[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 8th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
253/23:02:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 219
3
257/02:09:17
701 1
2 1
2 1
2
N/A 0
2 -0
2 227
9
000/00:02:35
402 0
1 0
0 219
8
Coasting Arc #1 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2014/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3592569
04 A = 6800413
35 meter
Y = -5751654
35 meter E =
0014805
Z = 426343
93 I = 51
97942
XDOT = 3805
348251 Wp = 118
97519
YDOT = -2834
011699 meter/sec RA = 60
82800 deg
ZDOT = -6016
480438 TA = 56
45652
MA = 56
31521
Ha = 228
235 n
mi
Hp = 219
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11786643
83 X = -3530056
72
Y = -18870257
06 feet Y = -5791479
23 meter
Z = 1398766
17 Z = 409044
11
XDOT = 12484
738356 XDOT = 3865
981798
YDOT = -9297
938644 feet/sec YDOT = -2791
119173 meter/sec
ZDOT = -19739
109047 ZDOT = -5997
847361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6020176
43 X = 1834949
78
Y = 21423514
21 feet Y = 6529887
13 meter
Z = 1326135
62 Z = 404206
14
XDOT = -13151
029233 XDOT = -4008
433710
YDOT = 4944
723560 feet/sec YDOT = 1507
151741 meter/sec
ZDOT = -19659
308287 ZDOT = -5992
157166
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 14248
53306125
00016717 00000-0 10270-3 0 9001
2 25544 51
6425 61
3613 0003390 71
4313 288
7205 15
50299690 23798
Satellite: ISS
Catalog Number: 25544
Epoch time: 14248
53306125 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 61
3613 deg
Eccentricity:
0003390
Arg of perigee: 71
4313 deg
Mean anomaly: 288
7205 deg
Mean motion: 15
50299690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 293
Coasting Arc #2 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2014/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3823041
10 A = 6800521
38 meter
Y = 5616712
05 meter E =
0015027
Z = -20782
46 I = 51
96351
XDOT = -3898
004347 Wp = 52
87030
YDOT = 2664
398482 meter/sec RA = 55
89576 deg
ZDOT = 6035
382269 TA = 306
90718
MA = 307
04478
Ha = 228
313 n
mi
Hp = 219
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12542785
76 X = 3760050
55
Y = 18427532
96 feet Y = 5659111
56 meter
Z = -68183
93 Z = -2364
37
XDOT = -12788
728172 XDOT = -3956
826114
YDOT = 8741
464837 feet/sec YDOT = 2620
480076 meter/sec
ZDOT = 19801
122931 ZDOT = 6016
303481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7225946
01 X = -2202468
34
Y = -21087572
49 feet Y = -6427492
10 meter
Z = 9226
47 Z = 2812
23
XDOT = 13227
205202 XDOT = 4031
652146
YDOT = -4491
952075 feet/sec YDOT = -1369
146992 meter/sec
ZDOT = 19719
452616 ZDOT = 6010
489157
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 14249
56445908
00016717 00000-0 10270-3 0 9019
2 25544 51
6423 56
2485 0003424 80
6941 279
4596 15
50286636 23957
Satellite: ISS
Catalog Number: 25544
Epoch time: 14249
56445908 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 56
2485 deg
Eccentricity:
0003424
Arg of perigee: 80
6941 deg
Mean anomaly: 279
4596 deg
Mean motion: 15
50286636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 330
Coasting Arc #3 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2014/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3993603
14 A = 6800228
29 meter
Y = -5480277
39 meter E =
0013180
Z = -446623
53 I = 51
94492
XDOT = 4052
937280 Wp = 124
93778
YDOT = -2474
325257 meter/sec RA = 50
96282 deg
ZDOT = -6012
071082 TA = 59
84994
MA = 59
71940
Ha = 228
184 n
mi
Hp = 219
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13102372
52 X = -3929855
08
Y = -17979912
69 feet Y = -5524580
05 meter
Z = -1465300
28 Z = -465868
21
XDOT = 13297
038320 XDOT = 4109
508860
YDOT = -8117
865018 feet/sec YDOT = -2428
687016 meter/sec
ZDOT = -19724
642657 ZDOT = -5992
245078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8231235
71 X = 2508880
64
Y = 20662826
64 feet Y = 6298029
56 meter
Z = -1546248
61 Z = -471296
58
XDOT = -13507
191437 XDOT = -4116
991950
YDOT = 3941
914832 feet/sec YDOT = 1201
495641 meter/sec
ZDOT = -19639
825535 ZDOT = -5986
218823
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 14250
53137276
00016717 00000-0 10270-3 0 9025
2 25544 51
6423 51
4553 0003447 79
1608 280
9930 15
50353642 24107
Satellite: ISS
Catalog Number: 25544
Epoch time: 14250
53137276 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 51
4553 deg
Eccentricity:
0003447
Arg of perigee: 79
1608 deg
Mean anomaly: 280
9930 deg
Mean motion: 15
50353642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 286
Coasting Arc #4 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2014/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4163119
27 A = 6799974
20 meter
Y = 5296856
26 meter E =
0016432
Z = 869932
08 I = 51
92455
XDOT = -4227
903480 Wp = 60
90438
YDOT = 2332
878824 meter/sec RA = 46
02818 deg
ZDOT = 5951
521235 TA = 308
45819
MA = 308
60553
Ha = 228
208 n
mi
Hp = 219
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13658527
78 X = 4099353
38
Y = 17378137
32 feet Y = 5343054
52 meter
Z = 2854107
89 Z = 890000
17
XDOT = -13871
074409 XDOT = -4282
586322
YDOT = 7653
801916 feet/sec YDOT = 2285
294672 meter/sec
ZDOT = 19525
988305 ZDOT = 5930
849780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9257020
63 X = -2821539
89
Y = -20059243
44 feet Y = -6114057
40 meter
Z = 2938586
67 Z = 895681
22
XDOT = 13920
935678 XDOT = 4243
101195
YDOT = -3540
859349 feet/sec YDOT = -1079
253930 meter/sec
ZDOT = 19437
599896 ZDOT = 5924
580448
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 14251
56272844
00016717 00000-0 10270-3 0 9031
2 25544 51
6431 46
3426 0003460 87
6809 272
4738 15
50358966 24263
Satellite: ISS
Catalog Number: 25544
Epoch time: 14251
56272844 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 46
3426 deg
Eccentricity:
0003460
Arg of perigee: 87
6809 deg
Mean anomaly: 272
4738 deg
Mean motion: 15
50358966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 318
Coasting Arc #5 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2014/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4262133
12 A = 6799381
23 meter
Y = -5119562
35 meter E =
0010996
Z = -1348101
88 I = 51
90085
XDOT = 4456
291997 Wp = 126
80241
YDOT = -2183
873062 meter/sec RA = 41
09198 deg
ZDOT = -5834
731949 TA = 67
79657
MA = 67
67994
Ha = 228
121 n
mi
Hp = 219
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13983376
37 X = -4198019
61
Y = -16796464
40 feet Y = -5166865
98 meter
Z = -4422906
43 Z = -1368650
17
XDOT = 14620
380568 XDOT = 4508
724458
YDOT = -7164
937869 feet/sec YDOT = -2133
747555 meter/sec
ZDOT = -19142
821355 ZDOT = -5812
956388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10032928
65 X = 3058036
65
Y = 19396477
08 feet Y = 5912046
21 meter
Z = -4509451
40 Z = -1374480
79
XDOT = -14519
274513 XDOT = -4425
474871
YDOT = 3110
725130 feet/sec YDOT = 948
149019 meter/sec
ZDOT = -19049
763781 ZDOT = -5806
368000
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 14252
52960373
00016717 00000-0 10270-3 0 9040
2 25544 51
6432 41
5492 0003476 86
7434 273
4114 15
50402087 24415
Satellite: ISS
Catalog Number: 25544
Epoch time: 14252
52960373 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 41
5492 deg
Eccentricity:
0003476
Arg of perigee: 86
7434 deg
Mean anomaly: 273
4114 deg
Mean motion: 15
50402087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 289
Coasting Arc #6 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2014/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4349408
12 A = 6798724
03 meter
Y = 4904268
65 meter E =
0017045
Z = 1776174
21 I = 51
87620
XDOT = -4697
057051 Wp = 70
70715
YDOT = 2092
845337 meter/sec RA = 36
15416 deg
ZDOT = 5684
340423 TA = 308
71032
MA = 308
86261
Ha = 228
066 n
mi
Hp = 219
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14269711
68 X = 4285616
12
Y = 16090120
26 feet Y = 4952550
11 meter
Z = 5827343
22 Z = 1797147
39
XDOT = -15410
292162 XDOT = -4747
723311
YDOT = 6866
290476 feet/sec YDOT = 2040
037291 meter/sec
ZDOT = 18649
410838 ZDOT = 5661
399457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10776518
93 X = -3284682
97
Y = -18583471
78 feet Y = -5664242
20 meter
Z = 5915723
67 Z = 1803112
57
XDOT = 15222
458173 XDOT = 4639
805251
YDOT = -2881
894315 feet/sec YDOT = -878
401387 meter/sec
ZDOT = 18551
413921 ZDOT = 5654
470963
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 14253
56091599
00016717 00000-0 10270-3 0 9051
2 25544 51
6446 36
4369 0003443 93
6848 266
4696 15
50433506 24570
Satellite: ISS
Catalog Number: 25544
Epoch time: 14253
56091599 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 36
4369 deg
Eccentricity:
0003443
Arg of perigee: 93
6848 deg
Mean anomaly: 266
4696 deg
Mean motion: 15
50433506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 335
Coasting Arc #7 (Orbit 2463)
---------------------------------------
Vector Time (GMT): 2014/253/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 35228
16 A = 6789872
65 meter
Y = 4677295
83 meter E =
0009544
Z = 4915133
56 I = 51
83394
XDOT = -6891
284598 Wp = 109
04630
YDOT = -2413
636106 meter/sec RA = 33
88802 deg
ZDOT = 2339
490888 TA = 318
08169
MA = 318
15472
Ha = 228
060 n
mi
Hp = 219
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 115577
95 X = -40953
23
Y = 15345458
75 feet Y = 4677264
47 meter
Z = 16125766
28 Z = 4915119
04
XDOT = -22609
201437 XDOT = -6875
147093
YDOT = -7918
753628 feet/sec YDOT = -2490
608368 meter/sec
ZDOT = 7675
495038 ZDOT = 2306
053486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6577733
65 X = -2004893
22
Y = 13865739
87 feet Y = 4226277
51 meter
Z = 16124871
43 Z = 4914860
81
XDOT = -16050
224196 XDOT = -4892
108335
YDOT = -16400
842206 feet/sec YDOT = -4998
976704 meter/sec
ZDOT = 7533
636413 ZDOT = 2296
252379
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 14254
01210830
00016717 00000-0 10270-3 0 9064
2 25544 51
6434 34
2044 0003356 85
1027 275
0507 15
50433832 24648
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
01210830 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 34
2044 deg
Eccentricity:
0003356
Arg of perigee: 85
1027 deg
Mean anomaly: 275
0507 deg
Mean motion: 15
50433832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2464
Checksum: 266
Coasting Arc #8 (Orbit 2478)
---------------------------------------
Vector Time (GMT): 2014/254/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 148723
51 A = 6789135
14 meter
Y = -4499724
87 meter E =
0016634
Z = -5096599
69 I = 51
80563
XDOT = 7072
980777 Wp = 78
50404
YDOT = 2282
831109 meter/sec RA = 28
93941 deg
ZDOT = -1810
872005 TA = 173
97577
MA = 173
95574
Ha = 228
062 n
mi
Hp = 219
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 487938
03 X = 223787
17
Y = -14762876
87 feet Y = -4497642
65 meter
Z = -16721127
58 Z = -5095694
34
XDOT = 23205
317511 XDOT = 7055
724623
YDOT = 7489
603376 feet/sec YDOT = 2361
829054 meter/sec
ZDOT = -5941
181119 ZDOT = -1776
554512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6649997
12 X = 2026919
12
Y = -13195224
85 feet Y = -4021904
54 meter
Z = -16716468
04 Z = -5095179
46
XDOT = 17097
220345 XDOT = 5211
232761
YDOT = 15951
220935 feet/sec YDOT = 4861
932141 meter/sec
ZDOT = -5795
565939 ZDOT = -1766
488498
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 14254
97893473
00016717 00000-0 10270-3 0 9070
2 25544 51
6439 29
4108 0003457 87
3098 272
8448 15
50445950 24793
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
97893473 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 29
4108 deg
Eccentricity:
0003457
Arg of perigee: 87
3098 deg
Mean anomaly: 272
8448 deg
Mean motion: 15
50445950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2479
Checksum: 347
Coasting Arc #9 (Orbit 2494)
---------------------------------------
Vector Time (GMT): 2014/255/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -358263
46 A = 6788424
64 meter
Y = 4331338
85 meter E =
0007044
Z = 5209377
72 I = 51
77642
XDOT = -7254
358732 Wp = 107
75714
YDOT = -2132
748243 meter/sec RA = 23
98980 deg
ZDOT = 1270
861424 TA = 330
04280
MA = 330
08309
Ha = 227
951 n
mi
Hp = 219
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1175405
05 X = -431976
48
Y = 14210429
31 feet Y = 4326920
90 meter
Z = 17091134
26 Z = 5207457
83
XDOT = -23800
389541 XDOT = -7236
144156
YDOT = -6997
205523 feet/sec YDOT = -2213
769201 meter/sec
ZDOT = 4169
492861 ZDOT = 1235
665053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6834880
83 X = -2083271
68
Y = 12526299
79 feet Y = 3818016
17 meter
Z = 17082182
71 Z = 5206649
29
XDOT = -18157
656770 XDOT = -5534
453783
YDOT = -15405
563386 feet/sec YDOT = -4695
615720 meter/sec
ZDOT = 4020
121563 ZDOT = 1225
333052
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 14256
01019293
00016717 00000-0 10270-3 0 9088
2 25544 51
6443 24
2989 0003317 88
5550 271
5980 15
50500612 24951
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
01019293 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 24
2989 deg
Eccentricity:
0003317
Arg of perigee: 88
5550 deg
Mean anomaly: 271
5980 deg
Mean motion: 15
50500612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2495
Checksum: 303
Coasting Arc #10 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2014/256/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 620269
68 A = 6788040
45 meter
Y = -4209937
11 meter E =
0017962
Z = -5304219
24 I = 51
74660
XDOT = 7361
121922 Wp = 85
58620
YDOT = 1959
826150 meter/sec RA = 19
03600 deg
ZDOT = -695
391010 TA = 177
76991
MA = 177
76189
Ha = 227
914 n
mi
Hp = 219
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2035005
51 X = 693066
38
Y = -13812129
62 feet Y = -4202594
29 meter
Z = -17402294
09 Z = -5301028
85
XDOT = 24150
662475 XDOT = 7342
037599
YDOT = 6429
875820 feet/sec YDOT = 2042
036208 meter/sec
ZDOT = -2281
466569 ZDOT = -659
678081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7262263
01 X = 2213537
77
Y = -11944646
85 feet Y = -3640728
36 meter
Z = -17387954
43 Z = -5299848
51
XDOT = 19000
309728 XDOT = 5791
294405
YDOT = 14649
257487 feet/sec YDOT = 4465
093682 meter/sec
ZDOT = -2129
874790 ZDOT = -649
185836
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 14256
97697695
00016717 00000-0 10270-3 0 9092
2 25544 51
6446 19
5051 0003349 90
6648 269
4887 15
50515115 25102
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
97697695 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 19
5051 deg
Eccentricity:
0003349
Arg of perigee: 90
6648 deg
Mean anomaly: 269
4887 deg
Mean motion: 15
50515115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2510
Checksum: 338
Coasting Arc #11 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2014/257/02:10:35
402
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1868329
74 A = 6788569
76 meter
Y = -3800107
12 meter E =
0017123
Z = -5320817
85 I = 51
74499
XDOT = 7107
064041 Wp = 93
27548
YDOT = 2783
385445 meter/sec RA = 18
37825 deg
ZDOT = 508
122520 TA = 181
57424
MA = 181
57964
Ha = 227
888 n
mi
Hp = 219
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6129690
75 X = 1936531
50
Y = -12467543
06 feet Y = -3778833
38 meter
Z = -17456751
49 Z = -5311575
74
XDOT = 23317
139241 XDOT = 7072
943060
YDOT = 9131
842012 feet/sec YDOT = 2862
670494 meter/sec
ZDOT = 1667
068636 ZDOT = 542
564669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 433441
77 X = 132113
05
Y = -13936293
87 feet Y = -4247782
37 meter
Z = -17416737
71 Z = -5308621
65
XDOT = 23970
956448 XDOT = 7306
347525
YDOT = -1518
476700 feet/sec YDOT = -462
831698 meter/sec
ZDOT = 1813
102755 ZDOT = 552
633720
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 14257
10588027
00016717 00000-0 10270-3 0 9108
2 25544 51
6470 18
8667 0002441 90
3239 269
8191 15
50320415 25120
Satellite: ISS
Catalog Number: 25544
Epoch time: 14257
10588027 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 18
8667 deg
Eccentricity:
0002441
Arg of perigee: 90
3239 deg
Mean anomaly: 269
8191 deg
Mean motion: 15
50320415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 292
Coasting Arc #12 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2014/258/02:10:35
402
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2080370
53 A = 6788638
45 meter
Y = 3762911
81 meter E =
0005772
Z = 5249014
63 I = 51
71567
XDOT = -7162
902086 Wp = 69
62694
YDOT = -2535
903342 meter/sec RA = 13
42487 deg
ZDOT = -1018
104475 TA = 30
13000
MA = 30
09681
Ha = 227
802 n
mi
Hp = 219
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6825362
62 X = -2147791
75
Y = 12345511
18 feet Y = 3739271
19 meter
Z = 17221176
62 Z = 5238744
41
XDOT = -23500
334929 XDOT = -7129
067028
YDOT = -8319
892855 feet/sec YDOT = -2615
814442 meter/sec
ZDOT = -3340
237780 ZDOT = -1052
818552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -871798
81 X = -265724
28
Y = 14133784
70 feet Y = 4307977
58 meter
Z = 17176793
71 Z = 5235486
72
XDOT = -23729
576962 XDOT = -7232
775058
YDOT = 2786
106694 feet/sec YDOT = 849
205320 meter/sec
ZDOT = -3487
466731 ZDOT = -1062
979860
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 14258
13723366
00016717 00000-0 10270-3 0 9110
2 25544 51
6467 13
7549 0002287 91
6137 268
5276 15
50385193 25289
Satellite: ISS
Catalog Number: 25544
Epoch time: 14258
13723366 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 13
7549 deg
Eccentricity:
0002287
Arg of perigee: 91
6137 deg
Mean anomaly: 268
5276 deg
Mean motion: 15
50385193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 323
Coasting Arc #13 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2014/259/02:10:35
402
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2307811
95 A = 6789081
62 meter
Y = -3778836
45 meter E =
0015901
Z = -5160644
92 I = 51
68718
XDOT = 7141
326331 Wp = 100
14305
YDOT = 2281
124276 meter/sec RA = 8
46885 deg
ZDOT = 1524
505718 TA = 184
56234
MA = 184
57685
Ha = 227
749 n
mi
Hp = 219
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7571561
52 X = 2374965
01
Y = -12397757
39 feet Y = -3752653
92 meter
Z = -16931249
73 Z = -5149270
50
XDOT = 23429
548329 XDOT = 7107
881951
YDOT = 7484
003530 feet/sec YDOT = 2360
796323 meter/sec
ZDOT = 5001
659181 ZDOT = 1559
115871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1269590
55 X = 386971
20
Y = -14528618
89 feet Y = -4428323
04 meter
Z = -16882165
82 Z = -5145684
14
XDOT = 23201
279843 XDOT = 7071
750096
YDOT = -3950
172355 feet/sec YDOT = -1204
012534 meter/sec
ZDOT = 5148
486835 ZDOT = 1569
258787
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 14259
10410839
00016717 00000-0 10270-3 0 9127
2 25544 51
6473 8
9620 0002357 93
2308 266
9112 15
50389191 25438
Satellite: ISS
Catalog Number: 25544
Epoch time: 14259
10410839 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 8
9620 deg
Eccentricity:
0002357
Arg of perigee: 93
2308 deg
Mean anomaly: 266
9112 deg
Mean motion: 15
50389191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 299
Coasting Arc #14 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2014/260/02:10:35
402
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2548203
50 A = 6789505
25 meter
Y = 3809082
21 meter E =
0008026
Z = 5004152
55 I = 51
65812
XDOT = -7097
504206 Wp = 66
06767
YDOT = -2055
199335 meter/sec RA = 3
51098 deg
ZDOT = -2044
014142 TA = 43
83667
MA = 43
77300
Ha = 227
677 n
mi
Hp = 219
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8360247
71 X = -2614916
66
Y = 12496988
88 feet Y = 3780213
94 meter
Z = 16417823
34 Z = 4991611
42
XDOT = -23285
774953 XDOT = -7064
065847
YDOT = -6742
779970 feet/sec YDOT = -2134
381417 meter/sec
ZDOT = -6706
083143 ZDOT = -2078
411351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1668344
24 X = -508511
33
Y = 15001900
01 feet Y = 4572579
12 meter
Z = 16363771
57 Z = 4987677
57
XDOT = -22614
938728 XDOT = -6893
033324
YDOT = 4979
825716 feet/sec YDOT = 1517
850878 meter/sec
ZDOT = -6852
041273 ZDOT = -2088
502180
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 14260
13541662
00016717 00000-0 10270-3 0 9132
2 25544 51
6472 3
8496 0002241 93
7800 266
3607 15
50455756 25597
Satellite: ISS
Catalog Number: 25544
Epoch time: 14260
13541662 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 3
8496 deg
Eccentricity:
0002241
Arg of perigee: 93
7800 deg
Mean anomaly: 266
3607 deg
Mean motion: 15
50455756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 303
Coasting Arc #15 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2014/261/02:10:35
402
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2782996
11 A = 6790278
11 meter
Y = -3894777
25 meter E =
0013577
Z = -4828785
80 I = 51
62983
XDOT = 6978
835159 Wp = 105
80919
YDOT = 1837
227917 meter/sec RA = 358
55099 deg
ZDOT = 2542
638139 TA = 189
25641
MA = 189
28146
Ha = 227
600 n
mi
Hp = 219
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9130564
68 X = 2849798
17
Y = -12778140
59 feet Y = -3863282
91 meter
Z = -15842473
11 Z = -4815103
85
XDOT = 22896
440810 XDOT = 6945
420900
YDOT = 6027
650647 feet/sec YDOT = 1915
083165 meter/sec
ZDOT = 8341
988645 ZDOT = 2576
458869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1947068
49 X = 593466
47
Y = -15643540
14 feet Y = -4768151
04 meter
Z = -15783555
32 Z = -4810827
66
XDOT = 21786
846280 XDOT = 6640
630746
YDOT = -5841
956169 feet/sec YDOT = -1780
628240 meter/sec
ZDOT = 8485
529356 ZDOT = 2586
389348
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 14261
10224862
00016717 00000-0 10270-3 0 9141
2 25544 51
6475 359
0565 0002243 96
1113 264
0294 15
50457858 25748
Satellite: ISS
Catalog Number: 25544
Epoch time: 14261
10224862 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 359
0565 deg
Eccentricity:
0002243
Arg of perigee: 96
1113 deg
Mean anomaly: 264
0294 deg
Mean motion: 15
50457858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 303
Coasting Arc #16 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2014/262/02:10:35
402
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3023133
79 A = 6791028
90 meter
Y = 3992251
02 meter E =
0010624
Z = 4579927
72 I = 51
60196
XDOT = -6833
765881 Wp = 72
02591
YDOT = -1665
003748 meter/sec RA = 353
58946 deg
ZDOT = -3050
460133 TA = 48
52989
MA = 48
43871
Ha = 227
539 n
mi
Hp = 219
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9918417
94 X = -3089799
09
Y = 13097936
40 feet Y = 3958072
10 meter
Z = 15026009
59 Z = 4565079
51
XDOT = -22420
491735 XDOT = -6799
821440
YDOT = -5462
610722 feet/sec YDOT = -1741
233856 meter/sec
ZDOT = -10008
071301 ZDOT = -3083
574818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2198807
76 X = -670196
61
Y = 16340508
09 feet Y = 4980586
87 meter
Z = 14962117
37 Z = 4560453
38
XDOT = -20932
034483 XDOT = -6380
084110
YDOT = 6503
166657 feet/sec YDOT = 1982
165197 meter/sec
ZDOT = -10148
634650 ZDOT = -3093
303841
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 14262
13351169
00016717 00000-0 10270-3 0 9157
2 25544 51
6477 353
9439 0002175 95
9717 264
1682 15
50525676 25908
Satellite: ISS
Catalog Number: 25544
Epoch time: 14262
13351169 = yrday
fracday
Element set: 915
Inclination: 51
6477 deg
RA of node: 353
9439 deg
Eccentricity:
0002175
Arg of perigee: 95
9717 deg
Mean anomaly: 264
1682 deg
Mean motion: 15
50525676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 329
Coasting Arc #17 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2014/263/02:10:35
402
Vector Time (MET): N/A
Weight (LBS) : 911967
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3236438
54 A = 6792063
19 meter
Y = -4141063
12 meter E =
0010439
Z = -4312846
42 I = 51
57430
XDOT = 6624
485198 Wp = 107
59070
YDOT = 1515
669565 meter/sec RA = 348
62602 deg
ZDOT = 3519
801611 TA = 198
33969
MA = 198
37736
Ha = 227
453 n
mi
Hp = 219
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10618236
67 X = 3303454
65
Y = -13586165
09 feet Y = -4104496
96 meter
Z = -14149758
59 Z = -4296961
08
XDOT = 21733
875323 XDOT = 6589
946297
YDOT = 4972
669176 feet/sec YDOT = 1589
556133 meter/sec
ZDOT = 11547
905548 ZDOT = 3551
898205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2264954
69 X = 690358
19
Y = -17150209
90 feet Y = -5227383
98 meter
Z = -14081433
90 Z = -4292021
05
XDOT = 19911
805007 XDOT = 6069
118166
YDOT = -6953
047991 feet/sec YDOT = -2119
289028 meter/sec
ZDOT = 11684
159295 ZDOT = 3561
331753
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 14263
10030115
00016717 00000-0 10270-3 0 9161
2 25544 51
6475 349
1504 0002131 99
3939 260
7452 15
50525085 26050
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
10030115 = yrday
fracday
Element set: 916
Inclination: 51
6475 deg
RA of node: 349
1504 deg
Eccentricity:
0002131
Arg of perigee: 99
3939 deg
Mean anomaly: 260
7452 deg
Mean motion: 15
50525085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 285
- 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