[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 16th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14537 7374 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
108/01:53:30
000 0
0 0
0 0
0
N/A 0
0 0
0 230
6
000/00:00:00
000 0
0 0
0 222
1
110/05:09:31
740 1
2 -3
1 3
1
N/A -2
9 0
3 228
6
000/00:01:03
479 0
4 -0
1 222
2
113/03:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 222
3
Coasting Arc #1 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2020/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936071
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4379110
22 A = 6793807
30 meter
Y = -598941
37 meter E =
0016895
Z = -5174360
49 I = 51
27918
XDOT = 2547
100315 Wp = 87
44296
YDOT = -7084
978226 meter/sec RA = 297
96913 deg
ZDOT = -1338
606148 TA = 169
60901
MA = 169
57405
Ha = 230
788 n
mi
Hp = 221
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14367159
51 X = -4346953
22
Y = -1965030
75 feet Y = -647731
91 meter
Z = -16976248
31 Z = -5195554
31
XDOT = 8356
628329 XDOT = 2632
639491
YDOT = -23244
679220 feet/sec YDOT = -7056
016462 meter/sec
ZDOT = -4391
752455 ZDOT = -1326
025604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13873051
57 X = -4228506
12
Y = 3808979
55 feet Y = 1160976
97 meter
Z = -17073363
46 Z = -5203961
18
XDOT = -1174
267964 XDOT = -357
916875
YDOT = -23657
107911 feet/sec YDOT = -7210
686491 meter/sec
ZDOT = -4333
635716 ZDOT = -1320
892166
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 20106
51844558
00016717 00000-0 10270-3 0 9006
2 25544 51
6398 298
6202 0003627 118
9770 241
1744 15
48693753 22293
Satellite: ISS
Catalog Number: 25544
Epoch time: 20106
51844558 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 298
6202 deg
Eccentricity:
0003627
Arg of perigee: 118
9770 deg
Mean anomaly: 241
1744 deg
Mean motion: 15
48693753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 323
Coasting Arc #2 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2020/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936071
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4437671
76 A = 6794015
74 meter
Y = 95300
26 meter E =
0008191
Z = 5138614
79 I = 51
26418
XDOT = -1838
121766 Wp = 123
29364
YDOT = 7298
298738 meter/sec RA = 293
00177 deg
ZDOT = 1445
940259 TA = 312
67478
MA = 312
74376
Ha = 230
696 n
mi
Hp = 222
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14559290
56 X = 4411315
93
Y = 312664
89 feet Y = 144778
18 meter
Z = 16858972
42 Z = 5160107
16
XDOT = -6030
583223 XDOT = -1926
620410
YDOT = 23944
549664 feet/sec YDOT = 7277
248749 meter/sec
ZDOT = 4743
898487 ZDOT = 1436
796356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13304303
93 X = 4055151
84
Y = -5633361
52 feet Y = -1717048
59 meter
Z = 16957487
64 Z = 5168642
23
XDOT = 3871
694033 XDOT = 1180
092341
YDOT = 23356
153859 feet/sec YDOT = 7118
955696 meter/sec
ZDOT = 4701
541080 ZDOT = 1433
029721
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 20107
55089336
00016717 00000-0 10270-3 0 9017
2 25544 51
6392 293
5156 0003645 121
9378 238
2127 15
48653847 22457
Satellite: ISS
Catalog Number: 25544
Epoch time: 20107
55089336 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 293
5156 deg
Eccentricity:
0003645
Arg of perigee: 121
9378 deg
Mean anomaly: 238
2127 deg
Mean motion: 15
48653847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 318
Coasting Arc #3 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2020/108/01:53:30
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4602676
11 A = 6795243
22 meter
Y = -1348230
84 meter E =
0010723
Z = 4808037
25 I = 51
26167
XDOT = -509
411239 Wp = 120
95656
YDOT = 7224
957873 meter/sec RA = 290
13552 deg
ZDOT = 2504
026809 TA = 304
22760
MA = 304
32915
Ha = 230
579 n
mi
Hp = 222
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15100643
42 X = 4594055
75
Y = -4423329
53 feet Y = -1296808
52 meter
Z = 15774400
42 Z = 4830374
25
XDOT = -1671
296716 XDOT = -602
328077
YDOT = 23703
930031 feet/sec YDOT = 7218
741806 meter/sec
ZDOT = 8215
311052 ZDOT = 2501
326442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5455843
91 X = -1662941
22
Y = 14648743
27 feet Y = 4464936
95 meter
Z = 15876872
24 Z = 4839270
66
XDOT = -16861
212916 XDOT = -5139
297697
YDOT = -15203
941633 feet/sec YDOT = -4634
161410 meter/sec
ZDOT = 8202
506546 ZDOT = 2500
123995
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 20108
13164308
00016717 00000-0 10270-3 0 9026
2 25544 51
6393 290
6467 0003574 124
2541 235
8948 15
48711140 22545
Satellite: ISS
Catalog Number: 25544
Epoch time: 20108
13164308 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 290
6467 deg
Eccentricity:
0003574
Arg of perigee: 124
2541 deg
Mean anomaly: 235
8948 deg
Mean motion: 15
48711140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 295
Coasting Arc #4 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2020/109/01:53:30
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4475969
86 A = 6795455
86 meter
Y = 1836572
98 meter E =
0013777
Z = -4784428
65 I = 51
25196
XDOT = -197
214895 Wp = 84
07876
YDOT = -7196
767941 meter/sec RA = 285
16525 deg
ZDOT = -2583
145985 TA = 160
28838
MA = 160
23508
Ha = 230
727 n
mi
Hp = 221
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14684940
50 X = -4472934
34
Y = 6025501
89 feet Y = 1786536
29 meter
Z = -15696944
40 Z = -4806163
81
XDOT = -647
030497 XDOT = -104
176431
YDOT = -23611
443377 feet/sec YDOT = -7198
453225 meter/sec
ZDOT = -8474
888401 ZDOT = -2583
877733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3661534
33 X = 1116035
66
Y = -15342955
34 feet Y = -4676532
79 meter
Z = -15796680
08 Z = -4814828
09
XDOT = 18358
940464 XDOT = 5595
805053
YDOT = 13092
844078 feet/sec YDOT = 3990
698875 meter/sec
ZDOT = -8477
837755 ZDOT = -2584
044948
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 20109
09956131
00016717 00000-0 10270-3 0 9036
2 25544 51
6395 285
8601 0003632 126
7909 233
3574 15
48686892 22692
Satellite: ISS
Catalog Number: 25544
Epoch time: 20109
09956131 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 285
8601 deg
Eccentricity:
0003632
Arg of perigee: 126
7909 deg
Mean anomaly: 233
3574 deg
Mean motion: 15
48686892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 332
Coasting Arc #5 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2020/110/01:53:30
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4277539
43 A = 6795501
77 meter
Y = -2337022
09 meter E =
0011042
Z = 4729379
71 I = 51
24584
XDOT = 909
451423 Wp = 122
11320
YDOT = 7119
458543 meter/sec RA = 280
19608 deg
ZDOT = 2685
120158 TA = 301
13284
MA = 301
24111
Ha = 230
454 n
mi
Hp = 222
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14033922
01 X = 4280382
15
Y = -7667395
32 feet Y = -2289171
49 meter
Z = 15516337
62 Z = 4750165
34
XDOT = 2983
764512 XDOT = 816
729150
YDOT = 23357
803619 feet/sec YDOT = 7129
110356 meter/sec
ZDOT = 8809
449336 ZDOT = 2689
312390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1678628
55 X = -511645
98
Y = 15809882
36 feet Y = 4818852
14 meter
Z = 15611741
64 Z = 4758458
85
XDOT = -19679
095055 XDOT = -5998
188173
YDOT = -10840
560546 feet/sec YDOT = -3304
202854 meter/sec
ZDOT = 8828
284097 ZDOT = 2690
860993
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 20110
13200269
00016717 00000-0 10270-3 0 9048
2 25544 51
6404 280
7560 0003475 132
2086 227
9359 15
48735252 22857
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
13200269 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 280
7560 deg
Eccentricity:
0003475
Arg of perigee: 132
2086 deg
Mean anomaly: 227
9359 deg
Mean motion: 15
48735252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 289
Coasting Arc #6 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2020/110/05:10:03
479
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3764573
17 A = 6792205
24 meter
Y = 2396815
10 meter E =
0004295
Z = 5116961
05 I = 51
24138
XDOT = -2434
776021 Wp = 74
04656
YDOT = 7102
727063 meter/sec RA = 279
48451 deg
ZDOT = -1533
445274 TA = 30
83481
MA = 30
80959
Ha = 228
598 n
mi
Hp = 222
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12350961
83 X = 3712636
18
Y = 7863566
61 feet Y = 2438623
08 meter
Z = 16787929
95 Z = 5135121
64
XDOT = -7988
110305 XDOT = -2506
571251
YDOT = 23302
910313 feet/sec YDOT = 7075
098161 meter/sec
ZDOT = -5030
988431 ZDOT = -1545
447182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4578280
60 X = -1395459
93
Y = 13806651
26 feet Y = 4208267
30 meter
Z = 16871047
91 Z = 5142295
40
XDOT = -23541
207630 XDOT = -7175
360086
YDOT = -1582
020109 feet/sec YDOT = -482
199729 meter/sec
ZDOT = -5086
381958 ZDOT = -1550
329221
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 20110
26103657
00016717 00000-0 10270-3 0 9056
2 25544 51
6422 280
1180 0001599 173
4350 186
6822 15
49310967 22876
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
26103657 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 280
1180 deg
Eccentricity:
0001599
Arg of perigee: 173
4350 deg
Mean anomaly: 186
6822 deg
Mean motion: 15
49310967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 296
Coasting Arc #7 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2020/111/05:10:03
479
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3933309
84 A = 6792404
70 meter
Y = -2191930
83 meter E =
0014018
Z = -5098095
67 I = 51
23796
XDOT = 1894
496916 Wp = 108
61980
YDOT = -7226
663138 meter/sec RA = 274
50775 deg
ZDOT = 1644
805663 TA = 177
39031
MA = 177
38299
Ha = 228
783 n
mi
Hp = 222
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12904559
86 X = -3883742
94
Y = -7191374
13 feet Y = -2235639
00 meter
Z = -16726035
65 Z = -5117081
75
XDOT = 6215
541064 XDOT = 1967
177235
YDOT = -23709
524730 feet/sec YDOT = -7205
071065 meter/sec
ZDOT = 5396
344039 ZDOT = 1654
185302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3545122
85 X = 1080553
45
Y = -14239399
95 feet Y = -4340169
10 meter
Z = -16812953
01 Z = -5124588
08
XDOT = 23460
593197 XDOT = 7150
788807
YDOT = -584
479479 feet/sec YDOT = -178
149345 meter/sec
ZDOT = 5439
706157 ZDOT = 1658
022437
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 20111
22858777
00016717 00000-0 10270-3 0 9064
2 25544 51
6427 275
3293 0001594 173
0358 187
0815 15
49286232 23023
Satellite: ISS
Catalog Number: 25544
Epoch time: 20111
22858777 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 275
3293 deg
Eccentricity:
0001594
Arg of perigee: 173
0358 deg
Mean anomaly: 187
0815 deg
Mean motion: 15
49286232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 311
Coasting Arc #8 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2020/112/05:10:03
479
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4077797
08 A = 6792417
96 meter
Y = 1972129
77 meter E =
0004590
Z = 5058151
71 I = 51
23652
XDOT = -1356
009710 Wp = 71
30250
YDOT = 7333
412774 meter/sec RA = 269
53202 deg
ZDOT = -1763
276183 TA = 35
87581
MA = 35
84499
Ha = 228
486 n
mi
Hp = 222
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13378599
35 X = 4030871
24
Y = 6470242
03 feet Y = 2017468
44 meter
Z = 16594985
91 Z = 5077846
17
XDOT = -4448
850755 XDOT = -1429
348257
YDOT = 24059
753196 feet/sec YDOT = 7317
838772 meter/sec
ZDOT = -5785
026847 ZDOT = -1770
041642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2473974
81 X = -754067
52
Y = 14550917
67 feet Y = 4435119
70 meter
Z = 16685165
68 Z = 5085638
50
XDOT = -23266
485718 XDOT = -7091
624847
YDOT = 2724
049288 feet/sec YDOT = 830
290223 meter/sec
ZDOT = -5816
395404 ZDOT = -1772
837319
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 20112
26064033
00016717 00000-0 10270-3 0 9074
2 25544 51
6423 270
2226 0001565 182
0074 178
1070 15
49322128 23188
Satellite: ISS
Catalog Number: 25544
Epoch time: 20112
26064033 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 270
2226 deg
Eccentricity:
0001565
Arg of perigee: 182
0074 deg
Mean anomaly: 178
1070 deg
Mean motion: 15
49322128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2318
Checksum: 266
Coasting Arc #9 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2020/113/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1069644
83 A = 6801699
97 meter
Y = 6400948
04 meter E =
0007835
Z = -2026115
06 I = 51
26818
XDOT = -4667
982923 Wp = 147
55273
YDOT = -2522
970056 meter/sec RA = 264
98524 deg
ZDOT = -5522
726894 TA = 54
90698
MA = 54
83354
Ha = 228
654 n
mi
Hp = 222
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3509333
43 X = -1131300
80
Y = 21000485
68 feet Y = 6388641
70 meter
Z = -6647359
12 Z = -2031461
00
XDOT = -15314
904603 XDOT = -4612
596805
YDOT = -8277
460814 feet/sec YDOT = -2574
861259 meter/sec
ZDOT = -18119
182724 ZDOT = -5545
267805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19887512
40 X = -6061713
78
Y = -7582366
17 feet Y = -2311105
21 meter
Z = -6672164
34 Z = -2033675
69
XDOT = 10588
717722 XDOT = 3227
441162
YDOT = -11785
187699 feet/sec YDOT = -3592
125211 meter/sec
ZDOT = -18222
388462 ZDOT = -5554
184003
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 20113
16368750
00016717 00000-0 10270-3 0 9088
2 25544 51
6421 265
7525 0001569 183
8904 176
2234 15
49284659 23325
Satellite: ISS
Catalog Number: 25544
Epoch time: 20113
16368750 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 265
7525 deg
Eccentricity:
0001569
Arg of perigee: 183
8904 deg
Mean anomaly: 176
2234 deg
Mean motion: 15
49284659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 317
Coasting Arc #10 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2020/114/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 583465
46 A = 6801577
38 meter
Y = -6434331
21 meter E =
0013284
Z = 2108322
24 I = 51
27202
XDOT = 4859
113238 Wp = 75
64415
YDOT = 2245
247238 meter/sec RA = 260
01043 deg
ZDOT = 5481
572902 TA = 307
78813
MA = 307
90836
Ha = 228
643 n
mi
Hp = 222
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1914256
74 X = 645131
50
Y = -21110010
53 feet Y = -6427461
65 meter
Z = 6917067
71 Z = 2111306
42
XDOT = 15941
972565 XDOT = 4807
018317
YDOT = 7366
296713 feet/sec YDOT = 2299
294115 meter/sec
ZDOT = 17984
163065 ZDOT = 5505
050370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20414152
73 X = 6222233
75
Y = 5689097
56 feet Y = 1734036
94 meter
Z = 6931037
90 Z = 2112580
35
XDOT = -9716
228879 XDOT = -2961
506562
YDOT = 12720
216503 feet/sec YDOT = 3877
121990 meter/sec
ZDOT = 18091
681270 ZDOT = 5514
344451
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 20114
19573795
00016717 00000-0 10270-3 0 9090
2 25544 51
6423 260
6451 0001486 186
3020 173
8111 15
49281700 23482
Satellite: ISS
Catalog Number: 25544
Epoch time: 20114
19573795 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 260
6451 deg
Eccentricity:
0001486
Arg of perigee: 186
3020 deg
Mean anomaly: 173
8111 deg
Mean motion: 15
49281700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 296
Coasting Arc #11 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2020/115/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -129367
61 A = 6801361
95 meter
Y = 6423303
54 meter E =
0007042
Z = -2224520
30 I = 51
27932
XDOT = -5030
732610 Wp = 146
70960
YDOT = -1975
523488 meter/sec RA = 255
03656 deg
ZDOT = -5425
747325 TA = 58
08500
MA = 58
01652
Ha = 228
595 n
mi
Hp = 222
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -424434
43 X = -190379
64
Y = 21073830
52 feet Y = 6421515
72 meter
Z = -7298294
94 Z = -2225296
91
XDOT = -16505
028248 XDOT = -4981
912187
YDOT = -6481
376273 feet/sec YDOT = -2031
507742 meter/sec
ZDOT = -17801
008285 ZDOT = -5450
066508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20720423
08 X = -6315584
95
Y = -3859335
29 feet Y = -1176325
40 meter
Z = -7302135
66 Z = -2225690
95
XDOT = 8824
482061 XDOT = 2689
702132
YDOT = -13573
082902 feet/sec YDOT = -4137
075668 meter/sec
ZDOT = -17912
404802 ZDOT = -5459
700984
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 20115
16328337
00016717 00000-0 10270-3 0 9100
2 25544 51
6433 255
8573 0001483 190
6935 169
4183 15
49282417 23637
Satellite: ISS
Catalog Number: 25544
Epoch time: 20115
16328337 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 255
8573 deg
Eccentricity:
0001483
Arg of perigee: 190
6935 deg
Mean anomaly: 169
4183 deg
Mean motion: 15
49282417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 311
Coasting Arc #12 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2020/116/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -348938
44 A = 6801223
12 meter
Y = -6382907
80 meter E =
0013110
Z = 2306262
35 I = 51
28815
XDOT = 5192
799106 Wp = 77
91318
YDOT = 1668
705895 meter/sec RA = 250
06312 deg
ZDOT = 5380
705210 TA = 307
86704
MA = 307
98557
Ha = 228
573 n
mi
Hp = 222
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1144811
15 X = -288739
64
Y = -20941298
56 feet Y = -6386473
33 meter
Z = 7566477
51 Z = 2304713
39
XDOT = 17036
742475 XDOT = 5147
616343
YDOT = 5474
756873 feet/sec YDOT = 1726
522721 meter/sec
ZDOT = 17653
232317 ZDOT = 5405
820545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20886135
10 X = 6366093
98
Y = 1929058
90 feet Y = 587977
15 meter
Z = 7559646
30 Z = 2304180
19
XDOT = -7788
145163 XDOT = -2373
826646
YDOT = 14391
780102 feet/sec YDOT = 4386
614575 meter/sec
ZDOT = 17768
301543 ZDOT = 5415
778310
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 20116
19533235
00016717 00000-0 10270-3 0 9110
2 25544 51
6428 250
7504 0001413 194
3017 165
8093 15
49280849 23798
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
19533235 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 250
7504 deg
Eccentricity:
0001413
Arg of perigee: 194
3017 deg
Mean anomaly: 165
8093 deg
Mean motion: 15
49280849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 302
Coasting Arc #13 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2020/117/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 789421
24 A = 6801013
78 meter
Y = 6304161
40 meter E =
0006232
Z = -2420593
20 I = 51
30101
XDOT = -5335
349087 Wp = 147
17673
YDOT = -1370
146753 meter/sec RA = 245
09098 deg
ZDOT = -5319
996544 TA = 59
96464
MA = 59
90282
Ha = 228
479 n
mi
Hp = 222
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2589964
69 X = 730625
62
Y = 20682944
21 feet Y = 6312660
62 meter
Z = -7941578
73 Z = -2416900
98
XDOT = -17504
426139 XDOT = -5293
789227
YDOT = -4495
232128 feet/sec YDOT = -1429
577826 meter/sec
ZDOT = -17454
056902 ZDOT = -5345
813136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20850575
85 X = -6355255
52
Y = -100422
64 feet Y = -30608
82 meter
Z = -7924908
39 Z = -2415512
08
XDOT = 6737
258277 XDOT = 2053
516323
YDOT = -15122
230395 feet/sec YDOT = -4609
255824 meter/sec
ZDOT = -17572
365487 ZDOT = -5356
057000
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 20117
16287577
00016717 00000-0 10270-3 0 9124
2 25544 51
6438 245
9631 0001598 204
4781 155
6294 15
49274614 23941
Satellite: ISS
Catalog Number: 25544
Epoch time: 20117
16287577 = yrday
fracday
Element set: 912
Inclination: 51
6438 deg
RA of node: 245
9631 deg
Eccentricity:
0001598
Arg of perigee: 204
4781 deg
Mean anomaly: 155
6294 deg
Mean motion: 15
49274614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 329
Coasting Arc #14 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2020/118/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1246935
19 A = 6800811
72 meter
Y = -6193253
05 meter E =
0012827
Z = 2503260
89 I = 51
31585
XDOT = 5463
576631 Wp = 79
92459
YDOT = 1038
596038 meter/sec RA = 240
11859 deg
ZDOT = 5270
164973 TA = 308
23383
MA = 308
34922
Ha = 228
458 n
mi
Hp = 222
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4090994
71 X = -1189747
31
Y = -20319071
68 feet Y = -6206877
55 meter
Z = 8212798
20 Z = 2497342
22
XDOT = 17925
120182 XDOT = 5425
956865
YDOT = 3407
467317 feet/sec YDOT = 1099
482989 meter/sec
ZDOT = 17290
567496 ZDOT = 5296
613959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20659805
27 X = 6297108
65
Y = -1792873
44 feet Y = -546467
82 meter
Z = 8185903
54 Z = 2495063
40
XDOT = -5555
726125 XDOT = -1693
385323
YDOT = 15793
264122 feet/sec YDOT = 4813
786904 meter/sec
ZDOT = 17411
803122 ZDOT = 5307
117591
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 20118
19492016
00016717 00000-0 10270-3 0 9135
2 25544 51
6440 240
8554 0001330 207
0841 153
0240 15
49289415 24109
Satellite: ISS
Catalog Number: 25544
Epoch time: 20118
19492016 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 240
8554 deg
Eccentricity:
0001330
Arg of perigee: 207
0841 deg
Mean anomaly: 153
0240 deg
Mean motion: 15
49289415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 268
Coasting Arc #15 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2020/119/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1662234
20 A = 6800607
38 meter
Y = 6051283
41 meter E =
0005405
Z = -2616640
27 I = 51
33234
XDOT = -5572
196294 Wp = 143
59176
YDOT = -715
215077 meter/sec RA = 235
14875 deg
ZDOT = -5203
601190 TA = 65
93982
MA = 65
88328
Ha = 228
413 n
mi
Hp = 222
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5453524
29 X = 1607153
70
Y = 19853292
03 feet Y = 6069563
90 meter
Z = -8584777
78 Z = -2608699
07
XDOT = -18281
483904 XDOT = -5538
508026
YDOT = -2346
506159 feet/sec YDOT = -777
338625 meter/sec
ZDOT = -17072
182383 ZDOT = -5230
587252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20295275
86 X = -6186000
08
Y = 3551892
17 feet Y = 1082616
73 meter
Z = -8548589
40 Z = -2605610
05
XDOT = 4364
539476 XDOT = 1330
311632
YDOT = -16370
072347 feet/sec YDOT = -4989
598051 meter/sec
ZDOT = -17195
909277 ZDOT = -5241
313148
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 20119
16245983
00016717 00000-0 10270-3 0 9143
2 25544 51
6435 236
0684 0001483 212
9422 147
1636 15
49276171 24257
Satellite: ISS
Catalog Number: 25544
Epoch time: 20119
16245983 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 236
0684 deg
Eccentricity:
0001483
Arg of perigee: 212
9422 deg
Mean anomaly: 147
1636 deg
Mean motion: 15
49276171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 304
Coasting Arc #16 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2020/120/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2089376
91 A = 6800396
72 meter
Y = -5875808
23 meter E =
0012526
Z = 2698640
30 I = 51
35114
XDOT = 5662
057243 Wp = 82
10546
YDOT = 360
364509 meter/sec RA = 230
17906 deg
ZDOT = 5149
473808 TA = 308
45962
MA = 308
57195
Ha = 228
375 n
mi
Hp = 222
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6854911
14 X = -2036625
14
Y = -19277586
04 feet Y = -5898878
36 meter
Z = 8853806
77 Z = 2688618
58
XDOT = 18576
303291 XDOT = 5632
593367
YDOT = 1182
298258 feet/sec YDOT = 423
516562 meter/sec
ZDOT = 16894
599107 ZDOT = 5176
906507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19769940
02 X = 6025877
72
Y = -5345341
89 feet Y = -1629260
21 meter
Z = 8808054
07 Z = 2684694
88
XDOT = -3050
966817 XDOT = -929
934686
YDOT = 16864
863350 feet/sec YDOT = 5140
410349 meter/sec
ZDOT = 17020
404474 ZDOT = 5187
819284
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 20120
19450193
00016717 00000-0 10270-3 0 9150
2 25544 51
6427 230
9610 0001292 219
2334 140
8723 15
49289639 24418
Satellite: ISS
Catalog Number: 25544
Epoch time: 20120
19450193 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 230
9610 deg
Eccentricity:
0001292
Arg of perigee: 219
2334 deg
Mean anomaly: 140
8723 deg
Mean motion: 15
49289639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 292
Coasting Arc #17 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2020/121/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2471391
78 A = 6800154
07 meter
Y = 5676793
79 meter E =
0004567
Z = -2809912
63 I = 51
37310
XDOT = -5731
310341 Wp = 139
44247
YDOT = -14
319472 meter/sec RA = 225
21143 deg
ZDOT = -5077
836014 TA = 72
49550
MA = 72
44559
Ha = 228
286 n
mi
Hp = 222
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8108240
76 X = 2421377
50
Y = 18624651
56 feet Y = 5704151
18 meter
Z = -9218873
45 Z = -2798028
66
XDOT = -18803
511617 XDOT = -5706
058959
YDOT = -46
979896 feet/sec YDOT = -78
269558 meter/sec
ZDOT = -16659
566974 ZDOT = -5105
615231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19102665
64 X = -5822492
49
Y = 6979108
93 feet Y = 2127232
40 meter
Z = -9164553
76 Z = -2793355
99
XDOT = 1736
182297 XDOT = 529
188364
YDOT = -17256
574703 feet/sec YDOT = -5259
803970 meter/sec
ZDOT = -16786
990907 ZDOT = -5116
674828
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 20121
16203879
00016717 00000-0 10270-3 0 9166
2 25544 51
6431 226
1734 0001524 226
0091 134
0933 15
49285307 24563
Satellite: ISS
Catalog Number: 25544
Epoch time: 20121
16203879 = yrday
fracday
Element set: 916
Inclination: 51
6431 deg
RA of node: 226
1734 deg
Eccentricity:
0001524
Arg of perigee: 226
0091 deg
Mean anomaly: 134
0933 deg
Mean motion: 15
49285307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 283
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