[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 2nd 2020
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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) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 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
277/01:16:14
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
7
277/05:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
5
279/10:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 222
6
280/09:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 222
6
281/08:14:31
819 -2
2 -2
4 2
4
N/A 0
8 0
2 228
3
000/00:07:03
639 0
1 -0
0 222
7
283/20:35:00
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
7
288/05:45:05
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
6
288/08:50:45
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
7
289/02:17:30
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
6
291/11:10:00
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
7
Coasting Arc #1 (Orbit 864)
---------------------------------------
Vector Time (GMT): 2020/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2478315
35 A = 6794154
35 meter
Y = -3828479
62 meter E =
0007112
Z = 5031822
93 I = 51
64989
XDOT = 7125
387748 Wp = 121
14153
YDOT = -2021
353075 meter/sec RA = 176
28421 deg
ZDOT = 1965
848026 TA = 309
73316
MA = 309
79581
Ha = 229
853 n
mi
Hp = 222
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8130955
87 X = -2459761
97
Y = -12560628
66 feet Y = -3856089
71 meter
Z = 16508605
41 Z = 5019829
52
XDOT = 23377
256390 XDOT = 7137
912465
YDOT = -6631
735809 feet/sec YDOT = -1941
601662 meter/sec
ZDOT = 6449
632631 ZDOT = 2000
491412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10443809
36 X = 3183273
09
Y = 10799798
88 feet Y = 3291778
70 meter
Z = 16453178
37 Z = 5014928
77
XDOT = -20896
565503 XDOT = -6369
273165
YDOT = 10109
754774 feet/sec YDOT = 3081
453255 meter/sec
ZDOT = 6609
677261 ZDOT = 2014
629629
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 20276
55192314
00016717 00000-0 10270-3 0 9004
2 25544 51
6436 177
2276 0001220 106
8798 253
2485 15
48833362 8654
Satellite: ISS
Catalog Number: 25544
Epoch time: 20276
55192314 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 177
2276 deg
Eccentricity:
0001220
Arg of perigee: 106
8798 deg
Mean anomaly: 253
2485 deg
Mean motion: 15
48833362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 865
Checksum: 312
Coasting Arc #2 (Orbit 872)
---------------------------------------
Vector Time (GMT): 2020/277/01:16:14
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -235944
96 A = 6793020
64 meter
Y = 4250602
83 meter E =
0015710
Z = -5307251
58 I = 51
66338
XDOT = -7613
573212 Wp = 96
89476
YDOT = 363
024566 meter/sec RA = 173
52856 deg
ZDOT = 628
989814 TA = 179
12505
MA = 179
12230
Ha = 229
767 n
mi
Hp = 222
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -774097
63 X = -257678
96
Y = 13945547
36 feet Y = 4247842
33 meter
Z = -17412242
70 Z = -5308450
89
XDOT = -24978
914739 XDOT = -7620
122122
YDOT = 1191
025478 feet/sec YDOT = 277
847567 meter/sec
ZDOT = 2063
614876 ZDOT = 591
989570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6483895
98 X = 1976291
49
Y = 12363018
65 feet Y = 3768248
09 meter
Z = -17417766
13 Z = -5308935
12
XDOT = -20060
556093 XDOT = -6114
457497
YDOT = 13188
525947 feet/sec YDOT = 4019
862709 meter/sec
ZDOT = 1892
663809 ZDOT = 576
883929
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 20277
06810324
00016717 00000-0 10270-3 0 9010
2 25544 51
6424 174
6735 0001171 121
3529 238
7736 15
48802735 8737
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
06810324 = yrday
fracday
Element set: 901
Inclination: 51
6424 deg
RA of node: 174
6735 deg
Eccentricity:
0001171
Arg of perigee: 121
3529 deg
Mean anomaly: 238
7736 deg
Mean motion: 15
48802735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 873
Checksum: 301
Coasting Arc #3 (Orbit 875)
---------------------------------------
Vector Time (GMT): 2020/277/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1755852
08 A = 6794201
13 meter
Y = 4236610
89 meter E =
0014104
Z = -5025857
22 I = 51
67198
XDOT = -7348
356273 Wp = 105
50266
YDOT = -649
929762 meter/sec RA = 172
54985 deg
ZDOT = 2020
445547 TA = 184
16915
MA = 184
18091
Ha = 229
845 n
mi
Hp = 222
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5760669
55 X = -1778683
51
Y = 13899642
03 feet Y = 4216847
60 meter
Z = -16489032
88 Z = -5034442
42
XDOT = -24108
780423 XDOT = -7350
356739
YDOT = -2132
315491 feet/sec YDOT = -732
115363 meter/sec
ZDOT = 6628
758355 ZDOT = 1984
744750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14727404
53 X = 4488912
90
Y = 2860029
24 feet Y = 871736
91 meter
Z = -16528682
83 Z = -5037942
53
XDOT = 2776
710056 XDOT = 846
341225
YDOT = 23037
143910 feet/sec YDOT = 7021
721464 meter/sec
ZDOT = 6463
803429 ZDOT = 1970
167285
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 20277
26167090
00016717 00000-0 10270-3 0 9028
2 25544 51
6405 173
7171 0001295 108
7630 251
3661 15
48800636 8768
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
26167090 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 173
7171 deg
Eccentricity:
0001295
Arg of perigee: 108
7630 deg
Mean anomaly: 251
3661 deg
Mean motion: 15
48800636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 876
Checksum: 300
Coasting Arc #4 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2020/278/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1327102
95 A = 6794046
74 meter
Y = -4360922
84 meter E =
0006477
Z = 5033607
07 I = 51
70508
XDOT = 7404
433207 Wp = 65
19175
YDOT = -30
732893 meter/sec RA = 167
60931 deg
ZDOT = -1974
144772 TA = 43
99619
MA = 43
94466
Ha = 229
731 n
mi
Hp = 222
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4354012
32 X = 1351318
63
Y = -14307489
62 feet Y = -4345946
45 meter
Z = 16514458
90 Z = 5040112
88
XDOT = 24292
759865 XDOT = 7413
816004
YDOT = -100
829700 feet/sec YDOT = 52
121108 meter/sec
ZDOT = -6476
852926 ZDOT = -1938
153464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14878063
03 X = -4534833
61
Y = -1145220
69 feet Y = -349063
27 meter
Z = 16544508
01 Z = 5042766
04
XDOT = -5287
850106 XDOT = -1611
736712
YDOT = -22688
797701 feet/sec YDOT = -6915
545539 meter/sec
ZDOT = -6310
539641 ZDOT = -1923
452483
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 20278
29402844
00016717 00000-0 10270-3 0 9032
2 25544 51
6404 168
6116 0001196 110
8616 249
2662 15
48829358 8924
Satellite: ISS
Catalog Number: 25544
Epoch time: 20278
29402844 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 168
6116 deg
Eccentricity:
0001196
Arg of perigee: 110
8616 deg
Mean anomaly: 249
2662 deg
Mean motion: 15
48829358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 320
Coasting Arc #5 (Orbit 906)
---------------------------------------
Vector Time (GMT): 2020/279/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -881171
74 A = 6794037
65 meter
Y = 4458257
43 meter E =
0014232
Z = -5063360
18 I = 51
73732
XDOT = -7370
235126 Wp = 104
81084
YDOT = 717
298895 meter/sec RA = 162
67140 deg
ZDOT = 1915
177917 TA = 183
78006
MA = 183
79082
Ha = 229
801 n
mi
Hp = 222
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2890983
40 X = -906364
40
Y = 14626828
82 feet Y = 4448262
38 meter
Z = -16612074
09 Z = -5067702
10
XDOT = -24180
561437 XDOT = -7387
011438
YDOT = 2353
342832 feet/sec YDOT = 634
785947 meter/sec
ZDOT = 6283
392116 ZDOT = 1879
334667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14874960
22 X = 4533887
87
Y = -608823
97 feet Y = -185569
55 meter
Z = -16632131
67 Z = -5069473
73
XDOT = 7736
319075 XDOT = 2358
030054
YDOT = 21975
059387 feet/sec YDOT = 6697
998101 meter/sec
ZDOT = 6117
744167 ZDOT = 1864
688422
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 20279
26186148
00016717 00000-0 10270-3 0 9047
2 25544 51
6401 163
8257 0001214 108
7110 251
4172 15
48810797 9075
Satellite: ISS
Catalog Number: 25544
Epoch time: 20279
26186148 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 163
8257 deg
Eccentricity:
0001214
Arg of perigee: 108
7110 deg
Mean anomaly: 251
4172 deg
Mean motion: 15
48810797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 907
Checksum: 296
Coasting Arc #6 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2020/279/10:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5836398
97 A = 6803822
04 meter
Y = -3149199
07 meter E =
0015024
Z = 1488139
97 I = 51
77815
XDOT = 3455
843982 Wp = 117
67153
YDOT = 3655
892684 meter/sec RA = 161
82835 deg
ZDOT = -5779
154498 TA = 46
14608
MA = 46
02203
Ha = 229
760 n
mi
Hp = 222
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19148290
58 X = 5863951
80
Y = -10332017
94 feet Y = -3083778
13 meter
Z = 4882348
99 Z = 1516558
60
XDOT = 11338
070807 XDOT = 3442
778261
YDOT = 11994
398570 feet/sec YDOT = 3694
465044 meter/sec
ZDOT = -18960
480636 ZDOT = -5762
398940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21146896
41 X = -6445574
02
Y = 4991664
46 feet Y = 1521459
33 meter
Z = 5013682
97 Z = 1528170
57
XDOT = -7580
433823 XDOT = -2310
516229
YDOT = -13026
203736 feet/sec YDOT = -3970
386899 meter/sec
ZDOT = -18883
036941 ZDOT = -5755
549660
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 20279
45542885
00016717 00000-0 10270-3 0 9053
2 25544 51
6427 162
8691 0001187 109
6530 250
4748 15
48820665 9106
Satellite: ISS
Catalog Number: 25544
Epoch time: 20279
45542885 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 162
8691 deg
Eccentricity:
0001187
Arg of perigee: 109
6530 deg
Mean anomaly: 250
4748 deg
Mean motion: 15
48820665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 323
Coasting Arc #7 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2020/280/09:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538559
19 A = 6799256
15 meter
Y = 4574232
41 meter E =
0006440
Z = -3582205
85 I = 51
79462
XDOT = -6093
800110 Wp = 100
54963
YDOT = -1221
793379 meter/sec RA = 156
90333 deg
ZDOT = 4465
088739 TA = 217
37368
MA = 217
41849
Ha = 229
695 n
mi
Hp = 222
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11609446
15 X = -3572045
96
Y = 15007324
19 feet Y = 4534474
34 meter
Z = -11752643
85 Z = -3599476
64
XDOT = -19992
782514 XDOT = -6101
374050
YDOT = -4008
508461 feet/sec YDOT = -1289
980813 meter/sec
ZDOT = 14649
241269 ZDOT = 4435
468464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15170305
51 X = 4623909
12
Y = -11312740
33 feet Y = -3448123
25 meter
Z = -11832472
00 Z = -3606537
46
XDOT = 17424
564376 XDOT = 5311
007222
YDOT = 8206
534582 feet/sec YDOT = 2501
351740 meter/sec
ZDOT = 14512
330102 ZDOT = 4423
358215
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 20280
42325970
00016717 00000-0 10270-3 0 9067
2 25544 51
6425 158
0831 0001129 112
7163 247
4106 15
48845256 9253
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42325970 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 158
0831 deg
Eccentricity:
0001129
Arg of perigee: 112
7163 deg
Mean anomaly: 247
4106 deg
Mean motion: 15
48845256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 294
Coasting Arc #8 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2020/281/08:18:03
639
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 40554
22 A = 6792610
64 meter
Y = -4522189
09 meter E =
0004558
Z = 5066008
38 I = 51
80428
XDOT = 7133
440710 Wp = 51
92103
YDOT = -2060
216039 meter/sec RA = 152
32351 deg
ZDOT = -1892
263454 TA = 56
41526
MA = 56
37176
Ha = 228
278 n
mi
Hp = 222
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 133051
90 X = 66511
43
Y = -14836578
39 feet Y = -4521590
35 meter
Z = 16620762
40 Z = 5066268
51
XDOT = 23403
676870 XDOT = 7165
140208
YDOT = -6759
238974 feet/sec YDOT = -1980
267583 meter/sec
ZDOT = -6208
213433 ZDOT = -1857
534270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9540720
95 X = -2908011
75
Y = 11361172
25 feet Y = 3462885
30 meter
Z = 16621970
78 Z = 5066376
69
XDOT = -21485
866716 XDOT = -6548
892175
YDOT = -9176
333917 feet/sec YDOT = -2796
946578 meter/sec
ZDOT = -6047
664715 ZDOT = -1843
328205
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 20281
39107118
00016717 00000-0 10270-3 0 9077
2 25544 51
6416 153
2964 0001025 254
7550 105
3487 15
49285966 9407
Satellite: ISS
Catalog Number: 25544
Epoch time: 20281
39107118 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 153
2964 deg
Eccentricity:
0001025
Arg of perigee: 254
7550 deg
Mean anomaly: 105
3487 deg
Mean motion: 15
49285966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 308
Coasting Arc #9 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2020/282/08:18:03
639
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 234264
59 A = 6792733
99 meter
Y = 4556125
90 meter E =
0011965
Z = -5043652
31 I = 51
83483
XDOT = -6925
248414 Wp = 106
70441
YDOT = 2567
071697 meter/sec RA = 147
38646 deg
ZDOT = 1997
855028 TA = 182
68942
MA = 182
69586
Ha = 228
262 n
mi
Hp = 222
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 768584
60 X = 207798
80
Y = 14947919
61 feet Y = 4558597
60 meter
Z = -16547415
72 Z = -5042578
64
XDOT = -22720
631279 XDOT = -6963
144086
YDOT = 8422
151237 feet/sec YDOT = 2489
416729 meter/sec
ZDOT = 6554
642479 ZDOT = 1964
122245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8713218
36 X = 2655788
96
Y = -12176808
91 feet Y = -3711491
35 meter
Z = -16542464
76 Z = -5042143
26
XDOT = 22109
304498 XDOT = 6738
916011
YDOT = 7130
346160 feet/sec YDOT = 2173
329510 meter/sec
ZDOT = 6398
672652 ZDOT = 1950
315424
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 20282
35861715
00016717 00000-0 10270-3 0 9085
2 25544 51
6423 148
5075 0000974 262
1100 97
9940 15
49292243 9553
Satellite: ISS
Catalog Number: 25544
Epoch time: 20282
35861715 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 148
5075 deg
Eccentricity:
0000974
Arg of perigee: 262
1100 deg
Mean anomaly: 97
9940 deg
Mean motion: 15
49292243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 312
Coasting Arc #10 (Orbit 970)
---------------------------------------
Vector Time (GMT): 2020/283/08:18:03
639
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -501335
82 A = 6792852
48 meter
Y = -4566943
80 meter E =
0005294
Z = 5000938
76 I = 51
86301
XDOT = 6700
680400 Wp = 51
51603
YDOT = -3056
273964 meter/sec RA = 142
45335 deg
ZDOT = -2114
587017 TA = 59
05047
MA = 58
99845
Ha = 228
276 n
mi
Hp = 222
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1644802
56 X = -474521
65
Y = -14983411
42 feet Y = -4572400
16 meter
Z = 16407279
41 Z = 4998568
57
XDOT = 21983
859581 XDOT = 6744
630160
YDOT = -10027
145550 feet/sec YDOT = -2981
096415 meter/sec
ZDOT = -6937
621447 ZDOT = -2081
930542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7834391
02 X = -2387922
38
Y = 12891438
38 feet Y = 3929310
42 meter
Z = 16396339
37 Z = 4997604
24
XDOT = -22596
304481 XDOT = -6887
353606
YDOT = -5080
786324 feet/sec YDOT = -1548
623671 meter/sec
ZDOT = -6786
599949 ZDOT = -2068
555665
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 20283
39066419
00016717 00000-0 10270-3 0 9099
2 25544 51
6421 143
4013 0000960 270
3844 89
7196 15
49303279 9710
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
39066419 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 143
4013 deg
Eccentricity:
0000960
Arg of perigee: 270
3844 deg
Mean anomaly: 89
7196 deg
Mean motion: 15
49303279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 971
Checksum: 313
Coasting Arc #11 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2020/283/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2989718
20 A = 6791413
26 meter
Y = -2954888
01 meter E =
0001841
Z = 5333081
53 I = 51
87321
XDOT = 5682
255105 Wp = 132
90806
YDOT = -5128
488472 meter/sec RA = 139
94574 deg
ZDOT = 342
639549 TA = 313
82544
MA = 313
84065
Ha = 228
265 n
mi
Hp = 222
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9808786
74 X = -2982358
91
Y = -9694514
45 feet Y = -2988280
02 meter
Z = 17496986
63 Z = 5318576
36
XDOT = 18642
569242 XDOT = 5737
516725
YDOT = -16825
749579 feet/sec YDOT = -5064
636432 meter/sec
ZDOT = 1124
145501 ZDOT = 370
376275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2990907
61 X = -911628
64
Y = -13549638
62 feet Y = -4129929
85 meter
Z = 17429922
95 Z = 5312640
51
XDOT = 23820
219770 XDOT = 7260
402986
YDOT = -3641
410668 feet/sec YDOT = -1109
901972 meter/sec
ZDOT = 1252
439458 ZDOT = 381
743547
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 20283
90668532
00016717 00000-0 10270-3 0 9102
2 25544 51
6434 140
8445 0001248 247
5311 112
5707 15
49326281 9798
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
90668532 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 140
8445 deg
Eccentricity:
0001248
Arg of perigee: 247
5311 deg
Mean anomaly: 112
5707 deg
Mean motion: 15
49326281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 979
Checksum: 304
Coasting Arc #12 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2020/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3142943
70 A = 6791517
39 meter
Y = 2787837
26 meter E =
0013572
Z = -5347878
01 I = 51
89762
XDOT = -5283
572761 Wp = 89
68429
YDOT = 5528
638741 meter/sec RA = 135
01480 deg
ZDOT = -223
501603 TA = 178
19061
MA = 178
18569
Ha = 228
184 n
mi
Hp = 222
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10311495
08 X = 3137512
82
Y = 9146447
69 feet Y = 2822953
49 meter
Z = -17545531
53 Z = -5332623
91
XDOT = -17334
556303 XDOT = -5343
917328
YDOT = 18138
578546 feet/sec YDOT = 5469
216631 meter/sec
ZDOT = -733
272977 ZDOT = -249
313970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3941429
45 X = 1201347
70
Y = 13301116
67 feet Y = 4054180
36 meter
Z = -17474997
63 Z = -5326379
28
XDOT = -23364
950847 XDOT = -7121
637018
YDOT = 5805
116135 feet/sec YDOT = 1769
399398 meter/sec
ZDOT = -852
693129 ZDOT = -259
900866
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 20284
87422859
00016717 00000-0 10270-3 0 9110
2 25544 51
6428 136
0574 0001272 253
5128 106
5882 15
49285487 9947
Satellite: ISS
Catalog Number: 25544
Epoch time: 20284
87422859 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 136
0574 deg
Eccentricity:
0001272
Arg of perigee: 253
5128 deg
Mean anomaly: 106
5882 deg
Mean motion: 15
49285487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 331
Coasting Arc #13 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2020/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3280212
12 A = 6791359
45 meter
Y = -2605460
92 meter E =
0001273
Z = 5344505
25 I = 51
92160
XDOT = 4869
900504 Wp = 114
38434
YDOT = -5914
290558 meter/sec RA = 130
08464 deg
ZDOT = 105
157441 TA = 334
61350
MA = 334
61976
Ha = 228
223 n
mi
Hp = 222
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10761850
78 X = -3276793
99
Y = -8548100
12 feet Y = -2642123
35 meter
Z = 17534466
06 Z = 5328579
54
XDOT = 15977
363859 XDOT = 4935
163145
YDOT = -19403
840413 feet/sec YDOT = -5859
466928 meter/sec
ZDOT = 345
004727 ZDOT = 128
972324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4865070
73 X = -1482873
56
Y = -12953603
40 feet Y = -3948258
32 meter
Z = 17460818
81 Z = 5322057
57
XDOT = 22780
800050 XDOT = 6943
587855
YDOT = -7939
977506 feet/sec YDOT = -2420
105144 meter/sec
ZDOT = 455
209031 ZDOT = 138
747713
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 20285
90626974
00016717 00000-0 10270-3 0 9120
2 25544 51
6437 130
9500 0001285 259
4381 100
6625 15
49330272 10102
Satellite: ISS
Catalog Number: 25544
Epoch time: 20285
90626974 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 130
9500 deg
Eccentricity:
0001285
Arg of perigee: 259
4381 deg
Mean anomaly: 100
6625 deg
Mean motion: 15
49330272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1010
Checksum: 286
Coasting Arc #14 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2020/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3417290
87 A = 6791484
83 meter
Y = 2428742
25 meter E =
0013636
Z = -5354762
28 I = 51
94147
XDOT = -4415
451293 Wp = 90
22166
YDOT = 6247
793523 meter/sec RA = 125
15626 deg
ZDOT = 15
931963 TA = 179
92997
MA = 179
92978
Ha = 228
181 n
mi
Hp = 222
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11211584
22 X = 3415888
49
Y = 7968314
47 feet Y = 2466948
76 meter
Z = -17568117
71 Z = -5338165
83
XDOT = -14486
388757 XDOT = -4485
065228
YDOT = 20498
010247 feet/sec YDOT = 6198
027543 meter/sec
ZDOT = 52
270221 ZDOT = -5
686067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5768084
03 X = 1758112
01
Y = 12594200
73 feet Y = 3838712
38 meter
Z = -17491361
60 Z = -5331367
02
XDOT = -21927
359211 XDOT = -6683
459087
YDOT = 9976
324892 feet/sec YDOT = 3040
783827 meter/sec
ZDOT = -47
791987 ZDOT = -14
566998
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 20286
87380778
00016717 00000-0 10270-3 0 9137
2 25544 51
6428 126
1624 0001198 269
4238 90
6775 15
49289019 10253
Satellite: ISS
Catalog Number: 25544
Epoch time: 20286
87380778 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 126
1624 deg
Eccentricity:
0001198
Arg of perigee: 269
4238 deg
Mean anomaly: 90
6775 deg
Mean motion: 15
49289019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 334
Coasting Arc #15 (Orbit 1040)
---------------------------------------
Vector Time (GMT): 2020/287/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3536464
98 A = 6791356
01 meter
Y = -2240022
95 meter E =
0001256
Z = 5346676
55 I = 51
95975
XDOT = 3949
498724 Wp = 78
10799
YDOT = -6564
240396 meter/sec RA = 120
22923 deg
ZDOT = -137
523422 TA = 13
19952
MA = 13
19623
Ha = 228
255 n
mi
Hp = 222
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11602575
40 X = -3537124
84
Y = -7349156
67 feet Y = -2279573
57 meter
Z = 17541589
72 Z = 5329496
20
XDOT = 12957
672980 XDOT = 4023
276521
YDOT = -21536
221772 feet/sec YDOT = -6519
661758 meter/sec
ZDOT = -451
192330 ZDOT = -118
158517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6627645
39 X = -2020106
31
Y = -12144367
08 feet Y = -3701603
09 meter
Z = 17462127
43 Z = 5322456
44
XDOT = 20955
145117 XDOT = 6387
128232
YDOT = -11957
189855 feet/sec YDOT = -3644
551468 meter/sec
ZDOT = -361
535140 ZDOT = -110
195911
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 20287
90584490
00016717 00000-0 10270-3 0 9140
2 25544 51
6426 121
0555 0001194 272
2496 87
8517 15
49330739 10418
Satellite: ISS
Catalog Number: 25544
Epoch time: 20287
90584490 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 121
0555 deg
Eccentricity:
0001194
Arg of perigee: 272
2496 deg
Mean anomaly: 87
8517 deg
Mean motion: 15
49330739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1041
Checksum: 312
Coasting Arc #16 (Orbit 1046)
---------------------------------------
Vector Time (GMT): 2020/288/05:45:05
000
Vector Time (MET): N/A
Weight (LBS) : 936818
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4739269
36 A = 6793804
43 meter
Y = 912324
77 meter E =
0006606
Z = 4777948
97 I = 51
97321
XDOT = 1386
642366 Wp = 119
44022
YDOT = -7031
122929 meter/sec RA = 118
37049 deg
ZDOT = 2711
998855 TA = 303
82908
MA = 303
89195
Ha = 228
315 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15548784
00 X = -4772327
78
Y = 2993191
49 feet Y = 859142
37 meter
Z = 15675685
60 Z = 4754846
88
XDOT = 4549
351595 XDOT = 1451
989981
YDOT = -23067
988611 feet/sec YDOT = -7015
250916 meter/sec
ZDOT = 8897
634040 ZDOT = 2718
893921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7831686
95 X = 2387098
18
Y = 13882665
37 feet Y = 4231436
41 meter
Z = 15568791
85 Z = 4745367
76
XDOT = -22281
847448 XDOT = -6791
507102
YDOT = 2533
659754 feet/sec YDOT = 772
259493 meter/sec
ZDOT = 8929
609048 ZDOT = 2721
744838
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 20288
29285995
00016717 00000-0 10270-3 0 9152
2 25544 51
6415 119
1417 0001133 287
5452 72
5574 15
49332728 10475
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
29285995 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 119
1417 deg
Eccentricity:
0001133
Arg of perigee: 287
5452 deg
Mean anomaly: 72
5574 deg
Mean motion: 15
49332728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1047
Checksum: 321
Coasting Arc #17 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2020/288/08:50:45
000
Vector Time (MET): N/A
Weight (LBS) : 951926
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4736358
60 A = 6793981
52 meter
Y = 1007158
29 meter E =
0006731
Z = 4761818
06 I = 51
97703
XDOT = 1272
739827 Wp = 117
70822
YDOT = -7038
497865 meter/sec RA = 117
73624 deg
ZDOT = 2748
617106 TA = 305
17298
MA = 305
23600
Ha = 228
416 n
mi
Hp = 222
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15539234
26 X = -4770399
36
Y = 3304325
09 feet Y = 954002
95 meter
Z = 15622762
66 Z = 4738727
70
XDOT = 4175
655599 XDOT = 1338
000496
YDOT = -23092
184596 feet/sec YDOT = -7023
900070 meter/sec
ZDOT = 9017
772659 ZDOT = 2754
958680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15585836
87 X = 4750563
08
Y = 3577003
99 feet Y = 1090270
82 meter
Z = 15515921
20 Z = 4729252
78
XDOT = -13177
517599 XDOT = -4016
507364
YDOT = 18087
516924 feet/sec YDOT = 5513
075159 meter/sec
ZDOT = 9047
188633 ZDOT = 2757
583095
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 20288
42186533
00016717 00000-0 10270-3 0 9166
2 25544 51
6431 118
5039 0001080 294
9168 65
1870 15
49294238 10495
Satellite: ISS
Catalog Number: 25544
Epoch time: 20288
42186533 = yrday
fracday
Element set: 916
Inclination: 51
6431 deg
RA of node: 118
5039 deg
Eccentricity:
0001080
Arg of perigee: 294
9168 deg
Mean anomaly: 65
1870 deg
Mean motion: 15
49294238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 315
Coasting Arc #18 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2020/289/02:17:30
000
Vector Time (MET): N/A
Weight (LBS) : 951926
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1305270
72 A = 6801911
82 meter
Y = -6413357
28 meter E =
0012812
Z = 1830045
57 I = 52
01124
XDOT = 5116
333540 Wp = 113
78974
YDOT = -585
076095 meter/sec RA = 114
11738 deg
ZDOT = -5673
284091 TA = 46
23109
MA = 46
12514
Ha = 228
225 n
mi
Hp = 222
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4282384
26 X = 1368000
37
Y = -21041198
42 feet Y = -6398409
91 meter
Z = 6004086
51 Z = 1836539
05
XDOT = 16785
871195 XDOT = 5150
053729
YDOT = -1919
540993 feet/sec YDOT = -527
673514 meter/sec
ZDOT = -18613
136781 ZDOT = -5648
348657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15480002
76 X = -4718304
84
Y = -14868683
41 feet Y = -4531974
70 meter
Z = 6034208
23 Z = 1839226
67
XDOT = 6369
945396 XDOT = 1941
559357
YDOT = -14173
696625 feet/sec YDOT = -4320
142731 meter/sec
ZDOT = -18497
758354 ZDOT = -5638
116746
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 20289
13138885
00016717 00000-0 10270-3 0 9173
2 25544 51
6395 114
9907 0001102 297
3799 62
7238 15
49322680 10607
Satellite: ISS
Catalog Number: 25544
Epoch time: 20289
13138885 = yrday
fracday
Element set: 917
Inclination: 51
6395 deg
RA of node: 114
9907 deg
Eccentricity:
0001102
Arg of perigee: 297
3799 deg
Mean anomaly: 62
7238 deg
Mean motion: 15
49322680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 324
Coasting Arc #19 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2020/290/02:17:30
000
Vector Time (MET): N/A
Weight (LBS) : 951926
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -829648
59 A = 6802047
90 meter
Y = 6519242
70 meter E =
0007465
Z = -1741971
27 I = 52
02486
XDOT = -5026
840526 Wp = 30
89359
YDOT = 881
601692 meter/sec RA = 109
19376 deg
ZDOT = 5710
535045 TA = 310
13867
MA = 310
20404
Ha = 228
273 n
mi
Hp = 222
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2721944
18 X = -894025
40
Y = 21388591
52 feet Y = 6509604
87 meter
Z = -5715128
84 Z = -1746158
36
XDOT = -16492
258945 XDOT = -5064
064319
YDOT = 2892
394002 feet/sec YDOT = 825
180291 meter/sec
ZDOT = 18735
351196 ZDOT = 5686
025658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16843242
40 X = 5133820
28
Y = 13452253
13 feet Y = 4100246
75 meter
Z = -5734596
45 Z = -1747905
00
XDOT = -5226
274701 XDOT = -1592
968529
YDOT = 14458
320320 feet/sec YDOT = 4406
896034 meter/sec
ZDOT = 18621
934087 ZDOT = 5675
965510
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 20290
09891931
00016717 00000-0 10270-3 0 9189
2 25544 51
6400 110
2025 0000998 301
7560 58
3492 15
49321201 10759
Satellite: ISS
Catalog Number: 25544
Epoch time: 20290
09891931 = yrday
fracday
Element set: 918
Inclination: 51
6400 deg
RA of node: 110
2025 deg
Eccentricity:
0000998
Arg of perigee: 301
7560 deg
Mean anomaly: 58
3492 deg
Mean motion: 15
49321201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 282
Coasting Arc #20 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2020/291/02:17:30
000
Vector Time (MET): N/A
Weight (LBS) : 951926
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 371431
02 A = 6802231
74 meter
Y = -6589831
87 meter E =
0012739
Z = 1620455
50 I = 52
03561
XDOT = 4925
438052 Wp = 115
52241
YDOT = -1145
094314 meter/sec RA = 104
27044 deg
ZDOT = -5755
830248 TA = 46
87412
MA = 46
76764
Ha = 228
275 n
mi
Hp = 222
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1218605
70 X = 437221
46
Y = -21620183
31 feet Y = -6585310
30 meter
Z = 5316455
05 Z = 1622420
04
XDOT = 16159
573662 XDOT = 4965
836004
YDOT = -3756
871110 feet/sec YDOT = -1089
789026 meter/sec
ZDOT = -18883
957508 ZDOT = -5731
805606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18032866
39 X = -5496417
68
Y = -11984786
30 feet Y = -3652962
86 meter
Z = 5325659
35 Z = 1623260
97
XDOT = 4149
281763 XDOT = 1264
701081
YDOT = -14628
672480 feet/sec YDOT = -4458
819372 meter/sec
ZDOT = -18772
772317 ZDOT = -5721
941002
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 20291
13094928
00016717 00000-0 10270-3 0 9197
2 25544 51
6402 105
0942 0001180 310
5665 49
5383 15
49320994 10916
Satellite: ISS
Catalog Number: 25544
Epoch time: 20291
13094928 = yrday
fracday
Element set: 919
Inclination: 51
6402 deg
RA of node: 105
0942 deg
Eccentricity:
0001180
Arg of perigee: 310
5665 deg
Mean anomaly: 49
5383 deg
Mean motion: 15
49320994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 297
Coasting Arc #21 (Orbit 1095)
---------------------------------------
Vector Time (GMT): 2020/291/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 951926
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4326427
52 A = 6793447
31 meter
Y = 1854601
66 meter E =
0005778
Z = 4895036
85 I = 52
00781
XDOT = -345
096617 Wp = 119
27801
YDOT = -7255
801385 meter/sec RA = 102
48159 deg
ZDOT = 2439
111278 TA = 306
87302
MA = 306
92598
Ha = 228
432 n
mi
Hp = 222
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14194316
03 X = -4370622
61
Y = 6084651
11 feet Y = 1805973
60 meter
Z = 16059832
17 Z = 4873912
75
XDOT = -1132
206750 XDOT = -275
782529
YDOT = -23805
122653 feet/sec YDOT = -7259
272808 meter/sec
ZDOT = 8002
333590 ZDOT = 2437
603646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12566593
18 X = 3830297
60
Y = -9149503
33 feet Y = -2788768
61 meter
Z = 15962052
52 Z = 4865233
61
XDOT = 5848
635686 XDOT = 1782
664157
YDOT = 22010
016043 feet/sec YDOT = 6708
652890 meter/sec
ZDOT = 7995
491702 ZDOT = 2437
025871
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 20291
51796025
00016717 00000-0 10270-3 0 9208
2 25544 51
6391 103
1772 0001221 305
7774 54
3262 15
49288341 10960
Satellite: ISS
Catalog Number: 25544
Epoch time: 20291
51796025 = yrday
fracday
Element set: 920
Inclination: 51
6391 deg
RA of node: 103
1772 deg
Eccentricity:
0001221
Arg of perigee: 305
7774 deg
Mean anomaly: 54
3262 deg
Mean motion: 15
49288341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1096
Checksum: 292
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