[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 31st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10494 81 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 ET - UTC (sec) : 67 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 2910)
---------------------------------------
Vector Time (GMT): 2012/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4463131
24 A = 6800735
65 meter
Y = -5063006
02 meter E =
0010630
Z = -880298
73 I = 51
94941
XDOT = 3057
436057 Wp = 46
48604
YDOT = 3721
797257 meter/sec RA = 125
53742 deg
ZDOT = -5942
421007 TA = 142
96693
MA = 142
89352
Ha = 231
566 n
mi
Hp = 218
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14642819
01 X = 4523691
33
Y = -16610912
13 feet Y = -5012757
90 meter
Z = -2888119
21 Z = -858470
29
XDOT = 10030
958193 XDOT = 3044
457385
YDOT = 12210
620921 feet/sec YDOT = 3755
914825 meter/sec
ZDOT = -19496
131912 ZDOT = -5927
599897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20257036
03 X = -6174344
58
Y = 8972329
87 feet Y = 2734766
14 meter
Z = -2797422
20 Z = -852654
29
XDOT = -3470
558665 XDOT = -1057
826281
YDOT = -13855
098159 feet/sec YDOT = -4223
033919 meter/sec
ZDOT = -19435
173671 ZDOT = -5923
840935
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 12240
53062650
00016717 00000-0 10270-3 0 9003
2 25544 51
6476 126
3433 0015224 4
8065 355
3226 15
50103334 29114
Satellite: ISS
Catalog Number: 25544
Epoch time: 12240
53062650 = yrday
fracday
Element set: 900
Inclination: 51
6476 deg
RA of node: 126
3433 deg
Eccentricity:
0015224
Arg of perigee: 4
8065 deg
Mean anomaly: 355
3226 deg
Mean motion: 15
50103334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 261
Coasting Arc #2 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2012/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4195057
04 A = 6800334
60 meter
Y = 5183843
42 meter E =
0026420
Z = 1241863
74 I = 51
96524
XDOT = -3046
530894 Wp = 31
87411
YDOT = -3882
087675 meter/sec RA = 120
60527 deg
ZDOT = 5878
566775 TA = 341
56655
MA = 341
66210
Ha = 231
743 n
mi
Hp = 217
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13763310
52 X = -4258744
65
Y = 17007360
29 feet Y = 5136575
61 meter
Z = 4074356
11 Z = 1221329
91
XDOT = -9995
180098 XDOT = -3031
450373
YDOT = -12736
508120 feet/sec YDOT = -3916
071419 meter/sec
ZDOT = 19286
636402 ZDOT = 5863
803869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19460344
45 X = 5931512
99
Y = -10033062
48 feet Y = -3058077
44 meter
Z = 3988991
01 Z = 1215844
46
XDOT = 3411
065147 XDOT = 1039
692657
YDOT = 14306
653661 feet/sec YDOT = 4360
668036 meter/sec
ZDOT = 19225
928842 ZDOT = 5860
063111
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 12241
56211210
00016717 00000-0 10270-3 0 9016
2 25544 51
6477 121
2320 0015467 8
4081 351
7326 15
50140710 29278
Satellite: ISS
Catalog Number: 25544
Epoch time: 12241
56211210 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 121
2320 deg
Eccentricity:
0015467
Arg of perigee: 8
4081 deg
Mean anomaly: 351
7326 deg
Mean motion: 15
50140710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 258
Coasting Arc #3 (Orbit 2941)
---------------------------------------
Vector Time (GMT): 2012/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3963243
20 A = 6799860
34 meter
Y = -5286097
62 meter E =
0011779
Z = -1639200
82 I = 51
97813
XDOT = 3031
891975 Wp = 42
48259
YDOT = 4047
490431 meter/sec RA = 115
67464 deg
ZDOT = -5737
515642 TA = 155
31641
MA = 155
26000
Ha = 231
758 n
mi
Hp = 217
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13002766
40 X = 4030021
59
Y = -17342839
96 feet Y = -5241404
86 meter
Z = -5377955
45 Z = -1619785
49
XDOT = 9947
152149 XDOT = 3014
277781
YDOT = 13279
168080 feet/sec YDOT = 4081
296176 meter/sec
ZDOT = -18823
870216 ZDOT = -5722
830109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18720212
82 X = -5705920
87
Y = 10966392
17 feet Y = 3342556
33 meter
Z = -5297198
44 Z = -1614586
08
XDOT = -3356
478529 XDOT = -1023
054656
YDOT = -14768
029277 feet/sec YDOT = -4501
295324 meter/sec
ZDOT = -18763
494276 ZDOT = -5719
113055
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 12242
52912132
00016717 00000-0 10270-3 0 9025
2 25544 51
6476 116
4407 0015281 11
6397 348
5104 15
50132547 29423
Satellite: ISS
Catalog Number: 25544
Epoch time: 12242
52912132 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 116
4407 deg
Eccentricity:
0015281
Arg of perigee: 11
6397 deg
Mean anomaly: 348
5104 deg
Mean motion: 15
50132547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2942
Checksum: 282
Coasting Arc #4 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2012/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3685887
75 A = 6799218
26 meter
Y = 5332759
62 meter E =
0026338
Z = 1993525
31 I = 51
98804
XDOT = -3083
749030 Wp = 40
08685
YDOT = -4236
286862 meter/sec RA = 110
74337 deg
ZDOT = 5609
193686 TA = 341
81820
MA = 341
91220
Ha = 231
928 n
mi
Hp = 217
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12092807
57 X = -3754929
75
Y = 17495930
50 feet Y = 5291155
82 meter
Z = 6540437
36 Z = 1975451
68
XDOT = -10117
286844 XDOT = -3063
396520
YDOT = -13898
578942 feet/sec YDOT = -4270
657081 meter/sec
ZDOT = 18402
866423 ZDOT = 5594
262965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17746784
56 X = 5409219
93
Y = -11763226
15 feet Y = -3585431
33 meter
Z = 6465218
32 Z = 1970598
55
XDOT = 3501
657700 XDOT = 1067
305267
YDOT = 15402
601819 feet/sec YDOT = 4694
713034 meter/sec
ZDOT = 18341
492053 ZDOT = 5590
486778
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 12243
56058764
00016717 00000-0 10270-3 0 9033
2 25544 51
6471 111
3288 0015496 15
2285 344
9329 15
50173717 29583
Satellite: ISS
Catalog Number: 25544
Epoch time: 12243
56058764 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 111
3288 deg
Eccentricity:
0015496
Arg of perigee: 15
2285 deg
Mean anomaly: 344
9329 deg
Mean motion: 15
50173717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 320
Coasting Arc #5 (Orbit 2972)
---------------------------------------
Vector Time (GMT): 2012/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3452176
14 A = 6798512
24 meter
Y = -5362850
53 meter E =
0013852
Z = -2380431
54 I = 51
99480
XDOT = 3136
269068 Wp = 40
24020
YDOT = 4412
754442 meter/sec RA = 105
81317 deg
ZDOT = -5400
419763 TA = 166
10441
MA = 166
06625
Ha = 231
925 n
mi
Hp = 217
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11326037
20 X = 3523451
50
Y = -17594653
98 feet Y = -5323847
83 meter
Z = -7809814
76 Z = -2363487
68
XDOT = 10289
596679 XDOT = 3112
925284
YDOT = 14477
540820 feet/sec YDOT = 4447
695172 meter/sec
ZDOT = -17717
912607 ZDOT = -5385
241209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16866985
98 X = -5141057
33
Y = 12427905
00 feet Y = 3788025
44 meter
Z = -7739259
34 Z = -2358926
25
XDOT = -3691
953715 XDOT = -1125
307492
YDOT = -15990
322483 feet/sec YDOT = -4873
850293 meter/sec
ZDOT = -17655
530066 ZDOT = -5381
405564
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 12244
52757877
00016717 00000-0 10270-3 0 9042
2 25544 51
6464 106
5371 0015357 18
5059 341
6647 15
50169285 29734
Satellite: ISS
Catalog Number: 25544
Epoch time: 12244
52757877 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 106
5371 deg
Eccentricity:
0015357
Arg of perigee: 18
5059 deg
Mean anomaly: 341
6647 deg
Mean motion: 15
50169285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2973
Checksum: 330
Coasting Arc #6 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2012/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3187699
80 A = 6797685
46 meter
Y = 5332338
59 meter E =
0025539
Z = 2718152
91 I = 51
99896
XDOT = -3255
847241 Wp = 48
05674
YDOT = -4607
292655 meter/sec RA = 100
88170 deg
ZDOT = 5205
426243 TA = 342
51933
MA = 342
60708
Ha = 232
078 n
mi
Hp = 217
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10458332
67 X = -3260294
23
Y = 17494549
17 feet Y = 5296286
11 meter
Z = 8917824
50 Z = 2702490
52
XDOT = -10681
913520 XDOT = -3229
372087
YDOT = -15115
789549 feet/sec YDOT = -4643
553034 meter/sec
ZDOT = 17078
170087 ZDOT = 5189
674400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15806651
06 X = 4817867
24
Y = -12912994
92 feet Y = -3935880
85 meter
Z = 8852565
23 Z = 2698261
88
XDOT = 4101
945431 XDOT = 1250
272967
YDOT = 16717
994609 feet/sec YDOT = 5095
644757 meter/sec
ZDOT = 17013
437433 ZDOT = 5185
695730
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 12245
55902594
00016717 00000-0 10270-3 0 9055
2 25544 51
6457 101
4246 0015486 22
0525 338
1289 15
50204647 29894
Satellite: ISS
Catalog Number: 25544
Epoch time: 12245
55902594 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 101
4246 deg
Eccentricity:
0015486
Arg of perigee: 22
0525 deg
Mean anomaly: 338
1289 deg
Mean motion: 15
50204647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 313
Coasting Arc #7 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2012/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2974242
07 A = 6796787
73 meter
Y = -5290619
94 meter E =
0016651
Z = -3084262
54 I = 51
99979
XDOT = 3375
468235 Wp = 41
07060
YDOT = 4769
946901 meter/sec RA = 95
95084 deg
ZDOT = -4930
046161 TA = 174
02257
MA = 174
00268
Ha = 232
069 n
mi
Hp = 216
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9758012
03 X = 3048164
39
Y = -17357676
97 feet Y = -5256947
10 meter
Z = -10118971
59 Z = -3069633
81
XDOT = 11074
370850 XDOT = 3345
827737
YDOT = 15649
432091 feet/sec YDOT = 4807
527267 meter/sec
ZDOT = -16174
692129 ZDOT = -4913
720863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14882064
18 X = -4536053
16
Y = 13276387
54 feet Y = 4046642
92 meter
Z = -10057983
61 Z = -3065673
41
XDOT = -4576
754389 XDOT = -1394
994738
YDOT = -17325
820263 feet/sec YDOT = -5280
910016 meter/sec
ZDOT = -16107
608155 ZDOT = -4909
598966
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 12246
52599893
00016717 00000-0 10270-3 0 9068
2 25544 51
6447 96
6323 0015429 25
5495 334
6415 15
50209696 30045
Satellite: ISS
Catalog Number: 25544
Epoch time: 12246
52599893 = yrday
fracday
Element set: 906
Inclination: 51
6447 deg
RA of node: 96
6323 deg
Eccentricity:
0015429
Arg of perigee: 25
5495 deg
Mean anomaly: 334
6415 deg
Mean motion: 15
50209696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 327
Coasting Arc #8 (Orbit 3019)
---------------------------------------
Vector Time (GMT): 2012/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2745389
85 A = 6795847
93 meter
Y = 5186996
30 meter E =
0024138
Z = 3395209
72 I = 51
99871
XDOT = -3559
757102 Wp = 55
55507
YDOT = -4946
238764 meter/sec RA = 91
01855 deg
ZDOT = 4667
884072 TA = 343
90107
MA = 343
97764
Ha = 232
201 n
mi
Hp = 216
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9007184
54 X = -2819681
00
Y = 17017704
40 feet Y = 5155880
58 meter
Z = 11139139
51 Z = 3381691
83
XDOT = -11678
993118 XDOT = -3526
858142
YDOT = -16227
817466 feet/sec YDOT = -4985
861788 meter/sec
ZDOT = 15314
580290 ZDOT = 4650
671362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13838687
20 X = 4218031
86
Y = -13434118
04 feet Y = -4094719
18 meter
Z = 11082746
71 Z = 3378021
20
XDOT = 5275
203652 XDOT = 1607
882073
YDOT = 18037
635626 feet/sec YDOT = 5497
871339 meter/sec
ZDOT = 15243
849682 ZDOT = 4646
325383
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 12247
55742693
00016717 00000-0 10270-3 0 9071
2 25544 51
6444 91
5194 0015448 29
0357 331
1650 15
50232920 30206
Satellite: ISS
Catalog Number: 25544
Epoch time: 12247
55742693 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 91
5194 deg
Eccentricity:
0015448
Arg of perigee: 29
0357 deg
Mean anomaly: 331
1650 deg
Mean motion: 15
50232920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3020
Checksum: 291
Coasting Arc #9 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2012/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2573819
35 A = 6794835
68 meter
Y = -5081091
13 meter E =
0019835
Z = -3729756
16 I = 51
99415
XDOT = 3737
920538 Wp = 44
72529
YDOT = 5071
061871 meter/sec RA = 86
08633 deg
ZDOT = -4329
242495 TA = 179
32217
MA = 179
31948
Ha = 232
193 n
mi
Hp = 216
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8444289
22 X = 2648564
19
Y = -16670246
50 feet Y = -5051891
48 meter
Z = -12236732
81 Z = -3717070
67
XDOT = 12263
518824 XDOT = 3701
967551
YDOT = 16637
342096 feet/sec YDOT = 5112
660231 meter/sec
ZDOT = -14203
551494 ZDOT = -4311
171608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12972733
21 X = -3954089
08
Y = 13498310
62 feet Y = 4114285
08 meter
Z = -12183783
16 Z = -3713617
11
XDOT = -6031
948637 XDOT = -1838
537944
YDOT = -18549
426137 feet/sec YDOT = -5653
865086 meter/sec
ZDOT = -14129
291677 ZDOT = -4306
608103
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 12248
52438186
00016717 00000-0 10270-3 0 9089
2 25544 51
6435 86
7268 0015480 32
8767 327
3343 15
50248438 30350
Satellite: ISS
Catalog Number: 25544
Epoch time: 12248
52438186 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 86
7268 deg
Eccentricity:
0015480
Arg of perigee: 32
8767 deg
Mean anomaly: 327
3343 deg
Mean motion: 15
50248438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 323
Coasting Arc #10 (Orbit 3050)
---------------------------------------
Vector Time (GMT): 2012/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2401562
34 A = 6793859
99 meter
Y = 4915582
76 meter E =
0022342
Z = 4003230
28 I = 51
98804
XDOT = -3975
662846 Wp = 62
19629
YDOT = -5206
636413 meter/sec RA = 81
15271 deg
ZDOT = 4001
387533 TA = 346
35155
MA = 346
41186
Ha = 232
311 n
mi
Hp = 216
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7879141
53 X = -2475797
73
Y = 16127240
01 feet Y = 4888312
21 meter
Z = 13133957
62 Z = 3991382
91
XDOT = -13043
513274 XDOT = -3936
583546
YDOT = -17082
140461 feet/sec YDOT = -5250
875957 meter/sec
ZDOT = 13127
911855 ZDOT = 3982
169215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12052228
28 X = 3673519
18
Y = -13349522
56 feet Y = -4068934
48 meter
Z = 13084480
32 Z = 3988149
60
XDOT = 7000
051769 XDOT = 2133
615779
YDOT = 19131
719272 feet/sec YDOT = 5831
348034 meter/sec
ZDOT = 13048
928033 ZDOT = 3977
313265
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 12249
55579051
00016717 00000-0 10270-3 0 9091
2 25544 51
6436 81
6139 0015414 36
3043 323
9151 15
50259442 30519
Satellite: ISS
Catalog Number: 25544
Epoch time: 12249
55579051 = yrday
fracday
Element set: 909
Inclination: 51
6436 deg
RA of node: 81
6139 deg
Eccentricity:
0015414
Arg of perigee: 36
3043 deg
Mean anomaly: 323
9151 deg
Mean motion: 15
50259442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3051
Checksum: 294
Coasting Arc #11 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2012/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2290554
84 A = 6792837
21 meter
Y = -4760024
87 meter E =
0023049
Z = -4295446
08 I = 51
97877
XDOT = 4195
742322 Wp = 50
39232
YDOT = 5273
457561 meter/sec RA = 76
21865 deg
ZDOT = -3605
050179 TA = 182
81918
MA = 182
83219
Ha = 232
300 n
mi
Hp = 216
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7514943
71 X = 2364478
53
Y = -15616879
51 feet Y = -4733997
39 meter
Z = -14092670
87 Z = -4284138
81
XDOT = 13765
558799 XDOT = 4153
974137
YDOT = 17301
369952 feet/sec YDOT = 5320
143212 meter/sec
ZDOT = -11827
592451 ZDOT = -3584
769190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11343860
07 X = -3457608
55
Y = 13153225
10 feet Y = 4009103
01 meter
Z = -14045432
89 Z = -4281047
94
XDOT = -7991
594615 XDOT = -2435
838039
YDOT = -19437
966159 feet/sec YDOT = -5924
692085 meter/sec
ZDOT = -11744
228306 ZDOT = -3579
640788
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 12250
52272721
00016717 00000-0 10270-3 0 9106
2 25544 51
6432 76
8213 0015513 40
4520 319
7781 15
50282963 30662
Satellite: ISS
Catalog Number: 25544
Epoch time: 12250
52272721 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 76
8213 deg
Eccentricity:
0015513
Arg of perigee: 40
4520 deg
Mean anomaly: 319
7781 deg
Mean motion: 15
50282963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 282
Coasting Arc #12 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2012/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2191738
46 A = 6791909
89 meter
Y = 4550267
89 meter E =
0020431
Z = 4520582
74 I = 51
96759
XDOT = -4468
013635 Wp = 67
38358
YDOT = -5350
157477 meter/sec RA = 71
28295 deg
ZDOT = 3215
154743 TA = 350
47280
MA = 350
51150
Ha = 232
415 n
mi
Hp = 215
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7190742
98 X = -2264417
59
Y = 14928700
43 feet Y = 4525352
36 meter
Z = 14831308
19 Z = 4509758
60
XDOT = -14658
837385 XDOT = -4423
473497
YDOT = -17553
010096 feet/sec YDOT = -5399
872391 meter/sec
ZDOT = 10548
407948 ZDOT = 3193
557776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10640946
71 X = 3243360
56
Y = -12754711
41 feet Y = -3887636
04 meter
Z = 14786080
40 Z = 4506797
31
XDOT = 9167
447220 XDOT = 2794
237913
YDOT = 19788
456078 feet/sec YDOT = 6031
521413 meter/sec
ZDOT = 10459
615854 ZDOT = 3188
090912
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 12251
55411605
00016717 00000-0 10270-3 0 9117
2 25544 51
6432 71
7085 0015418 43
8331 316
4040 15
50285667 30828
Satellite: ISS
Catalog Number: 25544
Epoch time: 12251
55411605 = yrday
fracday
Element set: 911
Inclination: 51
6432 deg
RA of node: 71
7085 deg
Eccentricity:
0015418
Arg of perigee: 43
8331 deg
Mean anomaly: 316
4040 deg
Mean motion: 15
50285667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 279
Coasting Arc #13 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2012/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2154683
33 A = 6790988
09 meter
Y = -4365309
48 meter E =
0025959
Z = -4760005
15 I = 51
95432
XDOT = 4706
797332 Wp = 57
29432
YDOT = 5345
312063 meter/sec RA = 66
34665 deg
ZDOT = -2768
858509 TA = 185
29786
MA = 185
32538
Ha = 232
389 n
mi
Hp = 215
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7069171
03 X = 2226459
99
Y = -14321881
51 feet Y = -4340813
36 meter
Z = -15616814
78 Z = -4749363
27
XDOT = 15442
248465 XDOT = 4660
125598
YDOT = 17537
113067 feet/sec YDOT = 5397
685325 meter/sec
ZDOT = -9084
181459 ZDOT = -2746
106728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10171168
17 X = -3100172
06
Y = 12370269
68 feet Y = 3770458
20 meter
Z = -15572351
75 Z = -4746452
81
XDOT = -10306
272869 XDOT = -3141
351970
YDOT = -19802
841407 feet/sec YDOT = -6035
906061 meter/sec
ZDOT = -8990
618496 ZDOT = -2740
340518
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 12252
52103389
00016717 00000-0 10270-3 0 9123
2 25544 51
6435 66
9161 0015544 48
0991 312
1482 15
50314669 30975
Satellite: ISS
Catalog Number: 25544
Epoch time: 12252
52103389 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 66
9161 deg
Eccentricity:
0015544
Arg of perigee: 48
0991 deg
Mean anomaly: 312
1482 deg
Mean motion: 15
50314669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 302
Coasting Arc #14 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2012/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2139892
46 A = 6790205
12 meter
Y = 4133829
75 meter E =
0018750
Z = 4926124
85 I = 51
93831
XDOT = -4988
482551 Wp = 70
44671
YDOT = -5351
761974 meter/sec RA = 61
40793 deg
ZDOT = 2322
975118 TA = 356
94360
MA = 356
95504
Ha = 232
512 n
mi
Hp = 215
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7020644
54 X = -2209888
68
Y = 13562433
58 feet Y = 4109508
99 meter
Z = 16161826
94 Z = 4915559
19
XDOT = -16366
412568 XDOT = -4939
551733
YDOT = -17558
274193 feet/sec YDOT = -5407
272607 meter/sec
ZDOT = 7621
309442 ZDOT = 2298
860461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9756490
73 X = 2973778
38
Y = -11809506
76 feet Y = -3599537
66 meter
Z = 16117696
57 Z = 4912673
91
XDOT = 11590
164672 XDOT = 3532
682192
YDOT = 19846
245838 feet/sec YDOT = 6049
135731 meter/sec
ZDOT = 7522
114679 ZDOT = 2292
740554
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 12253
55240233
00016717 00000-0 10270-3 0 9138
2 25544 51
6431 61
8031 0015465 51
4482 308
8052 15
50312621 31136
Satellite: ISS
Catalog Number: 25544
Epoch time: 12253
55240233 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 61
8031 deg
Eccentricity:
0015465
Arg of perigee: 51
4482 deg
Mean anomaly: 308
8052 deg
Mean motion: 15
50312621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 258
Coasting Arc #15 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2012/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2182926
56 A = 6789486
49 meter
Y = -3943547
65 meter E =
0028243
Z = -5102840
42 I = 51
92163
XDOT = 5218
573242 Wp = 64
84788
YDOT = 5270
077976 meter/sec RA = 56
46900 deg
ZDOT = -1836
661506 TA = 187
35087
MA = 187
39237
Ha = 232
456 n
mi
Hp = 215
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7161832
53 X = 2251650
18
Y = -12938148
46 feet Y = -3918752
79 meter
Z = -16741602
44 Z = -5092068
81
XDOT = 17121
303288 XDOT = 5168
176315
YDOT = 17290
282073 feet/sec YDOT = 5328
153441 meter/sec
ZDOT = -6025
792344 ZDOT = -1811
432728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9576199
26 X = -2918825
53
Y = 11335235
46 feet Y = 3454979
77 meter
Z = -16696635
22 Z = -5089134
42
XDOT = -12758
814765 XDOT = -3888
886740
YDOT = -19519
759874 feet/sec YDOT = -5949
622810 meter/sec
ZDOT = -5921
984329 ZDOT = -1805
020823
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 12254
51930040
00016717 00000-0 10270-3 0 9148
2 25544 51
6440 57
0110 0015579 55
6138 304
6483 15
50346436 31280
Satellite: ISS
Catalog Number: 25544
Epoch time: 12254
51930040 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 57
0110 deg
Eccentricity:
0015579
Arg of perigee: 55
6138 deg
Mean anomaly: 304
6483 deg
Mean motion: 15
50346436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 282
Coasting Arc #16 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2012/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2254796
69 A = 6788950
16 meter
Y = 3715579
85 meter E =
0017703
Z = 5199812
09 I = 51
90168
XDOT = -5480
689939 Wp = 71
16226
YDOT = -5203
579699 meter/sec RA = 51
52654 deg
ZDOT = 1343
525398 TA = 5
99739
MA = 5
97622
Ha = 232
591 n
mi
Hp = 215
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7397626
95 X = -2321436
81
Y = 12190222
62 feet Y = 3689993
02 meter
Z = 17059750
94 Z = 5188696
38
XDOT = -17981
266203 XDOT = -5428
621585
YDOT = -17072
111873 feet/sec YDOT = -5264
576978 meter/sec
ZDOT = 4407
891726 ZDOT = 1317
027450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9485471
54 X = 2891171
73
Y = -10720643
73 feet Y = -3267652
21 meter
Z = 17013381
25 Z = 5185678
61
XDOT = 14024
274205 XDOT = 4274
598778
YDOT = 19220
963007 feet/sec YDOT = 5858
549524 meter/sec
ZDOT = 4298
829953 ZDOT = 1310
283370
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 12255
55064779
00016717 00000-0 10270-3 0 9151
2 25544 51
6433 51
8974 0015532 58
9516 301
3157 15
50340864 31446
Satellite: ISS
Catalog Number: 25544
Epoch time: 12255
55064779 = yrday
fracday
Element set: 915
Inclination: 51
6433 deg
RA of node: 51
8974 deg
Eccentricity:
0015532
Arg of perigee: 58
9516 deg
Mean anomaly: 301
3157 deg
Mean motion: 15
50340864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 311
Coasting Arc #17 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2012/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2375462
37 A = 6788516
84 meter
Y = -3545376
57 meter E =
0029606
Z = -5304811
11 I = 51
88205
XDOT = 5673
556830 Wp = 72
63398
YDOT = 5049
528396 meter/sec RA = 46
58465 deg
ZDOT = -829
419430 TA = 189
40701
MA = 189
46258
Ha = 232
492 n
mi
Hp = 215
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7793511
71 X = 2440700
30
Y = -11631812
91 feet Y = -3518448
33 meter
Z = -17404235
93 Z = -5293112
59
XDOT = 18614
031595 XDOT = 5620
699381
YDOT = 16566
694213 feet/sec YDOT = 5112
678037 meter/sec
ZDOT = -2721
192357 ZDOT = -801
986583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9606357
73 X = -2928017
84
Y = 10268924
43 feet Y = 3129968
17 meter
Z = -17355471
96 Z = -5289947
85
XDOT = -15090
732901 XDOT = -4599
655388
YDOT = -18551
712788 feet/sec YDOT = -5654
562058 meter/sec
ZDOT = -2608
250442 ZDOT = -794
994735
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 12256
51752522
00016717 00000-0 10270-3 0 9169
2 25544 51
6445 47
1056 0015603 62
8840 297
3900 15
50379924 31596
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
51752522 = yrday
fracday
Element set: 916
Inclination: 51
6445 deg
RA of node: 47
1056 deg
Eccentricity:
0015603
Arg of perigee: 62
8840 deg
Mean anomaly: 297
3900 deg
Mean motion: 15
50379924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 309
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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