[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 3rd 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19912 1579 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
096/04:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
0
000/00:00:00
000 0
0 0
0 221
7
097/14:00:43
000 0
0 0
0 0
0
N/A 0
0 0
0 230
8
000/00:00:00
000 0
0 0
0 221
9
100/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 221
9
100/08:05:06
000 0
0 0
0 0
0
N/A 0
0 0
0 230
7
000/00:00:00
000 0
0 0
0 221
8
100/14:16:50
000 0
0 0
0 0
0
N/A 0
0 0
0 230
8
000/00:00:00
000 0
0 0
0 221
9
108/01:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
5
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 2028)
---------------------------------------
Vector Time (GMT): 2020/093/13:27:27
745
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2256404
89 A = 6794694
71 meter
Y = 4026213
35 meter E =
0009132
Z = 4979747
54 I = 51
64677
XDOT = -7227
197412 Wp = 105
24856
YDOT = 1415
623336 meter/sec RA = 2
11289 deg
ZDOT = 2124
602482 TA = 324
02136
MA = 324
08280
Ha = 230
904 n
mi
Hp = 221
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7402903
18 X = 2187026
26
Y = 13209361
40 feet Y = 4051058
26 meter
Z = 16337754
39 Z = 4990539
61
XDOT = -23711
277597 XDOT = -7252
810236
YDOT = 4644
433516 feet/sec YDOT = 1334
660511 meter/sec
ZDOT = 6970
480584 ZDOT = 2089
433550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13224852
26 X = 4030934
97
Y = 7265231
46 feet Y = 2214442
55 meter
Z = 16386949
60 Z = 4994742
24
XDOT = -17064
391834 XDOT = -5201
226631
YDOT = 15662
857674 feet/sec YDOT = 4774
039019 meter/sec
ZDOT = 6809
045327 ZDOT = 2075
397016
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 20093
61278098
00016717 00000-0 10270-3 0 9002
2 25544 51
6456 2
4313 0003790 77
2921 282
8652 15
48675836 20298
Satellite: ISS
Catalog Number: 25544
Epoch time: 20093
61278098 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 2
4313 deg
Eccentricity:
0003790
Arg of perigee: 77
2921 deg
Mean anomaly: 282
8652 deg
Mean motion: 15
48675836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2029
Checksum: 314
Coasting Arc #2 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2020/094/13:27:27
745
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2708935
14 A = 6794768
28 meter
Y = -3796993
98 meter E =
0016117
Z = -4955951
07 I = 51
61356
XDOT = 7008
244401 Wp = 74
48918
YDOT = -2106
358385 meter/sec RA = 357
16959 deg
ZDOT = -2218
772976 TA = 173
79481
MA = 173
77482
Ha = 230
904 n
mi
Hp = 221
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8887582
46 X = -2642201
71
Y = -12457329
32 feet Y = -3826914
26 meter
Z = -16259681
98 Z = -4968947
69
XDOT = 22992
927824 XDOT = 7042
054901
YDOT = -6910
624623 feet/sec YDOT = -2027
798244 meter/sec
ZDOT = -7279
438899 ZDOT = -2184
647753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14176168
86 X = -4320896
27
Y = -5592646
23 feet Y = -1704638
57 meter
Z = -16319006
67 Z = -4974033
23
XDOT = 15054
780114 XDOT = 4588
696979
YDOT = -17394
390189 feet/sec YDOT = -5301
810129 meter/sec
ZDOT = -7122
748515 ZDOT = -2171
013747
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 20094
58070763
00016717 00000-0 10270-3 0 9019
2 25544 51
6455 357
6459 0003742 78
0658 282
0911 15
48700919 20444
Satellite: ISS
Catalog Number: 25544
Epoch time: 20094
58070763 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 357
6459 deg
Eccentricity:
0003742
Arg of perigee: 78
0658 deg
Mean anomaly: 282
0911 deg
Mean motion: 15
48700919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 317
Coasting Arc #3 (Orbit 2059)
---------------------------------------
Vector Time (GMT): 2020/095/13:27:27
745
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3139246
13 A = 6795006
77 meter
Y = 3495422
60 meter E =
0009891
Z = 4901933
24 I = 51
58004
XDOT = -6749
937961 Wp = 106
80900
YDOT = 2786
280028 meter/sec RA = 352
22437 deg
ZDOT = 2329
214880 TA = 320
33326
MA = 320
40557
Ha = 230
917 n
mi
Hp = 221
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10299363
94 X = 3076115
38
Y = 11467921
93 feet Y = 3530175
18 meter
Z = 16082458
13 Z = 4917028
80
XDOT = -22145
465752 XDOT = -6791
907197
YDOT = 9141
338673 feet/sec YDOT = 2710
562886 meter/sec
ZDOT = 7641
781104 ZDOT = 2296
324519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14880205
08 X = 4535486
51
Y = 3734477
24 feet Y = 1138268
66 meter
Z = 16151432
34 Z = 4922956
58
XDOT = -12916
113631 XDOT = -3936
831435
YDOT = 18973
254848 feet/sec YDOT = 5783
048078 meter/sec
ZDOT = 7490
716621 ZDOT = 2283
170426
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 20095
61316164
00016717 00000-0 10270-3 0 9023
2 25544 51
6449 352
5415 0003857 82
4607 277
6981 15
48672184 20600
Satellite: ISS
Catalog Number: 25544
Epoch time: 20095
61316164 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 352
5415 deg
Eccentricity:
0003857
Arg of perigee: 82
4607 deg
Mean anomaly: 277
6981 deg
Mean motion: 15
48672184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2060
Checksum: 317
Coasting Arc #4 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2020/096/04:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5129106
43 A = 6798661
99 meter
Y = -2177653
78 meter E =
0010447
Z = -3905691
67 I = 51
57016
XDOT = 4897
535668 Wp = 78
40722
YDOT = -4229
058852 meter/sec RA = 349
21552 deg
ZDOT = -4080
923615 TA = 148
70516
MA = 148
64294
Ha = 230
989 n
mi
Hp = 221
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16827777
00 X = -5085402
59
Y = -7144533
41 feet Y = -2234767
01 meter
Z = -12813949
03 Z = -3930500
36
XDOT = 16068
030406 XDOT = 4964
284901
YDOT = -13874
865001 feet/sec YDOT = -4173
918194 meter/sec
ZDOT = -13388
857006 ZDOT = -4056
971073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11414594
17 X = 3479168
30
Y = -14177472
97 feet Y = -4321293
76 meter
Z = -12927568
45 Z = -3940322
86
XDOT = 7943
349067 XDOT = 2421
132795
YDOT = 18481
918694 feet/sec YDOT = 5633
288818 meter/sec
ZDOT = -13278
686768 ZDOT = -4047
343727
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 20096
19391456
00016717 00000-0 10270-3 0 9035
2 25544 51
6428 349
6695 0003928 87
7948 272
3651 15
48688203 20693
Satellite: ISS
Catalog Number: 25544
Epoch time: 20096
19391456 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 349
6695 deg
Eccentricity:
0003928
Arg of perigee: 87
7948 deg
Mean anomaly: 272
3651 deg
Mean motion: 15
48688203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2069
Checksum: 352
Coasting Arc #5 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2020/097/04:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939587
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5372800
52 A = 6798922
26 meter
Y = 1638072
90 meter E =
0015134
Z = 3818959
71 I = 51
53748
XDOT = -4404
499394 Wp = 95
56871
YDOT = 4683
851526 meter/sec RA = 344
26583 deg
ZDOT = 4171
817065 TA = 310
32586
MA = 310
45798
Ha = 230
881 n
mi
Hp = 221
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17627298
28 X = 5335533
54
Y = 5374254
92 feet Y = 1697947
35 meter
Z = 12529395
37 Z = 3844967
90
XDOT = -14450
457328 XDOT = -4476
812475
YDOT = 15366
966948 feet/sec YDOT = 4634
193329 meter/sec
ZDOT = 13687
063863 ZDOT = 4150
245764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9660881
19 X = -2944636
59
Y = 15597167
73 feet Y = 4754016
72 meter
Z = 12648547
05 Z = 3855277
14
XDOT = -10024
748829 XDOT = -3055
543443
YDOT = -17269
781168 feet/sec YDOT = -5263
829300 meter/sec
ZDOT = 13587
795994 ZDOT = 4141
560219
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 20097
22636365
00016717 00000-0 10270-3 0 9042
2 25544 51
6420 344
5650 0003857 90
2466 269
9125 15
48688873 20854
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
22636365 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 344
5650 deg
Eccentricity:
0003857
Arg of perigee: 90
2466 deg
Mean anomaly: 269
9125 deg
Mean motion: 15
48688873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 330
Coasting Arc #6 (Orbit 2090)
---------------------------------------
Vector Time (GMT): 2020/097/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915574
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6595727
05 A = 6804466
43 meter
Y = 1033386
27 meter E =
0011249
Z = -1299201
31 I = 51
54444
XDOT = 359
399098 Wp = 127
44422
YDOT = -4966
843904 meter/sec RA = 342
20502 deg
ZDOT = -5816
604907 TA = 66
67435
MA = 66
55602
Ha = 230
846 n
mi
Hp = 221
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21639524
44 X = -6600481
71
Y = 3390374
90 feet Y = 959601
45 meter
Z = -4262471
48 Z = -1331252
35
XDOT = 1179
130900 XDOT = 443
166791
YDOT = -16295
419634 feet/sec YDOT = -4962
357033 meter/sec
ZDOT = -19083
349431 ZDOT = -5814
655157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13007074
77 X = -3964556
39
Y = 17587052
73 feet Y = 5360533
67 meter
Z = -4409524
41 Z = -1344023
04
XDOT = -9227
889520 XDOT = -2812
660726
YDOT = -11574
224894 feet/sec YDOT = -3527
823748 meter/sec
ZDOT = -19074
046453 ZDOT = -5813
769359
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 20097
61353079
00016717 00000-0 10270-3 0 9054
2 25544 51
6441 342
6517 0003520 90
2535 269
9018 15
48673862 20912
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
61353079 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 342
6517 deg
Eccentricity:
0003520
Arg of perigee: 90
2535 deg
Mean anomaly: 269
9018 deg
Mean motion: 15
48673862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2091
Checksum: 310
Coasting Arc #7 (Orbit 2106)
---------------------------------------
Vector Time (GMT): 2020/098/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915574
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6475480
78 A = 6804459
41 meter
Y = -1694477
70 meter E =
0016766
Z = 1184135
33 I = 51
51227
XDOT = 215
538142 Wp = 65
00520
YDOT = 4948
849178 meter/sec RA = 337
25001 deg
ZDOT = 5844
880500 TA = 307
85394
MA = 308
00552
Ha = 230
814 n
mi
Hp = 221
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21245015
68 X = 6488195
78
Y = -5559310
04 feet Y = -1621993
05 meter
Z = 3884958
43 Z = 1215621
85
XDOT = 707
146136 XDOT = 131
791424
YDOT = 16236
381819 feet/sec YDOT = 4950
791801 meter/sec
ZDOT = 19176
117125 ZDOT = 5845
723608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10879096
09 X = 3315948
49
Y = -19046214
48 feet Y = -5805286
17 meter
Z = 4029454
48 Z = 1228177
73
XDOT = 10612
839486 XDOT = 3234
793475
YDOT = 10158
599534 feet/sec YDOT = 3096
341138 meter/sec
ZDOT = 19179
626787 ZDOT = 5845
950245
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 20098
64597318
00016717 00000-0 10270-3 0 9065
2 25544 51
6431 337
5461 0003584 93
2598 266
8962 15
48722143 21073
Satellite: ISS
Catalog Number: 25544
Epoch time: 20098
64597318 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 337
5461 deg
Eccentricity:
0003584
Arg of perigee: 93
2598 deg
Mean anomaly: 266
8962 deg
Mean motion: 15
48722143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2107
Checksum: 332
Coasting Arc #8 (Orbit 2121)
---------------------------------------
Vector Time (GMT): 2020/099/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915574
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6300848
92 A = 6804607
51 meter
Y = 2301120
04 meter E =
0012060
Z = -1120823
75 I = 51
48053
XDOT = -747
079701 Wp = 129
04057
YDOT = -4874
777569 meter/sec RA = 332
29429 deg
ZDOT = -5858
371472 TA = 63
11940
MA = 62
99619
Ha = 230
846 n
mi
Hp = 221
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20672076
52 X = -6320668
06
Y = 7549606
43 feet Y = 2230548
55 meter
Z = -3677243
27 Z = -1151479
43
XDOT = -2451
048889 XDOT = -664
056082
YDOT = -15993
364729 feet/sec YDOT = -4882
668232 meter/sec
ZDOT = -19220
378845 ZDOT = -5861
798461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8711586
19 X = -2655291
47
Y = 20183777
65 feet Y = 6152015
43 meter
Z = -3817958
70 Z = -1163713
81
XDOT = -11738
675488 XDOT = -3577
948289
YDOT = -8675
337617 feet/sec YDOT = -2644
242906 meter/sec
ZDOT = -19235
742946 ZDOT = -5863
054450
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 20099
61388812
00016717 00000-0 10270-3 0 9071
2 25544 51
6416 332
7607 0003607 96
2642 263
8919 15
48690918 21224
Satellite: ISS
Catalog Number: 25544
Epoch time: 20099
61388812 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 332
7607 deg
Eccentricity:
0003607
Arg of perigee: 96
2642 deg
Mean anomaly: 263
8919 deg
Mean motion: 15
48690918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2122
Checksum: 329
Coasting Arc #9 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915574
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1920465
93 A = 6797955
52 meter
Y = -5029140
70 meter E =
0011262
Z = -4162595
49 I = 51
43756
XDOT = 6657
845968 Wp = 104
97252
YDOT = -538
518575 meter/sec RA = 328
95659 deg
ZDOT = 3727
939912 TA = 203
55632
MA = 203
60794
Ha = 230
942 n
mi
Hp = 221
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6300741
24 X = 1996780
28
Y = -16499805
43 feet Y = -5007238
26 meter
Z = -13656809
35 Z = -4153080
81
XDOT = 21843
326666 XDOT = 6645
264600
YDOT = -1766
793225 feet/sec YDOT = -464
135895 meter/sec
ZDOT = 12230
773988 ZDOT = 3760
250980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17649812
96 X = 5379662
99
Y = 1275264
75 feet Y = 388700
70 meter
Z = -13612830
83 Z = -4149190
84
XDOT = 8160
502792 XDOT = 2487
321251
YDOT = 18998
943716 feet/sec YDOT = 5790
878045 meter/sec
ZDOT = 12378
945163 ZDOT = 3773
102486
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 20100
25916448
00016717 00000-0 10270-3 0 9087
2 25544 51
6406 329
5704 0003741 97
6744 262
4831 15
48687688 21321
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
25916448 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 329
5704 deg
Eccentricity:
0003741
Arg of perigee: 97
6744 deg
Mean anomaly: 262
4831 deg
Mean motion: 15
48687688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 322
Coasting Arc #10 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS) : 915574
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3785837
13 A = 6794030
09 meter
Y = 2436749
76 meter E =
0008552
Z = 5082189
36 I = 51
42433
XDOT = -5544
532330 Wp = 113
90239
YDOT = 5002
441252 meter/sec RA = 328
56556 deg
ZDOT = 1726
030073 TA = 319
32422
MA = 319
38806
Ha = 230
687 n
mi
Hp = 221
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12420725
50 X = 3733620
64
Y = 7994585
83 feet Y = 2478794
06 meter
Z = 16673849
59 Z = 5100452
70
XDOT = -18190
722866 XDOT = -5608
443193
YDOT = 16412
208833 feet/sec YDOT = 4940
081112 meter/sec
ZDOT = 5662
828325 ZDOT = 1698
941024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3896747
47 X = 1187728
63
Y = 14149551
01 feet Y = 4312783
15 meter
Z = 16757405
83 Z = 5107657
30
XDOT = -23496
301137 XDOT = -7161
672587
YDOT = -110
257253 feet/sec YDOT = -33
606411 meter/sec
ZDOT = 5538
281296 ZDOT = 1688
068139
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 20100
38821837
00016717 00000-0 10270-3 0 9099
2 25544 51
6422 328
9332 0003619 99
5058 260
6501 15
48738398 21343
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
38821837 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 328
9332 deg
Eccentricity:
0003619
Arg of perigee: 99
5058 deg
Mean anomaly: 260
6501 deg
Mean motion: 15
48738398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 316
Coasting Arc #11 (Orbit 2137)
---------------------------------------
Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3820772
02 A = 6794209
80 meter
Y = 2370263
58 meter E =
0008541
Z = 5087731
98 I = 51
41501
XDOT = -5448
189063 Wp = 114
12184
YDOT = 5114
797218 meter/sec RA = 327
28328 deg
ZDOT = 1702
904951 TA = 319
33314
MA = 319
39689
Ha = 230
805 n
mi
Hp = 221
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12535341
29 X = 3769269
46
Y = 7776455
33 feet Y = 2412702
50 meter
Z = 16692034
05 Z = 5106166
79
XDOT = -17874
636033 XDOT = -5513
251159
YDOT = 16780
830768 feet/sec YDOT = 5053
508006 meter/sec
ZDOT = 5586
958500 ZDOT = 1676
281127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13811152
44 X = 4209639
26
Y = -4902773
36 feet Y = -1494365
32 meter
Z = 16776379
85 Z = 5113440
58
XDOT = 1665
617532 XDOT = 507
680224
YDOT = 23454
247376 feet/sec YDOT = 7148
854600 meter/sec
ZDOT = 5464
538931 ZDOT = 1665
591466
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 20100
64632896
00016717 00000-0 10270-3 0 9105
2 25544 51
6404 327
6548 0003650 100
2581 259
8981 15
48668712 21382
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
64632896 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 327
6548 deg
Eccentricity:
0003650
Arg of perigee: 100
2581 deg
Mean anomaly: 259
8981 deg
Mean motion: 15
48668712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2138
Checksum: 311
Coasting Arc #12 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4086971
36 A = 6794196
35 meter
Y = -1964354
44 meter E =
0016576
Z = -5074446
12 I = 51
38731
XDOT = 4902
570971 Wp = 82
40099
YDOT = -5589
793388 meter/sec RA = 322
32309 deg
ZDOT = -1787
589624 TA = 170
20761
MA = 170
17526
Ha = 230
854 n
mi
Hp = 221
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13408698
68 X = -4040052
55
Y = -6444732
42 feet Y = -2009795
67 meter
Z = -16648445
27 Z = -5094185
26
XDOT = 16084
550431 XDOT = 4973
396520
YDOT = -18339
217153 feet/sec YDOT = -5534
573391 meter/sec
ZDOT = -5864
795355 ZDOT = -1763
602377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13197959
12 X = -4022737
94
Y = 6642673
00 feet Y = 2024686
73 meter
Z = -16738795
56 Z = -5101984
89
XDOT = -4283
469763 XDOT = -1305
601584
YDOT = -22987
316634 feet/sec YDOT = -7006
534110 meter/sec
ZDOT = -5754
437359 ZDOT = -1753
952507
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 20101
61423730
00016717 00000-0 10270-3 0 9119
2 25544 51
6400 322
8679 0003685 104
8038 255
3520 15
48711396 21539
Satellite: ISS
Catalog Number: 25544
Epoch time: 20101
61423730 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 322
8679 deg
Eccentricity:
0003685
Arg of perigee: 104
8038 deg
Mean anomaly: 255
3520 deg
Mean motion: 15
48711396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 282
Coasting Arc #13 (Orbit 2168)
---------------------------------------
Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4302910
97 A = 6794401
22 meter
Y = 1505955
69 meter E =
0009149
Z = 5032041
53 I = 51
36193
XDOT = -4328
349581 Wp = 116
81959
YDOT = 6036
829307 meter/sec RA = 317
36167 deg
ZDOT = 1887
806556 TA = 314
76209
MA = 314
83649
Ha = 230
771 n
mi
Hp = 221
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14117161
97 X = 4261308
10
Y = 4940799
51 feet Y = 1553841
30 meter
Z = 16509322
60 Z = 5052842
54
XDOT = -14200
621985 XDOT = -4404
703474
YDOT = 19805
870429 feet/sec YDOT = 5987
999707 meter/sec
ZDOT = 6193
591062 ZDOT = 1866
595452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12293053
69 X = 3746922
76
Y = -8332618
97 feet Y = -2539782
26 meter
Z = 16604571
25 Z = 5061073
32
XDOT = 6868
997212 XDOT = 2093
670350
YDOT = 22324
912451 feet/sec YDOT = 6804
633315 meter/sec
ZDOT = 6095
934857 ZDOT = 1858
040944
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 20102
64667188
00016717 00000-0 10270-3 0 9121
2 25544 51
6400 317
7623 0003702 106
7343 253
4213 15
48680522 21692
Satellite: ISS
Catalog Number: 25544
Epoch time: 20102
64667188 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 317
7623 deg
Eccentricity:
0003702
Arg of perigee: 106
7343 deg
Mean anomaly: 253
4213 deg
Mean motion: 15
48680522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2169
Checksum: 287
Coasting Arc #14 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4474678
68 A = 6794398
85 meter
Y = -1053124
89 meter E =
0016183
Z = -5017764
86 I = 51
33806
XDOT = 3706
432555 Wp = 83
37524
YDOT = -6393
264112 meter/sec RA = 312
39891 deg
ZDOT = -1967
125748 TA = 167
41100
MA = 167
37053
Ha = 230
882 n
mi
Hp = 221
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14680704
32 X = -4438196
18
Y = -3455134
16 feet Y = -1102959
89 meter
Z = -16462483
14 Z = -5039412
63
XDOT = 12160
211795 XDOT = 3787
203684
YDOT = -20975
275957 feet/sec YDOT = -6351
364504 meter/sec
ZDOT = -6453
824632 ZDOT = -1948
925137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11264622
05 X = -3433456
80
Y = 9863801
98 feet Y = 3006486
84 meter
Z = -16561644
94 Z = -5047989
38
XDOT = -9290
641297 XDOT = -2831
787467
YDOT = -21285
357013 feet/sec YDOT = -6487
776818 meter/sec
ZDOT = -6369
951904 ZDOT = -1941
561340
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 20103
61457596
00016717 00000-0 10270-3 0 9130
2 25544 51
6396 312
9765 0003897 111
7286 248
4279 15
48720298 21845
Satellite: ISS
Catalog Number: 25544
Epoch time: 20103
61457596 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 312
9765 deg
Eccentricity:
0003897
Arg of perigee: 111
7286 deg
Mean anomaly: 248
4279 deg
Mean motion: 15
48720298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2184
Checksum: 339
Coasting Arc #15 (Orbit 2199)
---------------------------------------
Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4589814
10 A = 6794576
14 meter
Y = 555299
87 meter E =
0009736
Z = 4973337
65 I = 51
31625
XDOT = -3059
065361 Wp = 120
08456
YDOT = 6716
690542 meter/sec RA = 307
43444 deg
ZDOT = 2065
372048 TA = 309
67675
MA = 309
76258
Ha = 230
699 n
mi
Hp = 221
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15058445
20 X = 4559105
77
Y = 1821849
96 feet Y = 606454
66 meter
Z = 16316724
58 Z = 4995558
64
XDOT = -10036
303679 XDOT = -3143
978441
YDOT = 22036
386293 feet/sec YDOT = 6682
007088 meter/sec
ZDOT = 6776
155013 ZDOT = 2050
306138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9960939
60 X = 3036094
39
Y = -11292579
25 feet Y = -3441978
16 meter
Z = 16418548
85 Z = 5004373
69
XDOT = 11640
711560 XDOT = 3548
088883
YDOT = 20056
110065 feet/sec YDOT = 6113
102348 meter/sec
ZDOT = 6706
640411 ZDOT = 2044
183997
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
64700648
00016717 00000-0 10270-3 0 9144
2 25544 51
6391 307
8712 0003745 115
9400 244
2136 15
48703601 22005
Satellite: ISS
Catalog Number: 25544
Epoch time: 20104
64700648 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 307
8712 deg
Eccentricity:
0003745
Arg of perigee: 115
9400 deg
Mean anomaly: 244
2136 deg
Mean motion: 15
48703601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2200
Checksum: 273
Coasting Arc #16 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2020/105/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4659883
87 A = 6794591
90 meter
Y = -76338
21 meter E =
0015492
Z = -4958247
96 I = 51
29905
XDOT = 2386
203775 Wp = 84
26941
YDOT = -6943
758976 meter/sec RA = 302
46902 deg
ZDOT = -2139
990979 TA = 164
74304
MA = 164
69627
Ha = 230
801 n
mi
Hp = 221
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15288332
89 X = -4634599
60
Y = -250453
45 feet Y = -128306
93 meter
Z = -16267217
72 Z = -4980822
41
XDOT = 7828
752542 XDOT = 2474
068430
YDOT = -22781
361470 feet/sec YDOT = -6916
583448 meter/sec
ZDOT = -7020
967779 ZDOT = -2128
186406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8581482
03 X = -2615635
72
Y = 12521052
09 feet Y = 3816416
68 meter
Z = -16370694
63 Z = -4989787
72
XDOT = -13744
907245 XDOT = -4189
447728
YDOT = -18510
250267 feet/sec YDOT = -5641
924281 meter/sec
ZDOT = -6966
402039 ZDOT = -2123
359341
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
61490669
00016717 00000-0 10270-3 0 9152
2 25544 51
6410 303
0859 0003883 119
1684 240
9855 15
48737339 22152
Satellite: ISS
Catalog Number: 25544
Epoch time: 20105
61490669 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 303
0859 deg
Eccentricity:
0003883
Arg of perigee: 119
1684 deg
Mean anomaly: 240
9855 deg
Mean motion: 15
48737339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 318
Coasting Arc #17 (Orbit 2230)
---------------------------------------
Vector Time (GMT): 2020/106/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4667599
41 A = 6794724
12 meter
Y = -436813
27 meter E =
0010227
Z = 4912819
64 I = 51
28187
XDOT = -1693
612568 Wp = 122
28159
YDOT = 7132
483389 meter/sec RA = 297
50111 deg
ZDOT = 2234
457749 TA = 305
72783
MA = 305
82292
Ha = 230
602 n
mi
Hp = 221
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15313646
34 X = 4648273
50
Y = -1433114
40 feet Y = -384724
89 meter
Z = 16118174
66 Z = 4935445
98
XDOT = -5556
471679 XDOT = -1784
097911
YDOT = 23400
536053 feet/sec YDOT = 7113
038281 meter/sec
ZDOT = 7330
898126 ZDOT = 2226
011077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6958915
87 X = 2121077
56
Y = -13593376
31 feet Y = -4143261
10 meter
Z = 16221921
77 Z = 4944441
76
XDOT = 15735
416673 XDOT = 4796
155002
YDOT = 16791
420903 feet/sec YDOT = 5118
025091 meter/sec
ZDOT = 7291
729846 ZDOT = 2222
519257
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
64733029
00016717 00000-0 10270-3 0 9167
2 25544 51
6403 297
9800 0003772 123
4978 236
6533 15
48739524 22313
Satellite: ISS
Catalog Number: 25544
Epoch time: 20106
64733029 = yrday
fracday
Element set: 916
Inclination: 51
6403 deg
RA of node: 297
9800 deg
Eccentricity:
0003772
Arg of perigee: 123
4978 deg
Mean anomaly: 236
6533 deg
Mean motion: 15
48739524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2231
Checksum: 314
Coasting Arc #18 (Orbit 2245)
---------------------------------------
Vector Time (GMT): 2020/107/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4633911
44 A = 6794831
82 meter
Y = 919304
42 meter E =
0014800
Z = -4897104
04 I = 51
26800
XDOT = 996
684437 Wp = 85
17617
YDOT = -7224
589219 meter/sec RA = 292
53408 deg
ZDOT = -2304
180283 TA = 162
13182
MA = 162
07973
Ha = 230
744 n
mi
Hp = 221
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15203121
53 X = -4620059
75
Y = 3016090
61 feet Y = 867562
09 meter
Z = -16066614
31 Z = -4919580
04
XDOT = 3269
962063 XDOT = 1088
590197
YDOT = -23702
720535 feet/sec YDOT = -7212
929748 meter/sec
ZDOT = -7559
646599 ZDOT = -2299
115451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5316851
51 X = -1620576
34
Y = 14444365
91 feet Y = 4402642
73 meter
Z = -16169699
62 Z = -4928524
44
XDOT = -17420
142417 XDOT = -5309
659409
YDOT = -14830
718601 feet/sec YDOT = -4520
403029 meter/sec
ZDOT = -7535
993944 ZDOT = -2296
970954
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
61522642
00016717 00000-0 10270-3 0 9173
2 25544 51
6405 293
1955 0003900 125
7671 234
3842 15
48741800 22466
Satellite: ISS
Catalog Number: 25544
Epoch time: 20107
61522642 = yrday
fracday
Element set: 917
Inclination: 51
6405 deg
RA of node: 293
1955 deg
Eccentricity:
0003900
Arg of perigee: 125
7671 deg
Mean anomaly: 234
3842 deg
Mean motion: 15
48741800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2246
Checksum: 293
Coasting Arc #19 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 916383
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4608391
04 A = 6795254
54 meter
Y = -1436261
91 meter E =
0010833
Z = 4776992
06 I = 51
26248
XDOT = -438
056863 Wp = 120
59194
YDOT = 7203
371547 meter/sec RA = 290
13706 deg
ZDOT = 2578
577604 TA = 303
80224
MA = 303
90535
Ha = 230
488 n
mi
Hp = 222
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15119393
18 X = 4600905
44
Y = -4712145
37 feet Y = -1384769
34 meter
Z = 15672546
13 Z = 4799359
58
XDOT = -1437
194434 XDOT = -531
099743
YDOT = 23633
108749 feet/sec YDOT = 7197
952712 meter/sec
ZDOT = 8459
900275 ZDOT = 2576
223541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5268872
09 X = -1605952
21
Y = 14826067
73 feet Y = 4518985
45 meter
Z = 15775163
04 Z = 4808269
69
XDOT = -16897
390569 XDOT = -5150
324645
YDOT = -15028
498667 feet/sec YDOT = -4580
686394 meter/sec
ZDOT = 8448
684487 ZDOT = 2575
159032
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
13143575
00016717 00000-0 10270-3 0 9186
2 25544 51
6395 290
6467 0003498 124
7902 235
3577 15
48750448 22545
Satellite: ISS
Catalog Number: 25544
Epoch time: 20108
13143575 = yrday
fracday
Element set: 918
Inclination: 51
6395 deg
RA of node: 290
6467 deg
Eccentricity:
0003498
Arg of perigee: 124
7902 deg
Mean anomaly: 235
3577 deg
Mean motion: 15
48750448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 325
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