[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 4th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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
219/03:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 222
5
223/13:37:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 222
5
Coasting Arc #1 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2020/216/12:38:59
863
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3891404
66 A = 6802409
85 meter
Y = -5225099
14 meter E =
0006140
Z = -1950320
12 I = 52
01810
XDOT = 2942
167937 Wp = 136
66916
YDOT = 4284
404724 meter/sec RA = 113
15999 deg
ZDOT = -5622
751432 TA = 64
66744
MA = 64
60386
Ha = 228
893 n
mi
Hp = 222
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12767075
66 X = 3959017
35
Y = -17142713
73 feet Y = -5181204
46 meter
Z = -6398688
06 Z = -1931253
96
XDOT = 9652
781946 XDOT = 2921
351147
YDOT = 14056
445945 feet/sec YDOT = 4317
190259 meter/sec
ZDOT = -18447
347219 ZDOT = -5608
510089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20706789
85 X = -6311429
55
Y = 5405604
71 feet Y = 1647628
31 meter
Z = -6310495
64 Z = -1923439
07
XDOT = 1520
893436 XDOT = 463
568319
YDOT = -15575
321374 feet/sec YDOT = -4747
357955 meter/sec
ZDOT = -18381
732072 ZDOT = -5602
751936
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 20216
55558371
00016717 00000-0 10270-3 0 9007
2 25544 51
6449 114
0295 0000952 347
7131 12
3996 15
49104665 39356
Satellite: ISS
Catalog Number: 25544
Epoch time: 20216
55558371 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 114
0295 deg
Eccentricity:
0000952
Arg of perigee: 347
7131 deg
Mean anomaly: 12
3996 deg
Mean motion: 15
49104665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 307
Coasting Arc #2 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2020/217/12:38:59
863
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443456
52 A = 6802299
33 meter
Y = 5513265
17 meter E =
0014264
Z = 1979684
73 I = 52
02952
XDOT = -3270
905071 Wp = 63
35682
YDOT = -4066
738040 meter/sec RA = 108
23761 deg
ZDOT = 5611
226709 TA = 318
33229
MA = 318
44086
Ha = 228
922 n
mi
Hp = 222
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11297429
52 X = -3514467
49
Y = 18088140
31 feet Y = 5474360
80 meter
Z = 6495028
64 Z = 1962786
12
XDOT = -10731
315851 XDOT = -3252
441873
YDOT = -13342
316404 feet/sec YDOT = -4103
212772 meter/sec
ZDOT = 18409
536448 ZDOT = 5595
382942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20024157
08 X = 6103363
08
Y = -7406460
68 feet Y = -2257489
22 meter
Z = 6416821
97 Z = 1955847
34
XDOT = -82
755546 XDOT = -25
223890
YDOT = 15734
368411 feet/sec YDOT = 4795
835492 meter/sec
ZDOT = 18336
514761 ZDOT = 5588
969699
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 20217
58773727
00016717 00000-0 10270-3 0 9016
2 25544 51
6444 108
9230 0001159 353
6538 6
4597 15
49126840 39517
Satellite: ISS
Catalog Number: 25544
Epoch time: 20217
58773727 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 108
9230 deg
Eccentricity:
0001159
Arg of perigee: 353
6538 deg
Mean anomaly: 6
4597 deg
Mean motion: 15
49126840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 317
Coasting Arc #3 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2020/218/12:38:59
863
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2999243
96 A = 6802226
29 meter
Y = -5751598
92 meter E =
0005777
Z = -2042869
21 I = 52
03903
XDOT = 3567
369268 Wp = 135
04935
YDOT = 3838
289361 meter/sec RA = 103
31661 deg
ZDOT = -5582
659031 TA = 67
34619
MA = 67
28511
Ha = 228
871 n
mi
Hp = 222
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9840039
25 X = 3073259
99
Y = -18870075
21 feet Y = -5717645
30 meter
Z = -6702326
81 Z = -2028120
92
XDOT = 11703
967414 XDOT = 3551
299894
YDOT = 12592
812864 feet/sec YDOT = 3878
092625 meter/sec
ZDOT = -18315
810469 ZDOT = -5565
369459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19191894
02 X = -5849689
30
Y = 9245980
00 feet Y = 2818174
70 meter
Z = -6634029
92 Z = -2022052
32
XDOT = -1306
015977 XDOT = -398
073670
YDOT = -15763
074377 feet/sec YDOT = -4804
585070 meter/sec
ZDOT = -18236
105668 ZDOT = -5558
365008
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 20218
55537890
00016717 00000-0 10270-3 0 9024
2 25544 51
6448 104
1363 0001027 346
9162 13
1961 15
49111412 39663
Satellite: ISS
Catalog Number: 25544
Epoch time: 20218
55537890 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 104
1363 deg
Eccentricity:
0001027
Arg of perigee: 346
9162 deg
Mean anomaly: 13
1961 deg
Mean motion: 15
49111412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 291
Coasting Arc #4 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2020/219/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2786439
47 A = 6795399
97 meter
Y = -4277494
64 meter E =
0009654
Z = 4480059
85 I = 52
01879
XDOT = 3670
471922 Wp = 63
70393
YDOT = -5859
816734 meter/sec RA = 100
16856 deg
ZDOT = -3302
304455 TA = 59
48892
MA = 59
39365
Ha = 228
976 n
mi
Hp = 222
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9141861
78 X = -2760161
19
Y = -14033775
06 feet Y = -4308507
81 meter
Z = 14698359
10 Z = 4466588
44
XDOT = 12042
230715 XDOT = 3751
765668
YDOT = -19225
120520 feet/sec YDOT = -5818
316247 meter/sec
ZDOT = -10834
332203 ZDOT = -3284
277916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11774772
86 X = -3588950
77
Y = -11987310
96 feet Y = -3653732
38 meter
Z = 14636302
11 Z = 4461144
88
XDOT = 7306
727068 XDOT = 2227
090410
YDOT = -20342
675852 feet/sec YDOT = -6200
447600 meter/sec
ZDOT = -10750
886760 ZDOT = -3276
870284
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 20219
20047024
00016717 00000-0 10270-3 0 9033
2 25544 51
6423 100
9426 0001046 5
8970 354
2192 15
49165556 39763
Satellite: ISS
Catalog Number: 25544
Epoch time: 20219
20047024 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 100
9426 deg
Eccentricity:
0001046
Arg of perigee: 5
8970 deg
Mean anomaly: 354
2192 deg
Mean motion: 15
49165556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3976
Checksum: 290
Coasting Arc #5 (Orbit 3990)
---------------------------------------
Vector Time (GMT): 2020/220/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3126120
50 A = 6795622
79 meter
Y = 4068731
20 meter E =
0009061
Z = -4464514
79 I = 52
02324
XDOT = -3180
062887 Wp = 103
49841
YDOT = 6105
640367 meter/sec RA = 95
24762 deg
ZDOT = 3341
278300 TA = 200
12104
MA = 200
15678
Ha = 229
037 n
mi
Hp = 222
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10256300
86 X = 3102076
00
Y = 13348855
63 feet Y = 4103555
35 meter
Z = -14647358
24 Z = -4449387
96
XDOT = -10433
277188 XDOT = -3264
331320
YDOT = 20031
628502 feet/sec YDOT = 6069
607394 meter/sec
ZDOT = 10962
199148 ZDOT = 3325
626567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12924899
69 X = 3939509
43
Y = 10879692
78 feet Y = 3316130
36 meter
Z = -14577654
49 Z = -4443269
09
XDOT = -5280
181655 XDOT = -1609
399368
YDOT = 20847
769102 feet/sec YDOT = 6354
400022 meter/sec
ZDOT = 10889
699421 ZDOT = 3319
180383
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 20220
16810910
00016717 00000-0 10270-3 0 9043
2 25544 51
6416 96
1558 0001126 12
1280 347
9897 15
49119782 39919
Satellite: ISS
Catalog Number: 25544
Epoch time: 20220
16810910 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 96
1558 deg
Eccentricity:
0001126
Arg of perigee: 12
1280 deg
Mean anomaly: 347
9897 deg
Mean motion: 15
49119782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3991
Checksum: 306
Coasting Arc #6 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2020/221/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3430273
53 A = 6795656
30 meter
Y = -3848440
25 meter E =
0009967
Z = 4422324
65 I = 52
02409
XDOT = 2690
537532 Wp = 64
77245
YDOT = -6317
539029 meter/sec RA = 90
32586 deg
ZDOT = -3400
632696 TA = 59
54059
MA = 59
44218
Ha = 229
020 n
mi
Hp = 222
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11254178
24 X = -3408464
94
Y = -12626116
30 feet Y = -3886678
14 meter
Z = 14508939
16 Z = 4405714
93
XDOT = 8827
222873 XDOT = 2777
500232
YDOT = -20726
834084 feet/sec YDOT = -6286
965232 meter/sec
ZDOT = -11156
931417 ZDOT = -3387
352205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13917449
08 X = -4242038
48
Y = -9726021
95 feet Y = -2964491
49 meter
Z = 14432385
95 Z = 4398991
24
XDOT = 3268
144474 XDOT = 996
130436
YDOT = -21190
349707 feet/sec YDOT = -6458
818591 meter/sec
ZDOT = -11095
361062 ZDOT = -3381
866052
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 20221
20025503
00016717 00000-0 10270-3 0 9056
2 25544 51
6401 91
0487 0001128 7
3517 352
7649 15
49157503 40070
Satellite: ISS
Catalog Number: 25544
Epoch time: 20221
20025503 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 91
0487 deg
Eccentricity:
0001128
Arg of perigee: 7
3517 deg
Mean anomaly: 352
7649 deg
Mean motion: 15
49157503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 270
Coasting Arc #7 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2020/222/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3738390
06 A = 6795848
23 meter
Y = 3588317
23 meter E =
0008779
Z = -4405358
02 I = 52
02386
XDOT = -2172
628413 Wp = 102
75267
YDOT = 6481
346489 meter/sec RA = 85
40474 deg
ZDOT = 3439
475064 TA = 201
99246
MA = 202
03015
Ha = 229
067 n
mi
Hp = 222
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12265059
26 X = 3719385
02
Y = 11772694
33 feet Y = 3630016
38 meter
Z = -14453274
36 Z = -4387244
73
XDOT = -7128
045976 XDOT = -2261
650086
YDOT = 21264
260133 feet/sec YDOT = 6456
552806 meter/sec
ZDOT = 11284
367009 ZDOT = 3428
705294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14855271
61 X = 4527886
79
Y = 8411635
48 feet Y = 2563866
49 meter
Z = -14369775
37 Z = -4379907
53
XDOT = -1203
461112 XDOT = -366
814947
YDOT = 21295
358637 feet/sec YDOT = 6490
825313 meter/sec
ZDOT = 11234
370210 ZDOT = 3424
236040
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 20222
16789177
00016717 00000-0 10270-3 0 9067
2 25544 51
6406 86
2615 0001180 15
5127 344
6058 15
49122882 40223
Satellite: ISS
Catalog Number: 25544
Epoch time: 20222
16789177 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 86
2615 deg
Eccentricity:
0001180
Arg of perigee: 15
5127 deg
Mean anomaly: 344
6058 deg
Mean motion: 15
49122882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 294
Coasting Arc #8 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2020/223/03:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4009004
45 A = 6795893
28 meter
Y = -3324108
06 meter E =
0010377
Z = 4360433
71 I = 52
02074
XDOT = 1662
535335 Wp = 66
15007
YDOT = -6610
560858 meter/sec RA = 80
48278 deg
ZDOT = -3500
266918 TA = 59
31799
MA = 59
21576
Ha = 229
087 n
mi
Hp = 222
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13152901
72 X = -3992715
61
Y = -10905866
35 feet Y = -3368848
63 meter
Z = 14305884
86 Z = 4340999
21
XDOT = 5454
512253 XDOT = 1753
335178
YDOT = -21688
191790 feet/sec YDOT = -6591
461435 meter/sec
ZDOT = -11483
815348 ZDOT = -3491
970647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15628869
20 X = -4763679
33
Y = -7087373
27 feet Y = -2160231
37 meter
Z = 14216282
01 Z = 4333122
76
XDOT = -810
036404 XDOT = -246
899096
YDOT = -21241
753550 feet/sec YDOT = -6474
486482 meter/sec
ZDOT = -11445
219774 ZDOT = -3488
502987
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 20223
20003363
00016717 00000-0 10270-3 0 9070
2 25544 51
6409 81
1543 0001231 13
6653 346
4530 15
49159525 40386
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
20003363 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 81
1543 deg
Eccentricity:
0001231
Arg of perigee: 13
6653 deg
Mean anomaly: 346
4530 deg
Mean motion: 15
49159525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 270
Coasting Arc #9 (Orbit 4043)
---------------------------------------
Vector Time (GMT): 2020/223/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3478545
57 A = 6793021
02 meter
Y = -2864844
69 meter E =
0013615
Z = -5095415
00 I = 52
00859
XDOT = 2883
176473 Wp = 71
43719
YDOT = 6833
396348 meter/sec RA = 78
50341 deg
ZDOT = -1873
604754 TA = 180
45613
MA = 180
45737
Ha = 228
973 n
mi
Hp = 222
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11412551
07 X = 3535072
99
Y = -9399096
76 feet Y = -2825628
92 meter
Z = -16717240
82 Z = -5078380
51
XDOT = 9459
240396 XDOT = 2815
649930
YDOT = 22419
279358 feet/sec YDOT = 6865
260569 meter/sec
ZDOT = -6146
997224 ZDOT = -1859
763368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13774457
38 X = -4198454
61
Y = 5610858
42 feet Y = 1710189
65 meter
Z = -16638451
67 Z = -5071400
07
XDOT = -2107
370452 XDOT = -642
326514
YDOT = -23214
272695 feet/sec YDOT = -7075
710317 meter/sec
ZDOT = -6083
380595 ZDOT = -1854
214405
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 20223
58708611
00016717 00000-0 10270-3 0 9080
2 25544 51
6408 79
2377 0001213 11
9334 348
1844 15
49153738 40449
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
58708611 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 79
2377 deg
Eccentricity:
0001213
Arg of perigee: 11
9334 deg
Mean anomaly: 348
1844 deg
Mean motion: 15
49153738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4044
Checksum: 303
Coasting Arc #10 (Orbit 4059)
---------------------------------------
Vector Time (GMT): 2020/224/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3244817
94 A = 6793055
01 meter
Y = 3090360
39 meter E =
0005145
Z = 5101888
84 I = 52
00015
XDOT = -3428
485817 Wp = 110
96321
YDOT = -6607
773681 meter/sec RA = 73
58110 deg
ZDOT = 1818
724001 TA = 321
49010
MA = 321
52680
Ha = 229
206 n
mi
Hp = 222
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10645728
14 X = -3303916
01
Y = 10138977
65 feet Y = 3053743
88 meter
Z = 16738480
45 Z = 5085983
47
XDOT = -11248
313048 XDOT = -3363
175164
YDOT = -21679
047510 feet/sec YDOT = -6645
748355 meter/sec
ZDOT = 5966
942260 ZDOT = 1802
228241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13143676
58 X = 4006192
62
Y = -6769963
73 feet Y = -2063484
95 meter
Z = 16664887
64 Z = 5079457
75
XDOT = 4361
834735 XDOT = 1329
487227
YDOT = 22996
282774 feet/sec YDOT = 7009
266990 meter/sec
ZDOT = 5891
075199 ZDOT = 1795
599721
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 20224
61922780
00016717 00000-0 10270-3 0 9091
2 25544 51
6405 74
1309 0001258 16
3824 343
7366 15
49114044 40602
Satellite: ISS
Catalog Number: 25544
Epoch time: 20224
61922780 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 74
1309 deg
Eccentricity:
0001258
Arg of perigee: 16
3824 deg
Mean anomaly: 343
7366 deg
Mean motion: 15
49114044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4060
Checksum: 287
Coasting Arc #11 (Orbit 4074)
---------------------------------------
Vector Time (GMT): 2020/225/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3012826
34 A = 6792861
11 meter
Y = -3301723
30 meter E =
0013998
Z = -5127741
57 I = 51
98889
XDOT = 3939
922129 Wp = 73
16581
YDOT = 6318
093241 meter/sec RA = 68
65795 deg
ZDOT = -1753
285239 TA = 179
92214
MA = 179
92192
Ha = 229
036 n
mi
Hp = 222
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9884600
85 X = 3074430
75
Y = -10832425
51 feet Y = -3267686
99 meter
Z = -16823299
10 Z = -5112957
09
XDOT = 12926
253704 XDOT = 3877
494897
YDOT = 20728
652365 feet/sec YDOT = 6361
803309 meter/sec
ZDOT = -5752
248161 ZDOT = -1734
298040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12471106
56 X = -3801193
28
Y = 7862328
06 feet Y = 2396437
59 meter
Z = -16754864
01 Z = -5106882
55
XDOT = -6559
339280 XDOT = -1999
286612
YDOT = -22476
220683 feet/sec YDOT = -6850
752064 meter/sec
ZDOT = -5664
878474 ZDOT = -1726
654959
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 20225
58685782
00016717 00000-0 10270-3 0 9108
2 25544 51
6402 69
3433 0001128 24
6229 335
4975 15
49156779 40751
Satellite: ISS
Catalog Number: 25544
Epoch time: 20225
58685782 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 69
3433 deg
Eccentricity:
0001128
Arg of perigee: 24
6229 deg
Mean anomaly: 335
4975 deg
Mean motion: 15
49156779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4075
Checksum: 323
Coasting Arc #12 (Orbit 4090)
---------------------------------------
Vector Time (GMT): 2020/226/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2754270
02 A = 6792869
16 meter
Y = 3488884
12 meter E =
0004993
Z = 5133039
47 I = 51
97575
XDOT = -4444
091085 Wp = 110
95688
YDOT = -6008
261957 meter/sec RA = 63
73364 deg
ZDOT = 1696
103646 TA = 322
70811
MA = 322
74277
Ha = 229
210 n
mi
Hp = 222
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9036318
95 X = -2818012
23
Y = 11446470
23 feet Y = 3457727
14 meter
Z = 16840680
66 Z = 5119505
84
XDOT = -14580
351329 XDOT = -4384
813242
YDOT = -19712
145529 feet/sec YDOT = -6057
627635 meter/sec
ZDOT = 5564
644509 ZDOT = 1674
659718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11660714
11 X = 3554185
66
Y = -8877589
60 feet Y = -2705889
31 meter
Z = 16778003
91 Z = 5113935
59
XDOT = 8736
906726 XDOT = 2663
009170
YDOT = 21825
217717 feet/sec YDOT = 6652
326360 meter/sec
ZDOT = 5465
928735 ZDOT = 1666
015079
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 20226
61899640
00016717 00000-0 10270-3 0 9114
2 25544 51
6407 64
2360 0001207 23
6783 336
4422 15
49126670 40914
Satellite: ISS
Catalog Number: 25544
Epoch time: 20226
61899640 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 64
2360 deg
Eccentricity:
0001207
Arg of perigee: 23
6783 deg
Mean anomaly: 336
4422 deg
Mean motion: 15
49126670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4091
Checksum: 292
Coasting Arc #13 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2020/227/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2500650
89 A = 6792679
81 meter
Y = -3662341
24 meter E =
0014468
Z = -5158305
02 I = 51
96029
XDOT = 4903
583993 Wp = 74
51997
YDOT = 5640
645062 meter/sec RA = 58
80900 deg
ZDOT = -1627
680301 TA = 179
80537
MA = 179
80481
Ha = 229
114 n
mi
Hp = 222
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8204235
20 X = 2566474
24
Y = -12015555
25 feet Y = -3634008
73 meter
Z = -16923572
90 Z = -5145998
39
XDOT = 16087
873993 XDOT = 4848
050418
YDOT = 18506
053353 feet/sec YDOT = 5695
170063 meter/sec
ZDOT = -5340
158468 ZDOT = -1603
995307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10825313
34 X = -3299555
51
Y = 9819501
39 feet Y = 2992984
02 meter
Z = -16866545
18 Z = -5140922
97
XDOT = -10796
894100 XDOT = -3290
893322
YDOT = -20887
756449 feet/sec YDOT = -6366
588166 meter/sec
ZDOT = -5231
086002 ZDOT = -1594
435013
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 20227
58662261
00016717 00000-0 10270-3 0 9129
2 25544 51
6415 59
4488 0001229 37
5565 322
5671 15
49168969 41062
Satellite: ISS
Catalog Number: 25544
Epoch time: 20227
58662261 = yrday
fracday
Element set: 912
Inclination: 51
6415 deg
RA of node: 59
4488 deg
Eccentricity:
0001229
Arg of perigee: 37
5565 deg
Mean anomaly: 322
5671 deg
Mean motion: 15
49168969 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 325
Coasting Arc #14 (Orbit 4121)
---------------------------------------
Vector Time (GMT): 2020/228/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2224075
61 A = 6792679
40 meter
Y = 3808995
21 meter E =
0004984
Z = 5162183
11 I = 51
94024
XDOT = -5353
587468 Wp = 110
51693
YDOT = -5254
524743 meter/sec RA = 53
88246 deg
ZDOT = 1567
667747 TA = 324
40781
MA = 324
44104
Ha = 229
254 n
mi
Hp = 222
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7296835
98 X = -2291578
18
Y = 12496703
46 feet Y = 3783746
17 meter
Z = 16936296
28 Z = 5151215
94
XDOT = -17564
263345 XDOT = -5302
046627
YDOT = -17239
254405 feet/sec YDOT = -5314
104325 meter/sec
ZDOT = 5143
266887 ZDOT = 1541
787275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9868609
64 X = 3007952
22
Y = -10664990
67 feet Y = -3250689
16 meter
Z = 16885439
35 Z = 5146681
91
XDOT = 12814
304234 XDOT = 3905
799931
YDOT = 19827
017721 feet/sec YDOT = 6043
275001 meter/sec
ZDOT = 5024
043584 ZDOT = 1531
328484
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 20228
61875758
00016717 00000-0 10270-3 0 9132
2 25544 51
6402 54
3414 0001224 37
9582 322
1654 15
49142721 41222
Satellite: ISS
Catalog Number: 25544
Epoch time: 20228
61875758 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 54
3414 deg
Eccentricity:
0001224
Arg of perigee: 37
9582 deg
Mean anomaly: 322
1654 deg
Mean motion: 15
49142721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4122
Checksum: 288
Coasting Arc #15 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2020/229/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1953953
60 A = 6792521
19 meter
Y = -3944323
52 meter E =
0014723
Z = -5186393
68 I = 51
92038
XDOT = 5749
840510 Wp = 76
04254
YDOT = 4817
314105 meter/sec RA = 48
95612 deg
ZDOT = -1497
517893 TA = 179
55677
MA = 179
55546
Ha = 229
127 n
mi
Hp = 222
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6410608
91 X = 2023107
02
Y = -12940693
98 feet Y = -3922086
00 meter
Z = -17015727
29 Z = -5176734
64
XDOT = 18864
306134 XDOT = 5702
818465
YDOT = 15804
836301 feet/sec YDOT = 4881
350118 meter/sec
ZDOT = -4913
116447 ZDOT = -1469
701835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8900309
40 X = -2712814
31
Y = 11439647
20 feet Y = 3486804
47 meter
Z = -16970898
82 Z = -5172729
96
XDOT = -14659
964743 XDOT = -4468
357254
YDOT = -18503
762017 feet/sec YDOT = -5639
946663 meter/sec
ZDOT = -4784
936659 ZDOT = -1458
448694
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 20229
58638192
00016717 00000-0 10270-3 0 9149
2 25544 51
6414 49
5550 0001180 45
3749 314
7497 15
49176210 41379
Satellite: ISS
Catalog Number: 25544
Epoch time: 20229
58638192 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 49
5550 deg
Eccentricity:
0001180
Arg of perigee: 45
3749 deg
Mean anomaly: 314
7497 deg
Mean motion: 15
49176210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 312
Coasting Arc #16 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2020/230/13:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1665301
42 A = 6792463
58 meter
Y = 4049755
97 meter E =
0004728
Z = 5189196
56 I = 51
89733
XDOT = -6133
918252 Wp = 110
50378
YDOT = -4364
101066 meter/sec RA = 44
02571 deg
ZDOT = 1434
686375 TA = 325
71787
MA = 325
74837
Ha = 229
188 n
mi
Hp = 222
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5463587
34 X = -1735668
80
Y = 13286600
94 feet Y = 4030739
66 meter
Z = 17024923
09 Z = 5180936
66
XDOT = -20124
403715 XDOT = -6091
630409
YDOT = -14317
916883 feet/sec YDOT = -4432
458551 meter/sec
ZDOT = 4706
976296 ZDOT = 1404
993376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7830932
62 X = 2386868
26
Y = -12098192
65 feet Y = -3687529
12 meter
Z = 16986547
21 Z = 5177499
59
XDOT = 16439
781843 XDOT = 5010
845506
YDOT = 17070
176961 feet/sec YDOT = 5202
989938 meter/sec
ZDOT = 4570
108527 ZDOT = 1392
969079
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20230
61851296
00016717 00000-0 10270-3 0 9158
2 25544 51
6417 44
4466 0001149 41
6830 318
4407 15
49170440 41536
Satellite: ISS
Catalog Number: 25544
Epoch time: 20230
61851296 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 44
4466 deg
Eccentricity:
0001149
Arg of perigee: 41
6830 deg
Mean anomaly: 318
4407 deg
Mean motion: 15
49170440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 288
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