[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 15th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 27986 17 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 ET - UTC (sec) : 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2014/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 871115
71 A = 6794786
96 meter
Y = -6728203
40 meter E =
0013333
Z = -343907
77 I = 51
30831
XDOT = 4793
177644 Wp = 75
44826
YDOT = 325
682452 meter/sec RA = 279
70398 deg
ZDOT = 5967
553997 TA = 280
83281
MA = 280
98284
Ha = 226
325 n
mi
Hp = 215
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2857991
19 X = 947957
91
Y = -22074158
13 feet Y = -6718032
36 meter
Z = -1128306
32 Z = -339489
55
XDOT = 15725
648438 XDOT = 4760
190958
YDOT = 1068
511981 feet/sec YDOT = 379
098251 meter/sec
ZDOT = 19578
589229 ZDOT = 5990
758570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21583001
03 X = 6578498
71
Y = 5445695
39 feet Y = 1659847
95 meter
Z = -1108203
12 Z = -337780
31
XDOT = -2503
794275 XDOT = -763
156495
YDOT = 13793
029006 feet/sec YDOT = 4204
115241 meter/sec
ZDOT = 19677
461063 ZDOT = 5997
690132
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 14349
50065383
00016717 00000-0 10270-3 0 9008
2 25544 51
6446 280
4836 0007215 134
2288 225
9457 15
52234038 39461
Satellite: ISS
Catalog Number: 25544
Epoch time: 14349
50065383 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 280
4836 deg
Eccentricity:
0007215
Arg of perigee: 134
2288 deg
Mean anomaly: 225
9457 deg
Mean motion: 15
52234038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 313
Coasting Arc #2 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2014/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1175653
81 A = 6794459
49 meter
Y = 6638241
12 meter E =
0017554
Z = -781012
43 I = 51
30421
XDOT = -4634
305971 Wp = 139
41334
YDOT = -1506
942149 meter/sec RA = 274
71842 deg
ZDOT = -5920
572853 TA = 49
06582
MA = 48
91399
Ha = 226
182 n
mi
Hp = 215
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3857131
93 X = -1246002
87
Y = 21779006
31 feet Y = 6624700
88 meter
Z = -2562376
73 Z = -786894
26
XDOT = -15204
415914 XDOT = -4588
350126
YDOT = -4944
035923 feet/sec YDOT = -1558
508800 meter/sec
ZDOT = -19424
451619 ZDOT = -5942
974241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21281217
87 X = -6486515
21
Y = -6014713
79 feet Y = -1833284
76 meter
Z = -2588694
90 Z = -789034
21
XDOT = 6000
952091 XDOT = 1829
090197
YDOT = -12954
744950 feet/sec YDOT = -3948
606261 meter/sec
ZDOT = -19519
680387 ZDOT = -5949
598582
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 14350
53072394
00016717 00000-0 10270-3 0 9014
2 25544 51
6456 275
3625 0007254 138
4159 221
7545 15
52275053 39629
Satellite: ISS
Catalog Number: 25544
Epoch time: 14350
53072394 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 275
3625 deg
Eccentricity:
0007254
Arg of perigee: 138
4159 deg
Mean anomaly: 221
7545 deg
Mean motion: 15
52275053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 307
Coasting Arc #3 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2014/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436572
49 A = 6793139
22 meter
Y = -6377925
50 meter E =
0017207
Z = 1830345
73 I = 51
29832
XDOT = 4507
131946 Wp = 90
07162
YDOT = 2638
323617 meter/sec RA = 269
73126 deg
ZDOT = 5609
975314 TA = 290
13823
MA = 290
32327
Ha = 226
055 n
mi
Hp = 215
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4713164
35 X = 1498893
87
Y = -20924952
42 feet Y = -6361512
44 meter
Z = 6005071
28 Z = 1837475
52
XDOT = 14787
178300 XDOT = 4450
042930
YDOT = 8655
917378 feet/sec YDOT = 2688
405817 meter/sec
ZDOT = 18405
430821 ZDOT = 5631
731971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20460418
86 X = 6236335
67
Y = 6407689
62 feet Y = 1953063
80 meter
Z = 6036655
28 Z = 1839972
53
XDOT = -9386
277029 XDOT = -2860
937239
YDOT = 12403
621486 feet/sec YDOT = 3780
623829 meter/sec
ZDOT = 18497
705120 ZDOT = 5638
100520
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 14351
56076109
00016717 00000-0 10270-3 0 9027
2 25544 51
6453 270
2419 0007202 142
0067 218
1594 15
52328272 39786
Satellite: ISS
Catalog Number: 25544
Epoch time: 14351
56076109 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 270
2419 deg
Eccentricity:
0007202
Arg of perigee: 142
0067 deg
Mean anomaly: 218
1594 deg
Mean motion: 15
52328272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 297
Coasting Arc #4 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2014/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1764389
79 A = 6790893
18 meter
Y = 5895965
86 meter E =
0011451
Z = -2866945
69 I = 51
29346
XDOT = -4395
148772 Wp = 134
37022
YDOT = -3752
424667 meter/sec RA = 264
74081 deg
ZDOT = -5032
447926 TA = 78
39013
MA = 78
26162
Ha = 225
864 n
mi
Hp = 215
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5788680
42 X = -1816261
90
Y = 19343720
03 feet Y = 5875945
47 meter
Z = -9405989
79 Z = -2875642
52
XDOT = -14419
779436 XDOT = -4328
415396
YDOT = -12311
104552 feet/sec YDOT = -3801
200609 meter/sec
ZDOT = -16510
655924 ZDOT = -5053
637287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18919541
99 X = -5766676
40
Y = -7001407
93 feet Y = -2134029
14 meter
Z = -9444161
55 Z = -2878580
44
XDOT = 12725
833110 XDOT = 3878
833932
YDOT = -12085
982872 feet/sec YDOT = -3683
807579 meter/sec
ZDOT = -16600
312566 ZDOT = -5059
775270
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 14352
52639091
00016717 00000-0 10270-3 0 9030
2 25544 51
6463 265
4408 0007193 145
8258 214
3358 15
52384418 39930
Satellite: ISS
Catalog Number: 25544
Epoch time: 14352
52639091 = yrday
fracday
Element set: 903
Inclination: 51
6463 deg
RA of node: 265
4408 deg
Eccentricity:
0007193
Arg of perigee: 145
8258 deg
Mean anomaly: 214
3358 deg
Mean motion: 15
52384418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 324
Coasting Arc #5 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2014/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2088415
88 A = 6788354
27 meter
Y = -5265899
01 meter E =
0016942
Z = 3733656
72 I = 51
28880
XDOT = 4303
810412 Wp = 116
10999
YDOT = 4725
185424 meter/sec RA = 259
74639 deg
ZDOT = 4234
666366 TA = 288
73952
MA = 288
92330
Ha = 225
757 n
mi
Hp = 215
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6851758
15 X = 2129008
14
Y = -17276571
54 feet Y = -5242318
34 meter
Z = 12249529
92 Z = 3743900
17
XDOT = 14120
112901 XDOT = 4230
081612
YDOT = 15502
576849 feet/sec YDOT = 4772
900813 meter/sec
ZDOT = 13893
262357 ZDOT = 4255
395160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16920795
76 X = 5157458
55
Y = 7616912
75 feet Y = 2321635
01 meter
Z = 12294177
82 Z = 3747265
40
XDOT = -15620
779272 XDOT = -4761
213522
YDOT = 12017
454224 feet/sec YDOT = 3662
920048 meter/sec
ZDOT = 13980
785975 ZDOT = 4261
343565
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 14353
55636585
00016717 00000-0 10270-3 0 9040
2 25544 51
6460 260
3198 0007205 149
5690 210
5881 15
52422162 40099
Satellite: ISS
Catalog Number: 25544
Epoch time: 14353
55636585 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 260
3198 deg
Eccentricity:
0007205
Arg of perigee: 149
5690 deg
Mean anomaly: 210
5881 deg
Mean motion: 15
52422162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 303
Coasting Arc #6 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2014/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2509120
91 A = 6785553
26 meter
Y = 4445500
54 meter E =
0012489
Z = -4479358
14 I = 51
28735
XDOT = -4174
381991 Wp = 104
23387
YDOT = -5567
169080 meter/sec RA = 254
74695 deg
ZDOT = -3197
334045 TA = 133
46807
MA = 133
36414
Ha = 225
535 n
mi
Hp = 215
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8232023
98 X = -2536885
67
Y = 14584975
54 feet Y = 4417287
15 meter
Z = -14696056
91 Z = -4491614
14
XDOT = -13695
478972 XDOT = -4096
286663
YDOT = -18264
990421 feet/sec YDOT = -5613
412740 meter/sec
ZDOT = -10489
941093 ZDOT = -3217
423590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14315106
77 X = -4363244
54
Y = -8602472
08 feet Y = -2622033
49 meter
Z = -14749135
95 Z = -4495536
64
XDOT = 18066
330070 XDOT = 5506
617405
YDOT = -11992
263680 feet/sec YDOT = -3655
241970 meter/sec
ZDOT = -10574
597382 ZDOT = -3223
137282
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 14354
52193745
00016717 00000-0 10270-3 0 9055
2 25544 51
6467 255
5186 0007132 153
4119 206
7400 15
52490879 40249
Satellite: ISS
Catalog Number: 25544
Epoch time: 14354
52193745 = yrday
fracday
Element set: 905
Inclination: 51
6467 deg
RA of node: 255
5186 deg
Eccentricity:
0007132
Arg of perigee: 153
4119 deg
Mean anomaly: 206
7400 deg
Mean motion: 15
52490879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 308
Coasting Arc #7 (Orbit 4039)
---------------------------------------
Vector Time (GMT): 2014/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2947038
57 A = 6783409
02 meter
Y = -3537577
96 meter E =
0012612
Z = 4977857
73 I = 51
28922
XDOT = 4018
943078 Wp = 142
14158
YDOT = 6210
346588 meter/sec RA = 249
74371 deg
ZDOT = 2021
607781 TA = 288
04432
MA = 288
18169
Ha = 225
378 n
mi
Hp = 215
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9668761
71 X = 2962196
73
Y = -11606226
90 feet Y = -3504538
06 meter
Z = 16331554
24 Z = 4992210
46
XDOT = 13185
508785 XDOT = 3939
378511
YDOT = 20375
152849 feet/sec YDOT = 6254
843919 meter/sec
ZDOT = 6632
571459 ZDOT = 2040
938685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11461178
06 X = 3493367
07
Y = 9736867
41 feet Y = 2967797
19 meter
Z = 16393411
18 Z = 4996711
73
XDOT = -19858
955745 XDOT = -6053
009711
YDOT = 12003
094839 feet/sec YDOT = 3658
543307 meter/sec
ZDOT = 6713
891302 ZDOT = 2046
394069
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 14355
55185078
00016717 00000-0 10270-3 0 9060
2 25544 51
6463 250
3973 0007166 157
7743 202
3721 15
52526669 40402
Satellite: ISS
Catalog Number: 25544
Epoch time: 14355
55185078 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 250
3973 deg
Eccentricity:
0007166
Arg of perigee: 157
7743 deg
Mean anomaly: 202
3721 deg
Mean motion: 15
52526669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4040
Checksum: 316
Coasting Arc #8 (Orbit 4054)
---------------------------------------
Vector Time (GMT): 2014/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3476208
17 A = 6782029
48 meter
Y = 2518077
48 meter E =
0017566
Z = -5264832
14 I = 51
29692
XDOT = -3752
773856 Wp = 107
65312
YDOT = -6633
921525 meter/sec RA = 244
73681 deg
ZDOT = -702
214376 TA = 155
63716
MA = 155
55402
Ha = 225
204 n
mi
Hp = 215
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11404882
46 X = -3478532
81
Y = 8261409
06 feet Y = 2479191
85 meter
Z = -17273071
34 Z = -5281724
36
XDOT = -12312
250185 XDOT = -3674
901766
YDOT = -21764
834401 feet/sec YDOT = -6675
451992 meter/sec
ZDOT = -2303
852941 ZDOT = -720
256321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8286104
06 X = -2525604
52
Y = -11276195
64 feet Y = -3436984
43 meter
Z = -17345578
93 Z = -5286932
46
XDOT = 20914
065582 XDOT = 6374
607189
YDOT = -11743
895450 feet/sec YDOT = -3579
539333 meter/sec
ZDOT = -2379
617507 ZDOT = -725
307416
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 14356
51736633
00016717 00000-0 10270-3 0 9077
2 25544 51
6463 245
5956 0007055 161
6375 198
5032 15
52583974 40550
Satellite: ISS
Catalog Number: 25544
Epoch time: 14356
51736633 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 245
5956 deg
Eccentricity:
0007055
Arg of perigee: 161
6375 deg
Mean anomaly: 198
5032 deg
Mean motion: 15
52583974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4055
Checksum: 331
Coasting Arc #9 (Orbit 4070)
---------------------------------------
Vector Time (GMT): 2014/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4006484
62 A = 6781805
75 meter
Y = -1492456
21 meter E =
0007058
Z = 5260110
30 I = 51
31059
XDOT = 3395
223422 Wp = 142
59162
YDOT = 6847
218115 meter/sec RA = 239
72986 deg
ZDOT = -648
332737 TA = 313
59590
MA = 313
65446
Ha = 224
907 n
mi
Hp = 215
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13144634
58 X = 3997324
17
Y = -4896509
89 feet Y = -1447704
85 meter
Z = 17257579
73 Z = 5279550
65
XDOT = 11139
184457 XDOT = 3321
553250
YDOT = 22464
626360 feet/sec YDOT = 6884
773856 meter/sec
ZDOT = -2127
075910 ZDOT = -632
017636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5148568
72 X = 1569283
75
Y = 12937190
61 feet Y = 3943255
70 meter
Z = 17340779
25 Z = 5285469
51
XDOT = -21298
935808 XDOT = -6491
915634
YDOT = 11213
599327 feet/sec YDOT = 3417
905075 meter/sec
ZDOT = -2058
694978 ZDOT = -627
490229
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 14357
54721985
00016717 00000-0 10270-3 0 9086
2 25544 51
6458 240
4738 0007022 166
5756 193
5584 15
52640689 40719
Satellite: ISS
Catalog Number: 25544
Epoch time: 14357
54721985 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 240
4738 deg
Eccentricity:
0007022
Arg of perigee: 166
5756 deg
Mean anomaly: 193
5584 deg
Mean motion: 15
52640689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 339
Coasting Arc #10 (Orbit 4085)
---------------------------------------
Vector Time (GMT): 2014/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4576492
44 A = 6782923
31 meter
Y = 459449
84 meter E =
0016928
Z = -5000140
02 I = 51
33067
XDOT = -2865
893212 Wp = 126
91123
YDOT = -6811
366966 meter/sec RA = 234
72349 deg
ZDOT = 1991
919649 TA = 162
58970
MA = 162
53158
Ha = 224
864 n
mi
Hp = 215
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15014738
96 X = -4557001
22
Y = 1507381
35 feet Y = 408381
92 meter
Z = -16404658
87 Z = -5022324
31
XDOT = -9402
536786 XDOT = -2799
189893
YDOT = -22347
004481 feet/sec YDOT = -6843
042448 meter/sec
ZDOT = 6535
169453 ZDOT = 1978
159180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2052460
50 X = -625589
96
Y = -14845367
86 feet Y = -4524868
12 meter
Z = -16499390
18 Z = -5029014
13
XDOT = 20901
957938 XDOT = 6370
916780
YDOT = -10108
327162 feet/sec YDOT = -3081
018119 meter/sec
ZDOT = 6477
660011 ZDOT = 1974
390771
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 14358
51268186
00016717 00000-0 10270-3 0 9094
2 25544 51
6454 235
6712 0006953 170
3513 189
7773 15
52663527 40868
Satellite: ISS
Catalog Number: 25544
Epoch time: 14358
51268186 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 235
6712 deg
Eccentricity:
0006953
Arg of perigee: 170
3513 deg
Mean anomaly: 189
7773 deg
Mean motion: 15
52663527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4086
Checksum: 336
Coasting Arc #11 (Orbit 4101)
---------------------------------------
Vector Time (GMT): 2014/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5088910
62 A = 6784853
20 meter
Y = 502709
40 meter E =
0009676
Z = 4449407
23 I = 51
35670
XDOT = 2188
682075 Wp = 111
37928
YDOT = 6597
754105 meter/sec RA = 229
72215 deg
ZDOT = -3246
453227 TA = 11
43637
MA = 11
41440
Ha = 224
467 n
mi
Hp = 216
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16695900
99 X = 5061297
51
Y = 1649309
06 feet Y = 559462
23 meter
Z = 14597792
75 Z = 4474061
05
XDOT = 7180
715469 XDOT = 2130
511776
YDOT = 21646
174886 feet/sec YDOT = 6621
904323 meter/sec
ZDOT = -10651
093264 ZDOT = -3235
961947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -753168
46 X = -229565
75
Y = 16668121
10 feet Y = 5080443
31 meter
Z = 14702903
11 Z = 4481444
87
XDOT = -20007
522320 XDOT = -6098
292803
YDOT = 8459
199210 feet/sec YDOT = 2578
363919 meter/sec
ZDOT = -10607
476335 ZDOT = -3233
158787
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 14359
54247782
00016717 00000-0 10270-3 0 9109
2 25544 51
6452 230
5488 0006824 174
8221 185
3002 15
52737765 41024
Satellite: ISS
Catalog Number: 25544
Epoch time: 14359
54247782 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 230
5488 deg
Eccentricity:
0006824
Arg of perigee: 174
8221 deg
Mean anomaly: 185
3002 deg
Mean motion: 15
52737765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4102
Checksum: 307
Coasting Arc #12 (Orbit 4116)
---------------------------------------
Vector Time (GMT): 2014/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5551665
65 A = 6787580
80 meter
Y = -1377221
90 meter E =
0009744
Z = -3666389
08 I = 51
38614
XDOT = -1325
937848 Wp = 144
60401
YDOT = -6175
960201 meter/sec RA = 224
72575 deg
ZDOT = 4325
651514 TA = 171
71561
MA = 171
69951
Ha = 224
501 n
mi
Hp = 216
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18214126
13 X = -5518042
72
Y = -4518444
56 feet Y = -1439116
07 meter
Z = -12028835
57 Z = -3693276
32
XDOT = -4350
189791 XDOT = -1277
790609
YDOT = -20262
336616 feet/sec YDOT = -6190
518684 meter/sec
ZDOT = 14191
770060 ZDOT = 4319
327052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3218918
66 X = 981126
41
Y = -18413080
76 feet Y = -5612307
02 meter
Z = -12143337
13 Z = -3701289
16
XDOT = 18551
505970 XDOT = 5654
499020
YDOT = -6103
461561 feet/sec YDOT = -1860
335084 meter/sec
ZDOT = 14165
845505 ZDOT = 4317
749710
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 14360
50788662
00016717 00000-0 10270-3 0 9115
2 25544 51
6445 225
7454 0006856 179
0684 181
0481 15
52740140 41171
Satellite: ISS
Catalog Number: 25544
Epoch time: 14360
50788662 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 225
7454 deg
Eccentricity:
0006856
Arg of perigee: 179
0684 deg
Mean anomaly: 181
0481 deg
Mean motion: 15
52740140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4117
Checksum: 310
Coasting Arc #13 (Orbit 4132)
---------------------------------------
Vector Time (GMT): 2014/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5866954
39 A = 6790142
56 meter
Y = 2131273
26 meter E =
0016092
Z = 2646959
43 I = 51
41847
XDOT = 300
793745 Wp = 126
67685
YDOT = 5639
209848 meter/sec RA = 219
73728 deg
ZDOT = -5194
749479 TA = 23
36208
MA = 23
28903
Ha = 224
180 n
mi
Hp = 216
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19248538
03 X = 5829828
02
Y = 6992366
33 feet Y = 2196673
68 meter
Z = 8684250
08 Z = 2675369
84
XDOT = 986
856120 XDOT = 262
946566
YDOT = 18501
344647 feet/sec YDOT = 5642
362075 meter/sec
ZDOT = -17043
141334 ZDOT = -5193
380022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5272554
92 X = -1607074
74
Y = 19735383
28 feet Y = 6015344
82 meter
Z = 8805135
69 Z = 2683805
36
XDOT = -16891
940284 XDOT = -5148
663399
YDOT = 3106
974162 feet/sec YDOT = 947
005725 meter/sec
ZDOT = -17038
260238 ZDOT = -5193
261720
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 14361
53762707
00016717 00000-0 10270-3 0 9122
2 25544 51
6448 220
6227 0006755 182
4213 177
6907 15
52800446 41338
Satellite: ISS
Catalog Number: 25544
Epoch time: 14361
53762707 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 220
6227 deg
Eccentricity:
0006755
Arg of perigee: 182
4213 deg
Mean anomaly: 177
6907 deg
Mean motion: 15
52800446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4133
Checksum: 304
Coasting Arc #14 (Orbit 4147)
---------------------------------------
Vector Time (GMT): 2014/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6033731
99 A = 6792159
30 meter
Y = -2743701
72 meter E =
0004155
Z = -1487417
51 I = 51
44913
XDOT = 853
032372 Wp = 93
27150
YDOT = -4986
389203 meter/sec RA = 214
75395 deg
ZDOT = 5751
293984 TA = 250
46947
MA = 250
51435
Ha = 224
119 n
mi
Hp = 216
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19795708
63 X = -5995377
50
Y = -9001646
08 feet Y = -2810960
34 meter
Z = -4879978
70 Z = -1516635
21
XDOT = 2798
662638 XDOT = 880
790233
YDOT = -16359
544630 feet/sec YDOT = -4976
695014 meter/sec
ZDOT = 18869
074750 ZDOT = 5755
505130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6869876
02 X = 2093938
21
Y = -20602827
47 feet Y = -6279741
81 meter
Z = -5004219
05 Z = -1525285
97
XDOT = 15046
662682 XDOT = 4586
222786
YDOT = 440
177695 feet/sec YDOT = 134
166162 meter/sec
ZDOT = 18887
895053 ZDOT = 5757
030412
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 14362
50298236
00016717 00000-0 10270-3 0 9132
2 25544 51
6438 215
8188 0006761 187
3799 172
7254 15
52814783 41485
Satellite: ISS
Catalog Number: 25544
Epoch time: 14362
50298236 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 215
8188 deg
Eccentricity:
0006761
Arg of perigee: 187
3799 deg
Mean anomaly: 172
7254 deg
Mean motion: 15
52814783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4148
Checksum: 341
Coasting Arc #15 (Orbit 4163)
---------------------------------------
Vector Time (GMT): 2014/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5961883
68 A = 6793032
67 meter
Y = 3227765
43 meter E =
0017125
Z = 200027
58 I = 51
47858
XDOT = -2115
327128 Wp = 152
47916
YDOT = 4290
646515 meter/sec RA = 209
77695 deg
ZDOT = -5997
962548 TA = 25
36056
MA = 25
27661
Ha = 223
967 n
mi
Hp = 216
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19559985
83 X = 5924375
29
Y = 10589781
60 feet Y = 3294225
36 meter
Z = 656258
47 Z = 228898
44
XDOT = -6940
049634 XDOT = -2134
012907
YDOT = 14076
924261 feet/sec YDOT = 4266
887299 meter/sec
ZDOT = -19678
354817 ZDOT = -6008
283682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8115856
25 X = -2473712
99
Y = 20704910
27 feet Y = 6310856
65 meter
Z = 778950
07 Z = 237423
98
XDOT = -13293
859527 XDOT = -4051
968384
YDOT = -4449
066386 feet/sec YDOT = -1356
075435 meter/sec
ZDOT = -19723
136680 ZDOT = -6011
612060
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 14363
53266744
00016717 00000-0 10270-3 0 9146
2 25544 51
6438 210
6959 0006829 190
7804 169
3202 15
52849157 41640
Satellite: ISS
Catalog Number: 25544
Epoch time: 14363
53266744 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 210
6959 deg
Eccentricity:
0006829
Arg of perigee: 190
7804 deg
Mean anomaly: 169
3202 deg
Mean motion: 15
52849157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4164
Checksum: 330
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list