[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 8th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19052 12 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
258/03:19:38
135 -3
4 4
2 4
2
N/A -1
6 -0
5 234
6
000/00:09:16
270 1
9 0
0 214
8
Coasting Arc #1 (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 = -2333118
46 A = 6791126
51 meter
Y = 4376062
41 meter E =
0019771
Z = 4620083
27 I = 51
96652
XDOT = -4375
471572 Wp = 66
85800
YDOT = -5532
678546 meter/sec RA = 71
28350 deg
ZDOT = 3028
185856 TA = 353
07283
MA = 353
10011
Ha = 232
184 n
mi
Hp = 215
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7654588
14 X = -2404322
43
Y = 14357160
14 feet Y = 4349574
13 meter
Z = 15157753
51 Z = 4608575
91
XDOT = -14355
221692 XDOT = -4327
989070
YDOT = -18151
832500 feet/sec YDOT = -5581
342155 meter/sec
ZDOT = 9934
992965 ZDOT = 3007
045611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10956561
66 X = 3339559
99
Y = -12088360
48 feet Y = -3684532
27 meter
Z = 15109717
26 Z = 4605441
82
XDOT = 8774
358153 XDOT = 2674
424365
YDOT = 20273
403527 feet/sec YDOT = 6179
333395 meter/sec
ZDOT = 9848
108294 ZDOT = 3001
703408
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
55374153
00016717 00000-0 10270-3 0 9001
2 25544 51
6433 71
7120 0015381 43
4346 316
8013 15
50422662 30822
Satellite: ISS
Catalog Number: 25544
Epoch time: 12251
55374153 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 71
7120 deg
Eccentricity:
0015381
Arg of perigee: 43
4346 deg
Mean anomaly: 316
8013 deg
Mean motion: 15
50422662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 267
Coasting Arc #2 (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 = 2341475
86 A = 6790118
11 meter
Y = -4145822
66 meter E =
0026457
Z = -4865969
16 I = 51
95308
XDOT = 4592
897883 Wp = 57
90101
YDOT = 5561
266228 meter/sec RA = 66
34559 deg
ZDOT = -2524
550613 TA = 187
27626
MA = 187
31474
Ha = 232
116 n
mi
Hp = 215
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7682007
41 X = 2411299
04
Y = -13601780
37 feet Y = -4119248
63 meter
Z = -15964465
74 Z = -4854424
61
XDOT = 15068
562608 XDOT = 4542
632979
YDOT = 18245
624106 feet/sec YDOT = 5612
345715 meter/sec
ZDOT = -8282
646368 ZDOT = -2502
360887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10610534
20 X = -3234090
83
Y = 11531438
18 feet Y = 3514782
36 meter
Z = -15916291
37 Z = -4851285
61
XDOT = -9840
725931 XDOT = -2999
453264
YDOT = -20377
396469 feet/sec YDOT = -6211
030444 meter/sec
ZDOT = -8191
430252 ZDOT = -2496
747941
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
52056651
00016717 00000-0 10270-3 0 9010
2 25544 51
6435 66
9190 0015476 47
6541 312
5918 15
50467875 30973
Satellite: ISS
Catalog Number: 25544
Epoch time: 12252
52056651 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 66
9190 deg
Eccentricity:
0015476
Arg of perigee: 47
6541 deg
Mean anomaly: 312
5918 deg
Mean motion: 15
50467875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 317
Coasting Arc #3 (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 = -2381691
96 A = 6789296
25 meter
Y = 3864146
39 meter E =
0018020
Z = 5032354
14 I = 51
93700
XDOT = -4846
444783 Wp = 68
59239
YDOT = -5603
225365 meter/sec RA = 61
40497 deg
ZDOT = 2009
436460 TA = 1
99129
MA = 1
98412
Ha = 232
249 n
mi
Hp = 215
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7813950
00 X = -2449170
59
Y = 12677645
65 feet Y = 3837135
75 meter
Z = 16510348
22 Z = 5020619
96
XDOT = -15900
409393 XDOT = -4793
189511
YDOT = -18383
285319 feet/sec YDOT = -5657
123477 meter/sec
ZDOT = 6592
639306 ZDOT = 1986
022329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10352968
08 X = 3155584
67
Y = -10780077
49 feet Y = -3285767
62 meter
Z = 16461412
26 Z = 5017438
46
XDOT = 11033
364969 XDOT = 3362
969643
YDOT = 20513
068883 feet/sec YDOT = 6252
383395 meter/sec
ZDOT = 6496
368150 ZDOT = 1980
093012
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
55182796
00016717 00000-0 10270-3 0 9025
2 25544 51
6431 61
8053 0015431 50
9541 309
2981 15
50471951 31131
Satellite: ISS
Catalog Number: 25544
Epoch time: 12253
55182796 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 61
8053 deg
Eccentricity:
0015431
Arg of perigee: 50
9541 deg
Mean anomaly: 309
2981 deg
Mean motion: 15
50471951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 290
Coasting Arc #4 (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 = 2484641
53 A = 6788555
05 meter
Y = -3624929
98 meter E =
0028636
Z = -5199161
49 I = 51
92040
XDOT = 5045
758216 Wp = 66
09477
YDOT = 5550
918251 meter/sec RA = 56
46406 deg
ZDOT = -1453
914398 TA = 189
88854
MA = 189
94501
Ha = 232
138 n
mi
Hp = 215
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8151711
06 X = 2550247
79
Y = -11892814
89 feet Y = -3596778
59 meter
Z = -17057616
45 Z = -5186931
76
XDOT = 16554
324856 XDOT = 4990
374431
YDOT = 18211
674053 feet/sec YDOT = 5607
033326 meter/sec
ZDOT = -4770
060361 ZDOT = -1429
537269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10352827
62 X = -3155541
86
Y = 10121487
04 feet Y = 3085029
25 meter
Z = -17006651
01 Z = -5183627
23
XDOT = -12109
047522 XDOT = -3690
837685
YDOT = -20259
547856 feet/sec YDOT = -6175
110186 meter/sec
ZDOT = -4669
804428 ZDOT = -1423
356390
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
51861715
00016717 00000-0 10270-3 0 9038
2 25544 51
6440 57
0125 0015502 55
0554 305
2051 15
50525364 31285
Satellite: ISS
Catalog Number: 25544
Epoch time: 12254
51861715 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 57
0125 deg
Eccentricity:
0015502
Arg of perigee: 55
0554 deg
Mean anomaly: 305
2051 deg
Mean motion: 15
50525364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 267
Coasting Arc #5 (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 = -2626887
50 A = 6788086
65 meter
Y = 3343960
39 meter E =
0017317
Z = 5276441
04 I = 51
90068
XDOT = -5264
882806 Wp = 67
57903
YDOT = -5516
058463 meter/sec RA = 51
51933 deg
ZDOT = 878
831449 TA = 14
07932
MA = 14
03111
Ha = 232
296 n
mi
Hp = 215
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8618397
31 X = -2689716
68
Y = 10970998
64 feet Y = 3314233
91 meter
Z = 17311158
25 Z = 5263527
03
XDOT = -17273
237553 XDOT = -5207
078929
YDOT = -18097
304668 feet/sec YDOT = -5574
610411 meter/sec
ZDOT = 2883
305279 ZDOT = 853
395824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10480040
57 X = 3194316
37
Y = -9309514
50 feet Y = -2837540
02 meter
Z = 17257388
93 Z = 5260052
15
XDOT = 13244
296496 XDOT = 4036
861572
YDOT = 20035
189849 feet/sec YDOT = 6106
725866 meter/sec
ZDOT = 2778
670581 ZDOT = 846
938793
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
54984043
00016717 00000-0 10270-3 0 9043
2 25544 51
6434 51
8981 0015501 58
3794 301
8867 15
50523165 31443
Satellite: ISS
Catalog Number: 25544
Epoch time: 12255
54984043 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 51
8981 deg
Eccentricity:
0015501
Arg of perigee: 58
3794 deg
Mean anomaly: 301
8867 deg
Mean motion: 15
50523165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 310
Coasting Arc #6 (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 = 2820724
89 A = 6787727
18 meter
Y = -3125498
35 meter E =
0029557
Z = -5349204
65 I = 51
88150
XDOT = 5410
783252 Wp = 74
45525
YDOT = 5387
619027 meter/sec RA = 46
57522 deg
ZDOT = -288
382092 TA = 192
75761
MA = 192
83257
Ha = 232
132 n
mi
Hp = 214
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9254346
74 X = 2881450
21
Y = -10254259
67 feet Y = -3093616
13 meter
Z = -17549884
03 Z = -5335354
08
XDOT = 17751
913558 XDOT = 5351
536519
YDOT = 17675
915442 feet/sec YDOT = 5447
794488 meter/sec
ZDOT = -946
135473 ZDOT = -262
241321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10837052
23 X = -3303133
52
Y = 8681604
47 feet Y = 2646153
04 meter
Z = -17492262
50 Z = -5331641
61
XDOT = -14172
227814 XDOT = -4319
695038
YDOT = -19422
702644 feet/sec YDOT = -5920
039766 meter/sec
ZDOT = -838
573814 ZDOT = -255
597298
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
51659247
00016717 00000-0 10270-3 0 9057
2 25544 51
6446 47
1055 0015518 62
2078 298
0644 15
50585231 31591
Satellite: ISS
Catalog Number: 25544
Epoch time: 12256
51659247 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 47
1055 deg
Eccentricity:
0015518
Arg of perigee: 62
2078 deg
Mean anomaly: 298
0644 deg
Mean motion: 15
50585231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 312
Coasting Arc #7 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2012/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 954334
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3055955
28 A = 6787736
40 meter
Y = 2874780
14 meter E =
0018125
Z = 5321771
16 I = 51
85964
XDOT = -5557
359318 Wp = 66
27687
YDOT = -5284
081755 meter/sec RA = 41
62653 deg
ZDOT = -328
818037 TA = 26
89241
MA = 26
79858
Ha = 232
308 n
mi
Hp = 214
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10026099
98 X = -3113726
29
Y = 9431693
36 feet Y = 2840284
06 meter
Z = 17459879
13 Z = 5306784
98
XDOT = -18232
806160 XDOT = -5496
261272
YDOT = -17336
226230 feet/sec YDOT = -5345
886027 meter/sec
ZDOT = -1078
799335 ZDOT = -355
666269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11336530
22 X = 3455374
41
Y = -7945686
98 feet Y = -2421845
39 meter
Z = 17397587
22 Z = 5302784
58
XDOT = 15082
221523 XDOT = 4597
061120
YDOT = 18856
891091 feet/sec YDOT = 5747
580404 meter/sec
ZDOT = -1189
293905 ZDOT = -362
496782
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 12257
54777636
00016717 00000-0 10270-3 0 9065
2 25544 51
6442 41
9906 0015551 65
6045 294
6727 15
50577931 31752
Satellite: ISS
Catalog Number: 25544
Epoch time: 12257
54777636 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 41
9906 deg
Eccentricity:
0015551
Arg of perigee: 65
6045 deg
Mean anomaly: 294
6727 deg
Mean motion: 15
50577931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 331
Coasting Arc #8 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2012/258/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1486479
58 A = 6790254
21 meter
Y = 4056348
41 meter E =
0021202
Z = 5220083
84 I = 51
84932
XDOT = -6481
245373 Wp = 73
85137
YDOT = -3933
605551 meter/sec RA = 38
47292 deg
ZDOT = 1212
740734 TA = 4
57122
MA = 4
55188
Ha = 234
628 n
mi
Hp = 214
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4876901
51 X = -1557085
84
Y = 13308229
69 feet Y = 4039331
49 meter
Z = 17126259
32 Z = 5212690
68
XDOT = -21263
928390 XDOT = -6442
668458
YDOT = -12905
530023 feet/sec YDOT = -4005
867044 meter/sec
ZDOT = 3978
808184 ZDOT = 1181
349516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5610861
45 X = 1710190
57
Y = 13056514
67 feet Y = 3979625
67 meter
Z = 17095249
70 Z = 5210632
11
XDOT = -23347
253438 XDOT = -7116
242848
YDOT = 5000
297813 feet/sec YDOT = 1524
090773 meter/sec
ZDOT = 3849
383368 ZDOT = 1173
292050
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 12258
19228679
00016717 00000-0 10270-3 0 9076
2 25544 51
6472 38
8014 0018883 65
2027 295
1086 15
49855110 31858
Satellite: ISS
Catalog Number: 25544
Epoch time: 12258
19228679 = yrday
fracday
Element set: 907
Inclination: 51
6472 deg
RA of node: 38
8014 deg
Eccentricity:
0018883
Arg of perigee: 65
2027 deg
Mean anomaly: 295
1086 deg
Mean motion: 15
49855110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 328
Coasting Arc #9 (Orbit 3199)
---------------------------------------
Vector Time (GMT): 2012/259/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1454597
78 A = 6790055
10 meter
Y = -4030877
67 meter E =
0033194
Z = -5295784
69 I = 51
82533
XDOT = 6682
290342 Wp = 74
49201
YDOT = 3587
567014 meter/sec RA = 33
53149 deg
ZDOT = -891
283090 TA = 186
94701
MA = 186
99314
Ha = 234
606 n
mi
Hp = 214
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4772302
42 X = 1525289
42
Y = -13224664
28 feet Y = -4014216
88 meter
Z = -17374621
67 Z = -5288546
11
XDOT = 21923
524745 XDOT = 6646
006416
YDOT = 11770
232984 feet/sec YDOT = 3662
089561 meter/sec
ZDOT = -2924
157120 ZDOT = -858
909546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5848976
01 X = -1782767
89
Y = -12826161
56 feet Y = -3909414
04 meter
Z = -17344254
18 Z = -5286528
68
XDOT = 22931
778987 XDOT = 6989
606235
YDOT = -6666
084510 feet/sec YDOT = -2031
822559 meter/sec
ZDOT = -2790
640738 ZDOT = -850
587297
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 12259
15949151
00016717 00000-0 10270-3 0 9089
2 25544 51
6483 34
0107 0019019 68
4447 291
8728 15
49864826 32002
Satellite: ISS
Catalog Number: 25544
Epoch time: 12259
15949151 = yrday
fracday
Element set: 908
Inclination: 51
6483 deg
RA of node: 34
0107 deg
Eccentricity:
0019019
Arg of perigee: 68
4447 deg
Mean anomaly: 291
8728 deg
Mean motion: 15
49864826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3200
Checksum: 325
Coasting Arc #10 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2012/260/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1448166
63 A = 6789710
52 meter
Y = 3962442
55 meter E =
0021083
Z = 5301881
17 I = 51
79905
XDOT = -6923
144795 Wp = 76
26877
YDOT = -3272
722832 meter/sec RA = 28
58815 deg
ZDOT = 557
949024 TA = 8
44312
MA = 8
40770
Ha = 234
580 n
mi
Hp = 214
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4751202
85 X = -1518123
23
Y = 13000139
61 feet Y = 3945857
82 meter
Z = 17394623
25 Z = 5294675
57
XDOT = -22713
729642 XDOT = -6888
744376
YDOT = -10737
279633 feet/sec YDOT = -3349
949337 meter/sec
ZDOT = 1830
541416 ZDOT = 524
400667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5922557
12 X = 1805195
41
Y = 12551949
66 feet Y = 3825834
26 meter
Z = 17364399
02 Z = 5292668
82
XDOT = -22633
168385 XDOT = -6898
589724
YDOT = 8352
181719 feet/sec YDOT = 2545
744988 meter/sec
ZDOT = 1692
143171 ZDOT = 515
765239
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 12260
19115438
00016717 00000-0 10270-3 0 9099
2 25544 51
6484 28
9007 0018881 72
0207 288
3000 15
49915451 32167
Satellite: ISS
Catalog Number: 25544
Epoch time: 12260
19115438 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 28
9007 deg
Eccentricity:
0018881
Arg of perigee: 72
0207 deg
Mean anomaly: 288
3000 deg
Mean motion: 15
49915451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 300
Coasting Arc #11 (Orbit 3230)
---------------------------------------
Vector Time (GMT): 2012/261/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1463955
45 A = 6789643
39 meter
Y = -3957647
34 meter E =
0033542
Z = -5347931
92 I = 51
77260
XDOT = 7058
802976 Wp = 80
65373
YDOT = 2906
071252 meter/sec RA = 23
64291 deg
ZDOT = -214
149791 TA = 187
27610
MA = 187
32490
Ha = 234
529 n
mi
Hp = 214
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4803003
44 X = 1534081
09
Y = -12984407
28 feet Y = -3940885
08 meter
Z = -17545708
40 Z = -5340649
20
XDOT = 23158
802414 XDOT = 7026
822352
YDOT = 9534
354502 feet/sec YDOT = 2984
828349 meter/sec
ZDOT = -702
591177 ZDOT = -179
936300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6090005
56 X = -1856233
69
Y = -12475832
95 feet Y = -3802633
88 meter
Z = -17515164
35 Z = -5338622
09
XDOT = 21908
580748 XDOT = 6677
735412
YDOT = -9887
230054 feet/sec YDOT = -3013
627720 meter/sec
ZDOT = -561
414861 ZDOT = -171
119250
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 12261
15832151
00016717 00000-0 10270-3 0 9106
2 25544 51
6493 24
1101 0018952 75
1927 285
1321 15
49926310 32316
Satellite: ISS
Catalog Number: 25544
Epoch time: 12261
15832151 = yrday
fracday
Element set: 910
Inclination: 51
6493 deg
RA of node: 24
1101 deg
Eccentricity:
0018952
Arg of perigee: 75
1927 deg
Mean anomaly: 285
1321 deg
Mean motion: 15
49926310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3231
Checksum: 276
Coasting Arc #12 (Orbit 3246)
---------------------------------------
Vector Time (GMT): 2012/262/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1506250
48 A = 6789455
09 meter
Y = 3917659
29 meter E =
0021301
Z = 5318711
32 I = 51
74453
XDOT = -7232
993249 Wp = 78
43918
YDOT = -2571
872530 meter/sec RA = 18
69545 deg
ZDOT = -149
301219 TA = 13
00717
MA = 12
95232
Ha = 234
501 n
mi
Hp = 214
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4941766
65 X = -1575783
97
Y = 12853212
89 feet Y = 3900427
28 meter
Z = 17449840
30 Z = 5311224
61
XDOT = -23730
292812 XDOT = -7202
971181
YDOT = -8437
902000 feet/sec YDOT = -2652
588526 meter/sec
ZDOT = -489
833397 ZDOT = -184
365900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6113678
87 X = 1863449
32
Y = 12383191
74 feet Y = 3774396
84 meter
Z = 17418454
54 Z = 5309144
94
XDOT = -21302
666987 XDOT = -6493
052898
YDOT = 11431
505152 feet/sec YDOT = 3484
322770 meter/sec
ZDOT = -634
554050 ZDOT = -193
412074
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 12262
18994428
00016717 00000-0 10270-3 0 9117
2 25544 51
6494 19
0001 0018845 78
7790 281
5478 15
49977294 32474
Satellite: ISS
Catalog Number: 25544
Epoch time: 12262
18994428 = yrday
fracday
Element set: 911
Inclination: 51
6494 deg
RA of node: 19
0001 deg
Eccentricity:
0018845
Arg of perigee: 78
7790 deg
Mean anomaly: 281
5478 deg
Mean motion: 15
49977294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3247
Checksum: 345
Coasting Arc #13 (Orbit 3261)
---------------------------------------
Vector Time (GMT): 2012/263/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1560385
12 A = 6789556
39 meter
Y = -3947513
96 meter E =
0033339
Z = -5327784
34 I = 51
71593
XDOT = 7295
246962 Wp = 86
88832
YDOT = 2199
917150 meter/sec RA = 13
74576 deg
ZDOT = 511
157770 TA = 187
97667
MA = 188
02981
Ha = 234
424 n
mi
Hp = 214
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5119373
76 X = 1630292
56
Y = -12951161
29 feet Y = -3929674
38 meter
Z = -17479607
41 Z = -5320033
79
XDOT = 23934
537277 XDOT = 7267
621709
YDOT = 7217
575952 feet/sec YDOT = 2281
342738 meter/sec
ZDOT = 1677
026803 ZDOT = 546
530859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6282043
81 X = -1914766
95
Y = -12474414
83 feet Y = -3802201
64 meter
Z = -17447124
17 Z = -5317883
45
XDOT = 20301
632598 XDOT = 6187
937616
YDOT = -12752
731921 feet/sec YDOT = -3887
032690 meter/sec
ZDOT = 1823
053516 ZDOT = 555
666712
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 12263
15707323
00016717 00000-0 10270-3 0 9122
2 25544 51
6495 14
2094 0018853 81
9486 278
3803 15
49987050 32625
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
15707323 = yrday
fracday
Element set: 912
Inclination: 51
6495 deg
RA of node: 14
2094 deg
Eccentricity:
0018853
Arg of perigee: 81
9486 deg
Mean anomaly: 278
3803 deg
Mean motion: 15
49987050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3262
Checksum: 321
Coasting Arc #14 (Orbit 3277)
---------------------------------------
Vector Time (GMT): 2012/264/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1640012
28 A = 6789562
38 meter
Y = 3948544
51 meter E =
0021953
Z = 5255946
54 I = 51
68687
XDOT = -7393
902158 Wp = 80
82330
YDOT = -1863
694770 meter/sec RA = 8
79382 deg
ZDOT = -900
380171 TA = 17
81028
MA = 17
73345
Ha = 234
395 n
mi
Hp = 214
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5380617
71 X = -1709576
33
Y = 12954542
36 feet Y = 3929816
29 meter
Z = 17243919
09 Z = 5247810
09
XDOT = -24258
209179 XDOT = -7368
138505
YDOT = -6114
484155 feet/sec YDOT = -1946
234007 meter/sec
ZDOT = -2954
003187 ZDOT = -936
237110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6330188
16 X = 1929441
35
Y = 12564800
16 feet Y = 3829751
09 meter
Z = 17209836
57 Z = 5245558
19
XDOT = -19427
892386 XDOT = -5921
621599
YDOT = 14066
549864 feet/sec YDOT = 4287
484398 meter/sec
ZDOT = -3102
060820 ZDOT = -945
508138
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 12264
18865527
00016717 00000-0 10270-3 0 9138
2 25544 51
6495 9
0991 0018776 85
5533 274
7762 15
50038335 32786
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
18865527 = yrday
fracday
Element set: 913
Inclination: 51
6495 deg
RA of node: 9
0991 deg
Eccentricity:
0018776
Arg of perigee: 85
5533 deg
Mean anomaly: 274
7762 deg
Mean motion: 15
50038335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3278
Checksum: 338
Coasting Arc #15 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2012/265/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1718709
30 A = 6789855
33 meter
Y = -4023444
59 meter E =
0032531
Z = -5220793
05 I = 51
65704
XDOT = 7378
369197 Wp = 93
13453
YDOT = 1505
211436 meter/sec RA = 3
83915 deg
ZDOT = 1274
143425 TA = 189
11699
MA = 189
17620
Ha = 234
305 n
mi
Hp = 214
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5638810
03 X = 1788934
22
Y = -13200277
54 feet Y = -4003832
55 meter
Z = -17128586
13 Z = -5212272
77
XDOT = 24207
248023 XDOT = 7354
799672
YDOT = 4938
357731 feet/sec YDOT = 1587
589245 meter/sec
ZDOT = 4180
260582 ZDOT = 1309
930201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6572297
60 X = -2003236
31
Y = -12808960
21 feet Y = -3904171
07 meter
Z = -17092905
29 Z = -5209917
53
XDOT = 18210
373722 XDOT = 5550
521910
YDOT = -15096
745676 feet/sec YDOT = -4601
488082 meter/sec
ZDOT = 4328
064252 ZDOT = 1319
193984
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 12265
15574567
00016717 00000-0 10270-3 0 9148
2 25544 51
6488 4
3076 0018752 88
8046 271
5253 15
50046311 32939
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
15574567 = yrday
fracday
Element set: 914
Inclination: 51
6488 deg
RA of node: 4
3076 deg
Eccentricity:
0018752
Arg of perigee: 88
8046 deg
Mean anomaly: 271
5253 deg
Mean motion: 15
50046311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 311
Coasting Arc #16 (Orbit 3308)
---------------------------------------
Vector Time (GMT): 2012/266/03:24:16
270
Vector Time (MET): N/A
Weight (LBS) : 953928
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1820045
41 A = 6790086
08 meter
Y = 4073705
91 meter E =
0023068
Z = 5099115
72 I = 51
62811
XDOT = -7396
854136 Wp = 83
96083
YDOT = -1187
942890 meter/sec RA = 358
88260 deg
ZDOT = -1682
214397 TA = 22
31677
MA = 22
21656
Ha = 234
266 n
mi
Hp = 214
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5971277
58 X = -1890233
65
Y = 13365176
88 feet Y = 4052960
82 meter
Z = 16729382
27 Z = 5090103
30
XDOT = -24267
894148 XDOT = -7374
848696
YDOT = -3897
450428 feet/sec YDOT = -1270
536162 meter/sec
ZDOT = -5519
076106 ZDOT = -1718
094665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6716257
20 X = 2047115
20
Y = 13055142
20 feet Y = 3979207
34 meter
Z = 16691659
33 Z = 5087617
77
XDOT = -17137
826354 XDOT = -5223
609473
YDOT = 16100
030025 feet/sec YDOT = 4907
289152 meter/sec
ZDOT = -5667
300409 ZDOT = -1727
393165
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 12266
18728666
00016717 00000-0 10270-3 0 9154
2 25544 51
6488 359
1969 0018681 92
4271 267
9018 15
50096968 33092
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
18728666 = yrday
fracday
Element set: 915
Inclination: 51
6488 deg
RA of node: 359
1969 deg
Eccentricity:
0018681
Arg of perigee: 92
4271 deg
Mean anomaly: 267
9018 deg
Mean motion: 15
50096968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3309
Checksum: 360
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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