[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 26th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
362/01:03:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 215
5
364/11:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
3
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2017/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5440335
40 A = 6783117
47 meter
Y = 1488395
07 meter E =
0003740
Z = -3772523
07 I = 51
73937
XDOT = -4247
253081 Wp = 55
83719
YDOT = 4756
583101 meter/sec RA = 163
46520 deg
ZDOT = -4249
261983 TA = 169
23898
MA = 169
23098
Ha = 219
942 n
mi
Hp = 215
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17848869
42 X = 5441612
38
Y = 4883185
91 feet Y = 1549239
95 meter
Z = -12377044
20 Z = -3746092
60
XDOT = -13934
557354 XDOT = -4279
486112
YDOT = 15605
587601 feet/sec YDOT = 4708
907397 meter/sec
ZDOT = -13941
148237 ZDOT = -4269
971742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3835130
43 X = -1168947
75
Y = 18182681
65 feet Y = 5542081
37 meter
Z = -12259719
82 Z = -3736762
60
XDOT = -15054
276221 XDOT = -4588
543392
YDOT = -12635
512304 feet/sec YDOT = -3851
304150 meter/sec
ZDOT = -14033
883830 ZDOT = -4277
527791
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 17359
52420138
00016717 00000-0 10270-3 0 9007
2 25544 51
6374 164
4767 0002775 289
5398 70
5454 15
54229921 11500
Satellite: ISS
Catalog Number: 25544
Epoch time: 17359
52420138 = yrday
fracday
Element set: 900
Inclination: 51
6374 deg
RA of node: 164
4767 deg
Eccentricity:
0002775
Arg of perigee: 289
5398 deg
Mean anomaly: 70
5454 deg
Mean motion: 15
54229921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1150
Checksum: 321
Coasting Arc #2 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2017/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157405
08 A = 6779463
31 meter
Y = -2410103
04 meter E =
0004829
Z = 4779706
24 I = 51
75720
XDOT = 5642
007673 Wp = 122
82110
YDOT = -4469
086425 meter/sec RA = 158
48182 deg
ZDOT = 2649
462697 TA = 301
06183
MA = 301
10922
Ha = 220
047 n
mi
Hp = 215
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13639780
45 X = -4153363
06
Y = -7907162
22 feet Y = -2456571
61 meter
Z = 15681450
93 Z = 4759520
64
XDOT = 18510
523861 XDOT = 5678
693131
YDOT = -14662
357039 feet/sec YDOT = -4405
788635 meter/sec
ZDOT = 8692
462917 ZDOT = 2676
958622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6851418
35 X = 2088312
31
Y = -14297621
50 feet Y = -4357915
03 meter
Z = 15592011
24 Z = 4752445
03
XDOT = 14963
437434 XDOT = 4560
855730
YDOT = 16800
083405 feet/sec YDOT = 5120
665422 meter/sec
ZDOT = 8815
350783 ZDOT = 2686
918919
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 17360
55297841
00016717 00000-0 10270-3 0 9016
2 25544 51
6363 159
3468 0002849 290
5676 69
5171 15
54224358 11662
Satellite: ISS
Catalog Number: 25544
Epoch time: 17360
55297841 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 159
3468 deg
Eccentricity:
0002849
Arg of perigee: 290
5676 deg
Mean anomaly: 69
5171 deg
Mean motion: 15
54224358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1166
Checksum: 332
Coasting Arc #3 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2017/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939513
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2621756
80 A = 6777277
65 meter
Y = 3346437
68 meter E =
0012299
Z = -5288843
88 I = 51
78097
XDOT = -6534
744758 Wp = 77
85573
YDOT = 3923
841002 meter/sec RA = 153
49393 deg
ZDOT = -755
576692 TA = 184
92532
MA = 184
93743
Ha = 220
013 n
mi
Hp = 215
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8601564
32 X = 2609831
77
Y = 10979126
24 feet Y = 3375689
54 meter
Z = -17351850
00 Z = -5276137
01
XDOT = -21439
451307 XDOT = -6574
466310
YDOT = 12873
494101 feet/sec YDOT = 3850
542955 meter/sec
ZDOT = -2478
926155 ZDOT = -787
416716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10126903
60 X = -3086680
22
Y = 9691035
62 feet Y = 2953827
66 meter
Z = -17295793
48 Z = -5271757
85
XDOT = -14087
791502 XDOT = -4293
958850
YDOT = -19405
405035 feet/sec YDOT = -5914
767455 meter/sec
ZDOT = -2621
077625 ZDOT = -798
904460
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 17361
51745567
00016717 00000-0 10270-3 0 9027
2 25544 51
6371 154
5395 0002696 294
4564 65
6307 15
54228444 11811
Satellite: ISS
Catalog Number: 25544
Epoch time: 17361
51745567 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 154
5395 deg
Eccentricity:
0002696
Arg of perigee: 294
4564 deg
Mean anomaly: 65
6307 deg
Mean motion: 15
54228444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1181
Checksum: 322
Coasting Arc #4 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2017/362/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4019730
50 A = 6778564
49 meter
Y = -2238983
54 meter E =
0003213
Z = 4976028
41 I = 51
80204
XDOT = 5431
200615 Wp = 124
44762
YDOT = -4971
268821 meter/sec RA = 150
80145 deg
ZDOT = 2147
825245 TA = 304
66169
MA = 304
69197
Ha = 220
086 n
mi
Hp = 215
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13188092
20 X = -4018565
95
Y = -7345746
53 feet Y = -2283928
68 meter
Z = 16325552
54 Z = 4956504
50
XDOT = 17818
899657 XDOT = 5475
953936
YDOT = -16309
937078 feet/sec YDOT = -4910
283307 meter/sec
ZDOT = 7046
670752 ZDOT = 2174
316775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1906980
57 X = -581247
68
Y = 15068745
01 feet Y = 4592953
48 meter
Z = 16239020
37 Z = 4949653
41
XDOT = -20626
601829 XDOT = -6286
988237
YDOT = -10341
803439 feet/sec YDOT = -3152
181688 meter/sec
ZDOT = 7165
188111 ZDOT = 2183
949336
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 17362
09613891
00016717 00000-0 10270-3 0 9036
2 25544 51
6378 151
6575 0003152 301
0836 59
0007 15
54253584 11908
Satellite: ISS
Catalog Number: 25544
Epoch time: 17362
09613891 = yrday
fracday
Element set: 903
Inclination: 51
6378 deg
RA of node: 151
6575 deg
Eccentricity:
0003152
Arg of perigee: 301
0836 deg
Mean anomaly: 59
0007 deg
Mean motion: 15
54253584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 298
Coasting Arc #5 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2017/363/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550490
28 A = 6777113
84 meter
Y = 3334389
87 meter E =
0012596
Z = -5331093
02 I = 51
82531
XDOT = -6240
180610 Wp = 79
30156
YDOT = 4436
904022 meter/sec RA = 145
81276 deg
ZDOT = -208
443803 TA = 188
70370
MA = 188
72556
Ha = 220
158 n
mi
Hp = 215
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8367750
28 X = 2538910
57
Y = 10939599
32 feet Y = 3362846
83 meter
Z = -17490462
67 Z = -5318731
39
XDOT = -20473
033498 XDOT = -6288
318961
YDOT = 14556
771725 feet/sec YDOT = 4366
852910 meter/sec
ZDOT = -683
870745 ZDOT = -238
873333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6819506
38 X = 2078585
55
Y = -12045446
97 feet Y = -3671452
24 meter
Z = -17435937
10 Z = -5314473
63
XDOT = 20447
077866 XDOT = 6232
269334
YDOT = 12771
684626 feet/sec YDOT = 3892
809474 meter/sec
ZDOT = -819
853037 ZDOT = -249
891206
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 17363
06061173
00016717 00000-0 10270-3 0 9045
2 25544 51
6381 146
8478 0003132 307
8657 52
2212 15
54219045 12057
Satellite: ISS
Catalog Number: 25544
Epoch time: 17363
06061173 = yrday
fracday
Element set: 904
Inclination: 51
6381 deg
RA of node: 146
8478 deg
Eccentricity:
0003132
Arg of perigee: 307
8657 deg
Mean anomaly: 52
2212 deg
Mean motion: 15
54219045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 286
Coasting Arc #6 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2017/364/01:03:30
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -993895
80 A = 6778055
94 meter
Y = -4354578
98 meter E =
0005511
Z = 5097806
20 I = 51
85503
XDOT = 6559
420453 Wp = 21
74434
YDOT = -3562
763811 meter/sec RA = 140
82684 deg
ZDOT = -1758
876332 TA = 85
24251
MA = 85
17958
Ha = 220
281 n
mi
Hp = 215
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3260812
99 X = -969890
54
Y = -14286676
44 feet Y = -4365559
66 meter
Z = 16725085
95 Z = 5093036
05
XDOT = 21520
408309 XDOT = 6607
316497
YDOT = -11688
857646 feet/sec YDOT = -3489
143917 meter/sec
ZDOT = -5770
591639 ZDOT = -1726
896645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11729400
36 X = -3575121
23
Y = 8823384
72 feet Y = 2689367
66 meter
Z = 16704477
67 Z = 5091524
79
XDOT = -18718
710232 XDOT = -5705
462879
YDOT = -14194
365996 feet/sec YDOT = -4326
442756 meter/sec
ZDOT = -5627
810544 ZDOT = -1715
356654
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 17364
08937929
00016717 00000-0 10270-3 0 9050
2 25544 51
6379 141
7192 0003129 313
6164 46
4729 15
54221406 12215
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
08937929 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 141
7192 deg
Eccentricity:
0003129
Arg of perigee: 313
6164 deg
Mean anomaly: 46
4729 deg
Mean motion: 15
54221406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 309
Coasting Arc #7 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3513099
18 A = 6777334
39 meter
Y = -2416651
40 meter E =
0000729
Z = 5267244
61 I = 51
86357
XDOT = 5207
692274 Wp = 100
39697
YDOT = -5553
943097 meter/sec RA = 138
63054 deg
ZDOT = 924
951822 TA = 340
78170
MA = 340
78445
Ha = 220
260 n
mi
Hp = 215
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11525915
94 X = -3511400
14
Y = -7928646
34 feet Y = -2455928
33 meter
Z = 17280986
25 Z = 5250182
92
XDOT = 17085
604575 XDOT = 5264
917948
YDOT = -18221
598086 feet/sec YDOT = -5495
387247 meter/sec
ZDOT = 3034
618839 ZDOT = 950
387614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6991823
63 X = 2131107
84
Y = -12224185
15 feet Y = -3725931
63 meter
Z = 17205416
49 Z = 5244210
95
XDOT = 18609
748485 XDOT = 5672
251338
YDOT = 15076
842157 feet/sec YDOT = 4595
421489 meter/sec
ZDOT = 3148
578362 ZDOT = 959
686685
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 17364
53946392
00016717 00000-0 10270-3 0 9065
2 25544 51
6375 139
4706 0002864 307
1921 52
8970 15
54237784 12282
Satellite: ISS
Catalog Number: 25544
Epoch time: 17364
53946392 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 139
4706 deg
Eccentricity:
0002864
Arg of perigee: 307
1921 deg
Mean anomaly: 52
8970 deg
Mean motion: 15
54237784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1228
Checksum: 331
Coasting Arc #8 (Orbit 1242)
---------------------------------------
Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 925079
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2164560
03 A = 6777343
00 meter
Y = 3704715
65 meter E =
0012096
Z = -5256603
52 I = 51
88905
XDOT = -5804
207223 Wp = 90
82119
YDOT = 4885
800783 meter/sec RA = 133
64670 deg
ZDOT = 1055
257013 TA = 189
25160
MA = 189
27391
Ha = 220
218 n
mi
Hp = 215
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7101574
90 X = 2148505
94
Y = 12154578
92 feet Y = 3728832
13 meter
Z = -17246074
53 Z = -5246127
33
XDOT = -19042
674616 XDOT = -5863
536084
YDOT = 16029
530129 feet/sec YDOT = 4820
562312 meter/sec
ZDOT = 3462
129309 ZDOT = 1026
918565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11409301
78 X = -3477555
18
Y = 8341551
53 feet Y = 2542504
91 meter
Z = -17199988
15 Z = -5242556
39
XDOT = -17167
381561 XDOT = -5232
617900
YDOT = -16616
724591 feet/sec YDOT = -5064
777655 meter/sec
ZDOT = 3335
322290 ZDOT = 1016
606234
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 17365
50392964
00016717 00000-0 10270-3 0 9074
2 25544 51
6389 134
6628 0002806 311
2416 48
8495 15
54250141 12434
Satellite: ISS
Catalog Number: 25544
Epoch time: 17365
50392964 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 134
6628 deg
Eccentricity:
0002806
Arg of perigee: 311
2416 deg
Mean anomaly: 48
8495 deg
Mean motion: 15
54250141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1243
Checksum: 312
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