[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 25th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14325 6884 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 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
267/16:05:05
000 0
0 0
0 0
0
N/A 0
0 0
0 230
1
000/00:00:00
000 0
0 0
0 218
3
268/13:57:43
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
3
268/17:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
268/19:45:47
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
3
271/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
272/00:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
3
275/04:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 218
3
276/07:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
4
Coasting Arc #1 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2019/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5325241
78 A = 6796913
11 meter
Y = -2855069
68 meter E =
0012001
Z = -3119322
39 I = 51
33577
XDOT = 349
092649 Wp = 76
20697
YDOT = -5919
376662 meter/sec RA = 232
59482 deg
ZDOT = 4840
505504 TA = 247
81389
MA = 247
94127
Ha = 230
029 n
mi
Hp = 218
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17471265
67 X = -5277767
82
Y = -9367026
50 feet Y = -2914354
92 meter
Z = -10233997
33 Z = -3145075
07
XDOT = 1145
317091 XDOT = 391
746364
YDOT = -19420
527106 feet/sec YDOT = -5915
234247 meter/sec
ZDOT = 15880
923568 ZDOT = 4842
305015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17587396
98 X = 5360638
60
Y = 9014527
88 feet Y = 2747628
10 meter
Z = -10350978
95 Z = -3154978
38
XDOT = 11
260350 XDOT = 3
432155
YDOT = 18154
078206 feet/sec YDOT = 5533
363037 meter/sec
ZDOT = 15889
449853 ZDOT = 4843
104315
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 19266
50650509
00016717 00000-0 10270-3 0 9001
2 25544 51
6391 233
6644 0007472 75
2278 284
9700 15
50083279 30504
Satellite: ISS
Catalog Number: 25544
Epoch time: 19266
50650509 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 233
6644 deg
Eccentricity:
0007472
Arg of perigee: 75
2278 deg
Mean anomaly: 284
9700 deg
Mean motion: 15
50083279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 309
Coasting Arc #2 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2019/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5538969
33 A = 6797714
12 meter
Y = 2778064
33 meter E =
0020468
Z = 2775775
63 I = 51
35965
XDOT = -298
001322 Wp = 92
50711
YDOT = 5718
728613 meter/sec RA = 227
62029 deg
ZDOT = -5097
032679 TA = 55
93300
MA = 55
73888
Ha = 229
975 n
mi
Hp = 218
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18172471
56 X = 5494009
39
Y = 9114384
30 feet Y = 2839753
71 meter
Z = 9106875
42 Z = 2802572
51
XDOT = -977
694626 XDOT = -337
169144
YDOT = 18762
232981 feet/sec YDOT = 5715
176956 meter/sec
ZDOT = -16722
548161 ZDOT = -5098
575605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18438700
66 X = -5620115
96
Y = -8431640
52 feet Y = -2569964
03 meter
Z = 9228632
59 Z = 2812887
21
XDOT = -451
755934 XDOT = -137
695209
YDOT = -17435
878824 feet/sec YDOT = -5314
455866 meter/sec
ZDOT = -16729
883022 ZDOT = -5099
268345
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 19267
53801202
00016717 00000-0 10270-3 0 9014
2 25544 51
6390 228
5527 0007446 78
2804 281
9182 15
50105366 30665
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
53801202 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 228
5527 deg
Eccentricity:
0007446
Arg of perigee: 78
2804 deg
Mean anomaly: 281
9182 deg
Mean motion: 15
50105366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 303
Coasting Arc #3 (Orbit 3068)
---------------------------------------
Vector Time (GMT): 2019/267/16:05:05
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3427781
93 A = 6799930
26 meter
Y = -5615700
66 meter E =
0021198
Z = 1682003
67 I = 51
37339
XDOT = 4979
258403 Wp = 69
25944
YDOT = -1323
666517 meter/sec RA = 226
81300 deg
ZDOT = 5677
228036 TA = 309
22514
MA = 309
41313
Ha = 230
068 n
mi
Hp = 218
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11246003
70 X = -3372901
00
Y = -18424214
77 feet Y = -5653725
61 meter
Z = 5518384
75 Z = 1665486
36
XDOT = 16336
149617 XDOT = 4966
113201
YDOT = -4342
737916 feet/sec YDOT = -1268
058203 meter/sec
ZDOT = 18626
076233 ZDOT = 5701
383476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21519936
44 X = 6559276
63
Y = -1907091
19 feet Y = -581281
39 meter
Z = 5443546
44 Z = 1659192
95
XDOT = -3463
417907 XDOT = -1055
649778
YDOT = 14879
729676 feet/sec YDOT = 4535
341605 meter/sec
ZDOT = 18736
044199 ZDOT = 5710
746272
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 19267
73142021
00016717 00000-0 10270-3 0 9024
2 25544 51
6418 227
5956 0007456 78
7125 281
4863 15
50093156 30690
Satellite: ISS
Catalog Number: 25544
Epoch time: 19267
73142021 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 227
5956 deg
Eccentricity:
0007456
Arg of perigee: 78
7125 deg
Mean anomaly: 281
4863 deg
Mean motion: 15
50093156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3069
Checksum: 318
Coasting Arc #4 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 840386
78 A = 6790604
83 meter
Y = -4572533
77 meter E =
0012868
Z = 4939454
38 I = 51
36274
XDOT = 6455
154039 Wp = 101
54448
YDOT = 3531
906780 meter/sec RA = 222
28138 deg
ZDOT = 2163
953948 TA = 327
24173
MA = 327
32145
Ha = 229
900 n
mi
Hp = 218
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2757174
47 X = 867462
68
Y = -15001751
21 feet Y = -4562984
27 meter
Z = 16205558
98 Z = 4943602
69
XDOT = 21178
326899 XDOT = 6404
668230
YDOT = 11587
620670 feet/sec YDOT = 3603
810716 meter/sec
ZDOT = 7099
586443 ZDOT = 2195
187701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5860472
03 X = 1786271
87
Y = 14060210
67 feet Y = 4285552
21 meter
Z = 16224673
67 Z = 4945280
53
XDOT = -23017
956903 XDOT = -7015
873264
YDOT = 1210
180291 feet/sec YDOT = 368
862953 meter/sec
ZDOT = 7241
514487 ZDOT = 2207
213616
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 19268
63398600
00016717 00000-0 10270-3 0 9031
2 25544 51
6403 223
1235 0007257 82
8812 277
3164 15
50137400 30839
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
63398600 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 223
1235 deg
Eccentricity:
0007257
Arg of perigee: 82
8812 deg
Mean anomaly: 277
3164 deg
Mean motion: 15
50137400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3083
Checksum: 294
Coasting Arc #5 (Orbit 3084)
---------------------------------------
Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 916975
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1027583
75 A = 6790388
30 meter
Y = -4449895
29 meter E =
0012387
Z = 5015271
28 I = 51
36645
XDOT = 6451
467587 Wp = 101
15834
YDOT = 3671
791477 meter/sec RA = 221
63704 deg
ZDOT = 1929
605252 TA = 330
01838
MA = 330
08926
Ha = 229
998 n
mi
Hp = 218
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3371337
77 X = 1052906
09
Y = -14599393
99 feet Y = -4438262
21 meter
Z = 16454302
11 Z = 5020324
67
XDOT = 21166
232240 XDOT = 6400
556153
YDOT = 12046
559964 feet/sec YDOT = 3743
651800 meter/sec
ZDOT = 6330
725893 ZDOT = 1960
820041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13742939
09 X = 4188847
83
Y = 5905505
87 feet Y = 1799998
19 meter
Z = 16477527
33 Z = 5022350
33
XDOT = -15317
139254 XDOT = -4668
664045
YDOT = 17526
760831 feet/sec YDOT = 5342
156701 meter/sec
ZDOT = 6472
563518 ZDOT = 1972
837360
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 19268
76292486
00016717 00000-0 10270-3 0 9041
2 25544 51
6419 222
4852 0007378 83
0286 277
1704 15
50099913 30851
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
76292486 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 222
4852 deg
Eccentricity:
0007378
Arg of perigee: 83
0286 deg
Mean anomaly: 277
1704 deg
Mean motion: 15
50099913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3085
Checksum: 336
Coasting Arc #6 (Orbit 3085)
---------------------------------------
Vector Time (GMT): 2019/268/19:45:47
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5792232
28 A = 6799369
03 meter
Y = -2976570
98 meter E =
0012938
Z = -1951828
43 I = 51
39650
XDOT = 804
440151 Wp = 62
83200
YDOT = -5194
386036 meter/sec RA = 221
04276 deg
ZDOT = 5568
612624 TA = 275
61419
MA = 275
76172
Ha = 229
907 n
mi
Hp = 218
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19003386
74 X = -5749036
05
Y = -9765652
83 feet Y = -3041102
42 meter
Z = -6403636
58 Z = -1979859
69
XDOT = 2639
239340 XDOT = 835
416372
YDOT = -17041
948936 feet/sec YDOT = -5185
216640 meter/sec
ZDOT = 18269
726457 ZDOT = 5572
595866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -982210
21 X = -299377
67
Y = -21304557
85 feet Y = -6493629
23 meter
Z = -6531027
66 Z = -1990657
23
XDOT = 14474
158641 XDOT = 4411
723554
YDOT = -6239
766443 feet/sec YDOT = -1901
880812 meter/sec
ZDOT = 18288
119852 ZDOT = 5574
218931
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 19268
82739258
00016717 00000-0 10270-3 0 9052
2 25544 51
6389 222
1636 0007159 83
5925 276
6041 15
50105959 30863
Satellite: ISS
Catalog Number: 25544
Epoch time: 19268
82739258 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 222
1636 deg
Eccentricity:
0007159
Arg of perigee: 83
5925 deg
Mean anomaly: 276
6041 deg
Mean motion: 15
50105959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3086
Checksum: 339
Coasting Arc #7 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2019/269/19:45:47
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5980387
43 A = 6799810
71 meter
Y = 2816082
81 meter E =
0020268
Z = 1561300
24 I = 51
42554
XDOT = -856
838656 Wp = 106
68030
YDOT = 5024
595623 meter/sec RA = 216
07330 deg
ZDOT = -5724
616599 TA = 56
22056
MA = 56
02768
Ha = 229
815 n
mi
Hp = 218
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19620693
68 X = 5940868
80
Y = 9239116
84 feet Y = 2882738
91 meter
Z = 5122376
11 Z = 1590254
39
XDOT = -2811
150446 XDOT = -885
154524
YDOT = 16484
893776 feet/sec YDOT = 5014
854986 meter/sec
ZDOT = -18781
550523 ZDOT = -5728
848034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2121738
31 X = 646705
84
Y = 21551459
41 feet Y = 6568884
83 meter
Z = 5253994
81 Z = 1601417
62
XDOT = -13953
549096 XDOT = -4253
041764
YDOT = 6000
957571 feet/sec YDOT = 1829
091868 meter/sec
ZDOT = -18801
054269 ZDOT = -5730
561341
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 19269
85889431
00016717 00000-0 10270-3 0 9066
2 25544 51
6401 217
0516 0007100 85
2424 274
9537 15
50160717 31020
Satellite: ISS
Catalog Number: 25544
Epoch time: 19269
85889431 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 217
0516 deg
Eccentricity:
0007100
Arg of perigee: 85
2424 deg
Mean anomaly: 274
9537 deg
Mean motion: 15
50160717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 300
Coasting Arc #8 (Orbit 3116)
---------------------------------------
Vector Time (GMT): 2019/270/19:45:47
000
Vector Time (MET): N/A
Weight (LBS) : 932083
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6168118
53 A = 6800343
02 meter
Y = -2581151
27 meter E =
0014537
Z = -1225629
78 I = 51
45365
XDOT = 897
234886 Wp = 61
89533
YDOT = -4884
371777 meter/sec RA = 211
10559 deg
ZDOT = 5830
641447 TA = 284
77645
MA = 284
93748
Ha = 229
947 n
mi
Hp = 218
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20236609
35 X = -6132843
49
Y = -8468344
05 feet Y = -2649930
43 meter
Z = -4021095
07 Z = -1255506
24
XDOT = 2943
684008 XDOT = 923
464606
YDOT = -16024
841789 feet/sec YDOT = -4874
190940 meter/sec
ZDOT = 19129
401072 ZDOT = 5835
064146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3475870
18 X = -1059445
23
Y = -21634245
81 feet Y = -6594118
12 meter
Z = -4156939
89 Z = -1267035
28
XDOT = 13517
313287 XDOT = 4120
077090
YDOT = -5814
918581 feet/sec YDOT = -1772
387184 meter/sec
ZDOT = 19149
760132 ZDOT = 5836
846888
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 19270
82592742
00016717 00000-0 10270-3 0 9072
2 25544 51
6392 212
2593 0007265 91
0925 269
1058 15
50113084 31179
Satellite: ISS
Catalog Number: 25544
Epoch time: 19270
82592742 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 212
2593 deg
Eccentricity:
0007265
Arg of perigee: 91
0925 deg
Mean anomaly: 269
1058 deg
Mean motion: 15
50113084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3117
Checksum: 305
Coasting Arc #9 (Orbit 3126)
---------------------------------------
Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6259128
93 A = 6800622
41 meter
Y = -2486202
75 meter E =
0015458
Z = -919648
85 I = 51
47423
XDOT = 1038
899738 Wp = 61
85590
YDOT = -4768
460051 meter/sec RA = 207
90501 deg
ZDOT = 5903
531628 TA = 288
18531
MA = 288
35353
Ha = 229
997 n
mi
Hp = 218
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20535199
91 X = -6226395
14
Y = -8156833
16 feet Y = -2556013
83 meter
Z = -3017220
64 Z = -949973
69
XDOT = 3408
463707 XDOT = 1063
468607
YDOT = -15644
553972 feet/sec YDOT = -4756
704257 meter/sec
ZDOT = 19368
542087 ZDOT = 5908
638484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19691316
01 X = 6001913
12
Y = 9981446
34 feet Y = 3042344
85 meter
Z = -3155120
54 Z = -961680
74
XDOT = -3953
266780 XDOT = -1204
955715
YDOT = 13846
340905 feet/sec YDOT = 4220
364708 meter/sec
ZDOT = 19392
005677 ZDOT = 5910
683330
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 19271
47061526
00016717 00000-0 10270-3 0 9086
2 25544 51
6402 209
0674 0007405 92
0045 268
1954 15
50115994 31272
Satellite: ISS
Catalog Number: 25544
Epoch time: 19271
47061526 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 209
0674 deg
Eccentricity:
0007405
Arg of perigee: 92
0045 deg
Mean anomaly: 268
1954 deg
Mean motion: 15
50115994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3127
Checksum: 302
Coasting Arc #10 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 263328
67 A = 6790375
30 meter
Y = 4560121
50 meter E =
0019730
Z = -5042101
00 I = 51
45917
XDOT = -7206
423016 Wp = 84
06983
YDOT = -1696
028204 meter/sec RA = 205
13325 deg
ZDOT = -1914
755329 TA = 167
28420
MA = 167
23437
Ha = 229
984 n
mi
Hp = 218
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 863939
21 X = 236808
43
Y = 14961028
55 feet Y = 4562917
34 meter
Z = -16542326
11 Z = -5040886
80
XDOT = -23643
120132 XDOT = -7177
621046
YDOT = -5564
396994 feet/sec YDOT = -1776
454701 meter/sec
ZDOT = -6282
005672 ZDOT = -1949
691551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5516114
00 X = 1681311
55
Y = 13940127
71 feet Y = 4248950
93 meter
Z = -16537008
35 Z = -5040480
15
XDOT = -23153
111844 XDOT = -7057
068490
YDOT = 1538
365983 feet/sec YDOT = 468
893952 meter/sec
ZDOT = -6440
938365 ZDOT = -1963
198014
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 19272
05083269
00016717 00000-0 10270-3 0 9090
2 25544 51
6428 206
1901 0007259 98
3458 261
8516 15
50105052 31363
Satellite: ISS
Catalog Number: 25544
Epoch time: 19272
05083269 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 206
1901 deg
Eccentricity:
0007259
Arg of perigee: 98
3458 deg
Mean anomaly: 261
8516 deg
Mean motion: 15
50105052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 307
Coasting Arc #11 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -200980
01 A = 6789757
52 meter
Y = -4427175
57 meter E =
0011876
Z = 5135389
20 I = 51
48878
XDOT = 7381
710271 Wp = 111
60789
YDOT = 1428
225513 meter/sec RA = 200
16529 deg
ZDOT = 1513
046257 TA = 323
74856
MA = 323
82898
Ha = 229
912 n
mi
Hp = 218
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -659383
24 X = -176404
32
Y = -14524854
23 feet Y = -4429285
09 meter
Z = 16848389
77 Z = 5134473
08
XDOT = 24218
209549 XDOT = 7357
841175
YDOT = 4685
779242 feet/sec YDOT = 1510
639713 meter/sec
ZDOT = 4964
062523 ZDOT = 1548
846187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5422566
52 X = -1652798
28
Y = -13495766
98 feet Y = -4113509
77 meter
Z = 16844419
27 Z = 5134178
99
XDOT = 23417
413477 XDOT = 7137
627628
YDOT = -2980
862834 feet/sec YDOT = -908
566992 meter/sec
ZDOT = 5126
954455 ZDOT = 1562
695718
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 19273
08232805
00016717 00000-0 10270-3 0 9108
2 25544 51
6433 201
0793 0007265 102
1206 258
0759 15
50151521 31521
Satellite: ISS
Catalog Number: 25544
Epoch time: 19273
08232805 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 201
0793 deg
Eccentricity:
0007265
Arg of perigee: 102
1206 deg
Mean anomaly: 258
0759 deg
Mean motion: 15
50151521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 273
Coasting Arc #12 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 90311
48 A = 6789501
62 meter
Y = 4339803
72 meter E =
0020958
Z = -5238867
68 I = 51
51920
XDOT = -7482
843652 Wp = 89
65406
YDOT = -1143
470037 meter/sec RA = 195
19936 deg
ZDOT = -1079
860026 TA = 169
97342
MA = 169
93154
Ha = 229
919 n
mi
Hp = 218
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 296297
52 X = 67223
77
Y = 14238201
17 feet Y = 4340684
09 meter
Z = -17187886
09 Z = -5238485
44
XDOT = -24550
011980 XDOT = -7464
255447
YDOT = -3751
542116 feet/sec YDOT = -1227
044638 meter/sec
ZDOT = -3542
847853 ZDOT = -1116
164234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5217268
23 X = 1590223
36
Y = 13253202
87 feet Y = 4039576
23 meter
Z = -17186341
05 Z = -5238396
75
XDOT = -23377
610204 XDOT = -7125
495590
YDOT = 4409
796405 feet/sec YDOT = 1344
105944 meter/sec
ZDOT = -3708
065769 ZDOT = -1130
218446
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 19274
04935348
00016717 00000-0 10270-3 0 9118
2 25544 51
6433 196
2884 0007180 104
9012 255
2934 15
50112718 31673
Satellite: ISS
Catalog Number: 25544
Epoch time: 19274
04935348 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 196
2884 deg
Eccentricity:
0007180
Arg of perigee: 104
9012 deg
Mean anomaly: 255
2934 deg
Mean motion: 15
50112718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 305
Coasting Arc #13 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2019/275/00:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 11450
39 A = 6789084
81 meter
Y = -4257928
12 meter E =
0010273
Z = 5279917
91 I = 51
55077
XDOT = 7594
724976 Wp = 111
08879
YDOT = 841
111408 meter/sec RA = 190
23535 deg
ZDOT = 657
180979 TA = 332
60258
MA = 332
65671
Ha = 229
856 n
mi
Hp = 218
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 37566
90 X = 33415
56
Y = -13969580
45 feet Y = -4257676
92 meter
Z = 17322565
32 Z = 5280027
16
XDOT = 24917
076694 XDOT = 7581
562690
YDOT = 2759
551863 feet/sec YDOT = 925
967428 meter/sec
ZDOT = 2156
105574 ZDOT = 694
041929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5037794
91 X = -1535519
89
Y = -13028711
19 feet Y = -3971151
17 meter
Z = 17323255
05 Z = 5280128
14
XDOT = 23307
285166 XDOT = 7104
060519
YDOT = -5902
003410 feet/sec YDOT = -1798
930639 meter/sec
ZDOT = 2323
892354 ZDOT = 708
322389
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 19275
08084249
00016717 00000-0 10270-3 0 9129
2 25544 51
6431 191
1777 0007228 108
0849 252
1089 15
50160818 31831
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
08084249 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 191
1777 deg
Eccentricity:
0007228
Arg of perigee: 108
0849 deg
Mean anomaly: 252
1089 deg
Mean motion: 15
50160818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 314
Coasting Arc #14 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2019/275/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3950936
84 A = 6791847
79 meter
Y = -3039161
41 meter E =
0014710
Z = 4601305
66 I = 51
56280
XDOT = 6158
689866 Wp = 84
72122
YDOT = 3449
353745 meter/sec RA = 189
53786 deg
ZDOT = -3000
298404 TA = 35
28746
MA = 35
19017
Ha = 229
819 n
mi
Hp = 218
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12962391
21 X = 3962277
00
Y = -9971002
01 feet Y = -2994915
56 meter
Z = 15096147
18 Z = 4620525
90
XDOT = 20205
675412 XDOT = 6134
234504
YDOT = 11316
777379 feet/sec YDOT = 3518
087635 meter/sec
ZDOT = -9843
498701 ZDOT = -2970
440888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4888716
79 X = -1490080
88
Y = -15520662
52 feet Y = -4730697
94 meter
Z = 15183794
31 Z = 4628020
51
XDOT = 16514
905935 XDOT = 5033
743329
YDOT = -14729
524233 feet/sec YDOT = -4489
558986 meter/sec
ZDOT = -9707
713338 ZDOT = -2958
911025
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 19275
20977929
00016717 00000-0 10270-3 0 9130
2 25544 51
6414 190
5407 0007365 106
0525 254
1437 15
50152674 31858
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
20977929 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 190
5407 deg
Eccentricity:
0007365
Arg of perigee: 106
0525 deg
Mean anomaly: 254
1437 deg
Mean motion: 15
50152674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 312
Coasting Arc #15 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2019/276/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965355
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4075194
67 A = 6792672
74 meter
Y = 3187192
47 meter E =
0016582
Z = -4418576
17 I = 51
59871
XDOT = -6103
783293 Wp = 110
41197
YDOT = -3157
617661 meter/sec RA = 184
57788 deg
ZDOT = 3356
403018 TA = 193
62131
MA = 193
66612
Ha = 229
954 n
mi
Hp = 218
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13370061
24 X = -4089068
57
Y = 10456668
21 feet Y = 3141543
00 meter
Z = -14496640
98 Z = -4438406
09
XDOT = -20025
535737 XDOT = -6084
324051
YDOT = -10359
637994 feet/sec YDOT = -3225
765522 meter/sec
ZDOT = 11011
820926 ZDOT = 3326
800059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5477147
28 X = 1669434
49
Y = 15983455
91 feet Y = 4871757
36 meter
Z = -14587084
78 Z = -4446143
44
XDOT = -15258
741538 XDOT = -4650
864421
YDOT = 15141
994580 feet/sec YDOT = 4615
279948 meter/sec
ZDOT = 10877
163120 ZDOT = 3315
359319
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 19276
17680029
00016717 00000-0 10270-3 0 9140
2 25544 51
6417 185
7492 0007415 109
2111 250
9842 15
50127421 32007
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
17680029 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 185
7492 deg
Eccentricity:
0007415
Arg of perigee: 109
2111 deg
Mean anomaly: 250
9842 deg
Mean motion: 15
50127421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 291
Coasting Arc #16 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/276/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2760496
44 A = 6791406
40 meter
Y = -3969246
82 meter E =
0014886
Z = 4760358
95 I = 51
59637
XDOT = 6996
730684 Wp = 114
31835
YDOT = -1647
798537 meter/sec RA = 183
87716 deg
ZDOT = 2670
805037 TA = 309
22774
MA = 309
35978
Ha = 229
923 n
mi
Hp = 218
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9056746
85 X = -2739029
55
Y = -13022463
33 feet Y = -3999996
42 meter
Z = 15617975
55 Z = 4747001
59
XDOT = 22955
153162 XDOT = 7001
663342
YDOT = -5406
163178 feet/sec YDOT = -1569
528469 meter/sec
ZDOT = 8762
483716 ZDOT = 2704
805104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5422776
51 X = -1652862
28
Y = 14969747
43 feet Y = 4562779
02 meter
Z = 15557330
49 Z = 4741874
33
XDOT = -16457
075419 XDOT = -5016
116588
YDOT = -15272
065883 feet/sec YDOT = -4654
925681 meter/sec
ZDOT = 8917
386829 ZDOT = 2718
019506
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 19276
37020356
00016717 00000-0 10270-3 0 9154
2 25544 51
6387 184
7914 0007206 110
0977 250
0950 15
50151191 32034
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
37020356 = yrday
fracday
Element set: 915
Inclination: 51
6387 deg
RA of node: 184
7914 deg
Eccentricity:
0007206
Arg of perigee: 110
0977 deg
Mean anomaly: 250
0950 deg
Mean motion: 15
50151191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 292
Coasting Arc #17 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2019/277/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2629165
73 A = 6790793
53 meter
Y = 3864369
39 meter E =
0018298
Z = -4942377
80 I = 51
62805
XDOT = -7051
117204 Wp = 88
51902
YDOT = 1920
132660 meter/sec RA = 178
91769 deg
ZDOT = -2256
401052 TA = 159
41309
MA = 159
33927
Ha = 229
901 n
mi
Hp = 218
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8625871
81 X = 2609765
45
Y = 12678377
27 feet Y = 3893661
95 meter
Z = -16215150
26 Z = -4929653
38
XDOT = -23133
586627 XDOT = -7061
104149
YDOT = 6299
647834 feet/sec YDOT = 1841
226182 meter/sec
ZDOT = -7402
890590 ZDOT = -2290
677478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5136412
64 X = 1565578
57
Y = -14513253
07 feet Y = -4423639
54 meter
Z = -16157374
88 Z = -4924767
86
XDOT = 17590
815491 XDOT = 5361
680562
YDOT = 14616
143262 feet/sec YDOT = 4455
000466 meter/sec
ZDOT = -7559
089419 ZDOT = -2304
010455
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 19277
33722147
00016717 00000-0 10270-3 0 9169
2 25544 51
6393 179
9987 0007292 113
0624 247
1296 15
50125681 32185
Satellite: ISS
Catalog Number: 25544
Epoch time: 19277
33722147 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 179
9987 deg
Eccentricity:
0007292
Arg of perigee: 113
0624 deg
Mean anomaly: 247
1296 deg
Mean motion: 15
50125681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 328
Coasting Arc #18 (Orbit 3233)
---------------------------------------
Vector Time (GMT): 2019/278/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2512184
40 A = 6790116
87 meter
Y = -3757816
31 meter E =
0012765
Z = 5059168
83 I = 51
66012
XDOT = 7097
759193 Wp = 120
31455
YDOT = -2229
128630 meter/sec RA = 173
96225 deg
ZDOT = 1858
927032 TA = 311
62765
MA = 311
73692
Ha = 229
828 n
mi
Hp = 218
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8242074
81 X = -2494551
56
Y = -12328793
68 feet Y = -3785810
59 meter
Z = 16598322
93 Z = 5047008
41
XDOT = 23286
611526 XDOT = 7113
128717
YDOT = -7313
414141 feet/sec YDOT = -2149
670488 meter/sec
ZDOT = 6098
841967 ZDOT = 1893
442994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4835564
87 X = -1473880
17
Y = 14084683
76 feet Y = 4293011
61 meter
Z = 16543103
41 Z = 5042337
92
XDOT = -18784
840903 XDOT = -5725
619507
YDOT = -13835
289410 feet/sec YDOT = -4216
996212 meter/sec
ZDOT = 6256
171217 ZDOT = 1906
880987
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 19278
36870184
00016717 00000-0 10270-3 0 9179
2 25544 51
6398 174
8884 0007118 116
6388 243
5492 15
50165715 32341
Satellite: ISS
Catalog Number: 25544
Epoch time: 19278
36870184 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 174
8884 deg
Eccentricity:
0007118
Arg of perigee: 116
6388 deg
Mean anomaly: 243
5492 deg
Mean motion: 15
50165715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3234
Checksum: 344
Coasting Arc #19 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2019/279/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2360716
76 A = 6789730
49 meter
Y = 3715260
25 meter E =
0019731
Z = -5186395
04 I = 51
69125
XDOT = -7078
887485 Wp = 93
00915
YDOT = 2520
005751 meter/sec RA = 169
00683 deg
ZDOT = -1422
627328 TA = 163
30974
MA = 163
24471
Ha = 229
793 n
mi
Hp = 218
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7745133
74 X = 2344188
97
Y = 12189174
06 feet Y = 3741566
86 meter
Z = -17015731
75 Z = -5174967
76
XDOT = -23224
696472 XDOT = -7099
630426
YDOT = 8267
735404 feet/sec YDOT = 2440
728606 meter/sec
ZDOT = -4667
412495 ZDOT = -1457
064587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4786023
99 X = 1458780
11
Y = -13690150
28 feet Y = -4172757
81 meter
Z = -16963842
35 Z = -5170579
15
XDOT = 19775
579731 XDOT = 6027
596702
YDOT = 12868
317035 feet/sec YDOT = 3922
263032 meter/sec
ZDOT = -4824
421154 ZDOT = -1470
483568
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 19279
33571457
00016717 00000-0 10270-3 0 9189
2 25544 51
6395 170
0960 0007180 119
4869 240
6998 15
50133987 32496
Satellite: ISS
Catalog Number: 25544
Epoch time: 19279
33571457 = yrday
fracday
Element set: 918
Inclination: 51
6395 deg
RA of node: 170
0960 deg
Eccentricity:
0007180
Arg of perigee: 119
4869 deg
Mean anomaly: 240
6998 deg
Mean motion: 15
50133987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 349
Coasting Arc #20 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2019/280/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2228933
23 A = 6789254
09 meter
Y = -3672192
19 meter E =
0010758
Z = 5250599
67 I = 51
72327
XDOT = 7053
101830 Wp = 123
81428
YDOT = -2837
536108 meter/sec RA = 164
05577 deg
ZDOT = 1002
259313 TA = 316
55936
MA = 316
64408
Ha = 229
727 n
mi
Hp = 218
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7312773
06 X = -2213208
66
Y = -12047874
65 feet Y = -3697029
54 meter
Z = 17226376
88 Z = 5239810
66
XDOT = 23140
097869 XDOT = 7079
439341
YDOT = -9309
501667 feet/sec YDOT = -2758
516040 meter/sec
ZDOT = 3288
252340 ZDOT = 1036
584873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4710455
95 X = -1435746
97
Y = 13346347
37 feet Y = 4067966
68 meter
Z = 17177386
60 Z = 5235667
44
XDOT = -20788
464474 XDOT = -6336
323972
YDOT = -11801
695928 feet/sec YDOT = -3597
156919 meter/sec
ZDOT = 3444
789798 ZDOT = 1049
971931
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 19280
36719133
00016717 00000-0 10270-3 0 9190
2 25544 51
6401 164
9861 0007043 123
8842 236
2980 15
50172406 32653
Satellite: ISS
Catalog Number: 25544
Epoch time: 19280
36719133 = yrday
fracday
Element set: 919
Inclination: 51
6401 deg
RA of node: 164
9861 deg
Eccentricity:
0007043
Arg of perigee: 123
8842 deg
Mean anomaly: 236
2980 deg
Mean motion: 15
50172406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 307
Coasting Arc #21 (Orbit 3279)
---------------------------------------
Vector Time (GMT): 2019/281/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 950247
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2078541
61 A = 6789100
61 meter
Y = 3694854
06 meter E =
0020469
Z = -5320015
84 I = 51
75507
XDOT = -6958
051010 Wp = 99
08112
YDOT = 3123
802721 meter/sec RA = 159
10415 deg
ZDOT = -553
952420 TA = 165
65580
MA = 165
59760
Ha = 229
651 n
mi
Hp = 218
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6819362
25 X = 2062911
98
Y = 12122224
61 feet Y = 3718010
08 meter
Z = -17454120
20 Z = -5309957
20
XDOT = -22828
251344 XDOT = -6989
774338
YDOT = 10248
696590 feet/sec YDOT = 3045
815476 meter/sec
ZDOT = -1817
429198 ZDOT = -587
829370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4852632
58 X = 1479082
41
Y = -13095649
97 feet Y = -3991554
11 meter
Z = -17408453
46 Z = -5306096
62
XDOT = 21539
571953 XDOT = 6565
261531
YDOT = 10581
210819 feet/sec YDOT = 3225
153058 meter/sec
ZDOT = -1971
956832 ZDOT = -601
052442
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 19281
33419932
00016717 00000-0 10270-3 0 9204
2 25544 51
6409 160
1936 0007059 127
1271 233
0526 15
50146194 32805
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
33419932 = yrday
fracday
Element set: 920
Inclination: 51
6409 deg
RA of node: 160
1936 deg
Eccentricity:
0007059
Arg of perigee: 127
1271 deg
Mean anomaly: 233
0526 deg
Mean motion: 15
50146194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3280
Checksum: 293
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