[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 7th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24218 8 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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 3089)
---------------------------------------
Vector Time (GMT): 2014/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5378140
12 A = 6794126
00 meter
Y = 472546
86 meter E =
0014140
Z = 4113730
45 I = 51
83436
XDOT = -3442
169537 Wp = 82
92739
YDOT = -5676
816327 meter/sec RA = 31
76736 deg
ZDOT = -3835
073743 TA = 46
64131
MA = 46
52359
Ha = 228
879 n
mi
Hp = 219
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17644816
68 X = -5403007
48
Y = 1550350
59 feet Y = 412266
21 meter
Z = 13496490
99 Z = 4087544
10
XDOT = -11293
207143 XDOT = -3359
804943
YDOT = -18624
725482 feet/sec YDOT = -5714
848526 meter/sec
ZDOT = -12582
262935 ZDOT = -3851
594789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13580659
35 X = -4139384
97
Y = -11501423
29 feet Y = -3505633
82 meter
Z = 13385864
40 Z = 4080011
47
XDOT = 4498
531115 XDOT = 1371
152284
YDOT = -20085
631582 feet/sec YDOT = -6122
100506 meter/sec
ZDOT = -12651
033205 ZDOT = -3856
034921
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 14036
54124330
00016717 00000-0 10270-3 0 9003
2 25544 51
6460 32
1708 0003756 100
5179 259
6395 15
50067791 30901
Satellite: ISS
Catalog Number: 25544
Epoch time: 14036
54124330 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 32
1708 deg
Eccentricity:
0003756
Arg of perigee: 100
5179 deg
Mean anomaly: 259
6395 deg
Mean motion: 15
50067791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 288
Coasting Arc #2 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2014/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5543659
78 A = 6794924
10 meter
Y = -625272
23 meter E =
0010074
Z = -3889570
72 I = 51
81015
XDOT = 3501
544804 Wp = 103
70895
YDOT = 5409
255745 meter/sec RA = 26
82523 deg
ZDOT = 4127
713648 TA = 209
59985
MA = 209
65690
Ha = 228
809 n
mi
Hp = 219
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18187860
19 X = 5569133
77
Y = -2051418
06 feet Y = -563137
18 meter
Z = -12761058
79 Z = -3862578
82
XDOT = 11488
007886 XDOT = 3420
746179
YDOT = 17746
902051 feet/sec YDOT = 5447
960631 meter/sec
ZDOT = 13542
367611 ZDOT = 4144
527021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14511766
49 X = 4423186
43
Y = 11283306
45 feet Y = 3439151
81 meter
Z = -12647008
51 Z = -3854808
19
XDOT = -3403
164550 XDOT = -1037
284555
YDOT = 19609
784208 feet/sec YDOT = 5977
062227 meter/sec
ZDOT = 13612
409490 ZDOT = 4149
062412
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 14037
50830336
00016717 00000-0 10270-3 0 9011
2 25544 51
6459 27
3800 0003832 103
2701 256
8877 15
50059449 31056
Satellite: ISS
Catalog Number: 25544
Epoch time: 14037
50830336 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 27
3800 deg
Eccentricity:
0003832
Arg of perigee: 103
2701 deg
Mean anomaly: 256
8877 deg
Mean motion: 15
50059449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 291
Coasting Arc #3 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2014/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5702216
78 A = 6795636
11 meter
Y = 766604
07 meter E =
0015594
Z = 3602485
96 I = 51
78470
XDOT = -3509
383641 Wp = 91
34051
YDOT = -5174
481068 meter/sec RA = 21
88048 deg
ZDOT = -4437
491295 TA = 46
17079
MA = 46
04198
Ha = 228
738 n
mi
Hp = 219
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18708060
29 X = -5727864
81
Y = 2515105
21 feet Y = 702694
91 meter
Z = 11819179
66 Z = 3574723
43
XDOT = -11513
725855 XDOT = -3429
704977
YDOT = -16976
643924 feet/sec YDOT = -5213
279837 meter/sec
ZDOT = -14558
698473 ZDOT = -4454
345514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15395961
56 X = -4692689
08
Y = -11047228
47 feet Y = -3367195
24 meter
Z = 11701854
24 Z = 3566725
17
XDOT = 2522
030127 XDOT = 768
714783
YDOT = -19067
627652 feet/sec YDOT = -5811
812908 meter/sec
ZDOT = -14628
946626 ZDOT = -4458
902932
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 14038
53981468
00016717 00000-0 10270-3 0 9029
2 25544 51
6456 22
2685 0003698 106
6661 253
4896 15
50119523 31212
Satellite: ISS
Catalog Number: 25544
Epoch time: 14038
53981468 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 22
2685 deg
Eccentricity:
0003698
Arg of perigee: 106
6661 deg
Mean anomaly: 253
4896 deg
Mean motion: 15
50119523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 315
Coasting Arc #4 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2014/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5851081
37 A = 6796436
50 meter
Y = -961270
93 meter E =
0008258
Z = -3329415
20 I = 51
75832
XDOT = 3481
295264 Wp = 95
09978
YDOT = 4934
233726 meter/sec RA = 16
93487 deg
ZDOT = 4702
722928 TA = 226
33770
MA = 226
40619
Ha = 228
687 n
mi
Hp = 219
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19196461
19 X = 5877568
64
Y = -3153776
02 feet Y = -895692
36 meter
Z = -10923278
20 Z = -3300927
54
XDOT = 11421
572387 XDOT = 3403
016845
YDOT = 16188
430861 feet/sec YDOT = 4972
726198 meter/sec
ZDOT = 15428
880997 ZDOT = 4719
444102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16370600
52 X = 4989759
04
Y = 10633442
02 feet Y = 3241073
13 meter
Z = -10802859
89 Z = -3292711
69
XDOT = -1746
102662 XDOT = -532
212091
YDOT = 18402
237768 feet/sec YDOT = 5609
002072 meter/sec
ZDOT = 15498
604476 ZDOT = 4723
974644
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 14039
50683972
00016717 00000-0 10270-3 0 9037
2 25544 51
6456 17
4773 0003813 109
6480 250
5083 15
50119323 31367
Satellite: ISS
Catalog Number: 25544
Epoch time: 14039
50683972 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 17
4773 deg
Eccentricity:
0003813
Arg of perigee: 109
6480 deg
Mean anomaly: 250
5083 deg
Mean motion: 15
50119323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 298
Coasting Arc #5 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2014/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5987287
94 A = 6797177
58 meter
Y = 1140591
29 meter E =
0016755
Z = 2990655
44 I = 51
73148
XDOT = -3399
534231 Wp = 100
60728
YDOT = -4736
779455 meter/sec RA = 11
98692 deg
ZDOT = -4978
635548 TA = 45
26293
MA = 45
12667
Ha = 228
593 n
mi
Hp = 219
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19643333
14 X = -6014124
69
Y = 3742097
40 feet Y = 1073487
60 meter
Z = 9811861
66 Z = 2961505
35
XDOT = -11153
327528 XDOT = -3322
129658
YDOT = -15540
615009 feet/sec YDOT = -4774
362510 meter/sec
ZDOT = -16334
106127 ZDOT = -4994
961628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17269870
36 X = -5263856
48
Y = -10198957
03 feet Y = -3108642
10 meter
Z = 9688617
67 Z = 2953090
67
XDOT = 1218
364671 XDOT = 371
357552
YDOT = -17709
813231 feet/sec YDOT = -5397
951073 meter/sec
ZDOT = -16402
193382 ZDOT = -4999
388543
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 14040
53831349
00016717 00000-0 10270-3 0 9046
2 25544 51
6457 12
3656 0003672 113
2209 246
9329 15
50171249 31520
Satellite: ISS
Catalog Number: 25544
Epoch time: 14040
53831349 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 12
3656 deg
Eccentricity:
0003672
Arg of perigee: 113
2209 deg
Mean anomaly: 246
9329 deg
Mean motion: 15
50171249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 290
Coasting Arc #6 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2014/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6101930
88 A = 6797899
01 meter
Y = -1370230
61 meter E =
0007507
Z = -2668963
70 I = 51
70373
XDOT = 3291
738932 Wp = 79
41353
YDOT = 4547
582952 meter/sec RA = 7
03778 deg
ZDOT = 5204
862405 TA = 250
57721
MA = 250
65835
Ha = 228
529 n
mi
Hp = 219
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20019458
27 X = 6129764
30
Y = -4495507
26 feet Y = -1301839
35 meter
Z = -8756442
59 Z = -2639254
35
XDOT = 10799
668413 XDOT = 3215
359161
YDOT = 14919
891575 feet/sec YDOT = 4583
966331 meter/sec
ZDOT = 17076
320227 ZDOT = 5220
667267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18212018
33 X = 5551023
19
Y = 9565315
41 feet Y = 2915508
14 meter
Z = -8630800
15 Z = -2630667
89
XDOT = -809
384926 XDOT = -246
700525
YDOT = 16967
029226 feet/sec YDOT = 5171
550508 meter/sec
ZDOT = 17142
239172 ZDOT = 5224
954500
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 14041
50530238
00016717 00000-0 10270-3 0 9058
2 25544 51
6458 7
5741 0003749 116
5994 243
5542 15
50183160 31675
Satellite: ISS
Catalog Number: 25544
Epoch time: 14041
50530238 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 7
5741 deg
Eccentricity:
0003749
Arg of perigee: 116
5994 deg
Mean anomaly: 243
5542 deg
Mean motion: 15
50183160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 297
Coasting Arc #7 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2014/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6198097
46 A = 6798589
94 meter
Y = 1577757
86 meter E =
0017431
Z = 2280262
36 I = 51
67621
XDOT = -3131
660078 Wp = 110
41268
YDOT = -4410
981250 meter/sec RA = 2
08656 deg
ZDOT = -5432
552623 TA = 44
24274
MA = 44
10352
Ha = 228
435 n
mi
Hp = 219
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20334965
43 X = -6226356
18
Y = 5176370
93 feet Y = 1508288
84 meter
Z = 7481175
73 Z = 2250084
88
XDOT = -10274
475323 XDOT = -3055
713752
YDOT = -14471
723261 feet/sec YDOT = -4445
577006 meter/sec
ZDOT = -17823
335377 ZDOT = -5447
580838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19043303
13 X = -5804398
79
Y = -8919187
74 feet Y = -2718568
42 meter
Z = 7353524
44 Z = 2241354
25
XDOT = 667
198864 XDOT = 203
362214
YDOT = -16247
151830 feet/sec YDOT = -4952
131878 meter/sec
ZDOT = -17886
000021 ZDOT = -5451
652806
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 14042
53673794
00016717 00000-0 10270-3 0 9068
2 25544 51
6465 2
4623 0003660 120
4249 239
7267 15
50222847 31830
Satellite: ISS
Catalog Number: 25544
Epoch time: 14042
53673794 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 2
4623 deg
Eccentricity:
0003660
Arg of perigee: 120
4249 deg
Mean anomaly: 239
7267 deg
Mean motion: 15
50222847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 302
Coasting Arc #8 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2014/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6262591
67 A = 6799148
36 meter
Y = -1828774
96 meter E =
0008287
Z = -1912634
84 I = 51
64753
XDOT = 2959
382495 Wp = 64
70292
YDOT = 4293
821791 meter/sec RA = 357
13398 deg
ZDOT = 5606
920400 TA = 274
27458
MA = 274
36928
Ha = 228
342 n
mi
Hp = 219
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20546560
58 X = 6291866
73
Y = -5999917
84 feet Y = -1758579
05 meter
Z = -6275048
69 Z = -1882141
60
XDOT = 9709
260155 XDOT = 2883
912114
YDOT = 14087
341835 feet/sec YDOT = 4326
493774 meter/sec
ZDOT = 18395
408138 ZDOT = 5621
112813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19864972
29 X = 6054843
55
Y = 8071285
20 feet Y = 2460127
73 meter
Z = -6146025
81 Z = -1873308
67
XDOT = -632
917788 XDOT = -192
913342
YDOT = 15552
921139 feet/sec YDOT = 4740
530363 meter/sec
ZDOT = 18454
566374 ZDOT = 5624
951831
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 14043
50368995
00016717 00000-0 10270-3 0 9071
2 25544 51
6466 357
6706 0003656 124
1771 235
9726 15
50247239 31980
Satellite: ISS
Catalog Number: 25544
Epoch time: 14043
50368995 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 357
6706 deg
Eccentricity:
0003656
Arg of perigee: 124
1771 deg
Mean anomaly: 235
9726 deg
Mean motion: 15
50247239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 335
Coasting Arc #9 (Orbit 3213)
---------------------------------------
Vector Time (GMT): 2014/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6303808
64 A = 6799683
24 meter
Y = 2047970
08 meter E =
0017429
Z = 1478683
92 I = 51
61978
XDOT = -2740
234313 Wp = 120
39146
YDOT = -4237
371508 meter/sec RA = 352
17947 deg
ZDOT = -5771
039252 TA = 43
48190
MA = 43
34460
Ha = 228
253 n
mi
Hp = 219
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20681786
87 X = -6333423
78
Y = 6719061
95 feet Y = 1977311
36 meter
Z = 4851325
18 Z = 1447989
61
XDOT = -8990
270056 XDOT = -2664
614256
YDOT = -13902
137492 feet/sec YDOT = -4267
592101 meter/sec
ZDOT = -18933
855813 ZDOT = -5784
166661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20537751
02 X = -6259906
51
Y = -7233699
83 feet Y = -2204831
71 meter
Z = 4721422
20 Z = 1439089
49
XDOT = 862
973865 XDOT = 263
034434
YDOT = -14936
705765 feet/sec YDOT = -4552
707917 meter/sec
ZDOT = -18988
530364 ZDOT = -5787
704055
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 14044
53508659
00016717 00000-0 10270-3 0 9089
2 25544 51
6477 352
5588 0003641 128
1986 231
9493 15
50275490 32146
Satellite: ISS
Catalog Number: 25544
Epoch time: 14044
53508659 = yrday
fracday
Element set: 908
Inclination: 51
6477 deg
RA of node: 352
5588 deg
Eccentricity:
0003641
Arg of perigee: 128
1986 deg
Mean anomaly: 231
9493 deg
Mean motion: 15
50275490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3214
Checksum: 329
Coasting Arc #10 (Orbit 3228)
---------------------------------------
Vector Time (GMT): 2014/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6306293
29 A = 6800002
87 meter
Y = -2300609
04 meter E =
0010081
Z = -1070809
48 I = 51
59054
XDOT = 2525
587161 Wp = 58
85667
YDOT = 4207
657977 meter/sec RA = 347
22335 deg
ZDOT = 5879
999974 TA = 289
54614
MA = 289
65497
Ha = 228
145 n
mi
Hp = 219
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20689938
62 X = 6336752
05
Y = -7547929
92 feet Y = -2229917
81 meter
Z = -3513154
46 Z = -1040100
97
XDOT = 8286
047116 XDOT = 2449
786017
YDOT = 13804
652155 feet/sec YDOT = 4235
477347 meter/sec
ZDOT = 19291
338498 ZDOT = 5892
084179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21150677
74 X = 6446726
58
Y = 6212096
64 feet Y = 1893447
06 meter
Z = -3383156
36 Z = -1031186
06
XDOT = -1165
422270 XDOT = -355
220708
YDOT = 14415
904766 feet/sec YDOT = 4393
967773 meter/sec
ZDOT = 19341
617221 ZDOT = 5895
324929
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 14045
50200168
00016717 00000-0 10270-3 0 9092
2 25544 51
6475 347
7671 0003570 131
9994 228
1461 15
50308054 32297
Satellite: ISS
Catalog Number: 25544
Epoch time: 14045
50200168 = yrday
fracday
Element set: 909
Inclination: 51
6475 deg
RA of node: 347
7671 deg
Eccentricity:
0003570
Arg of perigee: 131
9994 deg
Mean anomaly: 228
1461 deg
Mean motion: 15
50308054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3229
Checksum: 303
Coasting Arc #11 (Orbit 3244)
---------------------------------------
Vector Time (GMT): 2014/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6283057
25 A = 6800263
13 meter
Y = 2509105
86 meter E =
0016600
Z = 599742
25 I = 51
56275
XDOT = -2273
407981 Wp = 130
05516
YDOT = -4243
358859 meter/sec RA = 342
26531 deg
ZDOT = -5965
110198 TA = 43
47211
MA = 43
34136
Ha = 228
051 n
mi
Hp = 219
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20613704
88 X = -6313560
95
Y = 8231974
59 feet Y = 2438674
19 meter
Z = 1967658
31 Z = 569146
40
XDOT = -7458
687601 XDOT = -2196
812880
YDOT = -13921
781035 feet/sec YDOT = -4268
353866 meter/sec
ZDOT = -19570
571515 ZDOT = -5975
967401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21580639
70 X = -6577778
98
Y = -5240158
05 feet Y = -1597200
17 meter
Z = 1838109
74 Z = 560255
85
XDOT = 1705
189063 XDOT = 519
741626
YDOT = -14025
161022 feet/sec YDOT = -4274
869080 meter/sec
ZDOT = -19615
667841 ZDOT = -5978
855558
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 14046
53335903
00016717 00000-0 10270-3 0 9104
2 25544 51
6486 342
6554 0003613 136
1947 223
9491 15
50330473 32450
Satellite: ISS
Catalog Number: 25544
Epoch time: 14046
53335903 = yrday
fracday
Element set: 910
Inclination: 51
6486 deg
RA of node: 342
6554 deg
Eccentricity:
0003613
Arg of perigee: 136
1947 deg
Mean anomaly: 223
9491 deg
Mean motion: 15
50330473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3245
Checksum: 298
Coasting Arc #12 (Orbit 3259)
---------------------------------------
Vector Time (GMT): 2014/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6218165
23 A = 6800280
37 meter
Y = -2738847
90 meter E =
0012052
Z = -160723
23 I = 51
53356
XDOT = 2043
591362 Wp = 61
02753
YDOT = 4308
222871 meter/sec RA = 337
30529 deg
ZDOT = 5995
257895 TA = 297
24172
MA = 297
36446
Ha = 227
949 n
mi
Hp = 219
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20400804
57 X = 6249110
23
Y = -8985721
47 feet Y = -2669139
39 meter
Z = -527307
20 Z = -130441
39
XDOT = 6704
696069 XDOT = 1966
141488
YDOT = 14134
589472 feet/sec YDOT = 4330
643220 meter/sec
ZDOT = 19669
481282 ZDOT = 6004
996598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21910538
36 X = 6678332
09
Y = 4121059
83 feet Y = 1256099
04 meter
Z = -399055
48 Z = -121632
11
XDOT = -2260
934936 XDOT = -689
132968
YDOT = 13783
705682 feet/sec YDOT = 4201
273492 meter/sec
ZDOT = 19709
848480 ZDOT = 6007
561817
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 14047
50023719
00016717 00000-0 10270-3 0 9112
2 25544 51
6482 337
8635 0003513 139
6190 220
5222 15
50365275 32609
Satellite: ISS
Catalog Number: 25544
Epoch time: 14047
50023719 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 337
8635 deg
Eccentricity:
0003513
Arg of perigee: 139
6190 deg
Mean anomaly: 220
5222 deg
Mean motion: 15
50365275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3260
Checksum: 285
Coasting Arc #13 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2014/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6128721
25 A = 6800169
11 meter
Y = 2910528
61 meter E =
0014862
Z = -335501
60 I = 51
50604
XDOT = -1788
777101 Wp = 138
67211
YDOT = -4438
011497 meter/sec RA = 332
34320 deg
ZDOT = -5987
002025 TA = 44
94585
MA = 44
82563
Ha = 227
835 n
mi
Hp = 219
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20107353
17 X = -6159182
20
Y = 9548978
39 feet Y = 2841822
97 meter
Z = -1100727
02 Z = -365347
90
XDOT = -5868
691277 XDOT = -1709
934844
YDOT = -14560
405175 feet/sec YDOT = -4457
574601 meter/sec
ZDOT = -19642
395094 ZDOT = -5995
499505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22035085
93 X = -6716294
19
Y = -3106333
66 feet Y = -946810
50 meter
Z = -1227158
93 Z = -374038
04
XDOT = 3002
088942 XDOT = 915
036709
YDOT = -13711
222169 feet/sec YDOT = -4179
180517 meter/sec
ZDOT = -19677
504634 ZDOT = -5997
703412
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 14048
53155503
00016717 00000-0 10270-3 0 9124
2 25544 51
6490 332
7515 0003581 144
2644 215
8747 15
50386908 32762
Satellite: ISS
Catalog Number: 25544
Epoch time: 14048
53155503 = yrday
fracday
Element set: 912
Inclination: 51
6490 deg
RA of node: 332
7515 deg
Eccentricity:
0003581
Arg of perigee: 144
2644 deg
Mean anomaly: 215
8747 deg
Mean motion: 15
50386908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 310
Coasting Arc #14 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2014/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5999519
59 A = 6799833
89 meter
Y = -3090511
23 meter E =
0013607
Z = 792950
34 I = 51
47776
XDOT = 1573
164749 Wp = 68
33974
YDOT = 4594
210818 meter/sec RA = 327
37880 deg
ZDOT = 5926
053387 TA = 300
23818
MA = 300
37283
Ha = 227
747 n
mi
Hp = 219
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19683463
24 X = 6029780
64
Y = -10139472
52 feet Y = -3023251
47 meter
Z = 2601543
12 Z = 822168
65
XDOT = 5161
301669 XDOT = 1492
887823
YDOT = 15072
870137 feet/sec YDOT = 4611
354772 meter/sec
ZDOT = 19442
432373 ZDOT = 5933
499998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22036411
30 X = 6716698
17
Y = 1996177
71 feet Y = 608434
97 meter
Z = 2725345
10 Z = 830685
19
XDOT = -3689
906769 XDOT = -1124
683583
YDOT = 13817
955993 feet/sec YDOT = 4211
712987 meter/sec
ZDOT = 19473
083435 ZDOT = 5935
395831
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 14049
56285230
00016717 00000-0 10270-3 0 9130
2 25544 51
6485 327
6396 0003475 147
2964 212
8402 15
50422367 32929
Satellite: ISS
Catalog Number: 25544
Epoch time: 14049
56285230 = yrday
fracday
Element set: 913
Inclination: 51
6485 deg
RA of node: 327
6396 deg
Eccentricity:
0003475
Arg of perigee: 147
2964 deg
Mean anomaly: 212
8402 deg
Mean motion: 15
50422367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3292
Checksum: 313
Coasting Arc #15 (Orbit 3306)
---------------------------------------
Vector Time (GMT): 2014/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 896364
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5851447
95 A = 6799309
10 meter
Y = 3198661
07 meter E =
0012264
Z = -1298366
00 I = 51
45126
XDOT = -1346
857072 Wp = 144
83189
YDOT = -4808
106955 meter/sec RA = 322
41213 deg
ZDOT = -5812
546637 TA = 49
31211
MA = 49
20562
Ha = 227
606 n
mi
Hp = 219
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19197663
86 X = -5880474
21
Y = 10494294
83 feet Y = 3133063
99 meter
Z = -4259730
98 Z = -1326862
09
XDOT = -4418
822415 XDOT = -1264
756417
YDOT = -15774
629117 feet/sec YDOT = -4822
709940 meter/sec
ZDOT = -19070
034899 ZDOT = -5818
889491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21829415
98 X = -6653605
99
Y = -1055316
38 feet Y = -321660
43 meter
Z = -4380494
85 Z = -1335174
83
XDOT = 4490
210027 XDOT = 1368
616016
YDOT = -14108
973833 feet/sec YDOT = -4300
415224 meter/sec
ZDOT = -19095
995154 ZDOT = -5820
459323
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 14050
52967469
00016717 00000-0 10270-3 0 9140
2 25544 51
6491 322
8467 0003536 152
6875 207
4462 15
50442967 33072
Satellite: ISS
Catalog Number: 25544
Epoch time: 14050
52967469 = yrday
fracday
Element set: 914
Inclination: 51
6491 deg
RA of node: 322
8467 deg
Eccentricity:
0003536
Arg of perigee: 152
6875 deg
Mean anomaly: 207
4462 deg
Mean motion: 15
50442967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3307
Checksum: 326
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