[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 ET - UTC (sec) : 66 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 1556)
---------------------------------------
Vector Time (GMT): 2012/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2028115
82 A = 6774971
35 meter
Y = 4591762
34 meter E =
0017968
Z = -4567416
31 I = 51
50613
XDOT = -7020
231303 Wp = 43
19771
YDOT = 54
344666 meter/sec RA = 199
81673 deg
ZDOT = -3056
949021 TA = 196
10429
MA = 196
16148
Ha = 220
810 n
mi
Hp = 209
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6653923
29 X = 1998806
94
Y = 15064837
08 feet Y = 4614278
56 meter
Z = -14984961
64 Z = -4557634
38
XDOT = -23032
254930 XDOT = -7005
466991
YDOT = 178
296149 feet/sec YDOT = -24
077058 meter/sec
ZDOT = -10029
360305 ZDOT = -3091
017751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16470793
30 X = 5020297
80
Y = -1063051
00 feet Y = -324017
94 meter
Z = -14945098
78 Z = -4555266
11
XDOT = -7928
647245 XDOT = -2416
651680
YDOT = 20387
018976 feet/sec YDOT = 6213
963384 meter/sec
ZDOT = -10169
506227 ZDOT = -3099
665498
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 12153
52162644
00016717 00000-0 10270-3 0 9009
2 25544 51
6381 200
7451 0010190 16
7603 343
3885 15
56047451 15579
Satellite: ISS
Catalog Number: 25544
Epoch time: 12153
52162644 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 200
7451 deg
Eccentricity:
0010190
Arg of perigee: 16
7603 deg
Mean anomaly: 343
3885 deg
Mean motion: 15
56047451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 282
Coasting Arc #2 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2012/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 504481
19 A = 6771722
81 meter
Y = -4205081
60 meter E =
0010543
Z = 5277779
74 I = 51
52399
XDOT = 7501
290657 Wp = 36
49699
YDOT = 1549
132681 meter/sec RA = 194
79126 deg
ZDOT = 525
029125 TA = 48
53697
MA = 48
44648
Ha = 220
824 n
mi
Hp = 209
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1655122
00 X = 525827
04
Y = -13796199
48 feet Y = -4199321
50 meter
Z = 17315550
34 Z = 5280281
85
XDOT = 24610
533650 XDOT = 7480
859901
YDOT = 5082
456301 feet/sec YDOT = 1632
902454 meter/sec
ZDOT = 1722
536498 ZDOT = 561
421301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12492621
24 X = -3807750
96
Y = -6053128
61 feet Y = -1844993
60 meter
Z = 17326190
60 Z = 5281022
90
XDOT = 12539
672108 XDOT = 3822
092059
YDOT = -20593
993914 feet/sec YDOT = -6277
049345 meter/sec
ZDOT = 1872
125455 ZDOT = 570
623839
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 12154
54917290
00016717 00000-0 10270-3 0 9018
2 25544 51
6372 195
6072 0010298 20
6189 339
5379 15
56096716 15733
Satellite: ISS
Catalog Number: 25544
Epoch time: 12154
54917290 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 195
6072 deg
Eccentricity:
0010298
Arg of perigee: 20
6189 deg
Mean anomaly: 339
5379 deg
Mean motion: 15
56096716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1573
Checksum: 325
Coasting Arc #3 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2012/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3009188
79 A = 6773039
91 meter
Y = 3490022
33 meter E =
0017556
Z = -4976020
41 I = 51
55862
XDOT = -6786
087196 Wp = 69
84373
YDOT = -2864
551379 meter/sec RA = 189
76407 deg
ZDOT = 2106
656501 TA = 220
64360
MA = 220
77477
Ha = 220
944 n
mi
Hp = 209
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9872666
63 X = -3023818
53
Y = 11450204
49 feet Y = 3456290
68 meter
Z = -16325526
28 Z = -4990674
14
XDOT = -22264
065604 XDOT = -6763
784654
YDOT = -9398
134444 feet/sec YDOT = -2940
313228 meter/sec
ZDOT = 6911
602692 ZDOT = 2073
743214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7766134
55 X = 2367117
81
Y = 12895040
89 feet Y = 3930408
46 meter
Z = -16386110
34 Z = -4994486
43
XDOT = -15035
865502 XDOT = -4582
931805
YDOT = 17616
792753 feet/sec YDOT = 5369
598431 meter/sec
ZDOT = 6776
417399 ZDOT = 2065
452023
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 12155
51248183
00016717 00000-0 10270-3 0 9025
2 25544 51
6376 190
7901 0010394 23
8541 336
3093 15
56094674 15883
Satellite: ISS
Catalog Number: 25544
Epoch time: 12155
51248183 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 190
7901 deg
Eccentricity:
0010394
Arg of perigee: 23
8541 deg
Mean anomaly: 336
3093 deg
Mean motion: 15
56094674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1588
Checksum: 312
Coasting Arc #4 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2012/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5146736
55 A = 6777663
76 meter
Y = -2472160
90 meter E =
0019582
Z = 3646646
63 I = 51
60357
XDOT = 4975
288400 Wp = 58
78108
YDOT = 3882
638616 meter/sec RA = 184
75074 deg
ZDOT = -4362
510945 TA = 77
84204
MA = 77
62275
Ha = 220
927 n
mi
Hp = 208
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16885618
59 X = 5156283
47
Y = -8110764
11 feet Y = -2414554
16 meter
Z = 11964063
76 Z = 3671672
26
XDOT = 16323
124672 XDOT = 4952
694466
YDOT = 12738
315670 feet/sec YDOT = 3938
149790 meter/sec
ZDOT = -14312
699951 ZDOT = -4338
395187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2688230
05 X = -819372
52
Y = -18471658
43 feet Y = -5630161
49 meter
Z = 12067256
74 Z = 3678099
85
XDOT = 15729
620041 XDOT = 4794
388189
YDOT = -11632
780394 feet/sec YDOT = -3545
671464 meter/sec
ZDOT = -14213
783901 ZDOT = -4332
361333
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 12156
53999151
00016717 00000-0 10270-3 0 9037
2 25544 51
6362 185
6513 0010487 28
0280 332
1436 15
56166772 16043
Satellite: ISS
Catalog Number: 25544
Epoch time: 12156
53999151 = yrday
fracday
Element set: 903
Inclination: 51
6362 deg
RA of node: 185
6513 deg
Eccentricity:
0010487
Arg of perigee: 28
0280 deg
Mean anomaly: 332
1436 deg
Mean motion: 15
56166772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 304
Coasting Arc #5 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2012/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6442595
50 A = 6782125
64 meter
Y = 1316505
89 meter E =
0018171
Z = -1629757
64 I = 51
64997
XDOT = -2362
693285 Wp = 35
06977
YDOT = -4524
536703 meter/sec RA = 179
75920 deg
ZDOT = 5731
282981 TA = 307
06661
MA = 307
23262
Ha = 220
930 n
mi
Hp = 208
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21137124
35 X = -6448921
09
Y = 4319245
04 feet Y = 1244425
72 meter
Z = -5346973
88 Z = -1661070
73
XDOT = -7751
618390 XDOT = -2339
764766
YDOT = -14844
280523 feet/sec YDOT = -4550
830613 meter/sec
ZDOT = 18803
421854 ZDOT = 5719
859974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1847583
53 X = -563143
46
Y = 21462158
91 feet Y = 6541666
04 meter
Z = -5475965
97 Z = -1669074
43
XDOT = -14900
053293 XDOT = -4541
536244
YDOT = 3465
255428 feet/sec YDOT = 1056
209854 meter/sec
ZDOT = 18756
786474 ZDOT = 5717
068517
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 12157
50326586
00016717 00000-0 10270-3 0 9042
2 25544 51
6369 180
8341 0010422 32
1689 328
0098 15
56200305 16199
Satellite: ISS
Catalog Number: 25544
Epoch time: 12157
50326586 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 180
8341 deg
Eccentricity:
0010422
Arg of perigee: 32
1689 deg
Mean anomaly: 328
0098 deg
Mean motion: 15
56200305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 295
Coasting Arc #6 (Orbit 1634)
---------------------------------------
Vector Time (GMT): 2012/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6739328
73 A = 6783088
29 meter
Y = 5453
59 meter E =
0012834
Z = -782721
31 I = 51
68253
XDOT = -685
037828 Wp = 88
16769
YDOT = 4783
214609 meter/sec RA = 174
78028 deg
ZDOT = -5948
842270 TA = 100
28782
MA = 100
14309
Ha = 221
108 n
mi
Hp = 208
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22110658
58 X = 6742569
14
Y = 17892
34 feet Y = 80835
18 meter
Z = -2567983
31 Z = -749974
14
XDOT = -2247
499435 XDOT = -709
575718
YDOT = 15692
961316 feet/sec YDOT = 4775
417890 meter/sec
ZDOT = -19517
199050 ZDOT = -5952
228948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5930091
11 X = 1807491
77
Y = -21316419
60 feet Y = -6497244
69 meter
Z = -2433178
18 Z = -741632
71
XDOT = 12997
737496 XDOT = 3961
710389
YDOT = 5812
165493 feet/sec YDOT = 1771
548042 meter/sec
ZDOT = -19531
542706 ZDOT = -5953
214217
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 12158
53073923
00016717 00000-0 10270-3 0 9051
2 25544 51
6360 175
6944 0010490 35
7894 324
3961 15
56194284 16357
Satellite: ISS
Catalog Number: 25544
Epoch time: 12158
53073923 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 175
6944 deg
Eccentricity:
0010490
Arg of perigee: 35
7894 deg
Mean anomaly: 324
3961 deg
Mean motion: 15
56194284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1635
Checksum: 322
Coasting Arc #7 (Orbit 1650)
---------------------------------------
Vector Time (GMT): 2012/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5920636
85 A = 6779538
04 meter
Y = -1334967
55 meter E =
0022113
Z = 2991485
65 I = 51
70067
XDOT = 3570
040594 Wp = 63
66292
YDOT = -4636
680607 meter/sec RA = 169
79844 deg
ZDOT = 4977
733309 TA = 330
62458
MA = 330
74870
Ha = 221
225 n
mi
Hp = 208
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19424661
57 X = -5919800
82
Y = -4379814
79 feet Y = -1401171
55 meter
Z = 9814585
48 Z = 2962725
43
XDOT = 11712
731607 XDOT = 3597
442986
YDOT = -15212
206716 feet/sec YDOT = -4596
605732 meter/sec
ZDOT = 16331
146028 ZDOT = 4995
142190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9122693
25 X = -2780596
90
Y = 17764707
35 feet Y = 5414682
80 meter
Z = 9696287
11 Z = 2955428
31
XDOT = -10519
705694 XDOT = -3206
406296
YDOT = -14389
432334 feet/sec YDOT = -4385
898975 meter/sec
ZDOT = 16403
210165 ZDOT = 4999
698458
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 12159
55819352
00016717 00000-0 10270-3 0 9069
2 25544 51
6356 170
5557 0010573 39
1369 321
0548 15
56220738 16510
Satellite: ISS
Catalog Number: 25544
Epoch time: 12159
55819352 = yrday
fracday
Element set: 906
Inclination: 51
6356 deg
RA of node: 170
5557 deg
Eccentricity:
0010573
Arg of perigee: 39
1369 deg
Mean anomaly: 321
0548 deg
Mean motion: 15
56220738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1651
Checksum: 313
Coasting Arc #8 (Orbit 1665)
---------------------------------------
Vector Time (GMT): 2012/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4178063
72 A = 6774151
14 meter
Y = 2661006
86 meter E =
0020184
Z = -4640787
97 I = 51
71291
XDOT = -5824
674921 Wp = 56
52744
YDOT = 3996
346088 meter/sec RA = 164
79970 deg
ZDOT = -2950
820265 TA = 184
05276
MA = 184
06914
Ha = 221
142 n
mi
Hp = 208
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13707558
14 X = 4170541
04
Y = 8730337
48 feet Y = 2707687
09 meter
Z = -15225682
32 Z = -4620509
17
XDOT = -19109
825857 XDOT = -5854
595641
YDOT = 13111
371681 feet/sec YDOT = 3931
044048 meter/sec
ZDOT = -9681
168849 ZDOT = -2979
188279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11715520
17 X = 3570890
55
Y = -11375040
67 feet Y = -3467112
40 meter
Z = -15142403
42 Z = -4615404
56
XDOT = 7460
817150 XDOT = 2274
057067
YDOT = 20734
635677 feet/sec YDOT = 6319
916954 meter/sec
ZDOT = -9798
313918 ZDOT = -2986
526082
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 12160
52141381
00016717 00000-0 10270-3 0 9079
2 25544 51
6358 165
7376 0010531 42
6235 317
5734 15
56250599 16663
Satellite: ISS
Catalog Number: 25544
Epoch time: 12160
52141381 = yrday
fracday
Element set: 907
Inclination: 51
6358 deg
RA of node: 165
7376 deg
Eccentricity:
0010531
Arg of perigee: 42
6235 deg
Mean anomaly: 317
5734 deg
Mean motion: 15
56250599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1666
Checksum: 306
Coasting Arc #9 (Orbit 1681)
---------------------------------------
Vector Time (GMT): 2012/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1784915
39 A = 6771123
37 meter
Y = -3800626
38 meter E =
0012027
Z = 5302996
52 I = 51
73177
XDOT = 7108
034262 Wp = 57
10977
YDOT = -2891
413474 meter/sec RA = 159
78531 deg
ZDOT = 326
060856 TA = 29
82487
MA = 29
75638
Ha = 221
198 n
mi
Hp = 208
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5856021
61 X = -1768043
98
Y = -12469246
65 feet Y = -3820492
65 meter
Z = 17398282
55 Z = 5294366
09
XDOT = 23320
322382 XDOT = 7138
254429
YDOT = -9486
264679 feet/sec YDOT = -2811
758098 meter/sec
ZDOT = 1069
753465 ZDOT = 360
664297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13465362
30 X = -4104242
43
Y = 3111835
67 feet Y = 948487
51 meter
Z = 17363059
45 Z = 5292260
52
XDOT = -3969
648113 XDOT = -1209
948745
YDOT = -23835
215499 feet/sec YDOT = -7264
973684 meter/sec
ZDOT = 1212
497085 ZDOT = 369
569112
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 12161
54883019
00016717 00000-0 10270-3 0 9084
2 25544 51
6352 160
5979 0010539 46
0312 314
1709 15
56281181 16825
Satellite: ISS
Catalog Number: 25544
Epoch time: 12161
54883019 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 160
5979 deg
Eccentricity:
0010539
Arg of perigee: 46
0312 deg
Mean anomaly: 314
1709 deg
Mean motion: 15
56281181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1682
Checksum: 303
Coasting Arc #10 (Orbit 1696)
---------------------------------------
Vector Time (GMT): 2012/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -763188
27 A = 6772862
35 meter
Y = 4628298
12 meter E =
0019851
Z = -4901178
17 I = 51
76610
XDOT = -7164
210049 Wp = 80
53178
YDOT = 1313
627483 meter/sec RA = 154
77171 deg
ZDOT = 2367
417558 TA = 212
58114
MA = 212
70378
Ha = 221
189 n
mi
Hp = 207
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2503898
52 X = -791077
37
Y = 15184705
12 feet Y = 4619608
20 meter
Z = -16079980
88 Z = -4904953
01
XDOT = -23504
626146 XDOT = -7189
867189
YDOT = 4309
801453 feet/sec YDOT = 1233
369170 meter/sec
ZDOT = 7767
117971 ZDOT = 2332
552033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14393770
76 X = 4387221
33
Y = 5399203
81 feet Y = 1645677
32 meter
Z = -16095916
38 Z = -4906035
31
XDOT = -102
115799 XDOT = -31
124895
YDOT = 22887
968539 feet/sec YDOT = 6976
252811 meter/sec
ZDOT = 7623
413186 ZDOT = 2323
616339
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 12162
51201502
00016717 00000-0 10270-3 0 9094
2 25544 51
6353 155
7805 0010556 49
1796 311
0272 15
56286258 16976
Satellite: ISS
Catalog Number: 25544
Epoch time: 12162
51201502 = yrday
fracday
Element set: 909
Inclination: 51
6353 deg
RA of node: 155
7805 deg
Eccentricity:
0010556
Arg of perigee: 49
1796 deg
Mean anomaly: 311
0272 deg
Mean motion: 15
56286258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1697
Checksum: 304
Coasting Arc #11 (Orbit 1712)
---------------------------------------
Vector Time (GMT): 2012/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3122747
76 A = 6777808
71 meter
Y = -4937594
37 meter E =
0021718
Z = 3424891
82 I = 51
80995
XDOT = 6102
978737 Wp = 72
67367
YDOT = 641
099325 meter/sec RA = 149
77267 deg
ZDOT = -4609
938712 TA = 67
27608
MA = 67
04668
Ha = 221
083 n
mi
Hp = 207
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10245235
42 X = 3161091
49
Y = -16199456
59 feet Y = -4902459
78 meter
Z = 11236521
74 Z = 3440154
71
XDOT = 20022
896119 XDOT = 6117
750298
YDOT = 2103
344243 feet/sec YDOT = 709
429612 meter/sec
ZDOT = -15124
470839 ZDOT = -4580
254759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14056608
64 X = -4284454
31
Y = -12975855
02 feet Y = -3955040
61 meter
Z = 11299805
46 Z = 3444180
70
XDOT = 4811
031559 XDOT = 1466
402419
YDOT = -18362
506389 feet/sec YDOT = -5596
891947 meter/sec
ZDOT = -15002
260710 ZDOT = -4572
689064
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 12163
53939201
00016717 00000-0 10270-3 0 9103
2 25544 51
6348 150
6403 0010548 52
3432 307
8677 15
56359776 17139
Satellite: ISS
Catalog Number: 25544
Epoch time: 12163
53939201 = yrday
fracday
Element set: 910
Inclination: 51
6348 deg
RA of node: 150
6403 deg
Eccentricity:
0010548
Arg of perigee: 52
3432 deg
Mean anomaly: 307
8677 deg
Mean motion: 15
56359776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1713
Checksum: 306
Coasting Arc #12 (Orbit 1727)
---------------------------------------
Vector Time (GMT): 2012/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4797139
79 A = 6782043
05 meter
Y = 4612039
74 meter E =
0019217
Z = -1277003
01 I = 51
84982
XDOT = -4146
150631 Wp = 48
61567
YDOT = -2708
993810 meter/sec RA = 144
79675 deg
ZDOT = 5860
762389 TA = 297
51842
MA = 297
71359
Ha = 221
126 n
mi
Hp = 207
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15738647
60 X = -4842152
61
Y = 15131363
97 feet Y = 4558143
59 meter
Z = -4189642
43 Z = -1300416
31
XDOT = -13602
856400 XDOT = -4144
020322
YDOT = -8887
774966 feet/sec YDOT = -2755
347258 meter/sec
ZDOT = 19228
223062 ZDOT = 5840
625425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12302993
77 X = 3749952
50
Y = 18013293
11 feet Y = 5490451
74 meter
Z = -4286481
44 Z = -1306519
54
XDOT = -9733
778202 XDOT = -2966
855596
YDOT = 11151
125847 feet/sec YDOT = 3398
863158 meter/sec
ZDOT = 19145
506838 ZDOT = 5835
550484
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 12164
50254055
00016717 00000-0 10270-3 0 9119
2 25544 51
6344 145
8229 0010615 57
0720 303
1454 15
56386725 17286
Satellite: ISS
Catalog Number: 25544
Epoch time: 12164
50254055 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 145
8229 deg
Eccentricity:
0010615
Arg of perigee: 57
0720 deg
Mean anomaly: 303
1454 deg
Mean motion: 15
56386725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1728
Checksum: 289
Coasting Arc #13 (Orbit 1743)
---------------------------------------
Vector Time (GMT): 2012/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5663679
03 A = 6782101
76 meter
Y = -3527486
39 meter E =
0014945
Z = -1220516
11 I = 51
87475
XDOT = 1641
462558 Wp = 97
63817
YDOT = 4645
348760 meter/sec RA = 139
83045 deg
ZDOT = -5872
132472 TA = 95
58430
MA = 95
41384
Ha = 221
164 n
mi
Hp = 207
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18581624
10 X = 5708632
19
Y = -11573118
08 feet Y = -3463900
15 meter
Z = -4004317
95 Z = -1192893
20
XDOT = 5385
375847 XDOT = 1617
920996
YDOT = 15240
645539 feet/sec YDOT = 4663
573580 meter/sec
ZDOT = -19265
526484 ZDOT = -5864
214979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8660677
27 X = -2639774
43
Y = -20127276
35 feet Y = -6134793
83 meter
Z = -3890217
77 Z = -1185738
38
XDOT = 14423
269611 XDOT = 4396
212577
YDOT = -2530
200053 feet/sec YDOT = -771
204976 meter/sec
ZDOT = -19233
314090 ZDOT = -5862
314135
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 12165
52987823
00016717 00000-0 10270-3 0 9129
2 25544 51
6347 140
6820 0010612 59
6354 300
5848 15
56409120 17448
Satellite: ISS
Catalog Number: 25544
Epoch time: 12165
52987823 = yrday
fracday
Element set: 912
Inclination: 51
6347 deg
RA of node: 140
6820 deg
Eccentricity:
0010612
Arg of perigee: 59
6354 deg
Mean anomaly: 300
5848 deg
Mean motion: 15
56409120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1744
Checksum: 301
Coasting Arc #14 (Orbit 1759)
---------------------------------------
Vector Time (GMT): 2012/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5562582
35 A = 6777704
71 meter
Y = 1806673
68 meter E =
0022307
Z = 3401485
51 I = 51
88309
XDOT = 885
759189 Wp = 78
05746
YDOT = -6055
438655 meter/sec RA = 134
85809 deg
ZDOT = 4643
710040 TA = 321
66072
MA = 321
81908
Ha = 221
106 n
mi
Hp = 207
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18249942
10 X = -5598895
30
Y = 5927407
09 feet Y = 1744266
01 meter
Z = 11159729
35 Z = 3374374
52
XDOT = 2906
034084 XDOT = 930
848235
YDOT = -19866
924722 feet/sec YDOT = -6045
281981 meter/sec
ZDOT = 15235
269161 ZDOT = 4648
121870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3448326
67 X = 1051049
97
Y = 18941689
24 feet Y = 5773426
88 meter
Z = 11047875
47 Z = 3367392
44
XDOT = -17936
675891 XDOT = -5467
098812
YDOT = -5672
429378 feet/sec YDOT = -1728
956475 meter/sec
ZDOT = 15253
981543 ZDOT = 4649
413574
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 12166
55719347
00016717 00000-0 10270-3 0 9138
2 25544 51
6347 135
5429 0010367 63
8812 296
3407 15
56469180 17602
Satellite: ISS
Catalog Number: 25544
Epoch time: 12166
55719347 = yrday
fracday
Element set: 913
Inclination: 51
6347 deg
RA of node: 135
5429 deg
Eccentricity:
0010367
Arg of perigee: 63
8812 deg
Mean anomaly: 296
3407 deg
Mean motion: 15
56469180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1760
Checksum: 324
Coasting Arc #15 (Orbit 1774)
---------------------------------------
Vector Time (GMT): 2012/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 923792
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4669110
17 A = 6772490
72 meter
Y = 416738
20 meter E =
0022374
Z = -4908917
95 I = 51
88657
XDOT = -3081
235346 Wp = 70
24434
YDOT = 6593
270404 meter/sec RA = 129
86471 deg
ZDOT = -2372
404833 TA = 176
56490
MA = 176
54951
Ha = 221
094 n
mi
Hp = 207
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15318602
91 X = 4687949
71
Y = 1367251
31 feet Y = 469057
07 meter
Z = -16105373
86 Z = -4886189
61
XDOT = -10109
039850 XDOT = -3143
208934
YDOT = 21631
464579 feet/sec YDOT = 6558
467922 meter/sec
ZDOT = -7783
480422 ZDOT = -2387
523125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3136973
22 X = 956149
44
Y = -15155685
87 feet Y = -4619453
05 meter
Z = -16011765
15 Z = -4880386
02
XDOT = 19219
515069 XDOT = 5858
108193
YDOT = 12262
734008 feet/sec YDOT = 3737
681326 meter/sec
ZDOT = -7846
366868 ZDOT = -2391
572622
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 12167
52028502
00016717 00000-0 10270-3 0 9143
2 25544 51
6349 130
7232 0010496 66
8738 293
3521 15
56456361 17753
Satellite: ISS
Catalog Number: 25544
Epoch time: 12167
52028502 = yrday
fracday
Element set: 914
Inclination: 51
6349 deg
RA of node: 130
7232 deg
Eccentricity:
0010496
Arg of perigee: 66
8738 deg
Mean anomaly: 293
3521 deg
Mean motion: 15
56456361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1775
Checksum: 310
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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