[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 20th 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) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
238/15:14:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
242/21:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2018/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4981939
08 A = 6782090
13 meter
Y = 1420794
77 meter E =
0013759
Z = -4389800
41 I = 51
95394
XDOT = 1106
045275 Wp = 97
00608
YDOT = 6747
349334 meter/sec RA = 57
45629 deg
ZDOT = 3446
688333 TA = 207
81820
MA = 207
89184
Ha = 223
483 n
mi
Hp = 213
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16344944
48 X = 4987004
20
Y = 4661400
15 feet Y = 1476534
62 meter
Z = -14402232
33 Z = -4365587
82
XDOT = 3628
757464 XDOT = 1013
770328
YDOT = 22136
972881 feet/sec YDOT = 6759
201922 meter/sec
ZDOT = 11308
032589 ZDOT = 3451
837012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11449765
40 X = -3489888
49
Y = -12684756
26 feet Y = -3866313
71 meter
Z = -14293704
50 Z = -4356721
13
XDOT = 7829
741726 XDOT = 2386
505278
YDOT = -19806
432367 feet/sec YDOT = -6037
000585 meter/sec
ZDOT = 11330
222017 ZDOT = 3453
451671
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 18232
50982610
00016717 00000-0 10270-3 0 9004
2 25544 51
6379 58
1519 0005626 76
4843 283
6936 15
53857206 8516
Satellite: ISS
Catalog Number: 25544
Epoch time: 18232
50982610 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 58
1519 deg
Eccentricity:
0005626
Arg of perigee: 76
4843 deg
Mean anomaly: 283
6936 deg
Mean motion: 15
53857206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 324
Coasting Arc #2 (Orbit 866)
---------------------------------------
Vector Time (GMT): 2018/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5291620
38 A = 6785728
62 meter
Y = -2729016
98 meter E =
0018176
Z = 3240083
10 I = 51
94727
XDOT = 136
945387 Wp = 88
90681
YDOT = -5987
396621 meter/sec RA = 52
49395 deg
ZDOT = -4795
841717 TA = 53
71831
MA = 53
55055
Ha = 223
483 n
mi
Hp = 213
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17360959
25 X = -5276448
88
Y = -8953467
78 feet Y = -2788106
75 meter
Z = 10630193
89 Z = 3214415
40
XDOT = 449
295890 XDOT = 227
183298
YDOT = -19643
689702 feet/sec YDOT = -5985
360599 meter/sec
ZDOT = -15734
388836 ZDOT = -4794
957389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10296374
54 X = 3138334
96
Y = 16672770
91 feet Y = 5081860
57 meter
Z = 10515317
16 Z = 3205068
67
XDOT = -9410
605857 XDOT = -2868
352665
YDOT = 15781
180700 feet/sec YDOT = 4810
103877 meter/sec
ZDOT = -15729
583273 ZDOT = -4794
376982
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 18233
53883908
00016717 00000-0 10270-3 0 9019
2 25544 51
6376 53
0241 0005488 79
1987 280
9783 15
53869190 8676
Satellite: ISS
Catalog Number: 25544
Epoch time: 18233
53883908 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 53
0241 deg
Eccentricity:
0005488
Arg of perigee: 79
1987 deg
Mean anomaly: 280
9783 deg
Mean motion: 15
53869190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 867
Checksum: 349
Coasting Arc #3 (Orbit 881)
---------------------------------------
Vector Time (GMT): 2018/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923006
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5363935
71 A = 6788744
45 meter
Y = 3730632
36 meter E =
0012000
Z = -1837157
73 I = 51
93563
XDOT = -1501
860951 Wp = 58
23178
YDOT = 4934
685656 meter/sec RA = 47
53903 deg
ZDOT = 5668
938799 TA = 281
65935
MA = 281
79400
Ha = 223
543 n
mi
Hp = 213
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17598214
26 X = 5330743
89
Y = 12239607
49 feet Y = 3790430
03 meter
Z = -6027420
39 Z = -1811182
60
XDOT = -4927
365325 XDOT = -1584
466635
YDOT = 16189
913569 feet/sec YDOT = 4917
428897 meter/sec
ZDOT = 18598
880575 ZDOT = 5661
442791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9110619
26 X = -2776916
75
Y = -19439341
04 feet Y = -5925111
15 meter
Z = -5911308
65 Z = -1801766
88
XDOT = 11078
613055 XDOT = 3376
761259
YDOT = -10803
646134 feet/sec YDOT = -3292
951342 meter/sec
ZDOT = 18564
527389 ZDOT = 5658
467948
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 18234
50354018
00016717 00000-0 10270-3 0 9023
2 25544 51
6370 48
2168 0005675 84
8885 275
2915 15
53854174 8829
Satellite: ISS
Catalog Number: 25544
Epoch time: 18234
50354018 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 48
2168 deg
Eccentricity:
0005675
Arg of perigee: 84
8885 deg
Mean anomaly: 275
2915 deg
Mean motion: 15
53854174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 882
Checksum: 326
Coasting Arc #4 (Orbit 897)
---------------------------------------
Vector Time (GMT): 2018/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5100405
26 A = 6789949
32 meter
Y = -4468616
81 meter E =
0016739
Z = 206279
11 I = 51
91790
XDOT = 2971
977933 Wp = 118
15605
YDOT = -3687
373806 meter/sec RA = 42
58845 deg
ZDOT = -6031
154056 TA = 59
63013
MA = 59
46475
Ha = 223
388 n
mi
Hp = 212
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16733613
06 X = -5051058
86
Y = -14660816
31 feet Y = -4525377
16 meter
Z = 676768
73 Z = 181623
42
XDOT = 9750
583769 XDOT = 3042
285934
YDOT = -12097
683091 feet/sec YDOT = -3653
746005 meter/sec
ZDOT = -19787
250839 ZDOT = -6016
546692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7478089
37 X = 2279321
64
Y = 20956345
02 feet Y = 6387493
96 meter
Z = 566691
85 Z = 172727
68
XDOT = -12995
165673 XDOT = -3960
926497
YDOT = 5209
059128 feet/sec YDOT = 1587
721222 meter/sec
ZDOT = -19721
139151 ZDOT = -6011
003213
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 18235
53254918
00016717 00000-0 10270-3 0 9036
2 25544 51
6378 43
0884 0005613 85
4068 274
7726 15
53911023 8985
Satellite: ISS
Catalog Number: 25544
Epoch time: 18235
53254918 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 43
0884 deg
Eccentricity:
0005613
Arg of perigee: 85
4068 deg
Mean anomaly: 274
7726 deg
Mean motion: 15
53911023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 898
Checksum: 325
Coasting Arc #5 (Orbit 913)
---------------------------------------
Vector Time (GMT): 2018/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4522452
93 A = 6789228
11 meter
Y = 4859930
13 meter E =
0019017
Z = 1385701
13 I = 51
89016
XDOT = -4377
131943 Wp = 69
55957
YDOT = 2395
443463 meter/sec RA = 37
63680 deg
ZDOT = 5826
095012 TA = 305
49190
MA = 305
66918
Ha = 223
513 n
mi
Hp = 212
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14837444
01 X = 4461040
86
Y = 15944652
65 feet Y = 4910159
98 meter
Z = 4546263
54 Z = 1407519
97
XDOT = -14360
669105 XDOT = -4431
892706
YDOT = 7859
066481 feet/sec YDOT = 2346
189274 meter/sec
ZDOT = 19114
484947 ZDOT = 5804
699773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5529109
07 X = -1685272
45
Y = -21045585
93 feet Y = -6414694
59 meter
Z = 4643540
78 Z = 1415351
23
XDOT = 14947
483169 XDOT = 4555
992870
YDOT = 310
327021 feet/sec YDOT = 94
587676 meter/sec
ZDOT = 19018
079176 ZDOT = 5796
710533
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 18236
56155848
00016717 00000-0 10270-3 0 9043
2 25544 51
6378 37
9604 0005785 92
6216 267
5599 15
53873187 9147
Satellite: ISS
Catalog Number: 25544
Epoch time: 18236
56155848 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 37
9604 deg
Eccentricity:
0005785
Arg of perigee: 92
6216 deg
Mean anomaly: 267
5599 deg
Mean motion: 15
53873187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 914
Checksum: 354
Coasting Arc #6 (Orbit 928)
---------------------------------------
Vector Time (GMT): 2018/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3562997
19 A = 6786412
37 meter
Y = -4995694
04 meter E =
0010246
Z = -2904400
70 I = 51
85420
XDOT = 5647
978111 Wp = 103
04731
YDOT = -1097
200565 meter/sec RA = 32
67951 deg
ZDOT = -5058
728634 TA = 109
90903
MA = 109
79861
Ha = 223
491 n
mi
Hp = 212
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11689623
32 X = -3492761
36
Y = -16390072
32 feet Y = -5035145
34 meter
Z = -9528873
68 Z = -2921537
40
XDOT = 18530
111912 XDOT = 5684
399723
YDOT = -3599
739385 feet/sec YDOT = -1033
837507 meter/sec
ZDOT = -16596
878720 ZDOT = -5031
204727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2856967
34 X = 870803
65
Y = 19891227
45 feet Y = 6062846
13 meter
Z = -9605103
12 Z = -2927635
43
XDOT = -16776
524483 XDOT = -5113
484662
YDOT = -5517
847278 feet/sec YDOT = -1681
839850 meter/sec
ZDOT = -16473
145272 ZDOT = -5021
014679
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 18237
52625199
00016717 00000-0 10270-3 0 9052
2 25544 51
6379 33
1534 0005814 95
1399 265
0417 15
53881465 9297
Satellite: ISS
Catalog Number: 25544
Epoch time: 18237
52625199 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 33
1534 deg
Eccentricity:
0005814
Arg of perigee: 95
1399 deg
Mean anomaly: 265
0417 deg
Mean motion: 15
53881465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 929
Checksum: 333
Coasting Arc #7 (Orbit 944)
---------------------------------------
Vector Time (GMT): 2018/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2330903
42 A = 6782821
13 meter
Y = 4866013
11 meter E =
0016146
Z = 4099156
06 I = 51
81483
XDOT = -6640
331656 Wp = 101
91793
YDOT = -71
854650 meter/sec RA = 27
71107 deg
ZDOT = 3845
155865 TA = 308
40380
MA = 308
54868
Ha = 223
389 n
mi
Hp = 212
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7647320
92 X = 2256405
88
Y = 15964609
96 feet Y = 4891662
58 meter
Z = 13448674
72 Z = 4110297
37
XDOT = -21785
865012 XDOT = -6657
712056
YDOT = -235
743601 feet/sec YDOT = -146
208405 meter/sec
ZDOT = 12615
340766 ZDOT = 3812
857786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 264268
98 X = 80549
19
Y = -17662142
82 feet Y = -5383421
13 meter
Z = 13498000
34 Z = 4114190
50
XDOT = 18232
560143 XDOT = 5557
284332
YDOT = 9843
115101 feet/sec YDOT = 3000
181483 meter/sec
ZDOT = 12470
348130 ZDOT = 3800
962110
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 18238
55525573
00016717 00000-0 10270-3 0 9062
2 25544 51
6389 28
0252 0005666 100
3825 259
7966 15
53895409 9456
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
55525573 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 28
0252 deg
Eccentricity:
0005666
Arg of perigee: 100
3825 deg
Mean anomaly: 259
7966 deg
Mean motion: 15
53895409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 945
Checksum: 342
Coasting Arc #8 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1530320
49 A = 6778005
66 meter
Y = 3912471
46 meter E =
0008106
Z = 5312260
36 I = 51
79789
XDOT = -6955
687195 Wp = 101
42766
YDOT = -3222
348646 meter/sec RA = 27
01874 deg
ZDOT = 367
464744 TA = 345
06723
MA = 345
09115
Ha = 223
421 n
mi
Hp = 212
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5020736
51 X = -1599760
82
Y = 12836192
46 feet Y = 3894970
40 meter
Z = 17428675
71 Z = 5304657
84
XDOT = -22820
496045 XDOT = -6920
921962
YDOT = -10572
009993 feet/sec YDOT = -3299
937552 meter/sec
ZDOT = 1205
592993 ZDOT = 333
761626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -183902
05 X = -56053
34
Y = -13825692
58 feet Y = -4214071
10 meter
Z = 17393986
71 Z = 5301687
15
XDOT = 24129
064071 XDOT = 7354
538729
YDOT = 1014
457012 feet/sec YDOT = 309
206497 meter/sec
ZDOT = 1054
743077 ZDOT = 321
485690
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 18238
68387999
00016717 00000-0 10270-3 0 9075
2 25544 51
6419 27
3855 0005556 100
7515 259
4263 15
53911891 9472
Satellite: ISS
Catalog Number: 25544
Epoch time: 18238
68387999 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 27
3855 deg
Eccentricity:
0005556
Arg of perigee: 100
7515 deg
Mean anomaly: 259
4263 deg
Mean motion: 15
53911891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 947
Checksum: 351
Coasting Arc #9 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3066949
89 A = 6778796
16 meter
Y = -3155502
84 meter E =
0019355
Z = -5173638
07 I = 51
77042
XDOT = 6445
137282 Wp = 101
29659
YDOT = 3856
896240 meter/sec RA = 22
03267 deg
ZDOT = 1469
269175 TA = 182
84362
MA = 182
85464
Ha = 223
420 n
mi
Hp = 213
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10062171
55 X = 3127138
10
Y = -10352699
61 feet Y = -3120869
92 meter
Z = -16973878
19 Z = -5158593
69
XDOT = 21145
463522 XDOT = 6394
392553
YDOT = 12653
859056 feet/sec YDOT = 3928
686605 meter/sec
ZDOT = 4820
436926 ZDOT = 1500
453444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5189291
52 X = -1581696
05
Y = 13557296
54 feet Y = 4132263
99 meter
Z = -16905892
18 Z = -5152915
94
XDOT = -23422
133345 XDOT = -7139
066244
YDOT = -2784
255126 feet/sec YDOT = -848
640962 meter/sec
ZDOT = 4959
876367 ZDOT = 1511
770317
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18239
64856931
00016717 00000-0 10270-3 0 9080
2 25544 51
6420 22
5794 0005672 102
4349 257
7439 15
53895441 9621
Satellite: ISS
Catalog Number: 25544
Epoch time: 18239
64856931 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 22
5794 deg
Eccentricity:
0005672
Arg of perigee: 102
4349 deg
Mean anomaly: 257
7439 deg
Mean motion: 15
53895441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 962
Checksum: 335
Coasting Arc #10 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2018/240/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466237
54 A = 6781457
72 meter
Y = 2354751
53 meter E =
0013916
Z = 4516381
71 I = 51
74812
XDOT = -5497
904642 Wp = 82
08346
YDOT = -4308
458559 meter/sec RA = 17
04812 deg
ZDOT = -3180
271807 TA = 39
81538
MA = 39
71336
Ha = 223
525 n
mi
Hp = 213
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14653010
29 X = -4514175
05
Y = 7725562
77 feet Y = 2304539
30 meter
Z = 14817525
28 Z = 4494569
88
XDOT = -18037
744889 XDOT = -5433
869730
YDOT = -14135
362728 feet/sec YDOT = -4369
582156 meter/sec
ZDOT = -10433
962622 ZDOT = -3206
822558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10209546
30 X = 3111869
71
Y = -13155302
41 feet Y = -4009736
17 meter
Z = 14719282
22 Z = 4486437
22
XDOT = 21256
860746 XDOT = 6479
091155
YDOT = 4652
053625 feet/sec YDOT = 1417
945945 meter/sec
ZDOT = -10552
525927 ZDOT = -3216
409903
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18240
67756853
00016717 00000-0 10270-3 0 9098
2 25544 51
6420 17
4519 0005653 105
7773 254
4004 15
53893937 9782
Satellite: ISS
Catalog Number: 25544
Epoch time: 18240
67756853 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 17
4519 deg
Eccentricity:
0005653
Arg of perigee: 105
7773 deg
Mean anomaly: 254
4004 deg
Mean motion: 15
53893937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 978
Checksum: 334
Coasting Arc #11 (Orbit 992)
---------------------------------------
Vector Time (GMT): 2018/241/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5613811
29 A = 6785046
15 meter
Y = -1598925
74 meter E =
0010309
Z = -3469773
63 I = 51
72780
XDOT = 4117
192415 Wp = 100
55128
YDOT = 4565
298490 meter/sec RA = 12
07074 deg
ZDOT = 4567
219588 TA = 218
84224
MA = 218
91637
Ha = 223
375 n
mi
Hp = 213
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18418016
04 X = 5648127
91
Y = -5245819
35 feet Y = -1535956
63 meter
Z = -11383771
76 Z = -3442420
38
XDOT = 13507
849132 XDOT = 4043
650985
YDOT = 14978
013420 feet/sec YDOT = 4610
928978 meter/sec
ZDOT = 14984
316233 ZDOT = 4587
040345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14427270
14 X = -4397431
94
Y = 12703583
61 feet Y = 3872052
28 meter
Z = -11260774
16 Z = -3432283
96
XDOT = -17627
667712 XDOT = -5372
913119
YDOT = -6687
239820 feet/sec YDOT = -2038
270697 meter/sec
ZDOT = 15072
624496 ZDOT = 4594
135946
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18241
64225311
00016717 00000-0 10270-3 0 9108
2 25544 51
6417 12
6458 0005550 110
0985 250
0765 15
53885601 9939
Satellite: ISS
Catalog Number: 25544
Epoch time: 18241
64225311 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 12
6458 deg
Eccentricity:
0005550
Arg of perigee: 110
0985 deg
Mean anomaly: 250
0765 deg
Mean motion: 15
53885601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 993
Checksum: 291
Coasting Arc #12 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2018/242/15:14:30
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6407432
41 A = 6788312
51 meter
Y = 833725
73 meter E =
0019562
Z = 2050821
26 I = 51
70645
XDOT = -2402
912311 Wp = 111
19255
YDOT = -4718
170912 meter/sec RA = 7
09968 deg
ZDOT = -5553
663954 TA = 46
13558
MA = 45
97412
Ha = 223
408 n
mi
Hp = 213
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21021759
89 X = -6426240
94
Y = 2735320
62 feet Y = 761968
37 meter
Z = 6728416
21 Z = 2019650
51
XDOT = -7883
570574 XDOT = -2322
997126
YDOT = -15479
563359 feet/sec YDOT = -4744
595551 meter/sec
ZDOT = -18220
682264 ZDOT = -5565
141962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17629617
96 X = 5373507
55
Y = -11851473
14 feet Y = -3612329
01 meter
Z = 6588407
04 Z = 2008146
47
XDOT = 12992
179447 XDOT = 3960
016296
YDOT = 9102
525668 feet/sec YDOT = 2774
449823 meter/sec
ZDOT = -18271
517843 ZDOT = -5569
158638
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18242
67124702
00016717 00000-0 10270-3 0 9115
2 25544 51
6419 7
5183 0005624 112
0371 248
1379 15
53891925 10096
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
67124702 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 7
5183 deg
Eccentricity:
0005624
Arg of perigee: 112
0371 deg
Mean anomaly: 248
1379 deg
Mean motion: 15
53891925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1009
Checksum: 295
Coasting Arc #13 (Orbit 1012)
---------------------------------------
Vector Time (GMT): 2018/242/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -472891
17 A = 6778276
27 meter
Y = -4244850
89 meter E =
0019879
Z = -5280487
58 I = 51
66106
XDOT = 7610
955518 Wp = 90
75820
YDOT = 135
703837 meter/sec RA = 5
75045 deg
ZDOT = -793
526925 TA = 171
66227
MA = 171
62919
Ha = 223
421 n
mi
Hp = 213
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1551480
23 X = -399739
15
Y = -13926676
15 feet Y = -4249730
48 meter
Z = -17324434
32 Z = -5282606
72
XDOT = 24970
326503 XDOT = 7612
726909
YDOT = 445
222562 feet/sec YDOT = 220
824658 meter/sec
ZDOT = -2603
434793 ZDOT = -756
551316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10397787
58 X = 3169245
65
Y = -9377467
70 feet Y = -2858252
15 meter
Z = -17333336
01 Z = -5283200
82
XDOT = 13699
745981 XDOT = 4175
682575
YDOT = 19678
634418 feet/sec YDOT = 5998
047770 meter/sec
ZDOT = -2437
517316 ZDOT = -742
955278
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18242
92849552
00016717 00000-0 10270-3 0 9121
2 25544 51
6391 6
2374 0005686 109
4820 250
6947 15
53876969 10135
Satellite: ISS
Catalog Number: 25544
Epoch time: 18242
92849552 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 6
2374 deg
Eccentricity:
0005686
Arg of perigee: 109
4820 deg
Mean anomaly: 250
6947 deg
Mean motion: 15
53876969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1013
Checksum: 330
Coasting Arc #14 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2018/243/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1242522
15 A = 6778451
68 meter
Y = 4123182
39 meter E =
0008325
Z = 5227583
17 I = 51
62795
XDOT = -7544
206014 Wp = 89
98162
YDOT = -934
456759 meter/sec RA =
75419 deg
ZDOT = -1054
657214 TA = 10
12183
MA = 10
10507
Ha = 223
386 n
mi
Hp = 213
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4076516
23 X = -1313929
24
Y = 13527501
28 feet Y = 4108888
72 meter
Z = 17150863
41 Z = 5221373
72
XDOT = -24751
332066 XDOT = -7528
072985
YDOT = -3065
803016 feet/sec YDOT = -1018
731159 meter/sec
ZDOT = -3460
161464 ZDOT = -1091
265140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13314276
69 X = -4058191
54
Y = 4828727
07 feet Y = 1471796
01 meter
Z = 17122407
02 Z = 5218909
66
XDOT = -12135
031724 XDOT = -3698
757669
YDOT = -20591
479646 feet/sec YDOT = -6276
282996 meter/sec
ZDOT = -3624
299948 ZDOT = -1104
686624
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18243
95748621
00016717 00000-0 10270-3 0 9131
2 25544 51
6384 1
1102 0005569 113
0496 247
1244 15
53886089 10292
Satellite: ISS
Catalog Number: 25544
Epoch time: 18243
95748621 = yrday
fracday
Element set: 913
Inclination: 51
6384 deg
RA of node: 1
1102 deg
Eccentricity:
0005569
Arg of perigee: 113
0496 deg
Mean anomaly: 247
1244 deg
Mean motion: 15
53886089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 307
Coasting Arc #15 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2018/244/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2881523
64 A = 6780766
85 meter
Y = -3955881
95 meter E =
0016162
Z = -4708970
80 I = 51
60265
XDOT = 6916
843323 Wp = 111
29359
YDOT = 1710
372450 meter/sec RA = 355
75851 deg
ZDOT = 2797
752378 TA = 186
49375
MA = 186
51472
Ha = 223
317 n
mi
Hp = 213
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9453817
72 X = 2948418
99
Y = -12978615
33 feet Y = -3923284
94 meter
Z = -15449379
26 Z = -4694810
67
XDOT = 22693
055522 XDOT = 6883
613360
YDOT = 5611
458169 feet/sec YDOT = 1787
535711 meter/sec
ZDOT = 9178
977617 ZDOT = 2831
271276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16110513
54 X = 4910484
53
Y = -497167
96 feet Y = -151536
79 meter
Z = -15385272
90 Z = -4689431
18
XDOT = 9522
864657 XDOT = 2902
569147
YDOT = 20092
723009 feet/sec YDOT = 6124
261973 meter/sec
ZDOT = 9329
131548 ZDOT = 2843
519296
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18244
92216224
00016717 00000-0 10270-3 0 9149
2 25544 51
6386 356
3031 0005516 116
3408 243
8311 15
53877935 10446
Satellite: ISS
Catalog Number: 25544
Epoch time: 18244
92216224 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 356
3031 deg
Eccentricity:
0005516
Arg of perigee: 116
3408 deg
Mean anomaly: 243
8311 deg
Mean motion: 15
53877935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 299
Coasting Arc #16 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2018/245/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4313376
94 A = 6784217
13 meter
Y = 3681027
31 meter E =
0016581
Z = 3708695
47 I = 51
58236
XDOT = -5844
872416 Wp = 95
12728
YDOT = -2503
422920 meter/sec RA = 350
76794 deg
ZDOT = -4298
000394 TA = 40
55785
MA = 40
43442
Ha = 223
297 n
mi
Hp = 213
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14151499
15 X = -4372233
53
Y = 12076861
24 feet Y = 3632463
15 meter
Z = 12167636
05 Z = 3687599
51
XDOT = -19176
090605 XDOT = -5795
566610
YDOT = -8213
329791 feet/sec YDOT = -2568
508767 meter/sec
ZDOT = -14101
051163 ZDOT = -4326
272952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18349606
92 X = -5592960
19
Y = -3422670
52 feet Y = -1043229
97 meter
Z = 12072453
16 Z = 3679683
72
XDOT = -5914
725961 XDOT = -1802
808473
YDOT = -18649
523795 feet/sec YDOT = -5684
374853 meter/sec
ZDOT = -14227
542851 ZDOT = -4336
555061
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18245
95114588
00016717 00000-0 10270-3 0 9154
2 25544 51
6394 351
1751 0005439 119
0987 241
0711 15
53909662 10608
Satellite: ISS
Catalog Number: 25544
Epoch time: 18245
95114588 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 351
1751 deg
Eccentricity:
0005439
Arg of perigee: 119
0987 deg
Mean anomaly: 241
0711 deg
Mean motion: 15
53909662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 316
Coasting Arc #17 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2018/246/21:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 907880
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5410884
92 A = 6787660
12 meter
Y = -3330452
74 meter E =
0008754
Z = -2393540
76 I = 51
56066
XDOT = 4381
798310 Wp = 82
32491
YDOT = 3279
247908 meter/sec RA = 345
78500 deg
ZDOT = 5360
706866 TA = 250
92644
MA = 251
02126
Ha = 223
240 n
mi
Hp = 213
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17752247
13 X = 5459351
36
Y = -10926682
21 feet Y = -3269673
52 meter
Z = -7852824
01 Z = -2367138
84
XDOT = 14375
978707 XDOT = 4318
763755
YDOT = 10758
687362 feet/sec YDOT = 3327
895846 meter/sec
ZDOT = 17587
620951 ZDOT = 5381
838928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19826592
41 X = 6043145
37
Y = 6579868
57 feet Y = 2005543
94 meter
Z = -7733891
01 Z = -2357289
98
XDOT = 1433
978945 XDOT = 437
076782
YDOT = 16391
833672 feet/sec YDOT = 4996
230903 meter/sec
ZDOT = 17681
959864 ZDOT = 5389
461366
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 18246
91581526
00016717 00000-0 10270-3 0 9162
2 25544 51
6388 346
3681 0005434 122
0167 238
1514 15
53890727 10753
Satellite: ISS
Catalog Number: 25544
Epoch time: 18246
91581526 = yrday
fracday
Element set: 916
Inclination: 51
6388 deg
RA of node: 346
3681 deg
Eccentricity:
0005434
Arg of perigee: 122
0167 deg
Mean anomaly: 238
1514 deg
Mean motion: 15
53890727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 319
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list