[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 1st 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14262 1813 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
146/12:07:22
200 0
0 0
0 0
0
N/A -0
0 -0
0 228
5
000/00:12:03
600 0
0 0
0 222
2
148/20:33:33
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
149/04:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
2
149/15:39:55
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
152/12:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 222
0
160/04:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
7
Coasting Arc #1 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2020/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2889874
51 A = 6794559
08 meter
Y = 4146263
08 meter E =
0008863
Z = -4549652
35 I = 52
01546
XDOT = -3558
870999 Wp = 100
43334
YDOT = 5977
020061 meter/sec RA = 99
78665 deg
ZDOT = 3190
246072 TA = 201
47895
MA = 201
51616
Ha = 228
508 n
mi
Hp = 222
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9481215
58 X = 2865394
76
Y = 13603225
32 feet Y = 4178443
61 meter
Z = -14926680
95 Z = -4535673
11
XDOT = -11676
085955 XDOT = -3640
939819
YDOT = 19609
645868 feet/sec YDOT = 5936
762816 meter/sec
ZDOT = 10466
686589 ZDOT = 3172
760012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16485077
08 X = 5024651
49
Y = -2256772
27 feet Y = -687864
19 meter
Z = -14862577
33 Z = -4530113
57
XDOT = 11850
386685 XDOT = 3611
997862
YDOT = 18245
111353 feet/sec YDOT = 5561
109940 meter/sec
ZDOT = 10385
912307 ZDOT = 3165
626071
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
51043290
00016717 00000-0 10270-3 0 9004
2 25544 51
6406 100
7144 0001800 349
1600 10
9511 15
49370393 28497
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
51043290 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 100
7144 deg
Eccentricity:
0001800
Arg of perigee: 349
1600 deg
Mean anomaly: 10
9511 deg
Mean motion: 15
49370393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 265
Coasting Arc #2 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2020/146/12:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 953907
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -701260
56 A = 6802998
96 meter
Y = 6735841
02 meter E =
0011985
Z = -577568
87 I = 52
04380
XDOT = -4756
359817 Wp = 34
69622
YDOT = 13
772283 meter/sec RA = 99
75811 deg
ZDOT = 6006
255110 TA = 319
11688
MA = 319
20671
Ha = 228
479 n
mi
Hp = 222
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2300723
61 X = -773725
09
Y = 22099215
96 feet Y = 6727593
95 meter
Z = -1894911
00 Z = -581150
21
XDOT = -15604
855044 XDOT = -4785
335498
YDOT = 45
184656 feet/sec YDOT = -39
579749 meter/sec
ZDOT = 19705
561386 ZDOT = 5983
080014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19256206
59 X = 5869291
77
Y = 11081655
95 feet Y = 3377688
73 meter
Z = -1911745
70 Z = -582700
09
XDOT = -5553
452079 XDOT = -1692
692194
YDOT = 12991
496985 feet/sec YDOT = 3959
808281 meter/sec
ZDOT = 19598
924930 ZDOT = 5973
752319
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
51043288
00016717 00000-0 10270-3 0 9012
2 25544 51
6406 100
7145 0001739 350
4977 9
6140 15
49388265 28491
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
51043288 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 100
7145 deg
Eccentricity:
0001739
Arg of perigee: 350
4977 deg
Mean anomaly: 9
6140 deg
Mean motion: 15
49388265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 307
Coasting Arc #3 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2020/147/12:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 953907
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 240217
86 A = 6803092
67 meter
Y = -6780518
15 meter E =
0011549
Z = 426130
12 I = 52
04946
XDOT = 4730
741475 Wp = 124
45933
YDOT = -217
667071 meter/sec RA = 94
83664 deg
ZDOT = -6020
727335 TA = 50
98127
MA = 50
87850
Ha = 228
508 n
mi
Hp = 222
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 788116
33 X = 313951
87
Y = -22245794
47 feet Y = -6777419
67 meter
Z = 1398064
69 Z = 427474
94
XDOT = 15520
805365 XDOT = 4762
069237
YDOT = -714
130811 feet/sec YDOT = -164
588367 meter/sec
ZDOT = -19753
042439 ZDOT = -5997
671111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20169169
59 X = -6147562
89
Y = -9417149
50 feet Y = -2870347
17 meter
Z = 1404626
96 Z = 428130
30
XDOT = 4777
859810 XDOT = 1456
291670
YDOT = -13216
807430 feet/sec YDOT = -4028
482905 meter/sec
ZDOT = -19646
932111 ZDOT = -5988
384907
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
54241826
00016717 00000-0 10270-3 0 9025
2 25544 51
6415 95
6070 0001774 352
3114 7
8008 15
49379051 28657
Satellite: ISS
Catalog Number: 25544
Epoch time: 20147
54241826 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 95
6070 deg
Eccentricity:
0001774
Arg of perigee: 352
3114 deg
Mean anomaly: 7
8008 deg
Mean motion: 15
49379051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 296
Coasting Arc #4 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2020/148/12:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 953907
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 251524
14 A = 6803096
90 meter
Y = 6784787
01 meter E =
0012691
Z = -309656
41 I = 52
05143
XDOT = -4703
414238 Wp = 36
96813
YDOT = 443
375401 meter/sec RA = 89
91521 deg
ZDOT = 6032
082295 TA = 319
71962
MA = 319
81358
Ha = 228
529 n
mi
Hp = 222
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 825210
44 X = 177140
08
Y = 22259799
89 feet Y = 6787183
87 meter
Z = -1015933
11 Z = -308614
18
XDOT = -15431
149076 XDOT = -4737
323010
YDOT = 1454
643705 feet/sec YDOT = 390
587913 meter/sec
ZDOT = 19790
296244 ZDOT = 6009
152672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20945544
48 X = 6384201
96
Y = 7581079
66 feet Y = 2310713
08 meter
Z = -1011524
16 Z = -308312
57
XDOT = -3938
345258 XDOT = -1200
407635
YDOT = 13447
015885 feet/sec YDOT = 4098
650442 meter/sec
ZDOT = 19684
747180 ZDOT = 5999
910941
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
50990252
00016717 00000-0 10270-3 0 9037
2 25544 51
6417 90
8191 0001788 354
3512 5
7618 15
49390270 28806
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
50990252 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 90
8191 deg
Eccentricity:
0001788
Arg of perigee: 354
3512 deg
Mean anomaly: 5
7618 deg
Mean motion: 15
49390270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 307
Coasting Arc #5 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2020/148/20:33:33
000
Vector Time (MET): N/A
Weight (LBS) : 953907
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3083515
96 A = 6797274
51 meter
Y = -4746944
28 meter E =
0011636
Z = 3755767
29 I = 52
03018
XDOT = 3184
651135 Wp = 76
55949
YDOT = -5483
136797 meter/sec RA = 88
17932 deg
ZDOT = -4301
754022 TA = 58
90773
MA = 58
79359
Ha = 228
524 n
mi
Hp = 222
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10116522
17 X = -3048448
38
Y = -15573964
18 feet Y = -4781230
86 meter
Z = 12322071
15 Z = 3740873
23
XDOT = 10448
330497 XDOT = 3266
623933
YDOT = -17989
293953 feet/sec YDOT = -5447
064755 meter/sec
ZDOT = -14113
366215 ZDOT = -4286
086011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13518508
89 X = 4120441
51
Y = 12799223
14 feet Y = 3901203
21 meter
Z = 12253800
35 Z = 3734958
35
XDOT = -5174
880094 XDOT = -1577
303453
YDOT = 18951
894138 feet/sec YDOT = 5776
537333 meter/sec
ZDOT = -14040
942766 ZDOT = -4279
679355
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
89689468
00016717 00000-0 10270-3 0 9044
2 25544 51
6400 88
9000 0001552 350
3688 9
7432 15
49384063 28861
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
89689468 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 88
9000 deg
Eccentricity:
0001552
Arg of perigee: 350
3688 deg
Mean anomaly: 9
7432 deg
Mean motion: 15
49384063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 329
Coasting Arc #6 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 953907
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3424456
97 A = 6794135
53 meter
Y = -3586466
27 meter E =
0010891
Z = -4655231
62 I = 52
02236
XDOT = 2731
266477 Wp = 62
15332
YDOT = 6490
755674 meter/sec RA = 86
54889 deg
ZDOT = -2991
826359 TA = 178
10843
MA = 178
10431
Ha = 228
556 n
mi
Hp = 222
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11235095
06 X = 3486919
79
Y = -11766621
63 feet Y = -3547821
61 meter
Z = -15273069
62 Z = -4638445
81
XDOT = 8960
848023 XDOT = 2673
014472
YDOT = 21295
130164 feet/sec YDOT = 6520
973378 meter/sec
ZDOT = -9815
703276 ZDOT = -2978
699479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16324519
36 X = 4975713
50
Y = -742272
37 feet Y = -226244
62 meter
Z = -15195607
94 Z = -4631621
30
XDOT = -8148
749160 XDOT = -2483
738744
YDOT = 20475
963468 feet/sec YDOT = 6241
073665 meter/sec
ZDOT = -9755
668588 ZDOT = -2973
527786
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
21938957
00016717 00000-0 10270-3 0 9052
2 25544 51
6431 87
3066 0001595 359
6128
5021 15
49383675 28915
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
21938957 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 87
3066 deg
Eccentricity:
0001595
Arg of perigee: 359
6128 deg
Mean anomaly:
5021 deg
Mean motion: 15
49383675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 321
Coasting Arc #7 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2020/149/15:39:55
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3952090
34 A = 6791572
19 meter
Y = -1734265
44 meter E =
0014449
Z = -5256571
32 I = 52
01410
XDOT = 1662
795802 Wp = 73
23091
YDOT = 7373
070355 meter/sec RA = 84
29978 deg
ZDOT = -1181
030567 TA = 185
46516
MA = 185
48094
Ha = 228
516 n
mi
Hp = 222
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12966175
67 X = 3996723
02
Y = -5689847
24 feet Y = -1689820
06 meter
Z = -17245968
90 Z = -5237265
51
XDOT = 5455
366804 XDOT = 1585
961111
YDOT = 24189
863369 feet/sec YDOT = 7391
235476 meter/sec
ZDOT = -3874
772201 ZDOT = -1173
138962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11575416
21 X = -3528186
86
Y = -8340630
30 feet Y = -2542224
11 meter
Z = -17157014
37 Z = -5229457
98
XDOT = 17387
365052 XDOT = 5299
668868
YDOT = -16224
786995 feet/sec YDOT = -4945
315076 meter/sec
ZDOT = -3838
887915 ZDOT = -1170
093037
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
67088053
00016717 00000-0 10270-3 0 9066
2 25544 51
6442 85
0740 0001957 356
7746 3
3392 15
49414510 28989
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
67088053 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 85
0740 deg
Eccentricity:
0001957
Arg of perigee: 356
7746 deg
Mean anomaly: 3
3392 deg
Mean motion: 15
49414510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 319
Coasting Arc #8 (Orbit 2913)
---------------------------------------
Vector Time (GMT): 2020/150/15:39:55
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3833331
39 A = 6791512
11 meter
Y = 1899084
64 meter E =
0003154
Z = 5272106
00 I = 52
00853
XDOT = -2183
876654 Wp = 90
85231
YDOT = -7272
857605 meter/sec RA = 79
37532 deg
ZDOT = 1031
315979 TA = 349
31227
MA = 349
31897
Ha = 228
761 n
mi
Hp = 222
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12576546
55 X = -3879891
42
Y = 6230592
64 feet Y = 1855956
64 meter
Z = 17296935
71 Z = 5253372
37
XDOT = -7164
949653 XDOT = -2107
396620
YDOT = -23861
081382 feet/sec YDOT = -7296
851764 meter/sec
ZDOT = 3383
582607 ZDOT = 1020
892477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11972657
45 X = 3649265
99
Y = 7524927
84 feet Y = 2293598
01 meter
Z = 17210599
27 Z = 5245790
66
XDOT = -15974
229044 XDOT = -4868
945013
YDOT = 17781
672720 feet/sec YDOT = 5419
853845 meter/sec
ZDOT = 3336
050235 ZDOT = 1016
828112
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 20150
70286133
00016717 00000-0 10270-3 0 9072
2 25544 51
6435 79
9662 0001894 2
3710 357
7449 15
49392457 29144
Satellite: ISS
Catalog Number: 25544
Epoch time: 20150
70286133 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 79
9662 deg
Eccentricity:
0001894
Arg of perigee: 2
3710 deg
Mean anomaly: 357
7449 deg
Mean motion: 15
49392457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2914
Checksum: 320
Coasting Arc #9 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2020/151/15:39:55
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3725093
87 A = 6791367
59 meter
Y = -2065957
70 meter E =
0014870
Z = -5302329
77 I = 52
00036
XDOT = 2689
744462 Wp = 75
69881
YDOT = 7107
262304 meter/sec RA = 74
45019 deg
ZDOT = -878
060369 TA = 185
91686
MA = 185
93444
Ha = 228
581 n
mi
Hp = 222
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12221436
60 X = 3773674
85
Y = -6778076
44 feet Y = -2024028
87 meter
Z = -17396095
05 Z = -5284116
94
XDOT = 8824
620939 XDOT = 2614
334151
YDOT = 23317
789711 feet/sec YDOT = 7136
919385 meter/sec
ZDOT = -2880
775488 ZDOT = -865
177081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12369678
90 X = -3770278
13
Y = -6723894
36 feet Y = -2049443
00 meter
Z = -17312141
52 Z = -5276740
74
XDOT = 14357
603851 XDOT = 4376
197654
YDOT = -19134
660074 feet/sec YDOT = -5832
244391 meter/sec
ZDOT = -2821
923849 ZDOT = -860
122389
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 20151
67034205
00016717 00000-0 10270-3 0 9081
2 25544 51
6430 75
1776 0001969 1
9303 358
1854 15
49413342 29297
Satellite: ISS
Catalog Number: 25544
Epoch time: 20151
67034205 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 75
1776 deg
Eccentricity:
0001969
Arg of perigee: 1
9303 deg
Mean anomaly: 358
1854 deg
Mean motion: 15
49413342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 302
Coasting Arc #10 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2020/152/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3942327
12 A = 6791047
42 meter
Y = 1391871
96 meter E =
0003231
Z = 5349372
14 I = 51
99118
XDOT = -2583
917138 Wp = 51
65637
YDOT = -7214
389109 meter/sec RA = 70
14733 deg
ZDOT = -25
172616 TA = 38
59405
MA = 38
57096
Ha = 228
716 n
mi
Hp = 221
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12934144
10 X = -3983582
72
Y = 4566509
06 feet Y = 1347554
88 meter
Z = 17550433
52 Z = 5330121
72
XDOT = -8477
418432 XDOT = -2502
929379
YDOT = -23669
255606 feet/sec YDOT = -7242
831477 meter/sec
ZDOT = -82
587323 ZDOT = -37
528286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1650666
96 X = 503123
29
Y = 13730460
88 feet Y = 4185044
48 meter
Z = 17461745
26 Z = 5322339
96
XDOT = -23937
793464 XDOT = -7296
239448
YDOT = 3062
766006 feet/sec YDOT = 933
531079 meter/sec
ZDOT = -138
991037 ZDOT = -42
364468
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 20152
57332332
00016717 00000-0 10270-3 0 9094
2 25544 51
6434 70
7082 0001915 3
9610 356
1555 15
49434558 29430
Satellite: ISS
Catalog Number: 25544
Epoch time: 20152
57332332 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 70
7082 deg
Eccentricity:
0001915
Arg of perigee: 3
9610 deg
Mean anomaly: 356
1555 deg
Mean motion: 15
49434558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 298
Coasting Arc #11 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2020/153/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3885946
87 A = 6791126
99 meter
Y = -1572988
27 meter E =
0015324
Z = -5355806
04 I = 51
97990
XDOT = 3077
685885 Wp = 83
84458
YDOT = 7000
873640 meter/sec RA = 65
22082 deg
ZDOT = 178
933036 TA = 187
84489
MA = 187
86889
Ha = 228
711 n
mi
Hp = 222
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12749169
53 X = 3929263
33
Y = -5160722
67 feet Y = -1529290
13 meter
Z = -17571542
11 Z = -5336824
42
XDOT = 10097
394637 XDOT = 2998
302135
YDOT = 22968
745538 feet/sec YDOT = 7034
846636 meter/sec
ZDOT = 587
050644 ZDOT = 193
691209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2505678
05 X = -763730
67
Y = -13636790
95 feet Y = -4156493
88 meter
Z = -17484078
02 Z = -5329146
98
XDOT = 23520
373777 XDOT = 7169
009927
YDOT = -5152
285385 feet/sec YDOT = -1570
416585 meter/sec
ZDOT = 654
508009 ZDOT = 199
494041
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 20153
54080201
00016717 00000-0 10270-3 0 9109
2 25544 51
6446 65
9195 0002034 12
2919 347
8281 15
49415880 29588
Satellite: ISS
Catalog Number: 25544
Epoch time: 20153
54080201 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 65
9195 deg
Eccentricity:
0002034
Arg of perigee: 12
2919 deg
Mean anomaly: 347
8281 deg
Mean motion: 15
49415880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 301
Coasting Arc #12 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2020/154/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3817524
40 A = 6791078
99 meter
Y = 1736794
88 meter E =
0003967
Z = 5338849
60 I = 51
96452
XDOT = -3561
240704 Wp = 47
38391
YDOT = -6777
156614 meter/sec RA = 60
29411 deg
ZDOT = -338
984404 TA = 45
85191
MA = 45
81929
Ha = 228
816 n
mi
Hp = 221
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12524686
34 X = -3862595
40
Y = 5698145
94 feet Y = 1693852
01 meter
Z = 17515910
77 Z = 5320196
06
XDOT = -11683
860576 XDOT = -3483
545234
YDOT = -22234
765795 feet/sec YDOT = -6816
546483 meter/sec
ZDOT = -1112
153556 ZDOT = -356
095762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3309189
57 X = 1008640
98
Y = 13468113
97 feet Y = 4105081
14 meter
Z = 17429943
65 Z = 5312646
82
XDOT = -23002
860688 XDOT = -7011
271938
YDOT = 7204
381325 feet/sec YDOT = 2195
895428 meter/sec
ZDOT = -1190
436204 ZDOT = -362
844955
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 20154
57277630
00016717 00000-0 10270-3 0 9118
2 25544 51
6443 60
8122 0001995 12
6931 347
4269 15
49438452 29742
Satellite: ISS
Catalog Number: 25544
Epoch time: 20154
57277630 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 60
8122 deg
Eccentricity:
0001995
Arg of perigee: 12
6931 deg
Mean anomaly: 347
4269 deg
Mean motion: 15
49438452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 314
Coasting Arc #13 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2020/155/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3752880
36 A = 6791189
45 meter
Y = -1918724
59 meter E =
0015220
Z = -5337941
63 I = 51
94747
XDOT = 4016
024688 Wp = 86
26773
YDOT = 6492
048964 meter/sec RA = 55
36645 deg
ZDOT = 492
099615 TA = 188
40545
MA = 188
43097
Ha = 228
735 n
mi
Hp = 221
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12312599
60 X = 3799986
21
Y = -6295028
17 feet Y = -1876493
10 meter
Z = -17512931
84 Z = -5319597
19
XDOT = 13175
934017 XDOT = 3940
739817
YDOT = 21299
373240 feet/sec YDOT = 6536
538000 meter/sec
ZDOT = 1614
500048 ZDOT = 511
426182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4164024
01 X = -1269194
52
Y = -13298234
84 feet Y = -4053301
98 meter
Z = -17428371
24 Z = -5312167
56
XDOT = 22206
027415 XDOT = 6768
397156
YDOT = -9175
786450 feet/sec YDOT = -2796
779710 meter/sec
ZDOT = 1702
977018 ZDOT = 519
067395
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 20155
54025356
00016717 00000-0 10270-3 0 9123
2 25544 51
6448 56
0244 0002017 15
3179 344
8032 15
49420344 29895
Satellite: ISS
Catalog Number: 25544
Epoch time: 20155
54025356 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 56
0244 deg
Eccentricity:
0002017
Arg of perigee: 15
3179 deg
Mean anomaly: 344
8032 deg
Mean motion: 15
49420344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 292
Coasting Arc #14 (Orbit 3004)
---------------------------------------
Vector Time (GMT): 2020/156/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3679011
95 A = 6791177
98 meter
Y = 2080987
82 meter E =
0004608
Z = 5313011
36 I = 51
92842
XDOT = -4456
970395 Wp = 44
58426
YDOT = -6199
559359 meter/sec RA = 50
43717 deg
ZDOT = -654
476607 TA = 51
66437
MA = 51
62297
Ha = 228
833 n
mi
Hp = 221
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12070249
18 X = -3727816
65
Y = 6827387
87 feet Y = 2039572
75 meter
Z = 17431139
63 Z = 5295021
72
XDOT = -14622
606284 XDOT = -4384
134714
YDOT = -20339
761677 feet/sec YDOT = -6248
993018 meter/sec
ZDOT = -2147
232961 ZDOT = -675
951216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4954534
95 X = 1510142
25
Y = 13062981
02 feet Y = 3981596
61 meter
Z = 17348195
29 Z = 5287729
92
XDOT = -21320
609679 XDOT = -6498
521830
YDOT = 11084
232419 feet/sec YDOT = 3378
474041 meter/sec
ZDOT = -2245
597850 ZDOT = -684
458225
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 20156
57222510
00016717 00000-0 10270-3 0 9139
2 25544 51
6456 50
9169 0001990 15
7573 344
3639 15
49442796 30057
Satellite: ISS
Catalog Number: 25544
Epoch time: 20156
57222510 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 50
9169 deg
Eccentricity:
0001990
Arg of perigee: 15
7573 deg
Mean anomaly: 344
3639 deg
Mean motion: 15
49442796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3005
Checksum: 310
Coasting Arc #15 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2020/157/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3605128
07 A = 6791315
14 meter
Y = -2264003
83 meter E =
0015131
Z = -5304440
68 I = 51
90597
XDOT = 4860
536062 Wp = 88
27934
YDOT = 5851
447704 meter/sec RA = 45
50628 deg
ZDOT = 808
391358 TA = 189
42330
MA = 189
45172
Ha = 228
808 n
mi
Hp = 221
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11827847
99 X = 3655943
08
Y = -7427834
07 feet Y = -2223403
60 meter
Z = -17403020
60 Z = -5286805
20
XDOT = 15946
640624 XDOT = 4790
815448
YDOT = 19197
663071 feet/sec YDOT = 5905
411694 meter/sec
ZDOT = 2652
202618 ZDOT = 831
833936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5805483
09 X = -1769511
24
Y = -12813717
94 feet Y = -3905621
23 meter
Z = -17321686
74 Z = -5279650
12
XDOT = 20178
737011 XDOT = 6150
479041
YDOT = -12861
988900 feet/sec YDOT = -3920
334217 meter/sec
ZDOT = 2759
635004 ZDOT = 841
136749
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
53969837
00016717 00000-0 10270-3 0 9147
2 25544 51
6453 46
1285 0002133 20
6040 339
5196 15
49426741 30207
Satellite: ISS
Catalog Number: 25544
Epoch time: 20157
53969837 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 46
1285 deg
Eccentricity:
0002133
Arg of perigee: 20
6040 deg
Mean anomaly: 339
5196 deg
Mean motion: 15
49426741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 298
Coasting Arc #16 (Orbit 3035)
---------------------------------------
Vector Time (GMT): 2020/158/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3524345
89 A = 6791375
54 meter
Y = 2426894
50 meter E =
0005472
Z = 5270911
24 I = 51
88111
XDOT = -5248
194455 Wp = 44
97962
YDOT = -5499
066676 meter/sec RA = 40
57412 deg
ZDOT = -972
825434 TA = 54
33134
MA = 54
28041
Ha = 228
933 n
mi
Hp = 221
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11562814
60 X = -3576825
40
Y = 7962252
28 feet Y = 2387188
25 meter
Z = 17293015
87 Z = 5253664
28
XDOT = -17218
485745 XDOT = -5181
586749
YDOT = -18041
557336 feet/sec YDOT = -5557
383097 meter/sec
ZDOT = -3191
684495 ZDOT = -998
158578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6586160
78 X = 2007461
81
Y = 12508561
02 feet Y = 3812609
40 meter
Z = 17213451
95 Z = 5246660
16
XDOT = -18964
656344 XDOT = -5780
427254
YDOT = 14557
420570 feet/sec YDOT = 4437
101790 meter/sec
ZDOT = -3307
833379 ZDOT = -1008
227614
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
57166748
00016717 00000-0 10270-3 0 9153
2 25544 51
6445 41
0211 0002083 23
3917 336
7327 15
49437661 30363
Satellite: ISS
Catalog Number: 25544
Epoch time: 20158
57166748 = yrday
fracday
Element set: 915
Inclination: 51
6445 deg
RA of node: 41
0211 deg
Eccentricity:
0002083
Arg of perigee: 23
3917 deg
Mean anomaly: 336
7327 deg
Mean motion: 15
49437661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3036
Checksum: 300
Coasting Arc #17 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2020/159/12:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3437294
31 A = 6791528
11 meter
Y = -2613757
43 meter E =
0014880
Z = -5254844
43 I = 51
85456
XDOT = 5592
244878 Wp = 90
72103
YDOT = 5097
019119 meter/sec RA = 35
63977 deg
ZDOT = 1125
312688 TA = 190
04471
MA = 190
07448
Ha = 228
854 n
mi
Hp = 221
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11277212
31 X = 3491791
67
Y = -8575319
64 feet Y = -2575013
36 meter
Z = -17240303
25 Z = -5238015
58
XDOT = 18347
260099 XDOT = 5529
366749
YDOT = 16722
503672 feet/sec YDOT = 5159
203776 meter/sec
ZDOT = 3691
970762 ZDOT = 1152
325946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7438121
30 X = -2267139
37
Y = -12167895
01 feet Y = -3708774
40 meter
Z = -17162644
41 Z = -5231174
02
XDOT = 17523
468607 XDOT = 5341
153231
YDOT = -16082
209945 feet/sec YDOT = -4901
857591 meter/sec
ZDOT = 3815
875793 ZDOT = 1163
078942
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
53913921
00016717 00000-0 10270-3 0 9164
2 25544 51
6439 36
2325 0002106 25
7314 334
3941 15
49426941 30513
Satellite: ISS
Catalog Number: 25544
Epoch time: 20159
53913921 = yrday
fracday
Element set: 916
Inclination: 51
6439 deg
RA of node: 36
2325 deg
Eccentricity:
0002106
Arg of perigee: 25
7314 deg
Mean anomaly: 334
3941 deg
Mean motion: 15
49426941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 291
Coasting Arc #18 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2020/160/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2842517
57 A = 6791281
17 meter
Y = 3137908
83 meter E =
0004951
Z = 5306871
95 I = 51
83185
XDOT = -6171
099180 Wp = 51
01506
YDOT = -4498
843242 meter/sec RA = 32
30485 deg
ZDOT = -641
856605 TA = 45
12019
MA = 45
08000
Ha = 229
058 n
mi
Hp = 221
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9325845
04 X = -2903172
98
Y = 10294976
46 feet Y = 3105781
56 meter
Z = 17410997
20 Z = 5292917
47
XDOT = -20246
388385 XDOT = -6117
215371
YDOT = -14759
984389 feet/sec YDOT = -4567
551452 meter/sec
ZDOT = -2105
828757 ZDOT = -671
703309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13422958
21 X = -4091317
66
Y = 3875966
42 feet Y = 1181394
56 meter
Z = 17346522
04 Z = 5287219
92
XDOT = -9310
304367 XDOT = -2837
780771
YDOT = -22154
558397 feet/sec YDOT = -6752
709399 meter/sec
ZDOT = -2242
818002 ZDOT = -683
610927
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
24861767
00016717 00000-0 10270-3 0 9175
2 25544 51
6409 32
7196 0002088 33
6699 326
4584 15
49407739 30621
Satellite: ISS
Catalog Number: 25544
Epoch time: 20160
24861767 = yrday
fracday
Element set: 917
Inclination: 51
6409 deg
RA of node: 32
7196 deg
Eccentricity:
0002088
Arg of perigee: 33
6699 deg
Mean anomaly: 326
4584 deg
Mean motion: 15
49407739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 330
Coasting Arc #19 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2020/161/04:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 980162
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2718185
57 A = 6791403
09 meter
Y = -3287201
38 meter E =
0015683
Z = -5298311
04 I = 51
80358
XDOT = 6443
644369 Wp = 89
07041
YDOT = 4043
601805 meter/sec RA = 27
36740 deg
ZDOT = 799
320456 TA = 188
55721
MA = 188
58398
Ha = 229
023 n
mi
Hp = 221
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8917931
66 X = 2780477
97
Y = -10784781
43 feet Y = -3256455
41 meter
Z = -17382910
24 Z = -5284956
57
XDOT = 21140
565514 XDOT = 6394
066098
YDOT = 13266
410123 feet/sec YDOT = 4115
381865 meter/sec
ZDOT = 2622
442442 ZDOT = 830
501260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13249941
89 X = 4038582
29
Y = -4735212
94 feet Y = -1443292
90 meter
Z = -17321183
05 Z = -5279496
59
XDOT = 11167
812292 XDOT = 3403
949187
YDOT = 21160
662797 feet/sec YDOT = 6449
770021 meter/sec
ZDOT = 2765
603024 ZDOT = 842
955802
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
21608553
00016717 00000-0 10270-3 0 9186
2 25544 51
6415 27
9310 0002203 36
5304 323
5996 15
49397635 30770
Satellite: ISS
Catalog Number: 25544
Epoch time: 20161
21608553 = yrday
fracday
Element set: 918
Inclination: 51
6415 deg
RA of node: 27
9310 deg
Eccentricity:
0002203
Arg of perigee: 36
5304 deg
Mean anomaly: 323
5996 deg
Mean motion: 15
49397635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3077
Checksum: 300
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