[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 16th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
291/16:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
4
295/18:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 216
2
300/09:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
6
Coasting Arc #1 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2018/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5751335
63 A = 6788323
93 meter
Y = -2870463
86 meter E =
0003240
Z = -2176685
51 I = 51
90330
XDOT = 561
754308 Wp = 174
43075
YDOT = 5299
963765 meter/sec RA = 138
08033 deg
ZDOT = -5508
763143 TA = 29
62122
MA = 29
60288
Ha = 220
271 n
mi
Hp = 216
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18869211
40 X = 5793579
86
Y = -9417532
35 feet Y = -2805912
30 meter
Z = -7141356
67 Z = -2148644
40
XDOT = 1843
025945 XDOT = 529
205961
YDOT = 17388
332561 feet/sec YDOT = 5306
063524 meter/sec
ZDOT = -18073
369892 ZDOT = -5506
113521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13706975
26 X = -4177886
06
Y = 16082433
50 feet Y = 4901925
73 meter
Z = -7014997
60 Z = -2138171
27
XDOT = -7452
349211 XDOT = -2271
476040
YDOT = -14224
477847 feet/sec YDOT = -4335
620848 meter/sec
ZDOT = -18061
972688 ZDOT = -5505
289275
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 18288
52794481
00016717 00000-0 10270-3 0 9004
2 25544 51
6387 139
0295 0004152 291
1672 68
9037 15
53807105 17221
Satellite: ISS
Catalog Number: 25544
Epoch time: 18288
52794481 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 139
0295 deg
Eccentricity:
0004152
Arg of perigee: 291
1672 deg
Mean anomaly: 68
9037 deg
Mean motion: 15
53807105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 319
Coasting Arc #2 (Orbit 1737)
---------------------------------------
Vector Time (GMT): 2018/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5494919
60 A = 6785035
40 meter
Y = 1819071
74 meter E =
0008649
Z = 3531471
67 I = 51
91610
XDOT = 883
361271 Wp = 80
01879
YDOT = -6130
086736 meter/sec RA = 133
12066 deg
ZDOT = 4524
185105 TA = 321
41107
MA = 321
47285
Ha = 220
507 n
mi
Hp = 216
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18027951
46 X = -5532006
82
Y = 5968083
14 feet Y = 1757416
49 meter
Z = 11586193
14 Z = 3504688
77
XDOT = 2898
166898 XDOT = 929
867565
YDOT = -20111
833123 feet/sec YDOT = -6119
948185 meter/sec
ZDOT = 14843
126985 ZDOT = 4528
589395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14094376
06 X = 4295965
82
Y = -12835654
91 feet Y = -3912307
62 meter
Z = 11465576
66 Z = 3494707
77
XDOT = 4712
675767 XDOT = 1436
423574
YDOT = 18475
335160 feet/sec YDOT = 5631
282157 meter/sec
ZDOT = 14863
537948 ZDOT = 4530
406367
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 18289
55697908
00016717 00000-0 10270-3 0 9015
2 25544 51
6384 133
9006 0004165 296
8744 63
1983 15
53824177 17389
Satellite: ISS
Catalog Number: 25544
Epoch time: 18289
55697908 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 133
9006 deg
Eccentricity:
0004165
Arg of perigee: 296
8744 deg
Mean anomaly: 63
1983 deg
Mean motion: 15
53824177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1738
Checksum: 348
Coasting Arc #3 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2018/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4982730
53 A = 6781468
41 meter
Y = -539288
11 meter E =
0007876
Z = -4576101
32 I = 51
92436
XDOT = -2137
601858 Wp = 46
72152
YDOT = 6666
201451 meter/sec RA = 128
15474 deg
ZDOT = -3111
257661 TA = 192
21019
MA = 192
22928
Ha = 220
469 n
mi
Hp = 216
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16347541
12 X = 5010619
21
Y = -1769317
94 feet Y = -483412
01 meter
Z = -15013455
77 Z = -4551828
91
XDOT = -7013
129457 XDOT = -2196
873289
YDOT = 21870
739667 feet/sec YDOT = 6641
965764 meter/sec
ZDOT = -10207
538259 ZDOT = -3121
785748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14148528
66 X = -4312471
54
Y = 8570830
61 feet Y = 2612389
17 meter
Z = -14904242
36 Z = -4542813
07
XDOT = -2348
178979 XDOT = -715
724953
YDOT = -21721
095384 feet/sec YDOT = -6620
589873 meter/sec
ZDOT = -10255
553939 ZDOT = -3125
892841
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 18290
52169697
00016717 00000-0 10270-3 0 9024
2 25544 51
6367 129
0936 0004040 300
1807 59
8945 15
53828147 17537
Satellite: ISS
Catalog Number: 25544
Epoch time: 18290
52169697 = yrday
fracday
Element set: 902
Inclination: 51
6367 deg
RA of node: 129
0936 deg
Eccentricity:
0004040
Arg of perigee: 300
1807 deg
Mean anomaly: 59
8945 deg
Mean motion: 15
53828147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 325
Coasting Arc #4 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2018/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4272072
27 A = 6779005
62 meter
Y = -889538
00 meter E =
0000526
Z = 5187541
24 I = 51
93594
XDOT = 3149
224038 Wp = 135
88759
YDOT = -6846
248175 meter/sec RA = 123
18188 deg
ZDOT = 1419
046185 TA = 300
51568
MA = 300
52087
Ha = 220
760 n
mi
Hp = 216
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14015985
15 X = -4287006
31
Y = -2918431
75 feet Y = -937394
50 meter
Z = 17019492
27 Z = 5166752
55
XDOT = 10332
099862 XDOT = 3218
653583
YDOT = -22461
444143 feet/sec YDOT = -6810
643085 meter/sec
ZDOT = 4655
663338 ZDOT = 1434
513181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13974777
70 X = 4259512
24
Y = -3583510
24 feet Y = -1092253
92 meter
Z = 16926081
74 Z = 5159069
71
XDOT = 347
410766 XDOT = 105
890802
YDOT = 23683
960208 feet/sec YDOT = 7218
871071 meter/sec
ZDOT = 4725
924552 ZDOT = 1440
461803
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 18291
55072899
00016717 00000-0 10270-3 0 9036
2 25544 51
6372 123
9658 0004049 303
8498 56
2269 15
53795356 17694
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
55072899 = yrday
fracday
Element set: 903
Inclination: 51
6372 deg
RA of node: 123
9658 deg
Eccentricity:
0004049
Arg of perigee: 303
8498 deg
Mean anomaly: 56
2269 deg
Mean motion: 15
53795356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 354
Coasting Arc #5 (Orbit 1770)
---------------------------------------
Vector Time (GMT): 2018/291/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 492064
93 A = 6782857
45 meter
Y = 5329663
51 meter E =
0004058
Z = -4170472
40 I = 51
95378
XDOT = -5691
660185 Wp = 101
19808
YDOT = 3476
654504 meter/sec RA = 122
29878 deg
ZDOT = 3773
788024 TA = 207
49798
MA = 207
51946
Ha = 220
502 n
mi
Hp = 216
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1614386
24 X = 452688
74
Y = 17485772
69 feet Y = 5334945
73 meter
Z = -13682652
22 Z = -4168178
03
XDOT = -18673
425804 XDOT = -5748
445353
YDOT = 11406
346797 feet/sec YDOT = 3412
689111 meter/sec
ZDOT = 12381
194306 ZDOT = 3746
001509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17543084
47 X = -5347132
15
Y = 930657
66 feet Y = 283664
45 meter
Z = -13672875
51 Z = -4167492
46
XDOT = -10498
984722 XDOT = -3200
090543
YDOT = -17962
127259 feet/sec YDOT = -5474
856388 meter/sec
ZDOT = 12255
863423 ZDOT = 3735
587171
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 18291
67935777
00016717 00000-0 10270-3 0 9043
2 25544 51
6386 123
3224 0003779 298
8068 61
2705 15
53823726 17714
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
67935777 = yrday
fracday
Element set: 904
Inclination: 51
6386 deg
RA of node: 123
3224 deg
Eccentricity:
0003779
Arg of perigee: 298
8068 deg
Mean anomaly: 61
2705 deg
Mean motion: 15
53823726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1771
Checksum: 341
Coasting Arc #6 (Orbit 1786)
---------------------------------------
Vector Time (GMT): 2018/292/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 532763
53 A = 6786482
28 meter
Y = -6077264
39 meter E =
0009993
Z = 2964823
07 I = 51
98317
XDOT = 5444
560819 Wp = 88
56485
YDOT = -1980
482950 meter/sec RA = 117
33923 deg
ZDOT = -5023
118640 TA = 57
73670
MA = 57
63991
Ha = 220
593 n
mi
Hp = 216
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1747911
85 X = 586279
89
Y = -19938531
46 feet Y = -6071007
22 meter
Z = 9727109
79 Z = 2967541
48
XDOT = 17862
732347 XDOT = 5490
702416
YDOT = -6497
647475 feet/sec YDOT = -1919
340445 meter/sec
ZDOT = -16480
048032 ZDOT = -4996
558349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19885064
65 X = 6060967
71
Y = 2221301
69 feet Y = 677052
75 meter
Z = 9739965
10 Z = 2968741
36
XDOT = 6172
800838 XDOT = 1881
469695
YDOT = 16690
984559 feet/sec YDOT = 5087
412093 meter/sec
ZDOT = -16360
373051 ZDOT = -4986
641706
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 18292
70838518
00016717 00000-0 10270-3 0 9054
2 25544 51
6391 118
1944 0003678 303
0368 57
0430 15
53823381 17873
Satellite: ISS
Catalog Number: 25544
Epoch time: 18292
70838518 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 118
1944 deg
Eccentricity:
0003678
Arg of perigee: 303
0368 deg
Mean anomaly: 57
0430 deg
Mean motion: 15
53823381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 321
Coasting Arc #7 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2018/293/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1393180
95 A = 6789220
17 meter
Y = 6466576
99 meter E =
0009144
Z = -1504303
84 I = 52
00676
XDOT = -5009
376308 Wp = 13
63067
YDOT = 266
313832 meter/sec RA = 112
38983 deg
ZDOT = 5799
926253 TA = 330
02696
MA = 330
07927
Ha = 220
735 n
mi
Hp = 216
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4570803
64 X = -1458081
26
Y = 21215803
78 feet Y = 6450634
47 meter
Z = -4935380
05 Z = -1511229
69
XDOT = -16434
961641 XDOT = -5040
155352
YDOT = 873
733046 feet/sec YDOT = 210
123891 meter/sec
ZDOT = 19028
629438 ZDOT = 5775
517342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21169846
90 X = -6452569
34
Y = -4746043
58 feet Y = -1446594
08 meter
Z = -4967212
94 Z = -1514006
50
XDOT = -1058
466375 XDOT = -322
620551
YDOT = -15025
264388 feet/sec YDOT = -4579
700585 meter/sec
ZDOT = 18918
801898 ZDOT = 5766
450818
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 18293
67309554
00016717 00000-0 10270-3 0 9065
2 25544 51
6392 113
3878 0003750 309
1536 50
9282 15
53831041 18029
Satellite: ISS
Catalog Number: 25544
Epoch time: 18293
67309554 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 113
3878 deg
Eccentricity:
0003750
Arg of perigee: 309
1536 deg
Mean anomaly: 50
9282 deg
Mean motion: 15
53831041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 308
Coasting Arc #8 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2018/294/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2123879
60 A = 6790134
67 meter
Y = -6444079
78 meter E =
0008165
Z = -120635
98 I = 52
02111
XDOT = 4448
978836 Wp = 137
48651
YDOT = 1574
859657 meter/sec RA = 107
44619 deg
ZDOT = -6041
404436 TA = 43
80577
MA = 43
74103
Ha = 220
748 n
mi
Hp = 216
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6968108
92 X = 2196367
24
Y = -21141994
04 feet Y = -6419923
79 meter
Z = -395787
35 Z = -110142
10
XDOT = 14596
387256 XDOT = 4460
384096
YDOT = 5166
862392 feet/sec YDOT = 1624
674450 meter/sec
ZDOT = -19820
880695 ZDOT = -6019
764931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21192880
47 X = 6459589
97
Y = 6814388
40 feet Y = 2077025
58 meter
Z = -347892
97 Z = -106037
78
XDOT = -4559
705974 XDOT = -1389
798381
YDOT = 13220
241797 feet/sec YDOT = 4029
529700 meter/sec
ZDOT = -19723
702815 ZDOT = -6011
784618
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 18294
70211832
00016717 00000-0 10270-3 0 9072
2 25544 51
6388 108
2602 0003748 311
1839 48
8990 15
53849125 18189
Satellite: ISS
Catalog Number: 25544
Epoch time: 18294
70211832 = yrday
fracday
Element set: 907
Inclination: 51
6388 deg
RA of node: 108
2602 deg
Eccentricity:
0003748
Arg of perigee: 311
1839 deg
Mean anomaly: 48
8990 deg
Mean motion: 15
53849125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 325
Coasting Arc #9 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2018/295/16:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2695567
04 A = 6788913
75 meter
Y = 5981992
14 meter E =
0013321
Z = 1712532
27 I = 52
02721
XDOT = -3831
199127 Wp = 48
73120
YDOT = -3371
802022 meter/sec RA = 102
50235 deg
ZDOT = 5727
297992 TA = 329
95387
MA = 330
03023
Ha = 220
942 n
mi
Hp = 216
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8843723
90 X = -2770577
75
Y = 19625958
46 feet Y = 5951429
18 meter
Z = 5618544
19 Z = 1699255
14
XDOT = -12569
550942 XDOT = -3821
030713
YDOT = -11062
342593 feet/sec YDOT = -3414
587778 meter/sec
ZDOT = 18790
347742 ZDOT = 5708
711984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19838713
41 X = -6046839
85
Y = -8395832
06 feet Y = -2559049
61 meter
Z = 5558164
35 Z = 1694128
49
XDOT = 10133
405449 XDOT = 3088
661981
YDOT = -11515
658783 feet/sec YDOT = -3509
972797 meter/sec
ZDOT = 18707
102545 ZDOT = 5701
924856
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 18295
73113811
00016717 00000-0 10270-3 0 9085
2 25544 51
6400 103
1324 0003759 317
3191 42
7669 15
53854323 18340
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
73113811 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 103
1324 deg
Eccentricity:
0003759
Arg of perigee: 317
3191 deg
Mean anomaly: 42
7669 deg
Mean motion: 15
53854323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 299
Coasting Arc #10 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2018/295/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4042951
70 A = 6783120
69 meter
Y = -3584714
75 meter E =
0006727
Z = -4108026
52 I = 52
00735
XDOT = 1729
664836 Wp = 39
21814
YDOT = 6383
289607 meter/sec RA = 102
00799 deg
ZDOT = -3866
253106 TA = 190
95333
MA = 190
96798
Ha = 220
910 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13264277
24 X = 4102691
54
Y = -11760875
18 feet Y = -3539170
00 meter
Z = -13477777
31 Z = -4088241
44
XDOT = 5674
753399 XDOT = 1676
937169
YDOT = 20942
551203 feet/sec YDOT = 6402
336753 meter/sec
ZDOT = -12684
557434 ZDOT = -3857
979466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17504444
27 X = 5335354
61
Y = 3202408
80 feet Y = 976094
20 meter
Z = -13388380
24 Z = -4080778
30
XDOT = -12644
170611 XDOT = -3853
943202
YDOT = 16213
082195 feet/sec YDOT = 4941
747453 meter/sec
ZDOT = -12648
032979 ZDOT = -3855
120452
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 18295
79545149
00016717 00000-0 10270-3 0 9095
2 25544 51
6389 102
8141 0003934 317
2569 42
8277 15
53839635 18358
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
79545149 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 102
8141 deg
Eccentricity:
0003934
Arg of perigee: 317
2569 deg
Mean anomaly: 42
8277 deg
Mean motion: 15
53839635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 347
Coasting Arc #11 (Orbit 1850)
---------------------------------------
Vector Time (GMT): 2018/296/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4146825
21 A = 6779841
19 meter
Y = 2079016
85 meter E =
0003175
Z = 4941859
71 I = 52
00280
XDOT = -907
255369 Wp = 95
58993
YDOT = -7262
667035 meter/sec RA = 97
04307 deg
ZDOT = 2292
509205 TA = 332
11132
MA = 332
12833
Ha = 221
160 n
mi
Hp = 215
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13605069
57 X = -4193770
69
Y = 6820921
41 feet Y = 2032382
07 meter
Z = 16213450
49 Z = 4921601
19
XDOT = -2976
559610 XDOT = -837
110850
YDOT = -23827
647753 feet/sec YDOT = -7272
420210 meter/sec
ZDOT = 7521
355659 ZDOT = 2288
272917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13958444
21 X = -4254533
80
Y = -6303904
21 feet Y = -1921430
00 meter
Z = 16122080
84 Z = 4914010
24
XDOT = 16078
573120 XDOT = 4900
749087
YDOT = -16399
849196 feet/sec YDOT = -4998
674035 meter/sec
ZDOT = 7503
107330 ZDOT = 2286
947114
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 18296
82446741
00016717 00000-0 10270-3 0 9100
2 25544 51
6392 97
6861 0004019 322
2657 37
8214 15
53866653 18514
Satellite: ISS
Catalog Number: 25544
Epoch time: 18296
82446741 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 97
6861 deg
Eccentricity:
0004019
Arg of perigee: 322
2657 deg
Mean anomaly: 37
8214 deg
Mean motion: 15
53866653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 328
Coasting Arc #12 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2018/297/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4181703
81 A = 6778307
17 meter
Y = -415662
57 meter E =
0013208
Z = -5329509
30 I = 51
99956
XDOT = 115
828499 Wp = 70
84922
YDOT = 7641
318623 meter/sec RA = 92
07271 deg
ZDOT = -501
884577 TA = 194
36168
MA = 194
39926
Ha = 221
191 n
mi
Hp = 216
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13719500
69 X = 4211929
74
Y = -1363722
34 feet Y = -368731
18 meter
Z = -17485266
74 Z = -5309122
02
XDOT = 380
014760 XDOT = 32
810495
YDOT = 25069
942988 feet/sec YDOT = 7642
149684 meter/sec
ZDOT = -1646
602943 ZDOT = -501
524027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9977930
99 X = 3041273
37
Y = 9681220
00 feet Y = 2950835
86 meter
Z = -17393500
60 Z = -5301538
98
XDOT = -18181
213876 XDOT = -5541
633989
YDOT = 15762
496815 feet/sec YDOT = 4804
409029 meter/sec
ZDOT = -1645
853916 ZDOT = -501
656274
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 18297
78917046
00016717 00000-0 10270-3 0 9118
2 25544 51
6385 92
8794 0004012 326
2766 33
8131 15
53831065 18665
Satellite: ISS
Catalog Number: 25544
Epoch time: 18297
78917046 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 92
8794 deg
Eccentricity:
0004012
Arg of perigee: 326
2766 deg
Mean anomaly: 33
8131 deg
Mean motion: 15
53831065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 327
Coasting Arc #13 (Orbit 1881)
---------------------------------------
Vector Time (GMT): 2018/298/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4139439
20 A = 6778661
94 meter
Y = -1301966
80 meter E =
0006217
Z = 5207579
63 I = 52
00225
XDOT = 668
991994 Wp = 14
13448
YDOT = -7520
296938 meter/sec RA = 87
10039 deg
ZDOT = -1342
201171 TA = 88
73415
MA = 88
66293
Ha = 221
325 n
mi
Hp = 215
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13580837
27 X = -4149869
03
Y = -4271544
62 feet Y = -1348314
98 meter
Z = 17085235
02 Z = 5187445
79
XDOT = 2194
855623 XDOT = 759
556230
YDOT = -24672
890215 feet/sec YDOT = -7512
309484 meter/sec
ZDOT = -4403
547149 ZDOT = -1338
731060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5810819
49 X = -1771137
78
Y = -13114930
07 feet Y = -3997430
68 meter
Z = 16994807
33 Z = 5180017
27
XDOT = 19069
093221 XDOT = 5812
259614
YDOT = -14160
344615 feet/sec YDOT = -4316
073039 meter/sec
ZDOT = -4387
053824 ZDOT = -1337
174006
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 18298
81818152
00016717 00000-0 10270-3 0 9122
2 25544 51
6393 87
7517 0004102 330
3072 29
7847 15
53881812 18827
Satellite: ISS
Catalog Number: 25544
Epoch time: 18298
81818152 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 87
7517 deg
Eccentricity:
0004102
Arg of perigee: 330
3072 deg
Mean anomaly: 29
7847 deg
Mean motion: 15
53881812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1882
Checksum: 323
Coasting Arc #14 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2018/299/18:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4040681
05 A = 6781174
53 meter
Y = 2899276
13 meter E =
0007941
Z = -4616543
99 I = 52
00834
XDOT = -1454
687581 Wp = 87
03336
YDOT = 6876
278731 meter/sec RA = 82
13202 deg
ZDOT = 3050
111251 TA = 213
28185
MA = 213
33181
Ha = 221
513 n
mi
Hp = 215
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13256827
60 X = 4030385
64
Y = 9512060
80 feet Y = 2944404
18 meter
Z = -15146141
69 Z = -4596940
23
XDOT = -4772
597050 XDOT = -1546
288208
YDOT = 22559
969589 feet/sec YDOT = 6859
499291 meter/sec
ZDOT = 10006
926678 ZDOT = 3042
822052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1927034
99 X = 587360
26
Y = 16283818
62 feet Y = 4963307
91 meter
Z = -15058292
54 Z = -4589767
56
XDOT = -18775
841551 XDOT = -5722
876505
YDOT = 11429
667278 feet/sec YDOT = 3483
762586 meter/sec
ZDOT = 9973
305283 ZDOT = 3039
863450
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 18299
78287884
00016717 00000-0 10270-3 0 9132
2 25544 51
6399 82
9446 0004169 338
2043 21
8931 15
53864883 18971
Satellite: ISS
Catalog Number: 25544
Epoch time: 18299
78287884 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 82
9446 deg
Eccentricity:
0004169
Arg of perigee: 338
2043 deg
Mean anomaly: 21
8931 deg
Mean motion: 15
53864883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 367
Coasting Arc #15 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2018/300/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3385509
45 A = 6779574
50 meter
Y = -3090592
65 meter E =
0012938
Z = -5006504
39 I = 51
99688
XDOT = 2992
903543 Wp = 56
27691
YDOT = 6721
867393 meter/sec RA = 79
02570 deg
ZDOT = -2122
593674 TA = 193
11193
MA = 193
14560
Ha = 221
481 n
mi
Hp = 215
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11107314
48 X = 3444137
37
Y = -10139739
68 feet Y = -3052405
75 meter
Z = -16425539
33 Z = -4989915
86
XDOT = 9819
237347 XDOT = 2927
826049
YDOT = 22053
370712 feet/sec YDOT = 6754
972236 meter/sec
ZDOT = -6963
890006 ZDOT = -2108
212866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11023883
56 X = -3360079
71
Y = 10349846
48 feet Y = 3154633
21 meter
Z = -16350528
04 Z = -4983640
95
XDOT = -9523
162023 XDOT = -2902
659785
YDOT = -21059
778017 feet/sec YDOT = -6419
020340 meter/sec
ZDOT = -6900
010082 ZDOT = -2103
123073
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 18300
42600912
00016717 00000-0 10270-3 0 9148
2 25544 51
6370 79
7377 0004034 340
7218 19
3781 15
53871492 19071
Satellite: ISS
Catalog Number: 25544
Epoch time: 18300
42600912 = yrday
fracday
Element set: 914
Inclination: 51
6370 deg
RA of node: 79
7377 deg
Eccentricity:
0004034
Arg of perigee: 340
7218 deg
Mean anomaly: 19
3781 deg
Mean motion: 15
53871492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 303
Coasting Arc #16 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2018/301/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3911918
71 A = 6778256
19 meter
Y = 1481363
33 meter E =
0003567
Z = 5332304
03 I = 51
98452
XDOT = -2340
072783 Wp = 21
81730
YDOT = -7297
195494 meter/sec RA = 74
05342 deg
ZDOT = 313
646335 TA = 65
22587
MA = 65
18876
Ha = 221
779 n
mi
Hp = 215
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12834378
96 X = -3954095
17
Y = 4860115
91 feet Y = 1437381
65 meter
Z = 17494435
78 Z = 5313198
37
XDOT = -7677
404143 XDOT = -2259
823157
YDOT = -23940
930098 feet/sec YDOT = -7322
915113 meter/sec
ZDOT = 1029
023408 ZDOT = 302
473603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12767205
59 X = 3891444
26
Y = -5324211
75 feet Y = -1622819
74 meter
Z = 17408288
94 Z = 5306046
47
XDOT = 8152
268644 XDOT = 2484
811483
YDOT = 22717
877888 feet/sec YDOT = 6924
409180 meter/sec
ZDOT = 979
665812 ZDOT = 298
602140
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 18301
45501655
00016717 00000-0 10270-3 0 9157
2 25544 51
6368 74
6096 0004067 344
0113 16
0911 15
53826299 19239
Satellite: ISS
Catalog Number: 25544
Epoch time: 18301
45501655 = yrday
fracday
Element set: 915
Inclination: 51
6368 deg
RA of node: 74
6096 deg
Eccentricity:
0004067
Arg of perigee: 344
0113 deg
Mean anomaly: 16
0911 deg
Mean motion: 15
53826299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 300
Coasting Arc #17 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2018/302/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4388526
21 A = 6778849
77 meter
Y = 148450
10 meter E =
0012602
Z = -5174979
42 I = 51
97872
XDOT = 1537
384876 Wp = 84
44349
YDOT = 7347
862651 meter/sec RA = 69
08020 deg
ZDOT = 1518
884660 TA = 200
11179
MA = 200
16149
Ha = 221
676 n
mi
Hp = 215
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14398051
89 X = 4411677
89
Y = 487041
02 feet Y = 197655
22 meter
Z = -16978278
94 Z = -5153604
79
XDOT = 5043
913636 XDOT = 1447
726669
YDOT = 24107
160928 feet/sec YDOT = 7364
553411 meter/sec
ZDOT = 4983
217388 ZDOT = 1526
135301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14516024
18 X = -4424484
17
Y = 286355
26 feet Y = 87281
08 meter
Z = -16882123
85 Z = -5145671
35
XDOT = -6264
364181 XDOT = -1909
378202
YDOT = -22748
514538 feet/sec YDOT = -6933
747231 meter/sec
ZDOT = 5014
905370 ZDOT = 1528
543157
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 18302
41970578
00016717 00000-0 10270-3 0 9169
2 25544 51
6387 69
8026 0004014 348
0090 12
0967 15
53880137 19383
Satellite: ISS
Catalog Number: 25544
Epoch time: 18302
41970578 = yrday
fracday
Element set: 916
Inclination: 51
6387 deg
RA of node: 69
8026 deg
Eccentricity:
0004014
Arg of perigee: 348
0090 deg
Mean anomaly: 12
0967 deg
Mean motion: 15
53880137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 316
Coasting Arc #18 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2018/303/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4758192
15 A = 6781629
22 meter
Y = -1722708
60 meter E =
0010694
Z = 4511896
64 I = 51
97375
XDOT = -560
579697 Wp = 47
11308
YDOT = -6934
125499 meter/sec RA = 64
10986 deg
ZDOT = -3226
819005 TA = 75
23360
MA = 75
11512
Ha = 221
873 n
mi
Hp = 215
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15610866
62 X = -4760491
47
Y = -5651931
10 feet Y = -1775930
96 meter
Z = 14802810
49 Z = 4488776
99
XDOT = -1839
172234 XDOT = -467
324267
YDOT = -22749
755574 feet/sec YDOT = -6939
872797 meter/sec
ZDOT = -10586
676527 ZDOT = -3229
315797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16067582
68 X = 4897399
20
Y = 4531967
36 feet Y = 1381343
65 meter
Z = 14699004
69 Z = 4480256
63
XDOT = 3694
925262 XDOT = 1126
213220
YDOT = 21398
123607 feet/sec YDOT = 6522
148075 meter/sec
ZDOT = -10597
013954 ZDOT = -3229
969853
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 18303
44870654
00016717 00000-0 10270-3 0 9178
2 25544 51
6376 64
6743 0003978 352
2277 7
8813 15
53849039 19548
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
44870654 = yrday
fracday
Element set: 917
Inclination: 51
6376 deg
RA of node: 64
6743 deg
Eccentricity:
0003978
Arg of perigee: 352
2277 deg
Mean anomaly: 7
8813 deg
Mean motion: 15
53849039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 340
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