[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 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 3453)
---------------------------------------
Vector Time (GMT): 2012/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3651917
13 A = 6799416
33 meter
Y = 5561874
21 meter E =
0031702
Z = 1325535
81 I = 51
40790
XDOT = -4724
097790 Wp = 119
57668
YDOT = -1697
358283 meter/sec RA = 312
43711 deg
ZDOT = -5803
815607 TA = 45
94743
MA = 45
68677
Ha = 233
245 n
mi
Hp = 214
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11981355
43 X = -3720279
00
Y = 18247618
79 feet Y = 5520654
11 meter
Z = 4348870
78 Z = 1307627
98
XDOT = -15499
008498 XDOT = -4676
572401
YDOT = -5568
760772 feet/sec YDOT = -1749
921056 meter/sec
ZDOT = -19041
389788 ZDOT = -5826
649771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8720867
75 X = 2658120
49
Y = -20027938
40 feet Y = -6104515
62 meter
Z = 4274259
66 Z = 1302794
34
XDOT = 14646
078156 XDOT = 4464
124622
YDOT = 2229
988412 feet/sec YDOT = 679
700468 meter/sec
ZDOT = -19135
589432 ZDOT = -5832
527659
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 12275
53486261
00016717 00000-0 10270-3 0 9009
2 25544 51
6473 312
8903 0017946 119
4696 240
8247 15
50423460 34540
Satellite: ISS
Catalog Number: 25544
Epoch time: 12275
53486261 = yrday
fracday
Element set: 900
Inclination: 51
6473 deg
RA of node: 312
8903 deg
Eccentricity:
0017946
Arg of perigee: 119
4696 deg
Mean anomaly: 240
8247 deg
Mean motion: 15
50423460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 313
Coasting Arc #2 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2012/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3510568
47 A = 6799712
57 meter
Y = -5758253
80 meter E =
0021555
Z = -896939
27 I = 51
38935
XDOT = 4512
906943 Wp = 94
92607
YDOT = 1851
822168 meter/sec RA = 307
46590 deg
ZDOT = 5895
873160 TA = 255
36063
MA = 255
59971
Ha = 233
194 n
mi
Hp = 214
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11517613
09 X = 3579054
75
Y = -18891908
80 feet Y = -5718613
60 meter
Z = -2942714
15 Z = -879717
84
XDOT = 14806
125141 XDOT = 4463
222747
YDOT = 6075
532047 feet/sec YDOT = 1902
011128 meter/sec
ZDOT = 19343
415879 ZDOT = 5917
676159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7790362
73 X = -2374502
56
Y = 20719248
17 feet Y = 6315226
84 meter
Z = -2870923
17 Z = -875057
38
XDOT = -14055
150612 XDOT = -4284
009907
YDOT = -2648
379436 feet/sec YDOT = -807
226052 meter/sec
ZDOT = 19433
334796 ZDOT = 5923
280446
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 12276
50169717
00016717 00000-0 10270-3 0 9012
2 25544 51
6471 308
0980 0017956 122
8660 237
4222 15
50447957 34698
Satellite: ISS
Catalog Number: 25544
Epoch time: 12276
50169717 = yrday
fracday
Element set: 901
Inclination: 51
6471 deg
RA of node: 308
0980 deg
Eccentricity:
0017956
Arg of perigee: 122
8660 deg
Mean anomaly: 237
4222 deg
Mean motion: 15
50447957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 324
Coasting Arc #3 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2012/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3400506
73 A = 6799896
39 meter
Y = 5861890
38 meter E =
0030667
Z = 351371
64 I = 51
37240
XDOT = -4312
613388 Wp = 128
16601
YDOT = -2123
136763 meter/sec RA = 302
49273 deg
ZDOT = -5979
448924 TA = 48
03361
MA = 47
77273
Ha = 233
065 n
mi
Hp = 214
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11156518
14 X = -3467509
79
Y = 19231923
82 feet Y = 5823489
19 meter
Z = 1152794
09 Z = 334688
56
XDOT = -14148
994054 XDOT = -4259
504167
YDOT = -6965
671793 feet/sec YDOT = -2171
066679 meter/sec
ZDOT = -19617
614579 ZDOT = -6000
270586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6999172
04 X = 2133347
64
Y = -21106917
10 feet Y = -6433388
33 meter
Z = 1083220
32 Z = 330165
55
XDOT = 13616
843073 XDOT = 4150
413769
YDOT = 3443
813332 feet/sec YDOT = 1049
674304 meter/sec
ZDOT = -19703
448131 ZDOT = -6005
610990
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 12277
53295986
00016717 00000-0 10270-3 0 9025
2 25544 51
6469 302
9844 0018022 126
5244 233
7569 15
50488139 34859
Satellite: ISS
Catalog Number: 25544
Epoch time: 12277
53295986 = yrday
fracday
Element set: 902
Inclination: 51
6469 deg
RA of node: 302
9844 deg
Eccentricity:
0018022
Arg of perigee: 126
5244 deg
Mean anomaly: 233
7569 deg
Mean motion: 15
50488139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 338
Coasting Arc #4 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2012/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3223031
66 A = 6799771
61 meter
Y = -5988210
46 meter E =
0022987
Z = 114481
08 I = 51
35717
XDOT = 4153
608246 Wp = 97
52496
YDOT = 2369
727804 meter/sec RA = 297
51927 deg
ZDOT = 5976
849606 TA = 263
70987
MA = 263
97175
Ha = 232
957 n
mi
Hp = 214
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10574250
86 X = 3289197
40
Y = -19646359
76 feet Y = -5951798
54 meter
Z = 375594
10 Z = 130299
86
XDOT = 13627
323643 XDOT = 4097
766058
YDOT = 7774
697521 feet/sec YDOT = 2415
864261 meter/sec
ZDOT = 19609
086635 ZDOT = 5996
892175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5966487
13 X = -1818585
28
Y = 21497472
40 feet Y = 6552429
59 meter
Z = 441606
15 Z = 134601
55
XDOT = -13324
304051 XDOT = -4061
247875
YDOT = -4162
161973 feet/sec YDOT = -1268
626969 meter/sec
ZDOT = 19691
675207 ZDOT = 6002
022603
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 12278
56419444
00016717 00000-0 10270-3 0 9037
2 25544 51
6470 297
8723 0017961 130
1625 230
1102 15
50537954 35017
Satellite: ISS
Catalog Number: 25544
Epoch time: 12278
56419444 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 297
8723 deg
Eccentricity:
0017961
Arg of perigee: 130
1625 deg
Mean anomaly: 230
1102 deg
Mean motion: 15
50537954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 298
Coasting Arc #5 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2012/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3088798
71 A = 6799522
43 meter
Y = 6004640
80 meter E =
0028482
Z = -688411
20 I = 51
34281
XDOT = -4013
435077 Wp = 135
66861
YDOT = -2726
205641 meter/sec RA = 292
54362 deg
ZDOT = -5940
495565 TA = 51
79407
MA = 51
53794
Ha = 232
834 n
mi
Hp = 214
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10133854
05 X = -3152370
09
Y = 19700265
10 feet Y = 5969744
44 meter
Z = -2258566
91 Z = -703571
48
XDOT = -13167
437916 XDOT = -3953
793745
YDOT = -8944
244228 feet/sec YDOT = -2770
753288 meter/sec
ZDOT = -19489
814846 ZDOT = -5959
847910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5144074
34 X = 1567913
86
Y = -21541681
73 feet Y = -6565904
59 meter
Z = -2321855
86 Z = -707701
67
XDOT = 13230
136955 XDOT = 4032
545744
YDOT = 5210
477183 feet/sec YDOT = 1588
153446 meter/sec
ZDOT = -19569
516090 ZDOT = -5964
788504
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 12279
53095192
00016717 00000-0 10270-3 0 9046
2 25544 51
6464 293
0779 0018017 133
6794 226
5854 15
50557456 35165
Satellite: ISS
Catalog Number: 25544
Epoch time: 12279
53095192 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 293
0779 deg
Eccentricity:
0018017
Arg of perigee: 133
6794 deg
Mean anomaly: 226
5854 deg
Mean motion: 15
50557456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 335
Coasting Arc #6 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2012/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2897505
84 A = 6798911
52 meter
Y = -6037695
22 meter E =
0024512
Z = 1174570
76 I = 51
33074
XDOT = 3928
473354 Wp = 103
86455
YDOT = 3039
907717 meter/sec RA = 287
56789 deg
ZDOT = 5826
530978 TA = 268
91846
MA = 269
19931
Ha = 232
672 n
mi
Hp = 214
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9506252
75 X = 2959099
37
Y = -19808711
35 feet Y = -6004949
04 meter
Z = 3853578
60 Z = 1188796
87
XDOT = 12888
692105 XDOT = 3865
884137
YDOT = 9973
450515 feet/sec YDOT = 3083
488749 meter/sec
ZDOT = 19115
915283 ZDOT = 5845
463372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4128822
06 X = -1258464
96
Y = 21569542
61 feet Y = 6574396
59 meter
Z = 3913005
82 Z = 1192684
17
XDOT = -13316
577347 XDOT = -4058
892775
YDOT = -6094
741725 feet/sec YDOT = -1857
677278 meter/sec
ZDOT = 19193
852743 ZDOT = 5850
286316
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 12280
56213078
00016717 00000-0 10270-3 0 9057
2 25544 51
6464 287
9657 0017927 137
4852 222
7691 15
50632014 35327
Satellite: ISS
Catalog Number: 25544
Epoch time: 12280
56213078 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 287
9657 deg
Eccentricity:
0017927
Arg of perigee: 137
4852 deg
Mean anomaly: 222
7691 deg
Mean motion: 15
50632014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 318
Coasting Arc #7 (Orbit 3546)
---------------------------------------
Vector Time (GMT): 2012/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2766649
17 A = 6798168
14 meter
Y = 5946633
07 meter E =
0025380
Z = -1753659
51 I = 51
31935
XDOT = -3867
092876 Wp = 140
83859
YDOT = -3447
196339 meter/sec RA = 282
58951 deg
ZDOT = -5652
636497 TA = 58
48406
MA = 58
23637
Ha = 232
544 n
mi
Hp = 214
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9076932
98 X = -2824421
06
Y = 19509951
02 feet Y = 5915371
55 meter
Z = -5753476
09 Z = -1767240
60
XDOT = -12687
312586 XDOT = -3800
798651
YDOT = -11309
699276 feet/sec YDOT = -3490
070250 meter/sec
ZDOT = -18545
395330 ZDOT = -5671
261636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3413778
85 X = 1040519
79
Y = -21230139
32 feet Y = -6470946
47 meter
Z = -5810222
60 Z = -1770955
85
XDOT = 13620
918152 XDOT = 4151
655853
YDOT = 7229
638354 feet/sec YDOT = 2203
593770 meter/sec
ZDOT = -18622
027145 ZDOT = -5675
993874
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 12281
52883681
00016717 00000-0 10270-3 0 9068
2 25544 51
6456 283
1709 0017936 140
8113 219
4340 15
50637466 35478
Satellite: ISS
Catalog Number: 25544
Epoch time: 12281
52883681 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 283
1709 deg
Eccentricity:
0017936
Arg of perigee: 140
8113 deg
Mean anomaly: 219
4340 deg
Mean motion: 15
50637466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3547
Checksum: 320
Coasting Arc #8 (Orbit 3562)
---------------------------------------
Vector Time (GMT): 2012/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2592213
07 A = 6797104
54 meter
Y = -5871022
64 meter E =
0025600
Z = 2237333
14 I = 51
31065
XDOT = 3867
169655 Wp = 113
51723
YDOT = 3793
186647 meter/sec RA = 277
61118 deg
ZDOT = 5413
657777 TA = 271
42686
MA = 271
72011
Ha = 232
350 n
mi
Hp = 214
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8504636
04 X = 2646802
84
Y = -19261885
30 feet Y = -5841729
52 meter
Z = 7340331
83 Z = 2250059
09
XDOT = 12687
564486 XDOT = 3798
167461
YDOT = 12444
838080 feet/sec YDOT = 3836
046292 meter/sec
ZDOT = 17761
344414 ZDOT = 5432
276631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2562051
10 X = -780913
18
Y = 20880640
48 feet Y = 6364419
22 meter
Z = 7393529
49 Z = 2253547
79
XDOT = -14104
112915 XDOT = -4298
933616
YDOT = -8115
384725 feet/sec YDOT = -2473
569264 meter/sec
ZDOT = 17837
922914 ZDOT = 5436
998904
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 12282
55995893
00016717 00000-0 10270-3 0 9072
2 25544 51
6452 278
0584 0017855 144
9161 215
3170 15
50724805 35634
Satellite: ISS
Catalog Number: 25544
Epoch time: 12282
55995893 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 278
0584 deg
Eccentricity:
0017855
Arg of perigee: 144
9161 deg
Mean anomaly: 215
3170 deg
Mean motion: 15
50724805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3563
Checksum: 330
Coasting Arc #9 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2012/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2499278
69 A = 6795898
06 meter
Y = 5663027
13 meter E =
0022090
Z = -2792325
92 I = 51
30301
XDOT = -3889
067952 Wp = 142
00965
YDOT = -4207
474403 meter/sec RA = 272
62958 deg
ZDOT = -5090
731480 TA = 69
78431
MA = 69
54691
Ha = 232
215 n
mi
Hp = 214
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8199733
24 X = -2548853
49
Y = 18579485
34 feet Y = 5634801
23 meter
Z = -9161174
29 Z = -2804588
25
XDOT = -12759
409290 XDOT = -3817
000228
YDOT = -13804
049877 feet/sec YDOT = -4250
561826 meter/sec
ZDOT = -16701
874934 ZDOT = -5109
449168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2108930
01 X = 642801
87
Y = -20175321
93 feet Y = -6149438
12 meter
Z = -9212427
16 Z = -2807947
80
XDOT = 14783
915225 XDOT = 4506
137361
YDOT = 9149
375218 feet/sec YDOT = 2788
729566 meter/sec
ZDOT = -16778
829576 ZDOT = -5114
187255
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 12283
52661182
00016717 00000-0 10270-3 0 9082
2 25544 51
6446 273
2630 0017825 147
9330 212
2909 15
50726390 35787
Satellite: ISS
Catalog Number: 25544
Epoch time: 12283
52661182 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 273
2630 deg
Eccentricity:
0017825
Arg of perigee: 147
9330 deg
Mean anomaly: 212
2909 deg
Mean motion: 15
50726390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3578
Checksum: 313
Coasting Arc #10 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2012/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2377147
09 A = 6794504
37 meter
Y = -5475045
35 meter E =
0025867
Z = 3244893
42 I = 51
29838
XDOT = 3970
050720 Wp = 125
72205
YDOT = 4544
629140 meter/sec RA = 267
64835 deg
ZDOT = 4718
224584 TA = 272
01315
MA = 272
30936
Ha = 232
002 n
mi
Hp = 215
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7799039
00 X = 2422430
42
Y = -17962747
22 feet Y = -5448209
11 meter
Z = 10645975
79 Z = 3256552
09
XDOT = 13025
100788 XDOT = 3896
016414
YDOT = 14910
200590 feet/sec YDOT = 4588
611216 meter/sec
ZDOT = 15479
739448 ZDOT = 4737
330807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1571024
43 X = -478848
25
Y = 19493004
61 feet Y = 5941467
81 meter
Z = 10694706
68 Z = 3259746
60
XDOT = -15604
441793 XDOT = -4756
233858
YDOT = -9867
854373 feet/sec YDOT = -3007
722013 meter/sec
ZDOT = 15558
276883 ZDOT = 4742
162794
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 12284
55767589
00016717 00000-0 10270-3 0 9095
2 25544 51
6442 268
1500 0017763 152
3203 207
8897 15
50814435 35944
Satellite: ISS
Catalog Number: 25544
Epoch time: 12284
55767589 = yrday
fracday
Element set: 909
Inclination: 51
6442 deg
RA of node: 268
1500 deg
Eccentricity:
0017763
Arg of perigee: 152
3203 deg
Mean anomaly: 207
8897 deg
Mean motion: 15
50814435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3594
Checksum: 333
Coasting Arc #11 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2012/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2358632
95 A = 6793002
16 meter
Y = 5155078
40 meter E =
0019845
Z = -3741057
36 I = 51
29552
XDOT = -4061
657406 Wp = 138
34467
YDOT = -4918
007266 meter/sec RA = 262
66322 deg
ZDOT = -4243
671838 TA = 86
54922
MA = 86
32225
Ha = 231
858 n
mi
Hp = 215
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7738297
09 X = -2397929
43
Y = 16912986
86 feet Y = 5128482
56 meter
Z = -12273810
24 Z = -3752611
62
XDOT = -13325
647656 XDOT = -3985
746356
YDOT = -16135
194441 feet/sec YDOT = -4963
003284 meter/sec
ZDOT = -13922
807867 ZDOT = -4263
218433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1522328
97 X = 464005
87
Y = -18504752
71 feet Y = -5640248
63 meter
Z = -12322070
67 Z = -3755767
14
XDOT = 16550
027562 XDOT = 5044
448401
YDOT = 10626
073995 feet/sec YDOT = 3238
827354 meter/sec
ZDOT = -14003
139600 ZDOT = -4268
156950
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 12285
52427365
00016717 00000-0 10270-3 0 9100
2 25544 51
6440 263
3540 0017718 155
1845 205
0162 15
50818840 36092
Satellite: ISS
Catalog Number: 25544
Epoch time: 12285
52427365 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 263
3540 deg
Eccentricity:
0017718
Arg of perigee: 155
1845 deg
Mean anomaly: 205
0162 deg
Mean motion: 15
50818840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3609
Checksum: 296
Coasting Arc #12 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2012/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2323480
84 A = 6791478
84 meter
Y = -4865422
23 meter E =
0025068
Z = 4128702
55 I = 51
29604
XDOT = 4201
480559 Wp = 139
55810
YDOT = 5204
220461 meter/sec RA = 257
67909 deg
ZDOT = 3736
840686 TA = 271
61677
MA = 271
90390
Ha = 231
629 n
mi
Hp = 215
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7622968
63 X = 2357657
76
Y = -15962671
35 feet Y = -4839248
00 meter
Z = 13545612
03 Z = 4140073
67
XDOT = 13784
385035 XDOT = 4124
820658
YDOT = 17074
214112 feet/sec YDOT = 5250
775878 meter/sec
ZDOT = 12259
976003 ZDOT = 3757
064681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1423886
26 X = -434000
53
Y = 17595477
52 feet Y = 5363101
55 meter
Z = 13593081
02 Z = 4143171
09
XDOT = -17568
380103 XDOT = -5354
842255
YDOT = -11036
884595 feet/sec YDOT = -3364
042425 meter/sec
ZDOT = 12343
090168 ZDOT = 3762
173883
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 12286
55527816
00016717 00000-0 10270-3 0 9117
2 25544 51
6440 258
2405 0017672 159
6939 200
4918 15
50903935 36253
Satellite: ISS
Catalog Number: 25544
Epoch time: 12286
55527816 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 258
2405 deg
Eccentricity:
0017672
Arg of perigee: 159
6939 deg
Mean anomaly: 200
4918 deg
Mean motion: 15
50903935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 324
Coasting Arc #13 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2012/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2410970
88 A = 6789983
85 meter
Y = 4454608
71 meter E =
0019714
Z = -4527266
56 I = 51
29898
XDOT = -4329
719908 Wp = 133
03355
YDOT = -5491
997392 meter/sec RA = 252
69081 deg
ZDOT = -3119
918382 TA = 105
60566
MA = 105
38800
Ha = 231
476 n
mi
Hp = 215
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7910009
45 X = -2438611
24
Y = 14614857
97 feet Y = 4427492
60 meter
Z = -14853236
76 Z = -4539046
86
XDOT = -14205
117809 XDOT = -4252
829334
YDOT = -18018
364146 feet/sec YDOT = -5539
985508 meter/sec
ZDOT = -10235
952696 ZDOT = -3140
764837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1877512
02 X = 572265
66
Y = -16467415
25 feet Y = -5019268
17 meter
Z = -14902353
81 Z = -4542237
44
XDOT = 18590
258406 XDOT = 5666
310762
YDOT = 11395
599611 feet/sec YDOT = 3473
378761 meter/sec
ZDOT = -10321
621085 ZDOT = -3146
030107
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 12287
52181902
00016717 00000-0 10270-3 0 9128
2 25544 51
6443 253
4440 0017625 162
6517 197
5240 15
50911885 36400
Satellite: ISS
Catalog Number: 25544
Epoch time: 12287
52181902 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 253
4440 deg
Eccentricity:
0017625
Arg of perigee: 162
6517 deg
Mean anomaly: 197
5240 deg
Mean motion: 15
50911885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 302
Coasting Arc #14 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2012/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2489628
02 A = 6788610
20 meter
Y = -4089013
40 meter E =
0023098
Z = 4812562
54 I = 51
30567
XDOT = 4488
039480 Wp = 153
74472
YDOT = 5691
030393 meter/sec RA = 247
70447 deg
ZDOT = 2488
705162 TA = 271
53442
MA = 271
79900
Ha = 231
230 n
mi
Hp = 215
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8168070
93 X = 2511788
33
Y = -13415398
31 feet Y = -4061048
34 meter
Z = 15789247
18 Z = 4824711
62
XDOT = 14724
538976 XDOT = 4411
977794
YDOT = 18671
359558 feet/sec YDOT = 5740
793470 meter/sec
ZDOT = 8165
043182 ZDOT = 2510
322881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2288406
81 X = -697506
40
Y = 15487184
67 feet Y = 4720493
89 meter
Z = 15839852
48 Z = 4827987
03
XDOT = -19599
518098 XDOT = -5973
933116
YDOT = -11421
365726 feet/sec YDOT = -3481
232273 meter/sec
ZDOT = 8253
887975 ZDOT = 2515
785055
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 12288
55276259
00016717 00000-0 10270-3 0 9133
2 25544 51
6448 248
3302 0017593 167
0840 193
0766 15
50994536 36562
Satellite: ISS
Catalog Number: 25544
Epoch time: 12288
55276259 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 248
3302 deg
Eccentricity:
0017593
Arg of perigee: 167
0840 deg
Mean anomaly: 193
0766 deg
Mean motion: 15
50994536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 339
Coasting Arc #15 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2012/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2701951
23 A = 6787496
20 meter
Y = 3623528
49 meter E =
0021318
Z = -5073482
01 I = 51
31507
XDOT = -4602
373107 Wp = 132
14557
YDOT = -5860
230867 meter/sec RA = 242
71430 deg
ZDOT = -1753
150899 TA = 120
89801
MA = 120
68821
Ha = 231
069 n
mi
Hp = 215
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8864669
39 X = -2717622
99
Y = 11888216
83 feet Y = 3593225
45 meter
Z = -16645282
18 Z = -5086646
73
XDOT = -15099
649302 XDOT = -4527
984089
YDOT = -19226
479222 feet/sec YDOT = -5911
281721 meter/sec
ZDOT = -5751
807410 ZDOT = -1775
328310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3266908
16 X = 995753
61
Y = -14401851
70 feet Y = -4389684
40 meter
Z = -16700043
72 Z = -5090173
32
XDOT = 20454
476942 XDOT = 6234
524572
YDOT = 11344
042235 feet/sec YDOT = 3457
664073 meter/sec
ZDOT = -5842
955879 ZDOT = -1780
932952
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 12289
51924520
00016717 00000-0 10270-3 0 9142
2 25544 51
6453 243
5336 0017552 170
2721 189
8773 15
51005641 36710
Satellite: ISS
Catalog Number: 25544
Epoch time: 12289
51924520 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 243
5336 deg
Eccentricity:
0017552
Arg of perigee: 170
2721 deg
Mean anomaly: 189
8773 deg
Mean motion: 15
51005641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 306
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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