[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 21st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16953 16 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 3704)
---------------------------------------
Vector Time (GMT): 2012/291/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2210752
97 A = 6796959
48 meter
Y = -5962297
90 meter E =
0018370
Z = 2410643
60 I = 51
38207
XDOT = 5496
773970 Wp = 133
84521
YDOT = 129
991068 meter/sec RA = 232
02868 deg
ZDOT = 5324
512139 TA = 253
13529
MA = 253
33682
Ha = 230
962 n
mi
Hp = 217
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7253126
55 X = -2155627
67
Y = -19561344
81 feet Y = -5986711
59 meter
Z = 7908935
70 Z = 2400037
74
XDOT = 18034
035335 XDOT = 5469
045887
YDOT = 426
479883 feet/sec YDOT = 191
304613 meter/sec
ZDOT = 17468
871848 ZDOT = 5351
148560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20513078
70 X = 6252386
39
Y = -3892400
45 feet Y = -1186403
66 meter
Z = 7865630
33 Z = 2397444
12
XDOT = -3733
414399 XDOT = -1137
944709
YDOT = 16101
008136 feet/sec YDOT = 4907
587280 meter/sec
ZDOT = 17579
000374 ZDOT = 5358
079314
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 12291
71115127
00016717 00000-0 10270-3 0 9007
2 25544 51
6496 232
6859 0016500 179
8777 180
2381 15
50677151 37052
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
71115127 = yrday
fracday
Element set: 900
Inclination: 51
6496 deg
RA of node: 232
6859 deg
Eccentricity:
0016500
Arg of perigee: 179
8777 deg
Mean anomaly: 180
2381 deg
Mean motion: 15
50677151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 313
Coasting Arc #2 (Orbit 3719)
---------------------------------------
Vector Time (GMT): 2012/292/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2137509
91 A = 6795719
09 meter
Y = 5734063
12 meter E =
0018732
Z = -2933534
59 I = 51
39764
XDOT = -5805
088100 Wp = 171
14516
YDOT = -381
160696 meter/sec RA = 227
05411 deg
ZDOT = -4997
291136 TA = 42
43720
MA = 42
29251
Ha = 230
801 n
mi
Hp = 217
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7012827
78 X = 2087482
32
Y = 18812543
05 feet Y = 5757686
31 meter
Z = -9624457
30 Z = -2923272
08
XDOT = -19045
564631 XDOT = -5776
118165
YDOT = -1250
527218 feet/sec YDOT = -445
914950 meter/sec
ZDOT = -16395
312125 ZDOT = -5025
422252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19667955
32 X = -5994792
78
Y = 4131351
32 feet Y = 1259235
88 meter
Z = -9582545
48 Z = -2920759
86
XDOT = 4416
738748 XDOT = 1346
221970
YDOT = -17100
438341 feet/sec YDOT = -5212
213606 meter/sec
ZDOT = -16511
610503 ZDOT = -5032
738881
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 12292
67781165
00016717 00000-0 10270-3 0 9015
2 25544 51
6497 227
8924 0016645 184
2123 175
8891 15
50694230 37207
Satellite: ISS
Catalog Number: 25544
Epoch time: 12292
67781165 = yrday
fracday
Element set: 901
Inclination: 51
6497 deg
RA of node: 227
8924 deg
Eccentricity:
0016645
Arg of perigee: 184
2123 deg
Mean anomaly: 175
8891 deg
Mean motion: 15
50694230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3720
Checksum: 326
Coasting Arc #3 (Orbit 3735)
---------------------------------------
Vector Time (GMT): 2012/293/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2076196
90 A = 6794397
10 meter
Y = -5516395
80 meter E =
0019194
Z = 3387761
81 I = 51
41458
XDOT = 6091
297436 Wp = 147
55222
YDOT = 551
577853 meter/sec RA = 222
07912 deg
ZDOT = 4603
148236 TA = 252
05320
MA = 252
26254
Ha = 230
548 n
mi
Hp = 217
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6811669
62 X = -2030814
38
Y = -18098411
43 feet Y = -5539359
33 meter
Z = 11114704
11 Z = 3377785
88
XDOT = 19984
571642 XDOT = 6062
315392
YDOT = 1809
638624 feet/sec YDOT = 619
532567 meter/sec
ZDOT = 15102
192374 ZDOT = 4632
669614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18860373
19 X = 5748641
75
Y = -4375149
74 feet Y = -1333545
64 meter
Z = 11073950
26 Z = 3375340
04
XDOT = -4796
755092 XDOT = -1462
050952
YDOT = 18090
206416 feet/sec YDOT = 5513
894916 meter/sec
ZDOT = 15224
239310 ZDOT = 4640
348142
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 12293
70889392
00016717 00000-0 10270-3 0 9022
2 25544 51
6492 222
7787 0016439 187
5461 172
5445 15
50741269 37366
Satellite: ISS
Catalog Number: 25544
Epoch time: 12293
70889392 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 222
7787 deg
Eccentricity:
0016439
Arg of perigee: 187
5461 deg
Mean anomaly: 172
5445 deg
Mean motion: 15
50741269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3736
Checksum: 342
Coasting Arc #4 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2012/294/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1878628
57 A = 6792868
79 meter
Y = 5266871
36 meter E =
0014909
Z = -3846707
48 I = 51
43242
XDOT = -6415
875219 Wp = 170
29721
YDOT = -719
176684 meter/sec RA = 217
10422 deg
ZDOT = -4134
767830 TA = 56
16092
MA = 56
01911
Ha = 230
338 n
mi
Hp = 217
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6163479
58 X = 1838280
39
Y = 17279761
67 feet Y = 5287653
68 meter
Z = -12620431
38 Z = -3837679
17
XDOT = -21049
459379 XDOT = -6387
270337
YDOT = -2359
503557 feet/sec YDOT = -790
763148 meter/sec
ZDOT = -13565
511253 ZDOT = -4165
866802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17893980
94 X = -5454085
39
Y = 4160919
71 feet Y = 1268248
33 meter
Z = -12583565
69 Z = -3835470
82
XDOT = 5118
173602 XDOT = 1560
019314
YDOT = -19236
822425 feet/sec YDOT = -5863
383475 meter/sec
ZDOT = -13694
084050 ZDOT = -4173
956818
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 12294
67551017
00016717 00000-0 10270-3 0 9030
2 25544 51
6486 217
9845 0016575 191
9372 168
1389 15
50774940 37518
Satellite: ISS
Catalog Number: 25544
Epoch time: 12294
67551017 = yrday
fracday
Element set: 903
Inclination: 51
6486 deg
RA of node: 217
9845 deg
Eccentricity:
0016575
Arg of perigee: 191
9372 deg
Mean anomaly: 168
1389 deg
Mean motion: 15
50774940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3751
Checksum: 342
Coasting Arc #5 (Orbit 3766)
---------------------------------------
Vector Time (GMT): 2012/295/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1692725
93 A = 6791515
10 meter
Y = -5042915
14 meter E =
0019359
Z = 4229931
49 I = 51
45264
XDOT = 6699
248623 Wp = 163
81343
YDOT = 803
930914 meter/sec RA = 212
12925 deg
ZDOT = 3617
103835 TA = 248
91801
MA = 249
12511
Ha = 230
117 n
mi
Hp = 218
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5553562
77 X = -1656757
47
Y = -16544997
17 feet Y = -5061643
01 meter
Z = 13877728
00 Z = 4221795
75
XDOT = 21979
162149 XDOT = 6672
189724
YDOT = 2637
568616 feet/sec YDOT = 878
694916 meter/sec
ZDOT = 11867
138565 ZDOT = 3649
583086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17027980
86 X = 5190128
57
Y = -3943007
60 feet Y = -1201828
72 meter
Z = 13844525
42 Z = 4219811
35
XDOT = -5119
478991 XDOT = -1560
417196
YDOT = 20287
054195 feet/sec YDOT = 6183
494119 meter/sec
ZDOT = 12001
429694 ZDOT = 3658
035771
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 12295
70654653
00016717 00000-0 10270-3 0 9046
2 25544 51
6483 212
8703 0016412 195
2313 164
8346 15
50802454 37679
Satellite: ISS
Catalog Number: 25544
Epoch time: 12295
70654653 = yrday
fracday
Element set: 904
Inclination: 51
6483 deg
RA of node: 212
8703 deg
Eccentricity:
0016412
Arg of perigee: 195
2313 deg
Mean anomaly: 164
8346 deg
Mean motion: 15
50802454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3767
Checksum: 309
Coasting Arc #6 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2012/296/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1367545
47 A = 6789977
18 meter
Y = 4809477
53 meter E =
0012767
Z = -4590926
32 I = 51
47335
XDOT = -6988
480212 Wp = 162
48277
YDOT = -882
143049 meter/sec RA = 207
15384 deg
ZDOT = -3019
978113 TA = 77
34416
MA = 77
20145
Ha = 229
850 n
mi
Hp = 218
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4486697
73 X = 1335965
15
Y = 15779125
76 feet Y = 4824593
48 meter
Z = -15062094
24 Z = -4584359
73
XDOT = -22928
084685 XDOT = -6963
425987
YDOT = -2894
170109 feet/sec YDOT = -960
152660 meter/sec
ZDOT = -9908
064676 ZDOT = -3053
867258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16105767
24 X = -4909037
86
Y = 3243505
19 feet Y = 988620
38 meter
Z = -15035354
50 Z = -4582776
05
XDOT = 5033
357845 XDOT = 1534
167471
YDOT = -21370
329095 feet/sec YDOT = -6513
676308 meter/sec
ZDOT = -10048
197244 ZDOT = -3062
690520
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 12296
67311890
00016717 00000-0 10270-3 0 9057
2 25544 51
6473 208
0752 0016539 199
4801 160
5720 15
50855654 37823
Satellite: ISS
Catalog Number: 25544
Epoch time: 12296
67311890 = yrday
fracday
Element set: 905
Inclination: 51
6473 deg
RA of node: 208
0752 deg
Eccentricity:
0016539
Arg of perigee: 199
4801 deg
Mean anomaly: 160
5720 deg
Mean motion: 15
50855654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3782
Checksum: 324
Coasting Arc #7 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2012/297/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1060623
67 A = 6788863
99 meter
Y = -4616630
20 meter E =
0018712
Z = 4870610
24 I = 51
49735
XDOT = 7218
439077 Wp = 181
24849
YDOT = 886
301596 meter/sec RA = 202
17958 deg
ZDOT = 2393
829267 TA = 245
10620
MA = 245
30081
Ha = 229
671 n
mi
Hp = 218
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3479736
45 X = -1032581
28
Y = -15146424
55 feet Y = -4628333
65 meter
Z = 15979692
40 Z = 4865526
15
XDOT = 23682
542905 XDOT = 7196
362973
YDOT = 2907
813635 feet/sec YDOT = 966
899412 meter/sec
ZDOT = 7853
770562 ZDOT = 2428
842787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15349675
43 X = 4678581
07
Y = -2563022
01 feet Y = -781209
11 meter
Z = 15959063
07 Z = 4864322
42
XDOT = -4659
686863 XDOT = -1420
272556
YDOT = 22269
078278 feet/sec YDOT = 6787
615059 meter/sec
ZDOT = 7998
569110 ZDOT = 2437
963865
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 12297
70410945
00016717 00000-0 10270-3 0 9064
2 25544 51
6475 202
9608 0016448 202
8714 157
1706 15
50863675 37984
Satellite: ISS
Catalog Number: 25544
Epoch time: 12297
70410945 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 202
9608 deg
Eccentricity:
0016448
Arg of perigee: 202
8714 deg
Mean anomaly: 157
1706 deg
Mean motion: 15
50863675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3798
Checksum: 332
Coasting Arc #8 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2012/298/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 622850
30 A = 6787658
08 meter
Y = 4436841
75 meter E =
0013009
Z = -5100588
63 I = 51
52135
XDOT = -7419
394809 Wp = 155
35622
YDOT = -889
056956 meter/sec RA = 197
20443 deg
ZDOT = -1692
499458 TA = 98
32713
MA = 98
17961
Ha = 229
354 n
mi
Hp = 218
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2043472
11 X = 597968
13
Y = 14556567
41 feet Y = 4443667
32 meter
Z = -16734214
68 Z = -5097623
61
XDOT = -24341
846485 XDOT = -7400
679875
YDOT = -2916
853530 feet/sec YDOT = -971
920755 meter/sec
ZDOT = -5552
819744 ZDOT = -1728
497452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14643557
52 X = -4463356
33
Y = 1425885
57 feet Y = 434609
92 meter
Z = -16722333
79 Z = -5096967
34
XDOT = 4215
864276 XDOT = 1284
995431
YDOT = -23066
181703 feet/sec YDOT = -7030
572183 meter/sec
ZDOT = -5701
704442 ZDOT = -1737
879514
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 12298
67063871
00016717 00000-0 10270-3 0 9074
2 25544 51
6462 198
1650 0016552 206
8162 153
2135 15
50932046 38130
Satellite: ISS
Catalog Number: 25544
Epoch time: 12298
67063871 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 198
1650 deg
Eccentricity:
0016552
Arg of perigee: 206
8162 deg
Mean anomaly: 153
2135 deg
Mean motion: 15
50932046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 308
Coasting Arc #9 (Orbit 3828)
---------------------------------------
Vector Time (GMT): 2012/299/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -216672
94 A = 6787044
46 meter
Y = -4309258
81 meter E =
0017083
Z = 5245981
34 I = 51
54900
XDOT = 7547
723349 Wp = 198
18169
YDOT = 836
744912 meter/sec RA = 192
23200 deg
ZDOT = 984
070736 TA = 242
28678
MA = 242
46018
Ha = 229
197 n
mi
Hp = 218
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -710869
22 X = -193954
00
Y = -14137988
21 feet Y = -4311554
30 meter
Z = 17211224
85 Z = 5244984
28
XDOT = 24762
871880 XDOT = 7533
025254
YDOT = 2745
226090 feet/sec YDOT = 921
066173 meter/sec
ZDOT = 3228
578530 ZDOT = 1020
702031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14155777
84 X = 4314681
09
Y = -362035
54 feet Y = -110348
43 meter
Z = 17207474
84 Z = 5244838
33
XDOT = -3564
824894 XDOT = -1086
558628
YDOT = 23609
462711 feet/sec YDOT = 7196
164234 meter/sec
ZDOT = 3380
100097 ZDOT = 1030
254510
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 12299
70158349
00016717 00000-0 10270-3 0 9085
2 25544 51
6467 193
0507 0016534 210
3909 149
6285 15
50928758 38296
Satellite: ISS
Catalog Number: 25544
Epoch time: 12299
70158349 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 193
0507 deg
Eccentricity:
0016534
Arg of perigee: 210
3909 deg
Mean anomaly: 149
6285 deg
Mean motion: 15
50928758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3829
Checksum: 345
Coasting Arc #10 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2012/300/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -300297
75 A = 6786484
18 meter
Y = 4212994
07 meter E =
0014372
Z = -5316269
46 I = 51
57651
XDOT = -7615
328296 Wp = 157
68575
YDOT = -797
803293 meter/sec RA = 187
25852 deg
ZDOT = -215
263955 TA = 110
33584
MA = 110
18135
Ha = 228
849 n
mi
Hp = 218
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -985228
85 X = -321560
27
Y = 13822159
03 feet Y = 4209516
61 meter
Z = -17441828
95 Z = -5317780
33
XDOT = -24984
672888 XDOT = -7604
795374
YDOT = -2617
464871 feet/sec YDOT = -882
903777 meter/sec
ZDOT = -706
246570 ZDOT = -252
233938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13806378
63 X = -4208184
21
Y = -1084274
57 feet Y = -330486
89 meter
Z = -17448450
10 Z = -5318287
59
XDOT = 2910
588929 XDOT = 887
147506
YDOT = -23931
297248 feet/sec YDOT = -7294
259401 meter/sec
ZDOT = -859
184190 ZDOT = -261
879341
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
66807041
00016717 00000-0 10270-3 0 9094
2 25544 51
6454 188
2543 0016590 213
9642 146
0449 15
51003461 38449
Satellite: ISS
Catalog Number: 25544
Epoch time: 12300
66807041 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 188
2543 deg
Eccentricity:
0016590
Arg of perigee: 213
9642 deg
Mean anomaly: 146
0449 deg
Mean motion: 15
51003461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 297
Coasting Arc #11 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2012/301/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 767131
31 A = 6786553
66 meter
Y = -4173753
46 meter E =
0014364
Z = 5301786
62 I = 51
60717
XDOT = 7604
873687 Wp = 212
26160
YDOT = 730
510231 meter/sec RA = 182
28915 deg
ZDOT = -537
830438 TA = 242
80561
MA = 242
95209
Ha = 228
679 n
mi
Hp = 218
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2516835
02 X = 787990
60
Y = -13693416
88 feet Y = -4165057
87 meter
Z = 17394313
07 Z = 5305564
40
XDOT = 24950
372988 XDOT = 7598
752470
YDOT = 2396
687108 feet/sec YDOT = 815
518412 meter/sec
ZDOT = -1764
535557 ZDOT = -500
900385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13697756
53 X = 4175076
19
Y = 2378784
82 feet Y = 725053
61 meter
Z = 17410315
91 Z = 5306664
29
XDOT = -2165
885015 XDOT = -660
161753
YDOT = 23967
291475 feet/sec YDOT = 7305
230442 meter/sec
ZDOT = -1611
746212 ZDOT = -491
260246
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
69896938
00016717 00000-0 10270-3 0 9103
2 25544 51
6455 183
1400 0016623 217
7535 142
2451 15
50999553 38600
Satellite: ISS
Catalog Number: 25544
Epoch time: 12301
69896938 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 183
1400 deg
Eccentricity:
0016623
Arg of perigee: 217
7535 deg
Mean anomaly: 142
2451 deg
Mean motion: 15
50999553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3860
Checksum: 317
Coasting Arc #12 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2012/302/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1315031
13 A = 6786819
62 meter
Y = 4175327
00 meter E =
0015209
Z = -5191686
67 I = 51
63818
XDOT = -7510
889245 Wp = 169
49489
YDOT = -699
152669 meter/sec RA = 177
31915 deg
ZDOT = 1326
194897 TA = 113
34292
MA = 113
18283
Ha = 228
323 n
mi
Hp = 219
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4314406
60 X = -1336402
08
Y = 13698579
41 feet Y = 4160501
67 meter
Z = -17033092
75 Z = -5198127
38
XDOT = -24642
025082 XDOT = -7508
955462
YDOT = -2293
807970 feet/sec YDOT = -783
133225 meter/sec
ZDOT = 4351
033127 ZDOT = 1289
711142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13776912
43 X = -4199202
91
Y = -3942120
35 feet Y = -1201558
28 meter
Z = -17060123
15 Z = -5199925
54
XDOT = 1524
757863 XDOT = 464
746197
YDOT = -23703
622407 feet/sec YDOT = -7224
864110 meter/sec
ZDOT = 4200
076499 ZDOT = 1280
183317
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
66541439
00016717 00000-0 10270-3 0 9115
2 25544 51
6445 178
3431 0016619 221
0268 138
9634 15
51070827 38751
Satellite: ISS
Catalog Number: 25544
Epoch time: 12302
66541439 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 178
3431 deg
Eccentricity:
0016619
Arg of perigee: 221
0268 deg
Mean anomaly: 138
9634 deg
Mean motion: 15
51070827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 310
Coasting Arc #13 (Orbit 3890)
---------------------------------------
Vector Time (GMT): 2012/303/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1791912
19 A = 6787614
68 meter
Y = -4229345
82 meter E =
0010891
Z = 5000558
74 I = 51
67089
XDOT = 7343
476209 Wp = 218
91231
YDOT = 669
869986 meter/sec RA = 172
35413 deg
ZDOT = -2075
649963 TA = 251
23488
MA = 251
35308
Ha = 228
107 n
mi
Hp = 219
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5878977
01 X = 1814780
19
Y = -13875806
50 feet Y = -4209179
43 meter
Z = 16406032
62 Z = 5009319
77
XDOT = 24092
769716 XDOT = 7345
523109
YDOT = 2197
736175 feet/sec YDOT = 752
000665 meter/sec
ZDOT = -6809
875206 ZDOT = -2039
969770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14077370
05 X = 4290782
39
Y = 5265378
19 feet Y = 1604887
27 meter
Z = 16442680
08 Z = 5011728
89
XDOT = -926
407638 XDOT = -282
369048
YDOT = 23171
884209 feet/sec YDOT = 7062
790307 meter/sec
ZDOT = -6662
229472 ZDOT = -2030
647543
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
69626766
00016717 00000-0 10270-3 0 9127
2 25544 51
6442 173
2284 0016664 224
9901 134
9901 15
51073322 38918
Satellite: ISS
Catalog Number: 25544
Epoch time: 12303
69626766 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 173
2284 deg
Eccentricity:
0016664
Arg of perigee: 224
9901 deg
Mean anomaly: 134
9901 deg
Mean motion: 15
51073322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3891
Checksum: 309
Coasting Arc #14 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2012/304/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2314619
56 A = 6788657
74 meter
Y = 4321468
79 meter E =
0014805
Z = -4700886
69 I = 51
70480
XDOT = -7083
463599 Wp = 188
79185
YDOT = -702
399649 meter/sec RA = 167
38967 deg
ZDOT = 2826
577928 TA = 109
33823
MA = 109
17809
Ha = 227
761 n
mi
Hp = 219
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7593896
19 X = -2339934
61
Y = 14178047
20 feet Y = 4295443
57 meter
Z = -15422856
59 Z = -4712192
95
XDOT = -23239
709972 XDOT = -7088
814014
YDOT = -2304
460790 feet/sec YDOT = -781
641186 meter/sec
ZDOT = 9273
549631 ZDOT = 2792
152850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14560431
60 X = -4438019
55
Y = -6724574
33 feet Y = -2049650
26 meter
Z = -15470058
79 Z = -4715273
92
XDOT = 555
107966 XDOT = 169
196908
YDOT = -22324
633980 feet/sec YDOT = -6804
548437 meter/sec
ZDOT = 9131
089018 ZDOT = 2783
155933
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
66267077
00016717 00000-0 10270-3 0 9132
2 25544 51
6440 168
4314 0016614 228
1471 131
8263 15
51137007 39064
Satellite: ISS
Catalog Number: 25544
Epoch time: 12304
66267077 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 168
4314 deg
Eccentricity:
0016614
Arg of perigee: 228
1471 deg
Mean anomaly: 131
8263 deg
Mean motion: 15
51137007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 290
Coasting Arc #15 (Orbit 3921)
---------------------------------------
Vector Time (GMT): 2012/305/15:38:09
547
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2746994
17 A = 6790031
78 meter
Y = -4450918
44 meter E =
0008240
Z = 4328893
49 I = 51
73825
XDOT = 6765
359588 Wp = 209
28292
YDOT = 765
976525 meter/sec RA = 162
43034 deg
ZDOT = -3515
378683 TA = 276
42259
MA = 276
51642
Ha = 227
493 n
mi
Hp = 219
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9012448
08 X = 2775531
75
Y = -14602750
79 feet Y = -4420040
20 meter
Z = 14202406
46 Z = 4342308
01
XDOT = 22196
061642 XDOT = 6773
368832
YDOT = 2513
046343 feet/sec YDOT = 841
675726 meter/sec
ZDOT = -11533
394630 ZDOT = -3482
492544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15198961
79 X = 4632643
55
Y = 7865342
43 feet Y = 2397356
37 meter
Z = 14258360
67 Z = 4345948
33
XDOT = -350
551186 XDOT = -106
848001
YDOT = 21280
229394 feet/sec YDOT = 6486
213919 meter/sec
ZDOT = -11397
297043 ZDOT = -3473
896139
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
69347871
00016717 00000-0 10270-3 0 9148
2 25544 51
6433 163
3161 0016647 232
1697 127
7948 15
51144891 39222
Satellite: ISS
Catalog Number: 25544
Epoch time: 12305
69347871 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 163
3161 deg
Eccentricity:
0016647
Arg of perigee: 232
1697 deg
Mean anomaly: 127
7948 deg
Mean motion: 15
51144891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3922
Checksum: 324
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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