[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 23rd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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
117/05:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 214
2
121/08:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 213
9
122/14:29:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 213
8
128/00:24:00
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
Coasting Arc #1 (Orbit 3000)
---------------------------------------
Vector Time (GMT): 2018/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2581956
89 A = 6779544
73 meter
Y = 4045428
78 meter E =
0009127
Z = 4785445
13 I = 51
27148
XDOT = -4345
096078 Wp = 45
88282
YDOT = 5788
237680 meter/sec RA = 290
55148 deg
ZDOT = -2539
511214 TA = 69
27905
MA = 69
18125
Ha = 221
243 n
mi
Hp = 214
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8470987
17 X = 2513282
69
Y = 13272404
13 feet Y = 4073918
08 meter
Z = 15700279
31 Z = 4797820
56
XDOT = -14255
564559 XDOT = -4397
163165
YDOT = 18990
281101 feet/sec YDOT = 5739
356667 meter/sec
ZDOT = -8331
729706 ZDOT = -2560
744757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13959859
13 X = 4254965
06
Y = 7163747
83 feet Y = 2183510
34 meter
Z = 15754877
19 Z = 4802086
57
XDOT = -2029
990490 XDOT = -618
741101
YDOT = 22556
093748 feet/sec YDOT = 6875
097374 meter/sec
ZDOT = -8427
250013 ZDOT = -2568
625804
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 18113
54373637
00016717 00000-0 10270-3 0 9009
2 25544 51
6373 291
1192 0002769 3
4285 356
6886 15
54126974 30018
Satellite: ISS
Catalog Number: 25544
Epoch time: 18113
54373637 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 291
1192 deg
Eccentricity:
0002769
Arg of perigee: 3
4285 deg
Mean anomaly: 356
6886 deg
Mean motion: 15
54126974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3001
Checksum: 311
Coasting Arc #2 (Orbit 3015)
---------------------------------------
Vector Time (GMT): 2018/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1701426
58 A = 6783004
76 meter
Y = -5338878
80 meter E =
0006621
Z = -3827144
77 I = 51
27223
XDOT = 4675
868134 Wp = 80
36374
YDOT = -4447
232905 meter/sec RA = 285
53505 deg
ZDOT = 4132
380901 TA = 233
33665
MA = 233
39753
Ha = 221
333 n
mi
Hp = 214
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5582108
19 X = -1623009
04
Y = -17516006
56 feet Y = -5357466
99 meter
Z = -12556249
26 Z = -3835219
09
XDOT = 15340
774718 XDOT = 4705
177821
YDOT = -14590
659138 feet/sec YDOT = -4394
780115 meter/sec
ZDOT = 13557
680120 ZDOT = 4155
166019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13861233
01 X = -4224903
82
Y = -12039530
68 feet Y = -3669648
95 meter
Z = -12591494
49 Z = -3837887
52
XDOT = 4468
692793 XDOT = 1362
057563
YDOT = -19406
315911 feet/sec YDOT = -5915
045090 meter/sec
ZDOT = 13659
914467 ZDOT = 4163
541930
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 18114
50825247
00016717 00000-0 10270-3 0 9016
2 25544 51
6368 286
3105 0002697 10
9954 349
1257 15
54156448 30162
Satellite: ISS
Catalog Number: 25544
Epoch time: 18114
50825247 = yrday
fracday
Element set: 901
Inclination: 51
6368 deg
RA of node: 286
3105 deg
Eccentricity:
0002697
Arg of perigee: 10
9954 deg
Mean anomaly: 349
1257 deg
Mean motion: 15
54156448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3016
Checksum: 312
Coasting Arc #3 (Orbit 3031)
---------------------------------------
Vector Time (GMT): 2018/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 817277
71 A = 6786689
54 meter
Y = 6277520
07 meter E =
0013737
Z = 2432693
38 I = 51
27629
XDOT = -4831
939896 Wp = 93
98731
YDOT = 2696
598467 meter/sec RA = 280
52881 deg
ZDOT = -5310
142658 TA = 58
63975
MA = 58
50541
Ha = 221
321 n
mi
Hp = 214
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2681357
32 X = 735203
24
Y = 20595538
30 feet Y = 6286200
65 meter
Z = 7981277
48 Z = 2436463
80
XDOT = -15852
821180 XDOT = -4835
940899
YDOT = 8847
107831 feet/sec YDOT = 2642
541761 meter/sec
ZDOT = -17421
727880 ZDOT = -5333
624486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13305616
88 X = 4055552
02
Y = 15939630
08 feet Y = 4858399
25 meter
Z = 7997213
11 Z = 2437550
56
XDOT = -7335
212231 XDOT = -2235
772688
YDOT = 14957
775608 feet/sec YDOT = 4559
130005 meter/sec
ZDOT = -17526
813246 ZDOT = -5342
172677
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 18115
53706485
00016717 00000-0 10270-3 0 9023
2 25544 51
6362 281
1814 0002748 9
6810 350
4395 15
54170842 30329
Satellite: ISS
Catalog Number: 25544
Epoch time: 18115
53706485 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 281
1814 deg
Eccentricity:
0002748
Arg of perigee: 9
6810 deg
Mean anomaly: 350
4395 deg
Mean motion: 15
54170842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3032
Checksum: 296
Coasting Arc #4 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2018/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3736
82 A = 6788918
08 meter
Y = -6733610
23 meter E =
0012819
Z = -814028
96 I = 51
28050
XDOT = 4831
907088 Wp = 35
00226
YDOT = -710
715189 meter/sec RA = 275
52999 deg
ZDOT = 5913
520809 TA = 316
14911
MA = 316
25081
Ha = 221
415 n
mi
Hp = 214
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12259
90 X = 75514
68
Y = -22091897
09 feet Y = -6733208
95 meter
Z = -2670698
70 Z = -813854
24
XDOT = 15852
713544 XDOT = 4810
770399
YDOT = -2331
742745 feet/sec YDOT = -656
799323 meter/sec
ZDOT = 19401
314989 ZDOT = 5936
941415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12210208
75 X = -3721671
63
Y = -18411191
48 feet Y = -5611731
16 meter
Z = -2668994
14 Z = -813509
41
XDOT = 10471
172835 XDOT = 3191
613480
YDOT = -9745
127110 feet/sec YDOT = -2970
314743 meter/sec
ZDOT = 19505
847883 ZDOT = 5945
382435
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 18116
50157407
00016717 00000-0 10270-3 0 9036
2 25544 51
6379 276
3725 0002722 17
9115 342
2134 15
54172869 30473
Satellite: ISS
Catalog Number: 25544
Epoch time: 18116
50157407 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 276
3725 deg
Eccentricity:
0002722
Arg of perigee: 17
9115 deg
Mean anomaly: 342
2134 deg
Mean motion: 15
54172869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 303
Coasting Arc #5 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2018/117/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2672433
94 A = 6785112
49 meter
Y = -5403523
31 meter E =
0014488
Z = 3096996
21 I = 51
26864
XDOT = 3730
645298 Wp = 72
96543
YDOT = 4632
284571 meter/sec RA = 271
98205 deg
ZDOT = 4848
359288 TA = 322
89344
MA = 322
99352
Ha = 221
497 n
mi
Hp = 214
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8767827
88 X = 2717615
26
Y = -17728094
84 feet Y = -5373385
51 meter
Z = 10160748
72 Z = 3110088
15
XDOT = 12239
649927 XDOT = 3655
017539
YDOT = 15197
784025 feet/sec YDOT = 4673
580634 meter/sec
ZDOT = 15906
690576 ZDOT = 4866
297701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19689865
34 X = 6001470
95
Y = 1504855
79 feet Y = 458680
05 meter
Z = 10219861
99 Z = 3115013
93
XDOT = -9504
608439 XDOT = -2897
004652
YDOT = 15470
258162 feet/sec YDOT = 4715
334688 meter/sec
ZDOT = 15986
050102 ZDOT = 4872
548071
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 18117
27317798
00016717 00000-0 10270-3 0 9043
2 25544 51
6407 272
5302 0003245 17
0530 343
0732 15
54163142 30597
Satellite: ISS
Catalog Number: 25544
Epoch time: 18117
27317798 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 272
5302 deg
Eccentricity:
0003245
Arg of perigee: 17
0530 deg
Mean anomaly: 343
0732 deg
Mean motion: 15
54163142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 284
Coasting Arc #6 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2018/118/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3257872
15 A = 6781159
76 meter
Y = 4095549
11 meter E =
0010952
Z = -4324074
72 I = 51
25556
XDOT = -3092
790773 Wp = 56
18864
YDOT = -6099
446970 meter/sec RA = 266
97083 deg
ZDOT = -3447
233539 TA = 178
56479
MA = 178
56165
Ha = 221
529 n
mi
Hp = 214
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10688556
94 X = -3282423
19
Y = 13436840
92 feet Y = 4058979
85 meter
Z = -14186596
85 Z = -4339960
40
XDOT = -10146
951354 XDOT = -3007
610145
YDOT = -20011
308958 feet/sec YDOT = -6133
556590 meter/sec
ZDOT = -11309
821323 ZDOT = -3462
050253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16488007
11 X = -5025544
57
Y = -4572637
69 feet Y = -1393739
97 meter
Z = -14257983
01 Z = -4345833
22
XDOT = 14224
886411 XDOT = 4335
745378
YDOT = -15826
708472 feet/sec YDOT = -4823
980742 meter/sec
ZDOT = -11375
072631 ZDOT = -3467
122138
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 18118
23767843
00016717 00000-0 10270-3 0 9051
2 25544 51
6406 267
7225 0003210 17
6241 342
5023 15
54190026 30748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18118
23767843 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 267
7225 deg
Eccentricity:
0003210
Arg of perigee: 17
6241 deg
Mean anomaly: 342
5023 deg
Mean motion: 15
54190026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 283
Coasting Arc #7 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2018/119/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3757714
80 A = 6778133
72 meter
Y = -2470319
79 meter E =
0005440
Z = 5066790
86 I = 51
24902
XDOT = 2377
352399 Wp = 90
39899
YDOT = 7095
390953 meter/sec RA = 261
94856 deg
ZDOT = 1694
618145 TA = 343
14014
MA = 343
15821
Ha = 221
439 n
mi
Hp = 214
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12328460
63 X = 3760447
08
Y = -8104723
72 feet Y = -2428282
97 meter
Z = 16623329
60 Z = 5085051
58
XDOT = 7799
712594 XDOT = 2289
601405
YDOT = 23278
841710 feet/sec YDOT = 7121
485562 meter/sec
ZDOT = 5559
770818 ZDOT = 1705
953301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12336975
31 X = 3760310
08
Y = 7921597
62 feet Y = 2414502
96 meter
Z = 16705086
24 Z = 5091710
29
XDOT = -17605
907734 XDOT = -5366
280677
YDOT = 15578
968842 feet/sec YDOT = 4748
469703 meter/sec
ZDOT = 5609
375319 ZDOT = 1709
737597
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 18119
26647554
00016717 00000-0 10270-3 0 9062
2 25544 51
6414 262
5931 0003170 22
0763 338
0526 15
54189592 30900
Satellite: ISS
Catalog Number: 25544
Epoch time: 18119
26647554 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 262
5931 deg
Eccentricity:
0003170
Arg of perigee: 22
0763 deg
Mean anomaly: 338
0526 deg
Mean motion: 15
54189592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 306
Coasting Arc #8 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2018/120/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4197984
37 A = 6777126
95 meter
Y = 689154
51 meter E =
0016350
Z = -5289504
88 I = 51
25159
XDOT = -1538
074496 Wp = 81
11670
YDOT = -7496
700787 meter/sec RA = 256
92086 deg
ZDOT = 247
095529 TA = 191
23651
MA = 191
27306
Ha = 221
588 n
mi
Hp = 213
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13772914
61 X = -4179684
56
Y = 2261005
60 feet Y = 642311
99 meter
Z = -17354018
65 Z = -5309853
19
XDOT = -5046
176168 XDOT = -1455
330311
YDOT = -24595
475024 feet/sec YDOT = -7513
437940 meter/sec
ZDOT = 810
680871 ZDOT = 239
825054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7765677
05 X = -2366978
37
Y = -11460311
40 feet Y = -3493102
92 meter
Z = -17444850
50 Z = -5317190
43
XDOT = 19391
358863 XDOT = 5910
486181
YDOT = -14310
457908 feet/sec YDOT = -4361
827570 meter/sec
ZDOT = 779
244142 ZDOT = 237
513615
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 18120
23096706
00016717 00000-0 10270-3 0 9079
2 25544 51
6415 257
7844 0003300 23
4186 336
7116 15
54214202 31053
Satellite: ISS
Catalog Number: 25544
Epoch time: 18120
23096706 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 257
7844 deg
Eccentricity:
0003300
Arg of perigee: 23
4186 deg
Mean anomaly: 336
7116 deg
Mean motion: 15
54214202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 276
Coasting Arc #9 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2018/121/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4519851
16 A = 6778578
93 meter
Y = 1116440
71 meter E =
0009285
Z = 4923103
14 I = 51
26478
XDOT = 564
497190 Wp = 46
76830
YDOT = 7335
509767 meter/sec RA = 251
89496 deg
ZDOT = -2172
925548 TA = 64
57173
MA = 64
47567
Ha = 221
449 n
mi
Hp = 213
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14828907
99 X = 4483116
57
Y = 3662863
23 feet Y = 1166779
37 meter
Z = 16151913
18 Z = 4944970
22
XDOT = 1852
024903 XDOT = 492
982698
YDOT = 24066
633093 feet/sec YDOT = 7341
422514 meter/sec
ZDOT = -7129
020826 ZDOT = -2170
357018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3086089
92 X = 940640
21
Y = 14853756
61 feet Y = 4527425
01 meter
Z = 16249287
44 Z = 4952782
81
XDOT = -19775
792367 XDOT = -6027
661514
YDOT = 11927
605030 feet/sec YDOT = 3635
534013 meter/sec
ZDOT = -7118
521488 ZDOT = -2169
725350
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 18121
25975322
00016717 00000-0 10270-3 0 9083
2 25544 51
6410 252
6556 0003290 25
5984 334
5331 15
54242546 31214
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
25975322 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 252
6556 deg
Eccentricity:
0003290
Arg of perigee: 25
5984 deg
Mean anomaly: 334
5331 deg
Mean motion: 15
54242546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 291
Coasting Arc #10 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2018/121/08:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4476125
73 A = 6782068
44 meter
Y = 3090767
58 meter E =
0012810
Z = 4044112
57 I = 51
27395
XDOT = -1033
079837 Wp = 66
81639
YDOT = 6553
444148 meter/sec RA = 251
22220 deg
ZDOT = -3850
415234 TA = 63
29630
MA = 63
16523
Ha = 221
510 n
mi
Hp = 213
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14685451
87 X = 4421586
69
Y = 10140313
59 feet Y = 3140517
72 meter
Z = 13268085
86 Z = 4065724
02
XDOT = -3389
369543 XDOT = -1087
581803
YDOT = 21500
801012 feet/sec YDOT = 6541
586834 meter/sec
ZDOT = -12632
595912 ZDOT = -3855
565996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11078100
02 X = 3376604
89
Y = 13899929
66 feet Y = 4236698
56 meter
Z = 13364064
28 Z = 4073366
79
XDOT = -8316
011058 XDOT = -2534
720170
YDOT = 18842
316709 feet/sec YDOT = 5743
138133 meter/sec
ZDOT = -12656
419257 ZDOT = -3857
676589
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 18121
38835175
00016717 00000-0 10270-3 0 9099
2 25544 51
6375 252
0108 0003078 26
9497 333
1815 15
54204294 31231
Satellite: ISS
Catalog Number: 25544
Epoch time: 18121
38835175 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 252
0108 deg
Eccentricity:
0003078
Arg of perigee: 26
9497 deg
Mean anomaly: 333
1815 deg
Mean motion: 15
54204294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 304
Coasting Arc #11 (Orbit 3137)
---------------------------------------
Vector Time (GMT): 2018/122/08:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 928423
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4352181
98 A = 6785834
37 meter
Y = -4423240
71 meter E =
0007647
Z = -2743981
20 I = 51
29788
XDOT = 2152
496944 Wp = 49
37495
YDOT = -5284
276808 meter/sec RA = 246
21399 deg
ZDOT = 5118
402440 TA = 279
41237
MA = 279
49881
Ha = 221
619 n
mi
Hp = 213
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14278812
27 X = -4289067
57
Y = -14511944
58 feet Y = -4471556
83 meter
Z = -9002562
99 Z = -2764969
81
XDOT = 7061
997847 XDOT = 2186
564235
YDOT = -17336
866168 feet/sec YDOT = -5260
015772 meter/sec
ZDOT = 16792
658924 ZDOT = 5128
941307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9770457
12 X = -2978035
33
Y = -17813908
35 feet Y = -5429679
27 meter
Z = -9095602
92 Z = -2772339
77
XDOT = 10075
959618 XDOT = 3071
152491
YDOT = -14101
203247 feet/sec YDOT = -4298
046750 meter/sec
ZDOT = 16840
343893 ZDOT = 5132
936819
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 18122
35283603
00016717 00000-0 10270-3 0 9102
2 25544 51
6372 247
2019 0003060 33
9886 326
1462 15
54208190 31381
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
35283603 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 247
2019 deg
Eccentricity:
0003060
Arg of perigee: 33
9886 deg
Mean anomaly: 326
1462 deg
Mean motion: 15
54208190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3138
Checksum: 287
Coasting Arc #12 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2018/122/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4596568
94 A = 6784817
14 meter
Y = -3872901
94 meter E =
0006899
Z = -3148779
99 I = 51
30164
XDOT = 1562
379754 Wp = 61
59865
YDOT = -5757
142693 meter/sec RA = 244
93018 deg
ZDOT = 4811
637075 TA = 261
91790
MA = 261
99617
Ha = 221
567 n
mi
Hp = 213
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15080606
75 X = -4537624
08
Y = -12706371
20 feet Y = -3923974
25 meter
Z = -10330643
01 Z = -3170965
89
XDOT = 5125
917827 XDOT = 1603
268764
YDOT = -18888
263428 feet/sec YDOT = -5739
442623 meter/sec
ZDOT = 15786
210875 ZDOT = 4819
325832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15792960
73 X = -4813694
43
Y = 11722417
63 feet Y = 3572992
89 meter
Z = -10429097
30 Z = -3178788
86
XDOT = -16391
630257 XDOT = -4996
168902
YDOT = -8040
444795 feet/sec YDOT = -2450
727573 meter/sec
ZDOT = 15821
244152 ZDOT = 4822
315217
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 18122
61003016
00016717 00000-0 10270-3 0 9110
2 25544 51
6410 245
9213 0002886 33
6362 326
4973 15
54205900 31427
Satellite: ISS
Catalog Number: 25544
Epoch time: 18122
61003016 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 245
9213 deg
Eccentricity:
0002886
Arg of perigee: 33
6362 deg
Mean anomaly: 326
4973 deg
Mean motion: 15
54205900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 271
Coasting Arc #13 (Orbit 3157)
---------------------------------------
Vector Time (GMT): 2018/123/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4335985
15 A = 6787966
82 meter
Y = 4971636
88 meter E =
0014878
Z = 1576121
01 I = 51
32689
XDOT = -2809
543463 Wp = 105
48931
YDOT = 4274
839540 meter/sec RA = 239
93134 deg
ZDOT = -5713
912344 TA = 57
19429
MA = 57
05108
Ha = 221
690 n
mi
Hp = 213
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14225673
05 X = 4272412
60
Y = 16311144
60 feet Y = 5019769
32 meter
Z = 5171000
67 Z = 1597029
86
XDOT = -9217
662280 XDOT = -2829
381478
YDOT = 14025
064109 feet/sec YDOT = 4243
310629 meter/sec
ZDOT = -18746
431575 ZDOT = -5727
608331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18938963
79 X = 5772596
16
Y = -10429394
69 feet Y = -3178879
50 meter
Z = 5263633
44 Z = 1604355
47
XDOT = 11028
245751 XDOT = 3361
409305
YDOT = 10467
068083 feet/sec YDOT = 3190
362352 meter/sec
ZDOT = -18808
067719 ZDOT = -5732
699041
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 18123
63880433
00016717 00000-0 10270-3 0 9120
2 25544 51
6407 240
7925 0003071 39
2575 320
8800 15
54222694 31584
Satellite: ISS
Catalog Number: 25544
Epoch time: 18123
63880433 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 240
7925 deg
Eccentricity:
0003071
Arg of perigee: 39
2575 deg
Mean anomaly: 320
8800 deg
Mean motion: 15
54222694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3158
Checksum: 298
Coasting Arc #14 (Orbit 3173)
---------------------------------------
Vector Time (GMT): 2018/124/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3809968
68 A = 6789129
00 meter
Y = -5608668
64 meter E =
0015498
Z = 129043
05 I = 51
34725
XDOT = 4032
688375 Wp = 45
52553
YDOT = -2591
623237 meter/sec RA = 234
93956 deg
ZDOT = 5988
607364 TA = 315
87067
MA = 315
99422
Ha = 221
775 n
mi
Hp = 213
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12499897
25 X = -3747594
68
Y = -18401143
84 feet Y = -5650925
59 meter
Z = 423369
58 Z = 110686
53
XDOT = 13230
604905 XDOT = 4032
279038
YDOT = -8502
700910 feet/sec YDOT = -2546
529530 meter/sec
ZDOT = 19647
661954 ZDOT = 6008
195886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20478615
19 X = -6241881
91
Y = 8691259
76 feet Y = 2649095
98 meter
Z = 342185
84 Z = 104298
25
XDOT = -5161
661093 XDOT = -1573
274301
YDOT = -13008
516237 feet/sec YDOT = -3964
995749 meter/sec
ZDOT = 19735
373679 ZDOT = 6015
341897
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 18124
66757375
00016717 00000-0 10270-3 0 9133
2 25544 51
6401 235
6637 0003204 40
6135 319
5257 15
54197082 31748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18124
66757375 = yrday
fracday
Element set: 913
Inclination: 51
6401 deg
RA of node: 235
6637 deg
Eccentricity:
0003204
Arg of perigee: 40
6135 deg
Mean anomaly: 319
5257 deg
Mean motion: 15
54197082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3174
Checksum: 305
Coasting Arc #15 (Orbit 3188)
---------------------------------------
Vector Time (GMT): 2018/125/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2945916
44 A = 6787558
25 meter
Y = 5822577
67 meter E =
0007580
Z = -1865982
67 I = 51
36130
XDOT = -5161
989698 Wp = 117
32636
YDOT = 822
236488 meter/sec RA = 229
94877 deg
ZDOT = -5604
771113 TA = 83
28254
MA = 83
19629
Ha = 221
771 n
mi
Hp = 213
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9665080
17 X = 2889651
89
Y = 19102945
10 feet Y = 5855206
43 meter
Z = -6121990
38 Z = -1851808
66
XDOT = -16935
661739 XDOT = -5143
575232
YDOT = 2697
626274 feet/sec YDOT = 764
614804 meter/sec
ZDOT = -18388
356669 ZDOT = -5629
801750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20520454
86 X = 6254634
64
Y = -6165122
87 feet Y = -1879129
45 meter
Z = -6059475
64 Z = -1846928
17
XDOT = -776
859315 XDOT = -236
786719
YDOT = 15528
999347 feet/sec YDOT = 4733
239001 meter/sec
ZDOT = -18500
134837 ZDOT = -5638
841098
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 18125
63203799
00016717 00000-0 10270-3 0 9148
2 25544 51
6393 230
8555 0003118 45
7532 314
3876 15
54238518 31891
Satellite: ISS
Catalog Number: 25544
Epoch time: 18125
63203799 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 230
8555 deg
Eccentricity:
0003118
Arg of perigee: 45
7532 deg
Mean anomaly: 314
3876 deg
Mean motion: 15
54238518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3189
Checksum: 323
Coasting Arc #16 (Orbit 3204)
---------------------------------------
Vector Time (GMT): 2018/126/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1804888
50 A = 6784187
02 meter
Y = -5599326
63 meter E =
0015102
Z = 3363278
33 I = 51
37254
XDOT = 6065
911213 Wp = 81
36395
YDOT = 832
604342 meter/sec RA = 224
95144 deg
ZDOT = 4625
815966 TA = 318
07836
MA = 318
19389
Ha = 221
792 n
mi
Hp = 213
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5921550
18 X = -1758478
31
Y = -18370494
20 feet Y = -5619250
79 meter
Z = 11034377
72 Z = 3354623
22
XDOT = 19901
283507 XDOT = 6033
680024
YDOT = 2731
641541 feet/sec YDOT = 900
257118 meter/sec
ZDOT = 15176
561568 ZDOT = 4655
204042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19093045
81 X = -5819560
36
Y = 2971719
71 feet Y = 905780
17 meter
Z = 10996444
38 Z = 3351716
25
XDOT = 6088
727785 XDOT = 1855
844229
YDOT = -17713
940070 feet/sec YDOT = -5399
208933 meter/sec
ZDOT = 15307
591821 ZDOT = 4665
753987
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 18126
66079352
00016717 00000-0 10270-3 0 9159
2 25544 51
6397 225
7259 0003202 48
3161 311
8265 15
54257560 32051
Satellite: ISS
Catalog Number: 25544
Epoch time: 18126
66079352 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 225
7259 deg
Eccentricity:
0003202
Arg of perigee: 48
3161 deg
Mean anomaly: 311
8265 deg
Mean motion: 15
54257560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3205
Checksum: 304
Coasting Arc #17 (Orbit 3219)
---------------------------------------
Vector Time (GMT): 2018/127/14:29:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 387382
78 A = 6780323
11 meter
Y = 5042932
67 meter E =
0012909
Z = -4528734
11 I = 51
38291
XDOT = -6609
721434 Wp = 65
59675
YDOT = -2288
953585 meter/sec RA = 219
94576 deg
ZDOT = -3116
034156 TA = 173
02575
MA = 173
00777
Ha = 221
875 n
mi
Hp = 213
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1270940
88 X = 352960
88
Y = 16545054
69 feet Y = 5047072
34 meter
Z = -14858051
53 Z = -4526935
75
XDOT = -21685
437776 XDOT = -6568
498333
YDOT = -7509
690238 feet/sec YDOT = -2362
637438 meter/sec
ZDOT = -10223
209173 ZDOT = -3148
042057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16569308
36 X = 5050325
19
Y = 1016095
56 feet Y = 309705
93 meter
Z = -14850636
05 Z = -4526473
87
XDOT = -10457
139069 XDOT = -3187
335988
YDOT = 19109
511702 feet/sec YDOT = 5824
579167 meter/sec
ZDOT = -10365
771196 ZDOT = -3159
487061
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
62524885
00016717 00000-0 10270-3 0 9163
2 25544 51
6390 220
9177 0003316 52
3606 307
7847 15
54245394 32204
Satellite: ISS
Catalog Number: 25544
Epoch time: 18127
62524885 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 220
9177 deg
Eccentricity:
0003316
Arg of perigee: 52
3606 deg
Mean anomaly: 307
7847 deg
Mean motion: 15
54245394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3220
Checksum: 311
Coasting Arc #18 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2018/128/00:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 905676
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3163106
80 A = 6785697
36 meter
Y = -5296808
83 meter E =
0016621
Z = 2805407
17 I = 51
41216
XDOT = 5704
423159 Wp = 73
88978
YDOT = -702
641064 meter/sec RA = 217
88032 deg
ZDOT = 5084
563383 TA = 318
08681
MA = 318
21392
Ha = 221
961 n
mi
Hp = 213
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10377646
99 X = -3117268
62
Y = -17377981
74 feet Y = -5331924
66 meter
Z = 9204091
78 Z = 2790152
97
XDOT = 18715
299077 XDOT = 5687
158035
YDOT = -2305
252836 feet/sec YDOT = -638
946968 meter/sec
ZDOT = 16681
638395 ZDOT = 5112
231713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20069578
74 X = 6117207
60
Y = 2852842
97 feet Y = 869546
54 meter
Z = 9136651
91 Z = 2784851
50
XDOT = -9732
744590 XDOT = -2966
540551
YDOT = 14430
521483 feet/sec YDOT = 4398
422948 meter/sec
ZDOT = 16805
201629 ZDOT = 5122
225457
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
07532718
00016717 00000-0 10270-3 0 9178
2 25544 51
6398 218
6750 0003579 49
9110 310
2356 15
54247012 32276
Satellite: ISS
Catalog Number: 25544
Epoch time: 18128
07532718 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 218
6750 deg
Eccentricity:
0003579
Arg of perigee: 49
9110 deg
Mean anomaly: 310
2356 deg
Mean motion: 15
54247012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 308
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