[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 26th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2011/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4492232
21 A = 6770370
83 meter
Y = -4681600
24 meter E =
0017913
Z = -1899556
88 I = 51
47093
XDOT = 4730
381445 Wp = 15
41645
YDOT = 2273
632691 meter/sec RA = 327
29835 deg
ZDOT = 5612
339880 TA = 323
53446
MA = 323
65632
Ha = 214
490 n
mi
Hp = 203
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14738294
65 X = 4553476
51
Y = -15359580
85 feet Y = -4631022
71 meter
Z = -6232141
99 Z = -1877585
60
XDOT = 15519
624165 XDOT = 4677
342198
YDOT = 7459
424840 feet/sec YDOT = 2326
233493 meter/sec
ZDOT = 18413
188583 ZDOT = 5635
191289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20860384
66 X = -6358245
24
Y = -4368788
53 feet Y = -1331606
74 meter
Z = -6142612
26 Z = -1872268
22
XDOT = -2175
157612 XDOT = -662
988040
YDOT = -15497
471860 feet/sec YDOT = -4723
629423 meter/sec
ZDOT = 18505
848645 ZDOT = 5640
582667
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 11206
50367607
00016717 00000-0 10270-3 0 9001
2 25544 51
6404 327
8544 0011687 1
9167 358
2032 15
60153879 6893
Satellite: ISS
Catalog Number: 25544
Epoch time: 11206
50367607 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 327
8544 deg
Eccentricity:
0011687
Arg of perigee: 1
9167 deg
Mean anomaly: 358
2032 deg
Mean motion: 15
60153879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 308
Coasting Arc #2 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2011/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5915169
63 A = 6770357
43 meter
Y = 2788693
12 meter E =
0008205
Z = -1772040
91 I = 51
44657
XDOT = -728
519697 Wp = 44
09089
YDOT = -5130
047471 meter/sec RA = 322
28709 deg
ZDOT = -5651
412598 TA = 155
44750
MA = 155
40842
Ha = 214
525 n
mi
Hp = 203
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19406724
49 X = -5937305
55
Y = 9149255
64 feet Y = 2722422
54 meter
Z = -5813782
51 Z = -1800829
87
XDOT = -2390
156487 XDOT = -643
647163
YDOT = -16830
864406 feet/sec YDOT = -5137
718960 meter/sec
ZDOT = -18541
379916 ZDOT = -5654
746199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18232465
16 X = 5557255
38
Y = 11248634
19 feet Y = 3428583
70 meter
Z = -5930880
56 Z = -1807732
39
XDOT = -12046
117486 XDOT = -3671
656610
YDOT = 9759
061978 feet/sec YDOT = 2974
562091 meter/sec
ZDOT = -18554
593329 ZDOT = -5655
440047
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 11207
52851988
00016717 00000-0 10270-3 0 9015
2 25544 51
6404 322
6983 0011673 5
8821 354
2470 15
60192267 7053
Satellite: ISS
Catalog Number: 25544
Epoch time: 11207
52851988 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 322
6983 deg
Eccentricity:
0011673
Arg of perigee: 5
8821 deg
Mean anomaly: 354
2470 deg
Mean motion: 15
60192267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 302
Coasting Arc #3 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2011/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4958006
37 A = 6762584
51 meter
Y = 385603
13 meter E =
0012431
Z = 4570588
83 I = 51
39843
XDOT = -3257
408152 Wp = 49
54078
YDOT = 6279
973815 meter/sec RA = 317
24657 deg
ZDOT = 3006
255237 TA = 10
44304
MA = 10
41725
Ha = 214
451 n
mi
Hp = 203
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16266425
08 X = 4931123
25
Y = 1265102
14 feet Y = 440895
67 meter
Z = 14995370
19 Z = 4594609
20
XDOT = -10687
034619 XDOT = -3341
993547
YDOT = 20603
588632 feet/sec YDOT = 6243
074158 meter/sec
ZDOT = 9863
042116 ZDOT = 2990
226367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8003862
41 X = -2439577
26
Y = -14113846
10 feet Y = -4301900
29 meter
Z = 15092903
31 Z = 4600316
93
XDOT = 22060
085799 XDOT = 6723
914152
YDOT = -2041
839365 feet/sec YDOT = -622
352638 meter/sec
ZDOT = 9797
548272 ZDOT = 2986
292713
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 11208
55335288
00016717 00000-0 10270-3 0 9020
2 25544 51
6412 317
5422 0011685 9
4430 350
6944 15
60227162 7219
Satellite: ISS
Catalog Number: 25544
Epoch time: 11208
55335288 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 317
5422 deg
Eccentricity:
0011685
Arg of perigee: 9
4430 deg
Mean anomaly: 350
6944 deg
Mean motion: 15
60227162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 283
Coasting Arc #4 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2011/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2269931
72 A = 6760049
04 meter
Y = -3688520
32 meter E =
0019303
Z = -5203454
47 I = 51
36840
XDOT = 5701
661131 Wp = 60
46766
YDOT = -5011
900687 meter/sec RA = 312
16835 deg
ZDOT = 1077
820162 TA = 219
82811
MA = 219
96994
Ha = 214
703 n
mi
Hp = 202
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7447282
55 X = -2203240
35
Y = -12101444
63 feet Y = -3713530
54 meter
Z = -17071701
01 Z = -5214320
04
XDOT = 18706
237305 XDOT = 5752
045669
YDOT = -16443
243723 feet/sec YDOT = -4947
859659 meter/sec
ZDOT = 3536
155386 ZDOT = 1105
640021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5697077
91 X = -1736469
35
Y = 12959525
46 feet Y = 3950063
36 meter
Z = -17115605
68 Z = -5216836
61
XDOT = -23243
191965 XDOT = -7084
524911
YDOT = -5451
390631 feet/sec YDOT = -1661
583864 meter/sec
ZDOT = 3649
456505 ZDOT = 1112
354343
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 11209
51412721
00016717 00000-0 10270-3 0 9036
2 25544 51
6413 312
7098 0011856 13
2476 346
8989 15
60230628 7362
Satellite: ISS
Catalog Number: 25544
Epoch time: 11209
51412721 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 312
7098 deg
Eccentricity:
0011856
Arg of perigee: 13
2476 deg
Mean anomaly: 346
8989 deg
Mean motion: 15
60230628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 302
Coasting Arc #5 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2011/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1070667
46 A = 6767045
92 meter
Y = 5802222
00 meter E =
0019536
Z = 3311576
50 I = 51
37188
XDOT = -5882
192116 Wp = 55
66732
YDOT = 1595
373344 meter/sec RA = 307
10282 deg
ZDOT = -4666
491947 TA = 85
53902
MA = 85
31586
Ha = 214
896 n
mi
Hp = 202
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3512688
53 X = -1151556
10
Y = 19036161
43 feet Y = 5789796
51 meter
Z = 10864752
30 Z = 3306179
48
XDOT = -19298
530564 XDOT = -5876
926298
YDOT = 5234
164515 feet/sec YDOT = 1529
625038 meter/sec
ZDOT = -15310
012948 ZDOT = -4695
053974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17503663
69 X = 5335116
69
Y = -8295756
77 feet Y = -2528546
66 meter
Z = 10842483
20 Z = 3304788
88
XDOT = 14918
679187 XDOT = 4547
213416
YDOT = 11184
689745 feet/sec YDOT = 3409
093434 meter/sec
ZDOT = -15426
120137 ZDOT = -4701
881418
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 11210
53894371
00016717 00000-0 10270-3 0 9046
2 25544 51
6410 307
5537 0011859 17
4442 342
7119 15
60211316 7522
Satellite: ISS
Catalog Number: 25544
Epoch time: 11210
53894371 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 307
5537 deg
Eccentricity:
0011859
Arg of perigee: 17
4442 deg
Mean anomaly: 342
7119 deg
Mean motion: 15
60211316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 282
Coasting Arc #6 (Orbit 767)
---------------------------------------
Vector Time (GMT): 2011/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3679864
17 A = 6771683
86 meter
Y = -5666627
94 meter E =
0023863
Z = 135861
46 I = 51
37058
XDOT = 3954
816138 Wp = 33
66480
YDOT = 2723
796217 meter/sec RA = 302
07867 deg
ZDOT = 6003
468673 TA = 327
80984
MA = 327
95530
Ha = 214
989 n
mi
Hp = 202
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12073045
18 X = 3742296
04
Y = -18591299
01 feet Y = -5625128
39 meter
Z = 445739
70 Z = 153888
92
XDOT = 12975
118563 XDOT = 3894
901216
YDOT = 8936
339293 feet/sec YDOT = 2767
685872 meter/sec
ZDOT = 19696
419531 ZDOT = 6022
535351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22111951
30 X = -6739722
76
Y = 1544488
97 feet Y = 470760
24 meter
Z = 519293
89 Z = 158280
78
XDOT = -483
776923 XDOT = -147
455206
YDOT = -14033
835588 feet/sec YDOT = -4277
513087 meter/sec
ZDOT = 19773
707637 ZDOT = 6027
026088
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 11211
56375001
00016717 00000-0 10270-3 0 9055
2 25544 51
6415 302
3979 0012061 20
6471 339
5170 15
60219028 7680
Satellite: ISS
Catalog Number: 25544
Epoch time: 11211
56375001 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 302
3979 deg
Eccentricity:
0012061
Arg of perigee: 20
6471 deg
Mean anomaly: 339
5170 deg
Mean motion: 15
60219028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 768
Checksum: 279
Coasting Arc #7 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2011/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4817058
65 A = 6766118
84 meter
Y = 3167960
29 meter E =
0015434
Z = -3561141
25 I = 51
33611
XDOT = -807
948299 Wp = 41
09032
YDOT = -6204
044038 meter/sec RA = 297
05120 deg
ZDOT = -4425
697942 TA = 181
21010
MA = 181
21384
Ha = 215
034 n
mi
Hp = 202
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15803998
20 X = -4834826
48
Y = 10393570
51 feet Y = 3113993
86 meter
Z = -11683534
30 Z = -3584584
86
XDOT = -2650
749012 XDOT = -717
014773
YDOT = -20354
475189 feet/sec YDOT = -6212
570317 meter/sec
ZDOT = -14520
006370 ZDOT = -4429
402332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17873546
77 X = 5447857
06
Y = 6007543
33 feet Y = 1831099
21 meter
Z = -11778938
39 Z = -3590220
42
XDOT = -14030
419903 XDOT = -4276
471986
YDOT = 13241
970947 feet/sec YDOT = 4036
152745 meter/sec
ZDOT = -14534
705793 ZDOT = -4430
178326
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 11212
52449667
00016717 00000-0 10270-3 0 9063
2 25544 51
6404 297
5646 0011950 24
2331 335
9385 15
60244083 7839
Satellite: ISS
Catalog Number: 25544
Epoch time: 11212
52449667 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 297
5646 deg
Eccentricity:
0011950
Arg of perigee: 24
2331 deg
Mean anomaly: 335
9385 deg
Mean motion: 15
60244083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 306
Coasting Arc #8 (Orbit 798)
---------------------------------------
Vector Time (GMT): 2011/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4190762
44 A = 6759605
17 meter
Y = 816247
37 meter E =
0012393
Z = 5232473
43 I = 51
30206
XDOT = -2316
329214 Wp = 41
51509
YDOT = 7292
842767 meter/sec RA = 291
97784 deg
ZDOT = 725
675611 TA = 41
58380
MA = 41
48960
Ha = 214
925 n
mi
Hp = 202
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13749220
60 X = 4155905
77
Y = 2677976
93 feet Y = 862915
96 meter
Z = 17166907
59 Z = 5252747
01
XDOT = -7599
505294 XDOT = -2401
232156
YDOT = 23926
649497 feet/sec YDOT = 7266
465418 meter/sec
ZDOT = 2380
825494 ZDOT = 714
217188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6497056
62 X = -1980302
86
Y = -12295048
34 feet Y = -3747530
73 meter
Z = 17249214
05 Z = 5257560
44
XDOT = 22495
864736 XDOT = 6856
739572
YDOT = -8650
501085 feet/sec YDOT = -2636
672731 meter/sec
ZDOT = 2333
887766 ZDOT = 711
368991
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 11213
54928325
00016717 00000-0 10270-3 0 9070
2 25544 51
6405 292
4079 0012001 27
5851 332
5940 15
60295646 7993
Satellite: ISS
Catalog Number: 25544
Epoch time: 11213
54928325 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 292
4079 deg
Eccentricity:
0012001
Arg of perigee: 27
5851 deg
Mean anomaly: 332
5940 deg
Mean motion: 15
60295646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 799
Checksum: 307
Coasting Arc #9 (Orbit 813)
---------------------------------------
Vector Time (GMT): 2011/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2285343
37 A = 6763118
37 meter
Y = -4607115
49 meter E =
0016595
Z = -4401024
92 I = 51
30234
XDOT = 4398
994442 Wp = 64
37262
YDOT = -5336
093845 meter/sec RA = 286
89456 deg
ZDOT = 3318
515529 TA = 239
21017
MA = 239
37364
Ha = 215
145 n
mi
Hp = 201
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7497845
70 X = -2212276
93
Y = -15115208
30 feet Y = -4632262
97 meter
Z = -14439058
14 Z = -4411949
49
XDOT = 14432
396464 XDOT = 4442
216329
YDOT = -17506
869569 feet/sec YDOT = -5286
660000 meter/sec
ZDOT = 10887
518139 ZDOT = 3339
990280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6830518
03 X = -2081941
90
Y = 15386837
75 feet Y = 4689908
15 meter
Z = -14483192
31 Z = -4414477
02
XDOT = -21523
511929 XDOT = -6560
366436
YDOT = 723
948122 feet/sec YDOT = 220
659387 meter/sec
ZDOT = 10975
026380 ZDOT = 3345
188041
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 11214
51001468
00016717 00000-0 10270-3 0 9089
2 25544 51
6393 287
5749 0012187 31
7234 328
4653 15
60303444 8144
Satellite: ISS
Catalog Number: 25544
Epoch time: 11214
51001468 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 287
5749 deg
Eccentricity:
0012187
Arg of perigee: 31
7234 deg
Mean anomaly: 328
4653 deg
Mean motion: 15
60303444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 814
Checksum: 297
Coasting Arc #10 (Orbit 829)
---------------------------------------
Vector Time (GMT): 2011/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -255248
73 A = 6770606
23 meter
Y = 6620962
27 meter E =
0019405
Z = 1386151
38 I = 51
31944
XDOT = -4943
589867 Wp = 80
29537
YDOT = 1034
249480 meter/sec RA = 281
84946 deg
ZDOT = -5778
046612 TA = 84
49751
MA = 84
27620
Ha = 215
299 n
mi
Hp = 201
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -837430
22 X = -336000
21
Y = 21722317
15 feet Y = 6617656
39 meter
Z = 4547740
75 Z = 1384715
35
XDOT = -16219
126859 XDOT = -4926
719378
YDOT = 3393
206956 feet/sec YDOT = 979
061652 meter/sec
ZDOT = -18956
845839 ZDOT = -5802
021187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16977892
94 X = 5174861
77
Y = -13578202
57 feet Y = -4138636
14 meter
Z = 4541570
65 Z = 1384270
73
XDOT = 12123
768584 XDOT = 3695
324664
YDOT = 8706
586568 feet/sec YDOT = 2653
767586 meter/sec
ZDOT = -19054
281320 ZDOT = -5807
744946
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 11215
53478477
00016717 00000-0 10270-3 0 9091
2 25544 51
6390 282
4177 0012329 35
0660 325
1305 15
60308603 8306
Satellite: ISS
Catalog Number: 25544
Epoch time: 11215
53478477 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 282
4177 deg
Eccentricity:
0012329
Arg of perigee: 35
0660 deg
Mean anomaly: 325
1305 deg
Mean motion: 15
60308603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 830
Checksum: 291
Coasting Arc #11 (Orbit 845)
---------------------------------------
Vector Time (GMT): 2011/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2518821
73 A = 6769266
72 meter
Y = -5847779
10 meter E =
0025181
Z = 2254865
69 I = 51
30935
XDOT = 3919
923850 Wp = 56
41064
YDOT = 3790
806783 meter/sec RA = 276
82645 deg
ZDOT = 5422
412757 TA = 328
91024
MA = 329
05901
Ha = 215
348 n
mi
Hp = 201
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8263850
81 X = 2573071
93
Y = -19185626
96 feet Y = -5819308
82 meter
Z = 7397853
32 Z = 2267233
63
XDOT = 12860
642554 XDOT = 3850
902191
YDOT = 12437
030129 feet/sec YDOT = 3834
255725 meter/sec
ZDOT = 17790
068102 ZDOT = 5441
287947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19766893
64 X = -6024949
18
Y = 6700690
43 feet Y = 2042370
44 meter
Z = 7448383
02 Z = 2270267
14
XDOT = 1223
998106 XDOT = 373
074623
YDOT = -16357
677301 feet/sec YDOT = -4985
820041 meter/sec
ZDOT = 17866
548642 ZDOT = 5445
724026
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 11216
55954601
00016717 00000-0 10270-3 0 9104
2 25544 51
6387 277
2609 0012382 39
0450 321
1598 15
60294914 8460
Satellite: ISS
Catalog Number: 25544
Epoch time: 11216
55954601 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 277
2609 deg
Eccentricity:
0012382
Arg of perigee: 39
0450 deg
Mean anomaly: 321
1598 deg
Mean motion: 15
60294914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 846
Checksum: 308
Coasting Arc #12 (Orbit 860)
---------------------------------------
Vector Time (GMT): 2011/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3964856
78 A = 6761375
56 meter
Y = 2598578
62 meter E =
0023414
Z = -4843045
28 I = 51
28017
XDOT = -1703
810298 Wp = 57
19667
YDOT = -7073
508335 meter/sec RA = 271
76869 deg
ZDOT = -2396
497315 TA = 189
14292
MA = 189
18562
Ha = 215
452 n
mi
Hp = 201
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13008060
29 X = -3970093
49
Y = 8525520
40 feet Y = 2554212
08 meter
Z = -15889256
15 Z = -4862318
99
XDOT = -5589
928799 XDOT = -1612
944681
YDOT = -23207
048344 feet/sec YDOT = -7092
053231 meter/sec
ZDOT = -7862
524000 ZDOT = -2404
553910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15034489
67 X = 4582512
45
Y = 3655145
66 feet Y = 1114088
40 meter
Z = -15967674
29 Z = -4866947
12
XDOT = -12960
190862 XDOT = -3950
266175
YDOT = 18762
113313 feet/sec YDOT = 5718
692138 meter/sec
ZDOT = -7894
901968 ZDOT = -2406
366120
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 11217
52025111
00016717 00000-0 10270-3 0 9118
2 25544 51
6384 272
4260 0012358 42
4602 317
7508 15
60300911 8611
Satellite: ISS
Catalog Number: 25544
Epoch time: 11217
52025111 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 272
4260 deg
Eccentricity:
0012358
Arg of perigee: 42
4602 deg
Mean anomaly: 317
7508 deg
Mean motion: 15
60300911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 861
Checksum: 263
Coasting Arc #13 (Orbit 876)
---------------------------------------
Vector Time (GMT): 2011/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4140457
83 A = 6760334
21 meter
Y = 1793575
80 meter E =
0017786
Z = 5025715
12 I = 51
27758
XDOT = -1011
039231 Wp = 48
53526
YDOT = 7404
718333 meter/sec RA = 266
67856 deg
ZDOT = -1793
918779 TA = 58
95984
MA = 58
78533
Ha = 215
323 n
mi
Hp = 201
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13584179
22 X = 4095680
19
Y = 5884435
03 feet Y = 1839626
25 meter
Z = 16488566
67 Z = 5045720
63
XDOT = -3317
057844 XDOT = -1085
050634
YDOT = 24293
695317 feet/sec YDOT = 7392
998563 meter/sec
ZDOT = -5885
560298 ZDOT = -1799
009691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5106789
46 X = -1556549
43
Y = -13798317
11 feet Y = -4205727
05 meter
Z = 16569745
86 Z = 5050458
54
XDOT = 18776
945062 XDOT = 5723
212855
YDOT = -14104
001450 feet/sec YDOT = -4298
899642 meter/sec
ZDOT = -5906
600499 ZDOT = -1800
331832
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 11218
54499265
00016717 00000-0 10270-3 0 9127
2 25544 51
6385 267
2692 0012412 45
7242 314
4930 15
60362574 8773
Satellite: ISS
Catalog Number: 25544
Epoch time: 11218
54499265 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 267
2692 deg
Eccentricity:
0012412
Arg of perigee: 45
7242 deg
Mean anomaly: 314
4930 deg
Mean motion: 15
60362574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 877
Checksum: 314
Coasting Arc #14 (Orbit 891)
---------------------------------------
Vector Time (GMT): 2011/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3047928
36 A = 6767876
08 meter
Y = -5359370
32 meter E =
0017228
Z = -2788701
73 I = 51
30587
XDOT = 3446
305688 Wp = 52
92860
YDOT = -4593
405386 meter/sec RA = 261
61380 deg
ZDOT = 5092
967430 TA = 275
19974
MA = 275
39633
Ha = 215
495 n
mi
Hp = 200
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9999764
97 X = -2974225
45
Y = -17583235
95 feet Y = -5393041
80 meter
Z = -9149283
89 Z = -2803329
80
XDOT = 11306
777192 XDOT = 3472
673460
YDOT = -15070
227645 feet/sec YDOT = -4554
719665 meter/sec
ZDOT = 16709
210728 ZDOT = 5109
773086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5444652
72 X = -1659530
15
Y = 19453406
63 feet Y = 5929398
34 meter
Z = -9208453
12 Z = -2806736
51
XDOT = -17166
933177 XDOT = -5232
481232
YDOT = 3087
872830 feet/sec YDOT = 941
183639 meter/sec
ZDOT = 16777
703244 ZDOT = 5113
843949
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 11219
50568248
00016717 00000-0 10270-3 0 9133
2 25544 51
6386 262
4348 0012579 50
0125 310
2133 15
60368684 8926
Satellite: ISS
Catalog Number: 25544
Epoch time: 11219
50568248 = yrday
fracday
Element set: 913
Inclination: 51
6386 deg
RA of node: 262
4348 deg
Eccentricity:
0012579
Arg of perigee: 50
0125 deg
Mean anomaly: 310
2133 deg
Mean motion: 15
60368684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 892
Checksum: 303
Coasting Arc #15 (Orbit 907)
---------------------------------------
Vector Time (GMT): 2011/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 862090
52 A = 6770903
18 meter
Y = 6659321
56 meter E =
0016566
Z = -881913
38 I = 51
32184
XDOT = -4892
925743 Wp = 91
02665
YDOT = -135
956825 meter/sec RA = 256
58858 deg
ZDOT = -5906
071009 TA = 98
57539
MA = 98
38766
Ha = 215
626 n
mi
Hp = 200
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2828380
96 X = 791844
73
Y = 21848167
86 feet Y = 6668569
30 meter
Z = -2893416
60 Z = -877895
44
XDOT = -16052
905980 XDOT = -4862
351594
YDOT = -446
052576 feet/sec YDOT = -190
501029 meter/sec
ZDOT = -19376
873389 ZDOT = -5929
766242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13173301
38 X = 4015222
26
Y = -17660654
16 feet Y = -5382967
39 meter
Z = -2877405
52 Z = -877033
20
XDOT = 9836
995013 XDOT = 2998
316080
YDOT = 10458
367279 feet/sec YDOT = 3187
710347 meter/sec
ZDOT = -19473
136183 ZDOT = -5935
411908
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 11220
53040762
00016717 00000-0 10270-3 0 9145
2 25544 51
6389 257
2772 0012693 53
4493 306
7830 15
60371976 9084
Satellite: ISS
Catalog Number: 25544
Epoch time: 11220
53040762 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 257
2772 deg
Eccentricity:
0012693
Arg of perigee: 53
4493 deg
Mean anomaly: 306
7830 deg
Mean motion: 15
60371976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 908
Checksum: 313
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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