[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 20th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 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 1079)
---------------------------------------
Vector Time (GMT): 2011/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2566142
56 A = 6759389
25 meter
Y = -3448874
61 meter E =
0015658
Z = 5202990
09 I = 51
48944
XDOT = 6778
343507 Wp = 85
33465
YDOT = 3484
771580 meter/sec RA = 201
03890 deg
ZDOT = -1029
271098 TA = 14
53562
MA = 14
49064
Ha = 215
660 n
mi
Hp = 200
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8419102
89 X = 2579242
85
Y = -11315205
40 feet Y = -3420105
10 meter
Z = 17070177
46 Z = 5215488
19
XDOT = 22238
659800 XDOT = 6743
872301
YDOT = 11432
977626 feet/sec YDOT = 3560
378400 meter/sec
ZDOT = -3376
873680 ZDOT = -996
425960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13162477
64 X = -4011923
18
Y = 4891101
24 feet Y = 1490807
66 meter
Z = 17121110
84 Z = 5218514
58
XDOT = -11970
698071 XDOT = -3648
668772
YDOT = -20816
092740 feet/sec YDOT = -6344
745067 meter/sec
ZDOT = -3243
433645 ZDOT = -988
598575
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 11231
54640173
00016717 00000-0 10270-3 0 9005
2 25544 51
6357 201
8580 0012579 92
5549 267
7047 15
60424812 10806
Satellite: ISS
Catalog Number: 25544
Epoch time: 11231
54640173 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 201
8580 deg
Eccentricity:
0012579
Arg of perigee: 92
5549 deg
Mean anomaly: 267
7047 deg
Mean motion: 15
60424812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 295
Coasting Arc #2 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2011/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5791522
34 A = 6766229
28 meter
Y = 1099022
61 meter E =
0017399
Z = -3337841
35 I = 51
54126
XDOT = -3608
728930 Wp = 94
17516
YDOT = -4892
250338 meter/sec RA = 195
98160 deg
ZDOT = 4670
479593 TA = 226
83143
MA = 226
97698
Ha = 215
714 n
mi
Hp = 200
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19001057
55 X = -5787166
87
Y = 3605717
23 feet Y = 1034282
61 meter
Z = -10950923
06 Z = -3365965
80
XDOT = -11839
661843 XDOT = -3576
442814
YDOT = -16050
690084 feet/sec YDOT = -4932
424807 meter/sec
ZDOT = 15323
095776 ZDOT = 4653
026950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17929608
63 X = 5464944
71
Y = 7074724
63 feet Y = 2156376
07 meter
Z = -11065329
01 Z = -3372712
28
XDOT = 2020
309349 XDOT = 615
790290
YDOT = 18635
071198 feet/sec YDOT = 5679
969701 meter/sec
ZDOT = 15252
284823 ZDOT = 4648
896414
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 11232
50702826
00016717 00000-0 10270-3 0 9017
2 25544 51
6358 197
0234 0012623 95
7961 264
4635 15
60425410 10950
Satellite: ISS
Catalog Number: 25544
Epoch time: 11232
50702826 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 197
0234 deg
Eccentricity:
0012623
Arg of perigee: 95
7961 deg
Mean anomaly: 264
4635 deg
Mean motion: 15
60425410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 291
Coasting Arc #3 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2011/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6593678
82 A = 6770964
70 meter
Y = 1487606
71 meter E =
0022997
Z = -259471
88 I = 51
58730
XDOT = -1260
410988 Wp = 117
68371
YDOT = 4610
963883 meter/sec RA = 190
96942 deg
ZDOT = -6011
157299 TA = 65
12230
MA = 64
88339
Ha = 215
661 n
mi
Hp = 200
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21632804
53 X = 6577814
51
Y = 4880599
44 feet Y = 1561252
55 meter
Z = -851285
70 Z = -227478
53
XDOT = -4135
206654 XDOT = -1282
677095
YDOT = 15127
834261 feet/sec YDOT = 4596
744754 meter/sec
ZDOT = -19721
644682 ZDOT = -6017
334377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15945343
81 X = -4860140
79
Y = -15419112
30 feet Y = -4699745
43 meter
Z = -721218
79 Z = -219827
49
XDOT = 10171
406027 XDOT = 3100
244557
YDOT = -9670
482349 feet/sec YDOT = -2947
563020 meter/sec
ZDOT = -19746
919229 ZDOT = -6018
860981
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 11233
53168664
00016717 00000-0 10270-3 0 9028
2 25544 51
6364 191
8652 0012534 99
5248 260
7325 15
60460861 11117
Satellite: ISS
Catalog Number: 25544
Epoch time: 11233
53168664 = yrday
fracday
Element set: 902
Inclination: 51
6364 deg
RA of node: 191
8652 deg
Eccentricity:
0012534
Arg of perigee: 99
5248 deg
Mean anomaly: 260
7325 deg
Mean motion: 15
60460861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 299
Coasting Arc #4 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2011/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4548210
42 A = 6765197
58 meter
Y = -3395090
71 meter E =
0024298
Z = 3664671
53 I = 51
59840
XDOT = 5659
568716 Wp = 99
62638
YDOT = -2867
462864 meter/sec RA = 185
95682 deg
ZDOT = 4339
097251 TA = 304
17577
MA = 304
40589
Ha = 215
606 n
mi
Hp = 200
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14921950
19 X = -4527709
98
Y = -11138749
04 feet Y = -3445837
02 meter
Z = 12023200
55 Z = 3642626
24
XDOT = 18568
138833 XDOT = 5670
134241
YDOT = -9407
686561 feet/sec YDOT = -2804
115123 meter/sec
ZDOT = 14235
883369 ZDOT = 4366
616808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7313646
50 X = 2229199
45
Y = 17186982
35 feet Y = 5238592
22 meter
Z = 11933645
35 Z = 3637375
10
XDOT = -19449
230638 XDOT = -5928
125498
YDOT = -1751
337623 feet/sec YDOT = -533
807707 meter/sec
ZDOT = 14347
912897 ZDOT = 4373
243851
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 11234
55633338
00016717 00000-0 10270-3 0 9037
2 25544 51
6366 186
7088 0012470 104
0309 256
2234 15
60504697 11276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11234
55633338 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 186
7088 deg
Eccentricity:
0012470
Arg of perigee: 104
0309 deg
Mean anomaly: 256
2234 deg
Mean motion: 15
60504697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 297
Coasting Arc #5 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2011/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 457821
80 A = 6759018
61 meter
Y = 4203782
16 meter E =
0026757
Z = -5295631
16 I = 51
60789
XDOT = -7640
885134 Wp = 95
95420
YDOT = 250
017464 meter/sec RA = 180
89932 deg
ZDOT = -466
847089 TA = 169
61327
MA = 169
55788
Ha = 215
531 n
mi
Hp = 200
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1502040
04 X = 436505
19
Y = 13791936
21 feet Y = 4208782
75 meter
Z = -17374117
96 Z = -5293458
75
XDOT = -25068
520781 XDOT = -7640
845156
YDOT = 820
267269 feet/sec YDOT = 164
572658 meter/sec
ZDOT = -1531
650553 ZDOT = -503
965984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5360664
27 X = 1633930
47
Y = -12807773
02 feet Y = -3903809
22 meter
Z = -17365420
60 Z = -5292980
20
XDOT = 21309
045845 XDOT = 6494
997173
YDOT = 11179
184552 feet/sec YDOT = 3407
415452 meter/sec
ZDOT = -1682
657022 ZDOT = -512
873860
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 11235
51693214
00016717 00000-0 10270-3 0 9044
2 25544 51
6367 181
8727 0012410 106
9064 253
3453 15
60481042 11422
Satellite: ISS
Catalog Number: 25544
Epoch time: 11235
51693214 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 181
8727 deg
Eccentricity:
0012410
Arg of perigee: 106
9064 deg
Mean anomaly: 253
3453 deg
Mean motion: 15
60481042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 280
Coasting Arc #6 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2011/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3825790
01 A = 6763118
82 meter
Y = -3624843
86 meter E =
0021252
Z = 4219023
52 I = 51
65291
XDOT = 6326
517929 Wp = 94
40573
YDOT = 2425
714736 meter/sec RA = 175
83796 deg
ZDOT = -3638
634699 TA = 32
76359
MA = 32
63198
Ha = 215
390 n
mi
Hp = 200
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12551804
49 X = 3845544
43
Y = -11892532
34 feet Y = -3581951
19 meter
Z = 13841940
69 Z = 4237656
82
XDOT = 20756
292419 XDOT = 6316
598478
YDOT = 7958
381679 feet/sec YDOT = 2496
406354 meter/sec
ZDOT = -11937
777885 ZDOT = -3607
924965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16621396
22 X = -5066201
57
Y = 4538888
99 feet Y = 1383453
36 meter
Z = 13917870
45 Z = 4242166
91
XDOT = -14213
805323 XDOT = -4332
367862
YDOT = -15686
891361 feet/sec YDOT = -4781
364487 meter/sec
ZDOT = -11812
915832 ZDOT = -3600
576745
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 11236
54155931
00016717 00000-0 10270-3 0 9058
2 25544 51
6371 176
7156 0012407 110
5613 249
6875 15
60510935 11580
Satellite: ISS
Catalog Number: 25544
Epoch time: 11236
54155931 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 176
7156 deg
Eccentricity:
0012407
Arg of perigee: 110
5613 deg
Mean anomaly: 249
6875 deg
Mean motion: 15
60510935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 302
Coasting Arc #7 (Orbit 1172)
---------------------------------------
Vector Time (GMT): 2011/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6415255
38 A = 6770293
40 meter
Y = 1887089
28 meter E =
0017321
Z = -1063398
42 I = 51
70700
XDOT = -2246
011919 Wp = 82
36582
YDOT = -4357
288068 meter/sec RA = 170
82137 deg
ZDOT = 5901
767913 TA = 266
09128
MA = 266
28932
Ha = 215
389 n
mi
Hp = 200
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21047425
80 X = -6430714
69
Y = 6191237
81 feet Y = 1815263
56 meter
Z = -3488839
95 Z = -1094600
67
XDOT = -7368
805507 XDOT = -2225
790134
YDOT = -14295
564527 feet/sec YDOT = -4382
291370 meter/sec
ZDOT = 19362
755621 ZDOT = 5890
906040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21517420
04 X = 6558509
63
Y = 4174172
79 feet Y = 1272287
87 meter
Z = -3615864
93 Z = -1102115
63
XDOT = 375
682328 XDOT = 114
507973
YDOT = 14566
644876 feet/sec YDOT = 4439
913358 meter/sec
ZDOT = 19318
701415 ZDOT = 5888
340191
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 11237
50213744
00016717 00000-0 10270-3 0 9063
2 25544 51
6370 171
8804 0012358 114
0418 246
2033 15
60517003 11731
Satellite: ISS
Catalog Number: 25544
Epoch time: 11237
50213744 = yrday
fracday
Element set: 906
Inclination: 51
6370 deg
RA of node: 171
8804 deg
Eccentricity:
0012358
Arg of perigee: 114
0418 deg
Mean anomaly: 246
2033 deg
Mean motion: 15
60517003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1173
Checksum: 268
Coasting Arc #8 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2011/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6173003
78 A = 6767702
95 meter
Y = 637704
34 meter E =
0017274
Z = -2699937
79 I = 51
72949
XDOT = -2766
294477 Wp = 120
25910
YDOT = 4925
527923 meter/sec RA = 165
82434 deg
ZDOT = -5194
576103 TA = 90
28125
MA = 90
08331
Ha = 215
383 n
mi
Hp = 200
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20252637
08 X = 6178529
58
Y = 2092205
83 feet Y = 706765
52 meter
Z = -8858063
62 Z = -2669936
56
XDOT = -9075
769280 XDOT = -2795
933321
YDOT = 16159
868513 feet/sec YDOT = 4894
427783 meter/sec
ZDOT = -17042
572518 ZDOT = -5208
086490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17257950
95 X = -5260223
45
Y = -10902177
56 feet Y = -3322983
72 meter
Z = -8735993
27 Z = -2662730
75
XDOT = 14427
008090 XDOT = 4397
352066
YDOT = -9225
752727 feet/sec YDOT = -2812
009431 meter/sec
ZDOT = -17097
712923 ZDOT = -5211
382899
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 11238
52674373
00016717 00000-0 10270-3 0 9076
2 25544 51
6384 166
7221 0012353 117
7526 242
4884 15
60545507 11896
Satellite: ISS
Catalog Number: 25544
Epoch time: 11238
52674373 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 166
7221 deg
Eccentricity:
0012353
Arg of perigee: 117
7526 deg
Mean anomaly: 242
4884 deg
Mean motion: 15
60545507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 316
Coasting Arc #9 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2011/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3289837
74 A = 6759815
26 meter
Y = -3062781
71 meter E =
0017967
Z = 5038714
74 I = 51
73271
XDOT = 6418
200566 Wp = 123
18763
YDOT = -3796
778311 meter/sec RA = 160
79095 deg
ZDOT = 1868
220786 TA = 308
70149
MA = 308
86203
Ha = 215
298 n
mi
Hp = 200
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10793430
90 X = -3279821
23
Y = -10048496
43 feet Y = -3099514
52 meter
Z = 16531216
34 Z = 5022757
49
XDOT = 21057
088471 XDOT = 6451
104591
YDOT = -12456
621755 feet/sec YDOT = -3724
822035 meter/sec
ZDOT = 6129
333287 ZDOT = 1899
479749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5526656
50 X = 1684524
90
Y = 13750139
14 feet Y = 4191042
41 meter
Z = 16466368
34 Z = 5018949
07
XDOT = -23328
740211 XDOT = -7110
600016
YDOT = 1827
080083 feet/sec YDOT = 556
894009 meter/sec
ZDOT = 6256
677286 ZDOT = 1907
035237
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 11239
55133808
00016717 00000-0 10270-3 0 9084
2 25544 51
6385 161
5651 0012283 122
2651 237
9697 15
60586612 12051
Satellite: ISS
Catalog Number: 25544
Epoch time: 11239
55133808 = yrday
fracday
Element set: 908
Inclination: 51
6385 deg
RA of node: 161
5651 deg
Eccentricity:
0012283
Arg of perigee: 122
2651 deg
Mean anomaly: 237
9697 deg
Mean motion: 15
60586612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 309
Coasting Arc #10 (Orbit 1219)
---------------------------------------
Vector Time (GMT): 2011/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -915829
66 A = 6760559
67 meter
Y = 4622337
74 meter E =
0023928
Z = -4870228
87 I = 51
76418
XDOT = -7175
844555 Wp = 116
65935
YDOT = 1137
224775 meter/sec RA = 155
73117 deg
ZDOT = 2427
458442 TA = 177
14111
MA = 177
12741
Ha = 215
177 n
mi
Hp = 200
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3004690
48 X = -943791
27
Y = 15165150
05 feet Y = 4611939
74 meter
Z = -15978441
19 Z = -4874746
07
XDOT = -23542
797097 XDOT = -7199
819810
YDOT = 3731
052413 feet/sec YDOT = 1056
846186 meter/sec
ZDOT = 7964
102499 ZDOT = 2392
540616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8919368
15 X = 2718623
41
Y = -12604056
95 feet Y = -3841716
56 meter
Z = -15996972
96 Z = -4875877
36
XDOT = 22102
545071 XDOT = 6736
855738
YDOT = 5708
204514 feet/sec YDOT = 1739
860736 meter/sec
ZDOT = 7821
939655 ZDOT = 2384
127207
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 11240
51188775
00016717 00000-0 10270-3 0 9096
2 25544 51
6393 156
7293 0012263 125
0986 235
1321 15
60569771 12206
Satellite: ISS
Catalog Number: 25544
Epoch time: 11240
51188775 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 156
7293 deg
Eccentricity:
0012263
Arg of perigee: 125
0986 deg
Mean anomaly: 235
1321 deg
Mean motion: 15
60569771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1220
Checksum: 306
Coasting Arc #11 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2011/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4534742
59 A = 6768582
76 meter
Y = -4507630
77 meter E =
0025840
Z = 2177685
99 I = 51
81833
XDOT = 4879
833990 Wp = 118
64769
YDOT = 2229
818273 meter/sec RA = 150
70743 deg
ZDOT = -5508
934162 TA = 37
13813
MA = 36
95964
Ha = 215
108 n
mi
Hp = 200
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14877764
41 X = 4574232
14
Y = -14788814
86 feet Y = -4456699
54 meter
Z = 7144639
08 Z = 2199811
67
XDOT = 16009
954037 XDOT = 4881
298006
YDOT = 7315
676748 feet/sec YDOT = 2284
395314 meter/sec
ZDOT = -18073
930977 ZDOT = -5485
224947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19493348
49 X = -5941572
62
Y = 7666104
87 feet Y = 2336628
76 meter
Z = 7234845
36 Z = 2205180
87
XDOT = -11318
953851 XDOT = -3450
017134
YDOT = -11702
100645 feet/sec YDOT = -3566
800276 meter/sec
ZDOT = -17977
489902 ZDOT = -5479
538922
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 11241
53646272
00016717 00000-0 10270-3 0 9102
2 25544 51
6393 151
5717 0012314 129
1262 231
0991 15
60574727 12361
Satellite: ISS
Catalog Number: 25544
Epoch time: 11241
53646272 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 151
5717 deg
Eccentricity:
0012314
Arg of perigee: 129
1262 deg
Mean anomaly: 231
0991 deg
Mean motion: 15
60574727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 287
Coasting Arc #12 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2011/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6038003
67 A = 6769583
30 meter
Y = 2613665
59 meter E =
0021436
Z = 1580011
81 I = 51
84768
XDOT = -652
723167 Wp = 95
02239
YDOT = -5032
065483 meter/sec RA = 145
71958 deg
ZDOT = 5760
859147 TA = 282
25158
MA = 282
49154
Ha = 215
033 n
mi
Hp = 200
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19809723
34 X = -6074456
76
Y = 8575018
33 feet Y = 2545941
25 meter
Z = 5183765
78 Z = 1550590
76
XDOT = -2141
480208 XDOT = -624
390014
YDOT = -16509
401191 feet/sec YDOT = -5039
205724 meter/sec
ZDOT = 18900
456518 ZDOT = 5757
757502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21611677
64 X = 6587239
34
Y = -345924
68 feet Y = -105437
84 meter
Z = 5063914
62 Z = 1543481
18
XDOT = -4247
121905 XDOT = -1294
522757
YDOT = 14542
145208 feet/sec YDOT = 4432
445859 meter/sec
ZDOT = 18887
990048 ZDOT = 5757
059367
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 11242
56102620
00016717 00000-0 10270-3 0 9111
2 25544 51
6394 146
4140 0012185 132
6392 227
5793 15
60595079 12525
Satellite: ISS
Catalog Number: 25544
Epoch time: 11242
56102620 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 146
4140 deg
Eccentricity:
0012185
Arg of perigee: 132
6392 deg
Mean anomaly: 227
5793 deg
Mean motion: 15
60595079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 290
Coasting Arc #13 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2011/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4935204
75 A = 6761594
62 meter
Y = 623343
99 meter E =
0018550
Z = -4592310
27 I = 51
84616
XDOT = -3594
099248 Wp = 106
90066
YDOT = 6044
618700 meter/sec RA = 140
70716 deg
ZDOT = -3057
413215 TA = 132
71109
MA = 132
55475
Ha = 214
906 n
mi
Hp = 200
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16191616
63 X = 4950176
08
Y = 2045091
83 feet Y = 678615
82 meter
Z = -15066634
74 Z = -4568298
88
XDOT = -11791
664201 XDOT = -3646
571962
YDOT = 19831
426180 feet/sec YDOT = 6004
133656 meter/sec
ZDOT = -10030
883252 ZDOT = -3075
001166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14403761
27 X = -4390266
44
Y = -7862436
81 feet Y = -2396470
74 meter
Z = -14968903
79 Z = -4562521
87
XDOT = 17602
488369 XDOT = 5365
238455
YDOT = -13110
260478 feet/sec YDOT = -3996
007394 meter/sec
ZDOT = -10102
682418 ZDOT = -3079
297601
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 11243
52154354
00016717 00000-0 10270-3 0 9120
2 25544 51
6398 141
5781 0012115 136
3689 223
8427 15
60636712 12678
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52154354 = yrday
fracday
Element set: 912
Inclination: 51
6398 deg
RA of node: 141
5781 deg
Eccentricity:
0012115
Arg of perigee: 136
3689 deg
Mean anomaly: 223
8427 deg
Mean motion: 15
60636712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 302
Coasting Arc #14 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2011/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1905966
44 A = 6758768
78 meter
Y = -3852652
45 meter E =
0012961
Z = 5205339
34 I = 51
85944
XDOT = 6045
825567 Wp = 123
34797
YDOT = -4597
765593 meter/sec RA = 135
65639 deg
ZDOT = -1194
083432 TA = 338
01274
MA = 338
06830
Ha = 214
766 n
mi
Hp = 201
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6253170
74 X = -1888030
21
Y = -12639935
87 feet Y = -3873865
53 meter
Z = 17077884
96 Z = 5196123
98
XDOT = 19835
385718 XDOT = 6102
589965
YDOT = -15084
532786 feet/sec YDOT = -4529
840162 meter/sec
ZDOT = -3917
596561 ZDOT = -1164
574732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1530533
58 X = 466506
63
Y = 14064251
17 feet Y = 4286783
76 meter
Z = 17040498
34 Z = 5193943
89
XDOT = -22856
484202 XDOT = -6966
656385
YDOT = 7068
967293 feet/sec YDOT = 2154
621231 meter/sec
ZDOT = -3797
301203 ZDOT = -1157
417407
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 11244
54608440
00016717 00000-0 10270-3 0 9134
2 25544 51
6392 136
4201 0011984 140
7310 219
4718 15
60679579 12835
Satellite: ISS
Catalog Number: 25544
Epoch time: 11244
54608440 = yrday
fracday
Element set: 913
Inclination: 51
6392 deg
RA of node: 136
4201 deg
Eccentricity:
0011984
Arg of perigee: 140
7310 deg
Mean anomaly: 219
4718 deg
Mean motion: 15
60679579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 303
Coasting Arc #15 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2011/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1650428
64 A = 6766071
29 meter
Y = 5751461
14 meter E =
0014514
Z = -3178768
20 I = 51
90482
XDOT = -5855
952671 Wp = 127
80475
YDOT = 993
491789 meter/sec RA = 130
62381 deg
ZDOT = 4844
379906 TA = 195
60131
MA = 195
64609
Ha = 214
637 n
mi
Hp = 201
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5414792
13 X = -1699178
08
Y = 18869623
18 feet Y = 5732732
35 meter
Z = -10429029
54 Z = -3186904
61
XDOT = -19212
443147 XDOT = -5890
159949
YDOT = 3259
487498 feet/sec YDOT = 927
815874 meter/sec
ZDOT = 15893
634863 ZDOT = 4815
848604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11343668
88 X = 3457550
27
Y = -16000232
12 feet Y = -4876870
75 meter
Z = -10462363
91 Z = -3188928
52
XDOT = 18121
891710 XDOT = 5523
552593
YDOT = 2544
838470 feet/sec YDOT = 775
666766 meter/sec
ZDOT = 15777
431834 ZDOT = 4808
961223
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 11245
50658351
00016717 00000-0 10270-3 0 9148
2 25544 51
6393 131
5839 0011969 144
0353 216
1610 15
60659173 12985
Satellite: ISS
Catalog Number: 25544
Epoch time: 11245
50658351 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 131
5839 deg
Eccentricity:
0011969
Arg of perigee: 144
0353 deg
Mean anomaly: 216
1610 deg
Mean motion: 15
60659173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 307
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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