[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 20th 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
7
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
236/05:30:59
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
4
000/00:00:00
000 0
0 0
0 221
4
240/02:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
6
000/00:00:00
000 0
0 0
0 221
1
Coasting Arc #1 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2019/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5553500
77 A = 6797727
95 meter
Y = 3022839
34 meter E =
0007768
Z = -2481843
10 I = 51
93277
XDOT = -585
200688 Wp = 342
55034
YDOT = 5460
796710 meter/sec RA = 46
46325 deg
ZDOT = 5344
558360 TA = 349
79783
MA = 349
81359
Ha = 226
255 n
mi
Hp = 222
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18220146
90 X = 5531341
04
Y = 9917451
90 feet Y = 3084818
50 meter
Z = -8142529
85 Z = -2454920
53
XDOT = -1919
949764 XDOT = -672
181988
YDOT = 17915
999706 feet/sec YDOT = 5453
766445 meter/sec
ZDOT = 17534
640289 ZDOT = 5341
504241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9816596
35 X = -2992098
57
Y = -18328671
83 feet Y = -5586579
17 meter
Z = -8020263
24 Z = -2444576
24
XDOT = 10213
375641 XDOT = 3113
036895
YDOT = -13132
438783 feet/sec YDOT = -4002
767341 meter/sec
ZDOT = 17520
199018 ZDOT = 5340
156661
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 19231
50489250
00016717 00000-0 10270-3 0 9006
2 25544 51
6395 47
1442 0007365 300
7176 59
3248 15
50378298 25071
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
50489250 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 47
1442 deg
Eccentricity:
0007365
Arg of perigee: 300
7176 deg
Mean anomaly: 59
3248 deg
Mean motion: 15
50378298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 311
Coasting Arc #2 (Orbit 2522)
---------------------------------------
Vector Time (GMT): 2019/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5764473
51 A = 6798453
66 meter
Y = -2960267
27 meter E =
0006753
Z = 2048580
85 I = 51
91244
XDOT = 693
785833 Wp = 96
12492
YDOT = -5214
347245 meter/sec RA = 41
52763 deg
ZDOT = -5567
614528 TA = 61
35697
MA = 61
28907
Ha = 226
337 n
mi
Hp = 222
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18912314
68 X = -5740893
31
Y = -9712162
97 feet Y = -3024597
75 meter
Z = 6721065
77 Z = 2020636
80
XDOT = 2276
200238 XDOT = 779
086768
YDOT = -17107
438467 feet/sec YDOT = -5206
112099 meter/sec
ZDOT = -18266
451863 ZDOT = -5564
037034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10816847
49 X = 3296975
12
Y = 18349043
61 feet Y = 5592788
49 meter
Z = 6594155
75 Z = 2009898
67
XDOT = -9844
392505 XDOT = -3000
570835
YDOT = 12379
843702 feet/sec YDOT = 3773
376360 meter/sec
ZDOT = -18249
646099 ZDOT = -5562
492131
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 19232
53621182
00016717 00000-0 10270-3 0 9013
2 25544 51
6402 42
0319 0007594 305
1445 54
8993 15
50410529 25238
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
53621182 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 42
0319 deg
Eccentricity:
0007594
Arg of perigee: 305
1445 deg
Mean anomaly: 54
8993 deg
Mean motion: 15
50410529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2523
Checksum: 285
Coasting Arc #3 (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 = 5953134
61 A = 6799188
43 meter
Y = 2844540
37 meter E =
0010931
Z = -1612310
00 I = 51
88954
XDOT = -833
447753 Wp = 356
00836
YDOT = 4998
892263 meter/sec RA = 36
59051 deg
ZDOT = 5750
296214 TA = 346
43185
MA = 346
46122
Ha = 226
561 n
mi
Hp = 222
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19531281
54 X = 5928715
36
Y = 9332481
52 feet Y = 2910975
93 meter
Z = -5289730
97 Z = -1583451
43
XDOT = -2734
408640 XDOT = -917
216478
YDOT = 16400
565167 feet/sec YDOT = 4989
103842 meter/sec
ZDOT = 18865
801227 ZDOT = 5746
044061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11848723
29 X = -3611490
86
Y = -18153330
53 feet Y = -5533135
14 meter
Z = -5158659
77 Z = -1572359
50
XDOT = 9657
225441 XDOT = 2943
522314
YDOT = -11650
866856 feet/sec YDOT = -3551
184218 meter/sec
ZDOT = 18845
939817 ZDOT = 5744
242456
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
50307538
00016717 00000-0 10270-3 0 9028
2 25544 51
6408 37
2389 0007229 308
9726 51
0780 15
50385129 25381
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
50307538 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 37
2389 deg
Eccentricity:
0007229
Arg of perigee: 308
9726 deg
Mean anomaly: 51
0780 deg
Mean motion: 15
50385129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 313
Coasting Arc #4 (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 = 4342833
15 A = 6798415
69 meter
Y = 4797635
96 meter E =
0012614
Z = 2056124
14 I = 51
87092
XDOT = -4870
470054 Wp = 36
18681
YDOT = 2020
476153 meter/sec RA = 33
40692 deg
ZDOT = 5565
212622 TA = 346
45406
MA = 346
48789
Ha = 226
745 n
mi
Hp = 222
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14248140
27 X = 4278874
36
Y = 15740275
45 feet Y = 4845843
00 meter
Z = 6745814
10 Z = 2077064
49
XDOT = -15979
232462 XDOT = -4919
734242
YDOT = 6628
858771 feet/sec YDOT = 1965
735779 meter/sec
ZDOT = 18258
571596 ZDOT = 5541
434093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19363479
69 X = 5901988
61
Y = 8633257
14 feet Y = 2631416
78 meter
Z = 6840636
37 Z = 2085025
96
XDOT = -11403
087043 XDOT = -3475
660931
YDOT = 11175
344892 feet/sec YDOT = 3406
245123 meter/sec
ZDOT = 18150
133845 ZDOT = 5532
160796
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
21210780
00016717 00000-0 10270-3 0 9030
2 25544 51
6423 33
7288 0007592 313
9735 46
0789 15
50379699 25496
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
21210780 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 33
7288 deg
Eccentricity:
0007592
Arg of perigee: 313
9735 deg
Mean anomaly: 46
0789 deg
Mean motion: 15
50379699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 330
Coasting Arc #5 (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 = -4359666
83 A = 6797545
13 meter
Y = -4586067
01 meter E =
0002482
Z = -2486086
23 I = 51
84070
XDOT = 5127
484793 Wp = 331
37341
YDOT = -1983
157372 meter/sec RA = 28
46727 deg
ZDOT = -5329
049628 TA = 236
34135
MA = 236
36503
Ha = 226
910 n
mi
Hp = 222
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14303368
87 X = -4295984
10
Y = -15046151
60 feet Y = -4634463
80 meter
Z = -8156450
90 Z = -2507109
13
XDOT = 16822
456670 XDOT = 5175
165445
YDOT = -6506
421824 feet/sec YDOT = -1925
551639 meter/sec
ZDOT = -17483
758621 ZDOT = -5304
026480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19258416
68 X = -5869965
41
Y = -7650114
83 feet Y = -2331755
00 meter
Z = -8251658
03 Z = -2515105
37
XDOT = 12068
157670 XDOT = 3678
374458
YDOT = -11629
800335 feet/sec YDOT = -3544
763142 meter/sec
ZDOT = -17369
663777 ZDOT = -5294
273519
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
17896910
00016717 00000-0 10270-3 0 9042
2 25544 51
6433 28
9368 0007649 317
2229 42
8325 15
50391212 25642
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
17896910 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 28
9368 deg
Eccentricity:
0007649
Arg of perigee: 317
2229 deg
Mean anomaly: 42
8325 deg
Mean motion: 15
50391212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 318
Coasting Arc #6 (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 = 4363267
30 A = 6790626
62 meter
Y = -2067492
80 meter E =
0005619
Z = -4778755
90 I = 51
80233
XDOT = 5251
280953 Wp = 71
31150
YDOT = 4885
082847 meter/sec RA = 25
79553 deg
ZDOT = 2685
553859 TA = 225
16612
MA = 225
21179
Ha = 226
859 n
mi
Hp = 222
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14315181
43 X = 4409274
79
Y = -6783112
87 feet Y = -2018442
40 meter
Z = -15678333
02 Z = -4757449
12
XDOT = 17228
612050 XDOT = 5183
219371
YDOT = 16027
174694 feet/sec YDOT = 4943
425790 meter/sec
ZDOT = 8810
872242 ZDOT = 2710
897270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7487213
45 X = -2282102
66
Y = 14068216
25 feet Y = 4287992
31 meter
Z = -15581145
41 Z = -4749133
12
XDOT = -22322
030351 XDOT = -6803
754851
YDOT = -2010
226696 feet/sec YDOT = -612
717097 meter/sec
ZDOT = 8925
705726 ZDOT = 2720
555105
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
69462650
00016717 00000-0 10270-3 0 9050
2 25544 51
6438 26
3788 0007367 316
3454 43
7113 15
50415915 25723
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
69462650 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 26
3788 deg
Eccentricity:
0007367
Arg of perigee: 316
3454 deg
Mean anomaly: 43
7113 deg
Mean motion: 15
50415915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 317
Coasting Arc #7 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2019/236/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3588732
05 A = 6789441
07 meter
Y = 2789235
37 meter E =
0009286
Z = 5046492
71 I = 51
78317
XDOT = -6062
789951 Wp = 358
82105
YDOT = -4255
599520 meter/sec RA = 23
10018 deg
ZDOT = -1950
362740 TA = 110
13906
MA = 110
03914
Ha = 227
085 n
mi
Hp = 221
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11774055
29 X = -3644168
34
Y = 9151034
69 feet Y = 2748793
60 meter
Z = 16556734
61 Z = 5028925
46
XDOT = -19891
043147 XDOT = -6005
278268
YDOT = -13961
940683 feet/sec YDOT = -4323
076305 meter/sec
ZDOT = -6398
827888 ZDOT = -1979
673780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 435874
28 X = 132854
48
Y = 14994349
52 feet Y = 4570277
74 meter
Z = 16476491
46 Z = 5022034
60
XDOT = -21859
152365 XDOT = -6662
669641
YDOT = 7845
420346 feet/sec YDOT = 2391
284121 meter/sec
ZDOT = -6531
778297 ZDOT = -1990
886025
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
27474138
00016717 00000-0 10270-3 0 9060
2 25544 51
6449 23
5061 0007844 320
3627 39
6950 15
50436614 25817
Satellite: ISS
Catalog Number: 25544
Epoch time: 19236
27474138 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 23
5061 deg
Eccentricity:
0007844
Arg of perigee: 320
3627 deg
Mean anomaly: 39
6950 deg
Mean motion: 15
50436614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 311
Coasting Arc #8 (Orbit 2595)
---------------------------------------
Vector Time (GMT): 2019/237/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3811926
56 A = 6790239
19 meter
Y = -2796978
02 meter E =
0007173
Z = -4878322
54 I = 51
75388
XDOT = 6053
401200 Wp = 66
25131
YDOT = 4006
980568 meter/sec RA = 18
14946 deg
ZDOT = 2438
393296 TA = 227
63657
MA = 227
69732
Ha = 227
306 n
mi
Hp = 221
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12506320
73 X = 3866615
90
Y = -9176437
09 feet Y = -2754044
45 meter
Z = -16004995
20 Z = -4859672
99
XDOT = 19860
240159 XDOT = 5996
299802
YDOT = 13146
261705 feet/sec YDOT = 4074
354616 meter/sec
ZDOT = 7999
978004 ZDOT = 2467
659695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -297208
84 X = -90589
25
Y = -15596336
55 feet Y = -4753763
38 meter
Z = -15919826
63 Z = -4852363
16
XDOT = 20984
019942 XDOT = 6395
929278
YDOT = -8682
267104 feet/sec YDOT = -2646
355013 meter/sec
ZDOT = 8132
742051 ZDOT = 2478
859777
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
24160063
00016717 00000-0 10270-3 0 9078
2 25544 51
6444 18
7133 0007824 324
6769 35
3863 15
50405805 25960
Satellite: ISS
Catalog Number: 25544
Epoch time: 19237
24160063 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 18
7133 deg
Eccentricity:
0007824
Arg of perigee: 324
6769 deg
Mean anomaly: 35
3863 deg
Mean motion: 15
50405805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 312
Coasting Arc #9 (Orbit 2611)
---------------------------------------
Vector Time (GMT): 2019/238/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4061217
28 A = 6791035
73 meter
Y = 2821575
87 meter E =
0010780
Z = 4656468
60 I = 51
72419
XDOT = -5989
148610 Wp = 17
90408
YDOT = -3774
669634 meter/sec RA = 13
19751 deg
ZDOT = -2924
468766 TA = 101
25727
MA = 101
13609
Ha = 227
414 n
mi
Hp = 221
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13324203
67 X = -4115085
43
Y = 9257138
69 feet Y = 2775859
13 meter
Z = 15277127
96 Z = 4636610
18
XDOT = -19649
437697 XDOT = -5932
288740
YDOT = -12384
086725 feet/sec YDOT = -3841
326488 meter/sec
ZDOT = -9594
713799 ZDOT = -2953
423539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 178190
68 X = 54312
52
Y = 16308262
38 feet Y = 4970758
37 meter
Z = 15186457
28 Z = 4628832
18
XDOT = -20023
273983 XDOT = -6103
093910
YDOT = 9312
142187 feet/sec YDOT = 2838
340939 meter/sec
ZDOT = -9726
077883 ZDOT = -2964
508539
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
27291457
00016717 00000-0 10270-3 0 9085
2 25544 51
6438 13
6014 0007935 328
2940 31
7732 15
50439631 26127
Satellite: ISS
Catalog Number: 25544
Epoch time: 19238
27291457 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 13
6014 deg
Eccentricity:
0007935
Arg of perigee: 328
2940 deg
Mean anomaly: 31
7732 deg
Mean motion: 15
50439631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 306
Coasting Arc #10 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2019/239/05:30:59
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266807
99 A = 6792051
84 meter
Y = -2906016
44 meter E =
0005927
Z = -4415398
08 I = 51
69442
XDOT = 5894
674629 Wp = 49
32310
YDOT = 3544
152481 meter/sec RA = 8
24355 deg
ZDOT = 3370
441335 TA = 254
75217
MA = 254
81771
Ha = 227
597 n
mi
Hp = 221
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13998713
87 X = 4320434
03
Y = -9534174
66 feet Y = -2858002
03 meter
Z = -14486214
16 Z = -4394541
65
XDOT = 19339
483690 XDOT = 5838
233296
YDOT = 11627
796855 feet/sec YDOT = 3609
755209 meter/sec
ZDOT = 11057
878395 ZDOT = 3398
938054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -326832
93 X = -99618
68
Y = -17014913
45 feet Y = -5186145
62 meter
Z = -14390996
41 Z = -4386375
71
XDOT = 18999
756999 XDOT = 5791
125933
YDOT = -9808
104520 feet/sec YDOT = -2989
510258 meter/sec
ZDOT = 11187
178475 ZDOT = 3409
851999
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
23977295
00016717 00000-0 10270-3 0 9094
2 25544 51
6437 8
8085 0007901 331
4072 28
6645 15
50405415 26272
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
23977295 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 8
8085 deg
Eccentricity:
0007901
Arg of perigee: 331
4072 deg
Mean anomaly: 28
6645 deg
Mean motion: 15
50405415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 320
Coasting Arc #11 (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 = 2852856
18 A = 6789770
74 meter
Y = -3640959
23 meter E =
0008917
Z = -4976591
05 I = 51
67452
XDOT = 6915
538197 Wp = 68
73158
YDOT = 2482
353448 meter/sec RA = 6
34335 deg
ZDOT = 2154
507330 TA = 222
25282
MA = 222
32156
Ha = 227
439 n
mi
Hp = 221
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9359764
36 X = 2917531
53
Y = -11945404
29 feet Y = -3608694
85 meter
Z = -16327398
45 Z = -4962576
16
XDOT = 22688
773613 XDOT = 6876
800600
YDOT = 8144
204227 feet/sec YDOT = 2559
471223 meter/sec
ZDOT = 7068
593602 ZDOT = 2188
005850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5862257
69 X = -1786816
14
Y = 14072059
59 feet Y = 4289163
76 meter
Z = -16263237
26 Z = -4957034
72
XDOT = -22976
321738 XDOT = -7003
182866
YDOT = -1250
426076 feet/sec YDOT = -381
129868 meter/sec
ZDOT = 7220
765969 ZDOT = 2200
889467
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
62651543
00016717 00000-0 10270-3 0 9104
2 25544 51
6440 6
8887 0007465 331
9007 28
1740 15
50419151 26332
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
62651543 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 6
8887 deg
Eccentricity:
0007465
Arg of perigee: 331
9007 deg
Mean anomaly: 28
1740 deg
Mean motion: 15
50419151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 300
Coasting Arc #12 (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 = -658739
27 A = 6788174
89 meter
Y = 4170229
04 meter E =
0007943
Z = 5316663
83 I = 51
65322
XDOT = -7614
869456 Wp = 353
35237
YDOT = -784
252553 meter/sec RA = 3
98104 deg
ZDOT = -320
684866 TA = 99
75168
MA = 99
66197
Ha = 227
646 n
mi
Hp = 221
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2161218
08 X = -731147
95
Y = 13681853
79 feet Y = 4162457
63 meter
Z = 17443122
81 Z = 5313288
17
XDOT = -24983
167505 XDOT = -7603
976088
YDOT = -2573
007064 feet/sec YDOT = -869
346471 meter/sec
ZDOT = -1052
115702 ZDOT = -357
647935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -78469
74 X = -23917
58
Y = 13871151
13 feet Y = 4227926
86 meter
Z = 17427321
34 Z = 5311847
54
XDOT = -24055
858504 XDOT = -7332
225672
YDOT = 1428
582082 feet/sec YDOT = 435
431819 meter/sec
ZDOT = -1220
230645 ZDOT = -371
926300
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
14217174
00016717 00000-0 10270-3 0 9112
2 25544 51
6437 4
3350 0007898 335
0254 25
0514 15
50433576 26416
Satellite: ISS
Catalog Number: 25544
Epoch time: 19240
14217174 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 4
3350 deg
Eccentricity:
0007898
Arg of perigee: 335
0254 deg
Mean anomaly: 25
0514 deg
Mean motion: 15
50433576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 282
Coasting Arc #13 (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 = 880616
36 A = 6788463
57 meter
Y = -4193179
93 meter E =
0012939
Z = -5274764
44 I = 51
62141
XDOT = 7588
608827 Wp = 63
43824
YDOT = 539
713011 meter/sec RA = 359
02079 deg
ZDOT = 845
121098 TA = 214
61601
MA = 214
70030
Ha = 227
822 n
mi
Hp = 220
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2889161
27 X = 953061
61
Y = -13757152
01 feet Y = -4182927
27 meter
Z = -17305657
63 Z = -5270310
81
XDOT = 24897
010586 XDOT = 7577
904559
YDOT = 1770
711979 feet/sec YDOT = 624
514339 meter/sec
ZDOT = 2772
707014 ZDOT = 881
956953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 542335
67 X = 165303
91
Y = -14072259
87 feet Y = -4289224
81 meter
Z = -17284954
28 Z = -5268454
06
XDOT = 23775
878935 XDOT = 7246
887899
YDOT = -2665
937914 feet/sec YDOT = -812
577876 meter/sec
ZDOT = 2940
260703 ZDOT = 896
191462
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
10902713
00016717 00000-0 10270-3 0 9120
2 25544 51
6446 359
5424 0007896 339
9992 20
0848 15
50410513 26560
Satellite: ISS
Catalog Number: 25544
Epoch time: 19241
10902713 = yrday
fracday
Element set: 912
Inclination: 51
6446 deg
RA of node: 359
5424 deg
Eccentricity:
0007896
Arg of perigee: 339
9992 deg
Mean anomaly: 20
0848 deg
Mean motion: 15
50410513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2656
Checksum: 314
Coasting Arc #14 (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 = -1138328
01 A = 6788796
83 meter
Y = 4244403
18 meter E =
0010302
Z = 5175653
41 I = 51
58904
XDOT = -7528
932745 Wp = 7
05218
YDOT = -319
500870 meter/sec RA = 354
05902 deg
ZDOT = -1383
600612 TA = 96
33099
MA = 96
21366
Ha = 227
934 n
mi
Hp = 220
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3734671
94 X = -1210845
49
Y = 13925207
29 feet Y = 4231268
36 meter
Z = 16980490
19 Z = 5169947
63
XDOT = -24701
222917 XDOT = -7518
079805
YDOT = -1048
231200 feet/sec YDOT = -403
634079 meter/sec
ZDOT = -4539
372087 ZDOT = -1420
146233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1095361
48 X = -333866
18
Y = 14406775
27 feet Y = 4391185
10 meter
Z = 16954091
81 Z = 5167607
18
XDOT = -23359
741589 XDOT = -7120
049236
YDOT = 3801
368560 feet/sec YDOT = 1158
657137 meter/sec
ZDOT = -4705
616820 ZDOT = -1434
272007
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
14033687
00016717 00000-0 10270-3 0 9131
2 25544 51
6441 354
4310 0007968 342
7450 17
3429 15
50440096 26725
Satellite: ISS
Catalog Number: 25544
Epoch time: 19242
14033687 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 354
4310 deg
Eccentricity:
0007968
Arg of perigee: 342
7450 deg
Mean anomaly: 17
3429 deg
Mean motion: 15
50440096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 300
Coasting Arc #15 (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 = 1338361
02 A = 6789428
53 meter
Y = -4342215
83 meter E =
0011494
Z = -5052625
05 I = 51
55850
XDOT = 7418
311055 Wp = 66
31938
YDOT = 97
755359 meter/sec RA = 349
09528 deg
ZDOT = 1888
908401 TA = 221
99829
MA = 222
08648
Ha = 228
054 n
mi
Hp = 220
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4390948
22 X = 1411359
90
Y = -14246114
93 feet Y = -4326841
53 meter
Z = -16576853
85 Z = -5045946
30
XDOT = 24338
290864 XDOT = 7407
491471
YDOT = 320
719681 feet/sec YDOT = 180
651777 meter/sec
ZDOT = 6197
206039 ZDOT = 1924
916883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1419243
23 X = 432585
34
Y = -14874105
85 feet Y = -4533627
46 meter
Z = -16546027
44 Z = -5043229
16
XDOT = 22739
912303 XDOT = 6931
125270
YDOT = -4877
271629 feet/sec YDOT = -1486
592392 meter/sec
ZDOT = 6361
015342 ZDOT = 1938
837476
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
10719057
00016717 00000-0 10270-3 0 9141
2 25544 51
6448 349
6389 0007975 346
0112 14
0816 15
50413415 26879
Satellite: ISS
Catalog Number: 25544
Epoch time: 19243
10719057 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 349
6389 deg
Eccentricity:
0007975
Arg of perigee: 346
0112 deg
Mean anomaly: 14
0816 deg
Mean motion: 15
50413415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2687
Checksum: 314
Coasting Arc #16 (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 = -1567994
09 A = 6790078
51 meter
Y = 4467135
50 meter E =
0012400
Z = 4867838
76 I = 51
52883
XDOT = -7273
845163 Wp = 21
33104
YDOT = 81
547967 meter/sec RA = 344
12925 deg
ZDOT = -2404
593673 TA = 92
37311
MA = 92
23113
Ha = 228
186 n
mi
Hp = 220
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5144337
56 X = -1641475
34
Y = 14655956
37 feet Y = 4449190
64 meter
Z = 15970599
61 Z = 4860043
28
XDOT = -23864
321401 XDOT = -7262
536403
YDOT = 267
545823 feet/sec YDOT =
269733 meter/sec
ZDOT = -7889
086854 ZDOT = -2439
899420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1800351
35 X = -548747
09
Y = 15464984
19 feet Y = 4713727
18 meter
Z = 15934689
11 Z = 4856893
24
XDOT = -22005
365987 XDOT = -6707
235553
YDOT = 5777
303930 feet/sec YDOT = 1760
922238 meter/sec
ZDOT = -8049
701250 ZDOT = -2453
548941
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
13849651
00016717 00000-0 10270-3 0 9150
2 25544 51
6452 344
5269 0008116 349
5724 10
5257 15
50452738 27030
Satellite: ISS
Catalog Number: 25544
Epoch time: 19244
13849651 = yrday
fracday
Element set: 915
Inclination: 51
6452 deg
RA of node: 344
5269 deg
Eccentricity:
0008116
Arg of perigee: 349
5724 deg
Mean anomaly: 10
5257 deg
Mean motion: 15
50452738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2703
Checksum: 314
Coasting Arc #17 (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 = 1722802
22 A = 6791002
02 meter
Y = -4628104
99 meter E =
0010007
Z = -4667096
80 I = 51
49888
XDOT = 7091
823910 Wp = 62
57805
YDOT = -251
233905 meter/sec RA = 339
16185 deg
ZDOT = 2876
256121 TA = 236
05896
MA = 236
15413
Ha = 228
342 n
mi
Hp = 220
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5652238
24 X = 1797097
01
Y = -15184071
50 feet Y = -4608424
39 meter
Z = -15311997
36 Z = -4658547
29
XDOT = 23267
138811 XDOT = 7080
135029
YDOT = -824
258218 feet/sec YDOT = -171
993249 meter/sec
ZDOT = 9436
535829 ZDOT = 2910
676967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1894160
00 X = 577339
97
Y = -16128218
65 feet Y = -4915881
05 meter
Z = -15272649
04 Z = -4655103
43
XDOT = 21131
852077 XDOT = 6440
988513
YDOT = -6573
579910 feet/sec YDOT = -2003
627157 meter/sec
ZDOT = 9593
126038 ZDOT = 2923
984817
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
10534687
00016717 00000-0 10270-3 0 9169
2 25544 51
6443 339
7345 0008106 353
6375 6
4671 15
50416040 27184
Satellite: ISS
Catalog Number: 25544
Epoch time: 19245
10534687 = yrday
fracday
Element set: 916
Inclination: 51
6443 deg
RA of node: 339
7345 deg
Eccentricity:
0008106
Arg of perigee: 353
6375 deg
Mean anomaly: 6
4671 deg
Mean motion: 15
50416040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2718
Checksum: 307
Coasting Arc #18 (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 = -1899346
88 A = 6791906
75 meter
Y = 4811154
54 meter E =
0014125
Z = 4401104
41 I = 51
47091
XDOT = -6880
247632 Wp = 36
42820
YDOT = 363
830765 meter/sec RA = 334
19289 deg
ZDOT = -3350
294357 TA = 87
63959
MA = 87
47787
Ha = 228
436 n
mi
Hp = 219
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6231453
03 X = -1974383
52
Y = 15784627
75 feet Y = 4789495
46 meter
Z = 14439318
94 Z = 4391695
52
XDOT = -22572
990919 XDOT = -6867
530898
YDOT = 1193
670489 feet/sec YDOT = 286
961855 meter/sec
ZDOT = -10991
779385 ZDOT = -3383
685097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2014253
17 X = -613944
37
Y = 16887152
32 feet Y = 5147204
03 meter
Z = 14396050
91 Z = 4387916
32
XDOT = -20186
187464 XDOT = -6152
749939
YDOT = 7138
875780 feet/sec YDOT = 2175
929338 meter/sec
ZDOT = -11143
681498 ZDOT = -3396
594121
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
13665116
00016717 00000-0 10270-3 0 9176
2 25544 51
6437 334
6227 0008202 356
9364 3
1735 15
50454509 27346
Satellite: ISS
Catalog Number: 25544
Epoch time: 19246
13665116 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 334
6227 deg
Eccentricity:
0008202
Arg of perigee: 356
9364 deg
Mean anomaly: 3
1735 deg
Mean motion: 15
50454509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2734
Checksum: 306
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