[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 19th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 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
322/04:08:48
333 -1
0 11
1 11
1
N/A -9
4 -1
0 225
7
000/00:03:36
666 5
9 0
1 197
4
334/22:27:31
837 -2
8 3
3 3
3
N/A -1
4 0
0 226
5
000/00:01:03
675 1
0 -0
0 196
8
Coasting Arc #1 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2011/320/15:36:34
779
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -851387
14 A = 6765588
49 meter
Y = -5569353
12 meter E =
0032912
Z = 3728202
13 I = 51
95908
XDOT = 5179
858020 Wp = 71
16899
YDOT = -3702
356774 meter/sec RA = 112
49052 deg
ZDOT = -4306
584651 TA = 64
34845
MA = 64
00883
Ha = 219
194 n
mi
Hp = 197
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2793264
88 X = -807157
35
Y = -18272155
92 feet Y = -5578626
71 meter
Z = 12231634
30 Z = 3724173
26
XDOT = 16994
284842 XDOT = 5241
794330
YDOT = -12146
839809 feet/sec YDOT = -3644
085939 meter/sec
ZDOT = -14129
214735 ZDOT = -4281
270374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16385689
69 X = 4994358
22
Y = -8577713
10 feet Y = -2614486
95 meter
Z = 12215518
81 Z = 3723290
13
XDOT = 16359
591958 XDOT = 4986
403629
YDOT = 11084
161553 feet/sec YDOT = 3378
452441 meter/sec
ZDOT = -14025
635586 ZDOT = -4275
013727
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 11320
69048830
00016717 00000-0 10270-3 0 9002
2 25544 51
6403 113
2139 0021689 64
1576 296
1813 15
60276563 24722
Satellite: ISS
Catalog Number: 25544
Epoch time: 11320
69048830 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 113
2139 deg
Eccentricity:
0021689
Arg of perigee: 64
1576 deg
Mean anomaly: 296
1813 deg
Mean motion: 15
60276563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 298
Coasting Arc #2 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2011/321/15:36:34
779
Vector Time (MET): N/A
Weight (LBS) : 886882
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1729816
56 A = 6771362
18 meter
Y = 6524117
10 meter E =
0032284
Z = -399793
79 I = 51
98990
XDOT = -4667
600042 Wp = 58
67950
YDOT = -890
426939 meter/sec RA = 107
50325 deg
ZDOT = 6038
226917 TA = 297
01663
MA = 297
34584
Ha = 219
152 n
mi
Hp = 197
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5675251
19 X = -1800699
82
Y = 21404583
67 feet Y = 6504376
91 meter
Z = -1311659
40 Z = -408369
31
XDOT = -15313
648433 XDOT = -4686
629069
YDOT = -2921
348224 feet/sec YDOT = -942
729459 meter/sec
ZDOT = 19810
455766 ZDOT = 6015
505276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22062138
14 X = -6724539
70
Y = 1879516
61 feet Y = 572876
66 meter
Z = -1347073
34 Z = -410587
96
XDOT = -2315
763394 XDOT = -705
844683
YDOT = -13905
422553 feet/sec YDOT = -4238
372794 meter/sec
ZDOT = 19717
731679 ZDOT = 6009
964616
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 11321
65119457
00016717 00000-0 10270-3 0 9014
2 25544 51
6408 108
3804 0021691 67
0090 293
3351 15
60305837 24876
Satellite: ISS
Catalog Number: 25544
Epoch time: 11321
65119457 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 108
3804 deg
Eccentricity:
0021691
Arg of perigee: 67
0090 deg
Mean anomaly: 293
3351 deg
Mean motion: 15
60305837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 294
Coasting Arc #3 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2011/322/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4338131
07 A = 6768436
27 meter
Y = 2415230
94 meter E =
0036698
Z = 4564496
38 I = 51
96573
XDOT = -638
207103 Wp = 74
16876
YDOT = -7021
715700 meter/sec RA = 104
91092 deg
ZDOT = 3098
147445 TA = 345
06348
MA = 345
17158
Ha = 225
661 n
mi
Hp = 197
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14232713
48 X = -4386989
93
Y = 7923986
01 feet Y = 2366446
03 meter
Z = 14975381
82 Z = 4543302
91
XDOT = -2093
855326 XDOT = -574
691831
YDOT = -23037
125001 feet/sec YDOT = -7028
497444 meter/sec
ZDOT = 10164
525739 ZDOT = 3095
201166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13832938
26 X = 4216279
58
Y = 8752051
90 feet Y = 2667625
42 meter
Z = 14888692
18 Z = 4538073
38
XDOT = -18528
015026 XDOT = -5647
338980
YDOT = 11952
183163 feet/sec YDOT = 3643
025428 meter/sec
ZDOT = 10152
926765 ZDOT = 3094
612078
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 11322
22769602
00016717 00000-0 10270-3 0 9022
2 25544 51
6415 105
4845 0030501 63
8660 296
5628 15
58279311 24960
Satellite: ISS
Catalog Number: 25544
Epoch time: 11322
22769602 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 105
4845 deg
Eccentricity:
0030501
Arg of perigee: 63
8660 deg
Mean anomaly: 296
5628 deg
Mean motion: 15
58279311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 306
Coasting Arc #4 (Orbit 2510)
---------------------------------------
Vector Time (GMT): 2011/323/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4063710
19 A = 6765226
55 meter
Y = 1037043
02 meter E =
0044357
Z = -5344829
97 I = 51
96265
XDOT = -1538
643672 Wp = 75
33331
YDOT = 7481
197304 meter/sec RA = 99
89233 deg
ZDOT = 294
654707 TA = 197
39587
MA = 197
54832
Ha = 225
467 n
mi
Hp = 197
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13332382
51 X = 4077776
24
Y = 3402372
12 feet Y = 1082564
58 meter
Z = -17535531
41 Z = -5325054
09
XDOT = -5048
043542 XDOT = -1623
616938
YDOT = 24544
610578 feet/sec YDOT = 7463
516134 meter/sec
ZDOT = 966
714919 ZDOT = 286
973513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3705462
29 X = -1129424
91
Y = -13357452
15 feet Y = -4071351
42 meter
Z = -17454840
09 Z = -5320235
26
XDOT = 22848
983884 XDOT = 6964
370288
YDOT = -7504
411414 feet/sec YDOT = -2287
344599 meter/sec
ZDOT = 934
879755 ZDOT = 284
951349
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 11323
18964604
00016717 00000-0 10270-3 0 9038
2 25544 51
6421 100
6585 0030446 67
1398 293
2967 15
58319735 25111
Satellite: ISS
Catalog Number: 25544
Epoch time: 11323
18964604 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 100
6585 deg
Eccentricity:
0030446
Arg of perigee: 67
1398 deg
Mean anomaly: 293
2967 deg
Mean motion: 15
58319735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2511
Checksum: 313
Coasting Arc #5 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2011/324/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2968114
93 A = 6769342
43 meter
Y = -4326194
70 meter E =
0040474
Z = 4253003
15 I = 51
98079
XDOT = 3347
500060 Wp = 71
32359
YDOT = -5900
024076 meter/sec RA = 94
87614 deg
ZDOT = -3624
683770 TA = 55
60960
MA = 55
22753
Ha = 225
492 n
mi
Hp = 197
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9737909
86 X = -2940178
58
Y = -14193552
15 feet Y = -4359229
76 meter
Z = 13953422
42 Z = 4238651
72
XDOT = 10982
611747 XDOT = 3430
834815
YDOT = -19357
034369 feet/sec YDOT = -5862
124344 meter/sec
ZDOT = -11892
007119 ZDOT = -3608
218927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7190688
52 X = -2191721
86
Y = 15690832
05 feet Y = 4782565
61 meter
Z = 13895092
53 Z = 4235224
20
XDOT = -21144
255928 XDOT = -6444
769207
YDOT = 900
045295 feet/sec YDOT = 274
333806 meter/sec
ZDOT = -11824
392138 ZDOT = -3604
074724
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 11324
21570256
00016717 00000-0 10270-3 0 9040
2 25544 51
6417 95
5100 0030473 70
6722 289
7724 15
58373499 25276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11324
21570256 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 95
5100 deg
Eccentricity:
0030473
Arg of perigee: 70
6722 deg
Mean anomaly: 289
7724 deg
Mean motion: 15
58373499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2527
Checksum: 310
Coasting Arc #6 (Orbit 2541)
---------------------------------------
Vector Time (GMT): 2011/325/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1441298
28 A = 6775530
31 meter
Y = 6361437
77 meter E =
0036596
Z = -1829518
21 I = 52
00386
XDOT = -4437
483638 Wp = 67
53368
YDOT = 2611
041397 meter/sec RA = 89
89086 deg
ZDOT = 5686
865075 TA = 272
42498
MA = 272
84392
Ha = 225
396 n
mi
Hp = 197
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4728668
89 X = 1378943
94
Y = 20870858
81 feet Y = 6377206
60 meter
Z = -6002356
34 Z = -1822667
73
XDOT = -14558
673353 XDOT = -4493
977296
YDOT = 8566
408783 feet/sec YDOT = 2561
102868 meter/sec
ZDOT = 18657
693815 ZDOT = 5665
170144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15258341
37 X = 4650742
45
Y = -15015529
77 feet Y = -4576733
47 meter
Z = -5974798
99 Z = -1821118
73
XDOT = 13900
775059 XDOT = 4236
956238
YDOT = 6873
026971 feet/sec YDOT = 2094
898621 meter/sec
ZDOT = 18568
925020 ZDOT = 5659
808346
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 11325
17760901
00016717 00000-0 10270-3 0 9055
2 25544 51
6422 90
6841 0030401 74
2124 286
2380 15
58394476 25422
Satellite: ISS
Catalog Number: 25544
Epoch time: 11325
17760901 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 90
6841 deg
Eccentricity:
0030401
Arg of perigee: 74
2124 deg
Mean anomaly: 286
2380 deg
Mean motion: 15
58394476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2542
Checksum: 291
Coasting Arc #7 (Orbit 2557)
---------------------------------------
Vector Time (GMT): 2011/326/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 477780
86 A = 6776172
76 meter
Y = -6626805
75 meter E =
0034953
Z = -1359686
15 I = 52
00496
XDOT = 4718
704906 Wp = 91
02676
YDOT = 1512
981961 meter/sec RA = 84
92499 deg
ZDOT = -5845
727526 TA = 103
71200
MA = 103
32264
Ha = 225
365 n
mi
Hp = 197
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1567522
50 X = 558452
86
Y = -21741488
68 feet Y = -6621011
83 meter
Z = -4460912
56 Z = -1357169
18
XDOT = 15481
315310 XDOT = 4729
833869
YDOT = 4963
851577 feet/sec YDOT = 1565
811726 meter/sec
ZDOT = -19178
896082 ZDOT = -5822
776479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19163531
36 X = -5841044
36
Y = 10392503
60 feet Y = 3167635
10 meter
Z = -4450183
38 Z = -1356415
89
XDOT = -3482
489713 XDOT = -1061
462865
YDOT = -14411
213583 feet/sec YDOT = -4392
537900 meter/sec
ZDOT = -19085
270544 ZDOT = -5817
190462
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 11326
20361924
00016717 00000-0 10270-3 0 9063
2 25544 51
6423 85
5350 0030266 78
1434 282
3113 15
58389155 25583
Satellite: ISS
Catalog Number: 25544
Epoch time: 11326
20361924 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 85
5350 deg
Eccentricity:
0030266
Arg of perigee: 78
1434 deg
Mean anomaly: 282
3113 deg
Mean motion: 15
58389155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2558
Checksum: 300
Coasting Arc #8 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2011/327/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2262046
56 A = 6770159
95 meter
Y = 4974111
33 meter E =
0040979
Z = 3959883
55 I = 51
98161
XDOT = -4109
623007 Wp = 86
23855
YDOT = -5107
544734 meter/sec RA = 79
94376 deg
ZDOT = 4035
075553 TA = 321
90725
MA = 322
19625
Ha = 225
422 n
mi
Hp = 196
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7421412
60 X = -2336736
81
Y = 16319262
88 feet Y = 4948397
95 meter
Z = 12991743
94 Z = 3948713
04
XDOT = -13483
015114 XDOT = -4071
806148
YDOT = -16757
036530 feet/sec YDOT = -5153
289783 meter/sec
ZDOT = 13238
436853 ZDOT = 4015
202149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17741067
87 X = 5407477
49
Y = -2800458
17 feet Y = -853579
65 meter
Z = 12945773
88 Z = 3945871
88
XDOT = -6637
007453 XDOT = -2022
959872
YDOT = 19281
576792 feet/sec YDOT = 5877
024606 meter/sec
ZDOT = 13157
634782 ZDOT = 4010
447082
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 11327
22960514
00016717 00000-0 10270-3 0 9077
2 25544 51
6424 80
3869 0030418 81
4623 278
9977 15
58437375 25743
Satellite: ISS
Catalog Number: 25544
Epoch time: 11327
22960514 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 80
3869 deg
Eccentricity:
0030418
Arg of perigee: 81
4623 deg
Mean anomaly: 278
9977 deg
Mean motion: 15
58437375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 334
Coasting Arc #9 (Orbit 2588)
---------------------------------------
Vector Time (GMT): 2011/328/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3783674
91 A = 6764866
02 meter
Y = -1920635
44 meter E =
0044818
Z = -5307474
06 I = 51
95798
XDOT = 2553
893555 Wp = 84
48816
YDOT = 7160
876593 meter/sec RA = 74
92923 deg
ZDOT = -772
096074 TA = 178
14936
MA = 178
13272
Ha = 225
180 n
mi
Hp = 196
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12413631
60 X = 3830654
00
Y = -6301297
38 feet Y = -1878061
01 meter
Z = -17412972
63 Z = -5288978
54
XDOT = 8378
915864 XDOT = 2477
380197
YDOT = 23493
689609 feet/sec YDOT = 7189
008043 meter/sec
ZDOT = -2533
123601 ZDOT = -759
874288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12300553
04 X = -3749208
57
Y = -6717947
68 feet Y = -2047630
45 meter
Z = -17337294
72 Z = -5284407
43
XDOT = 14068
985891 XDOT = 4288
226899
YDOT = -19362
518289 feet/sec YDOT = -5901
695575 meter/sec
ZDOT = -2483
731472 ZDOT = -757
041353
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 11328
19144340
00016717 00000-0 10270-3 0 9086
2 25544 51
6423 75
5595 0030213 84
8938 275
5665 15
58501629 25890
Satellite: ISS
Catalog Number: 25544
Epoch time: 11328
19144340 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 75
5595 deg
Eccentricity:
0030213
Arg of perigee: 84
8938 deg
Mean anomaly: 275
5665 deg
Mean motion: 15
58501629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2589
Checksum: 330
Coasting Arc #10 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2011/329/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4531656
87 A = 6766963
89 meter
Y = -1621812
01 meter E =
0037311
Z = 4726826
92 I = 51
95744
XDOT = -329
740331 Wp = 83
00656
YDOT = -7180
540808 meter/sec RA = 69
90665 deg
ZDOT = -2756
879164 TA = 34
15860
MA = 33
91909
Ha = 225
187 n
mi
Hp = 196
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14867640
65 X = -4536147
19
Y = -5320905
56 feet Y = -1672513
36 meter
Z = 15507962
32 Z = 4704800
59
XDOT = -1081
825234 XDOT = -236
028895
YDOT = -23558
204752 feet/sec YDOT = -7183
703923 meter/sec
ZDOT = -9044
879147 ZDOT = -2758
254161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4389423
96 X = 1337896
42
Y = 15260083
46 feet Y = 4651273
44 meter
Z = 15418121
79 Z = 4699443
52
XDOT = -17439
198664 XDOT = -5315
467753
YDOT = 14236
412446 feet/sec YDOT = 4339
258514 meter/sec
ZDOT = -9049
953105 ZDOT = -2758
425707
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 11329
21738131
00016717 00000-0 10270-3 0 9098
2 25544 51
6429 70
4112 0030104 88
5102 271
9502 15
58568909 26051
Satellite: ISS
Catalog Number: 25544
Epoch time: 11329
21738131 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 70
4112 deg
Eccentricity:
0030104
Arg of perigee: 88
5102 deg
Mean anomaly: 271
9502 deg
Mean motion: 15
58568909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 293
Coasting Arc #11 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2011/330/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4349961
90 A = 6773679
55 meter
Y = 4515998
75 meter E =
0034191
Z = -2588214
70 I = 51
96759
XDOT = -2180
898393 Wp = 86
17200
YDOT = 5095
378250 meter/sec RA = 64
90954 deg
ZDOT = 5287
409995 TA = 244
85446
MA = 245
20951
Ha = 225
087 n
mi
Hp = 196
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14271528
55 X = 4311713
08
Y = 14816268
87 feet Y = 4564429
13 meter
Z = -8491518
04 Z = -2567174
64
XDOT = -7155
178455 XDOT = -2263
399504
YDOT = 16717
120244 feet/sec YDOT = 5070
528210 meter/sec
ZDOT = 17347
145653 ZDOT = 5276
615215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3352051
64 X = 1021705
34
Y = -20332445
88 feet Y = -6197329
50 meter
Z = -8405927
88 Z = -2562126
82
XDOT = 16266
847962 XDOT = 4958
135259
YDOT = -4386
289542 feet/sec YDOT = -1336
941052 meter/sec
ZDOT = 17302
657938 ZDOT = 5273
850140
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 11330
17917862
00016717 00000-0 10270-3 0 9107
2 25544 51
6421 65
5846 0030105 92
0653 268
3950 15
58556294 26202
Satellite: ISS
Catalog Number: 25544
Epoch time: 11330
17917862 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 65
5846 deg
Eccentricity:
0030105
Arg of perigee: 92
0653 deg
Mean anomaly: 268
3950 deg
Mean motion: 15
58556294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 303
Coasting Arc #12 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2011/331/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2966559
03 A = 6776274
23 meter
Y = -6057751
34 meter E =
0038701
Z = -596850
63 I = 51
96249
XDOT = 4484
779278 Wp = 106
72254
YDOT = -1636
805479 meter/sec RA = 59
93886 deg
ZDOT = -6009
471747 TA = 79
70294
MA = 79
26683
Ha = 225
035 n
mi
Hp = 196
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9732805
22 X = -2895700
15
Y = -19874512
28 feet Y = -6090528
96 meter
Z = -1958171
34 Z = -611090
90
XDOT = 14713
842776 XDOT = 4531
942237
YDOT = -5370
096716 feet/sec YDOT = -1586
389519 meter/sec
ZDOT = -19716
114655 ZDOT = -5987
570115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9817564
78 X = -2992393
75
Y = 19826999
13 feet Y = 6043269
34 meter
Z = -2015861
60 Z = -614434
61
XDOT = -11858
916045 XDOT = -3614
597611
YDOT = -7760
196299 feet/sec YDOT = -2365
307832 meter/sec
ZDOT = -19626
519492 ZDOT = -5982
163141
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 11331
20507193
00016717 00000-0 10270-3 0 9115
2 25544 51
6419 60
4353 0030140 96
0168 264
4423 15
58573427 26366
Satellite: ISS
Catalog Number: 25544
Epoch time: 11331
20507193 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 60
4353 deg
Eccentricity:
0030140
Arg of perigee: 96
0168 deg
Mean anomaly: 264
4423 deg
Mean motion: 15
58573427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 285
Coasting Arc #13 (Orbit 2651)
---------------------------------------
Vector Time (GMT): 2011/332/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 751035
10 A = 6771191
81 meter
Y = 5764690
61 meter E =
0042272
Z = 3440583
90 I = 51
92909
XDOT = -5820
364768 Wp = 96
65539
YDOT = -2020
488655 meter/sec RA = 54
95926 deg
ZDOT = 4602
830546 TA = 303
65762
MA = 304
06010
Ha = 224
894 n
mi
Hp = 196
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2464025
93 X = 669803
56
Y = 18913026
93 feet Y = 5772634
58 meter
Z = 11288004
91 Z = 3444035
75
XDOT = -19095
684936 XDOT = -5819
698496
YDOT = -6628
899786 feet/sec YDOT = -2085
572314 meter/sec
ZDOT = 15101
150085 ZDOT = 4574
556483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13291700
78 X = 4051310
40
Y = -13667355
97 feet Y = -4165810
10 meter
Z = 11301643
13 Z = 3444740
83
XDOT = 5786
605558 XDOT = 1763
757374
YDOT = 18163
064773 feet/sec YDOT = 5536
102143 meter/sec
ZDOT = 14985
809881 ZDOT = 4567
674852
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 11332
23094035
00016717 00000-0 10270-3 0 9126
2 25544 51
6410 55
2862 0030017 99
6190 260
8359 15
58636416 26525
Satellite: ISS
Catalog Number: 25544
Epoch time: 11332
23094035 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 55
2862 deg
Eccentricity:
0030017
Arg of perigee: 99
6190 deg
Mean anomaly: 260
8359 deg
Mean motion: 15
58636416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2652
Checksum: 295
Coasting Arc #14 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2011/333/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2030253
14 A = 6764924
86 meter
Y = -3897875
43 meter E =
0043077
Z = -5178886
21 I = 51
88878
XDOT = 5662
455172 Wp = 95
29838
YDOT = 4914
419977 meter/sec RA = 49
94426 deg
ZDOT = -1493
543681 TA = 160
40801
MA = 160
24198
Ha = 224
881 n
mi
Hp = 196
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6660935
49 X = 2098847
19
Y = -12788305
23 feet Y = -3874787
90 meter
Z = -16991096
50 Z = -5168856
97
XDOT = 18577
608831 XDOT = 5614
335681
YDOT = 16123
425121 feet/sec YDOT = 4977
472108 meter/sec
ZDOT = -4900
077695 ZDOT = -1466
151864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14167321
13 X = -4318199
48
Y = 2932095
06 feet Y = 893702
58 meter
Z = -16949808
35 Z = -5166301
59
XDOT = 791
532588 XDOT = 241
259133
YDOT = -23580
698494 feet/sec YDOT = -7187
396901 meter/sec
ZDOT = -4788
573973 ZDOT = -1459
557347
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 11333
19267174
00016717 00000-0 10270-3 0 9139
2 25544 51
6398 50
4573 0030116 103
2111 257
2407 15
58655305 26679
Satellite: ISS
Catalog Number: 25544
Epoch time: 11333
19267174 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 50
4573 deg
Eccentricity:
0030116
Arg of perigee: 103
2111 deg
Mean anomaly: 257
2407 deg
Mean motion: 15
58655305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 292
Coasting Arc #15 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2011/334/04:10:36
666
Vector Time (MET): N/A
Weight (LBS) : 885821
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4429009
00 A = 6765590
16 meter
Y = 1088770
86 meter E =
0034421
Z = 4966277
91 I = 51
87129
XDOT = -3931
371133 Wp = 98
55325
YDOT = -6272
927389 meter/sec RA = 44
91325 deg
ZDOT = -2123
369397 TA = 12
00508
MA = 11
92325
Ha = 224
931 n
mi
Hp = 196
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14530869
42 X = -4464979
97
Y = 3572082
86 feet Y = 1039041
48 meter
Z = 16293562
69 Z = 4944674
47
XDOT = -12898
199254 XDOT = -3850
618876
YDOT = -20580
470436 feet/sec YDOT = -6316
438730 meter/sec
ZDOT = -6966
435028 ZDOT = -2142
272308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12225515
00 X = 3726336
97
Y = 8792829
62 feet Y = 2680054
47 meter
Z = 16205216
99 Z = 4939350
14
XDOT = -6639
029874 XDOT = -2023
576305
YDOT = 22256
786616 feet/sec YDOT = 6783
868560 meter/sec
ZDOT = -7043
146401 ZDOT = -2146
751023
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 11334
21849542
00016717 00000-0 10270-3 0 9149
2 25544 51
6400 45
3079 0030049 106
9955 253
4497 15
58693394 26833
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
21849542 = yrday
fracday
Element set: 914
Inclination: 51
6400 deg
RA of node: 45
3079 deg
Eccentricity:
0030049
Arg of perigee: 106
9955 deg
Mean anomaly: 253
4497 deg
Mean motion: 15
58693394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 326
Coasting Arc #16 (Orbit 2694)
---------------------------------------
Vector Time (GMT): 2011/334/22:28:03
675
Vector Time (MET): N/A
Weight (LBS) : 885510
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -794969
20 A = 6767118
35 meter
Y = 4490591
06 meter E =
0038041
Z = 4972538
98 I = 51
85656
XDOT = -6522
294635 Wp = 108
70616
YDOT = -3507
480045 meter/sec RA = 41
13597 deg
ZDOT = 2099
791836 TA = 320
86175
MA = 321
13630
Ha = 226
496 n
mi
Hp = 196
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2608166
67 X = -869280
51
Y = 14732910
29 feet Y = 4481285
44 meter
Z = 16314104
25 Z = 4968496
77
XDOT = -21398
604444 XDOT = -6492
788961
YDOT = -11507
480464 feet/sec YDOT = -3580
251490 meter/sec
ZDOT = 6889
080827 ZDOT = 2068
177967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8646796
67 X = 2635543
63
Y = 12232933
27 feet Y = 3728598
06 meter
Z = 16297221
47 Z = 4967393
10
XDOT = -22322
006941 XDOT = -6803
747716
YDOT = 6662
566762 feet/sec YDOT = 2030
750349 meter/sec
ZDOT = 6760
216965 ZDOT = 2060
514131
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 11334
98787482
00016717 00000-0 10270-3 0 9158
2 25544 51
6422 41
4484 0032204 106
5595 253
9101 15
58131864 26954
Satellite: ISS
Catalog Number: 25544
Epoch time: 11334
98787482 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 41
4484 deg
Eccentricity:
0032204
Arg of perigee: 106
5595 deg
Mean anomaly: 253
9101 deg
Mean motion: 15
58131864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2695
Checksum: 316
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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