[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 15th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14537 7374 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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
108/01:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
6
000/00:00:00
000 0
0 0
0 222
1
110/05:09:32
740 1
1 -3
0 3
0
N/A -2
8 0
2 228
6
000/00:01:01
479 0
4 -0
1 222
2
113/03:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
3
Coasting Arc #1 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2020/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936071
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4090002
11 A = 6793640
14 meter
Y = -1544130
87 meter E =
0017329
Z = -5215309
78 I = 51
31604
XDOT = 3893
399403 Wp = 87
44845
YDOT = -6482
396340 meter/sec RA = 307
90168 deg
ZDOT = -1136
568315 TA = 171
58936
MA = 171
56028
Ha = 230
808 n
mi
Hp = 221
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13418642
11 X = -4047098
16
Y = -5066046
17 feet Y = -1589628
22 meter
Z = -17110596
39 Z = -5235073
27
XDOT = 12773
620089 XDOT = 3971
118922
YDOT = -21267
704528 feet/sec YDOT = -6438
423005 meter/sec
ZDOT = -3728
898670 ZDOT = -1117
466991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14234141
24 X = -4338566
25
Y = 95190
87 feet Y = 29014
18 meter
Z = -17201088
64 Z = -5242891
82
XDOT = 4233
182259 XDOT = 1290
273953
YDOT = -23421
548523 feet/sec YDOT = -7138
887990 meter/sec
ZDOT = -3640
900290 ZDOT = -1109
746408
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 20104
51807568
00016717 00000-0 10270-3 0 9004
2 25544 51
6403 308
5116 0003580 113
5023 246
6503 15
48693036 21987
Satellite: ISS
Catalog Number: 25544
Epoch time: 20104
51807568 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 308
5116 deg
Eccentricity:
0003580
Arg of perigee: 113
5023 deg
Mean anomaly: 246
6503 deg
Mean motion: 15
48693036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 285
Coasting Arc #2 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2020/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936071
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4255648
25 A = 6793815
10 meter
Y = 1067442
96 meter E =
0007640
Z = 5182077
90 I = 51
29730
XDOT = -3237
708926 Wp = 120
43829
YDOT = 6833
884551 meter/sec RA = 302
93663 deg
ZDOT = 1246
011123 TA = 317
50778
MA = 317
56690
Ha = 230
699 n
mi
Hp = 222
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13962100
55 X = 4218223
96
Y = 3502109
45 feet Y = 1114823
34 meter
Z = 17001567
92 Z = 5202659
26
XDOT = -10622
404613 XDOT = -3319
939213
YDOT = 22420
881072 feet/sec YDOT = 6797
218396 meter/sec
ZDOT = 4087
963001 ZDOT = 1230
083963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14142700
49 X = 4310695
11
Y = -1993612
26 feet Y = -607653
02 meter
Z = 17095843
57 Z = 5210813
12
XDOT = -1524
994637 XDOT = -464
818365
YDOT = 23752
225448 feet/sec YDOT = 7239
678317 meter/sec
ZDOT = 4014
504962 ZDOT = 1223
621113
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 20105
55052686
00016717 00000-0 10270-3 0 9013
2 25544 51
6410 303
4068 0003574 117
0527 243
0988 15
48658850 22148
Satellite: ISS
Catalog Number: 25544
Epoch time: 20105
55052686 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 303
4068 deg
Eccentricity:
0003574
Arg of perigee: 117
0527 deg
Mean anomaly: 243
0988 deg
Mean motion: 15
48658850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 295
Coasting Arc #3 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2020/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936071
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4379167
39 A = 6793810
56 meter
Y = -598758
40 meter E =
0016870
Z = -5174304
00 I = 51
27909
XDOT = 2546
925621 Wp = 87
67179
YDOT = -7085
031930 meter/sec RA = 297
96902 deg
ZDOT = -1338
807913 TA = 169
37858
MA = 169
34290
Ha = 230
787 n
mi
Hp = 221
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14367347
07 X = -4347012
71
Y = -1964430
46 feet Y = -647549
59 meter
Z = -16976063
01 Z = -5195498
11
XDOT = 8356
055186 XDOT = 2632
466391
YDOT = -23244
855415 feet/sec YDOT = -7056
072111 meter/sec
ZDOT = -4392
414413 ZDOT = -1326
228213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13872988
56 X = -4228486
91
Y = 3809605
68 feet Y = 1161167
81 meter
Z = -17073179
47 Z = -5203905
10
XDOT = -1174
814373 XDOT = -358
083421
YDOT = -23657
050406 feet/sec YDOT = -7210
668964 meter/sec
ZDOT = -4334
301543 ZDOT = -1321
095110
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 20106
51844596
00016717 00000-0 10270-3 0 9020
2 25544 51
6397 298
6201 0003641 120
0943 240
0568 15
48692688 22291
Satellite: ISS
Catalog Number: 25544
Epoch time: 20106
51844596 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 298
6201 deg
Eccentricity:
0003641
Arg of perigee: 120
0943 deg
Mean anomaly: 240
0568 deg
Mean motion: 15
48692688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 315
Coasting Arc #4 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2020/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936071
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4437894
12 A = 6794019
62 meter
Y = 94523
62 meter E =
0008207
Z = 5138479
81 I = 51
26409
XDOT = -1837
530581 Wp = 123
78809
YDOT = 7298
283005 meter/sec RA = 293
00166 deg
ZDOT = 1446
589339 TA = 312
17349
MA = 312
24317
Ha = 230
695 n
mi
Hp = 222
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14560020
07 X = 4411547
61
Y = 310116
86 feet Y = 144004
08 meter
Z = 16858529
56 Z = 5159973
27
XDOT = -6028
643637 XDOT = -1926
032245
YDOT = 23944
498048 feet/sec YDOT = 7277
239610 meter/sec
ZDOT = 4746
028016 ZDOT = 1437
448300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13303927
89 X = 4055037
22
Y = -5635985
98 feet Y = -1717848
53 meter
Z = 16957049
87 Z = 5168508
80
XDOT = 3873
237548 XDOT = 1180
562805
YDOT = 23355
345397 feet/sec YDOT = 7118
709277 meter/sec
ZDOT = 4703
683741 ZDOT = 1433
682804
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 20107
55089445
00016717 00000-0 10270-3 0 9030
2 25544 51
6391 293
5154 0003658 123
0524 237
0977 15
48652771 22459
Satellite: ISS
Catalog Number: 25544
Epoch time: 20107
55089445 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 293
5154 deg
Eccentricity:
0003658
Arg of perigee: 123
0524 deg
Mean anomaly: 237
0977 deg
Mean motion: 15
48652771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 313
Coasting Arc #5 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4615402
99 A = 6795554
21 meter
Y = -1565171
92 meter E =
0011191
Z = 4729828
54 I = 51
26266
XDOT = -333
008617 Wp = 120
09179
YDOT = 7169
167617 meter/sec RA = 290
13824 deg
ZDOT = 2687
034111 TA = 303
14204
MA = 303
24937
Ha = 230
574 n
mi
Hp = 222
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15142398
25 X = 4609587
47
Y = -5135078
47 feet Y = -1513591
60 meter
Z = 15517810
17 Z = 4752234
19
XDOT = -1092
547956 XDOT = -426
203643
YDOT = 23520
891131 feet/sec YDOT = 7164
922658 meter/sec
ZDOT = 8815
728712 ZDOT = 2685
189961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4945512
53 X = -1507392
22
Y = 15099740
23 feet Y = 4602400
82 meter
Z = 15620609
43 Z = 4761161
75
XDOT = -16993
706216 XDOT = -5179
681655
YDOT = -14711
220059 feet/sec YDOT = -4483
979874 meter/sec
ZDOT = 8806
852364 ZDOT = 2684
328601
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 20108
13164441
00016717 00000-0 10270-3 0 9046
2 25544 51
6392 290
6465 0003588 125
6476 234
5009 15
48713339 22545
Satellite: ISS
Catalog Number: 25544
Epoch time: 20108
13164441 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 290
6465 deg
Eccentricity:
0003588
Arg of perigee: 125
6476 deg
Mean anomaly: 234
5009 deg
Mean motion: 15
48713339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 305
Coasting Arc #6 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2020/109/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4467422
76 A = 6795777
66 meter
Y = 2052682
23 meter E =
0013217
Z = -4703689
34 I = 51
25296
XDOT = -367
693946 Wp = 84
12615
YDOT = -7122
679726 meter/sec RA = 285
16791 deg
ZDOT = -2764
516038 TA = 158
29526
MA = 158
23920
Ha = 230
721 n
mi
Hp = 221
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14656898
82 X = -4467196
65
Y = 6734521
74 feet Y = 2002725
41 meter
Z = -15432051
63 Z = -4725389
81
XDOT = -1206
344967 XDOT = -274
590298
YDOT = -23368
371806 feet/sec YDOT = -7126
271070 meter/sec
ZDOT = -9069
934507 ZDOT = -2766
075749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3106057
14 X = 946726
21
Y = -15730455
72 feet Y = -4794642
90 meter
Z = -15531640
47 Z = -4734044
01
XDOT = 18431
176971 XDOT = 5617
822741
YDOT = 12583
863359 feet/sec YDOT = 3835
561552 meter/sec
ZDOT = -9076
683339 ZDOT = -2766
573082
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 20109
09956345
00016717 00000-0 10270-3 0 9055
2 25544 51
6394 285
8600 0003648 127
8419 232
3061 15
48687155 22698
Satellite: ISS
Catalog Number: 25544
Epoch time: 20109
09956345 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 285
8600 deg
Eccentricity:
0003648
Arg of perigee: 127
8419 deg
Mean anomaly: 232
3061 deg
Mean motion: 15
48687155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 327
Coasting Arc #7 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2020/110/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 920963
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4247573
66 A = 6795836
89 meter
Y = -2551045
68 meter E =
0011491
Z = 4645427
41 I = 51
24687
XDOT = 1073
210706 Wp = 120
95001
YDOT = 7025
524486 meter/sec RA = 280
19869 deg
ZDOT = 2865
679310 TA = 300
33845
MA = 300
45205
Ha = 230
455 n
mi
Hp = 222
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13935609
11 X = 4253219
67
Y = -8369572
43 feet Y = -2503514
50 meter
Z = 15240903
57 Z = 4666074
30
XDOT = 3521
032501 XDOT = 980
649607
YDOT = 23049
621017 feet/sec YDOT = 7037
008481 meter/sec
ZDOT = 9401
835008 ZDOT = 2870
667417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1082784
47 X = -330032
71
Y = 16130111
20 feet Y = 4916457
89 meter
Z = 15335683
09 Z = 4674316
21
XDOT = -19685
308519 XDOT = -6000
082037
YDOT = -10316
026597 feet/sec YDOT = -3144
324907 meter/sec
ZDOT = 9424
322984 ZDOT = 2872
533645
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 20110
13200546
00016717 00000-0 10270-3 0 9068
2 25544 51
6403 280
7558 0003499 133
5307 226
6133 15
48735508 22859
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
13200546 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 280
7558 deg
Eccentricity:
0003499
Arg of perigee: 133
5307 deg
Mean anomaly: 226
6133 deg
Mean motion: 15
48735508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 291
Coasting Arc #8 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2020/110/05:10:03
479
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3765250
34 A = 6792206
55 meter
Y = 2394904
61 meter E =
0004238
Z = 5117379
95 I = 51
24129
XDOT = -2433
500675 Wp = 74
73001
YDOT = 7103
514623 meter/sec RA = 279
48440 deg
ZDOT = -1531
728207 TA = 30
13396
MA = 30
10959
Ha = 228
593 n
mi
Hp = 222
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12353183
53 X = 3713332
63
Y = 7857298
59 feet Y = 2436720
26 meter
Z = 16789304
29 Z = 5135543
87
XDOT = -7983
926100 XDOT = -2505
313147
YDOT = 23305
494171 feet/sec YDOT = 7075
899887 meter/sec
ZDOT = -5025
355011 ZDOT = -1543
723962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4571659
56 X = -1393441
83
Y = 13807237
22 feet Y = 4208445
90 meter
Z = 16872437
64 Z = 5142718
99
XDOT = -23542
638203 XDOT = -7175
796124
YDOT = -1577
845116 feet/sec YDOT = -480
927191 meter/sec
ZDOT = -5080
720374 ZDOT = -1548
603570
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 20110
26103949
00016717 00000-0 10270-3 0 9072
2 25544 51
6421 280
1178 0001657 175
0095 185
1071 15
49309909 22875
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
26103949 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 280
1178 deg
Eccentricity:
0001657
Arg of perigee: 175
0095 deg
Mean anomaly: 185
1071 deg
Mean motion: 15
49309909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 301
Coasting Arc #9 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2020/111/05:10:03
479
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3933890
01 A = 6792405
63 meter
Y = -2189723
63 meter E =
0014000
Z = -5098578
48 I = 51
23787
XDOT = 1892
947110 Wp = 108
89103
YDOT = -7227
540548 meter/sec RA = 274
50765 deg
ZDOT = 1642
806769 TA = 177
09950
MA = 177
09137
Ha = 228
776 n
mi
Hp = 222
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12906463
29 X = -3884345
40
Y = -7184132
64 feet Y = -2233438
41 meter
Z = -16727619
69 Z = -5117567
43
XDOT = 6210
456399 XDOT = 1965
647065
YDOT = -23712
403374 feet/sec YDOT = -7205
965697 meter/sec
ZDOT = 5389
785986 ZDOT = 1652
178927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3537638
80 X = 1078272
31
Y = -14239305
68 feet Y = -4340140
37 meter
Z = -16814550
32 Z = -5125074
94
XDOT = 23462
040344 XDOT = 7151
229897
YDOT = -589
556515 feet/sec YDOT = -179
696826 meter/sec
ZDOT = 5433
113858 ZDOT = 1656
013104
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 20111
22859135
00016717 00000-0 10270-3 0 9085
2 25544 51
6426 275
3292 0001649 174
7453 185
3715 15
49285184 23021
Satellite: ISS
Catalog Number: 25544
Epoch time: 20111
22859135 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 275
3292 deg
Eccentricity:
0001649
Arg of perigee: 174
7453 deg
Mean anomaly: 185
3715 deg
Mean motion: 15
49285184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 310
Coasting Arc #10 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2020/112/05:10:03
479
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4078347
38 A = 6792418
18 meter
Y = 1969285
91 meter E =
0004522
Z = 5058844
05 I = 51
23642
XDOT = -1354
015656 Wp = 71
80777
YDOT = 7334
348617 meter/sec RA = 269
53192 deg
ZDOT = -1760
812434 TA = 35
34548
MA = 35
31551
Ha = 228
478 n
mi
Hp = 222
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13380404
80 X = 4031449
94
Y = 6460911
79 feet Y = 2014630
89 meter
Z = 16597257
39 Z = 5078541
25
XDOT = -4442
308583 XDOT = -1427
376783
YDOT = 24062
823546 feet/sec YDOT = 7318
796788 meter/sec
ZDOT = -5776
943682 ZDOT = -1767
568261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2464518
18 X = -751185
14
Y = 14550008
03 feet Y = 4434842
45 meter
Z = 16687449
86 Z = 5086334
72
XDOT = -23267
671939 XDOT = -7091
986407
YDOT = 2730
448985 feet/sec YDOT = 832
240851 meter/sec
ZDOT = -5808
268135 ZDOT = -1770
360128
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 20112
26064461
00016717 00000-0 10270-3 0 9091
2 25544 51
6422 270
2224 0001623 183
5688 176
5451 15
49321056 23181
Satellite: ISS
Catalog Number: 25544
Epoch time: 20112
26064461 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 270
2224 deg
Eccentricity:
0001623
Arg of perigee: 183
5688 deg
Mean anomaly: 176
5451 deg
Mean motion: 15
49321056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2318
Checksum: 286
Coasting Arc #11 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2020/113/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1067596
73 A = 6801707
40 meter
Y = 6402005
44 meter E =
0007862
Z = -2023700
19 I = 51
26811
XDOT = -4668
614971 Wp = 148
08234
YDOT = -2519
461918 meter/sec RA = 264
98510 deg
ZDOT = -5523
870941 TA = 54
34932
MA = 54
27614
Ha = 228
644 n
mi
Hp = 222
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3502613
95 X = -1129276
40
Y = 21003954
86 feet Y = 6389721
88 meter
Z = -6639436
30 Z = -2029036
23
XDOT = -15316
978250 XDOT = -4613
262478
YDOT = -8265
951175 feet/sec YDOT = -2571
360377 meter/sec
ZDOT = -18122
936158 ZDOT = -5546
415004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19892241
55 X = -6063155
22
Y = -7576526
47 feet Y = -2309325
27 meter
Z = -6664196
23 Z = -2031247
01
XDOT = 10578
273732 XDOT = 3224
257833
YDOT = -11789
145022 feet/sec YDOT = -3593
331403 meter/sec
ZDOT = -18226
156509 ZDOT = -5555
332504
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 20113
16369240
00016717 00000-0 10270-3 0 9106
2 25544 51
6420 265
7523 0001627 185
5010 174
6122 15
49283549 23329
Satellite: ISS
Catalog Number: 25544
Epoch time: 20113
16369240 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 265
7523 deg
Eccentricity:
0001627
Arg of perigee: 185
5010 deg
Mean anomaly: 174
6122 deg
Mean motion: 15
49283549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 279
Coasting Arc #12 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2020/114/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 581101
97 A = 6801585
18 meter
Y = -6435466
18 meter E =
0013220
Z = 2105679
29 I = 51
27194
XDOT = 4859
453916 Wp = 75
76046
YDOT = 2241
235546 meter/sec RA = 260
01029 deg
ZDOT = 5482
835546 TA = 307
64053
MA = 307
76042
Ha = 228
632 n
mi
Hp = 222
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1906502
54 X = 642793
73
Y = -21113734
19 feet Y = -6428622
91 meter
Z = 6908396
62 Z = 2108652
05
XDOT = 15943
090275 XDOT = 4807
397696
YDOT = 7353
134994 feet/sec YDOT = 2295
286449 meter/sec
ZDOT = 17988
305598 ZDOT = 5506
314763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20419218
92 X = 6223777
93
Y = 5682211
52 feet Y = 1731938
07 meter
Z = 6922314
51 Z = 2109921
46
XDOT = -9703
989520 XDOT = -2957
776006
YDOT = 12723
320741 feet/sec YDOT = 3878
068162 meter/sec
ZDOT = 18095
832002 ZDOT = 5515
609594
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 20114
19574355
00016717 00000-0 10270-3 0 9116
2 25544 51
6422 260
6449 0001543 188
0528 172
0598 15
49280645 23481
Satellite: ISS
Catalog Number: 25544
Epoch time: 20114
19574355 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 260
6449 deg
Eccentricity:
0001543
Arg of perigee: 188
0528 deg
Mean anomaly: 172
0598 deg
Mean motion: 15
49280645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 311
Coasting Arc #13 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2020/115/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -126563
79 A = 6801370
97 meter
Y = 6424359
24 meter E =
0007061
Z = -2221495
80 I = 51
27926
XDOT = -5030
867628 Wp = 147
33081
YDOT = -1971
023157 meter/sec RA = 255
03641 deg
ZDOT = -5427
336063 TA = 57
42801
MA = 57
35985
Ha = 228
582 n
mi
Hp = 222
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -415235
53 X = -187602
53
Y = 21077294
10 feet Y = 6422602
63 meter
Z = -7288372
06 Z = -2222258
86
XDOT = -16505
471221 XDOT = -4982
089802
YDOT = -6466
611409 feet/sec YDOT = -2027
009160 meter/sec
ZDOT = -17806
220678 ZDOT = -5451
656004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20725351
46 X = -6317087
13
Y = -3850903
75 feet Y = -1173755
46 meter
Z = -7292150
67 Z = -2222647
53
XDOT = 8810
603646 XDOT = 2685
471991
YDOT = -13575
570392 feet/sec YDOT = -4137
833856 meter/sec
ZDOT = -17917
620873 ZDOT = -5461
290842
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 20115
16328963
00016717 00000-0 10270-3 0 9127
2 25544 51
6432 255
8571 0001540 192
4149 167
6963 15
49281287 23635
Satellite: ISS
Catalog Number: 25544
Epoch time: 20115
16328963 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 255
8571 deg
Eccentricity:
0001540
Arg of perigee: 192
4149 deg
Mean anomaly: 167
6963 deg
Mean motion: 15
49281287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 316
Coasting Arc #14 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2020/116/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -352082
21 A = 6801232
50 meter
Y = -6383955
36 meter E =
0013044
Z = 2303035
09 I = 51
28808
XDOT = 5192
507309 Wp = 77
99466
YDOT = 1663
768116 meter/sec RA = 250
06297 deg
ZDOT = 5382
440207 TA = 307
74665
MA = 307
86478
Ha = 228
559 n
mi
Hp = 222
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1155125
35 X = -291855
79
Y = -20944735
42 feet Y = -6387555
89 meter
Z = 7555889
41 Z = 2301470
93
XDOT = 17035
785136 XDOT = 5147
371356
YDOT = 5458
556812 feet/sec YDOT = 1721
581941 meter/sec
ZDOT = 17658
924565 ZDOT = 5407
554238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20891056
41 X = 6367593
99
Y = 1919441
43 feet Y = 585045
75 meter
Z = 7548988
54 Z = 2300931
71
XDOT = -7772
678588 XDOT = -2369
112434
YDOT = 14392
843705 feet/sec YDOT = 4386
938761 meter/sec
ZDOT = 17773
988022 ZDOT = 5417
511549
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 20116
19533931
00016717 00000-0 10270-3 0 9135
2 25544 51
6427 250
7501 0001470 196
1146 163
9958 15
49279796 23798
Satellite: ISS
Catalog Number: 25544
Epoch time: 20116
19533931 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 250
7501 deg
Eccentricity:
0001470
Arg of perigee: 196
1146 deg
Mean anomaly: 163
9958 deg
Mean motion: 15
49279796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 327
Coasting Arc #15 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2020/117/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 793028
43 A = 6801024
48 meter
Y = 6305045
86 meter E =
0006244
Z = -2416988
69 I = 51
30095
XDOT = -5334
719142 Wp = 147
90210
YDOT = -1364
768340 meter/sec RA = 245
09083 deg
ZDOT = -5322
087715 TA = 59
19575
MA = 59
13431
Ha = 228
464 n
mi
Hp = 222
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2601799
32 X = 734205
15
Y = 20685846
00 feet Y = 6313585
27 meter
Z = -7929752
92 Z = -2413279
01
XDOT = -17502
359391 XDOT = -5293
209315
YDOT = -4477
586418 feet/sec YDOT = -1424
192648 meter/sec
ZDOT = -17460
917701 ZDOT = -5347
901369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20854999
59 X = -6356603
88
Y = -89152
72 feet Y = -27173
75 meter
Z = -7913002
58 Z = -2411883
19
XDOT = 6720
310095 XDOT = 2048
350517
YDOT = -15122
134553 feet/sec YDOT = -4609
226612 meter/sec
ZDOT = -17579
213032 ZDOT = -5358
144132
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 20117
16288339
00016717 00000-0 10270-3 0 9143
2 25544 51
6437 245
9628 0001660 205
8394 154
2673 15
49273483 23940
Satellite: ISS
Catalog Number: 25544
Epoch time: 20117
16288339 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 245
9628 deg
Eccentricity:
0001660
Arg of perigee: 205
8394 deg
Mean anomaly: 154
2673 deg
Mean motion: 15
49273483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 327
Coasting Arc #16 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2020/118/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1250892
16 A = 6800822
84 meter
Y = -6194037
72 meter E =
0012759
Z = 2499478
85 I = 51
31579
XDOT = 5462
403585 Wp = 79
96855
YDOT = 1032
873907 meter/sec RA = 240
11843 deg
ZDOT = 5272
431749 TA = 308
14335
MA = 308
25828
Ha = 228
440 n
mi
Hp = 222
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4103976
90 X = -1193676
84
Y = -20321646
08 feet Y = -6207706
32 meter
Z = 8200389
94 Z = 2493541
03
XDOT = 17921
271604 XDOT = 5424
836881
YDOT = 3388
693920 feet/sec YDOT = 1093
748036 meter/sec
ZDOT = 17298
004426 ZDOT = 5298
875166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20663840
24 X = 6298338
50
Y = -1805391
32 feet Y = -550283
27 meter
Z = 8173407
48 Z = 2491254
60
XDOT = -5537
542965 XDOT = -1687
843096
YDOT = 15791
246088 feet/sec YDOT = 4813
171808 meter/sec
ZDOT = 17419
214739 ZDOT = 5309
376652
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 20118
19492849
00016717 00000-0 10270-3 0 9151
2 25544 51
6439 240
8552 0001391 208
7740 151
3333 15
49288353 24102
Satellite: ISS
Catalog Number: 25544
Epoch time: 20118
19492849 = yrday
fracday
Element set: 915
Inclination: 51
6439 deg
RA of node: 240
8552 deg
Eccentricity:
0001391
Arg of perigee: 208
7740 deg
Mean anomaly: 151
3333 deg
Mean motion: 15
49288353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 307
Coasting Arc #17 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2020/119/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 920645
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1666663
92 A = 6800619
83 meter
Y = 6051812
87 meter E =
0005403
Z = -2612490
27 I = 51
33229
XDOT = -5570
568076 Wp = 144
45035
YDOT = -709
130654 meter/sec RA = 235
14859 deg
ZDOT = -5206
253480 TA = 65
02998
MA = 64
97387
Ha = 228
394 n
mi
Hp = 222
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5468057
49 X = 1611557
01
Y = 19855029
09 feet Y = 6070142
74 meter
Z = -8571162
29 Z = -2604527
62
XDOT = -18276
141982 XDOT = -5536
935084
YDOT = -2326
544141 feet/sec YDOT = -771
236303 meter/sec
ZDOT = -17080
884120 ZDOT = -5233
231766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20298411
87 X = -6186955
94
Y = 3566094
58 feet Y = 1086945
63 meter
Z = -8534875
55 Z = -2601430
07
XDOT = 4345
182446 XDOT = 1324
411609
YDOT = -16366
412641 feet/sec YDOT = -4988
482573 meter/sec
ZDOT = -17204
575587 ZDOT = -5243
954639
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 20119
16246882
00016717 00000-0 10270-3 0 9164
2 25544 51
6434 236
0681 0001546 214
3596 145
7454 15
49275047 24254
Satellite: ISS
Catalog Number: 25544
Epoch time: 20119
16246882 = yrday
fracday
Element set: 916
Inclination: 51
6434 deg
RA of node: 236
0681 deg
Eccentricity:
0001546
Arg of perigee: 214
3596 deg
Mean anomaly: 145
7454 deg
Mean motion: 15
49275047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 312
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