[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 16th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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 3544)
---------------------------------------
Vector Time (GMT): 2011/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1144068
00 A = 6717603
93 meter
Y = 4036460
92 meter E =
0001140
Z = 5247043
49 I = 51
50122
XDOT = -7255
491059 Wp = 319
47988
YDOT = 2556
867760 meter/sec RA = 338
31093 deg
ZDOT = -384
157276 TA = 134
17863
MA = 134
16926
Ha = 187
514 n
mi
Hp = 183
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3753503
94 X = 1073357
03
Y = 13242982
03 feet Y = 4048859
15 meter
Z = 17214709
62 Z = 5252429
73
XDOT = -23804
104525 XDOT = -7281
677009
YDOT = 8388
673754 feet/sec YDOT = 2475
586045 meter/sec
ZDOT = -1260
358518 ZDOT = -419
468397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12502697
82 X = 3810822
30
Y = 5692454
84 feet Y = 1735060
24 meter
Z = 17236301
73 Z = 5253624
77
XDOT = -8408
963747 XDOT = -2563
052150
YDOT = 22726
398366 feet/sec YDOT = 6927
006222 meter/sec
ZDOT = -1403
358691 ZDOT = -427
743729
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 11133
54688841
00016717 00000-0 10270-3 0 9000
2 25544 51
6466 338
6058 0003224 270
2863 89
7932 15
74894549 35453
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
54688841 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 338
6058 deg
Eccentricity:
0003224
Arg of perigee: 270
2863 deg
Mean anomaly: 89
7932 deg
Mean motion: 15
74894549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3545
Checksum: 337
Coasting Arc #2 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2011/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6188244
32 A = 6729253
82 meter
Y = -2543763
76 meter E =
0011171
Z = 658170
95 I = 51
51162
XDOT = 1282
933852 Wp = 40
47133
YDOT = 4681
262738 meter/sec RA = 333
16820 deg
ZDOT = 5982
026243 TA = 326
71364
MA = 326
78384
Ha = 187
438 n
mi
Hp = 183
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20302638
84 X = 6213031
92
Y = -8345681
61 feet Y = -2474424
47 meter
Z = 2159353
53 Z = 688294
05
XDOT = 4209
100563 XDOT = 1201
431673
YDOT = 15358
473550 feet/sec YDOT = 4695
153409 meter/sec
ZDOT = 19626
070350 ZDOT = 5988
060993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6247338
81 X = 1904188
87
Y = -21030371
41 feet Y = -6410057
21 meter
Z = 2281356
92 Z = 695357
59
XDOT = 12988
618386 XDOT = 3958
930884
YDOT = 6006
313097 feet/sec YDOT = 1830
724232 meter/sec
ZDOT = 19650
251834 ZDOT = 5989
396759
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 11134
56211809
00016717 00000-0 10270-3 0 9010
2 25544 51
6453 333
3843 0003306 274
6850 85
3936 15
74955161 35610
Satellite: ISS
Catalog Number: 25544
Epoch time: 11134
56211809 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 333
3843 deg
Eccentricity:
0003306
Arg of perigee: 274
6850 deg
Mean anomaly: 85
3936 deg
Mean motion: 15
74955161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 304
Coasting Arc #3 (Orbit 3575)
---------------------------------------
Vector Time (GMT): 2011/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1092081
25 A = 6717697
61 meter
Y = -4169400
46 meter E =
0011075
Z = -5162448
17 I = 51
44506
XDOT = 6890
199344 Wp = 99
07464
YDOT = -3226
518338 meter/sec RA = 327
99634 deg
ZDOT = 1148
664337 TA = 181
92844
MA = 181
93271
Ha = 187
394 n
mi
Hp = 183
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3582943
74 X = -1020298
34
Y = -13679135
38 feet Y = -4181211
14 meter
Z = -16937165
91 Z = -5167579
46
XDOT = 22605
640893 XDOT = 6920
186683
YDOT = -10585
690085 feet/sec YDOT = -3149
300339 meter/sec
ZDOT = 3768
583783 ZDOT = 1182
210217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12931387
69 X = -3941486
97
Y = -5660294
54 feet Y = -1725257
77 meter
Z = -16957714
99 Z = -5168711
53
XDOT = 5114
156023 XDOT = 1558
794756
YDOT = -23377
440436 feet/sec YDOT = -7125
443845 meter/sec
ZDOT = 3904
467359 ZDOT = 1190
081651
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 11135
51386890
00016717 00000-0 10270-3 0 9020
2 25544 51
6442 328
4890 0003253 278
0769 82
0025 15
75007153 35762
Satellite: ISS
Catalog Number: 25544
Epoch time: 11135
51386890 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 328
4890 deg
Eccentricity:
0003253
Arg of perigee: 278
0769 deg
Mean anomaly: 82
0025 deg
Mean motion: 15
75007153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3576
Checksum: 306
Coasting Arc #4 (Orbit 3591)
---------------------------------------
Vector Time (GMT): 2011/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5833128
44 A = 6728298
50 meter
Y = 3056439
59 meter E =
0006378
Z = -1361869
02 I = 51
45613
XDOT = -1210
936987 Wp = 161
42101
YDOT = -4897
558914 meter/sec RA = 322
86330 deg
ZDOT = -5818
329798 TA = 33
58553
MA = 33
54512
Ha = 187
315 n
mi
Hp = 183
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19137560
51 X = -5860256
76
Y = 10027688
94 feet Y = 2991058
44 meter
Z = -4468074
21 Z = -1390272
54
XDOT = -3972
890377 XDOT = -1127
816610
YDOT = -16068
106672 feet/sec YDOT = -4910
635107 meter/sec
ZDOT = -19089
008522 ZDOT = -5824
011150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3467463
60 X = -1056882
90
Y = 21301078
17 feet Y = 6492568
63 meter
Z = -4583145
21 Z = -1396942
66
XDOT = -13609
790714 XDOT = -4148
264210
YDOT = -6318
308622 feet/sec YDOT = -1925
820468 meter/sec
ZDOT = -19111
742925 ZDOT = -5825
259244
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 11136
52903980
00016717 00000-0 10270-3 0 9038
2 25544 51
6444 323
2685 0003351 284
6834 75
3958 15
75063982 35924
Satellite: ISS
Catalog Number: 25544
Epoch time: 11136
52903980 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 323
2685 deg
Eccentricity:
0003351
Arg of perigee: 284
6834 deg
Mean anomaly: 75
3958 deg
Mean motion: 15
75063982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3592
Checksum: 326
Coasting Arc #5 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2011/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1041332
12 A = 6718377
23 meter
Y = 4408774
79 meter E =
0004569
Z = 4961173
16 I = 51
39822
XDOT = -6439
725091 Wp = 21
41990
YDOT = 3740
440172 meter/sec RA = 317
67414 deg
ZDOT = -1967
526997 TA = 87
68385
MA = 87
63154
Ha = 187
309 n
mi
Hp = 183
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3416443
97 X = 967854
08
Y = 14464484
23 feet Y = 4420008
21 meter
Z = 16276814
84 Z = 4966054
05
XDOT = -21127
706992 XDOT = -6471
514741
YDOT = 12271
785340 feet/sec YDOT = 3668
249732 meter/sec
ZDOT = -6455
141065 ZDOT = -1998
888509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13658789
10 X = 4163198
92
Y = 5804745
22 feet Y = 1769286
34 meter
Z = 16296334
19 Z = 4967122
66
XDOT = -2021
856413 XDOT = -616
261835
YDOT = 23280
336644 feet/sec YDOT = 7095
846609 meter/sec
ZDOT = -6582
218362 ZDOT = -2006
260157
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 11137
54418120
00016717 00000-0 10270-3 0 9049
2 25544 51
6439 318
0463 0003351 285
9770 74
1025 15
75071235 36087
Satellite: ISS
Catalog Number: 25544
Epoch time: 11137
54418120 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 318
0463 deg
Eccentricity:
0003351
Arg of perigee: 285
9770 deg
Mean anomaly: 74
1025 deg
Mean motion: 15
75071235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 290
Coasting Arc #6 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2011/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5395230
09 A = 6726996
24 meter
Y = -3427387
41 meter E =
0011723
Z = 2076301
41 I = 51
40587
XDOT = 1188
836051 Wp = 59
17229
YDOT = 5231
847557 meter/sec RA = 312
54762 deg
ZDOT = 5530
012408 TA = 324
11123
MA = 324
18992
Ha = 187
234 n
mi
Hp = 183
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17700886
12 X = 5423068
39
Y = -11244709
33 feet Y = -3366899
29 meter
Z = 6812012
49 Z = 2102578
93
XDOT = 3900
380745 XDOT = 1103
380048
YDOT = 17164
854191 feet/sec YDOT = 5244
663308 meter/sec
ZDOT = 18143
085329 ZDOT = 5535
580955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 904117
83 X = 275575
12
Y = -20916146
33 feet Y = -6375241
40 meter
Z = 6918508
90 Z = 2108761
51
XDOT = 14715
414921 XDOT = 4485
258468
YDOT = 6662
998106 feet/sec YDOT = 2030
881823 meter/sec
ZDOT = 18165
344478 ZDOT = 5536
796997
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 11138
55929084
00016717 00000-0 10270-3 0 9058
2 25544 51
6436 312
8239 0003329 289
9638 70
1167 15
75142062 36247
Satellite: ISS
Catalog Number: 25544
Epoch time: 11138
55929084 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 312
8239 deg
Eccentricity:
0003329
Arg of perigee: 289
9638 deg
Mean anomaly: 70
1167 deg
Mean motion: 15
75142062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 319
Coasting Arc #7 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2011/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1053586
64 A = 6719372
43 meter
Y = -4744105
48 meter E =
0007639
Z = -4647713
13 I = 51
36117
XDOT = 5910
941711 Wp = 107
27452
YDOT = -4055
424495 meter/sec RA = 307
34401 deg
ZDOT = 2801
135819 TA = 190
49000
MA = 190
50595
Ha = 187
294 n
mi
Hp = 182
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3456649
08 X = -977880
94
Y = -15564650
53 feet Y = -4755463
38 meter
Z = -15248402
65 Z = -4652648
26
XDOT = 19392
853383 XDOT = 5942
243427
YDOT = -13305
198476 feet/sec YDOT = -3989
150133 meter/sec
ZDOT = 9190
078145 ZDOT = 2829
926836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14788589
00 X = -4507561
93
Y = -5907832
49 feet Y = -1800707
34 meter
Z = -15268127
03 Z = -4653725
12
XDOT = -657
682833 XDOT = -200
461728
YDOT = -22392
878567 feet/sec YDOT = -6825
349387 meter/sec
ZDOT = 9306
780882 ZDOT = 2836
706813
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 11139
51092869
00016717 00000-0 10270-3 0 9068
2 25544 51
6443 307
9284 0003239 294
1215 65
9610 15
75188843 36397
Satellite: ISS
Catalog Number: 25544
Epoch time: 11139
51092869 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 307
9284 deg
Eccentricity:
0003239
Arg of perigee: 294
1215 deg
Mean anomaly: 65
9610 deg
Mean motion: 15
75188843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 329
Coasting Arc #8 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2011/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4932562
48 A = 6725063
93 meter
Y = 3598453
77 meter E =
0001329
Z = -2819714
84 I = 51
36375
XDOT = -1228
153068 Wp = 106
28475
YDOT = -5657
767795 meter/sec RA = 302
22523 deg
ZDOT = -5074
231169 TA = 106
17790
MA = 106
16327
Ha = 187
305 n
mi
Hp = 182
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16182947
77 X = -4958736
79
Y = 11805950
69 feet Y = 3543148
90 meter
Z = -9251032
95 Z = -2843740
36
XDOT = -4029
373582 XDOT = -1140
145803
YDOT = -18562
230298 feet/sec YDOT = -5671
008979 meter/sec
ZDOT = -16647
740056 ZDOT = -5079
984552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1120988
96 X = 341677
44
Y = 19954951
33 feet Y = 6082269
17 meter
Z = -9348432
06 Z = -2849402
09
XDOT = -16254
478742 XDOT = -4954
365120
YDOT = -6893
175124 feet/sec YDOT = -2101
039778 meter/sec
ZDOT = -16670
733977 ZDOT = -5081
239716
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 11140
52597818
00016717 00000-0 10270-3 0 9076
2 25544 51
6447 302
7070 0003338 301
2904 58
7933 15
75257359 36557
Satellite: ISS
Catalog Number: 25544
Epoch time: 11140
52597818 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 302
7070 deg
Eccentricity:
0003338
Arg of perigee: 301
2904 deg
Mean anomaly: 58
7933 deg
Mean motion: 15
75257359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 317
Coasting Arc #9 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2011/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1126065
39 A = 6720977
55 meter
Y = 5144075
73 meter E =
0008400
Z = 4173321
10 I = 51
33387
XDOT = -5380
271248 Wp = 56
80343
YDOT = 4139
604682 meter/sec RA = 297
01011 deg
ZDOT = -3640
968301 TA = 70
49553
MA = 70
40481
Ha = 187
314 n
mi
Hp = 182
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3694440
25 X = 1048186
45
Y = 16876888
89 feet Y = 5156232
12 meter
Z = 13691998
35 Z = 4178602
99
XDOT = -17651
808558 XDOT = -5408
474092
YDOT = 13581
380190 feet/sec YDOT = 4079
281985 meter/sec
ZDOT = -11945
434057 ZDOT = -3667
173610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16226742
93 X = 4945911
25
Y = 5881522
38 feet Y = 1792688
02 meter
Z = 13713117
60 Z = 4179758
24
XDOT = 2628
545334 XDOT = 801
180618
YDOT = 20922
204498 feet/sec YDOT = 6377
087931 meter/sec
ZDOT = -12051
680684 ZDOT = -3673
352272
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 11141
54099771
00016717 00000-0 10270-3 0 9085
2 25544 51
6441 297
4846 0003324 302
7790 57
3054 15
75261249 36716
Satellite: ISS
Catalog Number: 25544
Epoch time: 11141
54099771 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 297
4846 deg
Eccentricity:
0003324
Arg of perigee: 302
7790 deg
Mean anomaly: 57
3054 deg
Mean motion: 15
75261249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 315
Coasting Arc #10 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2011/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4471160
01 A = 6722854
07 meter
Y = -3570244
66 meter E =
0009519
Z = 3520296
27 I = 51
32902
XDOT = 1380
194419 Wp = 81
69890
YDOT = 6132
254101 meter/sec RA = 291
89406 deg
ZDOT = 4457
360757 TA = 320
45874
MA = 320
52814
Ha = 187
153 n
mi
Hp = 182
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14669160
15 X = 4493649
96
Y = -11713401
10 feet Y = -3520120
05 meter
Z = 11549528
43 Z = 3542071
34
XDOT = 4528
196914 XDOT = 1289
866818
YDOT = 20118
943902 feet/sec YDOT = 6147
182754 meter/sec
ZDOT = 14623
886997 ZDOT = 4463
846962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2514492
49 X = -766417
31
Y = -18547726
45 feet Y = -5653347
02 meter
Z = 11637817
79 Z = 3547206
86
XDOT = 18178
227685 XDOT = 5540
723798
YDOT = 6745
871014 feet/sec YDOT = 2056
141485 meter/sec
ZDOT = 14649
840292 ZDOT = 4465
271321
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 11142
55598399
00016717 00000-0 10270-3 0 9098
2 25544 51
6450 292
2626 0003393 306
3283 53
7567 15
75350021 36871
Satellite: ISS
Catalog Number: 25544
Epoch time: 11142
55598399 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 292
2626 deg
Eccentricity:
0003393
Arg of perigee: 306
3283 deg
Mean anomaly: 53
7567 deg
Mean motion: 15
75350021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 323
Coasting Arc #11 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2011/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1312108
76 A = 6722717
11 meter
Y = -5550767
75 meter E =
0003214
Z = -3559337
64 I = 51
31913
XDOT = 4886
406844 Wp = 60
47193
YDOT = -3985
395418 meter/sec RA = 286
67423 deg
ZDOT = 4418
436062 TA = 256
82682
MA = 256
86267
Ha = 187
318 n
mi
Hp = 182
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4304818
76 X = -1232650
92
Y = -18211180
29 feet Y = -5564995
97 meter
Z = -11677616
92 Z = -3565519
32
XDOT = 16031
518518 XDOT = 4909
145236
YDOT = -13075
444286 feet/sec YDOT = -3930
625893 meter/sec
ZDOT = 14496
181305 ZDOT = 4442
229042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17886043
18 X = -5451665
96
Y = -5448777
19 feet Y = -1660787
29 meter
Z = -11702374
78 Z = -3566883
83
XDOT = -3736
550136 XDOT = -1138
900482
YDOT = -19043
215345 feet/sec YDOT = -5804
372037 meter/sec
ZDOT = 14592
653046 ZDOT = 4447
840648
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 11143
50750662
00016717 00000-0 10270-3 0 9109
2 25544 51
6457 287
3674 0003415 312
2540 47
8334 15
75376747 37020
Satellite: ISS
Catalog Number: 25544
Epoch time: 11143
50750662 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 287
3674 deg
Eccentricity:
0003415
Arg of perigee: 312
2540 deg
Mean anomaly: 47
8334 deg
Mean motion: 15
75376747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3702
Checksum: 303
Coasting Arc #12 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2011/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4093153
53 A = 6720442
23 meter
Y = 3323617
68 meter E =
0007522
Z = -4175067
93 I = 51
30419
XDOT = -1630
152239 Wp = 43
99945
YDOT = -6581
631972 meter/sec RA = 281
55626 deg
ZDOT = -3639
815349 TA = 188
69320
MA = 188
70624
Ha = 187
365 n
mi
Hp = 182
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13428981
41 X = -4109732
95
Y = 10904257
48 feet Y = 3277753
15 meter
Z = -13697729
43 Z = -4194992
48
XDOT = -5348
268500 XDOT = -1538
752468
YDOT = -21593
280747 feet/sec YDOT = -6599
350023 meter/sec
ZDOT = -11941
651408 ZDOT = -3647
513074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3051940
23 X = 930231
38
Y = 16961910
99 feet Y = 5169990
47 meter
Z = -13778512
28 Z = -4199690
54
XDOT = -20202
796611 XDOT = -6157
812407
YDOT = -6094
182583 feet/sec YDOT = -1857
506851 meter/sec
ZDOT = -11972
506330 ZDOT = -3649
219929
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
52243262
00016717 00000-0 10270-3 0 9116
2 25544 51
6457 282
1452 0003545 316
6221 43
4664 15
75428200 37182
Satellite: ISS
Catalog Number: 25544
Epoch time: 11144
52243262 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 282
1452 deg
Eccentricity:
0003545
Arg of perigee: 316
6221 deg
Mean anomaly: 43
4664 deg
Mean motion: 15
75428200 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 282
Coasting Arc #13 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2011/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1564467
75 A = 6724681
16 meter
Y = 5925662
68 meter E =
0011114
Z = 2758584
92 I = 51
31360
XDOT = -4515
942664 Wp = 88
39370
YDOT = 3580
283690 meter/sec RA = 276
33708 deg
ZDOT = -5111
591863 TA = 59
88256
MA = 59
77243
Ha = 187
389 n
mi
Hp = 182
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5132768
19 X = 1484688
84
Y = 19441150
51 feet Y = 5942711
26 meter
Z = 9050475
47 Z = 2765991
71
XDOT = -14816
084856 XDOT = -4530
811216
YDOT = 11746
337566 feet/sec YDOT = 3529
700863 meter/sec
ZDOT = -16770
314512 ZDOT = -5133
566243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19545040
29 X = 5957328
28
Y = 4664363
73 feet Y = 1421698
07 meter
Z = 9080190
53 Z = 2767642
07
XDOT = 3782
502121 XDOT = 1152
906646
YDOT = 17085
478189 feet/sec YDOT = 5207
653752 meter/sec
ZDOT = -16859
401052 ZDOT = -5138
745441
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
53732761
00016717 00000-0 10270-3 0 9126
2 25544 51
6456 276
9221 0003536 320
5106 39
5800 15
75463194 37349
Satellite: ISS
Catalog Number: 25544
Epoch time: 11145
53732761 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 276
9221 deg
Eccentricity:
0003536
Arg of perigee: 320
5106 deg
Mean anomaly: 39
5800 deg
Mean motion: 15
75463194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3734
Checksum: 299
Coasting Arc #14 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2011/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3831490
01 A = 6717998
65 meter
Y = -2879281
93 meter E =
0004536
Z = 4703950
41 I = 51
29075
XDOT = 1976
030071 Wp = 98
27508
YDOT = 6961
178122 meter/sec RA = 271
21022 deg
ZDOT = 2648
580024 TA = 325
57589
MA = 325
60527
Ha = 187
214 n
mi
Hp = 182
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12570505
29 X = 3840550
87
Y = -9446463
04 feet Y = -2836385
52 meter
Z = 15432908
15 Z = 4722585
71
XDOT = 6483
038290 XDOT = 1885
175585
YDOT = 22838
510898 feet/sec YDOT = 6982
767129 meter/sec
ZDOT = 8689
567009 ZDOT = 2657
959381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2730973
48 X = -832400
72
Y = -15409663
03 feet Y = -4696865
29 meter
Z = 15508449
00 Z = 4726975
25
XDOT = 22139
276951 XDOT = 6748
051615
YDOT = 4868
813357 feet/sec YDOT = 1484
014311 meter/sec
ZDOT = 8727
227275 ZDOT = 2660
058873
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
55218905
00016717 00000-0 10270-3 0 9139
2 25544 51
6466 271
6993 0003703 324
1259 35
9656 15
75557424 37500
Satellite: ISS
Catalog Number: 25544
Epoch time: 11146
55218905 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 271
6993 deg
Eccentricity:
0003703
Arg of perigee: 324
1259 deg
Mean anomaly: 35
9656 deg
Mean motion: 15
75557424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3750
Checksum: 323
Coasting Arc #15 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2011/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1897584
78 A = 6726265
91 meter
Y = -6183814
54 meter E =
0009418
Z = -1825867
92 I = 51
31950
XDOT = 4317
118272 Wp = 16
17540
YDOT = -2985
157171 meter/sec RA = 266
00159 deg
ZDOT = 5639
275399 TA = 323
45994
MA = 323
52416
Ha = 187
462 n
mi
Hp = 181
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6225671
84 X = -1819425
33
Y = -20288105
46 feet Y = -6204597
35 meter
Z = -5990380
30 Z = -1834897
05
XDOT = 14163
773858 XDOT = 4322
783195
YDOT = -9793
822740 feet/sec YDOT = -2936
849254 meter/sec
ZDOT = 18501
559708 ZDOT = 5660
261694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20943150
88 X = -6383472
39
Y = -3363724
69 feet Y = -1025263
28 meter
Z = -6026662
13 Z = -1836926
62
XDOT = -2860
158141 XDOT = -871
776201
YDOT = -15400
270510 feet/sec YDOT = -4694
002451 meter/sec
ZDOT = 18586
618830 ZDOT = 5665
201419
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
50359550
00016717 00000-0 10270-3 0 9148
2 25544 51
6469 266
8032 0003845 330
4224 29
6722 15
75560174 37658
Satellite: ISS
Catalog Number: 25544
Epoch time: 11147
50359550 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 266
8032 deg
Eccentricity:
0003845
Arg of perigee: 330
4224 deg
Mean anomaly: 29
6722 deg
Mean motion: 15
75560174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3765
Checksum: 310
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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