[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 16th 2018
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) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
105/08:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 214
6
108/10:36:05
758 0
2 0
9 0
9
N/A -0
8 -0
1 220
9
000/00:02:11
515 -0
3 -0
0 214
8
117/05:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 214
3
Coasting Arc #1 (Orbit 2845)
---------------------------------------
Vector Time (GMT): 2018/103/13:18:14
956
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5139877
51 A = 6781692
30 meter
Y = -1641423
19 meter E =
0007898
Z = -4117206
54 I = 51
51305
XDOT = 4578
753284 Wp = 52
22275
YDOT = -4832
983741 meter/sec RA = 340
36063 deg
ZDOT = -3789
529699 TA = 178
58181
MA = 178
57957
Ha = 220
667 n
mi
Hp = 214
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16863115
19 X = -5101141
33
Y = -5385246
70 feet Y = -1698684
67 meter
Z = -13507895
47 Z = -4142080
17
XDOT = 15022
156443 XDOT = 4650
864363
YDOT = -15856
245870 feet/sec YDOT = -4781
378148 meter/sec
ZDOT = -12432
840219 ZDOT = -3767
111957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16268295
66 X = -4958576
52
Y = 6760576
94 feet Y = 2060623
85 meter
Z = -13618587
72 Z = -4150945
54
XDOT = 1729
685682 XDOT = 527
208196
YDOT = -20678
079577 feet/sec YDOT = -6302
678655 meter/sec
ZDOT = -12332
096158 ZDOT = -3758
822909
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 18103
57735587
00016717 00000-0 10270-3 0 9007
2 25544 51
6413 340
8119 0002435 337
4166 22
6879 15
54246025 28460
Satellite: ISS
Catalog Number: 25544
Epoch time: 18103
57735587 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 340
8119 deg
Eccentricity:
0002435
Arg of perigee: 337
4166 deg
Mean anomaly: 22
6879 deg
Mean motion: 15
54246025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2846
Checksum: 311
Coasting Arc #2 (Orbit 2861)
---------------------------------------
Vector Time (GMT): 2018/104/13:18:14
956
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3778562
30 A = 6778432
50 meter
Y = 2624633
94 meter E =
0004506
Z = 4974532
15 I = 51
47039
XDOT = -5856
547128 Wp = 102
24673
YDOT = 4501
139016 meter/sec RA = 335
35681 deg
ZDOT = 2071
134175 TA = 327
55016
MA = 327
57786
Ha = 220
719 n
mi
Hp = 214
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12396857
95 X = 3724768
21
Y = 8611003
74 feet Y = 2666588
13 meter
Z = 16320643
53 Z = 4992756
35
XDOT = -19214
393465 XDOT = -5916
505395
YDOT = 14767
516456 feet/sec YDOT = 4435
312028 meter/sec
ZDOT = 6795
059629 ZDOT = 2042
538763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14914654
26 X = 4545986
62
Y = -1654737
48 feet Y = -504363
98 meter
Z = 16401518
53 Z = 4999182
85
XDOT = -4819
526543 XDOT = -1468
991690
YDOT = 22722
475908 feet/sec YDOT = 6925
810657 meter/sec
ZDOT = 6666
826816 ZDOT = 2032
048814
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 18104
60610986
00016717 00000-0 10270-3 0 9018
2 25544 51
6404 335
6827 0002387 345
8401 14
2684 15
54225001 28629
Satellite: ISS
Catalog Number: 25544
Epoch time: 18104
60610986 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 335
6827 deg
Eccentricity:
0002387
Arg of perigee: 345
8401 deg
Mean anomaly: 14
2684 deg
Mean motion: 15
54225001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2862
Checksum: 291
Coasting Arc #3 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2018/105/08:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2623076
11 A = 6782711
74 meter
Y = -4935133
09 meter E =
0005584
Z = -3847206
68 I = 51
46140
XDOT = 6451
048043 Wp = 81
92010
YDOT = 213
087844 meter/sec RA = 331
24199 deg
ZDOT = 4130
981824 TA = 231
61907
MA = 231
66925
Ha = 220
820 n
mi
Hp = 214
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8605892
75 X = 2696755
11
Y = -16191381
54 feet Y = -4905388
43 meter
Z = -12622069
15 Z = -3834285
12
XDOT = 21164
855784 XDOT = 6428
119386
YDOT = 699
107099 feet/sec YDOT = 285
100077 meter/sec
ZDOT = 13553
089973 ZDOT = 4162
263473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14602984
79 X = 4450989
76
Y = -11155518
15 feet Y = -3400201
93 meter
Z = -12563682
02 Z = -3829410
28
XDOT = 18089
109950 XDOT = 5513
560713
YDOT = 8280
299818 feet/sec YDOT = 2523
835384 meter/sec
ZDOT = 13692
564962 ZDOT = 4173
493800
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 18105
37767305
00016717 00000-0 10270-3 0 9022
2 25544 51
6411 331
8364 0002316 348
6463 11
4637 15
54266353 28747
Satellite: ISS
Catalog Number: 25544
Epoch time: 18105
37767305 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 331
8364 deg
Eccentricity:
0002316
Arg of perigee: 348
6463 deg
Mean anomaly: 11
4637 deg
Mean motion: 15
54266353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 303
Coasting Arc #4 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2018/106/08:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3940780
93 A = 6786540
80 meter
Y = 4957848
21 meter E =
0012991
Z = 2425024
65 I = 51
44572
XDOT = -5282
454536 Wp = 96
43208
YDOT = -1579
984519 meter/sec RA = 326
24797 deg
ZDOT = -5330
858835 TA = 56
35742
MA = 56
23356
Ha = 220
896 n
mi
Hp = 214
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12929071
28 X = -4007707
74
Y = 16265906
22 feet Y = 4913405
66 meter
Z = 7956117
63 Z = 2405718
45
XDOT = -17330
887586 XDOT = -5238
499178
YDOT = -5183
676245 feet/sec YDOT = -1638
811199 meter/sec
ZDOT = -17489
694342 ZDOT = -5356
412713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18377094
41 X = -5601338
38
Y = 9767164
79 feet Y = 2977031
83 meter
Z = 7869262
35 Z = 2398551
16
XDOT = -13023
867739 XDOT = -3969
674887
YDOT = -10259
886141 feet/sec YDOT = -3127
213296 meter/sec
ZDOT = -17603
406564 ZDOT = -5365
518321
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 18106
40641947
00016717 00000-0 10270-3 0 9031
2 25544 51
6412 326
7073 0002304 351
7285 8
3830 15
54249352 28900
Satellite: ISS
Catalog Number: 25544
Epoch time: 18106
40641947 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 326
7073 deg
Eccentricity:
0002304
Arg of perigee: 351
7285 deg
Mean anomaly: 8
3830 deg
Mean motion: 15
54249352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2890
Checksum: 295
Coasting Arc #5 (Orbit 2904)
---------------------------------------
Vector Time (GMT): 2018/107/08:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4851799
01 A = 6788684
87 meter
Y = -4676657
73 meter E =
0012314
Z = -766788
13 I = 51
42678
XDOT = 3822
038013 Wp = 31
50342
YDOT = 3000
987744 meter/sec RA = 321
25969 deg
ZDOT = 5934
036656 TA = 320
18188
MA = 320
27218
Ha = 220
920 n
mi
Hp = 214
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15917975
75 X = 4907458
80
Y = -15343365
26 feet Y = -4622090
40 meter
Z = -2515709
09 Z = -743083
87
XDOT = 12539
494794 XDOT = 3759
371115
YDOT = 9845
760315 feet/sec YDOT = 3043
378345 meter/sec
ZDOT = 19468
624199 ZDOT = 5952
450765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20583599
65 X = 6273881
17
Y = -8101872
36 feet Y = -2469450
70 meter
Z = -2409292
67 Z = -734352
41
XDOT = 7122
877457 XDOT = 2171
053049
YDOT = 12337
054381 feet/sec YDOT = 3760
334175 meter/sec
ZDOT = 19550
275637 ZDOT = 5958
924014
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 18107
37086450
00016717 00000-0 10270-3 0 9041
2 25544 51
6416 321
8980 0002457 354
9714 5
1413 15
54271089 29059
Satellite: ISS
Catalog Number: 25544
Epoch time: 18107
37086450 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 321
8980 deg
Eccentricity:
0002457
Arg of perigee: 354
9714 deg
Mean anomaly: 5
1413 deg
Mean motion: 15
54271089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2905
Checksum: 304
Coasting Arc #6 (Orbit 2920)
---------------------------------------
Vector Time (GMT): 2018/108/08:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 928509
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5371428
01 A = 6788522
93 meter
Y = 4021765
25 meter E =
0007853
Z = -1010221
98 I = 51
40082
XDOT = -2193
976863 Wp = 131
37927
YDOT = -4399
005581 meter/sec RA = 316
27415 deg
ZDOT = -5882
074220 TA = 59
60203
MA = 59
52444
Ha = 220
939 n
mi
Hp = 214
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17622795
31 X = -5411094
05
Y = 13194767
90 feet Y = 3961476
43 meter
Z = -3314376
57 Z = -1036411
49
XDOT = -7198
086820 XDOT = -2116
050355
YDOT = -14432
433007 feet/sec YDOT = -4423
104620 meter/sec
ZDOT = -19298
143766 ZDOT = -5892
542585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21206275
22 X = -6463672
69
Y = 5845234
28 feet Y = 1781627
41 meter
Z = -3431768
37 Z = -1046003
00
XDOT = -876
842570 XDOT = -267
261615
YDOT = -14473
343884 feet/sec YDOT = -4411
475216 meter/sec
ZDOT = -19344
150435 ZDOT = -5896
097053
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 18108
39960451
00016717 00000-0 10270-3 0 9057
2 25544 51
6413 316
7692 0002307 357
1408 2
9731 15
54244938 29217
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
39960451 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 316
7692 deg
Eccentricity:
0002307
Arg of perigee: 357
1408 deg
Mean anomaly: 2
9731 deg
Mean motion: 15
54244938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2921
Checksum: 308
Coasting Arc #7 (Orbit 2921)
---------------------------------------
Vector Time (GMT): 2018/108/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4994192
47 A = 6780324
07 meter
Y = -268417
15 meter E =
0010525
Z = -4588627
64 I = 51
36938
XDOT = 3095
193592 Wp = 57
24765
YDOT = -6332
250181 meter/sec RA = 315
92039 deg
ZDOT = -2997
790705 TA = 182
68171
MA = 182
68736
Ha = 220
908 n
mi
Hp = 214
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16385145
89 X = -4968530
21
Y = -880633
70 feet Y = -324122
31 meter
Z = -15054552
61 Z = -4612825
82
XDOT = 10154
834619 XDOT = 3180
334464
YDOT = -20775
099018 feet/sec YDOT = -6297
161637 meter/sec
ZDOT = -9835
271341 ZDOT = -2982
548046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16300925
80 X = -4968522
18
Y = 518852
43 feet Y = 158146
22 meter
Z = -15162410
30 Z = -4621502
66
XDOT = 8436
988817 XDOT = 2571
594191
YDOT = -20387
480765 feet/sec YDOT = -6214
104137 meter/sec
ZDOT = -9766
338948 ZDOT = -2976
780111
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 18108
46389990
00016717 00000-0 10270-3 0 9069
2 25544 51
6402 316
4480 0002276 340
1015 20
0048 15
54117441 29229
Satellite: ISS
Catalog Number: 25544
Epoch time: 18108
46389990 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 316
4480 deg
Eccentricity:
0002276
Arg of perigee: 340
1015 deg
Mean anomaly: 20
0048 deg
Mean motion: 15
54117441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2922
Checksum: 282
Coasting Arc #8 (Orbit 2937)
---------------------------------------
Vector Time (GMT): 2018/109/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4020575
03 A = 6777855
71 meter
Y = 1693893
05 meter E =
0002692
Z = 5184668
62 I = 51
33889
XDOT = -4199
093457 Wp = 89
91186
YDOT = 6307
102115 meter/sec RA = 310
90415 deg
ZDOT = 1195
147329 TA = 348
57546
MA = 348
58157
Ha = 220
859 n
mi
Hp = 214
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13190862
94 X = 3976149
82
Y = 5557391
89 feet Y = 1738605
53 meter
Z = 17010067
67 Z = 5204091
60
XDOT = -13776
553335 XDOT = -4275
114599
YDOT = 20692
592242 feet/sec YDOT = 6259
719913 meter/sec
ZDOT = 3921
087038 ZDOT = 1174
564543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13580898
28 X = 4139457
80
Y = 4183019
86 feet Y = 1274984
45 meter
Z = 17096415
38 Z = 5210987
41
XDOT = -11293
818508 XDOT = -3442
355881
YDOT = 21013
349737 feet/sec YDOT = 6404
869000 meter/sec
ZDOT = 3828
353074 ZDOT = 1166
882017
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 18109
49274052
00016717 00000-0 10270-3 0 9076
2 25544 51
6410 311
3190 0002270 345
0498 15
0587 15
54107942 29387
Satellite: ISS
Catalog Number: 25544
Epoch time: 18109
49274052 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 311
3190 deg
Eccentricity:
0002270
Arg of perigee: 345
0498 deg
Mean anomaly: 15
0587 deg
Mean motion: 15
54107942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2938
Checksum: 297
Coasting Arc #9 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2018/110/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2923084
27 A = 6777512
93 meter
Y = -3141938
88 meter E =
0014010
Z = -5257860
59 I = 51
31628
XDOT = 4931
253314 Wp = 86
51366
YDOT = -5813
194818 meter/sec RA = 305
88091 deg
ZDOT = 734
816363 TA = 190
53210
MA = 190
56147
Ha = 220
972 n
mi
Hp = 214
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9590171
49 X = -2862192
76
Y = -10308198
41 feet Y = -3174286
31 meter
Z = -17250198
78 Z = -5271912
23
XDOT = 16178
652604 XDOT = 4992
322144
YDOT = -19072
161475 feet/sec YDOT = -5757
708699 meter/sec
ZDOT = 2410
814839 ZDOT = 758
919276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10644913
05 X = -3244569
50
Y = -9097638
36 feet Y = -2772960
17 meter
Z = -17312380
08 Z = -5276813
45
XDOT = 13092
934040 XDOT = 3990
726295
YDOT = -20097
787073 feet/sec YDOT = -6125
805500 meter/sec
ZDOT = 2519
163599 ZDOT = 767
841065
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 18110
45727321
00016717 00000-0 10270-3 0 9087
2 25544 51
6401 306
5093 0002341 347
5889 12
5205 15
54141615 29536
Satellite: ISS
Catalog Number: 25544
Epoch time: 18110
45727321 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 306
5093 deg
Eccentricity:
0002341
Arg of perigee: 347
5889 deg
Mean anomaly: 12
5205 deg
Mean motion: 15
54141615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 287
Coasting Arc #10 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2018/111/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1764331
05 A = 6779571
66 meter
Y = 4486496
89 meter E =
0008533
Z = 4763828
52 I = 51
30464
XDOT = -5330
937710 Wp = 45
86581
YDOT = 4864
228876 meter/sec RA = 300
86110 deg
ZDOT = -2597
944841 TA = 69
90065
MA = 69
80884
Ha = 220
946 n
mi
Hp = 214
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5788487
70 X = 1690890
33
Y = 14719477
98 feet Y = 4505816
16 meter
Z = 15629358
68 Z = 4772220
79
XDOT = -17489
953118 XDOT = -5372
315086
YDOT = 15958
756154 feet/sec YDOT = 4804
383340 meter/sec
ZDOT = -8523
441079 ZDOT = -2623
941341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7649436
95 X = 2331548
38
Y = 13802375
96 feet Y = 4206964
19 meter
Z = 15666110
13 Z = 4775030
37
XDOT = -14074
518370 XDOT = -4289
913199
YDOT = 17639
493057 feet/sec YDOT = 5376
517484 meter/sec
ZDOT = -8640
084196 ZDOT = -2633
497663
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 18111
48610571
00016717 00000-0 10270-3 0 9090
2 25544 51
6399 301
3811 0002382 349
3296 10
7806 15
54155747 29695
Satellite: ISS
Catalog Number: 25544
Epoch time: 18111
48610571 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 301
3811 deg
Eccentricity:
0002382
Arg of perigee: 349
3296 deg
Mean anomaly: 10
7806 deg
Mean motion: 15
54155747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 319
Coasting Arc #11 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2018/112/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -671026
58 A = 6783176
82 meter
Y = -5585867
97 meter E =
0005619
Z = -3793450
21 I = 51
29972
XDOT = 5402
264438 Wp = 81
06893
YDOT = -3479
958602 meter/sec RA = 295
84689 deg
ZDOT = 4174
806512 TA = 233
17748
MA = 233
22903
Ha = 221
022 n
mi
Hp = 214
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2201530
79 X = -590087
35
Y = -18326338
47 feet Y = -5592919
27 meter
Z = -12445702
80 Z = -3796513
28
XDOT = 17723
964690 XDOT = 5420
497682
YDOT = -11417
187013 feet/sec YDOT = -3419
444836 meter/sec
ZDOT = 13696
871759 ZDOT = 4201
093218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4918276
43 X = -1499090
66
Y = -17781796
95 feet Y = -5419891
71 meter
Z = -12458538
92 Z = -3797362
66
XDOT = 14366
460602 XDOT = 4378
897192
YDOT = -13638
447767 feet/sec YDOT = -4156
998879 meter/sec
ZDOT = 13814
597449 ZDOT = 4210
689303
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 18112
45063490
00016717 00000-0 10270-3 0 9102
2 25544 51
6391 296
5723 0002290 351
7015 8
4099 15
54142262 29841
Satellite: ISS
Catalog Number: 25544
Epoch time: 18112
45063490 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 296
5723 deg
Eccentricity:
0002290
Arg of perigee: 351
7015 deg
Mean anomaly: 8
4099 deg
Mean motion: 15
54142262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 297
Coasting Arc #12 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2018/113/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -357565
32 A = 6786732
86 meter
Y = 6334531
16 meter E =
0013077
Z = 2396025
05 I = 51
29901
XDOT = -5231
563890 Wp = 95
49957
YDOT = 1731
219431 meter/sec RA = 290
84236 deg
ZDOT = -5333
713330 TA = 57
58358
MA = 57
45715
Ha = 221
053 n
mi
Hp = 214
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1173114
57 X = -440011
85
Y = 20782582
54 feet Y = 6330071
66 meter
Z = 7860974
59 Z = 2394087
80
XDOT = -17163
923522 XDOT = -5224
625621
YDOT = 5679
853776 feet/sec YDOT = 1672
755216 meter/sec
ZDOT = -17499
059480 ZDOT = -5359
109668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2348597
33 X = 715852
47
Y = 20686376
54 feet Y = 6305207
57 meter
Z = 7851418
50 Z = 2393112
36
XDOT = -14316
625223 XDOT = -4363
707368
YDOT = 8340
036983 feet/sec YDOT = 2542
043272 meter/sec
ZDOT = -17612
555088 ZDOT = -5368
306791
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 18113
47945976
00016717 00000-0 10270-3 0 9114
2 25544 51
6395 291
4430 0002561 355
2180 4
8948 15
54187167 30003
Satellite: ISS
Catalog Number: 25544
Epoch time: 18113
47945976 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 291
4430 deg
Eccentricity:
0002561
Arg of perigee: 355
2180 deg
Mean anomaly: 4
8948 deg
Mean motion: 15
54187167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 311
Coasting Arc #13 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2018/114/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1232044
75 A = 6789039
43 meter
Y = -6624431
48 meter E =
0012236
Z = -778055
64 I = 51
29330
XDOT = 4870
304429 Wp = 32
92516
YDOT = 216
760266 meter/sec RA = 285
84512 deg
ZDOT = 5920
601052 TA = 318
62191
MA = 318
71453
Ha = 221
158 n
mi
Hp = 214
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4042141
58 X = 1309808
78
Y = -21733699
09 feet Y = -6610219
13 meter
Z = -2552675
99 Z = -771881
70
XDOT = 15978
689070 XDOT = 4838
759376
YDOT = 711
155727 feet/sec YDOT = 271
047168 meter/sec
ZDOT = 19424
544133 ZDOT = 5944
182719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -99464
08 X = -30316
65
Y = -22109437
99 feet Y = -6738956
70 meter
Z = -2524202
47 Z = -769376
91
XDOT = 14089
078507 XDOT = 4294
351129
YDOT = -2272
590666 feet/sec YDOT = -692
685635 meter/sec
ZDOT = 19529
667002 ZDOT = 5952
642502
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 18114
44398267
00016717 00000-0 10270-3 0 9128
2 25544 51
6372 286
6343 0002292 1
0716 359
0441 15
54141347 30158
Satellite: ISS
Catalog Number: 25544
Epoch time: 18114
44398267 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 286
6343 deg
Eccentricity:
0002292
Arg of perigee: 1
0716 deg
Mean anomaly: 359
0441 deg
Mean motion: 15
54141347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 290
Coasting Arc #14 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2018/115/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2010643
81 A = 6788798
25 meter
Y = 6410175
92 meter E =
0008235
Z = -958053
67 I = 51
28469
XDOT = -4371
547624 Wp = 129
45003
YDOT = -2244
656741 meter/sec RA = 280
85079 deg
ZDOT = -5883
243214 TA = 60
97436
MA = 60
89187
Ha = 221
188 n
mi
Hp = 214
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6596600
44 X = -2077520
98
Y = 21030760
88 feet Y = 6387317
53 meter
Z = -3143220
69 Z = -967983
45
XDOT = -14342
347848 XDOT = -4317
544555
YDOT = -7364
359386 feet/sec YDOT = -2293
240726 meter/sec
ZDOT = -19301
979047 ZDOT = -5904
347484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2127717
22 X = -648528
21
Y = 21931594
33 feet Y = 6684749
95 meter
Z = -3188395
60 Z = -971822
98
XDOT = -13822
728798 XDOT = -4213
167738
YDOT = -4142
389895 feet/sec YDOT = -1262
600440 meter/sec
ZDOT = -19395
771771 ZDOT = -5911
831236
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 18115
47280252
00016717 00000-0 10270-3 0 9137
2 25544 51
6370 281
5052 0002425 4
8715 355
2461 15
54172054 30312
Satellite: ISS
Catalog Number: 25544
Epoch time: 18115
47280252 = yrday
fracday
Element set: 913
Inclination: 51
6370 deg
RA of node: 281
5052 deg
Eccentricity:
0002425
Arg of perigee: 4
8715 deg
Mean anomaly: 355
2461 deg
Mean motion: 15
54172054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 273
Coasting Arc #15 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2018/116/10:37:11
515
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2647213
09 A = 6786395
62 meter
Y = -5691089
64 meter E =
0014622
Z = 2560267
39 I = 51
27114
XDOT = 3796
796364 Wp = 68
44831
YDOT = 4129
436949 meter/sec RA = 275
85083 deg
ZDOT = 5234
514525 TA = 320
50835
MA = 320
61482
Ha = 221
158 n
mi
Hp = 214
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8685082
33 X = 2698219
14
Y = -18671553
92 feet Y = -5661201
34 meter
Z = 8399827
41 Z = 2573250
94
XDOT = 12456
680985 XDOT = 3724
910990
YDOT = 13548
021485 feet/sec YDOT = 4171
493700 meter/sec
ZDOT = 17173
604084 ZDOT = 5252
783346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4275817
03 X = 1303269
03
Y = -20119288
11 feet Y = -6132359
02 meter
Z = 8458505
55 Z = 2578152
49
XDOT = 13572
253171 XDOT = 4136
822766
YDOT = 10164
363053 feet/sec YDOT = 3098
097859 meter/sec
ZDOT = 17254
498817 ZDOT = 5259
171239
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 18116
50161861
00016717 00000-0 10270-3 0 9147
2 25544 51
6367 276
3749 0002209 9
1508 350
9685 15
54168859 30476
Satellite: ISS
Catalog Number: 25544
Epoch time: 18116
50161861 = yrday
fracday
Element set: 914
Inclination: 51
6367 deg
RA of node: 276
3749 deg
Eccentricity:
0002209
Arg of perigee: 9
1508 deg
Mean anomaly: 350
9685 deg
Mean motion: 15
54168859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 327
Coasting Arc #16 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2018/117/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2655883
71 A = 6785205
77 meter
Y = -5424687
86 meter E =
0014073
Z = 3075272
58 I = 51
26901
XDOT = 3745
625193 Wp = 74
53895
YDOT = 4600
809547 meter/sec RA = 271
98397 deg
ZDOT = 4865
919489 TA = 321
02667
MA = 321
12801
Ha = 221
319 n
mi
Hp = 214
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8713529
24 X = 2701408
45
Y = -17797532
34 feet Y = -5394733
21 meter
Z = 10089476
97 Z = 3088284
96
XDOT = 12288
796566 XDOT = 3670
262984
YDOT = 15094
519512 feet/sec YDOT = 4642
274612 meter/sec
ZDOT = 15964
302784 ZDOT = 4883
931316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19734391
08 X = 6015042
40
Y = 1429112
25 feet Y = 435593
42 meter
Z = 10148238
35 Z = 3093183
05
XDOT = -9396
150150 XDOT = -2863
946566
YDOT = 15473
998756 feet/sec YDOT = 4716
474821 meter/sec
ZDOT = 16043
993950 ZDOT = 4890
209356
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 18117
27322991
00016717 00000-0 10270-3 0 9156
2 25544 51
6408 272
5316 0002604 14
0575 346
0650 15
54151041 30594
Satellite: ISS
Catalog Number: 25544
Epoch time: 18117
27322991 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 272
5316 deg
Eccentricity:
0002604
Arg of perigee: 14
0575 deg
Mean anomaly: 346
0650 deg
Mean motion: 15
54151041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 284
Coasting Arc #17 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2018/118/05:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 928421
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3241755
33 A = 6781265
39 meter
Y = 4126701
04 meter E =
0010253
Z = -4305940
74 I = 51
25596
XDOT = -3114
248392 Wp = 57
59187
YDOT = -6072
726897 meter/sec RA = 266
97304 deg
ZDOT = -3476
046626 TA = 176
82694
MA = 176
82043
Ha = 221
342 n
mi
Hp = 214
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10635680
21 X = -3266744
00
Y = 13539045
39 feet Y = 4090309
55 meter
Z = -14127102
16 Z = -4321749
19
XDOT = -10217
350368 XDOT = -3029
225000
YDOT = -19923
644675 feet/sec YDOT = -6107
077351 meter/sec
ZDOT = -11404
352446 ZDOT = -3490
967958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16561958
69 X = -5048085
01
Y = -4484704
35 feet Y = -1366937
89 meter
Z = -14198148
14 Z = -4327595
55
XDOT = 14123
475949 XDOT = 4304
835469
YDOT = -15851
749772 feet/sec YDOT = -4831
613331 meter/sec
ZDOT = -11470
073842 ZDOT = -3496
078507
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 18118
23773829
00016717 00000-0 10270-3 0 9164
2 25544 51
6407 267
7240 0002577 13
8755 346
2468 15
54176291 30741
Satellite: ISS
Catalog Number: 25544
Epoch time: 18118
23773829 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 267
7240 deg
Eccentricity:
0002577
Arg of perigee: 13
8755 deg
Mean anomaly: 346
2468 deg
Mean motion: 15
54176291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 329
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