[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 7th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14255 723 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
130/00:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
8
132/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 222
6
132/22:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
8
135/18:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
6
Coasting Arc #1 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2020/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1618892
22 A = 6791314
21 meter
Y = -3935052
67 meter E =
0001334
Z = 5292025
59 I = 51
52725
XDOT = 7306
346432 Wp = 68
48972
YDOT = 2235
241336 meter/sec RA = 193
59745 deg
ZDOT = -572
417150 TA = 26
98951
MA = 26
98257
Ha = 227
946 n
mi
Hp = 222
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5311326
17 X = 1637068
71
Y = -12910277
77 feet Y = -3916847
57 meter
Z = 17362288
67 Z = 5299933
72
XDOT = 23970
952861 XDOT = 7283
588803
YDOT = 7333
468951 feet/sec YDOT = 2316
818872 meter/sec
ZDOT = -1878
009021 ZDOT = -536
980330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5210503
86 X = -1588161
58
Y = -12902354
92 feet Y = -3932637
78 meter
Z = 17398689
97 Z = 5303120
70
XDOT = 21424
264065 XDOT = 6530
115687
YDOT = -10967
825535 feet/sec YDOT = -3342
993223 meter/sec
ZDOT = -1715
397766 ZDOT = -522
853239
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 20127
54749777
00016717 00000-0 10270-3 0 9009
2 25544 51
6425 194
5676 0001458 248
5349 111
5646 15
49374633 25552
Satellite: ISS
Catalog Number: 25544
Epoch time: 20127
54749777 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 194
5676 deg
Eccentricity:
0001458
Arg of perigee: 248
5349 deg
Mean anomaly: 111
5646 deg
Mean motion: 15
49374633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 335
Coasting Arc #2 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2020/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1430284
19 A = 6791502
14 meter
Y = 4028768
03 meter E =
0013324
Z = -5288742
38 I = 51
55919
XDOT = -7425
323333 Wp = 97
80161
YDOT = -1700
556961 meter/sec RA = 188
64206 deg
ZDOT = 712
455806 TA = 179
02780
MA = 179
02520
Ha = 228
069 n
mi
Hp = 222
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4692533
44 X = -1449538
56
Y = 13217742
88 feet Y = 4012666
21 meter
Z = -17351516
98 Z = -5295736
82
XDOT = -24361
297023 XDOT = -7409
216105
YDOT = -5579
255123 feet/sec YDOT = -1783
502190 meter/sec
ZDOT = 2337
453431 ZDOT = 676
424787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6086991
70 X = 1855315
07
Y = 12591985
50 feet Y = 3838037
18 meter
Z = -17383732
96 Z = -5298561
81
XDOT = -20289
079733 XDOT = -6184
111503
YDOT = 12807
431001 feet/sec YDOT = 3903
704969 meter/sec
ZDOT = 2172
079345 ZDOT = 662
049784
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 20128
51500711
00016717 00000-0 10270-3 0 9011
2 25544 51
6413 189
7795 0001388 253
6855 106
4142 15
49332805 25704
Satellite: ISS
Catalog Number: 25544
Epoch time: 20128
51500711 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 189
7795 deg
Eccentricity:
0001388
Arg of perigee: 253
6855 deg
Mean anomaly: 106
4142 deg
Mean motion: 15
49332805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 299
Coasting Arc #3 (Orbit 2585)
---------------------------------------
Vector Time (GMT): 2020/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1236428
73 A = 6791433
60 meter
Y = -4104290
05 meter E =
0001987
Z = 5266662
59 I = 51
59311
XDOT = 7524
255658 Wp = 48
61914
YDOT = 1165
608136 meter/sec RA = 183
68891 deg
ZDOT = -856
584435 TA = 49
59169
MA = 49
57435
Ha = 227
947 n
mi
Hp = 222
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4056524
70 X = 1256649
31
Y = -13465518
52 feet Y = -4090350
81 meter
Z = 17279076
75 Z = 5272717
55
XDOT = 24685
878143 XDOT = 7514
823136
YDOT = 3824
173675 feet/sec YDOT = 1249
697050 meter/sec
ZDOT = -2810
316387 ZDOT = -820
056671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6923000
17 X = -2110130
45
Y = -12201732
49 feet Y = -3719088
06 meter
Z = 17306988
99 Z = 5275170
24
XDOT = 19054
792629 XDOT = 5807
900793
YDOT = -14566
528931 feet/sec YDOT = -4439
878018 meter/sec
ZDOT = -2642
622371 ZDOT = -805
471299
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 20129
54701223
00016717 00000-0 10270-3 0 9027
2 25544 51
6415 184
6721 0001378 260
0071 100
0923 15
49376539 25866
Satellite: ISS
Catalog Number: 25544
Epoch time: 20129
54701223 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 184
6721 deg
Eccentricity:
0001378
Arg of perigee: 260
0071 deg
Mean anomaly: 100
0923 deg
Mean motion: 15
49376539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2586
Checksum: 287
Coasting Arc #4 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6603524
83 A = 6802744
52 meter
Y = 1077349
05 meter E =
0008427
Z = -1205591
42 I = 51
64861
XDOT = -1813
776805 Wp = 149
64657
YDOT = 4596
968893 meter/sec RA = 181
06975 deg
ZDOT = -5851
836501 TA = 43
42234
MA = 43
35599
Ha = 228
077 n
mi
Hp = 222
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21665107
72 X = 6596842
98
Y = 3534609
76 feet Y = 1151157
13 meter
Z = -3955352
44 Z = -1173529
67
XDOT = -5950
711304 XDOT = -1836
621324
YDOT = 15081
918939 feet/sec YDOT = 4576
558807 meter/sec
ZDOT = -19198
938652 ZDOT = -5860
702291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14412222
46 X = -4392845
41
Y = 16592197
29 feet Y = 5057301
73 meter
Z = -3808149
77 Z = -1160724
05
XDOT = -8557
473293 XDOT = -2608
317860
YDOT = -11829
397188 feet/sec YDOT = -3605
600263 meter/sec
ZDOT = -19239
776020 ZDOT = -5864
283731
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 20130
06301554
00016717 00000-0 10270-3 0 9030
2 25544 51
6420 182
1197 0001406 272
3947 87
7042 15
49329617 25949
Satellite: ISS
Catalog Number: 25544
Epoch time: 20130
06301554 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 182
1197 deg
Eccentricity:
0001406
Arg of perigee: 272
3947 deg
Mean anomaly: 87
7042 deg
Mean motion: 15
49329617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 293
Coasting Arc #5 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2020/131/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6641206
91 A = 6802482
89 meter
Y = -591602
04 meter E =
0012685
Z = 1315291
63 I = 51
68025
XDOT = 1580
619185 Wp = 55
62393
YDOT = -4720
825453 meter/sec RA = 176
12127 deg
ZDOT = 5824
396220 TA = 318
65744
MA = 318
75339
Ha = 227
996 n
mi
Hp = 222
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21788736
60 X = -6640486
87
Y = -1940951
56 feet Y = -665864
87 meter
Z = 4315261
27 Z = 1283032
54
XDOT = 5185
758482 XDOT = 1604
999461
YDOT = -15488
272482 feet/sec YDOT = -4703
014215 meter/sec
ZDOT = 19108
911483 ZDOT = 5832
132999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12819333
03 X = 3907332
71
Y = -17760565
45 feet Y = -5413420
35 meter
Z = 4167113
03 Z = 1270136
05
XDOT = 9432
316692 XDOT = 2874
970128
YDOT = 11326
374725 feet/sec YDOT = 3452
279016 meter/sec
ZDOT = 19144
577252 ZDOT = 5835
267146
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 20131
09501795
00016717 00000-0 10270-3 0 9044
2 25544 51
6404 177
0112 0001367 277
9708 82
1287 15
49382711 26106
Satellite: ISS
Catalog Number: 25544
Epoch time: 20131
09501795 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 177
0112 deg
Eccentricity:
0001367
Arg of perigee: 277
9708 deg
Mean anomaly: 82
1287 deg
Mean motion: 15
49382711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 294
Coasting Arc #6 (Orbit 2624)
---------------------------------------
Vector Time (GMT): 2020/132/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6640253
62 A = 6802437
33 meter
Y = 130823
51 meter E =
0007528
Z = -1454077
96 I = 51
71278
XDOT = -1357
773220 Wp = 150
17523
YDOT = 4832
067993 meter/sec RA = 171
17647 deg
ZDOT = -5784
986011 TA = 45
63648
MA = 45
57483
Ha = 228
053 n
mi
Hp = 222
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21785609
00 X = 6645360
33
Y = 429211
01 feet Y = 205108
29 meter
Z = -4770596
99 Z = -1421809
56
XDOT = -4454
636550 XDOT = -1383
605583
YDOT = 15853
241448 feet/sec YDOT = 4816
740680 meter/sec
ZDOT = -18979
612897 ZDOT = -5791
643736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11199434
78 X = -3413587
72
Y = 18728640
33 feet Y = 5708489
57 meter
Z = -4622366
21 Z = -1408897
22
XDOT = -10250
289364 XDOT = -3124
288198
YDOT = -10805
305033 feet/sec YDOT = -3293
456974 meter/sec
ZDOT = -19010
333681 ZDOT = -5794
349706
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 20132
06252240
00016717 00000-0 10270-3 0 9051
2 25544 51
6400 172
2233 0001451 280
5001 79
5985 15
49342632 26252
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
06252240 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 172
2233 deg
Eccentricity:
0001451
Arg of perigee: 280
5001 deg
Mean anomaly: 79
5985 deg
Mean motion: 15
49342632 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 267
Coasting Arc #7 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2020/132/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3854999
35 A = 6796623
23 meter
Y = -3985597
94 meter E =
0009919
Z = 3923746
64 I = 51
71317
XDOT = 6187
446708 Wp = 77
37053
YDOT = 1968
621985 meter/sec RA = 168
00399 deg
ZDOT = -4068
579091 TA = 55
24470
MA = 55
15135
Ha = 227
989 n
mi
Hp = 222
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12647635
66 X = 3880221
58
Y = -13076108
73 feet Y = -3942348
04 meter
Z = 12873184
52 Z = 3942533
58
XDOT = 20300
022009 XDOT = 6184
736037
YDOT = 6458
733546 feet/sec YDOT = 2037
799745 meter/sec
ZDOT = -13348
356597 ZDOT = -4038
529120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16451725
62 X = -5014485
97
Y = -7619408
44 feet Y = -2322395
69 meter
Z = 12959611
34 Z = 3950089
54
XDOT = -1086
825938 XDOT = -331
264546
YDOT = -20182
302715 feet/sec YDOT = -6151
565867 meter/sec
ZDOT = -13210
353515 ZDOT = -4026
515751
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 20132
70752452
00016717 00000-0 10270-3 0 9063
2 25544 51
6382 169
0302 0001251 286
1629 73
9383 15
49367818 26352
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
70752452 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 169
0302 deg
Eccentricity:
0001251
Arg of perigee: 286
1629 deg
Mean anomaly: 73
9383 deg
Mean motion: 15
49367818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 309
Coasting Arc #8 (Orbit 2638)
---------------------------------------
Vector Time (GMT): 2020/132/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6431466
60 A = 6801351
23 meter
Y = 256620
09 meter E =
0005177
Z = -2191394
19 I = 51
74148
XDOT = -2061
886726 Wp = 147
88148
YDOT = 4930
697653 meter/sec RA = 166
71118 deg
ZDOT = -5484
213286 TA = 56
35137
MA = 56
30200
Ha = 228
071 n
mi
Hp = 222
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21100612
20 X = 6438763
57
Y = 841929
43 feet Y = 328582
38 meter
Z = -7189613
48 Z = -2160134
79
XDOT = -6764
720230 XDOT = -2090
230758
YDOT = 16176
829571 feet/sec YDOT = 4907
482329 meter/sec
ZDOT = -17992
825741 ZDOT = -5494
297421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19262247
93 X = -5871133
17
Y = 8772396
08 feet Y = 2673826
32 meter
Z = -7045998
45 Z = -2147620
33
XDOT = -713
967835 XDOT = -217
617396
YDOT = -16029
374410 feet/sec YDOT = -4885
753320 meter/sec
ZDOT = -18039
298456 ZDOT = -5498
378170
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 20132
96552506
00016717 00000-0 10270-3 0 9070
2 25544 51
6425 167
7552 0001453 282
7283 77
3705 15
49335404 26390
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
96552506 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 167
7552 deg
Eccentricity:
0001453
Arg of perigee: 282
7283 deg
Mean anomaly: 77
3705 deg
Mean motion: 15
49335404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2639
Checksum: 314
Coasting Arc #9 (Orbit 2654)
---------------------------------------
Vector Time (GMT): 2020/133/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6391891
46 A = 6801077
93 meter
Y = 201646
64 meter E =
0012820
Z = 2295583
90 I = 51
77327
XDOT = 1797
171255 Wp = 67
57763
YDOT = -5097
047926 meter/sec RA = 161
76891 deg
ZDOT = 5432
348815 TA = 317
89475
MA = 317
99318
Ha = 228
101 n
mi
Hp = 222
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20970772
52 X = -6404821
91
Y = 661570
34 feet Y = 130095
42 meter
Z = 7531443
24 Z = 2264503
20
XDOT = 5896
231150 XDOT = 1827
647144
YDOT = -16722
598183 feet/sec YDOT = -5076
780838 meter/sec
ZDOT = 17822
666715 ZDOT = 5441
152264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18295604
03 X = 5576500
11
Y = -10373663
41 feet Y = -3161892
61 meter
Z = 7388612
39 Z = 2252049
06
XDOT = 1918
578614 XDOT = 584
782761
YDOT = 16153
176186 feet/sec YDOT = 4923
488102 meter/sec
ZDOT = 17863
268076 ZDOT = 5444
724110
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 20133
99752426
00016717 00000-0 10270-3 0 9088
2 25544 51
6425 162
6466 0001471 296
8216 63
2783 15
49364600 26558
Satellite: ISS
Catalog Number: 25544
Epoch time: 20133
99752426 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 162
6466 deg
Eccentricity:
0001471
Arg of perigee: 296
8216 deg
Mean anomaly: 63
2783 deg
Mean motion: 15
49364600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2655
Checksum: 320
Coasting Arc #10 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2020/134/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6320899
72 A = 6800888
10 meter
Y = -628530
13 meter E =
0004263
Z = -2426420
50 I = 51
80307
XDOT = -1533
672091 Wp = 140
50939
YDOT = 5246
030872 meter/sec RA = 156
82997 deg
ZDOT = -5362
559647 TA = 66
49504
MA = 66
45025
Ha = 228
104 n
mi
Hp = 222
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20737859
98 X = 6339244
50
Y = -2062106
73 feet Y = -557742
55 meter
Z = -7960697
19 Z = -2395671
57
XDOT = -5031
732582 XDOT = -1566
172561
YDOT = 17211
387376 feet/sec YDOT = 5228
699005 meter/sec
ZDOT = -17593
699629 ZDOT = -5370
088099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17239455
40 X = -5254586
01
Y = 11804348
85 feet Y = 3597965
53 meter
Z = -7819357
15 Z = -2383340
06
XDOT = -3106
317984 XDOT = -946
805722
YDOT = -16195
333771 feet/sec YDOT = -4936
337733 meter/sec
ZDOT = -17628
453131 ZDOT = -5373
152514
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 20134
96502332
00016717 00000-0 10270-3 0 9096
2 25544 51
6415 157
8585 0001465 294
9486 65
1511 15
49339985 26701
Satellite: ISS
Catalog Number: 25544
Epoch time: 20134
96502332 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 157
8585 deg
Eccentricity:
0001465
Arg of perigee: 294
9486 deg
Mean anomaly: 65
1511 deg
Mean motion: 15
49339985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 331
Coasting Arc #11 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2020/135/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4961002
29 A = 6794969
49 meter
Y = 1371606
70 meter E =
0008345
Z = -4444706
16 I = 51
80972
XDOT = -4445
950976 Wp = 62
37670
YDOT = 5256
763708 meter/sec RA = 152
66628 deg
ZDOT = -3341
231557 TA = 173
88269
MA = 173
87249
Ha = 228
122 n
mi
Hp = 222
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16276254
24 X = 4966885
69
Y = 4500021
99 feet Y = 1427117
39 meter
Z = -14582369
30 Z = -4420593
18
XDOT = -14586
453333 XDOT = -4488
173455
YDOT = 17246
600091 feet/sec YDOT = 5206
810087 meter/sec
ZDOT = -10962
045792 ZDOT = -3362
930394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12610778
26 X = -3843765
21
Y = -11373388
05 feet Y = -3466608
68 meter
Z = -14471574
22 Z = -4410935
82
XDOT = 19881
178603 XDOT = 6059
783238
YDOT = -7973
288641 feet/sec YDOT = -2430
258378 meter/sec
ZDOT = -11061
940015 ZDOT = -3371
679317
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 20135
80352329
00016717 00000-0 10270-3 0 9101
2 25544 51
6417 153
7083 0001304 306
7740 53
3290 15
49383931 26835
Satellite: ISS
Catalog Number: 25544
Epoch time: 20135
80352329 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 153
7083 deg
Eccentricity:
0001304
Arg of perigee: 306
7740 deg
Mean anomaly: 53
3290 deg
Mean motion: 15
49383931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 290
Coasting Arc #12 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2020/136/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4970558
07 A = 6794761
99 meter
Y = -1050261
59 meter E =
0007814
Z = 4507130
44 I = 51
83832
XDOT = 4116
571427 Wp = 108
93719
YDOT = -5599
475557 meter/sec RA = 147
72978 deg
ZDOT = 3227
994634 TA = 308
63266
MA = 308
70258
Ha = 228
274 n
mi
Hp = 222
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16307605
20 X = -4980337
40
Y = -3445740
11 feet Y = -1105900
87 meter
Z = 14787173
37 Z = 4482961
57
XDOT = 13505
811767 XDOT = 4163
200701
YDOT = -18370
982800 feet/sec YDOT = -5553
180607 meter/sec
ZDOT = 10590
533577 ZDOT = 3248
104255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13291218
23 X = 4051163
32
Y = 10218964
55 feet Y = 3114740
39 meter
Z = 14676099
29 Z = 4473275
06
XDOT = -19325
425744 XDOT = -5890
389767
YDOT = 9759
281278 feet/sec YDOT = 2974
628934 meter/sec
ZDOT = 10683
148204 ZDOT = 3256
223573
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20136
83552046
00016717 00000-0 10270-3 0 9114
2 25544 51
6419 148
6007 0001329 306
8244 53
2784 15
49367327 26998
Satellite: ISS
Catalog Number: 25544
Epoch time: 20136
83552046 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 148
6007 deg
Eccentricity:
0001329
Arg of perigee: 306
8244 deg
Mean anomaly: 53
2784 deg
Mean motion: 15
49367327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 316
Coasting Arc #13 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2020/137/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4963617
47 A = 6794410
08 meter
Y = 753368
62 meter E =
0009294
Z = -4587447
34 I = 51
86625
XDOT = -3757
012833 Wp = 62
12178
YDOT = 5903
919391 meter/sec RA = 142
79501 deg
ZDOT = -3096
088718 TA = 176
92496
MA = 176
91925
Ha = 228
139 n
mi
Hp = 222
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16284834
23 X = 4977107
46
Y = 2471681
83 feet Y = 808951
01 meter
Z = -15050680
26 Z = -4563303
12
XDOT = -12326
157587 XDOT = -3807
713891
YDOT = 19369
814274 feet/sec YDOT = 5861
622486 meter/sec
ZDOT = -10157
771385 ZDOT = -3114
461703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13853191
96 X = -4222452
91
Y = -9095189
09 feet Y = -2772213
63 meter
Z = -14939699
50 Z = -4553620
41
XDOT = 18568
509509 XDOT = 5659
681698
YDOT = -11461
256863 feet/sec YDOT = -3493
391092 meter/sec
ZDOT = -10242
427074 ZDOT = -3121
891772
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20137
80301483
00016717 00000-0 10270-3 0 9120
2 25544 51
6429 143
8125 0001424 315
1770 44
9265 15
49391731 27145
Satellite: ISS
Catalog Number: 25544
Epoch time: 20137
80301483 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 143
8125 deg
Eccentricity:
0001424
Arg of perigee: 315
1770 deg
Mean anomaly: 44
9265 deg
Mean motion: 15
49391731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 289
Coasting Arc #14 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2020/138/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4933347
53 A = 6794232
17 meter
Y = -449921
06 meter E =
0007233
Z = 4645204
64 I = 51
89076
XDOT = 3374
713980 Wp = 109
95932
YDOT = -6202
467611 meter/sec RA = 137
86182 deg
ZDOT = 2977
128925 TA = 310
42149
MA = 310
48457
Ha = 228
376 n
mi
Hp = 222
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16185523
40 X = -4950513
64
Y = -1476118
96 feet Y = -505185
51 meter
Z = 15240172
71 Z = 4621198
47
XDOT = 11071
896260 XDOT = 3429
359698
YDOT = -20349
303187 feet/sec YDOT = -6164
423781 meter/sec
ZDOT = 9767
483349 ZDOT = 2993
654466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14318444
24 X = 4364261
80
Y = 7904685
26 feet Y = 2409348
07 meter
Z = 15129807
16 Z = 4611565
22
XDOT = -17686
280919 XDOT = -5390
778424
YDOT = 13156
611388 feet/sec YDOT = 4010
135151 meter/sec
ZDOT = 9843
671035 ZDOT = 3000
350932
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20138
83500914
00016717 00000-0 10270-3 0 9135
2 25544 51
6422 138
7046 0001360 320
5655 39
5396 15
49366763 27304
Satellite: ISS
Catalog Number: 25544
Epoch time: 20138
83500914 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 138
7046 deg
Eccentricity:
0001360
Arg of perigee: 320
5655 deg
Mean anomaly: 39
5396 deg
Mean motion: 15
49366763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 303
Coasting Arc #15 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2020/139/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4893622
11 A = 6793896
24 meter
Y = 169938
15 meter E =
0010136
Z = -4719556
63 I = 51
91400
XDOT = -2964
640973 Wp = 62
72014
YDOT = 6456
580011 meter/sec RA = 132
93082 deg
ZDOT = -2841
668848 TA = 179
12784
MA = 179
12607
Ha = 228
151 n
mi
Hp = 222
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16055190
64 X = 4914283
26
Y = 557539
85 feet Y = 224777
93 meter
Z = -15484109
67 Z = -4695734
87
XDOT = -9726
512378 XDOT = -3022
816672
YDOT = 21183
005285 feet/sec YDOT = 6423
102183 meter/sec
ZDOT = -9323
060524 ZDOT = -2856
210967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14688721
79 X = -4477122
40
Y = -6760295
45 feet Y = -2060538
05 meter
Z = -15374573
40 Z = -4686169
97
XDOT = 16607
059129 XDOT = 5061
831622
YDOT = -14729
459305 feet/sec YDOT = -4489
539196 meter/sec
ZDOT = -9390
154867 ZDOT = -2862
119203
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20139
80250187
00016717 00000-0 10270-3 0 9148
2 25544 51
6422 133
9168 0001537 319
3784 40
7252 15
49391747 27452
Satellite: ISS
Catalog Number: 25544
Epoch time: 20139
80250187 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 133
9168 deg
Eccentricity:
0001537
Arg of perigee: 319
3784 deg
Mean anomaly: 40
7252 deg
Mean motion: 15
49391747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 314
Coasting Arc #16 (Orbit 2760)
---------------------------------------
Vector Time (GMT): 2020/140/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4829876
12 A = 6793720
85 meter
Y = 111800
66 meter E =
0006453
Z = 4772299
37 I = 51
93583
XDOT = 2535
230181 Wp = 111
55523
YDOT = -6701
476293 meter/sec RA = 128
00035 deg
ZDOT = 2717
556502 TA = 311
64600
MA = 311
70124
Ha = 228
394 n
mi
Hp = 222
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15846050
26 X = -4853948
77
Y = 366800
05 feet Y = 57654
58 meter
Z = 15657150
16 Z = 4748778
92
XDOT = 8317
684321 XDOT = 2596
779131
YDOT = -21986
470779 feet/sec YDOT = -6672
781608 meter/sec
ZDOT = 8915
867789 ZDOT = 2730
020820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14952289
87 X = 4557457
95
Y = 5571036
57 feet Y = 1698051
95 meter
Z = 15548980
08 Z = 4739329
13
XDOT = -15411
377977 XDOT = -4697
388007
YDOT = 16269
433412 feet/sec YDOT = 4958
923304 meter/sec
ZDOT = 8973
436188 ZDOT = 2735
103350
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20140
83449381
00016717 00000-0 10270-3 0 9150
2 25544 51
6428 128
8086 0001500 324
7319 35
3731 15
49368907 27616
Satellite: ISS
Catalog Number: 25544
Epoch time: 20140
83449381 = yrday
fracday
Element set: 915
Inclination: 51
6428 deg
RA of node: 128
8086 deg
Eccentricity:
0001500
Arg of perigee: 324
7319 deg
Mean anomaly: 35
3731 deg
Mean motion: 15
49368907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2761
Checksum: 310
Coasting Arc #17 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2020/141/18:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4762135
34 A = 6793391
60 meter
Y = -370359
96 meter E =
0011057
Z = -4841194
58 I = 51
95464
XDOT = -2083
970042 Wp = 63
50541
YDOT = 6896
366990 meter/sec RA = 123
07133 deg
ZDOT = -2577
278893 TA = 181
17078
MA = 181
17337
Ha = 228
201 n
mi
Hp = 222
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15623803
59 X = 4789439
01
Y = -1215091
74 feet Y = -316953
26 meter
Z = -15883184
33 Z = -4817995
33
XDOT = -6837
172053 XDOT = -2148
413227
YDOT = 22625
875952 feet/sec YDOT = 6872
702468 meter/sec
ZDOT = -8455
639413 ZDOT = -2587
558053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15140364
12 X = -4614782
98
Y = -4441570
83 feet Y = -1353790
79 meter
Z = -15776471
53 Z = -4808668
52
XDOT = 14038
191194 XDOT = 4278
840676
YDOT = -17646
989868 feet/sec YDOT = -5378
802512 meter/sec
ZDOT = -8503
187902 ZDOT = -2591
771672
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20141
80198229
00016717 00000-0 10270-3 0 9161
2 25544 51
6426 124
0199 0001681 327
5793 32
5253 15
49397570 27766
Satellite: ISS
Catalog Number: 25544
Epoch time: 20141
80198229 = yrday
fracday
Element set: 916
Inclination: 51
6426 deg
RA of node: 124
0199 deg
Eccentricity:
0001681
Arg of perigee: 327
5793 deg
Mean anomaly: 32
5253 deg
Mean motion: 15
49397570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2776
Checksum: 321
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