[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 26th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
118/11:34:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
5
120/08:22:21
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 217
5
122/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 217
4
128/05:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
2
Coasting Arc #1 (Orbit 690)
---------------------------------------
Vector Time (GMT): 2019/114/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -194688
15 A = 6793557
72 meter
Y = 6753216
68 meter E =
0010819
Z = -658224
78 I = 51
27355
XDOT = -4800
139863 Wp = 146
09283
YDOT = -711
367936 meter/sec RA = 267
17033 deg
ZDOT = -5934
797548 TA = 41
04729
MA = 40
96593
Ha = 223
082 n
mi
Hp = 217
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -638740
65 X = -266992
75
Y = 22156222
70 feet Y = 6750635
28 meter
Z = -2159530
11 Z = -659345
91
XDOT = -15748
490363 XDOT = -4763
000212
YDOT = -2333
884303 feet/sec YDOT = -764
838611 meter/sec
ZDOT = -19471
120565 ZDOT = -5958
024829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10991679
44 X = 3350263
89
Y = 19247453
02 feet Y = 5866623
68 meter
Z = -2165248
06 Z = -659967
61
XDOT = -13149
657214 XDOT = -4008
015519
YDOT = 5327
844276 feet/sec YDOT = 1623
926935 meter/sec
ZDOT = -19576
046209 ZDOT = -5966
778885
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 19114
53094369
00016717 00000-0 10270-3 0 9002
2 25544 51
6379 267
9101 0001239 224
3021 135
8031 15
52611347 6910
Satellite: ISS
Catalog Number: 25544
Epoch time: 19114
53094369 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 267
9101 deg
Eccentricity:
0001239
Arg of perigee: 224
3021 deg
Mean anomaly: 135
8031 deg
Mean motion: 15
52611347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 691
Checksum: 286
Coasting Arc #2 (Orbit 706)
---------------------------------------
Vector Time (GMT): 2019/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 572255
36 A = 6792344
40 meter
Y = -6515160
31 meter E =
0012602
Z = 1812237
59 I = 51
27308
XDOT = 4821
276460 Wp = 68
61631
YDOT = 1993
710647 meter/sec RA = 262
18109 deg
ZDOT = 5618
026139 TA = 311
39981
MA = 311
50806
Ha = 223
057 n
mi
Hp = 217
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1877478
23 X = 636264
32
Y = -21375197
85 feet Y = -6508403
10 meter
Z = 5945661
40 Z = 1815172
70
XDOT = 15817
836154 XDOT = 4771
334513
YDOT = 6541
045429 feet/sec YDOT = 2047
346137 meter/sec
ZDOT = 18431
844287 ZDOT = 5641
324960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9878061
01 X = -3010832
99
Y = -19044228
98 feet Y = -5804680
99 meter
Z = 5959542
80 Z = 1816468
65
XDOT = 15371
232053 XDOT = 4685
151530
YDOT = -2144
326396 feet/sec YDOT = -653
590685 meter/sec
ZDOT = 18536
981203 ZDOT = 5650
071871
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 19115
56079898
00016717 00000-0 10270-3 0 9017
2 25544 51
6387 262
7887 0001478 222
2954 137
8084 15
52613222 7072
Satellite: ISS
Catalog Number: 25544
Epoch time: 19115
56079898 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 262
7887 deg
Eccentricity:
0001478
Arg of perigee: 222
2954 deg
Mean anomaly: 137
8084 deg
Mean motion: 15
52613222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 707
Checksum: 333
Coasting Arc #3 (Orbit 721)
---------------------------------------
Vector Time (GMT): 2019/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1012074
28 A = 6790193
74 meter
Y = 6053199
90 meter E =
0004185
Z = -2904360
40 I = 51
27174
XDOT = -4841
151634 Wp = 132
02093
YDOT = -3204
964122 meter/sec RA = 257
18806 deg
ZDOT = -5000
136195 TA = 81
23087
MA = 81
18348
Ha = 223
034 n
mi
Hp = 217
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3320453
68 X = -1065579
86
Y = 19859579
71 feet Y = 6041583
06 meter
Z = -9528741
46 Z = -2909406
53
XDOT = -15883
043419 XDOT = -4780
665059
YDOT = -10514
974152 feet/sec YDOT = -3258
762973 meter/sec
ZDOT = -16404
646309 ZDOT = -5023
505908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8185867
26 X = 2495052
34
Y = 18384069
46 feet Y = 5603464
37 meter
Z = -9552109
71 Z = -2911483
04
XDOT = -17616
002313 XDOT = -5369
357505
YDOT = -721
904512 feet/sec YDOT = -220
036495 meter/sec
ZDOT = -16510
004601 ZDOT = -5032
249402
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 19116
52628668
00016717 00000-0 10270-3 0 9020
2 25544 51
6390 257
9866 0001355 230
6680 129
4352 15
52597734 7223
Satellite: ISS
Catalog Number: 25544
Epoch time: 19116
52628668 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 257
9866 deg
Eccentricity:
0001355
Arg of perigee: 230
6680 deg
Mean anomaly: 129
4352 deg
Mean motion: 15
52597734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 722
Checksum: 327
Coasting Arc #4 (Orbit 737)
---------------------------------------
Vector Time (GMT): 2019/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1480187
19 A = 6787501
63 meter
Y = -5407221
21 meter E =
0010428
Z = 3819480
03 I = 51
27213
XDOT = 4852
360304 Wp = 102
93642
YDOT = 4258
643749 meter/sec RA = 252
19097 deg
ZDOT = 4136
609324 TA = 303
26156
MA = 303
36144
Ha = 222
945 n
mi
Hp = 217
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4856257
18 X = 1521989
31
Y = -17740227
07 feet Y = -5390435
02 meter
Z = 12531102
46 Z = 3826771
73
XDOT = 15919
817271 XDOT = 4784
284910
YDOT = 13971
928310 feet/sec YDOT = 4312
525575 meter/sec
ZDOT = 13571
552900 ZDOT = 4160
015007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6054386
28 X = -1845376
94
Y = -17343697
74 feet Y = -5286359
07 meter
Z = 12564552
30 Z = 3829675
54
XDOT = 19685
257281 XDOT = 6000
066419
YDOT = 3064
577176 feet/sec YDOT = 934
083123 meter/sec
ZDOT = 13676
994925 ZDOT = 4168
748053
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 19117
55613511
00016717 00000-0 10270-3 0 9036
2 25544 51
6397 252
8646 0001363 235
1841 124
9183 15
52622377 7389
Satellite: ISS
Catalog Number: 25544
Epoch time: 19117
55613511 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 252
8646 deg
Eccentricity:
0001363
Arg of perigee: 235
1841 deg
Mean anomaly: 124
9183 deg
Mean motion: 15
52622377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 738
Checksum: 309
Coasting Arc #5 (Orbit 752)
---------------------------------------
Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4516387
05 A = 6788927
71 meter
Y = 3773424
89 meter E =
0011401
Z = 3373495
42 I = 51
28638
XDOT = -1511
999843 Wp = 94
06316
YDOT = 5940
429616 meter/sec RA = 247
23032 deg
ZDOT = -4607
717981 TA = 46
34324
MA = 46
24878
Ha = 222
976 n
mi
Hp = 217
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14817542
82 X = 4457469
27
Y = 12380002
91 feet Y = 3823600
87 meter
Z = 11067898
36 Z = 3395291
27
XDOT = -4960
629407 XDOT = -1555
933250
YDOT = 19489
598477 feet/sec YDOT = 5923
275709 meter/sec
ZDOT = -15117
184978 ZDOT = -4615
169458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18889976
36 X = 5757664
79
Y = 3716040
49 feet Y = 1132649
14 meter
Z = 11166120
98 Z = 3403433
67
XDOT = 5433
156662 XDOT = 1656
026150
YDOT = 18033
054249 feet/sec YDOT = 5496
474935 meter/sec
ZDOT = -15151
392386 ZDOT = -4618
144399
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 19118
52161846
00016717 00000-0 10270-3 0 9044
2 25544 51
6384 248
0630 0001284 235
0771 125
0260 15
52580892 7538
Satellite: ISS
Catalog Number: 25544
Epoch time: 19118
52161846 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 248
0630 deg
Eccentricity:
0001284
Arg of perigee: 235
0771 deg
Mean anomaly: 125
0260 deg
Mean motion: 15
52580892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 753
Checksum: 296
Coasting Arc #6 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4510491
51 A = 6791329
00 meter
Y = -4486074
50 meter E =
0004372
Z = -2374404
44 I = 51
30966
XDOT = 2192
368284 Wp = 41
63808
YDOT = -5030
236829 meter/sec RA = 242
23727 deg
ZDOT = 5348
070424 TA = 291
74652
MA = 291
79304
Ha = 222
961 n
mi
Hp = 217
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14798200
49 X = -4448458
13
Y = -14718092
19 feet Y = -4536167
16 meter
Z = -7790040
82 Z = -2396164
08
XDOT = 7192
809332 XDOT = 2222
476816
YDOT = -16503
401671 feet/sec YDOT = -5005
551808 meter/sec
ZDOT = 17546
162807 ZDOT = 5358
793372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20118032
79 X = -6131976
39
Y = -5416369
68 feet Y = -1650909
48 meter
Z = -7888054
74 Z = -2404279
09
XDOT = -2481
238700 XDOT = -756
281556
YDOT = -16366
293586 feet/sec YDOT = -4988
446285 meter/sec
ZDOT = 17595
074368 ZDOT = 5362
978667
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 19119
48709702
00016717 00000-0 10270-3 0 9050
2 25544 51
6396 243
2613 0001281 245
5208 114
5811 15
52599091 7689
Satellite: ISS
Catalog Number: 25544
Epoch time: 19119
48709702 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 243
2613 deg
Eccentricity:
0001281
Arg of perigee: 245
5208 deg
Mean anomaly: 114
5811 deg
Mean motion: 15
52599091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 313
Coasting Arc #7 (Orbit 781)
---------------------------------------
Vector Time (GMT): 2019/120/08:22:21
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5067750
28 A = 6788805
84 meter
Y = 2985346
76 meter E =
0011097
Z = 3380317
68 I = 51
31326
XDOT = -519
670988 Wp = 91
18133
YDOT = 6110
001028 meter/sec RA = 237
90294 deg
ZDOT = -4604
086228 TA = 49
14910
MA = 49
05296
Ha = 222
809 n
mi
Hp = 217
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16626477
29 X = 5017570
82
Y = 9794444
77 feet Y = 3041737
40 meter
Z = 11090281
11 Z = 3404813
14
XDOT = -1704
957310 XDOT = -565
591895
YDOT = 20045
935132 feet/sec YDOT = 6103
932849 meter/sec
ZDOT = -15105
269777 ZDOT = -4606
722271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12889045
90 X = 3928581
19
Y = 14275143
09 feet Y = 4351063
61 meter
Z = 11200804
26 Z = 3414005
14
XDOT = -6452
475007 XDOT = -1966
714382
YDOT = 17720
751542 feet/sec YDOT = 5401
285070 meter/sec
ZDOT = -15117
694339 ZDOT = -4607
873234
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 19120
38820622
00016717 00000-0 10270-3 0 9067
2 25544 51
6373 238
7797 0001321 262
0724 98
0278 15
52612381 7825
Satellite: ISS
Catalog Number: 25544
Epoch time: 19120
38820622 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 238
7797 deg
Eccentricity:
0001321
Arg of perigee: 262
0724 deg
Mean anomaly: 98
0278 deg
Mean motion: 15
52612381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 782
Checksum: 306
Coasting Arc #8 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2019/121/08:22:21
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177624
58 A = 6791254
61 meter
Y = -3692726
36 meter E =
0004688
Z = -2379169
05 I = 51
34061
XDOT = 1341
424669 Wp = 40
68519
YDOT = -5320
650976 meter/sec RA = 232
91132 deg
ZDOT = 5348
429487 TA = 292
65337
MA = 292
70294
Ha = 222
968 n
mi
Hp = 217
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16986957
29 X = -5124389
86
Y = -12115243
95 feet Y = -3750328
58 meter
Z = -7805672
75 Z = -2404190
88
XDOT = 4400
999570 XDOT = 1374
842048
YDOT = -17456
203991 feet/sec YDOT = -5305
463257 meter/sec
ZDOT = 17547
340838 ZDOT = 5355
026976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12847724
47 X = -3915986
42
Y = -16385884
35 feet Y = -4994417
55 meter
Z = -7918532
13 Z = -2413568
59
XDOT = 7820
408650 XDOT = 2383
660556
YDOT = -14611
421977 feet/sec YDOT = -4453
561419 meter/sec
ZDOT = 17577
605921 ZDOT = 5357
654285
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 19121
35367953
00016717 00000-0 10270-3 0 9079
2 25544 51
6378 233
9773 0001038 258
5061 101
5974 15
52618095 7977
Satellite: ISS
Catalog Number: 25544
Epoch time: 19121
35367953 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 233
9773 deg
Eccentricity:
0001038
Arg of perigee: 258
5061 deg
Mean anomaly: 101
5974 deg
Mean motion: 15
52618095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 330
Coasting Arc #9 (Orbit 812)
---------------------------------------
Vector Time (GMT): 2019/122/08:22:21
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5150515
94 A = 6792990
07 meter
Y = 4246665
05 meter E =
0012746
Z = 1223038
89 I = 51
36676
XDOT = -2267
161188 Wp = 124
27589
YDOT = 4438
303679 meter/sec RA = 227
92620 deg
ZDOT = -5826
692520 TA = 42
38576
MA = 42
28737
Ha = 222
880 n
mi
Hp = 217
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16898018
17 X = 5096704
80
Y = 13932628
11 feet Y = 4303960
87 meter
Z = 4012594
77 Z = 1247927
73
XDOT = -7438
192875 XDOT = -2288
319843
YDOT = 14561
363775 feet/sec YDOT = 4412
832287 meter/sec
ZDOT = -19116
445276 ZDOT = -5837
757157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12585919
23 X = 3836188
18
Y = 17898115
47 feet Y = 5455345
60 meter
Z = 4124822
46 Z = 1257245
88
XDOT = -9594
707704 XDOT = -2924
466908
YDOT = 11191
056353 feet/sec YDOT = 3411
033976 meter/sec
ZDOT = -19166
837852 ZDOT = -5842
052177
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 19122
38351273
00016717 00000-0 10270-3 0 9082
2 25544 51
6370 228
8554 0001186 269
8322 90
2694 15
52640970 8137
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
38351273 = yrday
fracday
Element set: 908
Inclination: 51
6370 deg
RA of node: 228
8554 deg
Eccentricity:
0001186
Arg of perigee: 269
8322 deg
Mean anomaly: 90
2694 deg
Mean motion: 15
52640970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 813
Checksum: 313
Coasting Arc #10 (Orbit 814)
---------------------------------------
Vector Time (GMT): 2019/122/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 295190
32 A = 6784930
66 meter
Y = -5036455
65 meter E =
0007797
Z = 4532730
60 I = 51
34560
XDOT = 6264
473114 Wp = 118
21428
YDOT = 3158
732878 meter/sec RA = 227
41407 deg
ZDOT = 3094
102117 TA = 300
63485
MA = 300
71171
Ha = 222
866 n
mi
Hp = 217
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 968472
17 X = 329469
66
Y = -16523804
63 feet Y = -5032962
88 meter
Z = 14871163
40 Z = 4534247
89
XDOT = 20552
733314 XDOT = 6213
656035
YDOT = 10363
296844 feet/sec YDOT = 3228
502518 meter/sec
ZDOT = 10151
253665 ZDOT = 3124
409524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5977199
93 X = -1821850
54
Y = -15428258
39 feet Y = -4702533
16 meter
Z = 14878423
40 Z = 4534943
45
XDOT = 21807
239857 XDOT = 6646
846708
YDOT = 1497
219977 feet/sec YDOT = 456
352649 meter/sec
ZDOT = 10288
075224 ZDOT = 3135
805328
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 19122
51224188
00016717 00000-0 10270-3 0 9092
2 25544 51
6404 228
2153 0001242 258
3630 101
7383 15
52645740 8157
Satellite: ISS
Catalog Number: 25544
Epoch time: 19122
51224188 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 228
2153 deg
Eccentricity:
0001242
Arg of perigee: 258
3630 deg
Mean anomaly: 101
7383 deg
Mean motion: 15
52645740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 815
Checksum: 283
Coasting Arc #11 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2019/123/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1181777
56 A = 6782911
36 meter
Y = 4385956
18 meter E =
0011807
Z = -5048090
52 I = 51
36302
XDOT = -6370
170412 Wp = 75
30257
YDOT = -3830
402310 meter/sec RA = 222
41467 deg
ZDOT = -1837
382390 TA = 176
81008
MA = 176
80254
Ha = 222
908 n
mi
Hp = 217
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3877222
95 X = -1206213
49
Y = 14389620
00 feet Y = 4372604
07 meter
Z = -16561976
77 Z = -5053890
62
XDOT = -20899
509227 XDOT = -6317
939179
YDOT = -12566
936714 feet/sec YDOT = -3901
345980 meter/sec
ZDOT = -6028
157447 ZDOT = -1868
199952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2711689
43 X = 826522
94
Y = 14623944
81 feet Y = 4457378
38 meter
Z = -16588552
52 Z = -5056190
81
XDOT = -23156
799600 XDOT = -7058
192518
YDOT = -2699
330726 feet/sec YDOT = -822
756005 meter/sec
ZDOT = -6167
248689 ZDOT = -1879
777400
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 19123
47770836
00016717 00000-0 10270-3 0 9106
2 25544 51
6414 223
4142 0001239 265
7901 94
3109 15
52623477 8305
Satellite: ISS
Catalog Number: 25544
Epoch time: 19123
47770836 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 223
4142 deg
Eccentricity:
0001239
Arg of perigee: 265
7901 deg
Mean anomaly: 94
3109 deg
Mean motion: 15
52623477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 295
Coasting Arc #12 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2019/124/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2119990
57 A = 6781688
14 meter
Y = -3688231
71 meter E =
0001698
Z = 5280335
13 I = 51
38505
XDOT = 6308
116906 Wp = 125
43610
YDOT = 4330
987794 meter/sec RA = 217
41278 deg
ZDOT = 491
416824 TA = 319
85268
MA = 319
86523
Ha = 222
764 n
mi
Hp = 217
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6955349
64 X = 2135426
42
Y = -12100497
73 feet Y = -3664438
26 meter
Z = 17323934
17 Z = 5290670
89
XDOT = 20695
921608 XDOT = 6256
830656
YDOT = 14209
277538 feet/sec YDOT = 4401
242807 meter/sec
ZDOT = 1612
259921 ZDOT = 521
935400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 804567
96 X = 245232
31
Y = -13875143
91 feet Y = -4229143
86 meter
Z = 17370972
36 Z = 5294672
37
XDOT = 23818
585514 XDOT = 7259
904865
YDOT = 3576
448111 feet/sec YDOT = 1090
101384 meter/sec
ZDOT = 1749
976106 ZDOT = 533
392717
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 19124
50753313
00016717 00000-0 10270-3 0 9113
2 25544 51
6417 218
2918 0001207 274
2526 85
8488 15
52670804 8462
Satellite: ISS
Catalog Number: 25544
Epoch time: 19124
50753313 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 218
2918 deg
Eccentricity:
0001207
Arg of perigee: 274
2526 deg
Mean anomaly: 85
8488 deg
Mean motion: 15
52670804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 309
Coasting Arc #13 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2019/125/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3093154
37 A = 6781888
06 meter
Y = 2998135
38 meter E =
0013383
Z = -5249828
62 I = 51
41226
XDOT = -6013
659532 Wp = 96
55043
YDOT = -4655
065746 meter/sec RA = 212
41365 deg
ZDOT = 885
178274 TA = 181
95289
MA = 181
95812
Ha = 222
915 n
mi
Hp = 217
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10148144
25 X = -3100949
19
Y = 9836402
18 feet Y = 2963502
18 meter
Z = -17223847
17 Z = -5264873
14
XDOT = -19729
854107 XDOT = -5965
458107
YDOT = -15272
525414 feet/sec YDOT = -4722
045218 meter/sec
ZDOT = 2904
128196 ZDOT = 856
082458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4440401
31 X = -1353434
32
Y = 13329116
04 feet Y = 4062714
57 meter
Z = -17292138
46 Z = -5270643
80
XDOT = -23569
491710 XDOT = -7183
981073
YDOT = -4256
467468 feet/sec YDOT = -1297
371284 meter/sec
ZDOT = 2772
856003 ZDOT = 845
166510
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 19125
47299363
00016717 00000-0 10270-3 0 9121
2 25544 51
6412 213
4915 0001114 281
1733 78
9294 15
52654559 8619
Satellite: ISS
Catalog Number: 25544
Epoch time: 19125
47299363 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 213
4915 deg
Eccentricity:
0001114
Arg of perigee: 281
1733 deg
Mean anomaly: 78
9294 deg
Mean motion: 15
52654559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 314
Coasting Arc #14 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2019/126/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4041020
43 A = 6783211
94 meter
Y = -2325296
23 meter E =
0005671
Z = 4924552
48 I = 51
44553
XDOT = 5506
262308 Wp = 49
01372
YDOT = 4851
371999 meter/sec RA = 207
41604 deg
ZDOT = -2222
299456 TA = 62
76870
MA = 62
71093
Ha = 222
775 n
mi
Hp = 217
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13257941
04 X = 4042800
99
Y = -7628924
63 feet Y = -2280097
04 meter
Z = 16156668
26 Z = 4944186
84
XDOT = 18065
165054 XDOT = 5462
398565
YDOT = 15916
574800 feet/sec YDOT = 4912
701751 meter/sec
ZDOT = -7291
008713 ZDOT = -2195
657801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7999909
00 X = 2438372
26
Y = -12926354
80 feet Y = -3939952
94 meter
Z = 16245683
38 Z = 4951684
29
XDOT = 22535
429009 XDOT = 6868
798762
YDOT = 4912
761553 feet/sec YDOT = 1497
409721 meter/sec
ZDOT = -7170
837028 ZDOT = -2185
671126
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 19126
50281446
00016717 00000-0 10270-3 0 9130
2 25544 51
6412 208
3690 0001171 286
9898 73
1126 15
52659725 8778
Satellite: ISS
Catalog Number: 25544
Epoch time: 19126
50281446 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 208
3690 deg
Eccentricity:
0001171
Arg of perigee: 286
9898 deg
Mean anomaly: 73
1126 deg
Mean motion: 15
52659725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 322
Coasting Arc #15 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2019/127/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4917459
44 A = 6785432
25 meter
Y = 1720738
59 meter E =
0007746
Z = -4355332
32 I = 51
48284
XDOT = -4760
265870 Wp = 110
76895
YDOT = -4920
390635 meter/sec RA = 202
42530 deg
ZDOT = 3432
936282 TA = 194
17213
MA = 194
19387
Ha = 222
883 n
mi
Hp = 217
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16133397
10 X = -4915179
58
Y = 5645467
80 feet Y = 1665761
21 meter
Z = -14289148
03 Z = -4379214
25
XDOT = -15617
670176 XDOT = -4721
566465
YDOT = -16143
013894 feet/sec YDOT = -4973
407149 meter/sec
ZDOT = 11262
914311 ZDOT = 3409
905881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11264397
87 X = -3433388
47
Y = 12734487
67 feet Y = 3881471
84 meter
Z = -14397351
30 Z = -4388312
68
XDOT = -20635
607190 XDOT = -6289
733071
YDOT = -5645
525127 feet/sec YDOT = -1720
756059 meter/sec
ZDOT = 11159
070614 ZDOT = 3401
284723
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 19127
46826845
00016717 00000-0 10270-3 0 9145
2 25544 51
6409 203
5680 0001158 291
9621 68
1408 15
52670184 8921
Satellite: ISS
Catalog Number: 25544
Epoch time: 19127
46826845 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 203
5680 deg
Eccentricity:
0001158
Arg of perigee: 291
9621 deg
Mean anomaly: 68
1408 deg
Mean motion: 15
52670184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 320
Coasting Arc #16 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2019/128/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5302570
08 A = 6786899
71 meter
Y = 1535875
72 meter E =
0005924
Z = -3954035
38 I = 51
50781
XDOT = -4385
877635 Wp = 104
75131
YDOT = -4834
750428 meter/sec RA = 198
56645 deg
ZDOT = 4007
280379 TA = 207
17894
MA = 207
20996
Ha = 223
009 n
mi
Hp = 217
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17396883
47 X = -5300143
79
Y = 5038962
35 feet Y = 1476592
60 meter
Z = -12972557
03 Z = -3979787
64
XDOT = -14389
362319 XDOT = -4350
953544
YDOT = -15862
042085 feet/sec YDOT = -4883
601474 meter/sec
ZDOT = 13147
245339 ZDOT = 3986
059491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14696030
46 X = -4479350
08
Y = -10441687
09 feet Y = -3182626
23 meter
Z = -13089224
24 Z = -3989595
55
XDOT = 2684
633766 XDOT = 818
276372
YDOT = -20124
796590 feet/sec YDOT = -6134
038001 meter/sec
ZDOT = 13051
570461 ZDOT = 3978
118677
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 19128
24063089
00016717 00000-0 10270-3 0 9156
2 25544 51
6371 199
7241 0000996 305
8681 54
2378 15
52650070 9046
Satellite: ISS
Catalog Number: 25544
Epoch time: 19128
24063089 = yrday
fracday
Element set: 915
Inclination: 51
6371 deg
RA of node: 199
7241 deg
Eccentricity:
0000996
Arg of perigee: 305
8681 deg
Mean anomaly: 54
2378 deg
Mean motion: 15
52650070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 316
Coasting Arc #17 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2019/129/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5987430
78 A = 6789689
74 meter
Y = -1022260
67 meter E =
0012085
Z = 3022587
97 I = 51
54748
XDOT = 3325
208288 Wp = 93
88468
YDOT = 4835
457457 meter/sec RA = 193
58658 deg
ZDOT = -4935
251392 TA = 51
44265
MA = 51
33442
Ha = 222
947 n
mi
Hp = 217
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19643801
77 X = 5983734
79
Y = -3353873
58 feet Y = -955325
99 meter
Z = 9916627
20 Z = 3051663
89
XDOT = 10909
476012 XDOT = 3294
862644
YDOT = 15864
361736 feet/sec YDOT = 4872
473079 meter/sec
ZDOT = -16191
769659 ZDOT = -4919
171835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15008852
28 X = 4574698
18
Y = 13008940
62 feet Y = 3965125
10 meter
Z = 10048319
66 Z = 3062727
83
XDOT = -4328
013515 XDOT = -1319
178519
YDOT = 17484
872312 feet/sec YDOT = 5329
389081 meter/sec
ZDOT = -16119
349168 ZDOT = -4913
177626
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 19129
27044466
00016717 00000-0 10270-3 0 9169
2 25544 51
6356 194
6020 0001104 304
8549 55
2499 15
52640179 9204
Satellite: ISS
Catalog Number: 25544
Epoch time: 19129
27044466 = yrday
fracday
Element set: 916
Inclination: 51
6356 deg
RA of node: 194
6020 deg
Eccentricity:
0001104
Arg of perigee: 304
8549 deg
Mean anomaly: 55
2499 deg
Mean motion: 15
52640179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 920
Checksum: 307
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