[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 3rd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
216/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
8
000/00:00:00
000 0
0 0
0 220
9
218/16:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
4
000/00:00:00
000 0
0 0
0 221
2
220/06:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
2
000/00:00:00
000 0
0 0
0 221
4
227/05:42:47
315 0
3 1
8 1
8
N/A 1
7 0
0 223
7
000/00:09:34
629 0
4 -0
0 222
9
227/08:44:47
258 0
6 1
8 1
8
N/A 1
7 -0
0 224
0
000/00:09:34
515 0
1 -0
0 223
6
Coasting Arc #1 (Orbit 2243)
---------------------------------------
Vector Time (GMT): 2019/214/12:08:31
897
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4523021
05 A = 6787850
16 meter
Y = -740059
83 meter E =
0008836
Z = 5008045
63 I = 51
91891
XDOT = 3403
236619 Wp = 167
41438
YDOT = -6536
224932 meter/sec RA = 130
39903 deg
ZDOT = 2098
658151 TA = 262
17237
MA = 262
27268
Ha = 226
068 n
mi
Hp = 220
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14839307
91 X = -4538734
98
Y = -2428017
81 feet Y = -790727
57 meter
Z = 16430595
89 Z = 4986036
87
XDOT = 11165
474471 XDOT = 3465
879793
YDOT = -21444
307520 feet/sec YDOT = -6497
817406 meter/sec
ZDOT = 6885
361387 ZDOT = 2115
341131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8209254
00 X = 2502180
62
Y = 12727435
60 feet Y = 3879322
37 meter
Z = 16330503
45 Z = 4977537
45
XDOT = -22443
164095 XDOT = -6840
676416
YDOT = 5504
861154 feet/sec YDOT = 1677
881680 meter/sec
ZDOT = 6961
739213 ZDOT = 2121
938112
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 19214
55795705
00016717 00000-0 10270-3 0 9007
2 25544 51
6429 131
2149 0006170 211
9520 148
1257 15
51041972 22449
Satellite: ISS
Catalog Number: 25544
Epoch time: 19214
55795705 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 131
2149 deg
Eccentricity:
0006170
Arg of perigee: 211
9520 deg
Mean anomaly: 148
1257 deg
Mean motion: 15
51041972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2244
Checksum: 290
Coasting Arc #2 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2019/215/12:08:31
897
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4206634
48 A = 6786981
40 meter
Y = 1130051
37 meter E =
0010472
Z = -5213138
31 I = 51
93715
XDOT = -3466
181343 Wp = 103
40886
YDOT = 6691
816227 meter/sec RA = 125
45265 deg
ZDOT = -1351
018430 TA = 153
66671
MA = 153
61344
Ha = 225
876 n
mi
Hp = 220
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13801294
21 X = 4219007
18
Y = 3707517
60 feet Y = 1177162
24 meter
Z = -17103472
15 Z = -5192674
47
XDOT = -11371
986034 XDOT = -3534
191209
YDOT = 21954
777648 feet/sec YDOT = 6652
674723 meter/sec
ZDOT = -4432
475163 ZDOT = -1368
020413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6786471
83 X = -2068516
62
Y = -12701938
96 feet Y = -3871551
00 meter
Z = -17010429
59 Z = -5184778
94
XDOT = 22862
030760 XDOT = 6968
346976
YDOT = -6195
137111 feet/sec YDOT = -1888
277792 meter/sec
ZDOT = -4510
326391 ZDOT = -1374
747484
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 19215
52442198
00016717 00000-0 10270-3 0 9011
2 25544 51
6433 126
4199 0005988 215
1914 144
8843 15
51040774 22593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19215
52442198 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 126
4199 deg
Eccentricity:
0005988
Arg of perigee: 215
1914 deg
Mean anomaly: 144
8843 deg
Mean motion: 15
51040774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 318
Coasting Arc #3 (Orbit 2274)
---------------------------------------
Vector Time (GMT): 2019/216/12:08:31
897
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3928715
75 A = 6786440
00 meter
Y = -1532065
53 meter E =
0006111
Z = 5318954
77 I = 51
95343
XDOT = 3468
888827 Wp = 192
49033
YDOT = -6806
172522 meter/sec RA = 120
50751 deg
ZDOT = 596
090168 TA = 251
80720
MA = 251
87373
Ha = 225
766 n
mi
Hp = 220
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12889487
38 X = -3937127
78
Y = -5026461
73 feet Y = -1576046
29 meter
Z = 17450639
02 Z = 5299850
48
XDOT = 11380
868854 XDOT = 3541
844176
YDOT = -22329
962344 feet/sec YDOT = -6766
973057 meter/sec
ZDOT = 1955
676405 ZDOT = 613
117502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5423513
68 X = 1653086
97
Y = 12845726
31 feet Y = 3915377
38 meter
Z = 17363807
75 Z = 5292488
60
XDOT = -23020
637944 XDOT = -7016
690445
YDOT = 6945
153511 feet/sec YDOT = 2116
882790 meter/sec
ZDOT = 2033
663511 ZDOT = 619
860638
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 19216
55531431
00016717 00000-0 10270-3 0 9025
2 25544 51
6428 121
3056 0006178 220
0454 140
0242 15
51055498 22757
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
55531431 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 121
3056 deg
Eccentricity:
0006178
Arg of perigee: 220
0454 deg
Mean anomaly: 140
0242 deg
Mean motion: 15
51055498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2275
Checksum: 276
Coasting Arc #4 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3803012
16 A = 6798138
74 meter
Y = 5581692
43 meter E =
0007213
Z = 748550
60 I = 51
99243
XDOT = -3546
444480 Wp = 65
20547
YDOT = -3223
398446 meter/sec RA = 119
29929 deg
ZDOT = 5975
963647 TA = 302
83093
MA = 302
90036
Ha = 225
771 n
mi
Hp = 220
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12477074
01 X = -3868781
58
Y = 18312639
20 feet Y = 5538796
72 meter
Z = 2455874
66 Z = 729917
65
XDOT = -11635
316537 XDOT = -3539
163299
YDOT = -10575
454219 feet/sec YDOT = -3263
016628 meter/sec
ZDOT = 19606
179944 ZDOT = 5958
754327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3016162
99 X = -919326
48
Y = -21962334
82 feet Y = -6694119
65 meter
Z = 2370666
66 Z = 722579
20
XDOT = 14218
537061 XDOT = 4333
810096
YDOT = 170
684567 feet/sec YDOT = 52
024656 meter/sec
ZDOT = 19528
095730 ZDOT = 5952
163579
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 19216
81303731
00016717 00000-0 10270-3 0 9035
2 25544 51
6389 120
0223 0006359 219
1229 140
9463 15
51026663 22795
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
81303731 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 120
0223 deg
Eccentricity:
0006359
Arg of perigee: 219
1229 deg
Mean anomaly: 140
9463 deg
Mean motion: 15
51026663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 294
Coasting Arc #5 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3718363
99 A = 6797404
00 meter
Y = -5498146
68 meter E =
0011249
Z = -1432306
06 I = 52
00678
XDOT = 3296
774172 Wp = 175
05853
YDOT = 3742
404282 meter/sec RA = 114
36652 deg
ZDOT = -5821
474714 TA = 20
46635
MA = 20
42132
Ha = 225
552 n
mi
Hp = 220
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12199356
92 X = 3786526
74
Y = -18038538
98 feet Y = -5456184
19 meter
Z = -4699166
87 Z = -1414078
39
XDOT = 10816
188229 XDOT = 3282
957600
YDOT = 12278
229272 feet/sec YDOT = 3779
193926 meter/sec
ZDOT = -19099
326488 ZDOT = -5805
493972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3398007
08 X = 1035712
56
Y = 21527734
33 feet Y = 6561653
42 meter
Z = -4615795
62 Z = -1406894
51
XDOT = -14810
199903 XDOT = -4514
148931
YDOT = -1731
666262 feet/sec YDOT = -527
811877 meter/sec
ZDOT = -19026
873841 ZDOT = -5799
391147
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 19217
77949514
00016717 00000-0 10270-3 0 9047
2 25544 51
6399 115
2267 0006119 223
6999 136
3668 15
51068141 22948
Satellite: ISS
Catalog Number: 25544
Epoch time: 19217
77949514 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 115
2267 deg
Eccentricity:
0006119
Arg of perigee: 223
6999 deg
Mean anomaly: 136
3668 deg
Mean motion: 15
51068141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 339
Coasting Arc #6 (Orbit 2307)
---------------------------------------
Vector Time (GMT): 2019/218/16:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -452472
17 A = 6796233
49 meter
Y = 6404651
43 meter E =
0000526
Z = -2227239
15 I = 52
01411
XDOT = -5111
019620 Wp = 298
90770
YDOT = 1548
201728 meter/sec RA = 109
75782 deg
ZDOT = 5489
602482 TA = 36
52158
MA = 36
51800
Ha = 225
371 n
mi
Hp = 221
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1484488
75 X = -513238
62
Y = 21012635
93 feet Y = 6399251
84 meter
Z = -7307215
05 Z = -2229584
55
XDOT = -16768
437072 XDOT = -5154
617352
YDOT = 5079
401996 feet/sec YDOT = 1490
802850 meter/sec
ZDOT = 18010
506831 ZDOT = 5464
669466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5046621
65 X = -1538210
28
Y = -20447563
52 feet Y = -6232417
36 meter
Z = -7318382
56 Z = -2230643
01
XDOT = 13041
585185 XDOT = 3975
075164
YDOT = -9625
101613 feet/sec YDOT = -2933
730972 meter/sec
ZDOT = 17896
904797 ZDOT = 5454
976582
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 19218
68152018
00016717 00000-0 10270-3 0 9054
2 25544 51
6395 110
7521 0006203 227
9580 132
1044 15
51034662 23083
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
68152018 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 110
7521 deg
Eccentricity:
0006203
Arg of perigee: 227
9580 deg
Mean anomaly: 132
1044 deg
Mean motion: 15
51034662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2308
Checksum: 281
Coasting Arc #7 (Orbit 2323)
---------------------------------------
Vector Time (GMT): 2019/219/16:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 470767
13 A = 6797134
39 meter
Y = -6586821
97 meter E =
0012385
Z = 1576390
66 I = 52
02787
XDOT = 4935
929973 Wp = 143
91455
YDOT = -1032
499112 meter/sec RA = 104
82605 deg
ZDOT = -5774
993669 TA = 18
95526
MA = 18
90921
Ha = 225
078 n
mi
Hp = 221
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1544511
57 X = 536730
71
Y = -21610308
31 feet Y = -6581188
75 meter
Z = 5171885
37 Z = 1578837
46
XDOT = 16193
995976 XDOT = 4975
160299
YDOT = -3387
464277 feet/sec YDOT = -977
082540 meter/sec
ZDOT = -18946
829623 ZDOT = -5750
921726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5519388
14 X = 1682309
51
Y = 20947710
07 feet Y = 6384862
03 meter
Z = 5183544
82 Z = 1579944
46
XDOT = -12837
157449 XDOT = -3912
765590
YDOT = 8054
424075 feet/sec YDOT = 2454
988458 meter/sec
ZDOT = -18837
177750 ZDOT = -5741
571778
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 19219
71240285
00016717 00000-0 10270-3 0 9064
2 25544 51
6396 105
6372 0006212 234
2067 125
8507 15
51086481 23249
Satellite: ISS
Catalog Number: 25544
Epoch time: 19219
71240285 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 105
6372 deg
Eccentricity:
0006212
Arg of perigee: 234
2067 deg
Mean anomaly: 125
8507 deg
Mean motion: 15
51086481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2324
Checksum: 297
Coasting Arc #8 (Orbit 2332)
---------------------------------------
Vector Time (GMT): 2019/220/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4103635
17 A = 6790773
76 meter
Y = -3344974
53 meter E =
0002772
Z = -4254521
89 I = 52
01139
XDOT = 1540
522078 Wp = 106
63054
YDOT = 6547
815999 meter/sec RA = 101
94257 deg
ZDOT = -3664
854669 TA = 126
00640
MA = 125
98070
Ha = 225
190 n
mi
Hp = 221
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13463369
99 X = 4161400
58
Y = -10974325
89 feet Y = -3298761
64 meter
Z = -13958405
14 Z = -4234447
97
XDOT = 5054
206294 XDOT = 1484
989703
YDOT = 21482
335956 feet/sec YDOT = 6564
732850 meter/sec
ZDOT = -12023
801407 ZDOT = -3657
506060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -481933
80 X = -146893
42
Y = -17436052
97 feet Y = -5314508
95 meter
Z = -13866759
93 Z = -4226588
43
XDOT = 18911
306384 XDOT = 5764
166186
YDOT = 9006
342714 feet/sec YDOT = 2745
133259 meter/sec
ZDOT = -11990
879791 ZDOT = -3654
820160
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 19220
29227698
00016717 00000-0 10270-3 0 9073
2 25544 51
6400 102
7619 0006018 234
2826 125
7765 15
51041346 23330
Satellite: ISS
Catalog Number: 25544
Epoch time: 19220
29227698 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 102
7619 deg
Eccentricity:
0006018
Arg of perigee: 234
2826 deg
Mean anomaly: 125
7765 deg
Mean motion: 15
51041346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2333
Checksum: 297
Coasting Arc #9 (Orbit 2348)
---------------------------------------
Vector Time (GMT): 2019/221/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4004875
41 A = 6789241
08 meter
Y = 2934503
38 meter E =
0007138
Z = 4631987
17 I = 52
01380
XDOT = -1532
313728 Wp = 160
35481
YDOT = -6871
856853 meter/sec RA = 97
00487 deg
ZDOT = 3020
785145 TA = 259
58717
MA = 259
66762
Ha = 224
895 n
mi
Hp = 221
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13139355
03 X = -4059891
64
Y = 9627635
76 feet Y = 2889410
18 meter
Z = 15196808
29 Z = 4612399
70
XDOT = -5027
276010 XDOT = -1470
029923
YDOT = -22545
462115 feet/sec YDOT = -6888
644180 meter/sec
ZDOT = 9910
712419 ZDOT = 3013
492699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -114340
35 X = -34850
94
Y = 16371636
09 feet Y = 4990074
68 meter
Z = 15107397
56 Z = 4604734
78
XDOT = -19971
376917 XDOT = -6087
275684
YDOT = -9278
783595 feet/sec YDOT = -2828
173240 meter/sec
ZDOT = 9878
087689 ZDOT = 3010
841127
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 19221
32315546
00016717 00000-0 10270-3 0 9089
2 25544 51
6413 97
6476 0006232 238
7782 121
2759 15
51083630 23498
Satellite: ISS
Catalog Number: 25544
Epoch time: 19221
32315546 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 97
6476 deg
Eccentricity:
0006232
Arg of perigee: 238
7782 deg
Mean anomaly: 121
2759 deg
Mean motion: 15
51083630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2349
Checksum: 311
Coasting Arc #10 (Orbit 2363)
---------------------------------------
Vector Time (GMT): 2019/222/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3952656
02 A = 6788085
20 meter
Y = -2461956
07 meter E =
0006302
Z = -4944625
46 I = 52
01268
XDOT = 1550
991188 Wp = 83
10414
YDOT = 7133
713357 meter/sec RA = 92
06443 deg
ZDOT = -2313
864674 TA = 164
36407
MA = 164
34460
Ha = 224
774 n
mi
Hp = 221
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12968031
56 X = 4003910
51
Y = -8077283
70 feet Y = -2417467
79 meter
Z = -16222524
48 Z = -4925300
84
XDOT = 5088
553765 XDOT = 1482
344016
YDOT = 23404
571382 feet/sec YDOT = 7150
673954 meter/sec
ZDOT = -7591
419535 ZDOT = -2306
496886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1000471
88 X = 304943
83
Y = -15338345
54 feet Y = -4675127
72 meter
Z = -16134338
14 Z = -4917746
26
XDOT = 20929
899877 XDOT = 6379
433482
YDOT = 9309
728373 feet/sec YDOT = 2837
605208 meter/sec
ZDOT = -7558
488314 ZDOT = -2303
827238
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 19222
28960440
00016717 00000-0 10270-3 0 9095
2 25544 51
6414 92
8517 0005986 243
0463 117
0077 15
51050264 23642
Satellite: ISS
Catalog Number: 25544
Epoch time: 19222
28960440 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 92
8517 deg
Eccentricity:
0005986
Arg of perigee: 243
0463 deg
Mean anomaly: 117
0077 deg
Mean motion: 15
51050264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2364
Checksum: 301
Coasting Arc #11 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2019/223/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3939001
50 A = 6787052
38 meter
Y = 1976923
13 meter E =
0005415
Z = 5164046
41 I = 52
00961
XDOT = -1601
523970 Wp = 197
96220
YDOT = -7324
002690 meter/sec RA = 87
12502 deg
ZDOT = 1577
637587 TA = 236
86536
MA = 236
91733
Ha = 224
505 n
mi
Hp = 221
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12923233
26 X = -3985898
95
Y = 6485968
26 feet Y = 1932611
86 meter
Z = 16942409
47 Z = 5144798
74
XDOT = -5254
343733 XDOT = -1527
169006
YDOT = -24028
880217 feet/sec YDOT = -7341
496423 meter/sec
ZDOT = 5175
976335 ZDOT = 1570
038181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2026046
86 X = -617539
08
Y = 14420138
34 feet Y = 4395258
17 meter
Z = 16854605
46 Z = 5137283
75
XDOT = -21754
511553 XDOT = -6630
775121
YDOT = -9084
262309 feet/sec YDOT = -2768
883152 meter/sec
ZDOT = 5142
020395 ZDOT = 1567
287816
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 19223
32047931
00016717 00000-0 10270-3 0 9104
2 25544 51
6414 87
7380 0006127 247
5453 112
5049 15
51081826 23804
Satellite: ISS
Catalog Number: 25544
Epoch time: 19223
32047931 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 87
7380 deg
Eccentricity:
0006127
Arg of perigee: 247
5453 deg
Mean anomaly: 112
5049 deg
Mean motion: 15
51081826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 292
Coasting Arc #12 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2019/224/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3982293
38 A = 6786529
49 meter
Y = -1460825
28 meter E =
0008717
Z = -5305026
69 I = 52
00511
XDOT = 1655
536699 Wp = 92
76773
YDOT = 7432
621670 meter/sec RA = 82
18267 deg
ZDOT = -805
489403 TA = 169
57043
MA = 169
55234
Ha = 224
369 n
mi
Hp = 221
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13065267
00 X = 4024101
17
Y = -4792733
86 feet Y = -1416058
37 meter
Z = -17404943
20 Z = -5285581
11
XDOT = 5431
550851 XDOT = 1576
212490
YDOT = 24385
241701 feet/sec YDOT = 7450
691569 meter/sec
ZDOT = -2642
681769 ZDOT = -797
639748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3270232
52 X = 996766
87
Y = -13640223
84 feet Y = -4157540
23 meter
Z = -17316276
17 Z = -5278000
98
XDOT = 22352
541427 XDOT = 6813
054627
YDOT = 8662
882053 feet/sec YDOT = 2640
446450 meter/sec
ZDOT = -2607
607810 ZDOT = -794
798861
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 19224
28692507
00016717 00000-0 10270-3 0 9116
2 25544 51
6418 82
9422 0006068 250
9964 109
0530 15
51053602 23954
Satellite: ISS
Catalog Number: 25544
Epoch time: 19224
28692507 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 82
9422 deg
Eccentricity:
0006068
Arg of perigee: 250
9964 deg
Mean anomaly: 109
0530 deg
Mean motion: 15
51053602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 304
Coasting Arc #13 (Orbit 2410)
---------------------------------------
Vector Time (GMT): 2019/225/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4070064
62 A = 6786232
15 meter
Y = 950738
69 meter E =
0003866
Z = 5349429
16 I = 51
99931
XDOT = -1710
516050 Wp = 246
72078
YDOT = -7467
826113 meter/sec RA = 77
24105 deg
ZDOT = 24
332950 TA = 203
03961
MA = 203
05695
Ha = 224
113 n
mi
Hp = 221
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13353230
37 X = -4106377
55
Y = 3119221
42 feet Y = 905021
04 meter
Z = 17550620
60 Z = 5329570
59
XDOT = -5611
929298 XDOT = -1626
999734
YDOT = -24500
741842 feet/sec YDOT = -7486
487339 meter/sec
ZDOT = 79
832513 ZDOT = 16
226522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4602007
82 X = -1402691
98
Y = 13039498
91 feet Y = 3974439
27 meter
Z = 17460113
96 Z = 5321842
73
XDOT = -22731
176214 XDOT = -6928
462510
YDOT = -8087
358641 feet/sec YDOT = -2465
026914 meter/sec
ZDOT = 43
602785 ZDOT = 13
290129
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 19225
31779532
00016717 00000-0 10270-3 0 9126
2 25544 51
6423 77
8281 0006151 256
1285 103
9182 15
51082947 24112
Satellite: ISS
Catalog Number: 25544
Epoch time: 19225
31779532 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 77
8281 deg
Eccentricity:
0006151
Arg of perigee: 256
1285 deg
Mean anomaly: 103
9182 deg
Mean motion: 15
51082947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2411
Checksum: 302
Coasting Arc #14 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2019/226/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213882
92 A = 6786505
01 meter
Y = -443231
75 meter E =
0008943
Z = -5308927
77 I = 51
99109
XDOT = 1742
222200 Wp = 106
55381
YDOT = 7417
171573 meter/sec RA = 72
29719 deg
ZDOT = 762
203130 TA = 170
71241
MA = 170
69586
Ha = 223
895 n
mi
Hp = 221
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13825075
21 X = 4244313
31
Y = -1454172
41 feet Y = -395938
81 meter
Z = -17417742
04 Z = -5288384
89
XDOT = 5715
952101 XDOT = 1655
449495
YDOT = 24334
552406 feet/sec YDOT = 7436
169123 meter/sec
ZDOT = 2500
666438 ZDOT = 770
455516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6042835
42 X = 1841856
24
Y = -12648421
49 feet Y = -3855238
87 meter
Z = -17324163
29 Z = -5280404
97
XDOT = 22804
774114 XDOT = 6950
895150
YDOT = 7413
066172 feet/sec YDOT = 2259
502569 meter/sec
ZDOT = 2537
556391 ZDOT = 773
447188
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 19226
28423585
00016717 00000-0 10270-3 0 9138
2 25544 51
6419 73
0320 0005990 259
9045 100
1431 15
51058627 24264
Satellite: ISS
Catalog Number: 25544
Epoch time: 19226
28423585 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 73
0320 deg
Eccentricity:
0005990
Arg of perigee: 259
9045 deg
Mean anomaly: 100
1431 deg
Mean motion: 15
51058627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 296
Coasting Arc #15 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2019/227/05:47:34
629
Vector Time (MET): N/A
Weight (LBS) : 937115
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4647146
89 A = 6791863
02 meter
Y = 2589535
88 meter E =
0002854
Z = -4224197
74 I = 51
99392
XDOT = -359
316606 Wp = 180
15597
YDOT = 6693
884121 meter/sec RA = 67
48071 deg
ZDOT = 3705
439238 TA = 127
73385
MA = 127
70798
Ha = 223
689 n
mi
Hp = 222
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15246544
93 X = 4638362
90
Y = 8495852
63 feet Y = 2641454
51 meter
Z = -13858916
47 Z = -4201645
46
XDOT = -1178
860257 XDOT = -452
141381
YDOT = 21961
562076 feet/sec YDOT = 6689
346909 meter/sec
ZDOT = 12156
952882 ZDOT = 3703
468522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16437156
36 X = 5010045
26
Y = -6106193
25 feet Y = -1861167
70 meter
Z = -13756471
37 Z = -4192972
47
XDOT = 15398
204135 XDOT = 4693
372620
YDOT = 14063
019797 feet/sec YDOT = 4286
408434 meter/sec
ZDOT = 12147
353301 ZDOT = 3702
513286
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 19227
25067459
00016717 00000-0 10270-3 0 9141
2 25544 51
6411 68
2370 0007402 268
3606 91
6697 15
50710502 24415
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
25067459 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 68
2370 deg
Eccentricity:
0007402
Arg of perigee: 268
3606 deg
Mean anomaly: 91
6697 deg
Mean motion: 15
50710502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 300
Coasting Arc #16 (Orbit 2442)
---------------------------------------
Vector Time (GMT): 2019/227/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4598658
26 A = 6790271
47 meter
Y = 1030676
00 meter E =
0004193
Z = -4891828
96 I = 51
98603
XDOT = 992
985152 Wp = 147
67027
YDOT = 7189
763086 meter/sec RA = 66
86390 deg
ZDOT = 2445
832142 TA = 146
25457
MA = 146
22787
Ha = 224
019 n
mi
Hp = 223
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15087461
48 X = 4610552
39
Y = 3381482
93 feet Y = 1082168
01 meter
Z = -16049307
62 Z = -4869462
03
XDOT = 3257
825303 XDOT = 900
633137
YDOT = 23588
461569 feet/sec YDOT = 7200
350936 meter/sec
ZDOT = 8024
383667 ZDOT = 2450
431384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2048370
92 X = 624343
46
Y = -15431321
24 feet Y = -4703466
71 meter
Z = -15947560
86 Z = -4860816
55
XDOT = 22096
448652 XDOT = 6734
997549
YDOT = -5389
126512 feet/sec YDOT = -1642
605761 meter/sec
ZDOT = 8044
651731 ZDOT = 2452
009847
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 19227
37956152
00016717 00000-0 10270-3 0 9152
2 25544 51
6433 67
5990 0008949 269
9492 90
0634 15
50382566 24437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
37956152 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 67
5990 deg
Eccentricity:
0008949
Arg of perigee: 269
9492 deg
Mean anomaly: 90
0634 deg
Mean motion: 15
50382566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 343
Coasting Arc #17 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2019/228/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4778065
69 A = 6790999
26 meter
Y = -1176264
08 meter E =
0004478
Z = 4683559
69 I = 51
97527
XDOT = -1141
995255 Wp = 339
07225
YDOT = -6988
710172 meter/sec RA = 61
92838 deg
ZDOT = -2917
027757 TA = 139
85890
MA = 139
82581
Ha = 224
894 n
mi
Hp = 224
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15676068
54 X = -4787306
88
Y = -3859134
11 feet Y = -1229747
42 meter
Z = 15366009
48 Z = 4660327
72
XDOT = -3746
703593 XDOT = -1049
591626
YDOT = -22928
839146 feet/sec YDOT = -7000
964116 meter/sec
ZDOT = -9570
301041 ZDOT = -2922
350566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2197033
28 X = -669655
74
Y = 16094760
88 feet Y = 4905683
12 meter
Z = 15260340
93 Z = 4651351
91
XDOT = -21248
813627 XDOT = -6476
638393
YDOT = 6205
942318 feet/sec YDOT = 1891
571219 meter/sec
ZDOT = -9593
874602 ZDOT = -2924
212979
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 19228
41088653
00016717 00000-0 10270-3 0 9161
2 25544 51
6439 62
4871 0009063 274
4342 85
5773 15
50422030 24599
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
41088653 = yrday
fracday
Element set: 916
Inclination: 51
6439 deg
RA of node: 62
4871 deg
Eccentricity:
0009063
Arg of perigee: 274
4342 deg
Mean anomaly: 85
5773 deg
Mean motion: 15
50422030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2459
Checksum: 314
Coasting Arc #18 (Orbit 2473)
---------------------------------------
Vector Time (GMT): 2019/229/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4977827
28 A = 6792029
93 meter
Y = 1288678
41 meter E =
0001953
Z = -4438226
81 I = 51
96155
XDOT = 1253
053076 Wp = 195
68062
YDOT = 6765
252310 meter/sec RA = 56
99137 deg
ZDOT = 3367
575805 TA = 108
25969
MA = 108
23844
Ha = 225
304 n
mi
Hp = 224
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16331454
34 X = 4984604
97
Y = 4227947
53 feet Y = 1344381
79 meter
Z = -14561111
57 Z = -4414030
43
XDOT = 4111
066521 XDOT = 1160
951457
YDOT = 22195
709678 feet/sec YDOT = 6778
749925 meter/sec
ZDOT = 11048
477051 ZDOT = 3373
438721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2207340
74 X = 672797
46
Y = -16819993
74 feet Y = -5126734
09 meter
Z = -14451068
09 Z = -4404685
55
XDOT = 20318
069873 XDOT = 6192
947697
YDOT = -6854
560379 feet/sec YDOT = -2089
270004 meter/sec
ZDOT = 11074
522712 ZDOT = 3375
514523
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 19229
37775307
00016717 00000-0 10270-3 0 9177
2 25544 51
6437 57
6937 0009037 278
1068 81
9057 15
50390000 24746
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
37775307 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 57
6937 deg
Eccentricity:
0009037
Arg of perigee: 278
1068 deg
Mean anomaly: 81
9057 deg
Mean motion: 15
50390000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2474
Checksum: 327
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