[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 20th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14538 8138 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
234/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
1
238/20:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
245/23:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
Coasting Arc #1 (Orbit 183)
---------------------------------------
Vector Time (GMT): 2020/232/14:41:08
714
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5948823
32 A = 6799830
86 meter
Y = 1041491
98 meter E =
0005633
Z = -3126741
97 I = 51
86967
XDOT = 1570
169367 Wp = 67
60362
YDOT = 5678
586671 meter/sec RA = 33
90910 deg
ZDOT = 4887
963272 TA = 256
62923
MA = 256
69204
Ha = 229
242 n
mi
Hp = 222
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19517136
87 X = 5951922
48
Y = 3416968
43 feet Y = 1108033
30 meter
Z = -10258339
81 Z = -3097838
08
XDOT = 5151
474300 XDOT = 1482
810647
YDOT = 18630
533697 feet/sec YDOT = 5695
656986 meter/sec
ZDOT = 16036
624908 ZDOT = 4895
378172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19869091
11 X = -6056098
97
Y = -729854
92 feet Y = -222459
78 meter
Z = -10124938
07 Z = -3086081
12
XDOT = -7574
056500 XDOT = -2308
572421
YDOT = -16327
028568 feet/sec YDOT = -4976
478308 meter/sec
ZDOT = 16070
533258 ZDOT = 4898
298537
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 20232
61824917
00016717 00000-0 10270-3 0 9004
2 25544 51
6431 34
5514 0001221 47
1989 312
9263 15
49148138 1841
Satellite: ISS
Catalog Number: 25544
Epoch time: 20232
61824917 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 34
5514 deg
Eccentricity:
0001221
Arg of perigee: 47
1989 deg
Mean anomaly: 312
9263 deg
Mean motion: 15
49148138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 184
Checksum: 289
Coasting Arc #2 (Orbit 199)
---------------------------------------
Vector Time (GMT): 2020/233/14:41:08
714
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6037858
93 A = 6800000
15 meter
Y = -597586
31 meter E =
0014017
Z = 3057236
06 I = 51
84184
XDOT = -1963
003223 Wp = 93
41506
YDOT = -5521
645879 meter/sec RA = 28
97576 deg
ZDOT = -4937
399732 TA = 51
67586
MA = 51
54993
Ha = 229
293 n
mi
Hp = 222
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19809248
45 X = -6045577
80
Y = -1960585
00 feet Y = -665149
05 meter
Z = 10030302
03 Z = 3027888
36
XDOT = -6440
299289 XDOT = -1877
130050
YDOT = -18115
636087 feet/sec YDOT = -5543
117564 meter/sec
ZDOT = -16198
818019 ZDOT = -4946
726335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19943642
81 X = 6078822
33
Y = -1095676
29 feet Y = -333962
13 meter
Z = 9894836
10 Z = 3015946
04
XDOT = 8939
640009 XDOT = 2724
802275
YDOT = 15484
256360 feet/sec YDOT = 4719
601339 meter/sec
ZDOT = -16241
558425 ZDOT = -4950
427008
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 20233
65037980
00016717 00000-0 10270-3 0 9016
2 25544 51
6434 29
4447 0001151 58
8822 301
2440 15
49152661 2002
Satellite: ISS
Catalog Number: 25544
Epoch time: 20233
65037980 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 29
4447 deg
Eccentricity:
0001151
Arg of perigee: 58
8822 deg
Mean anomaly: 301
2440 deg
Mean motion: 15
49152661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 200
Checksum: 272
Coasting Arc #3 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2020/234/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5178752
09 A = 6802288
78 meter
Y = -4013879
35 meter E =
0006963
Z = -1822094
69 I = 51
82478
XDOT = 4248
980822 Wp = 128
34980
YDOT = -2921
280169 meter/sec RA = 25
14883 deg
ZDOT = -5660
048499 TA = 71
57682
MA = 71
50113
Ha = 229
148 n
mi
Hp = 222
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16990656
46 X = -5124632
24
Y = -13168895
51 feet Y = -4071489
33 meter
Z = -5978000
95 Z = -1847119
04
XDOT = 13940
225794 XDOT = 4308
824499
YDOT = -9584
252524 feet/sec YDOT = -2873
430628 meter/sec
ZDOT = -18569
712923 ZDOT = -5639
263491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5946374
79 X = -1812455
03
Y = 20624040
90 feet Y = 6286207
67 meter
Z = -6093297
57 Z = -1857237
10
XDOT = -12613
491796 XDOT = -3844
592299
YDOT = -9076
756368 feet/sec YDOT = -2766
595341 meter/sec
ZDOT = -18473
583114 ZDOT = -5630
748133
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 20234
42447446
00016717 00000-0 10270-3 0 9025
2 25544 51
6417 25
6166 0001520 36
9922 323
1333 15
49181930 2125
Satellite: ISS
Catalog Number: 25544
Epoch time: 20234
42447446 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 25
6166 deg
Eccentricity:
0001520
Arg of perigee: 36
9922 deg
Mean anomaly: 323
1333 deg
Mean motion: 15
49181930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 274
Coasting Arc #4 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2020/235/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5468994
79 A = 6802247
03 meter
Y = 3576045
94 meter E =
0015281
Z = 1863027
94 I = 51
79315
XDOT = -4050
495861 Wp = 64
47506
YDOT = 3240
300696 meter/sec RA = 20
21116 deg
ZDOT = 5641
037063 TA = 315
94701
MA = 316
06866
Ha = 229
189 n
mi
Hp = 222
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17942896
29 X = 5419550
48
Y = 11732434
18 feet Y = 3636927
77 meter
Z = 6112296
41 Z = 1889473
66
XDOT = -13289
028414 XDOT = -4113
829481
YDOT = 10630
907795 feet/sec YDOT = 3194
651262 meter/sec
ZDOT = 18507
339446 ZDOT = 5621
207591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3898165
20 X = 1188160
75
Y = -21045122
50 feet Y = -6414553
34 meter
Z = 6234166
61 Z = 1900173
98
XDOT = 13457
556827 XDOT = 4101
863321
YDOT = 7976
225730 feet/sec YDOT = 2431
153602 meter/sec
ZDOT = 18415
609803 ZDOT = 5613
077868
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 20235
45660166
00016717 00000-0 10270-3 0 9036
2 25544 51
6414 20
5090 0001461 45
7802 314
3468 15
49175792 2288
Satellite: ISS
Catalog Number: 25544
Epoch time: 20235
45660166 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 20
5090 deg
Eccentricity:
0001461
Arg of perigee: 45
7802 deg
Mean anomaly: 314
3468 deg
Mean motion: 15
49175792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 228
Checksum: 288
Coasting Arc #5 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2020/236/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5708510
10 A = 6802044
12 meter
Y = -3145257
31 meter E =
0006963
Z = -1942137
96 I = 51
76030
XDOT = 3843
997817 Wp = 125
82127
YDOT = -3527
818554 meter/sec RA = 15
27257 deg
ZDOT = -5603
462510 TA = 75
49947
MA = 75
42224
Ha = 229
231 n
mi
Hp = 221
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18728707
67 X = -5663480
88
Y = -10319085
67 feet Y = -3208842
25 meter
Z = -6371843
70 Z = -1969758
04
XDOT = 12611
541393 XDOT = 3910
379506
YDOT = -11574
207855 feet/sec YDOT = -3484
461232 meter/sec
ZDOT = -18384
063353 ZDOT = -5584
628645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1926222
50 X = -587112
62
Y = 21257920
52 feet Y = 6479414
17 meter
Z = -6499145
68 Z = -1980939
60
XDOT = -14172
414147 XDOT = -4319
751832
YDOT = -6860
304710 feet/sec YDOT = -2091
020876 meter/sec
ZDOT = -18296
918373 ZDOT = -5576
900720
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 20236
42422004
00016717 00000-0 10270-3 0 9042
2 25544 51
6410 15
7217 0001651 48
9933 311
1359 15
49197195 2434
Satellite: ISS
Catalog Number: 25544
Epoch time: 20236
42422004 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 15
7217 deg
Eccentricity:
0001651
Arg of perigee: 48
9933 deg
Mean anomaly: 311
1359 deg
Mean motion: 15
49197195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 243
Checksum: 280
Coasting Arc #6 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2020/237/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5924852
98 A = 6802047
40 meter
Y = 2670481
70 meter E =
0015335
Z = 1983079
44 I = 51
72658
XDOT = -3600
281467 Wp = 67
11463
YDOT = 3820
939525 meter/sec RA = 10
33108 deg
ZDOT = 5582
581041 TA = 314
70969
MA = 314
83448
Ha = 229
240 n
mi
Hp = 221
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19438494
03 X = 5884917
87
Y = 8761422
89 feet Y = 2736514
38 meter
Z = 6506166
13 Z = 2011762
93
XDOT = -11811
947069 XDOT = -3669
857676
YDOT = 12535
890831 feet/sec YDOT = 3780
289648 meter/sec
ZDOT = 18315
554596 ZDOT = 5564
923305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -151072
88 X = -46047
01
Y = -21280430
37 feet Y = -6486275
18 meter
Z = 6638391
33 Z = 2023381
68
XDOT = 14827
869463 XDOT = 4519
534612
YDOT = 5611
416311 feet/sec YDOT = 1710
359692 meter/sec
ZDOT = 18233
824483 ZDOT = 5557
669702
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 20237
45634627
00016717 00000-0 10270-3 0 9053
2 25544 51
6405 10
6146 0001461 58
4021 301
7271 15
49174359 2598
Satellite: ISS
Catalog Number: 25544
Epoch time: 20237
45634627 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 10
6146 deg
Eccentricity:
0001461
Arg of perigee: 58
4021 deg
Mean anomaly: 301
7271 deg
Mean motion: 15
49174359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 259
Checksum: 285
Coasting Arc #7 (Orbit 273)
---------------------------------------
Vector Time (GMT): 2020/238/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6091117
63 A = 6801799
02 meter
Y = -2211711
51 meter E =
0006847
Z = -2063535
19 I = 51
69405
XDOT = 3353
702408 Wp = 124
46905
YDOT = -4081
059211 meter/sec RA = 5
38759 deg
ZDOT = -5542
222508 TA = 78
27829
MA = 78
20148
Ha = 229
243 n
mi
Hp = 221
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19983981
71 X = -6055909
46
Y = -7256271
34 feet Y = -2279629
86 meter
Z = -6770128
58 Z = -2093037
87
XDOT = 11002
960655 XDOT = 3426
009644
YDOT = -13389
301873 feet/sec YDOT = -4043
151367 meter/sec
ZDOT = -18183
144712 ZDOT = -5525
756002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2109100
21 X = 642853
74
Y = 21111712
68 feet Y = 6434850
03 meter
Z = -6906151
15 Z = -2104994
87
XDOT = -15351
764118 XDOT = -4679
217703
YDOT = -4371
739204 feet/sec YDOT = -1332
506109 meter/sec
ZDOT = -18106
899028 ZDOT = -5518
982824
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 20238
42396166
00016717 00000-0 10270-3 0 9065
2 25544 51
6419 5
8269 0001633 56
8985 303
2321 15
49208024 2744
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
42396166 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 5
8269 deg
Eccentricity:
0001633
Arg of perigee: 56
8985 deg
Mean anomaly: 303
2321 deg
Mean motion: 15
49208024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 274
Checksum: 303
Coasting Arc #8 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2020/238/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4108214
74 A = 6796473
59 meter
Y = -3503102
97 meter E =
0009415
Z = -4138370
76 I = 51
66108
XDOT = 6088
313686 Wp = 67
84479
YDOT = -2667
460003 meter/sec RA = 3
13943 deg
ZDOT = -3789
423868 TA = 163
01538
MA = 162
98384
Ha = 229
376 n
mi
Hp = 221
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13478394
81 X = -4048634
90
Y = -11493119
97 feet Y = -3548710
76 meter
Z = -13577331
88 Z = -4158182
13
XDOT = 19974
782435 XDOT = 6136
096310
YDOT = -8751
509197 feet/sec YDOT = -2599
108888 meter/sec
ZDOT = -12432
493006 ZDOT = -3759
733331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8854009
35 X = 2698702
05
Y = -15260414
94 feet Y = -4651374
47 meter
Z = -13668545
22 Z = -4166172
58
XDOT = 11157
789545 XDOT = 3400
894253
YDOT = 17476
320603 feet/sec YDOT = 5326
782520 meter/sec
ZDOT = -12295
306720 ZDOT = -3747
609488
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 20238
87551490
00016717 00000-0 10270-3 0 9078
2 25544 51
6423 3
5961 0001780 58
6755 301
4570 15
49172451 2819
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
87551490 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 3
5961 deg
Eccentricity:
0001780
Arg of perigee: 58
6755 deg
Mean anomaly: 301
4570 deg
Mean motion: 15
49172451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 301
Coasting Arc #9 (Orbit 296)
---------------------------------------
Vector Time (GMT): 2020/239/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4331781
67 A = 6796299
98 meter
Y = 3163088
58 meter E =
0011395
Z = 4165080
91 I = 51
62590
XDOT = -5903
601575 Wp = 98
09690
YDOT = 3148
245260 meter/sec RA = 358
19261 deg
ZDOT = 3738
669125 TA = 313
37742
MA = 313
47227
Ha = 229
224 n
mi
Hp = 221
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14211882
10 X = 4275857
67
Y = 10377587
19 feet Y = 3211216
83 meter
Z = 13664963
60 Z = 4185987
13
XDOT = -19368
771571 XDOT = -5956
527621
YDOT = 10328
888649 feet/sec YDOT = 3081
930917 meter/sec
ZDOT = 12265
974818 ZDOT = 3709
863490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7350820
57 X = -2240530
11
Y = 15905870
46 feet Y = 4848109
32 meter
Z = 13761244
90 Z = 4194427
44
XDOT = -12845
042230 XDOT = -3915
168872
YDOT = -16462
372124 feet/sec YDOT = -5017
731023 meter/sec
ZDOT = 12132
848662 ZDOT = 3698
092272
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 20239
90763518
00016717 00000-0 10270-3 0 9080
2 25544 51
6413 358
4898 0001690 56
4843 303
6468 15
49189983 2978
Satellite: ISS
Catalog Number: 25544
Epoch time: 20239
90763518 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 358
4898 deg
Eccentricity:
0001690
Arg of perigee: 56
4843 deg
Mean anomaly: 303
6468 deg
Mean motion: 15
49189983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 297
Checksum: 352
Coasting Arc #10 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2020/240/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4520347
95 A = 6796181
54 meter
Y = -2833873
88 meter E =
0009874
Z = -4220378
68 I = 51
59120
XDOT = 5672
543187 Wp = 67
92556
YDOT = -3597
131912 meter/sec RA = 353
24247 deg
ZDOT = -3663
620334 TA = 164
42246
MA = 164
39205
Ha = 229
393 n
mi
Hp = 221
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14830537
88 X = -4467822
80
Y = -9297486
50 feet Y = -2884129
81 meter
Z = -13846386
75 Z = -4242209
05
XDOT = 18610
705994 XDOT = 5730
141377
YDOT = -11801
613883 feet/sec YDOT = -3533
375291 meter/sec
ZDOT = -12019
751751 ZDOT = -3635
925880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5888003
47 X = 1794663
46
Y = -16398919
21 feet Y = -4998390
58 meter
Z = -13946949
46 Z = -4251030
19
XDOT = 14372
755584 XDOT = 4380
815902
YDOT = 15265
123400 feet/sec YDOT = 4652
809612 meter/sec
ZDOT = -11891
732170 ZDOT = -3624
599965
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 20240
87524856
00016717 00000-0 10270-3 0 9099
2 25544 51
6409 353
7019 0001788 61
4404 298
6925 15
49169890 3127
Satellite: ISS
Catalog Number: 25544
Epoch time: 20240
87524856 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 353
7019 deg
Eccentricity:
0001788
Arg of perigee: 61
4404 deg
Mean anomaly: 298
6925 deg
Mean motion: 15
49169890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 330
Coasting Arc #11 (Orbit 327)
---------------------------------------
Vector Time (GMT): 2020/241/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4687475
82 A = 6795934
35 meter
Y = 2471280
48 meter E =
0011083
Z = 4246876
41 I = 51
55786
XDOT = -5414
387759 Wp = 100
55077
YDOT = 4048
708069 meter/sec RA = 348
29122 deg
ZDOT = 3610
130174 TA = 312
43245
MA = 312
52613
Ha = 229
165 n
mi
Hp = 221
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15378857
69 X = 4638864
26
Y = 8107875
57 feet Y = 2523427
25 meter
Z = 13933321
56 Z = 4269528
00
XDOT = -17763
739368 XDOT = -5476
794902
YDOT = 13283
162957 feet/sec YDOT = 3987
811461 meter/sec
ZDOT = 11844
259102 ZDOT = 3583
678148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4320508
02 X = -1316890
84
Y = 16752931
85 feet Y = 5106293
63 meter
Z = 14037693
72 Z = 4278689
05
XDOT = -15857
478763 XDOT = -4833
359527
YDOT = -13939
021291 feet/sec YDOT = -4248
613690 meter/sec
ZDOT = 11721
953498 ZDOT = 3572
851426
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 20241
90736589
00016717 00000-0 10270-3 0 9104
2 25544 51
6414 348
5958 0001589 62
5432 297
5880 15
49211839 3285
Satellite: ISS
Catalog Number: 25544
Epoch time: 20241
90736589 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 348
5958 deg
Eccentricity:
0001589
Arg of perigee: 62
5432 deg
Mean anomaly: 297
5880 deg
Mean motion: 15
49211839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 328
Checksum: 333
Coasting Arc #12 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2020/242/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4821506
44 A = 6795832
80 meter
Y = -2125820
06 meter E =
0010377
Z = -4302350
93 I = 51
52523
XDOT = 5115
259480 Wp = 68
19806
YDOT = -4460
750978 meter/sec RA = 343
33598 deg
ZDOT = -3531
526628 TA = 165
68826
MA = 165
65884
Ha = 229
395 n
mi
Hp = 221
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15818590
67 X = -4776478
56
Y = -6974475
25 feet Y = -2179485
76 meter
Z = -14115324
58 Z = -4325662
17
XDOT = 16782
347375 XDOT = 5181
914583
YDOT = -14635
009770 feet/sec YDOT = -4403
175738 meter/sec
ZDOT = -11586
373450 ZDOT = -3506
517337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2824685
42 X = 860964
12
Y = -16966077
16 feet Y = -5171260
32 meter
Z = -14222759
30 Z = -4335097
03
XDOT = 17147
833039 XDOT = 5226
659510
YDOT = 12462
430179 feet/sec YDOT = 3798
548719 meter/sec
ZDOT = -11470
711587 ZDOT = -3496
272892
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 20242
87497564
00016717 00000-0 10270-3 0 9119
2 25544 51
6422 343
8074 0001831 64
4014 295
7325 15
49185619 3435
Satellite: ISS
Catalog Number: 25544
Epoch time: 20242
87497564 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 343
8074 deg
Eccentricity:
0001831
Arg of perigee: 64
4014 deg
Mean anomaly: 295
7325 deg
Mean motion: 15
49185619 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 308
Coasting Arc #13 (Orbit 358)
---------------------------------------
Vector Time (GMT): 2020/243/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4929968
97 A = 6795584
71 meter
Y = 1751245
87 meter E =
0010824
Z = 4329109
61 I = 51
49257
XDOT = -4789
602777 Wp = 102
24750
YDOT = 4871
534737 meter/sec RA = 338
38057 deg
ZDOT = 3474
088203 TA = 312
30859
MA = 312
40026
Ha = 229
161 n
mi
Hp = 221
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16174438
87 X = 4888991
69
Y = 5745557
31 feet Y = 1806147
21 meter
Z = 14203115
53 Z = 4352957
46
XDOT = -15713
919871 XDOT = -4860
596567
YDOT = 15982
725516 feet/sec YDOT = 4817
577036 meter/sec
ZDOT = 11397
927176 ZDOT = 3450
650202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1253284
08 X = -382000
99
Y = 17026990
42 feet Y = 5189826
68 meter
Z = 14313045
40 Z = 4362616
24
XDOT = -18372
426080 XDOT = -5599
915469
YDOT = -10868
695310 feet/sec YDOT = -3312
778331 meter/sec
ZDOT = 11289
505696 ZDOT = 3441
041336
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 20243
90708836
00016717 00000-0 10270-3 0 9122
2 25544 51
6420 338
7017 0001646 66
0417 294
0905 15
49226500 3590
Satellite: ISS
Catalog Number: 25544
Epoch time: 20243
90708836 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 338
7017 deg
Eccentricity:
0001646
Arg of perigee: 66
0417 deg
Mean anomaly: 294
0905 deg
Mean motion: 15
49226500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 359
Checksum: 296
Coasting Arc #14 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2020/244/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5010534
48 A = 6795505
95 meter
Y = -1397743
09 meter E =
0010817
Z = -4383729
52 I = 51
46080
XDOT = 4426
827533 Wp = 68
62628
YDOT = -5236
789079 meter/sec RA = 333
42133 deg
ZDOT = -3392
980637 TA = 166
84748
MA = 166
81925
Ha = 229
385 n
mi
Hp = 221
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16438761
42 X = -4973238
88
Y = -4585771
30 feet Y = -1453566
06 meter
Z = -14382314
70 Z = -4407977
63
XDOT = 14523
712380 XDOT = 4501
538707
YDOT = -17181
066533 feet/sec YDOT = -5186
867481 meter/sec
ZDOT = -11131
826237 ZDOT = -3371
295667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -226605
87 X = -69069
47
Y = -16970051
88 feet Y = -5172471
81 meter
Z = -14494107
10 Z = -4417803
84
XDOT = 19374
091196 XDOT = 5905
222996
YDOT = 9155
144486 feet/sec YDOT = 2790
488039 meter/sec
ZDOT = -11031
489258 ZDOT = -3362
397926
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 20244
87469642
00016717 00000-0 10270-3 0 9139
2 25544 51
6418 333
9138 0001809 67
1470 292
9871 15
49193554 3748
Satellite: ISS
Catalog Number: 25544
Epoch time: 20244
87469642 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 333
9138 deg
Eccentricity:
0001809
Arg of perigee: 67
1470 deg
Mean anomaly: 292
9871 deg
Mean motion: 15
49193554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 331
Coasting Arc #15 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2020/245/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5061847
95 A = 6795254
52 meter
Y = 1019505
55 meter E =
0010487
Z = 4410164
78 I = 51
43152
XDOT = -4038
812955 Wp = 104
64689
YDOT = 5596
629927 meter/sec RA = 328
46155 deg
ZDOT = 3332
579359 TA = 311
51914
MA = 311
60907
Ha = 229
130 n
mi
Hp = 221
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16607112
70 X = 5028649
65
Y = 3344834
49 feet Y = 1075925
35 meter
Z = 14469044
56 Z = 4434672
14
XDOT = -13250
698671 XDOT = -4117
283458
YDOT = 18361
646743 feet/sec YDOT = 5551
026433 meter/sec
ZDOT = 10933
659313 ZDOT = 3312
769880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1752687
86 X = 534219
26
Y = 16751994
84 feet Y = 5106008
03 meter
Z = 14582047
69 Z = 4444608
14
XDOT = -20288
800044 XDOT = -6184
026253
YDOT = -7341
085218 feet/sec YDOT = -2237
562775 meter/sec
ZDOT = 10841
974012 ZDOT = 3304
633679
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 20245
90680664
00016717 00000-0 10270-3 0 9144
2 25544 51
6426 328
8081 0001579 71
9138 288
2184 15
49235066 3903
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
90680664 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 328
8081 deg
Eccentricity:
0001579
Arg of perigee: 71
9138 deg
Mean anomaly: 288
2184 deg
Mean motion: 15
49235066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 321
Coasting Arc #16 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2020/245/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -447150
28 A = 6792846
16 meter
Y = -4502669
53 meter E =
0014559
Z = -5079555
32 I = 51
42136
XDOT = 6939
784415 Wp = 99
09800
YDOT = -2685
393475 meter/sec RA = 327
89806 deg
ZDOT = 1771
618361 TA = 188
12373
MA = 188
14733
Ha = 229
366 n
mi
Hp = 221
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1467028
48 X = -372093
70
Y = -14772537
84 feet Y = -4507250
48 meter
Z = -16665207
73 Z = -5081544
84
XDOT = 22768
321572 XDOT = 6960
692157
YDOT = -8810
346047 feet/sec YDOT = -2607
670844 meter/sec
ZDOT = 5812
396197 ZDOT = 1805
379439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7216682
40 X = 2199644
79
Y = -12961541
55 feet Y = -3950677
87 meter
Z = -16674145
59 Z = -5082279
58
XDOT = 22791
164681 XDOT = 6946
746995
YDOT = 5020
694197 feet/sec YDOT = 1530
307591 meter/sec
ZDOT = 5968
285202 ZDOT = 1819
133330
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 20245
97131545
00016717 00000-0 10270-3 0 9151
2 25544 51
6441 328
4891 0001748 67
1638 292
9696 15
49197972 3919
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
97131545 = yrday
fracday
Element set: 915
Inclination: 51
6441 deg
RA of node: 328
4891 deg
Eccentricity:
0001748
Arg of perigee: 67
1638 deg
Mean anomaly: 292
9696 deg
Mean motion: 15
49197972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 344
Coasting Arc #17 (Orbit 406)
---------------------------------------
Vector Time (GMT): 2020/246/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 739719
31 A = 6792871
85 meter
Y = 4486587
88 meter E =
0007409
Z = 5042060
68 I = 51
39362
XDOT = -6708
379606 Wp = 58
25767
YDOT = 3204
419105 meter/sec RA = 322
93545 deg
ZDOT = -1861
366406 TA = 49
88220
MA = 49
81730
Ha = 229
307 n
mi
Hp = 221
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2426900
62 X = 665002
85
Y = 14719776
49 feet Y = 4494442
51 meter
Z = 16542193
84 Z = 5045472
14
XDOT = -22009
119443 XDOT = -6734
672478
YDOT = 10513
186039 feet/sec YDOT = 3129
254065 meter/sec
ZDOT = -6106
845163 ZDOT = -1894
016696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6161204
63 X = -1877935
17
Y = 13567901
56 feet Y = 4135496
39 meter
Z = 16557700
58 Z = 5046787
14
XDOT = -23139
313899 XDOT = -7052
862876
YDOT = -2847
683656 feet/sec YDOT = -867
973978 meter/sec
ZDOT = -6257
618276 ZDOT = -1907
322051
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 20247
00342382
00016717 00000-0 10270-3 0 9161
2 25544 51
6439 323
3832 0001764 67
5916 292
5421 15
49223557 4075
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
00342382 = yrday
fracday
Element set: 916
Inclination: 51
6439 deg
RA of node: 323
3832 deg
Eccentricity:
0001764
Arg of perigee: 67
5916 deg
Mean anomaly: 292
5421 deg
Mean motion: 15
49223557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 407
Checksum: 300
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