[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 28th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18836 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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 3839)
---------------------------------------
Vector Time (GMT): 2012/300/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5552747
17 A = 6795393
38 meter
Y = 2914583
37 meter E =
0017764
Z = -2586481
13 I = 51
60096
XDOT = -4311
580959 Wp = 196
04332
YDOT = 3558
641112 meter/sec RA = 188
61481 deg
ZDOT = -5254
255087 TA = 13
06836
MA = 13
02239
Ha = 228
809 n
mi
Hp = 218
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18217674
45 X = 5532307
77
Y = 9562281
40 feet Y = 2976563
15 meter
Z = -8485830
48 Z = -2559555
54
XDOT = -14145
606821 XDOT = -4325
529519
YDOT = 11675
331733 feet/sec YDOT = 3510
347876 meter/sec
ZDOT = -17238
369709 ZDOT = -5275
235125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16802537
12 X = -5121413
31
Y = -11952831
59 feet Y = -3643223
07 meter
Z = -8374650
46 Z = -2552593
46
XDOT = 14622
627819 XDOT = 4456
976959
YDOT = -8435
390257 feet/sec YDOT = -2571
106950 meter/sec
ZDOT = -17325
508545 ZDOT = -5280
815004
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 12300
41003668
00016717 00000-0 10270-3 0 9001
2 25544 51
6475 189
5381 0016410 212
5768 147
4372 15
51099055 38401
Satellite: ISS
Catalog Number: 25544
Epoch time: 12300
41003668 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 189
5381 deg
Eccentricity:
0016410
Arg of perigee: 212
5768 deg
Mean anomaly: 147
4372 deg
Mean motion: 15
51099055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3840
Checksum: 296
Coasting Arc #2 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2012/301/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5281960
67 A = 6793873
99 meter
Y = -2863097
81 meter E =
0012616
Z = 3183384
63 I = 51
62609
XDOT = 4810
062335 Wp = 165
93651
YDOT = -3508
837046 meter/sec RA = 183
65287 deg
ZDOT = 4809
204884 TA = 230
73338
MA = 230
84537
Ha = 228
502 n
mi
Hp = 218
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17329267
30 X = -5265016
85
Y = -9393365
51 feet Y = -2922069
00 meter
Z = 10444175
31 Z = 3157765
93
XDOT = 15781
044407 XDOT = 4825
578834
YDOT = -11511
932564 feet/sec YDOT = -3454
960775 meter/sec
ZDOT = 15778
231246 ZDOT = 4832
610439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16155519
03 X = 4924202
20
Y = 11390191
37 feet Y = 3471730
33 meter
Z = 10338392
73 Z = 3151142
10
XDOT = -16108
546662 XDOT = -4909
885023
YDOT = 8390
390225 feet/sec YDOT = 2557
390941 meter/sec
ZDOT = 15875
412435 ZDOT = 4838
825710
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 12301
44086789
00016717 00000-0 10270-3 0 9011
2 25544 51
6472 184
4231 0016414 216
4423 143
5612 15
51130472 38561
Satellite: ISS
Catalog Number: 25544
Epoch time: 12301
44086789 = yrday
fracday
Element set: 901
Inclination: 51
6472 deg
RA of node: 184
4231 deg
Eccentricity:
0016414
Arg of perigee: 216
4423 deg
Mean anomaly: 143
5612 deg
Mean motion: 15
51130472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 286
Coasting Arc #3 (Orbit 3870)
---------------------------------------
Vector Time (GMT): 2012/302/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4890676
62 A = 6792080
23 meter
Y = 2848418
18 meter E =
0012412
Z = -3740753
35 I = 51
65151
XDOT = -5311
153210 Wp = 203
73526
YDOT = 3507
585951 meter/sec RA = 178
69084 deg
ZDOT = -4279
115405 TA = 20
93937
MA = 20
88858
Ha = 228
241 n
mi
Hp = 218
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16045526
98 X = 4876633
72
Y = 9345204
01 feet Y = 2903030
00 meter
Z = -12272812
84 Z = -3717028
38
XDOT = -17425
043340 XDOT = -5329
193526
YDOT = 11507
827923 feet/sec YDOT = 3448
092148 meter/sec
ZDOT = -14039
092535 ZDOT = -4304
961460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15088031
36 X = -4598831
96
Y = -10933333
15 feet Y = -3332479
94 meter
Z = -12174861
21 Z = -3710897
70
XDOT = 17620
428674 XDOT = 5370
706660
YDOT = -8586
169390 feet/sec YDOT = -2617
064430 meter/sec
ZDOT = -14146
385634 ZDOT = -4311
818341
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 12302
40724918
00016717 00000-0 10270-3 0 9022
2 25544 51
6477 179
6275 0016351 220
1727 139
8217 15
51180614 38718
Satellite: ISS
Catalog Number: 25544
Epoch time: 12302
40724918 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 179
6275 deg
Eccentricity:
0016351
Arg of perigee: 220
1727 deg
Mean anomaly: 139
8217 deg
Mean motion: 15
51180614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3871
Checksum: 304
Coasting Arc #4 (Orbit 3886)
---------------------------------------
Vector Time (GMT): 2012/303/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4480913
57 A = 6790408
81 meter
Y = -2870453
77 meter E =
0014552
Z = 4228995
87 I = 51
67588
XDOT = 5723
134199 Wp = 186
28154
YDOT = -3533
548774 meter/sec RA = 173
72875 deg
ZDOT = 3652
709180 TA = 226
19035
MA = 226
31078
Ha = 227
925 n
mi
Hp = 219
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14701160
00 X = -4469026
58
Y = -9417499
25 feet Y = -2920495
45 meter
Z = 13874658
37 Z = 4207256
24
XDOT = 18776
687006 XDOT = 5744
477198
YDOT = -11593
007789 feet/sec YDOT = -3469
429577 meter/sec
ZDOT = 11983
954001 ZDOT = 3680
564697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13938015
04 X = 4248306
98
Y = 10631426
13 feet Y = 3240458
69 meter
Z = 13784921
37 Z = 4201644
03
XDOT = -18839
644005 XDOT = -5742
323493
YDOT = 8955
224012 feet/sec YDOT = 2729
552279 meter/sec
ZDOT = 12099
580710 ZDOT = 3687
952201
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 12303
43803238
00016717 00000-0 10270-3 0 9030
2 25544 51
6471 174
5119 0016381 224
0177 135
9671 15
51203399 38872
Satellite: ISS
Catalog Number: 25544
Epoch time: 12303
43803238 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 174
5119 deg
Eccentricity:
0016381
Arg of perigee: 224
0177 deg
Mean anomaly: 135
9671 deg
Mean motion: 15
51203399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3887
Checksum: 306
Coasting Arc #5 (Orbit 3901)
---------------------------------------
Vector Time (GMT): 2012/304/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3966671
60 A = 6788636
09 meter
Y = 2952458
57 meter E =
0007844
Z = -4645496
81 I = 51
70109
XDOT = -6106
371888 Wp = 198
39566
YDOT = 3582
490052 meter/sec RA = 168
76621 deg
ZDOT = -2943
128061 TA = 42
35097
MA = 42
29044
Ha = 227
609 n
mi
Hp = 219
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13014014
43 X = 3955929
18
Y = 9686543
85 feet Y = 2996756
13 meter
Z = -15241131
27 Z = -4626252
57
XDOT = -20034
028504 XDOT = -6131
680743
YDOT = 11753
576287 feet/sec YDOT = 3514
063168 meter/sec
ZDOT = -9655
931959 ZDOT = -2972
854977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12425799
78 X = -3787383
77
Y = -10545487
93 feet Y = -3214264
72 meter
Z = -15161727
14 Z = -4621294
43
XDOT = 19951
000489 XDOT = 6081
064949
YDOT = -9476
221970 feet/sec YDOT = -2888
352457 meter/sec
ZDOT = -9779
326220 ZDOT = -2980
738632
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 12304
40436853
00016717 00000-0 10270-3 0 9044
2 25544 51
6475 169
7159 0016314 227
8763 132
1003 15
51260976 39024
Satellite: ISS
Catalog Number: 25544
Epoch time: 12304
40436853 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 169
7159 deg
Eccentricity:
0016314
Arg of perigee: 227
8763 deg
Mean anomaly: 132
1003 deg
Mean motion: 15
51260976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3902
Checksum: 302
Coasting Arc #6 (Orbit 3917)
---------------------------------------
Vector Time (GMT): 2012/305/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3455217
29 A = 6787279
24 meter
Y = -3082721
56 meter E =
0015483
Z = 4973419
95 I = 51
72582
XDOT = 6378
155300 Wp = 208
91148
YDOT = -3634
046174 meter/sec RA = 163
80374 deg
ZDOT = 2168
218345 TA = 219
88067
MA = 219
99454
Ha = 227
297 n
mi
Hp = 219
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11336014
73 X = -3444649
26
Y = -10113915
89 feet Y = -3121300
77 meter
Z = 16316994
58 Z = 4956659
93
XDOT = 20925
706365 XDOT = 6407
784914
YDOT = -11922
723667 feet/sec YDOT = -3562
555945 meter/sec
ZDOT = 7113
577249 ZDOT = 2199
276028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10914675
05 X = 3326792
95
Y = 10673190
38 feet Y = 3253188
43 meter
Z = 16247883
32 Z = 4952354
84
XDOT = -20674
619406 XDOT = -6301
623995
YDOT = 10064
928796 feet/sec YDOT = 3067
790297 meter/sec
ZDOT = 7242
504100 ZDOT = 2207
515250
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 12305
43510360
00016717 00000-0 10270-3 0 9055
2 25544 51
6469 164
5998 0016380 231
7581 128
2096 15
51282825 39188
Satellite: ISS
Catalog Number: 25544
Epoch time: 12305
43510360 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 164
5998 deg
Eccentricity:
0016380
Arg of perigee: 231
7581 deg
Mean anomaly: 128
2096 deg
Mean motion: 15
51282825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3918
Checksum: 317
Coasting Arc #7 (Orbit 3932)
---------------------------------------
Vector Time (GMT): 2012/306/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2867438
04 A = 6786092
54 meter
Y = 3284599
57 meter E =
0006704
Z = -5198843
92 I = 51
75174
XDOT = -6596
304592 Wp = 178
76064
YDOT = 3672
622165 meter/sec RA = 158
84102 deg
ZDOT = -1324
443037 TA = 78
56684
MA = 78
49154
Ha = 226
928 n
mi
Hp = 219
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9407605
13 X = 2855751
31
Y = 10776245
30 feet Y = 3316599
67 meter
Z = -17056574
53 Z = -5184942
08
XDOT = -21641
419264 XDOT = -6630
448351
YDOT = 12049
285319 feet/sec YDOT = 3598
667251 meter/sec
ZDOT = -4345
285554 ZDOT = -1356
571367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9152055
98 X = -2789546
66
Y = -11082438
69 feet Y = -3377927
31 meter
Z = -16999313
39 Z = -5181390
72
XDOT = 21191
223444 XDOT = 6459
084906
YDOT = -10663
427260 feet/sec YDOT = -3250
212629 meter/sec
ZDOT = -4478
669045 ZDOT = -1365
098325
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 12306
40139494
00016717 00000-0 10270-3 0 9069
2 25544 51
6472 159
8031 0016323 235
7390 124
2216 15
51338080 39338
Satellite: ISS
Catalog Number: 25544
Epoch time: 12306
40139494 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 159
8031 deg
Eccentricity:
0016323
Arg of perigee: 235
7390 deg
Mean anomaly: 124
2216 deg
Mean motion: 15
51338080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3933
Checksum: 291
Coasting Arc #8 (Orbit 3948)
---------------------------------------
Vector Time (GMT): 2012/307/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2310105
73 A = 6785487
29 meter
Y = -3535198
32 meter E =
0014854
Z = 5321838
20 I = 51
77791
XDOT = 6696
442511 Wp = 231
57994
YDOT = -3681
157857 meter/sec RA = 153
87948 deg
ZDOT = 453
332187 TA = 214
04925
MA = 214
14464
Ha = 226
613 n
mi
Hp = 219
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7579087
04 X = -2296255
60
Y = -11598419
70 feet Y = -3560953
95 meter
Z = 17460099
08 Z = 5310649
18
XDOT = 21969
955744 XDOT = 6734
906050
YDOT = -12077
289558 feet/sec YDOT = -3606
058995 meter/sec
ZDOT = 1487
310326 ZDOT = 485
957373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7502625
54 X = 2286800
27
Y = 11716694
07 feet Y = 3571248
35 meter
Z = 17414093
42 Z = 5307815
67
XDOT = -21293
261837 XDOT = -6490
186208
YDOT = 11183
197573 feet/sec YDOT = 3408
638620 meter/sec
ZDOT = 1622
772820 ZDOT = 494
621156
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 12307
43208170
00016717 00000-0 10270-3 0 9072
2 25544 51
6471 154
6867 0016414 239
7227 120
2301 15
51368279 39492
Satellite: ISS
Catalog Number: 25544
Epoch time: 12307
43208170 = yrday
fracday
Element set: 907
Inclination: 51
6471 deg
RA of node: 154
6867 deg
Eccentricity:
0016414
Arg of perigee: 239
7227 deg
Mean anomaly: 120
2301 deg
Mean motion: 15
51368279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3949
Checksum: 308
Coasting Arc #9 (Orbit 3963)
---------------------------------------
Vector Time (GMT): 2012/308/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1712046
61 A = 6785334
22 meter
Y = 3852710
53 meter E =
0008109
Z = -5317145
00 I = 51
80490
XDOT = -6731
101723 Wp = 179
95384
YDOT = 3635
731188 meter/sec RA = 148
91817 deg
ZDOT = 459
158455 TA = 94
46446
MA = 94
37181
Ha = 226
234 n
mi
Hp = 219
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5616950
82 X = 1694667
57
Y = 12640126
41 feet Y = 3871758
57 meter
Z = -17444701
45 Z = -5308869
97
XDOT = -22083
667071 XDOT = -6773
487486
YDOT = 11928
251928 feet/sec YDOT = 3560
222809 meter/sec
ZDOT = 1506
425377 ZDOT = 426
355470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5742408
00 X = -1750285
96
Y = -12630500
81 feet Y = -3849776
65 meter
Z = -17410793
80 Z = -5306809
95
XDOT = 21153
852918 XDOT = 6447
694369
YDOT = -11542
147488 feet/sec YDOT = -3518
046554 meter/sec
ZDOT = 1370
210330 ZDOT = 417
640109
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 12308
39832841
00016717 00000-0 10270-3 0 9087
2 25544 51
6473 149
8895 0016385 243
7183 116
2285 15
51408953 39641
Satellite: ISS
Catalog Number: 25544
Epoch time: 12308
39832841 = yrday
fracday
Element set: 908
Inclination: 51
6473 deg
RA of node: 149
8895 deg
Eccentricity:
0016385
Arg of perigee: 243
7183 deg
Mean anomaly: 116
2285 deg
Mean motion: 15
51408953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3964
Checksum: 342
Coasting Arc #10 (Orbit 3979)
---------------------------------------
Vector Time (GMT): 2012/309/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1172701
42 A = 6785715
24 meter
Y = -4205402
67 meter E =
0012326
Z = 5204127
43 I = 51
83248
XDOT = 6658
732802 Wp = 252
31462
YDOT = -3526
971768 meter/sec RA = 143
95981 deg
ZDOT = -1355
916521 TA = 210
66751
MA = 210
73961
Ha = 225
902 n
mi
Hp = 219
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3847445
62 X = -1150869
50
Y = -13797252
86 feet Y = -4218394
51 meter
Z = 17073908
90 Z = 5198483
41
XDOT = 21846
236228 XDOT = 6704
264094
YDOT = -11571
429686 feet/sec YDOT = -3452
255072 meter/sec
ZDOT = -4448
545015 ZDOT = -1323
457546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4208999
30 X = 1282902
99
Y = 13719889
86 feet Y = 4181822
43 meter
Z = 17050933
60 Z = 5197124
56
XDOT = -20652
713620 XDOT = -6294
947111
YDOT = 11671
255210 feet/sec YDOT = 3557
398588 meter/sec
ZDOT = -4313
745939 ZDOT = -1314
829762
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 12309
42896663
00016717 00000-0 10270-3 0 9095
2 25544 51
6476 144
7731 0016469 247
8703 112
0701 15
51455829 39802
Satellite: ISS
Catalog Number: 25544
Epoch time: 12309
42896663 = yrday
fracday
Element set: 909
Inclination: 51
6476 deg
RA of node: 144
7731 deg
Eccentricity:
0016469
Arg of perigee: 247
8703 deg
Mean anomaly: 112
0701 deg
Mean motion: 15
51455829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3980
Checksum: 331
Coasting Arc #11 (Orbit 3994)
---------------------------------------
Vector Time (GMT): 2012/310/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 628325
25 A = 6786708
80 meter
Y = 4601897
63 meter E =
0009418
Z = -4948103
80 I = 51
85980
XDOT = -6525
916740 Wp = 204
23507
YDOT = 3326
304963 meter/sec RA = 139
00234 deg
ZDOT = 2254
998885 TA = 87
78773
MA = 87
67988
Ha = 225
578 n
mi
Hp = 219
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2061434
54 X = 600856
32
Y = 15098089
35 feet Y = 4608770
36 meter
Z = -16233936
35 Z = -4945118
11
XDOT = -21410
487992 XDOT = -6573
581599
YDOT = 10913
074027 feet/sec YDOT = 3253
061581 meter/sec
ZDOT = 7398
290306 ZDOT = 2223
179996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2701071
27 X = -823286
52
Y = -15009763
01 feet Y = -4574975
77 meter
Z = -16222013
81 Z = -4944469
81
XDOT = 19955
633698 XDOT = 6082
477151
YDOT = -11479
192681 feet/sec YDOT = -3498
857929 meter/sec
ZDOT = 7266
144688 ZDOT = 2214
720901
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 12310
39516849
00016717 00000-0 10270-3 0 9100
2 25544 51
6473 139
9753 0016468 251
7060 108
2300 15
51477238 39954
Satellite: ISS
Catalog Number: 25544
Epoch time: 12310
39516849 = yrday
fracday
Element set: 910
Inclination: 51
6473 deg
RA of node: 139
9753 deg
Eccentricity:
0016468
Arg of perigee: 251
7060 deg
Mean anomaly: 108
2300 deg
Mean motion: 15
51477238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3995
Checksum: 318
Coasting Arc #12 (Orbit 4010)
---------------------------------------
Vector Time (GMT): 2012/311/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -164908
52 A = 6787983
52 meter
Y = -5006107
24 meter E =
0008207
Z = 4588104
59 I = 51
88737
XDOT = 6313
102945 Wp = 266
29961
YDOT = -3037
213747 meter/sec RA = 134
04945 deg
ZDOT = -3092
292400 TA = 214
55289
MA = 214
60626
Ha = 225
251 n
mi
Hp = 219
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -541038
44 X = -131205
22
Y = -16424236
36 feet Y = -5007762
85 meter
Z = 15052836
58 Z = 4587385
39
XDOT = 20712
280002 XDOT = 6361
618372
YDOT = -9964
612030 feet/sec YDOT = -2966
345462 meter/sec
ZDOT = -10145
316272 ZDOT = -3061
505300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1503769
83 X = 458349
04
Y = 16366486
59 feet Y = 4988505
11 meter
Z = 15050347
00 Z = 4587345
77
XDOT = -19022
660738 XDOT = -5798
106993
YDOT = 10943
774766 feet/sec YDOT = 3335
662549 meter/sec
ZDOT = -10017
458339 ZDOT = -3053
321302
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 12311
42575788
00016717 00000-0 10270-3 0 9113
2 25544 51
6477 134
8589 0016527 256
0513 103
8800 15
51538896 40110
Satellite: ISS
Catalog Number: 25544
Epoch time: 12311
42575788 = yrday
fracday
Element set: 911
Inclination: 51
6477 deg
RA of node: 134
8589 deg
Eccentricity:
0016527
Arg of perigee: 256
0513 deg
Mean anomaly: 103
8800 deg
Mean motion: 15
51538896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4011
Checksum: 317
Coasting Arc #13 (Orbit 4025)
---------------------------------------
Vector Time (GMT): 2012/312/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -276234
31 A = 6789791
04 meter
Y = 5414484
20 meter E =
0010759
Z = -4083345
58 I = 51
91297
XDOT = -6061
062479 Wp = 240
51282
YDOT = 2630
446515 meter/sec RA = 129
09799 deg
ZDOT = 3885
131061 TA = 69
63569
MA = 69
52014
Ha = 225
044 n
mi
Hp = 219
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -906280
55 X = -316923
41
Y = 17764055
79 feet Y = 5411167
56 meter
Z = -13396803
10 Z = -4084786
52
XDOT = -19885
375588 XDOT = -6108
899576
YDOT = 8630
073869 feet/sec YDOT = 2562
400560 meter/sec
ZDOT = 12746
492983 ZDOT = 3855
569990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -425324
54 X = -129638
92
Y = -17777169
84 feet Y = -5418481
37 meter
Z = -13403308
82 Z = -4085328
53
XDOT = 18011
436993 XDOT = 5489
885996
YDOT = -9980
509244 feet/sec YDOT = -3042
059218 meter/sec
ZDOT = 12623
742240 ZDOT = 3847
716635
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 12312
39191405
00016717 00000-0 10270-3 0 9121
2 25544 51
6467 130
0605 0016549 259
5882 100
3404 15
51545652 40263
Satellite: ISS
Catalog Number: 25544
Epoch time: 12312
39191405 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 130
0605 deg
Eccentricity:
0016549
Arg of perigee: 259
5882 deg
Mean anomaly: 100
3404 deg
Mean motion: 15
51545652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4026
Checksum: 288
Coasting Arc #14 (Orbit 4041)
---------------------------------------
Vector Time (GMT): 2012/313/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626306
69 A = 6791482
07 meter
Y = -5792961
17 meter E =
0004496
Z = 3491309
34 I = 51
93795
XDOT = 5767
215860 Wp = 251
47099
YDOT = -2127
071737 meter/sec RA = 124
15192 deg
ZDOT = -4570
132487 TA = 247
77533
MA = 247
82302
Ha = 224
788 n
mi
Hp = 218
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2054811
98 X = 674077
97
Y = -19005778
11 feet Y = -5785690
17 meter
Z = 11454426
97 Z = 3494468
23
XDOT = 18921
311875 XDOT = 5812
773626
YDOT = -6978
581814 feet/sec YDOT = -2062
324580 meter/sec
ZDOT = -14993
872988 ZDOT = -4542
004403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -316422
71 X = -96445
64
Y = 19105716
78 feet Y = 5823422
47 meter
Z = 11468095
49 Z = 3495475
51
XDOT = -16937
143157 XDOT = -5162
441234
YDOT = 8637
184300 feet/sec YDOT = 2632
613774 meter/sec
ZDOT = -14877
099781 ZDOT = -4534
540013
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 12313
42245400
00016717 00000-0 10270-3 0 9132
2 25544 51
6470 124
9437 0016577 264
0913 95
8349 15
51615119 40429
Satellite: ISS
Catalog Number: 25544
Epoch time: 12313
42245400 = yrday
fracday
Element set: 913
Inclination: 51
6470 deg
RA of node: 124
9437 deg
Eccentricity:
0016577
Arg of perigee: 264
0913 deg
Mean anomaly: 95
8349 deg
Mean motion: 15
51615119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4042
Checksum: 295
Coasting Arc #15 (Orbit 4056)
---------------------------------------
Vector Time (GMT): 2012/314/09:11:25
985
Vector Time (MET): N/A
Weight (LBS) : 908123
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -942458
38 A = 6793403
70 meter
Y = 6125532
51 meter E =
0012631
Z = -2768823
86 I = 51
95901
XDOT = -5465
756470 Wp = 277
89837
YDOT = 1500
496838 meter/sec RA = 119
20717 deg
ZDOT = 5161
620254 TA = 50
90860
MA = 50
79633
Ha = 224
735 n
mi
Hp = 218
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3092055
04 X = -997434
73
Y = 20096891
42 feet Y = 6114685
82 meter
Z = -9084067
77 Z = -2773536
20
XDOT = -17932
271883 XDOT = -5507
203590
YDOT = 4922
889890 feet/sec YDOT = 1439
143839 meter/sec
ZDOT = 16934
449653 ZDOT = 5134
966585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 919697
62 X = 280323
83
Y = -20303535
33 feet Y = -6188517
57 meter
Z = -9104215
84 Z = -2774964
99
XDOT = 15941
936783 XDOT = 4859
102332
YDOT = -6848
796726 feet/sec YDOT = -2087
513242 meter/sec
ZDOT = 16823
841102 ZDOT = 5127
906768
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 12314
38856332
00016717 00000-0 10270-3 0 9141
2 25544 51
6454 120
1445 0016612 267
3889 92
5361 15
51610665 40571
Satellite: ISS
Catalog Number: 25544
Epoch time: 12314
38856332 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 120
1445 deg
Eccentricity:
0016612
Arg of perigee: 267
3889 deg
Mean anomaly: 92
5361 deg
Mean motion: 15
51610665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4057
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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