[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 12th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 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
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 3809)
---------------------------------------
Vector Time (GMT): 2019/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6612352
48 A = 6801362
03 meter
Y = -1500575
73 meter E =
0008091
Z = -458931
19 I = 51
60004
XDOT = 1449
107127 Wp = 7
83322
YDOT = 4562
232768 meter/sec RA = 350
28927 deg
ZDOT = 5982
030275 TA = 347
22357
MA = 347
24406
Ha = 225
252 n
mi
Hp = 223
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21694069
81 X = 6630870
20
Y = -4923148
73 feet Y = -1426528
19 meter
Z = -1505679
74 Z = -426764
98
XDOT = 4754
288475 XDOT = 1368
924999
YDOT = 14967
955276 feet/sec YDOT = 4577
989306 meter/sec
ZDOT = 19626
083579 ZDOT = 5988
875000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10368487
97 X = -3160315
13
Y = 19692257
63 feet Y = 6002200
12 meter
Z = -1358887
97 Z = -414189
05
XDOT = -12942
925635 XDOT = -3945
003733
YDOT = -5463
433878 feet/sec YDOT = -1665
254646 meter/sec
ZDOT = 19656
824114 ZDOT = 5991
399990
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
50080136
00016717 00000-0 10270-3 0 9009
2 25544 51
6432 350
8820 0006364 267
3689 92
6733 15
49972798 38102
Satellite: ISS
Catalog Number: 25544
Epoch time: 19315
50080136 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 350
8820 deg
Eccentricity:
0006364
Arg of perigee: 267
3689 deg
Mean anomaly: 92
6733 deg
Mean motion: 15
49972798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3810
Checksum: 325
Coasting Arc #2 (Orbit 3825)
---------------------------------------
Vector Time (GMT): 2019/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6550473
00 A = 6801335
26 meter
Y = 1805324
81 meter E =
0008759
Z = 110873
67 I = 51
56773
XDOT = -1361
713601 Wp = 163
08418
YDOT = -4565
501582 meter/sec RA = 345
33357 deg
ZDOT = -6000
589812 TA = 15
72237
MA = 15
69519
Ha = 225
148 n
mi
Hp = 223
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21491053
14 X = -6570712
39
Y = 5922981
65 feet Y = 1731959
62 meter
Z = 363758
76 Z = 79003
88
XDOT = -4467
564307 XDOT = -1281
411230
YDOT = -14978
679732 feet/sec YDOT = -4580
280019 meter/sec
ZDOT = -19686
974450 ZDOT = -6007
009816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9123263
93 X = 2780770
85
Y = -20342020
52 feet Y = -6200247
85 meter
Z = 218296
87 Z = 66536
89
XDOT = 12825
792422 XDOT = 3909
301530
YDOT = 5534
174455 feet/sec YDOT = 1686
816374 meter/sec
ZDOT = -19715
774735 ZDOT = -6009
368139
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
53237707
00016717 00000-0 10270-3 0 9012
2 25544 51
6433 345
7717 0006330 270
5076 89
5349 15
50006661 38264
Satellite: ISS
Catalog Number: 25544
Epoch time: 19316
53237707 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 345
7717 deg
Eccentricity:
0006330
Arg of perigee: 270
5076 deg
Mean anomaly: 89
5349 deg
Mean motion: 15
50006661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 310
Coasting Arc #3 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2019/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6455442
81 A = 6801357
88 meter
Y = -2109381
59 meter E =
0009480
Z = 228121
92 I = 51
53481
XDOT = 1287
947667 Wp = 18
64040
YDOT = 4596
312902 meter/sec RA = 340
37552 deg
ZDOT = 5993
993133 TA = 343
81696
MA = 343
84721
Ha = 225
305 n
mi
Hp = 223
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21179274
31 X = 6477442
62
Y = -6920543
27 feet Y = -2037069
28 meter
Z = 748431
49 Z = 259534
27
XDOT = 4225
550089 XDOT = 1207
338299
YDOT = 15079
766739 feet/sec YDOT = 4610
264587 meter/sec
ZDOT = 19665
331801 ZDOT = 6000
054153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7793102
32 X = -2375337
59
Y = 20868347
36 feet Y = 6360672
27 meter
Z = 891831
87 Z = 271830
35
XDOT = -12820
140959 XDOT = -3907
578964
YDOT = -5636
239363 feet/sec YDOT = -1717
925758 meter/sec
ZDOT = 19692
490096 ZDOT = 6002
270981
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
56395313
00016717 00000-0 10270-3 0 9025
2 25544 51
6426 340
6614 0006282 275
4802 84
5631 15
49989463 38428
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
56395313 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 340
6614 deg
Eccentricity:
0006282
Arg of perigee: 275
4802 deg
Mean anomaly: 84
5631 deg
Mean motion: 15
49989463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 327
Coasting Arc #4 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2101465
26 A = 6792841
26 meter
Y = -4612075
60 meter E =
0003748
Z = -4526474
92 I = 51
49960
XDOT = 6981
075738 Wp = 134
88743
YDOT = 93
039020 meter/sec RA = 339
76470 deg
ZDOT = 3145
255771 TA = 166
77514
MA = 166
76531
Ha = 225
340 n
mi
Hp = 223
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6894571
07 X = 2174870
38
Y = -15131481
63 feet Y = -4588164
83 meter
Z = -14850639
49 Z = -4516088
47
XDOT = 22903
791792 XDOT = 6964
238149
YDOT = 305
246130 feet/sec YDOT = 171
012007 meter/sec
ZDOT = 10319
080615 ZDOT = 3179
127315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15587480
81 X = 4751064
15
Y = 5911442
48 feet Y = 1801807
67 meter
Z = -14802825
06 Z = -4511901
08
XDOT = 1734
249173 XDOT = 528
599148
YDOT = 21661
775648 feet/sec YDOT = 6602
509218 meter/sec
ZDOT = 10473
464894 ZDOT = 3192
312100
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
62842611
00016717 00000-0 10270-3 0 9031
2 25544 51
6397 340
3424 0006379 276
0674 83
9750 15
49977217 38432
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62842611 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 340
3424 deg
Eccentricity:
0006379
Arg of perigee: 276
0674 deg
Mean anomaly: 83
9750 deg
Mean motion: 15
49977217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 337
Coasting Arc #5 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2019/318/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2094614
11 A = 6793474
57 meter
Y = 4796780
99 meter E =
0004983
Z = 4330701
47 I = 51
47115
XDOT = -6826
566550 Wp = 35
15325
YDOT = 158
049381 meter/sec RA = 334
79917 deg
ZDOT = -3470
851217 TA = 90
27100
MA = 90
21389
Ha = 225
480 n
mi
Hp = 223
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6872093
52 X = -2169134
13
Y = 15737470
45 feet Y = 4772940
53 meter
Z = 14208338
16 Z = 4320345
73
XDOT = -22396
871884 XDOT = -6810
966622
YDOT = 518
534714 feet/sec YDOT = 81
797391 meter/sec
ZDOT = -11387
307141 ZDOT = -3503
975100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16288135
16 X = -4964623
60
Y = -5562665
44 feet Y = -1695500
43 meter
Z = 14160647
05 Z = 4316165
22
XDOT = -2876
305118 XDOT = -876
697800
YDOT = -21000
599959 feet/sec YDOT = -6400
982868 meter/sec
ZDOT = -11538
303664 ZDOT = -3516
874957
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
65999985
00016717 00000-0 10270-3 0 9043
2 25544 51
6399 335
2316 0006495 279
9380 80
1037 15
50008655 38599
Satellite: ISS
Catalog Number: 25544
Epoch time: 19318
65999985 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 335
2316 deg
Eccentricity:
0006495
Arg of perigee: 279
9380 deg
Mean anomaly: 80
1037 deg
Mean motion: 15
50008655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 356
Coasting Arc #6 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2019/319/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2053600
79 A = 6794271
87 meter
Y = -4995110
38 meter E =
0001105
Z = -4123574
47 I = 51
44476
XDOT = 6651
220114 Wp = 135
52300
YDOT = -383
926122 meter/sec RA = 329
83194 deg
ZDOT = 3777
320170 TA = 173
57951
MA = 173
57809
Ha = 225
763 n
mi
Hp = 223
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6737535
40 X = 2129335
42
Y = -16388157
42 feet Y = -4971721
73 meter
Z = -13528787
63 Z = -4113415
13
XDOT = 21821
588302 XDOT = 6636
670414
YDOT = -1259
600137 feet/sec YDOT = -309
629183 meter/sec
ZDOT = 12392
782709 ZDOT = 3809
594667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17013912
68 X = 5185840
58
Y = 5075165
26 feet Y = 1546910
37 meter
Z = -13481975
17 Z = -4109306
03
XDOT = 3898
042599 XDOT = 1188
123384
YDOT = 20245
440527 feet/sec YDOT = 6170
810273 meter/sec
ZDOT = 12539
927370 ZDOT = 3822
169862
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
62709836
00016717 00000-0 10270-3 0 9056
2 25544 51
6408 330
4404 0006446 284
4317 75
6118 15
49987373 38749
Satellite: ISS
Catalog Number: 25544
Epoch time: 19319
62709836 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 330
4404 deg
Eccentricity:
0006446
Arg of perigee: 284
4317 deg
Mean anomaly: 75
6118 deg
Mean motion: 15
49987373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 339
Coasting Arc #7 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2019/320/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1997326
91 A = 6794980
58 meter
Y = 5200207
61 meter E =
0006228
Z = 3889827
98 I = 51
41882
XDOT = -6460
975749 Wp = 52
41229
YDOT = 572
342677 meter/sec RA = 324
86337 deg
ZDOT = -4074
476880 TA = 80
50194
MA = 80
43155
Ha = 225
977 n
mi
Hp = 223
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6552909
82 X = -2074223
66
Y = 17061048
58 feet Y = 5177441
75 meter
Z = 12761902
83 Z = 3879939
28
XDOT = -21197
426998 XDOT = -6447
103757
YDOT = 1877
764687 feet/sec YDOT = 500
169445 meter/sec
ZDOT = -13367
706298 ZDOT = -4105
828697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17743413
93 X = -5408192
57
Y = -4511420
78 feet Y = -1375081
05 meter
Z = 12716308
99 Z = 3875930
98
XDOT = -4762
681397 XDOT = -1451
665290
YDOT = -19427
055530 feet/sec YDOT = -5921
366526 meter/sec
ZDOT = -13510
662282 ZDOT = -4118
049864
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
65866855
00016717 00000-0 10270-3 0 9067
2 25544 51
6405 325
3298 0006521 288
9754 71
0690 15
50014194 38905
Satellite: ISS
Catalog Number: 25544
Epoch time: 19320
65866855 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 325
3298 deg
Eccentricity:
0006521
Arg of perigee: 288
9754 deg
Mean anomaly: 71
0690 deg
Mean motion: 15
50014194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 326
Coasting Arc #8 (Orbit 3904)
---------------------------------------
Vector Time (GMT): 2019/321/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1898045
42 A = 6795806
63 meter
Y = -5408157
90 meter E =
0001813
Z = -3649192
17 I = 51
39456
XDOT = 6262
860660 Wp = 337
52274
YDOT = -735
536805 meter/sec RA = 319
89349 deg
ZDOT = 4348
486715 TA = 339
06356
MA = 339
07098
Ha = 226
197 n
mi
Hp = 223
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6227183
14 X = 1976105
93
Y = -17743300
18 feet Y = -5386495
81 meter
Z = -11972415
25 Z = -3639782
96
XDOT = 20547
443111 XDOT = 6249
497364
YDOT = -2413
178493 feet/sec YDOT = -665
576198 meter/sec
ZDOT = 14266
688697 ZDOT = 4378
877227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18448018
72 X = 5622956
10
Y = 3782978
83 feet Y = 1153051
95 meter
Z = -11928994
71 Z = -3635957
59
XDOT = 5504
413256 XDOT = 1677
745160
YDOT = 18572
315949 feet/sec YDOT = 5660
841901 meter/sec
ZDOT = 14405
277281 ZDOT = 4390
728515
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
62576530
00016717 00000-0 10270-3 0 9074
2 25544 51
6404 320
5390 0006564 292
3692 67
6753 15
49990430 39053
Satellite: ISS
Catalog Number: 25544
Epoch time: 19321
62576530 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 320
5390 deg
Eccentricity:
0006564
Arg of perigee: 292
3692 deg
Mean anomaly: 67
6753 deg
Mean motion: 15
49990430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 321
Coasting Arc #9 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2019/322/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1785722
72 A = 6796516
87 meter
Y = 5616969
84 meter E =
0007113
Z = 3381523
50 I = 51
37351
XDOT = -6056
682513 Wp = 67
00502
YDOT = 856
298673 meter/sec RA = 314
92225 deg
ZDOT = -4610
313272 TA = 73
42706
MA = 73
34895
Ha = 226
362 n
mi
Hp = 223
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5858670
34 X = -1864826
31
Y = 18428378
73 feet Y = 5596558
06 meter
Z = 11094237
20 Z = 3372657
35
XDOT = -19871
005620 XDOT = -6043
413187
YDOT = 2809
378848 feet/sec YDOT = 788
643127 meter/sec
ZDOT = -15125
699710 ZDOT = -4639
702363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19128651
11 X = -5830412
86
Y = -2988461
79 feet Y = -910883
15 meter
Z = 11053282
88 Z = 3369040
62
XDOT = -6073
281810 XDOT = -1851
136296
YDOT = -17694
160309 feet/sec YDOT = -5393
180062 meter/sec
ZDOT = -15259
732742 ZDOT = -4651
166540
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
65733379
00016717 00000-0 10270-3 0 9085
2 25544 51
6416 315
4287 0006606 296
4091 63
6381 15
50018677 39216
Satellite: ISS
Catalog Number: 25544
Epoch time: 19322
65733379 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 315
4287 deg
Eccentricity:
0006606
Arg of perigee: 296
4091 deg
Mean anomaly: 63
6381 deg
Mean motion: 15
50018677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 325
Coasting Arc #10 (Orbit 3935)
---------------------------------------
Vector Time (GMT): 2019/323/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1628035
42 A = 6797299
58 meter
Y = -5816954
78 meter E =
0004794
Z = -3110279
16 I = 51
35316
XDOT = 5854
936710 Wp = 342
71585
YDOT = -952
371176 meter/sec RA = 309
94951 deg
ZDOT = 4848
407451 TA = 341
40036
MA = 341
41788
Ha = 226
577 n
mi
Hp = 223
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5341323
56 X = 1708069
44
Y = -19084497
31 feet Y = -5798301
26 meter
Z = -10204327
96 Z = -3102176
65
XDOT = 19209
109941 XDOT = 5841
600179
YDOT = -3124
577348 feet/sec YDOT = -886
971986 meter/sec
ZDOT = 15906
848593 ZDOT = 4876
816338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19732963
82 X = 6014607
37
Y = 2030124
76 feet Y = 618782
03 meter
Z = -10166848
91 Z = -3098855
55
XDOT = 6525
990886 XDOT = 1989
122022
YDOT = 16834
957789 feet/sec YDOT = 5131
295134 meter/sec
ZDOT = 16036
418821 ZDOT = 4887
900457
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
62442667
00016717 00000-0 10270-3 0 9091
2 25544 51
6416 310
6377 0006659 300
3842 59
6650 15
50001189 39360
Satellite: ISS
Catalog Number: 25544
Epoch time: 19323
62442667 = yrday
fracday
Element set: 909
Inclination: 51
6416 deg
RA of node: 310
6377 deg
Eccentricity:
0006659
Arg of perigee: 300
3842 deg
Mean anomaly: 59
6650 deg
Mean motion: 15
50001189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 315
Coasting Arc #11 (Orbit 3951)
---------------------------------------
Vector Time (GMT): 2019/324/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1460561
73 A = 6797990
21 meter
Y = 6012325
48 meter E =
0007867
Z = 2811593
38 I = 51
33489
XDOT = -5653
098402 Wp = 79
18311
YDOT = 1003
899015 meter/sec RA = 304
97609 deg
ZDOT = -5069
826418 TA = 68
82183
MA = 68
73779
Ha = 226
764 n
mi
Hp = 223
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4791869
18 X = -1541342
04
Y = 19725477
28 feet Y = 5995540
67 meter
Z = 9224387
72 Z = 2804302
47
XDOT = -18546
910768 XDOT = -5639
277505
YDOT = 3293
631940 feet/sec YDOT = 940
759539 meter/sec
ZDOT = -16633
288773 ZDOT = -5097
253712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20288726
38 X = -6184003
80
Y = -1022819
72 feet Y = -311755
45 meter
Z = 9190604
72 Z = 2801296
32
XDOT = -6805
288675 XDOT = -2074
251988
YDOT = -15994
972425 feet/sec YDOT = -4875
267595 meter/sec
ZDOT = -16758
384278 ZDOT = -5107
955528
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
65599159
00016717 00000-0 10270-3 0 9106
2 25544 51
6414 305
5275 0006632 305
0724 54
9804 15
50020059 39524
Satellite: ISS
Catalog Number: 25544
Epoch time: 19324
65599159 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 305
5275 deg
Eccentricity:
0006632
Arg of perigee: 305
0724 deg
Mean anomaly: 54
9804 deg
Mean motion: 15
50020059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 304
Coasting Arc #12 (Orbit 3966)
---------------------------------------
Vector Time (GMT): 2019/325/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1246652
78 A = 6798682
03 meter
Y = -6186610
25 meter E =
0007649
Z = -2515318
77 I = 51
31828
XDOT = 5468
053963 Wp = 350
38843
YDOT = -1037
394326 meter/sec RA = 300
00154 deg
ZDOT = 5266
718959 TA = 341
29886
MA = 341
32695
Ha = 226
894 n
mi
Hp = 223
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4090068
17 X = 1327958
78
Y = -20297277
71 feet Y = -6172214
63 meter
Z = -8252358
16 Z = -2509065
57
XDOT = 17939
809591 XDOT = 5453
664890
YDOT = -3403
524690 feet/sec YDOT = -976
327254 meter/sec
ZDOT = 17279
261676 ZDOT = 5293
246082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20716368
28 X = 6314349
05
Y = -137518
48 feet Y = -41915
63 meter
Z = -8223304
03 Z = -2506463
07
XDOT = 7001
414261 XDOT = 2134
031067
YDOT = 15224
468256 feet/sec YDOT = 4640
417924 meter/sec
ZDOT = 17400
251272 ZDOT = 5303
596588
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 19325
62308272
00016717 00000-0 10270-3 0 9119
2 25544 51
6408 300
7367 0006687 307
8743 52
1802 15
50007439 39678
Satellite: ISS
Catalog Number: 25544
Epoch time: 19325
62308272 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 300
7367 deg
Eccentricity:
0006687
Arg of perigee: 307
8743 deg
Mean anomaly: 52
1802 deg
Mean motion: 15
50007439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 311
Coasting Arc #13 (Orbit 3982)
---------------------------------------
Vector Time (GMT): 2019/326/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1028551
35 A = 6799278
24 meter
Y = 6351462
02 meter E =
0008065
Z = 2190856
66 I = 51
30578
XDOT = -5290
384147 Wp = 90
42648
YDOT = 1026
623801 meter/sec RA = 295
02577 deg
ZDOT = -5442
573832 TA = 65
18134
MA = 65
09748
Ha = 227
065 n
mi
Hp = 222
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3374512
31 X = -1110140
95
Y = 20838129
99 feet Y = 6339503
79 meter
Z = 7187849
94 Z = 2185662
21
XDOT = -17356
903370 XDOT = -5275
033511
YDOT = 3368
188325 feet/sec YDOT = 967
548921 meter/sec
ZDOT = -17856
213358 ZDOT = -5468
235667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21076589
64 X = -6424144
52
Y = 1319127
12 feet Y = 402069
95 meter
Z = 7163620
21 Z = 2183471
44
XDOT = -7036
505372 XDOT = -2144
726837
YDOT = -14511
060104 feet/sec YDOT = -4422
971120 meter/sec
ZDOT = -17973
252539 ZDOT = -5478
247374
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 19326
65464452
00016717 00000-0 10270-3 0 9127
2 25544 51
6419 295
6260 0006722 311
8405 48
2171 15
50023445 39832
Satellite: ISS
Catalog Number: 25544
Epoch time: 19326
65464452 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 295
6260 deg
Eccentricity:
0006722
Arg of perigee: 311
8405 deg
Mean anomaly: 48
2171 deg
Mean motion: 15
50023445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3983
Checksum: 303
Coasting Arc #14 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2019/327/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 768822
73 A = 6799830
95 meter
Y = -6484444
59 meter E =
0010416
Z = -1872904
30 I = 51
29419
XDOT = 5139
562908 Wp = 358
71616
YDOT = -1004
049280 meter/sec RA = 290
04902 deg
ZDOT = 5595
648908 TA = 340
59445
MA = 340
63408
Ha = 227
218 n
mi
Hp = 222
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2522384
27 X = 850374
25
Y = -21274424
51 feet Y = -6475391
04 meter
Z = -6144699
15 Z = -1868971
67
XDOT = 16862
083033 XDOT = 5123
227367
YDOT = -3294
124935 feet/sec YDOT = -946
666550 meter/sec
ZDOT = 18358
428176 ZDOT = 5620
575802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21267924
46 X = 6482463
38
Y = -2620249
00 feet Y = -798651
89 meter
Z = -6126220
10 Z = -1867271
89
XDOT = 7025
048580 XDOT = 2141
234807
YDOT = 13906
210400 feet/sec YDOT = 4238
612930 meter/sec
ZDOT = 18472
111602 ZDOT = 5630
299616
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 19327
62173105
00016717 00000-0 10270-3 0 9138
2 25544 51
6416 290
8346 0006765 315
9977 44
0635 15
50018250 39980
Satellite: ISS
Catalog Number: 25544
Epoch time: 19327
62173105 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 290
8346 deg
Eccentricity:
0006765
Arg of perigee: 315
9977 deg
Mean anomaly: 44
0635 deg
Mean motion: 15
50018250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 322
Coasting Arc #15 (Orbit 4013)
---------------------------------------
Vector Time (GMT): 2019/328/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -510795
57 A = 6800319
58 meter
Y = 6604383
15 meter E =
0008026
Z = 1527256
25 I = 51
28597
XDOT = -5003
247200 Wp = 99
66528
YDOT = 941
831272 meter/sec RA = 285
07240 deg
ZDOT = -5721
657623 TA = 63
60058
MA = 63
51822
Ha = 227
392 n
mi
Hp = 222
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1675838
48 X = -592028
48
Y = 21667923
73 feet Y = 6598216
80 meter
Z = 5010683
25 Z = 1524577
95
XDOT = -16414
853018 XDOT = -4985
613875
YDOT = 3089
997610 feet/sec YDOT = 885
980290 meter/sec
ZDOT = -18771
842594 ZDOT = -5745
919235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21380580
44 X = -6516800
92
Y = 3912272
61 feet Y = 1192460
69 meter
Z = 4997919
85 Z = 1523365
97
XDOT = -6882
770665 XDOT = -2097
868499
YDOT = -13389
087044 feet/sec YDOT = -4080
993731 meter/sec
ZDOT = -18882
486855 ZDOT = -5755
381993
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 19328
65328940
00016717 00000-0 10270-3 0 9142
2 25544 51
6421 285
7242 0006710 319
8933 40
1722 15
50019711 40146
Satellite: ISS
Catalog Number: 25544
Epoch time: 19328
65328940 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 285
7242 deg
Eccentricity:
0006710
Arg of perigee: 319
8933 deg
Mean anomaly: 40
1722 deg
Mean motion: 15
50019711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 292
Coasting Arc #16 (Orbit 4028)
---------------------------------------
Vector Time (GMT): 2019/329/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 216948
39 A = 6800683
87 meter
Y = -6683114
40 meter E =
0012757
Z = -1194703
37 I = 51
27985
XDOT = 4901
638493 Wp = 6
87394
YDOT = -879
159609 meter/sec RA = 280
09497 deg
ZDOT = 5826
977140 TA = 340
09773
MA = 340
14745
Ha = 227
479 n
mi
Hp = 222
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 711772
92 X = 297468
14
Y = -21926228
33 feet Y = -6680238
03 meter
Z = -3919630
48 Z = -1193454
40
XDOT = 16081
491118 XDOT = 4882
800291
YDOT = -2884
381920 feet/sec YDOT = -824
451777 meter/sec
ZDOT = 19117
379069 ZDOT = 5850
742236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21292942
31 X = 6490088
82
Y = -5284473
04 feet Y = -1610707
38 meter
Z = -3913382
82 Z = -1192799
09
XDOT = 6749
192462 XDOT = 2057
153863
YDOT = 13003
282711 feet/sec YDOT = 3963
400570 meter/sec
ZDOT = 19225
756171 ZDOT = 5860
010481
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 19329
62037406
00016717 00000-0 10270-3 0 9155
2 25544 51
6423 280
9330 0006812 322
8911 37
1768 15
50025009 40295
Satellite: ISS
Catalog Number: 25544
Epoch time: 19329
62037406 = yrday
fracday
Element set: 915
Inclination: 51
6423 deg
RA of node: 280
9330 deg
Eccentricity:
0006812
Arg of perigee: 322
8911 deg
Mean anomaly: 37
1768 deg
Mean motion: 15
50025009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 294
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