[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 7th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16388 0536 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
190/18:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 221
4
190/19:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 221
5
192/13:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
8
000/00:00:00
000 0
0 0
0 221
4
193/01:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 221
4
193/19:18:06
661 -1
2 -1
8 1
8
N/A -1
3 -0
0 228
5
000/00:04:13
321 0
0 -0
0 221
5
195/04:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 221
5
200/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
7
000/00:00:00
000 0
0 0
0 221
5
202/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 221
6
202/16:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 221
6
203/04:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 221
6
Coasting Arc #1 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2020/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1463878
83 A = 6803563
34 meter
Y = -6586557
76 meter E =
0015685
Z = 817826
19 I = 51
28844
XDOT = 4869
221714 Wp = 58
59949
YDOT = -339
411698 meter/sec RA = 251
89467 deg
ZDOT = 5906
065809 TA = 310
27127
MA = 310
40831
Ha = 229
796 n
mi
Hp = 221
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4802752
07 X = -1394089
63
Y = -21609441
46 feet Y = -6602537
83 meter
Z = 2683156
78 Z = 810883
66
XDOT = 15975
136858 XDOT = 4843
967512
YDOT = -1113
555439 feet/sec YDOT = -285
102886 meter/sec
ZDOT = 19376
856329 ZDOT = 5929
656721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19796419
07 X = -6033948
53
Y = 9914885
85 feet Y = 3022057
21 meter
Z = 2651518
21 Z = 808182
75
XDOT = -4196
290552 XDOT = -1279
029360
YDOT = -13656
998249 feet/sec YDOT = -4162
653066 meter/sec
ZDOT = 19485
397191 ZDOT = 5939
149064
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 20188
56294904
00016717 00000-0 10270-3 0 9005
2 25544 51
6419 252
5730 0002658 83
1073 277
0379 15
49151608 35019
Satellite: ISS
Catalog Number: 25544
Epoch time: 20188
56294904 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 252
5730 deg
Eccentricity:
0002658
Arg of perigee: 83
1073 deg
Mean anomaly: 277
0379 deg
Mean motion: 15
49151608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 308
Coasting Arc #2 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2020/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1952611
16 A = 6803381
63 meter
Y = 6448600
94 meter E =
0011831
Z = -912786
76 I = 51
29875
XDOT = -4854
105711 Wp = 130
41123
YDOT = 644
440590 meter/sec RA = 246
92275 deg
ZDOT = -5889
100037 TA = 59
49407
MA = 59
37731
Ha = 229
778 n
mi
Hp = 221
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6406204
59 X = 1884789
56
Y = 21156827
22 feet Y = 6470057
36 meter
Z = -2994707
22 Z = -903465
62
XDOT = -15925
543671 XDOT = -4832
346026
YDOT = 2114
306399 feet/sec YDOT = 590
281141 meter/sec
ZDOT = -19321
194348 ZDOT = -5912
625917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18769869
61 X = 5721056
26
Y = -11687437
49 feet Y = -3562330
95 meter
Z = -2952095
21 Z = -899798
62
XDOT = 5279
907563 XDOT = 1609
315825
YDOT = 13338
231222 feet/sec YDOT = 4065
492876 meter/sec
ZDOT = -19429
458523 ZDOT = -5922
098958
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 20189
53056154
00016717 00000-0 10270-3 0 9017
2 25544 51
6408 247
7858 0002721 87
9037 272
2424 15
49188923 35161
Satellite: ISS
Catalog Number: 25544
Epoch time: 20189
53056154 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 247
7858 deg
Eccentricity:
0002721
Arg of perigee: 87
9037 deg
Mean anomaly: 272
2424 deg
Mean motion: 15
49188923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 322
Coasting Arc #3 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2020/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2463877
63 A = 6803478
36 meter
Y = -6260977
24 meter E =
0015813
Z = 961016
45 I = 51
31225
XDOT = 4812
894324 Wp = 60
92215
YDOT = -981
277381 meter/sec RA = 241
95109 deg
ZDOT = 5880
400203 TA = 309
51437
MA = 309
65406
Ha = 229
842 n
mi
Hp = 221
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8083588
01 X = -2398350
36
Y = -20541263
92 feet Y = -6288163
83 meter
Z = 3152941
11 Z = 949206
44
XDOT = 15790
335710 XDOT = 4794
946574
YDOT = -3219
413979 feet/sec YDOT = -927
557333 meter/sec
ZDOT = 19292
651586 ZDOT = 5903
735121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17511732
73 X = -5337576
14
Y = 13452335
45 feet Y = 4100271
85 meter
Z = 3098845
60 Z = 944528
14
XDOT = -6428
381825 XDOT = -1959
370780
YDOT = -12887
950355 feet/sec YDOT = -3928
247268 meter/sec
ZDOT = 19400
058239 ZDOT = 5913
137751
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 20190
56268288
00016717 00000-0 10270-3 0 9026
2 25544 51
6401 242
6791 0002738 88
8359 271
3105 15
49146290 35324
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
56268288 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 242
6791 deg
Eccentricity:
0002738
Arg of perigee: 88
8359 deg
Mean anomaly: 271
3105 deg
Mean motion: 15
49146290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 314
Coasting Arc #4 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2020/190/18:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 965635
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 941913
08 A = 6796088
97 meter
Y = -5232146
07 meter E =
0012578
Z = 4224862
48 I = 51
29186
XDOT = 5516
157996 Wp = 102
82759
YDOT = 3913
967721 meter/sec RA = 240
64683 deg
ZDOT = 3605
474531 TA = 310
04528
MA = 310
15555
Ha = 229
646 n
mi
Hp = 221
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3090266
00 X = 979828
97
Y = -17165833
56 feet Y = -5221401
49 meter
Z = 13861097
39 Z = 4229529
22
XDOT = 18097
631219 XDOT = 5454
467924
YDOT = 12841
101446 feet/sec YDOT = 3975
307923 meter/sec
ZDOT = 11828
984681 ZDOT = 3632
119977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3618477
16 X = 1102911
84
Y = 17044673
92 feet Y = 5195216
61 meter
Z = 13882770
64 Z = 4231468
49
XDOT = -20261
953958 XDOT = -6175
843567
YDOT = -5464
502922 feet/sec YDOT = -1665
580491 meter/sec
ZDOT = 11951
438610 ZDOT = 3642
798488
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 20190
82071030
00016717 00000-0 10270-3 0 9033
2 25544 51
6395 241
4031 0002584 90
2289 269
9157 15
49216951 35364
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
82071030 = yrday
fracday
Element set: 903
Inclination: 51
6395 deg
RA of node: 241
4031 deg
Eccentricity:
0002584
Arg of perigee: 90
2289 deg
Mean anomaly: 269
9157 deg
Mean motion: 15
49216951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 301
Coasting Arc #5 (Orbit 3536)
---------------------------------------
Vector Time (GMT): 2020/190/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965635
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2478839
22 A = 6803195
21 meter
Y = -6221888
60 meter E =
0015966
Z = 1153919
45 I = 51
31655
XDOT = 4890
224141 Wp = 62
40808
YDOT = -855
648188 meter/sec RA = 240
34815 deg
ZDOT = 5836
499804 TA = 310
15465
MA = 310
29438
Ha = 229
744 n
mi
Hp = 221
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8132674
61 X = -2414684
93
Y = -20413020
34 feet Y = -6249250
19 meter
Z = 3785824
98 Z = 1142033
48
XDOT = 16044
042456 XDOT = 4871
079048
YDOT = -2807
244711 feet/sec YDOT = -801
070030 meter/sec
ZDOT = 19148
621404 ZDOT = 5860
207474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19816718
62 X = 6040135
83
Y = 9515187
99 feet Y = 2900229
30 meter
Z = 3731370
67 Z = 1137321
78
XDOT = -9127
725075 XDOT = -2782
130603
YDOT = 11386
058500 feet/sec YDOT = 3470
470631 meter/sec
ZDOT = 19257
740537 ZDOT = 5869
759316
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 20190
88521922
00016717 00000-0 10270-3 0 9040
2 25544 51
6398 241
0839 0002637 87
6215 272
5237 15
49185438 35372
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
88521922 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 241
0839 deg
Eccentricity:
0002637
Arg of perigee: 87
6215 deg
Mean anomaly: 272
5237 deg
Mean motion: 15
49185438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3537
Checksum: 326
Coasting Arc #6 (Orbit 3551)
---------------------------------------
Vector Time (GMT): 2020/191/19:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965635
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2932002
47 A = 6803096
98 meter
Y = 6006451
71 meter E =
0010874
Z = -1249624
71 I = 51
33519
XDOT = -4847
669340 Wp = 131
05754
YDOT = 1165
317174 meter/sec RA = 235
37754 deg
ZDOT = -5813
094057 TA = 62
55565
MA = 62
44510
Ha = 229
768 n
mi
Hp = 221
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9619430
69 X = 2870688
47
Y = 19706206
39 feet Y = 6038896
77 meter
Z = -4099818
61 Z = -1235530
70
XDOT = -15904
426970 XDOT = -4832
103853
YDOT = 3823
219076 feet/sec YDOT = 1111
194772 meter/sec
ZDOT = -19071
830895 ZDOT = -5836
603738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20569491
72 X = -6269581
08
Y = -7634783
41 feet Y = -2327081
98 meter
Z = -4035173
16 Z = -1229920
78
XDOT = 8241
845186 XDOT = 2512
114413
YDOT = -12138
703834 feet/sec YDOT = -3699
876928 meter/sec
ZDOT = -19180
056747 ZDOT = -5846
081296
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 20191
85282888
00016717 00000-0 10270-3 0 9054
2 25544 51
6410 236
2957 0002652 89
0475 271
0979 15
49184710 35521
Satellite: ISS
Catalog Number: 25544
Epoch time: 20191
85282888 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 236
2957 deg
Eccentricity:
0002652
Arg of perigee: 89
0475 deg
Mean anomaly: 271
0979 deg
Mean motion: 15
49184710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3552
Checksum: 329
Coasting Arc #7 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2020/192/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965635
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1228962
17 A = 6794001
50 meter
Y = 4658147
55 meter E =
0013953
Z = -4803732
94 I = 51
32009
XDOT = -5880
178654 Wp = 76
72999
YDOT = -4176
048222 meter/sec RA = 231
81332 deg
ZDOT = -2548
271831 TA = 168
02498
MA = 167
99177
Ha = 229
799 n
mi
Hp = 221
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4032028
13 X = -1257626
26
Y = 15282636
33 feet Y = 4644244
66 meter
Z = -15760278
66 Z = -4809771
78
XDOT = -19291
924718 XDOT = -5820
665985
YDOT = -13700
945610 feet/sec YDOT = -4241
471550 meter/sec
ZDOT = -8360
471887 ZDOT = -2576
690835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14952861
71 X = 4557632
25
Y = -5034531
02 feet Y = -1534525
06 meter
Z = -15788224
46 Z = -4812250
81
XDOT = -1377
844526 XDOT = -419
967012
YDOT = 22503
499235 feet/sec YDOT = 6859
066567 meter/sec
ZDOT = -8491
117204 ZDOT = -2588
092524
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 20192
56240710
00016717 00000-0 10270-3 0 9062
2 25544 51
6420 232
7843 0002792 95
9896 264
1572 15
49186630 35632
Satellite: ISS
Catalog Number: 25544
Epoch time: 20192
56240710 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 232
7843 deg
Eccentricity:
0002792
Arg of perigee: 95
9896 deg
Mean anomaly: 264
1572 deg
Mean motion: 15
49186630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 318
Coasting Arc #8 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2020/193/01:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965635
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5465882
59 A = 6800560
06 meter
Y = -3012989
88 meter E =
0007024
Z = -2703073
43 I = 51
34979
XDOT = 567
478403 Wp = 70
96427
YDOT = -5636
378428 meter/sec RA = 229
12972 deg
ZDOT = 5148
367380 TA = 258
44643
MA = 258
52529
Ha = 229
687 n
mi
Hp = 221
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17932685
66 X = -5418654
43
Y = -9885137
40 feet Y = -3073848
94 meter
Z = -8868351
16 Z = -2729509
73
XDOT = 1861
805783 XDOT = 605
456466
YDOT = -18492
055209 feet/sec YDOT = -5629
820650 meter/sec
ZDOT = 16890
969094 ZDOT = 5151
215596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5573143
24 X = -1698694
06
Y = -19648567
80 feet Y = -5988883
47 meter
Z = -8989920
27 Z = -2740127
70
XDOT = 12921
908081 XDOT = 3938
597583
YDOT = -11379
855100 feet/sec YDOT = -3468
579834 meter/sec
ZDOT = 16904
257425 ZDOT = 5152
417663
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 20193
07846403
00016717 00000-0 10270-3 0 9071
2 25544 51
6383 230
2292 0002578 95
9522 264
1922 15
49188654 35715
Satellite: ISS
Catalog Number: 25544
Epoch time: 20193
07846403 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 230
2292 deg
Eccentricity:
0002578
Arg of perigee: 95
9522 deg
Mean anomaly: 264
1922 deg
Mean motion: 15
49188654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 320
Coasting Arc #9 (Orbit 3582)
---------------------------------------
Vector Time (GMT): 2020/193/19:20:13
321
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3739188
74 A = 6791001
36 meter
Y = -2168967
73 meter E =
0004403
Z = 5234172
25 I = 51
34004
XDOT = 4764
624051 Wp = 69
15888
YDOT = 5928
379591 meter/sec RA = 225
50709 deg
ZDOT = -944
932112 TA = 29
93817
MA = 29
91300
Ha = 228
505 n
mi
Hp = 221
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12267679
59 X = 3737740
60
Y = -7116035
85 feet Y = -2127162
06 meter
Z = 17172481
14 Z = 5252331
80
XDOT = 15631
968671 XDOT = 4702
566905
YDOT = 19450
064274 feet/sec YDOT = 5981
314125 meter/sec
ZDOT = -3100
170972 ZDOT = -921
937877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4893015
01 X = -1491390
98
Y = 13202747
17 feet Y = 4024197
34 meter
Z = 17256126
70 Z = 5259667
42
XDOT = -23470
244548 XDOT = -7153
730538
YDOT = -4775
024482 feet/sec YDOT = -1455
427462 meter/sec
ZDOT = -2994
520035 ZDOT = -912
729707
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 20193
85253778
00016717 00000-0 10270-3 0 9085
2 25544 51
6405 226
4020 0001164 98
6459 261
4823 15
49544637 35835
Satellite: ISS
Catalog Number: 25544
Epoch time: 20193
85253778 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 226
4020 deg
Eccentricity:
0001164
Arg of perigee: 98
6459 deg
Mean anomaly: 261
4823 deg
Mean motion: 15
49544637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3583
Checksum: 324
Coasting Arc #10 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2020/194/19:20:13
321
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3700117
55 A = 6791213
94 meter
Y = 2319680
98 meter E =
0015394
Z = -5214482
51 I = 51
36589
XDOT = -5110
114809 Wp = 99
24424
YDOT = -5575
484726 meter/sec RA = 220
53589 deg
ZDOT = 1146
272363 TA = 181
81284
MA = 181
81842
Ha = 228
684 n
mi
Hp = 221
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12139493
27 X = -3700453
19
Y = 7610501
89 feet Y = 2278302
27 meter
Z = -17107882
26 Z = -5232456
65
XDOT = -16765
468535 XDOT = -5052
956163
YDOT = -18292
272724 feet/sec YDOT = -5632
310197 meter/sec
ZDOT = 3760
736098 ZDOT = 1121
587931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4247952
64 X = 1294775
96
Y = -13579469
71 feet Y = -4139022
37 meter
Z = -17190682
72 Z = -5239720
09
XDOT = 23646
529511 XDOT = 7207
462195
YDOT = 2781
958015 feet/sec YDOT = 847
940803 meter/sec
ZDOT = 3647
274397 ZDOT = 1111
689236
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 20194
81994023
00016717 00000-0 10270-3 0 9098
2 25544 51
6414 221
6124 0001204 102
8479 257
2805 15
49522020 35983
Satellite: ISS
Catalog Number: 25544
Epoch time: 20194
81994023 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 221
6124 deg
Eccentricity:
0001204
Arg of perigee: 102
8479 deg
Mean anomaly: 257
2805 deg
Mean motion: 15
49522020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3598
Checksum: 295
Coasting Arc #11 (Orbit 3603)
---------------------------------------
Vector Time (GMT): 2020/195/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2956497
05 A = 6799147
00 meter
Y = 5372890
41 meter E =
0006005
Z = -2936922
77 I = 51
40068
XDOT = -5789
222351 Wp = 117
37286
YDOT = 464
478533 meter/sec RA = 218
70184 deg
ZDOT = -4988
659658 TA = 96
17750
MA = 96
10909
Ha = 228
715 n
mi
Hp = 221
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9699793
48 X = 2910461
82
Y = 17627593
22 feet Y = 5405694
98 meter
Z = -9635573
39 Z = -2922672
64
XDOT = -18993
511650 XDOT = -5769
754180
YDOT = 1523
879701 feet/sec YDOT = 399
848685 meter/sec
ZDOT = -16366
993630 ZDOT = -5016
733864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8387885
17 X = 2556627
40
Y = 18322617
87 feet Y = 5584733
93 meter
Z = -9570128
92 Z = -2916975
30
XDOT = -17606
515879 XDOT = -5366
466040
YDOT = -537
865789 feet/sec YDOT = -163
941492 meter/sec
ZDOT = -16496
235672 ZDOT = -5028
052633
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 20195
20689982
00016717 00000-0 10270-3 0 9109
2 25544 51
6400 219
6919 0001433 124
0474 236
0812 15
49527919 36045
Satellite: ISS
Catalog Number: 25544
Epoch time: 20195
20689982 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 219
6919 deg
Eccentricity:
0001433
Arg of perigee: 124
0474 deg
Mean anomaly: 236
0812 deg
Mean motion: 15
49527919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3604
Checksum: 308
Coasting Arc #12 (Orbit 3619)
---------------------------------------
Vector Time (GMT): 2020/196/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3245820
98 A = 6798719
08 meter
Y = -5114993
76 meter E =
0014096
Z = 3073381
97 I = 51
42763
XDOT = 5856
285858 Wp = 88
42225
YDOT = -771
155147 meter/sec RA = 213
73612 deg
ZDOT = 4882
374076 TA = 306
93663
MA = 307
06566
Ha = 228
664 n
mi
Hp = 221
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10649018
98 X = -3203311
00
Y = -16781475
59 feet Y = -5151053
51 meter
Z = 10083274
19 Z = 3057717
81
XDOT = 19213
536280 XDOT = 5840
758263
YDOT = -2530
036573 feet/sec YDOT = -705
753356 meter/sec
ZDOT = 16018
287651 ZDOT = 4910
783649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9702620
00 X = -2957358
57
Y = -17387495
67 feet Y = -5299708
68 meter
Z = 10011298
94 Z = 3051443
92
XDOT = 17952
358068 XDOT = 5471
878739
YDOT = -683
290248 feet/sec YDOT = -208
266868 meter/sec
ZDOT = 16149
095551 ZDOT = 4922
244324
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 20196
23879042
00016717 00000-0 10270-3 0 9112
2 25544 51
6411 214
5836 0001444 129
3320 230
7959 15
49559625 36209
Satellite: ISS
Catalog Number: 25544
Epoch time: 20196
23879042 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 214
5836 deg
Eccentricity:
0001444
Arg of perigee: 129
3320 deg
Mean anomaly: 230
7959 deg
Mean motion: 15
49559625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3620
Checksum: 305
Coasting Arc #13 (Orbit 3634)
---------------------------------------
Vector Time (GMT): 2020/197/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3481586
52 A = 6798373
71 meter
Y = 4858593
88 meter E =
0005904
Z = -3241861
67 I = 51
45416
XDOT = -5908
601632 Wp = 106
97378
YDOT = 1071
568376 meter/sec RA = 208
77258 deg
ZDOT = -4748
434614 TA = 110
58546
MA = 110
52211
Ha = 228
714 n
mi
Hp = 221
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11422527
96 X = 3442744
55
Y = 15940268
64 feet Y = 4897310
71 meter
Z = -10636029
11 Z = -3225043
28
XDOT = -19385
175957 XDOT = -5897
080028
YDOT = 3515
644278 feet/sec YDOT = 1005
559214 meter/sec
ZDOT = -15578
853722 ZDOT = -4777
108029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10812323
76 X = 3295596
28
Y = 16410317
93 feet Y = 5001864
91 meter
Z = -10558718
91 Z = -3218297
52
XDOT = -18212
889881 XDOT = -5551
288836
YDOT = 1910
165796 feet/sec YDOT = 582
218535 meter/sec
ZDOT = -15710
899869 ZDOT = -4788
682280
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 20197
20618955
00016717 00000-0 10270-3 0 9125
2 25544 51
6403 209
7950 0001470 128
4214 231
7068 15
49526437 36357
Satellite: ISS
Catalog Number: 25544
Epoch time: 20197
20618955 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 209
7950 deg
Eccentricity:
0001470
Arg of perigee: 128
4214 deg
Mean anomaly: 231
7068 deg
Mean motion: 15
49526437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3635
Checksum: 306
Coasting Arc #14 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2020/198/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3720151
36 A = 6797912
20 meter
Y = -4574933
55 meter E =
0013560
Z = 3371802
38 I = 51
48343
XDOT = 5942
014321 Wp = 93
78984
YDOT = -1406
395149 meter/sec RA = 203
81075 deg
ZDOT = 4630
660743 TA = 305
58807
MA = 305
71436
Ha = 228
643 n
mi
Hp = 221
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12205220
99 X = -3685094
79
Y = -15009624
52 feet Y = -4616339
42 meter
Z = 11062343
76 Z = 3353815
90
XDOT = 19494
797642 XDOT = 5934
806452
YDOT = -4614
157313 feet/sec YDOT = -1339
988292 meter/sec
ZDOT = 15192
456505 ZDOT = 4659
506860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11901594
83 X = -3627606
10
Y = -15311152
74 feet Y = -4666839
35 meter
Z = 10979632
94 Z = 3346592
12
XDOT = 18383
409896 XDOT = 5603
263336
YDOT = -3259
590809 feet/sec YDOT = -993
523279 meter/sec
ZDOT = 15325
324275 ZDOT = 4671
158839
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 20198
23807827
00016717 00000-0 10270-3 0 9138
2 25544 51
6407 204
6868 0001461 136
4537 223
6729 15
49562854 36515
Satellite: ISS
Catalog Number: 25544
Epoch time: 20198
23807827 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 204
6868 deg
Eccentricity:
0001461
Arg of perigee: 136
4537 deg
Mean anomaly: 223
6729 deg
Mean motion: 15
49562854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 327
Coasting Arc #15 (Orbit 3665)
---------------------------------------
Vector Time (GMT): 2020/199/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3906612
21 A = 6797552
44 meter
Y = 4301204
79 meter E =
0006082
Z = -3532204
23 I = 51
51378
XDOT = -5956
741442 Wp = 97
18840
YDOT = 1733
663267 meter/sec RA = 198
85081 deg
ZDOT = -4484
444788 TA = 124
38783
MA = 124
33029
Ha = 228
660 n
mi
Hp = 221
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12816969
21 X = 3875381
81
Y = 14111564
28 feet Y = 4344717
27 meter
Z = -11588596
56 Z = -3513302
73
XDOT = -19543
114966 XDOT = -5953
902363
YDOT = 5687
871611 feet/sec YDOT = 1667
067342 meter/sec
ZDOT = -14712
745366 ZDOT = -4513
372919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12785505
45 X = 3897022
06
Y = 14210891
68 feet Y = 4331479
79 meter
Z = -11501648
77 Z = -3505702
54
XDOT = -18449
697125 XDOT = -5623
467684
YDOT = 4603
253785 feet/sec YDOT = 1403
071754 meter/sec
ZDOT = -14846
018964 ZDOT = -4525
066580
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 20199
20547494
00016717 00000-0 10270-3 0 9148
2 25544 51
6412 199
8979 0001430 136
5296 223
5967 15
49529421 36660
Satellite: ISS
Catalog Number: 25544
Epoch time: 20199
20547494 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 199
8979 deg
Eccentricity:
0001430
Arg of perigee: 136
5296 deg
Mean anomaly: 223
5967 deg
Mean motion: 15
49529421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3666
Checksum: 342
Coasting Arc #16 (Orbit 3681)
---------------------------------------
Vector Time (GMT): 2020/200/04:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4091700
16 A = 6797065
99 meter
Y = -4002921
22 meter E =
0012991
Z = 3655960
04 I = 51
54516
XDOT = 5949
623565 Wp = 98
56940
YDOT = -2090
706082 meter/sec RA = 193
89280 deg
ZDOT = 4354
450407 TA = 304
85238
MA = 304
97447
Ha = 228
638 n
mi
Hp = 221
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13424213
12 X = -4064392
56
Y = -13132943
62 feet Y = -4048525
47 meter
Z = 11994619
56 Z = 3636150
01
XDOT = 19519
762353 XDOT = 5951
409084
YDOT = -6859
271923 feet/sec YDOT = -2024
163916 meter/sec
ZDOT = 14286
254617 ZDOT = 4383
355016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13628820
06 X = -4154064
35
Y = -13004517
03 feet Y = -3963776
79 meter
Z = 11903461
89 Z = 3628175
18
XDOT = 18408
082943 XDOT = 5610
783681
YDOT = -6047
302284 feet/sec YDOT = -1843
217736 meter/sec
ZDOT = 14419
450129 ZDOT = 4395
048399
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 20200
23735950
00016717 00000-0 10270-3 0 9151
2 25544 51
6415 194
7895 0001424 136
9197 223
2065 15
49568476 36828
Satellite: ISS
Catalog Number: 25544
Epoch time: 20200
23735950 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 194
7895 deg
Eccentricity:
0001424
Arg of perigee: 136
9197 deg
Mean anomaly: 223
2065 deg
Mean motion: 15
49568476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3682
Checksum: 323
Coasting Arc #17 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2020/200/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5874542
40 A = 6801212
70 meter
Y = 2828559
47 meter E =
0008219
Z = -1926681
57 I = 51
56693
XDOT = -3637
604051 Wp = 137
22523
YDOT = 3757
846097 meter/sec RA = 192
14904 deg
ZDOT = -5594
287586 TA = 63
98372
MA = 63
89911
Ha = 228
703 n
mi
Hp = 221
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19273433
08 X = 5851834
60
Y = 9280050
75 feet Y = 2894126
16 meter
Z = -6321133
75 Z = -1898200
35
XDOT = -11934
396494 XDOT = -3652
181549
YDOT = 12328
891395 feet/sec YDOT = 3717
087278 meter/sec
ZDOT = -18353
961896 ZDOT = -5611
992179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4263221
76 X = -1299429
99
Y = -21001194
77 feet Y = -6401164
17 meter
Z = -6189996
36 Z = -1886710
89
XDOT = 15425
555963 XDOT = 4701
709458
YDOT = 2282
727095 feet/sec YDOT = 695
775219 meter/sec
ZDOT = -18435
609511 ZDOT = -5619
173779
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 20200
55982480
00016717 00000-0 10270-3 0 9169
2 25544 51
6382 193
1961 0001257 113
1534 246
9748 15
49534206 36873
Satellite: ISS
Catalog Number: 25544
Epoch time: 20200
55982480 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 193
1961 deg
Eccentricity:
0001257
Arg of perigee: 113
1534 deg
Mean anomaly: 246
9748 deg
Mean motion: 15
49534206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 316
Coasting Arc #18 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2020/201/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 965443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5997495
16 A = 6800835
08 meter
Y = -2420752
85 meter E =
0014539
Z = 2082237
72 I = 51
59876
XDOT = 3529
280037 Wp = 73
50536
YDOT = -3967
941936 meter/sec RA = 187
19582 deg
ZDOT = 5524
387072 TA = 309
51446
MA = 309
64290
Ha = 228
565 n
mi
Hp = 221
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19676821
38 X = -5980093
98
Y = -7942102
53 feet Y = -2487724
18 meter
Z = 6831488
59 Z = 2053146
58
XDOT = 11579
002745 XDOT = 3546
554597
YDOT = -13018
182206 feet/sec YDOT = -3928
379368 meter/sec
ZDOT = 18124
629501 ZDOT = 5541
571920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5927603
47 X = 1806733
54
Y = 20418875
25 feet Y = 6223673
18 meter
Z = 6697505
43 Z = 2041399
66
XDOT = -15823
284257 XDOT = -4822
937041
YDOT = -1408
235713 feet/sec YDOT = -429
230245 meter/sec
ZDOT = 18203
899029 ZDOT = 5548
548424
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 20201
59170806
00016717 00000-0 10270-3 0 9176
2 25544 51
6377 188
0884 0001220 129
3298 230
7960 15
49578369 37034
Satellite: ISS
Catalog Number: 25544
Epoch time: 20201
59170806 = yrday
fracday
Element set: 917
Inclination: 51
6377 deg
RA of node: 188
0884 deg
Eccentricity:
0001220
Arg of perigee: 129
3298 deg
Mean anomaly: 230
7960 deg
Mean motion: 15
49578369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3703
Checksum: 324
Coasting Arc #19 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2020/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930614
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5751595
66 A = 6799592
11 meter
Y = -2390716
37 meter E =
0014222
Z = 2712262
84 I = 51
62749
XDOT = 4077
773814 Wp = 82
24716
YDOT = -3923
956313 meter/sec RA = 182
40169 deg
ZDOT = 5167
138312 TA = 308
36600
MA = 308
49369
Ha = 228
564 n
mi
Hp = 221
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18870064
52 X = -5737608
83
Y = -7843557
64 feet Y = -2454957
04 meter
Z = 8898500
13 Z = 2684358
02
XDOT = 13378
523012 XDOT = 4096
251139
YDOT = -12873
872418 feet/sec YDOT = -3878
253254 meter/sec
ZDOT = 16952
553517 ZDOT = 5186
990367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1900174
96 X = 579173
33
Y = 20402480
71 feet Y = 6218676
12 meter
Z = 8769957
34 Z = 2673083
00
XDOT = -16087
456025 XDOT = -4903
456596
YDOT = -5858
679225 feet/sec YDOT = -1785
725428 meter/sec
ZDOT = 17044
123791 ZDOT = 5195
048932
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 20202
55909922
00016717 00000-0 10270-3 0 9183
2 25544 51
6381 183
2992 0001170 132
9499 227
1749 15
49573738 37189
Satellite: ISS
Catalog Number: 25544
Epoch time: 20202
55909922 = yrday
fracday
Element set: 918
Inclination: 51
6381 deg
RA of node: 183
2992 deg
Eccentricity:
0001170
Arg of perigee: 132
9499 deg
Mean anomaly: 227
1749 deg
Mean motion: 15
49573738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 336
Coasting Arc #20 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2020/202/16:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 930614
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2761150
48 A = 6792909
35 meter
Y = -3893987
48 meter E =
0008399
Z = 4828281
36 I = 51
61474
XDOT = 7002
123788 Wp = 120
36502
YDOT = -1827
079552 meter/sec RA = 181
41077 deg
ZDOT = 2523
341406 TA = 304
75826
MA = 304
83731
Ha = 228
622 n
mi
Hp = 221
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9058892
65 X = -2740854
04
Y = -12775549
48 feet Y = -3924751
91 meter
Z = 15840818
11 Z = 4814917
75
XDOT = 22972
847073 XDOT = 7009
777654
YDOT = -5994
355484 feet/sec YDOT = -1748
734410 meter/sec
ZDOT = 8278
679155 ZDOT = 2557
372535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11226136
26 X = 3421726
33
Y = 11008940
68 feet Y = 3355525
12 meter
Z = 15779315
85 Z = 4809535
47
XDOT = -20741
706789 XDOT = -6322
072229
YDOT = 9024
999374 feet/sec YDOT = 2750
819809 meter/sec
ZDOT = 8435
551029 ZDOT = 2571
155954
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 20202
75257909
00016717 00000-0 10270-3 0 9197
2 25544 51
6411 182
3417 0001070 125
9083 234
2166 15
49548558 37213
Satellite: ISS
Catalog Number: 25544
Epoch time: 20202
75257909 = yrday
fracday
Element set: 919
Inclination: 51
6411 deg
RA of node: 182
3417 deg
Eccentricity:
0001070
Arg of perigee: 125
9083 deg
Mean anomaly: 234
2166 deg
Mean motion: 15
49548558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 304
Coasting Arc #21 (Orbit 3727)
---------------------------------------
Vector Time (GMT): 2020/203/04:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930614
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5974228
02 A = 6800039
57 meter
Y = -2065811
01 meter E =
0014777
Z = 2486609
47 I = 51
65503
XDOT = 3653
110907 Wp = 108
16677
YDOT = 4143
231781 meter/sec RA = 179
05479 deg
ZDOT = -5313
253915 TA = 44
00986
MA = 43
89230
Ha = 228
533 n
mi
Hp = 221
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19600485
62 X = 5984806
28
Y = -6777595
19 feet Y = -1998944
16 meter
Z = 8158167
56 Z = 2515654
63
XDOT = 11985
272003 XDOT = 3632
316676
YDOT = 13593
280122 feet/sec YDOT = 4183
967997 meter/sec
ZDOT = -17431
935417 ZDOT = -5295
558840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19716948
34 X = 6009725
85
Y = -6257311
12 feet Y = -1907228
43 meter
Z = 8292076
75 Z = 2527424
99
XDOT = 11283
522800 XDOT = 3439
217750
YDOT = 12470
288045 feet/sec YDOT = 3800
943796 meter/sec
ZDOT = -17350
468036 ZDOT = -5288
422657
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 20203
20402710
00016717 00000-0 10270-3 0 9202
2 25544 51
6417 180
1035 0001409 142
7324 217
3924 15
49529660 37286
Satellite: ISS
Catalog Number: 25544
Epoch time: 20203
20402710 = yrday
fracday
Element set: 920
Inclination: 51
6417 deg
RA of node: 180
1035 deg
Eccentricity:
0001409
Arg of perigee: 142
7324 deg
Mean anomaly: 217
3924 deg
Mean motion: 15
49529660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3728
Checksum: 272
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