[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 11th 2012
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) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
018/02:17:47
722 4
3 4
9 4
9
N/A 0
4 -0
0 216
3
000/00:01:35
444 -2
4 0
0 206
9
Coasting Arc #1 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2012/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1390412
85 A = 6763218
95 meter
Y = -3988784
67 meter E =
0021703
Z = 5300433
85 I = 51
48294
XDOT = 7149
199147 Wp = 260
83277
YDOT = 2745
361992 meter/sec RA = 202
12615 deg
ZDOT = 187
883228 TA = 187
35496
MA = 187
38685
Ha = 215
899 n
mi
Hp = 204
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4561721
93 X = 1409164
99
Y = -13086563
87 feet Y = -3973131
91 meter
Z = 17389874
85 Z = 5307233
45
XDOT = 23455
377779 XDOT = 7117
055938
YDOT = 9007
093151 feet/sec YDOT = 2825
128988 meter/sec
ZDOT = 616
414791 ZDOT = 222
535382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13820690
97 X = 4212546
61
Y = 280508
91 feet Y = 85499
12 meter
Z = 17417951
20 Z = 5308991
53
XDOT = -1455
096525 XDOT = -443
513421
YDOT = 24070
269665 feet/sec YDOT = 7336
618194 meter/sec
ZDOT = 758
005443 ZDOT = 231
040059
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 12009
54843757
00016717 00000-0 10270-3 0 9002
2 25544 51
6375 202
9297 0024051 262
6777 97
1645 15
59005547 33121
Satellite: ISS
Catalog Number: 25544
Epoch time: 12009
54843757 = yrday
fracday
Element set: 900
Inclination: 51
6375 deg
RA of node: 202
9297 deg
Eccentricity:
0024051
Arg of perigee: 262
6777 deg
Mean anomaly: 97
1645 deg
Mean motion: 15
59005547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 317
Coasting Arc #2 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2012/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4695420
16 A = 6766775
58 meter
Y = 2174651
22 meter E =
0016313
Z = -4349697
58 I = 51
52360
XDOT = -5244
283004 Wp = 253
32298
YDOT = -4453
064201 meter/sec RA = 197
06759 deg
ZDOT = 3419
573125 TA = 51
39878
MA = 51
25281
Ha = 215
621 n
mi
Hp = 204
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15404921
79 X = -4698259
10
Y = 7134682
48 feet Y = 2122128
62 meter
Z = -14270661
36 Z = -4372514
04
XDOT = -17205
652900 XDOT = -5210
709401
YDOT = -14609
790685 feet/sec YDOT = -4511
521549 meter/sec
ZDOT = 11219
071933 ZDOT = 3394
178283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11653327
66 X = -3551934
27
Y = -12236748
14 feet Y = -3729760
83 meter
Z = -14364157
99 Z = -4378195
36
XDOT = 7433
611619 XDOT = 2265
764821
YDOT = -20185
287385 feet/sec YDOT = -6152
475595 meter/sec
ZDOT = 11115
446013 ZDOT = 3387
987945
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 12010
50991132
00016717 00000-0 10270-3 0 9012
2 25544 51
6367 198
0987 0024062 266
1244 93
7160 15
59080369 33278
Satellite: ISS
Catalog Number: 25544
Epoch time: 12010
50991132 = yrday
fracday
Element set: 901
Inclination: 51
6367 deg
RA of node: 198
0987 deg
Eccentricity:
0024062
Arg of perigee: 266
1244 deg
Mean anomaly: 93
7160 deg
Mean motion: 15
59080369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 304
Coasting Arc #3 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2012/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6546468
69 A = 6773434
33 meter
Y = -10005
94 meter E =
0012835
Z = 1734780
20 I = 51
57651
XDOT = 1503
370509 Wp = 244
35831
YDOT = 4930
411684 meter/sec RA = 192
04703 deg
ZDOT = -5682
957443 TA = 276
55731
MA = 276
70342
Ha = 215
624 n
mi
Hp = 204
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21477915
63 X = 6537667
01
Y = -32827
88 feet Y = 63151
39 meter
Z = 5691536
09 Z = 1766560
69
XDOT = 4932
317942 XDOT = 1475
731942
YDOT = 16175
891351 feet/sec YDOT = 4947
069081 meter/sec
ZDOT = -18644
873500 ZDOT = -5675
721126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7228888
09 X = 2203365
09
Y = 20187813
11 feet Y = 6153245
44 meter
Z = 5821589
09 Z = 1774420
36
XDOT = -12070
459124 XDOT = -3679
075941
YDOT = 9655
087666 feet/sec YDOT = 2942
870721 meter/sec
ZDOT = -18615
568259 ZDOT = -5674
025205
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 12011
53546487
00016717 00000-0 10270-3 0 9026
2 25544 51
6374 192
9480 0024235 270
6183 89
2195 15
59146054 33431
Satellite: ISS
Catalog Number: 25544
Epoch time: 12011
53546487 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 192
9480 deg
Eccentricity:
0024235
Arg of perigee: 270
6183 deg
Mean anomaly: 89
2195 deg
Mean motion: 15
59146054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 311
Coasting Arc #4 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2012/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6239628
65 A = 6773753
91 meter
Y = -2067967
98 meter E =
0013991
Z = 1623730
83 I = 51
60687
XDOT = 2877
679562 Wp = 304
85733
YDOT = -4218
208776 meter/sec RA = 187
04887 deg
ZDOT = 5728
789278 TA = 72
95908
MA = 72
80584
Ha = 215
660 n
mi
Hp = 204
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20471222
61 X = -6223928
06
Y = -6784671
85 feet Y = -2137655
62 meter
Z = 5327200
90 Z = 1593457
58
XDOT = 9441
205913 XDOT = 2896
805848
YDOT = -13839
267637 feet/sec YDOT = -4185
922056 meter/sec
ZDOT = 18795
240412 ZDOT = 5742
814984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -863392
79 X = -263162
12
Y = -21579171
96 feet Y = -6577331
61 meter
Z = 5203430
33 Z = 1586005
56
XDOT = 14661
485848 XDOT = 4468
820887
YDOT = 3924
768514 feet/sec YDOT = 1196
269443 meter/sec
ZDOT = 18852
901408 ZDOT = 5746
364349
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 12012
56100296
00016717 00000-0 10270-3 0 9035
2 25544 51
6370 187
7948 0024007 273
9188 85
9222 15
59129701 33597
Satellite: ISS
Catalog Number: 25544
Epoch time: 12012
56100296 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 187
7948 deg
Eccentricity:
0024007
Arg of perigee: 273
9188 deg
Mean anomaly: 85
9222 deg
Mean motion: 15
59129701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 316
Coasting Arc #5 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2012/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3832920
50 A = 6766875
28 meter
Y = 3542440
02 meter E =
0016887
Z = -4297354
65 I = 51
61538
XDOT = -6330
634930 Wp = 291
71089
YDOT = 2562
709857 meter/sec RA = 182
03406 deg
ZDOT = -3516
733475 TA = 302
47342
MA = 302
63657
Ha = 215
631 n
mi
Hp = 204
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12575198
49 X = 3813898
64
Y = 11622178
53 feet Y = 3585195
83 meter
Z = -14098932
59 Z = -4278780
89
XDOT = -20769
799640 XDOT = -6341
737898
YDOT = 8407
840738 feet/sec YDOT = 2491
854799 meter/sec
ZDOT = -11537
839484 ZDOT = -3547
513898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6148620
28 X = -1874099
46
Y = 16047958
83 feet Y = 4891417
85 meter
Z = -14023125
08 Z = -4274248
52
XDOT = -14262
581801 XDOT = -4347
234933
YDOT = -15706
443407 feet/sec YDOT = -4787
323951 meter/sec
ZDOT = -11663
980078 ZDOT = -3555
181128
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 12013
52242583
00016717 00000-0 10270-3 0 9049
2 25544 51
6379 182
9663 0023836 277
8165 82
0285 15
59180139 33740
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
52242583 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 182
9663 deg
Eccentricity:
0023836
Arg of perigee: 277
8165 deg
Mean anomaly: 82
0285 deg
Mean motion: 15
59180139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 323
Coasting Arc #6 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2012/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -84618
75 A = 6762813
10 meter
Y = -4207087
37 meter E =
0021435
Z = 5312303
76 I = 51
63159
XDOT = 7654
026072 Wp = 283
55564
YDOT = -309
294136 meter/sec RA = 176
98414 deg
ZDOT = -118
518872 TA = 167
60137
MA = 167
54855
Ha = 215
692 n
mi
Hp = 204
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -277620
57 X = -63373
68
Y = -13802780
08 feet Y = -4207914
93 meter
Z = 17428818
11 Z = 5311944
22
XDOT = 25111
634094 XDOT = 7657
491528
YDOT = -1014
744540 feet/sec YDOT = -223
682730 meter/sec
ZDOT = -388
841444 ZDOT = -81
327920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12597482
15 X = 3839712
56
Y = -5651518
71 feet Y = -1722582
90 meter
Z = 17427601
43 Z = 5311932
92
XDOT = 10164
404692 XDOT = 3098
110550
YDOT = 21881
735074 feet/sec YDOT = 6669
552850 meter/sec
ZDOT = -236
586119 ZDOT = -72
111449
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 12014
54792664
00016717 00000-0 10270-3 0 9053
2 25544 51
6375 177
8134 0023760 281
6226 78
2263 15
59139923 33905
Satellite: ISS
Catalog Number: 25544
Epoch time: 12014
54792664 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 177
8134 deg
Eccentricity:
0023760
Arg of perigee: 281
6226 deg
Mean anomaly: 78
2263 deg
Mean motion: 15
59139923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 322
Coasting Arc #7 (Orbit 3404)
---------------------------------------
Vector Time (GMT): 2012/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3660007
13 A = 6767021
38 meter
Y = 3851337
02 meter E =
0015828
Z = -4175268
56 I = 51
67811
XDOT = -6408
054028 Wp = 282
97765
YDOT = -2055
937186 meter/sec RA = 171
93858 deg
ZDOT = 3712
490233 TA = 25
06230
MA = 24
98555
Ha = 215
648 n
mi
Hp = 204
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12007897
40 X = -3682519
14
Y = 12635620
16 feet Y = 3810282
80 meter
Z = -13698387
65 Z = -4193103
18
XDOT = -21023
799303 XDOT = -6402
622191
YDOT = -6745
200740 feet/sec YDOT = -2127
565707 meter/sec
ZDOT = 12180
086066 ZDOT = 3681
373536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16347721
78 X = -4982785
60
Y = -5881194
33 feet Y = -1792588
03 meter
Z = -13771632
69 Z = -4197593
64
XDOT = -2678
219038 XDOT = -816
321163
YDOT = -20842
471590 feet/sec YDOT = -6352
785341 meter/sec
ZDOT = 12052
827668 ZDOT = 3673
701873
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 12015
50931234
00016717 00000-0 10270-3 0 9069
2 25544 51
6386 172
9836 0023793 285
0496 74
8027 15
59221451 34050
Satellite: ISS
Catalog Number: 25544
Epoch time: 12015
50931234 = yrday
fracday
Element set: 906
Inclination: 51
6386 deg
RA of node: 172
9836 deg
Eccentricity:
0023793
Arg of perigee: 285
0496 deg
Mean anomaly: 74
8027 deg
Mean motion: 15
59221451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 313
Coasting Arc #8 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2012/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6123054
68 A = 6773579
91 meter
Y = -2547674
97 meter E =
0010548
Z = 1390626
20 I = 51
72947
XDOT = 2982
385072 Wp = 276
03558
YDOT = 4015
192152 meter/sec RA = 166
93078 deg
ZDOT = -5812
507959 TA = 248
81130
MA = 248
92404
Ha = 215
885 n
mi
Hp = 204
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20088762
06 X = 6144332
89
Y = -8358513
69 feet Y = -2479084
30 meter
Z = 4562421
91 Z = 1420423
18
XDOT = 9784
727928 XDOT = 2965
500471
YDOT = 13173
202597 feet/sec YDOT = 4048
448852 meter/sec
ZDOT = -19069
908002 ZDOT = -5798
060568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15935765
27 X = 4857221
25
Y = 14776500
79 feet Y = 4503877
44 meter
Z = 4684572
09 Z = 1427857
57
XDOT = -6792
278113 XDOT = -2070
286369
YDOT = 13314
944541 feet/sec YDOT = 4058
395096 meter/sec
ZDOT = -19011
005965 ZDOT = -5794
554618
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 12016
53477215
00016717 00000-0 10270-3 0 9078
2 25544 51
6377 167
8319 0023935 289
1261 70
7304 15
59258628 34219
Satellite: ISS
Catalog Number: 25544
Epoch time: 12016
53477215 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 167
8319 deg
Eccentricity:
0023935
Arg of perigee: 289
1261 deg
Mean anomaly: 70
7304 deg
Mean motion: 15
59258628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 321
Coasting Arc #9 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2012/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6445581
70 A = 6772666
92 meter
Y = 434607
40 meter E =
0016978
Z = 2010656
71 I = 51
75730
XDOT = 1388
723252 Wp = 328
32260
YDOT = -5083
314722 meter/sec RA = 161
94328 deg
ZDOT = 5586
029392 TA = 53
91060
MA = 53
75350
Ha = 216
036 n
mi
Hp = 204
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21146921
59 X = -6459729
79
Y = 1425877
31 feet Y = 362449
71 meter
Z = 6596642
75 Z = 1979310
15
XDOT = 4556
178649 XDOT = 1418
327118
YDOT = -16677
541739 feet/sec YDOT = -5067
620002 meter/sec
ZDOT = 18326
868084 ZDOT = 5592
847299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10417504
28 X = -3175255
31
Y = -18503466
76 feet Y = -5639856
67 meter
Z = 6468263
82 Z = 1971526
81
XDOT = 15614
716593 XDOT = 4759
365618
YDOT = -2416
155160 feet/sec YDOT = -736
444093 meter/sec
ZDOT = 18355
103326 ZDOT = 5594
635494
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 12017
56021217
00016717 00000-0 10270-3 0 9080
2 25544 51
6390 162
6793 0023800 292
7821 67
0820 15
59303530 34378
Satellite: ISS
Catalog Number: 25544
Epoch time: 12017
56021217 = yrday
fracday
Element set: 908
Inclination: 51
6390 deg
RA of node: 162
6793 deg
Eccentricity:
0023800
Arg of perigee: 292
7821 deg
Mean anomaly: 67
0820 deg
Mean motion: 15
59303530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 292
Coasting Arc #10 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2012/018/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3037517
51 A = 6770135
56 meter
Y = -4551138
43 meter E =
0013056
Z = 4001561
74 I = 51
75811
XDOT = 6500
642763 Wp = 323
27623
YDOT = 845
913350 meter/sec RA = 158
91479 deg
ZDOT = -3968
905969 TA = 167
99495
MA = 167
96380
Ha = 216
303 n
mi
Hp = 206
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9965608
62 X = 3068744
91
Y = -14931556
53 feet Y = -4516996
75 meter
Z = 13128483
41 Z = 4016393
29
XDOT = 21327
568120 XDOT = 6509
980397
YDOT = 2775
306267 feet/sec YDOT = 918
660053 meter/sec
ZDOT = -13021
345042 ZDOT = -3937
303551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15918905
67 X = -4852082
45
Y = 8200438
88 feet Y = 2499493
77 meter
Z = 13189505
55 Z = 4020161
29
XDOT = -16726
126643 XDOT = -5098
123401
YDOT = -11715
302574 feet/sec YDOT = -3570
824225 meter/sec
ZDOT = -12891
989540 ZDOT = -3929
478412
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 12018
13704528
00016717 00000-0 10270-3 0 9098
2 25544 51
6399 159
7871 0020249 294
1477 65
7560 15
58377856 34465
Satellite: ISS
Catalog Number: 25544
Epoch time: 12018
13704528 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 159
7871 deg
Eccentricity:
0020249
Arg of perigee: 294
1477 deg
Mean anomaly: 65
7560 deg
Mean motion: 15
58377856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 347
Coasting Arc #11 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2012/019/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5409052
47 A = 6776135
82 meter
Y = 3829206
10 meter E =
0020770
Z = -1348831
99 I = 51
80633
XDOT = -3776
933602 Wp = 322
71747
YDOT = -3267
113738 meter/sec RA = 153
91845 deg
ZDOT = 5840
466681 TA = 22
58222
MA = 22
49096
Ha = 216
549 n
mi
Hp = 206
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17746235
14 X = -5444917
14
Y = 12563012
12 feet Y = 3768518
34 meter
Z = -4425301
79 Z = -1375195
44
XDOT = -12391
514441 XDOT = -3768
490789
YDOT = -10718
877094 feet/sec YDOT = -3309
303076 meter/sec
ZDOT = 19161
636093 ZDOT = 5822
138867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21554805
03 X = 6569904
57
Y = -2679368
54 feet Y = -816671
53 meter
Z = -4533519
14 Z = -1381816
63
XDOT = 5749
192536 XDOT = 1752
353885
YDOT = 13789
478276 feet/sec YDOT = 4203
032979 meter/sec
ZDOT = 19086
785293 ZDOT = 5817
652157
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 12019
09893144
00016717 00000-0 10270-3 0 9109
2 25544 51
6399 154
9599 0020358 298
0700 61
8397 15
58399167 34613
Satellite: ISS
Catalog Number: 25544
Epoch time: 12019
09893144 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 154
9599 deg
Eccentricity:
0020358
Arg of perigee: 298
0700 deg
Mean anomaly: 61
8397 deg
Mean motion: 15
58399167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 346
Coasting Arc #12 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2012/020/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6191859
98 A = 6775597
64 meter
Y = -2126525
11 meter E =
0013412
Z = -1746655
37 I = 51
83262
XDOT = 146
523254 Wp = 290
76173
YDOT = 5136
272625 meter/sec RA = 148
94078 deg
ZDOT = -5694
017283 TA = 268
37801
MA = 268
53165
Ha = 216
770 n
mi
Hp = 206
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20314501
26 X = 6223663
76
Y = -6976788
41 feet Y = -2057105
92 meter
Z = -5730496
61 Z = -1716498
97
XDOT = 480
719337 XDOT = 116
737399
YDOT = 16851
288139 feet/sec YDOT = 5137
745166 meter/sec
ZDOT = -18681
159065 ZDOT = -5693
377323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21284310
95 X = -6487457
98
Y = -3120037
88 feet Y = -950987
55 meter
Z = -5606835
13 Z = -1708963
35
XDOT = 6963
720653 XDOT = 2122
542055
YDOT = -13698
121222 feet/sec YDOT = -4175
187348 meter/sec
ZDOT = -18678
872615 ZDOT = -5693
320373
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 12020
12492482
00016717 00000-0 10270-3 0 9116
2 25544 51
6409 149
8120 0020323 301
8764 58
0413 15
58433943 34778
Satellite: ISS
Catalog Number: 25544
Epoch time: 12020
12492482 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 149
8120 deg
Eccentricity:
0020323
Arg of perigee: 301
8764 deg
Mean anomaly: 58
0413 deg
Mean motion: 15
58433943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 288
Coasting Arc #13 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2012/021/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5229221
88 A = 6769042
28 meter
Y = -356960
72 meter E =
0011371
Z = 4283518
00 I = 51
83657
XDOT = 3329
912448 Wp = 323
10297
YDOT = -5910
567399 meter/sec RA = 143
94406 deg
ZDOT = 3586
321868 TA = 90
49160
MA = 90
36130
Ha = 217
084 n
mi
Hp = 206
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17156239
78 X = -5245649
59
Y = -1171130
98 feet Y = -415529
36 meter
Z = 14053536
75 Z = 4258075
23
XDOT = 10924
909606 XDOT = 3378
336905
YDOT = -19391
625324 feet/sec YDOT = -5873
059855 meter/sec
ZDOT = 11766
147861 ZDOT = 3602
615179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14941016
15 X = 4554021
72
Y = 8682871
05 feet Y = 2646539
10 meter
Z = 13949329
47 Z = 4251755
62
XDOT = -17683
791856 XDOT = -5390
019758
YDOT = 11491
957550 feet/sec YDOT = 3502
748661 meter/sec
ZDOT = 11833
284921 ZDOT = 3606
785244
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 12021
15089866
00016717 00000-0 10270-3 0 9129
2 25544 51
6411 144
6630 0020313 306
0805 53
8469 15
58464512 34930
Satellite: ISS
Catalog Number: 25544
Epoch time: 12021
15089866 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 144
6630 deg
Eccentricity:
0020313
Arg of perigee: 306
0805 deg
Mean anomaly: 53
8469 deg
Mean motion: 15
58464512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 293
Coasting Arc #14 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2012/022/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2961138
73 A = 6764611
43 meter
Y = 2957347
73 meter E =
0013644
Z = -5314544
00 I = 51
84731
XDOT = -5652
592403 Wp = 357
01641
YDOT = 5187
689308 meter/sec RA = 138
91905 deg
ZDOT = -249
403490 TA = 270
53749
MA = 270
69383
Ha = 217
277 n
mi
Hp = 206
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9715022
09 X = 2953665
24
Y = 9702584
43 feet Y = 2990419
65 meter
Z = -17436167
96 Z = -5300177
17
XDOT = -18545
250667 XDOT = -5708
970553
YDOT = 17019
978043 feet/sec YDOT = 5124
163336 meter/sec
ZDOT = -818
252919 ZDOT = -276
999395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4733948
71 X = -1442907
57
Y = -12967421
09 feet Y = -3952469
95 meter
Z = -17377499
01 Z = -5296661
70
XDOT = 23088
839537 XDOT = 7037
478291
YDOT = -7121
606136 feet/sec YDOT = -2170
665550 meter/sec
ZDOT = -931
662599 ZDOT = -283
970760
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 12022
11273057
00016717 00000-0 10270-3 0 9134
2 25544 51
6421 139
8369 0020375 309
8457 50
0905 15
58521658 35084
Satellite: ISS
Catalog Number: 25544
Epoch time: 12022
11273057 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 139
8369 deg
Eccentricity:
0020375
Arg of perigee: 309
8457 deg
Mean anomaly: 50
0905 deg
Mean motion: 15
58521658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 302
Coasting Arc #15 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2012/023/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -48703
82 A = 6767849
11 meter
Y = -5056812
65 meter E =
0018729
Z = 4512889
18 I = 51
88085
XDOT = 6312
083054 Wp = 339
67927
YDOT = -2933
237930 meter/sec RA = 133
89200 deg
ZDOT = -3205
510705 TA = 142
50708
MA = 142
37631
Ha = 217
445 n
mi
Hp = 206
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -159789
45 X = -14075
93
Y = -16590592
69 feet Y = -5057163
94 meter
Z = 14806066
85 Z = 4512736
38
XDOT = 20708
933903 XDOT = 6359
985213
YDOT = -9623
484022 feet/sec YDOT = -2862
384305 meter/sec
ZDOT = -10516
767404 ZDOT = -3174
731531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6601645
72 X = -2012181
62
Y = 15221701
68 feet Y = 4639574
67 meter
Z = 14805775
42 Z = 4512800
35
XDOT = -21782
459211 XDOT = -6639
293567
YDOT = 701
422248 feet/sec YDOT = 213
793501 meter/sec
ZDOT = -10390
448402 ZDOT = -3167
008673
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 12023
13866579
00016717 00000-0 10270-3 0 9145
2 25544 51
6422 134
6886 0020505 313
7905 46
1553 15
58552131 35242
Satellite: ISS
Catalog Number: 25544
Epoch time: 12023
13866579 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 134
6886 deg
Eccentricity:
0020505
Arg of perigee: 313
7905 deg
Mean anomaly: 46
1553 deg
Mean motion: 15
58552131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 301
Coasting Arc #16 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2012/024/02:18:35
444
Vector Time (MET): N/A
Weight (LBS) : 884650
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2602112
72 A = 6774513
44 meter
Y = 5868089
09 meter E =
0022078
Z = -2118092
14 I = 51
92441
XDOT = -5306
582817 Wp = 334
23398
YDOT = -348
583084 meter/sec RA = 128
89513 deg
ZDOT = 5551
315270 TA = 2
30944
MA = 2
29927
Ha = 217
673 n
mi
Hp = 205
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8537115
22 X = -2657248
54
Y = 19252260
80 feet Y = 5838682
46 meter
Z = -6949121
18 Z = -2130866
44
XDOT = -17410
048613 XDOT = -5329
256795
YDOT = -1143
645290 feet/sec YDOT = -408
051543 meter/sec
ZDOT = 18212
976609 ZDOT = 5525
481748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15422672
04 X = 4700830
44
Y = -14315631
18 feet Y = -4363404
38 meter
Z = -7001861
05 Z = -2134167
25
XDOT = 14592
323046 XDOT = 4447
740065
YDOT = 6860
986390 feet/sec YDOT = 2091
228652 meter/sec
ZDOT = 18107
130230 ZDOT = 5519
053294
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 12024
10046258
00016717 00000-0 10270-3 0 9158
2 25544 51
6429 129
8615 0020535 317
4030 42
5532 15
58568046 35393
Satellite: ISS
Catalog Number: 25544
Epoch time: 12024
10046258 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 129
8615 deg
Eccentricity:
0020535
Arg of perigee: 317
4030 deg
Mean anomaly: 42
5532 deg
Mean motion: 15
58568046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 295
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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