[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 17th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
199/04:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 210
3
200/03:25:42
685 4
3 7
9 8
0
N/A 1
4 -1
3 220
0
000/00:19:25
371 6
6 -0
1 214
3
Coasting Arc #1 (Orbit 2252)
---------------------------------------
Vector Time (GMT): 2012/198/04:24:36
440
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5074690
20 A = 6781633
62 meter
Y = 3967928
45 meter E =
0019158
Z = 2083897
62 I = 51
52008
XDOT = -4507
698123 Wp = 125
83049
YDOT = -2850
460749 meter/sec RA = 336
87808 deg
ZDOT = -5524
985568 TA = 31
01704
MA = 30
90405
Ha = 219
598 n
mi
Hp = 210
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16649246
06 X = -5128806
22
Y = 13018137
95 feet Y = 3910877
24 meter
Z = 6836934
46 Z = 2059114
38
XDOT = -14789
035838 XDOT = -4448
649822
YDOT = -9351
905343 feet/sec YDOT = -2900
537694 meter/sec
ZDOT = -18126
593072 ZDOT = -5546
740505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16744095
74 X = -5103600
38
Y = 12949816
58 feet Y = 3947104
09 meter
Z = 6734277
33 Z = 2052607
73
XDOT = -13695
148802 XDOT = -4174
281355
YDOT = -8192
391900 feet/sec YDOT = -2497
041051 meter/sec
ZDOT = -18215
961448 ZDOT = -5552
225049
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 12198
21996339
00016717 00000-0 10270-3 0 9000
2 25544 51
6408 337
2603 0006788 159
1740 200
9691 15
56163441 22531
Satellite: ISS
Catalog Number: 25544
Epoch time: 12198
21996339 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 337
2603 deg
Eccentricity:
0006788
Arg of perigee: 159
1740 deg
Mean anomaly: 200
9691 deg
Mean motion: 15
56163441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2253
Checksum: 315
Coasting Arc #2 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2012/199/04:24:36
440
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6068550
29 A = 6783193
19 meter
Y = -3015958
94 meter E =
0011488
Z = 250666
20 I = 51
49890
XDOT = 1919
676855 Wp = 78
77400
YDOT = 4380
052155 meter/sec RA = 331
88735 deg
ZDOT = 5993
799041 TA = 283
93325
MA = 284
06099
Ha = 219
297 n
mi
Hp = 210
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19909941
91 X = 6100606
67
Y = -9894878
40 feet Y = -2947917
44 meter
Z = 822395
68 Z = 280223
98
XDOT = 6298
152413 XDOT = 1841
439432
YDOT = 14370
249853 feet/sec YDOT = 4401
080897 meter/sec
ZDOT = 19664
695015 ZDOT = 6002
935182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19773333
19 X = 6026911
96
Y = -10154492
29 feet Y = -3095089
25 meter
Z = 944627
35 Z = 287922
42
XDOT = 5625
029616 XDOT = 1714
509027
YDOT = 12847
551449 feet/sec YDOT = 3915
933682 meter/sec
ZDOT = 19701
855220 ZDOT = 6005
125471
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 12199
24741878
00016717 00000-0 10270-3 0 9011
2 25544 51
6413 332
1214 0006528 163
7821 196
3543 15
56228805 22699
Satellite: ISS
Catalog Number: 25544
Epoch time: 12199
24741878 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 332
1214 deg
Eccentricity:
0006528
Arg of perigee: 163
7821 deg
Mean anomaly: 196
3543 deg
Mean motion: 15
56228805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 314
Coasting Arc #3 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2012/199/04:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 923981
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -533357
53 A = 6773071
63 meter
Y = 4679513
14 meter E =
0008176
Z = 4859780
72 I = 51
46490
XDOT = -7107
034614 Wp = 108
49393
YDOT = 1663
526839 meter/sec RA = 331
76741 deg
ZDOT = -2381
071237 TA = 4
86770
MA = 4
85975
Ha = 219
178 n
mi
Hp = 210
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1749860
66 X = -609252
54
Y = 15352733
41 feet Y = 4673123
79 meter
Z = 15944162
46 Z = 4857006
03
XDOT = -23317
042697 XDOT = -7113
541762
YDOT = 5457
765219 feet/sec YDOT = 1584
015514 meter/sec
ZDOT = -7811
913508 ZDOT = -2415
611981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 271857
55 X = 82862
18
Y = 15462104
09 feet Y = 4712849
33 meter
Z = 15932174
46 Z = 4856126
77
XDOT = -21175
348940 XDOT = -6454
246357
YDOT = 8571
179762 feet/sec YDOT = 2612
495591 meter/sec
ZDOT = -7954
533978 ZDOT = -2424
541957
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 12199
24741754
00016717 00000-0 10270-3 0 9025
2 25544 51
6415 332
1216 0006430 164
4338 195
7015 15
56265202 22695
Satellite: ISS
Catalog Number: 25544
Epoch time: 12199
24741754 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 332
1216 deg
Eccentricity:
0006430
Arg of perigee: 164
4338 deg
Mean anomaly: 195
7015 deg
Mean motion: 15
56265202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 294
Coasting Arc #4 (Orbit 2283)
---------------------------------------
Vector Time (GMT): 2012/200/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6116726
72 A = 6787013
23 meter
Y = -2458161
30 meter E =
0013234
Z = 1586878
70 I = 51
47250
XDOT = 547
317618 Wp = 60
91444
YDOT = 5076
686012 meter/sec RA = 327
05594 deg
ZDOT = 5724
557329 TA = 316
49274
MA = 316
59707
Ha = 220
010 n
mi
Hp = 214
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20068001
04 X = 6136051
21
Y = -8064833
68 feet Y = -2389652
43 meter
Z = 5206294
93 Z = 1616639
59
XDOT = 1795
661476 XDOT = 462
700272
YDOT = 16655
794004 feet/sec YDOT = 5082
332601 meter/sec
ZDOT = 18781
356066 ZDOT = 5727
011249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21176968
37 X = 6454739
96
Y = -4243384
08 feet Y = -1293383
47 meter
Z = 5329297
99 Z = 1624370
03
XDOT = -1719
604840 XDOT = -524
135555
YDOT = 15137
873266 feet/sec YDOT = 4614
023771 meter/sec
ZDOT = 18790
886701 ZDOT = 5727
462266
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 12200
21071102
00016717 00000-0 10270-3 0 9039
2 25544 51
6441 327
3030 0000852 277
9122 82
1934 15
54541540 22843
Satellite: ISS
Catalog Number: 25544
Epoch time: 12200
21071102 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 327
3030 deg
Eccentricity:
0000852
Arg of perigee: 277
9122 deg
Mean anomaly: 82
1934 deg
Mean motion: 15
54541540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2284
Checksum: 256
Coasting Arc #5 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2012/201/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5823350
00 A = 6783485
42 meter
Y = 1257328
97 meter E =
0003607
Z = -3246723
26 I = 51
43650
XDOT = 1374
344808 Wp = 95
25461
YDOT = -5863
163275 meter/sec RA = 322
06391 deg
ZDOT = -4740
484457 TA = 122
47922
MA = 122
44435
Ha = 219
902 n
mi
Hp = 214
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19105479
01 X = -5821205
37
Y = 4125095
05 feet Y = 1192221
01 meter
Z = -10651979
21 Z = -3275006
93
XDOT = 4509
005276 XDOT = 1462
833506
YDOT = -19236
099983 feet/sec YDOT = -5847
299201 meter/sec
ZDOT = -15552
770528 ZDOT = -4733
593805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19461374
50 X = -5931826
95
Y = 888423
24 feet Y = 270791
40 meter
Z = -10768751
32 Z = -3282315
40
XDOT = 7815
119782 XDOT = 2382
048510
YDOT = -16779
613090 feet/sec YDOT = -5114
426070 meter/sec
ZDOT = -15523
685905 ZDOT = -4731
619464
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 12201
17496834
00016717 00000-0 10270-3 0 9049
2 25544 51
6446 322
4930 0001043 278
0523 82
0512 15
54566855 22996
Satellite: ISS
Catalog Number: 25544
Epoch time: 12201
17496834 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 322
4930 deg
Eccentricity:
0001043
Arg of perigee: 278
0523 deg
Mean anomaly: 82
0512 deg
Mean motion: 15
54566855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 299
Coasting Arc #6 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2012/202/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5075632
91 A = 6779298
38 meter
Y = 168716
87 meter E =
0007938
Z = 4486162
78 I = 51
39941
XDOT = -3028
514943 Wp = 112
09417
YDOT = 6288
985660 meter/sec RA = 317
05783 deg
ZDOT = 3182
480333 TA = 305
80782
MA = 305
88156
Ha = 219
824 n
mi
Hp = 214
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16652338
94 X = 5051576
74
Y = 553533
03 feet Y = 225340
83 meter
Z = 14718381
82 Z = 4510761
05
XDOT = -9936
072649 XDOT = -3114
074035
YDOT = 20633
155053 feet/sec YDOT = 6254
640250 meter/sec
ZDOT = 10441
208440 ZDOT = 3167
561003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16291768
33 X = 4965730
99
Y = 3031423
53 feet Y = 923977
89 meter
Z = 14819794
56 Z = 4517073
38
XDOT = -12759
258055 XDOT = -3889
021855
YDOT = 17713
301183 feet/sec YDOT = 5399
014201 meter/sec
ZDOT = 10378
978841 ZDOT = 3163
512751
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 12202
20349301
00016717 00000-0 10270-3 0 9051
2 25544 51
6446 317
3619 0000924 292
4468 67
6587 15
54597925 23150
Satellite: ISS
Catalog Number: 25544
Epoch time: 12202
20349301 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 317
3619 deg
Eccentricity:
0000924
Arg of perigee: 292
4468 deg
Mean anomaly: 67
6587 deg
Mean motion: 15
54597925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 315
Coasting Arc #7 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2012/203/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3999382
94 A = 6776281
05 meter
Y = -1759897
33 meter E =
0013283
Z = -5191121
53 I = 51
36780
XDOT = 4305
643876 Wp = 77
72716
YDOT = -6218
263458 meter/sec RA = 312
03873 deg
ZDOT = -1208
923952 TA = 180
61521
MA = 180
61685
Ha = 219
817 n
mi
Hp = 214
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13121335
10 X = -3954189
38
Y = -5773941
39 feet Y = -1804367
87 meter
Z = -17031238
60 Z = -5210440
30
XDOT = 14126
128202 XDOT = 4380
730331
YDOT = -20401
126830 feet/sec YDOT = -6169
695160 meter/sec
ZDOT = -3966
285933 ZDOT = -1187
825804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12134051
41 X = -3698458
87
Y = -7453825
56 feet Y = -2271926
03 meter
Z = -17110704
35 Z = -5215342
69
XDOT = 16192
436660 XDOT = 4935
454694
YDOT = -17454
975125 feet/sec YDOT = -5320
276418 meter/sec
ZDOT = -3878
597200 ZDOT = -1182
196427
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 12203
16771660
00016717 00000-0 10270-3 0 9065
2 25544 51
6442 312
5514 0001116 298
0716 62
0324 15
54656587 23304
Satellite: ISS
Catalog Number: 25544
Epoch time: 12203
16771660 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 312
5514 deg
Eccentricity:
0001116
Arg of perigee: 298
0716 deg
Mean anomaly: 62
0324 deg
Mean motion: 15
54656587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2330
Checksum: 283
Coasting Arc #8 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2012/204/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2712254
78 A = 6776027
20 meter
Y = 3348254
85 meter E =
0003135
Z = 5228098
07 I = 51
34755
XDOT = -5150
006462 Wp = 38
83050
YDOT = 5610
440098 meter/sec RA = 307
01346 deg
ZDOT = -918
678925 TA = 60
00633
MA = 59
97521
Ha = 219
678 n
mi
Hp = 214
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8898473
70 X = 2649215
88
Y = 10985088
09 feet Y = 3378232
23 meter
Z = 17152552
73 Z = 5241120
89
XDOT = -16896
346661 XDOT = -5207
898145
YDOT = 18406
955703 feet/sec YDOT = 5552
525884 meter/sec
ZDOT = -3014
038467 ZDOT = -943
837297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7461742
95 X = 2274339
25
Y = 11930840
28 feet Y = 3636520
12 meter
Z = 17205885
68 Z = 5244353
96
XDOT = -18026
139219 XDOT = -5494
367234
YDOT = 15783
714296 feet/sec YDOT = 4810
876117 meter/sec
ZDOT = -3118
390891 ZDOT = -950
485544
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 12204
19620487
00016717 00000-0 10270-3 0 9070
2 25544 51
6442 307
4204 0001177 300
6388 59
4649 15
54684204 23469
Satellite: ISS
Catalog Number: 25544
Epoch time: 12204
19620487 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 307
4204 deg
Eccentricity:
0001177
Arg of perigee: 300
6388 deg
Mean anomaly: 59
4649 deg
Mean motion: 15
54684204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 303
Coasting Arc #9 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2012/205/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1371928
67 A = 6778604
75 meter
Y = -4777573
63 meter E =
0009114
Z = -4617798
40 I = 51
33764
XDOT = 5527
775918 Wp = 107
41027
YDOT = -4420
275238 meter/sec RA = 301
98943 deg
ZDOT = 2933
061038 TA = 191
93811
MA = 191
95973
Ha = 219
741 n
mi
Hp = 214
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4501078
31 X = -1295971
01
Y = -15674454
18 feet Y = -4792490
51 meter
Z = -15150257
22 Z = -4624278
75
XDOT = 18135
747763 XDOT = 5562
545575
YDOT = -14502
215348 feet/sec YDOT = -4358
265918 meter/sec
ZDOT = 9622
903667 ZDOT = 2959
998607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2839229
30 X = -865397
09
Y = -16034096
55 feet Y = -4887192
63 meter
Z = -15176463
31 Z = -4625786
02
XDOT = 18250
847553 XDOT = 5562
858334
YDOT = -12438
950822 feet/sec YDOT = -3791
392210 meter/sec
ZDOT = 9734
453339 ZDOT = 2967
061378
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 12205
16039693
00016717 00000-0 10270-3 0 9082
2 25544 51
6431 302
6090 0001264 306
1902 53
9134 15
54699340 23619
Satellite: ISS
Catalog Number: 25544
Epoch time: 12205
16039693 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 302
6090 deg
Eccentricity:
0001264
Arg of perigee: 306
1902 deg
Mean anomaly: 53
9134 deg
Mean motion: 15
54699340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2361
Checksum: 285
Coasting Arc #10 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2012/206/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 58044
58 A = 6782627
19 meter
Y = 5868293
47 meter E =
0011493
Z = 3391616
97 I = 51
33633
XDOT = -5508
659467 Wp = 85
15523
YDOT = 2718
333475 meter/sec RA = 296
97579 deg
ZDOT = -4594
656818 TA = 54
99123
MA = 54
88341
Ha = 219
679 n
mi
Hp = 214
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 190434
97 X = -24055
73
Y = 19252931
35 feet Y = 5868483
40 meter
Z = 11127352
27 Z = 3391699
73
XDOT = -18073
029746 XDOT = -5516
327454
YDOT = 8918
416912 feet/sec YDOT = 2656
689507 meter/sec
ZDOT = -15074
333394 ZDOT = -4621
435876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1449060
49 X = -441673
64
Y = 19199431
32 feet Y = 5851986
67 meter
Z = 11127068
80 Z = 3391530
57
XDOT = -17248
256105 XDOT = -5257
268461
YDOT = 7526
146731 feet/sec YDOT = 2293
969524 meter/sec
ZDOT = -15185
040466 ZDOT = -4628
400334
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 12206
18884995
00016717 00000-0 10270-3 0 9099
2 25544 51
6431 297
4775 0001415 314
9329 45
1709 15
54754960 23776
Satellite: ISS
Catalog Number: 25544
Epoch time: 12206
18884995 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 297
4775 deg
Eccentricity:
0001415
Arg of perigee: 314
9329 deg
Mean anomaly: 45
1709 deg
Mean motion: 15
54754960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 339
Coasting Arc #11 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2012/207/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1100213
55 A = 6786296
36 meter
Y = -6461053
14 meter E =
0007866
Z = -1746044
70 I = 51
33400
XDOT = 5139
659283 Wp = 27
70704
YDOT = -648
011727 meter/sec RA = 291
97219 deg
ZDOT = 5653
603635 TA = 313
04255
MA = 313
10840
Ha = 219
729 n
mi
Hp = 214
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3609624
51 X = 1180862
43
Y = -21197680
91 feet Y = -6448298
86 meter
Z = -5728493
10 Z = -1740504
32
XDOT = 16862
399223 XDOT = 5119
059760
YDOT = -2126
022725 feet/sec YDOT = -590
652278 meter/sec
ZDOT = 18548
568357 ZDOT = 5678
521627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5003071
12 X = 1524936
08
Y = -20919113
82 feet Y = -6376145
89 meter
Z = -5704967
51 Z = -1738874
10
XDOT = 15325
433503 XDOT = 4671
192132
YDOT = -1405
872930 feet/sec YDOT = -428
510069 meter/sec
ZDOT = 18651
379620 ZDOT = 5684
940508
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 12207
15301008
00016717 00000-0 10270-3 0 9108
2 25544 51
6416 292
6655 0001424 315
7620 44
3419 15
54729349 23925
Satellite: ISS
Catalog Number: 25544
Epoch time: 12207
15301008 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 292
6655 deg
Eccentricity:
0001424
Arg of perigee: 315
7620 deg
Mean anomaly: 44
3419 deg
Mean motion: 15
54729349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 287
Coasting Arc #12 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2012/208/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2105251
53 A = 6787496
86 meter
Y = 6445529
31 meter E =
0010422
Z = -164295
63 I = 51
32759
XDOT = -4513
258146 Wp = 135
32629
YDOT = -1620
582336 meter/sec RA = 286
97698 deg
ZDOT = -5984
512967 TA = 46
45166
MA = 46
36515
Ha = 219
732 n
mi
Hp = 213
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6906993
21 X = -2176372
19
Y = 21146749
71 feet Y = 6421589
43 meter
Z = -539027
67 Z = -174695
17
XDOT = -14807
277381 XDOT = -4465
729750
YDOT = -5316
871182 feet/sec YDOT = -1670
786293 meter/sec
ZDOT = -19634
228893 ZDOT = -6006
322719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7895440
47 X = -2406530
25
Y = 20796748
47 feet Y = 6338848
93 meter
Z = -582582
35 Z = -177571
10
XDOT = -12902
718151 XDOT = -3932
748493
YDOT = -5430
698792 feet/sec YDOT = -1655
276992 meter/sec
ZDOT = -19723
986756 ZDOT = -6011
871163
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 12208
18143033
00016717 00000-0 10270-3 0 9115
2 25544 51
6414 287
5337 0001339 320
1196 39
9858 15
54754094 24086
Satellite: ISS
Catalog Number: 25544
Epoch time: 12208
18143033 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 287
5337 deg
Eccentricity:
0001339
Arg of perigee: 320
1196 deg
Mean anomaly: 39
9858 deg
Mean motion: 15
54754094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 305
Coasting Arc #13 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2012/209/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2889286
50 A = 6785568
68 meter
Y = -5786292
10 meter E =
0013549
Z = 2029854
83 I = 51
31283
XDOT = 3718
549830 Wp = 63
35560
YDOT = 3804
151853 meter/sec RA = 281
97837 deg
ZDOT = 5528
466732 TA = 319
20312
MA = 319
30449
Ha = 219
606 n
mi
Hp = 213
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9479286
43 X = 2943914
74
Y = -18983897
96 feet Y = -5753677
02 meter
Z = 6659628
69 Z = 2044023
01
XDOT = 12199
966633 XDOT = 3648
878729
YDOT = 12480
813166 feet/sec YDOT = 3845
344983 meter/sec
ZDOT = 18138
014214 ZDOT = 5546
362281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10005171
41 X = 3049576
25
Y = -18690965
18 feet Y = -5697006
19 meter
Z = 6718651
13 Z = 2047844
86
XDOT = 10345
020976 XDOT = 3153
162393
YDOT = 12110
389967 feet/sec YDOT = 3691
246862 meter/sec
ZDOT = 18211
408983 ZDOT = 5550
837458
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 12209
20983156
00016717 00000-0 10270-3 0 9128
2 25544 51
6405 282
4002 0001376 320
0734 40
0318 15
54811439 24246
Satellite: ISS
Catalog Number: 25544
Epoch time: 12209
20983156 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 282
4002 deg
Eccentricity:
0001376
Arg of perigee: 320
0734 deg
Mean anomaly: 40
0318 deg
Mean motion: 15
54811439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 268
Coasting Arc #14 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2012/210/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3506435
93 A = 6781570
15 meter
Y = 4510310
54 meter E =
0005345
Z = -3660252
86 I = 51
29344
XDOT = -2794
618448 Wp = 65
22926
YDOT = -5677
412357 meter/sec RA = 276
97110 deg
ZDOT = -4321
540314 TA = 158
50435
MA = 158
48190
Ha = 219
712 n
mi
Hp = 213
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11504054
90 X = -3538829
99
Y = 14797606
76 feet Y = 4470918
64 meter
Z = -12008703
61 Z = -3677365
08
XDOT = -9168
695696 XDOT = -2709
931829
YDOT = -18626
680962 feet/sec YDOT = -5708
189566 meter/sec
ZDOT = -14178
281871 ZDOT = -4334
911232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11620127
54 X = -3541814
87
Y = 14648347
87 feet Y = 4464816
43 meter
Z = -12079732
93 Z = -3681902
60
XDOT = -7773
001507 XDOT = -2369
210859
YDOT = -17895
698722 feet/sec YDOT = -5454
608971 meter/sec
ZDOT = -14232
832432 ZDOT = -4338
167325
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 12210
17394433
00016717 00000-0 10270-3 0 9131
2 25544 51
6396 277
5886 0001403 331
1530 28
9537 15
54820620 24394
Satellite: ISS
Catalog Number: 25544
Epoch time: 12210
17394433 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 277
5886 deg
Eccentricity:
0001403
Arg of perigee: 331
1530 deg
Mean anomaly: 28
9537 deg
Mean motion: 15
54820620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2439
Checksum: 299
Coasting Arc #15 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2012/211/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3930197
18 A = 6777530
59 meter
Y = -2753513
59 meter E =
0006199
Z = 4781996
32 I = 51
27699
XDOT = 1804
947436 Wp = 111
38028
YDOT = 7008
321848 meter/sec RA = 271
94943 deg
ZDOT = 2547
119141 TA = 313
40932
MA = 313
46091
Ha = 219
646 n
mi
Hp = 213
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12894347
70 X = 3937465
83
Y = -9033837
23 feet Y = -2709523
58 meter
Z = 15688964
31 Z = 4801106
18
XDOT = 5921
743556 XDOT = 1714
071599
YDOT = 22993
181915 feet/sec YDOT = 7027
997488 meter/sec
ZDOT = 8356
690096 ZDOT = 2555
667457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12759095
96 X = 3888972
45
Y = -9088014
32 feet Y = -2770026
76 meter
Z = 15768052
67 Z = 4806102
45
XDOT = 5307
132012 XDOT = 1617
613837
YDOT = 22037
744957 feet/sec YDOT = 6717
104663 meter/sec
ZDOT = 8391
226755 ZDOT = 2557
645915
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 12211
20231527
00016717 00000-0 10270-3 0 9141
2 25544 51
6395 272
4554 0001443 335
4625 24
6460 15
54810340 24559
Satellite: ISS
Catalog Number: 25544
Epoch time: 12211
20231527 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 272
4554 deg
Eccentricity:
0001443
Arg of perigee: 335
4625 deg
Mean anomaly: 24
6460 deg
Mean motion: 15
54810340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2455
Checksum: 274
Coasting Arc #16 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2012/212/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203694
06 A = 6775271
70 meter
Y = 695709
70 meter E =
0014500
Z = -5280353
26 I = 51
26920
XDOT = -740
894090 Wp = 81
94622
YDOT = -7612
031544 meter/sec RA = 266
91751 deg
ZDOT = -412
071995 TA = 184
09312
MA = 184
10500
Ha = 219
742 n
mi
Hp = 213
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13791647
18 X = -4185510
86
Y = 2282512
13 feet Y = 648803
64 meter
Z = -17323993
63 Z = -5300730
04
XDOT = -2430
754889 XDOT = -653
718002
YDOT = -24973
856771 feet/sec YDOT = -7619
829207 meter/sec
ZDOT = -1351
942240 ZDOT = -415
460268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13633252
70 X = -4155415
42
Y = 2575369
79 feet Y = 784972
71 meter
Z = -17408102
71 Z = -5305989
71
XDOT = -2771
534857 XDOT = -844
763825
YDOT = -23921
877473 feet/sec YDOT = -7291
388254 meter/sec
ZDOT = -1365
149747 ZDOT = -416
097643
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 12212
16639583
00016717 00000-0 10270-3 0 9152
2 25544 51
6388 267
6434 0001270 341
1570 18
9536 15
54864991 24703
Satellite: ISS
Catalog Number: 25544
Epoch time: 12212
16639583 = yrday
fracday
Element set: 915
Inclination: 51
6388 deg
RA of node: 267
6434 deg
Eccentricity:
0001270
Arg of perigee: 341
1570 deg
Mean anomaly: 18
9536 deg
Mean motion: 15
54864991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 319
Coasting Arc #17 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2012/213/03:35:25
371
Vector Time (MET): N/A
Weight (LBS) : 923128
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4289528
82 A = 6776276
72 meter
Y = 1436024
00 meter E =
0005914
Z = 5042984
96 I = 51
27487
XDOT = -385
738208 Wp = 43
61880
YDOT = 7450
374955 meter/sec RA = 261
88383 deg
ZDOT = -1787
971562 TA = 63
79348
MA = 63
73269
Ha = 219
638 n
mi
Hp = 213
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14073257
29 X = 4248654
94
Y = 4711364
81 feet Y = 1483763
14 meter
Z = 16545226
25 Z = 5063723
72
XDOT = -1265
545301 XDOT = -460
335787
YDOT = 24443
487385 feet/sec YDOT = 7445
644468 meter/sec
ZDOT = -5866
048433 ZDOT = -1790
025884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14143839
66 X = 4311042
33
Y = 4167996
46 feet Y = 1270405
32 meter
Z = 16630623
74 Z = 5069014
12
XDOT = 21
489368 XDOT = 6
549959
YDOT = 23441
002740 feet/sec YDOT = 7144
817635 meter/sec
ZDOT = -5875
258609 ZDOT = -1790
778824
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 12213
19473322
00016717 00000-0 10270-3 0 9164
2 25544 51
6384 262
5107 0001271 343
5761 16
5351 15
54862066 24855
Satellite: ISS
Catalog Number: 25544
Epoch time: 12213
19473322 = yrday
fracday
Element set: 916
Inclination: 51
6384 deg
RA of node: 262
5107 deg
Eccentricity:
0001271
Arg of perigee: 343
5761 deg
Mean anomaly: 16
5351 deg
Mean motion: 15
54862066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 293
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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