[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 16th 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
2
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
1
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
8
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
0
Coasting Arc #1 (Orbit 2460)
---------------------------------------
Vector Time (GMT): 2019/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4888376
46 A = 6794719
59 meter
Y = -3017904
56 meter E =
0005930
Z = 3627353
22 I = 51
98264
XDOT = 543
526542 Wp = 54
17519
YDOT = -6221
374722 meter/sec RA = 61
26809 deg
ZDOT = -4435
165703 TA = 83
16279
MA = 83
09532
Ha = 225
685 n
mi
Hp = 223
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16037980
52 X = -4871885
35
Y = -9901261
68 feet Y = -3072477
60 meter
Z = 11900765
15 Z = 3603647
91
XDOT = 1783
223563 XDOT = 634
598447
YDOT = -20411
334391 feet/sec YDOT = -6214
787438 meter/sec
ZDOT = -14551
068578 ZDOT = -4432
304284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7129489
04 X = 2173068
26
Y = 17520639
12 feet Y = 5340290
80 meter
Z = 11793116
79 Z = 3594542
00
XDOT = -12321
930878 XDOT = -3755
724532
YDOT = 14817
993658 feet/sec YDOT = 4516
524467 meter/sec
ZDOT = -14537
449491 ZDOT = -4431
014605
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 19228
53983921
00016717 00000-0 10270-3 0 9009
2 25544 51
6410 61
8441 0007683 291
4190 68
6140 15
50406753 24617
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
53983921 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 61
8441 deg
Eccentricity:
0007683
Arg of perigee: 291
4190 deg
Mean anomaly: 68
6140 deg
Mean motion: 15
50406753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2461
Checksum: 300
Coasting Arc #2 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2019/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5109647
87 A = 6795814
01 meter
Y = 3053687
55 meter E =
0004359
Z = -3272560
96 I = 51
96758
XDOT = -510
635713 Wp = 329
60551
YDOT = 5970
425171 meter/sec RA = 56
33323 deg
ZDOT = 4774
710404 TA = 352
68650
MA = 352
69286
Ha = 225
982 n
mi
Hp = 223
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16763936
57 X = 5091016
87
Y = 10018659
93 feet Y = 3110722
98 meter
Z = -10736748
57 Z = -3247786
01
XDOT = -1675
314019 XDOT = -600
553218
YDOT = 19588
009091 feet/sec YDOT = 5964
212225 meter/sec
ZDOT = 15665
060382 ZDOT = 4772
011459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7947899
49 X = -2422519
77
Y = -17906347
50 feet Y = -5457854
72 meter
Z = -10624241
10 Z = -3238268
69
XDOT = 11470
170537 XDOT = 3496
107980
YDOT = -14376
210831 feet/sec YDOT = -4381
869061 meter/sec
ZDOT = 15652
198916 ZDOT = 4770
790230
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 19229
50670526
00016717 00000-0 10270-3 0 9012
2 25544 51
6395 57
0502 0007405 294
6717 65
3662 15
50381757 24761
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
50670526 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 57
0502 deg
Eccentricity:
0007405
Arg of perigee: 294
6717 deg
Mean anomaly: 65
3662 deg
Mean motion: 15
50381757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2476
Checksum: 317
Coasting Arc #3 (Orbit 2491)
---------------------------------------
Vector Time (GMT): 2019/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5334924
28 A = 6796753
78 meter
Y = -3066697
18 meter E =
0006606
Z = 2882551
60 I = 51
95149
XDOT = 530
429582 Wp = 77
20675
YDOT = -5708
263007 meter/sec RA = 51
39926 deg
ZDOT = -5080
001503 TA = 70
19963
MA = 70
12842
Ha = 226
034 n
mi
Hp = 223
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17503032
43 X = -5314236
71
Y = -10061342
46 feet Y = -3126240
29 meter
Z = 9457190
28 Z = 2856687
29
XDOT = 1740
254535 XDOT = 618
897038
YDOT = -18727
897004 feet/sec YDOT = -5701
836883 meter/sec
ZDOT = -16666
671598 ZDOT = -5077
209862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8833872
17 X = 2692564
24
Y = 18214205
22 feet Y = 5551689
75 meter
Z = 9339734
19 Z = 2846750
98
XDOT = -10762
793108 XDOT = -3280
499339
YDOT = 13778
460397 feet/sec YDOT = 4199
674729 meter/sec
ZDOT = -16653
407330 ZDOT = -5075
958554
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 19230
53802581
00016717 00000-0 10270-3 0 9026
2 25544 51
6395 51
9380 0007612 298
5027 61
5357 15
50405907 24926
Satellite: ISS
Catalog Number: 25544
Epoch time: 19230
53802581 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 51
9380 deg
Eccentricity:
0007612
Arg of perigee: 298
5027 deg
Mean anomaly: 61
5357 deg
Mean motion: 15
50405907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2492
Checksum: 306
Coasting Arc #4 (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 = 5553418
25 A = 6797725
26 meter
Y = 3023371
02 meter E =
0007802
Z = -2481347
10 I = 51
93247
XDOT = -585
980913 Wp = 343
33757
YDOT = 5460
434382 meter/sec RA = 46
46380 deg
ZDOT = 5344
860368 TA = 349
01643
MA = 349
03345
Ha = 226
280 n
mi
Hp = 222
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18219876
16 X = 5531250
17
Y = 9919196
25 feet Y = 3085349
21 meter
Z = -8140902
56 Z = -2454424
95
XDOT = -1922
509557 XDOT = -672
959570
YDOT = 17914
810963 feet/sec YDOT = 5453
395406 meter/sec
ZDOT = 17535
631130 ZDOT = 5341
802466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9815402
26 X = -2991734
61
Y = -18329974
38 feet Y = -5586976
19 meter
Z = -8018637
92 Z = -2444080
84
XDOT = 10214
771389 XDOT = 3113
462319
YDOT = -13130
122290 feet/sec YDOT = -4002
061274 meter/sec
ZDOT = 17521
172672 ZDOT = 5340
453430
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
50489143
00016717 00000-0 10270-3 0 9030
2 25544 51
6392 47
1447 0007317 301
5013 58
5422 15
50379548 25073
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
50489143 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 47
1447 deg
Eccentricity:
0007317
Arg of perigee: 301
5013 deg
Mean anomaly: 58
5422 deg
Mean motion: 15
50379548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2507
Checksum: 297
Coasting Arc #5 (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 = -5764312
39 A = 6798450
93 meter
Y = -2961411
69 meter E =
0006842
Z = 2047401
68 I = 51
91215
XDOT = 695
322700 Wp = 95
60217
YDOT = -5213
601220 meter/sec RA = 41
52815 deg
ZDOT = -5568
109097 TA = 61
89332
MA = 61
82418
Ha = 226
359 n
mi
Hp = 222
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18911786
06 X = -5740713
68
Y = -9715917
62 feet Y = -3025740
27 meter
Z = 6717197
11 Z = 2019458
46
XDOT = 2281
242455 XDOT = 780
617582
YDOT = -17104
990880 feet/sec YDOT = -5205
348922 meter/sec
ZDOT = -18268
074465 ZDOT = -5564
524153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10814369
50 X = 3296219
82
Y = 18351918
74 feet Y = 5593664
83 meter
Z = 6590290
97 Z = 2008720
69
XDOT = -9847
141632 XDOT = -3001
408769
YDOT = 12375
252723 feet/sec YDOT = 3771
977030 meter/sec
ZDOT = -18251
234860 ZDOT = -5562
976385
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
53620979
00016717 00000-0 10270-3 0 9049
2 25544 51
6399 42
0323 0007548 305
9095 54
1355 15
50412154 25237
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
53620979 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 42
0323 deg
Eccentricity:
0007548
Arg of perigee: 305
9095 deg
Mean anomaly: 54
1355 deg
Mean motion: 15
50412154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2523
Checksum: 300
Coasting Arc #6 (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 = 5952874
14 A = 6799184
97 meter
Y = 2845929
14 meter E =
0010979
Z = -1610742
10 I = 51
88925
XDOT = -835
635693 Wp = 356
55655
YDOT = 4997
904689 meter/sec RA = 36
59099 deg
ZDOT = 5750
862356 TA = 345
90117
MA = 345
93179
Ha = 226
583 n
mi
Hp = 222
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19530426
96 X = 5928431
76
Y = 9337037
86 feet Y = 2912361
66 meter
Z = -5284586
95 Z = -1581884
85
XDOT = -2741
586920 XDOT = -919
395962
YDOT = 16397
325095 feet/sec YDOT = 4988
091848 meter/sec
ZDOT = 18867
658649 ZDOT = 5746
599595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11845592
13 X = -3610536
48
Y = -18156758
29 feet Y = -5534179
93 meter
Z = -5153521
91 Z = -1570793
48
XDOT = 9661
428549 XDOT = 2944
803422
YDOT = -11644
585756 feet/sec YDOT = -3549
269739 meter/sec
ZDOT = 18847
749057 ZDOT = 5744
793912
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
50307224
00016717 00000-0 10270-3 0 9053
2 25544 51
6405 37
2393 0007183 309
7788 50
2729 15
50387018 25382
Satellite: ISS
Catalog Number: 25544
Epoch time: 19233
50307224 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 37
2393 deg
Eccentricity:
0007183
Arg of perigee: 309
7788 deg
Mean anomaly: 50
2729 deg
Mean motion: 15
50387018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2538
Checksum: 309
Coasting Arc #7 (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 = 4341039
45 A = 6798406
20 meter
Y = 4798344
78 meter E =
0012708
Z = 2058050
66 I = 51
87061
XDOT = -4872
523498 Wp = 36
45323
YDOT = 2018
292435 meter/sec RA = 33
40737 deg
ZDOT = 5564
297154 TA = 346
21035
MA = 346
24503
Ha = 226
765 n
mi
Hp = 222
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14242255
41 X = 4277063
51
Y = 15742600
97 feet Y = 4846531
66 meter
Z = 6752134
72 Z = 2078982
26
XDOT = -15985
969482 XDOT = -4921
758667
YDOT = 6621
694342 feet/sec YDOT = 1963
529261 meter/sec
ZDOT = 18255
568090 ZDOT = 5540
508720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19359003
84 X = 5900624
37
Y = 8637785
87 feet Y = 2632797
13 meter
Z = 6846917
07 Z = 2086940
32
XDOT = -11411
800946 XDOT = -3478
316928
YDOT = 11171
843943 feet/sec YDOT = 3405
178034 meter/sec
ZDOT = 18147
085482 ZDOT = 5531
231655
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
21210372
00016717 00000-0 10270-3 0 9060
2 25544 51
6420 33
7292 0007551 314
7548 45
2988 15
50381808 25491
Satellite: ISS
Catalog Number: 25544
Epoch time: 19234
21210372 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 33
7292 deg
Eccentricity:
0007551
Arg of perigee: 314
7548 deg
Mean anomaly: 45
2988 deg
Mean motion: 15
50381808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 305
Coasting Arc #8 (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 = -4357062
85 A = 6797532
14 meter
Y = -4587146
56 meter E =
0002479
Z = -2488791
84 I = 51
84038
XDOT = 5130
236979 Wp = 334
01725
YDOT = -1980
220371 meter/sec RA = 28
46767 deg
ZDOT = -5327
403110 TA = 233
73018
MA = 233
75309
Ha = 226
929 n
mi
Hp = 222
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14294825
63 X = -4293355
09
Y = -15049693
43 feet Y = -4635514
09 meter
Z = -8165327
55 Z = -2509802
02
XDOT = 16831
486150 XDOT = 5177
876586
YDOT = -6496
785994 feet/sec YDOT = -1922
584091 meter/sec
ZDOT = -17478
356661 ZDOT = -5302
366693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19252104
61 X = -5868041
49
Y = -7656949
66 feet Y = -2333838
26 meter
Z = -8260476
73 Z = -2517793
31
XDOT = 12079
873109 XDOT = 3681
945324
YDOT = -11625
305826 feet/sec YDOT = -3543
393216 meter/sec
ZDOT = -17364
201729 ZDOT = -5292
608687
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
17896357
00016717 00000-0 10270-3 0 9070
2 25544 51
6430 28
9372 0007609 317
9985 42
0582 15
50393707 25644
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
17896357 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 28
9372 deg
Eccentricity:
0007609
Arg of perigee: 317
9985 deg
Mean anomaly: 42
0582 deg
Mean motion: 15
50393707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2564
Checksum: 338
Coasting Arc #9 (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 = 4366236
38 A = 6790625
09 meter
Y = -2064786
22 meter E =
0005720
Z = -4777274
99 I = 51
80204
XDOT = 5248
089663 Wp = 71
26210
YDOT = 4886
570675 meter/sec RA = 25
79586 deg
ZDOT = 2688
942840 TA = 225
25142
MA = 225
29799
Ha = 226
877 n
mi
Hp = 222
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14324922
50 X = 4412206
19
Y = -6774233
02 feet Y = -2015702
83 meter
Z = -15673474
39 Z = -4755953
88
XDOT = 17218
141938 XDOT = 5179
995219
YDOT = 16032
056021 feet/sec YDOT = 4944
877748 meter/sec
ZDOT = 8821
990945 ZDOT = 2714
270669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7500306
09 X = -2286093
30
Y = 14066917
17 feet Y = 4287596
35 meter
Z = -15576221
84 Z = -4747632
42
XDOT = -22316
603000 XDOT = -6802
100594
YDOT = -2019
496083 feet/sec YDOT = -615
542406 meter/sec
ZDOT = 8936
753359 ZDOT = 2723
922424
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
69462009
00016717 00000-0 10270-3 0 9081
2 25544 51
6435 26
3791 0007322 317
1331 42
9247 15
50418530 25723
Satellite: ISS
Catalog Number: 25544
Epoch time: 19235
69462009 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 26
3791 deg
Eccentricity:
0007322
Arg of perigee: 317
1331 deg
Mean anomaly: 42
9247 deg
Mean motion: 15
50418530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2572
Checksum: 298
Coasting Arc #10 (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 = -3592755
33 A = 6789438
38 meter
Y = 2786377
73 meter E =
0009322
Z = 5045121
88 I = 51
78289
XDOT = -6059
812228 Wp = 359
53716
YDOT = -4258
020488 meter/sec RA = 23
10047 deg
ZDOT = -1954
607393 TA = 109
46598
MA = 109
36524
Ha = 227
102 n
mi
Hp = 221
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11787255
00 X = -3648152
70
Y = 9141659
23 feet Y = 2745891
19 meter
Z = 16552237
13 Z = 5027535
18
XDOT = -19881
273713 XDOT = -6002
253076
YDOT = -13969
883492 feet/sec YDOT = -4325
463708 meter/sec
ZDOT = -6412
753913 ZDOT = -1983
903853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 420554
62 X = 128185
05
Y = 14999510
74 feet Y = 4571850
87 meter
Z = 16471905
76 Z = 5020636
88
XDOT = -21859
420174 XDOT = -6662
751269
YDOT = 7833
889714 feet/sec YDOT = 2387
769585 meter/sec
ZDOT = -6545
637715 ZDOT = -1995
110375
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
27473397
00016717 00000-0 10270-3 0 9099
2 25544 51
6446 23
5064 0007802 321
1152 38
9437 15
50439476 25814
Satellite: ISS
Catalog Number: 25544
Epoch time: 19236
27473397 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 23
5064 deg
Eccentricity:
0007802
Arg of perigee: 321
1152 deg
Mean anomaly: 38
9437 deg
Mean motion: 15
50439476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 317
Coasting Arc #11 (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 = 3816881
33 A = 6790238
35 meter
Y = -2793754
14 meter E =
0007268
Z = -4876360
16 I = 51
75360
XDOT = 6049
376672 Wp = 66
36070
YDOT = 4009
888861 meter/sec RA = 18
14970 deg
ZDOT = 2443
428480 TA = 227
57955
MA = 227
64106
Ha = 227
320 n
mi
Hp = 221
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12522576
55 X = 3871524
72
Y = -9165860
03 feet Y = -2750765
42 meter
Z = -15998556
95 Z = -4857686
65
XDOT = 19847
036327 XDOT = 5992
218594
YDOT = 13155
803351 feet/sec YDOT = 4077
217588 meter/sec
ZDOT = 8016
497637 ZDOT = 2472
675192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -279252
12 X = -85116
05
Y = -15603566
43 feet Y = -4755967
05 meter
Z = -15913279
70 Z = -4850367
65
XDOT = 20983
687801 XDOT = 6395
828042
YDOT = -8667
196409 feet/sec YDOT = -2641
761465 meter/sec
ZDOT = 8149
171783 ZDOT = 2483
867559
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
24159132
00016717 00000-0 10270-3 0 9107
2 25544 51
6441 18
7136 0007784 325
4345 34
6299 15
50408930 25961
Satellite: ISS
Catalog Number: 25544
Epoch time: 19237
24159132 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 18
7136 deg
Eccentricity:
0007784
Arg of perigee: 325
4345 deg
Mean anomaly: 34
6299 deg
Mean motion: 15
50408930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2596
Checksum: 312
Coasting Arc #12 (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 = -4067326
04 A = 6791037
24 meter
Y = 2817685
16 meter E =
0010837
Z = 4653404
42 I = 51
72393
XDOT = -5983
931774 Wp = 18
51582
YDOT = -3778
390850 meter/sec RA = 13
19769 deg
ZDOT = -2930
515168 TA = 100
71175
MA = 100
58971
Ha = 227
427 n
mi
Hp = 221
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13344245
54 X = -4121135
35
Y = 9244373
89 feet Y = 2771900
44 meter
Z = 15267074
86 Z = 4633516
47
XDOT = -19632
322092 XDOT = -5927
001309
YDOT = -12396
295440 feet/sec YDOT = -3844
988971 meter/sec
ZDOT = -9614
551075 ZDOT = -2959
444428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 156444
90 X = 47684
41
Y = 16317697
75 feet Y = 4973634
27 meter
Z = 15176270
21 Z = 4625727
16
XDOT = -20023
077355 XDOT = -6103
033978
YDOT = 9292
600598 feet/sec YDOT = 2832
384662 meter/sec
ZDOT = -9745
798664 ZDOT = -2970
519433
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
27290300
00016717 00000-0 10270-3 0 9115
2 25544 51
6435 13
6016 0007896 329
0442 31
0242 15
50443200 26124
Satellite: ISS
Catalog Number: 25544
Epoch time: 19238
27290300 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 13
6016 deg
Eccentricity:
0007896
Arg of perigee: 329
0442 deg
Mean anomaly: 31
0242 deg
Mean motion: 15
50443200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2612
Checksum: 263
Coasting Arc #13 (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 = 4273966
75 A = 6792055
83 meter
Y = -2901758
68 meter E =
0006009
Z = -4411333
52 I = 51
69416
XDOT = 5888
030894 Wp = 49
70573
YDOT = 3548
643572 meter/sec RA = 8
24367 deg
ZDOT = 3377
225764 TA = 254
44764
MA = 254
51399
Ha = 227
608 n
mi
Hp = 221
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14022200
63 X = 4327524
90
Y = -9520205
64 feet Y = -2853664
59 meter
Z = -14472878
99 Z = -4390442
48
XDOT = 19317
686661 XDOT = 5831
506880
YDOT = 11642
531405 feet/sec YDOT = 3614
171542 meter/sec
ZDOT = 11080
137020 ZDOT = 3405
690010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -302379
37 X = -92165
23
Y = -17026937
24 feet Y = -5189810
47 meter
Z = -14377504
21 Z = -4382263
28
XDOT = 18999
297186 XDOT = 5790
985782
YDOT = -9783
456260 feet/sec YDOT = -2981
997468 meter/sec
ZDOT = 11209
288853 ZDOT = 3416
591242
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
23975904
00016717 00000-0 10270-3 0 9123
2 25544 51
6434 8
8086 0007860 332
1558 27
9171 15
50409274 26274
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
23975904 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 8
8086 deg
Eccentricity:
0007860
Arg of perigee: 332
1558 deg
Mean anomaly: 27
9171 deg
Mean motion: 15
50409274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 321
Coasting Arc #14 (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 = 2861867
68 A = 6789770
78 meter
Y = -3637779
16 meter E =
0009003
Z = -4973808
79 I = 51
67426
XDOT = 6910
748019 Wp = 68
90146
YDOT = 2488
376225 meter/sec RA = 6
34342 deg
ZDOT = 2162
717620 TA = 222
16683
MA = 222
23611
Ha = 227
450 n
mi
Hp = 221
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9389329
66 X = 2926493
29
Y = -11934971
01 feet Y = -3605414
30 meter
Z = -16318270
31 Z = -4959750
25
XDOT = 22673
057806 XDOT = 6871
903549
YDOT = 8163
963992 feet/sec YDOT = 2565
439834 meter/sec
ZDOT = 7095
530250 ZDOT = 2196
192613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5893486
61 X = -1796334
72
Y = 14070045
81 feet Y = 4288549
96 meter
Z = -16253910
82 Z = -4954192
02
XDOT = -22966
547522 XDOT = -7000
203685
YDOT = -1271
489738 feet/sec YDOT = -387
550072 meter/sec
ZDOT = 7247
594915 ZDOT = 2209
066930
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
62650051
00016717 00000-0 10270-3 0 9130
2 25544 51
6437 6
8888 0007422 332
6898 27
3862 15
50423253 26332
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
62650051 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 6
8888 deg
Eccentricity:
0007422
Arg of perigee: 332
6898 deg
Mean anomaly: 27
3862 deg
Mean motion: 15
50423253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 316
Coasting Arc #15 (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 = -669566
16 A = 6788164
91 meter
Y = 4169082
01 meter E =
0007959
Z = 5316110
76 I = 51
65292
XDOT = -7613
760044 Wp = 354
19841
YDOT = -791
805843 meter/sec RA = 3
98106 deg
ZDOT = -330
301412 TA = 98
99764
MA = 98
90756
Ha = 227
656 n
mi
Hp = 221
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2196739
37 X = -741958
52
Y = 13678090
59 feet Y = 4161189
62 meter
Z = 17441308
28 Z = 5312682
54
XDOT = -24979
527703 XDOT = -7602
735584
YDOT = -2597
788200 feet/sec YDOT = -876
886622 meter/sec
ZDOT = -1083
666051 ZDOT = -367
258774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -114125
26 X = -34785
38
Y = 13873070
26 feet Y = 4228511
81 meter
Z = 17425267
79 Z = 5311221
62
XDOT = -24055
847918 XDOT = -7332
222445
YDOT = 1406
101762 feet/sec YDOT = 428
579817 meter/sec
ZDOT = -1251
754225 ZDOT = -381
534688
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
14215544
00016717 00000-0 10270-3 0 9144
2 25544 51
6434 4
3351 0007859 335
7787 24
2994 15
50437833 26412
Satellite: ISS
Catalog Number: 25544
Epoch time: 19240
14215544 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 4
3351 deg
Eccentricity:
0007859
Arg of perigee: 335
7787 deg
Mean anomaly: 24
2994 deg
Mean motion: 15
50437833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 310
Coasting Arc #16 (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 = 893269
44 A = 6788456
99 meter
Y = -4192337
32 meter E =
0013018
Z = -5273372
33 I = 51
62113
XDOT = 7586
660424 Wp = 63
70054
YDOT = 548
580025 meter/sec RA = 359
02073 deg
ZDOT = 856
275308 TA = 214
46130
MA = 214
54578
Ha = 227
831 n
mi
Hp = 220
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2930674
01 X = 965697
56
Y = -13754387
55 feet Y = -4181943
26 meter
Z = -17301090
32 Z = -5268857
28
XDOT = 24890
618190 XDOT = 7575
802968
YDOT = 1799
803233 feet/sec YDOT = 633
358709 meter/sec
ZDOT = 2809
302193 ZDOT = 893
101327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 583657
41 X = 177898
78
Y = -14076824
18 feet Y = -4290616
01 meter
Z = -17280107
58 Z = -5266976
79
XDOT = 23774
120770 XDOT = 7246
352011
YDOT = -2639
143864 feet/sec YDOT = -804
411050 meter/sec
ZDOT = 2976
810196 ZDOT = 907
331748
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
10900801
00016717 00000-0 10270-3 0 9159
2 25544 51
6442 359
5425 0007860 340
7568 19
3285 15
50415084 26561
Satellite: ISS
Catalog Number: 25544
Epoch time: 19241
10900801 = yrday
fracday
Element set: 915
Inclination: 51
6442 deg
RA of node: 359
5425 deg
Eccentricity:
0007860
Arg of perigee: 340
7568 deg
Mean anomaly: 19
3285 deg
Mean motion: 15
50415084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2656
Checksum: 304
Coasting Arc #17 (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 = -1152975
82 A = 6788794
10 meter
Y = 4243741
43 meter E =
0010333
Z = 5172856
65 I = 51
58877
XDOT = -7526
192283 Wp = 7
77759
YDOT = -330
009278 meter/sec RA = 354
05888 deg
ZDOT = -1396
434480 TA = 95
73164
MA = 95
61381
Ha = 227
942 n
mi
Hp = 220
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3782729
06 X = -1225471
23
Y = 13923036
17 feet Y = 4230442
92 meter
Z = 16971314
46 Z = 5167079
77
XDOT = -24692
231901 XDOT = -7515
159700
YDOT = -1082
707605 feet/sec YDOT = -414
110837 meter/sec
ZDOT = -4581
477952 ZDOT = -1432
966352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1142875
70 X = -348348
51
Y = 14413885
83 feet Y = 4393352
40 meter
Z = 16944592
65 Z = 5164711
84
XDOT = -23356
761325 XDOT = -7119
140852
YDOT = 3769
213754 feet/sec YDOT = 1148
856352 meter/sec
ZDOT = -4747
659046 ZDOT = -1447
086477
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
14031446
00016717 00000-0 10270-3 0 9165
2 25544 51
6438 354
4310 0007931 343
4956 16
5935 15
50445249 26728
Satellite: ISS
Catalog Number: 25544
Epoch time: 19242
14031446 = yrday
fracday
Element set: 916
Inclination: 51
6438 deg
RA of node: 354
4310 deg
Eccentricity:
0007931
Arg of perigee: 343
4956 deg
Mean anomaly: 16
5935 deg
Mean motion: 15
50445249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 307
Coasting Arc #18 (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 = 1354983
62 A = 6789431
14 meter
Y = -4342045
53 meter E =
0011554
Z = -5048397
98 I = 51
55826
XDOT = 7414
415622 Wp = 66
58282
YDOT = 110
104786 meter/sec RA = 349
09506 deg
ZDOT = 1903
275162 TA = 221
87961
MA = 221
96805
Ha = 228
059 n
mi
Hp = 220
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4445484
33 X = 1427958
83
Y = -14245556
19 feet Y = -4326485
47 meter
Z = -16562985
49 Z = -5041638
54
XDOT = 24325
510572 XDOT = 7403
388448
YDOT = 361
236176 feet/sec YDOT = 192
956484 meter/sec
ZDOT = 6244
341082 ZDOT = 1939
264217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1472594
81 X = 448846
90
Y = -14884959
11 feet Y = -4536935
54 meter
Z = -16531792
02 Z = -5038890
21
XDOT = 22734
798775 XDOT = 6929
566667
YDOT = -4838
798376 feet/sec YDOT = -1474
865745 meter/sec
ZDOT = 6408
060745 ZDOT = 1953
176915
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
10716478
00016717 00000-0 10270-3 0 9178
2 25544 51
6445 349
6388 0007938 346
7565 13
3376 15
50418874 26870
Satellite: ISS
Catalog Number: 25544
Epoch time: 19243
10716478 = yrday
fracday
Element set: 917
Inclination: 51
6445 deg
RA of node: 349
6388 deg
Eccentricity:
0007938
Arg of perigee: 346
7565 deg
Mean anomaly: 13
3376 deg
Mean motion: 15
50418874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2687
Checksum: 352
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