[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 13th 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
7
Coasting Arc #1 (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 = 6455088
97 A = 6801367
65 meter
Y = -2110598
75 meter E =
0009500
Z = 226548
05 I = 51
53463
XDOT = 1290
144558 Wp = 18
39208
YDOT = 4595
627032 meter/sec RA = 340
37539 deg
ZDOT = 5994
069233 TA = 344
04833
MA = 344
07823
Ha = 225
310 n
mi
Hp = 223
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21178113
41 X = 6477110
06
Y = -6924536
60 feet Y = -2038290
28 meter
Z = 743267
90 Z = 257958
74
XDOT = 4232
757737 XDOT = 1209
542326
YDOT = 15077
516509 feet/sec YDOT = 4609
603324 meter/sec
ZDOT = 19665
581472 ZDOT = 6000
140942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7789278
08 X = -2374171
96
Y = 20869957
40 feet Y = 6361163
01 meter
Z = 886660
80 Z = 270254
21
XDOT = -12822
757733 XDOT = -3908
376557
YDOT = -5629
481808 feet/sec YDOT = -1715
866055 meter/sec
ZDOT = 19692
788562 ZDOT = 6002
361954
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
56395630
00016717 00000-0 10270-3 0 9005
2 25544 51
6424 340
6614 0006312 275
7466 84
2964 15
49986245 38420
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
56395630 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 340
6614 deg
Eccentricity:
0006312
Arg of perigee: 275
7466 deg
Mean anomaly: 84
2964 deg
Mean motion: 15
49986245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 329
Coasting Arc #2 (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 = 2099408
24 A = 6792847
70 meter
Y = -4612108
85 meter E =
0003711
Z = -4527368
54 I = 51
49941
XDOT = 6981
876401 Wp = 134
80285
YDOT = 91
333169 meter/sec RA = 339
76459 deg
ZDOT = 3143
586192 TA = 166
84088
MA = 166
83120
Ha = 225
350 n
mi
Hp = 223
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6887822
31 X = 2172818
23
Y = -15131590
71 feet Y = -4588221
06 meter
Z = -14853571
33 Z = -4516992
07
XDOT = 22906
418640 XDOT = 6965
065938
YDOT = 299
649505 feet/sec YDOT = 169
315261 meter/sec
ZDOT = 10313
602993 ZDOT = 3177
461691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15587115
86 X = 4750952
91
Y = 5904722
69 feet Y = 1799759
48 meter
Z = -14805802
38 Z = -4512808
57
XDOT = 1739
529842 XDOT = 530
208696
YDOT = 21664
065189 feet/sec YDOT = 6603
207069 meter/sec
ZDOT = 10468
005475 ZDOT = 3190
648069
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
62842942
00016717 00000-0 10270-3 0 9016
2 25544 51
6396 340
3423 0006410 276
3276 83
7144 15
49973815 38432
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62842942 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 340
3423 deg
Eccentricity:
0006410
Arg of perigee: 276
3276 deg
Mean anomaly: 83
7144 deg
Mean motion: 15
49973815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 322
Coasting Arc #3 (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 = -2091092
25 A = 6793482
12 meter
Y = 4796746
46 meter E =
0004994
Z = 4332505
53 I = 51
47095
XDOT = -6827
906510 Wp = 34
55657
YDOT = 161
199223 meter/sec RA = 334
79907 deg
ZDOT = -3467
976971 TA = 90
83437
MA = 90
77715
Ha = 225
499 n
mi
Hp = 223
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6860538
88 X = -2165620
91
Y = 15737357
14 feet Y = 4772945
33 meter
Z = 14214256
99 Z = 4322166
87
XDOT = -22401
268078 XDOT = -6812
355667
YDOT = 528
868842 feet/sec YDOT = 84
931974 meter/sec
ZDOT = -11377
877201 ZDOT = -3501
107483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16287014
18 X = -4964281
92
Y = -5551205
16 feet Y = -1692007
33 meter
Z = 14166643
77 Z = 4317993
02
XDOT = -2886
155016 XDOT = -879
700049
YDOT = -21004
219172 feet/sec YDOT = -6402
086004 meter/sec
ZDOT = -11528
904257 ZDOT = -3514
010017
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
66000591
00016717 00000-0 10270-3 0 9028
2 25544 51
6397 335
2315 0006528 280
1978 79
8437 15
50003835 38594
Satellite: ISS
Catalog Number: 25544
Epoch time: 19318
66000591 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 335
2315 deg
Eccentricity:
0006528
Arg of perigee: 280
1978 deg
Mean anomaly: 79
8437 deg
Mean motion: 15
50003835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 326
Coasting Arc #4 (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 = 2048086
70 A = 6794279
08 meter
Y = -4994798
46 meter E =
0001076
Z = -4126673
65 I = 51
44455
XDOT = 6653
391541 Wp = 134
99398
YDOT = -389
159150 meter/sec RA = 329
83186 deg
ZDOT = 3772
993874 TA = 174
05518
MA = 174
05390
Ha = 225
789 n
mi
Hp = 223
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6719444
55 X = 2123833
31
Y = -16387134
06 feet Y = -4971471
41 meter
Z = -13538955
56 Z = -4116541
07
XDOT = 21828
712404 XDOT = 6638
921211
YDOT = -1276
768866 feet/sec YDOT = -314
837485 meter/sec
ZDOT = 12378
588827 ZDOT = 3805
279112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17011008
58 X = 5184955
41
Y = 5057349
64 feet Y = 1541480
17 meter
Z = -13492265
08 Z = -4112442
40
XDOT = 3914
574642 XDOT = 1193
162351
YDOT = 20251
034627 feet/sec YDOT = 6172
515354 meter/sec
ZDOT = 12525
782974 ZDOT = 3817
858650
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
62710787
00016717 00000-0 10270-3 0 9031
2 25544 51
6406 330
4403 0006481 284
6927 75
3504 15
49981180 38740
Satellite: ISS
Catalog Number: 25544
Epoch time: 19319
62710787 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 330
4403 deg
Eccentricity:
0006481
Arg of perigee: 284
6927 deg
Mean anomaly: 75
3504 deg
Mean motion: 15
49981180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 325
Coasting Arc #5 (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 = -1989532
61 A = 6794986
59 meter
Y = 5199568
08 meter E =
0006229
Z = 3894757
90 I = 51
41858
XDOT = -6463
995603 Wp = 51
75791
YDOT = 580
310127 meter/sec RA = 324
86332 deg
ZDOT = -4068
460442 TA = 81
07840
MA = 81
00788
Ha = 226
007 n
mi
Hp = 223
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6527337
97 X = -2066446
74
Y = 17058950
39 feet Y = 5176889
29 meter
Z = 12778077
11 Z = 3884907
02
XDOT = -21207
334657 XDOT = -6450
241706
YDOT = 1903
904615 feet/sec YDOT = 508
102464 meter/sec
ZDOT = -13347
967331 ZDOT = -4099
827215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17738231
14 X = -5406612
85
Y = -4486403
74 feet Y = -1367455
86 meter
Z = 12732655
71 Z = 3880913
46
XDOT = -4788
026581 XDOT = -1459
390502
YDOT = -19434
215509 feet/sec YDOT = -5923
548887 meter/sec
ZDOT = -13490
992282 ZDOT = -4112
054448
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
65868268
00016717 00000-0 10270-3 0 9045
2 25544 51
6404 325
3298 0006558 289
2362 70
8078 15
50006596 38907
Satellite: ISS
Catalog Number: 25544
Epoch time: 19320
65868268 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 325
3298 deg
Eccentricity:
0006558
Arg of perigee: 289
2362 deg
Mean anomaly: 70
8078 deg
Mean motion: 15
50006596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 336
Coasting Arc #6 (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 = 1887545
11 A = 6795810
39 meter
Y = -5406925
01 meter E =
0001829
Z = -3656447
92 I = 51
39431
XDOT = 6266
904473 Wp = 337
58893
YDOT = -747
021536 meter/sec RA = 319
89347 deg
ZDOT = 4340
710842 TA = 338
88926
MA = 338
89681
Ha = 226
230 n
mi
Hp = 223
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6192733
29 X = 1965627
86
Y = -17739255
27 feet Y = -5385380
22 meter
Z = -11996220
22 Z = -3647089
66
XDOT = 20560
710213 XDOT = 6253
707073
YDOT = -2450
858057 feet/sec YDOT = -677
014780 meter/sec
ZDOT = 14241
177303 ZDOT = 4371
121400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18439253
42 X = 5620284
44
Y = 3749584
13 feet Y = 1142873
24 meter
Z = -11953032
04 Z = -3643284
16
XDOT = 5541
160246 XDOT = 1688
945643
YDOT = 18581
031890 feet/sec YDOT = 5663
498520 meter/sec
ZDOT = 14379
858387 ZDOT = 4382
980836
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
62578469
00016717 00000-0 10270-3 0 9055
2 25544 51
6403 320
5390 0006603 292
6354 67
4093 15
49981446 39056
Satellite: ISS
Catalog Number: 25544
Epoch time: 19321
62578469 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 320
5390 deg
Eccentricity:
0006603
Arg of perigee: 292
6354 deg
Mean anomaly: 67
4093 deg
Mean motion: 15
49981446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 325
Coasting Arc #7 (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 = -1772325
63 A = 6796517
90 meter
Y = 5615122
57 meter E =
0007107
Z = 3391731
00 I = 51
37323
XDOT = -6061
645191 Wp = 66
23307
YDOT = 872
069469 meter/sec RA = 314
92227 deg
ZDOT = -4600
726368 TA = 74
05612
MA = 73
97783
Ha = 226
398 n
mi
Hp = 223
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5814716
65 X = -1851459
15
Y = 18422318
16 feet Y = 5594860
45 meter
Z = 11127726
37 Z = 3382929
86
XDOT = -19887
287371 XDOT = -6048
598418
YDOT = 2861
120304 feet/sec YDOT = 804
357181 meter/sec
ZDOT = -15094
246615 ZDOT = -4630
140106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19115851
14 X = -5826511
43
Y = -2946214
03 feet Y = -898006
04 meter
Z = 11087068
52 Z = 3379338
48
XDOT = -6123
882874 XDOT = -1866
559500
YDOT = -17703
320826 feet/sec YDOT = -5395
972188 meter/sec
ZDOT = -15228
393510 ZDOT = -4641
614342
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
65735962
00016717 00000-0 10270-3 0 9063
2 25544 51
6414 315
4287 0006647 296
6817 63
3653 15
50008326 39216
Satellite: ISS
Catalog Number: 25544
Epoch time: 19322
65735962 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 315
4287 deg
Eccentricity:
0006647
Arg of perigee: 296
6817 deg
Mean anomaly: 63
3653 deg
Mean motion: 15
50008326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 323
Coasting Arc #8 (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 = 1611399
77 A = 6797297
91 meter
Y = -5814229
67 meter E =
0004792
Z = -3124012
70 I = 51
35286
XDOT = 5860
801376 Wp = 342
65627
YDOT = -973
334359 meter/sec RA = 309
94956 deg
ZDOT = 4837
139780 TA = 341
27654
MA = 341
29416
Ha = 226
615 n
mi
Hp = 223
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5286744
64 X = 1691471
26
Y = -19075556
66 feet Y = -5795761
97 meter
Z = -10249385
51 Z = -3115990
91
XDOT = 19228
350970 XDOT = 5847
753558
YDOT = -3193
354196 feet/sec YDOT = -907
867972 meter/sec
ZDOT = 15869
881169 ZDOT = 4865
577856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19714780
12 X = 6009064
98
Y = 1978212
96 feet Y = 602959
31 meter
Z = -10212274
60 Z = -3112701
30
XDOT = 6593
318056 XDOT = 2009
643343
YDOT = 16843
593276 feet/sec YDOT = 5133
927230 meter/sec
ZDOT = 15999
586414 ZDOT = 4876
673939
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
62445949
00016717 00000-0 10270-3 0 9075
2 25544 51
6414 310
6377 0006702 300
6555 59
3935 15
49989348 39364
Satellite: ISS
Catalog Number: 25544
Epoch time: 19323
62445949 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 310
6377 deg
Eccentricity:
0006702
Arg of perigee: 300
6555 deg
Mean anomaly: 59
3935 deg
Mean motion: 15
49989348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3936
Checksum: 343
Coasting Arc #9 (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 = -1440558
76 A = 6797986
25 meter
Y = 6008799
76 meter E =
0007862
Z = 2829530
44 I = 51
33457
XDOT = -5659
582434 Wp = 78
27283
YDOT = 1030
898595 meter/sec RA = 304
97618 deg
ZDOT = -5057
058049 TA = 69
50360
MA = 69
41923
Ha = 226
806 n
mi
Hp = 223
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4726242
65 X = -1521388
26
Y = 19713909
97 feet Y = 5992238
36 meter
Z = 9283236
34 Z = 2822336
57
XDOT = -18568
183838 XDOT = -5646
124994
YDOT = 3382
213237 feet/sec YDOT = 967
684576 meter/sec
ZDOT = -16591
397800 ZDOT = -5084
517722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20264995
71 X = -6176770
69
Y = -960971
46 feet Y = -292904
10 meter
Z = 9249895
97 Z = 2819368
29
XDOT = -6891
843298 XDOT = -2100
633837
YDOT = -16001
057836 feet/sec YDOT = -4877
122428 meter/sec
ZDOT = -16716
643365 ZDOT = -5095
232898
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
65603284
00016717 00000-0 10270-3 0 9088
2 25544 51
6413 305
5275 0006678 305
3547 54
6978 15
50006780 39523
Satellite: ISS
Catalog Number: 25544
Epoch time: 19324
65603284 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 305
5275 deg
Eccentricity:
0006678
Arg of perigee: 305
3547 deg
Mean anomaly: 54
6978 deg
Mean motion: 15
50006780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3952
Checksum: 325
Coasting Arc #10 (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 = 1222911
27 A = 6798677
24 meter
Y = -6182043
78 meter E =
0007626
Z = -2538133
24 I = 51
31795
XDOT = 5474
892592 Wp = 350
21677
YDOT = -1071
500074 meter/sec RA = 300
00167 deg
ZDOT = 5252
742019 TA = 341
19010
MA = 341
21826
Ha = 226
939 n
mi
Hp = 223
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4012176
08 X = 1304278
79
Y = -20282295
88 feet Y = -6167913
32 meter
Z = -8327208
79 Z = -2531995
23
XDOT = 17962
246036 XDOT = 5460
952283
YDOT = -3515
420190 feet/sec YDOT = -1010
354018 meter/sec
ZDOT = 17233
405573 ZDOT = 5279
303451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20685725
54 X = 6305009
14
Y = -210138
98 feet Y = -64050
36 meter
Z = -8298680
00 Z = -2529437
66
XDOT = 7110
302075 XDOT = 2167
220072
YDOT = 15225
838022 feet/sec YDOT = 4640
835429 meter/sec
ZDOT = 17354
554595 ZDOT = 5289
668241
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
62313292
00016717 00000-0 10270-3 0 9094
2 25544 51
6407 300
7368 0006735 308
1666 51
8877 15
49992365 39677
Satellite: ISS
Catalog Number: 25544
Epoch time: 19325
62313292 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 300
7368 deg
Eccentricity:
0006735
Arg of perigee: 308
1666 deg
Mean anomaly: 51
8877 deg
Mean motion: 15
49992365 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3967
Checksum: 345
Coasting Arc #11 (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 = -1000906
95 A = 6799273
91 meter
Y = 6346073
81 meter E =
0008071
Z = 2219278
69 I = 51
30543
XDOT = -5297
085273 Wp = 89
32324
YDOT = 1068
744251 meter/sec RA = 295
02594 deg
ZDOT = -5427
828267 TA = 65
94718
MA = 65
86275
Ha = 227
114 n
mi
Hp = 222
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3283815
44 X = -1082576
41
Y = 20820452
14 feet Y = 6334424
28 meter
Z = 7281098
06 Z = 2214218
33
XDOT = -17378
888691 XDOT = -5282
276769
YDOT = 3506
378777 feet/sec YDOT = 1009
591403 meter/sec
ZDOT = -17807
835522 ZDOT = -5453
523971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21039242
57 X = -6412761
14
Y = 1402967
41 feet Y = 427624
47 meter
Z = 7257479
91 Z = 2212079
88
XDOT = -7170
076750 XDOT = -2185
439393
YDOT = -14504
657023 feet/sec YDOT = -4421
019461 meter/sec
ZDOT = -17925
032745 ZDOT = -5463
549981
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
65470538
00016717 00000-0 10270-3 0 9107
2 25544 51
6418 295
6261 0006773 312
1429 47
9145 15
50006801 39832
Satellite: ISS
Catalog Number: 25544
Epoch time: 19326
65470538 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 295
6261 deg
Eccentricity:
0006773
Arg of perigee: 312
1429 deg
Mean anomaly: 47
9145 deg
Mean motion: 15
50006801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3983
Checksum: 313
Coasting Arc #12 (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 = 736876
63 A = 6799829
00 meter
Y = -6478057
27 meter E =
0010377
Z = -1907627
53 I = 51
29384
XDOT = 5145
544936 Wp = 358
41187
YDOT = -1055
280971 meter/sec RA = 290
04923 deg
ZDOT = 5580
659801 TA = 340
49703
MA = 340
53669
Ha = 227
270 n
mi
Hp = 222
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2417574
25 X = 818527
78
Y = -21253468
74 feet Y = -6469360
40 meter
Z = -6258620
51 Z = -1903849
85
XDOT = 16881
709106 XDOT = 5129
854647
YDOT = -3462
207911 feet/sec YDOT = -997
827738 meter/sec
ZDOT = 18309
251315 ZDOT = 5605
617319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21222604
39 X = 6468649
82
Y = -2716211
85 feet Y = -827901
37 meter
Z = -6240848
12 Z = -1902210
51
XDOT = 7186
010885 XDOT = 2190
296118
YDOT = 13888
523808 feet/sec YDOT = 4233
222057 meter/sec
ZDOT = 18423
078710 ZDOT = 5615
354391
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
62180297
00016717 00000-0 10270-3 0 9116
2 25544 51
6415 290
8348 0006818 316
2974 43
7636 15
49999873 39985
Satellite: ISS
Catalog Number: 25544
Epoch time: 19327
62180297 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 290
8348 deg
Eccentricity:
0006818
Arg of perigee: 316
2974 deg
Mean anomaly: 43
7636 deg
Mean motion: 15
49999873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 365
Coasting Arc #13 (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 = -474337
80 A = 6800323
67 meter
Y = 6597396
65 meter E =
0008062
Z = 1568925
06 I = 51
28561
XDOT = -5007
773066 Wp = 98
37370
YDOT = 1002
918366 meter/sec RA = 285
07266 deg
ZDOT = -5707
205722 TA = 64
42164
MA = 64
33833
Ha = 227
449 n
mi
Hp = 222
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1556226
39 X = -555697
71
Y = 21645002
13 feet Y = 6591637
28 meter
Z = 5147391
91 Z = 1566423
54
XDOT = -16429
701659 XDOT = -4990
892699
YDOT = 3290
414586 feet/sec YDOT = 947
012562 meter/sec
ZDOT = -18724
428223 ZDOT = -5731
491146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21327956
21 X = -6500761
05
Y = 4021093
75 feet Y = 1225629
38 meter
Z = 5135434
78 Z = 1565280
52
XDOT = -7072
428986 XDOT = -2155
676355
YDOT = -13356
114834 feet/sec YDOT = -4070
943801 meter/sec
ZDOT = -18835
186159 ZDOT = -5740
964741
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
65337423
00016717 00000-0 10270-3 0 9126
2 25544 51
6420 285
7244 0006766 320
2199 39
8455 15
49999645 40147
Satellite: ISS
Catalog Number: 25544
Epoch time: 19328
65337423 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 285
7244 deg
Eccentricity:
0006766
Arg of perigee: 320
2199 deg
Mean anomaly: 39
8455 deg
Mean motion: 15
49999645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4014
Checksum: 337
Coasting Arc #14 (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 = 175463
45 A = 6800695
78 meter
Y = -6675382
49 meter E =
0012711
Z = -1243985
14 I = 51
27951
XDOT = 4903
784970 Wp = 6
41565
YDOT = -951
142102 meter/sec RA = 280
09527 deg
ZDOT = 5813
792530 TA = 340
00855
MA = 340
05831
Ha = 227
538 n
mi
Hp = 222
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 575667
49 X = 256139
22
Y = -21900861
20 feet Y = -6672969
16 meter
Z = -4081316
08 Z = -1242937
31
XDOT = 16088
533365 XDOT = 4885
815582
YDOT = -3120
544955 feet/sec YDOT = -896
405407 meter/sec
ZDOT = 19074
122473 ZDOT = 5837
570158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21231640
19 X = 6471403
93
Y = -5407406
99 feet Y = -1648177
65 meter
Z = -4075985
74 Z = -1242360
45
XDOT = 6969
401369 XDOT = 2124
273537
YDOT = 12950
241335 feet/sec YDOT = 3947
233559 meter/sec
ZDOT = 19182
562675 ZDOT = 5846
845103
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
62047206
00016717 00000-0 10270-3 0 9132
2 25544 51
6422 280
9333 0006869 323
2137 36
8542 15
50003458 40294
Satellite: ISS
Catalog Number: 25544
Epoch time: 19329
62047206 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 280
9333 deg
Eccentricity:
0006869
Arg of perigee: 323
2137 deg
Mean anomaly: 36
8542 deg
Mean motion: 15
50003458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4029
Checksum: 300
Coasting Arc #15 (Orbit 4044)
---------------------------------------
Vector Time (GMT): 2019/330/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 114126
95 A = 6801036
04 meter
Y = 6739137
18 meter E =
0007486
Z = 891578
08 I = 51
27687
XDOT = -4818
365831 Wp = 106
13179
YDOT = 865
913082 meter/sec RA = 275
11824 deg
ZDOT = -5889
025632 TA = 64
19163
MA = 64
11443
Ha = 227
713 n
mi
Hp = 222
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 374432
25 X = 34428
58
Y = 22110030
13 feet Y = 6739967
72 meter
Z = 2925124
94 Z = 891939
56
XDOT = -15808
286848 XDOT = -4799
084338
YDOT = 2840
922184 feet/sec YDOT = 812
139097 meter/sec
ZDOT = -19320
950236 ZDOT = -5912
385073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21057911
90 X = -6418451
55
Y = 6749189
93 feet Y = 2057153
09 meter
Z = 2926220
99 Z = 891912
16
XDOT = -6770
499468 XDOT = -2063
648238
YDOT = -12645
358899 feet/sec YDOT = -3854
305392 meter/sec
ZDOT = -19427
481095 ZDOT = -5921
496238
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 19330
65204225
00016717 00000-0 10270-3 0 9144
2 25544 51
6432 275
8231 0006797 326
7320 33
3403 15
49993999 40459
Satellite: ISS
Catalog Number: 25544
Epoch time: 19330
65204225 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 275
8231 deg
Eccentricity:
0006797
Arg of perigee: 326
7320 deg
Mean anomaly: 33
3403 deg
Mean motion: 15
49993999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4045
Checksum: 317
Coasting Arc #16 (Orbit 4059)
---------------------------------------
Vector Time (GMT): 2019/331/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -430034
68 A = 6801189
57 meter
Y = -6755254
51 meter E =
0014765
Z = -556957
89 I = 51
27623
XDOT = 4771
319123 Wp = 14
82405
YDOT = -790
100736 meter/sec RA = 270
14040 deg
ZDOT = 5948
086248 TA = 339
14240
MA = 339
20258
Ha = 227
833 n
mi
Hp = 221
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1410874
95 X = -351758
06
Y = -22162908
50 feet Y = -6759625
72 meter
Z = -1827289
66 Z = -558857
55
XDOT = 15653
934130 XDOT = 4750
906591
YDOT = -2592
194017 feet/sec YDOT = -736
859314 meter/sec
ZDOT = 19514
718660 ZDOT = 5971
214305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20669226
23 X = 6299980
16
Y = -8120248
87 feet Y = -2475051
85 meter
Z = -1835405
65 Z = -559431
64
XDOT = 6628
906036 XDOT = 2020
490560
YDOT = 12474
687964 feet/sec YDOT = 3802
284891 meter/sec
ZDOT = 19620
194610 ZDOT = 5980
235317
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 19331
61913717
00016717 00000-0 10270-3 0 9155
2 25544 51
6437 271
0319 0006968 331
0449 29
0314 15
50012877 40609
Satellite: ISS
Catalog Number: 25544
Epoch time: 19331
61913717 = yrday
fracday
Element set: 915
Inclination: 51
6437 deg
RA of node: 271
0319 deg
Eccentricity:
0006968
Arg of perigee: 331
0449 deg
Mean anomaly: 29
0314 deg
Mean motion: 15
50012877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4060
Checksum: 298
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