[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 19th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14591 557 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
355/13:08:55
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
5
356/04:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 230
0
000/00:00:00
000 0
0 0
0 218
5
359/09:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
1
000/00:00:00
000 0
0 0
0 218
3
361/01:32:57
259 -0
9 1
8 1
8
N/A 1
5 -0
0 230
1
000/00:09:54
517 -0
1 -0
0 219
4
361/04:40:25
361 -0
9 1
6 1
6
N/A 1
3 0
0 230
0
000/00:08:50
721 0
1 0
0 220
3
362/07:16:34
000 0
0 0
0 0
0
N/A 0
0 0
0 230
1
000/00:00:00
000 0
0 0
0 220
2
362/13:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
1
000/00:00:00
000 0
0 0
0 220
4
Coasting Arc #1 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2019/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4381805
50 A = 6794395
75 meter
Y = 3402154
28 meter E =
0011805
Z = -3929708
41 I = 51
65650
XDOT = -5834
478017 Wp = 72
06998
YDOT = -2837
873058 meter/sec RA = 176
25071 deg
ZDOT = 4062
424269 TA = 240
45291
MA = 240
57065
Ha = 229
601 n
mi
Hp = 218
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14376002
29 X = -4400435
53
Y = 11161923
50 feet Y = 3353050
15 meter
Z = -12892744
14 Z = -3951038
25
XDOT = -19141
988246 XDOT = -5822
043308
YDOT = -9310
607146 feet/sec YDOT = -2903
049287 meter/sec
ZDOT = 13328
163613 ZDOT = 4034
112632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9592431
93 X = -2923773
25
Y = -15385591
95 feet Y = -4689528
43 meter
Z = -12990367
18 Z = -3959463
92
XDOT = 10163
622234 XDOT = 3097
872057
YDOT = -17443
448905 feet/sec YDOT = -5316
763226 meter/sec
ZDOT = 13198
976696 ZDOT = 4023
048097
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 19350
50859596
00016717 00000-0 10270-3 0 9002
2 25544 51
6378 177
4360 0007414 40
2449 319
9249 15
50120225 3530
Satellite: ISS
Catalog Number: 25544
Epoch time: 19350
50859596 = yrday
fracday
Element set: 900
Inclination: 51
6378 deg
RA of node: 177
4360 deg
Eccentricity:
0007414
Arg of perigee: 40
2449 deg
Mean anomaly: 319
9249 deg
Mean motion: 15
50120225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 306
Coasting Arc #2 (Orbit 368)
---------------------------------------
Vector Time (GMT): 2019/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4469672
21 A = 6795312
44 meter
Y = -3591436
87 meter E =
0017899
Z = 3638046
49 I = 51
69302
XDOT = 5705
942459 Wp = 69
82212
YDOT = 2632
944040 meter/sec RA = 171
29825 deg
ZDOT = -4387
485027 TA = 67
11940
MA = 66
93053
Ha = 229
582 n
mi
Hp = 218
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14664278
92 X = 4491829
05
Y = -11782929
36 feet Y = -3541330
30 meter
Z = 11935848
06 Z = 3659811
77
XDOT = 18720
283658 XDOT = 5697
387827
YDOT = 8638
267848 feet/sec YDOT = 2696
704521 meter/sec
ZDOT = -14394
635914 ZDOT = -4359
788435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10448277
75 X = 3184635
06
Y = 15566746
78 feet Y = 4744744
42 meter
Z = 12035483
21 Z = 3668415
28
XDOT = -9130
281371 XDOT = -2782
909762
YDOT = 17219
005069 feet/sec YDOT = 5248
352745 meter/sec
ZDOT = -14268
226627 ZDOT = -4348
955476
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 19351
54009333
00016717 00000-0 10270-3 0 9014
2 25544 51
6379 172
3247 0007324 42
8938 317
2782 15
50125834 3691
Satellite: ISS
Catalog Number: 25544
Epoch time: 19351
54009333 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 172
3247 deg
Eccentricity:
0007324
Arg of perigee: 42
8938 deg
Mean anomaly: 317
2782 deg
Mean motion: 15
50125834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 369
Checksum: 309
Coasting Arc #3 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2019/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4484695
67 A = 6796109
84 meter
Y = 3832253
01 meter E =
0011462
Z = -3378555
51 I = 51
72826
XDOT = -5570
614058 Wp = 65
10575
YDOT = -2428
196967 meter/sec RA = 166
34836 deg
ZDOT = 4657
271033 TA = 255
61932
MA = 255
74658
Ha = 229
704 n
mi
Hp = 218
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14713568
49 X = -4510804
69
Y = 12573008
58 feet Y = 3781956
25 meter
Z = -11084499
72 Z = -3400403
47
XDOT = -18276
292840 XDOT = -5565
669533
YDOT = -7966
525482 feet/sec YDOT = -2490
464225 meter/sec
ZDOT = 15279
760606 ZDOT = 4630
223056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11498714
12 X = -3504808
06
Y = -15495853
27 feet Y = -4723136
08 meter
Z = -11184537
60 Z = -3409047
06
XDOT = 8123
376273 XDOT = 2476
005088
YDOT = -16927
252902 feet/sec YDOT = -5159
426685 meter/sec
ZDOT = 15156
286371 ZDOT = 4619
636086
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 19352
50712477
00016717 00000-0 10270-3 0 9022
2 25544 51
6376 167
5328 0007356 48
5103 311
6678 15
50117311 3846
Satellite: ISS
Catalog Number: 25544
Epoch time: 19352
50712477 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 167
5328 deg
Eccentricity:
0007356
Arg of perigee: 48
5103 deg
Mean anomaly: 311
6678 deg
Mean motion: 15
50117311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 302
Coasting Arc #4 (Orbit 399)
---------------------------------------
Vector Time (GMT): 2019/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4516863
51 A = 6796990
89 meter
Y = -4053821
30 meter E =
0018893
Z = 3047816
06 I = 51
76400
XDOT = 5400
414416 Wp = 80
28794
YDOT = 2285
207373 meter/sec RA = 161
40112 deg
ZDOT = -4934
731234 TA = 64
86845
MA = 64
67257
Ha = 229
700 n
mi
Hp = 218
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14819106
00 X = 4547054
26
Y = -13299938
63 feet Y = -4003141
93 meter
Z = 9999396
53 Z = 3069830
30
XDOT = 17717
895065 XDOT = 5398
429319
YDOT = 7497
399517 feet/sec YDOT = 2345
587853 meter/sec
ZDOT = -16190
063105 ZDOT = -4908
502772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12483404
81 X = 3804941
79
Y = 15447730
66 feet Y = 4708468
31 meter
Z = 10100218
96 Z = 3078546
74
XDOT = -7321
607694 XDOT = -2231
626025
YDOT = 16485
904386 feet/sec YDOT = 5024
903657 meter/sec
ZDOT = -16070
311729 ZDOT = -4898
231015
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 19353
53862159
00016717 00000-0 10270-3 0 9030
2 25544 51
6381 162
4212 0007313 50
8051 309
3748 15
50127004 4000
Satellite: ISS
Catalog Number: 25544
Epoch time: 19353
53862159 = yrday
fracday
Element set: 903
Inclination: 51
6381 deg
RA of node: 162
4212 deg
Eccentricity:
0007313
Arg of perigee: 50
8051 deg
Mean anomaly: 309
3748 deg
Mean motion: 15
50127004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 400
Checksum: 274
Coasting Arc #5 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2019/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4470496
94 A = 6797720
52 meter
Y = 4314931
80 meter E =
0012245
Z = -2757435
12 I = 51
79809
XDOT = -5237
800881 Wp = 58
19429
YDOT = -2145
390046 meter/sec RA = 156
45660 deg
ZDOT = 5157
726396 TA = 270
72807
MA = 270
86837
Ha = 229
851 n
mi
Hp = 218
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14666984
70 X = -4505021
40
Y = 14156600
39 feet Y = 4264746
69 meter
Z = -9046703
14 Z = -2779234
72
XDOT = -17184
386092 XDOT = -5238
474631
YDOT = -7038
681252 feet/sec YDOT = -2203
966957 meter/sec
ZDOT = 16921
674528 ZDOT = 5132
281294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13608781
86 X = -4147956
71
Y = -15116675
09 feet Y = -4607562
57 meter
Z = -9146573
31 Z = -2787875
54
XDOT = 6567
351637 XDOT = 2001
728779
YDOT = -16035
285980 feet/sec YDOT = -4887
555167 meter/sec
ZDOT = 16805
483667 ZDOT = 5122
311422
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 19354
50565164
00016717 00000-0 10270-3 0 9045
2 25544 51
6384 157
6294 0007505 56
6864 303
5004 15
50120647 4151
Satellite: ISS
Catalog Number: 25544
Epoch time: 19354
50565164 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 157
6294 deg
Eccentricity:
0007505
Arg of perigee: 56
6864 deg
Mean anomaly: 303
5004 deg
Mean motion: 15
50120647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 300
Coasting Arc #6 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2019/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 957055
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438989
33 A = 6798539
42 meter
Y = -4549853
23 meter E =
0019603
Z = 2394097
45 I = 51
82951
XDOT = 5047
866093 Wp = 90
41022
YDOT = 2073
473422 meter/sec RA = 151
51497 deg
ZDOT = -5380
991213 TA = 62
95335
MA = 62
75341
Ha = 229
863 n
mi
Hp = 218
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14563613
28 X = 4477907
95
Y = -14927339
98 feet Y = -4499995
90 meter
Z = 7854650
44 Z = 2415754
66
XDOT = 16561
240462 XDOT = 5050
442729
YDOT = 6802
734323 feet/sec YDOT = 2129
937073 meter/sec
ZDOT = -17654
170647 ZDOT = -5356
464026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14639328
88 X = 4462067
44
Y = 14800181
33 feet Y = 4511095
27 meter
Z = 7953900
12 Z = 2424348
76
XDOT = -6048
322698 XDOT = -1843
528758
YDOT = 15476
122049 feet/sec YDOT = 4717
122000 meter/sec
ZDOT = -17542
160590 ZDOT = -5346
850548
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 19355
53714888
00016717 00000-0 10270-3 0 9059
2 25544 51
6369 152
5181 0007407 59
7690 300
4193 15
50117307 4317
Satellite: ISS
Catalog Number: 25544
Epoch time: 19355
53714888 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 152
5181 deg
Eccentricity:
0007407
Arg of perigee: 59
7690 deg
Mean anomaly: 300
4193 deg
Mean motion: 15
50117307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 310
Coasting Arc #7 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2019/355/13:08:55
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4692260
57 A = 6791972
90 meter
Y = -1588504
46 meter E =
0014056
Z = 4634386
32 I = 51
81095
XDOT = 4727
357454 Wp = 89
99626
YDOT = -5255
353225 meter/sec RA = 151
32077 deg
ZDOT = 2977
249685 TA = 330
36931
MA = 330
44887
Ha = 229
955 n
mi
Hp = 218
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15394555
68 X = -4696660
10
Y = -5211628
81 feet Y = -1641001
62 meter
Z = 15204679
52 Z = 4611582
14
XDOT = 15509
702933 XDOT = 4771
311106
YDOT = -17241
972523 feet/sec YDOT = -5202
243055 meter/sec
ZDOT = 9767
879544 ZDOT = 3000
319854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 693869
14 X = 211491
31
Y = -16334887
86 feet Y = -4978873
82 meter
Z = 15100519
30 Z = 4602638
28
XDOT = 19665
799201 XDOT = 5994
135597
YDOT = 9986
670435 feet/sec YDOT = 3043
937149 meter/sec
ZDOT = 9873
627580 ZDOT = 3009
481686
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 19355
60161715
00016717 00000-0 10270-3 0 9063
2 25544 51
6388 152
1985 0007289 60
8096 299
3783 15
50143729 4326
Satellite: ISS
Catalog Number: 25544
Epoch time: 19355
60161715 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 152
1985 deg
Eccentricity:
0007289
Arg of perigee: 60
8096 deg
Mean anomaly: 299
3783 deg
Mean motion: 15
50143729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 333
Coasting Arc #8 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2019/356/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 586291
59 A = 6789878
28 meter
Y = 4402488
87 meter E =
0019862
Z = -5152740
91 I = 51
82372
XDOT = -6930
595590 Wp = 87
15022
YDOT = 2802
250322 meter/sec RA = 148
22394 deg
ZDOT = 1611
986281 TA = 198
36729
MA = 198
43912
Ha = 229
971 n
mi
Hp = 218
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1923528
83 X = 562047
40
Y = 14443861
11 feet Y = 4408910
12 meter
Z = -16905317
95 Z = -5149951
38
XDOT = -22738
174508 XDOT = -6969
246253
YDOT = 9193
734652 feet/sec YDOT = 2724
531241 meter/sec
ZDOT = 5288
668901 ZDOT = 1578
226235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5418859
43 X = 1651668
35
Y = -13541928
86 feet Y = -4127579
92 meter
Z = -16892808
74 Z = -5148928
10
XDOT = 23341
352368 XDOT = 7114
444202
YDOT = 2961
473974 feet/sec YDOT = 902
657267 meter/sec
ZDOT = 5134
171351 ZDOT = 1564
895428
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 19356
18183597
00016717 00000-0 10270-3 0 9070
2 25544 51
6406 149
3283 0007631 59
1523 301
0378 15
50115485 4412
Satellite: ISS
Catalog Number: 25544
Epoch time: 19356
18183597 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 149
3283 deg
Eccentricity:
0007631
Arg of perigee: 59
1523 deg
Mean anomaly: 301
0378 deg
Mean motion: 15
50115485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 306
Coasting Arc #9 (Orbit 456)
---------------------------------------
Vector Time (GMT): 2019/357/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -515296
42 A = 6790281
42 meter
Y = -4534464
70 meter E =
0013457
Z = 5020057
36 I = 51
85351
XDOT = 6742
057739 Wp = 59
92910
YDOT = -3033
026424 meter/sec RA = 143
28085 deg
ZDOT = -2036
930850 TA = 49
87043
MA = 49
75260
Ha = 229
954 n
mi
Hp = 218
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1690605
06 X = -488937
20
Y = -14876852
70 feet Y = -4540080
31 meter
Z = 16470004
47 Z = 5017617
73
XDOT = 22119
612003 XDOT = 6785
367174
YDOT = -9950
874095 feet/sec YDOT = -2957
389574 meter/sec
ZDOT = -6682
843997 ZDOT = -2004
075436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5600662
27 X = -1707081
86
Y = 13898569
75 feet Y = 4236284
06 meter
Z = 16459109
34 Z = 5016736
53
XDOT = -23201
422469 XDOT = -7071
793569
YDOT = -1572
064479 feet/sec YDOT = -479
165253 meter/sec
ZDOT = -6532
443027 ZDOT = -1991
088635
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 19357
21333217
00016717 00000-0 10270-3 0 9082
2 25544 51
6408 144
2174 0007592 62
1308 298
0611 15
50146720 4576
Satellite: ISS
Catalog Number: 25544
Epoch time: 19357
21333217 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 144
2174 deg
Eccentricity:
0007592
Arg of perigee: 62
1308 deg
Mean anomaly: 298
0611 deg
Mean motion: 15
50146720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 457
Checksum: 292
Coasting Arc #10 (Orbit 471)
---------------------------------------
Vector Time (GMT): 2019/358/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 513082
37 A = 6790921
92 meter
Y = 4689934
39 meter E =
0018382
Z = -4900500
29 I = 51
88262
XDOT = -6493
904970 Wp = 91
45825
YDOT = 3233
870024 meter/sec RA = 138
33943 deg
ZDOT = 2422
403953 TA = 202
24098
MA = 202
32081
Ha = 230
038 n
mi
Hp = 218
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1683341
10 X = 484404
00
Y = 15386923
85 feet Y = 4695512
36 meter
Z = -16077756
87 Z = -4898076
94
XDOT = -21305
462501 XDOT = -6541
351137
YDOT = 10609
809790 feet/sec YDOT = 3160
984969 meter/sec
ZDOT = 7947
519531 ZDOT = 2390
744096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5607964
80 X = 1709307
67
Y = -14439151
01 feet Y = -4401053
23 meter
Z = -16066952
97 Z = -4897207
27
XDOT = 22788
404313 XDOT = 6945
905635
YDOT = 195
561811 feet/sec YDOT = 59
607240 meter/sec
ZDOT = 7802
545696 ZDOT = 2378
215928
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 19358
18036034
00016717 00000-0 10270-3 0 9097
2 25544 51
6419 139
4254 0007681 65
7269 294
4683 15
50120472 4729
Satellite: ISS
Catalog Number: 25544
Epoch time: 19358
18036034 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 139
4254 deg
Eccentricity:
0007681
Arg of perigee: 65
7269 deg
Mean anomaly: 294
4683 deg
Mean motion: 15
50120472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 320
Coasting Arc #11 (Orbit 487)
---------------------------------------
Vector Time (GMT): 2019/359/04:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -496114
79 A = 6791533
29 meter
Y = -4853993
99 meter E =
0015528
Z = 4714717
03 I = 51
90887
XDOT = 6265
219377 Wp = 66
35741
YDOT = -3399
611183 meter/sec RA = 133
40089 deg
ZDOT = -2827
343740 TA = 51
64740
MA = 51
50796
Ha = 230
032 n
mi
Hp = 218
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1627673
21 X = -464700
60
Y = -15925177
14 feet Y = -4859366
97 meter
Z = 15468231
73 Z = 4712382
66
XDOT = 20555
181683 XDOT = 6316
502830
YDOT = -11153
579996 feet/sec YDOT = -3329
261898 meter/sec
ZDOT = -9276
062140 ZDOT = -2796
785632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5655486
18 X = -1723792
19
Y = 14986562
45 feet Y = 4567904
23 meter
Z = 15457852
44 Z = 4711553
42
XDOT = -22340
114491 XDOT = -6809
266897
YDOT = 1038
359634 feet/sec YDOT = 316
492017 meter/sec
ZDOT = -9136
088657 ZDOT = -2784
679823
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 19359
21185671
00016717 00000-0 10270-3 0 9106
2 25544 51
6415 134
3149 0007665 69
0428 291
1542 15
50149197 4888
Satellite: ISS
Catalog Number: 25544
Epoch time: 19359
21185671 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 134
3149 deg
Eccentricity:
0007665
Arg of perigee: 69
0428 deg
Mean anomaly: 291
1542 deg
Mean motion: 15
50149197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 488
Checksum: 318
Coasting Arc #12 (Orbit 491)
---------------------------------------
Vector Time (GMT): 2019/359/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4859901
72 A = 6800907
17 meter
Y = 4714183
93 meter E =
0020141
Z = 546593
14 I = 51
94122
XDOT = -2943
949996 Wp = 59
21246
YDOT = -3748
755531 meter/sec RA = 132
24811 deg
ZDOT = 6002
610336 TA = 306
65323
MA = 306
83822
Ha = 230
052 n
mi
Hp = 218
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15944559
45 X = -4914910
94
Y = 15466482
72 feet Y = 4659529
42 meter
Z = 1793284
57 Z = 522852
72
XDOT = -9658
628597 XDOT = -2930
968803
YDOT = -12299
066703 feet/sec YDOT = -3781
605205 meter/sec
ZDOT = 19693
603464 ZDOT = 5988
340705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5030265
83 X = -1533225
02
Y = -21645233
49 feet Y = -6597467
17 meter
Z = 1684406
86 Z = 513407
21
XDOT = 14006
853941 XDOT = 4269
289081
YDOT = -1685
877711 feet/sec YDOT = -513
855526 meter/sec
ZDOT = 19628
566729 ZDOT = 5982
787139
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 19359
46973140
00016717 00000-0 10270-3 0 9110
2 25544 51
6376 133
0324 0007568 73
4145 286
7837 15
50117612 4921
Satellite: ISS
Catalog Number: 25544
Epoch time: 19359
46973140 = yrday
fracday
Element set: 911
Inclination: 51
6376 deg
RA of node: 133
0324 deg
Eccentricity:
0007568
Arg of perigee: 73
4145 deg
Mean anomaly: 286
7837 deg
Mean motion: 15
50117612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 315
Coasting Arc #13 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2019/360/09:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 987055
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4650710
03 A = 6800522
96 meter
Y = -4865188
21 meter E =
0014763
Z = -957820
33 I = 51
96338
XDOT = 2869
402410 Wp = 113
14478
YDOT = 3896
177790 meter/sec RA = 127
31671 deg
ZDOT = -5936
183785 TA = 77
15995
MA = 76
99504
Ha = 230
029 n
mi
Hp = 218
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15258235
00 X = 4709420
86
Y = -15961903
58 feet Y = -4812852
26 meter
Z = -3142455
14 Z = -935087
25
XDOT = 9414
049901 XDOT = 2854
455433
YDOT = 12782
735533 feet/sec YDOT = 3928
182845 meter/sec
ZDOT = -19475
668587 ZDOT = -5922
281082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6169784
39 X = 1880550
28
Y = 21217316
58 feet Y = 6467038
09 meter
Z = -3038151
29 Z = -926028
51
XDOT = -14296
000880 XDOT = -4357
421068
YDOT = 1415
452204 feet/sec YDOT = 431
429832 meter/sec
ZDOT = -19412
316410 ZDOT = -5916
874042
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 19360
43675898
00016717 00000-0 10270-3 0 9129
2 25544 51
6389 128
2405 0007611 75
0420 285
1573 15
50159779 5071
Satellite: ISS
Catalog Number: 25544
Epoch time: 19360
43675898 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 128
2405 deg
Eccentricity:
0007611
Arg of perigee: 75
0420 deg
Mean anomaly: 285
1573 deg
Mean motion: 15
50159779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 324
Coasting Arc #14 (Orbit 516)
---------------------------------------
Vector Time (GMT): 2019/361/01:37:54
517
Vector Time (MET): N/A
Weight (LBS) : 986864
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2348219
37 A = 6790857
11 meter
Y = 3751279
96 meter E =
0019287
Z = -5167551
30 I = 51
94359
XDOT = -5159
737435 Wp = 93
19124
YDOT = 5415
112626 meter/sec RA = 124
03451 deg
ZDOT = 1590
401914 TA = 192
10095
MA = 192
14735
Ha = 230
099 n
mi
Hp = 219
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7704131
78 X = 2331197
77
Y = 12307348
96 feet Y = 3777445
04 meter
Z = -16953908
47 Z = -5156185
40
XDOT = -16928
272425 XDOT = -5227
632534
YDOT = 17766
117539 feet/sec YDOT = 5357
032921 meter/sec
ZDOT = 5217
854047 ZDOT = 1565
174035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7008276
59 X = 2136122
71
Y = -12785180
73 feet Y = -3896923
09 meter
Z = -16902151
06 Z = -5151775
64
XDOT = 22813
118298 XDOT = 6953
438457
YDOT = 5777
882397 feet/sec YDOT = 1761
098555 meter/sec
ZDOT = 5102
085843 ZDOT = 1555
115765
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 19361
08144647
00016717 00000-0 10270-3 0 9135
2 25544 51
6420 125
0504 0006230 73
3223 286
8611 15
49777852 5178
Satellite: ISS
Catalog Number: 25544
Epoch time: 19361
08144647 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 125
0504 deg
Eccentricity:
0006230
Arg of perigee: 73
3223 deg
Mean anomaly: 286
8611 deg
Mean motion: 15
49777852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 517
Checksum: 297
Coasting Arc #15 (Orbit 518)
---------------------------------------
Vector Time (GMT): 2019/361/04:44:50
721
Vector Time (MET): N/A
Weight (LBS) : 986693
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2006062
59 A = 6792251
94 meter
Y = 4114587
64 meter E =
0016889
Z = -5033027
00 I = 51
94912
XDOT = -5304
053278 Wp = 95
27918
YDOT = 5107
944278 meter/sec RA = 123
39204 deg
ZDOT = 2066
201297 TA = 194
76046
MA = 194
80983
Ha = 230
045 n
mi
Hp = 220
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6581570
19 X = 1984350
36
Y = 13499303
28 feet Y = 4136900
23 meter
Z = -16512555
78 Z = -5023334
50
XDOT = -17401
749600 XDOT = -5370
813945
YDOT = 16758
347370 feet/sec YDOT = 5048
257003 meter/sec
ZDOT = 6778
875645 ZDOT = 2040
275111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3152510
08 X = -960885
07
Y = -14733081
05 feet Y = -4490643
10 meter
Z = -16468477
67 Z = -5019591
99
XDOT = 19971
029367 XDOT = 6087
169751
YDOT = -11701
312392 feet/sec YDOT = -3566
560017 meter/sec
ZDOT = 6659
929329 ZDOT = 2029
946459
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 19361
21041083
00016717 00000-0 10270-3 0 9141
2 25544 51
6431 124
4127 0004909 68
3107 291
8565 15
49492758 5195
Satellite: ISS
Catalog Number: 25544
Epoch time: 19361
21041083 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 124
4127 deg
Eccentricity:
0004909
Arg of perigee: 68
3107 deg
Mean anomaly: 291
8565 deg
Mean motion: 15
49492758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 519
Checksum: 310
Coasting Arc #16 (Orbit 534)
---------------------------------------
Vector Time (GMT): 2019/362/04:44:50
721
Vector Time (MET): N/A
Weight (LBS) : 986693
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2200141
05 A = 6792436
83 meter
Y = -4079459
07 meter E =
0011251
Z = 4958367
85 I = 51
96743
XDOT = 4939
134604 Wp = 63
71410
YDOT = -5412
933704 meter/sec RA = 118
46322 deg
ZDOT = -2253
042012 TA = 48
24210
MA = 48
14598
Ha = 230
081 n
mi
Hp = 220
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7218310
53 X = -2178444
47
Y = -13384052
08 feet Y = -4103942
00 meter
Z = 16267611
04 Z = 4947732
66
XDOT = 16204
509857 XDOT = 5010
240389
YDOT = -17758
968846 feet/sec YDOT = -5357
302912 meter/sec
ZDOT = -7391
870117 ZDOT = -2228
877965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4050017
63 X = 1234445
38
Y = 14710757
32 feet Y = 4483838
83 meter
Z = 16219217
07 Z = 4943617
36
XDOT = -18833
696489 XDOT = -5740
510690
YDOT = 13244
574974 feet/sec YDOT = 4036
946452 meter/sec
ZDOT = -7280
944141 ZDOT = -2219
231774
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 19362
24233354
00016717 00000-0 10270-3 0 9150
2 25544 51
6431 119
3047 0004877 71
0179 289
1499 15
49518344 5357
Satellite: ISS
Catalog Number: 25544
Epoch time: 19362
24233354 = yrday
fracday
Element set: 915
Inclination: 51
6431 deg
RA of node: 119
3047 deg
Eccentricity:
0004877
Arg of perigee: 71
0179 deg
Mean anomaly: 289
1499 deg
Mean motion: 15
49518344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 535
Checksum: 321
Coasting Arc #17 (Orbit 535)
---------------------------------------
Vector Time (GMT): 2019/362/07:16:34
000
Vector Time (MET): N/A
Weight (LBS) : 956693
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1716273
23 A = 6801431
94 meter
Y = 6314654
83 meter E =
0011550
Z = -1846275
91 I = 51
99506
XDOT = -5144
808470 Wp = 53
44067
YDOT = 249
402277 meter/sec RA = 117
94212 deg
ZDOT = 5666
791632 TA = 286
40097
MA = 286
52791
Ha = 230
098 n
mi
Hp = 220
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5630817
69 X = -1777789
94
Y = 20717371
48 feet Y = 6295118
55 meter
Z = -6057335
66 Z = -1854761
32
XDOT = -16879
292882 XDOT = -5174
740697
YDOT = 818
248940 feet/sec YDOT = 191
701235 meter/sec
ZDOT = 18591
836062 ZDOT = 5641
727789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3587119
12 X = -1093353
91
Y = -21155878
03 feet Y = -6448311
62 meter
Z = -6096581
46 Z = -1858238
03
XDOT = 13560
684482 XDOT = 4133
296630
YDOT = -7594
595290 feet/sec YDOT = -2314
832644 meter/sec
ZDOT = 18477
132684 ZDOT = 5631
830042
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 19362
30682995
00016717 00000-0 10270-3 0 9167
2 25544 51
6394 118
9825 0004921 74
2023 285
9670 15
49473916 5368
Satellite: ISS
Catalog Number: 25544
Epoch time: 19362
30682995 = yrday
fracday
Element set: 916
Inclination: 51
6394 deg
RA of node: 118
9825 deg
Eccentricity:
0004921
Arg of perigee: 74
2023 deg
Mean anomaly: 285
9670 deg
Mean motion: 15
49473916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 536
Checksum: 339
Coasting Arc #18 (Orbit 539)
---------------------------------------
Vector Time (GMT): 2019/362/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 956693
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3745810
46 A = 6790929
66 meter
Y = 1882306
30 meter E =
0019626
Z = -5359434
21 I = 51
96746
XDOT = -3438
785742 Wp = 87
21754
YDOT = 6829
428822 meter/sec RA = 116
74943 deg
ZDOT = -3
931879 TA = 182
73967
MA = 182
75044
Ha = 230
086 n
mi
Hp = 220
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12289404
40 X = 3750516
31
Y = 6175545
59 feet Y = 1924221
64 meter
Z = -17583445
57 Z = -5341227
06
XDOT = -11282
105452 XDOT = -3514
879735
YDOT = 22406
262541 feet/sec YDOT = 6790
548421 meter/sec
ZDOT = -12
899867 ZDOT = -20
819838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -757352
48 X = -230841
04
Y = 13838779
54 feet Y = 4218060
00 meter
Z = -17500256
56 Z = -5334078
20
XDOT = -24032
858568 XDOT = -7325
215292
YDOT = -1433
657616 feet/sec YDOT = -436
978841 meter/sec
ZDOT = -90
632391 ZDOT = -27
624753
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 19362
56481166
00016717 00000-0 10270-3 0 9173
2 25544 51
6431 117
7054 0004863 78
5130 281
6566 15
49480354 5408
Satellite: ISS
Catalog Number: 25544
Epoch time: 19362
56481166 = yrday
fracday
Element set: 917
Inclination: 51
6431 deg
RA of node: 117
7054 deg
Eccentricity:
0004863
Arg of perigee: 78
5130 deg
Mean anomaly: 281
6566 deg
Mean motion: 15
49480354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 540
Checksum: 315
Coasting Arc #19 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2019/363/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 956693
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3801627
74 A = 6790814
91 meter
Y = -1744376
53 meter E =
0007225
Z = 5343611
26 I = 51
98167
XDOT = 2981
340417 Wp = 82
58319
YDOT = -7061
089362 meter/sec RA = 111
82161 deg
ZDOT = -182
886354 TA = 9
15852
MA = 9
14535
Ha = 230
159 n
mi
Hp = 220
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12472531
94 X = -3807794
90
Y = -5723020
12 feet Y = -1786924
13 meter
Z = 17531533
01 Z = 5325129
52
XDOT = 9781
300581 XDOT = 3060
966348
YDOT = -23166
303682 feet/sec YDOT = -7027
304668 meter/sec
ZDOT = -600
020847 ZDOT = -168
211801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 31555
17 X = 9618
02
Y = -13830052
57 feet Y = -4215400
02 meter
Z = 17447071
74 Z = 5317867
47
XDOT = 24132
001902 XDOT = 7355
434180
YDOT = -621
214303 feet/sec YDOT = -189
346120 meter/sec
ZDOT = -532
385221 ZDOT = -162
271015
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 19363
59673552
00016717 00000-0 10270-3 0 9180
2 25544 51
6432 112
5972 0004775 82
5947 277
5746 15
49515571 5565
Satellite: ISS
Catalog Number: 25544
Epoch time: 19363
59673552 = yrday
fracday
Element set: 918
Inclination: 51
6432 deg
RA of node: 112
5972 deg
Eccentricity:
0004775
Arg of perigee: 82
5947 deg
Mean anomaly: 277
5746 deg
Mean motion: 15
49515571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 349
Coasting Arc #20 (Orbit 570)
---------------------------------------
Vector Time (GMT): 2019/364/13:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 956693
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3881356
32 A = 6790984
23 meter
Y = 1610957
96 meter E =
0019528
Z = -5351399
25 I = 51
99309
XDOT = -2492
223109 Wp = 90
96292
YDOT = 7219
518269 meter/sec RA = 106
89552 deg
ZDOT = 366
560378 TA = 182
52026
MA = 182
53011
Ha = 230
082 n
mi
Hp = 220
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12734108
67 X = 3889047
31
Y = 5285295
15 feet Y = 1654405
55 meter
Z = -17557084
14 Z = -5332526
57
XDOT = -8176
585002 XDOT = -2574
549160
YDOT = 23686
083560 feet/sec YDOT = 7191
188118 meter/sec
ZDOT = 1202
625912 ZDOT = 354
255054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 713937
67 X = 217608
20
Y = 13878177
93 feet Y = 4230068
63 meter
Z = -17470819
73 Z = -5325105
85
XDOT = -23900
219725 XDOT = -7284
786972
YDOT = 2668
454435 feet/sec YDOT = 813
344912 meter/sec
ZDOT = 1145
807820 ZDOT = 349
242223
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 19364
56416563
00016717 00000-0 10270-3 0 9196
2 25544 51
6431 107
8093 0004790 85
0216 275
1481 15
49475334 5718
Satellite: ISS
Catalog Number: 25544
Epoch time: 19364
56416563 = yrday
fracday
Element set: 919
Inclination: 51
6431 deg
RA of node: 107
8093 deg
Eccentricity:
0004790
Arg of perigee: 85
0216 deg
Mean anomaly: 275
1481 deg
Mean motion: 15
49475334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 571
Checksum: 318
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