[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 4th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 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 3354)
---------------------------------------
Vector Time (GMT): 2011/121/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4035035
81 A = 6719867
86 meter
Y = 1794576
35 meter E =
0004710
Z = 5061326
40 I = 51
85163
XDOT = -4759
254615 Wp = 78
70904
YDOT = -5806
144211 meter/sec RA = 40
21063 deg
ZDOT = -1733
297109 TA = 27
92563
MA = 27
90036
Ha = 189
807 n
mi
Hp = 182
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13238306
48 X = -4079390
59
Y = 5887717
67 feet Y = 1749206
18 meter
Z = 16605401
58 Z = 5041616
15
XDOT = -15614
352413 XDOT = -4685
555307
YDOT = -19049
029565 feet/sec YDOT = -5858
953028 meter/sec
ZDOT = -5686
670306 ZDOT = -1756
238837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10826201
44 X = -3299826
20
Y = 9765065
13 feet Y = 2976391
85 meter
Z = 16525562
17 Z = 5036991
35
XDOT = -20044
902270 XDOT = -6109
686212
YDOT = -12430
207691 feet/sec YDOT = -3788
727304 meter/sec
ZDOT = -5779
260683 ZDOT = -1761
518656
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 11121
48908022
00016717 00000-0 10270-3 0 9006
2 25544 51
6454 40
5757 0002198 173
0225 187
0970 15
74438420 33551
Satellite: ISS
Catalog Number: 25544
Epoch time: 11121
48908022 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 40
5757 deg
Eccentricity:
0002198
Arg of perigee: 173
0225 deg
Mean anomaly: 187
0970 deg
Mean motion: 15
74438420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3355
Checksum: 291
Coasting Arc #2 (Orbit 3370)
---------------------------------------
Vector Time (GMT): 2011/122/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4461251
03 A = 6729433
17 meter
Y = 4744398
11 meter E =
0013337
Z = 1674085
12 I = 51
86065
XDOT = -4595
432345 Wp = 72
71261
YDOT = 2282
451455 meter/sec RA = 35
11686 deg
ZDOT = 5744
331083 TA = 305
74140
MA = 305
86537
Ha = 189
463 n
mi
Hp = 182
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14636650
35 X = 4399734
14
Y = 15565610
61 feet Y = 4793942
56 meter
Z = 5492405
25 Z = 1695608
86
XDOT = -15076
877772 XDOT = -4648
519004
YDOT = 7488
357793 feet/sec YDOT = 2230
765672 meter/sec
ZDOT = 18846
230586 ZDOT = 5721
877162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18912773
05 X = 5764613
23
Y = 9892663
82 feet Y = 3015283
93 meter
Z = 5579292
12 Z = 1700568
24
XDOT = -11157
227734 XDOT = -3400
723013
YDOT = 10691
763135 feet/sec YDOT = 3258
849403 meter/sec
ZDOT = 18755
265789 ZDOT = 5716
605012
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 11122
50459778
00016717 00000-0 10270-3 0 9010
2 25544 51
6455 35
3571 0002216 179
6192 180
4974 15
74523759 33713
Satellite: ISS
Catalog Number: 25544
Epoch time: 11122
50459778 = yrday
fracday
Element set: 901
Inclination: 51
6455 deg
RA of node: 35
3571 deg
Eccentricity:
0002216
Arg of perigee: 179
6192 deg
Mean anomaly: 180
4974 deg
Mean motion: 15
74523759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3371
Checksum: 317
Coasting Arc #3 (Orbit 3385)
---------------------------------------
Vector Time (GMT): 2011/123/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4014145
63 A = 6719929
64 meter
Y = -2175147
86 meter E =
0013168
Z = -4942820
74 I = 51
80408
XDOT = 5385
085557 Wp = 115
19588
YDOT = 5054
469770 meter/sec RA = 29
95783 deg
ZDOT = 2147
982434 TA = 175
62428
MA = 175
61276
Ha = 189
256 n
mi
Hp = 182
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13169769
13 X = 4062181
96
Y = -7136311
87 feet Y = -2129990
52 meter
Z = -16216603
47 Z = -4923203
05
XDOT = 17667
603532 XDOT = 5317
730579
YDOT = 16582
906069 feet/sec YDOT = 5114
312401 meter/sec
ZDOT = 7047
186464 ZDOT = 2173
980175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9986264
37 X = 3043813
38
Y = -11279003
72 feet Y = -3437840
33 meter
Z = -16137118
49 Z = -4918593
71
XDOT = 21444
695142 XDOT = 6536
343079
YDOT = 8749
106778 feet/sec YDOT = 2666
727746 meter/sec
ZDOT = 7152
153308 ZDOT = 2179
976328
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 11123
45659311
00016717 00000-0 10270-3 0 9021
2 25544 51
6461 30
4646 0002225 185
3510 174
7630 15
74612517 33869
Satellite: ISS
Catalog Number: 25544
Epoch time: 11123
45659311 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 30
4646 deg
Eccentricity:
0002225
Arg of perigee: 185
3510 deg
Mean anomaly: 174
7630 deg
Mean motion: 15
74612517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3386
Checksum: 284
Coasting Arc #4 (Orbit 3401)
---------------------------------------
Vector Time (GMT): 2011/124/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4898872
92 A = 6728194
07 meter
Y = -4097238
69 meter E =
0007928
Z = -2106697
45 I = 51
80639
XDOT = 4617
691043 Wp = 151
37641
YDOT = -2674
288796 meter/sec RA = 24
86607 deg
ZDOT = -5552
134585 TA = 52
11407
MA = 52
04240
Ha = 189
008 n
mi
Hp = 182
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16072417
71 X = -4842458
59
Y = -13442384
16 feet Y = -4151705
33 meter
Z = -6911737
03 Z = -2130359
74
XDOT = 15149
904997 XDOT = 4674
223963
YDOT = -8773
913373 feet/sec YDOT = -2622
334607 meter/sec
ZDOT = -18215
664649 ZDOT = -5529
564281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19805350
33 X = -6036670
78
Y = -6740800
55 feet Y = -2054596
01 meter
Z = -7007290
37 Z = -2135822
11
XDOT = 10564
821419 XDOT = 3220
157568
YDOT = -12251
811803 feet/sec YDOT = -3734
352238 meter/sec
ZDOT = -18124
204874 ZDOT = -5524
257646
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 11124
47199959
00016717 00000-0 10270-3 0 9032
2 25544 51
6467 25
2458 0002288 191
3450 168
7662 15
74700894 34020
Satellite: ISS
Catalog Number: 25544
Epoch time: 11124
47199959 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 25
2458 deg
Eccentricity:
0002288
Arg of perigee: 191
3450 deg
Mean anomaly: 168
7662 deg
Mean motion: 15
74700894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3402
Checksum: 326
Coasting Arc #5 (Orbit 3417)
---------------------------------------
Vector Time (GMT): 2011/125/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4060665
19 A = 6720264
47 meter
Y = 2505067
40 meter E =
0006326
Z = 4727985
18 I = 51
75139
XDOT = -5791
006978 Wp = 76
28093
YDOT = -4318
031866 meter/sec RA = 19
69575 deg
ZDOT = -2681
337679 TA = 40
04489
MA = 39
99827
Ha = 188
921 n
mi
Hp = 182
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13322392
37 X = -4111343
56
Y = 8218725
07 feet Y = 2459374
91 meter
Z = 15511762
40 Z = 4708135
26
XDOT = -18999
366725 XDOT = -5729
265876
YDOT = -14166
771215 feet/sec YDOT = -4382
445028 meter/sec
ZDOT = -8797
039629 ZDOT = -2709
321107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9321351
34 X = -2841147
89
Y = 12674197
03 feet Y = 3863095
26 meter
Z = 15431315
30 Z = 4703464
90
XDOT = -21967
574027 XDOT = -6695
716564
YDOT = -5290
028532 feet/sec YDOT = -1612
400697 meter/sec
ZDOT = -8910
062240 ZDOT = -2715
786971
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 11125
48734877
00016717 00000-0 10270-3 0 9049
2 25544 51
6461 20
0269 0002287 197
4054 162
7032 15
74796558 34187
Satellite: ISS
Catalog Number: 25544
Epoch time: 11125
48734877 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 20
0269 deg
Eccentricity:
0002287
Arg of perigee: 197
4054 deg
Mean anomaly: 162
7032 deg
Mean motion: 15
74796558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3418
Checksum: 320
Coasting Arc #6 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2011/126/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5151051
19 A = 6726717
24 meter
Y = 3454351
10 meter E =
0012557
Z = 2592244
90 I = 51
74498
XDOT = -4714
493084 Wp = 85
71561
YDOT = 3062
546904 meter/sec RA = 14
60446 deg
ZDOT = 5266
255706 TA = 303
69663
MA = 303
81628
Ha = 188
592 n
mi
Hp = 182
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16899774
25 X = 5099448
34
Y = 11333172
91 feet Y = 3511664
55 meter
Z = 8504740
50 Z = 2617143
90
XDOT = -15467
496995 XDOT = -4773
971467
YDOT = 10047
726064 feet/sec YDOT = 3009
493615 meter/sec
ZDOT = 17277
741818 ZDOT = 5243
208212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19947984
49 X = 6080145
67
Y = 3794751
29 feet Y = 1156640
19 meter
Z = 8605321
97 Z = 2622902
14
XDOT = -10087
929533 XDOT = -3074
800922
YDOT = 13907
457229 feet/sec YDOT = 4238
992963 meter/sec
ZDOT = 17184
323956 ZDOT = 5237
781942
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 11126
50264129
00016717 00000-0 10270-3 0 9052
2 25544 51
6464 14
8065 0002309 202
7904 157
3158 15
74867920 34343
Satellite: ISS
Catalog Number: 25544
Epoch time: 11126
50264129 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 14
8065 deg
Eccentricity:
0002309
Arg of perigee: 202
7904 deg
Mean anomaly: 157
3158 deg
Mean motion: 15
74867920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 299
Coasting Arc #7 (Orbit 3448)
---------------------------------------
Vector Time (GMT): 2011/127/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4189388
35 A = 6721010
27 meter
Y = -2848535
72 meter E =
0009221
Z = -4426075
62 I = 51
69682
XDOT = 5938
373742 Wp = 124
95434
YDOT = 3620
038027 meter/sec RA = 9
42158 deg
ZDOT = 3290
666710 TA = 178
07288
MA = 178
06932
Ha = 188
361 n
mi
Hp = 182
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13744712
43 X = 4242431
07
Y = -9345589
62 feet Y = -2801390
51 meter
Z = -14521245
47 Z = -4405594
81
XDOT = 19482
853485 XDOT = 5881
466856
YDOT = 11876
765181 feet/sec YDOT = 3686
126081 meter/sec
ZDOT = 10796
150622 ZDOT = 3319
377586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8798964
14 X = 2681924
27
Y = -14185898
34 feet Y = -4323861
81 meter
Z = -14438221
96 Z = -4400770
05
XDOT = 21542
799099 XDOT = 6566
245165
YDOT = 2254
704689 feet/sec YDOT = 687
233989 meter/sec
ZDOT = 10912
147918 ZDOT = 3326
022685
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 11127
45442505
00016717 00000-0 10270-3 0 9064
2 25544 51
6469 9
9124 0002367 210
1316 149
9711 15
74965833 34493
Satellite: ISS
Catalog Number: 25544
Epoch time: 11127
45442505 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 9
9124 deg
Eccentricity:
0002367
Arg of perigee: 210
1316 deg
Mean anomaly: 149
9711 deg
Mean motion: 15
74965833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3449
Checksum: 311
Coasting Arc #8 (Orbit 3464)
---------------------------------------
Vector Time (GMT): 2011/128/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5168505
00 A = 6724743
96 meter
Y = -2905657
92 meter E =
0004035
Z = -3172228
09 I = 51
68020
XDOT = 4901
807299 Wp = 131
43089
YDOT = -3455
378399 meter/sec RA = 4
33088 deg
ZDOT = -4828
055444 TA = 85
53056
MA = 85
48447
Ha = 188
070 n
mi
Hp = 182
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16957037
41 X = -5120219
08
Y = -9532998
42 feet Y = -2963185
07 meter
Z = -10407572
47 Z = -3197219
69
XDOT = 16082
044943 XDOT = 4963
535578
YDOT = -11336
543303 feet/sec YDOT = -3400
217923 meter/sec
ZDOT = -15840
076916 ZDOT = -4804
092701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19343829
12 X = -5895999
11
Y = -1457142
71 feet Y = -444137
10 meter
Z = -10508556
11 Z = -3203007
90
XDOT = 9725
169533 XDOT = 2964
231674
YDOT = -15723
036465 feet/sec YDOT = -4792
381515 meter/sec
ZDOT = -15742
930616 ZDOT = -4798
445252
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 11128
46960649
00016717 00000-0 10270-3 0 9071
2 25544 51
6472 4
6916 0002514 217
8098 142
2889 15
75042010 34657
Satellite: ISS
Catalog Number: 25544
Epoch time: 11128
46960649 = yrday
fracday
Element set: 907
Inclination: 51
6472 deg
RA of node: 4
6916 deg
Eccentricity:
0002514
Arg of perigee: 217
8098 deg
Mean anomaly: 142
2889 deg
Mean motion: 15
75042010 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3465
Checksum: 312
Coasting Arc #9 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2011/129/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4368876
90 A = 6722121
70 meter
Y = 3207255
22 meter E =
0009215
Z = 3968989
72 I = 51
64103
XDOT = -5855
838931 Wp = 87
64885
YDOT = -3053
973644 meter/sec RA = 359
13789 deg
ZDOT = -3969
719914 TA = 43
45839
MA = 43
38579
Ha = 187
958 n
mi
Hp = 182
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14333585
62 X = -4423696
98
Y = 10522490
89 feet Y = 3158093
04 meter
Z = 13021619
80 Z = 3947632
73
XDOT = -19212
069984 XDOT = -5801
969398
YDOT = -10019
598570 feet/sec YDOT = -3119
155754 meter/sec
ZDOT = -13024
015467 ZDOT = -3998
036930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8308503
43 X = -2532431
85
Y = 15792112
20 feet Y = 4813435
80 meter
Z = 12935031
36 Z = 3942597
56
XDOT = -20439
410773 XDOT = -6229
932404
YDOT = 30
285338 feet/sec YDOT = 9
230971 meter/sec
ZDOT = -13138
448735 ZDOT = -4004
599174
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 11129
48473128
00016717 00000-0 10270-3 0 9086
2 25544 51
6469 359
4705 0002418 223
4000 136
6974 15
75152738 34818
Satellite: ISS
Catalog Number: 25544
Epoch time: 11129
48473128 = yrday
fracday
Element set: 908
Inclination: 51
6469 deg
RA of node: 359
4705 deg
Eccentricity:
0002418
Arg of perigee: 223
4000 deg
Mean anomaly: 136
6974 deg
Mean motion: 15
75152738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 318
Coasting Arc #10 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2011/130/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4996015
68 A = 6722495
64 meter
Y = 2469007
28 meter E =
0010084
Z = 3754084
97 I = 51
61277
XDOT = -5118
453816 Wp = 107
62238
YDOT = 3904
513159 meter/sec RA = 354
04401 deg
ZDOT = 4231
515435 TA = 297
83918
MA = 297
94133
Ha = 187
614 n
mi
Hp = 182
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16391127
55 X = 4949798
78
Y = 8100417
58 feet Y = 2524617
19 meter
Z = 12316551
74 Z = 3778243
46
XDOT = -16792
827479 XDOT = -5182
290351
YDOT = 12810
082542 feet/sec YDOT = 3846
918397 meter/sec
ZDOT = 13882
924654 ZDOT = 4206
495085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18215989
14 X = 5552233
49
Y = -221334
50 feet Y = -67462
76 meter
Z = 12414186
43 Z = 3783844
02
XDOT = -9203
496056 XDOT = -2805
225598
YDOT = 17763
452438 feet/sec YDOT = 5414
300303 meter/sec
ZDOT = 13781
478998 ZDOT = 4200
594799
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 11130
49979968
00016717 00000-0 10270-3 0 9093
2 25544 51
6473 354
2485 0002459 229
5870 130
5080 15
75211329 34978
Satellite: ISS
Catalog Number: 25544
Epoch time: 11130
49979968 = yrday
fracday
Element set: 909
Inclination: 51
6473 deg
RA of node: 354
2485 deg
Eccentricity:
0002459
Arg of perigee: 229
5870 deg
Mean anomaly: 130
5080 deg
Mean motion: 15
75211329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 335
Coasting Arc #11 (Orbit 3511)
---------------------------------------
Vector Time (GMT): 2011/131/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4560694
39 A = 6723597
35 meter
Y = -3619657
89 meter E =
0002800
Z = -3365689
43 I = 51
58662
XDOT = 5534
978721 Wp = 115
39391
YDOT = 2659
890146 meter/sec RA = 348
84443 deg
ZDOT = 4641
414832 TA = 204
91122
MA = 204
92473
Ha = 187
375 n
mi
Hp = 182
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14962908
12 X = 4617181
08
Y = -11875518
01 feet Y = -3568341
52 meter
Z = -11042288
17 Z = -3343396
42
XDOT = 18159
379005 XDOT = 5482
276750
YDOT = 8726
673707 feet/sec YDOT = 2721
490854 meter/sec
ZDOT = 15227
738950 ZDOT = 4668
175858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7668192
85 X = 2337265
18
Y = -17552875
23 feet Y = -5350116
37 meter
Z = -10951897
77 Z = -3338138
44
XDOT = 18769
020716 XDOT = 5720
797514
YDOT = -1365
413531 feet/sec YDOT = -416
178044 meter/sec
ZDOT = 15335
893389 ZDOT = 4674
380305
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 11131
45137307
00016717 00000-0 10270-3 0 9105
2 25544 51
6473 349
3530 0002662 238
4849 121
6055 15
75310040 35126
Satellite: ISS
Catalog Number: 25544
Epoch time: 11131
45137307 = yrday
fracday
Element set: 910
Inclination: 51
6473 deg
RA of node: 349
3530 deg
Eccentricity:
0002662
Arg of perigee: 238
4849 deg
Mean anomaly: 121
6055 deg
Mean motion: 15
75310040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3512
Checksum: 275
Coasting Arc #12 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2011/132/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4621140
46 A = 6719905
85 meter
Y = -2242141
90 meter E =
0006316
Z = -4339356
86 I = 51
54486
XDOT = 5329
634032 Wp = 70
83845
YDOT = -4379
134401 meter/sec RA = 343
74338 deg
ZDOT = -3415
022097 TA = 164
65952
MA = 164
64037
Ha = 187
081 n
mi
Hp = 182
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15161221
97 X = -4574645
01
Y = -7356108
60 feet Y = -2293558
27 meter
Z = -14236735
12 Z = -4361693
58
XDOT = 17485
675957 XDOT = 5394
795890
YDOT = -14367
238848 feet/sec YDOT = -4319
170812 meter/sec
ZDOT = -11204
140737 ZDOT = -3388
972371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16750981
43 X = -5105699
14
Y = 895081
61 feet Y = 272820
87 meter
Z = -14327004
65 Z = -4366871
02
XDOT = 8425
464693 XDOT = 2568
081638
YDOT = -19864
733190 feet/sec YDOT = -6054
770676 meter/sec
ZDOT = -11098
516584 ZDOT = -3382
827855
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 11132
46633034
00016717 00000-0 10270-3 0 9116
2 25544 51
6468 344
1307 0002819 244
8470 115
2401 15
75396274 35284
Satellite: ISS
Catalog Number: 25544
Epoch time: 11132
46633034 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 344
1307 deg
Eccentricity:
0002819
Arg of perigee: 244
8470 deg
Mean anomaly: 115
2401 deg
Mean motion: 15
75396274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3528
Checksum: 294
Coasting Arc #13 (Orbit 3543)
---------------------------------------
Vector Time (GMT): 2011/133/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4724961
19 A = 6725131
20 meter
Y = 4037137
82 meter E =
0011670
Z = 2553943
61 I = 51
53411
XDOT = -5018
414971 Wp = 111
07682
YDOT = -2528
371786 meter/sec RA = 338
54386 deg
ZDOT = -5272
521496 TA = 39
88082
MA = 39
79513
Ha = 186
953 n
mi
Hp = 182
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15501841
19 X = -4782160
80
Y = 13245202
84 feet Y = 3983980
58 meter
Z = 8379080
09 Z = 2530850
63
XDOT = -16464
616048 XDOT = -4964
156028
YDOT = -8295
183025 feet/sec YDOT = -2584
187300 meter/sec
ZDOT = -17298
298871 ZDOT = -5296
769446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6826579
08 X = -2080741
30
Y = 19253590
12 feet Y = 5868494
27 meter
Z = 8285441
88 Z = 2525402
69
XDOT = -16911
747955 XDOT = -5154
700777
YDOT = 1511
570349 feet/sec YDOT = 460
726642 meter/sec
ZDOT = -17396
282898 ZDOT = -5302
387027
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
48123112
00016717 00000-0 10270-3 0 9121
2 25544 51
6470 338
9083 0002727 250
2323 109
8547 15
75501018 35447
Satellite: ISS
Catalog Number: 25544
Epoch time: 11133
48123112 = yrday
fracday
Element set: 912
Inclination: 51
6470 deg
RA of node: 338
9083 deg
Eccentricity:
0002727
Arg of perigee: 250
2323 deg
Mean anomaly: 109
8547 deg
Mean motion: 15
75501018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3544
Checksum: 282
Coasting Arc #14 (Orbit 3559)
---------------------------------------
Vector Time (GMT): 2011/134/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4102639
49 A = 6717526
73 meter
Y = 2240664
24 meter E =
0005275
Z = 4823087
68 I = 51
48001
XDOT = -5474
004820 Wp = 143
56768
YDOT = 4865
436086 meter/sec RA = 333
42768 deg
ZDOT = 2390
474702 TA = 283
03756
MA = 283
09645
Ha = 186
654 n
mi
Hp = 182
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13460103
33 X = 4053848
99
Y = 7351260
63 feet Y = 2286269
51 meter
Z = 15823778
48 Z = 4842900
15
XDOT = -17959
333400 XDOT = -5539
616885
YDOT = 15962
716817 feet/sec YDOT = 4803
855517 meter/sec
ZDOT = 7842
764771 ZDOT = 2363
722343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15242189
76 X = 4645819
44
Y = -592740
54 feet Y = -180667
32 meter
Z = 15903826
26 Z = 4847486
24
XDOT = -7239
064047 XDOT = -2206
466722
YDOT = 21850
570908 feet/sec YDOT = 6660
054013 meter/sec
ZDOT = 7734
282677 ZDOT = 2357
409360
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
49607491
00016717 00000-0 10270-3 0 9131
2 25544 51
6461 333
6846 0002803 255
8956 104
1897 15
75548361 35600
Satellite: ISS
Catalog Number: 25544
Epoch time: 11134
49607491 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 333
6846 deg
Eccentricity:
0002803
Arg of perigee: 255
8956 deg
Mean anomaly: 104
1897 deg
Mean motion: 15
75548361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3560
Checksum: 325
Coasting Arc #15 (Orbit 3574)
---------------------------------------
Vector Time (GMT): 2011/135/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 893685
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4799896
46 A = 6726445
04 meter
Y = -4438832
23 meter E =
0006440
Z = -1566770
55 I = 51
48277
XDOT = 4358
949724 Wp = 17
11383
YDOT = 2686
999093 meter/sec RA = 328
23425 deg
ZDOT = 5753
374666 TA = 325
55714
MA = 325
59886
Ha = 186
487 n
mi
Hp = 182
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15747691
81 X = 4856786
82
Y = -14563097
86 feet Y = -4384838
70 meter
Z = -5140323
33 Z = -1543314
26
XDOT = 14301
016155 XDOT = 4300
629844
YDOT = 8815
613823 feet/sec YDOT = 2735
417131 meter/sec
ZDOT = 18875
901136 ZDOT = 5774
409315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5653399
88 X = 1723156
28
Y = -20714284
38 feet Y = -6313713
88 meter
Z = -5045199
01 Z = -1537776
66
XDOT = 15193
286976 XDOT = 4630
913870
YDOT = -461
745876 feet/sec YDOT = -140
740143 meter/sec
ZDOT = 18960
867295 ZDOT = 5779
272351
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
44743632
00016717 00000-0 10270-3 0 9146
2 25544 51
6450 328
7868 0003073 262
3764 97
7051 15
75651792 35755
Satellite: ISS
Catalog Number: 25544
Epoch time: 11135
44743632 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 328
7868 deg
Eccentricity:
0003073
Arg of perigee: 262
3764 deg
Mean anomaly: 97
7051 deg
Mean motion: 15
75651792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3575
Checksum: 325
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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