[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 30th 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
276/01:38:44
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
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
278/10:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 222
7
280/09:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 222
5
281/08:14:18
140 -2
3 -2
5 2
5
N/A 1
1 -0
0 228
1
000/00:06:36
280 0
1 -0
0 222
6
283/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
6
Coasting Arc #1 (Orbit 802)
---------------------------------------
Vector Time (GMT): 2020/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -759042
60 A = 6793863
75 meter
Y = -4430423
38 meter E =
0006431
Z = 5090354
72 I = 51
51362
XDOT = 7432
096846 Wp = 120
81535
YDOT = 714
184410 meter/sec RA = 196
07331 deg
ZDOT = 1724
974629 TA = 312
44441
MA = 312
49877
Ha = 229
787 n
mi
Hp = 222
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2490297
25 X = -734169
81
Y = -14535509
77 feet Y = -4438772
11 meter
Z = 16700638
84 Z = 5086728
32
XDOT = 24383
519836 XDOT = 7415
179339
YDOT = 2343
124706 feet/sec YDOT = 797
200976 meter/sec
ZDOT = 5659
365582 ZDOT = 1761
035589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4311700
63 X = 1314206
35
Y = 14122721
36 feet Y = 4304605
47 meter
Z = 16683882
68 Z = 5085247
44
XDOT = -23420
432651 XDOT = -7138
547872
YDOT = 249
072750 feet/sec YDOT = 75
917374 meter/sec
ZDOT = 5825
898384 ZDOT = 1775
733827
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 20272
55149341
00016717 00000-0 10270-3 0 9002
2 25544 51
6421 197
0085 0001162 100
5667 259
5613 15
48830030 8030
Satellite: ISS
Catalog Number: 25544
Epoch time: 20272
55149341 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 197
0085 deg
Eccentricity:
0001162
Arg of perigee: 100
5667 deg
Mean anomaly: 259
5613 deg
Mean motion: 15
48830030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 803
Checksum: 276
Coasting Arc #2 (Orbit 817)
---------------------------------------
Vector Time (GMT): 2020/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1204823
18 A = 6793969
53 meter
Y = 4353908
15 meter E =
0014275
Z = -5087343
23 I = 51
54782
XDOT = -7438
461786 Wp = 78
69550
YDOT = -20
948621 meter/sec RA = 191
12200 deg
ZDOT = -1781
086145 TA = 174
01478
MA = 173
99771
Ha = 229
826 n
mi
Hp = 222
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3952831
96 X = 1180758
32
Y = 14284475
57 feet Y = 4367246
36 meter
Z = -16690758
64 Z = -5081549
50
XDOT = -24404
402184 XDOT = -7429
023196
YDOT = -68
729071 feet/sec YDOT = -104
078214 meter/sec
ZDOT = -5843
458482 ZDOT = -1817
196333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5968794
33 X = -1819288
51
Y = -13599177
83 feet Y = -4145029
40 meter
Z = -16663985
23 Z = -5079182
70
XDOT = 23155
904529 XDOT = 7057
919701
YDOT = -2804
716506 feet/sec YDOT = -854
877591 meter/sec
ZDOT = -6010
236275 ZDOT = -1831
920017
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 20273
51934585
00016717 00000-0 10270-3 0 9012
2 25544 51
6433 192
2222 0001272 98
3936 261
7358 15
48819907 8185
Satellite: ISS
Catalog Number: 25544
Epoch time: 20273
51934585 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 192
2222 deg
Eccentricity:
0001272
Arg of perigee: 98
3936 deg
Mean anomaly: 261
7358 deg
Mean motion: 15
48819907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 818
Checksum: 321
Coasting Arc #3 (Orbit 833)
---------------------------------------
Vector Time (GMT): 2020/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1649632
45 A = 6793985
03 meter
Y = -4216232
11 meter E =
0006775
Z = 5061571
67 I = 51
58182
XDOT = 7406
330962 Wp = 121
31218
YDOT = -672
999570 meter/sec RA = 186
17387 deg
ZDOT = 1847
943585 TA = 310
73240
MA = 310
79120
Ha = 229
803 n
mi
Hp = 222
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5412179
97 X = -1626948
98
Y = -13832782
50 feet Y = -4234552
16 meter
Z = 16606206
25 Z = 5053613
87
XDOT = 24298
986095 XDOT = 7404
329907
YDOT = -2208
003837 feet/sec YDOT = -590
187675 meter/sec
ZDOT = 6062
807036 ZDOT = 1883
915964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7574416
75 X = 2308682
22
Y = 12825202
58 feet Y = 3909121
75 meter
Z = 16569430
88 Z = 5050362
53
XDOT = -22699
473668 XDOT = -6918
799574
YDOT = 5336
170839 feet/sec YDOT = 1626
464872 meter/sec
ZDOT = 6228
963288 ZDOT = 1898
588010
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 20274
55171330
00016717 00000-0 10270-3 0 9029
2 25544 51
6436 187
1176 0001178 105
0713 255
0568 15
48839673 8342
Satellite: ISS
Catalog Number: 25544
Epoch time: 20274
55171330 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 187
1176 deg
Eccentricity:
0001178
Arg of perigee: 105
0713 deg
Mean anomaly: 255
0568 deg
Mean motion: 15
48839673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 834
Checksum: 305
Coasting Arc #4 (Orbit 848)
---------------------------------------
Vector Time (GMT): 2020/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2066276
83 A = 6794054
12 meter
Y = 4052645
24 meter E =
0014043
Z = -5059109
18 I = 51
61638
XDOT = -7286
091918 Wp = 78
25638
YDOT = 1347
647928 meter/sec RA = 181
22761 deg
ZDOT = -1897
979273 TA = 173
29836
MA = 173
27956
Ha = 229
800 n
mi
Hp = 222
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6779123
45 X = 2045379
81
Y = 13296080
17 feet Y = 4075634
49 meter
Z = -16598127
22 Z = -5049123
09
XDOT = -23904
501043 XDOT = -7291
400833
YDOT = 4421
417088 feet/sec YDOT = 1266
139751 meter/sec
ZDOT = -6226
966118 ZDOT = -1933
385560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9049792
39 X = -2758376
72
Y = -11932032
16 feet Y = -3636883
40 meter
Z = -16551977
40 Z = -5045042
71
XDOT = 21894
154967 XDOT = 6673
338434
YDOT = -7748
363542 feet/sec YDOT = -2361
701207 meter/sec
ZDOT = -6390
521187 ZDOT = -1947
830858
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 20275
51955493
00016717 00000-0 10270-3 0 9037
2 25544 51
6442 182
3319 0001294 100
7312 259
3983 15
48840357 8496
Satellite: ISS
Catalog Number: 25544
Epoch time: 20275
51955493 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 182
3319 deg
Eccentricity:
0001294
Arg of perigee: 100
7312 deg
Mean anomaly: 259
3983 deg
Mean motion: 15
48840357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 849
Checksum: 317
Coasting Arc #5 (Orbit 857)
---------------------------------------
Vector Time (GMT): 2020/276/01:38:44
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6788547
61 A = 6804731
27 meter
Y = 98596
05 meter E =
0012655
Z = -364009
99 I = 51
66980
XDOT = -383
235661 Wp = 135
45294
YDOT = 4752
427023 meter/sec RA = 178
40267 deg
ZDOT = -5995
252475 TA = 48
46054
MA = 48
35207
Ha = 229
814 n
mi
Hp = 222
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22272137
81 X = 6788708
71
Y = 323477
84 feet Y = 174511
32 meter
Z = -1194258
49 Z = -331033
15
XDOT = -1257
334846 XDOT = -407
228430
YDOT = 15591
952175 feet/sec YDOT = 4748
006676 meter/sec
ZDOT = -19669
463500 ZDOT = -5997
172837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18431857
81 X = 5618030
26
Y = -12520385
52 feet Y = -3816213
51 meter
Z = -1041910
75 Z = -317574
40
XDOT = 7114
425756 XDOT = 2168
476970
YDOT = 12068
685124 feet/sec YDOT = 3678
535226 meter/sec
ZDOT = -19678
313371 ZDOT = -5997
949916
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
10025701
00016717 00000-0 10270-3 0 9044
2 25544 51
6428 179
4591 0001313 116
7713 243
3571 15
48830213 8589
Satellite: ISS
Catalog Number: 25544
Epoch time: 20276
10025701 = yrday
fracday
Element set: 904
Inclination: 51
6428 deg
RA of node: 179
4591 deg
Eccentricity:
0001313
Arg of perigee: 116
7713 deg
Mean anomaly: 243
3571 deg
Mean motion: 15
48830213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 858
Checksum: 287
Coasting Arc #6 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2020/277/01:38:44
000
Vector Time (MET): N/A
Weight (LBS) : 922360
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6771088
63 A = 6804871
28 meter
Y = 543057
69 meter E =
0013050
Z = 293542
37 I = 51
70309
XDOT = -113
675381 Wp = 53
27452
YDOT = -4757
686561 meter/sec RA = 173
45900 deg
ZDOT = 6002
124736 TA = 309
87897
MA = 309
99366
Ha = 229
813 n
mi
Hp = 222
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22214857
71 X = -6778083
91
Y = 1781685
35 feet Y = 467299
44 meter
Z = 963065
51 Z = 260633
54
XDOT = -372
950726 XDOT = -89
620376
YDOT = -15609
207877 feet/sec YDOT = -4758
822727 meter/sec
ZDOT = 19692
010288 ZDOT = 6001
631386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16928627
99 X = -5159845
81
Y = 14503985
81 feet Y = 4420814
88 meter
Z = 811018
57 Z = 247198
46
XDOT = -8528
394744 XDOT = -2599
454718
YDOT = -11093
757184 feet/sec YDOT = -3381
377190 meter/sec
ZDOT = 19689
710822 ZDOT = 6001
423858
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
13261532
00016717 00000-0 10270-3 0 9053
2 25544 51
6423 174
3542 0001206 114
2976 245
8300 15
48788685 8749
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
13261532 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 174
3542 deg
Eccentricity:
0001206
Arg of perigee: 114
2976 deg
Mean anomaly: 245
8300 deg
Mean motion: 15
48788685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 306
Coasting Arc #7 (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 = -1764120
09 A = 6794181
78 meter
Y = 4235861
78 meter E =
0014078
Z = -5023546
89 I = 51
67197
XDOT = -7345
887852 Wp = 105
87587
YDOT = -655
907237 meter/sec RA = 172
54958 deg
ZDOT = 2027
580505 TA = 183
86868
MA = 183
87958
Ha = 229
820 n
mi
Hp = 222
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5787795
56 X = -1786953
75
Y = 13897184
33 feet Y = 4216006
02 meter
Z = -16481453
04 Z = -5032172
25
XDOT = -24100
681930 XDOT = -7347
856318
YDOT = -2151
926632 feet/sec YDOT = -738
065055 meter/sec
ZDOT = 6652
167012 ZDOT = 1991
891778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14730236
83 X = 4489776
18
Y = 2887169
95 feet Y = 880009
40 meter
Z = -16521288
59 Z = -5035688
76
XDOT = 2757
915996 XDOT = 840
612796
YDOT = 23032
931839 feet/sec YDOT = 7020
437625 meter/sec
ZDOT = 6487
267824 ZDOT = 1977
319233
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
26165785
00016717 00000-0 10270-3 0 9061
2 25544 51
6404 173
7168 0001291 112
3921 247
7365 15
48810465 8764
Satellite: ISS
Catalog Number: 25544
Epoch time: 20277
26165785 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 173
7168 deg
Eccentricity:
0001291
Arg of perigee: 112
3921 deg
Mean anomaly: 247
7365 deg
Mean motion: 15
48810465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 876
Checksum: 319
Coasting Arc #8 (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 = 1339829
03 A = 6794024
34 meter
Y = -4360958
27 meter E =
0006436
Z = 5030175
38 I = 51
70509
XDOT = 7401
514808 Wp = 65
65827
YDOT = -21
182618 meter/sec RA = 167
60893 deg
ZDOT = -1985
226698 TA = 43
64111
MA = 43
59023
Ha = 229
699 n
mi
Hp = 222
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4395764
54 X = 1364060
82
Y = -14307605
88 feet Y = -4345839
48 meter
Z = 16503200
08 Z = 5036743
05
XDOT = 24283
185067 XDOT = 7410
844859
YDOT = -69
496777 feet/sec YDOT = 61
638452 meter/sec
ZDOT = -6513
210952 ZDOT = -1949
249696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14886952
20 X = -4537543
03
Y = -1186093
66 feet Y = -361521
35 meter
Z = 16533535
03 Z = 5039421
48
XDOT = -5258
240114 XDOT = -1602
711587
YDOT = -22685
604006 feet/sec YDOT = -6914
572101 meter/sec
ZDOT = -6346
963741 ZDOT = -1934
554548
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
29400787
00016717 00000-0 10270-3 0 9070
2 25544 51
6404 168
6112 0001188 114
9589 245
1684 15
48841847 8921
Satellite: ISS
Catalog Number: 25544
Epoch time: 20278
29400787 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 168
6112 deg
Eccentricity:
0001188
Arg of perigee: 114
9589 deg
Mean anomaly: 245
1684 deg
Mean motion: 15
48841847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 335
Coasting Arc #9 (Orbit 894)
---------------------------------------
Vector Time (GMT): 2020/278/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6665967
16 A = 6804732
90 meter
Y = 1294705
57 meter E =
0013163
Z = 337110
46 I = 51
74855
XDOT = -605
258861 Wp = 53
03356
YDOT = -4719
502724 meter/sec RA = 166
76547 deg
ZDOT = 6003
120567 TA = 310
58644
MA = 310
70092
Ha = 229
720 n
mi
Hp = 222
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21869971
01 X = -6681587
04
Y = 4247721
70 feet Y = 1220074
64 meter
Z = 1106005
45 Z = 304691
15
XDOT = -1985
757417 XDOT = -581
599268
YDOT = -15483
932820 feet/sec YDOT = -4726
138447 meter/sec
ZDOT = 19695
277450 ZDOT = 6000
238200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22235173
99 X = 6777281
03
Y = 1498245
99 feet Y = 456665
38 meter
Z = 956198
81 Z = 291449
40
XDOT = -1807
389897 XDOT = -550
892441
YDOT = 13888
160867 feet/sec YDOT = 4233
111432 meter/sec
ZDOT = 19681
943781 ZDOT = 5999
056464
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
48757445
00016717 00000-0 10270-3 0 9088
2 25544 51
6426 167
6545 0001102 109
3580 250
7689 15
48832660 8952
Satellite: ISS
Catalog Number: 25544
Epoch time: 20278
48757445 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 167
6545 deg
Eccentricity:
0001102
Arg of perigee: 109
3580 deg
Mean anomaly: 250
7689 deg
Mean motion: 15
48832660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 895
Checksum: 334
Coasting Arc #10 (Orbit 909)
---------------------------------------
Vector Time (GMT): 2020/279/10:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 937074
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6525663
17 A = 6804732
31 meter
Y = -1882614
20 meter E =
0012600
Z = -313081
09 I = 51
78153
XDOT = 1055
789730 Wp = 135
17536
YDOT = 4632
861572 meter/sec RA = 161
82725 deg
ZDOT = -6008
117874 TA = 48
18472
MA = 48
07718
Ha = 229
759 n
mi
Hp = 222
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21409656
06 X = 6547750
92
Y = -6176555
76 feet Y = -1809516
07 meter
Z = -1027168
94 Z = -281327
56
XDOT = 3463
877068 XDOT = 1033
089824
YDOT = 15199
677073 feet/sec YDOT = 4644
540923 meter/sec
ZDOT = -19711
672814 ZDOT = -6003
044537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22272192
62 X = -6788564
31
Y = 867516
90 feet Y = 264419
15 meter
Z = -880420
18 Z = -268352
07
XDOT = 209
576512 XDOT = 63
878921
YDOT = -13994
187477 feet/sec YDOT = -4265
428343 meter/sec
ZDOT = -19688
217931 ZDOT = -6000
968825
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
45539765
00016717 00000-0 10270-3 0 9090
2 25544 51
6429 162
8685 0001152 115
0702 245
0567 15
48834040 9106
Satellite: ISS
Catalog Number: 25544
Epoch time: 20279
45539765 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 162
8685 deg
Eccentricity:
0001152
Arg of perigee: 115
0702 deg
Mean anomaly: 245
0567 deg
Mean motion: 15
48834040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 910
Checksum: 310
Coasting Arc #11 (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 = -3560387
14 A = 6799251
89 meter
Y = 4569798
77 meter E =
0006346
Z = -3566099
78 I = 51
79474
XDOT = -6077
711064 Wp = 100
83191
YDOT = -1242
514814 meter/sec RA = 156
90279 deg
ZDOT = 4481
367260 TA = 217
32324
MA = 217
36735
Ha = 229
648 n
mi
Hp = 222
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11681060
18 X = -3593900
95
Y = 14992778
13 feet Y = 4529796
46 meter
Z = -11699802
42 Z = -3583476
67
XDOT = -19939
996930 XDOT = -6085
133560
YDOT = -4076
492173 feet/sec YDOT = -1310
521481 meter/sec
ZDOT = 14702
648490 ZDOT = 4451
825510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15235626
61 X = 4643818
99
Y = -11279200
81 feet Y = -3437900
41 meter
Z = -11780120
98 Z = -3590580
87
XDOT = 17358
102124 XDOT = 5290
749527
YDOT = 8252
965934 feet/sec YDOT = 2515
504017 meter/sec
ZDOT = 14566
100273 ZDOT = 4439
747363
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
42321805
00016717 00000-0 10270-3 0 9105
2 25544 51
6425 158
0825 0001108 117
3371 242
7892 15
48863180 9251
Satellite: ISS
Catalog Number: 25544
Epoch time: 20280
42321805 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 158
0825 deg
Eccentricity:
0001108
Arg of perigee: 117
3371 deg
Mean anomaly: 242
7892 deg
Mean motion: 15
48863180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 925
Checksum: 290
Coasting Arc #12 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2020/281/08:17:36
280
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -122172
26 A = 6792297
48 meter
Y = -4473682
04 meter E =
0004004
Z = 5107460
35 I = 51
80361
XDOT = 7132
233707 Wp = 50
35852
YDOT = -2190
395118 meter/sec RA = 152
32598 deg
ZDOT = -1744
585671 TA = 56
50148
MA = 56
46323
Ha = 228
143 n
mi
Hp = 222
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -400827
63 X = -96946
73
Y = -14677434
51 feet Y = -4474907
11 meter
Z = 16756759
67 Z = 5106928
22
XDOT = 23399
716885 XDOT = 7164
671648
YDOT = -7186
335689 feet/sec YDOT = -2110
456028 meter/sec
ZDOT = -5723
706269 ZDOT = -1709
860554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9051630
02 X = -2758936
83
Y = 11564513
86 feet Y = 3524863
82 meter
Z = 16754305
55 Z = 5106712
33
XDOT = -21720
603481 XDOT = -6620
439941
YDOT = -8924
954888 feet/sec YDOT = -2720
326250 meter/sec
ZDOT = -5563
176197 ZDOT = -1695
656105
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
39101646
00016717 00000-0 10270-3 0 9112
2 25544 51
6415 153
2963 0001230 252
7414 107
3601 15
49333722 9404
Satellite: ISS
Catalog Number: 25544
Epoch time: 20281
39101646 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 153
2963 deg
Eccentricity:
0001230
Arg of perigee: 252
7414 deg
Mean anomaly: 107
3601 deg
Mean motion: 15
49333722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 940
Checksum: 270
Coasting Arc #13 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2020/282/08:17:36
280
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 373708
19 A = 6792434
58 meter
Y = 4503090
29 meter E =
0012054
Z = -5082413
86 I = 51
83421
XDOT = -6917
674848 Wp = 106
37582
YDOT = 2682
575979 meter/sec RA = 147
38839 deg
ZDOT = 1868
516254 TA = 181
71815
MA = 181
72229
Ha = 228
120 n
mi
Hp = 222
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1226076
73 X = 348013
38
Y = 14773918
27 feet Y = 4507125
66 meter
Z = -16674586
15 Z = -5080660
94
XDOT = -22695
783623 XDOT = -6956
234422
YDOT = 8801
102293 feet/sec YDOT = 2605
001991 meter/sec
ZDOT = 6130
302672 ZDOT = 1834
818649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8271986
75 X = 2521301
56
Y = -12313242
56 feet Y = -3753076
33 meter
Z = -16666494
57 Z = -5079947
55
XDOT = 22301
135725 XDOT = 6797
386169
YDOT = 6896
727159 feet/sec YDOT = 2102
122438 meter/sec
ZDOT = 5974
495161 ZDOT = 1821
026125
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
35853315
00016717 00000-0 10270-3 0 9127
2 25544 51
6422 148
5071 0001174 259
1221 100
9797 15
49339436 9552
Satellite: ISS
Catalog Number: 25544
Epoch time: 20282
35853315 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 148
5071 deg
Eccentricity:
0001174
Arg of perigee: 259
1221 deg
Mean anomaly: 100
9797 deg
Mean motion: 15
49339436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 303
Coasting Arc #14 (Orbit 970)
---------------------------------------
Vector Time (GMT): 2020/283/08:17:36
280
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -618192
15 A = 6792550
08 meter
Y = -4512704
62 meter E =
0004825
Z = 5036833
66 I = 51
86243
XDOT = 6688
236261 Wp = 49
59364
YDOT = -3156
812023 meter/sec RA = 142
45477 deg
ZDOT = -2003
132163 TA = 59
84361
MA = 59
79582
Ha = 228
122 n
mi
Hp = 222
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2028189
48 X = -592150
17
Y = -14805461
34 feet Y = -4519472
07 meter
Z = 16525044
82 Z = 5033893
94
XDOT = 21943
032353 XDOT = 6732
769802
YDOT = -10356
994826 feet/sec YDOT = -3081
770370 meter/sec
ZDOT = -6571
955915 ZDOT = -1970
534719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7447946
36 X = -2270134
05
Y = 12972731
62 feet Y = 3954088
60 meter
Z = 16511470
97 Z = 5032696
35
XDOT = -22748
429240 XDOT = -6933
721232
YDOT = -4869
592408 feet/sec YDOT = -1484
251766 meter/sec
ZDOT = -6421
206954 ZDOT = -1957
183880
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
39054727
00016717 00000-0 10270-3 0 9133
2 25544 51
6421 143
4007 0001165 266
6677 93
4340 15
49355773 9712
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
39054727 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 143
4007 deg
Eccentricity:
0001165
Arg of perigee: 266
6677 deg
Mean anomaly: 93
4340 deg
Mean motion: 15
49355773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 971
Checksum: 309
Coasting Arc #15 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2020/283/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2924852
60 A = 6791243
56 meter
Y = -3012963
60 meter E =
0001616
Z = 5336523
68 I = 51
87309
XDOT = 5724
882145 Wp = 136
39735
YDOT = -5085
380944 meter/sec RA = 139
94398 deg
ZDOT = 265
347402 TA = 311
07243
MA = 311
08639
Ha = 228
112 n
mi
Hp = 222
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9595973
10 X = -2916865
44
Y = -9885051
17 feet Y = -3045626
72 meter
Z = 17508279
79 Z = 5322335
13
XDOT = 18782
421735 XDOT = 5780
034000
YDOT = -16684
320683 feet/sec YDOT = -5021
052833 meter/sec
ZDOT = 870
562344 ZDOT = 293
290930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2708543
19 X = -825563
96
Y = -13592405
41 feet Y = -4142965
17 meter
Z = 17442680
61 Z = 5316529
05
XDOT = 23858
011752 XDOT = 7271
921982
YDOT = -3466
115374 feet/sec YDOT = -1056
471966 meter/sec
ZDOT = 999
812435 ZDOT = 304
742830
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
90655146
00016717 00000-0 10270-3 0 9143
2 25544 51
6434 140
8438 0001460 247
9940 112
1055 15
49378318 9798
Satellite: ISS
Catalog Number: 25544
Epoch time: 20283
90655146 = yrday
fracday
Element set: 914
Inclination: 51
6434 deg
RA of node: 140
8438 deg
Eccentricity:
0001460
Arg of perigee: 247
9940 deg
Mean anomaly: 112
1055 deg
Mean motion: 15
49378318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 979
Checksum: 315
Coasting Arc #16 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2020/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3066671
43 A = 6791343
20 meter
Y = 2866599
50 meter E =
0013397
Z = -5350146
85 I = 51
89752
XDOT = -5339
921116 Wp = 90
73583
YDOT = 5477
661852 meter/sec RA = 135
01248 deg
ZDOT = -126
328920 TA = 178
06444
MA = 178
05925
Ha = 228
026 n
mi
Hp = 222
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10061257
96 X = 3060376
50
Y = 9404854
00 feet Y = 2900857
97 meter
Z = -17552975
22 Z = -5335265
35
XDOT = -17519
426235 XDOT = -5400
163469
YDOT = 17971
331534 feet/sec YDOT = 5417
610186 meter/sec
ZDOT = -414
464961 ZDOT = -152
414759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3591953
55 X = 1094827
44
Y = 13386148
37 feet Y = 4080098
02 meter
Z = -17484165
15 Z = -5329173
54
XDOT = -23427
696771 XDOT = -7140
761976
YDOT = 5589
354579 feet/sec YDOT = 1703
635276 meter/sec
ZDOT = -535
149630 ZDOT = -163
113607
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
87406170
00016717 00000-0 10270-3 0 9152
2 25544 51
6428 136
0565 0001481 253
7132 106
3855 15
49340325 9947
Satellite: ISS
Catalog Number: 25544
Epoch time: 20284
87406170 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 136
0565 deg
Eccentricity:
0001481
Arg of perigee: 253
7132 deg
Mean anomaly: 106
3855 deg
Mean motion: 15
49340325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 994
Checksum: 303
Coasting Arc #17 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2020/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3194865
65 A = 6791186
58 meter
Y = -2707833
05 meter E =
0000992
Z = 5345282
67 I = 51
92152
XDOT = 4941
292197 Wp = 109
37629
YDOT = -5855
618528 meter/sec RA = 130
08171 deg
ZDOT = -13
278069 TA = 340
74797
MA = 340
75172
Ha = 228
053 n
mi
Hp = 222
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10481842
70 X = -3190312
89
Y = -8883966
71 feet Y = -2743534
74 meter
Z = 17537016
63 Z = 5329774
29
XDOT = 16211
588574 XDOT = 5006
468740
YDOT = -19211
346878 feet/sec YDOT = -5799
997030 meter/sec
ZDOT = -43
563218 ZDOT = 10
883399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4451431
05 X = -1356796
19
Y = -13095376
23 feet Y = -3991470
68 meter
Z = 17465300
63 Z = 5323423
63
XDOT = 22873
040240 XDOT = 6971
702665
YDOT = -7682
676451 feet/sec YDOT = -2341
679782 meter/sec
ZDOT = 68
243835 ZDOT = 20
800721
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
90606598
00016717 00000-0 10270-3 0 9164
2 25544 51
6437 130
9489 0001501 259
3738 100
7243 15
49387251 10100
Satellite: ISS
Catalog Number: 25544
Epoch time: 20285
90606598 = yrday
fracday
Element set: 916
Inclination: 51
6437 deg
RA of node: 130
9489 deg
Eccentricity:
0001501
Arg of perigee: 259
3738 deg
Mean anomaly: 100
7243 deg
Mean motion: 15
49387251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1010
Checksum: 308
Coasting Arc #18 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2020/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936804
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3325169
39 A = 6791315
37 meter
Y = 2556817
18 meter E =
0013418
Z = -5352733
36 I = 51
94142
XDOT = -4503
366174 Wp = 91
52078
YDOT = 6183
105064 meter/sec RA = 125
15273 deg
ZDOT = 155
914351 TA = 179
96235
MA = 179
96225
Ha = 228
009 n
mi
Hp = 222
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10909348
41 X = 3322331
84
Y = 8388507
81 feet Y = 2593985
50 meter
Z = -17561461
16 Z = -5336587
90
XDOT = -14774
823407 XDOT = -4572
930168
YDOT = 20285
777769 feet/sec YDOT = 6132
356243 meter/sec
ZDOT = 511
530024 ZDOT = 133
869386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5295174
73 X = 1613969
26
Y = 12804650
62 feet Y = 3902857
51 meter
Z = -17486792
48 Z = -5329974
35
XDOT = -22056
800260 XDOT = -6722
912719
YDOT = 9680
532022 feet/sec YDOT = 2950
626160 meter/sec
ZDOT = 409
493313 ZDOT = 124
813562
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
87356795
00016717 00000-0 10270-3 0 9173
2 25544 51
6428 126
1611 0001411 268
5360 91
5629 15
49348595 10256
Satellite: ISS
Catalog Number: 25544
Epoch time: 20286
87356795 = yrday
fracday
Element set: 917
Inclination: 51
6428 deg
RA of node: 126
1611 deg
Eccentricity:
0001411
Arg of perigee: 268
5360 deg
Mean anomaly: 91
5629 deg
Mean motion: 15
49348595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1025
Checksum: 323
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