[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 16th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13747 6664 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
136/05:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
1
137/07:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 217
1
143/14:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
5
000/00:00:00
000 0
0 0
0 216
7
143/16:02:53
424 -2
1 7
1 7
1
N/A 6
7 -0
7 223
7
000/00:19:46
849 -1
1 -0
1 221
4
143/19:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
8
000/00:00:00
000 0
0 0
0 221
4
143/21:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
6
000/00:00:00
000 0
0 0
0 221
4
144/08:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 221
2
147/06:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 221
4
Coasting Arc #1 (Orbit 1016)
---------------------------------------
Vector Time (GMT): 2019/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -331910
55 A = 6782299
47 meter
Y = 4386180
56 meter E =
0013285
Z = -5174131
24 I = 51
73375
XDOT = -7428
484802 Wp = 94
98450
YDOT = 1149
831364 meter/sec RA = 162
42894 deg
ZDOT = 1453
340420 TA = 188
99482
MA = 189
01865
Ha = 223
268 n
mi
Hp = 217
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1088945
37 X = -355800
05
Y = 14390356
17 feet Y = 4382335
46 meter
Z = -16975496
18 Z = -5175801
46
XDOT = -24371
669299 XDOT = -7447
850048
YDOT = 3772
412613 feet/sec YDOT = 1066
652529 meter/sec
ZDOT = 4768
177230 ZDOT = 1417
208187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10745452
33 X = 3275213
87
Y = 9619535
62 feet Y = 2932034
46 meter
Z = -16983386
35 Z = -5176536
16
XDOT = -11334
115953 XDOT = -3454
638543
YDOT = 20777
717832 feet/sec YDOT = 6333
048395 meter/sec
ZDOT = 4604
393341 ZDOT = 1403
419090
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 19135
51368911
00016717 00000-0 10270-3 0 9000
2 25544 51
6402 163
5519 0001561 346
8371 13
2740 15
52655710 10178
Satellite: ISS
Catalog Number: 25544
Epoch time: 19135
51368911 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 163
5519 deg
Eccentricity:
0001561
Arg of perigee: 346
8371 deg
Mean anomaly: 13
2740 deg
Mean motion: 15
52655710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1017
Checksum: 282
Coasting Arc #2 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2019/136/05:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3832073
11 A = 6788499
39 meter
Y = -4409069
18 meter E =
0012037
Z = 3449061
49 I = 51
77696
XDOT = 5941
438519 Wp = 84
24546
YDOT = 1562
791215 meter/sec RA = 158
70559 deg
ZDOT = -4588
509821 TA = 55
42597
MA = 55
31246
Ha = 223
190 n
mi
Hp = 217
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12572418
34 X = 3864337
90
Y = -14465450
06 feet Y = -4366035
97 meter
Z = 11315818
55 Z = 3467754
76
XDOT = 19492
908527 XDOT = 5945
810127
YDOT = 5127
267766 feet/sec YDOT = 1629
257141 meter/sec
ZDOT = -15054
166079 ZDOT = -4559
637435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18782476
07 X = 5724898
70
Y = -3549933
29 feet Y = -1082019
67 meter
Z = 11400844
89 Z = 3474977
52
XDOT = 11891
573635 XDOT = 3624
551644
YDOT = 14833
672851 feet/sec YDOT = 4521
303485 meter/sec
ZDOT = -14923
463713 ZDOT = -4548
671740
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 19136
28603785
00016717 00000-0 10270-3 0 9017
2 25544 51
6390 159
7070 0001108 344
0954 16
0162 15
52656675 10290
Satellite: ISS
Catalog Number: 25544
Epoch time: 19136
28603785 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 159
7070 deg
Eccentricity:
0001108
Arg of perigee: 344
0954 deg
Mean anomaly: 16
0162 deg
Mean motion: 15
52656675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 301
Coasting Arc #3 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2019/137/05:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4569615
08 A = 6791031
12 meter
Y = 4390398
19 meter E =
0006151
Z = -2436487
75 I = 51
81706
XDOT = -4999
364236 Wp = 37
10766
YDOT = -2235
012722 meter/sec RA = 153
74633 deg
ZDOT = 5360
748209 TA = 295
72689
MA = 295
79037
Ha = 223
210 n
mi
Hp = 217
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14992175
46 X = -4606534
82
Y = 14404193
53 feet Y = 4339091
25 meter
Z = -7993726
23 Z = -2458775
07
XDOT = -16402
113635 XDOT = -5000
040124
YDOT = -7332
718904 feet/sec YDOT = -2290
923176 meter/sec
ZDOT = 17587
756592 ZDOT = 5336
460976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20619167
51 X = -6284722
26
Y = 2337906
66 feet Y = 712593
95 meter
Z = -8095053
97 Z = -2467372
45
XDOT = -8475
806707 XDOT = -2583
425884
YDOT = -14367
564291 feet/sec YDOT = -4379
233596 meter/sec
ZDOT = 17477
870131 ZDOT = 5327
254816
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 19137
25146880
00016717 00000-0 10270-3 0 9024
2 25544 51
6400 154
9050 0001398 344
7408 15
3701 15
52656512 10447
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
25146880 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 154
9050 deg
Eccentricity:
0001398
Arg of perigee: 344
7408 deg
Mean anomaly: 15
3701 deg
Mean motion: 15
52656512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1044
Checksum: 285
Coasting Arc #4 (Orbit 1045)
---------------------------------------
Vector Time (GMT): 2019/137/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5847817
47 A = 6788612
71 meter
Y = -94838
66 meter E =
0012139
Z = 3434916
77 I = 51
81116
XDOT = 2801
783248 Wp = 84
01952
YDOT = -5454
188435 meter/sec RA = 153
41418 deg
ZDOT = 4606
602885 TA = 316
09562
MA = 316
19203
Ha = 223
285 n
mi
Hp = 217
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19185752
85 X = -5863007
55
Y = -311150
44 feet Y = -160318
17 meter
Z = 11269411
97 Z = 3406472
85
XDOT = 9192
202258 XDOT = 2840
188582
YDOT = -17894
319014 feet/sec YDOT = -5422
642446 meter/sec
ZDOT = 15113
526525 ZDOT = 4620
306128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18919954
19 X = -5766802
04
Y = -3621268
98 feet Y = -1103762
79 meter
Z = 11140525
91 Z = 3395632
30
XDOT = 11770
978389 XDOT = 3587
794213
YDOT = -14681
700839 feet/sec YDOT = -4474
982416 meter/sec
ZDOT = 15176
038076 ZDOT = 4625
656406
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 19137
38019148
00016717 00000-0 10270-3 0 9035
2 25544 51
6398 154
2657 0001351 343
9260 16
1849 15
52696594 10463
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
38019148 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 154
2657 deg
Eccentricity:
0001351
Arg of perigee: 343
9260 deg
Mean anomaly: 16
1849 deg
Mean motion: 15
52696594 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1046
Checksum: 322
Coasting Arc #5 (Orbit 1060)
---------------------------------------
Vector Time (GMT): 2019/138/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5203654
26 A = 6785885
12 meter
Y = 768128
48 meter E =
0008577
Z = -4296347
66 I = 51
83031
XDOT = -3780
134888 Wp = 60
75723
YDOT = 5618
565856 meter/sec RA = 148
45207 deg
ZDOT = -3575
203319 TA = 172
81786
MA = 172
80557
Ha = 223
271 n
mi
Hp = 217
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17072356
49 X = 5215547
74
Y = 2520106
56 feet Y = 826386
23 meter
Z = -14095628
82 Z = -4271040
83
XDOT = -12402
017349 XDOT = -3825
315665
YDOT = 18433
615014 feet/sec YDOT = 5576
041402 meter/sec
ZDOT = -11729
669683 ZDOT = -3593
675441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16567692
62 X = 5049832
71
Y = 5152313
45 feet Y = 1570425
14 meter
Z = -13980996
84 Z = -4261407
84
XDOT = -14658
271861 XDOT = -4467
841263
YDOT = 15089
293700 feet/sec YDOT = 4599
216720 meter/sec
ZDOT = -11813
825312 ZDOT = -3600
853955
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 19138
34562066
00016717 00000-0 10270-3 0 9045
2 25544 51
6389 149
4637 0001441 350
0635 10
0488 15
52674946 10618
Satellite: ISS
Catalog Number: 25544
Epoch time: 19138
34562066 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 149
4637 deg
Eccentricity:
0001441
Arg of perigee: 350
0635 deg
Mean anomaly: 10
0488 deg
Mean motion: 15
52674946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1061
Checksum: 307
Coasting Arc #6 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2019/139/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4432390
82 A = 6783397
82 meter
Y = -1510973
36 meter E =
0006122
Z = 4903487
33 I = 51
85010
XDOT = 4563
172659 Wp = 109
93762
YDOT = -5691
253735 meter/sec RA = 143
48640 deg
ZDOT = 2366
622386 TA = 316
93349
MA = 316
98138
Ha = 223
396 n
mi
Hp = 216
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14541964
64 X = -4438984
10
Y = -4957261
68 feet Y = -1560576
83 meter
Z = 16087556
86 Z = 4881939
89
XDOT = 14971
038908 XDOT = 4614
978796
YDOT = -18672
092307 feet/sec YDOT = -5639
935724 meter/sec
ZDOT = 7764
509141 ZDOT = 2388
914200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13824355
54 X = -4213663
57
Y = -6932490
23 feet Y = -2113023
02 meter
Z = 15990010
57 Z = 4873755
22
XDOT = 16849
543228 XDOT = 5135
740776
YDOT = -15423
411404 feet/sec YDOT = -4701
055796 meter/sec
ZDOT = 7866
007249 ZDOT = 2397
559009
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 19139
37540803
00016717 00000-0 10270-3 0 9055
2 25544 51
6389 144
3411 0001484 353
9990 6
1143 15
52705843 10777
Satellite: ISS
Catalog Number: 25544
Epoch time: 19139
37540803 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 144
3411 deg
Eccentricity:
0001484
Arg of perigee: 353
9990 deg
Mean anomaly: 6
1143 deg
Mean motion: 15
52705843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1077
Checksum: 306
Coasting Arc #7 (Orbit 1091)
---------------------------------------
Vector Time (GMT): 2019/140/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598009
97 A = 6781979
14 meter
Y = 2335789
19 meter E =
0014493
Z = -5265620
51 I = 51
87059
XDOT = -5123
610935 Wp = 76
36297
YDOT = 5596
150988 meter/sec RA = 138
51878 deg
ZDOT = -1017
589147 TA = 183
90262
MA = 183
91393
Ha = 223
343 n
mi
Hp = 217
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11804494
66 X = 3597200
93
Y = 7663350
37 feet Y = 2376020
79 meter
Z = -17275657
84 Z = -5248144
14
XDOT = -16809
747163 XDOT = -5180
864937
YDOT = 18360
075420 feet/sec YDOT = 5538
535184 meter/sec
ZDOT = -3338
547069 ZDOT = -1042
616461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10904529
85 X = 3323700
70
Y = 9049239
35 feet Y = 2758208
15 meter
Z = -17196624
18 Z = -5241531
05
XDOT = -18226
827230 XDOT = -5555
536940
YDOT = 15396
759446 feet/sec YDOT = 4692
932279 meter/sec
ZDOT = -3452
464656 ZDOT = -1052
311227
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 19140
34083370
00016717 00000-0 10270-3 0 9066
2 25544 51
6383 139
5390 0001498 356
9842 3
1301 15
52668922 10923
Satellite: ISS
Catalog Number: 25544
Epoch time: 19140
34083370 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 139
5390 deg
Eccentricity:
0001498
Arg of perigee: 356
9842 deg
Mean anomaly: 3
1301 deg
Mean motion: 15
52668922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1092
Checksum: 303
Coasting Arc #8 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2019/141/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2726202
39 A = 6781492
97 meter
Y = -3192204
26 meter E =
0003434
Z = 5323934
21 I = 51
89483
XDOT = 5492
100875 Wp = 47
88643
YDOT = -5337
956933 meter/sec RA = 133
55081 deg
ZDOT = -385
894271 TA = 45
79431
MA = 45
76611
Ha = 223
417 n
mi
Hp = 216
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8944233
55 X = -2716164
62
Y = -10473111
09 feet Y = -3222635
16 meter
Z = 17466975
76 Z = 5310715
14
XDOT = 18018
703659 XDOT = 5553
257726
YDOT = -17512
982065 feet/sec YDOT = -5276
198416 meter/sec
ZDOT = -1266
057320 ZDOT = -359
067603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7922956
07 X = -2414917
01
Y = -11357505
81 feet Y = -3461767
77 meter
Z = 17407309
98 Z = 5305748
08
XDOT = 18922
210764 XDOT = 5767
489841
YDOT = -14965
531154 feet/sec YDOT = -4561
493896 meter/sec
ZDOT = -1143
975832 ZDOT = -348
683834
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 19141
37061532
00016717 00000-0 10270-3 0 9077
2 25544 51
6393 134
4165 0001619 1
7600 358
3557 15
52719225 11089
Satellite: ISS
Catalog Number: 25544
Epoch time: 19141
37061532 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 134
4165 deg
Eccentricity:
0001619
Arg of perigee: 1
7600 deg
Mean anomaly: 358
3557 deg
Mean motion: 15
52719225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1108
Checksum: 290
Coasting Arc #9 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2019/142/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1892123
18 A = 6782545
49 meter
Y = 4050904
84 meter E =
0013351
Z = -5112089
89 I = 51
92009
XDOT = -5646
253797 Wp = 95
63322
YDOT = 4860
279304 meter/sec RA = 128
58521 deg
ZDOT = 1764
215826 TA = 191
37404
MA = 191
40424
Ha = 223
492 n
mi
Hp = 216
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6207753
22 X = 1871516
03
Y = 13290370
21 feet Y = 4071949
37 meter
Z = -16771948
45 Z = -5102948
09
XDOT = -18524
454715 XDOT = -5708
752820
YDOT = 15945
798241 feet/sec YDOT = 4796
789245 meter/sec
ZDOT = 5788
109664 ZDOT = 1736
637127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5141678
08 X = 1567183
48
Y = 13788054
16 feet Y = 4202598
91 meter
Z = -16730842
90 Z = -5099560
92
XDOT = -18872
603850 XDOT = -5752
369654
YDOT = 13898
256361 feet/sec YDOT = 4236
188539 meter/sec
ZDOT = 5662
632584 ZDOT = 1725
970412
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 19142
33603556
00016717 00000-0 10270-3 0 9083
2 25544 51
6392 129
6143 0001780 10
3460 349
7728 15
52685878 11236
Satellite: ISS
Catalog Number: 25544
Epoch time: 19142
33603556 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 129
6143 deg
Eccentricity:
0001780
Arg of perigee: 10
3460 deg
Mean anomaly: 349
7728 deg
Mean motion: 15
52685878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 313
Coasting Arc #10 (Orbit 1138)
---------------------------------------
Vector Time (GMT): 2019/143/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1090339
93 A = 6784459
90 meter
Y = -4862445
39 meter E =
0009610
Z = 4599555
37 I = 51
94660
XDOT = 5656
030713 Wp = 57
93058
YDOT = -4174
971215 meter/sec RA = 123
62447 deg
ZDOT = -3063
170562 TA = 62
60142
MA = 62
50368
Ha = 223
454 n
mi
Hp = 216
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3577230
75 X = -1058227
80
Y = -15952904
82 feet Y = -4874459
38 meter
Z = 15090404
76 Z = 4594336
25
XDOT = 18556
531212 XDOT = 5717
175291
YDOT = -13697
412124 feet/sec YDOT = -4111
379240 meter/sec
ZDOT = -10049
772184 ZDOT = -3035
547628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2557121
43 X = -779410
61
Y = -16169534
00 feet Y = -4928473
96 meter
Z = 15067161
90 Z = 4592470
95
XDOT = 18354
245871 XDOT = 5594
374142
YDOT = -12179
689641 feet/sec YDOT = -3712
369403 meter/sec
ZDOT = -9924
130604 ZDOT = -3024
875008
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 19143
36581289
00016717 00000-0 10270-3 0 9096
2 25544 51
6389 124
4924 0001712 12
0503 348
0689 15
52730207 11396
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
36581289 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 124
4924 deg
Eccentricity:
0001712
Arg of perigee: 12
0503 deg
Mean anomaly: 348
0689 deg
Mean motion: 15
52730207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1139
Checksum: 306
Coasting Arc #11 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2019/143/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965984
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 259490
75 A = 6787852
15 meter
Y = -5723272
31 meter E =
0012617
Z = 3632206
34 I = 51
96206
XDOT = 5716
166802 Wp = 77
51601
YDOT = -2558
682593 meter/sec RA = 122
33177 deg
ZDOT = -4424
509087 TA = 59
65266
MA = 59
52795
Ha = 223
507 n
mi
Hp = 216
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 851347
60 X = 305827
44
Y = -18777140
13 feet Y = -5720111
88 meter
Z = 11916687
48 Z = 3633578
67
XDOT = 18753
828090 XDOT = 5765
845743
YDOT = -8394
627930 feet/sec YDOT = -2494
482077 meter/sec
ZDOT = -14516
105930 ZDOT = -4396
621683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18776434
78 X = -5723057
32
Y = -768680
00 feet Y = -234293
66 meter
Z = 11923416
14 Z = 3634257
24
XDOT = -8454
387124 XDOT = -2576
897195
YDOT = -17480
370445 feet/sec YDOT = -5328
016912 meter/sec
ZDOT = -14389
401809 ZDOT = -4385
889671
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 19143
62325853
00016717 00000-0 10270-3 0 9100
2 25544 51
6384 123
2120 0002000 12
5604 347
5597 15
52714153 11433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
62325853 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 123
2120 deg
Eccentricity:
0002000
Arg of perigee: 12
5604 deg
Mean anomaly: 347
5597 deg
Mean motion: 15
52714153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 267
Coasting Arc #12 (Orbit 1143)
---------------------------------------
Vector Time (GMT): 2019/143/16:12:46
849
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1888491
43 A = 6787699
07 meter
Y = 4272089
44 meter E =
0006985
Z = -4931516
87 I = 51
94942
XDOT = -5280
847690 Wp = 117
72741
YDOT = 5030
293339 meter/sec RA = 121
88099 deg
ZDOT = 2334
756915 TA = 175
05469
MA = 175
04778
Ha = 223
676 n
mi
Hp = 221
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6195838
04 X = 1864533
98
Y = 14016041
49 feet Y = 4293074
55 meter
Z = -16179517
29 Z = -4922400
91
XDOT = -17325
615782 XDOT = -5348
046359
YDOT = 16503
587071 feet/sec YDOT = 4970
863177 meter/sec
ZDOT = 7659
963633 ZDOT = 2308
941898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8253896
16 X = 2515787
55
Y = -12962831
34 feet Y = -3951070
99 meter
Z = -16138550
42 Z = -4919030
17
XDOT = 22388
603919 XDOT = 6824
046474
YDOT = 4862
784027 feet/sec YDOT = 1482
176572 meter/sec
ZDOT = 7542
438559 ZDOT = 2298
935273
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 19143
68762639
00016717 00000-0 10270-3 0 9114
2 25544 51
6396 122
8905 0005404 272
7392 87
3141 15
51181178 11446
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
68762639 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 122
8905 deg
Eccentricity:
0005404
Arg of perigee: 272
7392 deg
Mean anomaly: 87
3141 deg
Mean motion: 15
51181178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1144
Checksum: 314
Coasting Arc #13 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/19:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4362984
28 A = 6786826
65 meter
Y = -598361
63 meter E =
0002861
Z = 5165899
84 I = 51
94912
XDOT = 2792
387297 Wp = 211
78672
YDOT = -6964
779585 meter/sec RA = 121
14987 deg
ZDOT = 1549
676543 TA = 223
31930
MA = 223
34179
Ha = 223
835 n
mi
Hp = 221
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14314252
89 X = -4381062
08
Y = -1963128
72 feet Y = -647253
30 meter
Z = 16948490
30 Z = 5144662
07
XDOT = 9161
375647 XDOT = 2862
534431
YDOT = -22850
326722 feet/sec YDOT = -6933
161132 meter/sec
ZDOT = 5084
240627 ZDOT = 1563
410447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14391234
37 X = 4386448
23
Y = 2213158
85 feet Y = 674570
82 meter
Z = 16852220
48 Z = 5136556
80
XDOT = -9362
579125 XDOT = -2853
714117
YDOT = 21637
987494 feet/sec YDOT = 6595
258588 meter/sec
ZDOT = 5147
146918 ZDOT = 1568
850380
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 19143
88089899
00016717 00000-0 10270-3 0 9127
2 25544 51
6398 121
9319 0005490 273
8827 86
1696 15
51158885 11471
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88089899 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 121
9319 deg
Eccentricity:
0005490
Arg of perigee: 273
8827 deg
Mean anomaly: 86
1696 deg
Mean motion: 15
51158885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 362
Coasting Arc #14 (Orbit 1146)
---------------------------------------
Vector Time (GMT): 2019/143/21:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2568854
44 A = 6797268
02 meter
Y = 6166600
75 meter E =
0007403
Z = -1228881
93 I = 51
98325
XDOT = -4845
144606 Wp = 359
38055
YDOT = -848
715321 meter/sec RA = 120
88376 deg
ZDOT = 5876
251845 TA = 347
34329
MA = 347
36187
Ha = 223
578 n
mi
Hp = 221
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8428000
12 X = -2631650
97
Y = 20231629
75 feet Y = 6137523
05 meter
Z = -4031764
87 Z = -1241512
25
XDOT = -15896
143722 XDOT = -4863
837547
YDOT = -2784
499085 feet/sec YDOT = -903
002369 meter/sec
ZDOT = 19279
041486 ZDOT = 5852
670394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2290112
47 X = 698026
28
Y = -21786136
55 feet Y = -6640414
42 meter
Z = -4089596
01 Z = -1246508
86
XDOT = 14565
371652 XDOT = 4439
525280
YDOT = -2063
663213 feet/sec YDOT = -629
004547 meter/sec
ZDOT = 19172
163512 ZDOT = 5843
675438
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 19143
88089774
00016717 00000-0 10270-3 0 9130
2 25544 51
6379 121
9302 0005665 272
7869 87
2634 15
51175606 11474
Satellite: ISS
Catalog Number: 25544
Epoch time: 19143
88089774 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 121
9302 deg
Eccentricity:
0005665
Arg of perigee: 272
7869 deg
Mean anomaly: 87
2634 deg
Mean motion: 15
51175606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1147
Checksum: 338
Coasting Arc #15 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2019/144/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 490000
77 A = 6793724
93 meter
Y = -6011692
89 meter E =
0007703
Z = 3118810
10 I = 51
98094
XDOT = 5502
725382 Wp = 95
87572
YDOT = -2100
192303 meter/sec RA = 118
50459 deg
ZDOT = -4903
172225 TA = 48
46101
MA = 48
39497
Ha = 223
707 n
mi
Hp = 221
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1607614
08 X = 542039
36
Y = -19723401
86 feet Y = -6005922
76 meter
Z = 10232316
59 Z = 3121316
02
XDOT = 18053
560964 XDOT = 5549
618267
YDOT = -6890
394694 feet/sec YDOT = -2038
394202 meter/sec
ZDOT = -16086
523048 ZDOT = -4876
328370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1744726
76 X = -531792
72
Y = -19705562
39 feet Y = -6006255
42 meter
Z = 10244220
13 Z = 3122438
30
XDOT = 15333
960199 XDOT = 4673
791069
YDOT = -9673
462633 feet/sec YDOT = -2948
471411 meter/sec
ZDOT = -15964
579339 ZDOT = -4866
003783
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 19144
39629328
00016717 00000-0 10270-3 0 9143
2 25544 51
6391 119
3729 0005237 274
1701 85
8851 15
51204126 11552
Satellite: ISS
Catalog Number: 25544
Epoch time: 19144
39629328 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 119
3729 deg
Eccentricity:
0005237
Arg of perigee: 274
1701 deg
Mean anomaly: 85
8851 deg
Mean motion: 15
51204126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 309
Coasting Arc #16 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2019/145/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -613672
74 A = 6795148
41 meter
Y = 6286600
30 meter E =
0004273
Z = -2497542
32 I = 52
00223
XDOT = -5253
488469 Wp = 345
55412
YDOT = 1608
117538 meter/sec RA = 113
56805 deg
ZDOT = 5340
712207 TA = 346
63175
MA = 346
64307
Ha = 223
768 n
mi
Hp = 221
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2013362
01 X = -671794
01
Y = 20625329
06 feet Y = 6279413
06 meter
Z = -8194036
49 Z = -2500663
83
XDOT = -17235
854557 XDOT = -5297
022670
YDOT = 5275
976175 feet/sec YDOT = 1549
125378 meter/sec
ZDOT = 17522
021676 ZDOT = 5315
087147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1835551
03 X = 559475
95
Y = 20636059
32 feet Y = 6289870
88 meter
Z = -8208767
72 Z = -2502032
40
XDOT = -14594
919516 XDOT = -4448
531468
YDOT = 8219
264170 feet/sec YDOT = 2505
231719 meter/sec
ZDOT = 17405
636724 ZDOT = 5305
238074
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 19145
36265697
00016717 00000-0 10270-3 0 9157
2 25544 51
6406 114
5769 0005160 277
5202 82
5363 15
51220554 11700
Satellite: ISS
Catalog Number: 25544
Epoch time: 19145
36265697 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 114
5769 deg
Eccentricity:
0005160
Arg of perigee: 277
5202 deg
Mean anomaly: 82
5363 deg
Mean motion: 15
51220554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 301
Coasting Arc #17 (Orbit 1185)
---------------------------------------
Vector Time (GMT): 2019/146/08:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 699828
59 A = 6796468
67 meter
Y = -6507571
66 meter E =
0008937
Z = 1813757
28 I = 52
01663
XDOT = 5034
905678 Wp = 121
03230
YDOT = -1046
678459 meter/sec RA = 108
63442 deg
ZDOT = -5681
879778 TA = 39
16283
MA = 39
09819
Ha = 223
916 n
mi
Hp = 221
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2296025
54 X = 763735
86
Y = -21350300
72 feet Y = -6499388
52 meter
Z = 5950647
26 Z = 1817311
41
XDOT = 16518
719417 XDOT = 5073
835175
YDOT = -3433
984445 feet/sec YDOT = -990
156428 meter/sec
ZDOT = -18641
337854 ZDOT = -5657
327607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2042985
91 X = -622702
10
Y = -21371334
72 feet Y = -6513982
82 meter
Z = 5967372
76 Z = 1818855
22
XDOT = 14066
845939 XDOT = 4287
574642
YDOT = -6533
467960 feet/sec YDOT = -1991
401034 meter/sec
ZDOT = -18529
860754 ZDOT = -5647
901558
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 19146
39344311
00016717 00000-0 10270-3 0 9163
2 25544 51
6385 109
4614 0005159 282
5531 77
5043 15
51196551 11862
Satellite: ISS
Catalog Number: 25544
Epoch time: 19146
39344311 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 109
4614 deg
Eccentricity:
0005159
Arg of perigee: 282
5531 deg
Mean anomaly: 77
5043 deg
Mean motion: 15
51196551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1186
Checksum: 309
Coasting Arc #18 (Orbit 1199)
---------------------------------------
Vector Time (GMT): 2019/147/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4380590
33 A = 6787891
33 meter
Y = -1713056
51 meter E =
0007789
Z = -4901103
46 I = 51
99789
XDOT = 124
550921 Wp = 51
68899
YDOT = 7262
114348 meter/sec RA = 104
13847 deg
ZDOT = -2424
878932 TA = 194
60400
MA = 194
62652
Ha = 223
958 n
mi
Hp = 221
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14372015
51 X = 4423227
54
Y = -5620264
13 feet Y = -1663830
88 meter
Z = -16079735
75 Z = -4879720
71
XDOT = 408
631629 XDOT = 55
113376
YDOT = 23825
834475 feet/sec YDOT = 7263
119113 meter/sec
ZDOT = -7955
639542 ZDOT = -2424
441965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15497156
13 X = 4723533
19
Y = -1046802
42 feet Y = -319065
38 meter
Z = -15982567
29 Z = -4871486
51
XDOT = -6741
517400 XDOT = -2054
814504
YDOT = 21748
595575 feet/sec YDOT = 6628
971931 meter/sec
ZDOT = -7954
340923 ZDOT = -2424
483113
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 19147
29537980
00016717 00000-0 10270-3 0 9170
2 25544 51
6397 104
9842 0005319 284
3582 75
6979 15
51183454 12004
Satellite: ISS
Catalog Number: 25544
Epoch time: 19147
29537980 = yrday
fracday
Element set: 917
Inclination: 51
6397 deg
RA of node: 104
9842 deg
Eccentricity:
0005319
Arg of perigee: 284
3582 deg
Mean anomaly: 75
6979 deg
Mean motion: 15
51183454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1200
Checksum: 338
Coasting Arc #19 (Orbit 1215)
---------------------------------------
Vector Time (GMT): 2019/148/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4264555
66 A = 6786765
45 meter
Y = 1174870
15 meter E =
0001369
Z = 5148154
49 I = 52
00117
XDOT = -84
296262 Wp = 217
22464
YDOT = -7485
347650 meter/sec RA = 99
19526 deg
ZDOT = 1637
584398 TA = 217
03551
MA = 217
04496
Ha = 224
292 n
mi
Hp = 221
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13991324
34 X = -4302383
45
Y = 3854560
86 feet Y = 1126969
01 meter
Z = 16890270
63 Z = 5127346
97
XDOT = -276
562541 XDOT = -8
541222
YDOT = -24558
227198 feet/sec YDOT = -7485
866860 meter/sec
ZDOT = 5372
652225 ZDOT = 1637
358350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14619265
12 X = -4455952
01
Y = -275131
81 feet Y = -83860
18 meter
Z = 16795756
24 Z = 5119346
50
XDOT = 6600
367946 XDOT = 2011
792150
YDOT = -22584
658692 feet/sec YDOT = -6883
803969 meter/sec
ZDOT = 5372
346119 ZDOT = 1637
491097
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 19148
32616002
00016717 00000-0 10270-3 0 9189
2 25544 51
6394 99
8681 0005257 290
0827 69
9759 15
51204227 12162
Satellite: ISS
Catalog Number: 25544
Epoch time: 19148
32616002 = yrday
fracday
Element set: 918
Inclination: 51
6394 deg
RA of node: 99
8681 deg
Eccentricity:
0005257
Arg of perigee: 290
0827 deg
Mean anomaly: 69
9759 deg
Mean motion: 15
51204227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1216
Checksum: 325
Coasting Arc #20 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2019/149/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4199967
87 A = 6786139
21 meter
Y = -611175
04 meter E =
0010213
Z = -5303762
70 I = 52
00440
XDOT = 73
664399 Wp = 68
64721
YDOT = 7612
412430 meter/sec RA = 94
25176 deg
ZDOT = -816
526202 TA = 193
56151
MA = 193
58897
Ha = 224
314 n
mi
Hp = 221
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13779422
15 X = 4232253
01
Y = -2005167
46 feet Y = -564027
14 meter
Z = -17400796
25 Z = -5283282
28
XDOT = 241
681099 XDOT = -7
498980
YDOT = 24975
106398 feet/sec YDOT = 7612
782445 meter/sec
ZDOT = -2678
891740 ZDOT = -816
364928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13930285
69 X = 4245951
08
Y = 1751435
91 feet Y = 533837
66 meter
Z = -17307815
99 Z = -5275422
31
XDOT = -6246
594416 XDOT = -1903
961978
YDOT = 23133
357633 feet/sec YDOT = 7051
047407 meter/sec
ZDOT = -2678
908550 ZDOT = -816
531326
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 19149
29251435
00016717 00000-0 10270-3 0 9192
2 25544 51
6407 95
0722 0005350 293
5332 66
5257 15
51192249 12317
Satellite: ISS
Catalog Number: 25544
Epoch time: 19149
29251435 = yrday
fracday
Element set: 919
Inclination: 51
6407 deg
RA of node: 95
0722 deg
Eccentricity:
0005350
Arg of perigee: 293
5332 deg
Mean anomaly: 66
5257 deg
Mean motion: 15
51192249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 303
Coasting Arc #21 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2019/150/06:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 965081
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4178407
63 A = 6785874
26 meter
Y = 21983
94 meter E =
0003340
Z = 5348707
38 I = 52
00333
XDOT = -73
976104 Wp = 319
28862
YDOT = -7662
115878 meter/sec RA = 89
30755 deg
ZDOT = -23
844684 TA = 130
95208
MA = 130
92318
Ha = 224
591 n
mi
Hp = 220
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13708686
46 X = -4204324
27
Y = 72125
79 feet Y = -24887
29 meter
Z = 17548252
56 Z = 5328347
06
XDOT = -242
703754 XDOT = 11
825186
YDOT = -25138
175454 feet/sec YDOT = -7662
463384 meter/sec
ZDOT = -78
230592 ZDOT = -23
996274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13410193
77 X = -4087427
06
Y = -3366548
89 feet Y = -1026124
10 meter
Z = 17455873
11 Z = 5320550
12
XDOT = 5769
995057 XDOT = 1758
694493
YDOT = -23431
142122 feet/sec YDOT = -7141
812119 meter/sec
ZDOT = -78
145908 ZDOT = -23
818873
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 19150
32329062
00016717 00000-0 10270-3 0 9202
2 25544 51
6390 89
9562 0005219 298
5717 61
4908 15
51205519 12477
Satellite: ISS
Catalog Number: 25544
Epoch time: 19150
32329062 = yrday
fracday
Element set: 920
Inclination: 51
6390 deg
RA of node: 89
9562 deg
Eccentricity:
0005219
Arg of perigee: 298
5717 deg
Mean anomaly: 61
4908 deg
Mean motion: 15
51205519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 313
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list