[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 26th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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
149/04:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 187
5
000/00:00:00
000 0
0 0
0 181
9
149/04:46:45
559 -0
1 0
6 0
6
N/A -0
6 0
0 187
5
000/00:01:27
118 0
0 0
1 182
0
149/05:03:57
905 0
5 1
1 1
1
N/A -0
6 -0
0 188
0
000/00:00:59
809 0
8 -0
0 182
5
149/05:21:25
465 0
2 0
3 0
3
N/A 0
2 -0
0 188
2
000/00:00:50
930 0
2 -0
0 182
5
149/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
2
000/00:00:00
000 0
0 0
0 182
5
Coasting Arc #1 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2011/145/13:24:24
806
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3170156
61 A = 6719292
40 meter
Y = 3910906
24 meter E =
0008330
Z = 4448549
33 I = 51
29757
XDOT = -3220
046451 Wp = 42
80304
YDOT = 6235
095024 meter/sec RA = 276
04314 deg
ZDOT = -3177
325179 TA = 79
14976
MA = 79
05603
Ha = 187
203 n
mi
Hp = 182
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10400776
29 X = 3104578
20
Y = 12831057
22 feet Y = 3945989
91 meter
Z = 14594978
10 Z = 4463790
93
XDOT = -10564
456861 XDOT = -3274
094259
YDOT = 20456
348504 feet/sec YDOT = 6198
784510 meter/sec
ZDOT = -10424
295208 ZDOT = -3193
099088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13977872
23 X = 4260455
46
Y = -8696664
77 feet Y = -2650743
42 meter
Z = 14656489
09 Z = 4467297
87
XDOT = 18411
752517 XDOT = 5611
902167
YDOT = 11864
119306 feet/sec YDOT = 3616
183565 meter/sec
ZDOT = -10488
404792 ZDOT = -3196
865781
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
60058255
00016717 00000-0 10270-3 0 9000
2 25544 51
6480 276
6062 0003782 315
4321 44
6538 15
75472072 37352
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
60058255 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 276
6062 deg
Eccentricity:
0003782
Arg of perigee: 315
4321 deg
Mean anomaly: 44
6538 deg
Mean motion: 15
75472072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 296
Coasting Arc #2 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2011/146/13:24:24
806
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2645743
41 A = 6723210
38 meter
Y = -5281749
77 meter E =
0010913
Z = 3197211
79 I = 51
30989
XDOT = 3740
364127 Wp = 70
76950
YDOT = 4764
105048 meter/sec RA = 270
92057 deg
ZDOT = 4765
360169 TA = 326
80656
MA = 326
87498
Ha = 187
121 n
mi
Hp = 182
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8680260
53 X = 2689076
75
Y = -17328575
35 feet Y = -5251921
37 meter
Z = 10489539
98 Z = 3210169
80
XDOT = 12271
535851 XDOT = 3663
663611
YDOT = 15630
265904 feet/sec YDOT = 4805
502914 meter/sec
ZDOT = 15634
383755 ZDOT = 4783
344952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16347802
07 X = -4982810
07
Y = -10357032
69 feet Y = -3156823
56 meter
Z = 10542207
38 Z = 3213264
81
XDOT = 16047
459235 XDOT = 4891
265575
YDOT = -9309
808282 feet/sec YDOT = -2837
629564 meter/sec
ZDOT = 15706
964767 ZDOT = 4787
482861
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
61543166
00016717 00000-0 10270-3 0 9013
2 25544 51
6483 271
3830 0003911 318
9859 41
1010 15
75570743 37517
Satellite: ISS
Catalog Number: 25544
Epoch time: 11146
61543166 = yrday
fracday
Element set: 901
Inclination: 51
6483 deg
RA of node: 271
3830 deg
Eccentricity:
0003911
Arg of perigee: 318
9859 deg
Mean anomaly: 41
1010 deg
Mean motion: 15
75570743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3751
Checksum: 294
Coasting Arc #3 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2011/147/13:24:24
806
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3386907
64 A = 6721232
43 meter
Y = -4385741
41 meter E =
0003998
Z = -3805657
00 I = 51
30428
XDOT = 2886
873044 Wp = 66
20482
YDOT = -5816
042465 meter/sec RA = 265
69879 deg
ZDOT = 4138
360212 TA = 247
29638
MA = 247
33865
Ha = 187
203 n
mi
Hp = 182
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11111901
70 X = -3319126
35
Y = -14388915
39 feet Y = -4423236
62 meter
Z = -12485751
30 Z = -3821946
41
XDOT = 9471
368253 XDOT = 2931
591004
YDOT = -19081
504151 feet/sec YDOT = -5783
509958 meter/sec
ZDOT = 13577
297282 ZDOT = 4152
492976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15284649
01 X = -4658761
02
Y = 9759548
24 feet Y = 2974710
30 meter
Z = -12551492
10 Z = -3825694
79
XDOT = -17491
775314 XDOT = -5331
493116
YDOT = -9880
053305 feet/sec YDOT = -3011
440247 meter/sec
ZDOT = 13634
738370 ZDOT = 4155
868255
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
56682187
00016717 00000-0 10270-3 0 9026
2 25544 51
6483 266
4874 0004111 323
0039 37
0842 15
75605451 37668
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
56682187 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 266
4874 deg
Eccentricity:
0004111
Arg of perigee: 323
0039 deg
Mean anomaly: 37
0842 deg
Mean motion: 15
75605451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 308
Coasting Arc #4 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2011/148/13:24:24
806
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2452436
45 A = 6720456
16 meter
Y = 4814697
88 meter E =
0007410
Z = -4004309
74 I = 51
30529
XDOT = -4029
331579 Wp = 38
70055
YDOT = -5283
267907 meter/sec RA = 260
57919 deg
ZDOT = -3882
897568 TA = 191
01674
MA = 191
03298
Ha = 187
320 n
mi
Hp = 181
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8046051
36 X = -2486640
62
Y = 15796252
87 feet Y = 4787082
33 meter
Z = -13137499
14 Z = -4016306
49
XDOT = -13219
591795 XDOT = -3951
090957
YDOT = -17333
556125 feet/sec YDOT = -5327
888548 meter/sec
ZDOT = -12739
165249 ZDOT = -3902
282684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15210274
65 X = 4636091
71
Y = 9034640
11 feet Y = 2753758
31 meter
Z = -13186252
47 Z = -4019169
75
XDOT = -17538
231117 XDOT = -5345
652844
YDOT = 10810
487260 feet/sec YDOT = 3295
036517 meter/sec
ZDOT = -12817
402211 ZDOT = -3906
744194
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
58160210
00016717 00000-0 10270-3 0 9038
2 25544 51
6481 261
2644 0004140 327
3618 32
7289 15
75649875 37829
Satellite: ISS
Catalog Number: 25544
Epoch time: 11148
58160210 = yrday
fracday
Element set: 903
Inclination: 51
6481 deg
RA of node: 261
2644 deg
Eccentricity:
0004140
Arg of perigee: 327
3618 deg
Mean anomaly: 32
7289 deg
Mean motion: 15
75649875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3782
Checksum: 311
Coasting Arc #5 (Orbit 3791)
---------------------------------------
Vector Time (GMT): 2011/149/04:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 1124139
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 24815
80 A = 6726093
69 meter
Y = 6493561
01 meter E =
0003070
Z = -1750718
54 I = 51
32775
XDOT = -4988
327494 Wp = 127
00080
YDOT = -1506
585295 meter/sec RA = 257
31968 deg
ZDOT = -5667
414638 TA = 72
47566
MA = 72
44212
Ha = 187
489 n
mi
Hp = 181
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 81416
67 X = -39293
51
Y = 21304334
03 feet Y = 6493480
23 meter
Z = -5743827
22 Z = -1750753
09
XDOT = -16365
903852 XDOT = -4943
578191
YDOT = -4942
865140 feet/sec YDOT = -1562
117063 meter/sec
ZDOT = -18593
880046 ZDOT = -5691
539693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15483233
21 X = -4719289
48
Y = 14633731
06 feet Y = 4460361
23 meter
Z = -5744234
78 Z = -1750842
76
XDOT = -6421
894999 XDOT = -1957
393596
YDOT = -14120
575680 feet/sec YDOT = -4303
951467 meter/sec
ZDOT = -18691
460199 ZDOT = -5697
157069
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
21582079
00016717 00000-0 10270-3 0 9041
2 25544 51
6478 258
0019 0004659 332
1911 27
9004 15
75668325 37923
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
21582079 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 258
0019 deg
Eccentricity:
0004659
Arg of perigee: 332
1911 deg
Mean anomaly: 27
9004 deg
Mean motion: 15
75668325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3792
Checksum: 318
Coasting Arc #6 (Orbit 3791)
---------------------------------------
Vector Time (GMT): 2011/149/04:47:29
118
Vector Time (MET): N/A
Weight (LBS) : 1124074
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4055551
40 A = 6715547
02 meter
Y = 1121784
32 meter E =
0013304
Z = -5244663
03 I = 51
29075
XDOT = -1835
122409 Wp = 69
75480
YDOT = -7470
423244 meter/sec RA = 257
24089 deg
ZDOT = -174
623268 TA = 198
55433
MA = 198
60289
Ha = 187
505 n
mi
Hp = 181
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13305614
83 X = -4042316
03
Y = 3680394
74 feet Y = 1076507
17 meter
Z = -17206899
72 Z = -5264332
91
XDOT = -6020
742812 XDOT = -1750
602010
YDOT = -24509
262610 feet/sec YDOT = -7490
472101 meter/sec
ZDOT = -572
910984 ZDOT = -183
333809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12214793
03 X = -3723068
91
Y = -6215776
52 feet Y = -1894568
68 meter
Z = -17286556
71 Z = -5268942
49
XDOT = 11685
627940 XDOT = 3561
779396
YDOT = -21235
272359 feet/sec YDOT = -6472
511015 meter/sec
ZDOT = -607
857606 ZDOT = -185
274998
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
21582016
00016717 00000-0 10270-3 0 9053
2 25544 51
6469 258
0008 0004963 328
7680 31
3189 15
75602148 37927
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
21582016 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 258
0008 deg
Eccentricity:
0004963
Arg of perigee: 328
7680 deg
Mean anomaly: 31
3189 deg
Mean motion: 15
75602148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3792
Checksum: 314
Coasting Arc #7 (Orbit 3791)
---------------------------------------
Vector Time (GMT): 2011/149/05:04:27
809
Vector Time (MET): N/A
Weight (LBS) : 1123944
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3073305
61 A = 6726135
37 meter
Y = -5556970
72 meter E =
0009546
Z = -2200447
61 I = 51
32428
XDOT = 3544
991289 Wp = 6
50651
YDOT = -4118
610272 meter/sec RA = 257
15837 deg
ZDOT = 5461
532460 TA = 328
69739
MA = 328
75419
Ha = 187
987 n
mi
Hp = 182
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10083023
66 X = -3000248
56
Y = -18231531
23 feet Y = -5590929
60 meter
Z = -7219316
29 Z = -2215200
99
XDOT = 11630
548849 XDOT = 3564
251427
YDOT = -13512
500893 feet/sec YDOT = -4078
860853 meter/sec
ZDOT = 17918
413584 ZDOT = 5478
800648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3416574
18 X = 1041371
81
Y = -20530969
93 feet Y = -6257839
64 meter
Z = -7278799
30 Z = -2218578
03
XDOT = 15919
250762 XDOT = 4852
187632
YDOT = -3714
825746 feet/sec YDOT = -1132
278887 meter/sec
ZDOT = 17988
473601 ZDOT = 5482
886754
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
21582004
00016717 00000-0 10270-3 0 9061
2 25544 51
6468 258
0008 0005892 328
6261 31
4551 15
75368812 37923
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
21582004 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 258
0008 deg
Eccentricity:
0005892
Arg of perigee: 328
6261 deg
Mean anomaly: 31
4551 deg
Mean motion: 15
75368812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3792
Checksum: 308
Coasting Arc #8 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2011/149/05:21:50
930
Vector Time (MET): N/A
Weight (LBS) : 1123907
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1752531
88 A = 6722666
33 meter
Y = -5374332
59 meter E =
0009966
Z = 3627046
64 I = 51
31179
XDOT = 4577
272684 Wp = 64
98464
YDOT = 4426
644301 meter/sec RA = 257
14175 deg
ZDOT = 4342
319690 TA = 338
79179
MA = 338
83308
Ha = 188
169 n
mi
Hp = 182
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5749776
52 X = 1794878
69
Y = -17632324
77 feet Y = -5354498
28 meter
Z = 11899759
30 Z = 3635662
90
XDOT = 15017
298833 XDOT = 4506
338424
YDOT = 14523
111224 feet/sec YDOT = 4477
433119 meter/sec
ZDOT = 14246
455677 ZDOT = 4364
384489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14553020
36 X = 4435760
60
Y = -11460014
87 feet Y = -3493012
53 meter
Z = 11934853
83 Z = 3637743
45
XDOT = 3446
627640 XDOT = 1050
532105
YDOT = 19323
933724 feet/sec YDOT = 5889
934999 meter/sec
ZDOT = 14335
577120 ZDOT = 4369
483906
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
27925674
00016717 00000-0 10270-3 0 9072
2 25544 51
6466 257
6741 0005970 331
3254 28
7581 15
75315031 37938
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
27925674 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 257
6741 deg
Eccentricity:
0005970
Arg of perigee: 331
3254 deg
Mean anomaly: 28
7581 deg
Mean motion: 15
75315031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 324
Coasting Arc #9 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2011/149/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 463690
62 A = 6727696
65 meter
Y = 6586059
62 meter E =
0003340
Z = -1287885
45 I = 51
32818
XDOT = -4968
560286 Wp = 127
69257
YDOT = -787
287616 meter/sec RA = 256
99107 deg
ZDOT = -5827
271524 TA = 66
50252
MA = 66
46742
Ha = 188
214 n
mi
Hp = 182
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1521294
67 X = 396265
96
Y = 21607807
16 feet Y = 6590868
02 meter
Z = -4225345
97 Z = -1285795
96
XDOT = -16301
050808 XDOT = -4931
079208
YDOT = -2582
964621 feet/sec YDOT = -842
638953 meter/sec
ZDOT = -19118
344894 ZDOT = -5851
318138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7505564
44 X = -2287696
04
Y = 20321104
21 feet Y = 6193872
56 meter
Z = -4217160
45 Z = -1285390
51
XDOT = -12196
585936 XDOT = -3717
519393
YDOT = -8484
133935 feet/sec YDOT = -2585
964023 meter/sec
ZDOT = -19215
637539 ZDOT = -5856
926322
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
27925650
00016717 00000-0 10270-3 0 9087
2 25544 51
6457 257
6741 0005846 331
3142 28
7700 15
75320748 37930
Satellite: ISS
Catalog Number: 25544
Epoch time: 11149
27925650 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 257
6741 deg
Eccentricity:
0005846
Arg of perigee: 331
3142 deg
Mean anomaly: 28
7700 deg
Mean motion: 15
75320748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 321
Coasting Arc #10 (Orbit 3808)
---------------------------------------
Vector Time (GMT): 2011/150/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4460201
62 A = 6717511
71 meter
Y = 878609
66 meter E =
0008913
Z = 4946202
85 I = 51
30211
XDOT = 757
690625 Wp = 15
53386
YDOT = 7402
749198 meter/sec RA = 251
79255 deg
ZDOT = -1988
911045 TA = 93
83738
MA = 93
73546
Ha = 188
161 n
mi
Hp = 182
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14633207
41 X = 4426017
25
Y = 2882577
64 feet Y = 928294
65 meter
Z = 16227699
65 Z = 4967787
88
XDOT = 2485
861631 XDOT = 684
517250
YDOT = 24287
234901 feet/sec YDOT = 7410
813247 meter/sec
ZDOT = -6525
298705 ZDOT = -1985
407029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12197945
12 X = 3717933
67
Y = 8414757
72 feet Y = 2564818
15 meter
Z = 16315030
99 Z = 4972821
45
XDOT = -6706
506115 XDOT = -2044
143064
YDOT = 22405
276839 feet/sec YDOT = 6829
128380 meter/sec
ZDOT = -6511
418900 ZDOT = -1984
680481
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
29421704
00016717 00000-0 10270-3 0 9093
2 25544 51
6455 252
4510 0005844 334
7931 25
2947 15
75366786 38091
Satellite: ISS
Catalog Number: 25544
Epoch time: 11150
29421704 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 252
4510 deg
Eccentricity:
0005844
Arg of perigee: 334
7931 deg
Mean anomaly: 25
2947 deg
Mean motion: 15
75366786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3809
Checksum: 318
Coasting Arc #11 (Orbit 3824)
---------------------------------------
Vector Time (GMT): 2011/151/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -819626
45 A = 6726024
36 meter
Y = -6300211
27 meter E =
0015016
Z = 2179594
89 I = 51
34128
XDOT = 5291
383507 Wp = 48
29089
YDOT = 1210
260903 meter/sec RA = 246
65902 deg
ZDOT = 5473
770682 TA = 336
26348
MA = 336
33268
Ha = 188
233 n
mi
Hp = 182
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2689063
15 X = -759703
57
Y = -20669984
49 feet Y = -6309042
08 meter
Z = 7150901
86 Z = 2175757
80
XDOT = 17360
182109 XDOT = 5250
865931
YDOT = 3970
672254 feet/sec YDOT = 1269
205085 meter/sec
ZDOT = 17958
565231 ZDOT = 5499
378308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5348875
36 X = 1630337
21
Y = -20151602
60 feet Y = -6142208
47 meter
Z = 7135626
23 Z = 2174938
88
XDOT = 12968
496127 XDOT = 3952
797619
YDOT = 9854
710365 feet/sec YDOT = 3003
715719 meter/sec
ZDOT = 18062
172940 ZDOT = 5505
350312
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
30914218
00016717 00000-0 10270-3 0 9105
2 25544 51
6446 247
2277 0005815 338
9879 21
1045 15
75440405 38251
Satellite: ISS
Catalog Number: 25544
Epoch time: 11151
30914218 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 247
2277 deg
Eccentricity:
0005815
Arg of perigee: 338
9879 deg
Mean anomaly: 21
1045 deg
Mean motion: 15
75440405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3825
Checksum: 300
Coasting Arc #12 (Orbit 3839)
---------------------------------------
Vector Time (GMT): 2011/152/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4802661
74 A = 6718844
93 meter
Y = -1217732
59 meter E =
0008378
Z = -4544142
77 I = 51
33064
XDOT = -1067
240665 Wp = 76
46546
YDOT = -7003
355600 meter/sec RA = 241
44799 deg
ZDOT = 3011
285378 TA = 223
57035
MA = 223
63655
Ha = 188
262 n
mi
Hp = 181
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15756764
25 X = -4766613
02
Y = -3995185
65 feet Y = -1271236
61 meter
Z = -14908604
89 Z = -4567386
98
XDOT = -3501
445752 XDOT = -1003
476913
YDOT = -22976
888450 feet/sec YDOT = -7014
934070 meter/sec
ZDOT = 9879
545203 ZDOT = 3006
254481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13127435
76 X = -4001242
42
Y = -9438983
31 feet Y = -2877002
11 meter
Z = -15002654
83 Z = -4572809
19
XDOT = 4383
614032 XDOT = 1336
125557
YDOT = -21733
470961 feet/sec YDOT = -6624
361949 meter/sec
ZDOT = 9859
461888 ZDOT = 3005
163983
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
26060387
00016717 00000-0 10270-3 0 9111
2 25544 51
6443 242
3310 0005776 343
9958 16
1023 15
75486035 38408
Satellite: ISS
Catalog Number: 25544
Epoch time: 11152
26060387 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 242
3310 deg
Eccentricity:
0005776
Arg of perigee: 343
9958 deg
Mean anomaly: 16
1023 deg
Mean motion: 15
75486035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3840
Checksum: 293
Coasting Arc #13 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2011/153/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 976201
08 A = 6723642
70 meter
Y = 5902100
74 meter E =
0005605
Z = -3077385
11 I = 51
36306
XDOT = -5739
837495 Wp = 35
06379
YDOT = -1591
156695 meter/sec RA = 236
32836 deg
ZDOT = -4872
320272 TA = 180
78313
MA = 180
78401
Ha = 188
420 n
mi
Hp = 181
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3202759
46 X = 925079
59
Y = 19363847
56 feet Y = 5912731
88 meter
Z = -10096407
83 Z = -3072765
88
XDOT = -18831
487846 XDOT = -5697
949255
YDOT = -5220
330364 feet/sec YDOT = -1655
108026 meter/sec
ZDOT = -15985
302730 ZDOT = -4900
103127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3698753
70 X = -1127380
13
Y = 19284916
85 feet Y = 5878042
66 meter
Z = -10077941
98 Z = -3071756
72
XDOT = -14329
379089 XDOT = -4367
594746
YDOT = -11160
901064 feet/sec YDOT = -3401
842644 meter/sec
ZDOT = -16097
724503 ZDOT = -4906
586429
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
27546180
00016717 00000-0 10270-3 0 9124
2 25544 51
6443 237
1087 0005944 348
9745 11
1288 15
75556512 38560
Satellite: ISS
Catalog Number: 25544
Epoch time: 11153
27546180 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 237
1087 deg
Eccentricity:
0005944
Arg of perigee: 348
9745 deg
Mean anomaly: 11
1288 deg
Mean motion: 15
75556512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 318
Coasting Arc #14 (Orbit 3871)
---------------------------------------
Vector Time (GMT): 2011/154/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5246490
54 A = 6720935
84 meter
Y = 1526965
78 meter E =
0012720
Z = 3910592
02 I = 51
37147
XDOT = 1113
493022 Wp = 52
28193
YDOT = 6482
735982 meter/sec RA = 231
11031 deg
ZDOT = -4008
629468 TA = 79
56050
MA = 79
41717
Ha = 188
379 n
mi
Hp = 181
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17212895
47 X = 5210028
78
Y = 5009730
25 feet Y = 1585430
69 meter
Z = 12830026
31 Z = 3935991
25
XDOT = 3653
192331 XDOT = 1060
392318
YDOT = 21268
818840 feet/sec YDOT = 6494
891517 meter/sec
ZDOT = -13151
671482 ZDOT = -4003
347980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14491614
65 X = 4417044
14
Y = 10427184
46 feet Y = 3178205
82 meter
Z = 12932813
76 Z = 3941921
63
XDOT = -2797
965507 XDOT = -852
819887
YDOT = 20241
192231 feet/sec YDOT = 6169
515392 meter/sec
ZDOT = -13130
540549 ZDOT = -4002
188759
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
29028580
00016717 00000-0 10270-3 0 9137
2 25544 51
6435 231
8849 0005829 351
7380 8
3687 15
75572744 38721
Satellite: ISS
Catalog Number: 25544
Epoch time: 11154
29028580 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 231
8849 deg
Eccentricity:
0005829
Arg of perigee: 351
7380 deg
Mean anomaly: 8
3687 deg
Mean motion: 15
75572744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3872
Checksum: 332
Coasting Arc #15 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2011/155/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -903425
89 A = 6720885
63 meter
Y = -5400704
96 meter E =
0011354
Z = 3884809
92 I = 51
39204
XDOT = 6291
681562 Wp = 70
22466
YDOT = 1862
690071 meter/sec RA = 225
99604 deg
ZDOT = 4046
912695 TA = 337
54676
MA = 337
59641
Ha = 188
389 n
mi
Hp = 181
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2963995
70 X = -861838
70
Y = -17718848
30 feet Y = -5410575
74 meter
Z = 12745439
36 Z = 3880521
20
XDOT = 20641
999874 XDOT = 6250
725845
YDOT = 6111
187897 feet/sec YDOT = 1932
817806 meter/sec
ZDOT = 13277
272620 ZDOT = 4077
378480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2723910
02 X = 830247
77
Y = -17769645
91 feet Y = -5416188
07 meter
Z = 12728278
70 Z = 3879579
35
XDOT = 16274
619858 XDOT = 4960
504133
YDOT = 12107
064814 feet/sec YDOT = 3690
233355 meter/sec
ZDOT = 13400
580045 ZDOT = 4084
496798
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
30507462
00016717 00000-0 10270-3 0 9142
2 25544 51
6433 226
6610 0005783 355
8576 4
2539 15
75660438 38884
Satellite: ISS
Catalog Number: 25544
Epoch time: 11155
30507462 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 226
6610 deg
Eccentricity:
0005783
Arg of perigee: 355
8576 deg
Mean anomaly: 4
2539 deg
Mean motion: 15
75660438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 320
Coasting Arc #16 (Orbit 3902)
---------------------------------------
Vector Time (GMT): 2011/156/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5725839
86 A = 6723097
10 meter
Y = -1682054
54 meter E =
0008177
Z = -3091961
70 I = 51
42311
XDOT = -890
478015 Wp = 34
01366
YDOT = -5899
208848 meter/sec RA = 220
78064 deg
ZDOT = 4871
116391 TA = 289
93959
MA = 290
02766
Ha = 188
405 n
mi
Hp = 180
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18785563
86 X = -5691585
13
Y = -5518551
65 feet Y = -1745892
36 meter
Z = -10144231
32 Z = -3119694
76
XDOT = -2921
515797 XDOT = -848
108634
YDOT = -19354
359736 feet/sec YDOT = -5908
930560 meter/sec
ZDOT = 15981
352988 ZDOT = 4866
892479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16204516
59 X = -4939136
66
Y = -10884631
58 feet Y = -3317635
71 meter
Z = -10256494
92 Z = -3126179
65
XDOT = 2136
967544 XDOT = 651
347707
YDOT = -18185
254436 feet/sec YDOT = -5542
865552 meter/sec
ZDOT = 15964
465062 ZDOT = 4865
968951
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
25640983
00016717 00000-0 10270-3 0 9154
2 25544 51
6441 221
7641 0005799 1
0594 359
0581 15
75693218 39038
Satellite: ISS
Catalog Number: 25544
Epoch time: 11156
25640983 = yrday
fracday
Element set: 915
Inclination: 51
6441 deg
RA of node: 221
7641 deg
Eccentricity:
0005799
Arg of perigee: 1
0594 deg
Mean anomaly: 359
0581 deg
Mean motion: 15
75693218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3903
Checksum: 316
Coasting Arc #17 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2011/157/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 563477
93 A = 6718092
94 meter
Y = 4897308
69 meter E =
0013949
Z = -4577605
77 I = 51
43076
XDOT = -6816
354899 Wp = 47
66390
YDOT = -1986
122642 meter/sec RA = 215
66505 deg
ZDOT = -2960
383615 TA = 192
83121
MA = 192
86674
Ha = 188
537 n
mi
Hp = 180
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1848680
88 X = 530910
44
Y = 16067285
71 feet Y = 4903428
36 meter
Z = -15018391
62 Z = -4574946
85
XDOT = -22363
369092 XDOT = -6779
258173
YDOT = -6516
150399 feet/sec YDOT = -2062
139444 meter/sec
ZDOT = -9712
544670 ZDOT = -2993
407414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2698881
04 X = -822618
94
Y = 15956485
36 feet Y = 4863536
74 meter
Z = -15007797
78 Z = -4574376
76
XDOT = -18376
005883 XDOT = -5601
006593
YDOT = -12379
786076 feet/sec YDOT = -3773
358796 meter/sec
ZDOT = -9846
243937 ZDOT = -3001
135152
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
27113352
00016717 00000-0 10270-3 0 9163
2 25544 51
6442 216
5406 0005921 5
2140 354
9085 15
75754778 39199
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
27113352 = yrday
fracday
Element set: 916
Inclination: 51
6442 deg
RA of node: 216
5406 deg
Eccentricity:
0005921
Arg of perigee: 5
2140 deg
Mean anomaly: 354
9085 deg
Mean motion: 15
75754778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 306
Coasting Arc #18 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2011/158/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6164283
06 A = 6725234
02 meter
Y = 1749379
64 meter E =
0014068
Z = 2031484
34 I = 51
48046
XDOT = 330
830417 Wp = 87
01727
YDOT = 5324
774725 meter/sec RA = 210
46075 deg
ZDOT = -5555
474074 TA = 70
26036
MA = 70
10868
Ha = 188
521 n
mi
Hp = 180
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20224025
77 X = 6134394
49
Y = 5739434
50 feet Y = 1818145
05 meter
Z = 6664974
85 Z = 2061357
84
XDOT = 1085
401629 XDOT = 298
250487
YDOT = 17469
733350 feet/sec YDOT = 5328
292739 meter/sec
ZDOT = -18226
620978 ZDOT = -5553
945441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17916631
34 X = 5460989
23
Y = 10923351
39 feet Y = 3329437
50 meter
Z = 6785936
37 Z = 2068353
41
XDOT = -2719
066436 XDOT = -828
771450
YDOT = 15846
606295 feet/sec YDOT = 4830
045599 meter/sec
ZDOT = -18220
614064 ZDOT = -5553
643167
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
28582385
00016717 00000-0 10270-3 0 9172
2 25544 51
6435 211
3153 0005855 8
4249 351
7013 15
75787271 39352
Satellite: ISS
Catalog Number: 25544
Epoch time: 11158
28582385 = yrday
fracday
Element set: 917
Inclination: 51
6435 deg
RA of node: 211
3153 deg
Eccentricity:
0005855
Arg of perigee: 8
4249 deg
Mean anomaly: 351
7013 deg
Mean motion: 15
75787271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 318
Coasting Arc #19 (Orbit 3950)
---------------------------------------
Vector Time (GMT): 2011/159/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 44726
35 A = 6715715
23 meter
Y = -4424122
17 meter E =
0006056
Z = 5047012
63 I = 51
47743
XDOT = 7263
771471 Wp = 63
15426
YDOT = 1971
898278 meter/sec RA = 205
33294 deg
ZDOT = 1665
325076 TA = 10
82304
MA = 10
81001
Ha = 188
462 n
mi
Hp = 180
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 146740
00 X = 69677
04
Y = -14514836
50 feet Y = -4423482
99 meter
Z = 16558440
40 Z = 5047290
09
XDOT = 23831
271229 XDOT = 7233
091647
YDOT = 6469
482538 feet/sec YDOT = 2052
954483 meter/sec
ZDOT = 5463
664949 ZDOT = 1700
538011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3682237
60 X = 1122346
02
Y = -14039263
80 feet Y = -4279167
61 meter
Z = 16559714
91 Z = 5047401
10
XDOT = 20394
333859 XDOT = 6216
192960
YDOT = 11957
296222 feet/sec YDOT = 3644
583889 meter/sec
ZDOT = 5606
264560 ZDOT = 1708
789438
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 11159
30047977
00016717 00000-0 10270-3 0 9180
2 25544 51
6448 206
0909 0005904 11
4466 348
6831 15
75874265 39517
Satellite: ISS
Catalog Number: 25544
Epoch time: 11159
30047977 = yrday
fracday
Element set: 918
Inclination: 51
6448 deg
RA of node: 206
0909 deg
Eccentricity:
0005904
Arg of perigee: 11
4466 deg
Mean anomaly: 348
6831 deg
Mean motion: 15
75874265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3951
Checksum: 331
Coasting Arc #20 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2011/160/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6455854
79 A = 6726461
32 meter
Y = -1659222
43 meter E =
0015884
Z = -839212
86 I = 51
54332
XDOT = 483
632975 Wp = 30
95063
YDOT = -4863
907969 meter/sec RA = 200
15230 deg
ZDOT = 5959
137861 TA = 319
87048
MA = 319
98768
Ha = 188
536 n
mi
Hp = 179
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21180625
96 X = -6432744
49
Y = -5443643
16 feet Y = -1731286
43 meter
Z = -2753323
04 Z = -870519
42
XDOT = 1586
722360 XDOT = 509
037770
YDOT = -15957
703312 feet/sec YDOT = -4858
358173 meter/sec
ZDOT = 19550
977233 ZDOT = 5961
548628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19303859
85 X = -5883816
48
Y = -10242014
97 feet Y = -3121766
16 meter
Z = -2880117
89 Z = -877859
93
XDOT = 4413
289820 XDOT = 1345
170737
YDOT = -13763
049883 feet/sec YDOT = -4194
977604 meter/sec
ZDOT = 19560
908043 ZDOT = 5962
164771
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 11160
25169103
00016717 00000-0 10270-3 0 9193
2 25544 51
6458 201
1935 0005980 16
3342 343
8014 15
75891875 39666
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
25169103 = yrday
fracday
Element set: 919
Inclination: 51
6458 deg
RA of node: 201
1935 deg
Eccentricity:
0005980
Arg of perigee: 16
3342 deg
Mean anomaly: 343
8014 deg
Mean motion: 15
75891875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
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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