[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 4th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19912 1579 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
336/14:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 220
9
338/17:51:57
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 220
5
339/18:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
4
340/09:34:11
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 220
3
341/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
2
342/21:54:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 220
0
343/10:38:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 219
8
346/03:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 219
4
Coasting Arc #1 (Orbit 135)
---------------------------------------
Vector Time (GMT): 2019/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3055330
02 A = 6789896
31 meter
Y = 3247907
15 meter E =
0015602
Z = -5133261
22 I = 51
26980
XDOT = -4128
381262 Wp = 51
54804
YDOT = -6264
509010 meter/sec RA = 245
84212 deg
ZDOT = -1500
040033 TA = 203
85987
MA = 203
93227
Ha = 228
423 n
mi
Hp = 220
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10024048
61 X = -3066487
40
Y = 10655863
35 feet Y = 3213678
37 meter
Z = -16841408
19 Z = -5148129
70
XDOT = -13544
557945 XDOT = -4050
736490
YDOT = -20552
851082 feet/sec YDOT = -6310
241209 meter/sec
ZDOT = -4921
391186 ZDOT = -1519
906195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6656574
64 X = -2028923
95
Y = -12939213
14 feet Y = -3943872
16 meter
Z = -16909428
78 Z = -5153993
89
XDOT = 22976
293845 XDOT = 7003
174364
YDOT = -5243
527566 feet/sec YDOT = -1598
227202 meter/sec
ZDOT = -5011
546388 ZDOT = -1527
519339
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 19336
51877323
00016717 00000-0 10270-3 0 9005
2 25544 51
6422 246
7557 0007099 350
6795 9
4222 15
50098184 1368
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
51877323 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 246
7557 deg
Eccentricity:
0007099
Arg of perigee: 350
6795 deg
Mean anomaly: 9
4222 deg
Mean motion: 15
50098184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 136
Checksum: 317
Coasting Arc #2 (Orbit 137)
---------------------------------------
Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4731127
46 A = 6791494
43 meter
Y = 1247542
64 meter E =
0011962
Z = 4709966
47 I = 51
27726
XDOT = 858
778128 Wp = 27
54887
YDOT = 7105
846460 meter/sec RA = 245
29086 deg
ZDOT = -2731
568810 TA = 89
71406
MA = 89
57699
Ha = 228
281 n
mi
Hp = 220
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15522071
72 X = 4693947
00
Y = 4092987
67 feet Y = 1300241
14 meter
Z = 15452645
90 Z = 4732858
37
XDOT = 2817
513543 XDOT = 792
523129
YDOT = 23313
144554 feet/sec YDOT = 7115
079713 meter/sec
ZDOT = -8961
839928 ZDOT = -2727
557463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 801667
45 X = 244348
24
Y = 15931426
34 feet Y = 4855898
75 meter
Z = 15556944
03 Z = 4741756
54
XDOT = -20163
332253 XDOT = -6145
783671
YDOT = 9790
464411 feet/sec YDOT = 2984
133552 meter/sec
ZDOT = -8944
035129 ZDOT = -2726
141907
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 19336
64771099
00016717 00000-0 10270-3 0 9013
2 25544 51
6425 246
1175 0007199 349
1124 10
9870 15
50128825 1385
Satellite: ISS
Catalog Number: 25544
Epoch time: 19336
64771099 = yrday
fracday
Element set: 901
Inclination: 51
6425 deg
RA of node: 246
1175 deg
Eccentricity:
0007199
Arg of perigee: 349
1124 deg
Mean anomaly: 10
9870 deg
Mean motion: 15
50128825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 138
Checksum: 312
Coasting Arc #3 (Orbit 152)
---------------------------------------
Vector Time (GMT): 2019/337/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4899233
89 A = 6792247
15 meter
Y = -1243982
88 meter E =
0009157
Z = -4542439
56 I = 51
29434
XDOT = -1097
575080 Wp = 66
65089
YDOT = -6919
935219 meter/sec RA = 240
31030 deg
ZDOT = 3087
400163 TA = 234
41944
MA = 234
50482
Ha = 228
417 n
mi
Hp = 220
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16073602
00 X = -4862894
48
Y = -4081308
66 feet Y = -1298566
04 meter
Z = -14903016
94 Z = -4566150
11
XDOT = -3600
968110 XDOT = -1035
109692
YDOT = -22703
199539 feet/sec YDOT = -6931
860047 meter/sec
ZDOT = 10129
265626 ZDOT = 3082
219732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1265042
90 X = -385585
08
Y = -16437317
24 feet Y = -5010094
29 meter
Z = -15011060
72 Z = -4575371
31
XDOT = 19121
985764 XDOT = 5828
381261
YDOT = -10675
467732 feet/sec YDOT = -3253
882565 meter/sec
ZDOT = 10106
097395 ZDOT = 3080
338486
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 19337
61476291
00016717 00000-0 10270-3 0 9028
2 25544 51
6423 241
3259 0007158 352
4252 7
6789 15
50097064 1536
Satellite: ISS
Catalog Number: 25544
Epoch time: 19337
61476291 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 241
3259 deg
Eccentricity:
0007158
Arg of perigee: 352
4252 deg
Mean anomaly: 7
6789 deg
Mean motion: 15
50097064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 153
Checksum: 308
Coasting Arc #4 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2019/338/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5083330
65 A = 6792948
73 meter
Y = 1262498
99 meter E =
0013400
Z = 4324427
44 I = 51
31516
XDOT = 1283
387498 Wp = 39
59982
YDOT = 6716
894583 meter/sec RA = 235
33099 deg
ZDOT = -3453
504352 TA = 85
75145
MA = 85
59834
Ha = 228
518 n
mi
Hp = 220
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16677593
99 X = 5047829
45
Y = 4142057
07 feet Y = 1319145
61 meter
Z = 14187754
06 Z = 4349034
33
XDOT = 4210
588905 XDOT = 1224
957126
YDOT = 22037
055717 feet/sec YDOT = 6730
919847 meter/sec
ZDOT = -11330
394857 ZDOT = -3447
411589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1695916
52 X = 516915
36
Y = 17006703
60 feet Y = 5183643
26 meter
Z = 14299896
61 Z = 4358608
49
XDOT = -18056
639311 XDOT = -5503
663662
YDOT = 11348
651779 feet/sec YDOT = 3459
069062 meter/sec
ZDOT = -11303
034527 ZDOT = -3445
164924
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 19338
64627974
00016717 00000-0 10270-3 0 9039
2 25544 51
6429 236
2146 0007345 355
4999 4
6084 15
50135452 1695
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
64627974 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 236
2146 deg
Eccentricity:
0007345
Arg of perigee: 355
4999 deg
Mean anomaly: 4
6084 deg
Mean motion: 15
50135452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 328
Coasting Arc #5 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2019/338/17:51:57
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3383732
68 A = 6800709
37 meter
Y = 5847723
50 meter E =
0006478
Z = -777811
61 I = 51
34013
XDOT = -4505
318857 Wp = 97
56286
YDOT = 1826
072231 meter/sec RA = 234
66005 deg
ZDOT = -5914
228546 TA = 90
85935
MA = 90
78512
Ha = 228
613 n
mi
Hp = 220
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11101485
17 X = 3321868
44
Y = 19185444
55 feet Y = 5885216
93 meter
Z = -2551875
37 Z = -761524
51
XDOT = -14781
229845 XDOT = -4496
675503
YDOT = 5991
050628 feet/sec YDOT = 1775
739276 meter/sec
ZDOT = -19403
636961 ZDOT = -5936
092699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4019072
27 X = 1225013
23
Y = 21806950
10 feet Y = 6646758
39 meter
Z = -2477964
70 Z = -755283
64
XDOT = -14220
661078 XDOT = -4334
457496
YDOT = 421
333076 feet/sec YDOT = 128
422322 meter/sec
ZDOT = -19503
467525 ZDOT = -5944
656902
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 19338
77522043
00016717 00000-0 10270-3 0 9045
2 25544 51
6393 235
5715 0007138 358
2132 1
8992 15
50136929 1719
Satellite: ISS
Catalog Number: 25544
Epoch time: 19338
77522043 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 235
5715 deg
Eccentricity:
0007138
Arg of perigee: 358
2132 deg
Mean anomaly: 1
8992 deg
Mean motion: 15
50136929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 308
Coasting Arc #6 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/17:51:57
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3602960
69 A = 6800579
51 meter
Y = -5642641
79 meter E =
0018382
Z = 1129802
19 I = 51
35892
XDOT = 4627
879168 Wp = 39
84837
YDOT = -1775
662382 meter/sec RA = 229
68707 deg
ZDOT = 5850
979278 TA = 332
45255
MA = 332
54986
Ha = 228
666 n
mi
Hp = 220
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11820737
18 X = -3545083
24
Y = -18512604
30 feet Y = -5682609
09 meter
Z = 3706700
09 Z = 1112440
47
XDOT = 15183
330604 XDOT = 4618
970160
YDOT = -5825
663984 feet/sec YDOT = -1723
960317 meter/sec
ZDOT = 19196
126239 ZDOT = 5873
438216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5297747
54 X = -1614753
45
Y = -21329756
06 feet Y = -6501309
65 meter
Z = 3627857
28 Z = 1105770
90
XDOT = 14570
172808 XDOT = 4440
988672
YDOT = -314
143576 feet/sec YDOT = -95
750962 meter/sec
ZDOT = 19298
671394 ZDOT = 5882
235041
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 19339
80673852
00016717 00000-0 10270-3 0 9056
2 25544 51
6388 230
4603 0006784 2
5867 357
5318 15
50092054 1873
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80673852 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 230
4603 deg
Eccentricity:
0006784
Arg of perigee: 2
5867 deg
Mean anomaly: 357
5318 deg
Mean motion: 15
50092054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 323
Coasting Arc #7 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -349473
81 A = 6792622
96 meter
Y = 5107682
17 meter E =
0013568
Z = -4477749
86 I = 51
33445
XDOT = -6143
273981 Wp = 42
58236
YDOT = -3237
938305 meter/sec RA = 229
49969 deg
ZDOT = -3209
933109 TA = 194
89298
MA = 194
93298
Ha = 228
690 n
mi
Hp = 220
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1146567
62 X = -384812
83
Y = 16757487
44 feet Y = 5103576
77 meter
Z = -14690780
37 Z = -4479533
02
XDOT = -20155
098363 XDOT = -6091
017635
YDOT = -10623
157169 feet/sec YDOT = -3306
344368 meter/sec
ZDOT = -10531
276604 ZDOT = -3239
648334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2246460
20 X = -684721
07
Y = 16638305
62 feet Y = 5071355
55 meter
Z = -14699225
59 Z = -4480323
96
XDOT = -18056
419327 XDOT = -5503
596611
YDOT = -11873
176266 feet/sec YDOT = -3618
944126 meter/sec
ZDOT = -10666
612275 ZDOT = -3251
183421
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 19339
80673873
00016717 00000-0 10270-3 0 9060
2 25544 51
6399 230
4608 0006772 3
0230 357
0960 15
50099615 1875
Satellite: ISS
Catalog Number: 25544
Epoch time: 19339
80673873 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 230
4608 deg
Eccentricity:
0006772
Arg of perigee: 3
0230 deg
Mean anomaly: 357
0960 deg
Mean motion: 15
50099615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 319
Coasting Arc #8 (Orbit 196)
---------------------------------------
Vector Time (GMT): 2019/340/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 925173
85 A = 6791040
74 meter
Y = -4656137
18 meter E =
0007411
Z = 4849183
67 I = 51
34419
XDOT = 6234
017404 Wp = 61
45623
YDOT = 3753
187048 meter/sec RA = 226
44517 deg
ZDOT = 2415
045632 TA = 4
75840
MA = 4
75136
Ha = 228
714 n
mi
Hp = 220
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3035347
29 X = 953616
50
Y = -15276040
62 feet Y = -4645632
48 meter
Z = 15909395
26 Z = 4853746
68
XDOT = 20452
813004 XDOT = 6179
853781
YDOT = 12313
605800 feet/sec YDOT = 3822
597251 meter/sec
ZDOT = 7923
378058 ZDOT = 2445
197111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6985298
10 X = 2129118
86
Y = 13896214
00 feet Y = 4235566
03 meter
Z = 15930488
21 Z = 4855612
81
XDOT = -22664
718910 XDOT = -6908
206324
YDOT = 2154
802407 feet/sec YDOT = 656
783774 meter/sec
ZDOT = 8060
683529 ZDOT = 2456
896340
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 19340
45143540
00016717 00000-0 10270-3 0 9077
2 25544 51
6411 227
2707 0007127 3
4747 356
6452 15
50118305 1976
Satellite: ISS
Catalog Number: 25544
Epoch time: 19340
45143540 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 227
2707 deg
Eccentricity:
0007127
Arg of perigee: 3
4747 deg
Mean anomaly: 356
6452 deg
Mean motion: 15
50118305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 197
Checksum: 287
Coasting Arc #9 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2019/341/09:34:11
000
Vector Time (MET): N/A
Weight (LBS) : 920317
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -919003
79 A = 6790507
47 meter
Y = 4519554
75 meter E =
0016829
Z = -4998729
45 I = 51
36710
XDOT = -6463
690772 Wp = 51
66675
YDOT = -3556
272655 meter/sec RA = 221
46922 deg
ZDOT = -2021
462472 TA = 198
52934
MA = 198
59070
Ha = 228
949 n
mi
Hp = 220
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3015104
29 X = -945193
10
Y = 14827935
52 feet Y = 4509131
68 meter
Z = -16400030
99 Z = -5003257
01
XDOT = -21206
334555 XDOT = -6413
623831
YDOT = -11667
561205 feet/sec YDOT = -3628
274145 meter/sec
ZDOT = -6632
094725 ZDOT = -2052
739684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6962616
89 X = -2122205
63
Y = -13408725
55 feet Y = -4086979
55 meter
Z = -16420949
66 Z = -5005105
46
XDOT = 22844
843326 XDOT = 6963
108246
YDOT = -3543
596860 feet/sec YDOT = -1080
088323 meter/sec
ZDOT = -6774
565461 ZDOT = -2064
887553
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 19341
41848208
00016717 00000-0 10270-3 0 9088
2 25544 51
6420 222
4793 0007264 7
6972 352
4288 15
50108743 2120
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
41848208 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 222
4793 deg
Eccentricity:
0007264
Arg of perigee: 7
6972 deg
Mean anomaly: 352
4288 deg
Mean motion: 15
50108743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 302
Coasting Arc #10 (Orbit 212)
---------------------------------------
Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 942917
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1834093
33 A = 6795571
23 meter
Y = 5454239
89 meter E =
0009990
Z = -3627553
53 I = 51
38646
XDOT = -6228
111924 Wp = 38
25376
YDOT = -812
381084 meter/sec RA = 221
18284 deg
ZDOT = -4369
203248 TA = 184
78490
MA = 184
79445
Ha = 228
921 n
mi
Hp = 220
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6017366
57 X = 1790586
99
Y = 17894487
84 feet Y = 5474506
99 meter
Z = -11901422
35 Z = -3618749
40
XDOT = -20433
438072 XDOT = -6197
341317
YDOT = -2665
292271 feet/sec YDOT = -881
855907 meter/sec
ZDOT = -14334
656324 ZDOT = -4399
382791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18547604
92 X = -5653309
98
Y = -3654386
65 feet Y = -1113857
05 meter
Z = -11861579
14 Z = -3615409
32
XDOT = 12200
223760 XDOT = 3718
628202
YDOT = -14933
857709 feet/sec YDOT = -4551
839830 meter/sec
ZDOT = -14472
281450 ZDOT = -4411
151386
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 19341
48295118
00016717 00000-0 10270-3 0 9092
2 25544 51
6431 222
1607 0007203 6
5755 353
5489 15
50096908 2138
Satellite: ISS
Catalog Number: 25544
Epoch time: 19341
48295118 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 222
1607 deg
Eccentricity:
0007203
Arg of perigee: 6
5755 deg
Mean anomaly: 353
5489 deg
Mean motion: 15
50096908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 213
Checksum: 304
Coasting Arc #11 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2019/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 942917
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1899290
91 A = 6794771
16 meter
Y = -5231097
90 meter E =
0013723
Z = 3883022
28 I = 51
40992
XDOT = 6455
996808 Wp = 66
59458
YDOT = 690
205666 meter/sec RA = 216
21092 deg
ZDOT = 4081
486093 TA = 340
46622
MA = 340
51875
Ha = 229
106 n
mi
Hp = 220
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6231269
40 X = -1859515
95
Y = -17162394
67 feet Y = -5252115
02 meter
Z = 12739574
40 Z = 3873892
29
XDOT = 21181
091891 XDOT = 6427
973006
YDOT = 2264
454285 feet/sec YDOT = 762
244174 meter/sec
ZDOT = 13390
702406 ZDOT = 4112
779380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18073609
97 X = 5508836
32
Y = 2788018
55 feet Y = 849788
05 meter
Z = 12698221
94 Z = 3870418
05
XDOT = -11996
005587 XDOT = -3656
382503
YDOT = 16034
295250 feet/sec YDOT = 4887
253192 meter/sec
ZDOT = 13533
431378 ZDOT = 4124
989884
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 19342
51446445
00016717 00000-0 10270-3 0 9100
2 25544 51
6434 217
0494 0007335 11
3700 348
7615 15
50086538 2290
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
51446445 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 217
0494 deg
Eccentricity:
0007335
Arg of perigee: 11
3700 deg
Mean anomaly: 348
7615 deg
Mean motion: 15
50086538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 229
Checksum: 294
Coasting Arc #12 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2019/342/21:54:30
000
Vector Time (MET): N/A
Weight (LBS) : 942917
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -221950
37 A = 6791193
40 meter
Y = -4778496
05 meter E =
0008434
Z = 4812422
71 I = 51
41044
XDOT = 6894
276083 Wp = 68
71993
YDOT = 2217
245993 meter/sec RA = 213
94317 deg
ZDOT = 2519
012534 TA = 356
42316
MA = 356
42919
Ha = 228
870 n
mi
Hp = 220
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -728183
62 X = -191875
79
Y = -15677480
47 feet Y = -4780810
32 meter
Z = 15788788
41 Z = 4811417
17
XDOT = 22619
016020 XDOT = 6856
733633
YDOT = 7274
429110 feet/sec YDOT = 2294
132527 meter/sec
ZDOT = 8264
476817 ZDOT = 2552
411894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11692686
36 X = -3563930
80
Y = -10475254
12 feet Y = -3192857
45 meter
Z = 15784474
06 Z = 4811107
69
XDOT = 20316
558488 XDOT = 6192
487027
YDOT = -9992
307838 feet/sec YDOT = -3045
655429 meter/sec
ZDOT = 8416
735367 ZDOT = 2565
420940
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 19342
96574824
00016717 00000-0 10270-3 0 9113
2 25544 51
6431 214
8106 0006834 12
4679 347
6639 15
50127731 2365
Satellite: ISS
Catalog Number: 25544
Epoch time: 19342
96574824 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 214
8106 deg
Eccentricity:
0006834
Arg of perigee: 12
4679 deg
Mean anomaly: 347
6639 deg
Mean motion: 15
50127731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 312
Coasting Arc #13 (Orbit 243)
---------------------------------------
Vector Time (GMT): 2019/343/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6043964
34 A = 6797276
58 meter
Y = 899907
08 meter E =
0015944
Z = 2971059
90 I = 51
44479
XDOT = 1617
201039 Wp = 70
23411
YDOT = 5608
502941 meter/sec RA = 211
26892 deg
ZDOT = -4961
537346 TA = 75
76812
MA = 75
59107
Ha = 229
145 n
mi
Hp = 219
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19829279
33 X = 6019020
12
Y = 2952451
05 feet Y = 967355
19 meter
Z = 9747571
85 Z = 3000359
21
XDOT = 5305
777688 XDOT = 1578
465720
YDOT = 18400
600199 feet/sec YDOT = 5626
371533 meter/sec
ZDOT = -16278
009665 ZDOT = -4953
774986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13372363
65 X = -4075896
44
Y = 14848368
68 feet Y = 4525782
77 meter
Z = 9881208
48 Z = 3011792
34
XDOT = -17248
780877 XDOT = -5257
428411
YDOT = -4666
629582 feet/sec YDOT = -1422
388697 meter/sec
ZDOT = -16242
910353 ZDOT = -4950
839076
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 19343
48150674
00016717 00000-0 10270-3 0 9125
2 25544 51
6424 212
2589 0007323 15
5885 344
5490 15
50088510 2442
Satellite: ISS
Catalog Number: 25544
Epoch time: 19343
48150674 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 212
2589 deg
Eccentricity:
0007323
Arg of perigee: 15
5885 deg
Mean anomaly: 344
5490 deg
Mean motion: 15
50088510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 244
Checksum: 301
Coasting Arc #14 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2019/344/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6206944
50 A = 6797920
38 meter
Y = -691845
71 meter E =
0011517
Z = -2675711
60 I = 51
47621
XDOT = -1622
941675 Wp = 33
33762
YDOT = -5404
318952 meter/sec RA = 206
30276 deg
ZDOT = 5182
215733 TA = 296
43931
MA = 296
55743
Ha = 229
115 n
mi
Hp = 219
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20363991
14 X = -6185749
44
Y = -2269835
00 feet Y = -761137
31 meter
Z = -8778581
36 Z = -2705811
70
XDOT = -5324
611796 XDOT = -1587
561112
YDOT = -17730
705223 feet/sec YDOT = -5422
270638 meter/sec
ZDOT = 17002
020121 ZDOT = 5174
417239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12830338
64 X = 3910687
22
Y = -15899586
68 feet Y = -4846194
02 meter
Z = -8915903
24 Z = -2717567
31
XDOT = 16714
331606 XDOT = 5094
528274
YDOT = 4009
805058 feet/sec YDOT = 1222
188582 meter/sec
ZDOT = 16966
737036 ZDOT = 5171
461449
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 19344
44854734
00016717 00000-0 10270-3 0 9131
2 25544 51
6423 207
4676 0007336 17
4472 342
6930 15
50107925 2597
Satellite: ISS
Catalog Number: 25544
Epoch time: 19344
44854734 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 207
4676 deg
Eccentricity:
0007336
Arg of perigee: 17
4472 deg
Mean anomaly: 342
6930 deg
Mean motion: 15
50107925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 259
Checksum: 312
Coasting Arc #15 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2019/345/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6367349
43 A = 6798733
75 meter
Y = 507345
57 meter E =
0016162
Z = 2319604
08 I = 51
50912
XDOT = 1561
470006 Wp = 80
25820
YDOT = 5212
876779 meter/sec RA = 201
33968 deg
ZDOT = -5391
594112 TA = 73
88673
MA = 73
70887
Ha = 229
296 n
mi
Hp = 219
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20890254
04 X = 6349935
41
Y = 1664519
57 feet Y = 578452
07 meter
Z = 7610249
61 Z = 2350492
49
XDOT = 5122
933092 XDOT = 1529
251774
YDOT = 17102
614104 feet/sec YDOT = 5230
158859 meter/sec
ZDOT = -17688
957060 ZDOT = -5384
086485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12318349
04 X = -3754632
79
Y = 16889830
87 feet Y = 5148020
45 meter
Z = 7751201
75 Z = 2362566
29
XDOT = -16086
127612 XDOT = -4903
051696
YDOT = -3578
340421 feet/sec YDOT = -1090
678160 meter/sec
ZDOT = -17654
983505 ZDOT = -5381
238972
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 19345
48005757
00016717 00000-0 10270-3 0 9140
2 25544 51
6422 202
3571 0007338 21
8599 338
2863 15
50093296 2754
Satellite: ISS
Catalog Number: 25544
Epoch time: 19345
48005757 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 202
3571 deg
Eccentricity:
0007338
Arg of perigee: 21
8599 deg
Mean anomaly: 338
2863 deg
Mean motion: 15
50093296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 275
Checksum: 318
Coasting Arc #16 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2019/346/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6412682
71 A = 6800901
29 meter
Y = -2226889
02 meter E =
0019195
Z = 175276
71 I = 51
53475
XDOT = 1719
986948 Wp = 39
85852
YDOT = -4453
160253 meter/sec RA = 197
97485 deg
ZDOT = 5999
899453 TA = 322
03062
MA = 322
16579
Ha = 229
230 n
mi
Hp = 219
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21038985
26 X = -6388155
79
Y = -7306066
32 feet Y = -2298463
05 meter
Z = 575054
82 Z = 144185
18
XDOT = 5643
001798 XDOT = 1740
511147
YDOT = -14610
105818 feet/sec YDOT = -4433
812297 meter/sec
ZDOT = 19684
709492 ZDOT = 6008
303775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5948347
09 X = 1813056
19
Y = 21465732
02 feet Y = 6542755
12 meter
Z = 433255
06 Z = 132056
14
XDOT = -13586
135352 XDOT = -4141
054055
YDOT = 3335
967164 feet/sec YDOT = 1016
802792 meter/sec
ZDOT = 19723
322030 ZDOT = 6011
668555
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 19346
18921579
00016717 00000-0 10270-3 0 9158
2 25544 51
6387 198
8420 0007151 26
7415 333
4103 15
50155742 2861
Satellite: ISS
Catalog Number: 25544
Epoch time: 19346
18921579 = yrday
fracday
Element set: 915
Inclination: 51
6387 deg
RA of node: 198
8420 deg
Eccentricity:
0007151
Arg of perigee: 26
7415 deg
Mean anomaly: 333
4103 deg
Mean motion: 15
50155742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 286
Checksum: 313
Coasting Arc #17 (Orbit 300)
---------------------------------------
Vector Time (GMT): 2019/347/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6483280
91 A = 6800906
12 meter
Y = 1969754
13 meter E =
0010925
Z = -578430
10 I = 51
56577
XDOT = -1867
504392 Wp = 98
93894
YDOT = 4424
668460 meter/sec RA = 193
01549 deg
ZDOT = -5962
453509 TA = 87
29477
MA = 87
16972
Ha = 229
504 n
mi
Hp = 219
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21270606
67 X = 6463582
41
Y = 6462447
92 feet Y = 2042144
70 meter
Z = -1897736
56 Z = -546984
07
XDOT = -6126
982913 XDOT = -1887
881055
YDOT = 14516
628806 feet/sec YDOT = 4403
671730 meter/sec
ZDOT = -19561
855345 ZDOT = -5971
573989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7142644
60 X = -2177078
07
Y = -21064389
01 feet Y = -6420425
77 meter
Z = -1754277
25 Z = -534703
71
XDOT = 13754
689801 XDOT = 4192
429451
YDOT = -3060
427033 feet/sec YDOT = -932
818160 meter/sec
ZDOT = -19603
741204 ZDOT = -5975
220319
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 19347
15625527
00016717 00000-0 10270-3 0 9161
2 25544 51
6379 194
0494 0007506 28
6664 331
4898 15
50110653 3011
Satellite: ISS
Catalog Number: 25544
Epoch time: 19347
15625527 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 194
0494 deg
Eccentricity:
0007506
Arg of perigee: 28
6664 deg
Mean anomaly: 331
4898 deg
Mean motion: 15
50110653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 301
Checksum: 316
Coasting Arc #18 (Orbit 316)
---------------------------------------
Vector Time (GMT): 2019/348/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6516217
79 A = 6800600
14 meter
Y = -1666064
43 meter E =
0020291
Z = 928514
58 I = 51
59728
XDOT = 1991
600466 Wp = 47
43134
YDOT = -4454
049020 meter/sec RA = 188
05969 deg
ZDOT = 5915
829348 TA = 322
61863
MA = 322
75963
Ha = 229
413 n
mi
Hp = 219
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21378667
29 X = -6501613
29
Y = -5466090
64 feet Y = -1738851
87 meter
Z = 3046307
66 Z = 896896
39
XDOT = 6534
122263 XDOT = 2012
523077
YDOT = -14613
021720 feet/sec YDOT = -4431
661498 meter/sec
ZDOT = 19408
888937 ZDOT = 5925
553915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8372870
34 X = 2552050
88
Y = 20437193
78 feet Y = 6229256
67 meter
Z = 2902017
39 Z = 884534
90
XDOT = -14057
338999 XDOT = -4284
676927
YDOT = 2963
052927 feet/sec YDOT = 903
138532 meter/sec
ZDOT = 19453
540269 ZDOT = 5929
439074
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 19348
18775976
00016717 00000-0 10270-3 0 9170
2 25544 51
6373 188
9392 0007226 32
9653 327
1947 15
50148821 3171
Satellite: ISS
Catalog Number: 25544
Epoch time: 19348
18775976 = yrday
fracday
Element set: 917
Inclination: 51
6373 deg
RA of node: 188
9392 deg
Eccentricity:
0007226
Arg of perigee: 32
9653 deg
Mean anomaly: 327
1947 deg
Mean motion: 15
50148821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 317
Checksum: 345
Coasting Arc #19 (Orbit 331)
---------------------------------------
Vector Time (GMT): 2019/349/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6521526
54 A = 6800326
82 meter
Y = 1404257
35 meter E =
0009820
Z = -1324963
95 I = 51
63037
XDOT = -2141
404810 Wp = 95
89143
YDOT = 4494
413247 meter/sec RA = 183
10448 deg
ZDOT = -5814
865837 TA = 98
49587
MA = 98
38457
Ha = 229
613 n
mi
Hp = 219
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21396084
44 X = 6511774
94
Y = 4607143
55 feet Y = 1477131
34 meter
Z = -4346994
59 Z = -1293308
41
XDOT = -7025
606331 XDOT = -2163
258215
YDOT = 14745
450285 feet/sec YDOT = 4470
345229 meter/sec
ZDOT = -19077
643823 ZDOT = -5825
320345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9419836
12 X = -2871166
05
Y = -19786872
33 feet Y = -6031038
69 meter
Z = -4202491
40 Z = -1280919
38
XDOT = 14447
120411 XDOT = 4403
482301
YDOT = -2843
225487 feet/sec YDOT = -866
615129 meter/sec
ZDOT = -19125
636140 ZDOT = -5829
493895
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 19349
15479740
00016717 00000-0 10270-3 0 9189
2 25544 51
6383 184
1466 0007483 35
1564 325
0079 15
50113115 3321
Satellite: ISS
Catalog Number: 25544
Epoch time: 19349
15479740 = yrday
fracday
Element set: 918
Inclination: 51
6383 deg
RA of node: 184
1466 deg
Eccentricity:
0007483
Arg of perigee: 35
1564 deg
Mean anomaly: 325
0079 deg
Mean motion: 15
50113115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 332
Checksum: 304
Coasting Arc #20 (Orbit 347)
---------------------------------------
Vector Time (GMT): 2019/350/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6487082
01 A = 6799836
68 meter
Y = -1108454
00 meter E =
0020803
Z = 1665416
66 I = 51
66306
XDOT = 2260
906138 Wp = 55
42240
YDOT = -4591
725027 meter/sec RA = 178
15255 deg
ZDOT = 5711
243400 TA = 322
80365
MA = 322
94759
Ha = 229
601 n
mi
Hp = 219
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21283077
48 X = -6482294
44
Y = -3636660
11 feet Y = -1180970
59 meter
Z = 5463965
42 Z = 1633916
55
XDOT = 7417
671055 XDOT = 2284
342264
YDOT = -15064
714656 feet/sec YDOT = -4566
311689 meter/sec
ZDOT = 18737
675198 ZDOT = 5722
282276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10451782
84 X = 3185703
41
Y = 18934256
12 feet Y = 5771161
27 meter
Z = 5320129
90 Z = 1621575
59
XDOT = -14941
734416 XDOT = -4554
240650
YDOT = 2931
602168 feet/sec YDOT = 893
552341 meter/sec
ZDOT = 18788
346791 ZDOT = 5726
688102
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 19350
18629873
00016717 00000-0 10270-3 0 9199
2 25544 51
6389 179
0360 0007348 39
1090 321
0590 15
50143187 3484
Satellite: ISS
Catalog Number: 25544
Epoch time: 19350
18629873 = yrday
fracday
Element set: 919
Inclination: 51
6389 deg
RA of node: 179
0360 deg
Eccentricity:
0007348
Arg of perigee: 39
1090 deg
Mean anomaly: 321
0590 deg
Mean motion: 15
50143187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 348
Checksum: 317
Coasting Arc #21 (Orbit 362)
---------------------------------------
Vector Time (GMT): 2019/351/03:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 959319
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6428809
00 A = 6799312
73 meter
Y = 862736
53 meter E =
0009377
Z = -2047931
13 I = 51
69483
XDOT = -2391
091976 Wp = 87
06182
YDOT = 4698
582826 meter/sec RA = 173
20187 deg
ZDOT = -5548
192067 TA = 115
49952
MA = 115
40250
Ha = 229
748 n
mi
Hp = 218
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21091893
05 X = 6428631
46
Y = 2830500
42 feet Y = 934627
24 meter
Z = -6718934
15 Z = -2016702
98
XDOT = -7844
789948 XDOT = -2416
505379
YDOT = 15415
297986 feet/sec YDOT = 4671
702447 meter/sec
ZDOT = -18202
729877 ZDOT = -5559
868219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11281107
80 X = -3438481
66
Y = -18097308
88 feet Y = -5516059
75 meter
Z = -6576304
36 Z = -2004457
57
XDOT = 15481
453861 XDOT = 4718
747137
YDOT = -3042
623194 feet/sec YDOT = -927
391550 meter/sec
ZDOT = -18256
323250 ZDOT = -5564
527327
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 19351
15333299
00016717 00000-0 10270-3 0 9203
2 25544 51
6392 174
2439 0007595 41
4621 318
7105 15
50117553 3632
Satellite: ISS
Catalog Number: 25544
Epoch time: 19351
15333299 = yrday
fracday
Element set: 920
Inclination: 51
6392 deg
RA of node: 174
2439 deg
Eccentricity:
0007595
Arg of perigee: 41
4621 deg
Mean anomaly: 318
7105 deg
Mean motion: 15
50117553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 363
Checksum: 299
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