[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 6th 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 6 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
311/22:43:23
807 1
0 1
5 1
5
N/A 0
7 -0
0 225
8
000/00:06:43
614 0
8 -0
0 223
7
312/03:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
9
000/00:00:00
000 0
0 0
0 223
6
317/14:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
3
000/00:00:00
000 0
0 0
0 223
6
Coasting Arc #1 (Orbit 3732)
---------------------------------------
Vector Time (GMT): 2019/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6417669
54 A = 6798565
36 meter
Y = 87241
45 meter E =
0011385
Z = 2219845
18 I = 51
75953
XDOT = -1964
276837 Wp = 135
13262
YDOT = -4994
005168 meter/sec RA = 15
03806 deg
ZDOT = -5473
300744 TA = 20
27455
MA = 20
22938
Ha = 226
370 n
mi
Hp = 222
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21055346
27 X = -6428951
04
Y = 286225
24 feet Y = 15411
48 meter
Z = 7282956
63 Z = 2188642
74
XDOT = -6444
477811 XDOT = -1881
699826
YDOT = -16384
531392 feet/sec YDOT = -5015
509432 meter/sec
ZDOT = -17957
023437 ZDOT = -5482
641977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14845416
31 X = 4524882
89
Y = -15002529
15 feet Y = -4572770
89 meter
Z = 7140638
77 Z = 2176466
70
XDOT = 14903
752418 XDOT = 4542
663737
YDOT = 6166
047896 feet/sec YDOT = 1879
411399 meter/sec
ZDOT = -17999
128320 ZDOT = -5486
134312
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 19310
53656490
00016717 00000-0 10270-3 0 9009
2 25544 51
6434 15
4762 0006228 235
3385 124
7179 15
50271819 37333
Satellite: ISS
Catalog Number: 25544
Epoch time: 19310
53656490 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 15
4762 deg
Eccentricity:
0006228
Arg of perigee: 235
3385 deg
Mean anomaly: 124
7179 deg
Mean motion: 15
50271819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3733
Checksum: 306
Coasting Arc #2 (Orbit 3747)
---------------------------------------
Vector Time (GMT): 2019/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6540190
44 A = 6799318
37 meter
Y = -300633
82 meter E =
0002797
Z = -1827686
45 I = 51
72917
XDOT = 1801
408434 Wp = 342
93072
YDOT = 4847
433717 meter/sec RA = 10
09105 deg
ZDOT = 5649
220113 TA = 357
04114
MA = 357
04279
Ha = 226
108 n
mi
Hp = 222
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21457317
72 X = 6551944
16
Y = -986331
42 feet Y = -227431
10 meter
Z = -5996346
62 Z = -1795887
60
XDOT = 5910
132656 XDOT = 1719
627928
YDOT = 15903
653928 feet/sec YDOT = 4867
121176 meter/sec
ZDOT = 18534
186723 ZDOT = 5657
772099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14361392
04 X = -4377352
29
Y = 16026796
87 feet Y = 4884967
69 meter
Z = -5851299
60 Z = -1783476
12
XDOT = -14231
173925 XDOT = -4337
661812
YDOT = -5972
067397 feet/sec YDOT = -1820
286143 meter/sec
ZDOT = 18572
702073 ZDOT = 5660
959592
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 19311
50350625
00016717 00000-0 10270-3 0 9019
2 25544 51
6434 10
6841 0006241 240
0806 119
9726 15
50237390 37480
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
50350625 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 10
6841 deg
Eccentricity:
0006241
Arg of perigee: 240
0806 deg
Mean anomaly: 119
9726 deg
Mean motion: 15
50237390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3748
Checksum: 283
Coasting Arc #3 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/311/22:46:45
614
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6028796
20 A = 6798129
65 meter
Y = -1404666
02 meter E =
0002214
Z = -2807147
43 I = 51
70978
XDOT = 3440
933972 Wp = 285
46220
YDOT = 4548
561809 meter/sec RA = 7
86246 deg
ZDOT = 5111
114168 TA = 42
78947
MA = 42
77224
Ha = 225
845 n
mi
Hp = 223
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19779515
10 X = 6057691
31
Y = -4608484
31 feet Y = -1337086
25 meter
Z = -9209801
28 Z = -2777791
08
XDOT = 11289
153451 XDOT = 3364
987510
YDOT = 14923
103049 feet/sec YDOT = 4586
616224 meter/sec
ZDOT = 16768
747269 ZDOT = 5127
644668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15438353
90 X = 4705610
27
Y = -13288155
93 feet Y = -4050229
93 meter
Z = -9075787
89 Z = -2766300
15
XDOT = 15855
096865 XDOT = 4832
633524
YDOT = 6910
117136 feet/sec YDOT = 2106
203703 meter/sec
ZDOT = 16843
674553 ZDOT = 5133
952004
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 19311
95474502
00016717 00000-0 10270-3 0 9020
2 25544 51
6452 8
4495 0006481 253
1292 106
9148 15
49999498 37554
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
95474502 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 8
4495 deg
Eccentricity:
0006481
Arg of perigee: 253
1292 deg
Mean anomaly: 106
9148 deg
Mean motion: 15
49999498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 338
Coasting Arc #4 (Orbit 3757)
---------------------------------------
Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1867498
85 A = 6790820
59 meter
Y = -4209122
76 meter E =
0006173
Z = -4996755
79 I = 51
67536
XDOT = 7325
098313 Wp = 76
09440
YDOT = -766
082240 meter/sec RA = 7
01130 deg
ZDOT = -2093
099563 TA = 173
51659
MA = 173
50860
Ha = 225
852 n
mi
Hp = 223
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6126964
72 X = -1796020
52
Y = -13809457
87 feet Y = -4229606
89 meter
Z = -16393555
74 Z = -5005653
86
XDOT = 24032
474779 XDOT = 7343
287745
YDOT = -2513
393176 feet/sec YDOT = -684
066157 meter/sec
ZDOT = -6867
124550 ZDOT = -2057
472150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13548884
36 X = -4129699
95
Y = 6584100
93 feet Y = 2006833
96 meter
Z = -16433710
49 Z = -5008994
96
XDOT = -3030
748727 XDOT = -923
772212
YDOT = -22965
220700 feet/sec YDOT = -6999
799269 meter/sec
ZDOT = -6704
580094 ZDOT = -2043
556013
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 19312
14816645
00016717 00000-0 10270-3 0 9031
2 25544 51
6410 7
4887 0006507 253
3699 106
6737 15
49986728 37580
Satellite: ISS
Catalog Number: 25544
Epoch time: 19312
14816645 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 7
4887 deg
Eccentricity:
0006507
Arg of perigee: 253
3699 deg
Mean anomaly: 106
6737 deg
Mean motion: 15
49986728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3758
Checksum: 345
Coasting Arc #5 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1818002
05 A = 6790502
57 meter
Y = 4103368
58 meter E =
0004821
Z = 5098800
58 I = 51
64008
XDOT = -7377
287163 Wp = 204
96111
YDOT = 1108
656762 meter/sec RA = 2
05740 deg
ZDOT = 1734
522381 TA = 228
23147
MA = 228
27268
Ha = 225
653 n
mi
Hp = 223
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5964573
64 X = 1747214
19
Y = 13462495
33 feet Y = 4123303
06 meter
Z = 16728348
38 Z = 5107459
93
XDOT = -24203
698042 XDOT = -7397
561715
YDOT = 3637
325334 feet/sec YDOT = 1026
045398 meter/sec
ZDOT = 5690
690227 ZDOT = 1698
636249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13096942
09 X = 3991947
95
Y = -6631461
94 feet Y = -2021269
60 meter
Z = 16767420
17 Z = 5110709
67
XDOT = 4570
308831 XDOT = 1393
030132
YDOT = 23031
289934 feet/sec YDOT = 7019
937172 meter/sec
ZDOT = 5526
946664 ZDOT = 1684
613343
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 19313
17975342
00016717 00000-0 10270-3 0 9046
2 25544 51
6405 2
3784 0006448 257
5006 102
5423 15
49944748 37747
Satellite: ISS
Catalog Number: 25544
Epoch time: 19313
17975342 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 2
3784 deg
Eccentricity:
0006448
Arg of perigee: 257
5006 deg
Mean anomaly: 102
5423 deg
Mean motion: 15
49944748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 317
Coasting Arc #6 (Orbit 3788)
---------------------------------------
Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1748569
71 A = 6789994
74 meter
Y = -4026841
61 meter E =
0007529
Z = -5186561
95 I = 51
60468
XDOT = 7391
970292 Wp = 79
93864
YDOT = -1455
448791 meter/sec RA = 357
10082 deg
ZDOT = -1362
483754 TA = 176
93935
MA = 176
93475
Ha = 225
507 n
mi
Hp = 223
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5736777
28 X = -1678216
37
Y = -13211422
60 feet Y = -4046002
04 meter
Z = -17016279
37 Z = -5194885
14
XDOT = 24251
871038 XDOT = 7414
314509
YDOT = -4775
094460 feet/sec YDOT = -1372
661639 meter/sec
ZDOT = -4470
091057 ZDOT = -1326
521146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12748027
72 X = -3885598
85
Y = 6607650
13 feet Y = 2014011
76 meter
Z = -17053821
08 Z = -5198004
66
XDOT = -6121
342000 XDOT = -1865
785042
YDOT = -22919
781925 feet/sec YDOT = -6985
949531 meter/sec
ZDOT = -4305
978618 ZDOT = -1312
462283
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 19314
14686260
00016717 00000-0 10270-3 0 9053
2 25544 51
6398 357
5875 0006419 259
5209 100
5218 15
49991847 37897
Satellite: ISS
Catalog Number: 25544
Epoch time: 19314
14686260 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 357
5875 deg
Eccentricity:
0006419
Arg of perigee: 259
5209 deg
Mean anomaly: 100
5218 deg
Mean motion: 15
49991847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3789
Checksum: 354
Coasting Arc #7 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1678595
86 A = 6789834
35 meter
Y = 3971823
48 meter E =
0004214
Z = 5248177
23 I = 51
57062
XDOT = -7376
395695 Wp = 233
36440
YDOT = 1809
469236 meter/sec RA = 352
14123 deg
ZDOT = 987
978795 TA = 207
14680
MA = 207
16884
Ha = 225
288 n
mi
Hp = 223
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5507204
25 X = 1608563
57
Y = 13030916
93 feet Y = 3990203
12 meter
Z = 17218429
24 Z = 5256161
37
XDOT = -24200
773278 XDOT = -7400
880659
YDOT = 5936
578857 feet/sec YDOT = 1726
844260 meter/sec
ZDOT = 3241
400247 ZDOT = 952
086568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12474245
67 X = 3802150
08
Y = -6579238
67 feet Y = -2005351
95 meter
Z = 17254425
92 Z = 5259149
02
XDOT = 7683
534597 XDOT = 2341
941345
YDOT = 22655
508716 feet/sec YDOT = 6905
399057 meter/sec
ZDOT = 3077
586374 ZDOT = 938
048327
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 19315
17844541
00016717 00000-0 10270-3 0 9066
2 25544 51
6400 352
4765 0006426 264
1473 95
8945 15
49950964 38053
Satellite: ISS
Catalog Number: 25544
Epoch time: 19315
17844541 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 352
4765 deg
Eccentricity:
0006426
Arg of perigee: 264
1473 deg
Mean anomaly: 95
8945 deg
Mean motion: 15
49950964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 333
Coasting Arc #8 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1601198
68 A = 6789487
21 meter
Y = -3948193
21 meter E =
0008407
Z = -5293638
58 I = 51
53771
XDOT = 7320
259712 Wp = 84
36809
YDOT = -2158
303746 meter/sec RA = 347
17970 deg
ZDOT = -604
481900 TA = 179
84459
MA = 179
84433
Ha = 225
224 n
mi
Hp = 223
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5253276
51 X = -1531215
51
Y = -12953389
81 feet Y = -3965707
51 meter
Z = -17367580
63 Z = -5301246
95
XDOT = 24016
600104 XDOT = 7346
786755
YDOT = -7081
049036 feet/sec YDOT = -2076
295095 meter/sec
ZDOT = -1983
208334 ZDOT = -568
857397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12310252
38 X = -3752164
92
Y = 6530922
39 feet Y = 1990625
14 meter
Z = -17401862
49 Z = -5304087
69
XDOT = -9207
427928 XDOT = -2806
424032
YDOT = -22206
075794 feet/sec YDOT = -6768
411902 meter/sec
ZDOT = -1820
590990 ZDOT = -554
916134
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 19316
14554916
00016717 00000-0 10270-3 0 9079
2 25544 51
6407 347
6856 0006277 266
9013 93
1419 15
50005374 38203
Satellite: ISS
Catalog Number: 25544
Epoch time: 19316
14554916 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 347
6856 deg
Eccentricity:
0006277
Arg of perigee: 266
9013 deg
Mean anomaly: 93
1419 deg
Mean motion: 15
50005374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 316
Coasting Arc #9 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2019/317/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1526925
65 A = 6789535
84 meter
Y = 3947271
50 meter E =
0003795
Z = 5312278
50 I = 51
50367
XDOT = -7235
101029 Wp = 265
51467
YDOT = 2503
782339 meter/sec RA = 342
21505 deg
ZDOT = 219
026362 TA = 182
39048
MA = 182
39229
Ha = 225
230 n
mi
Hp = 223
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5009598
60 X = 1456867
77
Y = 12950365
81 feet Y = 3963954
68 meter
Z = 17428735
25 Z = 5319525
98
XDOT = -23737
208101 XDOT = -7263
625259
YDOT = 8214
508985 feet/sec YDOT = 2422
714831 meter/sec
ZDOT = 718
590427 ZDOT = 183
810751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12224141
40 X = 3725918
30
Y = -6499217
38 feet Y = -1980961
46 meter
Z = 17461368
95 Z = 5322225
26
XDOT = 10693
285484 XDOT = 3259
313415
YDOT = 21612
639274 feet/sec YDOT = 6587
532451 meter/sec
ZDOT = 557
810858 ZDOT = 170
020750
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 19317
17712723
00016717 00000-0 10270-3 0 9086
2 25544 51
6393 342
5744 0006220 270
8834 89
1604 15
49956428 38361
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
17712723 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 342
5744 deg
Eccentricity:
0006220
Arg of perigee: 270
8834 deg
Mean anomaly: 89
1604 deg
Mean motion: 15
49956428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 331
Coasting Arc #10 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2093549
43 A = 6792829
37 meter
Y = -4612182
70 meter E =
0003813
Z = -4530073
28 I = 51
49955
XDOT = 6984
087360 Wp = 135
17851
YDOT = 86
402123 meter/sec RA = 339
76519 deg
ZDOT = 3138
661306 TA = 166
41044
MA = 166
40017
Ha = 225
326 n
mi
Hp = 223
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6868600
49 X = 2166973
82
Y = -15131833
00 feet Y = -4588360
34 meter
Z = -14862445
14 Z = -4519725
24
XDOT = 22913
672441 XDOT = 6967
355796
YDOT = 283
471533 feet/sec YDOT = 164
409381 meter/sec
ZDOT = 10297
445230 ZDOT = 3172
547737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15586008
43 X = 4750615
37
Y = 5885591
71 feet Y = 1793928
35 meter
Z = -14814805
76 Z = -4515552
80
XDOT = 1754
792164 XDOT = 534
860652
YDOT = 21670
350802 feet/sec YDOT = 6605
122925 meter/sec
ZDOT = 10451
898045 ZDOT = 3185
738524
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 19317
62843943
00016717 00000-0 10270-3 0 9096
2 25544 51
6397 340
3427 0006363 275
5946 84
4479 15
49976566 38434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62843943 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 340
3427 deg
Eccentricity:
0006363
Arg of perigee: 275
5946 deg
Mean anomaly: 84
4479 deg
Mean motion: 15
49976566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 364
Coasting Arc #11 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2019/318/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086665
58 A = 6793459
29 meter
Y = 4796559
10 meter E =
0004939
Z = 4334732
95 I = 51
47110
XDOT = -6829
684495 Wp = 35
35428
YDOT = 165
091666 meter/sec RA = 334
79965 deg
ZDOT = -3464
443203 TA = 89
99447
MA = 89
93787
Ha = 225
456 n
mi
Hp = 223
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6846015
70 X = -2161203
30
Y = 15736742
44 feet Y = 4772807
42 meter
Z = 14221564
81 Z = 4324415
78
XDOT = -22407
101362 XDOT = -6814
194211
YDOT = 541
639325 feet/sec YDOT = 88
804196 meter/sec
ZDOT = -11366
283476 ZDOT = -3497
582499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16285134
64 X = -4963709
04
Y = -5536841
07 feet Y = -1687629
16 meter
Z = 14174049
52 Z = 4320250
29
XDOT = -2898
347433 XDOT = -883
416298
YDOT = -21009
126391 feet/sec YDOT = -6403
581724 meter/sec
ZDOT = -11517
350967 ZDOT = -3510
488575
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 19318
66001332
00016717 00000-0 10270-3 0 9101
2 25544 51
6398 335
2319 0006477 279
4698 80
5720 15
50008757 38594
Satellite: ISS
Catalog Number: 25544
Epoch time: 19318
66001332 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 335
2319 deg
Eccentricity:
0006477
Arg of perigee: 279
4698 deg
Mean anomaly: 80
5720 deg
Mean motion: 15
50008757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 329
Coasting Arc #12 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2019/319/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2046173
04 A = 6794254
18 meter
Y = -4994679
77 meter E =
0001172
Z = -4127826
71 I = 51
44471
XDOT = 6654
126839 Wp = 137
00986
YDOT = -391
017341 meter/sec RA = 329
83240 deg
ZDOT = 3771
392500 TA = 172
02010
MA = 172
01824
Ha = 225
734 n
mi
Hp = 223
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6713166
13 X = 2121924
06
Y = -16386744
64 feet Y = -4971374
08 meter
Z = -13542738
56 Z = -4117703
41
XDOT = 21831
124801 XDOT = 6639
685013
YDOT = -1282
865292 feet/sec YDOT = -316
687293 meter/sec
ZDOT = 12373
334975 ZDOT = 3803
681379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17009966
83 X = 5184637
89
Y = 5051172
02 feet Y = 1539597
23 meter
Z = -13496090
42 Z = -4113608
36
XDOT = 3920
443702 XDOT = 1194
951240
YDOT = 20252
906587 feet/sec YDOT = 6173
085928 meter/sec
ZDOT = 12520
545906 ZDOT = 3816
262392
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 19319
62711147
00016717 00000-0 10270-3 0 9111
2 25544 51
6407 330
4406 0006426 283
9604 76
0832 15
49988351 38746
Satellite: ISS
Catalog Number: 25544
Epoch time: 19319
62711147 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 330
4406 deg
Eccentricity:
0006426
Arg of perigee: 283
9604 deg
Mean anomaly: 76
0832 deg
Mean motion: 15
49988351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 321
Coasting Arc #13 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2019/320/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1990500
20 A = 6794961
09 meter
Y = 5199558
40 meter E =
0006194
Z = 3894125
78 I = 51
41876
XDOT = -6463
684481 Wp = 52
65934
YDOT = 579
278873 meter/sec RA = 324
86382 deg
ZDOT = -4069
257805 TA = 80
18636
MA = 80
11644
Ha = 225
947 n
mi
Hp = 223
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6530512
47 X = -2067411
07
Y = 17058918
65 feet Y = 5176868
81 meter
Z = 12776003
21 Z = 3884270
20
XDOT = -21206
313914 XDOT = -6449
915202
YDOT = 1900
521238 feet/sec YDOT = 507
074776 meter/sec
ZDOT = -13350
583351 ZDOT = -4100
623030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17738584
44 X = -5406720
54
Y = -4489544
51 feet Y = -1368413
17 meter
Z = 12730560
42 Z = 3880274
82
XDOT = -4784
770790 XDOT = -1458
398137
YDOT = -19433
571199 feet/sec YDOT = -5923
352501 meter/sec
ZDOT = -13493
601141 ZDOT = -4112
849628
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 19320
65868072
00016717 00000-0 10270-3 0 9127
2 25544 51
6405 325
3301 0006499 288
5081 71
5363 15
50015968 38905
Satellite: ISS
Catalog Number: 25544
Epoch time: 19320
65868072 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 325
3301 deg
Eccentricity:
0006499
Arg of perigee: 288
5081 deg
Mean anomaly: 71
5363 deg
Mean motion: 15
50015968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 316
Coasting Arc #14 (Orbit 3904)
---------------------------------------
Vector Time (GMT): 2019/321/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1892296
58 A = 6795786
52 meter
Y = -5407480
01 meter E =
0001741
Z = -3653220
81 I = 51
39452
XDOT = 6265
075306 Wp = 336
97283
YDOT = -741
864310 meter/sec RA = 319
89391 deg
ZDOT = 4344
156139 TA = 339
55374
MA = 339
56071
Ha = 226
165 n
mi
Hp = 223
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6208322
12 X = 1970369
51
Y = -17741076
15 feet Y = -5385882
14 meter
Z = -11985632
59 Z = -3643839
50
XDOT = 20554
709009 XDOT = 6251
803637
YDOT = -2433
938025 feet/sec YDOT = -671
878425 meter/sec
ZDOT = 14252
480772 ZDOT = 4374
557632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18443210
58 X = 5621490
59
Y = 3764698
04 feet Y = 1147479
96 meter
Z = -11942339
26 Z = -3640025
01
XDOT = 5524
661690 XDOT = 1683
916883
YDOT = 18577
074291 feet/sec YDOT = 5662
292244 meter/sec
ZDOT = 14391
120028 ZDOT = 4386
413384
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 19321
62577609
00016717 00000-0 10270-3 0 9139
2 25544 51
6403 320
5393 0006541 291
9010 68
1436 15
49993057 39051
Satellite: ISS
Catalog Number: 25544
Epoch time: 19321
62577609 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 320
5393 deg
Eccentricity:
0006541
Arg of perigee: 291
9010 deg
Mean anomaly: 68
1436 deg
Mean motion: 15
49993057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 314
Coasting Arc #15 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2019/322/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1781080
67 A = 6796496
62 meter
Y = 5616264
11 meter E =
0007087
Z = 3385053
90 I = 51
37347
XDOT = -6058
456315 Wp = 67
31195
YDOT = 861
735013 meter/sec RA = 314
92265 deg
ZDOT = -4607
031731 TA = 73
07034
MA = 72
99267
Ha = 226
330 n
mi
Hp = 223
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5843440
52 X = -1860193
87
Y = 18426063
35 feet Y = 5595904
19 meter
Z = 11105819
87 Z = 3376210
28
XDOT = -19876
825182 XDOT = -6045
263588
YDOT = 2827
214609 feet/sec YDOT = 794
059202 meter/sec
ZDOT = -15114
933501 ZDOT = -4636
429624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19124003
17 X = -5828996
17
Y = -2973856
51 feet Y = -906431
46 meter
Z = 11064968
29 Z = 3372602
33
XDOT = -6090
753592 XDOT = -1856
461695
YDOT = -17697
539260 feet/sec YDOT = -5394
209966 meter/sec
ZDOT = -15249
007180 ZDOT = -4647
897388
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 19322
65734255
00016717 00000-0 10270-3 0 9146
2 25544 51
6415 315
4289 0006583 295
9403 64
1069 15
50022117 39215
Satellite: ISS
Catalog Number: 25544
Epoch time: 19322
65734255 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 315
4289 deg
Eccentricity:
0006583
Arg of perigee: 295
9403 deg
Mean anomaly: 64
1069 deg
Mean motion: 15
50022117 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 305
Coasting Arc #16 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2019/323/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1624898
32 A = 6797280
16 meter
Y = -5816443
23 meter E =
0004728
Z = -3112916
56 I = 51
35313
XDOT = 5856
050060 Wp = 342
44196
YDOT = -956
367600 meter/sec RA = 309
94988 deg
ZDOT = 4846
224703 TA = 341
63920
MA = 341
65626
Ha = 226
544 n
mi
Hp = 223
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5331031
23 X = 1704939
66
Y = -19082819
00 feet Y = -5797824
75 meter
Z = -10212980
83 Z = -3104829
27
XDOT = 19212
762664 XDOT = 5842
768738
YDOT = -3137
688975 feet/sec YDOT = -890
955651 meter/sec
ZDOT = 15899
687347 ZDOT = 4874
639132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19729542
56 X = 6013564
57
Y = 2020335
10 feet Y = 615798
14 meter
Z = -10175571
19 Z = -3101514
10
XDOT = 6538
831414 XDOT = 1993
035815
YDOT = 16836
586355 feet/sec YDOT = 5131
791521 meter/sec
ZDOT = 16029
283214 ZDOT = 4885
725523
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 19323
62443301
00016717 00000-0 10270-3 0 9154
2 25544 51
6415 310
6379 0006634 299
9153 60
1338 15
50005462 39360
Satellite: ISS
Catalog Number: 25544
Epoch time: 19323
62443301 = yrday
fracday
Element set: 915
Inclination: 51
6415 deg
RA of node: 310
6379 deg
Eccentricity:
0006634
Arg of perigee: 299
9153 deg
Mean anomaly: 60
1338 deg
Mean motion: 15
50005462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 298
Coasting Arc #17 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2019/324/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932146
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1458920
62 A = 6797971
58 meter
Y = 6011980
08 meter E =
0007848
Z = 2813066
47 I = 51
33487
XDOT = -5653
676771 Wp = 79
56296
YDOT = 1006
094677 meter/sec RA = 304
97642 deg
ZDOT = -5068
812779 TA = 68
42297
MA = 68
33935
Ha = 226
730 n
mi
Hp = 223
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4786484
97 X = -1539704
35
Y = 19724344
08 feet Y = 5995213
60 meter
Z = 9229220
70 Z = 2805783
52
XDOT = -18548
808304 XDOT = -5639
885307
YDOT = 3300
835555 feet/sec YDOT = 942
948568 meter/sec
ZDOT = -16629
963187 ZDOT = -5096
242954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20286598
60 X = -6183355
25
Y = -1017780
47 feet Y = -310219
49 meter
Z = 9195474
02 Z = 2802780
48
XDOT = -6812
358462 XDOT = -2076
406859
YDOT = -15995
645719 feet/sec YDOT = -4875
472815 meter/sec
ZDOT = -16755
072025 ZDOT = -5106
945953
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 19324
65599479
00016717 00000-0 10270-3 0 9167
2 25544 51
6413 305
5277 0006604 304
5998 55
4529 15
50025221 39527
Satellite: ISS
Catalog Number: 25544
Epoch time: 19324
65599479 = yrday
fracday
Element set: 916
Inclination: 51
6413 deg
RA of node: 305
5277 deg
Eccentricity:
0006604
Arg of perigee: 304
5998 deg
Mean anomaly: 55
4529 deg
Mean motion: 15
50025221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 328
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