[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 20th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13552 8396 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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
140/01:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
5
141/17:30:57
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
4
143/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
5
145/22:00:00
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
3
146/12:14:26
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
2
148/20:33:31
100 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
3
149/04:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
2
149/15:17:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
2
152/12:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 2740)
---------------------------------------
Vector Time (GMT): 2020/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -994508
36 A = 6792875
37 meter
Y = -4540731
55 meter E =
0006382
Z = 4950955
82 I = 51
90009
XDOT = 6229
356487 Wp = 46
03139
YDOT = -3842
674954 meter/sec RA = 134
27654 deg
ZDOT = -2266
847270 TA = 66
08497
MA = 66
01813
Ha = 228
237 n
mi
Hp = 222
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3262822
72 X = -967707
80
Y = -14897413
22 feet Y = -4551703
30 meter
Z = 16243293
39 Z = 4946189
66
XDOT = 20437
521282 XDOT = 6282
874598
YDOT = -12607
201294 feet/sec YDOT = -3772
714479 meter/sec
ZDOT = -7437
162959 ZDOT = -2236
457430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14210052
72 X = -4331224
07
Y = -5599983
31 feet Y = -1706874
91 meter
Z = 16221532
03 Z = 4944322
96
XDOT = 708
352408 XDOT = 215
905814
YDOT = -22993
928195 feet/sec YDOT = -7008
549314 meter/sec
ZDOT = -7297
290435 ZDOT = -2224
214125
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 20139
54450298
00016717 00000-0 10270-3 0 9009
2 25544 51
6381 135
1920 0001375 318
7442 41
3604 15
49372117 27414
Satellite: ISS
Catalog Number: 25544
Epoch time: 20139
54450298 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 135
1920 deg
Eccentricity:
0001375
Arg of perigee: 318
7442 deg
Mean anomaly: 41
3604 deg
Mean motion: 15
49372117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2741
Checksum: 287
Coasting Arc #2 (Orbit 2749)
---------------------------------------
Vector Time (GMT): 2020/140/01:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5409847
89 A = 6797330
56 meter
Y = 1685043
42 meter E =
0010723
Z = 3745910
21 I = 51
92910
XDOT = 1037
715506 Wp = 92
70456
YDOT = -6256
326484 meter/sec RA = 131
51295 deg
ZDOT = 4301
881644 TA = 311
76382
MA = 311
85542
Ha = 228
252 n
mi
Hp = 222
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17748844
80 X = -5446484
19
Y = 5528357
69 feet Y = 1624341
56 meter
Z = 12289731
66 Z = 3719542
09
XDOT = 3404
578431 XDOT = 1086
702147
YDOT = -20526
005525 feet/sec YDOT = -6244
448393 meter/sec
ZDOT = 14113
784922 ZDOT = 4307
041089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2644761
12 X = -806123
19
Y = -18481249
44 feet Y = -5633084
83 meter
Z = 12168417
83 Z = 3708933
75
XDOT = 18397
940321 XDOT = 5607
692210
YDOT = 6699
951256 feet/sec YDOT = 2042
145143 meter/sec
ZDOT = 14137
731364 ZDOT = 4309
180520
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 20140
12500027
00016717 00000-0 10270-3 0 9012
2 25544 51
6391 132
3147 0001139 304
2631 55
8411 15
49392374 27506
Satellite: ISS
Catalog Number: 25544
Epoch time: 20140
12500027 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 132
3147 deg
Eccentricity:
0001139
Arg of perigee: 304
2631 deg
Mean anomaly: 55
8411 deg
Mean motion: 15
49392374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2750
Checksum: 262
Coasting Arc #3 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2020/141/01:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5236793
59 A = 6797045
92 meter
Y = -1997867
48 meter E =
0005560
Z = -3851304
25 I = 51
95030
XDOT = -647
329129 Wp = 66
28182
YDOT = 6373
105140 meter/sec RA = 126
58374 deg
ZDOT = -4188
864757 TA = 159
70310
MA = 159
68099
Ha = 228
221 n
mi
Hp = 222
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17181081
33 X = 5277452
84
Y = -6554683
35 feet Y = -1939078
28 meter
Z = -12635512
63 Z = -3825766
98
XDOT = -2123
783232 XDOT = -698
199559
YDOT = 20909
137598 feet/sec YDOT = 6365
582146 meter/sec
ZDOT = -13742
994610 ZDOT = -4192
132322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4058022
46 X = 1236885
25
Y = 18017821
74 feet Y = 5491832
07 meter
Z = -12517993
54 Z = -3815484
43
XDOT = -19100
114194 XDOT = -5821
714806
YDOT = -5250
858104 feet/sec YDOT = -1600
461550 meter/sec
ZDOT = -13758
261704 ZDOT = -4193
518167
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 20141
09249398
00016717 00000-0 10270-3 0 9021
2 25544 51
6400 127
5260 0001167 314
7381 45
3668 15
49377394 27657
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
09249398 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 127
5260 deg
Eccentricity:
0001167
Arg of perigee: 314
7381 deg
Mean anomaly: 45
3668 deg
Mean motion: 15
49377394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 312
Coasting Arc #4 (Orbit 2774)
---------------------------------------
Vector Time (GMT): 2020/141/17:30:57
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -389185
72 A = 6797625
75 meter
Y = 5745781
69 meter E =
0004598
Z = -3614745
23 I = 51
96795
XDOT = -5744
580792 Wp = 82
18492
YDOT = 2407
607164 meter/sec RA = 123
27859 deg
ZDOT = 4450
933857 TA = 235
36564
MA = 235
40900
Ha = 228
257 n
mi
Hp = 222
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1276856
02 X = -435849
18
Y = 18850989
81 feet Y = 5741168
96 meter
Z = -11859400
36 Z = -3616748
58
XDOT = -18847
049842 XDOT = -5792
696860
YDOT = 7898
973634 feet/sec YDOT = 2343
097729 meter/sec
ZDOT = 14602
801369 ZDOT = 4422
911829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12872941
49 X = 3923672
57
Y = -13822212
50 feet Y = -4213010
37 meter
Z = -11868840
47 Z = -3617622
57
XDOT = 18653
412299 XDOT = 5685
560069
YDOT = 4959
318791 feet/sec YDOT = 1511
600368 meter/sec
ZDOT = 14473
827891 ZDOT = 4411
622741
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 20141
73748856
00016717 00000-0 10270-3 0 9036
2 25544 51
6425 124
3384 0001592 330
6486 29
4574 15
49389407 27759
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
73748856 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 124
3384 deg
Eccentricity:
0001592
Arg of perigee: 330
6486 deg
Mean anomaly: 29
4574 deg
Mean motion: 15
49389407 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2775
Checksum: 329
Coasting Arc #5 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2020/142/17:30:57
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 29140
47 A = 6798015
73 meter
Y = -5820647
59 meter E =
0011736
Z = 3503429
08 I = 51
98583
XDOT = 5521
315890 Wp = 81
52836
YDOT = -2725
858895 meter/sec RA = 118
35276 deg
ZDOT = -4559
994304 TA = 57
58681
MA = 57
47333
Ha = 228
363 n
mi
Hp = 222
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 95605
21 X = 77208
57
Y = -19096612
82 feet Y = -5820053
34 meter
Z = 11494189
89 Z = 3503686
73
XDOT = 18114
553444 XDOT = 5573
537119
YDOT = -8943
106612 feet/sec YDOT = -2663
823115 meter/sec
ZDOT = -14960
611234 ZDOT = -4533
046914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11861227
89 X = -3615302
26
Y = 14965565
19 feet Y = 4561504
27 meter
Z = 11495620
66 Z = 3503865
18
XDOT = -18743
851739 XDOT = -5713
126010
YDOT = -3422
187893 feet/sec YDOT = -1043
082870 meter/sec
ZDOT = -14836
548826 ZDOT = -4522
180082
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 20142
76948014
00016717 00000-0 10270-3 0 9049
2 25544 51
6418 119
2314 0001568 337
8329 22
2753 15
49372146 27915
Satellite: ISS
Catalog Number: 25544
Epoch time: 20142
76948014 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 119
2314 deg
Eccentricity:
0001568
Arg of perigee: 337
8329 deg
Mean anomaly: 22
2753 deg
Mean motion: 15
49372146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 308
Coasting Arc #6 (Orbit 2794)
---------------------------------------
Vector Time (GMT): 2020/143/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4672155
16 A = 6793240
09 meter
Y = -752057
04 meter E =
0011494
Z = -4884631
00 I = 51
97169
XDOT = -1445
645468 Wp = 66
79521
YDOT = 7093
999559 meter/sec RA = 117
02696 deg
ZDOT = -2475
204670 TA = 178
95773
MA = 178
95534
Ha = 228
313 n
mi
Hp = 222
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15328593
05 X = 4703944
79
Y = -2467378
73 feet Y = -699631
35 meter
Z = -16025692
27 Z = -4861857
99
XDOT = -4742
931325 XDOT = -1512
841898
YDOT = 23274
276769 feet/sec YDOT = 7077
457893 meter/sec
ZDOT = -8120
750229 ZDOT = -2482
389550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5148303
10 X = -1569202
78
Y = 14761304
86 feet Y = 4499245
72 meter
Z = -15920910
44 Z = -4852693
50
XDOT = -17190
341252 XDOT = -5239
616014
YDOT = -14789
350921 feet/sec YDOT = -4507
794161 meter/sec
ZDOT = -8154
103725 ZDOT = -2485
370815
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 20143
02747744
00016717 00000-0 10270-3 0 9057
2 25544 51
6392 117
9498 0001155 332
9464 27
1626 15
49388500 27950
Satellite: ISS
Catalog Number: 25544
Epoch time: 20143
02747744 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 117
9498 deg
Eccentricity:
0001155
Arg of perigee: 332
9464 deg
Mean anomaly: 27
1626 deg
Mean motion: 15
49388500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2795
Checksum: 321
Coasting Arc #7 (Orbit 2810)
---------------------------------------
Vector Time (GMT): 2020/144/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4563290
23 A = 6792981
15 meter
Y = 997952
94 meter E =
0005681
Z = 4928548
01 I = 51
98573
XDOT = 957
208780 Wp = 115
99970
YDOT = -7231
989414 meter/sec RA = 112
09967 deg
ZDOT = 2346
115526 TA = 311
10849
MA = 311
15752
Ha = 228
389 n
mi
Hp = 222
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14971424
63 X = -4598050
93
Y = 3274123
82 feet Y = 946727
95 meter
Z = 16169776
92 Z = 4906296
67
XDOT = 3140
448753 XDOT = 1026
611619
YDOT = -23726
999390 feet/sec YDOT = -7220
897490 meter/sec
ZDOT = 7697
229417 ZDOT = 2350
932927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4013394
31 X = 1223282
59
Y = -14901589
55 feet Y = -4542004
50 meter
Z = 16067371
37 Z = 4897334
79
XDOT = 18574
765599 XDOT = 5661
588555
YDOT = 13342
412219 feet/sec YDOT = 4066
767244 meter/sec
ZDOT = 7719
722543 ZDOT = 2352
971431
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 20144
05946705
00016717 00000-0 10270-3 0 9060
2 25544 51
6397 112
8409 0001237 325
9375 34
1696 15
49401715 28113
Satellite: ISS
Catalog Number: 25544
Epoch time: 20144
05946705 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 112
8409 deg
Eccentricity:
0001237
Arg of perigee: 325
9375 deg
Mean anomaly: 34
1696 deg
Mean motion: 15
49401715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2811
Checksum: 307
Coasting Arc #8 (Orbit 2825)
---------------------------------------
Vector Time (GMT): 2020/145/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4457781
63 A = 6792800
79 meter
Y = -1222740
89 meter E =
0012227
Z = -4988800
32 I = 51
99811
XDOT = -459
004442 Wp = 68
19240
YDOT = 7312
686671 meter/sec RA = 107
17476 deg
ZDOT = -2202
381071 TA = 180
38066
MA = 180
38159
Ha = 228
336 n
mi
Hp = 222
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14625267
83 X = 4495356
44
Y = -4011617
09 feet Y = -1172679
94 meter
Z = -16367455
11 Z = -4967054
78
XDOT = -1505
920084 XDOT = -530
044906
YDOT = 23991
754171 feet/sec YDOT = 7307
156884 meter/sec
ZDOT = -7225
659681 ZDOT = -2204
782185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2942550
95 X = -896889
53
Y = 14986652
54 feet Y = 4567931
69 meter
Z = -16267352
49 Z = -4958289
04
XDOT = -19761
284152 XDOT = -6023
239410
YDOT = -11735
843122 feet/sec YDOT = -3577
084984 meter/sec
ZDOT = -7237
063476 ZDOT = -2205
856948
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 20145
02695725
00016717 00000-0 10270-3 0 9072
2 25544 51
6412 108
0531 0001249 337
3712 22
7382 15
49390188 28261
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
02695725 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 108
0531 deg
Eccentricity:
0001249
Arg of perigee: 337
3712 deg
Mean anomaly: 22
7382 deg
Mean motion: 15
49390188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2826
Checksum: 297
Coasting Arc #9 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2020/145/22:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3512496
34 A = 6792100
72 meter
Y = 2718840
52 meter E =
0012953
Z = -5149857
89 I = 52
00259
XDOT = -2884
798843 Wp = 97
12928
YDOT = 6886
541519 meter/sec RA = 102
66490 deg
ZDOT = 1670
153029 TA = 188
94109
MA = 188
96418
Ha = 228
450 n
mi
Hp = 222
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11523938
11 X = 3506847
72
Y = 8920080
45 feet Y = 2758089
02 meter
Z = -16895859
21 Z = -5132808
64
XDOT = -9464
563133 XDOT = -2969
704521
YDOT = 22593
640154 feet/sec YDOT = 6853
806632 meter/sec
ZDOT = 5479
504687 ZDOT = 1655
934574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14597916
07 X = -4449444
82
Y = -1381935
61 feet Y = -421213
97 meter
Z = -16817554
63 Z = -5125990
65
XDOT = -4039
765446 XDOT = -1231
320508
YDOT = -23127
471793 feet/sec YDOT = -7049
253403 meter/sec
ZDOT = 5413
731506 ZDOT = 1650
105363
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 20145
92994631
00016717 00000-0 10270-3 0 9080
2 25544 51
6399 103
5841 0001334 349
2665 10
8457 15
49386331 28405
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
92994631 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 103
5841 deg
Eccentricity:
0001334
Arg of perigee: 349
2665 deg
Mean anomaly: 10
8457 deg
Mean motion: 15
49386331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 319
Coasting Arc #10 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2020/146/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -991795
00 A = 6803130
38 meter
Y = 6720520
84 meter E =
0012732
Z = -207256
36 I = 52
04404
XDOT = -4690
182340 Wp = 37
57957
YDOT = -512
295026 meter/sec RA = 99
75863 deg
ZDOT = 6036
997331 TA = 320
20395
MA = 320
29727
Ha = 228
474 n
mi
Hp = 222
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3253920
61 X = -1065865
41
Y = 22048952
89 feet Y = 6709015
76 meter
Z = -679974
93 Z = -212252
91
XDOT = -15387
737337 XDOT = -4713
429627
YDOT = -1680
757960 feet/sec YDOT = -564
874990 meter/sec
ZDOT = 19806
421688 ZDOT = 6014
157525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18872943
59 X = 5752473
21
Y = 11854283
15 feet Y = 3613185
50 meter
Z = -703320
66 Z = -214372
14
XDOT = -6924
561635 XDOT = -2110
606386
YDOT = 12154
837399 feet/sec YDOT = 3704
794439 meter/sec
ZDOT = 19701
355795 ZDOT = 6004
973246
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 20146
51043899
00016717 00000-0 10270-3 0 9098
2 25544 51
6405 100
7148 0001726 349
7358 10
3756 15
49385963 28497
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
51043899 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 100
7148 deg
Eccentricity:
0001726
Arg of perigee: 349
7358 deg
Mean anomaly: 10
3756 deg
Mean motion: 15
49385963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 329
Coasting Arc #11 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2020/147/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 529354
37 A = 6803176
68 meter
Y = -6777678
65 meter E =
0010838
Z = 56488
76 I = 52
04955
XDOT = 4700
792380 Wp = 128
17414
YDOT = 310
319970 meter/sec RA = 94
83718 deg
ZDOT = -6039
561387 TA = 51
22212
MA = 51
12534
Ha = 228
503 n
mi
Hp = 222
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1736726
92 X = 604830
65
Y = -22236478
52 feet Y = -6771337
03 meter
Z = 185330
58 Z = 59242
33
XDOT = 15422
547177 XDOT = 4726
309745
YDOT = 1018
110139 feet/sec YDOT = 363
031277 meter/sec
ZDOT = -19814
833946 ZDOT = -6016
664666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19832763
15 X = -6045026
21
Y = -10204592
01 feet Y = -3110359
64 meter
Z = 198375
36 Z = 60464
81
XDOT = 6213
420573 XDOT = 1893
850591
YDOT = -12505
394535 feet/sec YDOT = -3811
644254 meter/sec
ZDOT = -19709
486711 ZDOT = -6007
451549
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 20147
54242661
00016717 00000-0 10270-3 0 9102
2 25544 51
6414 95
6074 0001768 351
4397 8
6723 15
49375882 28657
Satellite: ISS
Catalog Number: 25544
Epoch time: 20147
54242661 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 95
6074 deg
Eccentricity:
0001768
Arg of perigee: 351
4397 deg
Mean anomaly: 8
6723 deg
Mean motion: 15
49375882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 323
Coasting Arc #12 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2020/148/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -36196
76 A = 6803141
50 meter
Y = 6795777
05 meter E =
0013333
Z = 59228
85 I = 52
05140
XDOT = -4711
787836 Wp = 40
07610
YDOT = -84
238618 meter/sec RA = 89
91575 deg
ZDOT = 6041
812687 TA = 320
55714
MA = 320
65413
Ha = 228
519 n
mi
Hp = 222
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -118755
77 X = -112474
16
Y = 22295856
47 feet Y = 6794945
77 meter
Z = 194320
37 Z = 58868
85
XDOT = -15458
621508 XDOT = -4739
843313
YDOT = -276
373420 feet/sec YDOT = -137
087020 meter/sec
ZDOT = 19822
220102 ZDOT = 6018
856520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20659863
21 X = 6297126
31
Y = 8383922
80 feet Y = 2555419
67 meter
Z = 192275
51 Z = 58605
58
XDOT = -5429
785432 XDOT = -1654
998600
YDOT = 12871
455402 feet/sec YDOT = 3923
219606 meter/sec
ZDOT = 19716
579009 ZDOT = 6009
613282
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 20148
57441215
00016717 00000-0 10270-3 0 9113
2 25544 51
6416 90
5001 0001774 353
5954 6
5173 15
49389278 28810
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
57441215 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 90
5001 deg
Eccentricity:
0001774
Arg of perigee: 353
5954 deg
Mean anomaly: 6
5173 deg
Mean motion: 15
49389278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 307
Coasting Arc #13 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2020/148/20:33:31
100
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3092701
33 A = 6797247
29 meter
Y = -4731071
64 meter E =
0011592
Z = 3768210
69 I = 52
02986
XDOT = 3173
351539 Wp = 76
32810
YDOT = -5500
535983 meter/sec RA = 88
18004 deg
ZDOT = -4287
854780 TA = 58
95176
MA = 58
83801
Ha = 228
524 n
mi
Hp = 222
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10146657
89 X = -3057871
00
Y = -15521888
57 feet Y = -4765462
26 meter
Z = 12362895
96 Z = 3753271
44
XDOT = 10411
258329 XDOT = 3255
452224
YDOT = -18046
377896 feet/sec YDOT = -5464
589588 meter/sec
ZDOT = -14067
765025 ZDOT = -4272
241349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13534318
09 X = 4125260
15
Y = 12743408
12 feet Y = 3884190
79 meter
Z = 12294416
27 Z = 3747338
08
XDOT = -5132
174283 XDOT = -1564
286721
YDOT = 18996
816471 feet/sec YDOT = 5790
229660 meter/sec
ZDOT = -13995
591765 ZDOT = -4265
856370
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 20148
89690627
00016717 00000-0 10270-3 0 9122
2 25544 51
6399 88
9003 0001547 349
7014 10
4104 15
49379997 28865
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
89690627 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 88
9003 deg
Eccentricity:
0001547
Arg of perigee: 349
7014 deg
Mean anomaly: 10
4104 deg
Mean motion: 15
49379997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 341
Coasting Arc #14 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3421591
65 A = 6794158
93 meter
Y = -3593350
74 meter E =
0010854
Z = -4652025
02 I = 52
02221
XDOT = 2735
830496 Wp = 62
11116
YDOT = 6485
950150 meter/sec RA = 86
54954 deg
ZDOT = -2998
111916 TA = 178
08181
MA = 178
07765
Ha = 228
555 n
mi
Hp = 222
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11225694
39 X = 3484116
08
Y = -11789208
46 feet Y = -3554737
78 meter
Z = -15262549
26 Z = -4635252
98
XDOT = 8975
821836 XDOT = 2677
662419
YDOT = 21279
364009 feet/sec YDOT = 6516
219362 meter/sec
ZDOT = -9836
325183 ZDOT = -2984
962663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16333179
72 X = 4978353
18
Y = -765182
12 feet Y = -233227
51 meter
Z = -15185150
55 Z = -4628433
89
XDOT = -8128
603851 XDOT = -2477
598454
YDOT = 20474
282974 feet/sec YDOT = 6240
561450 meter/sec
ZDOT = -9776
187245 ZDOT = -2979
781872
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 20149
21940193
00016717 00000-0 10270-3 0 9136
2 25544 51
6430 87
3069 0001588 358
9628 1
1518 15
49379898 28916
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
21940193 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 87
3069 deg
Eccentricity:
0001588
Arg of perigee: 358
9628 deg
Mean anomaly: 1
1518 deg
Mean motion: 15
49379898 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 336
Coasting Arc #15 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2020/149/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1377828
11 A = 6802872
85 meter
Y = -6591516
56 meter E =
0012486
Z = 927676
08 I = 52
05121
XDOT = 4485
582340 Wp = 118
53064
YDOT = -1782
536798 meter/sec RA = 84
36074 deg
ZDOT = -5948
643438 TA = 51
50334
MA = 51
39143
Ha = 228
614 n
mi
Hp = 222
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4520433
43 X = -1308523
52
Y = -21625710
50 feet Y = -6606537
04 meter
Z = 3043556
70 Z = 921150
55
XDOT = 14716
477493 XDOT = 4534
076834
YDOT = -5848
217841 feet/sec YDOT = -1732
103838 meter/sec
ZDOT = -19516
546714 ZDOT = -5926
736765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17684554
09 X = -5390252
09
Y = 13249218
23 feet Y = 4038361
72 meter
Z = 3013913
27 Z = 918640
76
XDOT = -10606
996518 XDOT = -3233
012539
YDOT = -9699
871829 feet/sec YDOT = -2956
520934 meter/sec
ZDOT = -19415
619201 ZDOT = -5917
880733
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 20149
67089564
00016717 00000-0 10270-3 0 9143
2 25544 51
6442 85
0747 0001744 359
2656
8491 15
49359435 28984
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
67089564 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 85
0747 deg
Eccentricity:
0001744
Arg of perigee: 359
2656 deg
Mean anomaly:
8491 deg
Mean motion: 15
49359435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 341
Coasting Arc #16 (Orbit 2912)
---------------------------------------
Vector Time (GMT): 2020/150/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1854469
06 A = 6802819
94 meter
Y = 6488331
43 meter E =
0011780
Z = -812555
18 I = 52
04654
XDOT = -4367
241755 Wp = 33
62003
YDOT = 1989
747970 meter/sec RA = 79
43829 deg
ZDOT = 5971
912882 TA = 317
65959
MA = 317
75045
Ha = 228
585 n
mi
Hp = 222
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6084216
07 X = 1785723
70
Y = 21287176
60 feet Y = 6508685
14 meter
Z = -2665863
47 Z = -803713
12
XDOT = -14328
220982 XDOT = -4418
175180
YDOT = 6528
044521 feet/sec YDOT = 1940
624864 meter/sec
ZDOT = 19592
890033 ZDOT = 5950
575117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16466126
64 X = 5018875
40
Y = -14806805
84 feet Y = -4513114
42 meter
Z = -2625561
85 Z = -800271
25
XDOT = 11122
165992 XDOT = 3390
036194
YDOT = 8941
775905 feet/sec YDOT = 2725
453296 meter/sec
ZDOT = 19494
562527 ZDOT = 5941
942658
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 20150
63837857
00016717 00000-0 10270-3 0 9158
2 25544 51
6437 80
2860 0001909 359
5261
5887 15
49405956 29133
Satellite: ISS
Catalog Number: 25544
Epoch time: 20150
63837857 = yrday
fracday
Element set: 915
Inclination: 51
6437 deg
RA of node: 80
2860 deg
Eccentricity:
0001909
Arg of perigee: 359
5261 deg
Mean anomaly:
5887 deg
Mean motion: 15
49405956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2913
Checksum: 325
Coasting Arc #17 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2020/151/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2297035
61 A = 6803060
25 meter
Y = -6363972
86 meter E =
0012228
Z = 659775
11 I = 52
03944
XDOT = 4252
205639 Wp = 120
96612
YDOT = -2163
993609 meter/sec RA = 74
51653 deg
ZDOT = -5992
972538 TA = 51
96290
MA = 51
85260
Ha = 228
680 n
mi
Hp = 222
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7536206
07 X = -2228905
86
Y = -20879176
07 feet Y = -6389279
08 meter
Z = 2164616
49 Z = 648781
83
XDOT = 13950
805902 XDOT = 4305
198448
YDOT = -7099
716564 feet/sec YDOT = -2116
145507 meter/sec
ZDOT = -19661
983394 ZDOT = -5972
188502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15188774
65 X = -4629538
51
Y = 16194144
76 feet Y = 4935975
32 meter
Z = 2114417
08 Z = 644474
33
XDOT = -11532
390899 XDOT = -3515
072746
YDOT = -8228
429001 feet/sec YDOT = -2508
025159 meter/sec
ZDOT = -19566
189638 ZDOT = -5963
774602
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 20151
67036241
00016717 00000-0 10270-3 0 9162
2 25544 51
6436 75
1787 0001774 4
8848 355
2319 15
49356882 29294
Satellite: ISS
Catalog Number: 25544
Epoch time: 20151
67036241 = yrday
fracday
Element set: 916
Inclination: 51
6436 deg
RA of node: 75
1787 deg
Eccentricity:
0001774
Arg of perigee: 4
8848 deg
Mean anomaly: 355
2319 deg
Mean motion: 15
49356882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2929
Checksum: 330
Coasting Arc #18 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2020/152/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2709960
65 A = 6792946
98 meter
Y = 3816312
92 meter E =
0006222
Z = 4918429
80 I = 51
99711
XDOT = -4133
928537 Wp = 105
16029
YDOT = -6000
763171 meter/sec RA = 70
18674 deg
ZDOT = 2374
321680 TA = 321
66615
MA = 321
71036
Ha = 228
738 n
mi
Hp = 222
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8890947
02 X = -2776325
38
Y = 12520711
69 feet Y = 3785636
69 meter
Z = 16136580
71 Z = 4905105
00
XDOT = -13562
757668 XDOT = -4078
052112
YDOT = -19687
543211 feet/sec YDOT = -6046
679500 meter/sec
ZDOT = 7789
769290 ZDOT = 2354
375759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9985684
35 X = 3043636
59
Y = 11751024
61 feet Y = 3581712
30 meter
Z = 16075009
35 Z = 4899662
85
XDOT = -21529
614158 XDOT = -6562
226395
YDOT = 7745
772947 feet/sec YDOT = 2360
911594 meter/sec
ZDOT = 7698
353905 ZDOT = 2346
458270
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 20152
57334520
00016717 00000-0 10270-3 0 9174
2 25544 51
6432 70
7083 0001861 6
7131 353
4044 15
49408990 29432
Satellite: ISS
Catalog Number: 25544
Epoch time: 20152
57334520 = yrday
fracday
Element set: 917
Inclination: 51
6432 deg
RA of node: 70
7083 deg
Eccentricity:
0001861
Arg of perigee: 6
7131 deg
Mean anomaly: 353
4044 deg
Mean motion: 15
49408990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 290
Coasting Arc #19 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2020/153/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2484856
74 A = 6792705
39 meter
Y = -3909936
17 meter E =
0013429
Z = -4980224
13 I = 51
98512
XDOT = 4554
918496 Wp = 65
98604
YDOT = 5729
402385 meter/sec RA = 65
26089 deg
ZDOT = -2224
882065 TA = 182
34785
MA = 182
35416
Ha = 228
706 n
mi
Hp = 221
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8152417
13 X = 2552585
40
Y = -12827874
57 feet Y = -3881769
56 meter
Z = -16339318
00 Z = -4967989
44
XDOT = 14943
958319 XDOT = 4501
319372
YDOT = 18797
251919 feet/sec YDOT = 5780
039248 meter/sec
ZDOT = -7299
481839 ZDOT = -2202
885514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10650878
90 X = -3246387
89
Y = -10927964
12 feet Y = -3330843
46 meter
Z = -16282750
47 Z = -4962982
34
XDOT = 20881
675234 XDOT = 6364
734611
YDOT = -9623
375458 feet/sec YDOT = -2933
204839 meter/sec
ZDOT = -7198
626523 ZDOT = -2194
141364
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 20153
54082593
00016717 00000-0 10270-3 0 9183
2 25544 51
6445 65
9199 0002054 12
2599 347
8601 15
49417110 29581
Satellite: ISS
Catalog Number: 25544
Epoch time: 20153
54082593 = yrday
fracday
Element set: 918
Inclination: 51
6445 deg
RA of node: 65
9199 deg
Eccentricity:
0002054
Arg of perigee: 12
2599 deg
Mean anomaly: 347
8601 deg
Mean motion: 15
49417110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 318
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