[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 30th 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 2841)
---------------------------------------
Vector Time (GMT): 2018/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4820178
16 A = 6780073
13 meter
Y = -725722
76 meter E =
0010565
Z = 4710902
23 I = 51
87280
XDOT = 3687
429654 Wp = 142
63527
YDOT = -6103
624536 meter/sec RA = 139
22780 deg
ZDOT = 2821
191153 TA = 279
42267
MA = 279
54209
Ha = 221
627 n
mi
Hp = 214
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15814232
80 X = -4834587
38
Y = -2380980
18 feet Y = -779706
33 meter
Z = 15455715
99 Z = 4687452
80
XDOT = 12097
866319 XDOT = 3741
704409
YDOT = -20025
014881 feet/sec YDOT = -6062
085918 meter/sec
ZDOT = 9255
876487 ZDOT = 2839
234384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1248178
55 X = 380444
82
Y = -16045465
81 feet Y = -4890657
98 meter
Z = 15350024
75 Z = 4678687
54
XDOT = 19655
335396 XDOT = 5990
946229
YDOT = 10498
497773 feet/sec YDOT = 3199
942121 meter/sec
ZDOT = 9337
887645 ZDOT = 2846
188154
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
55328541
00016717 00000-0 10270-3 0 9008
2 25544 51
6379 140
0552 0004867 189
2410 170
8654 15
54118191 28423
Satellite: ISS
Catalog Number: 25544
Epoch time: 18360
55328541 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 140
0552 deg
Eccentricity:
0004867
Arg of perigee: 189
2410 deg
Mean anomaly: 170
8654 deg
Mean motion: 15
54118191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2842
Checksum: 305
Coasting Arc #2 (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 = -5004240
89 A = 6790585
46 meter
Y = 4578526
78 meter E =
0009938
Z = 222311
06 I = 51
92177
XDOT = -3043
113163 Wp = 53
72553
YDOT = -3627
627472 meter/sec RA = 136
07219 deg
ZDOT = 6029
244754 TA = 308
65955
MA = 308
74844
Ha = 221
509 n
mi
Hp = 215
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16418113
15 X = -5056147
19
Y = 15021413
33 feet Y = 4522275
64 meter
Z = 729367
00 Z = 197876
85
XDOT = -9983
967071 XDOT = -3031
608269
YDOT = -11901
664936 feet/sec YDOT = -3661
593803 meter/sec
ZDOT = 19780
986727 ZDOT = 6014
490272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22178860
11 X = 6760116
56
Y = -1855983
93 feet Y = -565703
90 meter
Z = 618677
52 Z = 188572
91
XDOT = 600
692225 XDOT = 183
090990
YDOT = 13984
014209 feet/sec YDOT = 4262
327531 meter/sec
ZDOT = 19714
808223 ZDOT = 6009
073546
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
19633821
00016717 00000-0 10270-3 0 9010
2 25544 51
6401 136
8548 0002776 205
3658 154
7359 15
53691193 28529
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
19633821 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 136
8548 deg
Eccentricity:
0002776
Arg of perigee: 205
3658 deg
Mean anomaly: 154
7359 deg
Mean motion: 15
53691193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2852
Checksum: 323
Coasting Arc #3 (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 = -945398
63 A = 6783767
67 meter
Y = 5402524
49 meter E =
0007292
Z = -4000697
67 I = 51
90213
XDOT = -6264
647599 Wp = 132
70403
YDOT = 1862
171058 meter/sec RA = 134
80931 deg
ZDOT = 3994
858843 TA = 178
80483
MA = 178
80309
Ha = 221
531 n
mi
Hp = 215
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3101701
53 X = -986307
93
Y = 17724817
87 feet Y = 5391723
92 meter
Z = -13125648
51 Z = -4005389
00
XDOT = -20553
305770 XDOT = -6304
409935
YDOT = 6109
485099 feet/sec YDOT = 1791
892808 meter/sec
ZDOT = 13106
492266 ZDOT = 3964
331380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12093172
81 X = -3685999
07
Y = -13303165
24 feet Y = -4054804
76 meter
Z = -13147369
92 Z = -4007318
35
XDOT = 6949
027494 XDOT = 2118
063580
YDOT = -19134
334978 feet/sec YDOT = -5832
145301 meter/sec
ZDOT = 12968
594532 ZDOT = 3952
827613
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
38929581
00016717 00000-0 10270-3 0 9023
2 25544 51
6370 135
8898 0003066 203
7339 156
3672 15
53704080 28551
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
38929581 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 135
8898 deg
Eccentricity:
0003066
Arg of perigee: 203
7339 deg
Mean anomaly: 156
3672 deg
Mean motion: 15
53704080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 328
Coasting Arc #4 (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 = 2036874
96 A = 6787210
73 meter
Y = -5838679
10 meter E =
0012644
Z = 2780673
93 I = 51
93676
XDOT = 5661
744397 Wp = 113
28585
YDOT = -485
701008 meter/sec RA = 129
84899 deg
ZDOT = -5153
474817 TA = 35
32186
MA = 35
23815
Ha = 221
357 n
mi
Hp = 215
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6682660
64 X = 2088506
45
Y = -19155771
32 feet Y = -5815612
81 meter
Z = 9122945
96 Z = 2790693
33
XDOT = 18575
276893 XDOT = 5691
787398
YDOT = -1593
507245 feet/sec YDOT = -422
219185 meter/sec
ZDOT = -16907
725779 ZDOT = -5125
899429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11286221
24 X = 3440040
24
Y = 16834036
64 feet Y = 5131014
37 meter
Z = 9168756
28 Z = 2794636
91
XDOT = -8770
563945 XDOT = -2673
267890
YDOT = 15045
538194 feet/sec YDOT = 4585
880042 meter/sec
ZDOT = -16783
274401 ZDOT = -5115
542037
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
41840914
00016717 00000-0 10270-3 0 9031
2 25544 51
6374 130
7626 0003001 211
3946 148
7028 15
53718716 28715
Satellite: ISS
Catalog Number: 25544
Epoch time: 18362
41840914 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 130
7626 deg
Eccentricity:
0003001
Arg of perigee: 211
3946 deg
Mean anomaly: 148
7028 deg
Mean motion: 15
53718716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 300
Coasting Arc #5 (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 = -2900120
15 A = 6789772
54 meter
Y = 5988966
20 meter E =
0005760
Z = -1339372
03 I = 51
96528
XDOT = -4846
557617 Wp = 42
82526
YDOT = -1043
958931 meter/sec RA = 124
89753 deg
ZDOT = 5844
964165 TA = 302
66604
MA = 302
72159
Ha = 221
432 n
mi
Hp = 215
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9514829
88 X = -2960369
00
Y = 19648839
23 feet Y = 5956198
23 meter
Z = -4394265
17 Z = -1353605
72
XDOT = -15900
779582 XDOT = -4862
915067
YDOT = -3425
062108 feet/sec YDOT = -1098
248257 meter/sec
ZDOT = 19176
391618 ZDOT = 5821
381699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10285292
53 X = -3134957
16
Y = -19241815
75 feet Y = -5864905
44 meter
Z = -4459116
67 Z = -1359138
76
XDOT = 10808
038893 XDOT = 3294
290255
YDOT = -10182
419302 feet/sec YDOT = -3103
601403 meter/sec
ZDOT = 19070
105732 ZDOT = 5812
568227
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
38320417
00016717 00000-0 10270-3 0 9040
2 25544 51
6371 125
9558 0003011 208
3003 151
7986 15
53705113 28863
Satellite: ISS
Catalog Number: 25544
Epoch time: 18363
38320417 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 125
9558 deg
Eccentricity:
0003011
Arg of perigee: 208
3003 deg
Mean anomaly: 151
7986 deg
Mean motion: 15
53705113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 297
Coasting Arc #6 (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 = 3551037
25 A = 6790421
52 meter
Y = -5774243
13 meter E =
0012483
Z = -247954
75 I = 51
98578
XDOT = 3913
213193 Wp = 149
71359
YDOT = 2659
640173 meter/sec RA = 119
95218 deg
ZDOT = -6036
279147 TA = 32
94567
MA = 32
86794
Ha = 221
255 n
mi
Hp = 215
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11650384
68 X = 3616546
96
Y = -18944367
23 feet Y = -5734166
66 meter
Z = -813499
84 Z = -230546
34
XDOT = 12838
625961 XDOT = 3912
502404
YDOT = 8725
853585 feet/sec YDOT = 2703
396798 meter/sec
ZDOT = -19804
065443 ZDOT = -6017
271805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8790322
29 X = 2679290
23
Y = 20432163
04 feet Y = 6227723
30 meter
Z = -734331
18 Z = -223824
14
XDOT = -13107
961509 XDOT = -3995
306668
YDOT = 4949
206353 feet/sec YDOT = 1508
518097 meter/sec
ZDOT = -19718
590136 ZDOT = -6010
226273
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
41231505
00016717 00000-0 10270-3 0 9055
2 25544 51
6369 120
8287 0002876 216
3698 143
7259 15
53746021 29026
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
41231505 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 120
8287 deg
Eccentricity:
0002876
Arg of perigee: 216
3698 deg
Mean anomaly: 143
7259 deg
Mean motion: 15
53746021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 315
Coasting Arc #7 (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 = 4931154
28 A = 6783931
14 meter
Y = -2404735
42 meter E =
0004714
Z = -3993739
38 I = 51
96949
XDOT = -63
299982 Wp = 99
39663
YDOT = 6527
659506 meter/sec RA = 119
29740 deg
ZDOT = -4013
408043 TA = 128
94903
MA = 128
90701
Ha = 221
418 n
mi
Hp = 216
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16178327
69 X = 4977077
59
Y = -7889551
91 feet Y = -2349334
83 meter
Z = -13102819
48 Z = -3969674
26
XDOT = -207
677106 XDOT = -116
794483
YDOT = 21416
205727 feet/sec YDOT = 6526
652757 meter/sec
ZDOT = -13167
349222 ZDOT = -4013
845097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11655150
29 X = 3552489
81
Y = 13819596
21 feet Y = 4212212
93 meter
Z = -12993976
56 Z = -3960564
06
XDOT = -19776
695331 XDOT = -6027
936737
YDOT = 4310
879665 feet/sec YDOT = 1313
956122 meter/sec
ZDOT = -13170
025669 ZDOT = -4014
223824
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
54095511
00016717 00000-0 10270-3 0 9065
2 25544 51
6405 120
1886 0003254 213
5985 146
4962 15
53699662 29045
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
54095511 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 120
1886 deg
Eccentricity:
0003254
Arg of perigee: 213
5985 deg
Mean anomaly: 146
4962 deg
Mean motion: 15
53699662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 324
Coasting Arc #8 (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 = -4625281
24 A = 6780608
81 meter
Y = 1023653
72 meter E =
0007446
Z = 4849983
96 I = 51
97500
XDOT = 1071
115999 Wp = 144
15828
YDOT = -7160
936350 meter/sec RA = 114
33263 deg
ZDOT = 2525
070578 TA = 281
09050
MA = 281
17422
Ha = 221
309 n
mi
Hp = 215
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15174807
20 X = -4659942
84
Y = 3358443
97 feet Y = 971736
47 meter
Z = 15912020
86 Z = 4827431
91
XDOT = 3514
160102 XDOT = 1138
846574
YDOT = -23493
885662 feet/sec YDOT = -7148
579853 meter/sec
ZDOT = 8284
352291 ZDOT = 2530
437686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7260771
46 X = -2213083
14
Y = -13858819
46 feet Y = -4224168
17 meter
Z = 15810143
85 Z = 4818931
84
XDOT = 22565
145113 XDOT = 6877
856230
YDOT = -2313
283314 feet/sec YDOT = -705
088754 meter/sec
ZDOT = 8309
359670 ZDOT = 2532
692828
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
57006331
00016717 00000-0 10270-3 0 9072
2 25544 51
6414 115
0614 0003123 218
3557 141
7374 15
53740471 29208
Satellite: ISS
Catalog Number: 25544
Epoch time: 18365
57006331 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 115
0614 deg
Eccentricity:
0003123
Arg of perigee: 218
3557 deg
Mean anomaly: 141
7374 deg
Mean motion: 15
53740471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 284
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