[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 18th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
354/01:40:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
1
000/00:00:00
000 0
0 0
0 214
1
358/04:25:00
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
6
361/02:52:50
495 -1
8 2
2 2
2
N/A 1
1 -0
0 221
4
000/00:05:40
991 0
6 -0
0 216
2
361/09:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
5
000/00:00:00
000 0
0 0
0 216
2
364/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
7
Coasting Arc #1 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2018/351/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6402949
33 A = 6787642
74 meter
Y = -895374
64 meter E =
0017980
Z = 2034308
32 I = 51
60338
XDOT = 2431
049173 Wp = 121
59194
YDOT = 4705
618394 meter/sec RA = 186
47917 deg
ZDOT = -5553
654440 TA = 35
89028
MA = 35
76962
Ha = 222
332 n
mi
Hp = 213
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21007051
60 X = 6402604
13
Y = -2937580
84 feet Y = -823774
45 meter
Z = 6674239
89 Z = 2065410
88
XDOT = 7975
883115 XDOT = 2405
225800
YDOT = 15438
380559 feet/sec YDOT = 4732
660004 meter/sec
ZDOT = -18220
651051 ZDOT = -5541
907644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -985358
70 X = -300337
33
Y = -21143889
61 feet Y = -6444657
55 meter
Z = 6814402
16 Z = 2077029
78
XDOT = 14578
040202 XDOT = 4443
386653
YDOT = -6562
622478 feet/sec YDOT = -2000
287331 meter/sec
ZDOT = -18168
206441 ZDOT = -5537
669323
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 18351
03630475
00016717 00000-0 10270-3 0 9003
2 25544 51
6379 187
5003 0004979 151
7704 208
3720 15
54080793 26946
Satellite: ISS
Catalog Number: 25544
Epoch time: 18351
03630475 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 187
5003 deg
Eccentricity:
0004979
Arg of perigee: 151
7704 deg
Mean anomaly: 208
3720 deg
Mean motion: 15
54080793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2694
Checksum: 313
Coasting Arc #2 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2018/352/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6773770
26 A = 6789289
54 meter
Y = 141728
75 meter E =
0010116
Z = -404141
78 I = 51
64320
XDOT = -449
660197 Wp = 68
82380
YDOT = -4756
349050 meter/sec RA = 181
50699 deg
ZDOT = 5993
301164 TA = 286
82136
MA = 286
93230
Ha = 222
242 n
mi
Hp = 213
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22223655
72 X = -6772888
55
Y = 464989
34 feet Y = 65984
70 meter
Z = -1325924
48 Z = -437044
50
XDOT = -1475
263113 XDOT = -425
552460
YDOT = -15604
819717 feet/sec YDOT = -4761
243067 meter/sec
ZDOT = 19663
061563 ZDOT = 5991
175092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1210622
09 X = -368997
61
Y = 22186177
51 feet Y = 6762346
91 meter
Z = -1474139
01 Z = -449317
57
XDOT = -14062
200603 XDOT = -4286
158744
YDOT = 514
129685 feet/sec YDOT = 156
706728 meter/sec
ZDOT = 19653
949167 ZDOT = 5990
523706
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 18352
00086897
00016717 00000-0 10270-3 0 9015
2 25544 51
6388 182
6927 0004966 156
8462 203
2916 15
54110660 27095
Satellite: ISS
Catalog Number: 25544
Epoch time: 18352
00086897 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 182
6927 deg
Eccentricity:
0004966
Arg of perigee: 156
8462 deg
Mean anomaly: 203
2916 deg
Mean motion: 15
54110660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2709
Checksum: 324
Coasting Arc #3 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2018/353/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6623788
91 A = 6788825
44 meter
Y = 637638
28 meter E =
0013717
Z = -1311067
00 I = 51
67269
XDOT = -1600
782827 Wp = 148
40035
YDOT = 4716
229205 meter/sec RA = 176
53825 deg
ZDOT = -5832
777225 TA = 45
86499
MA = 45
75226
Ha = 222
314 n
mi
Hp = 213
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21731590
92 X = 6622534
90
Y = 2091989
09 feet Y = 711703
19 meter
Z = -4301400
91 Z = -1278893
62
XDOT = -5251
912161 XDOT = -1625
069233
YDOT = 15473
192930 feet/sec YDOT = 4698
192840 meter/sec
ZDOT = -19136
408220 ZDOT = -5840
611934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3354581
72 X = 1022476
51
Y = -21601170
44 feet Y = -6584036
75 meter
Z = -4156528
50 Z = -1266909
89
XDOT = 13572
118947 XDOT = 4136
781855
YDOT = 5771
341025 feet/sec YDOT = 1759
104744 meter/sec
ZDOT = -19172
164225 ZDOT = -5843
675656
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 18353
02973733
00016717 00000-0 10270-3 0 9023
2 25544 51
6372 177
5636 0004861 158
6104 201
5252 15
54067346 27259
Satellite: ISS
Catalog Number: 25544
Epoch time: 18353
02973733 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 177
5636 deg
Eccentricity:
0004861
Arg of perigee: 158
6104 deg
Mean anomaly: 201
5252 deg
Mean motion: 15
54067346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2725
Checksum: 306
Coasting Arc #4 (Orbit 2740)
---------------------------------------
Vector Time (GMT): 2018/354/00:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 966149
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5995706
98 A = 6786094
97 meter
Y = -1387321
92 meter E =
0014630
Z = 2850496
54 I = 51
69540
XDOT = 3483
218215 Wp = 99
48074
YDOT = -4570
773338 meter/sec RA = 171
56751 deg
ZDOT = 5077
421546 TA = 292
90302
MA = 293
05738
Ha = 222
129 n
mi
Hp = 214
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19670954
65 X = -5993594
28
Y = -4551581
10 feet Y = -1454358
58 meter
Z = 9352022
77 Z = 2821376
17
XDOT = 11427
881283 XDOT = 3509
407332
YDOT = -14995
975520 feet/sec YDOT = -4531
675688 meter/sec
ZDOT = 16658
207172 ZDOT = 5094
405091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5356514
31 X = -1632665
56
Y = 19529601
80 feet Y = 5952622
63 meter
Z = 9220959
02 Z = 2810548
31
XDOT = -13093
771330 XDOT = -3990
981501
YDOT = -11531
487697 feet/sec YDOT = -3514
797450 meter/sec
ZDOT = 16735
177569 ZDOT = 5100
882123
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 18354
05860460
00016717 00000-0 10270-3 0 9030
2 25544 51
6357 172
4354 0004768 164
9787 195
1508 15
54090457 27415
Satellite: ISS
Catalog Number: 25544
Epoch time: 18354
05860460 = yrday
fracday
Element set: 903
Inclination: 51
6357 deg
RA of node: 172
4354 deg
Eccentricity:
0004768
Arg of perigee: 164
9787 deg
Mean anomaly: 195
1508 deg
Mean motion: 15
54090457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2741
Checksum: 329
Coasting Arc #5 (Orbit 2741)
---------------------------------------
Vector Time (GMT): 2018/354/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3600125
85 A = 6779982
15 meter
Y = -3237150
47 meter E =
0011444
Z = 4742979
15 I = 51
67692
XDOT = 6437
810744 Wp = 135
33210
YDOT = -3165
402514 meter/sec RA = 171
21740 deg
ZDOT = 2714
204614 TA = 287
79421
MA = 287
91905
Ha = 222
115 n
mi
Hp = 214
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11811436
53 X = -3586698
67
Y = -10620572
41 feet Y = -3277335
03 meter
Z = 15560955
20 Z = 4725523
07
XDOT = 21121
426325 XDOT = 6459
544390
YDOT = -10385
178853 feet/sec YDOT = -3093
289217 meter/sec
ZDOT = 8904
870781 ZDOT = 2745
530008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5161126
95 X = -1573111
49
Y = 15103011
50 feet Y = 4603397
90 meter
Z = 15482626
73 Z = 4719104
63
XDOT = -16644
944525 XDOT = -5073
379091
YDOT = -15002
109155 feet/sec YDOT = -4572
642871 meter/sec
ZDOT = 9046
320809 ZDOT = 2757
318583
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 18354
12290960
00016717 00000-0 10270-3 0 9041
2 25544 51
6353 172
1147 0004648 165
9021 194
2262 15
54092607 27424
Satellite: ISS
Catalog Number: 25544
Epoch time: 18354
12290960 = yrday
fracday
Element set: 904
Inclination: 51
6353 deg
RA of node: 172
1147 deg
Eccentricity:
0004648
Arg of perigee: 165
9021 deg
Mean anomaly: 194
2262 deg
Mean motion: 15
54092607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2742
Checksum: 299
Coasting Arc #6 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2018/355/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1945777
04 A = 6777821
21 meter
Y = 3808544
46 meter E =
0015542
Z = -5270953
25 I = 51
70272
XDOT = -7194
056473 Wp = 100
60650
YDOT = 2473
874723 meter/sec RA = 166
22326 deg
ZDOT = -873
165804 TA = 161
06810
MA = 161
01025
Ha = 222
021 n
mi
Hp = 214
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6383782
95 X = 1928647
92
Y = 12495224
61 feet Y = 3830208
42 meter
Z = -17293153
72 Z = -5261542
37
XDOT = -23602
547484 XDOT = -7216
943945
YDOT = 8116
386886 feet/sec YDOT = 2393
297927 meter/sec
ZDOT = -2864
717204 ZDOT = -908
167564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8803352
76 X = 2683261
92
Y = -10992547
75 feet Y = -3350528
56 meter
Z = -17251126
41 Z = -5258143
33
XDOT = 16150
225930 XDOT = 4922
588863
YDOT = 17651
815810 feet/sec YDOT = 5380
273459 meter/sec
ZDOT = -3022
690980 ZDOT = -921
316211
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 18355
08747389
00016717 00000-0 10270-3 0 9050
2 25544 51
6359 167
3055 0004621 167
8673 192
2592 15
54065581 27570
Satellite: ISS
Catalog Number: 25544
Epoch time: 18355
08747389 = yrday
fracday
Element set: 905
Inclination: 51
6359 deg
RA of node: 167
3055 deg
Eccentricity:
0004621
Arg of perigee: 167
8673 deg
Mean anomaly: 192
2592 deg
Mean motion: 15
54065581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2757
Checksum: 344
Coasting Arc #7 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2018/356/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -220292
35 A = 6777847
38 meter
Y = -4289802
94 meter E =
0004501
Z = 5239351
02 I = 51
73536
XDOT = 7418
830633 Wp = 124
95136
YDOT = -1652
450167 meter/sec RA = 161
22984 deg
ZDOT = -1042
925741 TA = 335
00815
MA = 335
02993
Ha = 221
940 n
mi
Hp = 214
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -722743
95 X = -197756
28
Y = -14074156
64 feet Y = -4292141
18 meter
Z = 17189471
85 Z = 5238335
01
XDOT = 24339
995515 XDOT = 7441
823409
YDOT = -5421
424431 feet/sec YDOT = -1569
358930 meter/sec
ZDOT = -3421
672378 ZDOT = -1006
831918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12422151
37 X = -3786271
74
Y = 6666103
01 feet Y = 2031828
20 meter
Z = 17185325
49 Z = 5238087
21
XDOT = -14659
242393 XDOT = -4468
137081
YDOT = -18931
846406 feet/sec YDOT = -5770
426784 meter/sec
ZDOT = -3258
829089 ZDOT = -993
291106
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 18356
11634065
00016717 00000-0 10270-3 0 9062
2 25544 51
6363 162
1769 0004504 171
6828 188
4400 15
54067837 27734
Satellite: ISS
Catalog Number: 25544
Epoch time: 18356
11634065 = yrday
fracday
Element set: 906
Inclination: 51
6363 deg
RA of node: 162
1769 deg
Eccentricity:
0004504
Arg of perigee: 171
6828 deg
Mean anomaly: 188
4400 deg
Mean motion: 15
54067837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 320
Coasting Arc #8 (Orbit 2787)
---------------------------------------
Vector Time (GMT): 2018/357/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1463275
01 A = 6780182
76 meter
Y = 4682651
42 meter E =
0013170
Z = -4692763
84 I = 51
77405
XDOT = -7074
176025 Wp = 127
72610
YDOT = 655
108476 meter/sec RA = 156
24163 deg
ZDOT = 2857
157115 TA = 170
64325
MA = 170
61869
Ha = 221
808 n
mi
Hp = 214
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4800771
03 X = -1492734
08
Y = 15363029
59 feet Y = 4666124
07 meter
Z = -15396206
83 Z = -4699942
73
XDOT = -23209
238927 XDOT = -7094
854384
YDOT = 2149
306022 feet/sec YDOT = 575
884060 meter/sec
ZDOT = 9373
875048 ZDOT = 2822
743196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15875290
93 X = 4838788
68
Y = -2456212
79 feet Y = -748653
66 meter
Z = -15429044
75 Z = -4702772
84
XDOT = 11884
830442 XDOT = 3622
496319
YDOT = 18858
229337 feet/sec YDOT = 5747
988302 meter/sec
ZDOT = 9218
674546 ZDOT = 2809
852002
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 18357
08090291
00016717 00000-0 10270-3 0 9077
2 25544 51
6361 157
3688 0004429 175
9159 184
2031 15
54057922 27882
Satellite: ISS
Catalog Number: 25544
Epoch time: 18357
08090291 = yrday
fracday
Element set: 907
Inclination: 51
6361 deg
RA of node: 157
3688 deg
Eccentricity:
0004429
Arg of perigee: 175
9159 deg
Mean anomaly: 184
2031 deg
Mean motion: 15
54057922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2788
Checksum: 333
Coasting Arc #9 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2018/358/01:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2950962
50 A = 6783747
55 meter
Y = -4889551
88 meter E =
0012266
Z = 3647700
06 I = 51
81755
XDOT = 6271
631231 Wp = 106
64627
YDOT = 501
282656 meter/sec RA = 151
26424 deg
ZDOT = -4392
991393 TA = 30
13401
MA = 30
06350
Ha = 221
635 n
mi
Hp = 214
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9681635
49 X = 2987701
08
Y = -16041836
86 feet Y = -4856347
28 meter
Z = 11967519
89 Z = 3662123
20
XDOT = 20576
217950 XDOT = 6286
898263
YDOT = 1644
628138 feet/sec YDOT = 571
502407 meter/sec
ZDOT = -14412
701420 ZDOT = -4362
489107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18646701
15 X = -5683514
51
Y = -1342527
29 feet Y = -409202
32 meter
Z = 12033049
69 Z = 3667673
54
XDOT = -7946
452682 XDOT = -2422
078778
YDOT = -17834
781303 feet/sec YDOT = -5436
041341 meter/sec
ZDOT = -14275
226860 ZDOT = -4351
089147
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 18358
10976968
00016717 00000-0 10270-3 0 9086
2 25544 51
6374 152
2403 0004393 180
1713 179
9438 15
54083834 28041
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
10976968 = yrday
fracday
Element set: 908
Inclination: 51
6374 deg
RA of node: 152
2403 deg
Eccentricity:
0004393
Arg of perigee: 180
1713 deg
Mean anomaly: 179
9438 deg
Mean motion: 15
54083834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 331
Coasting Arc #10 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2018/358/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4994923
40 A = 6781305
71 meter
Y = -1192101
10 meter E =
0011697
Z = 4425770
24 I = 51
81404
XDOT = 4273
532718 Wp = 130
96863
YDOT = -5414
891943 meter/sec RA = 150
74615 deg
ZDOT = 3351
326331 TA = 285
18985
MA = 285
31917
Ha = 221
808 n
mi
Hp = 214
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16387543
97 X = -5002719
60
Y = -3911092
86 feet Y = -1248002
04 meter
Z = 14520243
56 Z = 4401487
76
XDOT = 14020
776634 XDOT = 4317
487129
YDOT = -17765
393514 feet/sec YDOT = -5366
857053 meter/sec
ZDOT = 10995
165127 ZDOT = 3372
191436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13822942
72 X = 4213232
94
Y = 9794819
25 feet Y = 2985460
91 meter
Z = 14410880
89 Z = 4392436
50
XDOT = -18867
515954 XDOT = -5750
818863
YDOT = 10246
166966 feet/sec YDOT = 3123
031691 meter/sec
ZDOT = 11089
795664 ZDOT = 3380
169718
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 18358
23837854
00016717 00000-0 10270-3 0 9091
2 25544 51
6391 151
6000 0004456 180
1487 179
9665 15
54073573 28067
Satellite: ISS
Catalog Number: 25544
Epoch time: 18358
23837854 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 151
6000 deg
Eccentricity:
0004456
Arg of perigee: 180
1487 deg
Mean anomaly: 179
9665 deg
Mean motion: 15
54073573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 332
Coasting Arc #11 (Orbit 2820)
---------------------------------------
Vector Time (GMT): 2018/359/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3755232
83 A = 6778312
98 meter
Y = 2337554
29 meter E =
0013012
Z = -5146885
50 I = 51
83433
XDOT = -5403
842768 Wp = 96
80343
YDOT = 5189
585591 meter/sec RA = 145
76455 deg
ZDOT = -1590
713142 TA = 157
90788
MA = 157
85175
Ha = 221
583 n
mi
Hp = 214
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12320317
68 X = 3753815
04
Y = 7669141
37 feet Y = 2379540
63 meter
Z = -16886107
28 Z = -5128647
29
XDOT = -17729
142939 XDOT = -5453
745814
YDOT = 17026
199444 feet/sec YDOT = 5128
877238 meter/sec
ZDOT = -5218
875138 ZDOT = -1617
083313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8860730
49 X = -2700750
65
Y = -11612760
78 feet Y = -3539569
49 meter
Z = -16804101
24 Z = -5121890
06
XDOT = 21771
974884 XDOT = 6636
097945
YDOT = -8911
229994 feet/sec YDOT = -2716
142902 meter/sec
ZDOT = -5338
325511 ZDOT = -1627
121616
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 18359
20293915
00016717 00000-0 10270-3 0 9105
2 25544 51
6406 146
7921 0004331 183
5585 176
5538 15
54099566 28218
Satellite: ISS
Catalog Number: 25544
Epoch time: 18359
20293915 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 146
7921 deg
Eccentricity:
0004331
Arg of perigee: 183
5585 deg
Mean anomaly: 176
5538 deg
Mean motion: 15
54099566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2821
Checksum: 327
Coasting Arc #12 (Orbit 2836)
---------------------------------------
Vector Time (GMT): 2018/360/04:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950917
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2370499
26 A = 6777409
26 meter
Y = -3459929
70 meter E =
0004164
Z = 5322120
49 I = 51
85813
XDOT = 6090
781627 Wp = 155
04091
YDOT = -4651
808112 meter/sec RA = 140
78045 deg
ZDOT = -314
884850 TA = 297
93000
MA = 297
97216
Ha = 221
515 n
mi
Hp = 214
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7777228
55 X = -2357484
80
Y = -11351475
38 feet Y = -3486366
02 meter
Z = 17461025
22 Z = 5310636
88
XDOT = 19982
879355 XDOT = 6143
876293
YDOT = -15261
837638 feet/sec YDOT = -4583
399854 meter/sec
ZDOT = -1033
086778 ZDOT = -285
169933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3534158
45 X = 1077211
49
Y = 13365801
35 feet Y = 4073896
25 meter
Z = 17409588
08 Z = 5306442
45
XDOT = -23029
826994 XDOT = -7019
491268
YDOT = 7244
555861 feet/sec YDOT = 2208
140626 meter/sec
ZDOT = -898
587414 ZDOT = -273
889444
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 18360
23180351
00016717 00000-0 10270-3 0 9110
2 25544 51
6403 141
6641 0004362 189
0394 171
0681 15
54114975 28379
Satellite: ISS
Catalog Number: 25544
Epoch time: 18360
23180351 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 141
6641 deg
Eccentricity:
0004362
Arg of perigee: 189
0394 deg
Mean anomaly: 171
0681 deg
Mean motion: 15
54114975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2837
Checksum: 293
Coasting Arc #13 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2018/361/02:55:40
991
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -340907
84 A = 6782370
07 meter
Y = 5140076
36 meter E =
0009068
Z = -4420949
72 I = 51
89364
XDOT = -6407
403711 Wp = 138
47942
YDOT = 2485
625070 meter/sec RA = 136
09938 deg
ZDOT = 3381
388961 TA = 165
66152
MA = 165
63577
Ha = 221
413 n
mi
Hp = 216
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1118464
05 X = -376885
98
Y = 16863767
59 feet Y = 5136063
26 meter
Z = -14504428
23 Z = -4422692
71
XDOT = -21021
665720 XDOT = -6451
147201
YDOT = 8154
937893 feet/sec YDOT = 2413
728186 meter/sec
ZDOT = 11093
795804 ZDOT = 3350
158452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11920071
03 X = 3633237
65
Y = -11971047
03 feet Y = -3648775
13 meter
Z = -14512821
81 Z = -4423508
09
XDOT = 20342
861178 XDOT = 6200
504087
YDOT = 6967
516045 feet/sec YDOT = 2123
698891 meter/sec
ZDOT = 10952
666565 ZDOT = 3338
372769
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 18361
13206241
00016717 00000-0 10270-3 0 9128
2 25544 51
6398 137
1761 0004334 214
9459 145
1409 15
53675157 28513
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
13206241 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 137
1761 deg
Eccentricity:
0004334
Arg of perigee: 214
9459 deg
Mean anomaly: 145
1409 deg
Mean motion: 15
53675157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 305
Coasting Arc #14 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2018/361/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -918690
44 A = 6783813
19 meter
Y = 5394388
19 meter E =
0007216
Z = -4017587
78 I = 51
90136
XDOT = -6270
149094 Wp = 145
78940
YDOT = 1892
410399 meter/sec RA = 134
81079 deg
ZDOT = 3972
354824 TA = 165
44315
MA = 165
42235
Ha = 221
465 n
mi
Hp = 216
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3014076
23 X = -959428
70
Y = 17698123
97 feet Y = 5383887
25 meter
Z = -13181062
25 Z = -4022148
96
XDOT = -20571
355295 XDOT = -6310
139856
YDOT = 6208
695535 feet/sec YDOT = 1822
069352 meter/sec
ZDOT = 13032
660183 ZDOT = 3941
800084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12126423
13 X = -3696133
77
Y = -13217433
17 feet Y = -4028673
63 meter
Z = -13202195
73 Z = -4024029
26
XDOT = 6888
013643 XDOT = 2099
466558
YDOT = -19206
911645 feet/sec YDOT = -5854
266669 meter/sec
ZDOT = 12894
636282 ZDOT = 3930
285139
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 18361
38934599
00016717 00000-0 10270-3 0 9130
2 25544 51
6366 135
8908 0004588 214
4490 145
6365 15
53669069 28552
Satellite: ISS
Catalog Number: 25544
Epoch time: 18361
38934599 = yrday
fracday
Element set: 913
Inclination: 51
6366 deg
RA of node: 135
8908 deg
Eccentricity:
0004588
Arg of perigee: 214
4490 deg
Mean anomaly: 145
6365 deg
Mean motion: 15
53669069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2855
Checksum: 356
Coasting Arc #15 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2018/362/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1998112
33 A = 6787236
11 meter
Y = -5835238
66 meter E =
0011681
Z = 2815973
29 I = 51
93591
XDOT = 5679
075881 Wp = 119
48726
YDOT = -535
652011 meter/sec RA = 129
85053 deg
ZDOT = -5129
297042 TA = 28
67552
MA = 28
61134
Ha = 221
258 n
mi
Hp = 216
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6555486
63 X = 2049536
76
Y = -19144483
79 feet Y = -5812607
00 meter
Z = 9238757
50 Z = 2825803
89
XDOT = 18632
138717 XDOT = 5709
558719
YDOT = -1757
388486 feet/sec YDOT = -471
973917 meter/sec
ZDOT = -16828
402370 ZDOT = -5101
636399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11354371
42 X = 3460812
41
Y = 16725165
96 feet Y = 5097830
59 meter
Z = 9283715
75 Z = 2829676
56
XDOT = -8681
755400 XDOT = -2646
199046
YDOT = 15184
333168 feet/sec YDOT = 4628
184750 meter/sec
ZDOT = -16703
561170 ZDOT = -5091
245445
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 18362
41848312
00016717 00000-0 10270-3 0 9143
2 25544 51
6369 130
7638 0004563 220
8816 139
1995 15
53681057 28711
Satellite: ISS
Catalog Number: 25544
Epoch time: 18362
41848312 = yrday
fracday
Element set: 914
Inclination: 51
6369 deg
RA of node: 130
7638 deg
Eccentricity:
0004563
Arg of perigee: 220
8816 deg
Mean anomaly: 139
1995 deg
Mean motion: 15
53681057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2871
Checksum: 328
Coasting Arc #16 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2018/363/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2859705
44 A = 6789827
44 meter
Y = 5997703
83 meter E =
0004064
Z = -1388311
15 I = 51
96452
XDOT = -4877
649878 Wp = 35
16397
YDOT = -978
930233 meter/sec RA = 124
89899 deg
ZDOT = 5829
780513 TA = 309
78564
MA = 309
82141
Ha = 221
289 n
mi
Hp = 216
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9382235
69 X = -2919817
28
Y = 19677505
99 feet Y = 5965388
57 meter
Z = -4554826
62 Z = -1402348
19
XDOT = -16002
788314 XDOT = -4894
658434
YDOT = -3211
713364 feet/sec YDOT = -1033
570895 meter/sec
ZDOT = 19126
576487 ZDOT = 5806
045435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10387207
57 X = -3166020
87
Y = -19150710
57 feet Y = -5837136
58 meter
Z = -4618791
81 Z = -1407807
74
XDOT = 10702
227233 XDOT = 3262
038861
YDOT = -10382
851770 feet/sec YDOT = -3164
693219 meter/sec
ZDOT = 19019
595188 ZDOT = 5797
172613
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 18363
38330147
00016717 00000-0 10270-3 0 9153
2 25544 51
6366 125
9570 0004509 220
1005 139
9815 15
53666677 28868
Satellite: ISS
Catalog Number: 25544
Epoch time: 18363
38330147 = yrday
fracday
Element set: 915
Inclination: 51
6366 deg
RA of node: 125
9570 deg
Eccentricity:
0004509
Arg of perigee: 220
1005 deg
Mean anomaly: 139
9815 deg
Mean motion: 15
53666677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2886
Checksum: 325
Coasting Arc #17 (Orbit 2901)
---------------------------------------
Vector Time (GMT): 2018/364/09:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3507197
59 A = 6790551
53 meter
Y = -5802934
15 meter E =
0012516
Z = -180801
89 I = 51
98522
XDOT = 3963
052365 Wp = 156
75305
YDOT = 2578
610946 meter/sec RA = 119
95370 deg
ZDOT = -6039
655348 TA = 25
18583
MA = 25
12484
Ha = 221
062 n
mi
Hp = 216
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11506553
79 X = 3572705
21
Y = -19038497
87 feet Y = -5763347
94 meter
Z = -593182
04 Z = -163606
44
XDOT = 13002
140306 XDOT = 3963
260364
YDOT = 8460
009666 feet/sec YDOT = 2622
930045 meter/sec
ZDOT = -19815
142218 ZDOT = -6020
403678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8950891
41 X = 2728231
70
Y = 20367459
19 feet Y = 6208001
56 meter
Z = -514971
19 Z = -156963
22
XDOT = -12989
339959 XDOT = -3959
150819
YDOT = 5224
238811 feet/sec YDOT = 1592
347990 meter/sec
ZDOT = -19728
555781 ZDOT = -6013
263802
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 18364
41243837
00016717 00000-0 10270-3 0 9168
2 25544 51
6364 120
8301 0004425 227
0176 133
0605 15
53705298 29028
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
41243837 = yrday
fracday
Element set: 916
Inclination: 51
6364 deg
RA of node: 120
8301 deg
Eccentricity:
0004425
Arg of perigee: 227
0176 deg
Mean anomaly: 133
0605 deg
Mean motion: 15
53705298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2902
Checksum: 290
Coasting Arc #18 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2018/364/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4930869
77 A = 6784199
51 meter
Y = -2477502
71 meter E =
0003357
Z = -3947655
87 I = 51
96941
XDOT = 6
994506 Wp = 118
48103
YDOT = 6493
791195 meter/sec RA = 119
29965 deg
ZDOT = -4070
868783 TA = 109
13599
MA = 109
09965
Ha = 221
290 n
mi
Hp = 216
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16177394
27 X = 4977382
96
Y = -8128289
72 feet Y = -2422102
00 meter
Z = -12951626
86 Z = -3923590
70
XDOT = 22
947855 XDOT = -45
847382
YDOT = 21305
089221 feet/sec YDOT = 6493
574180 meter/sec
ZDOT = -13355
868712 ZDOT = -4070
962790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11886037
42 X = 3622864
21
Y = 13758889
48 feet Y = 4193709
51 meter
Z = -12842775
88 Z = -3914478
09
XDOT = -19616
281730 XDOT = -5979
042671
YDOT = 4491
387897 feet/sec YDOT = 1368
975031 meter/sec
ZDOT = -13356
993645 ZDOT = -4071
211663
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 18364
54108177
00016717 00000-0 10270-3 0 9170
2 25544 51
6401 120
1900 0004758 224
4459 135
6312 15
53659573 29041
Satellite: ISS
Catalog Number: 25544
Epoch time: 18364
54108177 = yrday
fracday
Element set: 917
Inclination: 51
6401 deg
RA of node: 120
1900 deg
Eccentricity:
0004758
Arg of perigee: 224
4459 deg
Mean anomaly: 135
6312 deg
Mean motion: 15
53659573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 305
Coasting Arc #19 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2018/365/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 950680
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4640080
48 A = 6780873
80 meter
Y = 1119823
28 meter E =
0007287
Z = 4816348
37 I = 51
97490
XDOT = 991
586149 Wp = 155
54171
YDOT = -7141
253508 meter/sec RA = 114
33553 deg
ZDOT = 2607
806626 TA = 268
83538
MA = 268
91886
Ha = 221
073 n
mi
Hp = 216
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15223361
15 X = -4675652
99
Y = 3673960
91 feet Y = 1067735
45 meter
Z = 15801667
89 Z = 4793722
22
XDOT = 3253
235396 XDOT = 1058
700649
YDOT = -23429
309411 feet/sec YDOT = -7129
789820 meter/sec
ZDOT = 8555
796016 ZDOT = 2612
785911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7577747
06 X = -2309697
30
Y = -13821959
65 feet Y = -4212933
30 meter
Z = 15699445
93 Z = 4785191
12
XDOT = 22436
402206 XDOT = 6838
615392
YDOT = -2526
655707 feet/sec YDOT = -770
124659 meter/sec
ZDOT = 8579
051204 ZDOT = 2614
894807
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 18365
57021737
00016717 00000-0 10270-3 0 9181
2 25544 51
6409 115
0629 0004645 229
2010 130
8740 15
53698262 29209
Satellite: ISS
Catalog Number: 25544
Epoch time: 18365
57021737 = yrday
fracday
Element set: 918
Inclination: 51
6409 deg
RA of node: 115
0629 deg
Eccentricity:
0004645
Arg of perigee: 229
2010 deg
Mean anomaly: 130
8740 deg
Mean motion: 15
53698262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 304
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