[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 21st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 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
057/02:24:45
635 -2
8 2
9 2
9
N/A -0
5 0
3 224
4
000/00:07:31
270 -0
6 -0
2 215
6
057/14:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
6
060/17:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
6
000/00:00:00
000 0
0 0
0 215
5
061/07:48:58
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
6
062/10:55:42
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 3711)
---------------------------------------
Vector Time (GMT): 2019/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -145442
13 A = 6782244
80 meter
Y = 4855739
32 meter E =
0016476
Z = -4748809
31 I = 51
37287
XDOT = -6600
209347 Wp = 63
53667
YDOT = -2808
552760 meter/sec RA = 220
35256 deg
ZDOT = -2669
665963 TA = 179
94456
MA = 179
94438
Ha = 224
174 n
mi
Hp = 214
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -477172
35 X = -176663
14
Y = 15930903
28 feet Y = 4853937
88 meter
Z = -15580083
04 Z = -4749592
06
XDOT = -21654
230142 XDOT = -6555
345389
YDOT = -9214
411942 feet/sec YDOT = -2882
110305 meter/sec
ZDOT = -8758
746598 ZDOT = -2701
617184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8465379
36 X = -2580247
63
Y = 13499491
93 feet Y = 4114645
14 meter
Z = -15584012
00 Z = -4750006
86
XDOT = -12862
981017 XDOT = -3920
636614
YDOT = -18343
644418 feet/sec YDOT = -5591
142818 meter/sec
ZDOT = -8902
762620 ZDOT = -2713
562047
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 19051
52092202
00016717 00000-0 10270-3 0 9005
2 25544 51
6364 221
3435 0005752 47
8879 312
2761 15
53289859 37129
Satellite: ISS
Catalog Number: 25544
Epoch time: 19051
52092202 = yrday
fracday
Element set: 900
Inclination: 51
6364 deg
RA of node: 221
3435 deg
Eccentricity:
0005752
Arg of perigee: 47
8879 deg
Mean anomaly: 312
2761 deg
Mean motion: 15
53289859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3712
Checksum: 308
Coasting Arc #2 (Orbit 3727)
---------------------------------------
Vector Time (GMT): 2019/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1347085
96 A = 6780359
85 meter
Y = -4132409
51 meter E =
0007902
Z = 5197040
60 I = 51
39147
XDOT = 6672
290815 Wp = 80
49610
YDOT = 3613
041386 meter/sec RA = 215
34566 deg
ZDOT = 1143
218150 TA = 358
51154
MA = 358
51389
Ha = 224
200 n
mi
Hp = 214
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4419573
35 X = 1367951
86
Y = -13557773
98 feet Y = -4117228
22 meter
Z = 17050658
12 Z = 5203635
21
XDOT = 21890
717896 XDOT = 6625
839881
YDOT = 11853
810321 feet/sec YDOT = 3687
396004 meter/sec
ZDOT = 3750
715715 ZDOT = 1175
515670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10467432
42 X = 3190473
40
Y = -9630748
93 feet Y = -2935452
27 meter
Z = 17080759
35 Z = 5206215
45
XDOT = 12393
434635 XDOT = 3777
518877
YDOT = 20381
573889 feet/sec YDOT = 6212
303721 meter/sec
ZDOT = 3896
249791 ZDOT = 1187
576936
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 19052
55031992
00016717 00000-0 10270-3 0 9019
2 25544 51
6355 216
2174 0005732 51
3966 308
7699 15
53253010 37284
Satellite: ISS
Catalog Number: 25544
Epoch time: 19052
55031992 = yrday
fracday
Element set: 901
Inclination: 51
6355 deg
RA of node: 216
2174 deg
Eccentricity:
0005732
Arg of perigee: 51
3966 deg
Mean anomaly: 308
7699 deg
Mean motion: 15
53253010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3728
Checksum: 307
Coasting Arc #3 (Orbit 3742)
---------------------------------------
Vector Time (GMT): 2019/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2592938
99 A = 6779868
46 meter
Y = 3375618
76 meter E =
0019564
Z = -5293884
95 I = 51
41969
XDOT = -6394
289845 Wp = 83
54735
YDOT = -4178
189097 meter/sec RA = 210
33987 deg
ZDOT = 471
371461 TA = 190
95042
MA = 190
99307
Ha = 224
223 n
mi
Hp = 214
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8507017
70 X = -2604779
11
Y = 11074864
71 feet Y = 3346555
92 meter
Z = -17368388
94 Z = -5306509
38
XDOT = -20978
641224 XDOT = -6349
382540
YDOT = -13707
969478 feet/sec YDOT = -4249
443369 meter/sec
ZDOT = 1546
494294 ZDOT = 440
420495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12685493
62 X = -3866538
46
Y = 5666371
15 feet Y = 1727109
93 meter
Z = -17425653
58 Z = -5311339
21
XDOT = -11383
479266 XDOT = -3469
684480
YDOT = -21194
227334 feet/sec YDOT = -6460
000491 meter/sec
ZDOT = 1407
066017 ZDOT = 428
873722
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 19053
51537736
00016717 00000-0 10270-3 0 9024
2 25544 51
6372 211
4137 0005665 55
7185 304
4503 15
53288820 37436
Satellite: ISS
Catalog Number: 25544
Epoch time: 19053
51537736 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 211
4137 deg
Eccentricity:
0005665
Arg of perigee: 55
7185 deg
Mean anomaly: 304
4503 deg
Mean motion: 15
53288820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3743
Checksum: 304
Coasting Arc #4 (Orbit 3758)
---------------------------------------
Vector Time (GMT): 2019/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3809635
21 A = 6781257
38 meter
Y = -2581316
76 meter E =
0011683
Z = 4974180
45 I = 51
45368
XDOT = 5806
274253 Wp = 58
36591
YDOT = 4569
960249 meter/sec RA = 205
33453 deg
ZDOT = -2065
779396 TA = 51
82352
MA = 51
71834
Ha = 224
216 n
mi
Hp = 214
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12498803
17 X = 3814055
61
Y = -8468887
02 feet Y = -2538689
55 meter
Z = 16319489
65 Z = 4992696
96
XDOT = 19049
456210 XDOT = 5764
774404
YDOT = 14993
307905 feet/sec YDOT = 4634
657818 meter/sec
ZDOT = -6777
491456 ZDOT = -2037
676343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14908454
11 X = 4544096
81
Y = -1713927
14 feet Y = -522404
99 meter
Z = 16403302
12 Z = 4999726
49
XDOT = 9775
631136 XDOT = 2979
612370
YDOT = 21079
463268 feet/sec YDOT = 6425
020404 meter/sec
ZDOT = -6650
936007 ZDOT = -2027
205295
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 19054
54477108
00016717 00000-0 10270-3 0 9035
2 25544 51
6375 206
2871 0005712 59
5442 300
6274 15
53254633 37592
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
54477108 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 206
2871 deg
Eccentricity:
0005712
Arg of perigee: 59
5442 deg
Mean anomaly: 300
6274 deg
Mean motion: 15
53254633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3759
Checksum: 311
Coasting Arc #5 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4898671
89 A = 6783764
60 meter
Y = 1852662
38 meter E =
0013235
Z = -4323398
27 I = 51
49361
XDOT = -4873
135225 Wp = 92
11558
YDOT = -4766
001204 meter/sec RA = 200
33856 deg
ZDOT = 3488
013225 TA = 213
44290
MA = 213
52655
Ha = 224
279 n
mi
Hp = 213
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16071758
16 X = -4898024
38
Y = 6078288
65 feet Y = 1797885
27 meter
Z = -14184377
51 Z = -4347192
48
XDOT = -15987
976461 XDOT = -4836
420907
YDOT = -15636
486890 feet/sec YDOT = -4820
290434 meter/sec
ZDOT = 11443
612943 ZDOT = 3464
431209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17000300
12 X = -5181691
48
Y = -1781223
06 feet Y = -542916
79 meter
Z = -14291977
08 Z = -4356194
62
XDOT = -7415
875186 XDOT = -2260
358757
YDOT = -19960
495068 feet/sec YDOT = -6083
958897 meter/sec
ZDOT = 11337
473655 ZDOT = 3455
661970
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 19055
50982336
00016717 00000-0 10270-3 0 9047
2 25544 51
6382 201
4833 0005720 62
2003 297
9728 15
53283376 37743
Satellite: ISS
Catalog Number: 25544
Epoch time: 19055
50982336 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 201
4833 deg
Eccentricity:
0005720
Arg of perigee: 62
2003 deg
Mean anomaly: 297
9728 deg
Mean motion: 15
53283376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 314
Coasting Arc #6 (Orbit 3789)
---------------------------------------
Vector Time (GMT): 2019/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5805625
78 A = 6787055
30 meter
Y = -1136049
15 meter E =
0017833
Z = 3313546
70 I = 51
53537
XDOT = 3639
771795 Wp = 83
96063
YDOT = 4860
550893 meter/sec RA = 195
35020 deg
ZDOT = -4687
196260 TA = 57
42129
MA = 57
24921
Ha = 224
254 n
mi
Hp = 214
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19047328
66 X = 5801802
73
Y = -3727195
36 feet Y = -1071147
74 meter
Z = 10871216
20 Z = 3341738
72
XDOT = 11941
508515 XDOT = 3607
916768
YDOT = 15946
689282 feet/sec YDOT = 4901
074943 meter/sec
ZDOT = -15377
940484 ZDOT = -4669
593503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18702783
37 X = 5700608
37
Y = 4910388
32 feet Y = 1496686
36 meter
Z = 10998637
95 Z = 3352384
85
XDOT = 4253
993556 XDOT = 1296
617236
YDOT = 18235
816395 feet/sec YDOT = 5558
276837 meter/sec
ZDOT = -15298
800182 ZDOT = -4663
074295
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 19056
53921253
00016717 00000-0 10270-3 0 9053
2 25544 51
6375 196
3577 0005653 66
7447 293
4300 15
53273468 37904
Satellite: ISS
Catalog Number: 25544
Epoch time: 19056
53921253 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 196
3577 deg
Eccentricity:
0005653
Arg of perigee: 66
7447 deg
Mean anomaly: 293
4300 deg
Mean motion: 15
53273468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3790
Checksum: 331
Coasting Arc #7 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2019/057/02:28:31
270
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1605161
19 A = 6781498
73 meter
Y = 3949783
94 meter E =
0017611
Z = -5288801
82 I = 51
53297
XDOT = -7324
507351 Wp = 86
90420
YDOT = -2125
479879 meter/sec RA = 192
36870 deg
ZDOT = 638
421818 TA = 189
19556
MA = 189
22785
Ha = 224
365 n
mi
Hp = 215
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5266276
86 X = -1623519
73
Y = 12958608
72 feet Y = 3931730
96 meter
Z = -17351712
00 Z = -5296643
81
XDOT = -24030
535929 XDOT = -7303
296327
YDOT = -6973
359183 feet/sec YDOT = -2207
269002 meter/sec
ZDOT = 2094
559769 ZDOT = 602
894170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2366902
43 X = 721431
86
Y = -13741036
42 feet Y = -4188267
90 meter
Z = -17387432
60 Z = -5299689
46
XDOT = 23963
261201 XDOT = 7304
002014
YDOT = 1691
651765 feet/sec YDOT = 515
615458 meter/sec
ZDOT = 1934
237746 ZDOT = 589
555665
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 19057
11824430
00016717 00000-0 10270-3 0 9068
2 25544 51
6395 193
4804 0003712 52
4628 307
6860 15
52747465 37994
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
11824430 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 193
4804 deg
Eccentricity:
0003712
Arg of perigee: 52
4628 deg
Mean anomaly: 307
6860 deg
Mean motion: 15
52747465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 326
Coasting Arc #8 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2327362
72 A = 6782005
79 meter
Y = 3755600
78 meter E =
0016502
Z = -5159812
69 I = 51
55235
XDOT = -7117
316601 Wp = 93
28602
YDOT = -2405
988732 meter/sec RA = 189
78861 deg
ZDOT = 1462
217670 TA = 190
81486
MA = 190
85038
Ha = 224
281 n
mi
Hp = 215
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7635704
46 X = -2344122
75
Y = 12321524
86 feet Y = 3729480
61 meter
Z = -16928519
32 Z = -5171158
90
XDOT = -23350
776250 XDOT = -7096
985736
YDOT = -7893
663819 feet/sec YDOT = -2485
465786 meter/sec
ZDOT = 4797
302067 ZDOT = 1427
694361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3277962
39 X = -999122
94
Y = 14058141
24 feet Y = 4284921
45 meter
Z = -16980057
47 Z = -5175521
52
XDOT = -23653
059103 XDOT = -7209
452414
YDOT = 78
671430 feet/sec YDOT = 23
979052 meter/sec
ZDOT = 4641
526190 ZDOT = 1414
737183
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 19057
63311763
00016717 00000-0 10270-3 0 9076
2 25544 51
6401 190
9169 0003402 58
5960 301
5524 15
52760682 38076
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
63311763 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 190
9169 deg
Eccentricity:
0003402
Arg of perigee: 58
5960 deg
Mean anomaly: 301
5524 deg
Mean motion: 15
52760682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 306
Coasting Arc #9 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3467185
97 A = 6783800
16 meter
Y = -3446005
64 meter E =
0011281
Z = 4697285
77 I = 51
59196
XDOT = 6575
694584 Wp = 62
51010
YDOT = 2781
985343 meter/sec RA = 184
80089 deg
ZDOT = -2802
511926 TA = 55
33551
MA = 55
22923
Ha = 224
195 n
mi
Hp = 215
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11375282
07 X = 3482646
04
Y = -11305792
79 feet Y = -3407146
50 meter
Z = 15411042
56 Z = 4714165
50
XDOT = 21573
801130 XDOT = 6557
709761
YDOT = 9127
248502 feet/sec YDOT = 2855
418670 meter/sec
ZDOT = -9194
592932 ZDOT = -2770
613961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6910415
38 X = 2106294
61
Y = -14390959
33 feet Y = -4386364
40 meter
Z = 15487565
15 Z = 4720609
86
XDOT = 22385
198660 XDOT = 6823
008552
YDOT = 972
759746 feet/sec YDOT = 296
497171 meter/sec
ZDOT = -9050
683180 ZDOT = -2758
648233
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 19058
66286444
00016717 00000-0 10270-3 0 9088
2 25544 51
6405 185
7937 0003464 60
2378 299
9118 15
52780819 38237
Satellite: ISS
Catalog Number: 25544
Epoch time: 19058
66286444 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 185
7937 deg
Eccentricity:
0003464
Arg of perigee: 60
2378 deg
Mean anomaly: 299
9118 deg
Mean motion: 15
52780819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 349
Coasting Arc #10 (Orbit 3837)
---------------------------------------
Vector Time (GMT): 2019/059/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4471389
50 A = 6786387
93 meter
Y = 3181755
78 meter E =
0009943
Z = -4001470
49 I = 51
63258
XDOT = -5761
081466 Wp = 94
76156
YDOT = -3120
383559 meter/sec RA = 179
82166 deg
ZDOT = 3964
178679 TA = 216
52347
MA = 216
59132
Ha = 224
316 n
mi
Hp = 215
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14669913
05 X = -4487199
90
Y = 10438831
29 feet Y = 3131665
00 meter
Z = -13128184
01 Z = -4023228
96
XDOT = -18901
185913 XDOT = -5745
015712
YDOT = -10237
478868 feet/sec YDOT = -3184
717994 meter/sec
ZDOT = 13005
835561 ZDOT = 3936
233172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10067100
97 X = -3068452
37
Y = 14840198
75 feet Y = 4523292
58 meter
Z = -13226743
44 Z = -4031511
40
XDOT = -20275
192056 XDOT = -6179
878539
YDOT = -2296
890262 feet/sec YDOT = -700
092152 meter/sec
ZDOT = 12879
788714 ZDOT = 3925
759600
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 19059
62825186
00016717 00000-0 10270-3 0 9098
2 25544 51
6392 180
9923 0003514 65
9421 294
2098 15
52777580 38383
Satellite: ISS
Catalog Number: 25544
Epoch time: 19059
62825186 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 180
9923 deg
Eccentricity:
0003514
Arg of perigee: 65
9421 deg
Mean anomaly: 294
2098 deg
Mean motion: 15
52777580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 345
Coasting Arc #11 (Orbit 3853)
---------------------------------------
Vector Time (GMT): 2019/060/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5326659
05 A = 6789243
87 meter
Y = -2894673
21 meter E =
0016179
Z = 3042320
94 I = 51
67585
XDOT = 4725
361571 Wp = 90
13581
YDOT = 3488
187310 meter/sec RA = 174
84912 deg
ZDOT = -4931
876750 TA = 54
99366
MA = 54
84191
Ha = 224
282 n
mi
Hp = 215
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17475915
52 X = 5343854
62
Y = -9496959
35 feet Y = -2835010
49 meter
Z = 9981367
92 Z = 3068237
22
XDOT = 15503
154759 XDOT = 4709
960298
YDOT = 11444
184087 feet/sec YDOT = 3540
943245 meter/sec
ZDOT = -16180
698000 ZDOT = -4908
960774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12786439
80 X = 3897306
85
Y = -15157524
99 feet Y = -4620013
62 meter
Z = 10098710
78 Z = 3078087
05
XDOT = 17590
697132 XDOT = 5361
644486
YDOT = 4078
509815 feet/sec YDOT = 1243
129792 meter/sec
ZDOT = -16077
389199 ZDOT = -4900
388228
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 19060
65799505
00016717 00000-0 10270-3 0 9100
2 25544 51
6397 175
8694 0003510 66
9084 293
2437 15
52779515 38542
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
65799505 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 175
8694 deg
Eccentricity:
0003510
Arg of perigee: 66
9084 deg
Mean anomaly: 293
2437 deg
Mean motion: 15
52779515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3854
Checksum: 346
Coasting Arc #12 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6108152
86 A = 6790671
75 meter
Y = -1439403
83 meter E =
0017599
Z = 2572514
99 I = 51
68252
XDOT = 3289
815783 Wp = 74
34367
YDOT = -4505
784714 meter/sec RA = 174
35813 deg
ZDOT = 5264
848478 TA = 314
56656
MA = 314
71010
Ha = 224
644 n
mi
Hp = 215
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20039871
59 X = -6104098
66
Y = -4722453
50 feet Y = -1507686
66 meter
Z = 8440009
81 Z = 2542854
42
XDOT = 10793
358869 XDOT = 3314
383067
YDOT = -14782
758247 feet/sec YDOT = -4468
858065 meter/sec
ZDOT = 17273
124928 ZDOT = 5280
888728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14079497
23 X = -4291430
76
Y = 15096649
72 feet Y = 4601458
83 meter
Z = 8306064
73 Z = 2531688
53
XDOT = -6425
261170 XDOT = -1958
419605
YDOT = -15582
421364 feet/sec YDOT = -4749
522032 meter/sec
ZDOT = 17345
954012 ZDOT = 5287
046783
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 19060
78671466
00016717 00000-0 10270-3 0 9110
2 25544 51
6388 175
2295 0003968 67
2698 292
8873 15
52735568 38566
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
78671466 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 175
2295 deg
Eccentricity:
0003968
Arg of perigee: 67
2698 deg
Mean anomaly: 292
8873 deg
Mean motion: 15
52735568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 370
Coasting Arc #13 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2019/061/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4337311
08 A = 6787340
35 meter
Y = -3641918
39 meter E =
0015007
Z = 3729920
76 I = 51
68967
XDOT = 5831
946860 Wp = 80
71532
YDOT = 2537
269032 meter/sec RA = 171
33384 deg
ZDOT = -4287
149593 TA = 54
78070
MA = 54
64030
Ha = 224
324 n
mi
Hp = 215
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14230023
24 X = 4359596
21
Y = -11948551
14 feet Y = -3593290
73 meter
Z = 12237272
85 Z = 3751043
66
XDOT = 19133
683925 XDOT = 5823
965091
YDOT = 8324
373463 feet/sec YDOT = 2602
441062 meter/sec
ZDOT = -14065
451422 ZDOT = -4258
840345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13400386
85 X = 4084437
91
Y = 12780399
66 feet Y = 3895465
82 meter
Z = 12333016
63 Z = 3759103
47
XDOT = -5274
702800 XDOT = -1607
729413
YDOT = 19034
032144 feet/sec YDOT = 5801
572997 meter/sec
ZDOT = -13937
683442 ZDOT = -4248
205913
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 19061
36594202
00016717 00000-0 10270-3 0 9128
2 25544 51
6368 172
3449 0003516 69
0960 291
0568 15
52754565 38654
Satellite: ISS
Catalog Number: 25544
Epoch time: 19061
36594202 = yrday
fracday
Element set: 912
Inclination: 51
6368 deg
RA of node: 172
3449 deg
Eccentricity:
0003516
Arg of perigee: 69
0960 deg
Mean anomaly: 291
0568 deg
Mean motion: 15
52754565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 326
Coasting Arc #14 (Orbit 3879)
---------------------------------------
Vector Time (GMT): 2019/062/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5139424
97 A = 6789992
84 meter
Y = 3481436
44 meter E =
0008437
Z = -2753298
00 I = 51
73201
XDOT = -4797
612748 Wp = 66
88803
YDOT = -3019
397376 meter/sec RA = 166
36651 deg
ZDOT = 5153
311215 TA = 262
02012
MA = 262
11587
Ha = 224
458 n
mi
Hp = 215
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16861630
47 X = -5164599
73
Y = 11422035
58 feet Y = 3423822
85 meter
Z = -9033129
93 Z = -2778324
20
XDOT = -15740
199306 XDOT = -4788
523767
YDOT = -9906
159371 feet/sec YDOT = -3072
996449 meter/sec
ZDOT = 16907
189024 ZDOT = 5130
029048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13426785
04 X = -4092484
08
Y = -15245902
72 feet Y = -4646951
15 meter
Z = -9146518
96 Z = -2787858
98
XDOT = 6739
702041 XDOT = 2054
261182
YDOT = -15985
010771 feet/sec YDOT = -4872
231283 meter/sec
ZDOT = 16802
163211 ZDOT = 5121
299347
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 19062
33132224
00016717 00000-0 10270-3 0 9139
2 25544 51
6374 167
5421 0003774 75
1457 285
0112 15
52768261 38805
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
33132224 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 167
5421 deg
Eccentricity:
0003774
Arg of perigee: 75
1457 deg
Mean anomaly: 285
0112 deg
Mean motion: 15
52768261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3880
Checksum: 298
Coasting Arc #15 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2019/062/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5477709
71 A = 6791000
02 meter
Y = 3277518
86 meter E =
0009060
Z = -2315215
37 I = 51
74215
XDOT = -4272
534329 Wp = 57
42499
YDOT = -3324
819859 meter/sec RA = 165
72533 deg
ZDOT = 5422
103959 TA = 276
83953
MA = 276
94260
Ha = 224
439 n
mi
Hp = 215
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17971488
54 X = -5502706
97
Y = 10753014
62 feet Y = 3216123
34 meter
Z = -7595850
97 Z = -2341884
36
XDOT = -14017
501080 XDOT = -4261
374665
YDOT = -10908
201638 feet/sec YDOT = -3372
535530 meter/sec
ZDOT = 17789
054982 ZDOT = 5401
377426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20817072
52 X = -6345043
70
Y = -1844296
94 feet Y = -562141
71 meter
Z = -7716653
17 Z = -2352035
89
XDOT = -5151
731990 XDOT = -1570
247910
YDOT = -15617
414064 feet/sec YDOT = -4760
187807 meter/sec
ZDOT = 17695
602814 ZDOT = 5393
619738
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 19062
46003923
00016717 00000-0 10270-3 0 9147
2 25544 51
6402 166
9023 0003640 74
9219 285
2335 15
52747501 38828
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
46003923 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 166
9023 deg
Eccentricity:
0003640
Arg of perigee: 74
9219 deg
Mean anomaly: 285
2335 deg
Mean motion: 15
52747501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 299
Coasting Arc #16 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2019/063/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5988479
84 A = 6792773
64 meter
Y = -2999528
18 meter E =
0016536
Z = 1091493
80 I = 51
77971
XDOT = 3020
757624 Wp = 114
90446
YDOT = 3862
790850 meter/sec RA = 160
76786 deg
ZDOT = -5894
940442 TA = 53
28183
MA = 53
13005
Ha = 224
455 n
mi
Hp = 215
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19647243
57 X = 6016274
59
Y = -9840971
72 feet Y = -2932405
30 meter
Z = 3581016
39 Z = 1120650
68
XDOT = 9910
622127 XDOT = 3005
971977
YDOT = 12673
198327 feet/sec YDOT = 3896
487877 meter/sec
ZDOT = -19340
355782 ZDOT = -5880
303333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21716158
59 X = 6619085
14
Y = 3210018
46 feet Y = 978413
63 meter
Z = 3713060
77 Z = 1131740
92
XDOT = 1178
113812 XDOT = 359
089090
YDOT = 14555
938780 feet/sec YDOT = 4436
650140 meter/sec
ZDOT = -19274
462099 ZDOT = -5874
856048
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 19063
48977480
00016717 00000-0 10270-3 0 9159
2 25544 51
6399 161
7798 0003596 81
7627 278
3932 15
52759211 38988
Satellite: ISS
Catalog Number: 25544
Epoch time: 19063
48977480 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 161
7798 deg
Eccentricity:
0003596
Arg of perigee: 81
7627 deg
Mean anomaly: 278
3932 deg
Mean motion: 15
52759211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 371
Coasting Arc #17 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2019/064/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6236216
46 A = 6793273
52 meter
Y = 2674252
20 meter E =
0015419
Z = 146700
57 I = 51
81404
XDOT = -1740
105386 Wp = 54
93999
YDOT = -4412
339160 meter/sec RA = 155
81474 deg
ZDOT = 6023
896755 TA = 306
63581
MA = 306
77750
Ha = 224
454 n
mi
Hp = 215
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20460027
74 X = -6266369
79
Y = 8773793
31 feet Y = 2604345
89 meter
Z = 481301
08 Z = 116334
52
XDOT = -5709
007171 XDOT = -1719
896139
YDOT = -14476
178347 feet/sec YDOT = -4431
684611 meter/sec
ZDOT = 19763
440798 ZDOT = 6015
493705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21866574
84 X = -6664932
01
Y = -4190291
44 feet Y = -1277200
83 meter
Z = 343798
46 Z = 104789
77
XDOT = 2961
151385 XDOT = 902
558942
YDOT = -13668
777924 feet/sec YDOT = -4166
243511 meter/sec
ZDOT = 19725
768408 ZDOT = 6012
414211
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 19064
51950676
00016717 00000-0 10270-3 0 9163
2 25544 51
6415 156
6575 0003658 82
4294 277
7273 15
52771709 39146
Satellite: ISS
Catalog Number: 25544
Epoch time: 19064
51950676 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 156
6575 deg
Eccentricity:
0003658
Arg of perigee: 82
4294 deg
Mean anomaly: 277
7273 deg
Mean motion: 15
52771709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 343
Coasting Arc #18 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2019/065/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6260925
41 A = 6792442
75 meter
Y = -2203706
59 meter E =
0011098
Z = -1429853
27 I = 51
84073
XDOT = 435
688058 Wp = 126
83450
YDOT = 4981
475933 meter/sec RA = 150
86351 deg
ZDOT = -5807
365080 TA = 68
70052
MA = 68
58207
Ha = 224
506 n
mi
Hp = 215
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20541093
88 X = 6292047
86
Y = -7230008
50 feet Y = -2133518
70 meter
Z = -4691119
64 Z = -1399364
78
XDOT = 1429
422763 XDOT = 408
159815
YDOT = 16343
424977 feet/sec YDOT = 4986
193504 meter/sec
ZDOT = -19053
035038 ZDOT = -5805
316152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21184708
39 X = 6457099
12
Y = 5166596
77 feet Y = 1574778
69 meter
Z = -4553083
82 Z = -1387779
95
XDOT = -7236
045042 XDOT = -2205
546529
YDOT = 12999
433047 feet/sec YDOT = 3962
227193 meter/sec
ZDOT = -19044
136075 ZDOT = -5804
652676
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 19065
48487706
00016717 00000-0 10270-3 0 9170
2 25544 51
6410 151
8553 0003671 86
3908 273
7664 15
52776414 39298
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
48487706 = yrday
fracday
Element set: 917
Inclination: 51
6410 deg
RA of node: 151
8553 deg
Eccentricity:
0003671
Arg of perigee: 86
3908 deg
Mean anomaly: 273
7664 deg
Mean motion: 15
52776414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3929
Checksum: 342
Coasting Arc #19 (Orbit 3943)
---------------------------------------
Vector Time (GMT): 2019/066/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6051656
88 A = 6790486
47 meter
Y = 1645669
27 meter E =
0017302
Z = 2584089
43 I = 51
86283
XDOT = 763
273003 Wp = 79
09156
YDOT = -5516
577276 meter/sec RA = 145
91147 deg
ZDOT = 5274
015758 TA = 309
87923
MA = 310
03125
Ha = 224
531 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19854517
32 X = -6082161
33
Y = 5399177
39 feet Y = 1577825
17 meter
Z = 8477983
69 Z = 2554618
92
XDOT = 2504
176519 XDOT = 799
286367
YDOT = -18099
006811 feet/sec YDOT = -5507
839801 meter/sec
ZDOT = 17303
201307 ZDOT = 5277
811551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19737857
46 X = -6016098
95
Y = -6001179
23 feet Y = -1829159
43 meter
Z = 8344579
84 Z = 2543427
93
XDOT = 11199
096959 XDOT = 3413
484753
YDOT = -12625
662968 feet/sec YDOT = -3848
302073 meter/sec
ZDOT = 17320
777068 ZDOT = 5279
372850
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 19066
51460283
00016717 00000-0 10270-3 0 9187
2 25544 51
6411 146
7332 0003714 88
8150 271
3427 15
52790598 39448
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
51460283 = yrday
fracday
Element set: 918
Inclination: 51
6411 deg
RA of node: 146
7332 deg
Eccentricity:
0003714
Arg of perigee: 88
8150 deg
Mean anomaly: 271
3427 deg
Mean motion: 15
52790598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3944
Checksum: 319
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