[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 1st 2013
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) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 185 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 157)
---------------------------------------
Vector Time (GMT): 2013/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -838829
31 A = 6795360
06 meter
Y = 5676989
52 meter E =
0001620
Z = -3640452
89 I = 51
31904
XDOT = -5204
084436 Wp = 101
79196
YDOT = -3556
668537 meter/sec RA = 247
88208 deg
ZDOT = -4349
188805 TA = 121
53880
MA = 121
52298
Ha = 225
976 n
mi
Hp = 222
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2752064
68 X = -884564
14
Y = 18625293
69 feet Y = 5667353
70 meter
Z = -11943743
07 Z = -3644638
55
XDOT = -17073
767836 XDOT = -5142
799237
YDOT = -11668
860028 feet/sec YDOT = -3614
520970 meter/sec
ZDOT = -14268
992144 ZDOT = -4374
320900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16249780
86 X = 4952933
21
Y = -9485924
84 feet Y = -2891309
89 meter
Z = -11962034
76 Z = -3646028
19
XDOT = 733
154573 XDOT = 223
465514
YDOT = 19373
421837 feet/sec YDOT = 5905
018976 meter/sec
ZDOT = -14373
688943 ZDOT = -4381
100390
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 13212
52452357
00016717 00000-0 10270-3 0 9009
2 25544 51
6489 248
6528 0004006 252
9843 107
0869 15
50133471 1588
Satellite: ISS
Catalog Number: 25544
Epoch time: 13212
52452357 = yrday
fracday
Element set: 900
Inclination: 51
6489 deg
RA of node: 248
6528 deg
Eccentricity:
0004006
Arg of perigee: 252
9843 deg
Mean anomaly: 107
0869 deg
Mean motion: 15
50133471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 158
Checksum: 301
Coasting Arc #2 (Orbit 173)
---------------------------------------
Vector Time (GMT): 2013/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 690032
84 A = 6794539
68 meter
Y = -5514034
47 meter E =
0007703
Z = 3905427
75 I = 51
32723
XDOT = 5452
936807 Wp = 110
11152
YDOT = 3552
738733 meter/sec RA = 242
90468 deg
ZDOT = 4043
504487 TA = 297
32118
MA = 297
39958
Ha = 225
959 n
mi
Hp = 222
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2263887
27 X = 732669
40
Y = -18090664
28 feet Y = -5506079
96 meter
Z = 12813083
18 Z = 3908883
02
XDOT = 17890
212622 XDOT = 5393
162018
YDOT = 11655
966972 feet/sec YDOT = 3613
382433 meter/sec
ZDOT = 13266
090836 ZDOT = 4069
849101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15357716
54 X = -4681032
00
Y = 9805504
88 feet Y = 2988717
89 meter
Z = 12828290
50 Z = 3910062
94
XDOT = -1595
915973 XDOT = -486
435189
YDOT = -20037
977973 feet/sec YDOT = -6107
575686 meter/sec
ZDOT = 13375
876558 ZDOT = 4076
967175
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 13213
55601297
00016717 00000-0 10270-3 0 9013
2 25544 51
6474 243
5417 0003863 257
5894 102
4824 15
50125580 1740
Satellite: ISS
Catalog Number: 25544
Epoch time: 13213
55601297 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 243
5417 deg
Eccentricity:
0003863
Arg of perigee: 257
5894 deg
Mean anomaly: 102
4824 deg
Mean motion: 15
50125580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 174
Checksum: 297
Coasting Arc #3 (Orbit 188)
---------------------------------------
Vector Time (GMT): 2013/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -591316
58 A = 6793567
66 meter
Y = 5335620
41 meter E =
0003912
Z = -4167714
62 I = 51
33996
XDOT = -5702
192093 Wp = 59
56853
YDOT = -3522
840957 meter/sec RA = 237
92804 deg
ZDOT = -3701
671730 TA = 172
18317
MA = 172
17707
Ha = 225
838 n
mi
Hp = 222
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1940015
04 X = -630691
37
Y = 17505316
31 feet Y = 5328788
06 meter
Z = -13673604
39 Z = -4170682
42
XDOT = -18707
979308 XDOT = -5644
393661
YDOT = -11557
877155 feet/sec YDOT = -3586
283059 meter/sec
ZDOT = -12144
592290 ZDOT = -3729
231917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14527657
79 X = 4428030
09
Y = -9939189
39 feet Y = -3029464
93 meter
Z = -13686741
32 Z = -4171718
75
XDOT = 2559
317311 XDOT = 780
079916
YDOT = 20619
737830 feet/sec YDOT = 6284
896091 meter/sec
ZDOT = -12259
485720 ZDOT = -3736
691248
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 13214
52302586
00016717 00000-0 10270-3 0 9021
2 25544 51
6483 238
7506 0003955 261
6482 98
4220 15
50154953 1892
Satellite: ISS
Catalog Number: 25544
Epoch time: 13214
52302586 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 238
7506 deg
Eccentricity:
0003955
Arg of perigee: 261
6482 deg
Mean anomaly: 98
4220 deg
Mean motion: 15
50154953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 189
Checksum: 307
Coasting Arc #4 (Orbit 204)
---------------------------------------
Vector Time (GMT): 2013/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 514448
85 A = 6792753
21 meter
Y = -5151670
33 meter E =
0006063
Z = 4395025
59 I = 51
35264
XDOT = 5962
850780 Wp = 124
07523
YDOT = 3456
624519 meter/sec RA = 232
95112 deg
ZDOT = 3347
088192 TA = 291
88297
MA = 291
94743
Ha = 225
834 n
mi
Hp = 222
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1687824
31 X = 550668
23
Y = -16901805
54 feet Y = -5145715
20 meter
Z = 14419375
30 Z = 4397612
35
XDOT = 19563
158728 XDOT = 5907
495911
YDOT = 11340
631625 feet/sec YDOT = 3522
995175 meter/sec
ZDOT = 10981
260474 ZDOT = 3375
920456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13732011
69 X = -4185517
16
Y = 9980959
38 feet Y = 3042196
42 meter
Z = 14430885
99 Z = 4398534
05
XDOT = -3662
140308 XDOT = -1116
220366
YDOT = -21121
032562 feet/sec YDOT = -6437
690725 meter/sec
ZDOT = 11101
505149 ZDOT = 3383
738769
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 13215
55449950
00016717 00000-0 10270-3 0 9033
2 25544 51
6466 233
6391 0003848 266
6501 93
4210 15
50150055 2059
Satellite: ISS
Catalog Number: 25544
Epoch time: 13215
55449950 = yrday
fracday
Element set: 903
Inclination: 51
6466 deg
RA of node: 233
6391 deg
Eccentricity:
0003848
Arg of perigee: 266
6501 deg
Mean anomaly: 93
4210 deg
Mean motion: 15
50150055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 205
Checksum: 286
Coasting Arc #5 (Orbit 219)
---------------------------------------
Vector Time (GMT): 2013/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -487204
96 A = 6791870
46 meter
Y = 4966789
21 meter E =
0006631
Z = -4613491
77 I = 51
36944
XDOT = -6210
566454 Wp = 58
41075
YDOT = -3358
531499 meter/sec RA = 227
97551 deg
ZDOT = -2959
610446 TA = 181
92667
MA = 181
92922
Ha = 225
774 n
mi
Hp = 222
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1598441
46 X = -520297
81
Y = 16295240
18 feet Y = 4961156
18 meter
Z = -15136127
86 Z = -4615938
64
XDOT = -20375
874193 XDOT = -6158
172333
YDOT = -11018
804129 feet/sec YDOT = -3427
688875 meter/sec
ZDOT = -9710
008024 ZDOT = -2989
653154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13047057
64 X = 3976743
17
Y = -9875943
64 feet Y = -3010187
62 meter
Z = -15147021
44 Z = -4616812
13
XDOT = 4840
727636 XDOT = 1475
453783
YDOT = 21481
089559 feet/sec YDOT = 6547
436098 meter/sec
ZDOT = -9835
351674 ZDOT = -2997
815190
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 13216
52149741
00016717 00000-0 10270-3 0 9047
2 25544 51
6468 228
8479 0003952 270
4242 89
6455 15
50172757 2203
Satellite: ISS
Catalog Number: 25544
Epoch time: 13216
52149741 = yrday
fracday
Element set: 904
Inclination: 51
6468 deg
RA of node: 228
8479 deg
Eccentricity:
0003952
Arg of perigee: 270
4242 deg
Mean anomaly: 89
6455 deg
Mean motion: 15
50172757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 220
Checksum: 314
Coasting Arc #6 (Orbit 235)
---------------------------------------
Vector Time (GMT): 2013/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 485760
43 A = 6791128
64 meter
Y = -4783445
82 meter E =
0004106
Z = 4795137
87 I = 51
38698
XDOT = 6459
964430 Wp = 141
29635
YDOT = 3227
452066 meter/sec RA = 222
99972 deg
ZDOT = 2560
836228 TA = 283
35647
MA = 283
40225
Ha = 225
770 n
mi
Hp = 222
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1593702
21 X = 515920
87
Y = -15693719
89 feet Y = -4777845
29 meter
Z = 15732079
63 Z = 4797570
68
XDOT = 21194
109023 XDOT = 6410
954651
YDOT = 10588
753499 feet/sec YDOT = 3299
417350 meter/sec
ZDOT = 8401
693660 ZDOT = 2592
098585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12432260
13 X = -3789352
89
Y = 9691831
47 feet Y = 2954070
23 meter
Z = 15742883
19 Z = 4798430
80
XDOT = -6119
420095 XDOT = -1865
199245
YDOT = -21732
017679 feet/sec YDOT = -6623
918988 meter/sec
ZDOT = 8532
179872 ZDOT = 2600
608425
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 13217
55295487
00016717 00000-0 10270-3 0 9051
2 25544 51
6456 223
7359 0003929 275
6805 84
3898 15
50174059 2364
Satellite: ISS
Catalog Number: 25544
Epoch time: 13217
55295487 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 223
7359 deg
Eccentricity:
0003929
Arg of perigee: 275
6805 deg
Mean anomaly: 84
3898 deg
Mean motion: 15
50174059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 236
Checksum: 339
Coasting Arc #7 (Orbit 250)
---------------------------------------
Vector Time (GMT): 2013/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -528649
92 A = 6790414
13 meter
Y = 4613934
51 meter E =
0008954
Z = -4962265
62 I = 51
40781
XDOT = -6682
581397 Wp = 63
49641
YDOT = -3062
824073 meter/sec RA = 218
02558 deg
ZDOT = -2134
988457 TA = 185
59231
MA = 185
60231
Ha = 225
799 n
mi
Hp = 222
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1734415
76 X = -556099
83
Y = 15137580
42 feet Y = 4607869
44 meter
Z = -16280399
01 Z = -4964900
27
XDOT = -21924
479648 XDOT = -6637
464593
YDOT = -10048
635409 feet/sec YDOT = -3137
300622 meter/sec
ZDOT = -7004
555305 ZDOT = -2167
341624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11962150
67 X = 3646063
52
Y = -9417165
15 feet Y = -2870351
94 meter
Z = -16292019
00 Z = -4965807
39
XDOT = 7430
819994 XDOT = 2264
913934
YDOT = 21796
027483 feet/sec YDOT = 6643
429177 meter/sec
ZDOT = -7139
648792 ZDOT = -2176
164952
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 13218
51993779
00016717 00000-0 10270-3 0 9068
2 25544 51
6455 218
9442 0003972 279
3736 80
6965 15
50190038 2510
Satellite: ISS
Catalog Number: 25544
Epoch time: 13218
51993779 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 218
9442 deg
Eccentricity:
0003972
Arg of perigee: 279
3736 deg
Mean anomaly: 80
6965 deg
Mean motion: 15
50190038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 251
Checksum: 332
Coasting Arc #8 (Orbit 266)
---------------------------------------
Vector Time (GMT): 2013/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 599160
04 A = 6789821
74 meter
Y = -4453183
13 meter E =
0002047
Z = 5090532
04 I = 51
43014
XDOT = 6897
116987 Wp = 168
60532
YDOT = 2871
982656 meter/sec RA = 213
05192 deg
ZDOT = 1698
522429 TA = 264
91131
MA = 264
93467
Ha = 225
794 n
mi
Hp = 222
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1965748
16 X = 624184
05
Y = -14610180
87 feet Y = -4446343
03 meter
Z = 16701220
59 Z = 5093503
41
XDOT = 22628
336573 XDOT = 6856
238452
YDOT = 9422
515276 feet/sec YDOT = 2948
882019 meter/sec
ZDOT = 5572
580147 ZDOT = 1731
928026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11590497
35 X = -3532783
59
Y = 9085560
41 feet Y = 2769278
81 meter
Z = 16714223
97 Z = 5094495
47
XDOT = -8790
873042 XDOT = -2679
458103
YDOT = -21735
416407 feet/sec YDOT = -6624
954921 meter/sec
ZDOT = 5712
122625 ZDOT = 1741
054976
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 13219
55137876
00016717 00000-0 10270-3 0 9072
2 25544 51
6449 213
8322 0004039 284
5203 75
5499 15
50197631 2674
Satellite: ISS
Catalog Number: 25544
Epoch time: 13219
55137876 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 213
8322 deg
Eccentricity:
0004039
Arg of perigee: 284
5203 deg
Mean anomaly: 75
5499 deg
Mean motion: 15
50197631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 267
Checksum: 320
Coasting Arc #9 (Orbit 281)
---------------------------------------
Vector Time (GMT): 2013/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -703982
42 A = 6789336
47 meter
Y = 4319753
39 meter E =
0010617
Z = -5199640
79 I = 51
45504
XDOT = -7072
192255 Wp = 70
28123
YDOT = -2650
527670 meter/sec RA = 208
08001 deg
ZDOT = -1243
065499 TA = 187
72618
MA = 187
74255
Ha = 225
902 n
mi
Hp = 222
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2309653
62 X = -726976
55
Y = 14172419
25 feet Y = 4311752
36 meter
Z = -17059188
95 Z = -5203116
53
XDOT = -23202
730497 XDOT = -7035
989495
YDOT = -8695
956923 feet/sec YDOT = -2729
411003 meter/sec
ZDOT = -4078
298880 ZDOT = -1277
332952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11377462
96 X = 3467850
71
Y = -8730985
09 feet Y = -2661204
25 meter
Z = -17074282
73 Z = -5204241
38
XDOT = 10127
665688 XDOT = 3086
912502
YDOT = 21462
199028 feet/sec YDOT = 6541
678264 meter/sec
ZDOT = -4221
494624 ZDOT = -1286
711561
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 13220
51834637
00016717 00000-0 10270-3 0 9080
2 25544 51
6450 209
0402 0004013 288
3946 71
6768 15
50210052 2826
Satellite: ISS
Catalog Number: 25544
Epoch time: 13220
51834637 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 209
0402 deg
Eccentricity:
0004013
Arg of perigee: 288
3946 deg
Mean anomaly: 71
6768 deg
Mean motion: 15
50210052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 282
Checksum: 280
Coasting Arc #10 (Orbit 297)
---------------------------------------
Vector Time (GMT): 2013/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 835986
76 A = 6788968
13 meter
Y = -4201706
42 meter E =
0000956
Z = 5267409
01 I = 51
48151
XDOT = 7230
241673 Wp = 271
04566
YDOT = 2412
755715 meter/sec RA = 203
10955 deg
ZDOT = 777
239790 TA = 171
50537
MA = 171
50375
Ha = 225
905 n
mi
Hp = 222
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2742738
72 X = 857321
78
Y = -13785126
05 feet Y = -4192238
44 meter
Z = 17281525
62 Z = 5271522
04
XDOT = 23721
265333 XDOT = 7198
948785
YDOT = 7915
865207 feet/sec YDOT = 2493
433913 meter/sec
ZDOT = 2549
999311 ZDOT = 812
287015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11280473
64 X = -3438288
37
Y = 8348029
93 feet Y = 2544479
52 meter
Z = 17299270
34 Z = 5272817
60
XDOT = -11454
491238 XDOT = -3491
328929
YDOT = -21065
059070 feet/sec YDOT = -6420
630005 meter/sec
ZDOT = 2696
504984 ZDOT = 821
894719
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 13221
54977053
00016717 00000-0 10270-3 0 9095
2 25544 51
6450 203
9285 0004134 293
1263 66
9452 15
50222334 2988
Satellite: ISS
Catalog Number: 25544
Epoch time: 13221
54977053 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 203
9285 deg
Eccentricity:
0004134
Arg of perigee: 293
1263 deg
Mean anomaly: 66
9452 deg
Mean motion: 15
50222334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 298
Checksum: 297
Coasting Arc #11 (Orbit 312)
---------------------------------------
Vector Time (GMT): 2013/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -988264
75 A = 6788756
61 meter
Y = 4121675
42 meter E =
0011410
Z = -5312822
75 I = 51
50995
XDOT = -7339
060605 Wp = 77
45789
YDOT = -2151
680171 meter/sec RA = 198
14080 deg
ZDOT = -302
220148 TA = 189
63953
MA = 189
66145
Ha = 226
048 n
mi
Hp = 222
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3242338
42 X = -1008472
84
Y = 13522557
16 feet Y = 4110510
84 meter
Z = -17430520
83 Z = -5317672
82
XDOT = -24078
282826 XDOT = -7312
986508
YDOT = -7059
318146 feet/sec YDOT = -2233
604420 meter/sec
ZDOT = -991
535917 ZDOT = -337
808791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11332973
24 X = 3454290
24
Y = -8013100
33 feet Y = -2442392
98 meter
Z = -17451341
14 Z = -5319168
78
XDOT = 12697
194303 XDOT = 3870
104823
YDOT = 20454
603183 feet/sec YDOT = 6234
563050 meter/sec
ZDOT = -1140
354760 ZDOT = -347
580131
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 13222
51672220
00016717 00000-0 10270-3 0 9103
2 25544 51
6454 199
1363 0004095 297
1264 62
9469 15
50234382 3134
Satellite: ISS
Catalog Number: 25544
Epoch time: 13222
51672220 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 199
1363 deg
Eccentricity:
0004095
Arg of perigee: 297
1264 deg
Mean anomaly: 62
9469 deg
Mean motion: 15
50234382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 313
Checksum: 291
Coasting Arc #12 (Orbit 328)
---------------------------------------
Vector Time (GMT): 2013/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1165067
70 A = 6788670
96 meter
Y = -4062285
02 meter E =
0002728
Z = 5313932
97 I = 51
53956
XDOT = 7423
455708 Wp = 334
86275
YDOT = 1886
785082 meter/sec RA = 193
17429 deg
ZDOT = -182
823208 TA = 116
89748
MA = 116
86960
Ha = 226
064 n
mi
Hp = 222
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3822400
59 X = 1184593
04
Y = -13327706
76 feet Y = -4049147
14 meter
Z = 17434163
30 Z = 5319640
28
XDOT = 24355
169645 XDOT = 7402
693635
YDOT = 6190
239769 feet/sec YDOT = 1969
682774 meter/sec
ZDOT = -599
813676 ZDOT = -146
811540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11506124
06 X = -3507066
61
Y = 7680891
45 feet Y = 2341135
71 meter
Z = 17458567
51 Z = 5321371
38
XDOT = -13869
730264 XDOT = -4227
493784
YDOT = -19738
408696 feet/sec YDOT = -6016
266970 meter/sec
ZDOT = -449
177618 ZDOT = -136
909338
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 13223
54812903
00016717 00000-0 10270-3 0 9112
2 25544 51
6456 194
0250 0004212 301
4156 58
6583 15
50249670 3297
Satellite: ISS
Catalog Number: 25544
Epoch time: 13223
54812903 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 194
0250 deg
Eccentricity:
0004212
Arg of perigee: 301
4156 deg
Mean anomaly: 58
6583 deg
Mean motion: 15
50249670 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 329
Checksum: 283
Coasting Arc #13 (Orbit 343)
---------------------------------------
Vector Time (GMT): 2013/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1345214
71 A = 6788759
81 meter
Y = 4047543
80 meter E =
0011214
Z = -5291140
61 I = 51
57044
XDOT = -7453
353083 Wp = 84
26732
YDOT = -1609
324394 meter/sec RA = 188
20941 deg
ZDOT = 666
168086 TA = 192
09798
MA = 192
12494
Ha = 226
208 n
mi
Hp = 221
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4413434
08 X = -1364672
46
Y = 13279343
17 feet Y = 4032391
83 meter
Z = -17359385
20 Z = -5297722
87
XDOT = -24453
258147 XDOT = -7438
039362
YDOT = -5279
935677 feet/sec YDOT = -1692
586871 meter/sec
ZDOT = 2185
590834 ZDOT = 629
997810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11796382
97 X = 3595537
53
Y = -7462530
22 feet Y = -2274579
21 meter
Z = -17387455
30 Z = -5299696
37
XDOT = 14902
240454 XDOT = 4542
202890
YDOT = 18834
626643 feet/sec YDOT = 5740
794201 meter/sec
ZDOT = 2034
243223 ZDOT = 620
037334
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 13224
51506397
00016717 00000-0 10270-3 0 9128
2 25544 51
6459 189
2328 0004218 305
2446 54
8310 15
50262620 3445
Satellite: ISS
Catalog Number: 25544
Epoch time: 13224
51506397 = yrday
fracday
Element set: 912
Inclination: 51
6459 deg
RA of node: 189
2328 deg
Eccentricity:
0004218
Arg of perigee: 305
2446 deg
Mean anomaly: 54
8310 deg
Mean motion: 15
50262620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 344
Checksum: 287
Coasting Arc #14 (Orbit 359)
---------------------------------------
Vector Time (GMT): 2013/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1545322
99 A = 6788989
06 meter
Y = -4056550
19 meter E =
0004815
Z = 5220724
78 I = 51
60219
XDOT = 7453
645037 Wp = 359
13963
YDOT = 1342
468070 meter/sec RA = 183
24718 deg
ZDOT = -1158
459050 TA = 102
01115
MA = 101
95717
Ha = 226
240 n
mi
Hp = 221
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5069957
33 X = 1565208
60
Y = -13308891
70 feet Y = -4039158
17 meter
Z = 17128362
15 Z = 5228280
14
XDOT = 24454
216002 XDOT = 7443
706752
YDOT = 4404
422803 feet/sec YDOT = 1425
763872 meter/sec
ZDOT = -3800
718669 ZDOT = -1122
274210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12198029
41 X = -3717959
36
Y = 7275759
49 feet Y = 2217651
49 meter
Z = 17160514
51 Z = 5230524
82
XDOT = -15808
762568 XDOT = -4818
510831
YDOT = -17860
508534 feet/sec YDOT = -5443
883001 meter/sec
ZDOT = -3649
262758 ZDOT = -1112
295289
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 13225
54645279
00016717 00000-0 10270-3 0 9136
2 25544 51
6462 184
1216 0004285 309
3079 50
7692 15
50279585 3604
Satellite: ISS
Catalog Number: 25544
Epoch time: 13225
54645279 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 184
1216 deg
Eccentricity:
0004285
Arg of perigee: 309
3079 deg
Mean anomaly: 50
7692 deg
Mean motion: 15
50279585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 360
Checksum: 314
Coasting Arc #15 (Orbit 374)
---------------------------------------
Vector Time (GMT): 2013/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 940051
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1730341
08 A = 6789378
79 meter
Y = 4111917
89 meter E =
0010049
Z = -5126671
55 I = 51
63440
XDOT = -7399
813404 Wp = 89
71771
YDOT = -1075
624584 meter/sec RA = 178
28653 deg
ZDOT = 1637
677205 TA = 196
10086
MA = 196
13282
Ha = 226
373 n
mi
Hp = 221
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5676972
06 X = -1751288
96
Y = 13490544
26 feet Y = 4092451
03 meter
Z = -16819788
56 Z = -5135128
21
XDOT = -24277
603031 XDOT = -7395
190922
YDOT = -3528
952046 feet/sec YDOT = -1158
348152 meter/sec
ZDOT = 5372
956709 ZDOT = 1601
740949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12663778
92 X = 3859919
81
Y = -7255422
12 feet Y = -2211452
66 meter
Z = -16855730
09 Z = -5137626
53
XDOT = 16534
401435 XDOT = 5039
685557
YDOT = 16748
202392 feet/sec YDOT = 5104
852089 meter/sec
ZDOT = 5222
492957 ZDOT = 1591
815853
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 13226
51337037
00016717 00000-0 10270-3 0 9145
2 25544 51
6462 179
3293 0004343 312
8221 47
2564 15
50293559 3750
Satellite: ISS
Catalog Number: 25544
Epoch time: 13226
51337037 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 179
3293 deg
Eccentricity:
0004343
Arg of perigee: 312
8221 deg
Mean anomaly: 47
2564 deg
Mean motion: 15
50293559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 375
Checksum: 299
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