[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 23rd 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
066/23:27:30
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
4
067/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (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 = -2592687
11 A = 6779869
69 meter
Y = 3375784
38 meter E =
0019561
Z = -5293898
85 I = 51
41968
XDOT = -6394
433964 Wp = 83
49147
YDOT = -4178
001846 meter/sec RA = 210
33948 deg
ZDOT = 471
142403 TA = 191
00400
MA = 191
04685
Ha = 224
225 n
mi
Hp = 214
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8506191
31 X = -2604529
04
Y = 11075408
07 feet Y = 3346724
34 meter
Z = -17368434
56 Z = -5306522
06
XDOT = -20979
114054 XDOT = -6349
527630
YDOT = -13707
355138 feet/sec YDOT = -4249
257735 meter/sec
ZDOT = 1545
742793 ZDOT = 440
190735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12685030
65 X = -3866397
34
Y = 5667245
38 feet Y = 1727376
39 meter
Z = -17425693
70 Z = -5311351
44
XDOT = -11384
121267 XDOT = -3469
880162
YDOT = -21193
947891 feet/sec YDOT = -6459
915317 meter/sec
ZDOT = 1406
311328 ZDOT = 428
643693
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
51537774
00016717 00000-0 10270-3 0 9004
2 25544 51
6372 211
4134 0005671 55
5374 304
6313 15
53288374 37433
Satellite: ISS
Catalog Number: 25544
Epoch time: 19053
51537774 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 211
4134 deg
Eccentricity:
0005671
Arg of perigee: 55
5374 deg
Mean anomaly: 304
6313 deg
Mean motion: 15
53288374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3743
Checksum: 301
Coasting Arc #2 (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 = 3809259
31 A = 6781258
99 meter
Y = -2581632
60 meter E =
0011688
Z = 4974315
73 I = 51
45368
XDOT = 5806
610228 Wp = 58
27972
YDOT = 4569
704580 meter/sec RA = 205
33415 deg
ZDOT = -2065
369073 TA = 51
90566
MA = 51
80031
Ha = 224
218 n
mi
Hp = 214
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12497569
91 X = 3813682
62
Y = -8469923
23 feet Y = -2539009
57 meter
Z = 16319933
50 Z = 4992830
43
XDOT = 19050
558490 XDOT = 5765
111220
YDOT = 14992
469094 feet/sec YDOT = 4634
405910 meter/sec
ZDOT = -6776
145254 ZDOT = -2037
264386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14907843
67 X = 4543910
75
Y = -1715420
20 feet Y = -522860
08 meter
Z = 16403737
78 Z = 4999859
28
XDOT = 9776
880469 XDOT = 2979
993167
YDOT = 21079
275586 feet/sec YDOT = 6424
963199 meter/sec
ZDOT = -6649
582406 ZDOT = -2026
792717
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
54477186
00016717 00000-0 10270-3 0 9019
2 25544 51
6375 206
2868 0005718 59
3685 300
8030 15
53253893 37590
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
54477186 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 206
2868 deg
Eccentricity:
0005718
Arg of perigee: 59
3685 deg
Mean anomaly: 300
8030 deg
Mean motion: 15
53253893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3759
Checksum: 333
Coasting Arc #3 (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 = -4898087
10 A = 6783766
10 meter
Y = 1853250
39 meter E =
0013234
Z = -4323801
26 I = 51
49360
XDOT = -4873
891156 Wp = 92
04229
YDOT = -4765
701502 meter/sec RA = 200
33818 deg
ZDOT = 3487
380215 TA = 213
50864
MA = 213
59243
Ha = 224
282 n
mi
Hp = 213
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16069839
55 X = -4897444
25
Y = 6080217
83 feet Y = 1798479
80 meter
Z = -14185699
67 Z = -4347592
64
XDOT = -15990
456547 XDOT = -4837
177058
YDOT = -15635
503614 feet/sec YDOT = -4819
999186 meter/sec
ZDOT = 11441
536140 ZDOT = 3463
794527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16999449
88 X = -5181432
32
Y = -1778632
04 feet Y = -542127
05 meter
Z = -14293286
51 Z = -4356593
73
XDOT = -7418
330728 XDOT = -2261
107206
YDOT = -19960
791821 feet/sec YDOT = -6084
049347 meter/sec
ZDOT = 11335
380242 ZDOT = 3455
023898
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
50982470
00016717 00000-0 10270-3 0 9024
2 25544 51
6382 201
4830 0005726 62
0299 298
1432 15
53282347 37743
Satellite: ISS
Catalog Number: 25544
Epoch time: 19055
50982470 = yrday
fracday
Element set: 902
Inclination: 51
6382 deg
RA of node: 201
4830 deg
Eccentricity:
0005726
Arg of perigee: 62
0299 deg
Mean anomaly: 298
1432 deg
Mean motion: 15
53282347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 311
Coasting Arc #4 (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 = 5804983
42 A = 6787056
77 meter
Y = -1136953
81 meter E =
0017832
Z = 3314385
42 I = 51
53536
XDOT = 3641
122364 Wp = 83
89329
YDOT = 4860
259273 meter/sec RA = 195
34982 deg
ZDOT = -4686
429553 TA = 57
47711
MA = 57
30494
Ha = 224
257 n
mi
Hp = 214
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19045221
20 X = 5801166
46
Y = -3730163
41 feet Y = -1072059
55 meter
Z = 10873967
92 Z = 3342574
34
XDOT = 11945
939515 XDOT = 3609
266773
YDOT = 15945
732523 feet/sec YDOT = 4900
798423 meter/sec
ZDOT = -15375
425043 ZDOT = -4668
820237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18702162
55 X = 5700419
15
Y = 4906790
83 feet Y = 1495589
84 meter
Z = 11001375
72 Z = 3353219
32
XDOT = 4258
121224 XDOT = 1297
875349
YDOT = 18236
923272 feet/sec YDOT = 5558
614213 meter/sec
ZDOT = -15296
255092 ZDOT = -4662
298552
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
53921464
00016717 00000-0 10270-3 0 9035
2 25544 51
6374 196
3574 0005659 66
5760 293
5987 15
53272150 37901
Satellite: ISS
Catalog Number: 25544
Epoch time: 19056
53921464 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 196
3574 deg
Eccentricity:
0005659
Arg of perigee: 66
5760 deg
Mean anomaly: 293
5987 deg
Mean motion: 15
53272150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3790
Checksum: 340
Coasting Arc #5 (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 = -1603454
85 A = 6781502
45 meter
Y = 3950284
39 meter E =
0017613
Z = -5288949
98 I = 51
53297
XDOT = -7324
984425 Wp = 86
84043
YDOT = -2124
289312 meter/sec RA = 192
36835 deg
ZDOT = 636
888559 TA = 189
24450
MA = 189
27696
Ha = 224
368 n
mi
Hp = 215
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5260678
66 X = -1621818
40
Y = 12960250
62 feet Y = 3932250
46 meter
Z = -17352198
11 Z = -5296783
70
XDOT = -24032
101131 XDOT = -7303
779231
YDOT = -6969
453124 feet/sec YDOT = -2206
083803 meter/sec
ZDOT = 2089
529393 ZDOT = 601
358580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2361082
90 X = 719658
07
Y = -13741487
72 feet Y = -4188405
46 meter
Z = -17387881
35 Z = -5299826
24
XDOT = 23963
921331 XDOT = 7304
203222
YDOT = 1687
938516 feet/sec YDOT = 514
483660 meter/sec
ZDOT = 1929
196747 ZDOT = 588
019168
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
11824695
00016717 00000-0 10270-3 0 9049
2 25544 51
6395 193
4802 0003722 52
2544 307
8945 15
52745985 37999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
11824695 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 193
4802 deg
Eccentricity:
0003722
Arg of perigee: 52
2544 deg
Mean anomaly: 307
8945 deg
Mean motion: 15
52745985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 342
Coasting Arc #6 (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 = -2325386
13 A = 6782008
95 meter
Y = 3756277
67 meter E =
0016504
Z = -5160214
82 I = 51
55234
XDOT = -7118
137871 Wp = 93
21902
YDOT = -2404
642174 meter/sec RA = 189
78826 deg
ZDOT = 1460
426644 TA = 190
86413
MA = 190
89982
Ha = 224
285 n
mi
Hp = 215
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7629219
59 X = -2342151
93
Y = 12323745
65 feet Y = 3730179
58 meter
Z = -16929838
66 Z = -5171551
44
XDOT = -23353
470706 XDOT = -7097
813303
YDOT = -7889
245977 feet/sec YDOT = -2484
128447 meter/sec
ZDOT = 4791
425998 ZDOT = 1425
899330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3271099
98 X = -997031
27
Y = 14058212
95 feet Y = 4284943
31 meter
Z = -16981333
55 Z = -5175910
47
XDOT = -23654
189287 XDOT = -7209
796895
YDOT = 83
198352 feet/sec YDOT = 25
358858 meter/sec
ZDOT = 4635
631928 ZDOT = 1412
940612
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
63312079
00016717 00000-0 10270-3 0 9055
2 25544 51
6401 190
9166 0003410 58
3581 301
7904 15
52759016 38072
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
63312079 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 190
9166 deg
Eccentricity:
0003410
Arg of perigee: 58
3581 deg
Mean anomaly: 301
7904 deg
Mean motion: 15
52759016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 301
Coasting Arc #7 (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 = 3464741
12 A = 6783801
76 meter
Y = -3447060
26 meter E =
0011284
Z = 4698326
50 I = 51
59194
XDOT = 6577
344776 Wp = 62
42359
YDOT = 2780
310098 meter/sec RA = 184
80055 deg
ZDOT = -2800
280660 TA = 55
39807
MA = 55
29169
Ha = 224
200 n
mi
Hp = 215
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11367260
90 X = 3480208
11
Y = -11309252
81 feet Y = -3408228
41 meter
Z = 15414457
03 Z = 4715194
37
XDOT = 21579
215144 XDOT = 6559
367725
YDOT = 9121
752289 feet/sec YDOT = 2853
761922 meter/sec
ZDOT = -9187
272506 ZDOT = -2768
374660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6901680
45 X = 2103632
20
Y = -14391571
14 feet Y = -4386550
88 meter
Z = 15490926
12 Z = 4721634
28
XDOT = 22388
405081 XDOT = 6823
985869
YDOT = 966
438547 feet/sec YDOT = 294
570469 meter/sec
ZDOT = -9043
326326 ZDOT = -2756
405864
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
66286881
00016717 00000-0 10270-3 0 9061
2 25544 51
6405 185
7934 0003473 60
0172 300
1324 15
52778871 38233
Satellite: ISS
Catalog Number: 25544
Epoch time: 19058
66286881 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 185
7934 deg
Eccentricity:
0003473
Arg of perigee: 60
0172 deg
Mean anomaly: 300
1324 deg
Mean motion: 15
52778871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 318
Coasting Arc #8 (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 = -4468530
71 A = 6786387
98 meter
Y = 3183321
83 meter E =
0009953
Z = -4003423
36 I = 51
63256
XDOT = -5763
895595 Wp = 94
70254
YDOT = -3118
360471 meter/sec RA = 179
82133 deg
ZDOT = 3961
672231 TA = 216
55064
MA = 216
61860
Ha = 224
322 n
mi
Hp = 215
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14660533
81 X = -4484349
35
Y = 10443969
25 feet Y = 3133262
97 meter
Z = -13134591
06 Z = -4025167
97
XDOT = -18910
418618 XDOT = -5747
840079
YDOT = -10230
841440 feet/sec YDOT = -3182
726433 meter/sec
ZDOT = 12997
612305 ZDOT = 3933
713029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10056483
18 X = -3065216
07
Y = 14841757
21 feet Y = 4523767
60 meter
Z = -13233087
95 Z = -4033445
21
XDOT = -20281
391116 XDOT = -6181
768012
YDOT = -2288
261123 feet/sec YDOT = -697
461990 meter/sec
ZDOT = 12871
503423 ZDOT = 3923
234243
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
62825756
00016717 00000-0 10270-3 0 9079
2 25544 51
6392 180
9920 0003522 65
7271 294
4249 15
52775303 38381
Satellite: ISS
Catalog Number: 25544
Epoch time: 19059
62825756 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 180
9920 deg
Eccentricity:
0003522
Arg of perigee: 65
7271 deg
Mean anomaly: 294
4249 deg
Mean motion: 15
52775303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 334
Coasting Arc #9 (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 = 5323695
45 A = 6789243
40 meter
Y = -2896893
73 meter E =
0016179
Z = 3045411
55 I = 51
67582
XDOT = 4729
636705 Wp = 90
04112
YDOT = 3485
835869 meter/sec RA = 174
84879 deg
ZDOT = -4929
425840 TA = 55
04781
MA = 54
89596
Ha = 224
288 n
mi
Hp = 215
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17466192
43 X = 5340901
06
Y = -9504244
53 feet Y = -2837264
10 meter
Z = 9991507
70 Z = 3071313
46
XDOT = 15517
180792 XDOT = 4714
249505
YDOT = 11436
469388 feet/sec YDOT = 3538
639692 meter/sec
ZDOT = -16172
656957 ZDOT = -4906
489063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12774675
27 X = 3893721
02
Y = -15160768
12 feet Y = -4621002
12 meter
Z = 10108785
77 Z = 3081157
90
XDOT = 17600
689236 XDOT = 5364
690079
YDOT = 4067
116231 feet/sec YDOT = 1239
657027 meter/sec
ZDOT = -16069
253972 ZDOT = -4897
908611
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
65800239
00016717 00000-0 10270-3 0 9084
2 25544 51
6397 175
8691 0003518 66
7046 293
4476 15
52776927 38542
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
65800239 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 175
8691 deg
Eccentricity:
0003518
Arg of perigee: 66
7046 deg
Mean anomaly: 293
4476 deg
Mean motion: 15
52776927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3854
Checksum: 350
Coasting Arc #10 (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 = -6110272
52 A = 6790686
86 meter
Y = -1436470
03 meter E =
0017610
Z = 2569129
74 I = 51
68254
XDOT = 3284
769491 Wp = 74
26141
YDOT = -4506
991193 meter/sec RA = 174
35780 deg
ZDOT = 5266
971822 TA = 314
60716
MA = 314
75069
Ha = 224
650 n
mi
Hp = 215
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20046825
86 X = -6106234
53
Y = -4712828
17 feet Y = -1504776
65 meter
Z = 8428903
35 Z = 2539458
84
XDOT = 10776
802792 XDOT = 3309
340327
YDOT = -14786
716511 feet/sec YDOT = -4470
120955 meter/sec
ZDOT = 17280
091280 ZDOT = 5282
987568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14074560
78 X = -4289926
13
Y = 15107401
26 feet Y = 4604735
90 meter
Z = 8294911
33 Z = 2528288
97
XDOT = -6436
158286 XDOT = -1961
741045
YDOT = -15570
337372 feet/sec YDOT = -4745
838831 meter/sec
ZDOT = 17352
809708 ZDOT = 5289
136399
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
78672222
00016717 00000-0 10270-3 0 9098
2 25544 51
6388 175
2293 0003977 67
0908 293
0664 15
52732892 38564
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
78672222 = yrday
fracday
Element set: 909
Inclination: 51
6388 deg
RA of node: 175
2293 deg
Eccentricity:
0003977
Arg of perigee: 67
0908 deg
Mean anomaly: 293
0664 deg
Mean motion: 15
52732892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 346
Coasting Arc #11 (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 = 4333015
44 A = 6787339
11 meter
Y = -3643813
20 meter E =
0015005
Z = 3733073
46 I = 51
68963
XDOT = 5836
024594 Wp = 80
61762
YDOT = 2533
810745 meter/sec RA = 171
33353 deg
ZDOT = -4283
629948 TA = 54
83080
MA = 54
69033
Ha = 224
331 n
mi
Hp = 215
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14215929
91 X = 4355306
76
Y = -11954767
72 feet Y = -3595233
54 meter
Z = 12247616
34 Z = 3754175
50
XDOT = 19147
062316 XDOT = 5828
064097
YDOT = 8313
027380 feet/sec YDOT = 2599
028495 meter/sec
ZDOT = -14053
904030 ZDOT = -4255
300841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13405043
11 X = 4085857
14
Y = 12765650
93 feet Y = 3890970
40 meter
Z = 12343266
02 Z = 3762227
48
XDOT = -5263
067952 XDOT = -1604
183112
YDOT = 19045
695730 feet/sec YDOT = 5805
128058 meter/sec
ZDOT = -13926
046029 ZDOT = -4244
658830
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
36595064
00016717 00000-0 10270-3 0 9103
2 25544 51
6368 172
3447 0003524 68
9073 291
2455 15
52751573 38657
Satellite: ISS
Catalog Number: 25544
Epoch time: 19061
36595064 = yrday
fracday
Element set: 910
Inclination: 51
6368 deg
RA of node: 172
3447 deg
Eccentricity:
0003524
Arg of perigee: 68
9073 deg
Mean anomaly: 291
2455 deg
Mean motion: 15
52751573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 324
Coasting Arc #12 (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 = -5135031
12 A = 6789991
48 meter
Y = 3484218
91 meter E =
0008441
Z = -2757995
61 I = 51
73197
XDOT = -4803
587223 Wp = 66
93301
YDOT = -3015
332647 meter/sec RA = 166
36621 deg
ZDOT = 5150
107780 TA = 261
91620
MA = 262
01198
Ha = 224
465 n
mi
Hp = 215
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16847214
97 X = -5160214
51
Y = 11431164
42 feet Y = 3426654
40 meter
Z = -9048542
03 Z = -2783000
49
XDOT = -15759
800599 XDOT = -4794
527689
YDOT = -9892
823644 feet/sec YDOT = -3068
998695 meter/sec
ZDOT = 16896
679068 ZDOT = 5126
796521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13434031
72 X = -4094692
87
Y = -15230359
76 feet Y = -4642213
66 meter
Z = -9161834
88 Z = -2792527
27
XDOT = 6725
169704 XDOT = 2049
831726
YDOT = -16002
198106 feet/sec YDOT = -4877
469983 meter/sec
ZDOT = 16791
521439 ZDOT = 5118
055735
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
33133280
00016717 00000-0 10270-3 0 9110
2 25544 51
6374 167
5419 0003782 74
9672 285
1898 15
52764949 38808
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
33133280 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 167
5419 deg
Eccentricity:
0003782
Arg of perigee: 74
9672 deg
Mean anomaly: 285
1898 deg
Mean motion: 15
52764949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3880
Checksum: 342
Coasting Arc #13 (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 = -5473692
83 A = 6790999
95 meter
Y = 3280660
94 meter E =
0009059
Z = -2320287
89 I = 51
74211
XDOT = -4279
074916 Wp = 57
45424
YDOT = -3320
892171 meter/sec RA = 165
72502 deg
ZDOT = 5419
337191 TA = 276
74978
MA = 276
85286
Ha = 224
446 n
mi
Hp = 215
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17958309
80 X = -5498700
89
Y = 10763323
29 feet Y = 3219310
28 meter
Z = -7612493
07 Z = -2346937
39
XDOT = -14038
959699 XDOT = -4267
945247
YDOT = -10895
315522 feet/sec YDOT = -3368
681151 meter/sec
ZDOT = 17779
977662 ZDOT = 5398
578814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20812387
22 X = -6343615
62
Y = -1828144
16 feet Y = -557218
34 meter
Z = -7733207
42 Z = -2357081
62
XDOT = -5175
437841 XDOT = -1577
473454
YDOT = -15619
920147 feet/sec YDOT = -4760
951661 meter/sec
ZDOT = 17686
381249 ZDOT = 5390
809005
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
46005007
00016717 00000-0 10270-3 0 9120
2 25544 51
6402 166
9021 0003648 74
7357 285
4198 15
52744072 38824
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
46005007 = yrday
fracday
Element set: 912
Inclination: 51
6402 deg
RA of node: 166
9021 deg
Eccentricity:
0003648
Arg of perigee: 74
7357 deg
Mean anomaly: 285
4198 deg
Mean motion: 15
52744072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 308
Coasting Arc #14 (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 = 5985057
68 A = 6792778
31 meter
Y = -3003936
40 meter E =
0016544
Z = 1098163
94 I = 51
77968
XDOT = 3029
427356 Wp = 114
79621
YDOT = 3858
428278 meter/sec RA = 160
76755 deg
ZDOT = -5893
341438 TA = 53
31684
MA = 53
16492
Ha = 224
463 n
mi
Hp = 215
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19636016
02 X = 6012869
59
Y = -9855434
39 feet Y = -2936851
70 meter
Z = 3602900
08 Z = 1127304
24
XDOT = 9939
066128 XDOT = 3014
682081
YDOT = 12658
885428 feet/sec YDOT = 3892
222482 meter/sec
ZDOT = -19335
109706 ZDOT = -5878
662118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21715149
81 X = 6618777
66
Y = 3191648
09 feet Y = 972814
34 meter
Z = 3734869
82 Z = 1138388
32
XDOT = 1208
250894 XDOT = 368
274872
YDOT = 14560
605507 feet/sec YDOT = 4438
072559 meter/sec
ZDOT = -19269
024855 ZDOT = -5873
198776
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
48978802
00016717 00000-0 10270-3 0 9136
2 25544 51
6398 161
7796 0003603 81
5799 278
5761 15
52755417 38988
Satellite: ISS
Catalog Number: 25544
Epoch time: 19063
48978802 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 161
7796 deg
Eccentricity:
0003603
Arg of perigee: 81
5799 deg
Mean anomaly: 278
5761 deg
Mean motion: 15
52755417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 368
Coasting Arc #15 (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 = -6233842
44 A = 6793286
41 meter
Y = 2680258
66 meter E =
0015414
Z = 138542
58 I = 51
81404
XDOT = -1750
906242 Wp = 54
86539
YDOT = -4407
704265 meter/sec RA = 155
81444 deg
ZDOT = 6024
145054 TA = 306
62276
MA = 306
76442
Ha = 224
463 n
mi
Hp = 215
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20452238
97 X = -6264023
49
Y = 8793499
54 feet Y = 2610378
74 meter
Z = 454536
03 Z = 108188
00
XDOT = -5744
443052 XDOT = -1730
749227
YDOT = -14460
971997 feet/sec YDOT = -4427
170790 meter/sec
ZDOT = 19764
255425 ZDOT = 6015
689411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21871008
32 X = -6666283
34
Y = -4169504
59 feet Y = -1270865
00 meter
Z = 317084
81 Z = 96647
45
XDOT = 2924
789441 XDOT = 891
475822
YDOT = -13675
703246 feet/sec YDOT = -4168
354350 meter/sec
ZDOT = 19726
344886 ZDOT = 6012
589921
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
51952261
00016717 00000-0 10270-3 0 9143
2 25544 51
6414 156
6573 0003665 82
2593 277
8975 15
52767513 39149
Satellite: ISS
Catalog Number: 25544
Epoch time: 19064
51952261 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 156
6573 deg
Eccentricity:
0003665
Arg of perigee: 82
2593 deg
Mean anomaly: 277
8975 deg
Mean motion: 15
52767513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 336
Coasting Arc #16 (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 = 6260229
38 A = 6792466
75 meter
Y = -2211685
64 meter E =
0011124
Z = -1420593
16 I = 51
84076
XDOT = 448
444440 Wp = 126
80253
YDOT = 4976
973338 meter/sec RA = 150
86324 deg
ZDOT = -5810
258530 TA = 68
62933
MA = 68
51067
Ha = 224
515 n
mi
Hp = 215
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20538810
30 X = 6291396
12
Y = -7256186
47 feet Y = -2141505
28 meter
Z = -4660738
71 Z = -1390107
95
XDOT = 1471
274409 XDOT = 420
979652
YDOT = 16328
652683 feet/sec YDOT = 4981
833914 meter/sec
ZDOT = -19062
527986 ZDOT = -5808
147484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21196907
93 X = 6460817
54
Y = 5143304
37 feet Y = 1567679
17 meter
Z = -4522717
11 Z = -1378524
17
XDOT = -7194
558317 XDOT = -2192
901375
YDOT = 13009
035209 feet/sec YDOT = 3965
153932 meter/sec
ZDOT = -19053
347779 ZDOT = -5807
460403
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
48489564
00016717 00000-0 10270-3 0 9152
2 25544 51
6410 151
8551 0003679 86
2280 273
9293 15
52771899 39298
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
48489564 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 151
8551 deg
Eccentricity:
0003679
Arg of perigee: 86
2280 deg
Mean anomaly: 273
9293 deg
Mean motion: 15
52771899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3929
Checksum: 354
Coasting Arc #17 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2019/066/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6053060
72 A = 6790522
26 meter
Y = 1655952
38 meter E =
0017317
Z = 2574279
06 I = 51
86290
XDOT = 748
867974 Wp = 78
94567
YDOT = -5512
659951 meter/sec RA = 145
91126 deg
ZDOT = 5280
161616 TA = 309
90463
MA = 310
05673
Ha = 224
541 n
mi
Hp = 215
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19859123
08 X = -6083632
39
Y = 5432914
65 feet Y = 1588092
21 meter
Z = 8445797
45 Z = 2544801
58
XDOT = 2456
915924 XDOT = 784
808751
YDOT = -18086
154694 feet/sec YDOT = -5504
083968 meter/sec
ZDOT = 17323
364882 ZDOT = 5283
887259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19759496
50 X = -6022694
53
Y = -5974928
82 feet Y = -1821158
30 meter
Z = 8312361
26 Z = 2533607
71
XDOT = 11154
028249 XDOT = 3399
747810
YDOT = -12638
369660 feet/sec YDOT = -3852
175072 meter/sec
ZDOT = 17340
623096 ZDOT = 5285
421920
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
51462456
00016717 00000-0 10270-3 0 9169
2 25544 51
6411 146
7330 0003721 88
6548 271
5030 15
52785578 39458
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
51462456 = yrday
fracday
Element set: 916
Inclination: 51
6411 deg
RA of node: 146
7330 deg
Eccentricity:
0003721
Arg of perigee: 88
6548 deg
Mean anomaly: 271
5030 deg
Mean motion: 15
52785578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 321
Coasting Arc #18 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2019/066/23:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4261207
21 A = 6782788
05 meter
Y = -1709399
97 meter E =
0009550
Z = 4985818
08 I = 51
85081
XDOT = 4757
264624 Wp = 108
71087
YDOT = -5629
077804 meter/sec RA = 143
32062 deg
ZDOT = 2129
607948 TA = 320
58383
MA = 320
65328
Ha = 224
619 n
mi
Hp = 215
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13980338
61 X = -4265993
52
Y = -5608267
62 feet Y = -1757077
90 meter
Z = 16357670
88 Z = 4965107
62
XDOT = 15607
823570 XDOT = 4809
512687
YDOT = -18468
103032 feet/sec YDOT = -5575
586336 meter/sec
ZDOT = 6986
902717 ZDOT = 2152
844249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10662396
78 X = 3249898
54
Y = 10782730
87 feet Y = 3286576
37 meter
Z = 16264130
47 Z = 4957306
97
XDOT = -20870
289846 XDOT = -6361
264345
YDOT = 9908
085360 feet/sec YDOT = 3019
984418 meter/sec
ZDOT = 7092
414462 ZDOT = 2161
767928
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 19067
02948932
00016717 00000-0 10270-3 0 9175
2 25544 51
6404 144
1749 0003777 84
1787 275
9795 15
52792346 39539
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
02948932 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 144
1749 deg
Eccentricity:
0003777
Arg of perigee: 84
1787 deg
Mean anomaly: 275
9795 deg
Mean motion: 15
52792346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 358
Coasting Arc #19 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2019/067/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910211
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5923830
40 A = 6790794
53 meter
Y = 2251877
10 meter E =
0017364
Z = 2418982
55 I = 51
88379
XDOT = 127
552165 Wp = 78
04472
YDOT = -5469
658333 meter/sec RA = 141
76081 deg
ZDOT = 5375
142061 TA = 308
90811
MA = 309
06282
Ha = 224
516 n
mi
Hp = 215
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19435139
11 X = -5960321
19
Y = 7388048
24 feet Y = 2185428
96 meter
Z = 7936294
46 Z = 2390118
25
XDOT = 418
478233 XDOT = 162
596822
YDOT = -17945
073270 feet/sec YDOT = -5468
035321 meter/sec
ZDOT = 17634
980516 ZDOT = 5375
847469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7325356
14 X = -2232768
55
Y = -19511657
70 feet Y = -5947153
27 meter
Z = 7805576
85 Z = 2379139
82
XDOT = 16520
017925 XDOT = 5035
301464
YDOT = 892
806500 feet/sec YDOT = 272
127421 meter/sec
ZDOT = 17638
580824 ZDOT = 5376
239435
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 19067
35127831
00016717 00000-0 10270-3 0 9189
2 25544 51
6382 142
5691 0003748 92
9767 267
1814 15
52802577 39583
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
35127831 = yrday
fracday
Element set: 918
Inclination: 51
6382 deg
RA of node: 142
5691 deg
Eccentricity:
0003748
Arg of perigee: 92
9767 deg
Mean anomaly: 267
1814 deg
Mean motion: 15
52802577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 346
Coasting Arc #20 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2019/068/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910211
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5621035
75 A = 6788159
40 meter
Y = -1514313
34 meter E =
0008761
Z = -3498816
65 I = 51
90072
XDOT = -1205
623406 Wp = 90
95935
YDOT = 6034
741489 meter/sec RA = 136
80698 deg
ZDOT = -4558
772167 TA = 129
93066
MA = 129
85364
Ha = 224
530 n
mi
Hp = 215
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18441718
35 X = 5654546
64
Y = -4968219
63 feet Y = -1451268
06 meter
Z = -11479057
26 Z = -3471430
43
XDOT = -3955
457368 XDOT = -1250
872192
YDOT = 19799
020634 feet/sec YDOT = 6021
005792 meter/sec
ZDOT = -14956
601597 ZDOT = -4564
739239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5227004
93 X = 1593191
10
Y = 18446944
69 feet Y = 5622628
74 meter
Z = -11355068
85 Z = -3461024
99
XDOT = -18504
741822 XDOT = -5640
245307
YDOT = -3959
690481 feet/sec YDOT = -1206
913659 meter/sec
ZDOT = -14984
051851 ZDOT = -4567
139004
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 19068
31664588
00016717 00000-0 10270-3 0 9192
2 25544 51
6386 137
7660 0003805 94
0765 266
0822 15
52788645 39737
Satellite: ISS
Catalog Number: 25544
Epoch time: 19068
31664588 = yrday
fracday
Element set: 919
Inclination: 51
6386 deg
RA of node: 137
7660 deg
Eccentricity:
0003805
Arg of perigee: 94
0765 deg
Mean anomaly: 266
0822 deg
Mean motion: 15
52788645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 353
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