 10270-3 0 9071
2 25544 51
6407 189
1847 0002745 58
5548 301
5873 15
54107868 33194
Satellite: ISS
Catalog Number: 25544
Epoch time: 18133
99097890 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 189
1847 deg
Eccentricity:
0002745
Arg of perigee: 58
5548 deg
Mean anomaly: 301
5873 deg
Mean motion: 15
54107868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3319
Checksum: 349
Coasting Arc #9 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2535506
52 A = 6778705
66 meter
Y = -3738636
58 meter E =
0008057
Z = 5049084
80 I = 51
57263
XDOT = 7082
857295 Wp = 61
89303
YDOT = 2298
132284 meter/sec RA = 186
61371 deg
ZDOT = -1849
169145 TA = 46
05783
MA = 45
99138
Ha = 222
043 n
mi
Hp = 213
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8318590
94 X = 2552598
21
Y = -12265868
05 feet Y = -3710187
43 meter
Z = 16565238
85 Z = 5061443
05
XDOT = 23237
720783 XDOT = 7065
615020
YDOT = 7539
804081 feet/sec YDOT = 2377
241336 meter/sec
ZDOT = -6066
827903 ZDOT = -1814
804120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13530788
98 X = 4124184
48
Y = -5892566
06 feet Y = -1796054
13 meter
Z = 16620861
21 Z = 5066038
50
XDOT = 15094
574760 XDOT = 4600
826387
YDOT = 17925
560273 feet/sec YDOT = 5463
710771 meter/sec
ZDOT = -5913
626149 ZDOT = -1802
473250
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 18134
31250535
00016717 00000-0 10270-3 0 9086
2 25544 51
6382 187
5767 0002725 73
5980 286
5472 15
54031739 33240
Satellite: ISS
Catalog Number: 25544
Epoch time: 18134
31250535 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 187
5767 deg
Eccentricity:
0002725
Arg of perigee: 73
5980 deg
Mean anomaly: 286
5472 deg
Mean motion: 15
54031739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 320
Coasting Arc #10 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4102317
02 A = 6781618
77 meter
Y = 3287485
17 meter E =
0010725
Z = -4294707
32 I = 51
61572
XDOT = -6097
955244 Wp = 103
01699
YDOT = -2982
829663 meter/sec RA = 181
61826 deg
ZDOT = 3546
620637 TA = 203
16869
MA = 203
21708
Ha = 221
995 n
mi
Hp = 213
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13459045
33 X = -4117911
79
Y = 10785712
49 feet Y = 3241523
31 meter
Z = -14090247
12 Z = -4314673
08
XDOT = -20006
414843 XDOT = -6081
375214
YDOT = -9786
186557 feet/sec YDOT = -3050
928715 meter/sec
ZDOT = 11635
894479 ZDOT = 3517
038297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17038061
82 X = -5193201
24
Y = 2156416
83 feet Y = 657275
85 meter
Z = -14179805
17 Z = -4322004
62
XDOT = -11792
082097 XDOT = -3594
226623
YDOT = -17633
183056 feet/sec YDOT = -5374
594196 meter/sec
ZDOT = 11504
115045 ZDOT = 3506
454266
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 18135
27707316
00016717 00000-0 10270-3 0 9097
2 25544 51
6384 182
7695 0002543 75
1259 285
0175 15
54061292 33391
Satellite: ISS
Catalog Number: 25544
Epoch time: 18135
27707316 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 182
7695 deg
Eccentricity:
0002543
Arg of perigee: 75
1259 deg
Mean anomaly: 285
0175 deg
Mean motion: 15
54061292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3339
Checksum: 322
Coasting Arc #11 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2018/136/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5383686
03 A = 6785443
60 meter
Y = -2747923
96 meter E =
0015522
Z = 3068920
82 I = 51
66182
XDOT = 4655
995436 Wp = 93
11308
YDOT = 3615
627633 meter/sec RA = 176
63322 deg
ZDOT = -4909
776460 TA = 51
63465
MA = 51
49528
Ha = 221
988 n
mi
Hp = 213
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17663011
92 X = 5399106
43
Y = -9015498
57 feet Y = -2687633
93 meter
Z = 10068637
88 Z = 3095110
67
XDOT = 15275
575576 XDOT = 4639
068057
YDOT = 11862
295385 feet/sec YDOT = 3667
599961 meter/sec
ZDOT = -16108
190487 ZDOT = -4887
199573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19732355
48 X = 6014421
95
Y = 1232554
70 feet Y = 375682
67 meter
Z = 10185952
55 Z = 3104678
34
XDOT = 7260
081985 XDOT = 2212
872989
YDOT = 16612
986183 feet/sec YDOT = 5063
638189 meter/sec
ZDOT = -16007
761897 ZDOT = -4879
165826
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 18136
30594376
00016717 00000-0 10270-3 0 9104
2 25544 51
6388 177
6401 0002619 79
9284 280
2164 15
54059410 33559
Satellite: ISS
Catalog Number: 25544
Epoch time: 18136
30594376 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 177
6401 deg
Eccentricity:
0002619
Arg of perigee: 79
9284 deg
Mean anomaly: 280
2164 deg
Mean motion: 15
54059410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 317
Coasting Arc #12 (Orbit 3369)
---------------------------------------
Vector Time (GMT): 2018/137/06:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237587
98 A = 6788405
80 meter
Y = 2164152
26 meter E =
0010144
Z = -1566106
12 I = 51
70474
XDOT = -2882
581942 Wp = 48
48929
YDOT = -4167
935851 meter/sec RA = 171
66091 deg
ZDOT = 5752
063887 TA = 294
40849
MA = 294
51431
Ha = 222
036 n
mi
Hp = 213
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20464527
49 X = -6253717
08
Y = 7100237
08 feet Y = 2094309
24 meter
Z = -5138143
45 Z = -1596445
62
XDOT = -9457
289836 XDOT = -2863
701669
YDOT = -13674
330219 feet/sec YDOT = -4200
065916 meter/sec
ZDOT = 18871
600679 ZDOT = 5738
106475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21262832
38 X = -6480911
31
Y = -3960829
54 feet Y = -1207260
84 meter
Z = -5273950
98 Z = -1607500
26
XDOT = -1833
205007 XDOT = -558
760886
YDOT = -15073
982377 feet/sec YDOT = -4594
549829 meter/sec
ZDOT = 18809
734088 ZDOT = 5733
206950
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 18137
27050637
00016717 00000-0 10270-3 0 9119
2 25544 51
6389 172
8325 0002709 79
4172 280
7285 15
54067548 33700
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
27050637 = yrday
fracday
Element set: 911
Inclination: 51
6389 deg
RA of node: 172
8325 deg
Eccentricity:
0002709
Arg of perigee: 79
4172 deg
Mean anomaly: 280
7285 deg
Mean motion: 15
54067548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3370
Checksum: 323
Coasting Arc #13 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2018/137/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -958947
70 A = 6777530
53 meter
Y = -4093764
16 meter E =
0005170
Z = 5311210
17 I = 51
67604
XDOT = 7523
121780 Wp = 87
54862
YDOT = -1494
279402 meter/sec RA = 169
98580 deg
ZDOT = 206
596996 TA =
48478
MA =
48428
Ha = 222
127 n
mi
Hp = 213
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3146153
86 X = -938898
28
Y = -13430984
79 feet Y = -4104376
27 meter
Z = 17425230
20 Z = 5306600
10
XDOT = 24682
158071 XDOT = 7538
268531
YDOT = -4902
491477 feet/sec YDOT = -1410
066009 meter/sec
ZDOT = 677
811666 ZDOT = 243
178898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13232172
07 X = -4033166
05
Y = 3987455
51 feet Y = 1215376
44 meter
Z = 17405117
21 Z = 5305079
72
XDOT = -5947
527444 XDOT = -1812
806365
YDOT = -23408
818416 feet/sec YDOT = -7135
007853 meter/sec
ZDOT = 841
439979 ZDOT = 256
470906
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 18137
65633025
00016717 00000-0 10270-3 0 9120
2 25544 51
6356 170
9125 0002823 74
1493 285
9971 15
54072126 33769
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
65633025 = yrday
fracday
Element set: 912
Inclination: 51
6356 deg
RA of node: 170
9125 deg
Eccentricity:
0002823
Arg of perigee: 74
1493 deg
Mean anomaly: 285
9971 deg
Mean motion: 15
54072126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 313
Coasting Arc #14 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2018/138/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -805105
50 A = 6778460
17 meter
Y = 4394241
17 meter E =
0016096
Z = -5112397
45 I = 51
71168
XDOT = -7440
943921 Wp = 98
52910
YDOT = 608
215717 meter/sec RA = 164
99107 deg
ZDOT = 1696
826356 TA = 187
85966
MA = 187
88491
Ha = 222
137 n
mi
Hp = 213
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2641422
24 X = -829349
69
Y = 14416801
73 feet Y = 4385102
97 meter
Z = -16772957
52 Z = -5116366
78
XDOT = -24412
545673 XDOT = -7455
434497
YDOT = 1995
458388 feet/sec YDOT = 524
924737 meter/sec
ZDOT = 5567
015603 ZDOT = 1660
645344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14559628
14 X = 4437774
66
Y = 1491831
05 feet Y = 454710
11 meter
Z = -16791219
62 Z = -5117963
74
XDOT = 3850
002702 XDOT = 1173
480824
YDOT = 23181
488471 feet/sec YDOT = 7065
717686 meter/sec
ZDOT = 5405
254727 ZDOT = 1647
521641
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 18138
62089105
00016717 00000-0 10270-3 0 9133
2 25544 51
6359 166
1046 0002865 77
1064 283
0409 15
54058986 33914
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
62089105 = yrday
fracday
Element set: 913
Inclination: 51
6359 deg
RA of node: 166
1046 deg
Eccentricity:
0002865
Arg of perigee: 77
1064 deg
Mean anomaly: 283
0409 deg
Mean motion: 15
54058986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 321
Coasting Arc #15 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2018/139/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2469467
24 A = 6781279
78 meter
Y = -4558541
38 meter E =
0012250
Z = 4363217
96 I = 51
75356
XDOT = 6844
036999 Wp = 72
98749
YDOT = 399
145818 meter/sec RA = 160
00330 deg
ZDOT = -3445
048285 TA = 51
93837
MA = 51
82791
Ha = 222
013 n
mi
Hp = 213
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8101926
65 X = 2499064
25
Y = -14955844
41 feet Y = -4530761
10 meter
Z = 14315019
55 Z = 4375285
21
XDOT = 22454
189628 XDOT = 6855
799289
YDOT = 1309
533522 feet/sec YDOT = 475
746706 meter/sec
ZDOT = -11302
651855 ZDOT = -3411
773540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15606258
16 X = -4756787
49
Y = -6648340
41 feet Y = -2026414
16 meter
Z = 14369500
98 Z = 4379823
90
XDOT = -1180
570754 XDOT = -359
837966
YDOT = -21417
687622 feet/sec YDOT = -6528
111187 meter/sec
ZDOT = -11153
973603 ZDOT = -3399
731154
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 18139
64975174
00016717 00000-0 10270-3 0 9147
2 25544 51
6364 160
9755 0002802 78
7548 281
3919 15
54095270 34076
Satellite: ISS
Catalog Number: 25544
Epoch time: 18139
64975174 = yrday
fracday
Element set: 914
Inclination: 51
6364 deg
RA of node: 160
9755 deg
Eccentricity:
0002802
Arg of perigee: 78
7548 deg
Mean anomaly: 281
3919 deg
Mean motion: 15
54095270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 337
Coasting Arc #16 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1572993
96 A = 6780171
84 meter
Y = -4685226
92 meter E =
0010679
Z = 4634844
58 I = 51
77687
XDOT = 7055
985684 Wp = 69
55750
YDOT = -568
103435 meter/sec RA = 156
17032 deg
ZDOT = -2959
814835 TA = 49
89783
MA = 49
80427
Ha = 221
909 n
mi
Hp = 213
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5160741
34 X = 1602754
86
Y = -15371479
40 feet Y = -4667470
69 meter
Z = 15206183
01 Z = 4642557
47
XDOT = 23149
559332 XDOT = 7076
191211
YDOT = -1863
856415 feet/sec YDOT = -489
085270 meter/sec
ZDOT = -9710
678591 ZDOT = -2925
490197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1390492
58 X = 423822
14
Y = -16121888
78 feet Y = -4913951
70 meter
Z = 15241222
53 Z = 4645524
63
XDOT = 20987
034686 XDOT = 6396
848172
YDOT = -7253
334366 feet/sec YDOT = -2210
816315 meter/sec
ZDOT = -9557
173194 ZDOT = -2913
026389
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 18140
42139420
00016717 00000-0 10270-3 0 9152
2 25544 51
6394 157
1282 0002570 83
8880 276
2565 15
54125073 34198
Satellite: ISS
Catalog Number: 25544
Epoch time: 18140
42139420 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 157
1282 deg
Eccentricity:
0002570
Arg of perigee: 83
8880 deg
Mean anomaly: 276
2565 deg
Mean motion: 15
54125073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 304
Coasting Arc #17 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3040486
52 A = 6783830
89 meter
Y = 4893523
29 meter E =
0008226
Z = -3589606
53 I = 51
81792
XDOT = -6202
342065 Wp = 95
48351
YDOT = -589
830817 meter/sec RA = 151
19387 deg
ZDOT = 4457
467919 TA = 222
23640
MA = 222
29979
Ha = 222
043 n
mi
Hp = 213
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9975349
48 X = -3077544
83
Y = 16054866
45 feet Y = 4859315
56 meter
Z = -11776924
32 Z = -3604465
79
XDOT = -20348
891290 XDOT = -6216
937493
YDOT = -1935
140476 feet/sec YDOT = -659
271645 meter/sec
ZDOT = 14624
238579 ZDOT = 4427
303563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5632121
07 X = -1716670
50
Y = 17998956
96 feet Y = 5486082
08 meter
Z = -11843945
34 Z = -3610034
54
XDOT = -18978
112998 XDOT = -5784
528842
YDOT = 3578
849384 feet/sec YDOT = 1090
833292 meter/sec
ZDOT = 14489
450247 ZDOT = 4416
384435
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 18141
38594947
00016717 00000-0 10270-3 0 9168
2 25544 51
6385 152
3209 0002862 89
7878 270
3603 15
54120458 34347
Satellite: ISS
Catalog Number: 25544
Epoch time: 18141
38594947 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 152
3209 deg
Eccentricity:
0002862
Arg of perigee: 89
7878 deg
Mean anomaly: 270
3603 deg
Mean motion: 15
54120458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 329
Coasting Arc #18 (Orbit 3449)
---------------------------------------
Vector Time (GMT): 2018/142/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907500
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4230613
99 A = 6787336
60 meter
Y = -4848098
27 meter E =
0016472
Z = 2137270
30 I = 51
85873
XDOT = 4974
874424 Wp = 106
47668
YDOT = 1892
192779 meter/sec RA = 146
22858 deg
ZDOT = -5524
698252 TA = 49
89508
MA = 49
75082
Ha = 221
969 n
mi
Hp = 213
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13879967
17 X = 4274130
58
Y = -15905834
20 feet Y = -4800545
44 meter
Z = 7012041
68 Z = 2157926
60
XDOT = 16321
766483 XDOT = 4980
181782
YDOT = 6207
981559 feet/sec YDOT = 1947
855262 meter/sec
ZDOT = -18125
650432 ZDOT = -5500
518986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9158022
18 X = 2791365
16
Y = -18985982
98 feet Y = -5786927
61 meter
Z = 7104988
31 Z = 2165600
44
XDOT = 16110
819274 XDOT = 4910
577715
YDOT = 991
394119 feet/sec YDOT = 302
176927 meter/sec
ZDOT = -18017
764626 ZDOT = -5491
814658
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 18142
41480288
00016717 00000-0 10270-3 0 9176
2 25544 51
6392 147
1918 0002724 88
8514 271
2951 15
54131174 34509
Satellite: ISS
Catalog Number: 25544
Epoch time: 18142
41480288 = yrday
fracday
Element set: 917
Inclination: 51
6392 deg
RA of node: 147
1918 deg
Eccentricity:
0002724
Arg of perigee: 88
8514 deg
Mean anomaly: 271
2951 deg
Mean motion: 15
54131174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3450
Checksum: 309
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