[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 26th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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 3714)
---------------------------------------
Vector Time (GMT): 2011/144/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1768925
02 A = 6728027
26 meter
Y = -6472366
78 meter E =
0013153
Z = 372490
16 I = 51
33366
XDOT = 4562
501830 Wp = 30
09088
YDOT = 1596
955230 meter/sec RA = 282
73984 deg
ZDOT = 6001
530631 TA = 333
98002
MA = 334
04608
Ha = 187
193 n
mi
Hp = 182
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5803559
77 X = 1839359
31
Y = -21234799
14 feet Y = -6452191
79 meter
Z = 1222080
59 Z = 381254
19
XDOT = 14968
838024 XDOT = 4515
150977
YDOT = 5239
354429 feet/sec YDOT = 1647
710701 meter/sec
ZDOT = 19690
061125 ZDOT = 6023
580328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13431799
09 X = 4094012
36
Y = -17438351
09 feet Y = -5315209
41 meter
Z = 1257841
85 Z = 383390
20
XDOT = 10472
829882 XDOT = 3192
118548
YDOT = 9511
755420 feet/sec YDOT = 2899
183052 meter/sec
ZDOT = 19779
221253 ZDOT = 6028
706638
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 11144
33196906
00016717 00000-0 10270-3 0 9005
2 25544 51
6481 283
1376 0004275 312
4040 47
6762 15
75438903 37152
Satellite: ISS
Catalog Number: 25544
Epoch time: 11144
33196906 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 283
1376 deg
Eccentricity:
0004275
Arg of perigee: 312
4040 deg
Mean anomaly: 47
6762 deg
Mean motion: 15
75438903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 301
Coasting Arc #2 (Orbit 3729)
---------------------------------------
Vector Time (GMT): 2011/145/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3963762
14 A = 6716199
45 meter
Y = -1652370
67 meter E =
0011474
Z = -5173516
46 I = 51
28741
XDOT = 1791
779246 Wp = 83
82658
YDOT = -7416
830148 meter/sec RA = 277
55666 deg
ZDOT = 999
181523 TA = 195
73427
MA = 195
76996
Ha = 187
246 n
mi
Hp = 182
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13004468
97 X = -3919858
39
Y = -5421163
62 feet Y = -1696450
06 meter
Z = -16973479
21 Z = -5192665
90
XDOT = 5878
540832 XDOT = 1869
728648
YDOT = -24333
432243 feet/sec YDOT = -7396
357609 meter/sec
ZDOT = 3278
154603 ZDOT = 1008
074861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10042695
98 X = -3061013
73
Y = -9747573
23 feet Y = -2971060
32 meter
Z = -17050903
16 Z = -5197115
28
XDOT = 13605
572284 XDOT = 4146
978432
YDOT = -19797
533702 feet/sec YDOT = -6034
288272 meter/sec
ZDOT = 3314
472919 ZDOT = 1010
251346
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 11145
28343825
00016717 00000-0 10270-3 0 9015
2 25544 51
6470 278
2408 0004377 316
7848 43
2972 15
75486486 37308
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
28343825 = yrday
fracday
Element set: 901
Inclination: 51
6470 deg
RA of node: 278
2408 deg
Eccentricity:
0004377
Arg of perigee: 316
7848 deg
Mean anomaly: 43
2972 deg
Mean motion: 15
75486486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3730
Checksum: 327
Coasting Arc #3 (Orbit 3745)
---------------------------------------
Vector Time (GMT): 2011/146/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1381371
21 A = 6727056
10 meter
Y = 6434145
56 meter E =
0004259
Z = -1386246
85 I = 51
32100
XDOT = -4552
214073 Wp = 146
10066
YDOT = -2223
944050 meter/sec RA = 272
40853 deg
ZDOT = -5798
083179 TA = 49
20944
MA = 49
17250
Ha = 187
354 n
mi
Hp = 182
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4532057
77 X = -1446482
23
Y = 21109401
44 feet Y = 6418334
26 meter
Z = -4548053
98 Z = -1393115
34
XDOT = -14935
085540 XDOT = -4498
841006
YDOT = -7296
404365 feet/sec YDOT = -2274
550888 meter/sec
ZDOT = -19022
582608 ZDOT = -5820
068428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11569627
77 X = -3526422
54
Y = 18221798
46 feet Y = 5554004
17 meter
Z = -4576127
82 Z = -1394803
76
XDOT = -10025
831832 XDOT = -3055
873542
YDOT = -11155
427835 feet/sec YDOT = -3400
174404 meter/sec
ZDOT = -19111
461266 ZDOT = -5825
173394
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 11146
29830572
00016717 00000-0 10270-3 0 9028
2 25544 51
6467 273
0187 0004428 319
7156 40
3679 15
75501474 37467
Satellite: ISS
Catalog Number: 25544
Epoch time: 11146
29830572 = yrday
fracday
Element set: 902
Inclination: 51
6467 deg
RA of node: 273
0187 deg
Eccentricity:
0004428
Arg of perigee: 319
7156 deg
Mean anomaly: 40
3679 deg
Mean motion: 15
75501474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3746
Checksum: 319
Coasting Arc #4 (Orbit 3761)
---------------------------------------
Vector Time (GMT): 2011/147/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030852
53 A = 6717167
33 meter
Y = 2233218
24 meter E =
0007614
Z = 4887340
46 I = 51
28804
XDOT = -1384
923271 Wp = 20
47444
YDOT = 7261
067211 meter/sec RA = 267
20530 deg
ZDOT = -2167
586055 TA = 90
70710
MA = 90
61985
Ha = 187
281 n
mi
Hp = 182
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13224581
78 X = 3981838
66
Y = 7326831
49 feet Y = 2278019
30 meter
Z = 16034581
56 Z = 4906803
59
XDOT = -4543
711520 XDOT = -1455
485164
YDOT = 23822
398986 feet/sec YDOT = 7245
185772 meter/sec
ZDOT = -7111
502805 ZDOT = -2174
484969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9952610
17 X = 3033555
58
Y = 11268910
96 feet Y = 3434764
06 meter
Z = 16113256
20 Z = 4911320
49
XDOT = -11329
489389 XDOT = -3453
228366
YDOT = 20252
740728 feet/sec YDOT = 6173
035374 meter/sec
ZDOT = -7139
729707 ZDOT = -2176
189615
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 11147
31313786
00016717 00000-0 10270-3 0 9036
2 25544 51
6465 267
7947 0004543 323
9682 36
1175 15
75579975 37621
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
31313786 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 267
7947 deg
Eccentricity:
0004543
Arg of perigee: 323
9682 deg
Mean anomaly: 36
1175 deg
Mean motion: 15
75579975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3762
Checksum: 341
Coasting Arc #5 (Orbit 3777)
---------------------------------------
Vector Time (GMT): 2011/148/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1068553
73 A = 6724992
53 meter
Y = -6186787
02 meter E =
0013336
Z = 2387658
69 I = 51
31665
XDOT = 4731
468386 Wp = 55
10085
YDOT = 2889
132527 meter/sec RA = 262
07141 deg
ZDOT = 5355
132151 TA = 331
98739
MA = 332
05910
Ha = 187
304 n
mi
Hp = 182
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3505753
71 X = 1126057
21
Y = -20297857
68 feet Y = -6174516
47 meter
Z = 7833525
88 Z = 2392988
97
XDOT = 15523
190242 XDOT = 4672
795346
YDOT = 9478
781257 feet/sec YDOT = 2941
714196 meter/sec
ZDOT = 17569
331205 ZDOT = 5377
975589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9687305
26 X = 2952690
64
Y = -18168845
96 feet Y = -5537864
25 meter
Z = 7855355
92 Z = 2394312
49
XDOT = 10313
343543 XDOT = 3143
507112
YDOT = 13154
154914 feet/sec YDOT = 4009
386418 meter/sec
ZDOT = 17661
662721 ZDOT = 5383
274797
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 11148
32793629
00016717 00000-0 10270-3 0 9047
2 25544 51
6454 262
5703 0004545 327
2550 32
8331 15
75649254 37787
Satellite: ISS
Catalog Number: 25544
Epoch time: 11148
32793629 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 262
5703 deg
Eccentricity:
0004545
Arg of perigee: 327
2550 deg
Mean anomaly: 32
8331 deg
Mean motion: 15
75649254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3778
Checksum: 318
Coasting Arc #6 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2011/149/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4260441
74 A = 6718925
09 meter
Y = -2794149
37 meter E =
0006740
Z = -4385485
31 I = 51
30128
XDOT = 1111
191034 Wp = 84
10218
YDOT = -6865
766235 meter/sec RA = 256
85347 deg
ZDOT = 3299
945687 TA = 219
18919
MA = 219
23801
Ha = 187
396 n
mi
Hp = 181
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13977827
21 X = -4207576
20
Y = -9167156
71 feet Y = -2841496
21 meter
Z = -14388075
16 Z = -4406054
66
XDOT = 3645
639875 XDOT = 1171
852017
YDOT = -22525
479774 feet/sec YDOT = -6853
001363 meter/sec
ZDOT = 10826
593460 ZDOT = 3305
490617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10511875
92 X = -3204019
78
Y = -12904170
73 feet Y = -3933191
24 meter
Z = -14471211
59 Z = -4410825
29
XDOT = 9215
172686 XDOT = 2808
784635
YDOT = -19655
209186 feet/sec YDOT = -5990
907760 meter/sec
ZDOT = 10849
318583 ZDOT = 3306
872304
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 11149
27928080
00016717 00000-0 10270-3 0 9054
2 25544 51
6447 257
6723 0004528 332
7162 27
3764 15
75679896 37938
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
27928080 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 257
6723 deg
Eccentricity:
0004528
Arg of perigee: 332
7162 deg
Mean anomaly: 27
3764 deg
Mean motion: 15
75679896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 346
Coasting Arc #7 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2011/150/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -933836
14 A = 6722292
44 meter
Y = 5751270
05 meter E =
0005259
Z = -3359689
18 I = 51
32119
XDOT = -5053
644786 Wp = 36
33027
YDOT = -3517
990333 meter/sec RA = 251
73198 deg
ZDOT = -4617
092737 TA = 183
45177
MA = 183
45540
Ha = 187
541 n
mi
Hp = 181
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3063766
85 X = -981757
55
Y = 18868996
22 feet Y = 5740559
77 meter
Z = -11022602
31 Z = -3364341
57
XDOT = -16580
199430 XDOT = -4991
501030
YDOT = -11541
963035 feet/sec YDOT = -3574
155265 meter/sec
ZDOT = -15147
942052 ZDOT = -4641
493140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8210267
84 X = -2502489
64
Y = 17250985
54 feet Y = 5258100
39 meter
Z = -11041668
68 Z = -3365500
61
XDOT = -11294
612925 XDOT = -3442
598019
YDOT = -15135
188709 feet/sec YDOT = -4613
205518 meter/sec
ZDOT = -15246
560896 ZDOT = -4647
151761
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 11150
29401467
00016717 00000-0 10270-3 0 9064
2 25544 51
6447 252
4490 0004645 338
1537 21
9428 15
75741865 38099
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
29401467 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 252
4490 deg
Eccentricity:
0004645
Arg of perigee: 338
1537 deg
Mean anomaly: 21
9428 deg
Mean motion: 15
75741865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 317
Coasting Arc #8 (Orbit 3824)
---------------------------------------
Vector Time (GMT): 2011/151/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4594004
96 A = 6721339
11 meter
Y = 3313874
31 meter E =
0011605
Z = 3613922
26 I = 51
32925
XDOT = -1078
619877 Wp = 62
63534
YDOT = 6262
008856 meter/sec RA = 246
50819 deg
ZDOT = -4355
007093 TA = 73
82205
MA = 73
69437
Ha = 187
480 n
mi
Hp = 181
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15072194
74 X = 4539051
13
Y = 10872291
03 feet Y = 3364939
51 meter
Z = 11856700
33 Z = 3636107
19
XDOT = -3538
779123 XDOT = -1127
406585
YDOT = 20544
648478 feet/sec YDOT = 6249
674879 meter/sec
ZDOT = -14288
081015 ZDOT = -4360
364759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11565129
43 X = 3525051
45
Y = 14473810
28 feet Y = 4411617
37 meter
Z = 11946367
94 Z = 3641252
95
XDOT = -7741
872391 XDOT = -2359
722705
YDOT = 18040
121291 feet/sec YDOT = 5498
628969 meter/sec
ZDOT = -14310
023206 ZDOT = -4361
695073
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 11151
30871472
00016717 00000-0 10270-3 0 9075
2 25544 51
6447 247
2244 0004651 339
8154 20
2825 15
75780009 38252
Satellite: ISS
Catalog Number: 25544
Epoch time: 11151
30871472 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 247
2244 deg
Eccentricity:
0004651
Arg of perigee: 339
8154 deg
Mean anomaly: 20
2825 deg
Mean motion: 15
75780009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3825
Checksum: 301
Coasting Arc #9 (Orbit 3840)
---------------------------------------
Vector Time (GMT): 2011/152/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1013852
13 A = 6719233
94 meter
Y = -5145652
19 meter E =
0008635
Z = 4191986
05 I = 51
33539
XDOT = 5489
795046 Wp = 79
65472
YDOT = 4028
346500 meter/sec RA = 241
38808 deg
ZDOT = 3612
288789 TA = 333
43965
MA = 333
48387
Ha = 187
475 n
mi
Hp = 181
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3326286
52 X = 1050952
32
Y = -16882061
00 feet Y = -5134107
89 meter
Z = 13753235
07 Z = 4197000
73
XDOT = 18011
138604 XDOT = 5426
793252
YDOT = 13216
359909 feet/sec YDOT = 4089
383907 meter/sec
ZDOT = 11851
341171 ZDOT = 3638
806088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7354414
85 X = 2241625
65
Y = -15537573
75 feet Y = -4735852
48 meter
Z = 13773744
03 Z = 4198237
18
XDOT = 12940
236246 XDOT = 3944
184008
YDOT = 16739
838507 feet/sec YDOT = 5102
302777 meter/sec
ZDOT = 11958
528044 ZDOT = 3644
959348
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 11152
32338218
00016717 00000-0 10270-3 0 9085
2 25544 51
6441 241
9997 0004600 344
3591 15
7431 15
75845996 38419
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
32338218 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 241
9997 deg
Eccentricity:
0004600
Arg of perigee: 344
3591 deg
Mean anomaly: 15
7431 deg
Mean motion: 15
75845996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3841
Checksum: 318
Coasting Arc #10 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2011/153/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4983636
45 A = 6723756
75 meter
Y = -3664292
94 meter E =
0008020
Z = -2627354
40 I = 51
36729
XDOT = 1316
203880 Wp = 24
37144
YDOT = -5517
685628 meter/sec RA = 236
16999 deg
ZDOT = 5211
584147 TA = 305
59828
MA = 305
67298
Ha = 187
546 n
mi
Hp = 180
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16350513
28 X = -4929527
92
Y = -12021958
45 feet Y = -3719720
01 meter
Z = -8619929
13 Z = -2651434
26
XDOT = 4318
254201 XDOT = 1352
488766
YDOT = -18102
643135 feet/sec YDOT = -5502
765020 meter/sec
ZDOT = 17098
373186 ZDOT = 5218
065536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13050455
75 X = -3977778
91
Y = -15487564
51 feet Y = -4720609
66 meter
Z = -8717275
85 Z = -2657025
68
XDOT = 7186
066902 XDOT = 2190
313192
YDOT = -15670
646426 feet/sec YDOT = -4776
413031 meter/sec
ZDOT = 17124
835334 ZDOT = 5219
649810
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 11153
27460394
00016717 00000-0 10270-3 0 9092
2 25544 51
6445 237
1017 0004534 350
3323 9
7753 15
75877168 38561
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
27460394 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 237
1017 deg
Eccentricity:
0004534
Arg of perigee: 350
3323 deg
Mean anomaly: 9
7753 deg
Mean motion: 15
75877168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 317
Coasting Arc #11 (Orbit 3871)
---------------------------------------
Vector Time (GMT): 2011/154/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1369126
38 A = 6716416
40 meter
Y = 4462686
00 meter E =
0013929
Z = -4841772
69 I = 51
36116
XDOT = -5906
962607 Wp = 54
29619
YDOT = -4343
518727 meter/sec RA = 231
04302 deg
ZDOT = -2329
787491 TA = 192
87428
MA = 192
90988
Ha = 187
674 n
mi
Hp = 180
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4491884
43 X = -1395406
71
Y = 14641358
28 feet Y = 4447229
48 meter
Z = -15885081
00 Z = -4848487
00
XDOT = -19379
798581 XDOT = -5846
635806
YDOT = -14250
389523 feet/sec YDOT = -4409
236266 meter/sec
ZDOT = -7643
659746 ZDOT = -2358
337810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7456836
42 X = -2272843
74
Y = 13344358
27 feet Y = 4067360
40 meter
Z = -15912444
48 Z = -4850113
08
XDOT = -14823
579040 XDOT = -4518
226891
YDOT = -17548
710530 feet/sec YDOT = -5348
846969 meter/sec
ZDOT = -7759
096203 ZDOT = -2364
972523
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 11154
28920784
00016717 00000-0 10270-3 0 9100
2 25544 51
6445 231
8780 0004615 356
0433 4
0694 15
75945875 38725
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
28920784 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 231
8780 deg
Eccentricity:
0004615
Arg of perigee: 356
0433 deg
Mean anomaly: 4
0694 deg
Mean motion: 15
75945875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3872
Checksum: 319
Coasting Arc #12 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2011/155/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5313223
65 A = 6725626
18 meter
Y = 3874396
83 meter E =
0012242
Z = 1394442
25 I = 51
41200
XDOT = -1892
220121 Wp = 100
39950
YDOT = 4698
238575 meter/sec RA = 225
84136 deg
ZDOT = -5803
044001 TA = 64
21029
MA = 64
08403
Ha = 187
645 n
mi
Hp = 180
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17431836
11 X = 5262730
56
Y = 12711275
69 feet Y = 3933529
97 meter
Z = 4574941
76 Z = 1420131
86
XDOT = -6208
071263 XDOT = -1916
425995
YDOT = 15414
168552 feet/sec YDOT = 4676
944240 meter/sec
ZDOT = -19038
858272 ZDOT = -5812
294414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14521507
34 X = 4426155
44
Y = 15925134
45 feet Y = 4853980
98 meter
Z = 4678829
90 Z = 1426107
35
XDOT = -7882
082793 XDOT = -2402
458835
YDOT = 12830
624638 feet/sec YDOT = 3910
774390 meter/sec
ZDOT = -19076
500728 ZDOT = -5814
517422
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 11155
30377828
00016717 00000-0 10270-3 0 9110
2 25544 51
6434 226
6520 0004694 357
4623 2
6517 15
75992865 38886
Satellite: ISS
Catalog Number: 25544
Epoch time: 11155
30377828 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 226
6520 deg
Eccentricity:
0004694
Arg of perigee: 357
4623 deg
Mean anomaly: 2
6517 deg
Mean motion: 15
75992865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 330
Coasting Arc #13 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2011/156/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1996322
12 A = 6714586
30 meter
Y = -3752993
64 meter E =
0004281
Z = 5194616
93 I = 51
39766
XDOT = 6223
564510 Wp = 46
33622
YDOT = 4468
532901 meter/sec RA = 220
69482 deg
ZDOT = 839
146816 TA = 35
66981
MA = 35
64121
Ha = 187
646 n
mi
Hp = 180
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6549613
24 X = 2012906
05
Y = -12312971
27 feet Y = -3730577
63 meter
Z = 17042706
47 Z = 5204354
73
XDOT = 20418
518733 XDOT = 6169
057560
YDOT = 14660
541015 feet/sec YDOT = 4537
823685 meter/sec
ZDOT = 2753
106352 ZDOT = 869
249041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8584989
99 X = 2616704
95
Y = -10929499
03 feet Y = -3331311
30 meter
Z = 17082287
23 Z = 5206681
15
XDOT = 16588
004248 XDOT = 5056
023695
YDOT = 17510
236036 feet/sec YDOT = 5337
119944 meter/sec
ZDOT = 2874
862152 ZDOT = 876
257984
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 11156
31831866
00016717 00000-0 10270-3 0 9120
2 25544 51
6438 221
4267 0004705 2
7603 357
3586 15
76021443 39043
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
31831866 = yrday
fracday
Element set: 912
Inclination: 51
6438 deg
RA of node: 221
4267 deg
Eccentricity:
0004705
Arg of perigee: 2
7603 deg
Mean anomaly: 357
3586 deg
Mean motion: 15
76021443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 297
Coasting Arc #14 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2011/157/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5487613
69 A = 6726263
44 meter
Y = -3874046
86 meter E =
0016060
Z = -44256
41 I = 51
46284
XDOT = 2743
101107 Wp = 34
87359
YDOT = -3942
093017 meter/sec RA = 215
52131 deg
ZDOT = 6029
194062 TA = 324
64382
MA = 324
75020
Ha = 187
682 n
mi
Hp = 180
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18003981
93 X = -5443670
51
Y = -12710127
48 feet Y = -3935166
98 meter
Z = -145198
18 Z = -70808
84
XDOT = 8999
675548 XDOT = 2757
689937
YDOT = -12933
376039 feet/sec YDOT = -3911
337232 meter/sec
ZDOT = 19780
820414 ZDOT = 6042
554869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15651382
39 X = -4770541
35
Y = -15513935
77 feet Y = -4728647
62 meter
Z = -252615
89 Z = -76997
32
XDOT = 9767
096631 XDOT = 2977
011053
YDOT = -10143
263909 feet/sec YDOT = -3091
666839 meter/sec
ZDOT = 19835
083816 ZDOT = 6045
733547
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 11157
26941956
00016717 00000-0 10270-3 0 9138
2 25544 51
6449 216
5283 0004636 7
2332 352
8899 15
76079727 39191
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
26941956 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 216
5283 deg
Eccentricity:
0004636
Arg of perigee: 7
2332 deg
Mean anomaly: 352
8899 deg
Mean motion: 15
76079727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 343
Coasting Arc #15 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2011/158/06:27:44
868
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2846005
47 A = 6714173
49 meter
Y = 3149515
79 meter E =
0015961
Z = -5215128
76 I = 51
44855
XDOT = -6270
687028 Wp = 79
00068
YDOT = -4388
975032 meter/sec RA = 210
35199 deg
ZDOT = 776
461368 TA = 198
38536
MA = 198
44311
Ha = 187
711 n
mi
Hp = 179
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9337288
27 X = -2855678
44
Y = 10333057
05 feet Y = 3117636
53 meter
Z = -17110002
50 Z = -5228977
71
XDOT = -20573
120170 XDOT = -6224
914496
YDOT = -14399
524384 feet/sec YDOT = -4458
841824 meter/sec
ZDOT = 2547
445434 ZDOT = 746
109244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10666281
55 X = -3251082
62
Y = 8846504
37 feet Y = 2696414
53 meter
Z = -17166216
95 Z = -5232262
92
XDOT = -17576
585900 XDOT = -5357
343382
YDOT = -16519
036077 feet/sec YDOT = -5035
002196 meter/sec
ZDOT = 2424
636721 ZDOT = 739
029273
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 11158
28389681
00016717 00000-0 10270-3 0 9143
2 25544 51
6449 211
3037 0004710 11
4003 348
7268 15
76144572 39359
Satellite: ISS
Catalog Number: 25544
Epoch time: 11158
28389681 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 211
3037 deg
Eccentricity:
0004710
Arg of perigee: 11
4003 deg
Mean anomaly: 348
7268 deg
Mean motion: 15
76144572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 306
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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