[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 28th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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
028/18:42:24
270 1
4 -2
2 2
2
N/A 1
0 0
3 220
2
000/00:04:48
540 -1
4 -0
0 216
8
Coasting Arc #1 (Orbit 599)
---------------------------------------
Vector Time (GMT): 2015/026/13:33:24
481
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2929316
41 A = 6780170
61 meter
Y = -3495206
32 meter E =
0010246
Z = -5025971
34 I = 51
97385
XDOT = 3925
020291 Wp = 47
54013
YDOT = 6249
209168 meter/sec RA = 70
44072 deg
ZDOT = -2054
173409 TA = 202
53454
MA = 202
57957
Ha = 221
065 n
mi
Hp = 217
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9610618
14 X = 2992596
96
Y = -11467212
35 feet Y = -3462095
09 meter
Z = -16489407
28 Z = -5011587
65
XDOT = 12877
363159 XDOT = 3864
826758
YDOT = 20502
654750 feet/sec YDOT = 6292
764693 meter/sec
ZDOT = -6739
414073 ZDOT = -2035
252945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14312455
02 X = 4362436
29
Y = -4589398
80 feet Y = -1398848
75 meter
Z = -16427189
12 Z = -5007007
24
XDOT = -223
098980 XDOT = -68
000569
YDOT = 23189
401339 feet/sec YDOT = 7068
129528 meter/sec
ZDOT = -6659
603880 ZDOT = -2029
847263
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 15026
58448633
00016717 00000-0 10270-3 0 9002
2 25544 51
6457 71
0684 0005930 307
3895 52
6717 15
53630755 6002
Satellite: ISS
Catalog Number: 25544
Epoch time: 15026
58448633 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 71
0684 deg
Eccentricity:
0005930
Arg of perigee: 307
3895 deg
Mean anomaly: 52
6717 deg
Mean motion: 15
53630755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 600
Checksum: 308
Coasting Arc #2 (Orbit 615)
---------------------------------------
Vector Time (GMT): 2015/027/13:33:24
481
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3645637
09 A = 6778748
59 meter
Y = 2060897
78 meter E =
0003876
Z = 5331926
85 I = 51
95684
XDOT = -3409
174626 Wp = 330
27614
YDOT = -6859
575035 meter/sec RA = 65
46817 deg
ZDOT = 323
762659 TA = 116
67000
MA = 116
63030
Ha = 221
320 n
mi
Hp = 216
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11960751
60 X = -3694311
85
Y = 6761475
64 feet Y = 2019857
78 meter
Z = 17493198
32 Z = 5314098
97
XDOT = -11184
956121 XDOT = -3333
788573
YDOT = -22505
167438 feet/sec YDOT = -6897
277133 meter/sec
ZDOT = 1062
213449 ZDOT = 307
384861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13830559
72 X = -4215554
60
Y = -412492
99 feet Y = -125727
86 meter
Z = 17416503
28 Z = 5308550
20
XDOT = 1954
167601 XDOT = 595
630285
YDOT = -24047
197452 feet/sec YDOT = -7329
585783 meter/sec
ZDOT = 993
413079 ZDOT = 302
792307
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 15027
61363941
00016717 00000-0 10270-3 0 9016
2 25544 51
6446 65
9411 0005914 312
4508 47
6144 15
53657534 6169
Satellite: ISS
Catalog Number: 25544
Epoch time: 15027
61363941 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 65
9411 deg
Eccentricity:
0005914
Arg of perigee: 312
4508 deg
Mean anomaly: 47
6144 deg
Mean motion: 15
53657534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 616
Checksum: 299
Coasting Arc #3 (Orbit 630)
---------------------------------------
Vector Time (GMT): 2015/028/13:33:24
481
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4328949
34 A = 6779415
72 meter
Y = -600107
72 meter E =
0009472
Z = -5190371
40 I = 51
94567
XDOT = 2688
475116 Wp = 79
48380
YDOT = 7029
337525 meter/sec RA = 60
49505 deg
ZDOT = 1433
451376 TA = 204
23976
MA = 204
28435
Ha = 221
433 n
mi
Hp = 216
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14202589
71 X = 4360550
78
Y = -1968857
35 feet Y = -551521
88 meter
Z = -17028777
54 Z = -5169265
66
XDOT = 8820
456416 XDOT = 2602
708499
YDOT = 23062
130989 feet/sec YDOT = 7058
922249 meter/sec
ZDOT = 4702
924462 ZDOT = 1446
303046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13379759
86 X = 4078150
80
Y = 5444658
64 feet Y = 1659531
95 meter
Z = -16938327
45 Z = -5162802
21
XDOT = -3514
176828 XDOT = -1071
121097
YDOT = 23393
517115 feet/sec YDOT = 7130
344017 meter/sec
ZDOT = 4756
588291 ZDOT = 1449
808111
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 15028
57845745
00016717 00000-0 10270-3 0 9020
2 25544 51
6452 61
1355 0006040 315
7940 44
2726 15
53657682 6318
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
57845745 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 61
1355 deg
Eccentricity:
0006040
Arg of perigee: 315
7940 deg
Mean anomaly: 44
2726 deg
Mean motion: 15
53657682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 631
Checksum: 302
Coasting Arc #4 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2015/028/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -895653
39 A = 6781515
28 meter
Y = 5142886
59 meter E =
0003796
Z = 4325215
98 I = 51
95363
XDOT = -5543
514746 Wp = 84
95564
YDOT = -3944
203300 meter/sec RA = 59
45769 deg
ZDOT = 3539
570180 TA = 329
15493
MA = 329
17723
Ha = 220
191 n
mi
Hp = 216
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2938495
37 X = -974105
85
Y = 16872987
49 feet Y = 5132432
13 meter
Z = 14190341
15 Z = 4320674
60
XDOT = -18187
384336 XDOT = -5516
191459
YDOT = -12940
299541 feet/sec YDOT = -4006
041736 meter/sec
ZDOT = 11612
763059 ZDOT = 3512
707484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10532721
47 X = 3210373
50
Y = 13526766
88 feet Y = 4122958
55 meter
Z = 14169918
84 Z = 4318991
26
XDOT = -20841
125401 XDOT = -6352
375022
YDOT = 4174
794184 feet/sec YDOT = 1272
477267 meter/sec
ZDOT = 11498
541723 ZDOT = 3504
755517
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 15028
83572381
00016717 00000-0 10270-3 0 9033
2 25544 51
6451 59
8530 0006398 301
3253 58
7273 15
54093666 6358
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
83572381 = yrday
fracday
Element set: 903
Inclination: 51
6451 deg
RA of node: 59
8530 deg
Eccentricity:
0006398
Arg of perigee: 301
3253 deg
Mean anomaly: 58
7273 deg
Mean motion: 15
54093666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 315
Coasting Arc #5 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2015/029/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2062312
75 A = 6778429
02 meter
Y = -3979066
42 meter E =
0010293
Z = -5093843
31 I = 51
92719
XDOT = 5400
158608 Wp = 48
21342
YDOT = 5123
520606 meter/sec RA = 54
48413 deg
ZDOT = -1811
596780 TA = 204
28216
MA = 204
33070
Ha = 220
314 n
mi
Hp = 216
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6766117
95 X = 2131397
99
Y = -13054679
85 feet Y = -3955617
95 meter
Z = -16712084
34 Z = -5083657
38
XDOT = 17717
055802 XDOT = 5351
264790
YDOT = 16809
450808 feet/sec YDOT = 5183
635336 meter/sec
ZDOT = -5943
558989 ZDOT = -1785
482890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5361184
36 X = -1634088
99
Y = -13745677
19 feet Y = -4189682
41 meter
Z = -16667718
55 Z = -5080320
62
XDOT = 23328
644088 XDOT = 7110
570718
YDOT = -2008
854131 feet/sec YDOT = -612
298739 meter/sec
ZDOT = -5832
774940 ZDOT = -1777
829802
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 15029
80027610
00016717 00000-0 10270-3 0 9042
2 25544 51
6456 55
0448 0006396 306
1622 53
8939 15
54119433 6503
Satellite: ISS
Catalog Number: 25544
Epoch time: 15029
80027610 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 55
0448 deg
Eccentricity:
0006396
Arg of perigee: 306
1622 deg
Mean anomaly: 53
8939 deg
Mean motion: 15
54119433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 299
Coasting Arc #6 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2015/030/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3263099
75 A = 6777260
60 meter
Y = 2618423
86 meter E =
0005131
Z = 5334105
29 I = 51
90435
XDOT = -4911
752396 Wp = 328
48036
YDOT = -5885
936852 meter/sec RA = 49
50374 deg
ZDOT = -111
206554 TA = 122
60048
MA = 122
55094
Ha = 220
477 n
mi
Hp = 216
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10705707
84 X = -3318047
72
Y = 8590629
46 feet Y = 2581626
45 meter
Z = 17500345
42 Z = 5318120
62
XDOT = -16114
673215 XDOT = -4845
029225
YDOT = -19310
816444 feet/sec YDOT = -5940
490190 meter/sec
ZDOT = -364
850898 ZDOT = -134
904526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -358114
75 X = -109153
38
Y = 13809076
53 feet Y = 4209006
53 meter
Z = 17431418
30 Z = 5313096
30
XDOT = -24142
674834 XDOT = -7358
687289
YDOT = -21
426678 feet/sec YDOT = -6
530851 meter/sec
ZDOT = -465
141006 ZDOT = -141
774979
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 15030
82911598
00016717 00000-0 10270-3 0 9054
2 25544 51
6454 49
9164 0006527 309
0852 50
9720 15
54160767 6660
Satellite: ISS
Catalog Number: 25544
Epoch time: 15030
82911598 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 49
9164 deg
Eccentricity:
0006527
Arg of perigee: 309
0852 deg
Mean anomaly: 50
9720 deg
Mean motion: 15
54160767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 318
Coasting Arc #7 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2015/031/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4385231
85 A = 6778666
27 meter
Y = -1220519
03 meter E =
0007681
Z = -5029160
60 I = 51
88818
XDOT = 4036
414249 Wp = 81
09245
YDOT = 6192
554633 meter/sec RA = 44
52157 deg
ZDOT = 2020
521127 TA = 208
46596
MA = 208
50793
Ha = 220
664 n
mi
Hp = 216
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14387243
61 X = 4422983
36
Y = -4004327
53 feet Y = -1171269
38 meter
Z = -16499870
72 Z = -5007766
73
XDOT = 13242
828900 XDOT = 3957
052914
YDOT = 20316
780292 feet/sec YDOT = 6237
248688 meter/sec
ZDOT = 6629
006322 ZDOT = 2039
936161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5997680
80 X = 1828093
11
Y = -13786824
30 feet Y = -4202224
05 meter
Z = -16408060
59 Z = -5001176
87
XDOT = 23093
261999 XDOT = 7038
826257
YDOT = 2074
310241 feet/sec YDOT = 632
249761 meter/sec
ZDOT = 6710
899627 ZDOT = 2045
482206
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 15031
79364230
00016717 00000-0 10270-3 0 9067
2 25544 51
6459 45
1077 0006463 313
6878 46
3748 15
54150891 6817
Satellite: ISS
Catalog Number: 25544
Epoch time: 15031
79364230 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 45
1077 deg
Eccentricity:
0006463
Arg of perigee: 313
6878 deg
Mean anomaly: 46
3748 deg
Mean motion: 15
54150891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 318
Coasting Arc #8 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2015/032/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5336015
95 A = 6781905
55 meter
Y = -148261
79 meter E =
0009292
Z = 4183308
84 I = 51
87562
XDOT = -2770
756176 Wp = 37
72111
YDOT = -6092
511102 meter/sec RA = 39
54474 deg
ZDOT = -3738
613811 TA = 90
64159
MA = 90
53512
Ha = 220
764 n
mi
Hp = 216
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17506614
01 X = -5354281
96
Y = -486423
19 feet Y = -208034
72 meter
Z = 13724766
52 Z = 4157343
73
XDOT = -9090
407402 XDOT = -2684
261982
YDOT = -19988
553484 feet/sec YDOT = -6123
011884 meter/sec
ZDOT = -12265
793342 ZDOT = -3751
863219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11208351
15 X = -3416305
43
Y = 13569397
53 feet Y = 4135952
37 meter
Z = 13613657
59 Z = 4149442
83
XDOT = -20313
334160 XDOT = -6191
504252
YDOT = -4379
034788 feet/sec YDOT = -1334
729803 meter/sec
ZDOT = -12321
311721 ZDOT = -3755
535813
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 15032
82245449
00016717 00000-0 10270-3 0 9073
2 25544 51
6455 39
9789 0006445 317
9161 42
1496 15
54171861 6977
Satellite: ISS
Catalog Number: 25544
Epoch time: 15032
82245449 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 39
9789 deg
Eccentricity:
0006445
Arg of perigee: 317
9161 deg
Mean anomaly: 42
1496 deg
Mean motion: 15
54171861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 334
Coasting Arc #9 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2015/033/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5976627
96 A = 6785608
07 meter
Y = 1346292
86 meter E =
0007128
Z = -2908091
12 I = 51
86417
XDOT = 1186
999510 Wp =
20269
YDOT = 5640
961456 meter/sec RA = 34
57545 deg
ZDOT = 5057
939366 TA = 326
75926
MA = 326
80402
Ha = 220
908 n
mi
Hp = 215
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19608359
44 X = 5975255
27
Y = 4416971
31 feet Y = 1413119
68 meter
Z = -9540981
36 Z = -2879061
89
XDOT = 3894
355347 XDOT = 1099
263758
YDOT = 18507
091392 feet/sec YDOT = 5653
744776 meter/sec
ZDOT = 16594
289258 ZDOT = 5063
492255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15361658
56 X = 4682233
53
Y = -13052486
13 feet Y = -3978397
77 meter
Z = -9416993
83 Z = -2870299
72
XDOT = 16111
409033 XDOT = 4910
757473
YDOT = 6989
843583 feet/sec YDOT = 2130
504324 meter/sec
ZDOT = 16616
950615 ZDOT = 5064
846548
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 15033
78695154
00016717 00000-0 10270-3 0 9082
2 25544 51
6462 35
1697 0006478 321
1755 38
8932 15
54205275 7125
Satellite: ISS
Catalog Number: 25544
Epoch time: 15033
78695154 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 35
1697 deg
Eccentricity:
0006478
Arg of perigee: 321
1755 deg
Mean anomaly: 38
8932 deg
Mean motion: 15
54205275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 321
Coasting Arc #10 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2015/034/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6226057
91 A = 6788477
70 meter
Y = -2366963
13 meter E =
0008302
Z = 1297029
51 I = 51
84710
XDOT = 644
927424 Wp = 102
97479
YDOT = -4916
166391 meter/sec RA = 29
61469 deg
ZDOT = -5846
111390 TA = 62
95787
MA = 62
87315
Ha = 220
931 n
mi
Hp = 215
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20426699
19 X = -6205427
57
Y = -7765627
06 feet Y = -2436471
57 meter
Z = 4255346
17 Z = 1266835
48
XDOT = 2115
903623 XDOT = 728
250728
YDOT = -16129
154827 feet/sec YDOT = -4908
488699 meter/sec
ZDOT = -19180
155480 ZDOT = -5842
775995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18305557
69 X = -5579533
98
Y = 11980855
31 feet Y = 3651764
70 meter
Z = 4126577
03 Z = 1257780
68
XDOT = -10860
269563 XDOT = -3310
210163
YDOT = -9957
880008 feet/sec YDOT = -3035
161827 meter/sec
ZDOT = -19164
915012 ZDOT = -5841
466096
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 15034
81573482
00016717 00000-0 10270-3 0 9097
2 25544 51
6462 30
0405 0006376 324
7287 35
3443 15
54190271 7287
Satellite: ISS
Catalog Number: 25544
Epoch time: 15034
81573482 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 30
0405 deg
Eccentricity:
0006376
Arg of perigee: 324
7287 deg
Mean anomaly: 35
3443 deg
Mean motion: 15
54190271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 298
Coasting Arc #11 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2015/035/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5996272
30 A = 6788905
94 meter
Y = 3131893
99 meter E =
0015330
Z = 438584
19 I = 51
82166
XDOT = -2549
472415 Wp = 24
56801
YDOT = 4030
724721 meter/sec RA = 24
65627 deg
ZDOT = 6011
370946 TA = 340
15285
MA = 340
21243
Ha = 221
042 n
mi
Hp = 215
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19672809
39 X = 5958674
65
Y = 10275242
73 feet Y = 3198738
01 meter
Z = 1438924
50 Z = 467620
72
XDOT = -8364
410811 XDOT = -2623
555720
YDOT = 13224
162469 feet/sec YDOT = 4001
800942 meter/sec
ZDOT = 19722
345622 ZDOT = 5998
806266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19699110
05 X = 6004288
74
Y = -10206563
59 feet Y = -3110960
58 meter
Z = 1562584
22 Z = 476275
67
XDOT = 5215
454684 XDOT = 1589
670588
YDOT = 13105
624601 feet/sec YDOT = 3994
594379 meter/sec
ZDOT = 19667
778966 ZDOT = 5994
739029
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 15035
84450062
00016717 00000-0 10270-3 0 9101
2 25544 51
6466 24
9107 0006588 328
7058 31
3702 15
54243202 7442
Satellite: ISS
Catalog Number: 25544
Epoch time: 15035
84450062 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 24
9107 deg
Eccentricity:
0006588
Arg of perigee: 328
7058 deg
Mean anomaly: 31
3702 deg
Mean motion: 15
54243202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 287
Coasting Arc #12 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2015/036/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5276189
07 A = 6786988
02 meter
Y = -3688532
50 meter E =
0001497
Z = -2152431
91 I = 51
78649
XDOT = 4372
786458 Wp = 40
63966
YDOT = -3041
100936 meter/sec RA = 19
69490 deg
ZDOT = -5508
515269 TA = 163
16238
MA = 163
15741
Ha = 221
112 n
mi
Hp = 215
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17310331
61 X = -5224095
43
Y = -12101484
57 feet Y = -3747243
15 meter
Z = -7061784
47 Z = -2177935
25
XDOT = 14346
412263 XDOT = 4433
225469
YDOT = -9977
365274 feet/sec YDOT = -2991
864020 meter/sec
ZDOT = -18072
556657 ZDOT = -5487
126607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19692279
55 X = -6002206
81
Y = 7534225
74 feet Y = 2296432
01 meter
Z = -7170207
63 Z = -2185479
29
XDOT = 373
335014 XDOT = 113
792512
YDOT = -16132
682729 feet/sec YDOT = -4917
241696 meter/sec
ZDOT = -17980
423416 ZDOT = -5480
433057
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 15036
80895556
00016717 00000-0 10270-3 0 9110
2 25544 51
6468 20
1022 0006522 330
8197 29
2591 15
54236359 7597
Satellite: ISS
Catalog Number: 25544
Epoch time: 15036
80895556 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 20
1022 deg
Eccentricity:
0006522
Arg of perigee: 330
8197 deg
Mean anomaly: 29
2591 deg
Mean motion: 15
54236359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 311
Coasting Arc #13 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2015/037/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4079014
63 A = 6783282
93 meter
Y = 4022601
84 meter E =
0010569
Z = 3619437
81 I = 51
74443
XDOT = -5934
522123 Wp = 59
98630
YDOT = 2040
578147 meter/sec RA = 14
72245 deg
ZDOT = 4415
713410 TA = 342
87196
MA = 342
90760
Ha = 221
234 n
mi
Hp = 215
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13382593
94 X = 4016148
27
Y = 13197512
61 feet Y = 4067864
82 meter
Z = 11874795
97 Z = 3639099
47
XDOT = -19470
216940 XDOT = -5978
348738
YDOT = 6694
810194 feet/sec YDOT = 1973
969747 meter/sec
ZDOT = 14487
248720 ZDOT = 4386
778627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18320221
74 X = 5584003
59
Y = -3956148
59 feet Y = -1205834
09 meter
Z = 11958147
96 Z = 3644843
50
XDOT = -5343
822539 XDOT = -1628
797110
YDOT = 18712
442576 feet/sec YDOT = 5703
552497 meter/sec
ZDOT = 14363
024706 ZDOT = 4377
849930
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 15037
83769234
00016717 00000-0 10270-3 0 9128
2 25544 51
6469 14
9721 0006654 336
7134 23
3716 15
54267643 7759
Satellite: ISS
Catalog Number: 25544
Epoch time: 15037
83769234 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 14
9721 deg
Eccentricity:
0006654
Arg of perigee: 336
7134 deg
Mean anomaly: 23
3716 deg
Mean motion: 15
54267643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 321
Coasting Arc #14 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2015/038/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2511010
06 A = 6779366
43 meter
Y = -4199695
33 meter E =
0012537
Z = -4703464
01 I = 51
70061
XDOT = 7044
079390 Wp = 38
08772
YDOT = -1049
254973 meter/sec RA = 9
73752 deg
ZDOT = -2818
081258 TA = 203
92392
MA = 203
98223
Ha = 221
288 n
mi
Hp = 214
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8238221
98 X = -2441014
17
Y = -13778527
99 feet Y = -4227384
10 meter
Z = -15431312
37 Z = -4715491
44
XDOT = 23110
496685 XDOT = 7068
977830
YDOT = -3442
437577 feet/sec YDOT = -970
344508 meter/sec
ZDOT = -9245
673419 ZDOT = -2783
802508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15999282
46 X = -4876581
29
Y = -416569
54 feet Y = -126970
39 meter
Z = -15481956
18 Z = -4718900
24
XDOT = 9350
816655 XDOT = 2850
128916
YDOT = -20295
681757 feet/sec YDOT = -6186
123799 meter/sec
ZDOT = -9098
784926 ZDOT = -2773
309646
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 15038
80211667
00016717 00000-0 10270-3 0 9139
2 25544 51
6465 10
1633 0006704 338
5233 21
5637 15
54314771 7905
Satellite: ISS
Catalog Number: 25544
Epoch time: 15038
80211667 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 10
1633 deg
Eccentricity:
0006704
Arg of perigee: 338
5233 deg
Mean anomaly: 21
5637 deg
Mean motion: 15
54314771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 288
Coasting Arc #15 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2015/039/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 668953
69 A = 6777008
74 meter
Y = 4225360
32 meter E =
0004751
Z = 5254714
67 I = 51
66182
XDOT = -7616
395128 Wp = 10
97049
YDOT = 86
240737 meter/sec RA = 4
74104 deg
ZDOT = 904
688110 TA = 70
40676
MA = 70
35548
Ha = 221
415 n
mi
Hp = 214
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2194729
96 X = 596129
92
Y = 13862730
70 feet Y = 4232434
25 meter
Z = 17239877
53 Z = 5257787
04
XDOT = -24988
172992 XDOT = -7621
188003
YDOT = 282
942049 feet/sec YDOT = 1
042522 meter/sec
ZDOT = 2968
136843 ZDOT = 867
678008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12950823
43 X = 3947410
98
Y = 5370609
20 feet Y = 1636961
68 meter
Z = 17252195
48 Z = 5258469
18
XDOT = -12274
192105 XDOT = -3741
173753
YDOT = 20619
025717 feet/sec YDOT = 6284
679039 meter/sec
ZDOT = 2809
760576 ZDOT = 856
415024
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 15039
83082244
00016717 00000-0 10270-3 0 9141
2 25544 51
6468 5
0337 0006611 343
1635 16
9297 15
54326241 8060
Satellite: ISS
Catalog Number: 25544
Epoch time: 15039
83082244 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 5
0337 deg
Eccentricity:
0006611
Arg of perigee: 343
1635 deg
Mean anomaly: 16
9297 deg
Mean motion: 15
54326241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 295
Coasting Arc #16 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2015/040/18:44:48
540
Vector Time (MET): N/A
Weight (LBS) : 949862
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1228517
05 A = 6777079
43 meter
Y = -4145448
64 meter E =
0013118
Z = -5228683
51 I = 51
62971
XDOT = 7532
869096 Wp = 70
54652
YDOT = 842
943892 meter/sec RA = 359
73818 deg
ZDOT = 1108
129041 TA = 210
04814
MA = 210
12348
Ha = 221
435 n
mi
Hp = 214
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4030567
74 X = 1300179
83
Y = -13600553
26 feet Y = -4131310
28 meter
Z = -17154473
47 Z = -5222541
30
XDOT = 24714
137455 XDOT = 7517
500426
YDOT = 2765
563951 feet/sec YDOT = 927
095499 meter/sec
ZDOT = 3635
593965 ZDOT = 1144
684446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9693454
61 X = -2954564
96
Y = -10401261
56 feet Y = -3170304
52 meter
Z = -17127381
04 Z = -5220425
74
XDOT = 14014
325576 XDOT = 4271
566436
YDOT = -19269
151281 feet/sec YDOT = -5873
237310 meter/sec
ZDOT = 3791
831827 ZDOT = 1155
750341
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 15040
79521793
00016717 00000-0 10270-3 0 9156
2 25544 51
6456
2238 0006652 345
9515 14
1452 15
54373097 8217
Satellite: ISS
Catalog Number: 25544
Epoch time: 15040
79521793 = yrday
fracday
Element set: 915
Inclination: 51
6456 deg
RA of node:
2238 deg
Eccentricity:
0006652
Arg of perigee: 345
9515 deg
Mean anomaly: 14
1452 deg
Mean motion: 15
54373097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 821
Checksum: 297
- 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