[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 20th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14537 7374 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
116/01:51:40
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 222
4
116/05:12:17
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 222
4
117/03:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
5
Coasting Arc #1 (Orbit 2306)
---------------------------------------
Vector Time (GMT): 2020/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4194568
67 A = 6792328
49 meter
Y = -1547880
12 meter E =
0006319
Z = 5110695
76 I = 51
23253
XDOT = 846
888634 Wp = 138
21412
YDOT = 7454
907214 meter/sec RA = 273
11271 deg
ZDOT = 1557
046515 TA = 296
64713
MA = 296
71184
Ha = 228
715 n
mi
Hp = 222
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13761708
25 X = 4186740
79
Y = -5078346
86 feet Y = -1501017
00 meter
Z = 16767374
55 Z = 5131052
52
XDOT = 2778
506016 XDOT = 755
899424
YDOT = 24458
357001 feet/sec YDOT = 7463
869045 meter/sec
ZDOT = 5108
420326 ZDOT = 1560
939051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9640579
34 X = 2938448
58
Y = -10912971
17 feet Y = -3326273
61 meter
Z = 16860763
93 Z = 5139160
84
XDOT = 13157
234291 XDOT = 4010
325012
YDOT = 19571
754569 feet/sec YDOT = 5965
470793 meter/sec
ZDOT = 5125
888621 ZDOT = 1562
370852
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 20111
55109624
00016717 00000-0 10270-3 0 9004
2 25544 51
6384 273
7284 0001948 173
2724 186
8452 15
49274779 23071
Satellite: ISS
Catalog Number: 25544
Epoch time: 20111
55109624 = yrday
fracday
Element set: 900
Inclination: 51
6384 deg
RA of node: 273
7284 deg
Eccentricity:
0001948
Arg of perigee: 173
2724 deg
Mean anomaly: 186
8452 deg
Mean motion: 15
49274779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2307
Checksum: 319
Coasting Arc #2 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2020/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4079546
25 A = 6792118
57 meter
Y = 1762483
95 meter E =
0013667
Z = -5148543
57 I = 51
23277
XDOT = -1389
432596 Wp = 87
57394
YDOT = -7385
980567 meter/sec RA = 268
13696 deg
ZDOT = -1430
216193 TA = 168
56874
MA = 168
53767
Ha = 228
769 n
mi
Hp = 222
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13384338
09 X = -4073942
73
Y = 5782427
66 feet Y = 1716894
69 meter
Z = -16891547
14 Z = -5168347
07
XDOT = -4558
505893 XDOT = -1299
789866
YDOT = -24232
219708 feet/sec YDOT = -7401
017023 meter/sec
ZDOT = -4692
310344 ZDOT = -1436
747561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8778398
48 X = -2675655
86
Y = 11508209
74 feet Y = 3507702
33 meter
Z = -16982407
64 Z = -5176237
85
XDOT = -14907
893654 XDOT = -4543
925986
YDOT = -18326
451299 feet/sec YDOT = -5585
902356 meter/sec
ZDOT = -4721
893627 ZDOT = -1439
233177
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 20112
51863896
00016717 00000-0 10270-3 0 9010
2 25544 51
6397 268
9412 0002036 175
9518 184
1649 15
49306608 23226
Satellite: ISS
Catalog Number: 25544
Epoch time: 20112
51863896 = yrday
fracday
Element set: 901
Inclination: 51
6397 deg
RA of node: 268
9412 deg
Eccentricity:
0002036
Arg of perigee: 175
9518 deg
Mean anomaly: 184
1649 deg
Mean motion: 15
49306608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2322
Checksum: 320
Coasting Arc #3 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2020/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938843
26 A = 6792025
51 meter
Y = -1981651
22 meter E =
0005575
Z = 5164143
51 I = 51
23528
XDOT = 1939
097473 Wp = 142
19654
YDOT = 7295
470529 meter/sec RA = 263
15896 deg
ZDOT = 1315
417565 TA = 295
05572
MA = 295
11359
Ha = 228
557 n
mi
Hp = 222
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922714
11 X = 3935625
13
Y = -6501480
38 feet Y = -1937622
12 meter
Z = 16942728
06 Z = 5183269
37
XDOT = 6361
868350 XDOT = 1850
983610
YDOT = 23935
270763 feet/sec YDOT = 7316
662257 meter/sec
ZDOT = 4315
674425 ZDOT = 1324
622856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7818823
05 X = 2383177
27
Y = -12047830
60 feet Y = -3672178
77 meter
Z = 17030490
46 Z = 5190893
49
XDOT = 16605
764578 XDOT = 5061
437043
YDOT = 16960
003354 feet/sec YDOT = 5169
409022 meter/sec
ZDOT = 4357
532953 ZDOT = 1328
176044
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 20113
55068260
00016717 00000-0 10270-3 0 9028
2 25544 51
6403 263
8322 0001956 183
9520 176
1615 15
49301290 23383
Satellite: ISS
Catalog Number: 25544
Epoch time: 20113
55068260 = yrday
fracday
Element set: 902
Inclination: 51
6403 deg
RA of node: 263
8322 deg
Eccentricity:
0001956
Arg of perigee: 183
9520 deg
Mean anomaly: 176
1615 deg
Mean motion: 15
49301290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2338
Checksum: 285
Coasting Arc #4 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2020/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3808347
25 A = 6791877
13 meter
Y = 2175459
76 meter E =
0013812
Z = -5197979
28 I = 51
24121
XDOT = -2466
729602 Wp = 88
67543
YDOT = -7144
169481 meter/sec RA = 258
18340 deg
ZDOT = -1185
140411 TA = 169
87991
MA = 169
85207
Ha = 228
654 n
mi
Hp = 222
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12494577
59 X = -3807141
61
Y = 7137335
16 feet Y = 2132878
79 meter
Z = -17053737
81 Z = -5216476
14
XDOT = -8092
944887 XDOT = -2380
901221
YDOT = -23438
876251 feet/sec YDOT = -7171
274323 meter/sec
ZDOT = -3888
255943 ZDOT = -1196
914472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6914799
54 X = -2107630
90
Y = 12503562
60 feet Y = 3811085
88 meter
Z = -17138624
94 Z = -5223852
88
XDOT = -18099
975615 XDOT = -5516
872567
YDOT = -15402
050685 feet/sec YDOT = -4694
545049 meter/sec
ZDOT = -3941
909673 ZDOT = -1201
494068
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 20114
51822052
00016717 00000-0 10270-3 0 9033
2 25544 51
6414 259
0449 0001912 182
9557 177
1583 15
49318052 23539
Satellite: ISS
Catalog Number: 25544
Epoch time: 20114
51822052 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 259
0449 deg
Eccentricity:
0001912
Arg of perigee: 182
9557 deg
Mean anomaly: 177
1583 deg
Mean motion: 15
49318052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 296
Coasting Arc #5 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2020/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3652813
10 A = 6791770
76 meter
Y = -2370429
84 meter E =
0004842
Z = 5210295
83 I = 51
24876
XDOT = 2997
224682 Wp = 144
56999
YDOT = 6970
918910 meter/sec RA = 253
20702 deg
ZDOT = 1065
768604 TA = 295
13123
MA = 295
18145
Ha = 228
441 n
mi
Hp = 222
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11984294
95 X = 3653739
37
Y = -7777000
78 feet Y = -2329576
35 meter
Z = 17094146
41 Z = 5228042
31
XDOT = 9833
414311 XDOT = 2913
874055
YDOT = 22870
468866 feet/sec YDOT = 7003
969958 meter/sec
ZDOT = 3496
616156 ZDOT = 1080
125821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5926393
87 X = 1806364
85
Y = -12891525
18 feet Y = -3929336
88 meter
Z = 17175603
11 Z = 5235123
83
XDOT = 19517
583094 XDOT = 5948
959327
YDOT = 13737
405139 feet/sec YDOT = 4187
161086 meter/sec
ZDOT = 3562
132341 ZDOT = 1085
737938
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 20115
55025888
00016717 00000-0 10270-3 0 9041
2 25544 51
6412 253
9369 0001909 191
1051 169
0057 15
49321783 23696
Satellite: ISS
Catalog Number: 25544
Epoch time: 20115
55025888 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 253
9369 deg
Eccentricity:
0001909
Arg of perigee: 191
1051 deg
Mean anomaly: 169
0057 deg
Mean motion: 15
49321783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 311
Coasting Arc #6 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2020/116/01:51:40
000
Vector Time (MET): N/A
Weight (LBS) : 921051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2535818
55 A = 6793822
52 meter
Y = -4168513
01 meter E =
0008146
Z = 4724133
40 I = 51
26222
XDOT = 4338
810396 Wp = 128
19274
YDOT = 5709
069270 meter/sec RA = 250
35079 deg
ZDOT = 2700
485957 TA = 294
90370
MA = 294
98835
Ha = 228
390 n
mi
Hp = 222
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8319614
65 X = 2559296
07
Y = -13676223
78 feet Y = -4140024
51 meter
Z = 15499125
33 Z = 4736508
58
XDOT = 14234
942243 XDOT = 4261
529770
YDOT = 18730
542226 feet/sec YDOT = 5757
156777 meter/sec
ZDOT = 8859
862064 ZDOT = 2721
374993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7872989
21 X = 2399687
11
Y = 13874573
33 feet Y = 4228969
95 meter
Z = 15556035
05 Z = 4741479
48
XDOT = -22267
256559 XDOT = -6787
059799
YDOT = 2564
825267 feet/sec YDOT = 781
758741 meter/sec
ZDOT = 8955
384413 ZDOT = 2729
601169
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 20116
13077956
00016717 00000-0 10270-3 0 9050
2 25544 51
6418 251
0691 0001529 197
5899 162
5198 15
49332286 23781
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
13077956 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 251
0691 deg
Eccentricity:
0001529
Arg of perigee: 197
5899 deg
Mean anomaly: 162
5198 deg
Mean motion: 15
49332286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 335
Coasting Arc #7 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2020/116/05:12:17
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4632295
66 A = 6794376
43 meter
Y = 1985313
64 meter E =
0007597
Z = 4551512
71 I = 51
26749
XDOT = -3
266309 Wp = 73
54544
YDOT = 7027
759106 meter/sec RA = 249
61564 deg
ZDOT = -3055
724319 TA = 47
22780
MA = 47
16392
Ha = 228
223 n
mi
Hp = 222
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15197820
40 X = 4587641
97
Y = 6513496
19 feet Y = 2036865
48 meter
Z = 14932784
50 Z = 4573906
59
XDOT = -10
716238 XDOT = -67
009322
YDOT = 23056
952446 feet/sec YDOT = 7027
366240 meter/sec
ZDOT = -10025
342255 ZDOT = -3055
894846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -713317
05 X = -217419
04
Y = 16426089
31 feet Y = 5006672
02 meter
Z = 15035364
95 Z = 4582779
24
XDOT = -20327
631966 XDOT = -6195
862223
YDOT = 8313
791122 feet/sec YDOT = 2534
043534 meter/sec
ZDOT = -10026
420335 ZDOT = -3056
052918
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 20116
25978289
00016717 00000-0 10270-3 0 9063
2 25544 51
6433 250
4316 0001388 204
4837 155
6248 15
49355298 23808
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
25978289 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 250
4316 deg
Eccentricity:
0001388
Arg of perigee: 204
4837 deg
Mean anomaly: 155
6248 deg
Mean motion: 15
49355298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 325
Coasting Arc #8 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2020/117/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2838506
73 A = 6803434
13 meter
Y = 6175517
15 meter E =
0012755
Z = -32742
85 I = 51
30871
XDOT = -4361
420389 Wp = 141
14821
YDOT = 1979
762433 meter/sec RA = 245
09359 deg
ZDOT = -5980
193139 TA = 39
20543
MA = 39
11310
Ha = 228
490 n
mi
Hp = 222
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9312686
13 X = 2769398
35
Y = 20260883
03 feet Y = 6206872
94 meter
Z = -107424
04 Z = -19121
86
XDOT = -14309
122010 XDOT = -4354
185678
YDOT = 6495
283573 feet/sec YDOT = 1931
030626 meter/sec
ZDOT = -19620
056229 ZDOT = -6001
361918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21501207
14 X = -6553567
94
Y = 5910760
52 feet Y = 1801599
81 meter
Z = -45226
73 Z = -13785
11
XDOT = -3682
982430 XDOT = -1122
573045
YDOT = -13471
841336 feet/sec YDOT = -4106
217239 meter/sec
ZDOT = -19717
192343 ZDOT = -6009
800226
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 20117
16281661
00016717 00000-0 10270-3 0 9076
2 25544 51
6434 245
9624 0001564 200
9500 159
1586 15
49289085 23943
Satellite: ISS
Catalog Number: 25544
Epoch time: 20117
16281661 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 245
9624 deg
Eccentricity:
0001564
Arg of perigee: 200
9500 deg
Mean anomaly: 159
1586 deg
Mean motion: 15
49289085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 313
Coasting Arc #9 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2020/118/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3293617
03 A = 6803342
22 meter
Y = -5945686
83 meter E =
0011005
Z = 132509
13 I = 51
32444
XDOT = 4247
572827 Wp = 48
97585
YDOT = -2212
606133 meter/sec RA = 240
12157 deg
ZDOT = 5978
179601 TA = 312
45479
MA = 312
54779
Ha = 228
378 n
mi
Hp = 222
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10805830
16 X = -3227529
48
Y = -19506846
54 feet Y = -5982148
88 meter
Z = 434741
23 Z = 116669
97
XDOT = 13935
606387 XDOT = 4242
960162
YDOT = -7259
206474 feet/sec YDOT = -2165
132888 meter/sec
ZDOT = 19613
450136 ZDOT = 5998
801614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20866884
96 X = 6360226
53
Y = -7868535
01 feet Y = -2398329
47 meter
Z = 362348
37 Z = 110443
78
XDOT = 4608
279992 XDOT = 1404
603742
YDOT = 13186
246002 feet/sec YDOT = 4019
167781 meter/sec
ZDOT = 19708
095458 ZDOT = 6007
027496
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 20118
19484760
00016717 00000-0 10270-3 0 9086
2 25544 51
6440 240
8548 0001344 209
4355 150
6719 15
49318559 24109
Satellite: ISS
Catalog Number: 25544
Epoch time: 20118
19484760 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 240
8548 deg
Eccentricity:
0001344
Arg of perigee: 209
4355 deg
Mean anomaly: 150
6719 deg
Mean motion: 15
49318559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 309
Coasting Arc #10 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2020/119/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3703417
48 A = 6803413
82 meter
Y = 5693265
93 meter E =
0012123
Z = -267300
62 I = 51
34155
XDOT = -4139
936735 Wp = 143
22415
YDOT = 2419
518036 meter/sec RA = 235
15219 deg
ZDOT = -5975
342327 TA = 39
66253
MA = 39
57393
Ha = 228
440 n
mi
Hp = 222
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12150319
82 X = 3640776
86
Y = 18678694
00 feet Y = 5734329
95 meter
Z = -876970
54 Z = -249462
43
XDOT = -13582
469604 XDOT = -4137
659713
YDOT = 7938
051299 feet/sec YDOT = 2373
235454 meter/sec
ZDOT = -19604
141494 ZDOT = -5995
447040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20079312
71 X = -6120174
51
Y = 9668584
50 feet Y = 2946984
56 meter
Z = -795382
59 Z = -242432
61
XDOT = -5447
654387 XDOT = -1660
445057
YDOT = -12888
961925 feet/sec YDOT = -3928
555595 meter/sec
ZDOT = -19696
429995 ZDOT = -6003
471862
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 20119
16237564
00016717 00000-0 10270-3 0 9093
2 25544 51
6434 236
0676 0001450 207
8835 152
2237 15
49287345 24251
Satellite: ISS
Catalog Number: 25544
Epoch time: 20119
16237564 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 236
0676 deg
Eccentricity:
0001450
Arg of perigee: 207
8835 deg
Mean anomaly: 152
2237 deg
Mean motion: 15
49287345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 308
Coasting Arc #11 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2020/120/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4115753
26 A = 6803262
51 meter
Y = -5397765
36 meter E =
0011350
Z = 369179
38 I = 51
36109
XDOT = 4009
921803 Wp = 50
15928
YDOT = -2641
411857 meter/sec RA = 230
18288 deg
ZDOT = 5968
697880 TA = 313
82758
MA = 313
92135
Ha = 228
270 n
mi
Hp = 222
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13503127
50 X = -4056881
24
Y = -17709203
95 feet Y = -5443461
50 meter
Z = 1211218
45 Z = 349329
15
XDOT = 13155
911426 XDOT = 4010
168121
YDOT = -8666
049401 feet/sec YDOT = -2596
569095 meter/sec
ZDOT = 19582
342126 ZDOT = 5988
177054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19096558
49 X = 5820631
03
Y = -11466631
17 feet Y = -3495029
18 meter
Z = 1120370
76 Z = 341489
01
XDOT = 6333
267711 XDOT = 1930
379998
YDOT = 12509
508497 feet/sec YDOT = 3812
898190 meter/sec
ZDOT = 19671
777019 ZDOT = 5995
957635
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 20120
19440156
00016717 00000-0 10270-3 0 9103
2 25544 51
6428 230
9602 0001340 220
5461 139
5590 15
49330999 24413
Satellite: ISS
Catalog Number: 25544
Epoch time: 20120
19440156 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 230
9602 deg
Eccentricity:
0001340
Arg of perigee: 220
5461 deg
Mean anomaly: 139
5590 deg
Mean motion: 15
49330999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 280
Coasting Arc #12 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2020/121/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4480187
24 A = 6803333
21 meter
Y = 5086924
09 meter E =
0011356
Z = -505215
98 I = 51
38375
XDOT = -3887
926260 Wp = 146
04299
YDOT = 2839
726594 meter/sec RA = 225
21582 deg
ZDOT = -5959
190927 TA = 39
41552
MA = 39
33295
Ha = 228
325 n
mi
Hp = 222
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14698777
05 X = 4425424
83
Y = 16689383
50 feet Y = 5136718
57 meter
Z = -1657532
74 Z = -483585
61
XDOT = -12755
663583 XDOT = -3890
445539
YDOT = 9316
688299 feet/sec YDOT = 2796
235320 meter/sec
ZDOT = -19551
151335 ZDOT = -5978
082952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17993369
37 X = -5484378
98
Y = 13082307
28 feet Y = 3987487
26 meter
Z = -1558485
93 Z = -475026
51
XDOT = -7138
765893 XDOT = -2175
895844
YDOT = -12127
222383 feet/sec YDOT = -3696
377382 meter/sec
ZDOT = -19637
906089 ZDOT = -5985
633776
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 20121
16192533
00016717 00000-0 10270-3 0 9115
2 25544 51
6432 226
1726 0001492 220
6520 139
4519 15
49290636 24566
Satellite: ISS
Catalog Number: 25544
Epoch time: 20121
16192533 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 226
1726 deg
Eccentricity:
0001492
Arg of perigee: 220
6520 deg
Mean anomaly: 139
4519 deg
Mean motion: 15
49290636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 285
Coasting Arc #13 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2020/122/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4839076
27 A = 6803102
65 meter
Y = -4734588
19 meter E =
0011676
Z = 610358
63 I = 51
40806
XDOT = 3743
242326 Wp = 51
42597
YDOT = -3050
078377 meter/sec RA = 220
24869 deg
ZDOT = 5947
551177 TA = 315
17080
MA = 315
26507
Ha = 228
144 n
mi
Hp = 222
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15876234
47 X = -4788737
83
Y = -15533425
81 feet Y = -4788420
75 meter
Z = 2002488
93 Z = 586974
30
XDOT = 12280
978761 XDOT = 3748
181170
YDOT = -10006
818823 feet/sec YDOT = -3008
191448 meter/sec
ZDOT = 19512
963180 ZDOT = 5965
746253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16703337
73 X = 5091177
34
Y = -14654631
24 feet Y = -4466731
60 meter
Z = 1895360
66 Z = 577705
93
XDOT = 7978
493032 XDOT = 2431
844676
YDOT = 11659
862685 feet/sec YDOT = 3553
926146 meter/sec
ZDOT = 19596
532333 ZDOT = 5973
023055
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 20122
19394383
00016717 00000-0 10270-3 0 9127
2 25544 51
6432 221
0642 0001348 233
1183 126
9844 15
49354612 24726
Satellite: ISS
Catalog Number: 25544
Epoch time: 20122
19394383 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 221
0642 deg
Eccentricity:
0001348
Arg of perigee: 233
1183 deg
Mean anomaly: 126
9844 deg
Mean motion: 15
49354612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 287
Coasting Arc #14 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2020/123/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5149083
07 A = 6803179
60 meter
Y = 4374507
12 meter E =
0010509
Z = -748218
49 I = 51
43343
XDOT = -3607
536112 Wp = 147
65300
YDOT = 3240
042457 meter/sec RA = 215
28452 deg
ZDOT = -5930
599442 TA = 40
43962
MA = 40
36155
Ha = 228
253 n
mi
Hp = 222
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16893317
17 X = 5103417
77
Y = 14352057
47 feet Y = 4431832
52 meter
Z = -2454785
07 Z = -723317
01
XDOT = -11835
748398 XDOT = -3614
691617
YDOT = 10630
060555 feet/sec YDOT = 3199
660587 meter/sec
ZDOT = -19457
347252 ZDOT = -5948
140744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15330008
55 X = -4672586
60
Y = 16028219
71 feet Y = 4885401
37 meter
Z = -2340662
12 Z = -713433
82
XDOT = -8747
053624 XDOT = -2666
101945
YDOT = -11195
397843 feet/sec YDOT = -3412
357263 meter/sec
ZDOT = -19537
926035 ZDOT = -5955
159855
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 20123
16146249
00016717 00000-0 10270-3 0 9132
2 25544 51
6424 216
2761 0001365 232
3373 127
7654 15
49302077 24878
Satellite: ISS
Catalog Number: 25544
Epoch time: 20123
16146249 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 216
2761 deg
Eccentricity:
0001365
Arg of perigee: 232
3373 deg
Mean anomaly: 127
7654 deg
Mean motion: 15
49302077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 294
Coasting Arc #15 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2020/124/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5447454
40 A = 6802934
45 meter
Y = -3974403
17 meter E =
0011963
Z = 854376
55 I = 51
46086
XDOT = 3446
336539 Wp = 53
51846
YDOT = -3441
464866 meter/sec RA = 210
32165 deg
ZDOT = 5913
720450 TA = 315
72910
MA = 315
82474
Ha = 228
085 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17872225
73 X = -5406756
67
Y = -13039380
49 feet Y = -4035092
94 meter
Z = 2803072
67 Z = 828013
66
XDOT = 11306
878408 XDOT = 3455
838314
YDOT = -11290
895229 feet/sec YDOT = -3402
872419 meter/sec
ZDOT = 19401
969979 ZDOT = 5930
484496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13781872
63 X = 4200714
78
Y = -17325265
95 feet Y = -5280741
06 meter
Z = 2682211
65 Z = 817538
11
XDOT = 9545
341949 XDOT = 2909
420226
YDOT = 10635
746396 feet/sec YDOT = 3241
775501 meter/sec
ZDOT = 19478
990600 ZDOT = 5937
196335
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 20124
19347737
00016717 00000-0 10270-3 0 9142
2 25544 51
6419 211
1683 0001367 240
3168 119
7846 15
49364092 25030
Satellite: ISS
Catalog Number: 25544
Epoch time: 20124
19347737 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 211
1683 deg
Eccentricity:
0001367
Arg of perigee: 240
3168 deg
Mean anomaly: 119
7846 deg
Mean motion: 15
49364092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2503
Checksum: 306
Coasting Arc #16 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2020/125/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5696752
92 A = 6802957
33 meter
Y = 3574221
94 meter E =
0009584
Z = -992448
03 I = 51
49072
XDOT = -3294
418962 Wp = 150
00402
YDOT = 3624
556207 meter/sec RA = 205
36133 deg
ZDOT = -5889
554275 TA = 40
74855
MA = 40
67690
Ha = 228
127 n
mi
Hp = 222
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18690134
26 X = 5661182
30
Y = 11726449
94 feet Y = 3637728
20 meter
Z = -3256063
08 Z = -964861
62
XDOT = -10808
461163 XDOT = -3306
096677
YDOT = 11891
588607 feet/sec YDOT = 3587
650379 meter/sec
ZDOT = -19322
684630 ZDOT = -5905
585753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12189766
23 X = -3715440
75
Y = 18413260
38 feet Y = 5612361
76 meter
Z = -3129558
29 Z = -953889
37
XDOT = -10277
582428 XDOT = -3132
607124
YDOT = -10081
480784 feet/sec YDOT = -3072
835343 meter/sec
ZDOT = -19396
351208 ZDOT = -5912
007848
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 20125
16099210
00016717 00000-0 10270-3 0 9151
2 25544 51
6425 206
3801 0001461 245
7378 114
3620 15
49320112 25184
Satellite: ISS
Catalog Number: 25544
Epoch time: 20125
16099210 = yrday
fracday
Element set: 915
Inclination: 51
6425 deg
RA of node: 206
3801 deg
Eccentricity:
0001461
Arg of perigee: 245
7378 deg
Mean anomaly: 114
3620 deg
Mean motion: 15
49320112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 269
Coasting Arc #17 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2020/126/03:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 935485
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5927718
33 A = 6802736
88 meter
Y = -3137870
72 meter E =
0012235
Z = 1100391
33 I = 51
52069
XDOT = 3116
647930 Wp = 55
34678
YDOT = -3816
255820 meter/sec RA = 200
40164 deg
ZDOT = 5866
957245 TA = 316
58895
MA = 316
68524
Ha = 228
033 n
mi
Hp = 222
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19447894
78 X = -5897534
31
Y = -10294851
43 feet Y = -3203989
92 meter
Z = 3610207
78 Z = 1071669
74
XDOT = 10225
222867 XDOT = 3130
592113
YDOT = -12520
524345 feet/sec YDOT = -3781
325287 meter/sec
ZDOT = 19248
547393 ZDOT = 5882
130755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10445558
69 X = 3183806
29
Y = -19391460
93 feet Y = -5910517
29 meter
Z = 3478465
78 Z = 1060236
37
XDOT = 11026
681864 XDOT = 3360
932632
YDOT = 9429
341801 feet/sec YDOT = 2874
063381 meter/sec
ZDOT = 19318
285665 ZDOT = 5888
213471
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 20126
19300233
00016717 00000-0 10270-3 0 9166
2 25544 51
6419 201
2715 0001379 251
6062 108
4938 15
49366145 25349
Satellite: ISS
Catalog Number: 25544
Epoch time: 20126
19300233 = yrday
fracday
Element set: 916
Inclination: 51
6419 deg
RA of node: 201
2715 deg
Eccentricity:
0001379
Arg of perigee: 251
6062 deg
Mean anomaly: 108
4938 deg
Mean motion: 15
49366145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2534
Checksum: 289
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