[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 25th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14255 723 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
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
093/12:44:28
870 1
5 1
5 1
5
N/A -0
0 0
0 230
9
000/00:06:57
740 -0
2 -0
0 221
9
096/03:42:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
1
000/00:00:00
000 0
0 0
0 221
8
097/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
8
000/00:00:00
000 0
0 0
0 221
9
Coasting Arc #1 (Orbit 1872)
---------------------------------------
Vector Time (GMT): 2020/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3471758
20 A = 6792639
51 meter
Y = 2351417
58 meter E =
0007339
Z = 5338883
99 I = 51
92752
XDOT = -4577
967936 Wp = 55
44574
YDOT = -6141
708288 meter/sec RA = 51
73128 deg
ZDOT = -267
629877 TA = 37
12172
MA = 37
07099
Ha = 230
960 n
mi
Hp = 221
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11390282
82 X = -3523727
41
Y = 7714624
60 feet Y = 2312303
94 meter
Z = 17516023
58 Z = 5321893
23
XDOT = -15019
579844 XDOT = -4507
649319
YDOT = -20149
961576 feet/sec YDOT = -6192
509237 meter/sec
ZDOT = -878
050777 ZDOT = -289
696141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11436004
44 X = -3485694
15
Y = 7823243
66 feet Y = 2384524
67 meter
Z = 17437881
71 Z = 5315066
35
XDOT = -14631
292861 XDOT = -4459
618064
YDOT = -19174
258585 feet/sec YDOT = -5844
314017 meter/sec
ZDOT = -978
944492 ZDOT = -298
382281
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
54791153
00016717 00000-0 10270-3 0 9005
2 25544 51
6404 52
2082 0005038 45
6844 314
4718 15
48900212 18737
Satellite: ISS
Catalog Number: 25544
Epoch time: 20083
54791153 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 52
2082 deg
Eccentricity:
0005038
Arg of perigee: 45
6844 deg
Mean anomaly: 314
4718 deg
Mean motion: 15
48900212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1873
Checksum: 286
Coasting Arc #2 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2020/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3237827
09 A = 6792651
41 meter
Y = -2680661
53 meter E =
0018735
Z = -5351681
12 I = 51
90606
XDOT = 5096
133751 Wp = 81
19098
YDOT = 5695
658153 meter/sec RA = 46
80589 deg
ZDOT = 233
744912 TA = 191
01459
MA = 191
05566
Ha = 230
844 n
mi
Hp = 221
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10622792
27 X = 3293557
65
Y = -8794821
29 feet Y = -2644142
85 meter
Z = -17558008
91 Z = -5335817
45
XDOT = 16719
598922 XDOT = 5030
929073
YDOT = 18686
542496 feet/sec YDOT = 5752
282190 meter/sec
ZDOT = 766
879631 ZDOT = 258
340770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10504106
55 X = 3201651
68
Y = -9078219
87 feet Y = -2767041
42 meter
Z = -17485020
55 Z = -5329434
26
XDOT = 16542
922406 XDOT = 5042
282749
YDOT = 17469
638361 feet/sec YDOT = 5324
745772 meter/sec
ZDOT = 879
395967 ZDOT = 268
039891
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
51569478
00016717 00000-0 10270-3 0 9017
2 25544 51
6407 47
4217 0004991 48
7501 311
4078 15
48899992 18881
Satellite: ISS
Catalog Number: 25544
Epoch time: 20084
51569478 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 47
4217 deg
Eccentricity:
0004991
Arg of perigee: 48
7501 deg
Mean anomaly: 311
4078 deg
Mean motion: 15
48899992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1888
Checksum: 342
Coasting Arc #3 (Orbit 1903)
---------------------------------------
Vector Time (GMT): 2020/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2974692
54 A = 6792593
07 meter
Y = 2957179
09 meter E =
0007307
Z = 5337452
69 I = 51
88355
XDOT = -5592
816614 Wp = 60
09773
YDOT = -5237
381184 meter/sec RA = 41
87931 deg
ZDOT = -211
512557 TA = 31
93435
MA = 31
89008
Ha = 230
973 n
mi
Hp = 221
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9759489
97 X = -3033465
77
Y = 9702031
15 feet Y = 2923585
93 meter
Z = 17511327
72 Z = 5322859
75
XDOT = -18349
135873 XDOT = -5532
807597
YDOT = -17183
009135 feet/sec YDOT = -5299
588530 meter/sec
ZDOT = -693
938834 ZDOT = -238
533907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9443907
69 X = -2878503
06
Y = 10126092
71 feet Y = 3086433
06 meter
Z = 17444153
90 Z = 5316978
11
XDOT = -18340
251327 XDOT = -5590
108605
YDOT = -15674
850450 feet/sec YDOT = -4777
694417 meter/sec
ZDOT = -817
599092 ZDOT = -249
204203
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
54799542
00016717 00000-0 10270-3 0 9029
2 25544 51
6420 42
3165 0004985 51
7187 308
4410 15
48912687 19041
Satellite: ISS
Catalog Number: 25544
Epoch time: 20085
54799542 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 42
3165 deg
Eccentricity:
0004985
Arg of perigee: 51
7187 deg
Mean anomaly: 308
4410 deg
Mean motion: 15
48912687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1904
Checksum: 314
Coasting Arc #4 (Orbit 1918)
---------------------------------------
Vector Time (GMT): 2020/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2687989
12 A = 6792610
57 meter
Y = -3235109
30 meter E =
0019042
Z = -5349933
34 I = 51
85833
XDOT = 6021
831761 Wp = 82
17710
YDOT = 4708
086261 meter/sec RA = 36
95022 deg
ZDOT = 181
664036 TA = 189
53593
MA = 189
57213
Ha = 230
892 n
mi
Hp = 221
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8818861
96 X = 2749952
28
Y = -10613875
65 feet Y = -3204704
36 meter
Z = -17552274
75 Z = -5336725
30
XDOT = 19756
665884 XDOT = 5967
854574
YDOT = 15446
477235 feet/sec YDOT = 4775
124880 meter/sec
ZDOT = 596
010617 ZDOT = 210
784239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8274165
80 X = 2521965
74
Y = -11139875
93 feet Y = -3395434
18 meter
Z = -17491437
22 Z = -5331390
07
XDOT = 19844
667048 XDOT = 6048
654516
YDOT = 13610
406043 feet/sec YDOT = 4148
451762 meter/sec
ZDOT = 729
319856 ZDOT = 222
296692
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
51577427
00016717 00000-0 10270-3 0 9034
2 25544 51
6425 37
5296 0005013 54
6365 305
5253 15
48911341 19195
Satellite: ISS
Catalog Number: 25544
Epoch time: 20086
51577427 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 37
5296 deg
Eccentricity:
0005013
Arg of perigee: 54
6365 deg
Mean anomaly: 305
5253 deg
Mean motion: 15
48911341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1919
Checksum: 303
Coasting Arc #5 (Orbit 1934)
---------------------------------------
Vector Time (GMT): 2020/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2379939
05 A = 6792531
43 meter
Y = 3457507
54 meter E =
0007402
Z = 5334718
46 I = 51
83075
XDOT = -6429
420175 Wp = 64
45118
YDOT = -4170
845989 meter/sec RA = 32
02087 deg
ZDOT = -161
837560 TA = 27
10695
MA = 27
06832
Ha = 231
004 n
mi
Hp = 221
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7808198
98 X = -2444338
19
Y = 11343528
69 feet Y = 3430533
74 meter
Z = 17502357
15 Z = 5323000
88
XDOT = -21093
898211 XDOT = -6381
516577
YDOT = -13683
877917 feet/sec YDOT = -4242
476506 meter/sec
ZDOT = -530
963122 ZDOT = -192
952628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7016434
79 X = -2138609
33
Y = 11929003
48 feet Y = 3635960
26 meter
Z = 17448342
02 Z = 5318254
65
XDOT = -21224
428948 XDOT = -6469
205943
YDOT = -11482
981838 feet/sec YDOT = -3500
012864 meter/sec
ZDOT = -673
445353 ZDOT = -205
266144
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
54807028
00016717 00000-0 10270-3 0 9042
2 25544 51
6425 32
4251 0005061 57
5339 302
6300 15
48931266 19353
Satellite: ISS
Catalog Number: 25544
Epoch time: 20087
54807028 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 32
4251 deg
Eccentricity:
0005061
Arg of perigee: 57
5339 deg
Mean anomaly: 302
6300 deg
Mean motion: 15
48931266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1935
Checksum: 289
Coasting Arc #6 (Orbit 1949)
---------------------------------------
Vector Time (GMT): 2020/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2050063
83 A = 6792594
64 meter
Y = -3677305
25 meter E =
0019322
Z = -5347039
88 I = 51
80169
XDOT = 6757
107019 Wp = 83
49642
YDOT = 3575
022105 meter/sec RA = 27
08843 deg
ZDOT = 134
593319 TA = 187
77212
MA = 187
80210
Ha = 230
945 n
mi
Hp = 221
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6725931
21 X = 2117005
22
Y = -12064649
78 feet Y = -3654006
04 meter
Z = -17542781
75 Z = -5336918
57
XDOT = 22168
986282 XDOT = 6715
974082
YDOT = 11729
075146 feet/sec YDOT = 3650
354901 meter/sec
ZDOT = 441
579131 ZDOT = 167
316780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5664465
54 X = 1726529
10
Y = -12662716
40 feet Y = -3859595
96 meter
Z = -17496072
70 Z = -5332802
96
XDOT = 22258
556029 XDOT = 6784
407877
YDOT = 9151
362425 feet/sec YDOT = 2789
335267 meter/sec
ZDOT = 591
467016 ZDOT = 180
279146
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
51584751
00016717 00000-0 10270-3 0 9056
2 25544 51
6425 27
6386 0005018 61
4729 298
6926 15
48915008 19508
Satellite: ISS
Catalog Number: 25544
Epoch time: 20088
51584751 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 27
6386 deg
Eccentricity:
0005018
Arg of perigee: 61
4729 deg
Mean anomaly: 298
6926 deg
Mean motion: 15
48915008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1950
Checksum: 328
Coasting Arc #7 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2020/089/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1195494
01 A = 6794824
34 meter
Y = -4669467
91 meter E =
0016080
Z = -4804610
33 I = 51
79054
XDOT = 7121
676008 Wp = 69
98729
YDOT = 890
184842 meter/sec RA = 23
94978 deg
ZDOT = -2639
010490 TA = 173
96915
MA = 173
94977
Ha = 230
895 n
mi
Hp = 221
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3922224
44 X = -1119851
58
Y = -15319776
60 feet Y = -4682414
09 meter
Z = -15763157
24 Z = -4810233
64
XDOT = 23365
078766 XDOT = 7124
011293
YDOT = 2920
553942 feet/sec YDOT = 969
837402 meter/sec
ZDOT = -8658
170898 ZDOT = -2604
410316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14890250
23 X = 4538548
27
Y = 5249446
32 feet Y = 1600031
24 meter
Z = -15788612
58 Z = -4812369
11
XDOT = -14950
073247 XDOT = -4556
782326
YDOT = 16860
839384 feet/sec YDOT = 5139
183844 meter/sec
ZDOT = -8499
483545 ZDOT = -2590
642585
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
16103020
00016717 00000-0 10270-3 0 9065
2 25544 51
6432 24
4470 0004743 67
4888 292
6764 15
48908191 19601
Satellite: ISS
Catalog Number: 25544
Epoch time: 20089
16103020 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 24
4470 deg
Eccentricity:
0004743
Arg of perigee: 67
4888 deg
Mean anomaly: 292
6764 deg
Mean motion: 15
48908191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 310
Coasting Arc #8 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2020/090/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1619425
15 A = 6794758
01 meter
Y = 4541384
15 meter E =
0011217
Z = 4778878
89 I = 51
76011
XDOT = -7182
939516 Wp = 99
15377
YDOT = -252
361499 meter/sec RA = 19
01393 deg
ZDOT = 2666
828583 TA = 324
51956
MA = 324
59412
Ha = 230
856 n
mi
Hp = 221
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5313074
66 X = 1545308
51
Y = 14899554
30 feet Y = 4559079
48 meter
Z = 15678736
50 Z = 4786565
28
XDOT = -23566
074527 XDOT = -7192
537685
YDOT = -827
957674 feet/sec YDOT = -332
739806 meter/sec
ZDOT = 8749
437607 ZDOT = 2631
913178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15369505
02 X = -4684625
13
Y = -3592701
72 feet Y = -1095055
48 meter
Z = 15713658
67 Z = 4789523
16
XDOT = 13101
488957 XDOT = 3993
333834
YDOT = -18378
985009 feet/sec YDOT = -5601
914631 meter/sec
ZDOT = 8589
266522 ZDOT = 2618
008436
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
19331988
00016717 00000-0 10270-3 0 9077
2 25544 51
6437 19
3412 0004822 69
7237 290
4431 15
48942654 19762
Satellite: ISS
Catalog Number: 25544
Epoch time: 20090
19331988 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 19
3412 deg
Eccentricity:
0004822
Arg of perigee: 69
7237 deg
Mean anomaly: 290
4431 deg
Mean motion: 15
48942654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 323
Coasting Arc #9 (Orbit 1990)
---------------------------------------
Vector Time (GMT): 2020/091/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2017227
03 A = 6794842
01 meter
Y = -4398448
64 meter E =
0016250
Z = -4785711
24 I = 51
72777
XDOT = 7155
242677 Wp = 71
57713
YDOT = -378
280757 meter/sec RA = 14
07622 deg
ZDOT = -2670
796290 TA = 172
01981
MA = 171
99393
Ha = 230
994 n
mi
Hp = 221
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6618198
93 X = -1944646
04
Y = -14430605
78 feet Y = -4420600
99 meter
Z = -15701152
37 Z = -4795333
78
XDOT = 23475
205632 XDOT = 7171
914169
YDOT = -1241
078599 feet/sec YDOT = -298
172592 meter/sec
ZDOT = -8762
455021 ZDOT = -2635
998325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15709399
35 X = 4788224
92
Y = 1969794
46 feet Y = 600393
35 meter
Z = -15744961
35 Z = -4799064
22
XDOT = -11069
665490 XDOT = -3374
034041
YDOT = 19582
696167 feet/sec YDOT = 5968
805792 meter/sec
ZDOT = -8602
783017 ZDOT = -2622
128263
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
16109137
00016717 00000-0 10270-3 0 9085
2 25544 51
6435 14
5551 0004988 73
2834 286
8863 15
48920496 19912
Satellite: ISS
Catalog Number: 25544
Epoch time: 20091
16109137 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 14
5551 deg
Eccentricity:
0004988
Arg of perigee: 73
2834 deg
Mean anomaly: 286
8863 deg
Mean motion: 15
48920496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1991
Checksum: 331
Coasting Arc #10 (Orbit 2006)
---------------------------------------
Vector Time (GMT): 2020/092/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2411777
20 A = 6794802
45 meter
Y = 4196273
56 meter E =
0011729
Z = 4760098
97 I = 51
69426
XDOT = -7104
124617 Wp = 101
27331
YDOT = 1015
024154 meter/sec RA = 9
13654 deg
ZDOT = 2696
738849 TA = 322
05232
MA = 322
13492
Ha = 230
916 n
mi
Hp = 221
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7912654
87 X = 2341552
16
Y = 13767301
72 feet Y = 4222851
20 meter
Z = 15617122
60 Z = 4771643
80
XDOT = -23307
495464 XDOT = -7128
046130
YDOT = 3330
131739 feet/sec YDOT = 935
447073 meter/sec
ZDOT = 8847
568401 ZDOT = 2662
171702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15825325
56 X = -4823559
23
Y = -246744
37 feet Y = -75207
68 meter
Z = 15669761
01 Z = 4776143
15
XDOT = 8951
423819 XDOT = 2728
393980
YDOT = -20678
564960 feet/sec YDOT = -6302
826600 meter/sec
ZDOT = 8688
913515 ZDOT = 2648
380840
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 20092
19337751
00016717 00000-0 10270-3 0 9095
2 25544 51
6427 9
4499 0004992 76
6286 283
5420 15
48945975 20071
Satellite: ISS
Catalog Number: 25544
Epoch time: 20092
19337751 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 9
4499 deg
Eccentricity:
0004992
Arg of perigee: 76
6286 deg
Mean anomaly: 283
5420 deg
Mean motion: 15
48945975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2007
Checksum: 340
Coasting Arc #11 (Orbit 2021)
---------------------------------------
Vector Time (GMT): 2020/093/03:22:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2774885
71 A = 6794862
93 meter
Y = -3984714
89 meter E =
0016169
Z = -4768564
23 I = 51
66196
XDOT = 6967
741705 Wp = 73
63928
YDOT = -1628
008861 meter/sec RA = 4
19360 deg
ZDOT = -2697
389495 TA = 169
65197
MA = 169
61865
Ha = 231
014 n
mi
Hp = 220
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9103955
75 X = -2706958
36
Y = -13073211
59 feet Y = -4015365
92 meter
Z = -15644895
76 Z = -4781878
42
XDOT = 22860
044964 XDOT = 6998
531044
YDOT = -5341
236420 feet/sec YDOT = -1549
918514 meter/sec
ZDOT = -8849
703066 ZDOT = -2663
468272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15808690
08 X = 4818488
74
Y = -1403944
68 feet Y = -427922
34 meter
Z = -15705664
32 Z = -4787086
49
XDOT = -6723
806767 XDOT = -2049
416303
YDOT = 21430
374860 feet/sec YDOT = 6531
978257 meter/sec
ZDOT = -8693
971381 ZDOT = -2649
922477
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 20093
16114519
00016717 00000-0 10270-3 0 9100
2 25544 51
6437 4
6630 0005021 80
2780 279
8937 15
48929579 20220
Satellite: ISS
Catalog Number: 25544
Epoch time: 20093
16114519 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 4
6630 deg
Eccentricity:
0005021
Arg of perigee: 80
2780 deg
Mean anomaly: 279
8937 deg
Mean motion: 15
48929579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2022
Checksum: 304
Coasting Arc #12 (Orbit 2027)
---------------------------------------
Vector Time (GMT): 2020/093/12:47:57
740
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 904849
59 A = 6793461
66 meter
Y = -4166176
92 meter E =
0018121
Z = -5304909
54 I = 51
64272
XDOT = 7574
466831 Wp = 91
07393
YDOT = 813
171777 meter/sec RA = 2
22630 deg
ZDOT = 654
955179 TA = 185
18799
MA = 185
20680
Ha = 230
940 n
mi
Hp = 221
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2968666
64 X = 977137
83
Y = -13668559
44 feet Y = -4155654
17 meter
Z = -17404558
85 Z = -5300338
50
XDOT = 24850
612962 XDOT = 7561
629376
YDOT = 2667
886409 feet/sec YDOT = 897
803087 meter/sec
ZDOT = 2148
803082 ZDOT = 691
717568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2359350
13 X = -719129
92
Y = -13813636
90 feet Y = -4210396
53 meter
Z = -17383269
83 Z = -5298420
64
XDOT = 22968
778956 XDOT = 7000
883826
YDOT = -6832
597599 feet/sec YDOT = -2082
575748 meter/sec
ZDOT = 2317
376362 ZDOT = 706
336315
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 20093
54825184
00016717 00000-0 10270-3 0 9110
2 25544 51
6450 2
7503 0003719 76
2049 283
9515 15
48671039 20287
Satellite: ISS
Catalog Number: 25544
Epoch time: 20093
54825184 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 2
7503 deg
Eccentricity:
0003719
Arg of perigee: 76
2049 deg
Mean anomaly: 283
9515 deg
Mean motion: 15
48671039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2028
Checksum: 301
Coasting Arc #13 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2020/094/12:47:57
740
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -411398
16 A = 6793313
82 meter
Y = 4223367
92 meter E =
0006510
Z = 5299758
55 I = 51
60938
XDOT = -7645
335379 Wp = 72
87188
YDOT = -64
999135 meter/sec RA = 357
28354 deg
ZDOT = -539
254488 TA = 22
29228
MA = 22
26399
Ha = 230
906 n
mi
Hp = 221
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1349731
50 X = -484337
52
Y = 13856193
96 feet Y = 4218359
73 meter
Z = 17387659
30 Z = 5297582
86
XDOT = -25083
121322 XDOT = -7641
420956
YDOT = -213
251754 feet/sec YDOT = -150
472844 meter/sec
ZDOT = -1769
207638 ZDOT = -576
382723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4156957
70 X = 1267040
71
Y = 13300140
72 feet Y = 4053882
89 meter
Z = 17377357
15 Z = 5296618
46
XDOT = -22122
948011 XDOT = -6743
074554
YDOT = 9458
990776 feet/sec YDOT = 2883
100388 meter/sec
ZDOT = -1939
507101 ZDOT = -591
161764
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 20094
58072076
00016717 00000-0 10270-3 0 9120
2 25544 51
6454 357
6458 0003665 79
2479 280
9084 15
48698797 20448
Satellite: ISS
Catalog Number: 25544
Epoch time: 20094
58072076 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 357
6458 deg
Eccentricity:
0003665
Arg of perigee: 79
2479 deg
Mean anomaly: 280
9084 deg
Mean motion: 15
48698797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 352
Coasting Arc #14 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2020/095/12:47:57
740
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -92891
80 A = 6793347
22 meter
Y = -4244982
14 meter E =
0018408
Z = -5318914
26 I = 51
57516
XDOT = 7603
385569 Wp = 90
73760
YDOT = -688
440070 meter/sec RA = 352
33889 deg
ZDOT = 417
674007 TA = 183
25481
MA = 183
26680
Ha = 230
956 n
mi
Hp = 221
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -304763
12 X = -19580
23
Y = -13927106
75 feet Y = -4245611
30 meter
Z = -17450506
10 Z = -5319187
19
XDOT = 24945
490711 XDOT = 7608
490008
YDOT = -2258
661647 feet/sec YDOT = -603
385040 meter/sec
ZDOT = 1370
321545 ZDOT = 454
620390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5920833
89 X = -1804670
17
Y = -12608265
98 feet Y = -3842999
47 meter
Z = -17451438
36 Z = -5319198
41
XDOT = 20858
461822 XDOT = 6357
659163
YDOT = -11921
791579 feet/sec YDOT = -3633
762073 meter/sec
ZDOT = 1539
831796 ZDOT = 469
340731
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 20095
54866092
00016717 00000-0 10270-3 0 9137
2 25544 51
6447 352
8608 0003758 81
8182 278
3394 15
48678823 20596
Satellite: ISS
Catalog Number: 25544
Epoch time: 20095
54866092 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 352
8608 deg
Eccentricity:
0003758
Arg of perigee: 81
8182 deg
Mean anomaly: 278
3394 deg
Mean motion: 15
48678823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 347
Coasting Arc #15 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2020/096/03:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4417239
82 A = 6799907
11 meter
Y = 3724048
57 meter E =
0016101
Z = 3572678
67 I = 51
57418
XDOT = -5719
834385 Wp = 87
00705
YDOT = -2502
823294 meter/sec RA = 349
24455 deg
ZDOT = -4444
936756 TA = 50
82237
MA = 50
67945
Ha = 231
111 n
mi
Hp = 221
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14492256
64 X = -4475908
83
Y = 12218007
12 feet Y = 3674324
06 meter
Z = 11721386
71 Z = 3551078
86
XDOT = -18765
860843 XDOT = -5669
831174
YDOT = -8211
362512 feet/sec YDOT = -2566
507278 meter/sec
ZDOT = -14583
125841 ZDOT = -4472
599630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6031076
52 X = -1838272
12
Y = -18034697
24 feet Y = -5496975
72 meter
Z = 11622044
50 Z = 3542399
16
XDOT = 13164
355144 XDOT = 4012
495448
YDOT = -13920
502244 feet/sec YDOT = -4242
969084 meter/sec
ZDOT = -14709
811332 ZDOT = -4483
550494
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 20096
19395267
00016717 00000-0 10270-3 0 9141
2 25544 51
6425 349
6696 0003994 86
8123 273
3484 15
48686428 20691
Satellite: ISS
Catalog Number: 25544
Epoch time: 20096
19395267 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 349
6696 deg
Eccentricity:
0003994
Arg of perigee: 86
8123 deg
Mean anomaly: 273
3484 deg
Mean motion: 15
48686428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2069
Checksum: 356
Coasting Arc #16 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2020/097/03:42:00
000
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3963189
20 A = 6799681
84 meter
Y = -4140291
74 meter E =
0009319
Z = -3667541
41 I = 51
54128
XDOT = 6001
414847 Wp = 94
54583
YDOT = 1900
441258 meter/sec RA = 344
29534 deg
ZDOT = 4348
640896 TA = 221
95661
MA = 222
02805
Ha = 231
056 n
mi
Hp = 221
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13002589
25 X = 4027007
36
Y = -13583634
32 feet Y = -4095616
04 meter
Z = -12032616
17 Z = -3648134
49
XDOT = 19689
681258 XDOT = 5958
594392
YDOT = 6235
043497 feet/sec YDOT = 1967
314319 meter/sec
ZDOT = 14267
194542 ZDOT = 4377
689120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8140574
08 X = 2481246
98
Y = 17013365
64 feet Y = 5185673
85 meter
Z = -11943313
77 Z = -3640322
04
XDOT = -11462
884792 XDOT = -3493
887284
YDOT = 15573
167825 feet/sec YDOT = 4746
701553 meter/sec
ZDOT = 14400
268425 ZDOT = 4389
201816
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 20097
16188957
00016717 00000-0 10270-3 0 9156
2 25544 51
6433 344
8848 0003898 90
0717 270
0880 15
48665184 20842
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
16188957 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 344
8848 deg
Eccentricity:
0003898
Arg of perigee: 90
0717 deg
Mean anomaly: 270
0880 deg
Mean motion: 15
48665184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2084
Checksum: 342
Coasting Arc #17 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2020/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915574
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1717347
35 A = 6793266
85 meter
Y = 3878800
91 meter E =
0006172
Z = 5300763
34 I = 51
51098
XDOT = -7195
636056 Wp = 96
39066
YDOT = 2605
907538 meter/sec RA = 342
61273 deg
ZDOT = 423
296077 TA = 349
55695
MA = 349
56976
Ha = 230
839 n
mi
Hp = 221
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5634341
72 X = 1648097
80
Y = 12725724
76 feet Y = 3897618
81 meter
Z = 17390955
83 Z = 5308936
95
XDOT = -23607
729842 XDOT = -7226
297417
YDOT = 8549
565412 feet/sec YDOT = 2525
269416 meter/sec
ZDOT = 1388
766656 ZDOT = 388
267864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8495627
08 X = 2589467
13
Y = 10964439
95 feet Y = 3341961
30 meter
Z = 17428155
36 Z = 5312101
75
XDOT = -19964
597445 XDOT = -6085
209301
YDOT = 13511
710348 feet/sec YDOT = 4118
369314 meter/sec
ZDOT = 1227
945032 ZDOT = 374
277646
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 20097
54906358
00016717 00000-0 10270-3 0 9162
2 25544 51
6451 342
9715 0003625 90
0205 270
1360 15
48691030 20904
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
54906358 = yrday
fracday
Element set: 916
Inclination: 51
6451 deg
RA of node: 342
9715 deg
Eccentricity:
0003625
Arg of perigee: 90
0205 deg
Mean anomaly: 270
1360 deg
Mean motion: 15
48691030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 290
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