[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 4th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 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
037/00:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
040/08:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
5
042/08:58:45
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
6
042/12:24:39
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
043/19:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 213
6
048/05:42:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 1756)
---------------------------------------
Vector Time (GMT): 2018/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4593474
84 A = 6779984
62 meter
Y = 1646404
79 meter E =
0009618
Z = 4699901
47 I = 51
44130
XDOT = -4754
418144 Wp = 101
79120
YDOT = 5350
148886 meter/sec RA = 329
56631 deg
ZDOT = 2765
837100 TA = 320
72520
MA = 320
79493
Ha = 221
935 n
mi
Hp = 213
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15070455
51 X = 4551893
88
Y = 5401590
53 feet Y = 1697539
89 meter
Z = 15419624
25 Z = 4722113
31
XDOT = -15598
484725 XDOT = -4827
326212
YDOT = 17552
981909 feet/sec YDOT = 5296
574187 meter/sec
ZDOT = 9074
268701 ZDOT = 2742
565109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5939032
57 X = 1810217
13
Y = 14763921
60 feet Y = 4500043
30 meter
Z = 15518219
39 Z = 4729953
27
XDOT = -22445
834998 XDOT = -6841
490507
YDOT = -421
907661 feet/sec YDOT = -128
597455 meter/sec
ZDOT = 8969
786913 ZDOT = 2733
991051
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 18033
55307924
00016717 00000-0 10270-3 0 9007
2 25544 51
6412 329
8930 0002951 58
7411 301
4031 15
54073013 17579
Satellite: ISS
Catalog Number: 25544
Epoch time: 18033
55307924 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 329
8930 deg
Eccentricity:
0002951
Arg of perigee: 58
7411 deg
Mean anomaly: 301
4031 deg
Mean motion: 15
54073013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1757
Checksum: 280
Coasting Arc #2 (Orbit 1771)
---------------------------------------
Vector Time (GMT): 2018/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3303299
91 A = 6777852
97 meter
Y = -2781472
74 meter E =
0017480
Z = -5239421
17 I = 51
40619
XDOT = 5717
998047 Wp = 78
63867
YDOT = -5000
691883 meter/sec RA = 324
55472 deg
ZDOT = -949
616360 TA = 182
22537
MA = 182
23316
Ha = 222
207 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10837598
12 X = -3246501
48
Y = -9125566
74 feet Y = -2818095
25 meter
Z = -17189702
01 Z = -5255328
96
XDOT = 18759
836113 XDOT = 5778
104793
YDOT = -16406
469433 feet/sec YDOT = -4936
413286 meter/sec
ZDOT = -3115
539240 ZDOT = -921
694677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -576325
78 X = -175664
10
Y = -14070321
61 feet Y = -4288634
03 meter
Z = -17260047
94 Z = -5260862
61
XDOT = 23769
463811 XDOT = 7244
932570
YDOT = 2697
462959 feet/sec YDOT = 822
186710 meter/sec
ZDOT = -2990
436909 ZDOT = -911
485170
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 18034
51766363
00016717 00000-0 10270-3 0 9011
2 25544 51
6413 325
0848 0003228 61
2521 298
8955 15
54053698 17723
Satellite: ISS
Catalog Number: 25544
Epoch time: 18034
51766363 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 325
0848 deg
Eccentricity:
0003228
Arg of perigee: 61
2521 deg
Mean anomaly: 298
8955 deg
Mean motion: 15
54053698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1772
Checksum: 318
Coasting Arc #3 (Orbit 1787)
---------------------------------------
Vector Time (GMT): 2018/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1881976
59 A = 6777822
04 meter
Y = 3880229
15 meter E =
0006716
Z = 5224286
35 I = 51
37951
XDOT = -6259
644492 Wp = 59
83573
YDOT = 4332
287966 meter/sec RA = 319
53988 deg
ZDOT = -958
528340 TA = 39
38957
MA = 39
34075
Ha = 222
077 n
mi
Hp = 213
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6174463
87 X = 1813070
61
Y = 12730410
61 feet Y = 3900889
78 meter
Z = 17140047
09 Z = 5233260
54
XDOT = -20536
891378 XDOT = -6302
968148
YDOT = 14213
543194 feet/sec YDOT = 4262
046024 meter/sec
ZDOT = -3144
778020 ZDOT = -989
040435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5009774
10 X = -1526979
14
Y = 13181065
63 feet Y = 4017588
80 meter
Z = 17179355
20 Z = 5236267
46
XDOT = -23491
249867 XDOT = -7160
132959
YDOT = -4633
708844 feet/sec YDOT = -1412
354456 meter/sec
ZDOT = -3281
283263 ZDOT = -1000
135139
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 18035
54654779
00016717 00000-0 10270-3 0 9023
2 25544 51
6406 319
9578 0003112 63
1400 297
0070 15
54078355 17889
Satellite: ISS
Catalog Number: 25544
Epoch time: 18035
54654779 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 319
9578 deg
Eccentricity:
0003112
Arg of perigee: 63
1400 deg
Mean anomaly: 297
0070 deg
Mean motion: 15
54078355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1788
Checksum: 316
Coasting Arc #4 (Orbit 1802)
---------------------------------------
Vector Time (GMT): 2018/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -486201
87 A = 6780138
61 meter
Y = -4869393
74 meter E =
0013318
Z = -4705285
07 I = 51
36321
XDOT = 6336
861413 Wp = 99
93247
YDOT = -3296
000715 meter/sec RA = 314
52455 deg
ZDOT = 2760
600159 TA = 197
52956
MA = 197
57556
Ha = 222
190 n
mi
Hp = 213
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1595150
48 X = -408859
43
Y = -15975701
24 feet Y = -4874398
62 meter
Z = -15437286
96 Z = -4707458
68
XDOT = 20790
227734 XDOT = 6359
837897
YDOT = -10813
650640 feet/sec YDOT = -3225
008942 meter/sec
ZDOT = 9057
087135 ZDOT = 2791
437939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10302337
37 X = 3140152
43
Y = -12302638
64 feet Y = -3749844
26 meter
Z = -15446174
00 Z = -4707993
83
XDOT = 21372
224929 XDOT = 6514
254158
YDOT = 6371
252266 feet/sec YDOT = 1941
957691 meter/sec
ZDOT = 9194
859524 ZDOT = 2802
593183
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 18036
51112474
00016717 00000-0 10270-3 0 9033
2 25544 51
6411 315
1495 0003142 67
7882 292
3604 15
54064960 18034
Satellite: ISS
Catalog Number: 25544
Epoch time: 18036
51112474 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 315
1495 deg
Eccentricity:
0003142
Arg of perigee: 67
7882 deg
Mean anomaly: 292
3604 deg
Mean motion: 15
54064960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1803
Checksum: 291
Coasting Arc #5 (Orbit 1810)
---------------------------------------
Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4181114
16 A = 6778296
56 meter
Y = -1496244
60 meter E =
0016543
Z = -5135837
40 I = 51
34610
XDOT = 4080
715385 Wp = 78
23218
YDOT = -6304
813602 meter/sec RA = 312
01887 deg
ZDOT = -1486
092931 TA = 177
37951
MA = 177
37083
Ha = 222
121 n
mi
Hp = 213
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13717566
16 X = -4139125
19
Y = -4908938
97 feet Y = -1542766
20 meter
Z = -16849860
25 Z = -5156045
43
XDOT = 13388
173836 XDOT = 4158
132779
YDOT = -20685
083995 feet/sec YDOT = -6258
747459 meter/sec
ZDOT = -4875
632977 ZDOT = -1466
082143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6762582
01 X = 2061235
00
Y = 12786953
72 feet Y = 3897463
49 meter
Z = -16939551
13 Z = -5163175
18
XDOT = -22913
178808 XDOT = -6983
936901
YDOT = 5781
619419 feet/sec YDOT = 1762
237599 meter/sec
ZDOT = -4785
565997 ZDOT = -1458
640516
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 18037
02556204
00016717 00000-0 10270-3 0 9044
2 25544 51
6418 312
5827 0002777 76
9274 283
2189 15
54048366 18119
Satellite: ISS
Catalog Number: 25544
Epoch time: 18037
02556204 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 312
5827 deg
Eccentricity:
0002777
Arg of perigee: 76
9274 deg
Mean anomaly: 283
2189 deg
Mean motion: 15
54048366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1811
Checksum: 317
Coasting Arc #6 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3088638
10 A = 6777476
14 meter
Y = 2918293
80 meter E =
0005527
Z = 5275438
96 I = 51
32295
XDOT = -4872
465045 Wp = 74
33559
YDOT = 5912
665420 meter/sec RA = 306
99835 deg
ZDOT = -416
260088 TA = 19
65982
MA = 19
63852
Ha = 221
954 n
mi
Hp = 213
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10133327
09 X = 3030150
44
Y = 9574454
73 feet Y = 2952506
28 meter
Z = 17307870
61 Z = 5290300
11
XDOT = -15985
777708 XDOT = -4936
197995
YDOT = 19398
508596 feet/sec YDOT = 5857
821802 meter/sec
ZDOT = -1365
682705 ZDOT = -440
083567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1207387
48 X = -368011
70
Y = -13806492
07 feet Y = -4208218
78 meter
Z = 17373539
61 Z = 5295454
87
XDOT = 23798
529891 XDOT = 7253
791911
YDOT = -3941
841762 feet/sec YDOT = -1201
473369 meter/sec
ZDOT = -1472
641277 ZDOT = -448
861061
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 18038
05443494
00016717 00000-0 10270-3 0 9055
2 25544 51
6421 307
4541 0002850 78
6757 281
4715 15
54105587 18277
Satellite: ISS
Catalog Number: 25544
Epoch time: 18038
05443494 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 307
4541 deg
Eccentricity:
0002850
Arg of perigee: 78
6757 deg
Mean anomaly: 281
4715 deg
Mean motion: 15
54105587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 316
Coasting Arc #7 (Orbit 1841)
---------------------------------------
Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1963925
55 A = 6779234
99 meter
Y = -4267199
98 meter E =
0014894
Z = -4901698
23 I = 51
30835
XDOT = 5294
182364 Wp = 101
65328
YDOT = -5043
242933 meter/sec RA = 301
97896 deg
ZDOT = 2272
173989 TA = 190
67704
MA = 190
70870
Ha = 222
149 n
mi
Hp = 213
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6443325
28 X = -1892253
05
Y = -13999999
94 feet Y = -4288761
35 meter
Z = -16081687
11 Z = -4911063
96
XDOT = 17369
364712 XDOT = 5339
146922
YDOT = -16546
072615 feet/sec YDOT = -4983
788271 meter/sec
ZDOT = 7454
639071 ZDOT = 2298
000314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4225863
17 X = -1288043
09
Y = 14776264
45 feet Y = 4503805
41 meter
Z = -16122691
72 Z = -4914196
44
XDOT = -22833
510889 XDOT = -6959
654119
YDOT = 1719
561263 feet/sec YDOT = 524
122273 meter/sec
ZDOT = 7570
361759 ZDOT = 2307
446264
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 18039
01900344
00016717 00000-0 10270-3 0 9065
2 25544 51
6408 302
6471 0003007 82
1188 278
0306 15
54088605 18420
Satellite: ISS
Catalog Number: 25544
Epoch time: 18039
01900344 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 302
6471 deg
Eccentricity:
0003007
Arg of perigee: 82
1188 deg
Mean anomaly: 278
0306 deg
Mean motion: 15
54088605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1842
Checksum: 289
Coasting Arc #8 (Orbit 1857)
---------------------------------------
Vector Time (GMT): 2018/040/00:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 842634
85 A = 6782589
54 meter
Y = 5406538
24 meter E =
0013730
Z = 3997972
12 I = 51
30383
XDOT = -5427
831929 Wp = 79
59447
YDOT = 3751
754202 meter/sec RA = 296
96424 deg
ZDOT = -3915
648770 TA = 51
30207
MA = 51
17936
Ha = 222
052 n
mi
Hp = 213
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2764550
04 X = 762695
09
Y = 17737986
34 feet Y = 5415514
27 meter
Z = 13116706
42 Z = 4001871
01
XDOT = -17807
847535 XDOT = -5450
361771
YDOT = 12308
904862 feet/sec YDOT = 3690
930406 meter/sec
ZDOT = -12846
616701 ZDOT = -3942
069715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9170340
64 X = 2795119
83
Y = -15419158
81 feet Y = -4699759
61 meter
Z = 13133212
78 Z = 4003003
26
XDOT = 20384
959106 XDOT = 6213
335536
YDOT = 1042
123790 feet/sec YDOT = 317
639331 meter/sec
ZDOT = -12964
774780 ZDOT = -3951
663353
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 18040
04787125
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 297
5184 0002878 83
8863 276
2617 15
54106945 18583
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
04787125 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 297
5184 deg
Eccentricity:
0002878
Arg of perigee: 83
8863 deg
Mean anomaly: 276
2617 deg
Mean motion: 15
54106945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1858
Checksum: 338
Coasting Arc #9 (Orbit 1862)
---------------------------------------
Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4450917
19 A = 6778255
53 meter
Y = -193625
97 meter E =
0016776
Z = -5123535
37 I = 51
28246
XDOT = 2061
064854 Wp = 78
62255
YDOT = -7214
868839 meter/sec RA = 295
28152 deg
ZDOT = -1518
822958 TA = 176
65268
MA = 176
64144
Ha = 222
191 n
mi
Hp = 213
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14602746
68 X = -4423534
15
Y = -635255
79 feet Y = -243246
16 meter
Z = -16809499
23 Z = -5145089
54
XDOT = 6762
023798 XDOT = 2148
967817
YDOT = -23670
829523 feet/sec YDOT = -7191
329131 meter/sec
ZDOT = -4983
014953 ZDOT = -1508
597536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1956842
32 X = 596445
54
Y = -14372952
09 feet Y = -4380875
80 meter
Z = -16905384
99 Z = -5152761
34
XDOT = 21904
042860 XDOT = 6676
352264
YDOT = 8784
517055 feet/sec YDOT = 2677
520798 meter/sec
ZDOT = -4936
390490 ZDOT = -1504
611821
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 18040
36939366
00016717 00000-0 10270-3 0 9083
2 25544 51
6398 295
9166 0003081 80
0707 280
0793 15
54078190 18633
Satellite: ISS
Catalog Number: 25544
Epoch time: 18040
36939366 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 295
9166 deg
Eccentricity:
0003081
Arg of perigee: 80
0707 deg
Mean anomaly: 280
0793 deg
Mean motion: 15
54078190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1863
Checksum: 330
Coasting Arc #10 (Orbit 1878)
---------------------------------------
Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3815709
21 A = 6777496
45 meter
Y = 1876422
68 meter E =
0005716
Z = 5272915
79 I = 51
26702
XDOT = -2942
494714 Wp = 76
76767
YDOT = 7075
917882 meter/sec RA = 290
25786 deg
ZDOT = -387
082291 TA = 16
94973
MA = 16
93064
Ha = 222
037 n
mi
Hp = 213
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12518731
00 X = 3768830
35
Y = 6156242
38 feet Y = 1918830
52 meter
Z = 17299592
48 Z = 5291336
97
XDOT = -9653
854049 XDOT = -3019
520641
YDOT = 23214
953680 feet/sec YDOT = 7042
582203 meter/sec
ZDOT = -1269
955022 ZDOT = -401
562846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7060396
95 X = -2152008
99
Y = 11913679
49 feet Y = 3631289
51 meter
Z = 17381279
64 Z = 5297814
03
XDOT = -21567
065416 XDOT = -6573
641539
YDOT = -10825
078204 feet/sec YDOT = -3299
483837 meter/sec
ZDOT = -1335
480228 ZDOT = -407
054374
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 18041
39825697
00016717 00000-0 10270-3 0 9099
2 25544 51
6398 290
7890 0003092 81
2940 278
8563 15
54094702 18798
Satellite: ISS
Catalog Number: 25544
Epoch time: 18041
39825697 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 290
7890 deg
Eccentricity:
0003092
Arg of perigee: 81
2940 deg
Mean anomaly: 278
8563 deg
Mean motion: 15
54094702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1879
Checksum: 351
Coasting Arc #11 (Orbit 1893)
---------------------------------------
Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3125982
79 A = 6779194
63 meter
Y = -3500437
45 meter E =
0015134
Z = -4906095
28 I = 51
26171
XDOT = 3605
136728 Wp = 102
19536
YDOT = -6368
958531 meter/sec RA = 285
23378 deg
ZDOT = 2249
878797 TA = 189
92068
MA = 189
95059
Ha = 222
196 n
mi
Hp = 213
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10255849
04 X = -3062776
86
Y = -11484374
85 feet Y = -3535041
00 meter
Z = -16096113
14 Z = -4921126
36
XDOT = 11827
876403 XDOT = 3665
159695
YDOT = -20895
533237 feet/sec YDOT = -6328
307776 meter/sec
ZDOT = 7381
492117 ZDOT = 2267
536833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12045319
00 X = 3671413
23
Y = -9478548
45 feet Y = -2889061
57 meter
Z = -16162474
21 Z = -4926322
14
XDOT = 19498
660903 XDOT = 5943
191843
YDOT = 12071
984440 feet/sec YDOT = 3679
540857 meter/sec
ZDOT = 7461
036612 ZDOT = 2274
123959
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 18042
36281519
00016717 00000-0 10270-3 0 9108
2 25544 51
6394 285
9811 0003114 85
6183 274
5325 15
54085397 18941
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
36281519 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 285
9811 deg
Eccentricity:
0003114
Arg of perigee: 85
6183 deg
Mean anomaly: 274
5325 deg
Mean motion: 15
54085397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1894
Checksum: 323
Coasting Arc #12 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2018/042/08:58:45
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4451391
35 A = 6779783
82 meter
Y = -1947262
82 meter E =
0010344
Z = 4721507
34 I = 51
26428
XDOT = 285
719794 Wp = 109
27587
YDOT = 7182
484715 meter/sec RA = 285
15558 deg
ZDOT = 2684
673027 TA = 314
03153
MA = 314
11671
Ha = 221
988 n
mi
Hp = 213
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14604302
33 X = 4449901
19
Y = -6388657
54 feet Y = -1897492
57 meter
Z = 15490509
64 Z = 4743126
64
XDOT = 937
400900 XDOT = 192
341603
YDOT = 23564
582397 feet/sec YDOT = 7185
157759 meter/sec
ZDOT = 8807
982372 ZDOT = 2685
834027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7674052
15 X = 2339051
10
Y = 13863997
10 feet Y = 4225746
32 meter
Z = 15587013
46 Z = 4750921
70
XDOT = -22377
942862 XDOT = -6820
796984
YDOT = 2449
505383 feet/sec YDOT = 746
609241 meter/sec
ZDOT = 8812
062711 ZDOT = 2685
916714
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 18042
42711795
00016717 00000-0 10270-3 0 9110
2 25544 51
6399 285
6612 0003014 87
5369 272
6129 15
54113135 18952
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
42711795 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 285
6612 deg
Eccentricity:
0003014
Arg of perigee: 87
5369 deg
Mean anomaly: 272
6129 deg
Mean motion: 15
54113135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 316
Coasting Arc #13 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2018/042/12:24:39
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1050272
34 A = 6785281
83 meter
Y = 5931418
85 meter E =
0016020
Z = 3108471
30 I = 51
28269
XDOT = -4880
147422 Wp = 92
86588
YDOT = 3410
879945 meter/sec RA = 284
39517 deg
ZDOT = -4838
734427 TA = 51
13712
MA = 50
99429
Ha = 222
137 n
mi
Hp = 213
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3445775
39 X = 968768
54
Y = 19460035
59 feet Y = 5942708
05 meter
Z = 10198396
66 Z = 3113375
01
XDOT = -16010
982357 XDOT = -4894
422556
YDOT = 11190
551001 feet/sec YDOT = 3356
226898 meter/sec
ZDOT = -15875
112949 ZDOT = -4862
474737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7825876
01 X = -2385327
01
Y = 18135455
03 feet Y = 5527686
69 meter
Z = 10219324
02 Z = 3114849
96
XDOT = -18113
763830 XDOT = -5521
075215
YDOT = 1227
393639 feet/sec YDOT = 374
109581 meter/sec
ZDOT = -15981
276112 ZDOT = -4871
092959
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 18042
55572559
00016717 00000-0 10270-3 0 9128
2 25544 51
6413 285
0210 0003098 84
5786 275
5720 15
54105660 18974
Satellite: ISS
Catalog Number: 25544
Epoch time: 18042
55572559 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 285
0210 deg
Eccentricity:
0003098
Arg of perigee: 84
5786 deg
Mean anomaly: 275
5720 deg
Mean motion: 15
54105660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1897
Checksum: 316
Coasting Arc #14 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2018/043/12:24:39
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -222146
09 A = 6788314
66 meter
Y = -6587099
86 meter E =
0010069
Z = -1614786
83 I = 51
28558
XDOT = 4886
600275 Wp = 50
50312
YDOT = -1554
260755 meter/sec RA = 279
39422 deg
ZDOT = 5698
067540 TA = 291
74002
MA = 291
84716
Ha = 222
108 n
mi
Hp = 213
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -728825
74 X = -140627
24
Y = -21611220
00 feet Y = -6589128
28 meter
Z = -5297857
05 Z = -1615667
78
XDOT = 16032
153134 XDOT = 4875
939677
YDOT = -5099
280693 feet/sec YDOT = -1499
674923 meter/sec
ZDOT = 18694
447309 ZDOT = 5721
778555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10930560
26 X = 3331634
77
Y = -18656571
95 feet Y = -5686523
13 meter
Z = -5300800
12 Z = -1615683
88
XDOT = 14817
372757 XDOT = 4516
335216
YDOT = 3367
690726 feet/sec YDOT = 1026
472133 meter/sec
ZDOT = 18800
199548 ZDOT = 5730
300822
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 18043
52027983
00016717 00000-0 10270-3 0 9133
2 25544 51
6413 280
2130 0002918 87
5352 272
6135 15
54094937 19124
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
52027983 = yrday
fracday
Element set: 913
Inclination: 51
6413 deg
RA of node: 280
2130 deg
Eccentricity:
0002918
Arg of perigee: 87
5352 deg
Mean anomaly: 272
6135 deg
Mean motion: 15
54094937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 301
Coasting Arc #15 (Orbit 1916)
---------------------------------------
Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3600748
56 A = 6779005
75 meter
Y = 2908354
03 meter E =
0008817
Z = 4946546
47 I = 51
25172
XDOT = -2666
501913 Wp = 71
22805
YDOT = 6881
991631 meter/sec RA = 277
98335 deg
ZDOT = -2099
409907 TA = 39
34093
MA = 39
27691
Ha = 222
130 n
mi
Hp = 213
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11813479
54 X = 3543931
79
Y = 9541843
92 feet Y = 2948302
51 meter
Z = 16228827
01 Z = 4963899
19
XDOT = -8748
365857 XDOT = -2733
062437
YDOT = 22578
712700 feet/sec YDOT = 6851
800763 meter/sec
ZDOT = -6887
827778 ZDOT = -2112
524374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13116289
83 X = 3997845
14
Y = -7487956
22 feet Y = -2282329
06 meter
Z = 16305623
66 Z = 4969954
09
XDOT = 17388
031571 XDOT = 5299
872023
YDOT = 15287
930710 feet/sec YDOT = 4659
761281 meter/sec
ZDOT = -6947
208051 ZDOT = -2117
509014
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 18043
84179942
00016717 00000-0 10270-3 0 9142
2 25544 51
6403 278
6049 0003200 99
8973 260
2541 15
54068628 19170
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
84179942 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 278
6049 deg
Eccentricity:
0003200
Arg of perigee: 99
8973 deg
Mean anomaly: 260
2541 deg
Mean motion: 15
54068628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1917
Checksum: 326
Coasting Arc #16 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3078508
41 A = 6782186
71 meter
Y = -4433588
32 meter E =
0010646
Z = -4117665
20 I = 51
25878
XDOT = 3318
832602 Wp = 107
25456
YDOT = -5789
733152 meter/sec RA = 272
96526 deg
ZDOT = 3757
646041 TA = 201
70212
MA = 201
74726
Ha = 222
154 n
mi
Hp = 213
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10100093
20 X = -3008701
08
Y = -14545893
45 feet Y = -4467624
15 meter
Z = -13509400
25 Z = -4132449
44
XDOT = 10888
558406 XDOT = 3365
076098
YDOT = -18995
187507 feet/sec YDOT = -5752
360986 meter/sec
ZDOT = 12328
235043 ZDOT = 3773
879903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17101674
22 X = -5212590
30
Y = 4400336
82 feet Y = 1341222
66 meter
Z = -13574555
94 Z = -4137524
65
XDOT = -13801
062558 XDOT = -4206
563868
YDOT = -15430
492713 feet/sec YDOT = -4703
214179 meter/sec
ZDOT = 12401
323045 ZDOT = 3779
923264
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 18044
80634894
00016717 00000-0 10270-3 0 9152
2 25544 51
6401 273
7978 0003082 102
4752 257
6746 15
54093071 19323
Satellite: ISS
Catalog Number: 25544
Epoch time: 18044
80634894 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 273
7978 deg
Eccentricity:
0003082
Arg of perigee: 102
4752 deg
Mean anomaly: 257
6746 deg
Mean motion: 15
54093071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1932
Checksum: 319
Coasting Arc #17 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2471631
22 A = 6786024
66 meter
Y = 5642149
03 meter E =
0016504
Z = 2828933
33 I = 51
27007
XDOT = -3903
389284 Wp = 101
03092
YDOT = 4254
583337 meter/sec RA = 267
95610 deg
ZDOT = -5053
118124 TA = 46
62564
MA = 46
48829
Ha = 222
147 n
mi
Hp = 213
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8109026
31 X = 2394614
38
Y = 18510987
62 feet Y = 5669358
03 meter
Z = 9281277
32 Z = 2840751
99
XDOT = -12806
395290 XDOT = -3926
130333
YDOT = 13958
606749 feet/sec YDOT = 4210
805538 meter/sec
ZDOT = -16578
471536 ZDOT = -5072
134402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20126497
02 X = 6134556
29
Y = -1540405
71 feet Y = -469515
66 meter
Z = 9333078
12 Z = 2844722
21
XDOT = 8916
358419 XDOT = 2717
706046
YDOT = 15100
265380 feet/sec YDOT = 4602
560888 meter/sec
ZDOT = -16663
711112 ZDOT = -5079
099147
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 18045
83520117
00016717 00000-0 10270-3 0 9169
2 25544 51
6393 268
6692 0003180 108
0535 252
0965 15
54085291 19483
Satellite: ISS
Catalog Number: 25544
Epoch time: 18045
83520117 = yrday
fracday
Element set: 916
Inclination: 51
6393 deg
RA of node: 268
6692 deg
Eccentricity:
0003180
Arg of perigee: 108
0535 deg
Mean anomaly: 252
0965 deg
Mean motion: 15
54085291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1948
Checksum: 316
Coasting Arc #18 (Orbit 1962)
---------------------------------------
Vector Time (GMT): 2018/046/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1829816
85 A = 6788716
44 meter
Y = -6407074
38 meter E =
0010367
Z = -1285265
00 I = 51
28246
XDOT = 4389
970937 Wp = 53
91335
YDOT = -2410
130687 meter/sec RA = 262
95636 deg
ZDOT = 5803
481818 TA = 292
03816
MA = 292
14824
Ha = 222
131 n
mi
Hp = 213
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6003336
13 X = -1751792
24
Y = -21020585
23 feet Y = -6427100
48 meter
Z = -4216748
69 Z = -1293963
44
XDOT = 14402
791788 XDOT = 4388
405865
YDOT = -7907
252909 feet/sec YDOT = -2361
047362 meter/sec
ZDOT = 19040
294678 ZDOT = 5824
802597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21836627
87 X = -6655804
17
Y = -863885
58 feet Y = -263312
32 meter
Z = -4254574
33 Z = -1296794
25
XDOT = -3132
563777 XDOT = -954
805439
YDOT = -14435
975985 feet/sec YDOT = -4400
085480 meter/sec
ZDOT = 19135
525405 ZDOT = 5832
508143
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 18046
79974612
00016717 00000-0 10270-3 0 9179
2 25544 51
6404 263
8613 0003067 107
4807 252
6681 15
54092169 19635
Satellite: ISS
Catalog Number: 25544
Epoch time: 18046
79974612 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 263
8613 deg
Eccentricity:
0003067
Arg of perigee: 107
4807 deg
Mean anomaly: 252
6681 deg
Mean motion: 15
54092169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1963
Checksum: 328
Coasting Arc #19 (Orbit 1978)
---------------------------------------
Vector Time (GMT): 2018/047/19:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1066012
13 A = 6789307
09 meter
Y = 6684779
21 meter E =
0014076
Z = -438753
26 I = 51
28893
XDOT = -4805
679339 Wp = 132
50852
YDOT = 383
560058 meter/sec RA = 257
96169 deg
ZDOT = -5964
043829 TA = 52
24620
MA = 52
11875
Ha = 222
113 n
mi
Hp = 213
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3497415
11 X = 993313
07
Y = 21931690
33 feet Y = 6696293
57 meter
Z = -1439479
18 Z = -433752
20
XDOT = -15766
664497 XDOT = -4780
641754
YDOT = 1258
399139 feet/sec YDOT = 329
959135 meter/sec
ZDOT = -19567
072930 ZDOT = -5987
326817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21990586
93 X = 6702730
90
Y = 3115453
77 feet Y = 949590
31 meter
Z = -1418128
33 Z = -432245
51
XDOT = -3182
408326 XDOT = -969
998058
YDOT = 13709
082072 feet/sec YDOT = 4178
528215 meter/sec
ZDOT = -19670
758112 ZDOT = -5995
647073
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 18047
82859123
00016717 00000-0 10270-3 0 9184
2 25544 51
6397 258
7324 0003130 112
2535 247
8950 15
54108702 19794
Satellite: ISS
Catalog Number: 25544
Epoch time: 18047
82859123 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 258
7324 deg
Eccentricity:
0003130
Arg of perigee: 112
2535 deg
Mean anomaly: 247
8950 deg
Mean motion: 15
54108702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1979
Checksum: 322
Coasting Arc #20 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2018/048/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4182302
14 A = 6782620
45 meter
Y = 3576600
53 meter E =
0013722
Z = 3954084
14 I = 51
26819
XDOT = -1668
070686 Wp = 84
13260
YDOT = 6352
105828 meter/sec RA = 255
72707 deg
ZDOT = -3968
063272 TA = 47
44856
MA = 47
33280
Ha = 221
982 n
mi
Hp = 213
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13721463
72 X = 4122790
37
Y = 11734253
71 feet Y = 3623037
52 meter
Z = 12972716
98 Z = 3974254
98
XDOT = -5472
672853 XDOT = -1719
703356
YDOT = 20840
242217 feet/sec YDOT = 6333
163258 meter/sec
ZDOT = -13018
580288 ZDOT = -3976
291979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17647884
45 X = -5379075
18
Y = 3492640
71 feet Y = 1064556
89 meter
Z = 13062017
37 Z = 3981302
89
XDOT = -12823
952430 XDOT = -3908
740701
YDOT = -15808
056685 feet/sec YDOT = -4818
295677 meter/sec
ZDOT = -13056
062748 ZDOT = -3979
487926
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 18048
27871039
00016717 00000-0 10270-3 0 9195
2 25544 51
6381 256
4914 0002977 102
0724 258
0762 15
54121242 19869
Satellite: ISS
Catalog Number: 25544
Epoch time: 18048
27871039 = yrday
fracday
Element set: 919
Inclination: 51
6381 deg
RA of node: 256
4914 deg
Eccentricity:
0002977
Arg of perigee: 102
0724 deg
Mean anomaly: 258
0762 deg
Mean motion: 15
54121242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 318
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