[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 12th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15581 7398 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
073/19:14:09
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
074/01:07:11
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
5
074/14:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
6
082/14:09:43
786 0
6 2
1 2
1
N/A 2
0 0
0 224
1
000/00:05:27
573 0
3 -0
0 217
1
082/22:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
1
000/00:00:00
000 0
0 0
0 217
0
Coasting Arc #1 (Orbit 6)
---------------------------------------
Vector Time (GMT): 2019/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2044728
34 A = 6790763
14 meter
Y = 6021032
95 meter E =
0008434
Z = -2384376
02 I = 51
95846
XDOT = -5423
466064 Wp = 66
91663
YDOT = 290
590386 meter/sec RA = 125
81904 deg
ZDOT = 5403
079903 TA = 266
60826
MA = 266
70474
Ha = 224
437 n
mi
Hp = 215
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6708426
31 X = -2100323
31
Y = 19754045
11 feet Y = 5997856
28 meter
Z = -7822755
95 Z = -2394444
14
XDOT = -17793
523831 XDOT = -5452
557556
YDOT = 953
380531 feet/sec YDOT = 229
779266 meter/sec
ZDOT = 17726
640101 ZDOT = 5376
664109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10624845
33 X = -3238452
86
Y = 17933645
29 feet Y = 5466175
08 meter
Z = -7868787
76 Z = -2398406
51
XDOT = -16409
901431 XDOT = -5001
737956
YDOT = -2022
875918 feet/sec YDOT = -616
572580 meter/sec
ZDOT = 17607
113534 ZDOT = 5366
648205
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 19070
50479253
00016717 00000-0 10270-3 0 9009
2 25544 51
6382 126
8816 0003713 97
5397 262
6177 15
52796877 78
Satellite: ISS
Catalog Number: 25544
Epoch time: 19070
50479253 = yrday
fracday
Element set: 900
Inclination: 51
6382 deg
RA of node: 126
8816 deg
Eccentricity:
0003713
Arg of perigee: 97
5397 deg
Mean anomaly: 262
6177 deg
Mean motion: 15
52796877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 7
Checksum: 331
Coasting Arc #2 (Orbit 22)
---------------------------------------
Vector Time (GMT): 2019/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2624901
09 A = 6792538
80 meter
Y = -6149291
89 meter E =
0017175
Z = 1154645
23 I = 51
98410
XDOT = 4812
055481 Wp = 117
29309
YDOT = 935
564436 meter/sec RA = 120
87444 deg
ZDOT = -5897
478657 TA = 50
23262
MA = 50
08147
Ha = 224
418 n
mi
Hp = 215
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8611880
20 X = 2687860
50
Y = -20174842
16 feet Y = -6119586
29 meter
Z = 3788206
13 Z = 1167549
40
XDOT = 15787
583599 XDOT = 4829
882728
YDOT = 3069
437125 feet/sec YDOT = 989
475410 meter/sec
ZDOT = -19348
683259 ZDOT = -5874
060310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12290104
02 X = 3746023
71
Y = -18157434
54 feet Y = -5534386
05 meter
Z = 3847097
17 Z = 1172595
22
XDOT = 13710
769562 XDOT = 4179
042562
YDOT = 5162
582801 feet/sec YDOT = 1573
555238 meter/sec
ZDOT = -19242
809059 ZDOT = -5865
208201
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 19071
53450714
00016717 00000-0 10270-3 0 9015
2 25544 51
6391 121
7578 0003748 98
1225 262
0352 15
52826415 231
Satellite: ISS
Catalog Number: 25544
Epoch time: 19071
53450714 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 121
7578 deg
Eccentricity:
0003748
Arg of perigee: 98
1225 deg
Mean anomaly: 262
0352 deg
Mean motion: 15
52826415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 23
Checksum: 290
Coasting Arc #3 (Orbit 38)
---------------------------------------
Vector Time (GMT): 2019/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3033578
74 A = 6793292
65 meter
Y = 6071495
70 meter E =
0014867
Z = 93187
52 I = 52
00209
XDOT = -4180
952438 Wp = 58
18120
YDOT = -2192
388905 meter/sec RA = 115
93409 deg
ZDOT = 6040
157137 TA = 302
81703
MA = 302
96011
Ha = 224
528 n
mi
Hp = 215
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9952686
17 X = -3101699
12
Y = 19919605
31 feet Y = 6037191
22 meter
Z = 305733
35 Z = 78285
75
XDOT = -13717
035559 XDOT = -4185
465436
YDOT = -7192
876985 feet/sec YDOT = -2239
168093 meter/sec
ZDOT = 19816
788506 ZDOT = 6019
836873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13278618
53 X = -4047322
93
Y = 17876293
13 feet Y = 5448694
15 meter
Z = 237790
82 Z = 72478
64
XDOT = -11077
907036 XDOT = -3376
546065
YDOT = -8530
236077 feet/sec YDOT = -2600
015956 meter/sec
ZDOT = 19725
032041 ZDOT = 6012
189766
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 19072
56422196
00016717 00000-0 10270-3 0 9023
2 25544 51
6391 116
6351 0003806 98
9616 261
1967 15
52765628 397
Satellite: ISS
Catalog Number: 25544
Epoch time: 19072
56422196 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 116
6351 deg
Eccentricity:
0003806
Arg of perigee: 98
9616 deg
Mean anomaly: 261
1967 deg
Mean motion: 15
52765628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 39
Checksum: 324
Coasting Arc #4 (Orbit 53)
---------------------------------------
Vector Time (GMT): 2019/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3360859
89 A = 6792353
18 meter
Y = -5732869
43 meter E =
0011986
Z = -1387835
45 I = 52
01353
XDOT = 3545
268681 Wp = 131
16375
YDOT = 3481
389724 meter/sec RA = 110
99465 deg
ZDOT = -5835
825072 TA = 63
86948
MA = 63
74622
Ha = 224
482 n
mi
Hp = 215
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11026443
22 X = 3431457
97
Y = -18808626
75 feet Y = -5694891
28 meter
Z = -4553265
91 Z = -1371337
99
XDOT = 11631
458926 XDOT = 3534
422341
YDOT = 11421
882298 feet/sec YDOT = 3520
974463 meter/sec
ZDOT = -19146
407717 ZDOT = -5818
630100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13882517
37 X = 4231391
29
Y = -16831557
90 feet Y = -5130258
85 meter
Z = -4478112
41 Z = -1364928
66
XDOT = 8585
316666 XDOT = 2616
804520
YDOT = 12118
670927 feet/sec YDOT = 3693
770899 meter/sec
ZDOT = -19068
902658 ZDOT = -5812
201530
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 19073
52957514
00016717 00000-0 10270-3 0 9038
2 25544 51
6396 111
8323 0003864 104
8647 255
2933 15
52816510 544
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
52957514 = yrday
fracday
Element set: 903
Inclination: 51
6396 deg
RA of node: 111
8323 deg
Eccentricity:
0003864
Arg of perigee: 104
8647 deg
Mean anomaly: 255
2933 deg
Mean motion: 15
52816510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 54
Checksum: 306
Coasting Arc #5 (Orbit 58)
---------------------------------------
Vector Time (GMT): 2019/073/19:14:09
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4230822
96 A = 6781378
39 meter
Y = -415438
09 meter E =
0006914
Z = 5278291
53 I = 51
97981
XDOT = 1862
357330 Wp = 112
73031
YDOT = -7386
170168 meter/sec RA = 109
49861 deg
ZDOT = 907
887501 TA = 328
60889
MA = 328
65014
Ha = 224
455 n
mi
Hp = 215
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13880652
77 X = -4251501
81
Y = -1362985
85 feet Y = -462865
48 meter
Z = 17317229
44 Z = 5257689
72
XDOT = 6110
096226 XDOT = 1940
403179
YDOT = -24232
841759 feet/sec YDOT = -7364
907563 meter/sec
ZDOT = 2978
633532 ZDOT = 917
123975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1032482
23 X = 314700
58
Y = 14024378
08 feet Y = 4274630
44 meter
Z = 17224038
06 Z = 5249886
80
XDOT = -23891
886492 XDOT = -7282
247003
YDOT = -1965
768696 feet/sec YDOT = -599
166299 meter/sec
ZDOT = 3021
080669 ZDOT = 920
825388
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 19073
85135934
00016717 00000-0 10270-3 0 9049
2 25544 51
6387 110
2329 0003534 104
4456 255
7088 15
52840519 598
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
85135934 = yrday
fracday
Element set: 904
Inclination: 51
6387 deg
RA of node: 110
2329 deg
Eccentricity:
0003534
Arg of perigee: 104
4456 deg
Mean anomaly: 255
7088 deg
Mean motion: 15
52840519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 59
Checksum: 311
Coasting Arc #6 (Orbit 62)
---------------------------------------
Vector Time (GMT): 2019/074/01:07:11
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2944181
49 A = 6792616
39 meter
Y = 6001574
22 meter E =
0016200
Z = 1168606
84 I = 52
01826
XDOT = -3842
194596 Wp = 67
13559
YDOT = -3044
317991 meter/sec RA = 108
28629 deg
ZDOT = 5895
914052 TA = 305
48385
MA = 305
63491
Ha = 224
349 n
mi
Hp = 215
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9659388
09 X = -3016750
37
Y = 19690204
14 feet Y = 5968244
62 meter
Z = 3834011
94 Z = 1154128
70
XDOT = -12605
625315 XDOT = -3836
505469
YDOT = -9987
919919 feet/sec YDOT = -3087
252021 meter/sec
ZDOT = 19343
550039 ZDOT = 5877
264210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6752649
17 X = 2058207
47
Y = -20878499
80 feet Y = -6363766
74 meter
Z = 3767962
35 Z = 1148474
92
XDOT = 12516
051335 XDOT = 3814
892447
YDOT = 7559
136803 feet/sec YDOT = 2304
024898 meter/sec
ZDOT = 19259
422615 ZDOT = 5870
272013
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 19074
10878636
00016717 00000-0 10270-3 0 9052
2 25544 51
6373 108
9504 0003520 106
6925 253
4613 15
52807918 632
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
10878636 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 108
9504 deg
Eccentricity:
0003520
Arg of perigee: 106
6925 deg
Mean anomaly: 253
4613 deg
Mean motion: 15
52807918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 63
Checksum: 308
Coasting Arc #7 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2019/074/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3871180
92 A = 6781351
87 meter
Y = 1646020
96 meter E =
0018464
Z = -5334902
13 I = 51
98595
XDOT = -2406
142780 Wp = 96
61182
YDOT = 7247
971488 meter/sec RA = 105
49187 deg
ZDOT = 489
686064 TA = 178
05044
MA = 178
04323
Ha = 224
468 n
mi
Hp = 215
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12700724
79 X = 3878400
67
Y = 5400331
22 feet Y = 1689351
34 meter
Z = -17502959
74 Z = -5316080
11
XDOT = -7894
169226 XDOT = -2489
391421
YDOT = 23779
434016 feet/sec YDOT = 7220
598867 meter/sec
ZDOT = 1606
581575 ZDOT = 477
795531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13766702
93 X = 4196091
05
Y = -1979721
01 feet Y = -603418
96 meter
Z = -17417927
04 Z = -5308984
16
XDOT = 5338
267460 XDOT = 1627
103922
YDOT = 23447
949898 feet/sec YDOT = 7146
935129 meter/sec
ZDOT = 1552
120802 ZDOT = 473
086420
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 19074
62364219
00016717 00000-0 10270-3 0 9067
2 25544 51
6372 106
3898 0003807 107
4569 252
7000 15
52784653 711
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
62364219 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 106
3898 deg
Eccentricity:
0003807
Arg of perigee: 107
4569 deg
Mean anomaly: 252
7000 deg
Mean motion: 15
52784653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 71
Checksum: 312
Coasting Arc #8 (Orbit 86)
---------------------------------------
Vector Time (GMT): 2019/075/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3498679
31 A = 6782372
48 meter
Y = -2834846
89 meter E =
0008372
Z = 5065359
34 I = 51
99744
XDOT = 2799
643938 Wp = 76
87545
YDOT = -6881
580479 meter/sec RA = 100
53075 deg
ZDOT = -1913
068353 TA = 31
59894
MA = 31
54870
Ha = 224
515 n
mi
Hp = 215
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11478606
65 X = -3491323
58
Y = -9300678
76 feet Y = -2873930
18 meter
Z = 16618632
99 Z = 5048382
31
XDOT = 9185
183522 XDOT = 2885
680141
YDOT = -22577
363776 feet/sec YDOT = -6849
791940 meter/sec
ZDOT = -6276
470975 ZDOT = -1899
259617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14756886
96 X = -4497899
15
Y = -1742040
80 feet Y = -530974
04 meter
Z = 16542054
88 Z = 5042018
33
XDOT = -4271
232926 XDOT = -1301
871796
YDOT = -22959
696134 feet/sec YDOT = -6998
115382 meter/sec
ZDOT = -6213
345212 ZDOT = -1893
827620
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 19075
65334940
00016717 00000-0 10270-3 0 9070
2 25544 51
6371 101
2666 0003704 109
9749 250
1802 15
52811057 878
Satellite: ISS
Catalog Number: 25544
Epoch time: 19075
65334940 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 101
2666 deg
Eccentricity:
0003704
Arg of perigee: 109
9749 deg
Mean anomaly: 250
1802 deg
Mean motion: 15
52811057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 87
Checksum: 302
Coasting Arc #9 (Orbit 101)
---------------------------------------
Vector Time (GMT): 2019/076/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3171404
26 A = 6784640
11 meter
Y = 3944084
22 meter E =
0013305
Z = -4531879
66 I = 52
00931
XDOT = -3127
383906 Wp = 110
88995
YDOT = 6203
934566 meter/sec RA = 95
57406 deg
ZDOT = 3213
721125 TA = 191
28312
MA = 191
31298
Ha = 224
416 n
mi
Hp = 215
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10404869
62 X = 3149077
68
Y = 12939908
84 feet Y = 3979423
94 meter
Z = -14868371
59 Z = -4516528
92
XDOT = -10260
445887 XDOT = -3212
135839
YDOT = 20354
116029 feet/sec YDOT = 6168
488308 meter/sec
ZDOT = 10543
704477 ZDOT = 3198
323468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15856290
84 X = 4832997
45
Y = 5131382
34 feet Y = 1564045
34 meter
Z = -14799256
15 Z = -4510813
27
XDOT = 2794
850118 XDOT = 851
870316
YDOT = 21541
406526 feet/sec YDOT = 6565
820709 meter/sec
ZDOT = 10473
435933 ZDOT = 3192
303272
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 19076
61869924
00016717 00000-0 10270-3 0 9083
2 25544 51
6367 96
4642 0003716 111
9583 248
1964 15
52787249 1023
Satellite: ISS
Catalog Number: 25544
Epoch time: 19076
61869924 = yrday
fracday
Element set: 908
Inclination: 51
6367 deg
RA of node: 96
4642 deg
Eccentricity:
0003716
Arg of perigee: 111
9583 deg
Mean anomaly: 248
1964 deg
Mean motion: 15
52787249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 102
Checksum: 340
Coasting Arc #10 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2019/077/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2839417
10 A = 6787372
78 meter
Y = -4917195
49 meter E =
0014972
Z = 3705138
90 I = 52
02061
XDOT = 3456
363175 Wp = 92
10653
YDOT = -5287
208296 meter/sec RA = 90
62196 deg
ZDOT = -4353
450628 TA = 44
00209
MA = 43
88300
Ha = 224
375 n
mi
Hp = 215
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9315672
90 X = -2802217
79
Y = -16132531
13 feet Y = -4948739
50 meter
Z = 12155967
52 Z = 3691437
12
XDOT = 11339
774195 XDOT = 3536
375624
YDOT = -17346
483911 feet/sec YDOT = -5248
109845 meter/sec
ZDOT = -14282
974500 ZDOT = -4336
466399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16808594
26 X = -5123259
53
Y = -8124302
52 feet Y = -2476287
41 meter
Z = 12094409
31 Z = 3686375
96
XDOT = -806
496631 XDOT = -245
820173
YDOT = -19550
472974 feet/sec YDOT = -5958
984163 meter/sec
ZDOT = -14205
600018 ZDOT = -4329
866885
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 19077
64840420
00016717 00000-0 10270-3 0 9098
2 25544 51
6364 91
3407 0003601 116
0774 244
0749 15
52821166 1184
Satellite: ISS
Catalog Number: 25544
Epoch time: 19077
64840420 = yrday
fracday
Element set: 909
Inclination: 51
6364 deg
RA of node: 91
3407 deg
Eccentricity:
0003601
Arg of perigee: 116
0774 deg
Mean anomaly: 244
0749 deg
Mean motion: 15
52821166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 118
Checksum: 296
Coasting Arc #11 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2019/078/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2543258
32 A = 6790121
59 meter
Y = 5689858
55 meter E =
0007356
Z = -2699727
40 I = 52
02969
XDOT = -3768
904431 Wp = 81
77408
YDOT = 4153
600157 meter/sec RA = 85
67582 deg
ZDOT = 5216
667515 TA = 247
94674
MA = 248
02488
Ha = 224
342 n
mi
Hp = 215
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8344023
35 X = 2492557
25
Y = 18667514
91 feet Y = 5718015
24 meter
Z = -8857373
35 Z = -2687497
21
XDOT = -12365
172019 XDOT = -3840
410324
YDOT = 13627
297103 feet/sec YDOT = 4111
054428 meter/sec
ZDOT = 17115
050901 ZDOT = 5198
185729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17584520
05 X = 5359761
71
Y = 10481010
44 feet Y = 3194611
98 meter
Z = -8802555
08 Z = -2683018
79
XDOT = -1651
541968 XDOT = -503
389992
YDOT = 17038
048255 feet/sec YDOT = 5193
197108 meter/sec
ZDOT = 17030
997847 ZDOT = 5191
048144
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 19078
61375039
00016717 00000-0 10270-3 0 9107
2 25544 51
6371 86
5377 0003681 118
4671 241
6852 15
52807553 1333
Satellite: ISS
Catalog Number: 25544
Epoch time: 19078
61375039 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 86
5377 deg
Eccentricity:
0003681
Arg of perigee: 118
4671 deg
Mean anomaly: 241
6852 deg
Mean motion: 15
52807553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 314
Coasting Arc #12 (Orbit 148)
---------------------------------------
Vector Time (GMT): 2019/079/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2200444
43 A = 6792208
40 meter
Y = -6240342
31 meter E =
0017430
Z = 1495386
50 I = 52
03334
XDOT = 4122
959575 Wp = 118
91254
YDOT = -2854
787648 meter/sec RA = 80
73400 deg
ZDOT = -5803
599675 TA = 44
85061
MA = 44
70987
Ha = 224
278 n
mi
Hp = 215
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7219305
86 X = -2137763
28
Y = -20473564
02 feet Y = -6264598
55 meter
Z = 4906123
67 Z = 1484850
78
XDOT = 13526
770258 XDOT = 4182
766530
YDOT = -9366
101206 feet/sec YDOT = -2808
348220 meter/sec
ZDOT = -19040
681347 ZDOT = -5783
426474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17890909
08 X = -5453149
09
Y = -12315046
71 feet Y = -3753626
24 meter
Z = 4859037
64 Z = 1481034
67
XDOT = 4654
838621 XDOT = 1418
794812
YDOT = -14294
813091 feet/sec YDOT = -4357
059030 meter/sec
ZDOT = -18949
092336 ZDOT = -5775
683344
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 19079
64345076
00016717 00000-0 10270-3 0 9110
2 25544 51
6373 81
4136 0003567 121
2610 238
8892 15
52821119 1493
Satellite: ISS
Catalog Number: 25544
Epoch time: 19079
64345076 = yrday
fracday
Element set: 911
Inclination: 51
6373 deg
RA of node: 81
4136 deg
Eccentricity:
0003567
Arg of perigee: 121
2610 deg
Mean anomaly: 238
8892 deg
Mean motion: 15
52821119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 149
Checksum: 307
Coasting Arc #13 (Orbit 163)
---------------------------------------
Vector Time (GMT): 2019/080/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1852931
06 A = 6793077
09 meter
Y = 6526611
82 meter E =
0012591
Z = -249590
43 I = 52
02954
XDOT = -4481
151493 Wp = 59
92220
YDOT = 1494
135884 meter/sec RA = 75
79582 deg
ZDOT = 6035
935334 TA = 297
40488
MA = 297
53291
Ha = 224
218 n
mi
Hp = 215
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6079170
15 X = 1781023
29
Y = 21412768
45 feet Y = 6546930
50 meter
Z = -818866
23 Z = -240765
23
XDOT = -14701
940594 XDOT = -4526
845340
YDOT = 4902
020618 feet/sec YDOT = 1443
769886 meter/sec
ZDOT = 19802
937449 ZDOT = 6014
056525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17731565
67 X = 5404581
22
Y = 13457985
12 feet Y = 4101993
87 meter
Z = -779563
77 Z = -237611
04
XDOT = -7928
425340 XDOT = -2416
584044
YDOT = 11540
955597 feet/sec YDOT = 3517
683266 meter/sec
ZDOT = 19703
759422 ZDOT = 6005
705872
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 19080
60879384
00016717 00000-0 10270-3 0 9123
2 25544 51
6370 76
6110 0003600 126
2933 233
8552 15
52830598 1645
Satellite: ISS
Catalog Number: 25544
Epoch time: 19080
60879384 = yrday
fracday
Element set: 912
Inclination: 51
6370 deg
RA of node: 76
6110 deg
Eccentricity:
0003600
Arg of perigee: 126
2933 deg
Mean anomaly: 233
8552 deg
Mean motion: 15
52830598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 164
Checksum: 302
Coasting Arc #14 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2019/081/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1400575
16 A = 6792629
26 meter
Y = -6556282
01 meter E =
0012945
Z = -1059084
39 I = 52
02056
XDOT = 4864
653186 Wp = 138
26440
YDOT = -90
392006 meter/sec RA = 70
85716 deg
ZDOT = -5924
494261 TA = 53
15327
MA = 53
03463
Ha = 224
139 n
mi
Hp = 215
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4595062
85 X = -1322012
42
Y = -21510111
57 feet Y = -6571505
09 meter
Z = -3474686
32 Z = -1065696
15
XDOT = 15960
148249 XDOT = 4894
080299
YDOT = -296
561701 feet/sec YDOT = -35
828313 meter/sec
ZDOT = -19437
317130 ZDOT = -5900
792146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16827107
72 X = -5128902
43
Y = -14157814
78 feet Y = -4315301
94 meter
Z = -3503951
18 Z = -1068004
32
XDOT = 11476
517965 XDOT = 3498
042676
YDOT = -8897
199377 feet/sec YDOT = -2711
866370 meter/sec
ZDOT = -19330
027888 ZDOT = -5891
792500
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 19081
63849120
00016717 00000-0 10270-3 0 9133
2 25544 51
6387 71
4872 0003452 129
6862 230
4595 15
52827333 1805
Satellite: ISS
Catalog Number: 25544
Epoch time: 19081
63849120 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 71
4872 deg
Eccentricity:
0003452
Arg of perigee: 129
6862 deg
Mean anomaly: 230
4595 deg
Mean motion: 15
52827333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 180
Checksum: 312
Coasting Arc #15 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2019/082/14:12:27
573
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4611249
40 A = 6784282
49 meter
Y = 930103
08 meter E =
0013301
Z = -4901050
02 I = 51
97690
XDOT = 1126
854900 Wp = 114
00809
YDOT = 7173
820069 meter/sec RA = 65
95847 deg
ZDOT = 2421
562854 TA = 179
66870
MA = 179
66782
Ha = 224
114 n
mi
Hp = 217
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15128771
00 X = 4624312
64
Y = 3051519
30 feet Y = 981741
77 meter
Z = -16079560
44 Z = -4878618
64
XDOT = 3697
030511 XDOT = 1034
788825
YDOT = 23536
155082 feet/sec YDOT = 7185
906856 meter/sec
ZDOT = 7944
760020 ZDOT = 2426
812261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14438507
94 X = 4400857
22
Y = -5742173
44 feet Y = -1750214
46 meter
Z = -15978131
26 Z = -4870134
41
XDOT = 15459
081482 XDOT = 4711
928036
YDOT = 16699
524293 feet/sec YDOT = 5090
015005 meter/sec
ZDOT = 7967
777535 ZDOT = 2428
578593
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 19082
60383005
00016717 00000-0 10270-3 0 9147
2 25544 51
6387 66
6844 0002111 155
3735 204
7517 15
52423009 1952
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
60383005 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 66
6844 deg
Eccentricity:
0002111
Arg of perigee: 155
3735 deg
Mean anomaly: 204
7517 deg
Mean motion: 15
52423009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 293
Coasting Arc #16 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2019/082/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1642051
25 A = 6785612
60 meter
Y = 4767246
83 meter E =
0010418
Z = 4536280
45 I = 51
97520
XDOT = -5070
666941 Wp = 121
04221
YDOT = -4788
786360 meter/sec RA = 64
29489 deg
ZDOT = 3186
488622 TA = 297
06600
MA = 297
17227
Ha = 224
126 n
mi
Hp = 217
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5387307
26 X = -1717272
71
Y = 15640573
58 feet Y = 4748464
16 meter
Z = 14882809
87 Z = 4528120
74
XDOT = -16636
046395 XDOT = -5032
218749
YDOT = -15711
241338 feet/sec YDOT = -4845
274784 meter/sec
ZDOT = 10454
358996 ZDOT = 3161
951057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11112218
63 X = 3387004
24
Y = -12299669
90 feet Y = -3748939
39 meter
Z = 14845382
06 Z = 4524872
45
XDOT = 8427
630826 XDOT = 2568
741876
YDOT = 20140
902618 feet/sec YDOT = 6138
947118 meter/sec
ZDOT = 10343
801286 ZDOT = 3152
790632
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 19082
99006276
00016717 00000-0 10270-3 0 9152
2 25544 51
6371 64
7617 0002161 160
1040 200
0197 15
52425435 2016
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
99006276 = yrday
fracday
Element set: 915
Inclination: 51
6371 deg
RA of node: 64
7617 deg
Eccentricity:
0002161
Arg of perigee: 160
1040 deg
Mean anomaly: 200
0197 deg
Mean motion: 15
52425435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 272
Coasting Arc #17 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2019/083/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2252419
19 A = 6783553
42 meter
Y = -3947306
82 meter E =
0013306
Z = -5047816
10 I = 51
95269
XDOT = 5027
725952 Wp = 85
46816
YDOT = 5417
195903 meter/sec RA = 59
33863 deg
ZDOT = -1996
203424 TA = 165
21520
MA = 165
17625
Ha = 224
122 n
mi
Hp = 217
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7389826
73 X = 2320911
25
Y = -12950481
69 feet Y = -3921736
15 meter
Z = -16561076
43 Z = -5036707
97
XDOT = 16495
163884 XDOT = 4976
472140
YDOT = 17772
952439 feet/sec YDOT = 5473
132706 meter/sec
ZDOT = -6549
223832 ZDOT = -1971
905482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11770824
23 X = -3587747
23
Y = 9243852
26 feet Y = 2817526
17 meter
Z = -16510380
37 Z = -5032363
94
XDOT = -8089
272615 XDOT = -2465
610293
YDOT = -21782
173396 feet/sec YDOT = -6639
206451 meter/sec
ZDOT = -6439
832903 ZDOT = -1962
861069
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 19083
95564599
00016717 00000-0 10270-3 0 9167
2 25544 51
6368 59
9604 0002390 159
8835 200
2412 15
52439534 2168
Satellite: ISS
Catalog Number: 25544
Epoch time: 19083
95564599 = yrday
fracday
Element set: 916
Inclination: 51
6368 deg
RA of node: 59
9604 deg
Eccentricity:
0002390
Arg of perigee: 159
8835 deg
Mean anomaly: 200
2412 deg
Mean motion: 15
52439534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 329
Coasting Arc #18 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2019/084/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2894954
89 A = 6782548
32 meter
Y = 3085110
16 meter E =
0004935
Z = 5298811
32 I = 51
93136
XDOT = -4897
841340 Wp = 136
73808
YDOT = -5855
111793 meter/sec RA = 54
37808 deg
ZDOT = 729
212934 TA = 306
30146
MA = 306
34702
Ha = 224
209 n
mi
Hp = 217
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9497883
49 X = -2954977
04
Y = 10121752
50 feet Y = 3052401
49 meter
Z = 17384551
57 Z = 5284602
71
XDOT = -16069
033268 XDOT = -4835
545921
YDOT = -19209
684361 feet/sec YDOT = -5909
534518 meter/sec
ZDOT = 2392
430887 ZDOT = 705
572699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12581660
36 X = 3834890
08
Y = -6050196
59 feet Y = -1844099
92 meter
Z = 17319908
82 Z = 5279108
21
XDOT = 7775
756337 XDOT = 2370
050531
YDOT = 22751
185339 feet/sec YDOT = 6934
561291 meter/sec
ZDOT = 2286
079697 ZDOT = 696
797092
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 19084
98560049
00016717 00000-0 10270-3 0 9178
2 25544 51
6372 54
8386 0002325 164
3069 195
8155 15
52399157 2329
Satellite: ISS
Catalog Number: 25544
Epoch time: 19084
98560049 = yrday
fracday
Element set: 917
Inclination: 51
6372 deg
RA of node: 54
8386 deg
Eccentricity:
0002325
Arg of perigee: 164
3069 deg
Mean anomaly: 195
8155 deg
Mean motion: 15
52399157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 331
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