[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 19th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14538 8138 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
231/17:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 222
2
234/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
1
238/20:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
Coasting Arc #1 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2020/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 45749
22 A = 6795045
68 meter
Y = 5038022
27 meter E =
0008960
Z = 4553222
62 I = 51
90609
XDOT = -6398
607446 Wp = 104
85480
YDOT = -2799
745923 meter/sec RA = 44
36971 deg
ZDOT = 3154
721855 TA = 313
57084
MA = 313
64519
Ha = 229
103 n
mi
Hp = 222
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 150095
87 X = -32707
30
Y = 16528944
45 feet Y = 5038094
95 meter
Z = 14938394
43 Z = 4553254
56
XDOT = -20992
806583 XDOT = -6382
147776
YDOT = -9185
518120 feet/sec YDOT = -2871
207858 meter/sec
ZDOT = 10350
137320 ZDOT = 3123
680468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9341278
24 X = 2847221
61
Y = -13637202
50 feet Y = -4156619
32 meter
Z = 14938252
60 Z = 4553179
39
XDOT = 11135
440149 XDOT = 3394
082157
YDOT = 18834
999291 feet/sec YDOT = 5740
907784 meter/sec
ZDOT = 10206
952596 ZDOT = 3111
079151
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 20230
55398756
00016717 00000-0 10270-3 0 9002
2 25544 51
6401 44
7655 0001220 30
8856 329
2365 15
49165643 1527
Satellite: ISS
Catalog Number: 25544
Epoch time: 20230
55398756 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 44
7655 deg
Eccentricity:
0001220
Arg of perigee: 30
8856 deg
Mean anomaly: 329
2365 deg
Mean motion: 15
49165643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 152
Checksum: 293
Coasting Arc #2 (Orbit 166)
---------------------------------------
Vector Time (GMT): 2020/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -402064
81 A = 6794866
32 meter
Y = -4999484
93 meter E =
0011379
Z = -4595425
33 I = 51
88145
XDOT = 6610
958842 Wp = 66
66193
YDOT = 2303
034714 meter/sec RA = 39
43930 deg
ZDOT = -3085
623777 TA = 172
50570
MA = 172
48868
Ha = 229
203 n
mi
Hp = 222
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1319110
27 X = -323807
80
Y = -16402509
62 feet Y = -5003543
42 meter
Z = -15076854
76 Z = -4597188
43
XDOT = 21689
497514 XDOT = 6599
702105
YDOT = 7555
888169 feet/sec YDOT = 2376
900327 meter/sec
ZDOT = -10123
437588 ZDOT = -3053
538400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8062388
72 X = -2457416
08
Y = 14336785
61 feet Y = 4369852
25 meter
Z = -15084707
15 Z = -4597818
74
XDOT = -12898
994195 XDOT = -3931
613431
YDOT = -17743
837714 feet/sec YDOT = -5408
321735 meter/sec
ZDOT = -9975
408962 ZDOT = -3040
504652
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 20231
52161227
00016717 00000-0 10270-3 0 9012
2 25544 51
6410 39
9777 0001434 46
5137 313
6132 15
49179465 1673
Satellite: ISS
Catalog Number: 25544
Epoch time: 20231
52161227 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 39
9777 deg
Eccentricity:
0001434
Arg of perigee: 46
5137 deg
Mean anomaly: 313
6132 deg
Mean motion: 15
49179465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 167
Checksum: 289
Coasting Arc #3 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2020/231/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3264693
38 A = 6791943
61 meter
Y = 2719609
76 meter E =
0004299
Z = 5295942
04 I = 51
86934
XDOT = -5587
879815 Wp = 54
40289
YDOT = -5185
887467 meter/sec RA = 38
26435 deg
ZDOT = -778
683455 TA = 43
03614
MA = 43
00253
Ha = 229
151 n
mi
Hp = 222
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10710936
28 X = -3320586
25
Y = 8922604
20 feet Y = 2682788
99 meter
Z = 17375137
93 Z = 5279948
14
XDOT = -18332
939025 XDOT = -5525
692063
YDOT = -17014
066492 feet/sec YDOT = -5248
027405 meter/sec
ZDOT = -2554
735746 ZDOT = -805
675584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 30256
48 X = 9222
18
Y = -14032197
73 feet Y = -4277013
87 meter
Z = 17301125
73 Z = 5273383
12
XDOT = 23761
574524 XDOT = 7242
527915
YDOT = -3263
663783 feet/sec YDOT = -994
764721 meter/sec
ZDOT = -2679
076685 ZDOT = -816
582573
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 20231
77964303
00016717 00000-0 10270-3 0 9026
2 25544 51
6446 38
7020 0001110 37
0600 323
0626 15
49203669 1713
Satellite: ISS
Catalog Number: 25544
Epoch time: 20231
77964303 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 38
7020 deg
Eccentricity:
0001110
Arg of perigee: 37
0600 deg
Mean anomaly: 323
0626 deg
Mean motion: 15
49203669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 263
Coasting Arc #4 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2020/232/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3082179
74 A = 6792117
92 meter
Y = -2953671
08 meter E =
0015143
Z = -5296042
44 I = 51
84107
XDOT = 5963
911788 Wp = 92
66793
YDOT = 4714
948531 meter/sec RA = 33
33271 deg
ZDOT = 842
673924 TA = 185
37796
MA = 185
39425
Ha = 229
141 n
mi
Hp = 222
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10112138
26 X = 3140704
05
Y = -9690521
93 feet Y = -2918876
74 meter
Z = -17375467
33 Z = -5280928
62
XDOT = 19566
639726 XDOT = 5906
651442
YDOT = 15468
991245 feet/sec YDOT = 4781
321101 meter/sec
ZDOT = 2764
678227 ZDOT = 871
504493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1184819
66 X = 361133
03
Y = 14042221
04 feet Y = 4280068
97 meter
Z = -17305509
27 Z = -5274719
22
XDOT = -23263
236945 XDOT = -7090
634621
YDOT = 5528
065237 feet/sec YDOT = 1684
954284 meter/sec
ZDOT = 2897
527115 ZDOT = 883
166265
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 20232
74726802
00016717 00000-0 10270-3 0 9035
2 25544 51
6434 33
9154 0001197 41
5885 318
5356 15
49161078 1867
Satellite: ISS
Catalog Number: 25544
Epoch time: 20232
74726802 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 33
9154 deg
Eccentricity:
0001197
Arg of perigee: 41
5885 deg
Mean anomaly: 318
5356 deg
Mean motion: 15
49161078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 186
Checksum: 306
Coasting Arc #5 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2020/233/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2882784
63 A = 6792041
28 meter
Y = 3157624
68 meter E =
0004587
Z = 5274518
04 I = 51
81305
XDOT = -6320
275693 Wp = 54
36496
YDOT = -4235
677618 meter/sec RA = 28
39827 deg
ZDOT = -915
462194 TA = 44
39554
MA = 44
35878
Ha = 229
165 n
mi
Hp = 222
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9457954
81 X = -2943499
97
Y = 10359661
01 feet Y = 3125047
98 meter
Z = 17304849
20 Z = 5260367
32
XDOT = -20735
812642 XDOT = -6267
994639
YDOT = -13896
580110 feet/sec YDOT = -4306
063166 meter/sec
ZDOT = -3003
484890 ZDOT = -946
035921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2355844
15 X = -718061
30
Y = -13910023
37 feet Y = -4239775
12 meter
Z = 17239331
18 Z = 5254548
15
XDOT = 22640
612029 XDOT = 6900
858546
YDOT = -7744
397007 feet/sec YDOT = -2360
492208 meter/sec
ZDOT = -3144
398272 ZDOT = -958
412593
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 20233
77939838
00016717 00000-0 10270-3 0 9045
2 25544 51
6442 28
8086 0001090 42
9226 317
2009 15
49198894 2025
Satellite: ISS
Catalog Number: 25544
Epoch time: 20233
77939838 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 28
8086 deg
Eccentricity:
0001090
Arg of perigee: 42
9226 deg
Mean anomaly: 317
2009 deg
Mean motion: 15
49198894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 202
Checksum: 314
Coasting Arc #6 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2020/234/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5180890
11 A = 6802300
20 meter
Y = -4012385
38 meter E =
0006985
Z = -1819198
28 I = 51
82470
XDOT = 4245
658933 Wp = 128
76740
YDOT = -2923
888796 meter/sec RA = 25
14894 deg
ZDOT = -5661
246344 TA = 71
12631
MA = 71
05059
Ha = 229
142 n
mi
Hp = 222
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16997670
97 X = -5126800
88
Y = -13163994
03 feet Y = -4070019
44 meter
Z = -5968498
29 Z = -1844233
09
XDOT = 13929
327207 XDOT = 4305
537846
YDOT = -9592
811010 feet/sec YDOT = -2876
076205 meter/sec
ZDOT = -18573
642861 ZDOT = -5640
477387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5939197
49 X = -1810267
39
Y = 20628798
14 feet Y = 6287657
67 meter
Z = -6083843
29 Z = -1854355
43
XDOT = -12617
062832 XDOT = -3845
680751
YDOT = -9064
009856 feet/sec YDOT = -2762
710204 meter/sec
ZDOT = -18477
587001 ZDOT = -5631
968518
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 20234
42448036
00016717 00000-0 10270-3 0 9054
2 25544 51
6416 25
6166 0001473 37
4363 322
6889 15
49179573 2126
Satellite: ISS
Catalog Number: 25544
Epoch time: 20234
42448036 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 25
6166 deg
Eccentricity:
0001473
Arg of perigee: 37
4363 deg
Mean anomaly: 322
6889 deg
Mean motion: 15
49179573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 304
Coasting Arc #7 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2020/235/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5471639
10 A = 6802260
67 meter
Y = 3573982
62 meter E =
0015244
Z = 1859386
64 I = 51
79307
XDOT = -4045
979462 Wp = 64
54431
YDOT = 3243
228047 meter/sec RA = 20
21128 deg
ZDOT = 5642
535972 TA = 315
83594
MA = 315
95755
Ha = 229
183 n
mi
Hp = 222
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17951571
84 X = 5422235
35
Y = 11725664
76 feet Y = 3634894
24 meter
Z = 6100349
89 Z = 1885845
31
XDOT = -13274
210834 XDOT = -4109
353433
YDOT = 10640
511964 feet/sec YDOT = 3197
628893 meter/sec
ZDOT = 18512
257127 ZDOT = 5622
728341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3888535
65 X = 1185225
67
Y = -21050580
44 feet Y = -6416216
92 meter
Z = 6222279
96 Z = 1896550
93
XDOT = 13460
299550 XDOT = 4102
699303
YDOT = 7959
580405 feet/sec YDOT = 2426
080107 meter/sec
ZDOT = 18420
628134 ZDOT = 5614
607455
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 20235
45660922
00016717 00000-0 10270-3 0 9069
2 25544 51
6413 20
5090 0001416 46
4214 313
7054 15
49173106 2283
Satellite: ISS
Catalog Number: 25544
Epoch time: 20235
45660922 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 20
5090 deg
Eccentricity:
0001416
Arg of perigee: 46
4214 deg
Mean anomaly: 313
7054 deg
Mean motion: 15
49173106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 228
Checksum: 266
Coasting Arc #8 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2020/236/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5711568
60 A = 6802060
10 meter
Y = -3142424
28 meter E =
0006981
Z = -1937626
51 I = 51
76023
XDOT = 3838
209989 Wp = 126
28732
YDOT = -3531
035851 meter/sec RA = 15
27269 deg
ZDOT = -5605
459369 TA = 74
98160
MA = 74
90435
Ha = 229
224 n
mi
Hp = 221
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18738742
12 X = -5666592
75
Y = -10309790
94 feet Y = -3206043
71 meter
Z = -6357042
34 Z = -1965261
57
XDOT = 12592
552458 XDOT = 3904
637785
YDOT = -11584
763290 feet/sec YDOT = -3487
742995 meter/sec
ZDOT = -18390
614727 ZDOT = -5586
653507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1913633
85 X = -583275
60
Y = 21263457
34 feet Y = 6481101
80 meter
Z = -6484413
67 Z = -1976449
29
XDOT = -14174
048744 XDOT = -4320
250057
YDOT = -6839
632546 feet/sec YDOT = -2084
720000 meter/sec
ZDOT = -18303
598812 ZDOT = -5578
936918
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 20236
42422934
00016717 00000-0 10270-3 0 9077
2 25544 51
6410 15
7217 0001605 49
5608 310
5681 15
49194293 2436
Satellite: ISS
Catalog Number: 25544
Epoch time: 20236
42422934 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 15
7217 deg
Eccentricity:
0001605
Arg of perigee: 49
5608 deg
Mean anomaly: 310
5681 deg
Mean motion: 15
49194293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 243
Checksum: 287
Coasting Arc #9 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2020/237/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5928377
58 A = 6802066
08 meter
Y = 2666799
82 meter E =
0015296
Z = 1977665
93 I = 51
72651
XDOT = -3592
944327 Wp = 67
15290
YDOT = 3824
219603 meter/sec RA = 10
33120 deg
ZDOT = 5584
997984 TA = 314
60865
MA = 314
73334
Ha = 229
234 n
mi
Hp = 221
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19450057
67 X = 5888509
68
Y = 8749343
24 feet Y = 2732872
29 meter
Z = 6488405
27 Z = 2006366
70
XDOT = -11787
875087 XDOT = -3662
569500
YDOT = 12546
652240 feet/sec YDOT = 3783
651501 meter/sec
ZDOT = 18323
484200 ZDOT = 5567
375770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -166932
67 X = -50881
08
Y = -21285992
57 feet Y = -6487970
54 meter
Z = 6620710
46 Z = 2017992
55
XDOT = 14827
196067 XDOT = 4519
329361
YDOT = 5586
256048 feet/sec YDOT = 1702
690843 meter/sec
ZDOT = 18241
917837 ZDOT = 5560
136557
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 20237
45635761
00016717 00000-0 10270-3 0 9086
2 25544 51
6404 10
6147 0001417 59
2493 300
8796 15
49171110 2595
Satellite: ISS
Catalog Number: 25544
Epoch time: 20237
45635761 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 10
6147 deg
Eccentricity:
0001417
Arg of perigee: 59
2493 deg
Mean anomaly: 300
8796 deg
Mean motion: 15
49171110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 259
Checksum: 295
Coasting Arc #10 (Orbit 273)
---------------------------------------
Vector Time (GMT): 2020/238/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6094984
90 A = 6801820
51 meter
Y = -2206974
83 meter E =
0006862
Z = -2057083
32 I = 51
69399
XDOT = 3344
753119 Wp = 124
99563
YDOT = -4084
331777 meter/sec RA = 5
38772 deg
ZDOT = -5545
280203 TA = 77
67674
MA = 77
59993
Ha = 229
235 n
mi
Hp = 221
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19996669
62 X = -6059860
75
Y = -7240731
05 feet Y = -2274936
90 meter
Z = -6748961
03 Z = -2086604
99
XDOT = 10973
599472 XDOT = 3417
112467
YDOT = -13400
038640 feet/sec YDOT = -4046
523720 meter/sec
ZDOT = -18193
176518 ZDOT = -5528
857042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2128669
37 X = 648818
42
Y = 21116534
13 feet Y = 6436319
60 meter
Z = -6885071
53 Z = -2098569
80
XDOT = -15348
382134 XDOT = -4678
186875
YDOT = -4342
115857 feet/sec YDOT = -1323
476913 meter/sec
ZDOT = -18117
130678 ZDOT = -5522
101431
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 20238
42397510
00016717 00000-0 10270-3 0 9092
2 25544 51
6418 5
8270 0001586 57
5159 302
6145 15
49204572 2744
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
42397510 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 5
8270 deg
Eccentricity:
0001586
Arg of perigee: 57
5159 deg
Mean anomaly: 302
6145 deg
Mean motion: 15
49204572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 274
Checksum: 300
Coasting Arc #11 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2020/238/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4115794
68 A = 6796500
81 meter
Y = -3499771
23 meter E =
0009348
Z = -4133614
54 I = 51
66104
XDOT = 6081
842948 Wp = 68
02989
YDOT = -2673
000877 meter/sec RA = 3
13962 deg
ZDOT = -3795
991914 TA = 162
74973
MA = 162
71794
Ha = 229
368 n
mi
Hp = 221
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13503263
37 X = -4056274
63
Y = -11482189
09 feet Y = -3545464
12 meter
Z = -13561727
50 Z = -4153462
88
XDOT = 19953
552978 XDOT = 6129
719916
YDOT = -8769
687918 feet/sec YDOT = -2604
721595 meter/sec
ZDOT = -12454
041714 ZDOT = -3766
332581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8838697
65 X = 2694035
04
Y = -15282971
15 feet Y = -4658249
61 meter
Z = -13653111
64 Z = -4161468
43
XDOT = 11170
165577 XDOT = 3404
666468
YDOT = 17453
388049 feet/sec YDOT = 5319
792677 meter/sec
ZDOT = -12316
999088 ZDOT = -3754
221322
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 20238
87552939
00016717 00000-0 10270-3 0 9101
2 25544 51
6422 3
5962 0001734 59
2656 300
8665 15
49168746 2815
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
87552939 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 3
5962 deg
Eccentricity:
0001734
Arg of perigee: 59
2656 deg
Mean anomaly: 300
8665 deg
Mean motion: 15
49168746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 320
Coasting Arc #12 (Orbit 296)
---------------------------------------
Vector Time (GMT): 2020/239/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4340452
18 A = 6796330
50 meter
Y = 3158506
05 meter E =
0011390
Z = 4159616
97 I = 51
62587
XDOT = -5895
499024 Wp = 98
22071
YDOT = 3154
106668 meter/sec RA = 358
19284 deg
ZDOT = 3746
415993 TA = 313
15876
MA = 313
25391
Ha = 229
216 n
mi
Hp = 221
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14240328
66 X = 4284605
32
Y = 10362552
65 feet Y = 3206731
70 meter
Z = 13647037
32 Z = 4180565
51
XDOT = -19342
188400 XDOT = -5948
528847
YDOT = 10348
118989 feet/sec YDOT = 3087
882353 meter/sec
ZDOT = 12291
391052 ZDOT = 3717
649465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7330384
52 X = -2234301
20
Y = 15930862
12 feet Y = 4855726
77 meter
Z = 13743514
12 Z = 4189023
10
XDOT = -12856
792052 XDOT = -3918
750217
YDOT = -16434
145724 feet/sec YDOT = -5009
127617 meter/sec
ZDOT = 12158
445002 ZDOT = 3705
894036
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 20239
90765220
00016717 00000-0 10270-3 0 9116
2 25544 51
6413 358
4899 0001641 56
9567 303
1740 15
49186138 2970
Satellite: ISS
Catalog Number: 25544
Epoch time: 20239
90765220 = yrday
fracday
Element set: 911
Inclination: 51
6413 deg
RA of node: 358
4899 deg
Eccentricity:
0001641
Arg of perigee: 56
9567 deg
Mean anomaly: 303
1740 deg
Mean motion: 15
49186138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 297
Checksum: 320
Coasting Arc #13 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2020/240/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4529940
56 A = 6796216
21 meter
Y = -2827776
35 meter E =
0009796
Z = -4214139
19 I = 51
59118
XDOT = 5662
864954 Wp = 68
07300
YDOT = -3603
213161 meter/sec RA = 353
24272 deg
ZDOT = -3672
704019 TA = 164
16565
MA = 164
13500
Ha = 229
386 n
mi
Hp = 221
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14862009
70 X = -4477513
19
Y = -9277481
45 feet Y = -2878140
09 meter
Z = -13825915
99 Z = -4236016
40
XDOT = 18578
953261 XDOT = 5720
575988
YDOT = -11821
565489 feet/sec YDOT = -3539
564138 meter/sec
ZDOT = -12049
553869 ZDOT = -3645
056304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5861629
16 X = 1786624
57
Y = -16425450
13 feet Y = -5006477
20 meter
Z = -13926695
19 Z = -4244856
69
XDOT = 14383
471858 XDOT = 4384
082222
YDOT = 15231
927177 feet/sec YDOT = 4642
691403 meter/sec
ZDOT = -11921
749590 ZDOT = -3633
749275
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 20240
87526820
00016717 00000-0 10270-3 0 9126
2 25544 51
6409 353
7019 0001740 61
9395 298
1930 15
49165541 3129
Satellite: ISS
Catalog Number: 25544
Epoch time: 20240
87526820 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 353
7019 deg
Eccentricity:
0001740
Arg of perigee: 61
9395 deg
Mean anomaly: 298
1930 deg
Mean motion: 15
49165541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 299
Coasting Arc #14 (Orbit 327)
---------------------------------------
Vector Time (GMT): 2020/241/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4698060
45 A = 6795973
13 meter
Y = 2463408
18 meter E =
0011082
Z = 4239844
82 I = 51
55785
XDOT = -5402
725353 Wp = 100
64556
YDOT = 4054
795165 meter/sec RA = 348
29150 deg
ZDOT = 3620
657095 TA = 312
21137
MA = 312
30538
Ha = 229
157 n
mi
Hp = 221
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15413584
16 X = 4649570
29
Y = 8082047
84 feet Y = 2515674
00 meter
Z = 13910252
02 Z = 4262548
11
XDOT = -17725
476879 XDOT = -5465
252563
YDOT = 13303
133744 feet/sec YDOT = 3994
028303 meter/sec
ZDOT = 11878
796243 ZDOT = 3594
261427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4287255
82 X = -1306755
58
Y = 16780829
25 feet Y = 5114796
76 meter
Z = 14014863
26 Z = 4271730
32
XDOT = -15865
997642 XDOT = -4835
956081
YDOT = -13899
811055 feet/sec YDOT = -4236
662410 meter/sec
ZDOT = 11756
750329 ZDOT = 3583
457500
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 20241
90738857
00016717 00000-0 10270-3 0 9137
2 25544 51
6413 348
5959 0001539 63
0630 297
0678 15
49207227 3282
Satellite: ISS
Catalog Number: 25544
Epoch time: 20241
90738857 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 348
5959 deg
Eccentricity:
0001539
Arg of perigee: 63
0630 deg
Mean anomaly: 297
0678 deg
Mean motion: 15
49207227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 328
Checksum: 323
Coasting Arc #15 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2020/242/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4832848
19 A = 6795875
67 meter
Y = -2115907
35 meter E =
0010287
Z = -4294466
64 I = 51
52523
XDOT = 5101
716453 Wp = 68
30237
YDOT = -4466
724707 meter/sec RA = 343
33629 deg
ZDOT = -3543
657162 TA = 165
44056
MA = 165
41090
Ha = 229
387 n
mi
Hp = 221
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15855801
13 X = -4787968
61
Y = -6941953
25 feet Y = -2169700
71 meter
Z = -14089457
47 Z = -4317833
32
XDOT = 16737
914871 XDOT = 5168
498284
YDOT = -14654
608620 feet/sec YDOT = -4409
300206 meter/sec
ZDOT = -11626
171791 ZDOT = -3518
713349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2783850
75 X = 848517
71
Y = -16994149
05 feet Y = -5179816
63 meter
Z = -14197148
64 Z = -4327290
91
XDOT = 17153
728595 XDOT = 5228
456476
YDOT = 12417
751129 feet/sec YDOT = 3784
930544 meter/sec
ZDOT = -11510
811695 ZDOT = -3508
495405
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 20242
87500139
00016717 00000-0 10270-3 0 9145
2 25544 51
6421 343
8075 0001782 64
7914 295
3421 15
49180640 3434
Satellite: ISS
Catalog Number: 25544
Epoch time: 20242
87500139 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 343
8075 deg
Eccentricity:
0001782
Arg of perigee: 64
7914 deg
Mean anomaly: 295
3421 deg
Mean motion: 15
49180640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 293
Coasting Arc #16 (Orbit 358)
---------------------------------------
Vector Time (GMT): 2020/243/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4942042
29 A = 6795632
63 meter
Y = 1739007
14 meter E =
0010830
Z = 4320372
47 I = 51
49259
XDOT = -4773
790136 Wp = 102
30589
YDOT = 4877
079816 meter/sec RA = 338
38092 deg
ZDOT = 3487
939584 TA = 312
08727
MA = 312
17931
Ha = 229
153 n
mi
Hp = 221
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16214049
50 X = 4901243
41
Y = 5705404
01 feet Y = 1794044
50 meter
Z = 14174450
37 Z = 4344279
40
XDOT = -15662
041128 XDOT = -4844
914389
YDOT = 16000
918030 feet/sec YDOT = 4823
298213 meter/sec
ZDOT = 11443
371337 ZDOT = 3464
578076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1203972
40 X = -366970
79
Y = 17054653
43 feet Y = 5198258
36 meter
Z = 14284653
52 Z = 4353962
39
XDOT = -18374
200955 XDOT = -5600
456451
YDOT = -10817
740105 feet/sec YDOT = -3297
247184 meter/sec
ZDOT = 11335
302465 ZDOT = 3455
000191
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 20243
90711761
00016717 00000-0 10270-3 0 9156
2 25544 51
6419 338
7018 0001596 66
4644 293
6674 15
49221073 3597
Satellite: ISS
Catalog Number: 25544
Epoch time: 20243
90711761 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 338
7018 deg
Eccentricity:
0001596
Arg of perigee: 66
4644 deg
Mean anomaly: 293
6674 deg
Mean motion: 15
49221073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 359
Checksum: 317
Coasting Arc #17 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2020/244/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5023026
47 A = 6795557
95 meter
Y = -1382929
16 meter E =
0010713
Z = -4374084
93 I = 51
46083
XDOT = 4408
904463 Wp = 68
68370
YDOT = -5241
776696 meter/sec RA = 333
42172 deg
ZDOT = -3408
705152 TA = 166
60750
MA = 166
57904
Ha = 229
377 n
mi
Hp = 221
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16479745
64 X = -4985942
44
Y = -4537169
17 feet Y = -1438893
01 meter
Z = -14350672
34 Z = -4398394
24
XDOT = 14464
909656 XDOT = 4483
749121
YDOT = -17197
430104 feet/sec YDOT = -5192
054780 meter/sec
ZDOT = -11183
415854 ZDOT = -3387
106920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -284884
05 X = -86832
66
Y = -16995807
76 feet Y = -5180322
21 meter
Z = -14462747
89 Z = -4408245
56
XDOT = 19371
364294 XDOT = 5904
391837
YDOT = 9098
703290 feet/sec YDOT = 2773
284763 meter/sec
ZDOT = -11083
478763 ZDOT = -3378
244327
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 20244
87472918
00016717 00000-0 10270-3 0 9162
2 25544 51
6417 333
9139 0001759 67
4295 292
7042 15
49187853 3743
Satellite: ISS
Catalog Number: 25544
Epoch time: 20244
87472918 = yrday
fracday
Element set: 916
Inclination: 51
6417 deg
RA of node: 333
9139 deg
Eccentricity:
0001759
Arg of perigee: 67
4295 deg
Mean anomaly: 292
7042 deg
Mean motion: 15
49187853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 339
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