[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 21st 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 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
There are no maneuvers
Coasting Arc #1 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2020/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5379849
16 A = 6801789
43 meter
Y = 3800758
45 meter E =
0015382
Z = 1669491
70 I = 51
50160
XDOT = -4025
220986 Wp = 110
15439
YDOT = -3181
083481 meter/sec RA = 336
38971 deg
ZDOT = -5691
485512 TA = 51
54979
MA = 51
41185
Ha = 229
095 n
mi
Hp = 221
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17650423
76 X = -5430060
00
Y = 12469679
94 feet Y = 3740316
07 meter
Z = 5477334
96 Z = 1643237
15
XDOT = -13206
105597 XDOT = -3961
703900
YDOT = -10436
625593 feet/sec YDOT = -3225
740127 meter/sec
ZDOT = -18672
852729 ZDOT = -5710
884894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11613947
66 X = 3539931
25
Y = 18260833
55 feet Y = 5565902
07 meter
Z = 5356281
63 Z = 1632594
64
XDOT = -9716
754274 XDOT = -2961
666703
YDOT = 11720
050897 feet/sec YDOT = 3572
271513 meter/sec
ZDOT = -18761
805278 ZDOT = -5718
598249
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
53549068
00016717 00000-0 10270-3 0 9008
2 25544 51
6398 336
8471 0002126 68
3295 291
8082 15
49468267 32377
Satellite: ISS
Catalog Number: 25544
Epoch time: 20171
53549068 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 336
8471 deg
Eccentricity:
0002126
Arg of perigee: 68
3295 deg
Mean anomaly: 291
8082 deg
Mean motion: 15
49468267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 329
Coasting Arc #2 (Orbit 3251)
---------------------------------------
Vector Time (GMT): 2020/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5129146
90 A = 6802000
98 meter
Y = -4188778
08 meter E =
0010143
Z = -1539426
05 I = 51
47340
XDOT = 4125
315161 Wp = 45
69546
YDOT = 2954
328589 meter/sec RA = 331
42894 deg
ZDOT = 5736
653263 TA = 297
48077
MA = 297
58385
Ha = 229
227 n
mi
Hp = 221
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16827909
78 X = 5183083
52
Y = -13742710
25 feet Y = -4131118
41 meter
Z = -5050610
40 Z = -1514380
48
XDOT = 13534
498561 XDOT = 4064
106964
YDOT = 9692
679098 feet/sec YDOT = 3000
117383 meter/sec
ZDOT = 18821
040890 ZDOT = 5756
544408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13223859
04 X = -4030632
24
Y = -17272050
56 feet Y = -5264521
01 meter
Z = -4935090
61 Z = -1504215
62
XDOT = 8837
417482 XDOT = 2693
644848
YDOT = -12140
680130 feet/sec YDOT = -3700
479304 meter/sec
ZDOT = 18912
273325 ZDOT = 5764
460910
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
50294005
00016717 00000-0 10270-3 0 9015
2 25544 51
6415 332
0580 0002310 77
6183 282
5226 15
49451199 32520
Satellite: ISS
Catalog Number: 25544
Epoch time: 20172
50294005 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 332
0580 deg
Eccentricity:
0002310
Arg of perigee: 77
6183 deg
Mean anomaly: 282
5226 deg
Mean motion: 15
49451199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3252
Checksum: 279
Coasting Arc #3 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2020/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4875339
20 A = 6802195
48 meter
Y = 4533659
01 meter E =
0015543
Z = 1362373
69 I = 51
44394
XDOT = -4194
234585 Wp = 114
24653
YDOT = -2756
602179 meter/sec RA = 326
46672 deg
ZDOT = -5789
950999 TA = 50
89868
MA = 50
76056
Ha = 229
187 n
mi
Hp = 221
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15995207
34 X = -4932291
19
Y = 14874209
34 feet Y = 4478820
76 meter
Z = 4469729
95 Z = 1338553
90
XDOT = -13760
612156 XDOT = -4134
973530
YDOT = -9043
970403 feet/sec YDOT = -2803
172514 meter/sec
ZDOT = -18995
902228 ZDOT = -5810
181552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14661427
04 X = 4468802
96
Y = 16220410
82 feet Y = 4943981
22 meter
Z = 4359825
35 Z = 1328874
77
XDOT = -8041
516997 XDOT = -2451
054381
YDOT = 12441
050780 feet/sec YDOT = 3792
032278 meter/sec
ZDOT = -19088
713599 ZDOT = -5818
239905
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 20173
53488267
00016717 00000-0 10270-3 0 9025
2 25544 51
6403 326
9496 0002290 78
6532 281
4875 15
49459007 32682
Satellite: ISS
Catalog Number: 25544
Epoch time: 20173
53488267 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 326
9496 deg
Eccentricity:
0002290
Arg of perigee: 78
6532 deg
Mean anomaly: 281
4875 deg
Mean motion: 15
49459007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 331
Coasting Arc #4 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4566178
64 A = 6802352
63 meter
Y = -4884728
73 meter E =
0010891
Z = -1229284
90 I = 51
41828
XDOT = 4274
194837 Wp = 46
73478
YDOT = 2539
310129 meter/sec RA = 321
50318 deg
ZDOT = 5826
180408 TA = 299
89151
MA = 299
99966
Ha = 229
242 n
mi
Hp = 221
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14980901
04 X = 4626432
88
Y = -16026012
89 feet Y = -4833329
30 meter
Z = -4033086
94 Z = -1206959
04
XDOT = 14022
948940 XDOT = 4217
181815
YDOT = 8331
069978 feet/sec YDOT = 2586
787202 meter/sec
ZDOT = 19114
765117 ZDOT = 5846
804691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16085982
15 X = -4903007
36
Y = -14943971
97 feet Y = -4554922
66 meter
Z = -3930032
48 Z = -1197873
90
XDOT = 7186
905855 XDOT = 2190
568905
YDOT = -12752
506787 feet/sec YDOT = -3886
964069 meter/sec
ZDOT = 19209
408360 ZDOT = 5855
027668
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 20174
50233003
00016717 00000-0 10270-3 0 9030
2 25544 51
6416 322
1617 0002339 85
2993 274
8424 15
49450369 32833
Satellite: ISS
Catalog Number: 25544
Epoch time: 20174
50233003 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 322
1617 deg
Eccentricity:
0002339
Arg of perigee: 85
2993 deg
Mean anomaly: 274
8424 deg
Mean motion: 15
49450369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3283
Checksum: 297
Coasting Arc #5 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2020/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4259186
20 A = 6802509
02 meter
Y = 5190536
97 meter E =
0015374
Z = 1048949
55 I = 51
39320
XDOT = -4328
232004 Wp = 118
58360
YDOT = -2353
865695 meter/sec RA = 316
53713 deg
ZDOT = -5868
379030 TA = 50
02429
MA = 49
88939
Ha = 229
170 n
mi
Hp = 221
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13973708
01 X = -4322006
92
Y = 17029320
77 feet Y = 5142556
25 meter
Z = 3441435
52 Z = 1028108
80
XDOT = -14200
236233 XDOT = -4273
083809
YDOT = -7722
656481 feet/sec YDOT = -2401
957522 meter/sec
ZDOT = -19253
212041 ZDOT = -5889
270180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17322280
36 X = 5279831
05
Y = 13632828
59 feet Y = 4155286
15 meter
Z = 3345197
68 Z = 1019616
25
XDOT = -6429
745226 XDOT = -1959
786345
YDOT = 12966
061448 feet/sec YDOT = 3952
055529 meter/sec
ZDOT = -19349
101972 ZDOT = -5897
606281
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 20175
53427170
00016717 00000-0 10270-3 0 9045
2 25544 51
6416 317
0533 0002231 87
3068 272
8337 15
49456341 32994
Satellite: ISS
Catalog Number: 25544
Epoch time: 20175
53427170 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 317
0533 deg
Eccentricity:
0002231
Arg of perigee: 87
3068 deg
Mean anomaly: 272
8337 deg
Mean motion: 15
49456341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3299
Checksum: 303
Coasting Arc #6 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2020/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3898675
79 A = 6802617
16 meter
Y = -5494195
27 meter E =
0011682
Z = -912019
87 I = 51
37145
XDOT = 4392
644372 Wp = 47
73523
YDOT = 2147
670356 meter/sec RA = 311
56991 deg
ZDOT = 5895
832665 TA = 302
37665
MA = 302
48965
Ha = 229
231 n
mi
Hp = 221
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12790931
06 X = 3964253
76
Y = -18025575
04 feet Y = -5450230
66 meter
Z = -2992191
18 Z = -892923
65
XDOT = 14411
562899 XDOT = 4339
663863
YDOT = 7046
162585 feet/sec YDOT = 2196
494707 meter/sec
ZDOT = 19343
283023 ZDOT = 5917
041821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18504198
33 X = -5640079
65
Y = -12109669
72 feet Y = -3691027
33 meter
Z = -2903967
04 Z = -885129
16
XDOT = 5610
873292 XDOT = 1710
194180
YDOT = -13190
046865 feet/sec YDOT = -4020
326284 meter/sec
ZDOT = 19440
656110 ZDOT = 5925
511982
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 20176
50171568
00016717 00000-0 10270-3 0 9051
2 25544 51
6432 312
2651 0002340 89
0786 271
0633 15
49454025 33142
Satellite: ISS
Catalog Number: 25544
Epoch time: 20176
50171568 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 312
2651 deg
Eccentricity:
0002340
Arg of perigee: 89
0786 deg
Mean anomaly: 271
0633 deg
Mean motion: 15
49454025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3314
Checksum: 287
Coasting Arc #7 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2020/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3546655
63 A = 6802728
68 meter
Y = 5751399
83 meter E =
0015153
Z = 727707
32 I = 51
34940
XDOT = -4436
586413 Wp = 122
09872
YDOT = -1975
506053 meter/sec RA = 306
60139 deg
ZDOT = -5926
438384 TA = 50
02074
MA = 49
88777
Ha = 229
192 n
mi
Hp = 221
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11636009
29 X = -3614240
63
Y = 18869422
03 feet Y = 5711360
59 meter
Z = 2387491
22 Z = 710316
11
XDOT = -14555
729703 XDOT = -4385
379196
YDOT = -6481
319072 feet/sec YDOT = -2024
831847 meter/sec
ZDOT = -19443
695485 ZDOT = -5947
865196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19487869
00 X = 5939902
47
Y = 10585468
23 feet Y = 3226450
72 meter
Z = 2307106
05 Z = 703205
92
XDOT = -4899
019211 XDOT = -1493
221055
YDOT = 13339
732965 feet/sec YDOT = 4065
950608 meter/sec
ZDOT = -19542
086539 ZDOT = -5956
427977
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 20177
53365428
00016717 00000-0 10270-3 0 9066
2 25544 51
6422 307
1575 0002325 92
6699 267
4718 15
49459597 33305
Satellite: ISS
Catalog Number: 25544
Epoch time: 20177
53365428 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 307
1575 deg
Eccentricity:
0002325
Arg of perigee: 92
6699 deg
Mean anomaly: 267
4718 deg
Mean motion: 15
49459597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 335
Coasting Arc #8 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2020/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3142336
73 A = 6802820
34 meter
Y = -5999487
20 meter E =
0012363
Z = -588473
93 I = 51
33091
XDOT = 4491
705931 Wp = 49
71057
YDOT = 1778
434345 meter/sec RA = 301
63139 deg
ZDOT = 5944
427849 TA = 303
92392
MA = 304
04141
Ha = 229
226 n
mi
Hp = 221
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10309503
70 X = 3212049
66
Y = -19683356
97 feet Y = -5963957
48 meter
Z = -1930688
74 Z = -573041
41
XDOT = 14736
568015 XDOT = 4442
610906
YDOT = 5834
758351 feet/sec YDOT = 1828
388479 meter/sec
ZDOT = 19502
716039 ZDOT = 5966
127491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20382117
52 X = -6212469
42
Y = -8863419
85 feet Y = -2701570
37 meter
Z = -1859312
02 Z = -566718
30
XDOT = 4111
875277 XDOT = 1253
299585
YDOT = -13502
808433 feet/sec YDOT = -4115
656011 meter/sec
ZDOT = 19602
378774 ZDOT = 5974
805050
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 20178
50109655
00016717 00000-0 10270-3 0 9073
2 25544 51
6426 302
3695 0002341 95
2545 264
8872 15
49451420 33451
Satellite: ISS
Catalog Number: 25544
Epoch time: 20178
50109655 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 302
3695 deg
Eccentricity:
0002341
Arg of perigee: 95
2545 deg
Mean anomaly: 264
8872 deg
Mean motion: 15
49451420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 308
Coasting Arc #9 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2020/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2753244
18 A = 6802864
51 meter
Y = 6200716
21 meter E =
0014731
Z = 401731
73 I = 51
31454
XDOT = -4531
421530 Wp = 126
00005
YDOT = -1616
284202 meter/sec RA = 296
65984 deg
ZDOT = -5963
129380 TA = 49
65710
MA = 49
52853
Ha = 229
152 n
mi
Hp = 221
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9032953
36 X = -2824329
17
Y = 20343557
12 feet Y = 6169529
96 meter
Z = 1318017
49 Z = 388185
78
XDOT = -14866
868537 XDOT = -4484
045821
YDOT = -5302
769691 feet/sec YDOT = -1666
692182 meter/sec
ZDOT = -19564
072769 ZDOT = -5985
026145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21073951
64 X = 6423340
46
Y = 7176661
03 feet Y = 2187446
28 meter
Z = 1255321
18 Z = 382621
89
XDOT = -3434
830300 XDOT = -1046
936275
YDOT = 13613
524008 feet/sec YDOT = 4149
402118 meter/sec
ZDOT = -19664
654857 ZDOT = -5993
786800
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 20179
53303300
00016717 00000-0 10270-3 0 9081
2 25544 51
6426 297
2614 0002266 100
0140 260
1266 15
49463083 33618
Satellite: ISS
Catalog Number: 25544
Epoch time: 20179
53303300 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 297
2614 deg
Eccentricity:
0002266
Arg of perigee: 100
0140 deg
Mean anomaly: 260
1266 deg
Mean motion: 15
49463083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 273
Coasting Arc #10 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2020/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2315863
90 A = 6802912
47 meter
Y = -6385848
58 meter E =
0013083
Z = -259477
38 I = 51
30151
XDOT = 4580
759249 Wp = 51
92616
YDOT = 1427
293446 meter/sec RA = 291
68706 deg
ZDOT = 5971
670699 TA = 305
27043
MA = 305
39276
Ha = 229
216 n
mi
Hp = 221
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7597978
66 X = 2388360
62
Y = -20950946
77 feet Y = -6359545
55 meter
Z = -851303
76 Z = -248052
54
XDOT = 15028
737693 XDOT = 4535
451603
YDOT = 4682
721279 feet/sec YDOT = 1478
264750 meter/sec
ZDOT = 19592
095470 ZDOT = 5993
812218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21644284
14 X = -6597177
80
Y = -5318246
34 feet Y = -1621001
49 meter
Z = -798366
08 Z = -243341
98
XDOT = 2675
370167 XDOT = 815
452827
YDOT = -13732
178236 feet/sec YDOT = -4185
567926 meter/sec
ZDOT = 19693
816478 ZDOT = 6002
675263
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 20180
50047177
00016717 00000-0 10270-3 0 9098
2 25544 51
6435 292
4730 0002371 98
6876 261
4543 15
49457984 33760
Satellite: ISS
Catalog Number: 25544
Epoch time: 20180
50047177 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 292
4730 deg
Eccentricity:
0002371
Arg of perigee: 98
6876 deg
Mean anomaly: 261
4543 deg
Mean motion: 15
49457984 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 332
Coasting Arc #11 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2020/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1900594
98 A = 6802938
23 meter
Y = 6525183
73 meter E =
0014299
Z = 70219
87 I = 51
28930
XDOT = -4620
164066 Wp = 129
01888
YDOT = -1272
626985 meter/sec RA = 286
71375 deg
ZDOT = -5977
823846 TA = 50
22250
MA = 50
09665
Ha = 229
189 n
mi
Hp = 221
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6235547
83 X = -1973761
36
Y = 21408083
10 feet Y = 6503520
81 meter
Z = 230380
15 Z = 60810
64
XDOT = -15158
018588 XDOT = -4576
553007
YDOT = -4175
285385 feet/sec YDOT = -1324
048375 meter/sec
ZDOT = -19612
282958 ZDOT = -6000
160985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22016555
62 X = 6710646
15
Y = 3532360
27 feet Y = 1076663
41 meter
Z = 186716
57 Z = 56911
21
XDOT = -2022
248006 XDOT = -616
381192
YDOT = 13820
631547 feet/sec YDOT = 4212
528496 meter/sec
ZDOT = -19714
914574 ZDOT = -6009
105962
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 20181
53240543
00016717 00000-0 10270-3 0 9106
2 25544 51
6426 287
3651 0002376 104
4909 255
6505 15
49458206 33922
Satellite: ISS
Catalog Number: 25544
Epoch time: 20181
53240543 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node: 287
3651 deg
Eccentricity:
0002376
Arg of perigee: 104
4909 deg
Mean anomaly: 255
6505 deg
Mean motion: 15
49458206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 302
Coasting Arc #12 (Orbit 3407)
---------------------------------------
Vector Time (GMT): 2020/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1440240
98 A = 6802934
92 meter
Y = -6642744
89 meter E =
0013605
Z = 73030
68 I = 51
28149
XDOT = 4667
810269 Wp = 54
71213
YDOT = 1086
365497 meter/sec RA = 281
73966 deg
ZDOT = 5976
446209 TA = 306
07686
MA = 306
20279
Ha = 229
188 n
mi
Hp = 221
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4725200
08 X = 1514060
35
Y = -21793782
45 feet Y = -6626226
35 meter
Z = 239601
98 Z = 80205
16
XDOT = 15314
338152 XDOT = 4626
285117
YDOT = 3564
191264 feet/sec YDOT = 1138
331246 meter/sec
ZDOT = 19607
763152 ZDOT = 5999
019918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22242264
20 X = -6779442
13
Y = -1600325
24 feet Y = -487779
13 meter
Z = 272984
68 Z = 83205
73
XDOT = 1270
406581 XDOT = 387
219926
YDOT = -13909
637484 feet/sec YDOT = -4239
657505 meter/sec
ZDOT = 19711
496511 ZDOT = 6008
064136
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 20182
56433869
00016717 00000-0 10270-3 0 9116
2 25544 51
6433 282
2576 0002341 105
0526 255
0884 15
49458882 34086
Satellite: ISS
Catalog Number: 25544
Epoch time: 20182
56433869 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 282
2576 deg
Eccentricity:
0002341
Arg of perigee: 105
0526 deg
Mean anomaly: 255
0884 deg
Mean motion: 15
49458882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3408
Checksum: 316
Coasting Arc #13 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2020/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1009110
27 A = 6802901
53 meter
Y = 6716517
83 meter E =
0013646
Z = -262998
34 I = 51
27559
XDOT = -4709
890568 Wp = 132
32943
YDOT = -933
236410 meter/sec RA = 276
76509 deg
ZDOT = -5969
978797 TA = 50
51340
MA = 50
39280
Ha = 229
146 n
mi
Hp = 221
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3310729
24 X = -1082863
88
Y = 22035819
65 feet Y = 6704820
90 meter
Z = -862855
45 Z = -268078
22
XDOT = -15452
396877 XDOT = -4670
106032
YDOT = -3061
799245 feet/sec YDOT = -985
682320 meter/sec
ZDOT = -19586
544610 ZDOT = -5992
761151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22281104
62 X = 6791280
69
Y = -221613
19 feet Y = -67547
70 meter
Z = -886600
18 Z = -270235
73
XDOT = -617
972986 XDOT = -188
358166
YDOT = 13985
372701 feet/sec YDOT = 4262
741599 meter/sec
ZDOT = -19691
251189 ZDOT = -6001
893362
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 20183
53177455
00016717 00000-0 10270-3 0 9121
2 25544 51
6432 277
4690 0002319 110
8244 249
3155 15
49460393 34238
Satellite: ISS
Catalog Number: 25544
Epoch time: 20183
53177455 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 277
4690 deg
Eccentricity:
0002319
Arg of perigee: 110
8244 deg
Mean anomaly: 249
3155 deg
Mean motion: 15
49460393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 303
Coasting Arc #14 (Orbit 3438)
---------------------------------------
Vector Time (GMT): 2020/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 538720
56 A = 6802864
77 meter
Y = -6763389
15 meter E =
0014128
Z = 408024
30 I = 51
27349
XDOT = 4757
191988 Wp = 57
38512
YDOT = 747
066805 meter/sec RA = 271
78996 deg
ZDOT = 5958
524020 TA = 307
02798
MA = 307
15715
Ha = 229
153 n
mi
Hp = 221
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1767455
89 X = 612328
80
Y = -22189596
95 feet Y = -6756953
30 meter
Z = 1338662
39 Z = 410818
69
XDOT = 15607
585262 XDOT = 4719
541446
YDOT = 2451
006579 feet/sec YDOT = 800
053477 meter/sec
ZDOT = 19548
963320 ZDOT = 5981
541264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22154576
91 X = -6752715
04
Y = 2154355
68 feet Y = 656647
61 meter
Z = 1351888
97 Z = 412055
76
XDOT = -138
265302 XDOT = -42
143264
YDOT = -14048
720603 feet/sec YDOT = -4282
050040 meter/sec
ZDOT = 19654
767970 ZDOT = 5990
773277
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 20184
56370444
00016717 00000-0 10270-3 0 9139
2 25544 51
6440 272
3612 0002279 107
7307 252
4092 15
49459725 34394
Satellite: ISS
Catalog Number: 25544
Epoch time: 20184
56370444 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 272
3612 deg
Eccentricity:
0002279
Arg of perigee: 107
7307 deg
Mean anomaly: 252
4092 deg
Mean motion: 15
49459725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 307
Coasting Arc #15 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2020/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -103838
42 A = 6802776
01 meter
Y = 6770190
57 meter E =
0012888
Z = -598219
81 I = 51
27202
XDOT = -4802
922920 Wp = 134
55524
YDOT = -590
632622 meter/sec RA = 266
81573 deg
ZDOT = -5938
875693 TA = 51
92221
MA = 51
80603
Ha = 229
139 n
mi
Hp = 221
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -340677
22 X = -176631
19
Y = 22211911
32 feet Y = 6768622
49 meter
Z = -1962663
43 Z = -598899
64
XDOT = -15757
621130 XDOT = -4767
113835
YDOT = -1937
771068 feet/sec YDOT = -644
140901 meter/sec
ZDOT = -19484
500306 ZDOT = -5962
119435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21861335
48 X = 6663335
05
Y = -3943775
75 feet Y = -1202062
85 meter
Z = -1966152
86 Z = -599283
39
XDOT = 809
758972 XDOT = 246
814535
YDOT = 14111
819381 feet/sec YDOT = 4301
282547 meter/sec
ZDOT = -19591
364867 ZDOT = -5971
448011
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 20185
53113843
00016717 00000-0 10270-3 0 9146
2 25544 51
6426 267
5734 0002319 113
1063 247
0332 15
49461732 34549
Satellite: ISS
Catalog Number: 25544
Epoch time: 20185
53113843 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 267
5734 deg
Eccentricity:
0002319
Arg of perigee: 113
1063 deg
Mean anomaly: 247
0332 deg
Mean motion: 15
49461732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 289
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