[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 28th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 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
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
4
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
249/18:11:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 219
3
250/16:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 219
0
Coasting Arc #1 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2019/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 937174
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6472569
26 A = 6799919
23 meter
Y = -1949698
39 meter E =
0003180
Z = -729347
03 I = 51
74237
XDOT = 1988
659053 Wp = 120
80614
YDOT = -4381
479419 meter/sec RA = 11
88297 deg
ZDOT = -5956
581592 TA = 67
04563
MA = 67
01207
Ha = 227
268 n
mi
Hp = 221
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21235463
44 X = -6446743
39
Y = -6396648
26 feet Y = -2021934
79 meter
Z = -2392870
85 Z = -760725
34
XDOT = 6524
471960 XDOT = 2066
439661
YDOT = -14374
932477 feet/sec YDOT = -4358
805743 meter/sec
ZDOT = -19542
590524 ZDOT = -5946
732768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16150965
46 X = 4922814
27
Y = 15175823
59 feet Y = 4625591
03 meter
Z = -2535456
65 Z = -772807
19
XDOT = -11254
363706 XDOT = -3430
330058
YDOT = 8730
884564 feet/sec YDOT = 2661
173615 meter/sec
ZDOT = -19497
305115 ZDOT = -5942
778599
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
53075622
00016717 00000-0 10270-3 0 9000
2 25544 51
6413 12
3176 0007394 328
2730 31
7974 15
50404173 26166
Satellite: ISS
Catalog Number: 25544
Epoch time: 19238
53075622 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 12
3176 deg
Eccentricity:
0007394
Arg of perigee: 328
2730 deg
Mean anomaly: 31
7974 deg
Mean motion: 15
50404173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 290
Coasting Arc #2 (Orbit 2631)
---------------------------------------
Vector Time (GMT): 2019/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6458231
53 A = 6799566
49 meter
Y = 1727219
73 meter E =
0015896
Z = 1184114
65 I = 51
70994
XDOT = -2254
329171 Wp = 30
55073
YDOT = 4392
107807 meter/sec RA = 6
93475 deg
ZDOT = 5867
426844 TA = 342
28820
MA = 342
34355
Ha = 227
357 n
mi
Hp = 221
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21188423
67 X = 6432685
60
Y = 5666731
41 feet Y = 1799297
36 meter
Z = 3884890
60 Z = 1215423
83
XDOT = -7396
093080 XDOT = -2331
775698
YDOT = 14409
802515 feet/sec YDOT = 4366
465147 meter/sec
ZDOT = 19250
088071 ZDOT = 5856
288328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16671753
25 X = -5081550
39
Y = -14212247
34 feet Y = -4331892
99 meter
Z = 4027180
95 Z = 1227484
75
XDOT = 11952
552781 XDOT = 3643
138088
YDOT = -8561
758979 feet/sec YDOT = -2609
624137 meter/sec
ZDOT = 19198
935522 ZDOT = 5851
835547
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
56207620
00016717 00000-0 10270-3 0 9010
2 25544 51
6431 7
2053 0007339 331
8719 28
2034 15
50397433 26325
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
56207620 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 7
2053 deg
Eccentricity:
0007339
Arg of perigee: 331
8719 deg
Mean anomaly: 28
2034 deg
Mean motion: 15
50397433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2632
Checksum: 289
Coasting Arc #3 (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 = 2842341
56 A = 6789783
22 meter
Y = -3644763
58 meter E =
0008959
Z = -4979853
03 I = 51
67431
XDOT = 6921
016795 Wp = 68
48984
YDOT = 2475
319343 meter/sec RA = 6
34310 deg
ZDOT = 2144
919730 TA = 222
39648
MA = 222
46573
Ha = 227
469 n
mi
Hp = 221
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9325267
59 X = 2907076
08
Y = -11957885
77 feet Y = -3612616
46 meter
Z = -16338100
48 Z = -4965889
07
XDOT = 22706
748014 XDOT = 6882
404018
YDOT = 8121
126455 feet/sec YDOT = 2552
499082 meter/sec
ZDOT = 7037
138222 ZDOT = 2178
445166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5825736
36 X = -1775684
44
Y = 14074705
69 feet Y = 4289970
29 meter
Z = -16274170
66 Z = -4960367
22
XDOT = -22987
349728 XDOT = -7006
544197
YDOT = -1225
932486 feet/sec YDOT = -373
664222 meter/sec
ZDOT = 7189
433815 ZDOT = 2191
339427
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
62653297
00016717 00000-0 10270-3 0 9023
2 25544 51
6439 6
8885 0007503 332
0649 28
0098 15
50410139 26337
Satellite: ISS
Catalog Number: 25544
Epoch time: 19239
62653297 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 6
8885 deg
Eccentricity:
0007503
Arg of perigee: 332
0649 deg
Mean anomaly: 28
0098 deg
Mean motion: 15
50410139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2633
Checksum: 314
Coasting Arc #4 (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 = -645486
45 A = 6788197
26 meter
Y = 4171618
89 meter E =
0007963
Z = 5317218
05 I = 51
65305
XDOT = -7616
301921 Wp = 353
34462
YDOT = -774
978739 meter/sec RA = 3
98085 deg
ZDOT = -308
894703 TA = 99
64700
MA = 99
55703
Ha = 227
675 n
mi
Hp = 221
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2117737
71 X = -717914
35
Y = 13686413
67 feet Y = 4163995
57 meter
Z = 17444941
10 Z = 5313906
71
XDOT = -24987
867195 XDOT = -7605
569418
YDOT = -2542
581166 feet/sec YDOT = -860
089576 meter/sec
ZDOT = -1013
434064 ZDOT = -345
865121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -34829
77 X = -10616
11
Y = 13868755
61 feet Y = 4227196
71 meter
Z = 17429432
21 Z = 5312490
94
XDOT = -24056
101863 XDOT = -7332
299848
YDOT = 1456
229650 feet/sec YDOT = 443
858797 meter/sec
ZDOT = -1181
583426 ZDOT = -360
146628
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
14219220
00016717 00000-0 10270-3 0 9037
2 25544 51
6436 4
3348 0007936 335
1736 24
9032 15
50424942 26411
Satellite: ISS
Catalog Number: 25544
Epoch time: 19240
14219220 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 4
3348 deg
Eccentricity:
0007936
Arg of perigee: 335
1736 deg
Mean anomaly: 24
9032 deg
Mean motion: 15
50424942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2641
Checksum: 282
Coasting Arc #5 (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 = 863800
21 A = 6788477
72 meter
Y = -4194395
66 meter E =
0012990
Z = -5276622
55 I = 51
62122
XDOT = 7591
039625 Wp = 63
19985
YDOT = 527
936334 meter/sec RA = 359
02067 deg
ZDOT = 830
320513 TA = 214
71145
MA = 214
79629
Ha = 227
851 n
mi
Hp = 220
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2833990
20 X = 936269
34
Y = -13761140
62 feet Y = -4184330
92 meter
Z = -17311753
76 Z = -5272250
54
XDOT = 24904
985646 XDOT = 7580
538758
YDOT = 1732
074587 feet/sec YDOT = 612
765982 meter/sec
ZDOT = 2724
148664 ZDOT = 867
168670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 487363
36 X = 148548
35
Y = -14066503
55 feet Y = -4287470
28 meter
Z = -17291421
70 Z = -5270425
33
XDOT = 23777
684488 XDOT = 7247
438232
YDOT = -2701
427139 feet/sec YDOT = -823
394992 meter/sec
ZDOT = 2891
759560 ZDOT = 881
408314
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
10905272
00016717 00000-0 10270-3 0 9044
2 25544 51
6445 359
5422 0007936 340
1471 19
9370 15
50402726 26562
Satellite: ISS
Catalog Number: 25544
Epoch time: 19241
10905272 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 359
5422 deg
Eccentricity:
0007936
Arg of perigee: 340
1471 deg
Mean anomaly: 19
9370 deg
Mean motion: 15
50402726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2656
Checksum: 300
Coasting Arc #6 (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 = -1118610
39 A = 6788801
42 meter
Y = 4245256
69 meter E =
0010318
Z = 5179254
22 I = 51
58881
XDOT = -7532
674760 Wp = 6
91210
YDOT = -305
337192 meter/sec RA = 354
05894 deg
ZDOT = -1366
323746 TA = 96
30183
MA = 96
18429
Ha = 227
962 n
mi
Hp = 220
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3669981
59 X = -1191156
37
Y = 13928007
51 feet Y = 4232342
21 meter
Z = 16992303
88 Z = 5173644
15
XDOT = -24713
499869 XDOT = -7522
063844
YDOT = -1001
762442 feet/sec YDOT = -389
513599 meter/sec
ZDOT = -4482
689456 ZDOT = -1402
888132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1031421
95 X = -314377
41
Y = 14397082
88 feet Y = 4388230
86 meter
Z = 16966340
87 Z = 5171340
70
XDOT = -23363
921479 XDOT = -7121
323267
YDOT = 3844
746038 feet/sec YDOT = 1171
878592 meter/sec
ZDOT = -4649
021030 ZDOT = -1417
021610
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
14036744
00016717 00000-0 10270-3 0 9059
2 25544 51
6440 354
4308 0008008 342
8941 17
1939 15
50432941 26727
Satellite: ISS
Catalog Number: 25544
Epoch time: 19242
14036744 = yrday
fracday
Element set: 905
Inclination: 51
6440 deg
RA of node: 354
4308 deg
Eccentricity:
0008008
Arg of perigee: 342
8941 deg
Mean anomaly: 17
1939 deg
Mean motion: 15
50432941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2672
Checksum: 300
Coasting Arc #7 (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 = 1316002
43 A = 6789422
36 meter
Y = -4342518
06 meter E =
0011570
Z = -5058280
35 I = 51
55825
XDOT = 7423
359140 Wp = 66
13834
YDOT = 81
179288 meter/sec RA = 349
09524 deg
ZDOT = 1869
594868 TA = 221
98488
MA = 222
07363
Ha = 228
081 n
mi
Hp = 220
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4317593
27 X = 1389033
82
Y = -14247106
49 feet Y = -4327393
61 meter
Z = -16595407
98 Z = -5051710
13
XDOT = 24354
852823 XDOT = 7412
818353
YDOT = 266
336248 feet/sec YDOT = 164
133716 meter/sec
ZDOT = 6133
841431 ZDOT = 1905
628550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1347430
65 X = 410696
86
Y = -14859742
00 feet Y = -4529249
36 meter
Z = -16565075
29 Z = -5049034
95
XDOT = 22746
182432 XDOT = 6933
036405
YDOT = -4928
773925 feet/sec YDOT = -1502
290292 meter/sec
ZDOT = 6297
767065 ZDOT = 1919
559401
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
10722537
00016717 00000-0 10270-3 0 9069
2 25544 51
6448 349
6387 0008016 346
1694 13
9235 15
50407129 26878
Satellite: ISS
Catalog Number: 25544
Epoch time: 19243
10722537 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 349
6387 deg
Eccentricity:
0008016
Arg of perigee: 346
1694 deg
Mean anomaly: 13
9235 deg
Mean motion: 15
50407129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2687
Checksum: 321
Coasting Arc #8 (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 = -1543735
46 A = 6790061
57 meter
Y = 4466869
07 meter E =
0012419
Z = 4875814
90 I = 51
52855
XDOT = -7280
421871 Wp = 21
07874
YDOT = 100
502026 meter/sec RA = 344
12923 deg
ZDOT = -2383
892863 TA = 92
40994
MA = 92
26775
Ha = 228
212 n
mi
Hp = 220
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5064748
89 X = -1617254
28
Y = 14655082
26 feet Y = 4449195
28 meter
Z = 15996768
05 Z = 4868137
16
XDOT = -23885
898528 XDOT = -7269
425124
YDOT = 329
731057 feet/sec YDOT = 19
148504 meter/sec
ZDOT = -7821
170811 ZDOT = -2419
231316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1723196
33 X = -525230
24
Y = 15446171
91 feet Y = 4707993
20 meter
Z = 15961393
21 Z = 4865032
65
XDOT = -22014
133884 XDOT = -6709
908008
YDOT = 5837
239263 feet/sec YDOT = 1779
190527 meter/sec
ZDOT = -7981
935893 ZDOT = -2432
894060
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
13853533
00016717 00000-0 10270-3 0 9075
2 25544 51
6451 344
5268 0008157 349
7194 10
3789 15
50447088 27036
Satellite: ISS
Catalog Number: 25544
Epoch time: 19244
13853533 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 344
5268 deg
Eccentricity:
0008157
Arg of perigee: 349
7194 deg
Mean anomaly: 10
3789 deg
Mean motion: 15
50447088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2703
Checksum: 325
Coasting Arc #9 (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 = 1696923
52 A = 6790974
56 meter
Y = -4627180
26 meter E =
0010098
Z = -4677530
76 I = 51
49858
XDOT = 7099
712049 Wp = 62
60527
YDOT = -272
620823 meter/sec RA = 339
16184 deg
ZDOT = 2854
627526 TA = 235
79634
MA = 235
89208
Ha = 228
367 n
mi
Hp = 220
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5567334
37 X = 1771260
58
Y = -15181037
59 feet Y = -4607788
81 meter
Z = -15346229
54 Z = -4669106
86
XDOT = 23293
018533 XDOT = 7088
366796
YDOT = -894
425272 feet/sec YDOT = -193
290037 meter/sec
ZDOT = 9365
575873 ZDOT = 2889
087526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1812761
35 X = 552529
66
Y = -16104709
42 feet Y = -4908715
43 meter
Z = -15307452
64 Z = -4665711
57
XDOT = 21142
088183 XDOT = 6444
108478
YDOT = -6642
116364 feet/sec YDOT = -2024
517068 meter/sec
ZDOT = 9522
346304 ZDOT = 2902
411153
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
10538900
00016717 00000-0 10270-3 0 9082
2 25544 51
6442 339
7344 0008149 353
7947 6
3101 15
50411224 27181
Satellite: ISS
Catalog Number: 25544
Epoch time: 19245
10538900 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 339
7344 deg
Eccentricity:
0008149
Arg of perigee: 353
7947 deg
Mean anomaly: 6
3101 deg
Mean motion: 15
50411224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2718
Checksum: 297
Coasting Arc #10 (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 = -1872595
74 A = 6791869
79 meter
Y = 4809732
20 meter E =
0014152
Z = 4414066
70 I = 51
47058
XDOT = -6889
546570 Wp = 36
09371
YDOT = 387
607300 meter/sec RA = 334
19286 deg
ZDOT = -3328
461057 TA = 87
72303
MA = 87
56100
Ha = 228
461 n
mi
Hp = 219
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6143686
82 X = -1947681
43
Y = 15779961
28 feet Y = 4788371
99 meter
Z = 14481846
14 Z = 4404787
64
XDOT = -22603
499244 XDOT = -6877
201074
YDOT = 1271
677495 feet/sec YDOT = 310
632329 meter/sec
ZDOT = -10920
147824 ZDOT = -3361
897872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1930984
40 X = -588564
04
Y = 16859941
84 feet Y = 5138910
27 meter
Z = 14439168
74 Z = 4401058
63
XDOT = -20197
850399 XDOT = -6156
304802
YDOT = 7216
185292 feet/sec YDOT = 2199
493277 meter/sec
ZDOT = -11072
261837 ZDOT = -3374
825408
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
13669632
00016717 00000-0 10270-3 0 9094
2 25544 51
6437 334
6226 0008245 357
0824 3
0278 15
50450453 27340
Satellite: ISS
Catalog Number: 25544
Epoch time: 19246
13669632 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 334
6226 deg
Eccentricity:
0008245
Arg of perigee: 357
0824 deg
Mean anomaly: 3
0278 deg
Mean motion: 15
50450453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2734
Checksum: 308
Coasting Arc #11 (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 = 1961349
68 A = 6792937
53 meter
Y = -5013395
58 meter E =
0009142
Z = -4144942
03 I = 51
44415
XDOT = 6659
524061 Wp = 50
79851
YDOT = -486
626310 meter/sec RA = 329
22193 deg
ZDOT = 3751
037191 TA = 257
92837
MA = 258
03082
Ha = 228
568 n
mi
Hp = 219
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6434874
29 X = 2037398
98
Y = -16448148
22 feet Y = -4991037
38 meter
Z = -13598891
18 Z = -4135229
55
XDOT = 21848
832221 XDOT = 6646
250246
YDOT = -1596
543012 feet/sec YDOT = -412
228840 meter/sec
ZDOT = 12306
552465 ZDOT = 3783
354457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1730328
33 X = 527404
07
Y = -17611583
34 feet Y = -5368010
60 meter
Z = -13554229
03 Z = -4131329
01
XDOT = 19194
192486 XDOT = 5850
389870
YDOT = -7670
265987 feet/sec YDOT = -2337
897073 meter/sec
ZDOT = 12453
573434 ZDOT = 3795
849183
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
10354693
00016717 00000-0 10270-3 0 9102
2 25544 51
6435 329
8296 0008191
1567 359
9585 15
50416094 27494
Satellite: ISS
Catalog Number: 25544
Epoch time: 19247
10354693 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 329
8296 deg
Eccentricity:
0008191
Arg of perigee:
1567 deg
Mean anomaly: 359
9585 deg
Mean motion: 15
50416094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2749
Checksum: 330
Coasting Arc #12 (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 = -2068792
54 A = 6793969
13 meter
Y = 5231488
35 meter E =
0015426
Z = 3807111
12 I = 51
42008
XDOT = -6406
899752 Wp = 50
37849
YDOT = 515
135951 meter/sec RA = 324
24932 deg
ZDOT = -4168
430604 TA = 83
81903
MA = 83
64331
Ha = 228
694 n
mi
Hp = 219
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6787377
09 X = -2145631
63
Y = 17163675
70 feet Y = 5207924
16 meter
Z = 12490522
04 Z = 3796874
88
XDOT = -21020
012309 XDOT = -6391
936048
YDOT = 1690
078578 feet/sec YDOT = 443
573001 meter/sec
ZDOT = -13675
953424 ZDOT = -4199
516606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1547687
63 X = -471735
19
Y = 18423850
79 feet Y = 5615589
72 meter
Z = 12443463
23 Z = 3792767
59
XDOT = -18173
470699 XDOT = -5539
273869
YDOT = 7852
212334 feet/sec YDOT = 2393
354319 meter/sec
ZDOT = -13817
369671 ZDOT = -4211
534276
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
13484957
00016717 00000-0 10270-3 0 9114
2 25544 51
6438 324
7166 0008393 3
8381 356
2833 15
50452760 27659
Satellite: ISS
Catalog Number: 25544
Epoch time: 19248
13484957 = yrday
fracday
Element set: 911
Inclination: 51
6438 deg
RA of node: 324
7166 deg
Eccentricity:
0008393
Arg of perigee: 3
8381 deg
Mean anomaly: 356
2833 deg
Mean motion: 15
50452760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 327
Coasting Arc #13 (Orbit 2779)
---------------------------------------
Vector Time (GMT): 2019/249/02:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 933315
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2082080
13 A = 6795086
94 meter
Y = -5453561
73 meter E =
0010055
Z = -3475154
60 I = 51
39527
XDOT = 6155
505030 Wp = 36
65625
YDOT = -526
976337 meter/sec RA = 319
27588 deg
ZDOT = 4529
651112 TA = 282
45603
MA = 282
56852
Ha = 228
801 n
mi
Hp = 219
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6830971
54 X = 2159789
03
Y = -17892262
88 feet Y = -5429844
02 meter
Z = -11401425
85 Z = -3464851
78
XDOT = 20195
226476 XDOT = 6138
937840
YDOT = -1728
924989 feet/sec YDOT = -458
233669 meter/sec
ZDOT = 14861
060079 ZDOT = 4559
511984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1039886
31 X = 316957
35
Y = -19151812
80 feet Y = -5837472
54 meter
Z = -11354050
26 Z = -3460714
52
XDOT = 17180
397360 XDOT = 5236
585115
YDOT = -7929
276890 feet/sec YDOT = -2416
843596 meter/sec
ZDOT = 14996
900628 ZDOT = 4571
055311
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 19249
10169668
00016717 00000-0 10270-3 0 9122
2 25544 51
6420 319
9235 0008266 7
6118 352
5156 15
50414462 27803
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
10169668 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 319
9235 deg
Eccentricity:
0008266
Arg of perigee: 7
6118 deg
Mean anomaly: 352
5156 deg
Mean motion: 15
50414462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2780
Checksum: 309
Coasting Arc #14 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2019/249/18:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 918206
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4819167
62 A = 6790479
26 meter
Y = 610621
41 meter E =
0009321
Z = 4735770
09 I = 51
36147
XDOT = -3439
798488 Wp = 61
15015
YDOT = 6304
984530 meter/sec RA = 316
02234 deg
ZDOT = 2687
811840 TA = 2
19075
MA = 2
18667
Ha = 228
672 n
mi
Hp = 219
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15810917
40 X = 4788977
64
Y = 2003351
09 feet Y = 664344
03 meter
Z = 15537303
43 Z = 4759106
39
XDOT = -11285
428110 XDOT = -3523
102851
YDOT = 20685
644783 feet/sec YDOT = 6266
052546 meter/sec
ZDOT = 8818
280315 ZDOT = 2670
900191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5380871
97 X = -1640089
78
Y = 14890860
09 feet Y = 4538734
16 meter
Z = 15643363
61 Z = 4768097
23
XDOT = -16628
735038 XDOT = -5068
438439
YDOT = -15190
009642 feet/sec YDOT = -4629
914939 meter/sec
ZDOT = 8740
776727 ZDOT = 2664
188746
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 19249
81071738
00016717 00000-0 10270-3 0 9131
2 25544 51
6397 316
4087 0008159 10
9762 349
1566 15
50430147 27913
Satellite: ISS
Catalog Number: 25544
Epoch time: 19249
81071738 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 316
4087 deg
Eccentricity:
0008159
Arg of perigee: 10
9762 deg
Mean anomaly: 349
1566 deg
Mean motion: 15
50430147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 328
Coasting Arc #15 (Orbit 2804)
---------------------------------------
Vector Time (GMT): 2019/250/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 918206
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5440919
32 A = 6794214
32 meter
Y = 1664240
80 meter E =
0012122
Z = -3728241
62 I = 51
35239
XDOT = 996
863020 Wp = 40
78369
YDOT = -6278
272608 meter/sec RA = 311
39314 deg
ZDOT = -4256
226226 TA = 183
78458
MA = 183
79376
Ha = 228
988 n
mi
Hp = 219
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17850785
17 X = -5441015
34
Y = 5460107
60 feet Y = 1603396
00 meter
Z = -12231763
84 Z = -3754671
67
XDOT = 3270
547966 XDOT = 1087
668649
YDOT = -20598
007245 feet/sec YDOT = -6266
617327 meter/sec
ZDOT = -13963
996804 ZDOT = -4251
163216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6157960
88 X = 1876946
48
Y = -17538083
89 feet Y = -5345607
97 meter
Z = -12352104
42 Z = -3764921
43
XDOT = 13297
311760 XDOT = 4053
020625
YDOT = 14489
741556 feet/sec YDOT = 4416
473226 meter/sec
ZDOT = -13940
385999 ZDOT = -4249
029653
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 19250
71310607
00016717 00000-0 10270-3 0 9144
2 25544 51
6401 311
9352 0008177 15
8798 344
2607 15
50402806 28056
Satellite: ISS
Catalog Number: 25544
Epoch time: 19250
71310607 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 311
9352 deg
Eccentricity:
0008177
Arg of perigee: 15
8798 deg
Mean anomaly: 344
2607 deg
Mean motion: 15
50402806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2805
Checksum: 294
Coasting Arc #16 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2019/251/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 918206
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5205541
96 A = 6793042
56 meter
Y = -1605758
85 meter E =
0014014
Z = 4042979
06 I = 51
32780
XDOT = -986
587553 Wp = 66
75348
YDOT = 6550
596481 meter/sec RA = 306
41573 deg
ZDOT = 3866
732047 TA = 343
00586
MA = 343
05275
Ha = 228
848 n
mi
Hp = 218
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17078549
72 X = 5203472
76
Y = -5268237
69 feet Y = -1547558
30 meter
Z = 13264366
99 Z = 4068260
41
XDOT = -3236
835805 XDOT = -1078
547158
YDOT = 21491
458271 feet/sec YDOT = 6539
049664 meter/sec
ZDOT = 12686
128764 ZDOT = 3861
716134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5559913
98 X = -1694661
78
Y = 16895314
57 feet Y = 5149691
88 meter
Z = 13379473
94 Z = 4078063
66
XDOT = -14351
369330 XDOT = -4374
297372
YDOT = -14763
976314 feet/sec YDOT = -4500
059980 meter/sec
ZDOT = 12662
720660 ZDOT = 3859
597257
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 19251
74440357
00016717 00000-0 10270-3 0 9155
2 25544 51
6403 306
8235 0008198 18
3727 341
7718 15
50437515 28212
Satellite: ISS
Catalog Number: 25544
Epoch time: 19251
74440357 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 306
8235 deg
Eccentricity:
0008198
Arg of perigee: 18
3727 deg
Mean anomaly: 341
7718 deg
Mean motion: 15
50437515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 311
Coasting Arc #17 (Orbit 2835)
---------------------------------------
Vector Time (GMT): 2019/252/16:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 918206
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5007143
24 A = 6792086
67 meter
Y = 1510491
38 meter E =
0015751
Z = -4350080
08 I = 51
30471
XDOT = 930
454355 Wp = 46
47692
YDOT = -6777
257715 meter/sec RA = 301
43506 deg
ZDOT = -3421
481343 TA = 188
54020
MA = 188
56704
Ha = 229
193 n
mi
Hp = 218
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16427635
32 X = -5002531
82
Y = 4955680
37 feet Y = 1454523
62 meter
Z = -14271916
26 Z = -4374391
47
XDOT = 3052
671770 XDOT = 1022
789924
YDOT = -22235
097490 feet/sec YDOT = -6766
336544 meter/sec
ZDOT = -11225
332489 ZDOT = -3416
737124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5154135
67 X = 1570980
55
Y = -16269274
53 feet Y = -4958874
88 meter
Z = -14382599
05 Z = -4383816
19
XDOT = 15378
510884 XDOT = 4687
370118
YDOT = 14783
980746 feet/sec YDOT = 4506
157331 meter/sec
ZDOT = -11203
155977 ZDOT = -3414
721942
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 19252
71124600
00016717 00000-0 10270-3 0 9164
2 25544 51
6396 302
0304 0008346 22
6810 337
4708 15
50407050 28362
Satellite: ISS
Catalog Number: 25544
Epoch time: 19252
71124600 = yrday
fracday
Element set: 916
Inclination: 51
6396 deg
RA of node: 302
0304 deg
Eccentricity:
0008346
Arg of perigee: 22
6810 deg
Mean anomaly: 337
4708 deg
Mean motion: 15
50407050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2836
Checksum: 280
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