[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 16th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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
044/08:13:33
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
4
046/10:43:00
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
7
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
052/22:48:00
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
7
Coasting Arc #1 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2018/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4289077
69 A = 6779347
53 meter
Y = 2039615
57 meter E =
0014746
Z = -4851521
23 I = 51
25561
XDOT = -735
396032 Wp = 75
48652
YDOT = -7235
487169 meter/sec RA = 279
51361 deg
ZDOT = -2394
216884 TA = 170
89125
MA = 170
86447
Ha = 222
110 n
mi
Hp = 213
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14071777
19 X = -4288000
85
Y = 6691652
12 feet Y = 1991658
07 meter
Z = -15917064
41 Z = -4872353
04
XDOT = -2412
716640 XDOT = -642
802620
YDOT = -23738
474964 feet/sec YDOT = -7243
193202 meter/sec
ZDOT = -7855
042271 ZDOT = -2397
564060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15102125
25 X = -4603127
78
Y = -3427733
58 feet Y = -1044773
19 meter
Z = -16010075
46 Z = -4879871
00
XDOT = 12639
604037 XDOT = 3852
551311
YDOT = -18973
056211 feet/sec YDOT = -5782
987533 meter/sec
ZDOT = -7868
864224 ZDOT = -2398
429816
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
52031425
00016717 00000-0 10270-3 0 9005
2 25544 51
6413 280
2131 0002935 87
2723 272
8765 15
54098880 19125
Satellite: ISS
Catalog Number: 25544
Epoch time: 18043
52031425 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 280
2131 deg
Eccentricity:
0002935
Arg of perigee: 87
2723 deg
Mean anomaly: 272
8765 deg
Mean motion: 15
54098880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 294
Coasting Arc #2 (Orbit 1924)
---------------------------------------
Vector Time (GMT): 2018/044/08:13:33
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945393
13 A = 6778229
39 meter
Y = -2055109
65 meter E =
0016775
Z = -5129174
70 I = 51
24634
XDOT = 1864
588896 Wp = 99
20927
YDOT = -7275
682820 meter/sec RA = 275
25848 deg
ZDOT = 1482
430197 TA = 185
15916
MA = 185
17647
Ha = 222
204 n
mi
Hp = 213
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12944203
17 X = -3897204
89
Y = -6742485
72 feet Y = -2098960
46 meter
Z = -16828001
00 Z = -5148222
49
XDOT = 6117
417638 XDOT = 1938
608282
YDOT = -23870
350458 feet/sec YDOT = -7254
417794 meter/sec
ZDOT = 4863
616133 ZDOT = 1491
667502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7658182
03 X = 2334213
88
Y = -12309169
81 feet Y = -3751834
96 meter
Z = -16912472
13 Z = -5154921
51
XDOT = 22467
290965 XDOT = 6848
030286
YDOT = 7244
526736 feet/sec YDOT = 2208
131749 meter/sec
ZDOT = 4905
789667 ZDOT = 1495
284690
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
35626556
00016717 00000-0 10270-3 0 9013
2 25544 51
6398 276
0449 0003113 90
0398 270
1111 15
54083762 19254
Satellite: ISS
Catalog Number: 25544
Epoch time: 18044
35626556 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 276
0449 deg
Eccentricity:
0003113
Arg of perigee: 90
0398 deg
Mean anomaly: 270
1111 deg
Mean motion: 15
54083762 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1925
Checksum: 301
Coasting Arc #3 (Orbit 1940)
---------------------------------------
Vector Time (GMT): 2018/045/08:13:33
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3543274
75 A = 6781029
30 meter
Y = 3699869
67 meter E =
0012050
Z = 4434395
65 I = 51
25300
XDOT = -2635
149736 Wp = 75
27581
YDOT = 6431
812974 meter/sec RA = 270
23776 deg
ZDOT = -3250
393776 TA = 47
67299
MA = 47
57097
Ha = 222
119 n
mi
Hp = 213
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11624917
16 X = 3480099
06
Y = 12138680
01 feet Y = 3739139
96 meter
Z = 14548542
15 Z = 4451453
60
XDOT = -8645
504384 XDOT = -2691
087867
YDOT = 21101
748603 feet/sec YDOT = 6402
032004 meter/sec
ZDOT = -10664
021574 ZDOT = -3263
330243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12760667
07 X = -3889451
32
Y = 10837543
69 feet Y = 3303283
32 meter
Z = 14623930
83 Z = 4457374
12
XDOT = -19802
454159 XDOT = -6035
788028
YDOT = -8801
719847 feet/sec YDOT = -2682
764209 meter/sec
ZDOT = -10722
518381 ZDOT = -3268
223603
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
38512595
00016717 00000-0 10270-3 0 9025
2 25544 51
6391 270
9175 0003141 94
0767 266
0744 15
54080529 19413
Satellite: ISS
Catalog Number: 25544
Epoch time: 18045
38512595 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 270
9175 deg
Eccentricity:
0003141
Arg of perigee: 94
0767 deg
Mean anomaly: 266
0744 deg
Mean motion: 15
54080529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1941
Checksum: 312
Coasting Arc #4 (Orbit 1955)
---------------------------------------
Vector Time (GMT): 2018/046/08:13:33
000
Vector Time (MET): N/A
Weight (LBS) : 905723
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3089610
52 A = 6784707
72 meter
Y = -5054714
24 meter E =
0007729
Z = -3313881
39 I = 51
26667
XDOT = 3328
673154 Wp = 90
90391
YDOT = -5085
773048 meter/sec RA = 265
22466 deg
ZDOT = 4663
350118 TA = 230
35255
MA = 230
42077
Ha = 222
135 n
mi
Hp = 213
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10136517
44 X = -3016761
04
Y = -16583708
14 feet Y = -5088857
27 meter
Z = -10872314
28 Z = -3328712
01
XDOT = 10920
843680 XDOT = 3362
644741
YDOT = -16685
607114 feet/sec YDOT = -5048
359302 meter/sec
ZDOT = 15299
705111 ZDOT = 4679
602065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16957771
18 X = 5168728
66
Y = -9422217
86 feet Y = -2871892
00 meter
Z = -10937613
38 Z = -3333784
56
XDOT = 15570
804631 XDOT = 4745
981252
YDOT = 10213
965076 feet/sec YDOT = 3113
216555 meter/sec
ZDOT = 15372
752565 ZDOT = 4685
614982
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
34968029
00016717 00000-0 10270-3 0 9030
2 25544 51
6394 266
1091 0003045 98
0116 262
1382 15
54097739 19567
Satellite: ISS
Catalog Number: 25544
Epoch time: 18046
34968029 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 266
1091 deg
Eccentricity:
0003045
Arg of perigee: 98
0116 deg
Mean anomaly: 262
1382 deg
Mean motion: 15
54097739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1956
Checksum: 321
Coasting Arc #5 (Orbit 1957)
---------------------------------------
Vector Time (GMT): 2018/046/10:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 436363
42 A = 6789522
65 meter
Y = 6765669
77 meter E =
0014190
Z = -232701
50 I = 51
28367
XDOT = -4802
007663 Wp = 129
49196
YDOT = 112
812875 meter/sec RA = 264
73308 deg
ZDOT = -5978
012849 TA = 53
02780
MA = 52
89797
Ha = 222
182 n
mi
Hp = 213
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1431638
52 X = 361805
75
Y = 22197079
28 feet Y = 6770132
59 meter
Z = -763456
38 Z = -230763
37
XDOT = -15754
618316 XDOT = -4773
874988
YDOT = 370
120981 feet/sec YDOT = 59
270444 meter/sec
ZDOT = -19612
903048 ZDOT = -6001
270413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17292837
75 X = -5270856
94
Y = 13990330
48 feet Y = 4264252
73 meter
Z = -755777
04 Z = -230360
84
XDOT = -8303
107442 XDOT = -2530
787148
YDOT = -11282
881115 feet/sec YDOT = -3439
022164 meter/sec
ZDOT = -19716
433860 ZDOT = -6009
569041
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
47828725
00016717 00000-0 10270-3 0 9043
2 25544 51
6405 265
4692 0002986 101
4373 258
7115 15
54054152 19585
Satellite: ISS
Catalog Number: 25544
Epoch time: 18046
47828725 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 265
4692 deg
Eccentricity:
0002986
Arg of perigee: 101
4373 deg
Mean anomaly: 258
7115 deg
Mean motion: 15
54054152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1958
Checksum: 322
Coasting Arc #6 (Orbit 1973)
---------------------------------------
Vector Time (GMT): 2018/047/10:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 349209
54 A = 6787909
94 meter
Y = -6507201
53 meter E =
0016420
Z = 1874993
76 I = 51
28247
XDOT = 4898
687171 Wp = 72
15701
YDOT = 1884
988552 meter/sec RA = 259
73605 deg
ZDOT = 5593
965701 TA = 308
59908
MA = 308
74602
Ha = 222
055 n
mi
Hp = 213
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1145700
59 X = 412841
37
Y = -21349086
39 feet Y = -6502940
49 meter
Z = 6151554
32 Z = 1876845
12
XDOT = 16071
808304 XDOT = 4850
072771
YDOT = 6184
345642 feet/sec YDOT = 1939
497666 meter/sec
ZDOT = 18352
905842 ZDOT = 5617
643013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17868648
33 X = 5446364
01
Y = -11734355
26 feet Y = -3576631
48 meter
Z = 6160686
14 Z = 1877777
13
XDOT = 3589
191159 XDOT = 1093
985465
YDOT = 15217
359653 feet/sec YDOT = 4638
251222 meter/sec
ZDOT = 18458
034557 ZDOT = 5626
008933
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
50714045
00016717 00000-0 10270-3 0 9058
2 25544 51
6402 260
3396 0002849 99
8112 260
3363 15
54104121 19740
Satellite: ISS
Catalog Number: 25544
Epoch time: 18047
50714045 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 260
3396 deg
Eccentricity:
0002849
Arg of perigee: 99
8112 deg
Mean anomaly: 260
3363 deg
Mean motion: 15
54104121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1974
Checksum: 292
Coasting Arc #7 (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 = 4192368
60 A = 6782580
83 meter
Y = 3537953
79 meter E =
0013682
Z = 3978087
67 I = 51
26770
XDOT = -1635
519264 Wp = 83
71634
YDOT = 6379
760971 meter/sec RA = 255
72738 deg
ZDOT = -3937
123226 TA = 47
47064
MA = 47
35517
Ha = 222
019 n
mi
Hp = 213
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13754490
15 X = 4133171
64
Y = 11607459
93 feet Y = 3584505
11 meter
Z = 13051468
74 Z = 3998308
18
XDOT = -5365
876851 XDOT = -1687
613889
YDOT = 20930
974315 feet/sec YDOT = 6361
179833 meter/sec
ZDOT = -12917
070952 ZDOT = -3945
194938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17568148
32 X = -5354771
61
Y = 3596437
94 feet Y = 1096194
29 meter
Z = 13140995
40 Z = 4005375
40
XDOT = -12953
267099 XDOT = -3948
155812
YDOT = -15786
321886 feet/sec YDOT = -4811
670911 meter/sec
ZDOT = -12953
858340 ZDOT = -3948
336022
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
27878125
00016717 00000-0 10270-3 0 9064
2 25544 51
6379 256
4918 0003015 101
5616 258
5875 15
54106744 19868
Satellite: ISS
Catalog Number: 25544
Epoch time: 18048
27878125 = yrday
fracday
Element set: 906
Inclination: 51
6379 deg
RA of node: 256
4918 deg
Eccentricity:
0003015
Arg of perigee: 101
5616 deg
Mean anomaly: 258
5875 deg
Mean motion: 15
54106744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1986
Checksum: 336
Coasting Arc #8 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2018/049/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3964366
95 A = 6786315
78 meter
Y = -4809637
30 meter E =
0007155
Z = -2687554
20 I = 51
28881
XDOT = 2617
025284 Wp = 75
10772
YDOT = -5029
753165 meter/sec RA = 250
72038 deg
ZDOT = 5154
236869 TA = 254
39968
MA = 254
47866
Ha = 222
096 n
mi
Hp = 213
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13006453
26 X = -3897235
18
Y = -15779649
93 feet Y = -4853594
49 meter
Z = -8817435
04 Z = -2706647
81
XDOT = 8586
040957 XDOT = 2648
038765
YDOT = -16501
814845 feet/sec YDOT = -5000
313864 meter/sec
ZDOT = 16910
225949 ZDOT = 5167
025053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20396544
96 X = 6216866
90
Y = -807110
28 feet Y = -246007
21 meter
Z = -8901790
03 Z = -2713265
60
XDOT = 7988
927025 XDOT = 2435
024957
YDOT = 15225
297533 feet/sec YDOT = 4640
670688 meter/sec
ZDOT = 16967
813469 ZDOT = 5171
789545
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 18049
24333015
00016717 00000-0 10270-3 0 9077
2 25544 51
6376 251
6839 0002974 106
1866 253
9614 15
54090328 20014
Satellite: ISS
Catalog Number: 25544
Epoch time: 18049
24333015 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 251
6839 deg
Eccentricity:
0002974
Arg of perigee: 106
1866 deg
Mean anomaly: 253
9614 deg
Mean motion: 15
54090328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 305
Coasting Arc #9 (Orbit 2016)
---------------------------------------
Vector Time (GMT): 2018/050/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3516022
54 A = 6788908
10 meter
Y = 5697714
45 meter E =
0016532
Z = 1076920
59 I = 51
31076
XDOT = -3633
128274 Wp = 120
82148
YDOT = 3360
849901 meter/sec RA = 245
72262 deg
ZDOT = -5860
904784 TA = 47
43939
MA = 47
29997
Ha = 222
067 n
mi
Hp = 213
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11535507
02 X = 3446816
81
Y = 18693288
88 feet Y = 5736646
19 meter
Z = 3533204
04 Z = 1093831
26
XDOT = -11919
712184 XDOT = -3641
971447
YDOT = 11026
410437 feet/sec YDOT = 3320
171709 meter/sec
ZDOT = -19228
690236 ZDOT = -5878
574811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21886488
24 X = -6671001
62
Y = -1719400
72 feet Y = -524073
34 meter
Z = 3607741
10 Z = 1099639
49
XDOT = -2080
268412 XDOT = -634
065812
YDOT = -14428
734729 feet/sec YDOT = -4397
878345 meter/sec
ZDOT = -19307
782672 ZDOT = -5885
012158
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 18050
27217979
00016717 00000-0 10270-3 0 9083
2 25544 51
6390 246
5545 0002960 109
6568 250
4904 15
54098365 20179
Satellite: ISS
Catalog Number: 25544
Epoch time: 18050
27217979 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 246
5545 deg
Eccentricity:
0002960
Arg of perigee: 109
6568 deg
Mean anomaly: 250
4904 deg
Mean motion: 15
54098365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2017
Checksum: 326
Coasting Arc #10 (Orbit 2032)
---------------------------------------
Vector Time (GMT): 2018/051/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2874113
25 A = 6789272
21 meter
Y = -6114878
36 meter E =
0014789
Z = 602861
39 I = 51
32612
XDOT = 4583
873552 Wp = 61
42897
YDOT = -1557
876739 meter/sec RA = 240
73024 deg
ZDOT = 5947
404012 TA = 305
10741
MA = 305
24596
Ha = 222
072 n
mi
Hp = 213
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9429505
42 X = -2808449
77
Y = -20061936
88 feet Y = -6146651
46 meter
Z = 1977891
71 Z = 589060
22
XDOT = 15038
955222 XDOT = 4572
064459
YDOT = -5111
144156 feet/sec YDOT = -1506
682144 meter/sec
ZDOT = 19512
480353 ZDOT = 5969
642087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21840807
83 X = 6657078
23
Y = 3822598
78 feet Y = 1165128
11 meter
Z = 1917235
37 Z = 584373
34
XDOT = -4122
586920 XDOT = -1256
564493
YDOT = 13541
454420 feet/sec YDOT = 4127
435307 meter/sec
ZDOT = 19611
674646 ZDOT = 5977
638432
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 18051
30102653
00016717 00000-0 10270-3 0 9091
2 25544 51
6388 241
4258 0002954 111
1516 248
9952 15
54099167 20339
Satellite: ISS
Catalog Number: 25544
Epoch time: 18051
30102653 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 241
4258 deg
Eccentricity:
0002954
Arg of perigee: 111
1516 deg
Mean anomaly: 248
9952 deg
Mean motion: 15
54099167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2033
Checksum: 304
Coasting Arc #11 (Orbit 2047)
---------------------------------------
Vector Time (GMT): 2018/052/05:42:30
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1954208
43 A = 6787230
27 meter
Y = 6090089
70 meter E =
0008776
Z = -2266742
50 I = 51
33734
XDOT = -5421
461806 Wp = 129
78552
YDOT = -267
454540 meter/sec RA = 235
73715 deg
ZDOT = -5412
030198 TA = 75
54272
MA = 75
44536
Ha = 222
040 n
mi
Hp = 213
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6411444
97 X = 1896972
69
Y = 19980609
26 feet Y = 6111622
77 meter
Z = -7436819
23 Z = -2257389
29
XDOT = -17786
948184 XDOT = -5391
779572
YDOT = -877
475526 feet/sec YDOT = -327
915576 meter/sec
ZDOT = -17756
004585 ZDOT = -5438
293421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20161846
49 X = -6145330
81
Y = -5868352
06 feet Y = -1788673
71 meter
Z = -7395947
78 Z = -2254284
88
XDOT = 10217
477091 XDOT = 3114
287017
YDOT = -12659
753807 feet/sec YDOT = -3858
692960 meter/sec
ZDOT = -17872
891678 ZDOT = -5447
657384
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 18052
26556860
00016717 00000-0 10270-3 0 9102
2 25544 51
6398 236
6180 0002925 115
5415 244
6040 15
54107941 20481
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
26556860 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 236
6180 deg
Eccentricity:
0002925
Arg of perigee: 115
5415 deg
Mean anomaly: 244
6040 deg
Mean motion: 15
54107941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2048
Checksum: 297
Coasting Arc #12 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2018/052/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -107849
57 A = 6781897
90 meter
Y = 5335181
25 meter E =
0010149
Z = -4194965
28 I = 51
33259
XDOT = -6028
358344 Wp = 84
08815
YDOT = -2992
452560 meter/sec RA = 232
17657 deg
ZDOT = -3657
460010 TA = 148
24113
MA = 148
17988
Ha = 222
040 n
mi
Hp = 213
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -353837
19 X = -147124
23
Y = 17503875
49 feet Y = 5333755
27 meter
Z = -13763009
44 Z = -4195584
98
XDOT = -19778
078557 XDOT = -5976
682020
YDOT = -9817
757744 feet/sec YDOT = -3059
577155 meter/sec
ZDOT = -11999
540715 ZDOT = -3686
617698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12994355
75 X = 3960679
63
Y = -11728735
97 feet Y = -3574918
72 meter
Z = -13766435
92 Z = -4196009
67
XDOT = 5372
484162 XDOT = 1637
533173
YDOT = 20162
922597 feet/sec YDOT = 6145
658808 meter/sec
ZDOT = -12128
980136 ZDOT = -3696
913145
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 18052
97289707
00016717 00000-0 10270-3 0 9114
2 25544 51
6392 233
0916 0003099 120
5032 239
6427 15
54120647 20590
Satellite: ISS
Catalog Number: 25544
Epoch time: 18052
97289707 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 233
0916 deg
Eccentricity:
0003099
Arg of perigee: 120
5032 deg
Mean anomaly: 239
6427 deg
Mean motion: 15
54120647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 308
Coasting Arc #13 (Orbit 2074)
---------------------------------------
Vector Time (GMT): 2018/053/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1410584
11 A = 6778729
07 meter
Y = -4354888
38 meter E =
0009033
Z = 4994580
10 I = 51
34233
XDOT = 6082
700113 Wp = 123
27275
YDOT = 4240
196954 meter/sec RA = 227
16207 deg
ZDOT = 1971
773309 TA = 307
47184
MA = 307
55395
Ha = 222
001 n
mi
Hp = 213
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4627900
62 X = 1434915
97
Y = -14287691
53 feet Y = -4338977
90 meter
Z = 16386417
66 Z = 5001491
54
XDOT = 19956
365199 XDOT = 6025
255248
YDOT = 13911
407329 feet/sec YDOT = 4307
896812 meter/sec
ZDOT = 6469
072536 ZDOT = 2001
180927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13426166
88 X = -4092295
66
Y = 6653303
28 feet Y = 2027926
84 meter
Z = 16417730
53 Z = 5004124
27
XDOT = -3305
189848 XDOT = -1007
421866
YDOT = -23014
961116 feet/sec YDOT = -7014
960148 meter/sec
ZDOT = 6599
486347 ZDOT = 2011
523438
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 18054
00173795
00016717 00000-0 10270-3 0 9120
2 25544 51
6386 227
9621 0003099 121
9082 238
2372 15
54115067 20750
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
00173795 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 227
9621 deg
Eccentricity:
0003099
Arg of perigee: 121
9082 deg
Mean anomaly: 238
2372 deg
Mean motion: 15
54115067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2075
Checksum: 304
Coasting Arc #14 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2018/054/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2792501
50 A = 6777441
52 meter
Y = 3190065
56 meter E =
0017390
Z = -5302653
64 I = 51
36033
XDOT = -5709
751471 Wp = 95
46440
YDOT = -5099
469499 meter/sec RA = 222
14395 deg
ZDOT = -62
742835 TA = 173
94495
MA = 173
92390
Ha = 222
010 n
mi
Hp = 213
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9161750
33 X = -2802208
91
Y = 10466094
35 feet Y = 3158783
37 meter
Z = -17397157
62 Z = -5316242
23
XDOT = -18732
780418 XDOT = -5651
998696
YDOT = -16730
542977 feet/sec YDOT = -5162
996948 meter/sec
ZDOT = -205
849196 ZDOT = -90
338032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13798394
54 X = 4205750
66
Y = -978955
95 feet Y = -298385
77 meter
Z = -17458059
65 Z = -5321216
58
XDOT = 1300
111897 XDOT = 396
274106
YDOT = 24071
321845 feet/sec YDOT = 7336
938898 meter/sec
ZDOT = -328
107113 ZDOT = -100
007048
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 18054
96627396
00016717 00000-0 10270-3 0 9137
2 25544 51
6379 223
1548 0003015 125
5506 234
5928 15
54101760 20905
Satellite: ISS
Catalog Number: 25544
Epoch time: 18054
96627396 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 223
1548 deg
Eccentricity:
0003015
Arg of perigee: 125
5506 deg
Mean anomaly: 234
5928 deg
Mean motion: 15
54101760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 306
Coasting Arc #15 (Orbit 2105)
---------------------------------------
Vector Time (GMT): 2018/055/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4095213
45 A = 6778453
41 meter
Y = -1942808
20 meter E =
0006860
Z = 5034535
77 I = 51
38777
XDOT = 4927
369305 Wp = 79
89996
YDOT = 5583
309320 meter/sec RA = 217
12624 deg
ZDOT = -1850
130792 TA = 28
09229
MA = 28
05529
Ha = 221
784 n
mi
Hp = 213
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13435739
65 X = 4092179
31
Y = -6374042
66 feet Y = -1897029
49 meter
Z = 16517505
80 Z = 5054421
32
XDOT = 16165
909792 XDOT = 4873
555851
YDOT = 18317
943964 feet/sec YDOT = 5638
109589 meter/sec
ZDOT = -6069
982915 ZDOT = -1826
326587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14003898
52 X = -4268388
27
Y = -4700742
99 feet Y = -1432786
46 meter
Z = 16606304
81 Z = 5061601
71
XDOT = 772
321469 XDOT = 235
403584
YDOT = -23410
519513 feet/sec YDOT = -7135
526348 meter/sec
ZDOT = -5964
644403 ZDOT = -1818
023614
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 18055
99511054
00016717 00000-0 10270-3 0 9145
2 25544 51
6365 218
0258 0002911 129
5219 230
6192 15
54124014 21065
Satellite: ISS
Catalog Number: 25544
Epoch time: 18055
99511054 = yrday
fracday
Element set: 914
Inclination: 51
6365 deg
RA of node: 218
0258 deg
Eccentricity:
0002911
Arg of perigee: 129
5219 deg
Mean anomaly: 230
6192 deg
Mean motion: 15
54124014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2106
Checksum: 284
Coasting Arc #16 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2018/056/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5230415
45 A = 6781573
34 meter
Y = 733654
32 meter E =
0011215
Z = -4265634
00 I = 51
42543
XDOT = -3700
891048 Wp = 115
74064
YDOT = -5678
964044 meter/sec RA = 212
11676 deg
ZDOT = 3563
764826 TA = 190
77683
MA = 190
80088
Ha = 221
933 n
mi
Hp = 213
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17160155
68 X = -5217510
82
Y = 2407002
37 feet Y = 675236
22 meter
Z = -13994862
19 Z = -4291009
76
XDOT = -12142
030996 XDOT = -3654
422850
YDOT = -18631
771797 feet/sec YDOT = -5720
089993 meter/sec
ZDOT = 11692
141817 ZDOT = 3545
900590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14101187
80 X = 4298042
04
Y = 9911717
61 feet Y = 3021091
53 meter
Z = -14107981
01 Z = -4300112
61
XDOT = -3095
783161 XDOT = -943
594707
YDOT = 20922
330543 feet/sec YDOT = 6377
126350 meter/sec
ZDOT = 11613
249431 ZDOT = 3539
718427
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 18056
95964251
00016717 00000-0 10270-3 0 9154
2 25544 51
6371 213
2178 0002915 129
9724 230
1685 15
54105258 21217
Satellite: ISS
Catalog Number: 25544
Epoch time: 18056
95964251 = yrday
fracday
Element set: 915
Inclination: 51
6371 deg
RA of node: 213
2178 deg
Eccentricity:
0002915
Arg of perigee: 129
9724 deg
Mean anomaly: 230
1685 deg
Mean motion: 15
54105258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 305
Coasting Arc #17 (Orbit 2136)
---------------------------------------
Vector Time (GMT): 2018/057/22:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 920849
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6054273
83 A = 6785294
31 meter
Y = 397791
99 meter E =
0015315
Z = 3020636
42 I = 51
46602
XDOT = 2107
535501 Wp = 102
46420
YDOT = 5489
831949 meter/sec RA = 207
11826 deg
ZDOT = -4929
209982 TA = 42
80348
MA = 42
68433
Ha = 221
689 n
mi
Hp = 213
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19863103
11 X = 6034703
32
Y = 1305091
83 feet Y = 465385
76 meter
Z = 9910224
49 Z = 3049997
78
XDOT = 6914
486551 XDOT = 2069
933047
YDOT = 18011
259676 feet/sec YDOT = 5513
189362 meter/sec
ZDOT = -16171
948761 ZDOT = -4919
064140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13803282
34 X = -4207240
46
Y = -14251554
02 feet Y = -4343873
66 meter
Z = 10040980
24 Z = 3060490
78
XDOT = 5838
758650 XDOT = 1779
653636
YDOT = -17058
545253 feet/sec YDOT = -5199
444593 meter/sec
ZDOT = -16127
397591 ZDOT = -4915
630786
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 18057
98847269
00016717 00000-0 10270-3 0 9168
2 25544 51
6364 208
0882 0002721 132
9187 227
2194 15
54149921 21379
Satellite: ISS
Catalog Number: 25544
Epoch time: 18057
98847269 = yrday
fracday
Element set: 916
Inclination: 51
6364 deg
RA of node: 208
0882 deg
Eccentricity:
0002721
Arg of perigee: 132
9187 deg
Mean anomaly: 227
2194 deg
Mean motion: 15
54149921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2137
Checksum: 331
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