[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 23rd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12398 9484 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
144/03:23:00
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
5
144/09:20:00
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
6
146/20:57:30
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
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
153/12:25:00
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
9
154/09:16:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
156/19:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 214
1
Coasting Arc #1 (Orbit 3466)
---------------------------------------
Vector Time (GMT): 2018/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1863129
55 A = 6783487
79 meter
Y = 5339941
89 meter E =
0009812
Z = -3756081
17 I = 51
87374
XDOT = -6295
692261 Wp = 105
89459
YDOT = 812
936128 meter/sec RA = 140
64934 deg
ZDOT = 4285
264331 TA = 209
41466
MA = 209
46991
Ha = 222
464 n
mi
Hp = 213
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6112629
75 X = -1904458
62
Y = 17519494
40 feet Y = 5318876
18 meter
Z = -12323100
96 Z = -3765231
79
XDOT = -20655
158337 XDOT = -6325
130482
YDOT = 2667
113280 feet/sec YDOT = 742
368563 meter/sec
ZDOT = 14059
266177 ZDOT = 4254
610426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12199285
91 X = 3718342
35
Y = 13944464
19 feet Y = 4250272
69 meter
Z = -12364670
85 Z = -3768751
68
XDOT = -6986
380006 XDOT = -2129
448626
YDOT = 18437
490488 feet/sec YDOT = 5619
747101 meter/sec
ZDOT = 13922
087031 ZDOT = 4243
452127
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
50806457
00016717 00000-0 10270-3 0 9009
2 25544 51
6376 141
7447 0003897 109
7913 250
3660 15
54069155 34678
Satellite: ISS
Catalog Number: 25544
Epoch time: 18143
50806457 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 141
7447 deg
Eccentricity:
0003897
Arg of perigee: 109
7913 deg
Mean anomaly: 250
3660 deg
Mean motion: 15
54069155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3467
Checksum: 321
Coasting Arc #2 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2018/144/03:23:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -423302
92 A = 6781095
53 meter
Y = 5117897
39 meter E =
0013076
Z = -4441804
04 I = 51
88322
XDOT = -6466
346780 Wp = 113
54267
YDOT = 2368
317960 meter/sec RA = 137
46338 deg
ZDOT = 3347
759344 TA = 190
20426
MA = 190
23083
Ha = 222
379 n
mi
Hp = 213
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1388789
11 X = -458925
09
Y = 16791001
95 feet Y = 5112964
75 meter
Z = -14572847
89 Z = -4443946
61
XDOT = -21215
048492 XDOT = -6508
611134
YDOT = 7770
072048 feet/sec YDOT = 2295
770357 meter/sec
ZDOT = 10983
462414 ZDOT = 3316
245292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16090064
14 X = -4904251
55
Y = 4967764
16 feet Y = 1514174
52 meter
Z = -14583056
34 Z = -4444915
57
XDOT = -14687
338393 XDOT = -4476
700742
YDOT = -15769
077829 feet/sec YDOT = -4806
414922 meter/sec
ZDOT = 10842
237546 ZDOT = 3304
714004
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
15110373
00016717 00000-0 10270-3 0 9017
2 25544 51
6387 138
5356 0003879 119
5056 240
6484 15
54086543 34777
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
15110373 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 138
5356 deg
Eccentricity:
0003879
Arg of perigee: 119
5056 deg
Mean anomaly: 240
6484 deg
Mean motion: 15
54086543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 318
Coasting Arc #3 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2018/144/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4285011
58 A = 6778716
79 meter
Y = 1410375
85 meter E =
0016108
Z = -5073929
89 I = 51
88172
XDOT = -4233
004596 Wp = 84
94723
YDOT = 6094
937817 meter/sec RA = 136
27331 deg
ZDOT = -1884
418849 TA = 166
84288
MA = 166
80081
Ha = 222
418 n
mi
Hp = 213
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14058436
95 X = 4293568
58
Y = 4627217
34 feet Y = 1458341
86 meter
Z = -16646751
60 Z = -5053093
77
XDOT = -13887
810353 XDOT = -4291
691664
YDOT = 19996
515149 feet/sec YDOT = 6047
273385 meter/sec
ZDOT = -6182
476539 ZDOT = -1905
123767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14884274
02 X = 4536726
72
Y = -772770
01 feet Y = -235540
30 meter
Z = -16553741
02 Z = -5045580
26
XDOT = -5795
165826 XDOT = -1766
366544
YDOT = 22550
081787 feet/sec YDOT = 6873
264929 meter/sec
ZDOT = -6275
821858 ZDOT = -1912
870502
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
40831837
00016717 00000-0 10270-3 0 9021
2 25544 51
6395 137
2561 0003848 115
9255 244
2295 15
54077432 34819
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
40831837 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 137
2561 deg
Eccentricity:
0003848
Arg of perigee: 115
9255 deg
Mean anomaly: 244
2295 deg
Mean motion: 15
54077432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 314
Coasting Arc #4 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2018/145/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3131147
63 A = 6777438
89 meter
Y = -2768447
68 meter E =
0006171
Z = 5330226
31 I = 51
89956
XDOT = 5071
619746 Wp = 107
87904
YDOT = -5758
518463 meter/sec RA = 131
29186 deg
ZDOT = -13
497727 TA = 342
23826
MA = 342
25982
Ha = 222
520 n
mi
Hp = 213
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10272794
06 X = -3125849
11
Y = -9082833
61 feet Y = -2803432
97 meter
Z = 17487619
14 Z = 5315028
84
XDOT = 16639
172395 XDOT = 5135
701707
YDOT = -18892
777110 feet/sec YDOT = -5701
445812 meter/sec
ZDOT = -44
283882 ZDOT = 11
294101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13036917
79 X = -3973652
54
Y = -4519696
14 feet Y = -1377603
38 meter
Z = 17419991
64 Z = 5309613
45
XDOT = 8004
249072 XDOT = 2439
695117
YDOT = -22805
253959 feet/sec YDOT = -6951
041407 meter/sec
ZDOT = 67
316840 ZDOT = 20
518173
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
43717720
00016717 00000-0 10270-3 0 9030
2 25544 51
6382 132
1274 0003925 117
7767 242
3784 15
54095672 34979
Satellite: ISS
Catalog Number: 25544
Epoch time: 18145
43717720 = yrday
fracday
Element set: 903
Inclination: 51
6382 deg
RA of node: 132
1274 deg
Eccentricity:
0003925
Arg of perigee: 117
7767 deg
Mean anomaly: 242
3784 deg
Mean motion: 15
54095672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 323
Coasting Arc #5 (Orbit 3511)
---------------------------------------
Vector Time (GMT): 2018/146/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1920327
19 A = 6778685
28 meter
Y = 4090721
48 meter E =
0016606
Z = -5067706
71 I = 51
92619
XDOT = -5507
861908 Wp = 108
06381
YDOT = 4959
601056 meter/sec RA = 126
31178 deg
ZDOT = 1916
482370 TA = 180
47778
MA = 180
47937
Ha = 222
323 n
mi
Hp = 213
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6300286
07 X = 1899057
51
Y = 13421002
22 feet Y = 4112077
29 meter
Z = -16626334
33 Z = -5058429
69
XDOT = -18070
413084 XDOT = -5572
221563
YDOT = 16271
657008 feet/sec YDOT = 4897
648374 meter/sec
ZDOT = 6287
671818 ZDOT = 1889
570683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11148358
73 X = 3398019
74
Y = 9843370
67 feet Y = 3000259
38 meter
Z = -16585356
49 Z = -5055216
66
XDOT = -9586
394364 XDOT = -2921
933002
YDOT = 21246
909412 feet/sec YDOT = 6476
057989 meter/sec
ZDOT = 6166
668923 ZDOT = 1879
600688
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
40172945
00016717 00000-0 10270-3 0 9043
2 25544 51
6398 127
3193 0003699 121
0768 239
0747 15
54075188 35129
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
40172945 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 127
3193 deg
Eccentricity:
0003699
Arg of perigee: 121
0768 deg
Mean anomaly: 239
0747 deg
Mean motion: 15
54075188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3512
Checksum: 326
Coasting Arc #6 (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 = -1082129
96 A = 6780381
11 meter
Y = -4851558
46 meter E =
0010697
Z = 4603107
00 I = 51
94007
XDOT = 5676
599664 Wp = 81
26346
YDOT = -4166
735806 meter/sec RA = 123
89979 deg
ZDOT = -3049
529526 TA = 39
08813
MA = 39
01089
Ha = 222
187 n
mi
Hp = 213
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3550295
13 X = -1050157
88
Y = -15917186
56 feet Y = -4863481
14 meter
Z = 15102057
10 Z = 4597927
62
XDOT = 18624
014646 XDOT = 5737
584580
YDOT = -13670
393065 feet/sec YDOT = -4102
914955 meter/sec
ZDOT = -10005
018131 ZDOT = -3021
806316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8359800
73 X = 2548067
26
Y = 14026963
35 feet Y = 4275418
43 meter
Z = 15079508
71 Z = 4596234
25
XDOT = -12567
727309 XDOT = -3830
643284
YDOT = 18138
887636 feet/sec YDOT = 5528
732951 meter/sec
ZDOT = -9880
475937 ZDOT = -3011
569066
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
91615526
00016717 00000-0 10270-3 0 9057
2 25544 51
6382 124
7541 0003369 122
5389 237
6090 15
54118633 35206
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
91615526 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 124
7541 deg
Eccentricity:
0003369
Arg of perigee: 122
5389 deg
Mean anomaly: 237
6090 deg
Mean motion: 15
54118633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 307
Coasting Arc #7 (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 = -47148
39 A = 6784121
25 meter
Y = 5797166
40 meter E =
0008343
Z = -3532885
14 I = 51
96829
XDOT = -5548
547303 Wp = 108
38151
YDOT = 2712
218918 meter/sec RA = 118
93317 deg
ZDOT = 4530
765528 TA = 210
26816
MA = 210
31638
Ha = 222
171 n
mi
Hp = 213
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -154686
32 X = -94809
22
Y = 19019574
81 feet Y = 5796372
99 meter
Z = -11590830
53 Z = -3533229
41
XDOT = -18203
895352 XDOT = -5600
472121
YDOT = 8898
356029 feet/sec YDOT = 2649
880498 meter/sec
ZDOT = 14864
716300 ZDOT = 4503
686298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6075048
63 X = -1851674
82
Y = -18022450
66 feet Y = -5493242
96 meter
Z = -11593125
65 Z = -3533584
70
XDOT = 13127
448511 XDOT = 4001
246306
YDOT = -13895
688593 feet/sec YDOT = -4235
405883 meter/sec
ZDOT = 14743
223252 ZDOT = 4493
734447
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
88070636
00016717 00000-0 10270-3 0 9062
2 25544 51
6366 119
9455 0003522 127
5882 232
5591 15
54100667 35356
Satellite: ISS
Catalog Number: 25544
Epoch time: 18147
88070636 = yrday
fracday
Element set: 906
Inclination: 51
6366 deg
RA of node: 119
9455 deg
Eccentricity:
0003522
Arg of perigee: 127
5882 deg
Mean anomaly: 232
5591 deg
Mean motion: 15
54100667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 322
Coasting Arc #8 (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 = 3837003
73 A = 6777539
81 meter
Y = 1680711
98 meter E =
0017691
Z = -5343078
83 I = 51
95371
XDOT = -3327
520851 Wp = 96
46552
YDOT = 6890
847698 meter/sec RA = 117
09148 deg
ZDOT = -224
576449 TA = 171
41484
MA = 171
38454
Ha = 222
233 n
mi
Hp = 213
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12588594
91 X = 3843878
65
Y = 5514146
93 feet Y = 1723658
97 meter
Z = -17529786
19 Z = -5324422
83
XDOT = -10917
063159 XDOT = -3403
237995
YDOT = 22607
768037 feet/sec YDOT = 6853
213729 meter/sec
ZDOT = -736
799372 ZDOT = -240
923879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9158751
99 X = 2791587
61
Y = 10387841
16 feet Y = 3166213
99 meter
Z = -17446545
79 Z = -5317707
16
XDOT = -18725
448906 XDOT = -5707
516826
YDOT = 15162
288732 feet/sec YDOT = 4621
465606 meter/sec
ZDOT = -810
836707 ZDOT = -247
143028
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
26652695
00016717 00000-0 10270-3 0 9077
2 25544 51
6384 118
0227 0003664 131
3750 228
7718 15
54073731 35413
Satellite: ISS
Catalog Number: 25544
Epoch time: 18148
26652695 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 118
0227 deg
Eccentricity:
0003664
Arg of perigee: 131
3750 deg
Mean anomaly: 228
7718 deg
Mean motion: 15
54073731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 314
Coasting Arc #9 (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 = -2994536
52 A = 6778268
99 meter
Y = -3269885
07 meter E =
0006748
Z = 5121242
95 I = 51
97177
XDOT = 4001
397091 Wp = 86
71266
YDOT = -6324
037614 meter/sec RA = 112
11458 deg
ZDOT = -1695
836538 TA = 19
59422
MA = 19
56830
Ha = 222
212 n
mi
Hp = 213
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9824594
89 X = -2982625
88
Y = -10727969
40 feet Y = -3303306
05 meter
Z = 16801978
17 Z = 5106724
85
XDOT = 13127
943211 XDOT = 4080
054419
YDOT = -20748
154903 feet/sec YDOT = -6278
851235 meter/sec
ZDOT = -5563
768168 ZDOT = -1676
208545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4676201
24 X = -1425306
14
Y = -13853123
05 feet Y = -4222431
91 meter
Z = 16737460
57 Z = 5101577
98
XDOT = 19492
109223 XDOT = 5941
194891
YDOT = -13203
875022 feet/sec YDOT = -4024
541107 meter/sec
ZDOT = -5475
104415 ZDOT = -1668
811826
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
29537577
00016717 00000-0 10270-3 0 9083
2 25544 51
6393 112
8941 0003589 134
6249 225
5197 15
54127428 35579
Satellite: ISS
Catalog Number: 25544
Epoch time: 18149
29537577 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 112
8941 deg
Eccentricity:
0003589
Arg of perigee: 134
6249 deg
Mean anomaly: 225
5197 deg
Mean motion: 15
54127428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 346
Coasting Arc #10 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2018/150/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2144453
21 A = 6781241
14 meter
Y = 4707306
39 meter E =
0012369
Z = -4397804
74 I = 51
99347
XDOT = -4421
417589 Wp = 117
27147
YDOT = 5222
868961 meter/sec RA = 107
14382 deg
ZDOT = 3436
363499 TA = 187
43747
MA = 187
45584
Ha = 222
155 n
mi
Hp = 213
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7035607
64 X = 2113017
93
Y = 15443918
61 feet Y = 4731111
97 meter
Z = -14428493
25 Z = -4387463
32
XDOT = -14505
963219 XDOT = -4496
184782
YDOT = 17135
396854 feet/sec YDOT = 5173
007117 meter/sec
ZDOT = 11274
158461 ZDOT = 3414
704608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 479807
89 X = 146245
45
Y = 17002907
48 feet Y = 5182486
20 meter
Z = -14382862
58 Z = -4383896
51
XDOT = -18906
726455 XDOT = -5762
770223
YDOT = 9982
553183 feet/sec YDOT = 3042
682210 meter/sec
ZDOT = 11176
533281 ZDOT = 3406
607344
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 18150
25992160
00016717 00000-0 10270-3 0 9095
2 25544 51
6397 108
0860 0003685 133
2141 226
9320 15
54114438 35720
Satellite: ISS
Catalog Number: 25544
Epoch time: 18150
25992160 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 108
0860 deg
Eccentricity:
0003685
Arg of perigee: 133
2141 deg
Mean anomaly: 226
9320 deg
Mean motion: 15
54114438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 299
Coasting Arc #11 (Orbit 3587)
---------------------------------------
Vector Time (GMT): 2018/151/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1289526
58 A = 6785009
37 meter
Y = -5837393
26 meter E =
0015619
Z = 3191896
92 I = 52
01468
XDOT = 4667
949657 Wp = 103
25119
YDOT = -3689
889707 meter/sec RA = 102
18393 deg
ZDOT = -4845
923112 TA = 40
05171
MA = 39
93664
Ha = 222
087 n
mi
Hp = 213
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4230730
26 X = -1239660
12
Y = -19151552
69 feet Y = -5851535
27 meter
Z = 10472102
74 Z = 3185753
07
XDOT = 15314
795461 XDOT = 4732
403244
YDOT = -12105
937359 feet/sec YDOT = -3637
328408 meter/sec
ZDOT = -15898
697875 ZDOT = -4823
091585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3249273
29 X = 990378
50
Y = -19356689
11 feet Y = -5899918
84 meter
Z = 10445419
81 Z = 3183763
96
XDOT = 17438
197127 XDOT = 5315
162484
YDOT = -5625
780693 feet/sec YDOT = -1714
737955 meter/sec
ZDOT = -15796
016624 ZDOT = -4814
625867
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 18151
28876711
00016717 00000-0 10270-3 0 9104
2 25544 51
6394 102
9579 0003596 138
4425 221
7001 15
54135126 35883
Satellite: ISS
Catalog Number: 25544
Epoch time: 18151
28876711 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 102
9579 deg
Eccentricity:
0003596
Arg of perigee: 138
4425 deg
Mean anomaly: 221
7001 deg
Mean motion: 15
54135126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 311
Coasting Arc #12 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2018/152/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 498111
88 A = 6788110
29 meter
Y = 6554699
92 meter E =
0007753
Z = -1690809
84 I = 52
03190
XDOT = -4742
963550 Wp = 65
68191
YDOT = 1833
294118 meter/sec RA = 97
23367 deg
ZDOT = 5733
512879 TA = 275
89810
MA = 275
98647
Ha = 222
048 n
mi
Hp = 213
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1634225
34 X = 432991
53
Y = 21504921
00 feet Y = 6559906
28 meter
Z = -5547276
39 Z = -1688547
40
XDOT = -15560
904034 XDOT = -4790
961995
YDOT = 6014
744483 feet/sec YDOT = 1779
985833 meter/sec
ZDOT = 18810
737792 ZDOT = 5710
356739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6218088
15 X = -1895273
27
Y = 20653563
70 feet Y = 6295206
22 meter
Z = -5538075
56 Z = -1688005
43
XDOT = -15293
104212 XDOT = -4661
338164
YDOT = 390
939382 feet/sec YDOT = 119
158324 meter/sec
ZDOT = 18706
848778 ZDOT = 5701
847508
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 18152
25330920
00016717 00000-0 10270-3 0 9110
2 25544 51
6404 98
1500 0003687 141
1852 218
9566 15
54130124 36036
Satellite: ISS
Catalog Number: 25544
Epoch time: 18152
25330920 = yrday
fracday
Element set: 911
Inclination: 51
6404 deg
RA of node: 98
1500 deg
Eccentricity:
0003687
Arg of perigee: 141
1852 deg
Mean anomaly: 218
9566 deg
Mean motion: 15
54130124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 280
Coasting Arc #13 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2018/153/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 292609
17 A = 6789357
40 meter
Y = -6775271
72 meter E =
0015659
Z = -27739
58 I = 52
03978
XDOT = 4713
430565 Wp = 136
74654
YDOT = 220
050049 meter/sec RA = 92
29010 deg
ZDOT = -6048
001949 TA = 43
55071
MA = 43
42718
Ha = 222
035 n
mi
Hp = 213
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 960003
82 X = 368485
11
Y = -22228581
77 feet Y = -6771575
31 meter
Z = -91009
11 Z = -26134
83
XDOT = 15464
011040 XDOT = 4739
997694
YDOT = 721
948981 feet/sec YDOT = 272
908268 meter/sec
ZDOT = -19842
526081 ZDOT = -6025
041098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8581519
19 X = 2615647
05
Y = -20527795
80 feet Y = -6256872
16 meter
Z = -82857
97 Z = -25255
11
XDOT = 12888
823834 XDOT = 3928
513505
YDOT = 5438
373948 feet/sec YDOT = 1657
616379 meter/sec
ZDOT = -19739
793389 ZDOT = -6016
689025
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 18153
28214974
00016717 00000-0 10270-3 0 9125
2 25544 51
6411 93
0213 0003631 143
7191 216
4208 15
54119546 36190
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
28214974 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 93
0213 deg
Eccentricity:
0003631
Arg of perigee: 143
7191 deg
Mean anomaly: 216
4208 deg
Mean motion: 15
54119546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 289
Coasting Arc #14 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2018/153/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3569470
38 A = 6780880
59 meter
Y = -3628764
45 meter E =
0010843
Z = -4489759
59 I = 52
01101
XDOT = 2454
003748 Wp = 86
74317
YDOT = 6470
083650 meter/sec RA = 90
98759 deg
ZDOT = -3284
552204 TA = 150
32587
MA = 150
26431
Ha = 221
960 n
mi
Hp = 213
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11710860
82 X = 3631591
87
Y = -11905395
19 feet Y = -3588500
22 meter
Z = -14730182
37 Z = -4472269
90
XDOT = 8051
193399 XDOT = 2397
425779
YDOT = 21227
308563 feet/sec YDOT = 6497
210116 meter/sec
ZDOT = -10776
089907 ZDOT = -3272
767996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8771436
44 X = -2673533
83
Y = -14291950
34 feet Y = -4356186
46 meter
Z = -14651383
09 Z = -4465741
57
XDOT = 21503
983324 XDOT = 6554
414117
YDOT = -2224
750760 feet/sec YDOT = -678
104032 meter/sec
ZDOT = -10724
275811 ZDOT = -3268
759267
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 18153
53936057
00016717 00000-0 10270-3 0 9137
2 25544 51
6402 91
7396 0003367 142
3774 217
7615 15
54130692 36231
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
53936057 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 91
7396 deg
Eccentricity:
0003367
Arg of perigee: 142
3774 deg
Mean anomaly: 217
7615 deg
Mean motion: 15
54130692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 312
Coasting Arc #15 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2018/154/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3514112
94 A = 6779848
76 meter
Y = 3334511
67 meter E =
0010857
Z = 4738641
93 I = 52
00520
XDOT = -2564
899011 Wp = 126
64474
YDOT = -6672
754479 meter/sec RA = 86
67604 deg
ZDOT = 2782
713445 TA = 295
89290
MA = 296
00479
Ha = 221
931 n
mi
Hp = 213
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11529241
93 X = -3574157
03
Y = 10939998
92 feet Y = 3294878
10 meter
Z = 15546725
48 Z = 4721426
16
XDOT = -8415
023001 XDOT = -2503
608781
YDOT = -21892
239103 feet/sec YDOT = -6701
094613 meter/sec
ZDOT = 9129
637286 ZDOT = 2770
402038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4594228
91 X = -1400320
97
Y = 15293954
09 feet Y = 4661597
21 meter
Z = 15469185
44 Z = 4715007
72
XDOT = -17178
642909 XDOT = -5236
050359
YDOT = -14375
581700 feet/sec YDOT = -4381
677302 meter/sec
ZDOT = 9075
500297 ZDOT = 2766
212490
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 18154
43959303
00016717 00000-0 10270-3 0 9147
2 25544 51
6379 87
2527 0003386 149
6557 210
4792 15
54142777 36378
Satellite: ISS
Catalog Number: 25544
Epoch time: 18154
43959303 = yrday
fracday
Element set: 914
Inclination: 51
6379 deg
RA of node: 87
2527 deg
Eccentricity:
0003386
Arg of perigee: 149
6557 deg
Mean anomaly: 210
4792 deg
Mean motion: 15
54142777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 339
Coasting Arc #16 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2018/155/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3937236
26 A = 6777675
08 meter
Y = -1624440
09 meter E =
0016006
Z = -5285789
76 I = 51
99508
XDOT = 1807
757960 Wp = 94
28395
YDOT = 7382
584824 meter/sec RA = 81
70290 deg
ZDOT = -925
853745 TA = 166
90952
MA = 166
86793
Ha = 221
867 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12917441
80 X = 3980784
14
Y = -5329527
86 feet Y = -1580167
09 meter
Z = -17341829
92 Z = -5266558
45
XDOT = 5930
964437 XDOT = 1729
566827
YDOT = 24221
078818 feet/sec YDOT = 7402
363334 meter/sec
ZDOT = -3037
577905 ZDOT = -917
261325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8421380
03 X = 2566836
63
Y = -11284101
97 feet Y = -3439394
28 meter
Z = -17255510
30 Z = -5259479
54
XDOT = 16758
343393 XDOT = 5107
943066
YDOT = 17076
700997 feet/sec YDOT = 5204
978464 meter/sec
ZDOT = -3000
200451 ZDOT = -914
461097
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 18155
40412811
00016717 00000-0 10270-3 0 9154
2 25544 51
6383 82
4438 0003400 151
4630 208
6709 15
54114515 36524
Satellite: ISS
Catalog Number: 25544
Epoch time: 18155
40412811 = yrday
fracday
Element set: 915
Inclination: 51
6383 deg
RA of node: 82
4438 deg
Eccentricity:
0003400
Arg of perigee: 151
4630 deg
Mean anomaly: 208
6709 deg
Mean motion: 15
54114515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 282
Coasting Arc #17 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2018/156/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263863
79 A = 6777706
41 meter
Y = -163164
85 meter E =
0004607
Z = 5261928
77 I = 51
99023
XDOT = -964
038683 Wp = 102
76980
YDOT = -7543
499838 meter/sec RA = 76
72763 deg
ZDOT = -1015
342274 TA = 356
89811
MA = 356
90097
Ha = 221
927 n
mi
Hp = 214
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13989054
44 X = -4287282
01
Y = -535317
75 feet Y = -210977
80 meter
Z = 17263545
84 Z = 5241159
50
XDOT = -3162
856571 XDOT = -874
681556
YDOT = -24749
015215 feet/sec YDOT = -7553
780649 meter/sec
ZDOT = -3331
175439 ZDOT = -1019
808998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12242540
33 X = -3731526
29
Y = 7021455
66 feet Y = 2140139
68 meter
Z = 17170602
52 Z = 5233599
65
XDOT = -15267
852837 XDOT = -4653
641545
YDOT = -18430
488158 feet/sec YDOT = -5617
612790 meter/sec
ZDOT = -3350
050692 ZDOT = -1021
095451
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 18156
43296106
00016717 00000-0 10270-3 0 9166
2 25544 51
6390 77
3154 0003299 154
8597 205
2716 15
54122422 36689
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
43296106 = yrday
fracday
Element set: 916
Inclination: 51
6390 deg
RA of node: 77
3154 deg
Eccentricity:
0003299
Arg of perigee: 154
8597 deg
Mean anomaly: 205
2716 deg
Mean motion: 15
54122422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 319
Coasting Arc #18 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2018/156/19:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064196
25 A = 6783769
26 meter
Y = 4036464
92 meter E =
0007975
Z = -3644099
88 I = 52
00645
XDOT = -1943
946053 Wp = 121
35560
YDOT = 5945
379414 meter/sec RA = 74
60066 deg
ZDOT = 4420
564132 TA = 195
71416
MA = 195
73893
Ha = 221
834 n
mi
Hp = 214
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13333977
19 X = 4036458
45
Y = 13242995
14 feet Y = 4081758
83 meter
Z = -11955708
25 Z = -3624424
38
XDOT = -6377
775763 XDOT = -2031
757211
YDOT = 19505
837972 feet/sec YDOT = 5923
149447 meter/sec
ZDOT = 14503
163162 ZDOT = 4410
908425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14578090
25 X = -4443401
91
Y = -11947177
42 feet Y = -3641499
68 meter
Z = -11868237
62 Z = -3617438
83
XDOT = 3773
859720 XDOT = 1150
272443
YDOT = -18958
301865 feet/sec YDOT = -5778
490409 meter/sec
ZDOT = 14459
056226 ZDOT = 4407
120338
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 18156
81877242
00016717 00000-0 10270-3 0 9175
2 25544 51
6382 75
3883 0003699 156
9195 203
2125 15
54134823 36745
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
81877242 = yrday
fracday
Element set: 917
Inclination: 51
6382 deg
RA of node: 75
3883 deg
Eccentricity:
0003699
Arg of perigee: 156
9195 deg
Mean anomaly: 203
2125 deg
Mean motion: 15
54134823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 334
Coasting Arc #19 (Orbit 3689)
---------------------------------------
Vector Time (GMT): 2018/157/19:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3755526
22 A = 6787309
70 meter
Y = -5199503
82 meter E =
0016298
Z = 2192652
42 I = 52
00735
XDOT = 2938
769157 Wp = 119
46842
YDOT = -4456
737871 meter/sec RA = 69
64680 deg
ZDOT = -5512
083000 TA = 36
29803
MA = 36
18758
Ha = 221
767 n
mi
Hp = 214
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12321280
26 X = -3707755
60
Y = -17058739
56 feet Y = -5241233
79 meter
Z = 7193741
53 Z = 2174524
89
XDOT = 9641
631092 XDOT = 3015
162055
YDOT = -14621
843410 feet/sec YDOT = -4423
446900 meter/sec
ZDOT = -18084
261810 ZDOT = -5497
622296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14161139
48 X = 4316315
31
Y = 15602127
67 feet Y = 4755528
51 meter
Z = 7113381
80 Z = 2168158
77
XDOT = -6964
462818 XDOT = -2122
768267
YDOT = 14571
041110 feet/sec YDOT = 4441
253330 meter/sec
ZDOT = -18018
861248 ZDOT = -5492
148908
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 18157
84760093
00016717 00000-0 10270-3 0 9185
2 25544 51
6370 70
2595 0003606 163
0291 197
0983 15
54138578 36901
Satellite: ISS
Catalog Number: 25544
Epoch time: 18157
84760093 = yrday
fracday
Element set: 918
Inclination: 51
6370 deg
RA of node: 70
2595 deg
Eccentricity:
0003606
Arg of perigee: 163
0291 deg
Mean anomaly: 197
0983 deg
Mean motion: 15
54138578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3690
Checksum: 330
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