[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 31st 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
093/12:44:33
314 1
5 1
5 1
5
N/A -0
0 0
0 231
0
000/00:07:06
628 -0
2 -0
0 222
0
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
9
000/00:00:00
000 0
0 0
0 222
0
100/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
0
000/00:00:00
000 0
0 0
0 222
0
100/08:05:06
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
100/14:16:50
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 222
0
Coasting Arc #1 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2020/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1345338
14 A = 6792550
14 meter
Y = -3994561
34 meter E =
0019602
Z = -5343428
42 I = 51
74102
XDOT = 7280
596651 Wp = 84
51889
YDOT = 2332
018574 meter/sec RA = 17
21775 deg
ZDOT = 91
845100 TA = 186
34526
MA = 186
37012
Ha = 230
996 n
mi
Hp = 221
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4413839
05 X = 1415861
96
Y = -13105516
21 feet Y = -3979122
66 meter
Z = -17530933
15 Z = -5336721
85
XDOT = 23886
471952 XDOT = 7253
532089
YDOT = 7650
979573 feet/sec YDOT = 2413
284058 meter/sec
ZDOT = 301
329069 ZDOT = 127
145747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2798157
69 X = 852878
46
Y = -13582905
27 feet Y = -4140069
53 meter
Z = -17499861
30 Z = -5333957
72
XDOT = 23682
806164 XDOT = 7218
519319
YDOT = 4291
092295 feet/sec YDOT = 1307
924932 meter/sec
ZDOT = 463
106528 ZDOT = 141
154870
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 20090
51591554
00016717 00000-0 10270-3 0 9003
2 25544 51
6438 17
7469 0005115 67
1240 293
0449 15
48928755 19819
Satellite: ISS
Catalog Number: 25544
Epoch time: 20090
51591554 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 17
7469 deg
Eccentricity:
0005115
Arg of perigee: 67
1240 deg
Mean anomaly: 293
0449 deg
Mean motion: 15
48928755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1981
Checksum: 316
Coasting Arc #2 (Orbit 1996)
---------------------------------------
Vector Time (GMT): 2020/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -979844
47 A = 6792416
83 meter
Y = 4090903
36 meter E =
0007394
Z = 5326912
81 I = 51
70819
XDOT = -7477
138588 Wp = 74
06329
YDOT = -1689
077594 meter/sec RA = 12
28012 deg
ZDOT = -76
131974 TA = 16
67386
MA = 16
64956
Ha = 230
964 n
mi
Hp = 221
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3214712
83 X = -1051392
47
Y = 13421598
96 feet Y = 4079546
10 meter
Z = 17476748
06 Z = 5321979
24
XDOT = -24531
294580 XDOT = -7457
325302
YDOT = -5541
593157 feet/sec YDOT = -1772
581493 meter/sec
ZDOT = -249
776819 ZDOT = -112
404886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1331277
69 X = -405773
44
Y = 13766007
49 feet Y = 4195879
08 meter
Z = 17453800
66 Z = 5319918
44
XDOT = -24072
349479 XDOT = -7337
252121
YDOT = -1791
842687 feet/sec YDOT = -546
153651 meter/sec
ZDOT = -416
053909 ZDOT = -126
813231
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 20091
54820301
00016717 00000-0 10270-3 0 9013
2 25544 51
6434 12
6423 0005008 70
1565 290
0125 15
48967147 19977
Satellite: ISS
Catalog Number: 25544
Epoch time: 20091
54820301 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 12
6423 deg
Eccentricity:
0005008
Arg of perigee: 70
1565 deg
Mean anomaly: 290
0125 deg
Mean motion: 15
48967147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1997
Checksum: 284
Coasting Arc #3 (Orbit 2011)
---------------------------------------
Vector Time (GMT): 2020/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 601421
69 A = 6792508
75 meter
Y = -4177635
57 meter E =
0019771
Z = -5339092
05 I = 51
67571
XDOT = 7576
707071 Wp = 86
09752
YDOT = 1020
701757 meter/sec RA = 7
33888 deg
ZDOT = 56
309393 TA = 184
43162
MA = 184
44916
Ha = 231
009 n
mi
Hp = 221
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1973168
28 X = 674026
75
Y = -13706153
44 feet Y = -4170504
17 meter
Z = -17516706
20 Z = -5335994
17
XDOT = 24857
962832 XDOT = 7564
456649
YDOT = 3348
759045 feet/sec YDOT = 1105
361387 meter/sec
ZDOT = 184
742103 ZDOT = 93
084221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -176770
96 X = -53879
79
Y = -13864693
90 feet Y = -4225958
70 meter
Z = -17502172
62 Z = -5334662
21
XDOT = 24058
172882 XDOT = 7332
931094
YDOT = -746
623320 feet/sec YDOT = -227
570788 meter/sec
ZDOT = 353
364828 ZDOT = 107
705599
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 20092
51597385
00016717 00000-0 10270-3 0 9025
2 25544 51
6440 7
8556 0005107 74
2499 285
9214 15
48942018 20129
Satellite: ISS
Catalog Number: 25544
Epoch time: 20092
51597385 = yrday
fracday
Element set: 902
Inclination: 51
6440 deg
RA of node: 7
8556 deg
Eccentricity:
0005107
Arg of perigee: 74
2499 deg
Mean anomaly: 285
9214 deg
Mean motion: 15
48942018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2012
Checksum: 308
Coasting Arc #4 (Orbit 2027)
---------------------------------------
Vector Time (GMT): 2020/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -225054
54 A = 6792384
47 meter
Y = 4206258
47 meter E =
0007303
Z = 5322318
26 I = 51
64252
XDOT = -7657
706299 Wp = 79
54701
YDOT = -354
148325 meter/sec RA = 2
39606 deg
ZDOT = -42
576100 TA = 10
86668
MA = 10
85092
Ha = 230
908 n
mi
Hp = 221
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -738367
90 X = -297926
07
Y = 13800060
61 feet Y = 4203334
42 meter
Z = 17461674
09 Z = 5321047
96
XDOT = -25123
708331 XDOT = -7652
970164
YDOT = -1161
903952 feet/sec YDOT = -439
755761 meter/sec
ZDOT = -139
685367 ZDOT = -79
762521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1647048
77 X = 502020
46
Y = 13729124
80 feet Y = 4184637
24 meter
Z = 17455523
04 Z = 5320443
42
XDOT = -23918
419924 XDOT = -7290
334393
YDOT = 3269
490990 feet/sec YDOT = 996
540854 meter/sec
ZDOT = -310
239416 ZDOT = -94
560974
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
54825725
00016717 00000-0 10270-3 0 9032
2 25544 51
6442 2
7503 0004895 77
5235 282
6463 15
48977249 20285
Satellite: ISS
Catalog Number: 25544
Epoch time: 20093
54825725 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 2
7503 deg
Eccentricity:
0004895
Arg of perigee: 77
5235 deg
Mean anomaly: 282
6463 deg
Mean motion: 15
48977249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2028
Checksum: 321
Coasting Arc #5 (Orbit 2027)
---------------------------------------
Vector Time (GMT): 2020/093/12:48:06
628
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 967565
13 A = 6793512
62 meter
Y = -4159258
41 meter E =
0018078
Z = -5299285
15 I = 51
64299
XDOT = 7564
668648 Wp = 91
22234
YDOT = 856
675896 meter/sec RA = 2
22534 deg
ZDOT = 710
534727 TA = 185
57347
MA = 185
59362
Ha = 230
958 n
mi
Hp = 221
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3174426
28 X = 1039744
03
Y = -13645860
94 feet Y = -4148034
95 meter
Z = -17386106
15 Z = -5294409
73
XDOT = 24818
466694 XDOT = 7551
075474
YDOT = 2810
616458 feet/sec YDOT = 941
193411 meter/sec
ZDOT = 2331
150679 ZDOT = 747
247683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2169593
13 X = -661291
99
Y = -13869666
63 feet Y = -4227474
39 meter
Z = -17363421
41 Z = -5292370
84
XDOT = 22983
815006 XDOT = 7005
466814
YDOT = -6717
304257 feet/sec YDOT = -2047
434338 meter/sec
ZDOT = 2499
493853 ZDOT = 761
845726
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
54825878
00016717 00000-0 10270-3 0 9042
2 25544 51
6452 2
7505 0003740 75
3775 284
7790 15
48662792 20281
Satellite: ISS
Catalog Number: 25544
Epoch time: 20093
54825878 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 2
7505 deg
Eccentricity:
0003740
Arg of perigee: 75
3775 deg
Mean anomaly: 284
7790 deg
Mean motion: 15
48662792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2028
Checksum: 327
Coasting Arc #6 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2020/094/12:48:06
628
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -471421
78 A = 6793357
92 meter
Y = 4222687
51 meter E =
0006608
Z = 5295344
34 I = 51
60962
XDOT = -7640
927822 Wp = 71
67245
YDOT = -107
088902 meter/sec RA = 357
28268 deg
ZDOT = -592
202885 TA = 24
00020
MA = 23
96941
Ha = 230
926 n
mi
Hp = 221
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1546659
38 X = -544327
63
Y = 13853961
65 feet Y = 4217008
28 meter
Z = 17373176
96 Z = 5292877
15
XDOT = -25068
660834 XDOT = -7636
285876
YDOT = -351
341542 feet/sec YDOT = -192
509257 meter/sec
ZDOT = -1942
922850 ZDOT = -629
307941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3984106
42 X = 1214355
64
Y = 13373690
09 feet Y = 4076300
74 meter
Z = 17361537
83 Z = 5291796
73
XDOT = -22151
838098 XDOT = -6751
880252
YDOT = 9353
636257 feet/sec YDOT = 2850
988331 meter/sec
ZDOT = -2113
112780 ZDOT = -644
076775
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
58073311
00016717 00000-0 10270-3 0 9055
2 25544 51
6456 357
6461 0003687 78
3704 281
7860 15
48691144 20449
Satellite: ISS
Catalog Number: 25544
Epoch time: 20094
58073311 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 357
6461 deg
Eccentricity:
0003687
Arg of perigee: 78
3704 deg
Mean anomaly: 281
7860 deg
Mean motion: 15
48691144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 318
Coasting Arc #7 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2020/095/12:48:06
628
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -36845
40 A = 6793388
01 meter
Y = -4249914
09 meter E =
0018393
Z = -5315691
95 I = 51
57539
XDOT = 7603
967938 Wp = 90
86272
YDOT = -648
936610 meter/sec RA = 352
33813 deg
ZDOT = 467
254718 TA = 183
60459
MA = 183
61786
Ha = 230
977 n
mi
Hp = 221
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -120883
86 X = 36501
50
Y = -13943287
71 feet Y = -4249916
31 meter
Z = -17439934
22 Z = -5315692
55
XDOT = 24947
401370 XDOT = 7608
389762
YDOT = -2129
057118 feet/sec YDOT = -563
878881 meter/sec
ZDOT = 1532
987920 ZDOT = 504
202270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5768342
73 X = -1758190
86
Y = -12695163
29 feet Y = -3869485
77 meter
Z = -17439617
02 Z = -5315595
27
XDOT = 20898
444550 XDOT = 6369
845899
YDOT = -11829
344307 feet/sec YDOT = -3605
584145 meter/sec
ZDOT = 1702
500555 ZDOT = 518
922169
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
54867848
00016717 00000-0 10270-3 0 9069
2 25544 51
6450 352
8611 0003782 81
0068 279
1509 15
48670390 20594
Satellite: ISS
Catalog Number: 25544
Epoch time: 20095
54867848 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 352
8611 deg
Eccentricity:
0003782
Arg of perigee: 81
0068 deg
Mean anomaly: 279
1509 deg
Mean motion: 15
48670390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 327
Coasting Arc #8 (Orbit 2068)
---------------------------------------
Vector Time (GMT): 2020/096/04:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5153994
43 A = 6798828
19 meter
Y = -2156222
18 meter E =
0010367
Z = -3884943
22 I = 51
57021
XDOT = 4864
517199 Wp = 78
34575
YDOT = -4242
886992 meter/sec RA = 349
21640 deg
ZDOT = -4105
943998 TA = 148
43898
MA = 148
37676
Ha = 231
040 n
mi
Hp = 221
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16909430
54 X = -5110629
17
Y = -7074219
76 feet Y = -2213615
62 meter
Z = -12745876
70 Z = -3909873
63
XDOT = 15959
702096 XDOT = 4931
545050
YDOT = -13920
232915 feet/sec YDOT = -4188
114014 meter/sec
ZDOT = -13470
944875 ZDOT = -4082
151167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11369162
02 X = 3465320
58
Y = -14275570
56 feet Y = -4351193
91 meter
Z = -12860055
97 Z = -3919745
06
XDOT = 8009
076081 XDOT = 2441
166389
YDOT = 18393
792643 feet/sec YDOT = 5606
427998 meter/sec
ZDOT = -13361
506101 ZDOT = -4072
587060
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
19397380
00016717 00000-0 10270-3 0 9071
2 25544 51
6427 349
6699 0003924 86
8672 273
2927 15
48654658 20699
Satellite: ISS
Catalog Number: 25544
Epoch time: 20096
19397380 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 349
6699 deg
Eccentricity:
0003924
Arg of perigee: 86
8672 deg
Mean anomaly: 273
2927 deg
Mean motion: 15
48654658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2069
Checksum: 364
Coasting Arc #9 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2020/097/04:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 939584
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5403344
53 A = 6799116
35 meter
Y = 1605501
96 meter E =
0015212
Z = 3789822
60 I = 51
53761
XDOT = -4356
826939 Wp = 94
92171
YDOT = 4698
157156 meter/sec RA = 344
26694 deg
ZDOT = 4205
579247 TA = 310
52241
MA = 310
65482
Ha = 230
934 n
mi
Hp = 221
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17727508
30 X = 5366581
03
Y = 5267394
87 feet Y = 1665720
79 meter
Z = 12433801
18 Z = 3815980
38
XDOT = -14294
051636 XDOT = -4429
467529
YDOT = 15413
901429 feet/sec YDOT = 4649
030238 meter/sec
ZDOT = 13797
832176 ZDOT = 4184
238722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9583191
48 X = -2920956
76
Y = 15721893
73 feet Y = 4792033
21 meter
Z = 12553641
29 Z = 3826349
86
XDOT = -10100
648444 XDOT = -3078
677646
YDOT = -17136
860203 feet/sec YDOT = -5223
314990 meter/sec
ZDOT = 13699
621580 ZDOT = 4175
644657
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
22644558
00016717 00000-0 10270-3 0 9089
2 25544 51
6419 344
5656 0003856 89
2997 270
8595 15
48654684 20859
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
22644558 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 344
5656 deg
Eccentricity:
0003856
Arg of perigee: 89
2997 deg
Mean anomaly: 270
8595 deg
Mean motion: 15
48654684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 362
Coasting Arc #10 (Orbit 2090)
---------------------------------------
Vector Time (GMT): 2020/097/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6598428
29 A = 6804620
60 meter
Y = 1071935
23 meter E =
0011345
Z = -1253906
85 I = 51
54443
XDOT = 294
340309 Wp = 127
29256
YDOT = -4956
397693 meter/sec RA = 342
20582 deg
ZDOT = -5829
146255 TA = 66
32396
MA = 66
20494
Ha = 230
904 n
mi
Hp = 222
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21648386
77 X = -6603833
83
Y = 3516847
86 feet Y = 998116
56 meter
Z = -4113867
61 Z = -1285972
59
XDOT = 965
683427 XDOT = 378
056943
YDOT = -16261
147287 feet/sec YDOT = -4952
638642 meter/sec
ZDOT = -19124
495587 ZDOT = -5827
512660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12925297
61 X = -3939630
71
Y = 17684044
07 feet Y = 5390096
63 meter
Z = -4260990
80 Z = -1298749
99
XDOT = -9348
536933 XDOT = -2849
434057
YDOT = -11406
117760 feet/sec YDOT = -3476
584693 meter/sec
ZDOT = -19116
643171 ZDOT = -5826
752838
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
61362154
00016717 00000-0 10270-3 0 9092
2 25544 51
6439 342
6523 0003525 89
2103 270
9450 15
48638395 20914
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
61362154 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 342
6523 deg
Eccentricity:
0003525
Arg of perigee: 89
2103 deg
Mean anomaly: 270
9450 deg
Mean motion: 15
48638395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2091
Checksum: 310
Coasting Arc #11 (Orbit 2106)
---------------------------------------
Vector Time (GMT): 2020/098/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6473063
53 A = 6804628
16 meter
Y = -1742751
77 meter E =
0016745
Z = 1126832
88 I = 51
51228
XDOT = 296
033450 Wp = 64
27679
YDOT = 4927
478376 meter/sec RA = 337
25093 deg
ZDOT = 5859
280533 TA = 307
94990
MA = 308
10109
Ha = 230
879 n
mi
Hp = 221
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21237085
07 X = 6486596
87
Y = -5717689
52 feet Y = -1670289
58 meter
Z = 3696958
26 Z = 1158309
65
XDOT = 971
238353 XDOT = 212
449776
YDOT = 16166
267638 feet/sec YDOT = 4930
322067 meter/sec
ZDOT = 19223
361328 ZDOT = 5860
515056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10761305
89 X = 3280046
03
Y = -19152313
11 feet Y = -5837625
04 meter
Z = 3841413
09 Z = 1170862
71
XDOT = 10739
623600 XDOT = 3273
437273
YDOT = 9929
719232 feet/sec YDOT = 3026
578422 meter/sec
ZDOT = 19228
667267 ZDOT = 5860
897783
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
64608809
00016717 00000-0 10270-3 0 9108
2 25544 51
6429 337
5469 0003593 92
1418 268
0143 15
48684219 21073
Satellite: ISS
Catalog Number: 25544
Epoch time: 20098
64608809 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 337
5469 deg
Eccentricity:
0003593
Arg of perigee: 92
1418 deg
Mean anomaly: 268
0143 deg
Mean motion: 15
48684219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2107
Checksum: 325
Coasting Arc #12 (Orbit 2121)
---------------------------------------
Vector Time (GMT): 2020/099/14:00:43
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6291590
28 A = 6804787
32 meter
Y = 2358816
09 meter E =
0012233
Z = -1051088
58 I = 51
48059
XDOT = -841
978633 Wp = 128
78737
YDOT = -4839
581867 meter/sec RA = 332
29536 deg
ZDOT = -5874
703270 TA = 62
60544
MA = 62
48103
Ha = 230
913 n
mi
Hp = 221
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20641700
39 X = -6312394
02
Y = 7738897
94 feet Y = 2288342
64 meter
Z = -3448453
34 Z = -1081701
68
XDOT = -2762
397091 XDOT = -759
262199
YDOT = -15877
893263 feet/sec YDOT = -4848
535475 meter/sec
ZDOT = -19273
960860 ZDOT = -5878
591994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8554298
31 X = -2607350
13
Y = 20292988
60 feet Y = 6185302
93 meter
Z = -3588977
67 Z = -1093920
40
XDOT = -11860
646308 XDOT = -3615
124995
YDOT = -8381
591348 feet/sec YDOT = -2554
709043 meter/sec
ZDOT = -19291
444451 ZDOT = -5880
032269
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
61402654
00016717 00000-0 10270-3 0 9117
2 25544 51
6414 332
7616 0003617 95
2323 264
9240 15
48652172 21227
Satellite: ISS
Catalog Number: 25544
Epoch time: 20099
61402654 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 332
7616 deg
Eccentricity:
0003617
Arg of perigee: 95
2323 deg
Mean anomaly: 264
9240 deg
Mean motion: 15
48652172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2122
Checksum: 288
Coasting Arc #13 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1831520
39 A = 6797895
80 meter
Y = -5021436
48 meter E =
0011511
Z = -4211924
46 I = 51
43681
XDOT = 6689
436133 Wp = 105
00896
YDOT = -623
062209 meter/sec RA = 328
95864 deg
ZDOT = 3657
144308 TA = 202
65979
MA = 202
71065
Ha = 231
010 n
mi
Hp = 221
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6008925
17 X = 1907994
82
Y = -16474529
13 feet Y = -5000527
81 meter
Z = -13818649
82 Z = -4202841
46
XDOT = 21946
968939 XDOT = 6678
141698
YDOT = -2044
167353 feet/sec YDOT = -548
319074 meter/sec
ZDOT = 11998
504946 ZDOT = 3689
611962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17540432
52 X = 5346323
83
Y = 1004734
27 feet Y = 306243
01 meter
Z = -13776650
91 Z = -4199123
20
XDOT = 8436
819737 XDOT = 2571
542656
YDOT = 19026
197643 feet/sec YDOT = 5799
185042 meter/sec
ZDOT = 12147
400023 ZDOT = 3702
527527
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
25931909
00016717 00000-0 10270-3 0 9121
2 25544 51
6404 329
5715 0003752 96
6487 263
5090 15
48648513 21329
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
25931909 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 329
5715 deg
Eccentricity:
0003752
Arg of perigee: 96
6487 deg
Mean anomaly: 263
5090 deg
Mean motion: 15
48648513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 304
Coasting Arc #14 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS) : 915571
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3860339
91 A = 6794247
94 meter
Y = 2368983
32 meter E =
0008759
Z = 5058325
91 I = 51
42450
XDOT = -5478
950318 Wp = 113
57195
YDOT = 5043
578312 meter/sec RA = 328
56810 deg
ZDOT = 1813
335169 TA = 318
77965
MA = 318
84576
Ha = 230
756 n
mi
Hp = 221
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12665157
18 X = 3808991
58
Y = 7772254
99 feet Y = 2411865
62 meter
Z = 16595557
45 Z = 5076953
28
XDOT = -17975
558785 XDOT = -5543
750146
YDOT = 16547
172939 feet/sec YDOT = 4981
946592 meter/sec
ZDOT = 5949
262364 ZDOT = 1786
562533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4227539
93 X = 1288554
17
Y = 14145879
94 feet Y = 4311664
21 meter
Z = 16680787
39 Z = 5084304
00
XDOT = -23426
712551 XDOT = -7140
461986
YDOT = 108
107192 feet/sec YDOT = 32
951072 meter/sec
ZDOT = 5826
163020 ZDOT = 1775
814488
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
38837628
00016717 00000-0 10270-3 0 9139
2 25544 51
6421 328
9342 0003633 98
4814 261
6748 15
48698498 21347
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
38837628 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 328
9342 deg
Eccentricity:
0003633
Arg of perigee: 98
4814 deg
Mean anomaly: 261
6748 deg
Mean motion: 15
48698498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 330
Coasting Arc #15 (Orbit 2137)
---------------------------------------
Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931488
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3897042
88 A = 6794430
78 meter
Y = 2298045
06 meter E =
0008751
Z = 5063156
67 I = 51
41517
XDOT = -5379
201238 Wp = 113
77190
YDOT = 5156
443062 meter/sec RA = 327
28592 deg
ZDOT = 1793
988097 TA = 318
77113
MA = 318
83720
Ha = 230
873 n
mi
Hp = 221
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12785573
74 X = 3846461
59
Y = 7539517
91 feet Y = 2341342
04 meter
Z = 16611406
40 Z = 5081964
23
XDOT = -17648
298024 XDOT = -5445
176592
YDOT = 16917
464113 feet/sec YDOT = 5095
920219 meter/sec
ZDOT = 5885
787720 ZDOT = 1767
697173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13781259
09 X = 4200527
77
Y = -5246481
74 feet Y = -1599127
64 meter
Z = 16697466
15 Z = 5089387
68
XDOT = 1886
977863 XDOT = 575
150853
YDOT = 23365
541979 feet/sec YDOT = 7121
817195 meter/sec
ZDOT = 5764
891357 ZDOT = 1757
138886
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
64649349
00016717 00000-0 10270-3 0 9140
2 25544 51
6402 327
6559 0003660 99
1383 261
0181 15
48628813 21384
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
64649349 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 327
6559 deg
Eccentricity:
0003660
Arg of perigee: 99
1383 deg
Mean anomaly: 261
0181 deg
Mean motion: 15
48628813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2138
Checksum: 308
Coasting Arc #16 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931488
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4166546
86 A = 6794442
29 meter
Y = -1872723
92 meter E =
0016398
Z = -5044441
29 I = 51
38756
XDOT = 4817
479875 Wp = 81
69726
YDOT = -5629
197251 meter/sec RA = 322
32612 deg
ZDOT = -1892
256393 TA = 169
85691
MA = 169
82378
Ha = 230
925 n
mi
Hp = 221
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13669773
17 X = -4120792
53
Y = -6144107
34 feet Y = -1919061
52 meter
Z = -16550004
24 Z = -5064569
81
XDOT = 15805
380168 XDOT = 4889
260792
YDOT = -18468
494919 feet/sec YDOT = -5574
923465 meter/sec
ZDOT = -6208
190265 ZDOT = -1868
680169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13118237
12 X = -3998438
67
Y = 7033222
92 feet Y = 2143726
35 meter
Z = -16642146
02 Z = -5072526
11
XDOT = -4525
892922 XDOT = -1379
492163
YDOT = -22851
832790 feet/sec YDOT = -6965
238634 meter/sec
ZDOT = -6099
713704 ZDOT = -1859
192737
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
61442714
00016717 00000-0 10270-3 0 9156
2 25544 51
6398 322
8691 0003696 103
7424 256
4137 15
48670366 21535
Satellite: ISS
Catalog Number: 25544
Epoch time: 20101
61442714 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 322
8691 deg
Eccentricity:
0003696
Arg of perigee: 103
7424 deg
Mean anomaly: 256
4137 deg
Mean motion: 15
48670366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 305
Coasting Arc #17 (Orbit 2168)
---------------------------------------
Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931488
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4382800
05 A = 6794672
24 meter
Y = 1393057
18 meter E =
0009440
Z = 4995732
71 I = 51
36228
XDOT = -4225
467242 Wp = 116
27205
YDOT = 6071
078999 meter/sec RA = 317
36506 deg
ZDOT = 2007
065447 TA = 314
10090
MA = 314
17854
Ha = 230
839 n
mi
Hp = 221
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14379265
25 X = 4342630
08
Y = 4570397
57 feet Y = 1441844
18 meter
Z = 16390199
19 Z = 5016925
28
XDOT = -13863
081503 XDOT = -4302
791069
YDOT = 19918
238185 feet/sec YDOT = 6023
394479 meter/sec
ZDOT = 6584
860390 ZDOT = 1986
351755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12151180
29 X = 3703679
75
Y = -8764120
92 feet Y = -2671304
06 meter
Z = 16487250
67 Z = 5025314
00
XDOT = 7126
832212 XDOT = 2172
258458
YDOT = 22132
581912 feet/sec YDOT = 6746
010967 meter/sec
ZDOT = 6489
481961 ZDOT = 1977
994102
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
64688949
00016717 00000-0 10270-3 0 9163
2 25544 51
6398 317
7637 0003707 105
7018 254
4541 15
48640196 21694
Satellite: ISS
Catalog Number: 25544
Epoch time: 20102
64688949 = yrday
fracday
Element set: 916
Inclination: 51
6398 deg
RA of node: 317
7637 deg
Eccentricity:
0003707
Arg of perigee: 105
7018 deg
Mean anomaly: 254
4541 deg
Mean motion: 15
48640196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2169
Checksum: 331
Coasting Arc #18 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931488
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4551658
46 A = 6794702
83 meter
Y = -918208
83 meter E =
0015928
Z = -4974993
62 I = 51
33851
XDOT = 3586
513003 Wp = 82
63408
YDOT = -6419
283038 meter/sec RA = 312
40269 deg
ZDOT = -2100
365852 TA = 166
79327
MA = 166
75152
Ha = 230
961 n
mi
Hp = 221
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14933262
65 X = -4516886
66
Y = -3012496
16 feet Y = -968914
23 meter
Z = -16322157
56 Z = -4997019
49
XDOT = 11766
774943 XDOT = 3668
231204
YDOT = -21060
639887 feet/sec YDOT = -6378
719158 meter/sec
ZDOT = -6890
964080 ZDOT = -2082
745467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11051047
63 X = -3368359
32
Y = 10327036
34 feet Y = 3147680
68 meter
Z = -16423061
85 Z = -5005749
25
XDOT = -9552
873033 XDOT = -2911
715701
YDOT = -21032
368302 feet/sec YDOT = -6410
665858 meter/sec
ZDOT = -6809
749327 ZDOT = -2075
611595
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
61482054
00016717 00000-0 10270-3 0 9171
2 25544 51
6395 312
9780 0003914 110
6729 249
4840 15
48677293 21842
Satellite: ISS
Catalog Number: 25544
Epoch time: 20103
61482054 = yrday
fracday
Element set: 917
Inclination: 51
6395 deg
RA of node: 312
9780 deg
Eccentricity:
0003914
Arg of perigee: 110
6729 deg
Mean anomaly: 249
4840 deg
Mean motion: 15
48677293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2184
Checksum: 317
Coasting Arc #19 (Orbit 2199)
---------------------------------------
Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931488
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4660266
36 A = 6794906
57 meter
Y = 397162
88 meter E =
0010113
Z = 4923018
13 I = 51
31678
XDOT = -2920
954288 Wp = 119
22301
YDOT = 6730
812289 meter/sec RA = 307
43862 deg
ZDOT = 2213
749294 TA = 309
01445
MA = 309
10445
Ha = 230
771 n
mi
Hp = 222
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15289587
80 X = 4631565
56
Y = 1303027
81 feet Y = 449116
74 meter
Z = 16151634
29 Z = 4945586
22
XDOT = -9583
183359 XDOT = -3006
756278
YDOT = 22082
717482 feet/sec YDOT = 6697
668318 meter/sec
ZDOT = 7262
957002 ZDOT = 2199
352117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9664590
80 X = 2945767
28
Y = -11777663
81 feet Y = -3589831
93 meter
Z = 16255060
34 Z = 4954542
39
XDOT = 11898
087195 XDOT = 3626
536977
YDOT = 19733
090123 feet/sec YDOT = 6014
645869 meter/sec
ZDOT = 7196
506921 ZDOT = 2193
495310
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
64728047
00016717 00000-0 10270-3 0 9181
2 25544 51
6389 307
8729 0003751 115
0572 245
0968 15
48662581 22001
Satellite: ISS
Catalog Number: 25544
Epoch time: 20104
64728047 = yrday
fracday
Element set: 918
Inclination: 51
6389 deg
RA of node: 307
8729 deg
Eccentricity:
0003751
Arg of perigee: 115
0572 deg
Mean anomaly: 245
0968 deg
Mean motion: 15
48662581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2200
Checksum: 316
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