[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 7th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19920 769 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
160/04:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 221
6
Coasting Arc #1 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2020/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5543854
56 A = 6797864
60 meter
Y = -1701670
17 meter E =
0013317
Z = 3538002
15 I = 51
92864
XDOT = -1021
261733 Wp = 79
58504
YDOT = -6103
445288 meter/sec RA = 45
61076 deg
ZDOT = -4519
047535 TA = 58
99531
MA = 58
86458
Ha = 228
950 n
mi
Hp = 221
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18188499
23 X = -5541599
71
Y = -5582907
38 feet Y = -1763653
55 meter
Z = 11607618
59 Z = 3511077
15
XDOT = -3350
596238 XDOT = -930
984125
YDOT = -20024
426799 feet/sec YDOT = -6114
360148 meter/sec
ZDOT = -14826
271441 ZDOT = -4523
790344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10547979
47 X = -3215024
14
Y = 15924469
27 feet Y = 4853778
23 meter
Z = 11483839
77 Z = 3500274
36
XDOT = -18961
101317 XDOT = -5779
343682
YDOT = -1811
953575 feet/sec YDOT = -552
283450 meter/sec
ZDOT = -14847
627498 ZDOT = -4525
556861
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 20157
53964957
00016717 00000-0 10270-3 0 9000
2 25544 51
6454 46
1284 0002209 24
4117 335
7137 15
49427407 30201
Satellite: ISS
Catalog Number: 25544
Epoch time: 20157
53964957 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 46
1284 deg
Eccentricity:
0002209
Arg of perigee: 24
4117 deg
Mean anomaly: 335
7137 deg
Mean motion: 15
49427407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 295
Coasting Arc #2 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2020/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5707267
35 A = 6798152
93 meter
Y = 1347764
46 meter E =
0006082
Z = -3441566
78 I = 51
90471
XDOT = 1372
715770 Wp = 69
61613
YDOT = 5951
477743 meter/sec RA = 40
67978 deg
ZDOT = 4615
766519 TA = 250
35704
MA = 250
42269
Ha = 228
910 n
mi
Hp = 221
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18724630
42 X = 5708489
32
Y = 4421799
42 feet Y = 1411594
72 meter
Z = -11291229
59 Z = -3413839
72
XDOT = 4503
660662 XDOT = 1283
641690
YDOT = 19525
845615 feet/sec YDOT = 5966
329450 meter/sec
ZDOT = 15143
590942 ZDOT = 4622
219529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9296924
27 X = 2833702
52
Y = -16929092
94 feet Y = -5159987
53 meter
Z = -11163734
66 Z = -3402706
32
XDOT = 18757
285620 XDOT = 5717
220657
YDOT = 314
297620 feet/sec YDOT = 95
797915 meter/sec
ZDOT = 15172
816554 ZDOT = 4624
674486
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 20158
50711083
00016717 00000-0 10270-3 0 9019
2 25544 51
6449 41
3400 0002201 23
5980 336
5271 15
49425941 30357
Satellite: ISS
Catalog Number: 25544
Epoch time: 20158
50711083 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 41
3400 deg
Eccentricity:
0002201
Arg of perigee: 23
5980 deg
Mean anomaly: 336
5271 deg
Mean motion: 15
49425941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 270
Coasting Arc #3 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2020/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5847211
75 A = 6798470
17 meter
Y = -1011306
14 meter E =
0013783
Z = 3307426
95 I = 51
87952
XDOT = -1685
500360 Wp = 83
70617
YDOT = -5787
350794 meter/sec RA = 35
74765 deg
ZDOT = -4730
994521 TA = 58
06226
MA = 57
92831
Ha = 228
955 n
mi
Hp = 221
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19183765
60 X = -5851534
03
Y = -3317933
52 feet Y = -1076718
67 meter
Z = 10851138
27 Z = 3279012
78
XDOT = -5529
856824 XDOT = -1597
678764
YDOT = -18987
371373 feet/sec YDOT = -5805
707244 meter/sec
ZDOT = -15521
635569 ZDOT = -4738
969910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8050568
07 X = -2453813
15
Y = 17805418
46 feet Y = 5427091
55 meter
Z = 10720455
89 Z = 3267594
95
XDOT = -18443
570272 XDOT = -5621
600219
YDOT = 1064
909170 feet/sec YDOT = 324
584315 meter/sec
ZDOT = -15557
871213 ZDOT = -4742
039146
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 20159
53906874
00016717 00000-0 10270-3 0 9028
2 25544 51
6448 36
2327 0002243 27
8710 332
2560 15
49447646 30519
Satellite: ISS
Catalog Number: 25544
Epoch time: 20159
53906874 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 36
2327 deg
Eccentricity:
0002243
Arg of perigee: 27
8710 deg
Mean anomaly: 332
2560 deg
Mean motion: 15
49447646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 301
Coasting Arc #4 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2020/160/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2884376
67 A = 6791247
49 meter
Y = 3107161
10 meter E =
0005070
Z = 5302316
16 I = 51
83224
XDOT = -6146
438702 Wp = 50
42544
YDOT = -4525
779133 meter/sec RA = 32
30324 deg
ZDOT = -687
869508 TA = 46
15083
MA = 46
10894
Ha = 229
039 n
mi
Hp = 221
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9463178
06 X = -2944663
01
Y = 10194098
10 feet Y = 3074567
80 meter
Z = 17396050
38 Z = 5288159
24
XDOT = -20165
481307 XDOT = -6092
032018
YDOT = -14848
356734 feet/sec YDOT = -4594
208639 meter/sec
ZDOT = -2256
789726 ZDOT = -717
595158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13487628
50 X = -4111029
17
Y = 3718403
99 feet Y = 1133369
54 meter
Z = 17330646
06 Z = 5282380
92
XDOT = -9205
833182 XDOT = -2805
937954
YDOT = -22182
664337 feet/sec YDOT = -6761
276090 meter/sec
ZDOT = -2393
219666 ZDOT = -729
453354
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 20160
24853832
00016717 00000-0 10270-3 0 9034
2 25544 51
6411 32
7190 0002123 33
6509 326
4775 15
49426596 30622
Satellite: ISS
Catalog Number: 25544
Epoch time: 20160
24853832 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 32
7190 deg
Eccentricity:
0002123
Arg of perigee: 33
6509 deg
Mean anomaly: 326
4775 deg
Mean motion: 15
49426596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 290
Coasting Arc #5 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2020/161/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2768602
39 A = 6791377
26 meter
Y = -3255311
70 meter E =
0015644
Z = -5291814
46 I = 51
80400
XDOT = 6416
505331 Wp = 89
31049
YDOT = 4075
967932 meter/sec RA = 27
36564 deg
ZDOT = 852
016067 TA = 188
82371
MA = 188
85124
Ha = 229
003 n
mi
Hp = 221
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9083341
17 X = 2830502
89
Y = -10680156
49 feet Y = -3224004
13 meter
Z = -17361596
00 Z = -5278216
04
XDOT = 21051
526678 XDOT = 6366
311187
YDOT = 13372
598201 feet/sec YDOT = 4147
441050 meter/sec
ZDOT = 2795
328303 ZDOT = 883
063551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13339601
69 X = 4065910
59
Y = -4561377
38 feet Y = -1390307
82 meter
Z = -17298748
75 Z = -5272658
62
XDOT = 11048
955270 XDOT = 3367
721566
YDOT = 21200
119217 feet/sec YDOT = 6461
796337 meter/sec
ZDOT = 2937
872684 ZDOT = 895
463594
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 20161
21599438
00016717 00000-0 10270-3 0 9042
2 25544 51
6417 27
9304 0002238 36
5014 323
6288 15
49416730 30774
Satellite: ISS
Catalog Number: 25544
Epoch time: 20161
21599438 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 27
9304 deg
Eccentricity:
0002238
Arg of perigee: 36
5014 deg
Mean anomaly: 323
6288 deg
Mean motion: 15
49416730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3077
Checksum: 300
Coasting Arc #6 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2020/162/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2652471
56 A = 6791446
89 meter
Y = 3382779
10 meter E =
0005943
Z = 5254506
28 I = 51
77340
XDOT = -6671
803399 Wp = 49
66494
YDOT = -3628
785873 meter/sec RA = 22
42596 deg
ZDOT = -1027
241414 TA = 50
18518
MA = 50
13288
Ha = 229
105 n
mi
Hp = 221
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8702334
51 X = -2715624
80
Y = 11098356
63 feet Y = 3352763
29 meter
Z = 17239193
84 Z = 5241468
91
XDOT = -21889
118764 XDOT = -6625
739674
YDOT = -11905
465464 feet/sec YDOT = -3703
137001 meter/sec
ZDOT = -3370
214612 ZDOT = -1059
538842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13131740
03 X = -4002554
36
Y = 5341918
25 feet Y = 1628216
68 meter
Z = 17178919
16 Z = 5236134
56
XDOT = -12818
149417 XDOT = -3906
971942
YDOT = -20147
129043 feet/sec YDOT = -6140
844932 meter/sec
ZDOT = -3518
541514 ZDOT = -1072
451453
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 20162
24794645
00016717 00000-0 10270-3 0 9054
2 25544 51
6412 22
8224 0002258 38
5532 321
5780 15
49428663 30933
Satellite: ISS
Catalog Number: 25544
Epoch time: 20162
24794645 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 22
8224 deg
Eccentricity:
0002258
Arg of perigee: 38
5532 deg
Mean anomaly: 321
5780 deg
Mean motion: 15
49428663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 301
Coasting Arc #7 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2020/163/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2524147
48 A = 6791597
94 meter
Y = -3533279
37 meter E =
0015306
Z = -5235432
12 I = 51
74240
XDOT = 6869
394184 Wp = 91
82687
YDOT = 3147
770360 meter/sec RA = 17
48440 deg
ZDOT = 1190
101285 TA = 189
58631
MA = 189
61555
Ha = 229
023 n
mi
Hp = 221
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8281323
75 X = 2588900
55
Y = -11592123
91 feet Y = -3504689
73 meter
Z = -17176614
58 Z = -5223014
16
XDOT = 22537
382494 XDOT = 6827
903560
YDOT = 10327
330579 feet/sec YDOT = 3224
356656 meter/sec
ZDOT = 3904
531775 ZDOT = 1223
369489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12902133
11 X = 3932570
17
Y = -6201803
19 feet Y = -1890309
61 meter
Z = -17119180
66 Z = -5217926
27
XDOT = 14434
275757 XDOT = 4399
567251
YDOT = 18852
144124 feet/sec YDOT = 5746
133529 meter/sec
ZDOT = 4057
357262 ZDOT = 1236
682493
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 20163
21540038
00016717 00000-0 10270-3 0 9068
2 25544 51
6414 18
0340 0002225 40
5016 319
6299 15
49423472 31088
Satellite: ISS
Catalog Number: 25544
Epoch time: 20163
21540038 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 18
0340 deg
Eccentricity:
0002225
Arg of perigee: 40
5016 deg
Mean anomaly: 319
6299 deg
Mean motion: 15
49423472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 270
Coasting Arc #8 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2020/164/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2398548
19 A = 6791706
06 meter
Y = 3662603
42 meter E =
0006715
Z = 5188633
77 I = 51
71165
XDOT = -7051
227513 Wp = 50
57385
YDOT = -2673
818791 meter/sec RA = 12
54062 deg
ZDOT = -1366
801147 TA = 52
58973
MA = 52
52863
Ha = 229
112 n
mi
Hp = 221
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7869252
59 X = -2464529
46
Y = 12016415
41 feet Y = 3635411
54 meter
Z = 17023076
68 Z = 5176822
88
XDOT = -23133
948534 XDOT = -7014
164932
YDOT = -8772
371361 feet/sec YDOT = -2752
463230 meter/sec
ZDOT = -4484
255732 ZDOT = -1400
963318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12622255
39 X = -3847263
44
Y = 6989677
29 feet Y = 2130453
64 meter
Z = 16968429
37 Z = 5171977
27
XDOT = -15957
207862 XDOT = -4863
756956
YDOT = -17506
256947 feet/sec YDOT = -5335
907118 meter/sec
ZDOT = -4641
223291 ZDOT = -1414
644859
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 20164
24734926
00016717 00000-0 10270-3 0 9074
2 25544 51
6426 12
9262 0002243 43
0426 317
0899 15
49436581 31241
Satellite: ISS
Catalog Number: 25544
Epoch time: 20164
24734926 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 12
9262 deg
Eccentricity:
0002243
Arg of perigee: 43
0426 deg
Mean anomaly: 317
0899 deg
Mean motion: 15
49436581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3124
Checksum: 299
Coasting Arc #9 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2020/165/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2255602
69 A = 6791872
42 meter
Y = -3813935
72 meter E =
0014918
Z = -5160522
03 I = 51
67918
XDOT = 7172
298875 Wp = 94
00360
YDOT = 2175
895818 meter/sec RA = 7
59440 deg
ZDOT = 1529
617337 TA = 190
74650
MA = 190
77841
Ha = 229
058 n
mi
Hp = 221
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7400271
29 X = 2323150
34
Y = -12512912
45 feet Y = -3788333
65 meter
Z = -16930846
57 Z = -5149401
66
XDOT = 23531
164288 XDOT = 7140
004336
YDOT = 7138
765808 feet/sec YDOT = 2255
920817 meter/sec
ZDOT = 5018
429584 ZDOT = 1564
379211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12300704
21 X = 3749254
64
Y = -7859399
54 feet Y = -2395544
98 meter
Z = -16879368
28 Z = -5144831
45
XDOT = 17287
996949 XDOT = 5269
381470
YDOT = 15956
188319 feet/sec YDOT = 4863
446200 meter/sec
ZDOT = 5178
184978 ZDOT = 1578
310781
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 20165
21479843
00016717 00000-0 10270-3 0 9087
2 25544 51
6427 8
1374 0002301 44
8564 315
2772 15
49438105 31390
Satellite: ISS
Catalog Number: 25544
Epoch time: 20165
21479843 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 8
1374 deg
Eccentricity:
0002301
Arg of perigee: 44
8564 deg
Mean anomaly: 315
2772 deg
Mean motion: 15
49438105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 301
Coasting Arc #10 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2020/166/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2117177
88 A = 6792056
25 meter
Y = 3944795
68 meter E =
0007668
Z = 5103572
36 I = 51
64613
XDOT = -7278
137844 Wp = 52
65008
YDOT = -1688
984607 meter/sec RA = 2
64679 deg
ZDOT = -1707
469294 TA = 53
89021
MA = 53
81925
Ha = 229
173 n
mi
Hp = 221
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6946121
66 X = -2185922
59
Y = 12942243
04 feet Y = 3920734
90 meter
Z = 16744003
79 Z = 5093121
45
XDOT = -23878
405000 XDOT = -7250
416298
YDOT = -5541
288080 feet/sec YDOT = -1770
218725 meter/sec
ZDOT = -5601
933379 ZDOT = -1742
756448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11936970
61 X = -3638388
64
Y = 8653186
03 feet Y = 2637491
10 meter
Z = 16695599
06 Z = 5088818
59
XDOT = -18513
789215 XDOT = -5643
002953
YDOT = -14378
069373 feet/sec YDOT = -4382
435545 meter/sec
ZDOT = -5764
131784 ZDOT = -1756
907368
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 20166
24674390
00016717 00000-0 10270-3 0 9096
2 25544 51
6425 3
0303 0002372 48
3814 311
7539 15
49440134 31554
Satellite: ISS
Catalog Number: 25544
Epoch time: 20166
24674390 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 3
0303 deg
Eccentricity:
0002372
Arg of perigee: 48
3814 deg
Mean anomaly: 311
7539 deg
Mean motion: 15
49440134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 284
Coasting Arc #11 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2020/167/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1953740
51 A = 6792238
63 meter
Y = -4095819
48 meter E =
0014416
Z = -5066755
70 I = 51
61309
XDOT = 7322
813915 Wp = 96
44811
YDOT = 1186
264731 meter/sec RA = 357
69631 deg
ZDOT = 1867
736508 TA = 191
68407
MA = 191
71756
Ha = 229
085 n
mi
Hp = 221
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6409909
80 X = 2024007
41
Y = -13437727
94 feet Y = -4073577
85 meter
Z = -16623214
24 Z = -5057095
02
XDOT = 24024
980036 XDOT = 7299
932097
YDOT = 3891
944657 feet/sec YDOT = 1268
025484 meter/sec
ZDOT = 6127
744449 ZDOT = 1903
252497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11502751
46 X = 3506038
65
Y = -9530629
13 feet Y = -2904935
76 meter
Z = -16578436
14 Z = -5053107
34
XDOT = 19522
461206 XDOT = 5950
446176
YDOT = 12636
148539 feet/sec YDOT = 3851
498075 meter/sec
ZDOT = 6291
022879 ZDOT = 1917
503773
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 20167
21419126
00016717 00000-0 10270-3 0 9100
2 25544 51
6426 358
2417 0002295 51
0076 309
1278 15
49446927 31705
Satellite: ISS
Catalog Number: 25544
Epoch time: 20167
21419126 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 358
2417 deg
Eccentricity:
0002295
Arg of perigee: 51
0076 deg
Mean anomaly: 309
1278 deg
Mean motion: 15
49446927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 299
Coasting Arc #12 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2020/168/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1797897
71 A = 6792464
60 meter
Y = 4226398
42 meter E =
0008440
Z = 4999757
40 I = 51
58091
XDOT = -7352
964199 Wp = 55
33254
YDOT = -699
420180 meter/sec RA = 352
74399 deg
ZDOT = -2045
710561 TA = 54
62510
MA = 54
54626
Ha = 229
154 n
mi
Hp = 221
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5898614
53 X = -1869310
99
Y = 13866136
54 feet Y = 4205893
08 meter
Z = 16403403
56 Z = 4990851
00
XDOT = -24123
898291 XDOT = -7334
659655
YDOT = -2294
685630 feet/sec YDOT = -781
543644 meter/sec
ZDOT = -6711
648822 ZDOT = -2081
384172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11037470
65 X = -3364221
05
Y = 10324310
16 feet Y = 3146849
74 meter
Z = 16362087
45 Z = 4987164
25
XDOT = -20416
823618 XDOT = -6223
047839
YDOT = -10893
159983 feet/sec YDOT = -3320
235163 meter/sec
ZDOT = -6875
678981 ZDOT = -2095
706953
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 20168
24613308
00016717 00000-0 10270-3 0 9113
2 25544 51
6432 353
1344 0002308 52
8116 307
3244 15
49448633 31860
Satellite: ISS
Catalog Number: 25544
Epoch time: 20168
24613308 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 353
1344 deg
Eccentricity:
0002308
Arg of perigee: 52
8116 deg
Mean anomaly: 307
3244 deg
Mean motion: 15
49448633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 287
Coasting Arc #13 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2020/169/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1612476
96 A = 6792671
46 meter
Y = -4373445
65 meter E =
0013851
Z = -4953552
62 I = 51
54839
XDOT = 7322
542621 Wp = 98
17140
YDOT = 206
454990 meter/sec RA = 347
78828 deg
ZDOT = 2204
728737 TA = 193
40292
MA = 193
43975
Ha = 229
137 n
mi
Hp = 221
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5290278
75 X = 1685323
96
Y = -14348574
97 feet Y = -4355005
73 meter
Z = -16251813
06 Z = -4945543
51
XDOT = 24024
089965 XDOT = 7308
980380
YDOT = 677
345769 feet/sec YDOT = 288
264717 meter/sec
ZDOT = 7233
361997 ZDOT = 2240
266092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10479824
43 X = 3194250
49
Y = -11191498
42 feet Y = -3411168
72 meter
Z = -16214614
50 Z = -4942214
50
XDOT = 21074
934712 XDOT = 6423
640100
YDOT = 9034
135215 feet/sec YDOT = 2753
604414 meter/sec
ZDOT = 7396
794205 ZDOT = 2254
542874
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 20169
21357579
00016717 00000-0 10270-3 0 9127
2 25544 51
6432 348
3452 0002413 55
6362 304
5016 15
49457773 32016
Satellite: ISS
Catalog Number: 25544
Epoch time: 20169
21357579 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 348
3452 deg
Eccentricity:
0002413
Arg of perigee: 55
6362 deg
Mean anomaly: 304
5016 deg
Mean motion: 15
49457773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3201
Checksum: 297
Coasting Arc #14 (Orbit 3216)
---------------------------------------
Vector Time (GMT): 2020/170/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1435937
38 A = 6792947
32 meter
Y = 4500701
56 meter E =
0009397
Z = 4876020
80 I = 51
51621
XDOT = -7279
887976 Wp = 58
87567
YDOT = 267
005503 meter/sec RA = 342
83192 deg
ZDOT = -2382
138793 TA = 54
56223
MA = 54
47453
Ha = 229
197 n
mi
Hp = 221
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4711080
65 X = -1509843
91
Y = 14766081
23 feet Y = 4484229
82 meter
Z = 15997443
57 Z = 4868866
79
XDOT = -23884
146904 XDOT = -7270
761515
YDOT = 876
002307 feet/sec YDOT = 185
648042 meter/sec
ZDOT = -7815
415988 ZDOT = -2417
479661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9898372
06 X = -3017023
80
Y = 11971514
53 feet Y = 3648917
63 meter
Z = 15964169
48 Z = 4865878
86
XDOT = -21618
972483 XDOT = -6589
462813
YDOT = -7200
619314 feet/sec YDOT = -2194
748767 meter/sec
ZDOT = -7977
973873 ZDOT = -2431
686437
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 20170
24551420
00016717 00000-0 10270-3 0 9134
2 25544 51
6427 343
2383 0002417 58
5986 301
5400 15
49456280 32178
Satellite: ISS
Catalog Number: 25544
Epoch time: 20170
24551420 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 343
2383 deg
Eccentricity:
0002417
Arg of perigee: 58
5986 deg
Mean anomaly: 301
5400 deg
Mean motion: 15
49456280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3217
Checksum: 286
Coasting Arc #15 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2020/171/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1223738
69 A = 6793185
99 meter
Y = -4639443
12 meter E =
0013095
Z = -4821028
51 I = 51
48590
XDOT = 7179
326621 Wp = 100
25765
YDOT = -739
355870 meter/sec RA = 337
87174 deg
ZDOT = 2537
477620 TA = 194
80403
MA = 194
84240
Ha = 229
140 n
mi
Hp = 221
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4014890
71 X = 1298945
29
Y = -15221270
07 feet Y = -4625336
99 meter
Z = -15817022
67 Z = -4814902
24
XDOT = 23554
221197 XDOT = 7174
735059
YDOT = -2425
708235 feet/sec YDOT = -659
097676 meter/sec
ZDOT = 8325
057809 ZDOT = 2572
340878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9197421
16 X = 2803373
97
Y = -12810792
25 feet Y = -3904729
48 meter
Z = -15788466
11 Z = -4812324
47
XDOT = 21921
765580 XDOT = 6681
754149
YDOT = 5295
464991 feet/sec YDOT = 1614
057729 meter/sec
ZDOT = 8485
450831 ZDOT = 2586
365413
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 20171
21295496
00016717 00000-0 10270-3 0 9141
2 25544 51
6434 338
4490 0002357 61
4780 298
6607 15
49463431 32327
Satellite: ISS
Catalog Number: 25544
Epoch time: 20171
21295496 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 338
4490 deg
Eccentricity:
0002357
Arg of perigee: 61
4780 deg
Mean anomaly: 298
6607 deg
Mean motion: 15
49463431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3232
Checksum: 312
Coasting Arc #16 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2020/172/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1023423
35 A = 6793466
90 meter
Y = 4758869
17 meter E =
0010183
Z = 4733095
33 I = 51
45643
XDOT = -7068
978018 Wp = 62
56621
YDOT = 1187
602673 meter/sec RA = 332
91048 deg
ZDOT = -2713
476667 TA = 54
39510
MA = 54
30027
Ha = 229
160 n
mi
Hp = 221
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3357688
14 X = -1099553
10
Y = 15613087
83 feet Y = 4746997
90 meter
Z = 15528527
98 Z = 4727939
98
XDOT = -23192
185100 XDOT = -7068
552216
YDOT = 3896
334228 feet/sec YDOT = 1108
555257 meter/sec
ZDOT = -8902
482503 ZDOT = -2747
813815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8485526
48 X = -2586388
47
Y = 13556778
87 feet Y = 4132106
20 meter
Z = 15504430
00 Z = 4725750
26
XDOT = -22113
504106 XDOT = -6740
196052
YDOT = -3445
032366 feet/sec YDOT = -1050
045865 meter/sec
ZDOT = -9060
487731 ZDOT = -2761
636661
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 20172
24488927
00016717 00000-0 10270-3 0 9159
2 25544 51
6437 333
3415 0002363 63
3296 296
8096 15
49472946 32481
Satellite: ISS
Catalog Number: 25544
Epoch time: 20172
24488927 = yrday
fracday
Element set: 915
Inclination: 51
6437 deg
RA of node: 333
3415 deg
Eccentricity:
0002363
Arg of perigee: 63
3296 deg
Mean anomaly: 296
8096 deg
Mean motion: 15
49472946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 334
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