[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 15th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
016/05:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
2
018/18:05:10
698 3
0 3
2 3
2
N/A 0
8 0
0 220
9
000/00:08:17
397 -0
6 -0
0 218
0
020/01:03:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 217
9
025/12:55:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 217
5
026/08:59:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 217
4
Coasting Arc #1 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2019/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2829696
45 A = 6787626
57 meter
Y = -5628335
52 meter E =
0003091
Z = -2524477
48 I = 51
92620
XDOT = 5505
483972 Wp = 146
58238
YDOT = -385
072906 meter/sec RA = 45
01300 deg
ZDOT = -5318
198167 TA = 61
61581
MA = 61
58465
Ha = 220
719 n
mi
Hp = 216
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9283781
02 X = -2754286
09
Y = -18465667
70 feet Y = -5659557
42 meter
Z = -8282406
43 Z = -2538040
02
XDOT = 18062
611458 XDOT = 5535
213467
YDOT = -1263
362551 feet/sec YDOT = -323
340344 meter/sec
ZDOT = -17448
156715 ZDOT = -5291
382574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13452162
09 X = 4100219
01
Y = -15658974
03 feet Y = -4772855
28 meter
Z = -8342877
04 Z = -2542908
92
XDOT = 7063
413020 XDOT = 2152
928288
YDOT = 15289
851465 feet/sec YDOT = 4660
346727 meter/sec
ZDOT = -17327
048985 ZDOT = -5281
284531
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 19014
52708432
00016717 00000-0 10270-3 0 9003
2 25544 51
6422 45
5300 0002452 287
2155 72
8729 15
53770861 31374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19014
52708432 = yrday
fracday
Element set: 900
Inclination: 51
6422 deg
RA of node: 45
5300 deg
Eccentricity:
0002452
Arg of perigee: 287
2155 deg
Mean anomaly: 72
8729 deg
Mean motion: 15
53770861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3137
Checksum: 291
Coasting Arc #2 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2019/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1735385
68 A = 6784308
64 meter
Y = 5345456
63 meter E =
0009272
Z = 3792576
05 I = 51
88865
XDOT = -6317
419207 Wp = 92
76245
YDOT = -964
724541 meter/sec RA = 40
05289 deg
ZDOT = 4241
062848 TA = 312
54859
MA = 312
62682
Ha = 220
859 n
mi
Hp = 216
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5693522
56 X = 1657060
17
Y = 17537587
36 feet Y = 5364424
80 meter
Z = 12442834
81 Z = 3800815
88
XDOT = -20726
440969 XDOT = -6326
762490
YDOT = -3165
106762 feet/sec YDOT = -1035
422762 meter/sec
ZDOT = 13914
248189 ZDOT = 4210
352606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13789876
04 X = -4203154
22
Y = 12203015
80 feet Y = 3719479
22 meter
Z = 12479304
14 Z = 3803691
90
XDOT = -4605
049008 XDOT = -1403
618938
YDOT = -19322
838392 feet/sec YDOT = -5889
601142 meter/sec
ZDOT = 13775
747544 ZDOT = 4198
847851
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 19015
55616275
00016717 00000-0 10270-3 0 9011
2 25544 51
6402 40
4028 0002312 294
1684 65
9227 15
53745097 31539
Satellite: ISS
Catalog Number: 25544
Epoch time: 19015
55616275 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 40
4028 deg
Eccentricity:
0002312
Arg of perigee: 294
1684 deg
Mean anomaly: 65
9227 deg
Mean motion: 15
53745097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 294
Coasting Arc #3 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5936183
90 A = 6787015
53 meter
Y = -1566921
04 meter E =
0010879
Z = 2881736
78 I = 51
87942
XDOT = -975
177622 Wp = 98
20537
YDOT = -5666
323504 meter/sec RA = 36
39803 deg
ZDOT = -5074
986258 TA = 49
10465
MA = 49
01047
Ha = 220
802 n
mi
Hp = 216
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19475668
98 X = -5932218
78
Y = -5140817
07 feet Y = -1633281
59 meter
Z = 9454517
00 Z = 2852910
69
XDOT = -3199
401648 XDOT = -887
091372
YDOT = -18590
300210 feet/sec YDOT = -5676
735795 meter/sec
ZDOT = -16650
217381 ZDOT = -5079
509679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20200160
38 X = 6157008
88
Y = -350365
99 feet Y = -106791
55 meter
Z = 9324609
29 Z = 2842140
91
XDOT = 7988
070137 XDOT = 2434
763778
YDOT = 15584
615103 feet/sec YDOT = 4750
190683 meter/sec
ZDOT = -16669
858994 ZDOT = -5080
973021
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 19016
26365308
00016717 00000-0 10270-3 0 9029
2 25544 51
6410 36
8752 0002482 283
3022 76
7854 15
53747168 31644
Satellite: ISS
Catalog Number: 25544
Epoch time: 19016
26365308 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 36
8752 deg
Eccentricity:
0002482
Arg of perigee: 283
3022 deg
Mean anomaly: 76
7854 deg
Mean motion: 15
53747168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 307
Coasting Arc #4 (Orbit 3178)
---------------------------------------
Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6163261
66 A = 6789600
00 meter
Y = 2448057
32 meter E =
0008332
Z = -1434397
95 I = 51
86204
XDOT = -624
072454 Wp = 20
10035
YDOT = 4964
754004 meter/sec RA = 31
44094 deg
ZDOT = 5809
373304 TA = 324
30761
MA = 324
36329
Ha = 220
841 n
mi
Hp = 216
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20220674
74 X = 6142396
20
Y = 8031684
12 feet Y = 2516862
65 meter
Z = -4706030
02 Z = -1404509
78
XDOT = -2047
481803 XDOT = -707
761897
YDOT = 16288
563005 feet/sec YDOT = 4957
306791 meter/sec
ZDOT = 19059
623701 ZDOT = 5806
138942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21705992
01 X = -6615986
36
Y = -1866025
05 feet Y = -568764
43 meter
Z = -4571456
75 Z = -1393380
02
XDOT = -2739
427061 XDOT = -834
977368
YDOT = -14644
144467 feet/sec YDOT = -4463
535234 meter/sec
ZDOT = 19044
335112 ZDOT = 5804
713342
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 19017
22841008
00016717 00000-0 10270-3 0 9033
2 25544 51
6423 32
0688 0002536 292
9444 67
1441 15
53751354 31792
Satellite: ISS
Catalog Number: 25544
Epoch time: 19017
22841008 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 32
0688 deg
Eccentricity:
0002536
Arg of perigee: 292
9444 deg
Mean anomaly: 67
1441 deg
Mean motion: 15
53751354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 299
Coasting Arc #5 (Orbit 3194)
---------------------------------------
Vector Time (GMT): 2019/018/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 928709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6011679
70 A = 6790369
24 meter
Y = -3142412
48 meter E =
0009430
Z = -167195
90 I = 51
83495
XDOT = 2322
870056 Wp = 141
26601
YDOT = -4133
385208 meter/sec RA = 26
48690 deg
ZDOT = -6025
324510 TA = 40
52991
MA = 40
45972
Ha = 220
793 n
mi
Hp = 216
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19723358
59 X = -5975281
42
Y = -10309752
24 feet Y = -3209435
74 meter
Z = -548542
98 Z = -196310
04
XDOT = 7620
964751 XDOT = 2398
185518
YDOT = -13560
975091 feet/sec YDOT = -4106
987556 meter/sec
ZDOT = -19768
125034 ZDOT = -6013
858450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21920578
10 X = 6681392
20
Y = 3824823
40 feet Y = 1165806
17 meter
Z = -679519
52 Z = -207117
55
XDOT = -2982
363790 XDOT = -909
024483
YDOT = 13679
275511 feet/sec YDOT = 4169
443176 meter/sec
ZDOT = -19715
790181 ZDOT = -6009
372847
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 19018
25748341
00016717 00000-0 10270-3 0 9044
2 25544 51
6414 26
9420 0002471 294
9208 65
1687 15
53764139 31959
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
25748341 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 26
9420 deg
Eccentricity:
0002471
Arg of perigee: 294
9208 deg
Mean anomaly: 65
1687 deg
Mean motion: 15
53764139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3195
Checksum: 317
Coasting Arc #6 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/018/18:09:19
397
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1978710
32 A = 6780178
40 meter
Y = -3711628
21 meter E =
0010205
Z = -5326606
75 I = 51
77926
XDOT = 6910
898202 Wp = 86
86691
YDOT = 3291
485180 meter/sec RA = 23
84784 deg
ZDOT = 274
698500 TA = 185
74362
MA = 185
75534
Ha = 220
947 n
mi
Hp = 217
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6491831
76 X = 2045941
14
Y = -12177257
90 feet Y = -3689124
43 meter
Z = -17475743
95 Z = -5316832
12
XDOT = 22673
550533 XDOT = 6872
243943
YDOT = 10798
835894 feet/sec YDOT = 3368
551498 meter/sec
ZDOT = 901
241799 ZDOT = 308
175143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -198942
88 X = -60637
79
Y = -13854538
50 feet Y = -4222863
34 meter
Z = -17431101
53 Z = -5312999
75
XDOT = 24041
484986 XDOT = 7327
844624
YDOT = -1664
524446 feet/sec YDOT = -507
347051 meter/sec
ZDOT = 1051
886530 ZDOT = 320
615014
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 19018
77202257
00016717 00000-0 10270-3 0 9053
2 25544 51
6414 24
3821 0004744 283
7239 76
3385 15
53170510 32034
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
77202257 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 24
3821 deg
Eccentricity:
0004744
Arg of perigee: 283
7239 deg
Mean anomaly: 76
3385 deg
Mean motion: 15
53170510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 291
Coasting Arc #7 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2019/019/18:09:19
397
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3247629
22 A = 6781237
02 meter
Y = 3116494
70 meter E =
0004618
Z = 5073430
95 I = 51
75198
XDOT = -6443
508778 Wp = 358
22806
YDOT = -3727
145510 meter/sec RA = 18
86814 deg
ZDOT = -1830
686914 TA = 109
50062
MA = 109
45073
Ha = 221
058 n
mi
Hp = 217
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10654951
51 X = -3306880
86
Y = 10224720
15 feet Y = 3079845
62 meter
Z = 16645114
67 Z = 5057511
87
XDOT = -21140
120663 XDOT = -6392
459589
YDOT = -12228
167683 feet/sec YDOT = -3798
915683 meter/sec
ZDOT = -6006
190662 ZDOT = -1861
862946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4137512
10 X = -1261113
69
Y = 14260272
40 feet Y = 4346531
03 meter
Z = 16572819
95 Z = 5051395
52
XDOT = -23347
045175 XDOT = -7116
179369
YDOT = 386
241740 feet/sec YDOT = 117
726482 meter/sec
ZDOT = -6146
386608 ZDOT = -1873
418638
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 19019
80149679
00016717 00000-0 10270-3 0 9067
2 25544 51
6413 19
2582 0004951 287
3682 72
6929 15
53193896 32194
Satellite: ISS
Catalog Number: 25544
Epoch time: 19019
80149679 = yrday
fracday
Element set: 906
Inclination: 51
6413 deg
RA of node: 19
2582 deg
Eccentricity:
0004951
Arg of perigee: 287
3682 deg
Mean anomaly: 72
6929 deg
Mean motion: 15
53193896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 345
Coasting Arc #8 (Orbit 3222)
---------------------------------------
Vector Time (GMT): 2019/020/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1820716
88 A = 6780253
91 meter
Y = -3816708
92 meter E =
0010188
Z = -5308756
95 I = 51
73723
XDOT = 7154
952543 Wp = 89
82382
YDOT = 2683
196869 meter/sec RA = 17
44620 deg
ZDOT = 525
726351 TA = 185
18580
MA = 185
19636
Ha = 220
985 n
mi
Hp = 217
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5973480
57 X = 1889047
58
Y = -12522010
91 feet Y = -3795965
79 meter
Z = -17417181
61 Z = -5299747
20
XDOT = 23474
253749 XDOT = 7121
862876
YDOT = 8803
139334 feet/sec YDOT = 2763
023459 meter/sec
ZDOT = 1724
823987 ZDOT = 560
401693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13239044
54 X = -4035260
78
Y = 4317942
42 feet Y = 1316108
85 meter
Z = -17375975
24 Z = -5296197
25
XDOT = -9649
252720 XDOT = -2941
092229
YDOT = -22027
834444 feet/sec YDOT = -6714
083939 meter/sec
ZDOT = 1880
961847 ZDOT = 573
317171
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 19020
05886592
00016717 00000-0 10270-3 0 9079
2 25544 51
6391 17
9724 0004596 283
7195 76
3446 15
53170504 32237
Satellite: ISS
Catalog Number: 25544
Epoch time: 19020
05886592 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 17
9724 deg
Eccentricity:
0004596
Arg of perigee: 283
7195 deg
Mean anomaly: 76
3446 deg
Mean motion: 15
53170504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3223
Checksum: 320
Coasting Arc #9 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2019/021/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3133093
51 A = 6781742
52 meter
Y = 3348126
14 meter E =
0004819
Z = 4997336
25 I = 51
70928
XDOT = -6675
471755 Wp = 10
30574
YDOT = -3149
235811 meter/sec RA = 12
46214 deg
ZDOT = -2070
332732 TA = 99
84792
MA = 99
79350
Ha = 221
258 n
mi
Hp = 217
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10279178
18 X = -3194574
03
Y = 10984665
80 feet Y = 3312745
51 meter
Z = 16395460
13 Z = 4981968
20
XDOT = -21901
154051 XDOT = -6629
703706
YDOT = -10332
138487 feet/sec YDOT = -3223
629498 meter/sec
ZDOT = -6792
430223 ZDOT = -2102
647995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15114072
59 X = 4606769
33
Y = -417587
45 feet Y = -127280
65 meter
Z = 16325621
90 Z = 4976049
55
XDOT = 8110
038362 XDOT = 2471
939693
YDOT = 21660
760474 feet/sec YDOT = 6602
199792 meter/sec
ZDOT = -6937
848359 ZDOT = -2114
656180
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 19021
08833941
00016717 00000-0 10270-3 0 9084
2 25544 51
6386 12
8464 0004509 287
8517 72
2143 15
53130165 32398
Satellite: ISS
Catalog Number: 25544
Epoch time: 19021
08833941 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 12
8464 deg
Eccentricity:
0004509
Arg of perigee: 287
8517 deg
Mean anomaly: 72
2143 deg
Mean motion: 15
53130165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 306
Coasting Arc #10 (Orbit 3253)
---------------------------------------
Vector Time (GMT): 2019/022/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324456
33 A = 6784229
01 meter
Y = -2900794
42 meter E =
0003976
Z = -4352625
85 I = 51
68592
XDOT = 5852
664258 Wp = 108
79321
YDOT = 3529
308393 meter/sec RA = 7
48243 deg
ZDOT = 3464
030130 TA = 196
38349
MA = 196
39634
Ha = 221
253 n
mi
Hp = 217
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14187848
84 X = 4377714
47
Y = -9517042
06 feet Y = -2852137
29 meter
Z = -14280268
55 Z = -4331490
68
XDOT = 19201
654390 XDOT = 5795
937703
YDOT = 11579
095779 feet/sec YDOT = 3594
439579 meter/sec
ZDOT = 11364
928249 ZDOT = 3492
321814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16884341
14 X = -5146347
18
Y = -3084659
83 feet Y = -940204
31 meter
Z = -14184467
29 Z = -4323425
63
XDOT = -5926
114396 XDOT = -1806
279668
YDOT = -20387
472132 feet/sec YDOT = -6214
101506 meter/sec
ZDOT = 11492
130727 ZDOT = 3502
801445
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 19022
05346789
00016717 00000-0 10270-3 0 9092
2 25544 51
6394 8
0428 0004585 291
4174 68
6488 15
53161727 32544
Satellite: ISS
Catalog Number: 25544
Epoch time: 19022
05346789 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 8
0428 deg
Eccentricity:
0004585
Arg of perigee: 291
4174 deg
Mean anomaly: 68
6488 deg
Mean motion: 15
53161727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3254
Checksum: 330
Coasting Arc #11 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2019/023/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5338626
77 A = 6787398
38 meter
Y = 2452548
81 meter E =
0008477
Z = 3393595
34 I = 51
66343
XDOT = -4728
357610 Wp = 78
08431
YDOT = -3871
168335 meter/sec RA = 2
50588 deg
ZDOT = -4629
215342 TA = 62
29682
MA = 62
21084
Ha = 221
350 n
mi
Hp = 217
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17515179
68 X = -5382138
81
Y = 8046419
98 feet Y = 2392605
18 meter
Z = 11133842
99 Z = 3367557
43
XDOT = -15512
984284 XDOT = -4662
232189
YDOT = -12700
683514 feet/sec YDOT = -3923
674269 meter/sec
ZDOT = -15187
714378 ZDOT = -4652
022775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18347077
79 X = 5592189
31
Y = 6125494
48 feet Y = 1867050
72 meter
Z = 11015984
17 Z = 3357671
97
XDOT = 3038
838668 XDOT = 926
238026
YDOT = 18464
125266 feet/sec YDOT = 5627
865381 meter/sec
ZDOT = -15290
114605 ZDOT = -4660
426932
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 19023
08293871
00016717 00000-0 10270-3 0 9101
2 25544 51
6395 2
9178 0004617 294
2978 65
7692 15
53151143 32703
Satellite: ISS
Catalog Number: 25544
Epoch time: 19023
08293871 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 2
9178 deg
Eccentricity:
0004617
Arg of perigee: 294
2978 deg
Mean anomaly: 65
7692 deg
Mean motion: 15
53151143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 318
Coasting Arc #12 (Orbit 3284)
---------------------------------------
Vector Time (GMT): 2019/024/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6088239
54 A = 6790110
59 meter
Y = -2017584
53 meter E =
0006900
Z = -2216023
52 I = 51
64120
XDOT = 3373
938490 Wp =
63998
YDOT = 4184
843322 meter/sec RA = 357
53442 deg
ZDOT = 5466
265841 TA = 334
74862
MA = 334
78233
Ha = 221
514 n
mi
Hp = 217
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19974539
17 X = 6121112
18
Y = -6619371
80 feet Y = -1949317
78 meter
Z = -7270418
37 Z = -2186370
08
XDOT = 11069
352000 XDOT = 3300
340257
YDOT = 13729
800925 feet/sec YDOT = 4222
161540 meter/sec
ZDOT = 17933
943048 ZDOT = 5482
475985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19300214
19 X = -5882705
28
Y = -8498943
71 feet Y = -2590478
04 meter
Z = -7136313
45 Z = -2175148
34
XDOT = 450
035474 XDOT = 137
170812
YDOT = -16122
151433 feet/sec YDOT = -4914
031757 meter/sec
ZDOT = 18006
523706 ZDOT = 5488
388426
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 19024
04806487
00016717 00000-0 10270-3 0 9112
2 25544 51
6412 358
1137 0004659 299
7091 60
3597 15
53169889 32853
Satellite: ISS
Catalog Number: 25544
Epoch time: 19024
04806487 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 358
1137 deg
Eccentricity:
0004659
Arg of perigee: 299
7091 deg
Mean anomaly: 60
3597 deg
Mean motion: 15
53169889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3285
Checksum: 339
Coasting Arc #13 (Orbit 3300)
---------------------------------------
Vector Time (GMT): 2019/025/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 928366
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6552033
19 A = 6791807
87 meter
Y = 1546519
23 meter E =
0008710
Z = 865714
30 I = 51
61316
XDOT = -1848
950872 Wp = 127
16501
YDOT = -4494
801544 meter/sec RA = 352
56636 deg
ZDOT = -5927
973487 TA = 43
47023
MA = 43
40160
Ha = 221
549 n
mi
Hp = 217
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21496171
88 X = -6573044
91
Y = 5073881
98 feet Y = 1473132
35 meter
Z = 2840270
01 Z = 833836
64
XDOT = -6066
111785 XDOT = -1769
757163
YDOT = -14746
724226 feet/sec YDOT = -4515
035093 meter/sec
ZDOT = -19448
731913 ZDOT = -5936
762384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19552596
24 X = 5959631
34
Y = 10311317
77 feet Y = 3142889
66 meter
Z = 2696205
38 Z = 821803
40
XDOT = -4463
623998 XDOT = -1360
512595
YDOT = 13592
238051 feet/sec YDOT = 4142
914158 meter/sec
ZDOT = -19487
779015 ZDOT = -5939
875044
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 19025
07753157
00016717 00000-0 10270-3 0 9122
2 25544 51
6405 352
9896 0004656 303
5351 56
5356 15
53177678 33013
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
07753157 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 352
9896 deg
Eccentricity:
0004656
Arg of perigee: 303
5351 deg
Mean anomaly: 56
5356 deg
Mean motion: 15
53177678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3301
Checksum: 319
Coasting Arc #14 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2019/025/12:55:30
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060136
58 A = 6783115
20 meter
Y = 2960978
54 meter E =
0003984
Z = 4552865
75 I = 51
56783
XDOT = -6055
953289 Wp = 94
17228
YDOT = 3544
102569 meter/sec RA = 350
13646 deg
ZDOT = 3093
009432 TA = 324
82304
MA = 324
84933
Ha = 221
599 n
mi
Hp = 217
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13320658
07 X = 4004609
48
Y = 9714496
52 feet Y = 3006071
43 meter
Z = 14937223
60 Z = 4572453
06
XDOT = -19868
613152 XDOT = -6110
158171
YDOT = 11627
633100 feet/sec YDOT = 3476
077655 meter/sec
ZDOT = 10147
668739 ZDOT = 3063
460765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3193825
03 X = 973477
87
Y = 16092689
00 feet Y = 4905051
61 meter
Z = 15025207
66 Z = 4579683
29
XDOT = -21383
990261 XDOT = -6517
840231
YDOT = -5113
615911 feet/sec YDOT = -1558
630130 meter/sec
ZDOT = 10013
848294 ZDOT = 3052
220960
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 19025
59226340
00016717 00000-0 10270-3 0 9139
2 25544 51
6400 350
4317 0004980 309
1721 50
8988 15
53207744 33096
Satellite: ISS
Catalog Number: 25544
Epoch time: 19025
59226340 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 350
4317 deg
Eccentricity:
0004980
Arg of perigee: 309
1721 deg
Mean anomaly: 50
8988 deg
Mean motion: 15
53207744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 299
Coasting Arc #15 (Orbit 3321)
---------------------------------------
Vector Time (GMT): 2019/026/08:59:00
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4592363
79 A = 6783957
71 meter
Y = 2422975
74 meter E =
0005360
Z = 4361162
40 I = 51
54198
XDOT = -5452
809776 Wp = 87
45205
YDOT = 4165
489121 meter/sec RA = 345
97313 deg
ZDOT = 3424
212794 TA = 327
76632
MA = 327
79906
Ha = 221
794 n
mi
Hp = 217
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15066810
34 X = 4543744
34
Y = 7949395
49 feet Y = 2474058
98 meter
Z = 14308275
59 Z = 4383351
88
XDOT = -17889
795853 XDOT = -5515
616828
YDOT = 13666
302890 feet/sec YDOT = 4104
160880 meter/sec
ZDOT = 11234
293943 ZDOT = 3397
572928
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10606641
65 X = -3232904
38
Y = 13222522
19 feet Y = 4030224
76 meter
Z = 14408069
70 Z = 4391579
64
XDOT = -9107
163589 XDOT = -2775
863462
YDOT = -19427
520206 feet/sec YDOT = -5921
508159 meter/sec
ZDOT = 11113
525881 ZDOT = 3387
402689
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 19026
42870485
00016717 00000-0 10270-3 0 9148
2 25544 51
6390 346
2679 0004860 313
5493 46
5255 15
53164039 33223
Satellite: ISS
Catalog Number: 25544
Epoch time: 19026
42870485 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 346
2679 deg
Eccentricity:
0004860
Arg of perigee: 313
5493 deg
Mean anomaly: 46
5255 deg
Mean motion: 15
53164039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3322
Checksum: 315
Coasting Arc #16 (Orbit 3336)
---------------------------------------
Vector Time (GMT): 2019/027/08:59:00
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3453483
88 A = 6781419
20 meter
Y = -3019730
07 meter E =
0011479
Z = -5004320
10 I = 51
50199
XDOT = 6298
732230 Wp = 53
15425
YDOT = -3863
732097 meter/sec RA = 340
98049 deg
ZDOT = -2011
753922 TA = 197
21423
MA = 197
25319
Ha = 222
025 n
mi
Hp = 217
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11330327
67 X = -3395151
87
Y = -9907250
89 feet Y = -3058023
21 meter
Z = -16418373
03 Z = -5020953
90
XDOT = 20665
131989 XDOT = 6351
241285
YDOT = -12676
286408 feet/sec YDOT = -3793
001698 meter/sec
ZDOT = -6600
242527 ZDOT = -1981
029916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11670180
98 X = 3557071
16
Y = -9374447
78 feet Y = -2857331
68 meter
Z = -16493014
37 Z = -5027070
78
XDOT = 8291
698191 XDOT = 2527
309609
YDOT = 21709
967819 feet/sec YDOT = 6617
198191 meter/sec
ZDOT = -6461
100172 ZDOT = -1969
343333
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 19027
39382636
00016717 00000-0 10270-3 0 9152
2 25544 51
6394 341
4639 0004780 318
2479 41
8308 15
53175743 33374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19027
39382636 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 341
4639 deg
Eccentricity:
0004780
Arg of perigee: 318
2479 deg
Mean anomaly: 41
8308 deg
Mean motion: 15
53175743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3337
Checksum: 330
Coasting Arc #17 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2019/028/08:59:00
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2188289
78 A = 6780191
07 meter
Y = 3635818
79 meter E =
0003094
Z = 5288322
67 I = 51
46553
XDOT = -6833
149168 Wp = 349
22462
YDOT = 3446
840031 meter/sec RA = 335
98074 deg
ZDOT = 460
791105 TA = 96
38658
MA = 96
35134
Ha = 222
125 n
mi
Hp = 217
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7179428
40 X = 2121782
98
Y = 11928539
34 feet Y = 3659917
87 meter
Z = 17350139
99 Z = 5298790
92
XDOT = -22418
468399 XDOT = -6873
423092
YDOT = 11308
530287 feet/sec YDOT = 3370
201805 meter/sec
ZDOT = 1511
781840 ZDOT = 427
500859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12869319
53 X = -3922568
59
Y = 5156625
93 feet Y = 1571739
58 meter
Z = 17396879
73 Z = 5302568
94
XDOT = -7371
153172 XDOT = -2246
727487
YDOT = -22954
745743 feet/sec YDOT = -6996
606503 meter/sec
ZDOT = 1361
129030 ZDOT = 414
872128
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 19028
42328729
00016717 00000-0 10270-3 0 9161
2 25544 51
6382 336
3390 0004944 321
7154 38
3647 15
53171978 33530
Satellite: ISS
Catalog Number: 25544
Epoch time: 19028
42328729 = yrday
fracday
Element set: 916
Inclination: 51
6382 deg
RA of node: 336
3390 deg
Eccentricity:
0004944
Arg of perigee: 321
7154 deg
Mean anomaly: 38
3647 deg
Mean motion: 15
53171978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3353
Checksum: 325
Coasting Arc #18 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2019/029/08:59:00
000
Vector Time (MET): N/A
Weight (LBS) : 913933
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -914478
66 A = 6780614
68 meter
Y = -4247390
75 meter E =
0011339
Z = -5215137
31 I = 51
43666
XDOT = 7011
476078 Wp = 79
92519
YDOT = -2873
526272 meter/sec RA = 330
97857 deg
ZDOT = 1114
847045 TA = 200
78033
MA = 200
82646
Ha = 222
289 n
mi
Hp = 217
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3000258
08 X = -841583
27
Y = -13935009
03 feet Y = -4257209
39 meter
Z = -17110030
54 Z = -5219402
49
XDOT = 23003
530441 XDOT = 7037
672318
YDOT = -9427
579631 feet/sec YDOT = -2794
972610 meter/sec
ZDOT = 3657
634661 ZDOT = 1148
969283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14199072
00 X = 4327877
15
Y = -965912
05 feet Y = -294409
99 meter
Z = -17128705
10 Z = -5220829
32
XDOT = 6147
930116 XDOT = 1873
889099
YDOT = 23010
811451 feet/sec YDOT = 7013
695330 meter/sec
ZDOT = 3811
954469 ZDOT = 1161
883722
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 19029
38840601
00016717 00000-0 10270-3 0 9176
2 25544 51
6380 331
5353 0004968 325
4799 34
6030 15
53162305 33681
Satellite: ISS
Catalog Number: 25544
Epoch time: 19029
38840601 = yrday
fracday
Element set: 917
Inclination: 51
6380 deg
RA of node: 331
5353 deg
Eccentricity:
0004968
Arg of perigee: 325
4799 deg
Mean anomaly: 34
6030 deg
Mean motion: 15
53162305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 311
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