[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 21st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15269 8125 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 626 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
234/03:38:33
000 0
0 0
0 0
0
N/A 0
0 0
0 226
8
000/00:00:00
000 0
0 0
0 222
3
235/16:24:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
9
000/00:00:00
000 0
0 0
0 222
2
236/05:30:52
000 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 221
9
239/14:44:31
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 221
3
240/02:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
7
000/00:00:00
000 0
0 0
0 221
1
Coasting Arc #1 (Orbit 2537)
---------------------------------------
Vector Time (GMT): 2019/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5953041
03 A = 6799187
29 meter
Y = 2844792
76 meter E =
0011021
Z = -1611961
62 I = 51
88955
XDOT = -833
906153 Wp = 356
07489
YDOT = 4998
715409 meter/sec RA = 36
59038 deg
ZDOT = 5750
471305 TA = 346
36909
MA = 346
39882
Ha = 226
597 n
mi
Hp = 222
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19530974
51 X = 5928617
28
Y = 9333309
58 feet Y = 2911227
25 meter
Z = -5288588
00 Z = -1583103
52
XDOT = -2735
912574 XDOT = -917
673716
YDOT = 16399
984938 feet/sec YDOT = 4988
921869 meter/sec
ZDOT = 18866
375672 ZDOT = 5746
216928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11848023
51 X = -3611277
56
Y = -18153873
79 feet Y = -5533300
73 meter
Z = -5157518
95 Z = -1572011
77
XDOT = 9658
171194 XDOT = 2943
810580
YDOT = -11649
637636 feet/sec YDOT = -3550
809551 meter/sec
ZDOT = 18846
504157 ZDOT = 5744
414467
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 19233
50307464
00016717 00000-0 10270-3 0 9004
2 25544 51
6408 37
2388 0007281 309
5568 50
4939 15
50385689 25389
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
50307464 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 37
2388 deg
Eccentricity:
0007281
Arg of perigee: 309
5568 deg
Mean anomaly: 50
4939 deg
Mean motion: 15
50385689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 327
Coasting Arc #2 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2019/234/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4342360
43 A = 6798412
97 meter
Y = 4797767
34 meter E =
0012692
Z = 2056614
35 I = 51
87092
XDOT = -4871
001186 Wp = 35
98844
YDOT = 2019
960360 meter/sec RA = 33
40679 deg
ZDOT = 5565
027715 TA = 346
65835
MA = 346
69188
Ha = 226
780 n
mi
Hp = 222
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14246589
35 X = 4278397
83
Y = 15740706
50 feet Y = 4845969
07 meter
Z = 6747422
42 Z = 2077552
40
XDOT = -15980
975021 XDOT = -4920
258669
YDOT = 6627
166536 feet/sec YDOT = 1965
214084 meter/sec
ZDOT = 18257
964945 ZDOT = 5541
246622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19362226
76 X = 5901606
72
Y = 8634284
27 feet Y = 2631729
85 meter
Z = 6842234
17 Z = 2085512
98
XDOT = -11405
287288 XDOT = -3476
331565
YDOT = 11174
593843 feet/sec YDOT = 3406
016203 meter/sec
ZDOT = 18149
515577 ZDOT = 5531
972348
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 19234
21210678
00016717 00000-0 10270-3 0 9014
2 25544 51
6423 33
7287 0007647 314
5140 45
5385 15
50380337 25490
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
21210678 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 33
7287 deg
Eccentricity:
0007647
Arg of perigee: 314
5140 deg
Mean anomaly: 45
5385 deg
Mean motion: 15
50380337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 298
Coasting Arc #3 (Orbit 2563)
---------------------------------------
Vector Time (GMT): 2019/235/03:38:33
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4359085
70 A = 6797541
32 meter
Y = -4586337
30 meter E =
0002556
Z = -2486759
69 I = 51
84069
XDOT = 5128
128121 Wp = 332
65932
YDOT = -1982
425214 meter/sec RA = 28
46713 deg
ZDOT = -5328
609280 TA = 235
06334
MA = 235
08735
Ha = 226
945 n
mi
Hp = 222
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14301462
27 X = -4295396
71
Y = -15047038
40 feet Y = -4634727
57 meter
Z = -8158660
40 Z = -2507779
74
XDOT = 16824
567326 XDOT = 5175
798399
YDOT = -6504
019731 feet/sec YDOT = -1924
812345 meter/sec
ZDOT = -17482
313910 ZDOT = -5303
583032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19257047
19 X = -5869547
98
Y = -7651728
24 feet Y = -2332246
77 meter
Z = -8253854
60 Z = -2515774
88
XDOT = 12070
956940 XDOT = 3679
227675
YDOT = -11628
605693 feet/sec YDOT = -3544
399015 meter/sec
ZDOT = -17368
205034 ZDOT = -5293
828894
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 19235
17896763
00016717 00000-0 10270-3 0 9026
2 25544 51
6433 28
9367 0007704 317
7620 42
2936 15
50392030 25644
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
17896763 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 28
9367 deg
Eccentricity:
0007704
Arg of perigee: 317
7620 deg
Mean anomaly: 42
2936 deg
Mean motion: 15
50392030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 314
Coasting Arc #4 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2019/235/16:24:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4363966
29 A = 6790625
56 meter
Y = -2066831
57 meter E =
0005663
Z = -4778377
02 I = 51
80233
XDOT = 5250
508104 Wp = 70
51231
YDOT = 4885
460271 meter/sec RA = 25
79538 deg
ZDOT = 2686
436801 TA = 225
97412
MA = 226
02079
Ha = 226
894 n
mi
Hp = 222
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14317474
72 X = 4409964
50
Y = -6780943
48 feet Y = -2017773
40 meter
Z = -15677089
96 Z = -4757066
86
XDOT = 17226
076457 XDOT = 5182
438070
YDOT = 16028
412962 feet/sec YDOT = 4943
794525 meter/sec
ZDOT = 8813
769033 ZDOT = 2711
776437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7490342
46 X = -2283056
38
Y = 14067846
85 feet Y = 4287879
72 meter
Z = -15579887
07 Z = -4748749
58
XDOT = -22320
752501 XDOT = -6803
365362
YDOT = -2012
520337 feet/sec YDOT = -613
416199 meter/sec
ZDOT = 8928
585297 ZDOT = 2721
432799
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 19235
69462492
00016717 00000-0 10270-3 0 9032
2 25544 51
6438 26
3787 0007418 316
9241 43
1337 15
50416771 25722
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
69462492 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 26
3787 deg
Eccentricity:
0007418
Arg of perigee: 316
9241 deg
Mean anomaly: 43
1337 deg
Mean motion: 15
50416771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 318
Coasting Arc #5 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2019/236/05:30:52
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3547364
70 A = 6789381
93 meter
Y = 2818121
52 meter E =
0009333
Z = 5059617
84 I = 51
78299
XDOT = -6093
649066 Wp = 358
33046
YDOT = -4231
338407 meter/sec RA = 23
10073 deg
ZDOT = -1906
544052 TA = 110
18950
MA = 110
08909
Ha = 227
119 n
mi
Hp = 221
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11638335
63 X = -3603190
83
Y = 9245805
52 feet Y = 2778140
17 meter
Z = 16599796
05 Z = 5042250
58
XDOT = -19992
286963 XDOT = -6036
619230
YDOT = -13882
343855 feet/sec YDOT = -4299
162975 meter/sec
ZDOT = -6255
065788 ZDOT = -1936
006163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 584459
43 X = 178143
23
Y = 14940609
45 feet Y = 4553897
76 meter
Z = 16520460
08 Z = 5035436
23
XDOT = -21862
677275 XDOT = -6663
744034
YDOT = 7952
345805 feet/sec YDOT = 2423
875001 meter/sec
ZDOT = -6388
706287 ZDOT = -1947
277676
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 19236
27473932
00016717 00000-0 10270-3 0 9049
2 25544 51
6449 23
5060 0007896 320
8831 39
1748 15
50437349 25811
Satellite: ISS
Catalog Number: 25544
Epoch time: 19236
27473932 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 23
5060 deg
Eccentricity:
0007896
Arg of perigee: 320
8831 deg
Mean anomaly: 39
1748 deg
Mean motion: 15
50437349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 324
Coasting Arc #6 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2019/237/05:30:52
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3770752
72 A = 6790167
27 meter
Y = -2824074
24 meter E =
0007344
Z = -4894708
39 I = 51
75366
XDOT = 6085
992300 Wp = 65
98752
YDOT = 3982
822382 meter/sec RA = 18
14997 deg
ZDOT = 2396
292369 TA = 227
46197
MA = 227
52400
Ha = 227
338 n
mi
Hp = 221
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12371235
94 X = 3825827
71
Y = -9265335
45 feet Y = -2781598
95 meter
Z = -16058754
56 Z = -4876257
91
XDOT = 19967
166337 XDOT = 6029
363125
YDOT = 13067
002564 feet/sec YDOT = 4050
563528 meter/sec
ZDOT = 7861
851603 ZDOT = 2425
718228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -439318
85 X = -133904
39
Y = -15537059
42 feet Y = -4735695
71 meter
Z = -15974489
07 Z = -4869024
27
XDOT = 20989
656700 XDOT = 6397
647362
YDOT = -8794
425028 feet/sec YDOT = -2680
540749 meter/sec
ZDOT = 7995
343900 ZDOT = 2436
980821
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 19237
24159795
00016717 00000-0 10270-3 0 9056
2 25544 51
6444 18
7132 0007878 325
2106 34
8529 15
50407099 25960
Satellite: ISS
Catalog Number: 25544
Epoch time: 19237
24159795 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 18
7132 deg
Eccentricity:
0007878
Arg of perigee: 325
2106 deg
Mean anomaly: 34
8529 deg
Mean motion: 15
50407099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 330
Coasting Arc #7 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2019/238/05:30:52
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4021052
66 A = 6790955
31 meter
Y = 2846746
47 meter E =
0010848
Z = 4675893
24 I = 51
72394
XDOT = -6023
493724 Wp = 17
29457
YDOT = -3750
564886 meter/sec RA = 13
19795 deg
ZDOT = -2884
699483 TA = 101
43441
MA = 101
31255
Ha = 227
446 n
mi
Hp = 221
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13192430
00 X = -4075299
62
Y = 9339719
38 feet Y = 2801476
76 meter
Z = 15340857
07 Z = 4656229
00
XDOT = -19762
118517 XDOT = -5967
094022
YDOT = -12305
002908 feet/sec YDOT = -3817
608386 meter/sec
ZDOT = -9464
237148 ZDOT = -2913
822207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 311766
61 X = 95026
46
Y = 16245621
19 feet Y = 4951665
34 meter
Z = 15251067
40 Z = 4648525
34
XDOT = -20030
506024 XDOT = -6105
298236
YDOT = 9429
942974 feet/sec YDOT = 2874
246618 meter/sec
ZDOT = -9596
368099 ZDOT = -2924
972996
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 19238
27291114
00016717 00000-0 10270-3 0 9063
2 25544 51
6438 13
6013 0007988 328
7983 31
2693 15
50440746 26126
Satellite: ISS
Catalog Number: 25544
Epoch time: 19238
27291114 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 13
6013 deg
Eccentricity:
0007988
Arg of perigee: 328
7983 deg
Mean anomaly: 31
2693 deg
Mean motion: 15
50440746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 313
Coasting Arc #8 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2019/239/05:30:52
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227486
74 A = 6791963
96 meter
Y = -2929499
96 meter E =
0006071
Z = -4437670
04 I = 51
69414
XDOT = 5930
494184 Wp = 50
01549
YDOT = 3519
547874 meter/sec RA = 8
24391 deg
ZDOT = 3333
028500 TA = 253
63001
MA = 253
69676
Ha = 227
629 n
mi
Hp = 221
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13869707
16 X = 4281486
49
Y = -9611220
36 feet Y = -2881923
18 meter
Z = -14559284
90 Z = -4417003
71
XDOT = 19457
001917 XDOT = 5874
507054
YDOT = 11547
073078 feet/sec YDOT = 3585
553701 meter/sec
ZDOT = 10935
132874 ZDOT = 3361
700317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -452765
36 X = -138002
88
Y = -16949274
97 feet Y = -5166139
01 meter
Z = -14464929
71 Z = -4408910
58
XDOT = 19006
318272 XDOT = 5793
125809
YDOT = -9931
808366 feet/sec YDOT = -3027
215190 meter/sec
ZDOT = 11065
232368 ZDOT = 3372
682826
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 19239
23976875
00016717 00000-0 10270-3 0 9075
2 25544 51
6437 8
8083 0007955 331
9401 28
1320 15
50406913 26279
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
23976875 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 8
8083 deg
Eccentricity:
0007955
Arg of perigee: 331
9401 deg
Mean anomaly: 28
1320 deg
Mean motion: 15
50406913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 318
Coasting Arc #9 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2019/239/14:44:31
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2855484
30 A = 6789770
12 meter
Y = -3640020
19 meter E =
0008978
Z = -4975769
71 I = 51
67453
XDOT = 6914
132200 Wp = 68
33132
YDOT = 2484
131249 meter/sec RA = 6
34315 deg
ZDOT = 2156
970845 TA = 222
67773
MA = 222
74750
Ha = 227
472 n
mi
Hp = 221
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9368386
82 X = 2920144
97
Y = -11942323
44 feet Y = -3607726
51 meter
Z = -16324703
76 Z = -4961742
09
XDOT = 22684
160760 XDOT = 6875
362861
YDOT = 8150
036905 feet/sec YDOT = 2561
233123 meter/sec
ZDOT = 7076
676000 ZDOT = 2190
462458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5871375
48 X = -1789595
24
Y = 14071435
59 feet Y = 4288973
57 meter
Z = -16260484
74 Z = -4956195
75
XDOT = -22973
463043 XDOT = -7002
311535
YDOT = -1256
644095 feet/sec YDOT = -383
025120 meter/sec
ZDOT = 7228
816749 ZDOT = 2203
343345
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 19239
62651089
00016717 00000-0 10270-3 0 9086
2 25544 51
6440 6
8886 0007518 332
4665 27
6087 15
50420552 26331
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
62651089 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 6
8886 deg
Eccentricity:
0007518
Arg of perigee: 332
4665 deg
Mean anomaly: 27
6087 deg
Mean motion: 15
50420552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 321
Coasting Arc #10 (Orbit 2640)
---------------------------------------
Vector Time (GMT): 2019/240/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -662154
23 A = 6788171
35 meter
Y = 4169858
54 meter E =
0008025
Z = 5316495
35 I = 51
65323
XDOT = -7614
531322 Wp = 353
73397
YDOT = -786
580705 meter/sec RA = 3
98083 deg
ZDOT = -323
686131 TA = 99
39925
MA = 99
30851
Ha = 227
678 n
mi
Hp = 221
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2172422
02 X = -734557
70
Y = 13680638
26 feet Y = 4162048
97 meter
Z = 17442570
06 Z = 5313103
11
XDOT = -24982
058142 XDOT = -7603
597367
YDOT = -2580
645357 feet/sec YDOT = -871
670614 meter/sec
ZDOT = -1061
962373 ZDOT = -360
647460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -89720
68 X = -27346
86
Y = 13871728
27 feet Y = 4228102
78 meter
Z = 17426693
20 Z = 5311656
09
XDOT = -24055
867856 XDOT = -7332
228522
YDOT = 1421
673841 feet/sec YDOT = 433
326187 meter/sec
ZDOT = -1230
069146 ZDOT = -374
925076
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 19240
14216674
00016717 00000-0 10270-3 0 9093
2 25544 51
6437 4
3349 0007953 335
5524 24
5248 15
50435038 26414
Satellite: ISS
Catalog Number: 25544
Epoch time: 19240
14216674 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 4
3349 deg
Eccentricity:
0007953
Arg of perigee: 335
5524 deg
Mean anomaly: 24
5248 deg
Mean motion: 15
50435038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 301
Coasting Arc #11 (Orbit 2655)
---------------------------------------
Vector Time (GMT): 2019/241/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 884450
42 A = 6788460
95 meter
Y = -4192920
34 meter E =
0013010
Z = -5274350
80 I = 51
62142
XDOT = 7588
011460 Wp = 63
23938
YDOT = 542
418841 meter/sec RA = 359
02057 deg
ZDOT = 848
561669 TA = 214
84759
MA = 214
93284
Ha = 227
854 n
mi
Hp = 220
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2901740
23 X = 956890
48
Y = -13756300
32 feet Y = -4182624
83 meter
Z = -17304300
52 Z = -5269878
55
XDOT = 24895
050721 XDOT = 7577
260267
YDOT = 1779
589372 feet/sec YDOT = 627
213226 meter/sec
ZDOT = 2783
994977 ZDOT = 885
394509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 554859
40 X = 169121
14
Y = -14073629
16 feet Y = -4289642
17 meter
Z = -17283512
51 Z = -5268014
61
XDOT = 23775
334298 XDOT = 7246
721894
YDOT = -2657
753503 feet/sec YDOT = -810
083268 meter/sec
ZDOT = 2951
534660 ZDOT = 899
627764
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 19241
10902117
00016717 00000-0 10270-3 0 9106
2 25544 51
6446 359
5423 0007953 340
5154 19
5691 15
50412096 26568
Satellite: ISS
Catalog Number: 25544
Epoch time: 19241
10902117 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 359
5423 deg
Eccentricity:
0007953
Arg of perigee: 340
5154 deg
Mean anomaly: 19
5691 deg
Mean motion: 15
50412096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2656
Checksum: 298
Coasting Arc #12 (Orbit 2671)
---------------------------------------
Vector Time (GMT): 2019/242/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1143067
30 A = 6788795
53 meter
Y = 4244186
06 meter E =
0010390
Z = 5174756
63 I = 51
58905
XDOT = -7528
057471 Wp = 7
32368
YDOT = -322
844404 meter/sec RA = 354
05878 deg
ZDOT = -1387
720872 TA = 96
10039
MA = 95
98200
Ha = 227
966 n
mi
Hp = 220
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3750220
81 X = -1215577
65
Y = 13924494
94 feet Y = 4230998
28 meter
Z = 16977548
00 Z = 5169027
85
XDOT = -24698
351284 XDOT = -7517
147194
YDOT = -1059
200799 feet/sec YDOT = -406
967504 meter/sec
ZDOT = -4552
890001 ZDOT = -1424
262102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1110736
78 X = -338552
57
Y = 14409066
23 feet Y = 4391883
39 meter
Z = 16951044
97 Z = 5166678
51
XDOT = -23358
779765 XDOT = -7119
756072
YDOT = 3791
154145 feet/sec YDOT = 1155
543783 meter/sec
ZDOT = -4719
114409 ZDOT = -1438
386072
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 19242
14032978
00016717 00000-0 10270-3 0 9111
2 25544 51
6442 354
4309 0008024 343
2658 16
8227 15
50441897 26724
Satellite: ISS
Catalog Number: 25544
Epoch time: 19242
14032978 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 354
4309 deg
Eccentricity:
0008024
Arg of perigee: 343
2658 deg
Mean anomaly: 16
8227 deg
Mean motion: 15
50441897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 309
Coasting Arc #13 (Orbit 2686)
---------------------------------------
Vector Time (GMT): 2019/243/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1343588
65 A = 6789428
72 meter
Y = -4342159
43 meter E =
0011564
Z = -5051301
22 I = 51
55852
XDOT = 7417
078323 Wp = 66
10484
YDOT = 101
659455 meter/sec RA = 349
09503 deg
ZDOT = 1893
486152 TA = 222
25846
MA = 222
34763
Ha = 228
085 n
mi
Hp = 220
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4408099
25 X = 1416580
08
Y = -14245929
88 feet Y = -4326726
71 meter
Z = -16572510
57 Z = -5044597
09
XDOT = 24334
246468 XDOT = 7406
192939
YDOT = 333
528396 feet/sec YDOT = 184
541721 meter/sec
ZDOT = 6212
224908 ZDOT = 1929
488486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1436023
82 X = 437700
06
Y = -14877509
99 feet Y = -4534665
05 meter
Z = -16541568
72 Z = -5041870
15
XDOT = 22738
292929 XDOT = 6930
631685
YDOT = -4865
101573 feet/sec YDOT = -1482
882959 meter/sec
ZDOT = 6376
005843 ZDOT = 1943
406581
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 19243
10718231
00016717 00000-0 10270-3 0 9122
2 25544 51
6449 349
6387 0008031 346
5325 13
5610 15
50415328 26874
Satellite: ISS
Catalog Number: 25544
Epoch time: 19243
10718231 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 349
6387 deg
Eccentricity:
0008031
Arg of perigee: 346
5325 deg
Mean anomaly: 13
5610 deg
Mean motion: 15
50415328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2687
Checksum: 300
Coasting Arc #14 (Orbit 2702)
---------------------------------------
Vector Time (GMT): 2019/244/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1574164
11 A = 6790080
89 meter
Y = 4467190
92 meter E =
0012493
Z = 4865771
18 I = 51
52886
XDOT = -7272
186276 Wp = 21
53970
YDOT = 76
786545 meter/sec RA = 344
12898 deg
ZDOT = -2409
830807 TA = 92
21952
MA = 92
07646
Ha = 228
217 n
mi
Hp = 220
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5164580
40 X = -1647635
48
Y = 14656138
18 feet Y = 4449177
11 meter
Z = 15963816
19 Z = 4857945
74
XDOT = -23858
878859 XDOT = -7260
798957
YDOT = 251
924359 feet/sec YDOT = -4
472700 meter/sec
ZDOT = -7906
269051 ZDOT = -2445
128304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1819983
53 X = -554730
98
Y = 15469729
30 feet Y = 4715173
49 meter
Z = 15927769
45 Z = 4854784
13
XDOT = -22003
139607 XDOT = -6706
556952
YDOT = 5762
260695 feet/sec YDOT = 1756
337060 meter/sec
ZDOT = -8066
845441 ZDOT = -2458
774491
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 19244
13848690
00016717 00000-0 10270-3 0 9130
2 25544 51
6452 344
5268 0008172 350
0897 10
0091 15
50454867 27035
Satellite: ISS
Catalog Number: 25544
Epoch time: 19244
13848690 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 344
5268 deg
Eccentricity:
0008172
Arg of perigee: 350
0897 deg
Mean anomaly: 10
0091 deg
Mean motion: 15
50454867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2703
Checksum: 309
Coasting Arc #15 (Orbit 2717)
---------------------------------------
Vector Time (GMT): 2019/245/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1729480
20 A = 6791006
23 meter
Y = -4628353
16 meter E =
0010081
Z = -4664387
97 I = 51
49892
XDOT = 7089
724901 Wp = 62
36968
YDOT = -245
673548 meter/sec RA = 339
16157 deg
ZDOT = 2881
895518 TA = 236
32831
MA = 236
42450
Ha = 228
372 n
mi
Hp = 220
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5674147
64 X = 1803764
12
Y = -15184885
69 feet Y = -4608597
93 meter
Z = -15303110
13 Z = -4655806
05
XDOT = 23260
252301 XDOT = 7077
946606
YDOT = -806
015578 feet/sec YDOT = -166
456865 meter/sec
ZDOT = 9455
037790 ZDOT = 2916
305951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1915156
92 X = 583739
83
Y = -16134315
46 feet Y = -4917739
35 meter
Z = -15263614
35 Z = -4652349
66
XDOT = 21129
038240 XDOT = 6440
130856
YDOT = -6555
710628 feet/sec YDOT = -1998
180599 meter/sec
ZDOT = 9611
580078 ZDOT = 2929
609608
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 19245
10533589
00016717 00000-0 10270-3 0 9147
2 25544 51
6443 339
7344 0008163 354
1495 5
9559 15
50418285 27187
Satellite: ISS
Catalog Number: 25544
Epoch time: 19245
10533589 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 339
7344 deg
Eccentricity:
0008163
Arg of perigee: 354
1495 deg
Mean anomaly: 5
9559 deg
Mean motion: 15
50418285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2718
Checksum: 328
Coasting Arc #16 (Orbit 2733)
---------------------------------------
Vector Time (GMT): 2019/246/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1906944
42 A = 6791913
66 meter
Y = 4811543
94 meter E =
0014221
Z = 4397373
58 I = 51
47096
XDOT = -6877
607035 Wp = 36
59389
YDOT = 357
132809 meter/sec RA = 334
19259 deg
ZDOT = -3356
470413 TA = 87
54557
MA = 87
38277
Ha = 228
466 n
mi
Hp = 219
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6256379
32 X = -1981966
73
Y = 15785905
31 feet Y = 4789799
98 meter
Z = 14427078
69 Z = 4387927
82
XDOT = -22564
327543 XDOT = -6864
785599
YDOT = 1171
695569 feet/sec YDOT = 280
294013 meter/sec
ZDOT = -11012
042038 ZDOT = -3389
848072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2037913
51 X = -621156
04
Y = 16894833
90 feet Y = 5149545
37 meter
Z = 14383642
93 Z = 4384134
37
XDOT = -20182
833557 XDOT = -6151
727668
YDOT = 7117
094088 feet/sec YDOT = 2169
290278 meter/sec
ZDOT = -11163
883991 ZDOT = -3402
751840
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 19246
13663859
00016717 00000-0 10270-3 0 9156
2 25544 51
6438 334
6225 0008258 357
4503 2
6605 15
50456933 27340
Satellite: ISS
Catalog Number: 25544
Epoch time: 19246
13663859 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 334
6225 deg
Eccentricity:
0008258
Arg of perigee: 357
4503 deg
Mean anomaly: 2
6605 deg
Mean motion: 15
50456933 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2734
Checksum: 320
Coasting Arc #17 (Orbit 2748)
---------------------------------------
Vector Time (GMT): 2019/247/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1996845
02 A = 6792990
57 meter
Y = -5015887
98 meter E =
0009158
Z = -4124876
54 I = 51
44456
XDOT = 6646
101127 Wp = 50
31580
YDOT = -452
652863 meter/sec RA = 329
22168 deg
ZDOT = 3779
128588 TA = 258
75573
MA = 258
85867
Ha = 228
573 n
mi
Hp = 219
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6551328
80 X = 2072822
08
Y = -16456325
40 feet Y = -4993133
26 meter
Z = -13533059
52 Z = -4114991
81
XDOT = 21804
793725 XDOT = 6632
311957
YDOT = -1485
081573 feet/sec YDOT = -378
408378 meter/sec
ZDOT = 12398
715841 ZDOT = 3811
379397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1839568
94 X = 560700
61
Y = -17651473
47 feet Y = -5380169
11 meter
Z = -13487613
77 Z = -4111024
68
XDOT = 19179
142428 XDOT = 5845
802612
YDOT = -7558
767035 feet/sec YDOT = -2303
912192 meter/sec
ZDOT = 12545
431242 ZDOT = 3823
847443
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 19247
10348520
00016717 00000-0 10270-3 0 9160
2 25544 51
6436 329
8295 0008203
5066 359
6091 15
50422045 27498
Satellite: ISS
Catalog Number: 25544
Epoch time: 19247
10348520 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 329
8295 deg
Eccentricity:
0008203
Arg of perigee:
5066 deg
Mean anomaly: 359
6091 deg
Mean motion: 15
50422045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2749
Checksum: 302
Coasting Arc #18 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2019/248/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2105122
52 A = 6794029
89 meter
Y = 5234262
73 meter E =
0015478
Z = 3783359
70 I = 51
42051
XDOT = -6391
879367 Wp = 50
89969
YDOT = 477
417308 meter/sec RA = 324
24910 deg
ZDOT = -4195
893591 TA = 83
66482
MA = 83
48856
Ha = 228
699 n
mi
Hp = 219
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6906569
95 X = -2181874
57
Y = 17172777
99 feet Y = 5210292
76 meter
Z = 12412597
43 Z = 3772947
19
XDOT = -20970
732830 XDOT = -6376
361599
YDOT = 1566
329752 feet/sec YDOT = 406
025425 meter/sec
ZDOT = -13766
055087 ZDOT = -4226
905282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1658495
92 X = -505509
56
Y = 18467275
47 feet Y = 5628825
56 meter
Z = 12364736
76 Z = 3768771
77
XDOT = -18158
817141 XDOT = -5534
807465
YDOT = 7727
357544 feet/sec YDOT = 2355
298580 meter/sec
ZDOT = -13907
129731 ZDOT = -4238
893142
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 19248
13478393
00016717 00000-0 10270-3 0 9177
2 25544 51
6439 324
7165 0008405 4
1981 355
9238 15
50458189 27659
Satellite: ISS
Catalog Number: 25544
Epoch time: 19248
13478393 = yrday
fracday
Element set: 917
Inclination: 51
6439 deg
RA of node: 324
7165 deg
Eccentricity:
0008405
Arg of perigee: 4
1981 deg
Mean anomaly: 355
9238 deg
Mean motion: 15
50458189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 340
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