[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 10th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19212 3638 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 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
175/23:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 216
2
Coasting Arc #1 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2019/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5881736
57 A = 6797838
06 meter
Y = -3344129
78 meter E =
0014398
Z = 635913
09 I = 51
87995
XDOT = 1849
191772 Wp = 95
31946
YDOT = -4411
888748 meter/sec RA = 33
85022 deg
ZDOT = -5982
298447 TA = 77
84943
MA = 77
68817
Ha = 228
030 n
mi
Hp = 217
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19297036
00 X = -5846993
32
Y = -10971554
38 feet Y = -3409709
28 meter
Z = 2086329
02 Z = 607425
93
XDOT = 6066
902139 XDOT = 1927
447945
YDOT = -14474
700618 feet/sec YDOT = -4390
771637 meter/sec
ZDOT = -19626
963408 ZDOT = -5973
126158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14842797
66 X = -4524084
73
Y = 16521592
46 feet Y = 5035781
38 meter
Z = 1957476
14 Z = 596638
73
XDOT = -11613
255313 XDOT = -3539
720219
YDOT = -8065
080960 feet/sec YDOT = -2458
236677 meter/sec
ZDOT = -19584
803391 ZDOT = -5969
448074
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 19161
53341990
00016717 00000-0 10270-3 0 9009
2 25544 51
6436 34
3293 0007869 31
6250 328
5372 15
51153380 14218
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
53341990 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 34
3293 deg
Eccentricity:
0007869
Arg of perigee: 31
6250 deg
Mean anomaly: 328
5372 deg
Mean motion: 15
51153380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 291
Coasting Arc #2 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2019/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5912130
40 A = 6797825
00 meter
Y = 3333098
23 meter E =
0020098
Z = 76199
43 I = 51
85260
XDOT = -2394
228607 Wp = 41
07920
YDOT = 4088
677100 meter/sec RA = 28
90786 deg
ZDOT = 6030
523715 TA = 319
73876
MA = 319
88742
Ha = 228
015 n
mi
Hp = 217
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19396753
28 X = 5874049
21
Y = 10935361
64 feet Y = 3398998
88 meter
Z = 249998
12 Z = 104826
22
XDOT = -7855
080730 XDOT = -2469
064399
YDOT = 13414
294947 feet/sec YDOT = 4061
484150 meter/sec
ZDOT = 19785
182791 ZDOT = 6018
712056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14537612
31 X = 4431064
23
Y = -16863940
79 feet Y = -5140129
15 meter
Z = 379473
92 Z = 115663
65
XDOT = 10352
039686 XDOT = 3155
301696
YDOT = 9411
086778 feet/sec YDOT = 2868
499250 meter/sec
ZDOT = 19731
085773 ZDOT = 6014
034944
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 19162
56420355
00016717 00000-0 10270-3 0 9017
2 25544 51
6440 29
2133 0007918 33
7094 326
4559 15
51210774 14375
Satellite: ISS
Catalog Number: 25544
Epoch time: 19162
56420355 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 29
2133 deg
Eccentricity:
0007918
Arg of perigee: 33
7094 deg
Mean anomaly: 326
4559 deg
Mean motion: 15
51210774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 296
Coasting Arc #3 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2019/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5865042
20 A = 6797612
20 meter
Y = -3331965
92 meter E =
0011226
Z = -842684
23 I = 51
82170
XDOT = 2994
347069 Wp = 97
18500
YDOT = -3784
718989 meter/sec RA = 23
96385 deg
ZDOT = -5945
076084 TA = 91
88817
MA = 91
75960
Ha = 228
102 n
mi
Hp = 217
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19242264
42 X = -5823253
99
Y = -10931646
71 feet Y = -3397319
19 meter
Z = -2764712
06 Z = -871073
42
XDOT = 9823
973323 XDOT = 3065
324368
YDOT = -12417
057049 feet/sec YDOT = -3750
836628 meter/sec
ZDOT = -19504
842794 ZDOT = -5930
358585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14211070
85 X = -4331534
39
Y = 16943574
85 feet Y = 5164401
61 meter
Z = -2893096
88 Z = -881815
93
XDOT = -9189
863906 XDOT = -2801
070518
YDOT = -10989
652635 feet/sec YDOT = -3349
646123 meter/sec
ZDOT = -19437
599124 ZDOT = -5924
580213
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 19163
53056358
00016717 00000-0 10270-3 0 9024
2 25544 51
6438 24
4172 0007893 37
2498 322
9199 15
51168104 14528
Satellite: ISS
Catalog Number: 25544
Epoch time: 19163
53056358 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 24
4172 deg
Eccentricity:
0007893
Arg of perigee: 37
2498 deg
Mean anomaly: 322
9199 deg
Mean motion: 15
51168104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 316
Coasting Arc #4 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2019/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5746709
10 A = 6796757
72 meter
Y = 3262568
63 meter E =
0021440
Z = 1539402
36 I = 51
78701
XDOT = -3582
974656 Wp = 54
30277
YDOT = 3568
579723 meter/sec RA = 19
01692 deg
ZDOT = 5768
295247 TA = 322
48046
MA = 322
62990
Ha = 228
077 n
mi
Hp = 217
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18854032
49 X = 5702321
40
Y = 10703965
31 feet Y = 3326583
98 meter
Z = 5050532
69 Z = 1567210
54
XDOT = -11755
166193 XDOT = -3650
632639
YDOT = 11707
938723 feet/sec YDOT = 3528
133395 meter/sec
ZDOT = 18924
853173 ZDOT = 5750
726455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13627283
75 X = 4153596
09
Y = -16824404
41 feet Y = -5128078
46 meter
Z = 5176277
52 Z = 1577729
39
XDOT = 8390
216016 XDOT = 2557
337842
YDOT = 12637
094144 feet/sec YDOT = 3851
786295 meter/sec
ZDOT = 18844
701024 ZDOT = 5743
864872
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 19164
56134345
00016717 00000-0 10270-3 0 9032
2 25544 51
6424 19
3013 0007928 40
8422 319
3322 15
51218419 14686
Satellite: ISS
Catalog Number: 25544
Epoch time: 19164
56134345 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 19
3013 deg
Eccentricity:
0007928
Arg of perigee: 40
8422 deg
Mean anomaly: 319
3322 deg
Mean motion: 15
51218419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 292
Coasting Arc #5 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2019/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5543721
51 A = 6795660
19 meter
Y = -3224568
82 meter E =
0009655
Z = -2258460
65 I = 51
75084
XDOT = 4179
171768 Wp = 80
61985
YDOT = -3381
218078 meter/sec RA = 14
06757 deg
ZDOT = -5449
144744 TA = 124
40145
MA = 124
31012
Ha = 228
161 n
mi
Hp = 217
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18188062
71 X = -5496281
00
Y = -10579294
03 feet Y = -3286297
02 meter
Z = -7409647
80 Z = -2285275
44
XDOT = 13711
193463 XDOT = 4243
140058
YDOT = -11093
235165 feet/sec YDOT = -3334
125209 meter/sec
ZDOT = -17877
771470 ZDOT = -5428
688823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13113202
96 X = -3996904
26
Y = 16399991
62 feet Y = 4998717
45 meter
Z = -7530879
81 Z = -2295412
17
XDOT = -7761
630605 XDOT = -2365
745008
YDOT = -14345
530242 feet/sec YDOT = -4372
517618 meter/sec
ZDOT = -17784
545995 ZDOT = -5420
729619
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 19165
52770056
00016717 00000-0 10270-3 0 9045
2 25544 51
6419 14
5057 0007864 43
7904 316
3870 15
51187976 14836
Satellite: ISS
Catalog Number: 25544
Epoch time: 19165
52770056 = yrday
fracday
Element set: 904
Inclination: 51
6419 deg
RA of node: 14
5057 deg
Eccentricity:
0007864
Arg of perigee: 43
7904 deg
Mean anomaly: 316
3870 deg
Mean motion: 15
51187976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 325
Coasting Arc #6 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2019/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5268483
93 A = 6794191
84 meter
Y = 3151350
48 meter E =
0020162
Z = 2884777
23 I = 51
71354
XDOT = -4744
225553 Wp = 68
50337
YDOT = 3282
331427 meter/sec RA = 9
11287 deg
ZDOT = 5057
576247 TA = 324
30466
MA = 324
43930
Ha = 228
085 n
mi
Hp = 216
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17285052
27 X = 5218840
32
Y = 10339076
36 feet Y = 3209988
31 meter
Z = 9464492
22 Z = 2910249
69
XDOT = -15565
044465 XDOT = -4805
143999
YDOT = 10768
803895 feet/sec YDOT = 3228
936731 meter/sec
ZDOT = 16593
097923 ZDOT = 5034
382974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12472932
98 X = 3801749
97
Y = -15744925
23 feet Y = -4799053
21 meter
Z = 9579635
55 Z = 2919872
92
XDOT = 7511
668350 XDOT = 2289
556513
YDOT = 16023
851886 feet/sec YDOT = 4884
070055 meter/sec
ZDOT = 16487
468440 ZDOT = 5025
380381
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 19166
55847701
00016717 00000-0 10270-3 0 9052
2 25544 51
6418 9
3889 0007825 47
2021 312
9787 15
51220849 14999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19166
55847701 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 9
3889 deg
Eccentricity:
0007825
Arg of perigee: 47
2021 deg
Mean anomaly: 312
9787 deg
Mean motion: 15
51220849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 335
Coasting Arc #7 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2019/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4916093
84 A = 6792558
94 meter
Y = -3132767
20 meter E =
0012637
Z = -3502021
41 I = 51
67336
XDOT = 5266
150035 Wp = 63
87048
YDOT = -3207
994994 meter/sec RA = 4
15459 deg
ZDOT = -4530
109665 TA = 157
15829
MA = 157
10203
Ha = 228
295 n
mi
Hp = 216
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16128916
81 X = -4863686
02
Y = -10278107
62 feet Y = -3187448
74 meter
Z = -11489571
54 Z = -3525775
34
XDOT = 17277
395127 XDOT = 5323
636218
YDOT = -10524
917960 feet/sec YDOT = -3148
782971 meter/sec
ZDOT = -14862
564517 ZDOT = -4504
389511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12009031
00 X = -3660352
65
Y = 14801568
47 feet Y = 4511518
07 meter
Z = -11596915
67 Z = -3534739
90
XDOT = -7437
840529 XDOT = -2267
053793
YDOT = -17568
970464 feet/sec YDOT = -5355
022197 meter/sec
ZDOT = -14745
483687 ZDOT = -4494
423428
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 19167
52482930
00016717 00000-0 10270-3 0 9060
2 25544 51
6401 4
5923 0008042 51
3290 308
8579 15
51209637 15146
Satellite: ISS
Catalog Number: 25544
Epoch time: 19167
52482930 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 4
5923 deg
Eccentricity:
0008042
Arg of perigee: 51
3290 deg
Mean anomaly: 308
8579 deg
Mean motion: 15
51209637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1514
Checksum: 300
Coasting Arc #8 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2019/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4501922
28 A = 6790934
47 meter
Y = 3108619
57 meter E =
0017094
Z = 4006667
08 I = 51
63407
XDOT = -5741
722366 Wp = 81
64613
YDOT = 3208
339937 meter/sec RA = 359
19236 deg
ZDOT = 3950
226944 TA = 327
25514
MA = 327
36097
Ha = 228
192 n
mi
Hp = 216
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14770086
23 X = 4447364
04
Y = 10198883
12 feet Y = 3158657
40 meter
Z = 13145233
19 Z = 4028403
83
XDOT = -18837
671805 XDOT = -5796
360226
YDOT = 10526
049662 feet/sec YDOT = 3143
825722 meter/sec
ZDOT = 12960
062151 ZDOT = 3922
203685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11544172
60 X = 3518663
81
Y = -13649671
98 feet Y = -4160420
02 meter
Z = 13243426
81 Z = 4036596
49
XDOT = 7692
315455 XDOT = 2344
617751
YDOT = 18994
245870 feet/sec YDOT = 5789
446141 meter/sec
ZDOT = 12832
536715 ZDOT = 3911
357191
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 19168
55560317
00016717 00000-0 10270-3 0 9071
2 25544 51
6396 359
4762 0007864 54
9160 305
2728 15
51206967 15306
Satellite: ISS
Catalog Number: 25544
Epoch time: 19168
55560317 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 359
4762 deg
Eccentricity:
0007864
Arg of perigee: 54
9160 deg
Mean anomaly: 305
2728 deg
Mean motion: 15
51206967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 331
Coasting Arc #9 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2019/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4034325
67 A = 6789282
89 meter
Y = -3156540
13 meter E =
0017421
Z = -4473728
74 I = 51
59513
XDOT = 6127
305253 Wp = 64
42505
YDOT = -3216
206523 meter/sec RA = 354
22516 deg
ZDOT = -3258
818003 TA = 172
65382
MA = 172
62826
Ha = 228
362 n
mi
Hp = 216
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13235976
62 X = -3976997
69
Y = -10356102
78 feet Y = -3201333
38 meter
Z = -14677587
72 Z = -4493187
29
XDOT = 20102
707522 XDOT = 6178
643873
YDOT = -10551
858672 feet/sec YDOT = -3147
399025 meter/sec
ZDOT = -10691
660116 ZDOT = -3228
929870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11344751
23 X = -3457880
18
Y = 12294304
80 feet Y = 3747304
10 meter
Z = -14765439
78 Z = -4500506
05
XDOT = -8059
722156 XDOT = -2456
603313
YDOT = -20104
417377 feet/sec YDOT = -6127
826416 meter/sec
ZDOT = -10555
678661 ZDOT = -3217
370856
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 19169
52195245
00016717 00000-0 10270-3 0 9084
2 25544 51
6394 354
6792 0007996 59
4959 300
6981 15
51216222 15457
Satellite: ISS
Catalog Number: 25544
Epoch time: 19169
52195245 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 354
6792 deg
Eccentricity:
0007996
Arg of perigee: 59
4959 deg
Mean anomaly: 300
6981 deg
Mean motion: 15
51216222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 345
Coasting Arc #10 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2019/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3521652
13 A = 6787948
88 meter
Y = 3221823
10 meter E =
0013253
Z = 4814807
65 I = 51
55776
XDOT = -6461
723490 Wp = 88
85918
YDOT = 3271
535548 meter/sec RA = 349
25403 deg
ZDOT = 2531
325466 TA = 336
19733
MA = 336
25857
Ha = 228
333 n
mi
Hp = 216
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11553976
81 X = 3461975
56
Y = 10570285
75 feet Y = 3260870
11 meter
Z = 15796613
03 Z = 4831770
05
XDOT = -21199
880216 XDOT = -6510
122172
YDOT = 10733
384345 feet/sec YDOT = 3199
004949 meter/sec
ZDOT = 8304
873575 ZDOT = 2499
820104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11243429
15 X = 3426997
21
Y = -10788289
97 feet Y = -3288270
78 meter
Z = 15873134
68 Z = 4838131
45
XDOT = 8644
008063 XDOT = 2634
693658
YDOT = 21044
750773 feet/sec YDOT = 6414
440036 meter/sec
ZDOT = 8161
555575 ZDOT = 2487
642139
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 19170
55272233
00016717 00000-0 10270-3 0 9093
2 25544 51
6397 349
5626 0007989 62
6159 297
5804 15
51194442 15614
Satellite: ISS
Catalog Number: 25544
Epoch time: 19170
55272233 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 349
5626 deg
Eccentricity:
0007989
Arg of perigee: 62
6159 deg
Mean anomaly: 297
5804 deg
Mean motion: 15
51194442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1561
Checksum: 341
Coasting Arc #11 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2019/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2990708
79 A = 6786793
48 meter
Y = -3366792
59 meter E =
0021433
Z = -5096919
48 I = 51
52142
XDOT = 6673
985292 Wp = 73
19861
YDOT = -3307
859022 meter/sec RA = 344
27986 deg
ZDOT = -1731
061892 TA = 179
99393
MA = 179
99390
Ha = 228
481 n
mi
Hp = 216
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9812036
71 X = -2928080
32
Y = -11045907
44 feet Y = -3399885
74 meter
Z = -16722176
77 Z = -5111295
54
XDOT = 21896
277206 XDOT = 6718
887149
YDOT = -10852
555848 feet/sec YDOT = -3232
974486 meter/sec
ZDOT = -5679
336915 ZDOT = -1698
533992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11455887
88 X = -3491754
62
Y = 9213048
25 feet Y = 2808137
11 meter
Z = -16786950
47 Z = -5116662
50
XDOT = -9223
129717 XDOT = -2811
209938
YDOT = -21547
059073 feet/sec YDOT = -6567
543605 meter/sec
ZDOT = -5531
384782 ZDOT = -1685
966082
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 19171
51906683
00016717 00000-0 10270-3 0 9105
2 25544 51
6396 344
7666 0008137 67
8133 292
3880 15
51218198 15767
Satellite: ISS
Catalog Number: 25544
Epoch time: 19171
51906683 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 344
7666 deg
Eccentricity:
0008137
Arg of perigee: 67
8133 deg
Mean anomaly: 292
3880 deg
Mean motion: 15
51218198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 336
Coasting Arc #12 (Orbit 1591)
---------------------------------------
Vector Time (GMT): 2019/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2437185
33 A = 6786184
59 meter
Y = 3539402
10 meter E =
0010603
Z = 5242862
43 I = 51
48662
XDOT = -6837
671093 Wp = 84
42139
YDOT = 3358
312087 meter/sec RA = 339
30201 deg
ZDOT = 910
805246 TA = 356
84860
MA = 356
85527
Ha = 228
481 n
mi
Hp = 216
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7996014
88 X = 2371958
97
Y = 11612211
60 feet Y = 3566290
90 meter
Z = 17200992
23 Z = 5254543
36
XDOT = -22433
304112 XDOT = -6879
140649
YDOT = 11018
084275 feet/sec YDOT = 3281
616446 meter/sec
ZDOT = 2988
206188 ZDOT = 877
490562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11814518
50 X = 3601065
24
Y = -7575417
32 feet Y = -2308987
20 meter
Z = 17253522
86 Z = 5258873
77
XDOT = 9877
874718 XDOT = 3010
776214
YDOT = 21870
455332 feet/sec YDOT = 6666
114785 meter/sec
ZDOT = 2836
690040 ZDOT = 864
623124
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 19172
54983437
00016717 00000-0 10270-3 0 9112
2 25544 51
6390 339
6504 0008104 71
2963 288
9067 15
51180476 15922
Satellite: ISS
Catalog Number: 25544
Epoch time: 19172
54983437 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 339
6504 deg
Eccentricity:
0008104
Arg of perigee: 71
2963 deg
Mean anomaly: 288
9067 deg
Mean motion: 15
51180476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1592
Checksum: 328
Coasting Arc #13 (Orbit 1606)
---------------------------------------
Vector Time (GMT): 2019/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1905574
31 A = 6785822
84 meter
Y = -3785740
24 meter E =
0022777
Z = -5319164
79 I = 51
45695
XDOT = 6868
307415 Wp = 84
24637
YDOT = -3360
985578 meter/sec RA = 334
32225 deg
ZDOT = -66
493012 TA = 185
10499
MA = 185
12826
Ha = 228
495 n
mi
Hp = 216
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6251884
21 X = -1837262
19
Y = -12420407
61 feet Y = -3806667
02 meter
Z = -17451328
05 Z = -5328255
86
XDOT = 22533
816978 XDOT = 6905
703436
YDOT = -11026
855571 feet/sec YDOT = -3283
970247 meter/sec
ZDOT = -218
152927 ZDOT = -33
039345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12475238
66 X = -3802452
74
Y = 6024681
37 feet Y = 1836322
88 meter
Z = -17492085
84 Z = -5331587
76
XDOT = -10388
292204 XDOT = -3166
351464
YDOT = -21721
472209 feet/sec YDOT = -6620
704729 meter/sec
ZDOT = -66
018953 ZDOT = -20
122577
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 19173
51617465
00016717 00000-0 10270-3 0 9126
2 25544 51
6409 334
8549 0008100 75
2908 284
9140 15
51228041 16074
Satellite: ISS
Catalog Number: 25544
Epoch time: 19173
51617465 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 334
8549 deg
Eccentricity:
0008100
Arg of perigee: 75
2908 deg
Mean anomaly: 284
9140 deg
Mean motion: 15
51228041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1607
Checksum: 304
Coasting Arc #14 (Orbit 1622)
---------------------------------------
Vector Time (GMT): 2019/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1371012
05 A = 6786145
15 meter
Y = 4058420
56 meter E =
0011378
Z = 5254128
19 I = 51
42739
XDOT = -6861
898936 Wp = 73
21179
YDOT = 3340
292584 meter/sec RA = 329
33869 deg
ZDOT = -784
946161 TA = 24
33467
MA = 24
28099
Ha = 228
575 n
mi
Hp = 216
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4498071
05 X = 1300006
35
Y = 13315028
08 feet Y = 4073354
51 meter
Z = 17237953
36 Z = 5260616
03
XDOT = -22512
791786 XDOT = -6894
928260
YDOT = 10958
965172 feet/sec YDOT = 3263
373439 meter/sec
ZDOT = -2575
282682 ZDOT = -818
358191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13279014
77 X = 4047443
70
Y = -4493594
30 feet Y = -1369647
54 meter
Z = 17266876
65 Z = 5262944
00
XDOT = 10819
213829 XDOT = 3297
696375
YDOT = 21434
042962 feet/sec YDOT = 6533
096295 meter/sec
ZDOT = -2727
211090 ZDOT = -831
253940
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 19174
54693723
00016717 00000-0 10270-3 0 9132
2 25544 51
6402 329
7380 0008213 79
0359 281
1716 15
51188064 16236
Satellite: ISS
Catalog Number: 25544
Epoch time: 19174
54693723 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 329
7380 deg
Eccentricity:
0008213
Arg of perigee: 79
0359 deg
Mean anomaly: 281
1716 deg
Mean motion: 15
51188064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1623
Checksum: 312
Coasting Arc #15 (Orbit 1637)
---------------------------------------
Vector Time (GMT): 2019/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -897839
55 A = 6786721
90 meter
Y = -4385346
68 meter E =
0021263
Z = -5120029
38 I = 51
40189
XDOT = 6733
656572 Wp = 94
61996
YDOT = -3250
084952 meter/sec RA = 324
35627 deg
ZDOT = 1607
034574 TA = 190
95383
MA = 191
00020
Ha = 228
532 n
mi
Hp = 216
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2945667
83 X = -823864
54
Y = -14387620
35 feet Y = -4394972
76 meter
Z = -16797996
64 Z = -5124211
54
XDOT = 22092
049121 XDOT = 6761
693470
YDOT = -10663
008372 feet/sec YDOT = -3174
627900 meter/sec
ZDOT = 5272
423143 ZDOT = 1639
811655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14311595
13 X = -4362174
20
Y = 3199872
42 feet Y = 975321
11 meter
Z = -16816430
38 Z = -5125647
98
XDOT = -10989
986917 XDOT = -3349
748012
YDOT = -20732
555061 feet/sec YDOT = -6319
282783 meter/sec
ZDOT = 5421
446663 ZDOT = 1652
456943
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 19175
51327351
00016717 00000-0 10270-3 0 9142
2 25544 51
6405 324
9434 0008135 82
7109 277
4967 15
51228497 16380
Satellite: ISS
Catalog Number: 25544
Epoch time: 19175
51327351 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 324
9434 deg
Eccentricity:
0008135
Arg of perigee: 82
7109 deg
Mean anomaly: 277
4967 deg
Mean motion: 15
51228497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1638
Checksum: 326
Coasting Arc #16 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2019/175/23:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5579301
42 A = 6797531
44 meter
Y = -3836470
97 meter E =
0020379
Z = 507115
02 I = 51
42478
XDOT = 2337
044739 Wp = 62
71074
YDOT = 4210
392914 meter/sec RA = 322
06201 deg
ZDOT = 5964
871987 TA = 302
77116
MA = 302
96736
Ha = 228
473 n
mi
Hp = 216
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18304794
67 X = 5619324
00
Y = -12586847
00 feet Y = -3773855
58 meter
Z = 1663763
19 Z = 534313
81
XDOT = 7667
469615 XDOT = 2260
815361
YDOT = 13813
625047 feet/sec YDOT = 4236
100507 meter/sec
ZDOT = 19569
789985 ZDOT = 5976
039728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9015489
59 X = 2747921
23
Y = 20292558
34 feet Y = 6185171
78 meter
Z = 1787556
07 Z = 544847
09
XDOT = -13483
610375 XDOT = -4109
804442
YDOT = 4214
875357 feet/sec YDOT = 1284
694009 meter/sec
ZDOT = 19619
923332 ZDOT = 5980
152632
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 19176
02865060
00016717 00000-0 10270-3 0 9154
2 25544 51
6393 322
3892 0008153 83
0421 277
1658 15
51269574 16461
Satellite: ISS
Catalog Number: 25544
Epoch time: 19176
02865060 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 322
3892 deg
Eccentricity:
0008153
Arg of perigee: 83
0421 deg
Mean anomaly: 277
1658 deg
Mean motion: 15
51269574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 319
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