[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 14th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 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
137/14:37:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
5
000/00:00:00
000 0
0 0
0 213
3
138/21:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
4
140/09:04:46
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
4
142/00:19:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
4
144/12:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
4
146/20:57:30
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
148/06:00:00
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
8
Coasting Arc #1 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2018/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6056330
72 A = 6786433
14 meter
Y = 1533811
87 meter E =
0008464
Z = -2652793
54 I = 51
60684
XDOT = -3406
432866 Wp = 70
00178
YDOT = -4470
760790 meter/sec RA = 185
44972 deg
ZDOT = 5208
301479 TA = 260
08631
MA = 260
18186
Ha = 222
479 n
mi
Hp = 213
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19869851
44 X = -6060145
94
Y = 5032191
16 feet Y = 1466064
59 meter
Z = -8703390
88 Z = -2682222
95
XDOT = -11175
960848 XDOT = -3381
486165
YDOT = -14667
850360 feet/sec YDOT = -4508
714613 meter/sec
ZDOT = 17087
603278 ZDOT = 5191
814237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8458175
68 X = -2578051
95
Y = 18608735
03 feet Y = 5671942
44 meter
Z = -8834998
67 Z = -2692907
60
XDOT = -17147
441373 XDOT = -5226
540130
YDOT = 259
023024 feet/sec YDOT = 78
950218 meter/sec
ZDOT = 17014
490187 ZDOT = 5186
016609
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 18134
50543685
00016717 00000-0 10270-3 0 9000
2 25544 51
6386 186
6192 0003886 87
0681 273
0916 15
54065806 33272
Satellite: ISS
Catalog Number: 25544
Epoch time: 18134
50543685 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 186
6192 deg
Eccentricity:
0003886
Arg of perigee: 87
0681 deg
Mean anomaly: 273
0916 deg
Mean motion: 15
54065806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 326
Coasting Arc #2 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2018/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6656180
31 A = 6788965
57 meter
Y = -772276
50 meter E =
0016957
Z = 1045815
08 I = 51
64834
XDOT = 1479
630813 Wp = 116
11490
YDOT = 4677
608205 meter/sec RA = 180
47531 deg
ZDOT = -5896
195501 TA = 52
54477
MA = 52
39064
Ha = 222
480 n
mi
Hp = 213
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21837861
90 X = 6659241
28
Y = -2533715
56 feet Y = -697825
47 meter
Z = 3431151
85 Z = 1078156
61
XDOT = 4854
431800 XDOT = 1455
855798
YDOT = 15346
483611 feet/sec YDOT = 4694
021926 meter/sec
ZDOT = -19344
473427 ZDOT = -5889
065231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11338144
48 X = 3455866
44
Y = -18808125
88 feet Y = -5732716
77 meter
Z = 3575697
18 Z = 1089872
50
XDOT = 13815
864733 XDOT = 4211
075571
YDOT = 4616
901118 feet/sec YDOT = 1407
231461 meter/sec
ZDOT = -19313
171238 ZDOT = -5886
654593
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 18135
53431844
00016717 00000-0 10270-3 0 9018
2 25544 51
6387 181
4901 0003875 88
4115 271
7482 15
54081605 33435
Satellite: ISS
Catalog Number: 25544
Epoch time: 18135
53431844 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 181
4901 deg
Eccentricity:
0003875
Arg of perigee: 88
4115 deg
Mean anomaly: 271
7482 deg
Mean motion: 15
54081605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 307
Coasting Arc #3 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2018/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6754240
76 A = 6789486
14 meter
Y = 38334
19 meter E =
0016421
Z = 621137
30 I = 51
68224
XDOT = 532
557202 Wp = 60
24821
YDOT = -4778
508543 meter/sec RA = 175
50730 deg
ZDOT = 5975
419319 TA = 306
45448
MA = 306
60573
Ha = 222
621 n
mi
Hp = 213
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22159582
56 X = -6757184
65
Y = 125768
33 feet Y = -37212
90 meter
Z = 2037852
03 Z = 588319
73
XDOT = 1747
234915 XDOT = 556
926190
YDOT = -15677
521467 feet/sec YDOT = -4772
417418 meter/sec
ZDOT = 19604
394090 ZDOT = 5978
065097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13156669
73 X = -4010152
94
Y = 17847716
89 feet Y = 5439984
11 meter
Z = 1891243
25 Z = 576450
94
XDOT = -10296
408825 XDOT = -3138
345410
YDOT = -9710
229201 feet/sec YDOT = -2959
677861 meter/sec
ZDOT = 19616
775120 ZDOT = 5979
193057
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 18136
56319776
00016717 00000-0 10270-3 0 9022
2 25544 51
6386 176
3617 0004008 89
0723 271
0889 15
54027288 33590
Satellite: ISS
Catalog Number: 25544
Epoch time: 18136
56319776 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 176
3617 deg
Eccentricity:
0004008
Arg of perigee: 89
0723 deg
Mean anomaly: 271
0889 deg
Mean motion: 15
54027288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 336
Coasting Arc #4 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2018/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6346816
80 A = 6787340
93 meter
Y = 766007
37 meter E =
0009388
Z = -2278403
71 I = 51
70872
XDOT = -2521
260505 Wp = 120
59207
YDOT = 4773
975842 meter/sec RA = 170
53939 deg
ZDOT = -5439
641331 TA = 84
73157
MA = 84
62446
Ha = 222
573 n
mi
Hp = 213
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20822889
76 X = 6348846
84
Y = 2513147
53 feet Y = 836993
44 meter
Z = -7475077
80 Z = -2247567
57
XDOT = -8271
852051 XDOT = -2548
033697
YDOT = 15662
650401 feet/sec YDOT = 4745
632275 meter/sec
ZDOT = -17846
592294 ZDOT = -5451
953437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14229739
02 X = 4337224
45
Y = -15474580
32 feet Y = -4716652
08 meter
Z = -7337392
45 Z = -2236437
22
XDOT = 6821
899034 XDOT = 2079
314826
YDOT = 14727
748201 feet/sec YDOT = 4489
017652 meter/sec
ZDOT = -17902
168115 ZDOT = -5456
580841
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 18137
52776486
00016717 00000-0 10270-3 0 9035
2 25544 51
6390 171
5536 0003994 94
7119 265
4489 15
54081467 33746
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
52776486 = yrday
fracday
Element set: 903
Inclination: 51
6390 deg
RA of node: 171
5536 deg
Eccentricity:
0003994
Arg of perigee: 94
7119 deg
Mean anomaly: 265
4489 deg
Mean motion: 15
54081467 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 345
Coasting Arc #5 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2018/137/14:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 149946
63 A = 6777701
73 meter
Y = -4255002
10 meter E =
0006731
Z = 5267890
66 I = 51
67650
XDOT = 7599
888718 Wp = 80
28836
YDOT = -711
168568 meter/sec RA = 169
96891 deg
ZDOT = -788
784911 TA = 17
25176
MA = 17
22890
Ha = 222
511 n
mi
Hp = 213
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 491950
90 X = 171927
06
Y = -13959980
66 feet Y = -4253202
99 meter
Z = 17283105
84 Z = 5268671
97
XDOT = 24934
018104 XDOT = 7611
107918
YDOT = -2333
230210 feet/sec YDOT = -626
118563 meter/sec
ZDOT = -2587
877005 ZDOT = -751
839548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13953436
06 X = -4253007
31
Y = 535331
53 feet Y = 163169
05 meter
Z = 17287101
13 Z = 5269108
42
XDOT = -3919
846681 XDOT = -1194
769268
YDOT = -23727
276797 feet/sec YDOT = -7232
073968 meter/sec
ZDOT = -2422
717455 ZDOT = -738
444280
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 18137
65637346
00016717 00000-0 10270-3 0 9041
2 25544 51
6354 170
9128 0003871 94
0139 266
1456 15
54067750 33768
Satellite: ISS
Catalog Number: 25544
Epoch time: 18137
65637346 = yrday
fracday
Element set: 904
Inclination: 51
6354 deg
RA of node: 170
9128 deg
Eccentricity:
0003871
Arg of perigee: 94
0139 deg
Mean anomaly: 266
1456 deg
Mean motion: 15
54067750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 323
Coasting Arc #6 (Orbit 3390)
---------------------------------------
Vector Time (GMT): 2018/138/14:37:30
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1876702
00 A = 6779782
57 meter
Y = 4423930
83 meter E =
0015290
Z = -4796954
07 I = 51
71591
XDOT = -7190
485545 Wp = 105
77072
YDOT = -211
834434 meter/sec RA = 164
97640 deg
ZDOT = 2620
657379 TA = 190
06770
MA = 190
09836
Ha = 222
547 n
mi
Hp = 213
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6157158
80 X = -1902730
82
Y = 14514208
76 feet Y = 4402799
29 meter
Z = -15738038
30 Z = -4806133
23
XDOT = -23590
831841 XDOT = -7200
312238
YDOT = -694
994862 feet/sec YDOT = -292
298648 meter/sec
ZDOT = 8597
957281 ZDOT = 2585
704251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14962844
06 X = 4560674
87
Y = 4834942
94 feet Y = 1473690
61 meter
Z = -15779586
00 Z = -4809617
81
XDOT = 1611
557596 XDOT = 491
202755
YDOT = 22532
746899 feet/sec YDOT = 6867
981255 meter/sec
ZDOT = 8441
781315 ZDOT = 2573
054945
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 18138
62093963
00016717 00000-0 10270-3 0 9051
2 25544 51
6357 166
1050 0003917 96
8223 263
3376 15
54048827 33918
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
62093963 = yrday
fracday
Element set: 905
Inclination: 51
6357 deg
RA of node: 166
1050 deg
Eccentricity:
0003917
Arg of perigee: 96
8223 deg
Mean anomaly: 263
3376 deg
Mean motion: 15
54048827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3391
Checksum: 323
Coasting Arc #7 (Orbit 3394)
---------------------------------------
Vector Time (GMT): 2018/138/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5872781
40 A = 6788323
84 meter
Y = 3014450
23 meter E =
0010329
Z = -1574016
48 I = 51
75744
XDOT = -3440
890964 Wp = 56
18725
YDOT = -3716
478279 meter/sec RA = 163
66052 deg
ZDOT = 5753
388469 TA = 286
63629
MA = 286
74968
Ha = 222
370 n
mi
Hp = 213
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19267655
51 X = -5898407
52
Y = 9889928
59 feet Y = 2948633
65 meter
Z = -5164096
07 Z = -1602606
55
XDOT = -11289
012349 XDOT = -3427
023715
YDOT = -12193
170207 feet/sec YDOT = -3754
879835 meter/sec
ZDOT = 18875
946422 ZDOT = 5736
706911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17081239
09 X = 5206361
68
Y = -13264415
89 feet Y = -4042993
96 meter
Z = -5292227
03 Z = -1613070
80
XDOT = 12497
581345 XDOT = 3809
262794
YDOT = 8633
969329 feet/sec YDOT = 2631
633852 meter/sec
ZDOT = 18801
838438 ZDOT = 5730
800356
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 18138
87815676
00016717 00000-0 10270-3 0 9062
2 25544 51
6398 164
8238 0003695 97
1074 263
0499 15
54092873 33954
Satellite: ISS
Catalog Number: 25544
Epoch time: 18138
87815676 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 164
8238 deg
Eccentricity:
0003695
Arg of perigee: 97
1074 deg
Mean anomaly: 263
0499 deg
Mean motion: 15
54092873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3395
Checksum: 360
Coasting Arc #8 (Orbit 3410)
---------------------------------------
Vector Time (GMT): 2018/139/21:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6357328
16 A = 6789562
86 meter
Y = -2362216
27 meter E =
0015221
Z = -137810
98 I = 51
79289
XDOT = 1546
523241 Wp = 127
93717
YDOT = 4486
612140 meter/sec RA = 158
69980 deg
ZDOT = -6024
358364 TA = 53
54434
MA = 53
40415
Ha = 222
513 n
mi
Hp = 213
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20857375
84 X = 6383940
03
Y = -7750053
38 feet Y = -2290975
44 meter
Z = -452135
75 Z = -106864
77
XDOT = 5073
895146 XDOT = 1525
501047
YDOT = 14719
856104 feet/sec YDOT = 4503
789545 meter/sec
ZDOT = -19764
955262 ZDOT = -6016
896427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18874493
57 X = -5752945
64
Y = 11787835
82 feet Y = 3592932
36 meter
Z = -313528
83 Z = -95563
59
XDOT = -7199
290553 XDOT = -2194
343760
YDOT = -11994
114054 feet/sec YDOT = -3655
805964 meter/sec
ZDOT = -19732
138570 ZDOT = -6014
355836
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 18139
90702223
00016717 00000-0 10270-3 0 9071
2 25544 51
6403 159
6953 0003771 102
2574 257
9001 15
54046963 34114
Satellite: ISS
Catalog Number: 25544
Epoch time: 18139
90702223 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 159
6953 deg
Eccentricity:
0003771
Arg of perigee: 102
2574 deg
Mean anomaly: 257
9001 deg
Mean motion: 15
54046963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3411
Checksum: 299
Coasting Arc #9 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2018/140/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1539037
65 A = 6780132
30 meter
Y = -4681797
22 meter E =
0011155
Z = 4648243
11 I = 51
77649
XDOT = 7066
396047 Wp = 77
08584
YDOT = -596
471173 meter/sec RA = 156
17067 deg
ZDOT = -2932
116331 TA = 42
05931
MA = 41
97373
Ha = 222
293 n
mi
Hp = 213
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5049336
13 X = 1568697
64
Y = -15360227
09 feet Y = -4664421
27 meter
Z = 15250141
44 Z = 4655790
81
XDOT = 23183
714066 XDOT = 7086
783471
YDOT = -1956
926419 feet/sec YDOT = -517
335577 meter/sec
ZDOT = -9619
804237 ZDOT = -2897
740685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1284379
37 X = 391478
83
Y = -16085253
63 feet Y = -4902785
31 meter
Z = 15284442
12 Z = 4658697
96
XDOT = 21000
962800 XDOT = 6401
093461
YDOT = -7343
880476 feet/sec YDOT = -2238
414769 meter/sec
ZDOT = -9466
067422 ZDOT = -2885
257350
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 18140
42145035
00016717 00000-0 10270-3 0 9083
2 25544 51
6392 157
1285 0003647 105
4204 254
7352 15
54119536 34198
Satellite: ISS
Catalog Number: 25544
Epoch time: 18140
42145035 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 157
1285 deg
Eccentricity:
0003647
Arg of perigee: 105
4204 deg
Mean anomaly: 254
7352 deg
Mean motion: 15
54119536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 295
Coasting Arc #10 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2018/141/09:04:46
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3010516
11 A = 6783777
13 meter
Y = 4897121
09 meter E =
0009374
Z = -3611946
06 I = 51
81751
XDOT = -6220
336436 Wp = 103
39630
YDOT = -559
073177 meter/sec RA = 151
19406 deg
ZDOT = 4434
135376 TA = 214
00668
MA = 214
06679
Ha = 222
412 n
mi
Hp = 213
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9877021
34 X = -3047508
36
Y = 16066670
25 feet Y = 4863248
88 meter
Z = -11850216
74 Z = -3626659
57
XDOT = -20407
927941 XDOT = -6235
161130
YDOT = -1834
229582 feet/sec YDOT = -628
716510 meter/sec
ZDOT = 14547
688240 ZDOT = 4403
883055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5533452
75 X = -1686596
40
Y = 17986020
82 feet Y = 5482139
15 meter
Z = -11916586
59 Z = -3632175
59
XDOT = -19010
891182 XDOT = -5794
519632
YDOT = 3683
877111 feet/sec YDOT = 1122
845744 meter/sec
ZDOT = 14412
502939 ZDOT = 4392
930896
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 18141
38600853
00016717 00000-0 10270-3 0 9094
2 25544 51
6383 152
3211 0003961 108
9980 251
1602 15
54116258 34346
Satellite: ISS
Catalog Number: 25544
Epoch time: 18141
38600853 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 152
3211 deg
Eccentricity:
0003961
Arg of perigee: 108
9980 deg
Mean anomaly: 251
1602 deg
Mean motion: 15
54116258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 294
Coasting Arc #11 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2018/142/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2033951
12 A = 6777466
44 meter
Y = 3676267
96 meter E =
0018521
Z = -5334052
18 I = 51
81178
XDOT = -6572
877605 Wp = 95
45306
YDOT = 3918
615036 meter/sec RA = 148
05915 deg
ZDOT = 193
268123 TA = 176
39445
MA = 176
38108
Ha = 222
402 n
mi
Hp = 213
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6673067
97 X = 2018600
96
Y = 12061246
59 feet Y = 3698927
53 meter
Z = -17500171
19 Z = -5324208
97
XDOT = -21564
559073 XDOT = -6617
146917
YDOT = 12856
348542 feet/sec YDOT = 3844
865053 meter/sec
ZDOT = 634
081768 ZDOT = 161
232063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13822334
13 X = -4213047
44
Y = 685252
86 feet Y = 208865
07 meter
Z = -17456603
48 Z = -5320772
74
XDOT = -1815
430222 XDOT = -553
343132
YDOT = -24031
983316 feet/sec YDOT = -7324
948515 meter/sec
ZDOT = 490
371214 ZDOT = 149
465146
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 18142
02904428
00016717 00000-0 10270-3 0 9103
2 25544 51
6358 149
1134 0003829 110
3056 249
8508 15
54095227 34442
Satellite: ISS
Catalog Number: 25544
Epoch time: 18142
02904428 = yrday
fracday
Element set: 910
Inclination: 51
6358 deg
RA of node: 149
1134 deg
Eccentricity:
0003829
Arg of perigee: 110
3056 deg
Mean anomaly: 249
8508 deg
Mean motion: 15
54095227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3444
Checksum: 299
Coasting Arc #12 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2018/143/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -478145
23 A = 6778900
74 meter
Y = -4550144
70 meter E =
0008681
Z = 4995322
63 I = 51
84433
XDOT = 6741
487360 Wp = 78
52361
YDOT = -3010
410926 meter/sec RA = 143
07338 deg
ZDOT = -2092
085635 TA = 31
78857
MA = 31
73619
Ha = 222
445 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1568717
93 X = -451493
45
Y = -14928296
26 feet Y = -4555342
88 meter
Z = 16388853
76 Z = 4993064
46
XDOT = 22117
740684 XDOT = 6784
811840
YDOT = -9876
676265 feet/sec YDOT = -2934
780621 meter/sec
ZDOT = -6863
798016 ZDOT = -2059
232642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14190420
00 X = 4325240
02
Y = 4925414
13 feet Y = 1501266
23 meter
Z = 16379307
33 Z = 4992412
87
XDOT = -289
159000 XDOT = -88
135663
YDOT = 23220
585932 feet/sec YDOT = 7077
634592 meter/sec
ZDOT = -6716
526006 ZDOT = -2047
197127
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 18143
05789873
00016717 00000-0 10270-3 0 9113
2 25544 51
6363 143
9843 0003791 113
9190 246
2360 15
54071296 34608
Satellite: ISS
Catalog Number: 25544
Epoch time: 18143
05789873 = yrday
fracday
Element set: 911
Inclination: 51
6363 deg
RA of node: 143
9843 deg
Eccentricity:
0003791
Arg of perigee: 113
9190 deg
Mean anomaly: 246
2360 deg
Mean motion: 15
54071296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3460
Checksum: 315
Coasting Arc #13 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2018/144/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -971389
32 A = 6782017
17 meter
Y = 5268819
26 meter E =
0011752
Z = -4170811
48 I = 51
88065
XDOT = -6422
267411 Wp = 112
65073
YDOT = 1793
476670 meter/sec RA = 138
09583 deg
ZDOT = 3765
430940 TA = 196
01411
MA = 196
05129
Ha = 222
406 n
mi
Hp = 213
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3186972
84 X = -1009974
76
Y = 17286152
43 feet Y = 5257740
95 meter
Z = -13683764
70 Z = -4175623
67
XDOT = -21070
431137 XDOT = -6460
135842
YDOT = 5884
109811 feet/sec YDOT = 1721
446553 meter/sec
ZDOT = 12353
776049 ZDOT = 3734
141680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14433085
95 X = -4399204
60
Y = -10002340
14 feet Y = -3048713
27 meter
Z = -13705929
37 Z = -4177567
27
XDOT = 2712
073136 XDOT = 826
639892
YDOT = -20631
278373 feet/sec YDOT = -6288
413648 meter/sec
ZDOT = 12213
628737 ZDOT = 3722
714039
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 18144
02244624
00016717 00000-0 10270-3 0 9122
2 25544 51
6361 139
1756 0003998 117
5474 242
6085 15
54103792 34757
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
02244624 = yrday
fracday
Element set: 912
Inclination: 51
6361 deg
RA of node: 139
1756 deg
Eccentricity:
0003998
Arg of perigee: 117
5474 deg
Mean anomaly: 242
6085 deg
Mean motion: 15
54103792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 313
Coasting Arc #14 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2018/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3096521
33 A = 6787011
82 meter
Y = -5565582
51 meter E =
0017523
Z = 2320764
11 I = 51
90931
XDOT = 5370
155764 Wp = 108
81695
YDOT = 710
111522 meter/sec RA = 135
68605 deg
ZDOT = -5434
332918 TA = 45
39748
MA = 45
25465
Ha = 222
286 n
mi
Hp = 213
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10159190
71 X = 3147253
91
Y = -18259785
13 feet Y = -5530671
51 meter
Z = 7614055
48 Z = 2335929
05
XDOT = 17618
621274 XDOT = 5388
213332
YDOT = 2329
762210 feet/sec YDOT = 770
265504 meter/sec
ZDOT = -17829
176241 ZDOT = -5408
202448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11119461
79 X = -3389211
95
Y = -17661782
73 feet Y = -5383311
38 meter
Z = 7682561
42 Z = 2341644
72
XDOT = 9306
154333 XDOT = 2836
515841
YDOT = -13603
025199 feet/sec YDOT = -4146
202081 meter/sec
ZDOT = -17712
401030 ZDOT = -5398
739834
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 18144
53686927
00016717 00000-0 10270-3 0 9135
2 25544 51
6361 136
6148 0003736 114
2856 245
8687 15
54127035 34830
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
53686927 = yrday
fracday
Element set: 913
Inclination: 51
6361 deg
RA of node: 136
6148 deg
Eccentricity:
0003736
Arg of perigee: 114
2856 deg
Mean anomaly: 245
8687 deg
Mean motion: 15
54127035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 329
Coasting Arc #15 (Orbit 3497)
---------------------------------------
Vector Time (GMT): 2018/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3971993
32 A = 6789058
72 meter
Y = 5456869
08 meter E =
0011795
Z = -703781
45 I = 51
93908
XDOT = -4203
952819 Wp = 59
84546
YDOT = -2298
615598 meter/sec RA = 130
73364 deg
ZDOT = 5984
038266 TA = 292
58550
MA = 292
71025
Ha = 222
315 n
mi
Hp = 213
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13031474
15 X = -4029299
68
Y = 17903113
79 feet Y = 5412131
13 meter
Z = -2308994
26 Z = -723215
17
XDOT = -13792
496125 XDOT = -4207
004278
YDOT = -7541
389756 feet/sec YDOT = -2345
644453 meter/sec
ZDOT = 19632
671476 ZDOT = 5963
609146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9748409
62 X = 2971315
25
Y = 19872018
01 feet Y = 6056991
09 meter
Z = -2396594
75 Z = -730482
08
XDOT = -11721
424037 XDOT = -3572
690047
YDOT = 8076
128807 feet/sec YDOT = 2461
604060 meter/sec
ZDOT = 19541
585964 ZDOT = 5956
275402
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 18145
50141333
00016717 00000-0 10270-3 0 9141
2 25544 51
6360 131
8072 0003991 120
6069 239
5478 15
54141993 34985
Satellite: ISS
Catalog Number: 25544
Epoch time: 18145
50141333 = yrday
fracday
Element set: 914
Inclination: 51
6360 deg
RA of node: 131
8072 deg
Eccentricity:
0003991
Arg of perigee: 120
6069 deg
Mean anomaly: 239
5478 deg
Mean motion: 15
54141993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3498
Checksum: 310
Coasting Arc #16 (Orbit 3513)
---------------------------------------
Vector Time (GMT): 2018/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4549311
57 A = 6788924
80 meter
Y = -4924245
35 meter E =
0013334
Z = -1036770
12 I = 51
95987
XDOT = 2895
962321 Wp = 135
96053
YDOT = 3911
557895 meter/sec RA = 125
78384 deg
ZDOT = -5925
874547 TA = 55
22882
MA = 55
10338
Ha = 222
325 n
mi
Hp = 213
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14925562
88 X = 4609073
87
Y = -16155660
59 feet Y = -4873037
59 meter
Z = -3401476
78 Z = -1014525
98
XDOT = 9501
188718 XDOT = 2880
792173
YDOT = 12833
195193 feet/sec YDOT = 3943
858098 meter/sec
ZDOT = -19441
845626 ZDOT = -5911
843353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7657358
25 X = -2333962
79
Y = -20635255
44 feet Y = -6289625
86 meter
Z = -3301353
97 Z = -1006252
69
XDOT = 14293
580471 XDOT = 4356
683328
YDOT = -2233
315836 feet/sec YDOT = -680
714667 meter/sec
ZDOT = -19379
580101 ZDOT = -5906
896015
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 18146
53025504
00016717 00000-0 10270-3 0 9157
2 25544 51
6368 126
6770 0003781 120
9389 239
2135 15
54119230 35140
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
53025504 = yrday
fracday
Element set: 915
Inclination: 51
6368 deg
RA of node: 126
6770 deg
Eccentricity:
0003781
Arg of perigee: 120
9389 deg
Mean anomaly: 239
2135 deg
Mean motion: 15
54119230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3514
Checksum: 301
Coasting Arc #17 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2018/146/20:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1039568
76 A = 6780399
32 meter
Y = -4882548
44 meter E =
0010783
Z = 4580009
59 I = 51
94021
XDOT = 5686
817221 Wp = 82
09996
YDOT = -4120
060589 meter/sec RA = 123
89879 deg
ZDOT = -3093
772671 TA = 38
73847
MA = 38
66120
Ha = 222
148 n
mi
Hp = 213
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3410658
67 X = -1007141
12
Y = -16018859
73 feet Y = -4893992
63 meter
Z = 15026278
20 Z = 4575038
07
XDOT = 18657
536815 XDOT = 5747
494356
YDOT = -13517
259151 feet/sec YDOT = -4056
127196 meter/sec
ZDOT = -10150
172805 ZDOT = -3066
000571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8257645
80 X = 2516930
44
Y = 14166751
71 feet Y = 4318025
92 meter
Z = 15004663
53 Z = 4573421
44
XDOT = -12637
356357 XDOT = -3851
866218
YDOT = 18011
193261 feet/sec YDOT = 5489
811706 meter/sec
ZDOT = -10025
417879 ZDOT = -3055
747370
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 18146
91606752
00016717 00000-0 10270-3 0 9160
2 25544 51
6381 124
7534 0003410 124
4260 235
7215 15
54142876 35207
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
91606752 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 124
7534 deg
Eccentricity:
0003410
Arg of perigee: 124
4260 deg
Mean anomaly: 235
7215 deg
Mean motion: 15
54142876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 291
Coasting Arc #18 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2018/147/20:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -96595
92 A = 6784164
91 meter
Y = 5821051
31 meter E =
0008208
Z = -3492256
03 I = 51
96854
XDOT = -5547
714004 Wp = 108
45563
YDOT = 2646
329488 meter/sec RA = 118
93224 deg
ZDOT = 4570
730124 TA = 210
77112
MA = 210
81926
Ha = 222
130 n
mi
Hp = 213
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -316915
76 X = -144717
52
Y = 19097937
36 feet Y = 5819702
36 meter
Z = -11457532
91 Z = -3492841
62
XDOT = -18201
161431 XDOT = -5599
096221
YDOT = 8682
183360 feet/sec YDOT = 2584
003418 meter/sec
ZDOT = 14995
833740 ZDOT = 4543
656253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5946039
07 X = -1812352
71
Y = -18149348
55 feet Y = -5531921
44 meter
Z = -11460910
70 Z = -3493285
58
XDOT = 13186
315515 XDOT = 4019
188969
YDOT = -13699
939715 feet/sec YDOT = -4175
741625 meter/sec
ZDOT = 14874
373249 ZDOT = 4533
708966
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 18147
88060308
00016717 00000-0 10270-3 0 9179
2 25544 51
6365 119
9446 0003568 129
4653 230
6816 15
54126759 35351
Satellite: ISS
Catalog Number: 25544
Epoch time: 18147
88060308 = yrday
fracday
Element set: 917
Inclination: 51
6365 deg
RA of node: 119
9446 deg
Eccentricity:
0003568
Arg of perigee: 129
4653 deg
Mean anomaly: 230
6816 deg
Mean motion: 15
54126759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 334
Coasting Arc #19 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2018/148/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3805187
15 A = 6777450
95 meter
Y = 1745928
89 meter E =
0017699
Z = -5344806
06 I = 51
95352
XDOT = -3373
470948 Wp = 97
26468
YDOT = 6870
331264 meter/sec RA = 117
08986 deg
ZDOT = -160
086257 TA = 171
22923
MA = 171
19827
Ha = 222
190 n
mi
Hp = 213
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12484209
80 X = 3811343
55
Y = 5728113
15 feet Y = 1788516
06 meter
Z = -17535452
97 Z = -5326306
36
XDOT = -11067
818071 XDOT = -3449
268521
YDOT = 22540
456902 feet/sec YDOT = 6832
182994 meter/sec
ZDOT = -525
217379 ZDOT = -176
657099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8973389
86 X = 2735089
23
Y = 10537206
99 feet Y = 3211740
69 meter
Z = -17452920
35 Z = -5319650
12
XDOT = -18823
705453 XDOT = -5737
465422
YDOT = 15050
245803 feet/sec YDOT = 4587
314921 meter/sec
ZDOT = -600
251494 ZDOT = -182
956655
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 18148
26641699
00016717 00000-0 10270-3 0 9181
2 25544 51
6383 118
0218 0003714 133
1268 227
0196 15
54101136 35415
Satellite: ISS
Catalog Number: 25544
Epoch time: 18148
26641699 = yrday
fracday
Element set: 918
Inclination: 51
6383 deg
RA of node: 118
0218 deg
Eccentricity:
0003714
Arg of perigee: 133
1268 deg
Mean anomaly: 227
0196 deg
Mean motion: 15
54101136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 300
Coasting Arc #20 (Orbit 3556)
---------------------------------------
Vector Time (GMT): 2018/149/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2950189
95 A = 6778263
26 meter
Y = -3339309
69 meter E =
0006849
Z = 5102069
48 I = 51
97189
XDOT = 4043
319366 Wp = 87
04379
YDOT = -6277
451654 meter/sec RA = 112
11273 deg
ZDOT = -1768
231380 TA = 19
97965
MA = 19
95285
Ha = 222
162 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9679100
88 X = -2937413
14
Y = -10955740
46 feet Y = -3372229
91 meter
Z = 16739073
10 Z = 5087768
90
XDOT = 13265
483484 XDOT = 4121
804303
YDOT = -20595
313826 feet/sec YDOT = -6231
797427 meter/sec
ZDOT = -5801
284055 ZDOT = -1748
400153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4449861
87 X = -1356317
90
Y = -14001248
98 feet Y = -4267580
69 meter
Z = 16675537
99 Z = 5082703
98
XDOT = 19545
700519 XDOT = 5957
529518
YDOT = -13024
014340 feet/sec YDOT = -3969
719571 meter/sec
ZDOT = -5711
717246 ZDOT = -1740
931416
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 18149
29524686
00016717 00000-0 10270-3 0 9192
2 25544 51
6393 112
8930 0003640 136
4940 223
6500 15
54157387 35577
Satellite: ISS
Catalog Number: 25544
Epoch time: 18149
29524686 = yrday
fracday
Element set: 919
Inclination: 51
6393 deg
RA of node: 112
8930 deg
Eccentricity:
0003640
Arg of perigee: 136
4940 deg
Mean anomaly: 223
6500 deg
Mean motion: 15
54157387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 323
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