[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 18th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13552 8396 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
140/01:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
5
141/17:30:57
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
4
143/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
3
000/00:00:00
000 0
0 0
0 222
4
145/22:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 222
3
146/12:14:26
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
2
148/20:33:31
100 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
2
149/04:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 222
2
149/15:17:02
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
2
Coasting Arc #1 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2020/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 267527
86 A = 6792378
51 meter
Y = 4503654
68 meter E =
0011959
Z = -5088392
87 I = 51
82170
XDOT = -6992
971236 Wp = 101
85277
YDOT = 2498
005792 meter/sec RA = 149
07901 deg
ZDOT = 1844
561231 TA = 185
99904
MA = 186
01338
Ha = 228
155 n
mi
Hp = 222
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 877716
08 X = 241863
29
Y = 14775769
94 feet Y = 4506503
20 meter
Z = -16694202
34 Z = -5087155
36
XDOT = -22942
819017 XDOT = -7029
344775
YDOT = 8195
557062 feet/sec YDOT = 2419
601912 meter/sec
ZDOT = 6051
710074 ZDOT = 1810
503911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12364418
86 X = 3768674
87
Y = 8148637
83 feet Y = 2483704
81 meter
Z = -16688648
90 Z = -5086700
19
XDOT = -6783
317593 XDOT = -2067
555202
YDOT = 22357
424020 feet/sec YDOT = 6814
542841 meter/sec
ZDOT = 5895
076341 ZDOT = 1796
819269
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 20136
51301705
00016717 00000-0 10270-3 0 9001
2 25544 51
6413 150
1962 0001279 302
9506 57
1521 15
49348462 26948
Satellite: ISS
Catalog Number: 25544
Epoch time: 20136
51301705 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 150
1962 deg
Eccentricity:
0001279
Arg of perigee: 302
9506 deg
Mean anomaly: 57
1521 deg
Mean motion: 15
49348462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 283
Coasting Arc #2 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2020/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -497676
51 A = 6792460
03 meter
Y = -4524574
63 meter E =
0005601
Z = 5039473
24 I = 51
84979
XDOT = 6777
405376 Wp = 44
20272
YDOT = -2968
774621 meter/sec RA = 144
14257 deg
ZDOT = -1990
893444 TA = 65
11990
MA = 65
06168
Ha = 228
192 n
mi
Hp = 222
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1632796
96 X = -471523
35
Y = -14844404
95 feet Y = -4529994
06 meter
Z = 16533704
85 Z = 5037118
97
XDOT = 22235
581942 XDOT = 6819
770037
YDOT = -9740
074216 feet/sec YDOT = -2892
747858 meter/sec
ZDOT = -6531
802638 ZDOT = -1957
868627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13003839
54 X = -3963570
29
Y = -7367204
10 feet Y = -2245523
81 meter
Z = 16523021
55 Z = 5036216
97
XDOT = 4777
213166 XDOT = 1456
094573
YDOT = -22779
544236 feet/sec YDOT = -6943
205083 meter/sec
ZDOT = -6379
881527 ZDOT = -1944
587889
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 20137
54501191
00016717 00000-0 10270-3 0 9017
2 25544 51
6405 145
0879 0001233 312
5199 47
5846 15
49381470 27102
Satellite: ISS
Catalog Number: 25544
Epoch time: 20137
54501191 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 145
0879 deg
Eccentricity:
0001233
Arg of perigee: 312
5199 deg
Mean anomaly: 47
5846 deg
Mean motion: 15
49381470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2710
Checksum: 293
Coasting Arc #3 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2020/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 751158
77 A = 6792735
97 meter
Y = 4540973
20 meter E =
0011532
Z = -5006185
54 I = 51
87626
XDOT = -6509
245973 Wp = 102
15042
YDOT = 3415
767743 meter/sec RA = 139
20920 deg
ZDOT = 2123
434786 TA = 188
49655
MA = 188
51609
Ha = 228
255 n
mi
Hp = 222
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2464431
67 X = 724641
78
Y = 14898206
04 feet Y = 4549225
21 meter
Z = -16424493
23 Z = -5002600
83
XDOT = -21355
793874 XDOT = -6557
272820
YDOT = 11206
587082 feet/sec YDOT = 3342
708066 meter/sec
ZDOT = 6966
649562 ZDOT = 2091
698747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13652157
14 X = 4161177
50
Y = 6494990
31 feet Y = 1979673
05 meter
Z = -16408158
05 Z = -5001206
57
XDOT = -2728
206908 XDOT = -831
557466
YDOT = 22950
641046 feet/sec YDOT = 6995
355391 meter/sec
ZDOT = 6820
620656 ZDOT = 2078
925176
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 20138
51250657
00016717 00000-0 10270-3 0 9024
2 25544 51
6398 140
3000 0001296 318
9044 41
2009 15
49349939 27257
Satellite: ISS
Catalog Number: 25544
Epoch time: 20138
51250657 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 140
3000 deg
Eccentricity:
0001296
Arg of perigee: 318
9044 deg
Mean anomaly: 41
2009 deg
Mean motion: 15
49349939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 295
Coasting Arc #4 (Orbit 2740)
---------------------------------------
Vector Time (GMT): 2020/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -992772
70 A = 6792869
96 meter
Y = -4541789
49 meter E =
0006410
Z = 4950315
96 I = 51
90010
XDOT = 6229
717141 Wp = 46
04613
YDOT = -3841
085700 meter/sec RA = 134
27657 deg
ZDOT = -2268
588038 TA = 66
08819
MA = 66
02106
Ha = 228
240 n
mi
Hp = 222
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3257128
27 X = -965957
32
Y = -14900884
16 feet Y = -4552741
75 meter
Z = 16241194
11 Z = 4945558
27
XDOT = 20438
704531 XDOT = 6283
225910
YDOT = -12601
987206 feet/sec YDOT = -3771
121244 meter/sec
ZDOT = -7442
874142 ZDOT = -2238
196469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14209706
96 X = -4331118
68
Y = -5606655
40 feet Y = -1708908
56 meter
Z = 16219471
72 Z = 4943694
98
XDOT = 712
862715 XDOT = 217
280556
YDOT = -22992
027663 feet/sec YDOT = -7007
970032 meter/sec
ZDOT = -7302
993720 ZDOT = -2225
952486
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20139
54449976
00016717 00000-0 10270-3 0 9033
2 25544 51
6382 135
1919 0001377 319
7460 40
3588 15
49374848 27419
Satellite: ISS
Catalog Number: 25544
Epoch time: 20139
54449976 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 135
1919 deg
Eccentricity:
0001377
Arg of perigee: 319
7460 deg
Mean anomaly: 40
3588 deg
Mean motion: 15
49374848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2741
Checksum: 336
Coasting Arc #5 (Orbit 2749)
---------------------------------------
Vector Time (GMT): 2020/140/01:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5409449
07 A = 6797316
49 meter
Y = 1682744
14 meter E =
0010735
Z = 3747469
41 I = 51
92909
XDOT = 1040
239458 Wp = 92
64485
YDOT = -6257
127826 meter/sec RA = 131
51298 deg
ZDOT = 4300
147525 TA = 311
84719
MA = 311
93878
Ha = 228
254 n
mi
Hp = 222
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17747536
33 X = -5446067
26
Y = 5520814
12 feet Y = 1622046
84 meter
Z = 12294847
14 Z = 3721103
27
XDOT = 3412
859113 XDOT = 1089
243296
YDOT = -20528
634599 feet/sec YDOT = -6245
221414 meter/sec
ZDOT = 14108
095556 ZDOT = 4305
319272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2637513
46 X = -803914
10
Y = -18478800
99 feet Y = -5632338
54 meter
Z = 12173542
50 Z = 3710495
75
XDOT = 18399
402024 XDOT = 5608
137737
YDOT = 6708
052700 feet/sec YDOT = 2044
614463 meter/sec
ZDOT = 14132
098598 ZDOT = 4307
463653
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20140
12499594
00016717 00000-0 10270-3 0 9041
2 25544 51
6392 132
3146 0001134 305
4402 54
6643 15
49395490 27506
Satellite: ISS
Catalog Number: 25544
Epoch time: 20140
12499594 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 132
3146 deg
Eccentricity:
0001134
Arg of perigee: 305
4402 deg
Mean anomaly: 54
6643 deg
Mean motion: 15
49395490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2750
Checksum: 291
Coasting Arc #6 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2020/141/01:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5236433
18 A = 6797026
98 meter
Y = -1994283
22 meter E =
0005593
Z = -3853660
39 I = 51
95028
XDOT = -651
057417 Wp = 66
18094
YDOT = 6374
515465 meter/sec RA = 126
58374 deg
ZDOT = -4186
109925 TA = 159
84024
MA = 159
81814
Ha = 228
223 n
mi
Hp = 222
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17179898
89 X = 5277063
82
Y = -6542923
94 feet Y = -1935498
20 meter
Z = -12643242
74 Z = -3828124
94
XDOT = -2136
015146 XDOT = -701
956721
YDOT = 20913
764648 feet/sec YDOT = 6366
950616 meter/sec
ZDOT = -13733
956446 ZDOT = -4189
395670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4046539
83 X = 1233385
34
Y = 18015046
93 feet Y = 5490986
30 meter
Z = -12525732
16 Z = -3817843
16
XDOT = -19103
166467 XDOT = -5822
645139
YDOT = -5262
843124 feet/sec YDOT = -1604
114584 meter/sec
ZDOT = -13749
307205 ZDOT = -4190
788836
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20141
09248740
00016717 00000-0 10270-3 0 9054
2 25544 51
6401 127
5259 0001164 315
8721 44
2328 15
49381278 27650
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
09248740 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 127
5259 deg
Eccentricity:
0001164
Arg of perigee: 315
8721 deg
Mean anomaly: 44
2328 deg
Mean motion: 15
49381278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 298
Coasting Arc #7 (Orbit 2774)
---------------------------------------
Vector Time (GMT): 2020/141/17:30:57
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -393271
99 A = 6797622
30 meter
Y = 5747482
88 meter E =
0004612
Z = -3611573
37 I = 51
96798
XDOT = -5744
231455 Wp = 81
90718
YDOT = 2402
413281 meter/sec RA = 123
27857 deg
ZDOT = 4454
211017 TA = 235
68927
MA = 235
73293
Ha = 228
258 n
mi
Hp = 222
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1290262
44 X = -439969
58
Y = 18856571
14 feet Y = 5742824
27 meter
Z = -11848994
01 Z = -3613596
66
XDOT = -18845
903724 XDOT = -5792
305389
YDOT = 7881
933338 feet/sec YDOT = 2337
907989 meter/sec
ZDOT = 14613
553207 ZDOT = 4426
190788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12886903
52 X = 3927928
19
Y = -13817988
05 feet Y = -4211722
76 meter
Z = -11858525
85 Z = -3614478
68
XDOT = 18642
090320 XDOT = 5682
109130
YDOT = 4970
800475 feet/sec YDOT = 1515
099985 meter/sec
ZDOT = 14484
588207 ZDOT = 4414
902485
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20141
73748029
00016717 00000-0 10270-3 0 9061
2 25544 51
6426 124
3383 0001593 331
4679 28
6383 15
49393848 27756
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
73748029 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 124
3383 deg
Eccentricity:
0001593
Arg of perigee: 331
4679 deg
Mean anomaly: 28
6383 deg
Mean motion: 15
49393848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2775
Checksum: 331
Coasting Arc #8 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2020/142/17:30:57
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 34595
10 A = 6798013
91 meter
Y = -5823320
97 meter E =
0011765
Z = 3498912
14 I = 51
98588
XDOT = 5521
285101 Wp = 81
58322
YDOT = -2718
569081 meter/sec RA = 118
35271 deg
ZDOT = -4564
400874 TA = 57
59582
MA = 57
48205
Ha = 228
363 n
mi
Hp = 222
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 113500
97 X = 82714
62
Y = -19105383
76 feet Y = -5822665
44 meter
Z = 11479370
54 Z = 3499196
42
XDOT = 18114
452430 XDOT = 5573
446220
YDOT = -8919
189898 feet/sec YDOT = -2656
533981 meter/sec
ZDOT = -14975
068483 ZDOT = -4537
453778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11880783
88 X = -3621262
93
Y = 14961279
38 feet Y = 4560197
95 meter
Z = 11480923
87 Z = 3499385
60
XDOT = -18729
324207 XDOT = -5708
698018
YDOT = -3439
516686 feet/sec YDOT = -1048
364686 meter/sec
ZDOT = -14851
007738 ZDOT = -4526
587158
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20142
76946865
00016717 00000-0 10270-3 0 9074
2 25544 51
6419 119
2313 0001570 338
6347 21
4738 15
49377291 27917
Satellite: ISS
Catalog Number: 25544
Epoch time: 20142
76946865 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 119
2313 deg
Eccentricity:
0001570
Arg of perigee: 338
6347 deg
Mean anomaly: 21
4738 deg
Mean motion: 15
49377291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2791
Checksum: 325
Coasting Arc #9 (Orbit 2794)
---------------------------------------
Vector Time (GMT): 2020/143/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4670609
36 A = 6793213
38 meter
Y = -744491
12 meter E =
0011532
Z = -4887266
48 I = 51
97165
XDOT = -1451
942195 Wp = 66
83426
YDOT = 7095
001369 meter/sec RA = 117
02686 deg
ZDOT = -2468
595085 TA = 178
98749
MA = 178
98516
Ha = 228
313 n
mi
Hp = 222
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15323521
52 X = 4702327
30
Y = -2442556
18 feet Y = -692083
13 meter
Z = -16034338
83 Z = -4864501
14
XDOT = -4763
589877 XDOT = -1519
181465
YDOT = 23277
563547 feet/sec YDOT = 7078
389049 meter/sec
ZDOT = -8099
065240 ZDOT = -2475
810657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5167778
76 X = -1575138
97
Y = 14745119
69 feet Y = 4494312
48 meter
Z = -15929592
67 Z = -4855339
84
XDOT = -17184
548848 XDOT = -5237
850489
YDOT = -14807
806988 feet/sec YDOT = -4513
419570 meter/sec
ZDOT = -8132
559952 ZDOT = -2478
804273
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20143
02746506
00016717 00000-0 10270-3 0 9085
2 25544 51
6392 117
9496 0001155 334
0340 26
0752 15
49393938 27953
Satellite: ISS
Catalog Number: 25544
Epoch time: 20143
02746506 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 117
9496 deg
Eccentricity:
0001155
Arg of perigee: 334
0340 deg
Mean anomaly: 26
0752 deg
Mean motion: 15
49393938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2795
Checksum: 312
Coasting Arc #10 (Orbit 2810)
---------------------------------------
Vector Time (GMT): 2020/144/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4561930
34 A = 6792949
65 meter
Y = 987886
72 meter E =
0005673
Z = 4931782
56 I = 51
98569
XDOT = 965
271756 Wp = 115
90761
YDOT = -7233
770011 meter/sec RA = 112
09950 deg
ZDOT = 2337
385433 TA = 311
29063
MA = 311
33946
Ha = 228
387 n
mi
Hp = 222
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14966963
07 X = -4596594
30
Y = 3241098
15 feet Y = 936677
47 meter
Z = 16180388
98 Z = 4909538
07
XDOT = 3166
902087 XDOT = 1034
736313
YDOT = -23732
841242 feet/sec YDOT = -7222
587574 meter/sec
ZDOT = 7668
587379 ZDOT = 2342
242150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4040719
28 X = 1231611
24
Y = -14882529
98 feet Y = -4536195
14 meter
Z = 16078015
35 Z = 4900579
08
XDOT = 18569
114275 XDOT = 5659
866031
YDOT = 13366
776067 feet/sec YDOT = 4074
193345 meter/sec
ZDOT = 7691
261452 ZDOT = 2344
296491
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20144
05945077
00016717 00000-0 10270-3 0 9094
2 25544 51
6397 112
8408 0001232 326
9188 33
1885 15
49407844 28118
Satellite: ISS
Catalog Number: 25544
Epoch time: 20144
05945077 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 112
8408 deg
Eccentricity:
0001232
Arg of perigee: 326
9188 deg
Mean anomaly: 33
1885 deg
Mean motion: 15
49407844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2811
Checksum: 316
Coasting Arc #11 (Orbit 2825)
---------------------------------------
Vector Time (GMT): 2020/145/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4456960
07 A = 6792764
13 meter
Y = -1209875
34 meter E =
0012271
Z = -4992660
91 I = 51
99806
XDOT = -468
908828 Wp = 68
28603
YDOT = 7315
387550 meter/sec RA = 107
17453 deg
ZDOT = -2191
249955 TA = 180
40054
MA = 180
40152
Ha = 228
332 n
mi
Hp = 222
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14622572
40 X = 4494409
82
Y = -3969407
28 feet Y = -1159824
28 meter
Z = -16380121
10 Z = -4970919
67
XDOT = -1538
414790 XDOT = -540
032828
YDOT = 24000
615320 feet/sec YDOT = 7309
746536 meter/sec
ZDOT = -7189
140272 ZDOT = -2193
699384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2979220
04 X = -908066
27
Y = 14965586
11 feet Y = 4561510
65 meter
Z = -16280038
86 Z = -4962155
84
XDOT = -19756
235519 XDOT = -6021
700586
YDOT = -11766
444704 feet/sec YDOT = -3586
412346 meter/sec
ZDOT = -7200
766478 ZDOT = -2194
793622
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20145
02693683
00016717 00000-0 10270-3 0 9107
2 25544 51
6413 108
0529 0001246 338
3334 21
7764 15
49397207 28269
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
02693683 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 108
0529 deg
Eccentricity:
0001246
Arg of perigee: 338
3334 deg
Mean anomaly: 21
7764 deg
Mean motion: 15
49397207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2826
Checksum: 300
Coasting Arc #12 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2020/145/22:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918884
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3506344
73 A = 6792093
58 meter
Y = 2733483
09 meter E =
0012946
Z = -5146280
22 I = 52
00263
XDOT = -2894
232676 Wp = 97
19712
YDOT = 6879
207235 meter/sec RA = 102
66458 deg
ZDOT = 1684
047983 TA = 189
01059
MA = 189
03385
Ha = 228
445 n
mi
Hp = 222
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11503755
69 X = 3500515
46
Y = 8968120
36 feet Y = 2772661
79 meter
Z = -16884121
45 Z = -5129261
29
XDOT = -9495
514028 XDOT = -2979
123132
YDOT = 22569
577542 feet/sec YDOT = 6846
366934 meter/sec
ZDOT = 5525
091808 ZDOT = 1669
783737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14606241
46 X = -4451982
40
Y = -1433405
25 feet Y = -436901
92 meter
Z = -16805957
12 Z = -5122455
73
XDOT = -4004
254715 XDOT = -1220
496837
YDOT = -23123
064762 feet/sec YDOT = -7047
910139 meter/sec
ZDOT = 5459
108319 ZDOT = 1663
936216
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20145
92992162
00016717 00000-0 10270-3 0 9111
2 25544 51
6400 103
5839 0001333 350
1284 9
9840 15
49393943 28404
Satellite: ISS
Catalog Number: 25544
Epoch time: 20145
92992162 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 103
5839 deg
Eccentricity:
0001333
Arg of perigee: 350
1284 deg
Mean anomaly: 9
9840 deg
Mean motion: 15
49393943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2840
Checksum: 299
Coasting Arc #13 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2020/146/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1002975
36 A = 6803109
07 meter
Y = 6719251
19 meter E =
0012773
Z = -192838
75 I = 52
04405
XDOT = -4687
161296 Wp = 37
76961
YDOT = -532
705649 meter/sec RA = 99
75852 deg
ZDOT = 6037
617609 TA = 320
16816
MA = 320
26184
Ha = 228
468 n
mi
Hp = 222
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3290601
56 X = -1077100
77
Y = 22044787
38 feet Y = 6707620
78 meter
Z = -632673
08 Z = -197889
75
XDOT = -15377
825773 XDOT = -4710
183583
YDOT = -1747
721946 feet/sec YDOT = -585
250572 meter/sec
ZDOT = 19808
456722 ZDOT = 6014
793022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18854230
63 X = 5746769
50
Y = 11886474
76 feet Y = 3622997
51 meter
Z = -656269
27 Z = -200030
87
XDOT = -6979
520596 XDOT = -2127
357878
YDOT = 12120
172878 feet/sec YDOT = 3694
228693 meter/sec
ZDOT = 19703
461931 ZDOT = 6005
615197
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20146
51041135
00016717 00000-0 10270-3 0 9123
2 25544 51
6406 100
7146 0001724 350
3927 9
7190 15
49394126 28499
Satellite: ISS
Catalog Number: 25544
Epoch time: 20146
51041135 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 100
7146 deg
Eccentricity:
0001724
Arg of perigee: 350
3927 deg
Mean anomaly: 9
7190 deg
Mean motion: 15
49394126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 286
Coasting Arc #14 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2020/147/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 542823
64 A = 6803151
27 meter
Y = -6776727
01 meter E =
0010818
Z = 39154
89 I = 52
04955
XDOT = 4698
849592 Wp = 128
27448
YDOT = 335
002435 meter/sec RA = 94
83704 deg
ZDOT = -6039
748552 TA = 51
30705
MA = 51
21034
Ha = 228
496 n
mi
Hp = 222
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1780917
47 X = 618372
48
Y = -22233356
35 feet Y = -6770234
36 meter
Z = 128460
92 Z = 41974
07
XDOT = 15416
173203 XDOT = 4724
092005
YDOT = 1099
089353 feet/sec YDOT = 387
690479 meter/sec
ZDOT = -19815
448004 ZDOT = -6016
861932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19812638
29 X = -6038892
15
Y = -10244489
16 feet Y = -3122520
30 meter
Z = 141807
54 Z = 43222
94
XDOT = 6282
717534 XDOT = 1914
972304
YDOT = -12469
653882 feet/sec YDOT = -3800
750503 meter/sec
ZDOT = -19710
148611 ZDOT = -6007
653297
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20147
54239329
00016717 00000-0 10270-3 0 9132
2 25544 51
6415 95
6071 0001765 352
0438 8
0684 15
49384821 28658
Satellite: ISS
Catalog Number: 25544
Epoch time: 20147
54239329 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 95
6071 deg
Eccentricity:
0001765
Arg of perigee: 352
0438 deg
Mean anomaly: 8
0684 deg
Mean motion: 15
49384821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 314
Coasting Arc #15 (Orbit 2880)
---------------------------------------
Vector Time (GMT): 2020/148/12:14:26
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -52105
47 A = 6803112
06 meter
Y = 6795416
91 meter E =
0013376
Z = 79655
95 I = 52
05140
XDOT = -4711
606443 Wp = 40
33141
YDOT = -113
456508 meter/sec RA = 89
91557 deg
ZDOT = 6041
523749 TA = 320
52024
MA = 320
61762
Ha = 228
509 n
mi
Hp = 222
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -170949
69 X = -128476
88
Y = 22294674
91 feet Y = 6794407
20 meter
Z = 261338
41 Z = 79218
44
XDOT = -15458
026389 XDOT = -4739
333808
YDOT = -372
232639 feet/sec YDOT = -166
301047 meter/sec
ZDOT = 19821
272141 ZDOT = 6018
569255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20639235
17 X = 6290838
88
Y = 8432376
54 feet Y = 2570188
37 meter
Z = 258936
89 Z = 78923
96
XDOT = -5515
045885 XDOT = -1680
985986
YDOT = 12836
834414 feet/sec YDOT = 3912
667129 meter/sec
ZDOT = 19715
640417 ZDOT = 6009
327199
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20148
57437261
00016717 00000-0 10270-3 0 9142
2 25544 51
6417 90
4998 0001768 354
1707 5
9422 15
49398970 28810
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
57437261 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 90
4998 deg
Eccentricity:
0001768
Arg of perigee: 354
1707 deg
Mean anomaly: 5
9422 deg
Mean motion: 15
49398970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2881
Checksum: 336
Coasting Arc #16 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2020/148/20:33:31
100
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3081327
38 A = 6797265
34 meter
Y = -4750663
32 meter E =
0011640
Z = 3752825
51 I = 52
03002
XDOT = 3187
365497 Wp = 76
67560
YDOT = -5479
033363 meter/sec RA = 88
17964 deg
ZDOT = -4304
999911 TA = 58
83547
MA = 58
72138
Ha = 228
513 n
mi
Hp = 222
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10109341
80 X = -3046204
09
Y = -15586165
74 feet Y = -4784925
11 meter
Z = 12312419
66 Z = 3737942
22
XDOT = 10457
235881 XDOT = 3269
307973
YDOT = -17975
831245 feet/sec YDOT = -5442
931137 meter/sec
ZDOT = -14124
015457 ZDOT = -4289
318787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13512498
94 X = 4118609
68
Y = 12814640
24 feet Y = 3905902
35 meter
Z = 12244198
62 Z = 3732031
74
XDOT = -5188
358499 XDOT = -1581
411670
YDOT = 18940
457124 feet/sec YDOT = 5773
051331 meter/sec
ZDOT = -14051
531902 ZDOT = -4282
906924
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20148
89686467
00016717 00000-0 10270-3 0 9152
2 25544 51
6400 88
9000 0001541 350
3110 9
8010 15
49390330 28866
Satellite: ISS
Catalog Number: 25544
Epoch time: 20148
89686467 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 88
9000 deg
Eccentricity:
0001541
Arg of perigee: 350
3110 deg
Mean anomaly: 9
8010 deg
Mean motion: 15
49390330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 292
Coasting Arc #17 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 954372
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3431845
59 A = 6794085
84 meter
Y = -3568882
69 meter E =
0010932
Z = -4663265
06 I = 52
02206
XDOT = 2719
536984 Wp = 62
29285
YDOT = 6503
001284 meter/sec RA = 86
54900 deg
ZDOT = -2975
868396 TA = 178
14317
MA = 178
13911
Ha = 228
545 n
mi
Hp = 222
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11259335
92 X = 3494150
25
Y = -11708932
72 feet Y = -3530156
29 meter
Z = -15299426
04 Z = -4646443
74
XDOT = 8922
365433 XDOT = 2661
071402
YDOT = 21335
306049 feet/sec YDOT = 6533
086624 meter/sec
ZDOT = -9763
347756 ZDOT = -2962
799011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16302564
85 X = 4969021
77
Y = -683602
41 feet Y = -208362
02 meter
Z = -15221801
96 Z = -4639605
24
XDOT = -8200
298479 XDOT = -2499
450976
YDOT = 20480
014262 feet/sec YDOT = 6242
308347 meter/sec
ZDOT = -9703
578384 ZDOT = -2957
650692
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20149
21935824
00016717 00000-0 10270-3 0 9164
2 25544 51
6431 87
3066 0001583 359
6092
5057 15
49390011 28913
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
21935824 = yrday
fracday
Element set: 916
Inclination: 51
6431 deg
RA of node: 87
3066 deg
Eccentricity:
0001583
Arg of perigee: 359
6092 deg
Mean anomaly:
5057 deg
Mean motion: 15
49390011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 301
Coasting Arc #18 (Orbit 2897)
---------------------------------------
Vector Time (GMT): 2020/149/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1359789
99 A = 6802860
59 meter
Y = -6598577
47 meter E =
0012473
Z = 903733
08 I = 52
05127
XDOT = 4492
583852 Wp = 118
79387
YDOT = -1748
862366 meter/sec RA = 84
36050 deg
ZDOT = -5953
354777 TA = 51
49985
MA = 51
38806
Ha = 228
603 n
mi
Hp = 222
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4461253
26 X = -1290291
48
Y = -21648876
23 feet Y = -6613395
15 meter
Z = 2965003
55 Z = 897295
65
XDOT = 14739
448334 XDOT = 4540
724154
YDOT = -5737
737421 feet/sec YDOT = -1698
353090 meter/sec
ZDOT = -19532
003860 ZDOT = -5931
414948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17730774
92 X = -5404340
20
Y = 13204876
66 feet Y = 4024846
41 meter
Z = 2935765
97 Z = 894821
47
XDOT = -10519
831745 XDOT = -3206
444716
YDOT = -9764
076344 feet/sec YDOT = -2976
090470 meter/sec
ZDOT = -19430
925745 ZDOT = -5922
546167
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20149
67084892
00016717 00000-0 10270-3 0 9175
2 25544 51
6443 85
0744 0001737 359
8193
2956 15
49369843 28980
Satellite: ISS
Catalog Number: 25544
Epoch time: 20149
67084892 = yrday
fracday
Element set: 917
Inclination: 51
6443 deg
RA of node: 85
0744 deg
Eccentricity:
0001737
Arg of perigee: 359
8193 deg
Mean anomaly:
2956 deg
Mean motion: 15
49369843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2898
Checksum: 349
Coasting Arc #19 (Orbit 2912)
---------------------------------------
Vector Time (GMT): 2020/150/15:17:02
000
Vector Time (MET): N/A
Weight (LBS) : 981788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1834246
89 A = 6802805
19 meter
Y = 6497422
42 meter E =
0011850
Z = -784889
66 I = 52
04660
XDOT = -4378
097224 Wp = 33
87708
YDOT = 1951
546144 meter/sec RA = 79
43800 deg
ZDOT = 5976
636084 TA = 317
70158
MA = 317
79291
Ha = 228
572 n
mi
Hp = 222
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6017870
37 X = 1765266
99
Y = 21317002
69 feet Y = 6517548
68 meter
Z = -2575097
31 Z = -776146
39
XDOT = -14363
836038 XDOT = -4428
625600
YDOT = 6402
710445 feet/sec YDOT = 1902
303908 meter/sec
ZDOT = 19608
386102 ZDOT = 5955
246567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16522265
72 X = 5035986
59
Y = -14759665
71 feet Y = -4498746
11 meter
Z = -2535250
97 Z = -772744
49
XDOT = 11028
563252 XDOT = 3361
506079
YDOT = 9024
673596 feet/sec YDOT = 2750
720512 meter/sec
ZDOT = 19509
822725 ZDOT = 5946
593967
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20150
63832497
00016717 00000-0 10270-3 0 9186
2 25544 51
6438 80
2856 0001901
0095
1055 15
49417269 29137
Satellite: ISS
Catalog Number: 25544
Epoch time: 20150
63832497 = yrday
fracday
Element set: 918
Inclination: 51
6438 deg
RA of node: 80
2856 deg
Eccentricity:
0001901
Arg of perigee:
0095 deg
Mean anomaly:
1055 deg
Mean motion: 15
49417269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2913
Checksum: 287
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