[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 9th 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 3264)
---------------------------------------
Vector Time (GMT): 2012/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5941912
61 A = 6773696
30 meter
Y = 2657724
17 meter E =
0016563
Z = 1852584
02 I = 51
44240
XDOT = -579
856283 Wp = 217
33773
YDOT = 5191
346869 meter/sec RA = 217
21027 deg
ZDOT = -5627
003001 TA = 302
17143
MA = 302
33197
Ha = 216
273 n
mi
Hp = 204
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19494463
94 X = 5902752
38
Y = 8719567
50 feet Y = 2723951
11 meter
Z = 6078031
57 Z = 1881354
68
XDOT = -1902
415628 XDOT = -610
529241
YDOT = 17031
977917 feet/sec YDOT = 5184
691743 meter/sec
ZDOT = -18461
295934 ZDOT = -5629
893779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3501968
47 X = -1067399
99
Y = 21032340
17 feet Y = 6410657
28 meter
Z = 6195509
11 Z = 1888391
18
XDOT = -15394
715524 XDOT = -4692
309292
YDOT = 2841
209961 feet/sec YDOT = 866
000796 meter/sec
ZDOT = -18473
467139 ZDOT = -5630
712784
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 12006
53570426
00016717 00000-0 10270-3 0 9008
2 25544 51
6405 218
0602 0024092 251
4392 108
4145 15
58994607 32658
Satellite: ISS
Catalog Number: 25544
Epoch time: 12006
53570426 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 218
0602 deg
Eccentricity:
0024092
Arg of perigee: 251
4392 deg
Mean anomaly: 108
4145 deg
Mean motion: 15
58994607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 290
Coasting Arc #2 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2012/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4895972
21 A = 6774277
96 meter
Y = -4452811
36 meter E =
0011243
Z = 1454943
90 I = 51
46763
XDOT = 4223
209084 Wp = 272
36838
YDOT = -2770
847623 meter/sec RA = 212
20293 deg
ZDOT = 5770
298349 TA = 103
56301
MA = 103
43774
Ha = 216
206 n
mi
Hp = 204
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16062900
97 X = -4852883
85
Y = -14608961
14 feet Y = -4507320
39 meter
Z = 4773437
98 Z = 1431263
76
XDOT = 13855
672849 XDOT = 4225
848781
YDOT = -9090
707424 feet/sec YDOT = -2723
607065 meter/sec
ZDOT = 18931
425030 ZDOT = 5790
820425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9718709
23 X = 2962262
57
Y = -19439591
18 feet Y = -5925187
39 meter
Z = 4676882
41 Z = 1425513
76
XDOT = 11045
961246 XDOT = 3366
808988
YDOT = 10065
771414 feet/sec YDOT = 3068
047127 meter/sec
ZDOT = 19015
545380 ZDOT = 5795
938232
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 12007
56132704
00016717 00000-0 10270-3 0 9016
2 25544 51
6388 212
9076 0024218 254
9717 104
8758 15
59018840 32810
Satellite: ISS
Catalog Number: 25544
Epoch time: 12007
56132704 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 212
9076 deg
Eccentricity:
0024218
Arg of perigee: 254
9717 deg
Mean anomaly: 104
8758 deg
Mean motion: 15
59018840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 310
Coasting Arc #3 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2012/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2193891
32 A = 6767752
87 meter
Y = 4851790
36 meter E =
0016471
Z = -4161755
66 I = 51
47082
XDOT = -6732
432913 Wp = 262
97100
YDOT = -141
797151 meter/sec RA = 207
18030 deg
ZDOT = -3703
758358 TA = 328
95230
MA = 329
04954
Ha = 216
016 n
mi
Hp = 204
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7197806
18 X = 2159691
21
Y = 15917947
36 feet Y = 4876133
06 meter
Z = -13654054
02 Z = -4151180
46
XDOT = -22088
034493 XDOT = -6712
355134
YDOT = -465
213751 feet/sec YDOT = -216
970654 meter/sec
ZDOT = -12151
438184 ZDOT = -3736
415079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13162203
83 X = -4011839
73
Y = 11537617
53 feet Y = 3516665
82 meter
Z = -13611114
03 Z = -4148667
56
XDOT = -5022
738887 XDOT = -1530
930813
YDOT = -20263
914329 feet/sec YDOT = -6176
441088 meter/sec
ZDOT = -12285
014583 ZDOT = -3744
472445
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 12008
52283333
00016717 00000-0 10270-3 0 9029
2 25544 51
6375 208
0789 0024102 258
7936 101
0510 15
59030352 32963
Satellite: ISS
Catalog Number: 25544
Epoch time: 12008
52283333 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 208
0789 deg
Eccentricity:
0024102
Arg of perigee: 258
7936 deg
Mean anomaly: 101
0510 deg
Mean motion: 15
59030352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 286
Coasting Arc #4 (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 = 1399350
22 A = 6763202
03 meter
Y = -3985303
47 meter E =
0021686
Z = 5300655
99 I = 51
48311
XDOT = 7147
068773 Wp = 260
72387
YDOT = 2751
566904 meter/sec RA = 202
12331 deg
ZDOT = 179
177238 TA = 187
54673
MA = 187
57942
Ha = 215
886 n
mi
Hp = 204
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4591044
04 X = 1418061
69
Y = -13075142
62 feet Y = -3969550
99 meter
Z = 17390603
64 Z = 5307498
91
XDOT = 23448
388363 XDOT = 7114
898629
YDOT = 9027
450474 feet/sec YDOT = 2831
309927 meter/sec
ZDOT = 587
851831 ZDOT = 213
818978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13818692
73 X = 4211937
54
Y = 311908
73 feet Y = 95069
78 meter
Z = 17418856
99 Z = 5309267
61
XDOT = -1474
270924 XDOT = -449
357778
YDOT = 24070
089451 feet/sec YDOT = 7336
563265 meter/sec
ZDOT = 729
399482 ZDOT = 222
320962
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
54842254
00016717 00000-0 10270-3 0 9036
2 25544 51
6377 202
9269 0024032 262
5387 97
3037 15
59010911 33125
Satellite: ISS
Catalog Number: 25544
Epoch time: 12009
54842254 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 202
9269 deg
Eccentricity:
0024032
Arg of perigee: 262
5387 deg
Mean anomaly: 97
3037 deg
Mean motion: 15
59010911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 295
Coasting Arc #5 (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 = -4703638
72 A = 6766780
60 meter
Y = 2167800
01 meter E =
0016331
Z = -4344288
50 I = 51
52383
XDOT = -5234
888956 Wp = 253
17715
YDOT = -4457
219048 meter/sec RA = 197
06476 deg
ZDOT = 3428
460232 TA = 51
64799
MA = 51
50134
Ha = 215
608 n
mi
Hp = 204
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15431885
57 X = -4706426
72
Y = 7112204
76 feet Y = 2115185
79 meter
Z = -14252915
02 Z = -4367144
75
XDOT = -17174
832533 XDOT = -5201
312761
YDOT = -14623
422074 feet/sec YDOT = -4515
571332 meter/sec
ZDOT = 11248
229108 ZDOT = 3403
111031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11640676
10 X = -3548078
07
Y = -12269580
59 feet Y = -3739768
16 meter
Z = -14346574
08 Z = -4372835
78
XDOT = 7453
921680 XDOT = 2271
955328
YDOT = -20161
526213 feet/sec YDOT = -6145
233190 meter/sec
ZDOT = 11144
790197 ZDOT = 3396
932052
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
50989303
00016717 00000-0 10270-3 0 9042
2 25544 51
6369 198
0959 0024043 265
9865 93
8542 15
59085617 33270
Satellite: ISS
Catalog Number: 25544
Epoch time: 12010
50989303 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 198
0959 deg
Eccentricity:
0024043
Arg of perigee: 265
9865 deg
Mean anomaly: 93
8542 deg
Mean motion: 15
59085617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 336
Coasting Arc #6 (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 = 6549213
92 A = 6773434
74 meter
Y = -1076
26 meter E =
0012870
Z = 1724121
85 I = 51
57672
XDOT = 1487
865064 Wp = 243
99919
YDOT = 4930
374503 meter/sec RA = 192
04430 deg
ZDOT = -5687
183642 TA = 277
03802
MA = 277
18436
Ha = 215
607 n
mi
Hp = 204
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21486922
30 X = 6540363
96
Y = -3531
04 feet Y = 72111
49 meter
Z = 5656567
74 Z = 1755915
55
XDOT = 4881
447060 XDOT = 1460
248595
YDOT = 16175
769368 feet/sec YDOT = 4946
858633 meter/sec
ZDOT = -18658
738983 ZDOT = -5680
022595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7204387
75 X = 2195897
39
Y = 20206330
67 feet Y = 6158889
59 meter
Z = 5786674
29 Z = 1763778
32
XDOT = -12086
041622 XDOT = -3683
825486
YDOT = 9608
994151 feet/sec YDOT = 2928
821417 meter/sec
ZDOT = -18629
741757 ZDOT = -5678
345287
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
53544310
00016717 00000-0 10270-3 0 9052
2 25544 51
6375 192
9451 0024215 270
4838 89
3543 15
59151474 33433
Satellite: ISS
Catalog Number: 25544
Epoch time: 12011
53544310 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 192
9451 deg
Eccentricity:
0024215
Arg of perigee: 270
4838 deg
Mean anomaly: 89
3543 deg
Mean motion: 15
59151474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 299
Coasting Arc #7 (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 = -6233508
74 A = 6773721
41 meter
Y = -2076782
98 meter E =
0013910
Z = 1636112
74 I = 51
60696
XDOT = 2894
811253 Wp = 304
62998
YDOT = -4212
550029 meter/sec RA = 187
04614 deg
ZDOT = 5724
232214 TA = 73
32677
MA = 73
17412
Ha = 215
643 n
mi
Hp = 204
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20451144
15 X = -6217770
18
Y = -6813592
46 feet Y = -2146401
97 meter
Z = 5367823
94 Z = 1605869
30
XDOT = 9497
412246 XDOT = 2913
895125
YDOT = -13820
702195 feet/sec YDOT = -4180
071969 meter/sec
ZDOT = 18780
289416 ZDOT = 5738
341042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -829345
82 X = -252784
61
Y = -21570782
95 feet Y = -6574774
64 meter
Z = 5244175
96 Z = 1598424
83
XDOT = 14664
527570 XDOT = 4469
748003
YDOT = 3981
513880 feet/sec YDOT = 1213
565431 meter/sec
ZDOT = 18838
290250 ZDOT = 5741
910868
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
56097770
00016717 00000-0 10270-3 0 9060
2 25544 51
6372 187
7920 0023987 273
7801 86
0611 15
59135085 33591
Satellite: ISS
Catalog Number: 25544
Epoch time: 12012
56097770 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 187
7920 deg
Eccentricity:
0023987
Arg of perigee: 273
7801 deg
Mean anomaly: 86
0611 deg
Mean motion: 15
59135085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 325
Coasting Arc #8 (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 = 3817417
29 A = 6766827
60 meter
Y = 3548547
55 meter E =
0016822
Z = -4306012
80 I = 51
61542
XDOT = -6342
683418 Wp = 291
65641
YDOT = 2551
752493 meter/sec RA = 182
03115 deg
ZDOT = -3503
053957 TA = 302
68885
MA = 302
85097
Ha = 215
613 n
mi
Hp = 204
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12524334
96 X = 3798370
35
Y = 11642216
37 feet Y = 3591129
85 meter
Z = -14127338
59 Z = -4287514
41
XDOT = -20809
328798 XDOT = -6353
729414
YDOT = 8371
891380 feet/sec YDOT = 2480
763019 meter/sec
ZDOT = -11492
959176 ZDOT = -3533
892772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6185900
10 X = -1885462
35
Y = 16008194
70 feet Y = 4879297
74 meter
Z = -14051839
96 Z = -4283000
82
XDOT = -14246
698114 XDOT = -4342
393585
YDOT = -15753
958710 feet/sec YDOT = -4801
806615 meter/sec
ZDOT = -11619
338109 ZDOT = -3541
574256
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
52239729
00016717 00000-0 10270-3 0 9070
2 25544 51
6380 182
9634 0023816 277
6768 82
1682 15
59185475 33745
Satellite: ISS
Catalog Number: 25544
Epoch time: 12013
52239729 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 182
9634 deg
Eccentricity:
0023816
Arg of perigee: 277
6768 deg
Mean anomaly: 82
1682 deg
Mean motion: 15
59185475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 339
Coasting Arc #9 (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 = -63809
71 A = 6762799
04 meter
Y = -4207887
21 meter E =
0021419
Z = 5311946
17 I = 51
63174
XDOT = 7654
287378 Wp = 283
50009
YDOT = -294
884810 meter/sec RA = 176
98110 deg
ZDOT = -137
226552 TA = 167
83490
MA = 167
78310
Ha = 215
672 n
mi
Hp = 204
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -209349
43 X = -42555
50
Y = -13805404
23 feet Y = -4208482
02 meter
Z = 17427644
92 Z = 5311687
74
XDOT = 25112
491399 XDOT = 7657
682564
YDOT = -967
469849 feet/sec YDOT = -209
270875 meter/sec
ZDOT = -450
218348 ZDOT = -100
034501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12626112
53 X = 3848439
10
Y = -5589478
93 feet Y = -1703673
18 meter
Z = 17426842
17 Z = 5311701
49
XDOT = 10125
750270 XDOT = 3086
328682
YDOT = 21898
926834 feet/sec YDOT = 6674
792899 meter/sec
ZDOT = -297
959392 ZDOT = -90
818023
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
54789459
00016717 00000-0 10270-3 0 9084
2 25544 51
6376 177
8105 0023739 281
4809 78
3680 15
59145127 33902
Satellite: ISS
Catalog Number: 25544
Epoch time: 12014
54789459 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 177
8105 deg
Eccentricity:
0023739
Arg of perigee: 281
4809 deg
Mean anomaly: 78
3680 deg
Mean motion: 15
59145127 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 340
Coasting Arc #10 (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 = -3679409
95 A = 6767046
38 meter
Y = 3845198
26 meter E =
0015869
Z = -4163902
16 I = 51
67838
XDOT = -6393
670218 Wp = 282
83281
YDOT = -2070
783132 meter/sec RA = 171
93562 deg
ZDOT = 3728
966798 TA = 25
40662
MA = 25
32868
Ha = 215
626 n
mi
Hp = 204
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12071554
96 X = -3701907
10
Y = 12615479
86 feet Y = 3803927
15 meter
Z = -13661096
32 Z = -4181831
00
XDOT = -20976
608326 XDOT = -6388
153478
YDOT = -6793
907913 feet/sec YDOT = -2142
250330 meter/sec
ZDOT = 12234
143039 ZDOT = 3697
920183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16354793
33 X = -4984941
01
Y = -5947801
40 feet Y = -1812889
87 meter
Z = -13734726
70 Z = -4186344
70
XDOT = -2619
701705 XDOT = -798
485080
YDOT = -20818
464110 feet/sec YDOT = -6345
467861 meter/sec
ZDOT = 12107
172436 ZDOT = 3690
266158
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
50927700
00016717 00000-0 10270-3 0 9095
2 25544 51
6387 172
9808 0023774 284
9105 74
9418 15
59226819 34052
Satellite: ISS
Catalog Number: 25544
Epoch time: 12015
50927700 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 172
9808 deg
Eccentricity:
0023774
Arg of perigee: 284
9105 deg
Mean anomaly: 74
9418 deg
Mean motion: 15
59226819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 331
Coasting Arc #11 (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 = 6132813
38 A = 6773586
91 meter
Y = -2534500
16 meter E =
0010575
Z = 1371170
03 I = 51
72967
XDOT = 2956
301537 Wp = 275
44936
YDOT = 4025
968805 meter/sec RA = 166
92801 deg
ZDOT = -5818
500686 TA = 249
61436
MA = 249
72798
Ha = 215
862 n
mi
Hp = 204
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20120778
80 X = 6154038
05
Y = -8315289
25 feet Y = -2465800
66 meter
Z = 4498589
34 Z = 1401014
29
XDOT = 9699
152025 XDOT = 2939
327479
YDOT = 13208
559072 feet/sec YDOT = 4058
933324 meter/sec
ZDOT = -19089
569181 ZDOT = -5804
180225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15909908
71 X = 4849340
18
Y = 14823928
99 feet Y = 4518333
56 meter
Z = 4620932
28 Z = 1408460
16
XDOT = -6856
476318 XDOT = -2089
853982
YDOT = 13253
781223 feet/sec YDOT = 4039
752517 meter/sec
ZDOT = -19031
187472 ZDOT = -5800
705941
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
53473328
00016717 00000-0 10270-3 0 9103
2 25544 51
6378 167
8290 0023916 288
9918 70
8646 15
59264324 34213
Satellite: ISS
Catalog Number: 25544
Epoch time: 12016
53473328 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 167
8290 deg
Eccentricity:
0023916
Arg of perigee: 288
9918 deg
Mean anomaly: 70
8646 deg
Mean motion: 15
59264324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 330
Coasting Arc #12 (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 = -6440472
27 A = 6772616
60 meter
Y = 416413
34 meter E =
0016863
Z = 2030985
20 I = 51
75730
XDOT = 1418
699180 Wp = 328
14756
YDOT = -5085
344298 meter/sec RA = 161
94047 deg
ZDOT = 5576
505833 TA = 54
32241
MA = 54
16556
Ha = 216
014 n
mi
Hp = 204
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21130158
37 X = -6454516
05
Y = 1366185
51 feet Y = 344313
37 meter
Z = 6663337
28 Z = 1999663
71
XDOT = 4654
524869 XDOT = 1448
369776
YDOT = -16684
200454 feet/sec YDOT = -5069
313995 meter/sec
ZDOT = 18295
622812 ZDOT = 5583
469523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10356593
63 X = -3156689
74
Y = -18514428
17 feet Y = -5643197
71 meter
Z = 6535062
15 Z = 1991886
94
XDOT = 15662
391422 XDOT = 4773
896905
YDOT = -2334
553077 feet/sec YDOT = -711
571778 meter/sec
ZDOT = 18324
455107 ZDOT = 5585
293917
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
56016977
00016717 00000-0 10270-3 0 9111
2 25544 51
6391 162
6764 0023781 292
6428 67
2213 15
59308977 34375
Satellite: ISS
Catalog Number: 25544
Epoch time: 12017
56016977 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 162
6764 deg
Eccentricity:
0023781
Arg of perigee: 292
6428 deg
Mean anomaly: 67
2213 deg
Mean motion: 15
59308977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 330
Coasting Arc #13 (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 = 3062032
45 A = 6770170
90 meter
Y = -4547985
69 meter E =
0012934
Z = 3986379
47 I = 51
75840
XDOT = 6485
829409 Wp = 323
10092
YDOT = 867
797623 meter/sec RA = 158
91177 deg
ZDOT = -3988
476505 TA = 168
41730
MA = 168
38751
Ha = 216
276 n
mi
Hp = 206
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10046038
22 X = 3093296
52
Y = -14921212
89 feet Y = -4513569
66 meter
Z = 13078672
81 Z = 4001330
20
XDOT = 21278
967877 XDOT = 6495
018499
YDOT = 2847
105061 feet/sec YDOT = 940
377844 meter/sec
ZDOT = -13085
552839 ZDOT = -3956
946409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15984301
18 X = -4872015
00
Y = 8151985
80 feet Y = 2484725
27 meter
Z = 13140182
79 Z = 4005127
72
XDOT = -16652
525480 XDOT = -5075
689766
YDOT = -11749
636749 feet/sec YDOT = -3581
289281 meter/sec
ZDOT = -12956
494868 ZDOT = -3949
139636
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
13700085
00016717 00000-0 10270-3 0 9126
2 25544 51
6400 159
7842 0020235 293
9370 65
9666 15
58383283 34460
Satellite: ISS
Catalog Number: 25544
Epoch time: 12018
13700085 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 159
7842 deg
Eccentricity:
0020235
Arg of perigee: 293
9370 deg
Mean anomaly: 65
9666 deg
Mean motion: 15
58383283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 310
Coasting Arc #14 (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 = -5424411
10 A = 6776148
79 meter
Y = 3815964
44 meter E =
0020741
Z = -1324734
49 I = 51
80653
XDOT = -3748
269483 Wp = 322
74480
YDOT = -3287
226904 meter/sec RA = 153
91564 deg
ZDOT = 5847
572385 TA = 22
82343
MA = 22
73137
Ha = 216
522 n
mi
Hp = 206
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17796624
33 X = -5460243
61
Y = 12519568
36 feet Y = 3755105
11 meter
Z = -4346241
76 Z = -1351172
48
XDOT = -12297
472056 XDOT = -3739
638409
YDOT = -10784
865171 feet/sec YDOT = -3329
094650 meter/sec
ZDOT = 19184
948770 ZDOT = 5829
384274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21579052
38 X = 6577295
17
Y = -2617026
44 feet Y = -797669
66 meter
Z = -4454763
51 Z = -1357811
92
XDOT = 5639
790572 XDOT = 1719
008166
YDOT = 13801
391471 feet/sec YDOT = 4206
664120 meter/sec
ZDOT = 19110
671414 ZDOT = 5824
932647
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
09888372
00016717 00000-0 10270-3 0 9139
2 25544 51
6400 154
9570 0020342 297
8627 62
0467 15
58404396 34615
Satellite: ISS
Catalog Number: 25544
Epoch time: 12019
09888372 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 154
9570 deg
Eccentricity:
0020342
Arg of perigee: 297
8627 deg
Mean anomaly: 62
0467 deg
Mean motion: 15
58404396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 318
Coasting Arc #15 (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 = 6192264
33 A = 6775544
90 meter
Y = -2104117
08 meter E =
0013472
Z = -1771744
27 I = 51
83261
XDOT = 111
723126 Wp = 290
66829
YDOT = 5148
273586 meter/sec RA = 148
93794 deg
ZDOT = -5684
090536 TA = 268
75767
MA = 268
91201
Ha = 216
742 n
mi
Hp = 206
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20315827
85 X = 6223939
37
Y = -6903271
26 feet Y = -2034694
09 meter
Z = -5812809
29 Z = -1741586
22
XDOT = 366
545690 XDOT = 81
757439
YDOT = 16890
661371 feet/sec YDOT = 5149
355965 meter/sec
ZDOT = -18648
590999 ZDOT = -5683
620067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21252257
11 X = -6477687
97
Y = -3186219
13 feet Y = -971159
59 meter
Z = -5689142
49 Z = -1734050
63
XDOT = 7078
594882 XDOT = 2157
555720
YDOT = -13683
065702 feet/sec YDOT = -4170
598426 meter/sec
ZDOT = -18646
999579 ZDOT = -5683
605472
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
12487358
00016717 00000-0 10270-3 0 9145
2 25544 51
6410 149
8091 0020309 301
6694 58
2480 15
58439498 34778
Satellite: ISS
Catalog Number: 25544
Epoch time: 12020
12487358 = yrday
fracday
Element set: 914
Inclination: 51
6410 deg
RA of node: 149
8091 deg
Eccentricity:
0020309
Arg of perigee: 301
6694 deg
Mean anomaly: 58
2480 deg
Mean motion: 15
58439498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 317
Coasting Arc #16 (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 = -5213526
12 A = 6768965
10 meter
Y = -384489
36 meter E =
0011351
Z = 4300345
63 I = 51
83648
XDOT = 3361
139430 Wp = 322
30879
YDOT = -5908
453953 meter/sec RA = 143
94091 deg
ZDOT = 3560
315908 TA = 91
59141
MA = 91
46139
Ha = 217
056 n
mi
Hp = 206
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17104744
49 X = -5229728
91
Y = -1261448
03 feet Y = -442881
22 meter
Z = 14108745
51 Z = 4274979
65
XDOT = 11027
360334 XDOT = 3409
664261
YDOT = -19384
691448 feet/sec YDOT = -5870
596646 meter/sec
ZDOT = 11680
826471 ZDOT = 3576
761160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14855157
71 X = 4527852
07
Y = 8741199
64 feet Y = 2664317
65 meter
Z = 14004854
63 Z = 4268679
69
XDOT = -17768
794765 XDOT = -5415
928644
YDOT = 11446
417381 feet/sec YDOT = 3488
868018 meter/sec
ZDOT = 11748
585848 ZDOT = 3580
968966
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
15084389
00016717 00000-0 10270-3 0 9157
2 25544 51
6412 144
6601 0020297 305
8691 54
0578 15
58470020 34935
Satellite: ISS
Catalog Number: 25544
Epoch time: 12021
15084389 = yrday
fracday
Element set: 915
Inclination: 51
6412 deg
RA of node: 144
6601 deg
Eccentricity:
0020297
Arg of perigee: 305
8691 deg
Mean anomaly: 54
0578 deg
Mean motion: 15
58470020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 296
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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