[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 14th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14857 4255 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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
135/19:02:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
5
140/01:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 222
5
143/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
4
145/22:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 222
3
149/04:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
2
Coasting Arc #1 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2020/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -191695
61 A = 6792067
83 meter
Y = 4428400
22 meter E =
0012431
Z = -5157431
88 I = 51
76080
XDOT = -7337
405199 Wp = 100
48096
YDOT = 1502
556272 meter/sec RA = 158
95610 deg
ZDOT = 1563
890679 TA = 184
59737
MA = 184
60880
Ha = 228
125 n
mi
Hp = 222
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -628922
60 X = -216149
21
Y = 14528872
10 feet Y = 4426120
30 meter
Z = -16920708
26 Z = -5158422
03
XDOT = -24072
851702 XDOT = -7361
258378
YDOT = 4929
646562 feet/sec YDOT = 1420
370667 meter/sec
ZDOT = 5130
874932 ZDOT = 1528
190668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10934286
11 X = 3332770
41
Y = 9579493
28 feet Y = 2919829
55 meter
Z = -16925387
20 Z = -5158858
02
XDOT = -10715
927232 XDOT = -3266
214620
YDOT = 21001
064956 feet/sec YDOT = 6401
124598 meter/sec
ZDOT = 4966
764918 ZDOT = 1513
869947
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 20134
51352130
00016717 00000-0 10270-3 0 9007
2 25544 51
6421 160
0916 0001259 296
1566 63
9455 15
49348724 26632
Satellite: ISS
Catalog Number: 25544
Epoch time: 20134
51352130 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 160
0916 deg
Eccentricity:
0001259
Arg of perigee: 296
1566 deg
Mean anomaly: 63
9455 deg
Mean motion: 15
49348724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2663
Checksum: 293
Coasting Arc #2 (Orbit 2678)
---------------------------------------
Vector Time (GMT): 2020/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -27260
60 A = 6792117
33 meter
Y = -4466173
61 meter E =
0004764
Z = 5115246
85 I = 51
79050
XDOT = 7193
884932 Wp = 43
07700
YDOT = -2008
116738 meter/sec RA = 154
01647 deg
ZDOT = -1710
634922 TA = 63
45405
MA = 63
40523
Ha = 228
149 n
mi
Hp = 222
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -89437
68 X = -2163
42
Y = -14652800
57 feet Y = -4466338
54 meter
Z = 16782305
95 Z = 5115175
04
XDOT = 23601
984684 XDOT = 7224
114903
YDOT = -6588
309507 feet/sec YDOT = -1927
500436 meter/sec
ZDOT = -5612
319298 ZDOT = -1675
616608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11638584
37 X = -3547440
52
Y = -8902953
91 feet Y = -2713620
35 meter
Z = 16782107
21 Z = 5115186
28
XDOT = 8796
081538 XDOT = 2681
045653
YDOT = -21801
407308 feet/sec YDOT = -6645
068948 meter/sec
ZDOT = -5451
304002 ZDOT = -1661
557460
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 20135
54551835
00016717 00000-0 10270-3 0 9015
2 25544 51
6403 154
9841 0001117 302
6259 57
4783 15
49382733 26793
Satellite: ISS
Catalog Number: 25544
Epoch time: 20135
54551835 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 154
9841 deg
Eccentricity:
0001117
Arg of perigee: 302
6259 deg
Mean anomaly: 57
4783 deg
Mean motion: 15
49382733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2679
Checksum: 312
Coasting Arc #3 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2020/135/19:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1565968
53 A = 6794509
00 meter
Y = 4826109
07 meter E =
0008397
Z = -4527363
53 I = 51
80857
XDOT = -6912
039562 Wp = 108
10623
YDOT = 754
560315 meter/sec RA = 152
56117 deg
ZDOT = 3197
490849 TA = 193
99522
MA = 194
01851
Ha = 228
100 n
mi
Hp = 222
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5137692
02 X = -1597827
80
Y = 15833691
19 feet Y = 4808419
50 meter
Z = -14853554
89 Z = -4535047
41
XDOT = -22677
295152 XDOT = -6935
495134
YDOT = 2475
591584 feet/sec YDOT = 677
133583 meter/sec
ZDOT = 10490
455541 ZDOT = 3163
857971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10694719
96 X = 3259750
64
Y = -12714947
76 feet Y = -3875516
08 meter
Z = -14889016
66 Z = -4538172
28
XDOT = 21045
697006 XDOT = 6414
728447
YDOT = 5607
667805 feet/sec YDOT = 1709
217147 meter/sec
ZDOT = 10335
838987 ZDOT = 3150
363723
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 20135
80351897
00016717 00000-0 10270-3 0 9021
2 25544 51
6415 153
7080 0001378 306
7680 53
3344 15
49377049 26837
Satellite: ISS
Catalog Number: 25544
Epoch time: 20135
80351897 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 153
7080 deg
Eccentricity:
0001378
Arg of perigee: 306
7680 deg
Mean anomaly: 53
3344 deg
Mean motion: 15
49377049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 312
Coasting Arc #4 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2020/136/19:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1304046
31 A = 6794802
37 meter
Y = -4964997
79 meter E =
0008556
Z = 4447576
70 I = 51
83896
XDOT = 6793
655126 Wp = 61
22132
YDOT = -1207
661330 meter/sec RA = 147
62529 deg
ZDOT = -3331
215002 TA = 62
39070
MA = 62
30384
Ha = 228
094 n
mi
Hp = 222
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4278367
15 X = 1337865
66
Y = -16289362
84 feet Y = -4950226
20 meter
Z = 14591787
08 Z = 4453993
09
XDOT = 22288
894771 XDOT = 6822
835792
YDOT = -3962
143472 feet/sec YDOT = -1131
526474 meter/sec
ZDOT = -10929
183076 ZDOT = -3298
143241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9842748
63 X = -3000069
78
Y = 13634587
80 feet Y = 4155822
36 meter
Z = 14621434
00 Z = 4456613
08
XDOT = -21269
795139 XDOT = -6483
033558
YDOT = -3766
292256 feet/sec YDOT = -1147
965880 meter/sec
ZDOT = -10777
113186 ZDOT = -3284
864099
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 20136
83551399
00016717 00000-0 10270-3 0 9035
2 25544 51
6417 148
6012 0001442 310
4179 49
6845 15
49375700 26997
Satellite: ISS
Catalog Number: 25544
Epoch time: 20136
83551399 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 148
6012 deg
Eccentricity:
0001442
Arg of perigee: 310
4179 deg
Mean anomaly: 49
6845 deg
Mean motion: 15
49375700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 316
Coasting Arc #5 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2020/137/19:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1008646
34 A = 6795035
93 meter
Y = 5097432
12 meter E =
0007540
Z = -4386025
58 I = 51
86866
XDOT = -6630
898021 Wp = 106
01123
YDOT = 1651
298895 meter/sec RA = 142
68992 deg
ZDOT = 3446
933062 TA = 198
90333
MA = 198
93134
Ha = 228
132 n
mi
Hp = 222
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3309207
15 X = -1044267
48
Y = 16723858
65 feet Y = 5085953
79 meter
Z = -14389847
71 Z = -4391011
44
XDOT = -21754
914768 XDOT = -6665
613813
YDOT = 5417
647294 feet/sec YDOT = 1576
953170 meter/sec
ZDOT = 11308
835506 ZDOT = 3414
638392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8851799
75 X = 2698028
56
Y = -14547133
70 feet Y = -4433966
35 meter
Z = -14412930
29 Z = -4393061
15
XDOT = 21287
745063 XDOT = 6488
504695
YDOT = 1905
465676 feet/sec YDOT = 580
785938 meter/sec
ZDOT = 11160
306953 ZDOT = 3401
661559
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 20137
80300590
00016717 00000-0 10270-3 0 9049
2 25544 51
6427 143
8121 0001513 315
6531 44
4498 15
49382773 27147
Satellite: ISS
Catalog Number: 25544
Epoch time: 20137
80300590 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 143
8121 deg
Eccentricity:
0001513
Arg of perigee: 315
6531 deg
Mean anomaly: 44
4498 deg
Mean motion: 15
49382773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 290
Coasting Arc #6 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2020/138/19:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 721434
57 A = 6795307
32 meter
Y = -5209134
69 meter E =
0009376
Z = 4298869
15 I = 51
89489
XDOT = 6451
890842 Wp = 64
20828
YDOT = -2067
970711 meter/sec RA = 137
75760 deg
ZDOT = -3578
567263 TA = 62
24750
MA = 62
15246
Ha = 228
161 n
mi
Hp = 222
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2366911
32 X = 758749
43
Y = -17090336
90 feet Y = -5200858
69 meter
Z = 14103901
40 Z = 4302463
96
XDOT = 21167
620872 XDOT = 6491
918751
YDOT = -6784
680812 feet/sec YDOT = -1995
597062 meter/sec
ZDOT = -11740
706242 ZDOT = -3547
129155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7835796
34 X = -2388350
72
Y = 15356133
45 feet Y = 4680549
47 meter
Z = 14120601
28 Z = 4303959
27
XDOT = -21173
916942 XDOT = -6453
809884
YDOT = -111
108541 feet/sec YDOT = -33
865883 meter/sec
ZDOT = -11596
085815 ZDOT = -3534
486956
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 20138
83499640
00016717 00000-0 10270-3 0 9059
2 25544 51
6419 138
7050 0001536 322
4513 37
6529 15
49396206 27306
Satellite: ISS
Catalog Number: 25544
Epoch time: 20138
83499640 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 138
7050 deg
Eccentricity:
0001536
Arg of perigee: 322
4513 deg
Mean anomaly: 37
6529 deg
Mean motion: 15
49396206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 309
Coasting Arc #7 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2020/139/19:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -398155
14 A = 6795610
79 meter
Y = 5307431
53 meter E =
0006664
Z = -4231897
60 I = 51
91991
XDOT = -6233
512646 Wp = 103
19427
YDOT = 2471
996336 meter/sec RA = 132
82625 deg
ZDOT = 3690
136517 TA = 204
55907
MA = 204
59083
Ha = 228
156 n
mi
Hp = 222
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1306283
28 X = -436918
46
Y = 17412833
09 feet Y = 5302762
60 meter
Z = -13884178
48 Z = -4233925
52
XDOT = -20451
156974 XDOT = -6278
616726
YDOT = 8110
224199 feet/sec YDOT = 2402
036334 meter/sec
ZDOT = 12106
747103 ZDOT = 3659
746817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6668209
34 X = 2032470
21
Y = -16130219
08 feet Y = -4916490
77 meter
Z = -13893687
81 Z = -4234796
05
XDOT = 20868
913418 XDOT = 6360
844810
YDOT = -1670
843439 feet/sec YDOT = -509
273080 meter/sec
ZDOT = 11966
916856 ZDOT = 3647
516258
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 20139
80248631
00016717 00000-0 10270-3 0 9060
2 25544 51
6419 133
9165 0001637 320
0527 40
0503 15
49382171 27453
Satellite: ISS
Catalog Number: 25544
Epoch time: 20139
80248631 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 133
9165 deg
Eccentricity:
0001637
Arg of perigee: 320
0527 deg
Mean anomaly: 40
0503 deg
Mean motion: 15
49382171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 287
Coasting Arc #8 (Orbit 2749)
---------------------------------------
Vector Time (GMT): 2020/140/01:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5408233
21 A = 6797283
73 meter
Y = 1675498
87 meter E =
0010703
Z = 3752418
00 I = 51
92893
XDOT = 1048
165530 Wp = 92
62001
YDOT = -6259
603502 meter/sec RA = 131
51296 deg
ZDOT = 4294
638153 TA = 311
94675
MA = 312
03792
Ha = 228
240 n
mi
Hp = 222
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17743547
28 X = -5444794
50
Y = 5497043
55 feet Y = 1614815
48 meter
Z = 12311082
69 Z = 3726057
91
XDOT = 3438
863287 XDOT = 1097
223225
YDOT = -20536
756895 feet/sec YDOT = -6247
608153 meter/sec
ZDOT = 14090
020187 ZDOT = 4299
848533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2614654
06 X = -796946
56
Y = -18471218
86 feet Y = -5630027
51 meter
Z = 12189806
10 Z = 3715452
90
XDOT = 18403
852051 XDOT = 5609
494105
YDOT = 6733
467034 feet/sec YDOT = 2052
360752 meter/sec
ZDOT = 14114
200971 ZDOT = 4302
008456
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 20140
12498237
00016717 00000-0 10270-3 0 9077
2 25544 51
6391 132
3145 0001163 305
8845 54
2197 15
49401356 27500
Satellite: ISS
Catalog Number: 25544
Epoch time: 20140
12498237 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 132
3145 deg
Eccentricity:
0001163
Arg of perigee: 305
8845 deg
Mean anomaly: 54
2197 deg
Mean motion: 15
49401356 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2750
Checksum: 291
Coasting Arc #9 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2020/141/01:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5235447
24 A = 6796987
57 meter
Y = -1984748
68 meter E =
0005615
Z = -3859893
04 I = 51
95010
XDOT = -660
973334 Wp = 65
77453
YDOT = 6378
295489 meter/sec RA = 126
58366 deg
ZDOT = -4178
779408 TA = 160
34303
MA = 160
32138
Ha = 228
208 n
mi
Hp = 222
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17176664
18 X = 5276001
61
Y = -6511642
64 feet Y = -1925975
12 meter
Z = -12663691
07 Z = -3834362
56
XDOT = -2168
547685 XDOT = -711
949780
YDOT = 20926
166304 feet/sec YDOT = 6370
619322 meter/sec
ZDOT = -13709
906194 ZDOT = -4182
113509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4016007
48 X = 1224079
08
Y = 18007576
46 feet Y = 5488709
30 meter
Z = -12546203
72 Z = -3824082
89
XDOT = -19111
385411 XDOT = -5825
150273
YDOT = -5294
733060 feet/sec YDOT = -1613
834637 meter/sec
ZDOT = -13725
479479 ZDOT = -4183
526145
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 20141
09246993
00016717 00000-0 10270-3 0 9085
2 25544 51
6400 127
5258 0001192 316
1127 43
9921 15
49387894 27658
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
09246993 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 127
5258 deg
Eccentricity:
0001192
Arg of perigee: 316
1127 deg
Mean anomaly: 43
9921 deg
Mean motion: 15
49387894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 317
Coasting Arc #10 (Orbit 2780)
---------------------------------------
Vector Time (GMT): 2020/142/01:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5034379
30 A = 6796633
83 meter
Y = 2290972
39 meter E =
0010281
Z = 3941663
72 I = 51
96880
XDOT = 250
248049 Wp = 95
13282
YDOT = -6483
510795 meter/sec RA = 121
65561 deg
ZDOT = 4077
935704 TA = 312
32525
MA = 312
41231
Ha = 228
305 n
mi
Hp = 222
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16516992
45 X = -5078770
13
Y = 7516313
62 feet Y = 2234425
79 meter
Z = 12931967
58 Z = 3917100
67
XDOT = 821
023784 XDOT = 302
921382
YDOT = -21271
360876 feet/sec YDOT = -6480
418229 meter/sec
ZDOT = 13379
054146 ZDOT = 4079
278629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5403565
51 X = -1647006
77
Y = -17407441
88 feet Y = -5305788
28 meter
Z = 12818901
78 Z = 3907201
26
XDOT = 19747
259323 XDOT = 6018
964642
YDOT = 3751
686600 feet/sec YDOT = 1143
514076 meter/sec
ZDOT = 13385
492001 ZDOT = 4079
897962
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 20142
12445283
00016717 00000-0 10270-3 0 9094
2 25544 51
6405 122
4176 0001183 319
4144 40
6918 15
49412316 27817
Satellite: ISS
Catalog Number: 25544
Epoch time: 20142
12445283 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 122
4176 deg
Eccentricity:
0001183
Arg of perigee: 319
4144 deg
Mean anomaly: 40
6918 deg
Mean motion: 15
49412316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2781
Checksum: 285
Coasting Arc #11 (Orbit 2794)
---------------------------------------
Vector Time (GMT): 2020/143/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4667250
83 A = 6793166
30 meter
Y = -728201
63 meter E =
0011564
Z = -4892890
70 I = 51
97147
XDOT = -1465
495325 Wp = 66
79680
YDOT = 7097
158765 meter/sec RA = 117
02657 deg
ZDOT = -2454
350005 TA = 179
17303
MA = 179
17112
Ha = 228
297 n
mi
Hp = 222
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15312502
71 X = 4698814
18
Y = -2389112
95 feet Y = -675832
05 meter
Z = -16052791
00 Z = -4870142
05
XDOT = -4808
055528 XDOT = -1532
826909
YDOT = 23284
641616 feet/sec YDOT = 7080
394365 meter/sec
ZDOT = -8052
329413 ZDOT = -2461
631638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5209662
25 X = -1587905
05
Y = 14710184
00 feet Y = 4483664
08 meter
Z = -15948122
29 Z = -4860987
67
XDOT = -17172
091372 XDOT = -5234
053450
YDOT = -14847
536685 feet/sec YDOT = -4525
529182 meter/sec
ZDOT = -8086
128081 ZDOT = -2464
651839
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 20143
02743829
00016717 00000-0 10270-3 0 9103
2 25544 51
6391 117
9495 0001182 333
9484 26
1606 15
49402132 27954
Satellite: ISS
Catalog Number: 25544
Epoch time: 20143
02743829 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 117
9495 deg
Eccentricity:
0001182
Arg of perigee: 333
9484 deg
Mean anomaly: 26
1606 deg
Mean motion: 15
49402132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2795
Checksum: 301
Coasting Arc #12 (Orbit 2810)
---------------------------------------
Vector Time (GMT): 2020/144/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4559211
78 A = 6792897
02 meter
Y = 967753
53 meter E =
0005606
Z = 4938237
70 I = 51
98549
XDOT = 981
359860 Wp = 115
86939
YDOT = -7237
239753 meter/sec RA = 112
09910 deg
ZDOT = 2319
907324 TA = 311
50895
MA = 311
55705
Ha = 228
371 n
mi
Hp = 222
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14958043
91 X = -4593682
16
Y = 3175044
38 feet Y = 916575
76 meter
Z = 16201567
25 Z = 4916006
88
XDOT = 3219
684579 XDOT = 1050
946921
YDOT = -23744
224913 feet/sec YDOT = -7225
876721 meter/sec
ZDOT = 7611
244500 ZDOT = 2324
842489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4095373
05 X = 1248269
71
Y = -14844412
92 feet Y = -4524577
06 meter
Z = 16099257
45 Z = 4907053
67
XDOT = 18557
601740 XDOT = 5656
357010
YDOT = 13415
255794 feet/sec YDOT = 4088
969966 meter/sec
ZDOT = 7634
279608 ZDOT = 2326
928425
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 20144
05941828
00016717 00000-0 10270-3 0 9117
2 25544 51
6397 112
8405 0001259 327
0713 33
0358 15
49416627 28113
Satellite: ISS
Catalog Number: 25544
Epoch time: 20144
05941828 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 112
8405 deg
Eccentricity:
0001259
Arg of perigee: 327
0713 deg
Mean anomaly: 33
0358 deg
Mean motion: 15
49416627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2811
Checksum: 294
Coasting Arc #13 (Orbit 2825)
---------------------------------------
Vector Time (GMT): 2020/145/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4455371
04 A = 6792705
41 meter
Y = -1185773
05 meter E =
0012314
Z = -4999816
11 I = 51
99785
XDOT = -487
453001 Wp = 68
31825
YDOT = 7320
397814 meter/sec RA = 107
17403 deg
ZDOT = -2170
372624 TA = 180
58086
MA = 180
58229
Ha = 228
315 n
mi
Hp = 222
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14617359
07 X = 4492586
15
Y = -3890331
52 feet Y = -1135741
06 meter
Z = -16403596
17 Z = -4978083
15
XDOT = -1599
255253 XDOT = -558
733061
YDOT = 24017
053194 feet/sec YDOT = 7314
548550 meter/sec
ZDOT = -7120
645093 ZDOT = -2172
912513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3047842
44 X = -928982
38
Y = 14925972
04 feet Y = 4549436
28 meter
Z = -16303553
22 Z = -4969323
02
XDOT = -19746
657842 XDOT = -6018
781310
YDOT = -11823
675933 feet/sec YDOT = -3603
856424 meter/sec
ZDOT = -7132
687717 ZDOT = -2174
043216
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 20145
02689850
00016717 00000-0 10270-3 0 9120
2 25544 51
6412 108
0527 0001271 338
2937 21
8159 15
49407037 28264
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
02689850 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 108
0527 deg
Eccentricity:
0001271
Arg of perigee: 338
2937 deg
Mean anomaly: 21
8159 deg
Mean motion: 15
49407037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2826
Checksum: 298
Coasting Arc #14 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2020/145/22:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3495296
56 A = 6792090
72 meter
Y = 2759612
63 meter E =
0012887
Z = -5139784
33 I = 52
00261
XDOT = -2911
067733 Wp = 97
26482
YDOT = 6866
025869 meter/sec RA = 102
66395 deg
ZDOT = 1708
874729 TA = 189
18847
MA = 189
21208
Ha = 228
428 n
mi
Hp = 222
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11467508
38 X = 3489144
36
Y = 9053847
20 feet Y = 2798665
97 meter
Z = -16862809
48 Z = -5122819
85
XDOT = -9550
747156 XDOT = -2995
930136
YDOT = 22526
331591 feet/sec YDOT = 6832
997460 meter/sec
ZDOT = 5606
544386 ZDOT = 1694
528770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14620899
39 X = -4456450
13
Y = -1525376
84 feet Y = -464934
86 meter
Z = -16784897
01 Z = -5116036
61
XDOT = -3940
730682 XDOT = -1201
134712
YDOT = -23114
956419 feet/sec YDOT = -7045
438717 meter/sec
ZDOT = 5540
185607 ZDOT = 1688
648573
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 20145
92987742
00016717 00000-0 10270-3 0 9131
2 25544 51
6399 103
5836 0001356 349
8648 10
2474 15
49404278 28404
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
92987742 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 103
5836 deg
Eccentricity:
0001356
Arg of perigee: 349
8648 deg
Mean anomaly: 10
2474 deg
Mean motion: 15
49404278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 329
Coasting Arc #15 (Orbit 2855)
---------------------------------------
Vector Time (GMT): 2020/146/22:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3655290
82 A = 6792384
63 meter
Y = -2617966
36 meter E =
0006260
Z = 5088747
82 I = 52
00853
XDOT = 2425
612859 Wp = 45
01630
YDOT = -7025
029324 meter/sec RA = 97
73931 deg
ZDOT = -1866
068418 TA = 63
01484
MA = 62
95093
Ha = 228
632 n
mi
Hp = 222
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11992423
95 X = -3650462
65
Y = -8589128
47 feet Y = -2658816
29 meter
Z = 16695366
86 Z = 5071003
02
XDOT = 7958
047438 XDOT = 2513
052891
YDOT = -23047
996471 feet/sec YDOT = -6997
415168 meter/sec
ZDOT = -6122
271712 ZDOT = -1854
074490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14830651
57 X = 4520382
60
Y = 598510
22 feet Y = 182425
92 meter
Z = 16613855
49 Z = 5063903
15
XDOT = 5905
117581 XDOT = 1799
879839
YDOT = 22601
038077 feet/sec YDOT = 6888
796406 meter/sec
ZDOT = -6066
703907 ZDOT = -1849
131351
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 20146
96185317
00016717 00000-0 10270-3 0 9145
2 25544 51
6389 98
4758 0001321 353
7075 6
4058 15
49366377 28567
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
96185317 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 98
4758 deg
Eccentricity:
0001321
Arg of perigee: 353
7075 deg
Mean anomaly: 6
4058 deg
Mean motion: 15
49366377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2856
Checksum: 336
Coasting Arc #16 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2020/147/22:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3831093
00 A = 6792451
13 meter
Y = 2454346
72 meter E =
0012381
Z = -5054578
18 I = 52
01428
XDOT = -1920
602981 Wp = 99
10337
YDOT = 7128
746233 meter/sec RA = 92
81586 deg
ZDOT = 2008
076131 TA = 190
33450
MA = 190
35998
Ha = 228
464 n
mi
Hp = 222
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12569202
77 X = 3827915
32
Y = 8052318
63 feet Y = 2497171
80 meter
Z = -16583261
76 Z = -5035975
51
XDOT = -6301
190884 XDOT = -2009
930094
YDOT = 23388
275044 feet/sec YDOT = 7106
768889 meter/sec
ZDOT = 6588
176282 ZDOT = 1998
530809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15015739
30 X = -4576797
34
Y = 423901
51 feet Y = 129205
18 meter
Z = -16497792
12 Z = -5028527
04
XDOT = -7797
983926 XDOT = -2376
825501
YDOT = -21839
875218 feet/sec YDOT = -6656
793966 meter/sec
ZDOT = 6543
850945 ZDOT = 1994
565768
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 20147
92932709
00016717 00000-0 10270-3 0 9158
2 25544 51
6407 93
6882 0001312 354
7694 5
3442 15
49408315 28712
Satellite: ISS
Catalog Number: 25544
Epoch time: 20147
92932709 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 93
6882 deg
Eccentricity:
0001312
Arg of perigee: 354
7694 deg
Mean anomaly: 5
3442 deg
Mean motion: 15
49408315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 314
Coasting Arc #17 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2020/148/22:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3987464
58 A = 6792757
27 meter
Y = -2293730
92 meter E =
0007110
Z = 4995022
12 I = 52
01568
XDOT = 1426
643044 Wp = 48
45059
YDOT = -7210
627169 meter/sec RA = 87
89066 deg
ZDOT = -2165
698774 TA = 62
59852
MA = 62
52620
Ha = 228
683 n
mi
Hp = 222
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13082232
87 X = -3985781
96
Y = -7525363
90 feet Y = -2338312
94 meter
Z = 16387867
85 Z = 4975656
34
XDOT = 4680
587415 XDOT = 1517
688092
YDOT = -23656
913283 feet/sec YDOT = -7194
164032 meter/sec
ZDOT = -7105
310939 ZDOT = -2158
548693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15122972
31 X = 4609481
96
Y = -1407298
53 feet Y = -428944
59 meter
Z = 16298875
75 Z = 4967897
33
XDOT = 9598
165605 XDOT = 2925
520876
YDOT = 20986
230802 feet/sec YDOT = 6396
603148 meter/sec
ZDOT = -7071
987833 ZDOT = -2155
541891
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 20148
96129838
00016717 00000-0 10270-3 0 9165
2 25544 51
6409 88
5794 0001331 1
1560 358
9593 15
49378039 28875
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
96129838 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 88
5794 deg
Eccentricity:
0001331
Arg of perigee: 1
1560 deg
Mean anomaly: 358
9593 deg
Mean motion: 15
49378039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 344
Coasting Arc #18 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3447962
81 A = 6793978
98 meter
Y = -3530000
30 meter E =
0011037
Z = -4680887
32 I = 52
02172
XDOT = 2693
632466 Wp = 62
36662
YDOT = 6529
790027 meter/sec RA = 86
54806 deg
ZDOT = -2940
503820 TA = 178
45437
MA = 178
45096
Ha = 228
524 n
mi
Hp = 222
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11312213
94 X = 3509917
08
Y = -11581365
80 feet Y = -3491095
62 meter
Z = -15357241
87 Z = -4663988
56
XDOT = 8837
376858 XDOT = 2634
697469
YDOT = 21423
195628 feet/sec YDOT = 6559
583055 meter/sec
ZDOT = -9647
322244 ZDOT = -2927
561405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16253488
11 X = 4954063
18
Y = -554367
35 feet Y = -168971
17 meter
Z = -15279263
63 Z = -4657119
55
XDOT = -8313
594579 XDOT = -2533
983628
YDOT = 20488
392888 feet/sec YDOT = 6244
862152 meter/sec
ZDOT = -9588
138786 ZDOT = -2922
464702
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 20149
21928892
00016717 00000-0 10270-3 0 9172
2 25544 51
6430 87
3061 0001603 359
3399
7749 15
49403153 28919
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
21928892 = yrday
fracday
Element set: 917
Inclination: 51
6430 deg
RA of node: 87
3061 deg
Eccentricity:
0001603
Arg of perigee: 359
3399 deg
Mean anomaly:
7749 deg
Mean motion: 15
49403153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 315
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