[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 5th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
157/11:12:41
000 0
0 0
0 0
0
N/A 0
0 0
0 221
7
000/00:00:00
000 0
0 0
0 214
1
159/13:07:16
000 0
0 0
0 0
0
N/A 0
0 0
0 221
6
000/00:00:00
000 0
0 0
0 214
3
164/10:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
6
Coasting Arc #1 (Orbit 3653)
---------------------------------------
Vector Time (GMT): 2018/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1259032
52 A = 6789314
39 meter
Y = -6657514
32 meter E =
0015784
Z = 278545
47 I = 52
03600
XDOT = 4593
266908 Wp = 135
82674
YDOT = -1129
455336 meter/sec RA = 81
12923 deg
ZDOT = -6039
536388 TA = 41
18677
MA = 41
06777
Ha = 221
840 n
mi
Hp = 214
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4130684
13 X = -1185845
83
Y = -21842238
59 feet Y = -6671184
51 meter
Z = 913863
08 Z = 272606
50
XDOT = 15069
773321 XDOT = 4634
892280
YDOT = -3705
562126 feet/sec YDOT = -1077
856815 meter/sec
ZDOT = -19814
751930 ZDOT = -6017
122923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22051673
95 X = -6721350
22
Y = -2813495
75 feet Y = -857553
51 meter
Z = 888257
54 Z = 270740
90
XDOT = 965
014533 XDOT = 294
136430
YDOT = -13994
282659 feet/sec YDOT = -4265
457354 meter/sec
ZDOT = -19714
260530 ZDOT = -6008
906610
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
53271703
00016717 00000-0 10270-3 0 9005
2 25544 51
6406 81
8028 0003333 151
2742 208
8595 15
54124041 36547
Satellite: ISS
Catalog Number: 25544
Epoch time: 18155
53271703 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 81
8028 deg
Eccentricity:
0003333
Arg of perigee: 151
2742 deg
Mean anomaly: 208
8595 deg
Mean motion: 15
54124041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3654
Checksum: 286
Coasting Arc #2 (Orbit 3669)
---------------------------------------
Vector Time (GMT): 2018/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 490038
98 A = 6788471
38 meter
Y = 6616267
76 meter E =
0014092
Z = 1414406
79 I = 52
02697
XDOT = -4903
582816 Wp = 73
99919
YDOT = -892
107323 meter/sec RA = 76
18532 deg
ZDOT = 5827
745176 TA = 301
33820
MA = 301
47605
Ha = 221
767 n
mi
Hp = 214
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1607739
44 X = 409147
20
Y = 21706915
22 feet Y = 6621295
27 meter
Z = 4640442
22 Z = 1416591
44
XDOT = -16087
870130 XDOT = -4921
550694
YDOT = -2926
861297 feet/sec YDOT = -947
043632 meter/sec
ZDOT = 19119
898873 ZDOT = 5803
881535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21219056
09 X = 6467568
30
Y = 4841997
07 feet Y = 1475840
71 meter
Z = 4649238
81 Z = 1417087
99
XDOT = -7187
368352 XDOT = -2190
709874
YDOT = 13101
775700 feet/sec YDOT = 3993
421233 meter/sec
ZDOT = 19013
212439 ZDOT = 5795
227151
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
56154383
00016717 00000-0 10270-3 0 9014
2 25544 51
6403 76
6741 0003253 153
4147 206
7173 15
54131781 36708
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
56154383 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 76
6741 deg
Eccentricity:
0003253
Arg of perigee: 153
4147 deg
Mean anomaly: 206
7173 deg
Mean motion: 15
54131781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3670
Checksum: 296
Coasting Arc #3 (Orbit 3684)
---------------------------------------
Vector Time (GMT): 2018/157/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -101257
87 A = 6786282
78 meter
Y = 6233297
58 meter E =
0014518
Z = 2668951
61 I = 52
01061
XDOT = -5097
856423 Wp = 90
40571
YDOT = -2334
013362 meter/sec RA = 71
39726 deg
ZDOT = 5233
052195 TA = 299
55285
MA = 299
69750
Ha = 221
703 n
mi
Hp = 214
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -332210
85 X = -183917
16
Y = 20450451
38 feet Y = 6231702
82 meter
Z = 8756402
93 Z = 2668259
54
XDOT = -16725
250730 XDOT = -5096
797406
YDOT = -7657
524154 feet/sec YDOT = -2391
015666 meter/sec
ZDOT = 17168
806415 ZDOT = 5208
290895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17893991
25 X = 5454088
53
Y = 9909945
30 feet Y = 3020551
33 meter
Z = 8752369
92 Z = 2667722
35
XDOT = -13919
966263 XDOT = -4242
805717
YDOT = 9997
684439 feet/sec YDOT = 3047
294217 meter/sec
ZDOT = 17058
319187 ZDOT = 5199
375688
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
52606595
00016717 00000-0 10270-3 0 9029
2 25544 51
6397 71
8660 0003245 157
2572 202
8725 15
54139710 36858
Satellite: ISS
Catalog Number: 25544
Epoch time: 18157
52606595 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 71
8660 deg
Eccentricity:
0003245
Arg of perigee: 157
2572 deg
Mean anomaly: 202
8725 deg
Mean motion: 15
54139710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3685
Checksum: 321
Coasting Arc #4 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2018/158/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1093190
95 A = 6782401
48 meter
Y = -5355926
55 meter E =
0007737
Z = -4020942
45 I = 51
98753
XDOT = 5154
759236 Wp = 96
32372
YDOT = 4035
570653 meter/sec RA = 66
43954 deg
ZDOT = -3981
351379 TA = 132
44647
MA = 132
38102
Ha = 221
602 n
mi
Hp = 214
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3586584
49 X = 1172532
84
Y = -17571937
51 feet Y = -5343257
77 meter
Z = -13192068
39 Z = -4015439
83
XDOT = 16911
939750 XDOT = 5128
588647
YDOT = 13240
061196 feet/sec YDOT = 4093
068732 meter/sec
ZDOT = -13062
176440 ZDOT = -3956
374466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14009433
35 X = -4270075
28
Y = -11226887
58 feet Y = -3421955
33 meter
Z = -13166625
13 Z = -4013187
34
XDOT = 18678
311099 XDOT = 5693
149223
YDOT = -8147
534601 feet/sec YDOT = -2483
368546 meter/sec
ZDOT = -12950
987479 ZDOT = -3947
460983
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 18158
49058526
00016717 00000-0 10270-3 0 9032
2 25544 51
6408 67
0578 0003183 161
1142 199
0129 15
54164072 37006
Satellite: ISS
Catalog Number: 25544
Epoch time: 18158
49058526 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 67
0578 deg
Eccentricity:
0003183
Arg of perigee: 161
1142 deg
Mean anomaly: 199
0129 deg
Mean motion: 15
54164072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 302
Coasting Arc #5 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2018/159/11:12:41
000
Vector Time (MET): N/A
Weight (LBS) : 907993
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2129881
16 A = 6778967
92 meter
Y = 4143379
81 meter E =
0009229
Z = 4921299
15 I = 51
96229
XDOT = -4983
263037 Wp = 135
66878
YDOT = -5344
212587 meter/sec RA = 61
47090 deg
ZDOT = 2333
681121 TA = 291
55906
MA = 291
65739
Ha = 221
554 n
mi
Hp = 214
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6987799
10 X = -2199960
52
Y = 13593765
79 feet Y = 4119169
76 meter
Z = 16145994
59 Z = 4910782
99
XDOT = -16349
288179 XDOT = -4934
468092
YDOT = -17533
505864 feet/sec YDOT = -5399
666238 meter/sec
ZDOT = 7656
434123 ZDOT = 2309
592046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9127596
95 X = 2782091
55
Y = 12322543
07 feet Y = 3755911
13 meter
Z = 16098287
24 Z = 4906757
95
XDOT = -22038
412180 XDOT = -6717
308032
YDOT = 6422
761963 feet/sec YDOT = 1957
657846 meter/sec
ZDOT = 7549
430192 ZDOT = 2301
066323
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 18159
51940064
00016717 00000-0 10270-3 0 9044
2 25544 51
6411 61
9291 0003230 166
8473 193
2764 15
54176225 37168
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
51940064 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 61
9291 deg
Eccentricity:
0003230
Arg of perigee: 166
8473 deg
Mean anomaly: 193
2764 deg
Mean motion: 15
54176225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 306
Coasting Arc #6 (Orbit 3716)
---------------------------------------
Vector Time (GMT): 2018/159/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4585806
70 A = 6786844
20 meter
Y = -4358360
67 meter E =
0015662
Z = 2433291
19 I = 51
98811
XDOT = 1982
578709 Wp = 116
01370
YDOT = -5100
392127 meter/sec RA = 61
03843 deg
ZDOT = -5379
051187 TA = 36
88103
MA = 36
77342
Ha = 221
636 n
mi
Hp = 214
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15045297
56 X = -4548549
22
Y = -14299083
56 feet Y = -4409434
21 meter
Z = 7983238
82 Z = 2411104
89
XDOT = 6504
523322 XDOT = 2065
594123
YDOT = -16733
569972 feet/sec YDOT = -5077
756940 meter/sec
ZDOT = -17647
805730 ZDOT = -5369
219239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13541059
21 X = -4127314
85
Y = 15780673
23 feet Y = 4809949
20 meter
Z = 7884601
41 Z = 2403226
51
XDOT = -15888
729454 XDOT = -4842
884738
YDOT = -4805
365666 feet/sec YDOT = -1464
675455 meter/sec
ZDOT = -17603
013162 ZDOT = -5365
398412
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 18159
58370253
00016717 00000-0 10270-3 0 9059
2 25544 51
6423 61
6096 0003224 165
5443 194
5802 15
54141616 37171
Satellite: ISS
Catalog Number: 25544
Epoch time: 18159
58370253 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 61
6096 deg
Eccentricity:
0003224
Arg of perigee: 165
5443 deg
Mean anomaly: 194
5802 deg
Mean motion: 15
54141616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3717
Checksum: 304
Coasting Arc #7 (Orbit 3731)
---------------------------------------
Vector Time (GMT): 2018/160/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4264175
06 A = 6788917
67 meter
Y = 5217925
26 meter E =
0008613
Z = -802759
99 I = 51
97851
XDOT = -3235
530049 Wp = 55
20897
YDOT = 3555
021688 meter/sec RA = 56
08825 deg
ZDOT = 5970
868207 TA = 296
15501
MA = 296
24358
Ha = 221
394 n
mi
Hp = 214
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13990075
65 X = 4209409
29
Y = 17119177
36 feet Y = 5265304
07 meter
Z = -2633727
01 Z = -782178
42
XDOT = -10615
256066 XDOT = -3304
046430
YDOT = 11663
456983 feet/sec YDOT = 3518
456099 meter/sec
ZDOT = 19589
462621 ZDOT = 5954
984879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16154140
94 X = 4923782
16
Y = -15109758
75 feet Y = -4605454
47 meter
Z = -2542417
98 Z = -774929
00
XDOT = 11248
915933 XDOT = 3428
669577
YDOT = 8770
945492 feet/sec YDOT = 2673
384186 meter/sec
ZDOT = 19517
816046 ZDOT = 5949
030331
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 18160
54821273
00016717 00000-0 10270-3 0 9061
2 25544 51
6422 56
8010 0003109 171
2100 188
9108 15
54180665 37328
Satellite: ISS
Catalog Number: 25544
Epoch time: 18160
54821273 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 56
8010 deg
Eccentricity:
0003109
Arg of perigee: 171
2100 deg
Mean anomaly: 188
9108 deg
Mean motion: 15
54180665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3732
Checksum: 283
Coasting Arc #8 (Orbit 3747)
---------------------------------------
Vector Time (GMT): 2018/161/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3609732
62 A = 6788933
08 meter
Y = -5663169
09 meter E =
0012616
Z = -948553
43 I = 51
95878
XDOT = 4473
051970 Wp = 149
54420
YDOT = -1862
873769 meter/sec RA = 51
14138 deg
ZDOT = -5945
361985 TA = 40
68450
MA = 40
59032
Ha = 221
399 n
mi
Hp = 214
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11842954
80 X = -3541529
60
Y = -18579951
09 feet Y = -5703154
16 meter
Z = -3112051
93 Z = -965923
46
XDOT = 14675
367356 XDOT = 4522
430485
YDOT = -6111
790580 feet/sec YDOT = -1812
576265 meter/sec
ZDOT = -19505
780790 ZDOT = -5923
513445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17530130
03 X = -5343183
63
Y = 13329683
88 feet Y = 4062887
65 meter
Z = -3188902
17 Z = -971977
38
XDOT = -6354
048770 XDOT = -1936
714065
YDOT = -12964
785061 feet/sec YDOT = -3951
666487 meter/sec
ZDOT = -19407
696615 ZDOT = -5915
465928
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 18161
57702285
00016717 00000-0 10270-3 0 9077
2 25544 51
6422 51
6729 0003255 176
7829 183
3345 15
54126851 37484
Satellite: ISS
Catalog Number: 25544
Epoch time: 18161
57702285 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 51
6729 deg
Eccentricity:
0003255
Arg of perigee: 176
7829 deg
Mean anomaly: 183
3345 deg
Mean motion: 15
54126851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3748
Checksum: 325
Coasting Arc #9 (Orbit 3763)
---------------------------------------
Vector Time (GMT): 2018/162/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2668447
67 A = 6786377
44 meter
Y = 5683015
56 meter E =
0013192
Z = 2564544
52 I = 51
92940
XDOT = -5546
654383 Wp = 88
76405
YDOT = 205
874580 meter/sec RA = 46
18791 deg
ZDOT = 5291
994199 TA = 299
94332
MA = 300
07424
Ha = 221
184 n
mi
Hp = 214
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8754749
58 X = 2592242
94
Y = 18645064
18 feet Y = 5712429
55 meter
Z = 8413859
97 Z = 2577322
76
XDOT = -18197
684985 XDOT = -5574
250352
YDOT = 675
441537 feet/sec YDOT = 143
693063 meter/sec
ZDOT = 17362
185693 ZDOT = 5264
983107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17677288
74 X = 5388037
61
Y = -10528403
21 feet Y = -3209057
30 meter
Z = 8470140
88 Z = 2581698
94
XDOT = 1745
733351 XDOT = 532
099526
YDOT = 16862
504788 feet/sec YDOT = 5139
691460 meter/sec
ZDOT = 17241
258934 ZDOT = 5255
135723
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 18162
60582709
00016717 00000-0 10270-3 0 9080
2 25544 51
6423 46
5436 0002958 181
6347 178
4797 15
54172905 37647
Satellite: ISS
Catalog Number: 25544
Epoch time: 18162
60582709 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 46
5436 deg
Eccentricity:
0002958
Arg of perigee: 181
6347 deg
Mean anomaly: 178
4797 deg
Mean motion: 15
54172905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3764
Checksum: 341
Coasting Arc #10 (Orbit 3778)
---------------------------------------
Vector Time (GMT): 2018/163/13:07:16
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1401859
49 A = 6782582
83 meter
Y = -5340604
30 meter E =
0006199
Z = -3943562
62 I = 51
89210
XDOT = 6357
425671 Wp = 99
07726
YDOT = 1329
458570 meter/sec RA = 41
22423 deg
ZDOT = -4066
767202 TA = 128
53862
MA = 128
48304
Ha = 221
117 n
mi
Hp = 214
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4599276
55 X = -1322879
23
Y = -17521667
65 feet Y = -5355838
63 meter
Z = -12938197
56 Z = -3950181
45
XDOT = 20857
695771 XDOT = 6361
841249
YDOT = 4361
740716 feet/sec YDOT = 1400
577012 meter/sec
ZDOT = -13342
412080 ZDOT = -4035
873719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16870452
67 X = -5142113
97
Y = 6542558
94 feet Y = 1994171
97 meter
Z = -12966953
67 Z = -3952327
48
XDOT = 2344
680705 XDOT = 714
658679
YDOT = -20082
816442 feet/sec YDOT = -6121
242451 meter/sec
ZDOT = -13204
359378 ZDOT = -4024
688738
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 18163
57032785
00016717 00000-0 10270-3 0 9092
2 25544 51
6412 41
7349 0002972 186
0233 174
0885 15
54171786 37796
Satellite: ISS
Catalog Number: 25544
Epoch time: 18163
57032785 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 41
7349 deg
Eccentricity:
0002972
Arg of perigee: 186
0233 deg
Mean anomaly: 174
0885 deg
Mean motion: 15
54171786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3779
Checksum: 332
Coasting Arc #11 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2018/164/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -41696
87 A = 6779239
94 meter
Y = -4764947
50 meter E =
0010688
Z = -4831472
03 I = 51
85915
XDOT = 6759
791185 Wp = 86
27006
YDOT = 2534
235524 meter/sec RA = 36
73133 deg
ZDOT = -2561
882813 TA = 158
58753
MA = 158
54278
Ha = 221
065 n
mi
Hp = 214
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -136800
75 X = 35058
12
Y = -15633029
85 feet Y = -4764983
77 meter
Z = -15851286
18 Z = -4831488
98
XDOT = 22177
792602 XDOT = 6743
394647
YDOT = 8314
421010 feet/sec YDOT = 2609
736934 meter/sec
ZDOT = -8405
127338 ZDOT = -2529
085185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13923219
22 X = -4243797
22
Y = -7111729
42 feet Y = -2167655
13 meter
Z = -15850579
85 Z = -4831256
74
XDOT = 17031
120800 XDOT = 5191
085620
YDOT = -14966
902721 feet/sec YDOT = -4561
911949 meter/sec
ZDOT = -8258
752403 ZDOT = -2517
267732
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 18164
47052765
00016717 00000-0 10270-3 0 9104
2 25544 51
6422 37
2482 0002964 187
0208 173
0904 15
54200064 37938
Satellite: ISS
Catalog Number: 25544
Epoch time: 18164
47052765 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 37
2482 deg
Eccentricity:
0002964
Arg of perigee: 187
0208 deg
Mean anomaly: 173
0904 deg
Mean motion: 15
54200064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 296
Coasting Arc #12 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2018/165/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1537357
52 A = 6777260
85 meter
Y = 3942041
15 meter E =
0004714
Z = 5292780
83 I = 51
82585
XDOT = -6762
253803 Wp = 153
85295
YDOT = -3555
697835 meter/sec RA = 31
74697 deg
ZDOT = 679
724578 TA = 289
64913
MA = 289
70000
Ha = 221
023 n
mi
Hp = 214
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5043823
89 X = -1607033
85
Y = 12933205
86 feet Y = 3924458
79 meter
Z = 17364766
50 Z = 5285144
35
XDOT = -22185
872057 XDOT = -6725
292184
YDOT = -11665
675311 feet/sec YDOT = -3631
111474 meter/sec
ZDOT = 2230
067514 ZDOT = 646
964910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9330220
36 X = 2843851
16
Y = 10337476
64 feet Y = 3150862
88 meter
Z = 17329935
19 Z = 5282164
25
XDOT = -19511
598394 XDOT = -5947
135191
YDOT = 14092
702739 feet/sec YDOT = 4295
455795 meter/sec
ZDOT = 2084
034340 ZDOT = 635
213667
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 18165
49932292
00016717 00000-0 10270-3 0 9110
2 25544 51
6426 32
1192 0003051 191
9702 168
1379 15
54203814 38090
Satellite: ISS
Catalog Number: 25544
Epoch time: 18165
49932292 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 32
1192 deg
Eccentricity:
0003051
Arg of perigee: 191
9702 deg
Mean anomaly: 168
1379 deg
Mean motion: 15
54203814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 304
Coasting Arc #13 (Orbit 3823)
---------------------------------------
Vector Time (GMT): 2018/166/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3141363
31 A = 6777705
75 meter
Y = -3008131
83 meter E =
0013942
Z = -5210255
89 I = 51
79831
XDOT = 6225
217418 Wp = 111
63750
YDOT = 4271
345681 meter/sec RA = 26
75769 deg
ZDOT = 1284
999635 TA = 170
70416
MA = 170
67833
Ha = 220
870 n
mi
Hp = 214
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10306310
06 X = 3200076
18
Y = -9869198
92 feet Y = -2972673
71 meter
Z = -17094015
39 Z = -5194854
23
XDOT = 20423
941660 XDOT = 6170
749561
YDOT = 14013
601314 feet/sec YDOT = 4340
655566 meter/sec
ZDOT = 4215
878066 ZDOT = 1315
107977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4494236
14 X = -1369843
18
Y = -13630552
12 feet Y = -4154592
28 meter
Z = -17024581
26 Z = -5189092
37
XDOT = 20370
815549 XDOT = 6209
024579
YDOT = -12158
938684 feet/sec YDOT = -3706
044511 meter/sec
ZDOT = 4349
923149 ZDOT = 1325
856576
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 18166
46381549
00016717 00000-0 10270-3 0 9122
2 25544 51
6422 27
3103 0002901 196
5301 163
5757 15
54208987 38245
Satellite: ISS
Catalog Number: 25544
Epoch time: 18166
46381549 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 27
3103 deg
Eccentricity:
0002901
Arg of perigee: 196
5301 deg
Mean anomaly: 163
5757 deg
Mean motion: 15
54208987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3824
Checksum: 311
Coasting Arc #14 (Orbit 3839)
---------------------------------------
Vector Time (GMT): 2018/167/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4585970
59 A = 6780301
35 meter
Y = 2032386
96 meter E =
0007113
Z = 4556211
84 I = 51
77665
XDOT = -5189
033764 Wp = 83
37292
YDOT = -4714
294285 meter/sec RA = 21
77168 deg
ZDOT = -3115
054467 TA = 37
77387
MA = 37
72397
Ha = 220
832 n
mi
Hp = 214
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15045835
25 X = -4630487
95
Y = 6667936
20 feet Y = 1980853
80 meter
Z = 14948201
56 Z = 4533827
17
XDOT = -17024
388989 XDOT = -5120
800407
YDOT = -15466
844767 feet/sec YDOT = -4771
939598 meter/sec
ZDOT = -10219
994969 ZDOT = -3140
095859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -129924
96 X = -39601
13
Y = 16547413
62 feet Y = 5043651
67 meter
Z = 14847676
03 Z = 4525571
65
XDOT = -19855
208009 XDOT = -6051
867401
YDOT = 9128
893213 feet/sec YDOT = 2782
486651 meter/sec
ZDOT = -10331
285895 ZDOT = -3148
975941
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 18167
49260404
00016717 00000-0 10270-3 0 9133
2 25544 51
6415 22
1815 0002833 202
3739 157
7290 15
54241752 38407
Satellite: ISS
Catalog Number: 25544
Epoch time: 18167
49260404 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 22
1815 deg
Eccentricity:
0002833
Arg of perigee: 202
3739 deg
Mean anomaly: 157
7290 deg
Mean motion: 15
54241752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3840
Checksum: 294
Coasting Arc #15 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2018/168/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5751420
07 A = 6784230
53 meter
Y = -1091514
21 meter E =
0004343
Z = -3434278
68 I = 51
75817
XDOT = 3677
128990 Wp = 125
43658
YDOT = 4898
720500 meter/sec RA = 16
79229 deg
ZDOT = 4602
809385 TA = 194
45350
MA = 194
46592
Ha = 220
692 n
mi
Hp = 215
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18869488
43 X = 5779879
97
Y = -3581083
37 feet Y = -1027038
24 meter
Z = -11267318
50 Z = -3406271
59
XDOT = 12064
071489 XDOT = 3599
719078
YDOT = 16071
917652 feet/sec YDOT = 4939
407201 meter/sec
ZDOT = 15101
080661 ZDOT = 4620
484114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4180685
88 X = 1274273
06
Y = -18820643
47 feet Y = -5736532
13 meter
Z = -11141789
04 Z = -3396017
30
XDOT = 18116
548011 XDOT = 5521
923834
YDOT = -4958
651944 feet/sec YDOT = -1511
397112 meter/sec
ZDOT = 15179
368524 ZDOT = 4626
671526
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 18168
45709335
00016717 00000-0 10270-3 0 9142
2 25544 51
6413 17
3727 0002925 206
7505 153
3498 15
54201123 38550
Satellite: ISS
Catalog Number: 25544
Epoch time: 18168
45709335 = yrday
fracday
Element set: 914
Inclination: 51
6413 deg
RA of node: 17
3727 deg
Eccentricity:
0002925
Arg of perigee: 206
7505 deg
Mean anomaly: 153
3498 deg
Mean motion: 15
54201123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 306
Coasting Arc #16 (Orbit 3870)
---------------------------------------
Vector Time (GMT): 2018/169/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6498748
02 A = 6787590
15 meter
Y = 188931
58 meter E =
0013918
Z = 1922562
10 I = 51
73840
XDOT = -1810
190288 Wp = 124
35328
YDOT = -4903
756481 meter/sec RA = 11
82130 deg
ZDOT = -5615
716978 TA = 34
47586
MA = 34
38566
Ha = 220
663 n
mi
Hp = 215
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21321351
77 X = -6509716
40
Y = 619854
28 feet Y = 116196
55 meter
Z = 6307618
44 Z = 1890967
14
XDOT = -5938
944514 XDOT = -1727
942693
YDOT = -16088
439898 feet/sec YDOT = -4923
538727 meter/sec
ZDOT = -18424
268302 ZDOT = -5624
310992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7513288
31 X = -2290050
28
Y = 20007471
94 feet Y = 6098277
45 meter
Z = 6166188
16 Z = 1879454
15
XDOT = -15635
470055 XDOT = -4765
691273
YDOT = -159
619246 feet/sec YDOT = -48
651946 meter/sec
ZDOT = -18461
913829 ZDOT = -5627
191335
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 18169
48587748
00016717 00000-0 10270-3 0 9159
2 25544 51
6421 12
2432 0002795 209
9285 150
1708 15
54212458 38711
Satellite: ISS
Catalog Number: 25544
Epoch time: 18169
48587748 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 12
2432 deg
Eccentricity:
0002795
Arg of perigee: 209
9285 deg
Mean anomaly: 150
1708 deg
Mean motion: 15
54212458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3871
Checksum: 324
Coasting Arc #17 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2018/170/10:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 923225
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6751970
76 A = 6789072
15 meter
Y = 628793
76 meter E =
0008962
Z = -229986
71 I = 51
70931
XDOT = -242
922725 Wp = 46
62712
YDOT = 4751
471141 meter/sec RA = 6
85479 deg
ZDOT = 6012
120990 TA = 310
89772
MA = 310
97531
Ha = 220
547 n
mi
Hp = 215
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22152135
04 X = 6745554
74
Y = 2062971
67 feet Y = 704263
10 meter
Z = -754549
58 Z = -197203
76
XDOT = -796
990569 XDOT = -325
240398
YDOT = 15588
816078 feet/sec YDOT = 4748
293735 meter/sec
ZDOT = 19724
806396 ZDOT = 6010
741513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9956579
91 X = 3034765
56
Y = -19900733
66 feet Y = -6065743
62 meter
Z = -607947
66 Z = -185302
45
XDOT = 12741
825896 XDOT = 3883
708533
YDOT = 5791
580032 feet/sec YDOT = 1765
273594 meter/sec
ZDOT = 19717
844375 ZDOT = 6009
998965
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 18170
45035965
00016717 00000-0 10270-3 0 9168
2 25544 51
6404 7
4341 0002832 213
9878 146
1094 15
54210759 38863
Satellite: ISS
Catalog Number: 25544
Epoch time: 18170
45035965 = yrday
fracday
Element set: 916
Inclination: 51
6404 deg
RA of node: 7
4341 deg
Eccentricity:
0002832
Arg of perigee: 213
9878 deg
Mean anomaly: 146
1094 deg
Mean motion: 15
54210759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 315
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