[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 18th 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
303/21:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (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 = 4982485
14 A = 6781463
73 meter
Y = -538548
77 meter E =
0007878
Z = -4576446
97 I = 51
92433
XDOT = -2138
308719 Wp = 46
58204
YDOT = 6666
291645 meter/sec RA = 128
15455 deg
ZDOT = -3110
588212 TA = 192
35698
MA = 192
37631
Ha = 220
467 n
mi
Hp = 216
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16346736
02 X = 5010367
25
Y = -1766892
28 feet Y = -482675
45 meter
Z = -15014589
81 Z = -4552175
78
XDOT = -7015
448552 XDOT = -2197
584357
YDOT = 21871
035580 feet/sec YDOT = 6642
048031 meter/sec
ZDOT = -10205
341902 ZDOT = -3121
119743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14148833
71 X = -4312564
52
Y = 8568295
56 feet Y = 2611616
49 meter
Z = -14905381
91 Z = -4543160
41
XDOT = -2346
375326 XDOT = -715
175199
YDOT = -21722
329892 feet/sec YDOT = -6620
966151 meter/sec
ZDOT = -10253
373080 ZDOT = -3125
228115
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
52169558
00016717 00000-0 10270-3 0 9008
2 25544 51
6367 129
0935 0004059 300
2730 59
8020 15
53829294 17530
Satellite: ISS
Catalog Number: 25544
Epoch time: 18290
52169558 = yrday
fracday
Element set: 900
Inclination: 51
6367 deg
RA of node: 129
0935 deg
Eccentricity:
0004059
Arg of perigee: 300
2730 deg
Mean anomaly: 59
8020 deg
Mean motion: 15
53829294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 312
Coasting Arc #2 (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 = -4271469
33 A = 6779000
05 meter
Y = -890849
21 meter E =
0000502
Z = 5187814
32 I = 51
93590
XDOT = 3150
244328 Wp = 135
65991
YDOT = -6846
037584 meter/sec RA = 123
18167 deg
ZDOT = 1417
772495 TA = 300
75591
MA = 300
76085
Ha = 220
758 n
mi
Hp = 216
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14014007
00 X = -4286390
08
Y = -2922733
62 feet Y = -938698
90 meter
Z = 17020388
20 Z = 5167028
60
XDOT = 10335
447271 XDOT = 3219
677630
YDOT = -22460
753229 feet/sec YDOT = -6810
421064 meter/sec
ZDOT = 4651
484565 ZDOT = 1433
244457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13974894
92 X = 4259547
97
Y = -3578779
36 feet Y = -1090811
95 meter
Z = 16926991
13 Z = 5159346
90
XDOT = 344
420176 XDOT = 104
979270
YDOT = 23684
813314 feet/sec YDOT = 7219
131098 meter/sec
ZDOT = 4721
768091 ZDOT = 1439
194914
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
55072673
00016717 00000-0 10270-3 0 9014
2 25544 51
6372 123
9657 0004068 303
9418 56
1347 15
53796853 17696
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
55072673 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 123
9657 deg
Eccentricity:
0004068
Arg of perigee: 303
9418 deg
Mean anomaly: 56
1347 deg
Mean motion: 15
53796853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1769
Checksum: 334
Coasting Arc #3 (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 = 490924
31 A = 6782855
63 meter
Y = 5330356
40 meter E =
0004039
Z = -4169691
30 I = 51
95376
XDOT = -5691
791485 Wp = 100
98117
YDOT = 3475
294518 meter/sec RA = 122
29858 deg
ZDOT = 3774
882582 TA = 207
72807
MA = 207
74961
Ha = 220
500 n
mi
Hp = 216
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1610644
06 X = 451536
67
Y = 17488045
94 feet Y = 5335625
80 meter
Z = -13680089
56 Z = -4167402
50
XDOT = -18673
856578 XDOT = -5748
566753
YDOT = 11401
884902 feet/sec YDOT = 3411
327712 meter/sec
ZDOT = 12384
785375 ZDOT = 3747
095453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17545189
49 X = -5347773
76
Y = 926801
67 feet Y = 282489
15 meter
Z = -13670337
96 Z = -4166719
01
XDOT = -10494
788531 XDOT = -3198
811544
YDOT = -17962
230707 feet/sec YDOT = -5474
887920 meter/sec
ZDOT = 12259
451869 ZDOT = 3736
680930
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
67935537
00016717 00000-0 10270-3 0 9025
2 25544 51
6386 123
3223 0003798 298
9346 61
1425 15
53825271 17719
Satellite: ISS
Catalog Number: 25544
Epoch time: 18291
67935537 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 123
3223 deg
Eccentricity:
0003798
Arg of perigee: 298
9346 deg
Mean anomaly: 61
1425 deg
Mean motion: 15
53825271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1771
Checksum: 328
Coasting Arc #4 (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 = 534380
87 A = 6786480
49 meter
Y = -6077870
60 meter E =
0009983
Z = 2963313
27 I = 51
98315
XDOT = 5444
341906 Wp = 88
49615
YDOT = -1978
160100 meter/sec RA = 117
33902 deg
ZDOT = -5024
251212 TA = 57
82490
MA = 57
72812
Ha = 220
590 n
mi
Hp = 216
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1753218
07 X = 587911
22
Y = -19940520
33 feet Y = -6071595
27 meter
Z = 9722156
40 Z = 2966039
58
XDOT = 17862
014127 XDOT = 5490
463046
YDOT = -6490
026576 feet/sec YDOT = -1917
020158 meter/sec
ZDOT = -16483
763819 ZDOT = -4997
692034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19886908
88 X = 6061529
83
Y = 2226692
55 feet Y = 678695
89 meter
Z = 9735047
26 Z = 2967242
40
XDOT = 6165
594838 XDOT = 1879
273307
YDOT = 16689
950922 feet/sec YDOT = 5087
097041 meter/sec
ZDOT = -16364
094085 ZDOT = -4987
775877
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
70838163
00016717 00000-0 10270-3 0 9038
2 25544 51
6391 118
1943 0003697 303
1658 56
9140 15
53825292 17875
Satellite: ISS
Catalog Number: 25544
Epoch time: 18292
70838163 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 118
1943 deg
Eccentricity:
0003697
Arg of perigee: 303
1658 deg
Mean anomaly: 56
9140 deg
Mean motion: 15
53825292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 327
Coasting Arc #5 (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 = -1395246
32 A = 6789216
67 meter
Y = 6466673
34 meter E =
0009166
Z = -1501873
73 I = 52
00674
XDOT = -5008
646732 Wp = 13
55597
YDOT = 262
879967 meter/sec RA = 112
38961 deg
ZDOT = 5800
743370 TA = 330
12873
MA = 330
18102
Ha = 220
733 n
mi
Hp = 216
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4577579
78 X = -1460159
35
Y = 21216119
87 feet Y = 6450707
65 meter
Z = -4927407
25 Z = -1508809
64
XDOT = -16432
568019 XDOT = -5039
391401
YDOT = 862
467084 feet/sec YDOT = 206
698377 meter/sec
ZDOT = 19031
310268 ZDOT = 5776
338087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21170096
48 X = -6452645
41
Y = -4752875
40 feet Y = -1448676
42 meter
Z = -4959285
42 Z = -1511590
20
XDOT = -1047
722671 XDOT = -319
345870
YDOT = -15022
759908 feet/sec YDOT = -4578
937220 meter/sec
ZDOT = 18921
499407 ZDOT = 5767
273019
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
67309069
00016717 00000-0 10270-3 0 9044
2 25544 51
6392 113
3876 0003770 309
2686 50
8132 15
53833310 18020
Satellite: ISS
Catalog Number: 25544
Epoch time: 18293
67309069 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 113
3876 deg
Eccentricity:
0003770
Arg of perigee: 309
2686 deg
Mean anomaly: 50
8132 deg
Mean motion: 15
53833310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 308
Coasting Arc #6 (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 = 2126308
91 A = 6790126
60 meter
Y = -6443223
63 meter E =
0008137
Z = -123967
20 I = 52
02107
XDOT = 4447
482784 Wp = 137
48615
YDOT = 1579
386601 meter/sec RA = 107
44597 deg
ZDOT = -6041
307198 TA = 43
84182
MA = 43
77726
Ha = 220
746 n
mi
Hp = 216
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6976079
10 X = 2198802
98
Y = -21139185
14 feet Y = -6419040
44 meter
Z = -406716
54 Z = -113461
50
XDOT = 14591
478949 XDOT = 4458
837062
YDOT = 5181
714570 feet/sec YDOT = 1629
184378 meter/sec
ZDOT = -19820
561674 ZDOT = -6019
675085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21190131
78 X = 6458752
17
Y = 6822451
63 feet Y = 2079483
26 meter
Z = -358769
09 Z = -109352
82
XDOT = -4574
006022 XDOT = -1394
157036
YDOT = 13215
641644 feet/sec YDOT = 4028
127573 meter/sec
ZDOT = -19723
417529 ZDOT = -6011
697663
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
70211184
00016717 00000-0 10270-3 0 9050
2 25544 51
6387 108
2601 0003768 311
3126 48
7702 15
53851787 18187
Satellite: ISS
Catalog Number: 25544
Epoch time: 18294
70211184 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 108
2601 deg
Eccentricity:
0003768
Arg of perigee: 311
3126 deg
Mean anomaly: 48
7702 deg
Mean motion: 15
53851787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 311
Coasting Arc #7 (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 = -2698261
63 A = 6788899
15 meter
Y = 5979583
23 meter E =
0013325
Z = 1716603
29 I = 52
02716
XDOT = -3828
772707 Wp = 48
69462
YDOT = -3377
232788 meter/sec RA = 102
50210 deg
ZDOT = 5725
745284 TA = 330
03660
MA = 330
11280
Ha = 220
940 n
mi
Hp = 216
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8852564
41 X = -2773264
98
Y = 19618055
22 feet Y = 5948990
18 meter
Z = 5631900
56 Z = 1703313
09
XDOT = -12561
590246 XDOT = -3818
536202
YDOT = -11080
160064 feet/sec YDOT = -3419
991028 meter/sec
ZDOT = 18785
253556 ZDOT = 5707
171229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19831032
99 X = -6044498
86
Y = -8404952
77 feet Y = -2561829
60 meter
Z = 5571462
18 Z = 1698181
67
XDOT = 10150
749302 XDOT = 3093
948387
YDOT = -11508
664793 feet/sec YDOT = -3507
841029 meter/sec
ZDOT = 18702
062722 ZDOT = 5700
388718
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
73112977
00016717 00000-0 10270-3 0 9065
2 25544 51
6400 103
1322 0003780 317
4331 42
6528 15
53857339 18342
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
73112977 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 103
1322 deg
Eccentricity:
0003780
Arg of perigee: 317
4331 deg
Mean anomaly: 42
6528 deg
Mean motion: 15
53857339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 301
Coasting Arc #8 (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 = 4044184
81 A = 6783102
34 meter
Y = -3580115
05 meter E =
0006751
Z = -4110814
73 I = 52
00729
XDOT = 1725
963783 Wp = 39
08263
YDOT = 6386
587247 meter/sec RA = 102
00770 deg
ZDOT = -3862
449969 TA = 191
13561
MA = 191
15056
Ha = 220
909 n
mi
Hp = 216
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13268322
87 X = 4103886
67
Y = -11745784
29 feet Y = -3534556
73 meter
Z = -13486924
97 Z = -4091023
75
XDOT = 5662
610837 XDOT = 1673
181042
YDOT = 20953
370232 feet/sec YDOT = 6405
592698 meter/sec
ZDOT = -12672
079951 ZDOT = -3854
194442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17495137
89 X = 5332518
03
Y = 3214977
36 feet Y = 979925
10 meter
Z = -13397501
87 Z = -4083558
57
XDOT = -12659
320238 XDOT = -3858
560809
YDOT = 16210
861165 feet/sec YDOT = 4941
070483 meter/sec
ZDOT = -12635
637340 ZDOT = -3851
342261
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
79544302
00016717 00000-0 10270-3 0 9073
2 25544 51
6389 102
8139 0003955 317
3679 42
7166 15
53842646 18353
Satellite: ISS
Catalog Number: 25544
Epoch time: 18295
79544302 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 102
8139 deg
Eccentricity:
0003955
Arg of perigee: 317
3679 deg
Mean anomaly: 42
7166 deg
Mean motion: 15
53842646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 340
Coasting Arc #9 (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 = -4147634
62 A = 6779822
62 meter
Y = 2072427
55 meter E =
0003151
Z = 4943931
50 I = 52
00274
XDOT = -902
485127 Wp = 95
18606
YDOT = -7265
074269 meter/sec RA = 97
04272 deg
ZDOT = 2286
767073 TA = 332
57419
MA = 332
59081
Ha = 221
159 n
mi
Hp = 215
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13607725
14 X = -4194516
43
Y = 6799303
00 feet Y = 2025784
08 meter
Z = 16220247
69 Z = 4923669
19
XDOT = -2960
909208 XDOT = -832
286150
YDOT = -23835
545502 feet/sec YDOT = -7274
773795 meter/sec
ZDOT = 7502
516644 ZDOT = 2282
554090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13943410
75 X = -4249951
60
Y = -6319672
01 feet Y = -1926236
03 meter
Z = 16128861
79 Z = 4916077
07
XDOT = 16093
520823 XDOT = 4905
305147
YDOT = -16393
725401 feet/sec YDOT = -4996
807502 meter/sec
ZDOT = 7484
373429 ZDOT = 2281
237021
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
82445681
00016717 00000-0 10270-3 0 9089
2 25544 51
6392 97
6859 0004041 322
3696 37
7173 15
53870058 18517
Satellite: ISS
Catalog Number: 25544
Epoch time: 18296
82445681 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 97
6859 deg
Eccentricity:
0004041
Arg of perigee: 322
3696 deg
Mean anomaly: 37
7173 deg
Mean motion: 15
53870058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1851
Checksum: 340
Coasting Arc #10 (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 = 4181820
47 A = 6778293
67 meter
Y = -407266
69 meter E =
0013210
Z = -5330044
64 I = 51
99952
XDOT = 110
000838 Wp = 70
81380
YDOT = 7641
904675 meter/sec RA = 92
07230 deg
ZDOT = -494
388446 TA = 194
46838
MA = 194
50623
Ha = 221
190 n
mi
Hp = 216
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13719883
42 X = 4211955
10
Y = -1336176
79 feet Y = -360334
51 meter
Z = -17487023
08 Z = -5309657
01
XDOT = 360
895138 XDOT = 26
940301
YDOT = 25071
865733 feet/sec YDOT = 7642
670330 meter/sec
ZDOT = -1622
009336 ZDOT = -494
056308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9957156
03 X = 3034941
16
Y = 9699311
61 feet Y = 2956350
18 meter
Z = -17395256
36 Z = -5302074
14
XDOT = -18193
817920 XDOT = -5545
475702
YDOT = 15750
533145 feet/sec YDOT = 4800
762502 meter/sec
ZDOT = -1621
388202 ZDOT = -494
199124
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
78915762
00016717 00000-0 10270-3 0 9098
2 25544 51
6384 92
8792 0004035 326
3824 33
7072 15
53834855 18666
Satellite: ISS
Catalog Number: 25544
Epoch time: 18297
78915762 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 92
8792 deg
Eccentricity:
0004035
Arg of perigee: 326
3824 deg
Mean anomaly: 33
7072 deg
Mean motion: 15
53834855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 348
Coasting Arc #11 (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 = -4138550
57 A = 6778657
63 meter
Y = -1311949
75 meter E =
0006254
Z = 5205781
33 I = 52
00224
XDOT = 675
972344 Wp = 14
14235
YDOT = -7518
083431 meter/sec RA = 87
09995 deg
ZDOT = -1351
055249 TA = 88
81262
MA = 88
74097
Ha = 221
323 n
mi
Hp = 215
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13577921
82 X = -4148860
10
Y = -4304297
10 feet Y = -1358287
33 meter
Z = 17079335
06 Z = 5185652
10
XDOT = 2217
757034 XDOT = 766
554319
YDOT = -24665
628055 feet/sec YDOT = -7510
017820 meter/sec
ZDOT = -4432
595960 ZDOT = -1347
551185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5784234
88 X = -1763034
79
Y = -13134288
31 feet Y = -4003331
08 meter
Z = 16988929
29 Z = 5178225
65
XDOT = 19077
437044 XDOT = 5814
802811
YDOT = -14140
127364 feet/sec YDOT = -4309
910821 meter/sec
ZDOT = -4415
950145 ZDOT = -1345
981604
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
81816603
00016717 00000-0 10270-3 0 9109
2 25544 51
6393 87
7515 0004124 330
4100 29
6818 15
53886002 18825
Satellite: ISS
Catalog Number: 25544
Epoch time: 18298
81816603 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 87
7515 deg
Eccentricity:
0004124
Arg of perigee: 330
4100 deg
Mean anomaly: 29
6818 deg
Mean motion: 15
53886002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1882
Checksum: 308
Coasting Arc #12 (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 = 4038400
41 A = 6781179
25 meter
Y = 2910011
85 meter E =
0007912
Z = -4611740
09 I = 52
00836
XDOT = -1462
722228 Wp = 86
80909
YDOT = 6870
502828 meter/sec RA = 82
13157 deg
ZDOT = 3059
358956 TA = 213
60755
MA = 213
65776
Ha = 221
511 n
mi
Hp = 215
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13249345
17 X = 4027961
78
Y = 9547282
99 feet Y = 2955113
60 meter
Z = -15130380
88 Z = -4592147
76
XDOT = -4798
957442 XDOT = -1554
302592
YDOT = 22541
019776 feet/sec YDOT = 6853
633653 meter/sec
ZDOT = 10037
266916 ZDOT = 3052
030775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1895845
41 X = 577853
68
Y = 16301859
08 feet Y = 4968806
65 meter
Z = -15042584
42 Z = -4584979
73
XDOT = -18778
332403 XDOT = -5723
635716
YDOT = 11399
537236 feet/sec YDOT = 3474
578950 meter/sec
ZDOT = 10003
470836 ZDOT = 3049
057911
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
78286063
00016717 00000-0 10270-3 0 9118
2 25544 51
6399 82
9443 0004192 338
2908 21
8066 15
53869605 18970
Satellite: ISS
Catalog Number: 25544
Epoch time: 18299
78286063 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 82
9443 deg
Eccentricity:
0004192
Arg of perigee: 338
2908 deg
Mean anomaly: 21
8066 deg
Mean motion: 15
53869605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 352
Coasting Arc #13 (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 = 3390664
81 A = 6779545
35 meter
Y = -3078964
66 meter E =
0012967
Z = -5010160
27 I = 51
99679
XDOT = 2985
479150 Wp = 56
27904
YDOT = 6728
650381 meter/sec RA = 79
02519 deg
ZDOT = -2111
525439 TA = 193
22183
MA = 193
25585
Ha = 221
480 n
mi
Hp = 215
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11124228
36 X = 3449180
07
Y = -10101590
09 feet Y = -3040720
74 meter
Z = -16437533
68 Z = -4993546
97
XDOT = 9794
879102 XDOT = 2920
272593
YDOT = 22075
624611 feet/sec YDOT = 6761
671478 meter/sec
ZDOT = -6927
576898 ZDOT = -2097
181010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11041590
51 X = -3365476
79
Y = 10312023
71 feet Y = 3143104
83 meter
Z = -16362412
36 Z = -4987263
29
XDOT = -9501
743208 XDOT = -2896
131330
YDOT = -21081
201522 feet/sec YDOT = -6425
550224 meter/sec
ZDOT = -6863
861480 ZDOT = -2092
104979
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
42598897
00016717 00000-0 10270-3 0 9124
2 25544 51
6369 79
7375 0004058 340
8002 19
2997 15
53876259 19079
Satellite: ISS
Catalog Number: 25544
Epoch time: 18300
42598897 = yrday
fracday
Element set: 912
Inclination: 51
6369 deg
RA of node: 79
7375 deg
Eccentricity:
0004058
Arg of perigee: 340
8002 deg
Mean anomaly: 19
2997 deg
Mean motion: 15
53876259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 347
Coasting Arc #14 (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 = -3916617
32 A = 6778238
47 meter
Y = 1466650
53 meter E =
0003613
Z = 5332908
96 I = 51
98448
XDOT = -2330
044079 Wp = 21
42020
YDOT = -7300
984039 meter/sec RA = 74
05283 deg
ZDOT = 299
878265 TA = 65
75402
MA = 65
71627
Ha = 221
776 n
mi
Hp = 215
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12849794
35 X = -3958631
85
Y = 4811845
58 feet Y = 1422617
21 meter
Z = 17496420
49 Z = 5313780
87
XDOT = -7644
501571 XDOT = -2249
685954
YDOT = -23953
359707 feet/sec YDOT = -7326
590903 meter/sec
ZDOT = 983
852575 ZDOT = 288
754513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12784360
65 X = 3896673
13
Y = -5276527
94 feet Y = -1608285
72 meter
Z = 17410174
56 Z = 5306621
21
XDOT = 8123
012224 XDOT = 2475
894126
YDOT = 22730
246419 feet/sec YDOT = 6928
179109 meter/sec
ZDOT = 934
715833 ZDOT = 284
901386
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
45499307
00016717 00000-0 10270-3 0 9135
2 25544 51
6368 74
6093 0004091 344
0939 16
0084 15
53831488 19236
Satellite: ISS
Catalog Number: 25544
Epoch time: 18301
45499307 = yrday
fracday
Element set: 913
Inclination: 51
6368 deg
RA of node: 74
6093 deg
Eccentricity:
0004091
Arg of perigee: 344
0939 deg
Mean anomaly: 16
0084 deg
Mean motion: 15
53831488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 315
Coasting Arc #15 (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 = 4392053
38 A = 6778848
96 meter
Y = 165391
22 meter E =
0012575
Z = -5171435
64 I = 51
97873
XDOT = 1524
528688 Wp = 84
40843
YDOT = 7347
404245 meter/sec RA = 69
07956 deg
ZDOT = 1534
140340 TA = 200
29636
MA = 200
34638
Ha = 221
675 n
mi
Hp = 215
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14409623
94 X = 4414998
14
Y = 542622
12 feet Y = 214634
62 meter
Z = -16966652
36 Z = -5150044
38
XDOT = 5001
734541 XDOT = 1434
802457
YDOT = 24105
656971 feet/sec YDOT = 7363
950857 meter/sec
ZDOT = 5033
268833 ZDOT = 1541
328364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14530457
40 X = -4428883
42
Y = 231463
02 feet Y = 70549
93 meter
Z = -16870424
59 Z = -5142105
42
XDOT = -6225
836106 XDOT = -1897
634845
YDOT = -22748
224002 feet/sec YDOT = -6933
658676 meter/sec
ZDOT = 5064
675127 ZDOT = 1543
712979
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
41967895
00016717 00000-0 10270-3 0 9145
2 25544 51
6387 69
8023 0004039 348
0941 12
0115 15
53885692 19388
Satellite: ISS
Catalog Number: 25544
Epoch time: 18302
41967895 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 69
8023 deg
Eccentricity:
0004039
Arg of perigee: 348
0941 deg
Mean anomaly: 12
0115 deg
Mean motion: 15
53885692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 327
Coasting Arc #16 (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 = -4759659
27 A = 6781644
00 meter
Y = -1740966
95 meter E =
0010738
Z = 4503350
50 I = 51
97382
XDOT = -544
599884 Wp = 47
24692
YDOT = -6928
289882 meter/sec RA = 64
10923 deg
ZDOT = -3242
042785 TA = 75
27096
MA = 75
15199
Ha = 221
870 n
mi
Hp = 215
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15615680
03 X = -4761712
81
Y = -5711833
84 feet Y = -1794204
35 meter
Z = 14774772
00 Z = 4480224
32
XDOT = -1786
745027 XDOT = -451
336947
YDOT = -22730
609850 feet/sec YDOT = -6933
858441 meter/sec
ZDOT = -10636
623312 ZDOT = -3244
461933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16076411
31 X = 4900090
17
Y = 4591398
38 feet Y = 1399458
23 meter
Z = 14670939
17 Z = 4471702
26
XDOT = 3645
284897 XDOT = 1111
082837
YDOT = 21382
095885 feet/sec YDOT = 6517
262826 meter/sec
ZDOT = -10646
612126 ZDOT = -3245
087376
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
44867587
00016717 00000-0 10270-3 0 9157
2 25544 51
6375 64
6740 0004003 352
3013 7
8077 15
53855137 19541
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
44867587 = yrday
fracday
Element set: 915
Inclination: 51
6375 deg
RA of node: 64
6740 deg
Eccentricity:
0004003
Arg of perigee: 352
3013 deg
Mean anomaly: 7
8077 deg
Mean motion: 15
53855137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 312
Coasting Arc #17 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2018/303/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4835076
54 A = 6785079
47 meter
Y = 3258667
19 meter E =
0006275
Z = -3469341
57 I = 51
97834
XDOT = -807
410892 Wp = 45
49763
YDOT = 6080
973704 meter/sec RA = 61
70421 deg
ZDOT = 4595
836789 TA = 274
02904
MA = 274
10076
Ha = 221
996 n
mi
Hp = 215
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15863112
00 X = 4815130
33
Y = 10691165
33 feet Y = 3312624
91 meter
Z = -11382354
22 Z = -3445902
49
XDOT = -2648
985867 XDOT = -897
674501
YDOT = 19950
701128 feet/sec YDOT = 6071
439903 meter/sec
ZDOT = 15078
204687 ZDOT = 4591
695472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15799431
43 X = 4815666
70
Y = 10894839
94 feet Y = 3320747
21 meter
Z = -11277311
53 Z = -3437324
55
XDOT = -2211
690270 XDOT = -674
123194
YDOT = 18762
607424 feet/sec YDOT = 5718
842743 meter/sec
ZDOT = 15058
778642 ZDOT = 4589
915730
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
89885976
00016717 00000-0 10270-3 0 9169
2 25544 51
6376 62
4353 0004497 354
5309 5
5793 15
53866648 19614
Satellite: ISS
Catalog Number: 25544
Epoch time: 18303
89885976 = yrday
fracday
Element set: 916
Inclination: 51
6376 deg
RA of node: 62
4353 deg
Eccentricity:
0004497
Arg of perigee: 354
5309 deg
Mean anomaly: 5
5793 deg
Mean motion: 15
53866648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 357
Coasting Arc #18 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2018/304/21:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 929140
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4777292
45 A = 6788257
37 meter
Y = -4358162
59 meter E =
0012721
Z = 2053114
63 I = 51
97290
XDOT = 2025
613944 Wp = 92
08451
YDOT = -4859
756644 meter/sec RA = 56
75001 deg
ZDOT = -5573
271267 TA = 65
32375
MA = 65
19135
Ha = 221
947 n
mi
Hp = 214
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15673531
64 X = -4738176
26
Y = -14298433
71 feet Y = -4411366
88 meter
Z = 6735940
40 Z = 2030002
94
XDOT = 6645
715039 XDOT = 2106
878879
YDOT = -15944
083479 feet/sec YDOT = -4836
650446 meter/sec
ZDOT = -18285
010719 ZDOT = -5563
234038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15779573
03 X = -4809613
86
Y = -14229984
25 feet Y = -4337299
20 meter
Z = 6632519
64 Z = 2021591
99
XDOT = 5660
724730 XDOT = 1725
388898
YDOT = -14823
809262 feet/sec YDOT = -4518
297063 meter/sec
ZDOT = -18239
207150 ZDOT = -5559
310339
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 18304
92785238
00016717 00000-0 10270-3 0 9175
2 25544 51
6379 57
3069 0004576 356
8373 3
2750 15
53902093 19778
Satellite: ISS
Catalog Number: 25544
Epoch time: 18304
92785238 = yrday
fracday
Element set: 917
Inclination: 51
6379 deg
RA of node: 57
3069 deg
Eccentricity:
0004576
Arg of perigee: 356
8373 deg
Mean anomaly: 3
2750 deg
Mean motion: 15
53902093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 337
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