[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 25th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 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
361/03:07:48
737 -1
0 2
1 2
1
N/A -0
5 -0
2 221
5
000/00:05:37
474 1
8 -0
1 215
8
361/09:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 215
7
364/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 216
1
Coasting Arc #1 (Orbit 2810)
---------------------------------------
Vector Time (GMT): 2018/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6185269
46 A = 6787290
29 meter
Y = 1613573
54 meter E =
0013058
Z = 2271569
77 I = 51
84166
XDOT = 615
067674 Wp = 92
73576
YDOT = -5356
010883 meter/sec RA = 149
16502 deg
ZDOT = 5451
711931 TA = 292
46864
MA = 292
60686
Ha = 221
778 n
mi
Hp = 214
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20292878
79 X = -6213887
14
Y = 5293876
43 feet Y = 1544245
22 meter
Z = 7452656
71 Z = 2241454
94
XDOT = 2017
938562 XDOT = 648
433146
YDOT = -17572
214183 feet/sec YDOT = -5348
946975 meter/sec
ZDOT = 17886
193998 ZDOT = 5454
779969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6030760
89 X = -1838175
92
Y = -20136135
15 feet Y = -6137493
99 meter
Z = 7316702
37 Z = 2230130
88
XDOT = 16159
947409 XDOT = 4925
551970
YDOT = 1698
025042 feet/sec YDOT = 517
558033 meter/sec
ZDOT = 17900
576587 ZDOT = 5456
095744
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 18358
55987496
00016717 00000-0 10270-3 0 9005
2 25544 51
6371 149
9915 0004937 181
4299 178
6840 15
54105784 28116
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
55987496 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 149
9915 deg
Eccentricity:
0004937
Arg of perigee: 181
4299 deg
Mean anomaly: 178
6840 deg
Mean motion: 15
54105784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2811
Checksum: 355
Coasting Arc #2 (Orbit 2825)
---------------------------------------
Vector Time (GMT): 2018/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5666555
87 A = 6783750
60 meter
Y = -508675
53 meter E =
0006450
Z = -3695613
01 I = 51
85830
XDOT = -2304
349666 Wp = 127
13708
YDOT = 5874
439413 meter/sec RA = 144
20060 deg
ZDOT = -4350
895214 TA = 96
70055
MA = 96
62714
Ha = 221
756 n
mi
Hp = 214
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18591062
57 X = 5689773
94
Y = -1668882
99 feet Y = -445177
91 meter
Z = -12124714
61 Z = -3668030
94
XDOT = -7560
202317 XDOT = -2348
734006
YDOT = 19273
095186 feet/sec YDOT = 5848
422914 meter/sec
ZDOT = -14274
590597 ZDOT = -4362
195886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2667325
53 X = 813000
82
Y = 18555330
51 feet Y = 5655664
74 meter
Z = -12000273
60 Z = -3657683
39
XDOT = -18291
063578 XDOT = -5575
116179
YDOT = -6616
480782 feet/sec YDOT = -2016
703342 meter/sec
ZDOT = -14326
157595 ZDOT = -4366
612835
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 18359
52442964
00016717 00000-0 10270-3 0 9010
2 25544 51
6377 145
1837 0004787 183
6623 176
4495 15
54095812 28269
Satellite: ISS
Catalog Number: 25544
Epoch time: 18359
52442964 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 145
1837 deg
Eccentricity:
0004787
Arg of perigee: 183
6623 deg
Mean anomaly: 176
4495 deg
Mean motion: 15
54095812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2826
Checksum: 343
Coasting Arc #3 (Orbit 2841)
---------------------------------------
Vector Time (GMT): 2018/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4820336
25 A = 6780073
98 meter
Y = -725500
22 meter E =
0010588
Z = 4710788
12 I = 51
87264
XDOT = 3687
199179 Wp = 142
72213
YDOT = -6103
653155 meter/sec RA = 139
22785 deg
ZDOT = 2821
403185 TA = 279
33328
MA = 279
45299
Ha = 221
635 n
mi
Hp = 214
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15814751
48 X = -4834747
39
Y = -2380250
08 feet Y = -779485
58 meter
Z = 15455341
60 Z = 4687337
92
XDOT = 12097
110167 XDOT = 3741
473241
YDOT = -20025
108777 feet/sec YDOT = -6062
117119 meter/sec
ZDOT = 9256
572129 ZDOT = 2839
445294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1247413
80 X = 380211
73
Y = -16045929
05 feet Y = -4890799
17 meter
Z = 15349646
85 Z = 4678572
36
XDOT = 19655
341422 XDOT = 5990
948065
YDOT = 10497
788030 feet/sec YDOT = 3199
725791 meter/sec
ZDOT = 9338
578233 ZDOT = 2846
398645
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 18360
55328581
00016717 00000-0 10270-3 0 9024
2 25544 51
6378 140
0553 0004895 189
1810 170
9253 15
54118070 28429
Satellite: ISS
Catalog Number: 25544
Epoch time: 18360
55328581 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 140
0553 deg
Eccentricity:
0004895
Arg of perigee: 189
1810 deg
Mean anomaly: 170
9253 deg
Mean motion: 15
54118070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2842
Checksum: 307
Coasting Arc #4 (Orbit 2851)
---------------------------------------
Vector Time (GMT): 2018/361/03:10:37
474
Vector Time (MET): N/A
Weight (LBS) : 949512
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5004138
01 A = 6790586
04 meter
Y = 4578680
64 meter E =
0009921
Z = 222070
66 I = 51
92161
XDOT = -3043
368053 Wp = 53
85263
YDOT = -3627
398387 meter/sec RA = 136
07224 deg
ZDOT = 6029
225535 TA = 308
52987
MA = 308
61876
Ha = 221
514 n
mi
Hp = 215
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16417775
63 X = -5056044
87
Y = 15021918
10 feet Y = 4522430
64 meter
Z = 728578
29 Z = 197636
95
XDOT = -9984
803325 XDOT = -3031
865609
YDOT = -11900
913342 feet/sec YDOT = -3661
367582 meter/sec
ZDOT = 19780
923670 ZDOT = 6014
469808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22178897
17 X = 6760127
86
Y = -1856592
91 feet Y = -565889
52 meter
Z = 617891
03 Z = 188333
19
XDOT = 601
768699 XDOT = 183
419100
YDOT = 13983
927271 feet/sec YDOT = 4262
301032 meter/sec
ZDOT = 19714
739531 ZDOT = 6009
052609
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 18361
19633867
00016717 00000-0 10270-3 0 9032
2 25544 51
6400 136
8548 0002802 205
1293 154
9724 15
53690997 28520
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
19633867 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 136
8548 deg
Eccentricity:
0002802
Arg of perigee: 205
1293 deg
Mean anomaly: 154
9724 deg
Mean motion: 15
53690997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 326
Coasting Arc #5 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/361/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949512
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -945153
18 A = 6783767
89 meter
Y = 5402469
69 meter E =
0007311
Z = -4000851
46 I = 51
90197
XDOT = -6264
694282 Wp = 132
87349
YDOT = 1862
435637 meter/sec RA = 134
80935 deg
ZDOT = 3994
634695 TA = 178
63286
MA = 178
63086
Ha = 221
537 n
mi
Hp = 215
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3100896
26 X = -986061
14
Y = 17724638
10 feet Y = 5391671
88 meter
Z = -13126153
09 Z = -4005541
60
XDOT = -20553
458930 XDOT = -6304
458485
YDOT = 6110
353141 feet/sec YDOT = 1792
156855 meter/sec
ZDOT = 13105
756872 ZDOT = 3964
107000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12093529
95 X = -3686107
93
Y = -13302417
82 feet Y = -4054576
95 meter
Z = -13147869
10 Z = -4007470
50
XDOT = 6948
490156 XDOT = 2117
899800
YDOT = -19134
960935 feet/sec YDOT = -5832
336093 meter/sec
ZDOT = 12967
858068 ZDOT = 3952
603139
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 18361
38929630
00016717 00000-0 10270-3 0 9040
2 25544 51
6369 135
8898 0003093 203
5392 156
5619 15
53703841 28553
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
38929630 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 135
8898 deg
Eccentricity:
0003093
Arg of perigee: 203
5392 deg
Mean anomaly: 156
5619 deg
Mean motion: 15
53703841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 337
Coasting Arc #6 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2018/362/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949512
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2036516
18 A = 6787211
10 meter
Y = -5838640
77 meter E =
0012652
Z = 2780981
38 I = 51
93660
XDOT = 5661
925505 Wp = 113
40527
YDOT = -486
141912 meter/sec RA = 129
84902 deg
ZDOT = -5153
259281 TA = 35
19842
MA = 35
11492
Ha = 221
362 n
mi
Hp = 215
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6681483
53 X = 2088145
77
Y = -19155645
57 feet Y = -5815578
50 meter
Z = 9123954
67 Z = 2790999
03
XDOT = 18575
871078 XDOT = 5691
972376
YDOT = -1594
953780 feet/sec YDOT = -422
658042 meter/sec
ZDOT = -16907
018640 ZDOT = -5125
683004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11286834
81 X = 3440227
25
Y = 16833016
45 feet Y = 5130703
42 meter
Z = 9169757
11 Z = 2794941
97
XDOT = -8769
839998 XDOT = -2673
047232
YDOT = 15046
835994 feet/sec YDOT = 4586
275611 meter/sec
ZDOT = -16782
563205 ZDOT = -5115
325265
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 18362
41840982
00016717 00000-0 10270-3 0 9058
2 25544 51
6373 130
7626 0003026 211
1603 148
9370 15
53718334 28717
Satellite: ISS
Catalog Number: 25544
Epoch time: 18362
41840982 = yrday
fracday
Element set: 905
Inclination: 51
6373 deg
RA of node: 130
7626 deg
Eccentricity:
0003026
Arg of perigee: 211
1603 deg
Mean anomaly: 148
9370 deg
Mean motion: 15
53718334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 299
Coasting Arc #7 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2018/363/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949512
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2899737
39 A = 6789773
43 meter
Y = 5989068
65 meter E =
0005734
Z = -1339841
73 I = 51
96512
XDOT = -4846
858272 Wp = 42
98296
YDOT = -1043
345055 meter/sec RA = 124
89754 deg
ZDOT = 5844
796148 TA = 302
50314
MA = 302
55855
Ha = 221
437 n
mi
Hp = 215
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9513574
12 X = -2959985
14
Y = 19649175
36 feet Y = 5956304
97 meter
Z = -4395806
21 Z = -1354073
56
XDOT = -15901
765985 XDOT = -4863
221749
YDOT = -3423
048081 feet/sec YDOT = -1097
637777 meter/sec
ZDOT = 19175
840379 ZDOT = 5821
212206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10286310
03 X = -3135267
30
Y = -19240990
90 feet Y = -5864654
03 meter
Z = -4460649
32 Z = -1359605
91
XDOT = 10807
050952 XDOT = 3293
989130
YDOT = -10184
325849 feet/sec YDOT = -3104
182519 meter/sec
ZDOT = 19069
547774 ZDOT = 5812
398162
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 18363
38320512
00016717 00000-0 10270-3 0 9068
2 25544 51
6369 125
9558 0003038 208
1242 151
9746 15
53704622 28862
Satellite: ISS
Catalog Number: 25544
Epoch time: 18363
38320512 = yrday
fracday
Element set: 906
Inclination: 51
6369 deg
RA of node: 125
9558 deg
Eccentricity:
0003038
Arg of perigee: 208
1242 deg
Mean anomaly: 151
9746 deg
Mean motion: 15
53704622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 314
Coasting Arc #8 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2018/364/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 949512
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3550582
22 A = 6790423
55 meter
Y = -5774531
19 meter E =
0012505
Z = -247266
00 I = 51
98562
XDOT = 3913
753774 Wp = 149
79933
YDOT = 2658
817750 meter/sec RA = 119
95217 deg
ZDOT = -6036
318431 TA = 32
85256
MA = 32
77489
Ha = 221
260 n
mi
Hp = 215
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11648891
79 X = 3616091
84
Y = -18945312
32 feet Y = -5734459
81 meter
Z = -811240
16 Z = -229859
80
XDOT = 12840
399521 XDOT = 3913
052333
YDOT = 8723
155348 feet/sec YDOT = 2702
580473 meter/sec
ZDOT = -19804
194326 ZDOT = -6017
308439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8791962
68 X = 2679790
23
Y = 20431473
23 feet Y = 6227513
04 meter
Z = -732081
45 Z = -223138
42
XDOT = -13106
825556 XDOT = -3994
960429
YDOT = 4952
090358 feet/sec YDOT = 1509
397141 meter/sec
ZDOT = -19718
706981 ZDOT = -6010
261888
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 18364
41231636
00016717 00000-0 10270-3 0 9072
2 25544 51
6368 120
8287 0002903 216
1454 143
9503 15
53745379 29023
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
41231636 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 120
8287 deg
Eccentricity:
0002903
Arg of perigee: 216
1454 deg
Mean anomaly: 143
9503 deg
Mean motion: 15
53745379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 309
Coasting Arc #9 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2018/364/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949512
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4931160
36 A = 6783934
59 meter
Y = -2405474
90 meter E =
0004710
Z = -3993261
48 I = 51
96934
XDOT = -62
558945 Wp = 99
77087
YDOT = 6527
323496 meter/sec RA = 119
29740 deg
ZDOT = -4014
001599 TA = 128
56735
MA = 128
52514
Ha = 221
424 n
mi
Hp = 216
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16178347
65 X = 4977089
62
Y = -7891978
01 feet Y = -2350074
20 meter
Z = -13101251
59 Z = -3969196
32
XDOT = -205
245881 XDOT = -116
046860
YDOT = 21415
103332 feet/sec YDOT = 6526
325071 meter/sec
ZDOT = -13169
296585 ZDOT = -4014
435038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11657503
81 X = 3553207
16
Y = 13819007
64 feet Y = 4212033
53 meter
Z = -12992408
38 Z = -3960086
08
XDOT = -19775
067445 XDOT = -6027
440557
YDOT = 4312
805173 feet/sec YDOT = 1314
543017 meter/sec
ZDOT = -13171
956682 ZDOT = -4014
812397
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 18364
54095647
00016717 00000-0 10270-3 0 9087
2 25544 51
6404 120
1885 0003281 213
4262 146
6684 15
53699014 29044
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
54095647 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 120
1885 deg
Eccentricity:
0003281
Arg of perigee: 213
4262 deg
Mean anomaly: 146
6684 deg
Mean motion: 15
53699014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 315
Coasting Arc #10 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2018/365/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 949512
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4625476
04 A = 6780612
85 meter
Y = 1024804
28 meter E =
0007465
Z = 4849578
37 I = 51
97484
XDOT = 1070
166120 Wp = 144
32187
YDOT = -7160
716558 meter/sec RA = 114
33262 deg
ZDOT = 2526
046393 TA = 280
91648
MA = 281
00046
Ha = 221
313 n
mi
Hp = 215
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15175446
34 X = -4660148
53
Y = 3362218
77 feet Y = 972884
79 meter
Z = 15910690
19 Z = 4827025
35
XDOT = 3511
043702 XDOT = 1137
889568
YDOT = -23493
164561 feet/sec YDOT = -7148
370723 meter/sec
ZDOT = 8287
553784 ZDOT = 2531
408870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7264579
01 X = -2214243
68
Y = -13858434
59 feet Y = -4224050
86 meter
Z = 15808808
66 Z = 4818524
88
XDOT = 22563
651895 XDOT = 6877
401098
YDOT = -2315
843121 feet/sec YDOT = -705
868983 meter/sec
ZDOT = 8312
540240 ZDOT = 2533
662265
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 18365
57006513
00016717 00000-0 10270-3 0 9096
2 25544 51
6413 115
0614 0003150 218
1673 141
9257 15
53739680 29206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18365
57006513 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 115
0614 deg
Eccentricity:
0003150
Arg of perigee: 218
1673 deg
Mean anomaly: 141
9257 deg
Mean motion: 15
53739680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 296
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