[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 20th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13861 7638 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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
079/17:18:26
637 1
0 1
9 1
9
N/A 1
5 0
0 230
6
000/00:08:53
274 -0
6 -0
0 221
9
081/01:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
7
000/00:00:00
000 0
0 0
0 221
7
085/12:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 221
4
089/03:22:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2020/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4182721
87 A = 6791667
75 meter
Y = -215070
14 meter E =
0018647
Z = -5361948
74 I = 52
00956
XDOT = 461
619916 Wp = 74
15035
YDOT = 7633
052823 meter/sec RA = 86
19365 deg
ZDOT = 59
044997 TA = 196
38080
MA = 196
44114
Ha = 230
453 n
mi
Hp = 221
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13722840
77 X = 4210861
01
Y = -705610
70 feet Y = -168138
83 meter
Z = -17591695
34 Z = -5341562
56
XDOT = 1514
501036 XDOT = 375
943756
YDOT = 25042
824224 feet/sec YDOT = 7637
735942 meter/sec
ZDOT = 193
717181 ZDOT = 61
078976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13834993
35 X = 4216905
97
Y = 831481
17 feet Y = 253435
46 meter
Z = -17498102
42 Z = -5333421
62
XDOT = -1210
265684 XDOT = -368
888980
YDOT = 24047
433666 feet/sec YDOT = 7329
657781 meter/sec
ZDOT = 202
651256 ZDOT = 61
768103
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 20076
51604214
00016717 00000-0 10270-3 0 9005
2 25544 51
6412 86
9962 0006063 30
9353 329
2153 15
49228202 17647
Satellite: ISS
Catalog Number: 25544
Epoch time: 20076
51604214 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 86
9962 deg
Eccentricity:
0006063
Arg of perigee: 30
9353 deg
Mean anomaly: 329
2153 deg
Mean motion: 15
49228202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1764
Checksum: 286
Coasting Arc #2 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2020/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4156973
49 A = 6791592
59 meter
Y = 448002
64 meter E =
0007995
Z = 5347125
44 I = 52
00547
XDOT = -1036
349837 Wp = 47
33983
YDOT = -7593
198429 meter/sec RA = 81
26985 deg
ZDOT = -164
068946 TA = 44
24846
MA = 44
18456
Ha = 230
639 n
mi
Hp = 220
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13638364
47 X = -4187647
17
Y = 1469824
95 feet Y = 401345
11 meter
Z = 17543062
46 Z = 5326858
24
XDOT = -3400
097892 XDOT = -950
566487
YDOT = -24912
068337 feet/sec YDOT = -7604
307991 meter/sec
ZDOT = -538
283943 ZDOT = -168
894425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13834420
90 X = -4216731
49
Y = 175416
54 feet Y = 53466
96 meter
Z = 17449998
24 Z = 5318759
46
XDOT = -1034
679557 XDOT = -315
370329
YDOT = -24111
901569 feet/sec YDOT = -7349
307598 meter/sec
ZDOT = -560
018412 ZDOT = -170
693612
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 20077
54812008
00016717 00000-0 10270-3 0 9012
2 25544 51
6404 81
8884 0006130 34
4716 325
6831 15
49251001 17806
Satellite: ISS
Catalog Number: 25544
Epoch time: 20077
54812008 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 81
8884 deg
Eccentricity:
0006130
Arg of perigee: 34
4716 deg
Mean anomaly: 325
6831 deg
Mean motion: 15
49251001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1780
Checksum: 282
Coasting Arc #3 (Orbit 1794)
---------------------------------------
Vector Time (GMT): 2020/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4134729
11 A = 6791679
21 meter
Y = -709646
48 meter E =
0019145
Z = -5357001
02 I = 51
99965
XDOT = 1608
399872 Wp = 76
68309
YDOT = 7471
332940 meter/sec RA = 76
34701 deg
ZDOT = 256
738037 TA = 195
72905
MA = 195
78861
Ha = 230
622 n
mi
Hp = 220
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13565384
20 X = 4168378
11
Y = -2328236
49 feet Y = -663221
11 meter
Z = -17575462
67 Z = -5336834
69
XDOT = 5276
902466 XDOT = 1523
486618
YDOT = 24512
247180 feet/sec YDOT = 7488
844443 meter/sec
ZDOT = 842
316394 ZDOT = 264
344303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13822527
03 X = 4213106
24
Y = -1274822
83 feet Y = -388566
00 meter
Z = -17482842
88 Z = -5328770
51
XDOT = 3286
265363 XDOT = 1001
653683
YDOT = 23835
907593 feet/sec YDOT = 7265
184634 meter/sec
ZDOT = 876
810021 ZDOT = 267
251695
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 20078
51569135
00016717 00000-0 10270-3 0 9021
2 25544 51
6408 77
1009 0006237 38
2141 321
9450 15
49231924 17953
Satellite: ISS
Catalog Number: 25544
Epoch time: 20078
51569135 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 77
1009 deg
Eccentricity:
0006237
Arg of perigee: 38
2141 deg
Mean anomaly: 321
9450 deg
Mean motion: 15
49231924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1795
Checksum: 298
Coasting Arc #4 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2020/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4086451
68 A = 6791631
15 meter
Y = 936784
90 meter E =
0008571
Z = 5337816
02 I = 51
98926
XDOT = -2167
483713 Wp = 49
94193
YDOT = -7343
836800 meter/sec RA = 71
42263 deg
ZDOT = -364
758133 TA = 43
55424
MA = 43
48659
Ha = 230
775 n
mi
Hp = 220
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13406993
70 X = -4122550
97
Y = 3073441
27 feet Y = 890885
77 meter
Z = 17512519
76 Z = 5317878
26
XDOT = -7111
167036 XDOT = -2083
429917
YDOT = -24093
952756 feet/sec YDOT = -7367
605192 meter/sec
ZDOT = -1196
713035 ZDOT = -375
082136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13684278
54 X = -4170968
10
Y = 2265714
44 feet Y = 690589
76 meter
Z = 17420933
63 Z = 5309900
57
XDOT = -5494
278704 XDOT = -1674
656149
YDOT = -23475
433170 feet/sec YDOT = -7155
312030 meter/sec
ZDOT = -1243
679029 ZDOT = -379
073368
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 20079
54776502
00016717 00000-0 10270-3 0 9034
2 25544 51
6395 71
9934 0006245 40
8160 319
3456 15
49250983 18118
Satellite: ISS
Catalog Number: 25544
Epoch time: 20079
54776502 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 71
9934 deg
Eccentricity:
0006245
Arg of perigee: 40
8160 deg
Mean anomaly: 319
3456 deg
Mean motion: 15
49250983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 316
Coasting Arc #5 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2020/079/17:22:53
274
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3721277
88 A = 6792705
05 meter
Y = -1987029
38 meter E =
0018172
Z = -5339373
82 I = 51
99053
XDOT = 2964
910517 Wp = 72
95046
YDOT = 7027
404502 meter/sec RA = 70
32726 deg
ZDOT = -545
189960 TA = 191
83640
MA = 191
87917
Ha = 230
649 n
mi
Hp = 221
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12208916
91 X = 3769156
01
Y = -6519125
26 feet Y = -1945148
05 meter
Z = -17517630
63 Z = -5321181
22
XDOT = 9727
396708 XDOT = 2888
755823
YDOT = 23055
789048 feet/sec YDOT = 7060
134396 meter/sec
ZDOT = -1788
680972 ZDOT = -530
973264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3706342
71 X = -1129693
26
Y = -13444065
71 feet Y = -4097751
23 meter
Z = -17433994
10 Z = -5313881
40
XDOT = 23633
767712 XDOT = 7203
572399
YDOT = -4264
520150 feet/sec YDOT = -1299
825742 meter/sec
ZDOT = -1723
828024 ZDOT = -525
422782
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 20079
74128176
00016717 00000-0 10270-3 0 9045
2 25544 51
6430 71
0368 0005042 32
9998 327
1466 15
48904919 18140
Satellite: ISS
Catalog Number: 25544
Epoch time: 20079
74128176 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 71
0368 deg
Eccentricity:
0005042
Arg of perigee: 32
9998 deg
Mean anomaly: 327
1466 deg
Mean motion: 15
48904919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 319
Coasting Arc #6 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2020/080/17:22:53
274
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514612
94 A = 6792638
70 meter
Y = 2322829
92 meter E =
0006136
Z = 5323501
01 I = 51
97786
XDOT = -3586
842932 Wp = 61
83848
YDOT = -6748
855916 meter/sec RA = 65
40651 deg
ZDOT = 579
013533 TA = 22
67228
MA = 22
64519
Ha = 230
734 n
mi
Hp = 221
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11530882
36 X = -3566184
37
Y = 7620833
07 feet Y = 2283239
10 meter
Z = 17465554
51 Z = 5306303
26
XDOT = -11767
857388 XDOT = -3513
921121
YDOT = -22141
915734 feet/sec YDOT = -6788
558764 meter/sec
ZDOT = 1899
650699 ZDOT = 561
768029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5151693
25 X = 1570236
10
Y = 12932706
61 feet Y = 3941888
97 meter
Z = 17386462
99 Z = 5299393
92
XDOT = -23099
907021 XDOT = -7040
851660
YDOT = 6764
031575 feet/sec YDOT = 2061
676824 meter/sec
ZDOT = 1820
887179 ZDOT = 555
006412
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 20080
77359581
00016717 00000-0 10270-3 0 9057
2 25544 51
6427 65
9315 0004866 35
4273 324
7199 15
48924579 18305
Satellite: ISS
Catalog Number: 25544
Epoch time: 20080
77359581 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 65
9315 deg
Eccentricity:
0004866
Arg of perigee: 35
4273 deg
Mean anomaly: 324
7199 deg
Mean motion: 15
48924579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 336
Coasting Arc #7 (Orbit 1834)
---------------------------------------
Vector Time (GMT): 2020/081/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2854292
66 A = 6793361
70 meter
Y = 3353256
19 meter E =
0006858
Z = 5166799
80 I = 51
97332
XDOT = -4358
861676 Wp = 83
24573
YDOT = -6110
030035 meter/sec RA = 63
82941 deg
ZDOT = 1556
466227 TA = 351
81048
MA = 351
82166
Ha = 230
702 n
mi
Hp = 221
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9364477
22 X = -2916674
55
Y = 11001496
68 feet Y = 3320989
11 meter
Z = 16951442
93 Z = 5152783
20
XDOT = -14300
727283 XDOT = -4297
773853
YDOT = -20046
030298 feet/sec YDOT = -6158
432225 meter/sec
ZDOT = 5106
516492 ZDOT = 1535
441854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6452543
43 X = 1966735
24
Y = -13010585
32 feet Y = -3965626
41 meter
Z = 16886892
35 Z = 5147124
79
XDOT = 17912
375308 XDOT = 5459
691994
YDOT = 15390
901349 feet/sec YDOT = 4691
146731 meter/sec
ZDOT = 5010
369916 ZDOT = 1527
160750
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 20081
09619434
00016717 00000-0 10270-3 0 9060
2 25544 51
6404 64
3305 0004564 39
8863 320
2621 15
48906907 18351
Satellite: ISS
Catalog Number: 25544
Epoch time: 20081
09619434 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 64
3305 deg
Eccentricity:
0004564
Arg of perigee: 39
8863 deg
Mean anomaly: 320
2621 deg
Mean motion: 15
48906907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1835
Checksum: 305
Coasting Arc #8 (Orbit 1849)
---------------------------------------
Vector Time (GMT): 2020/082/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2538375
95 A = 6793399
27 meter
Y = -3624515
38 meter E =
0017650
Z = -5170315
70 I = 51
95888
XDOT = 4871
890799 Wp = 69
41614
YDOT = 5676
199709 meter/sec RA = 58
90761 deg
ZDOT = -1585
642131 TA = 185
30839
MA = 185
32713
Ha = 230
667 n
mi
Hp = 221
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8328005
08 X = 2603831
75
Y = -11891454
66 feet Y = -3595764
00 meter
Z = -16962978
02 Z = -5157826
10
XDOT = 15983
893698 XDOT = 4815
757799
YDOT = 18622
702457 feet/sec YDOT = 5730
366635 meter/sec
ZDOT = -5202
237961 ZDOT = -1562
113666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4992767
08 X = -1521795
40
Y = 13703433
71 feet Y = 4176806
60 meter
Z = -16905418
28 Z = -5152771
49
XDOT = -19378
709144 XDOT = -5906
630547
YDOT = -13352
203426 feet/sec YDOT = -4069
751604 meter/sec
ZDOT = -5094
581296 ZDOT = -1552
828379
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 20082
06398687
00016717 00000-0 10270-3 0 9073
2 25544 51
6417 59
5446 0004686 44
2158 315
9365 15
48909741 18501
Satellite: ISS
Catalog Number: 25544
Epoch time: 20082
06398687 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 59
5446 deg
Eccentricity:
0004686
Arg of perigee: 44
2158 deg
Mean anomaly: 315
9365 deg
Mean motion: 15
48909741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1850
Checksum: 338
Coasting Arc #9 (Orbit 1865)
---------------------------------------
Vector Time (GMT): 2020/083/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2187910
62 A = 6793352
34 meter
Y = 3845648
18 meter E =
0007390
Z = 5148505
13 I = 51
94096
XDOT = -5368
329597 Wp = 86
93257
YDOT = -5226
270866 meter/sec RA = 53
98329 deg
ZDOT = 1620
789635 TA = 347
48102
MA = 347
49937
Ha = 230
749 n
mi
Hp = 221
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7178184
44 X = -2255759
38
Y = 12616955
97 feet Y = 3820802
61 meter
Z = 16891421
03 Z = 5137712
03
XDOT = -17612
629913 XDOT = -5317
361688
YDOT = -17146
557959 feet/sec YDOT = -5286
018186 meter/sec
ZDOT = 5317
551295 ZDOT = 1594
837074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3448386
99 X = 1051068
36
Y = -14159874
63 feet Y = -4315929
79 meter
Z = 16841632
70 Z = 5133329
65
XDOT = 20726
733074 XDOT = 6317
508241
YDOT = 11237
313050 feet/sec YDOT = 3425
133018 meter/sec
ZDOT = 5198
752746 ZDOT = 1584
579837
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 20083
09629534
00016717 00000-0 10270-3 0 9086
2 25544 51
6421 54
4381 0004626 47
0147 313
1390 15
48930171 18667
Satellite: ISS
Catalog Number: 25544
Epoch time: 20083
09629534 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 54
4381 deg
Eccentricity:
0004626
Arg of perigee: 47
0147 deg
Mean anomaly: 313
1390 deg
Mean motion: 15
48930171 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1866
Checksum: 297
Coasting Arc #10 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2020/084/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1829172
62 A = 6793467
74 meter
Y = -4052321
62 meter E =
0017813
Z = -5152504
11 I = 51
92036
XDOT = 5793
834111 Wp = 70
75861
YDOT = 4710
213790 meter/sec RA = 49
05955 deg
ZDOT = -1646
566062 TA = 183
35860
MA = 183
37057
Ha = 230
756 n
mi
Hp = 221
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6001222
51 X = 1899378
66
Y = -13295018
43 feet Y = -4031474
55 meter
Z = -16904541
04 Z = -5143447
79
XDOT = 19008
642096 XDOT = 5748
730517
YDOT = 15453
457316 feet/sec YDOT = 4774
752186 meter/sec
ZDOT = -5402
119626 ZDOT = -1618
532192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1878932
89 X = -572698
74
Y = 14513936
83 feet Y = 4423847
95 meter
Z = -16862708
66 Z = -5139753
60
XDOT = -21724
312919 XDOT = -6621
570578
YDOT = -8943
596859 feet/sec YDOT = -2726
008323 meter/sec
ZDOT = -5273
750474 ZDOT = -1607
439145
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 20084
06408546
00016717 00000-0 10270-3 0 9093
2 25544 51
6420 49
6527 0004698 51
4204 308
7366 15
48905772 18815
Satellite: ISS
Catalog Number: 25544
Epoch time: 20084
06408546 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 49
6527 deg
Eccentricity:
0004698
Arg of perigee: 51
4204 deg
Mean anomaly: 308
7366 deg
Mean motion: 15
48905772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1881
Checksum: 322
Coasting Arc #11 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2020/085/01:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1442543
00 A = 6793382
72 meter
Y = 4205160
50 meter E =
0007829
Z = 5129994
46 I = 51
89856
XDOT = -6201
673502 Wp = 91
28931
YDOT = -4180
582718 meter/sec RA = 44
13278 deg
ZDOT = 1680
628213 TA = 342
52018
MA = 342
54711
Ha = 230
762 n
mi
Hp = 221
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4732752
62 X = -1514377
63
Y = 13796458
33 feet Y = 4188627
88 meter
Z = 16830690
47 Z = 5122812
23
XDOT = -20346
697842 XDOT = -6162
627576
YDOT = -13715
822566 feet/sec YDOT = -4249
715735 meter/sec
ZDOT = 5513
872089 ZDOT = 1650
598318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 266768
15 X = 81310
93
Y = -14621491
05 feet Y = -4456630
47 meter
Z = 16797445
81 Z = 5119861
48
XDOT = 22594
377277 XDOT = 6886
766194
YDOT = 6597
657454 feet/sec YDOT = 2010
965992 meter/sec
ZDOT = 5376
324333 ZDOT = 1638
703657
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 20085
09639090
00016717 00000-0 10270-3 0 9109
2 25544 51
6430 44
5466 0004560 54
6332 305
5243 15
48939559 18973
Satellite: ISS
Catalog Number: 25544
Epoch time: 20085
09639090 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 44
5466 deg
Eccentricity:
0004560
Arg of perigee: 54
6332 deg
Mean anomaly: 305
5243 deg
Mean motion: 15
48939559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 316
Coasting Arc #12 (Orbit 1903)
---------------------------------------
Vector Time (GMT): 2020/085/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 574514
97 A = 6794379
68 meter
Y = -4664039
86 meter E =
0016799
Z = -4922954
92 I = 51
88913
XDOT = 6480
337030 Wp = 66
55538
YDOT = 3297
054636 meter/sec RA = 41
76289 deg
ZDOT = -2367
302966 TA = 180
27338
MA = 180
27430
Ha = 230
863 n
mi
Hp = 221
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1884891
65 X = 650539
82
Y = -15301968
06 feet Y = -4657190
68 meter
Z = -16151426
90 Z = -4919979
00
XDOT = 21260
948262 XDOT = 6454
485751
YDOT = 10817
108387 feet/sec YDOT = 3369
377573 meter/sec
ZDOT = -7766
742013 ZDOT = -2335
887216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1374695
73 X = -419007
26
Y = -15370895
66 feet Y = -4685049
00 meter
Z = -16137453
70 Z = -4918695
89
XDOT = 22032
064915 XDOT = 6715
373386
YDOT = 6032
792286 feet/sec YDOT = 1838
795089 meter/sec
ZDOT = -7622
783076 ZDOT = -2323
424282
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 20085
54802571
00016717 00000-0 10270-3 0 9116
2 25544 51
6423 42
3165 0005019 51
9271 308
2331 15
48912442 19048
Satellite: ISS
Catalog Number: 25544
Epoch time: 20085
54802571 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 42
3165 deg
Eccentricity:
0005019
Arg of perigee: 51
9271 deg
Mean anomaly: 308
2331 deg
Mean motion: 15
48912442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1904
Checksum: 278
Coasting Arc #13 (Orbit 1919)
---------------------------------------
Vector Time (GMT): 2020/086/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -139672
55 A = 6794305
91 meter
Y = 4699080
78 meter E =
0009828
Z = 4897020
53 I = 51
86406
XDOT = -6758
420438 Wp = 93
39148
YDOT = -2707
524116 meter/sec RA = 36
83498 deg
ZDOT = 2400
604125 TA = 333
12214
MA = 333
17302
Ha = 230
828 n
mi
Hp = 221
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -458243
29 X = -215995
67
Y = 15416931
70 feet Y = 4697092
60 meter
Z = 16066340
33 Z = 4896156
22
XDOT = -22173
295399 XDOT = -6739
302597
YDOT = -8882
953135 feet/sec YDOT = -2782
994449 meter/sec
ZDOT = 7875
997786 ZDOT = 2367
820986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3053403
06 X = 930677
25
Y = 15123042
44 feet Y = 4609503
34 meter
Z = 16062047
77 Z = 4895712
16
XDOT = -22584
272192 XDOT = -6883
686164
YDOT = -3662
026704 feet/sec YDOT = -1116
185739 meter/sec
ZDOT = 7725
740575 ZDOT = 2354
805727
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 20086
58032669
00016717 00000-0 10270-3 0 9125
2 25544 51
6429 37
2117 0004907 54
7378 305
4230 15
48948256 19205
Satellite: ISS
Catalog Number: 25544
Epoch time: 20086
58032669 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 37
2117 deg
Eccentricity:
0004907
Arg of perigee: 54
7378 deg
Mean anomaly: 305
4230 deg
Mean motion: 15
48948256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1920
Checksum: 314
Coasting Arc #14 (Orbit 1934)
---------------------------------------
Vector Time (GMT): 2020/087/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -285326
77 A = 6794417
78 meter
Y = -4714264
04 meter E =
0016970
Z = -4900525
87 I = 51
83643
XDOT = 6947
568334 Wp = 68
04884
YDOT = 2089
455457 meter/sec RA = 31
90438 deg
ZDOT = -2415
096852 TA = 178
26869
MA = 178
26280
Ha = 230
960 n
mi
Hp = 221
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -936111
45 X = -208785
19
Y = -15466745
55 feet Y = -4717027
21 meter
Z = -16077840
77 Z = -4901725
58
XDOT = 22793
859363 XDOT = 6935
418291
YDOT = 6855
168822 feet/sec YDOT = 2167
079970 meter/sec
ZDOT = -7923
546101 ZDOT = -2381
377792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4675353
79 X = -1425047
84
Y = -14767238
74 feet Y = -4501054
37 meter
Z = -16083010
08 Z = -4902101
47
XDOT = 22758
969183 XDOT = 6936
933807
YDOT = 1253
678770 feet/sec YDOT = 382
121289 meter/sec
ZDOT = -7768
966990 ZDOT = -2367
981139
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 20087
54811012
00016717 00000-0 10270-3 0 9130
2 25544 51
6428 32
4252 0005172 58
2932 301
8721 15
48922869 19354
Satellite: ISS
Catalog Number: 25544
Epoch time: 20087
54811012 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 32
4252 deg
Eccentricity:
0005172
Arg of perigee: 58
2932 deg
Mean anomaly: 301
8721 deg
Mean motion: 15
48922869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1935
Checksum: 298
Coasting Arc #15 (Orbit 1950)
---------------------------------------
Vector Time (GMT): 2020/088/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 720531
89 A = 6794379
11 meter
Y = 4669400
87 meter E =
0010336
Z = 4874287
04 I = 51
80757
XDOT = -7116
631301 Wp = 96
23633
YDOT = -1461
929565 meter/sec RA = 26
97322 deg
ZDOT = 2446
930142 TA = 329
77275
MA = 329
83234
Ha = 230
865 n
mi
Hp = 221
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2363949
77 X = 644587
06
Y = 15319556
67 feet Y = 4677034
06 meter
Z = 15991755
36 Z = 4877602
36
XDOT = -23348
527892 XDOT = -7111
640519
YDOT = -4796
356839 feet/sec YDOT = -1541
484732 meter/sec
ZDOT = 8027
986031 ZDOT = 2412
372318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6265842
10 X = 1909828
67
Y = 14161230
39 feet Y = 4316343
02 meter
Z = 16006626
48 Z = 4878819
75
XDOT = -22800
554606 XDOT = -6949
609044
YDOT = 1172
840881 feet/sec YDOT = 357
481900 meter/sec
ZDOT = 7869
527428 ZDOT = 2398
631960
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 20088
58040815
00016717 00000-0 10270-3 0 9141
2 25544 51
6428 27
3208 0004915 62
1442 298
0205 15
48947090 19517
Satellite: ISS
Catalog Number: 25544
Epoch time: 20088
58040815 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 27
3208 deg
Eccentricity:
0004915
Arg of perigee: 62
1442 deg
Mean anomaly: 298
0205 deg
Mean motion: 15
48947090 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1951
Checksum: 302
Coasting Arc #16 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2020/089/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1223315
92 A = 6794880
56 meter
Y = -4672956
73 meter E =
0016042
Z = -4794241
97 I = 51
79051
XDOT = 7115
667533 Wp = 69
90006
YDOT = 867
173575 meter/sec RA = 23
95079 deg
ZDOT = -2662
777333 TA = 173
80408
MA = 173
78421
Ha = 230
912 n
mi
Hp = 221
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4013503
66 X = -1147682
77
Y = -15331222
87 feet Y = -4686214
08 meter
Z = -15729140
32 Z = -4800000
45
XDOT = 23345
365921 XDOT = 7118
376029
YDOT = 2845
057661 feet/sec YDOT = 946
761030 meter/sec
ZDOT = -8736
146105 ZDOT = -2628
205438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14950181
74 X = 4556815
40
Y = 5179354
09 feet Y = 1578667
13 meter
Z = -15755215
59 Z = -4802189
71
XDOT = -14881
594571 XDOT = -4535
910025
YDOT = 16882
019624 feet/sec YDOT = 5145
639581 meter/sec
ZDOT = -8577
586797 ZDOT = -2614
448456
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 20089
16107565
00016717 00000-0 10270-3 0 9153
2 25544 51
6431 24
4474 0004768 67
5070 292
6584 15
48903006 19605
Satellite: ISS
Catalog Number: 25544
Epoch time: 20089
16107565 = yrday
fracday
Element set: 915
Inclination: 51
6431 deg
RA of node: 24
4474 deg
Eccentricity:
0004768
Arg of perigee: 67
5070 deg
Mean anomaly: 292
6584 deg
Mean motion: 15
48903006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 312
Coasting Arc #17 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2020/090/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1649451
78 A = 6794815
73 meter
Y = 4542421
22 meter E =
0011311
Z = 4767637
34 I = 51
76009
XDOT = -7174
240775 Wp = 99
05169
YDOT = -228
238595 meter/sec RA = 19
01496 deg
ZDOT = 2692
327865 TA = 324
35026
MA = 324
42575
Ha = 230
871 n
mi
Hp = 221
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5411587
20 X = 1575375
91
Y = 14902956
76 feet Y = 4560452
55 meter
Z = 15641854
80 Z = 4775469
70
XDOT = -23537
535351 XDOT = -7184
233202
YDOT = -748
814288 feet/sec YDOT = -308
521830 meter/sec
ZDOT = 8833
096669 ZDOT = 2657
453757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15425319
54 X = -4701637
40
Y = -3511154
32 feet Y = -1070199
84 meter
Z = 15677446
54 Z = 4778485
70
XDOT = 13025
627127 XDOT = 3970
211148
YDOT = -18393
733046 feet/sec YDOT = -5606
409832 meter/sec
ZDOT = 8673
113229 ZDOT = 2643
564912
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 20090
19336858
00016717 00000-0 10270-3 0 9168
2 25544 51
6436 19
3417 0004845 69
7582 290
4089 15
48938201 19766
Satellite: ISS
Catalog Number: 25544
Epoch time: 20090
19336858 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 19
3417 deg
Eccentricity:
0004845
Arg of perigee: 69
7582 deg
Mean anomaly: 290
4089 deg
Mean motion: 15
48938201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 338
Coasting Arc #18 (Orbit 1990)
---------------------------------------
Vector Time (GMT): 2020/091/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939545
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2048771
68 A = 6794899
26 meter
Y = -4396775
65 meter E =
0016199
Z = -4773858
74 I = 51
72777
XDOT = 7143
891486 Wp = 71
50393
YDOT = -402
727267 meter/sec RA = 14
07727 deg
ZDOT = -2697
510191 TA = 171
80832
MA = 171
78184
Ha = 231
008 n
mi
Hp = 221
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6721691
86 X = -1976264
62
Y = -14425116
95 feet Y = -4419281
17 meter
Z = -15662266
21 Z = -4783634
69
XDOT = 23437
964194 XDOT = 7160
966952
YDOT = -1321
283685 feet/sec YDOT = -322
743781 meter/sec
ZDOT = -8850
099051 ZDOT = -2662
766384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15758820
44 X = 4803288
47
Y = 1878401
24 feet Y = 572536
70 meter
Z = -15706779
13 Z = -4787426
28
XDOT = -10988
780087 XDOT = -3349
380171
YDOT = 19589
652173 feet/sec YDOT = 5970
925982 meter/sec
ZDOT = -8690
673635 ZDOT = -2648
917324
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 20091
16114263
00016717 00000-0 10270-3 0 9171
2 25544 51
6434 14
5556 0005011 73
3228 286
8472 15
48916906 19919
Satellite: ISS
Catalog Number: 25544
Epoch time: 20091
16114263 = yrday
fracday
Element set: 917
Inclination: 51
6434 deg
RA of node: 14
5556 deg
Eccentricity:
0005011
Arg of perigee: 73
3228 deg
Mean anomaly: 286
8472 deg
Mean motion: 15
48916906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1991
Checksum: 304
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