[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 5th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 111 9 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
322/03:29:51
341 -0
8 5
9 5
9
N/A 5
8 0
0 219
2
000/00:01:52
682 -0
9 -0
0 200
7
Coasting Arc #1 (Orbit 2281)
---------------------------------------
Vector Time (GMT): 2011/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2016667
34 A = 6762190
40 meter
Y = 3888508
08 meter E =
0031302
Z = -5174553
92 I = 51
65819
XDOT = -7283
185167 Wp = 42
29042
YDOT = 1927
010823 meter/sec RA = 173
46531 deg
ZDOT = -1372
585672 TA = 214
39759
MA = 214
60062
Ha = 219
513 n
mi
Hp = 200
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6616362
67 X = 1998172
71
Y = 12757572
44 feet Y = 3910956
09 meter
Z = -16976882
94 Z = -5164801
92
XDOT = -23894
964460 XDOT = -7297
524230
YDOT = 6322
213986 feet/sec YDOT = 1845
485554 meter/sec
ZDOT = -4503
233833 ZDOT = -1408
002663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13579768
34 X = -4139113
39
Y = -4844049
11 feet Y = -1476466
17 meter
Z = -16937282
66 Z = -5162483
76
XDOT = 12938
772123 XDOT = 3943
737743
YDOT = -19816
951135 feet/sec YDOT = -6040
206706 meter/sec
ZDOT = -4647
762622 ZDOT = -1416
638047
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 11308
51846785
00016717 00000-0 10270-3 0 9004
2 25544 51
6405 174
4254 0021948 19
4342 340
7645 15
59589169 22828
Satellite: ISS
Catalog Number: 25544
Epoch time: 11308
51846785 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 174
4254 deg
Eccentricity:
0021948
Arg of perigee: 19
4342 deg
Mean anomaly: 340
7645 deg
Mean motion: 15
59589169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2282
Checksum: 326
Coasting Arc #2 (Orbit 2297)
---------------------------------------
Vector Time (GMT): 2011/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2089640
31 A = 6763426
25 meter
Y = -4290512
86 meter E =
0027993
Z = 4789304
67 I = 51
69359
XDOT = 7209
068737 Wp = 32
36786
YDOT = 600
134453 meter/sec RA = 168
41053 deg
ZDOT = -2577
665758 TA = 83
11582
MA = 82
79744
Ha = 219
409 n
mi
Hp = 200
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6855775
28 X = 2114196
46
Y = -14076485
77 feet Y = -4267007
71 meter
Z = 15712941
84 Z = 4799516
13
XDOT = 23651
800318 XDOT = 7214
344124
YDOT = 1968
945057 feet/sec YDOT = 680
780063 meter/sec
ZDOT = -8456
908656 ZDOT = -2542
630832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4805367
21 X = 1464675
92
Y = 14857352
75 feet Y = 4528521
12 meter
Z = 15754782
23 Z = 4802057
62
XDOT = -17444
299443 XDOT = -5317
022470
YDOT = 14562
811182 feet/sec YDOT = 4438
744848 meter/sec
ZDOT = -8314
038828 ZDOT = -2534
119035
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 11309
54368818
00016717 00000-0 10270-3 0 9015
2 25544 51
6408 169
2715 0021882 22
9120 337
3007 15
59666369 22984
Satellite: ISS
Catalog Number: 25544
Epoch time: 11309
54368818 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 169
2715 deg
Eccentricity:
0021882
Arg of perigee: 22
9120 deg
Mean anomaly: 337
3007 deg
Mean motion: 15
59666369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2298
Checksum: 323
Coasting Arc #3 (Orbit 2312)
---------------------------------------
Vector Time (GMT): 2011/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5256784
29 A = 6770781
69 meter
Y = 3524555
64 meter E =
0027116
Z = -2377638
20 I = 51
74660
XDOT = -4499
953674 Wp = 30
87185
YDOT = -3101
536395 meter/sec RA = 163
38814 deg
ZDOT = 5401
305814 TA = 302
52328
MA = 302
78499
Ha = 219
466 n
mi
Hp = 199
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17246667
61 X = -5284255
52
Y = 11563502
76 feet Y = 3465617
35 meter
Z = -7800650
25 Z = -2403242
98
XDOT = -14763
627540 XDOT = -4491
176261
YDOT = -10175
644339 feet/sec YDOT = -3151
808322 meter/sec
ZDOT = 17720
819600 ZDOT = 5379
466114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4139912
25 X = 1261845
25
Y = -20307151
85 feet Y = -6189619
88 meter
Z = -7905251
07 Z = -2409520
53
XDOT = 16253
471728 XDOT = 4954
058183
YDOT = -3487
432861 feet/sec YDOT = -1062
969536 meter/sec
ZDOT = 17631
875876 ZDOT = 5374
195767
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 11310
50480113
00016717 00000-0 10270-3 0 9027
2 25544 51
6396 164
4399 0021859 26
3099 333
9162 15
59669357 23134
Satellite: ISS
Catalog Number: 25544
Epoch time: 11310
50480113 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 164
4399 deg
Eccentricity:
0021859
Arg of perigee: 26
3099 deg
Mean anomaly: 333
9162 deg
Mean motion: 15
59669357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2313
Checksum: 315
Coasting Arc #4 (Orbit 2328)
---------------------------------------
Vector Time (GMT): 2011/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6491091
69 A = 6772577
72 meter
Y = -1591102
76 meter E =
0020251
Z = -1155878
62 I = 51
78104
XDOT = 168
427081 Wp = 56
27207
YDOT = 4910
768690 meter/sec RA = 158
39960 deg
ZDOT = -5877
018146 TA = 136
25596
MA = 136
09533
Ha = 219
515 n
mi
Hp = 199
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21296232
57 X = 6514016
44
Y = -5220153
41 feet Y = -1518387
26 meter
Z = -3792252
69 Z = -1124288
49
XDOT = 552
582287 XDOT = 142
051473
YDOT = 16111
445832 feet/sec YDOT = 4912
504455 meter/sec
ZDOT = -19281
555597 ZDOT = -5876
264158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11202659
24 X = -3414570
54
Y = 18874354
53 feet Y = 5752903
26 meter
Z = -3663314
19 Z = -1116578
16
XDOT = -10592
764737 XDOT = -3228
674692
YDOT = -9987
459979 feet/sec YDOT = -3044
177802 meter/sec
ZDOT = -19278
706695 ZDOT = -5876
149801
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 11311
52995238
00016717 00000-0 10270-3 0 9030
2 25544 51
6389 159
2858 0021744 30
2883 329
9525 15
59719302 23297
Satellite: ISS
Catalog Number: 25544
Epoch time: 11311
52995238 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 159
2858 deg
Eccentricity:
0021744
Arg of perigee: 30
2883 deg
Mean anomaly: 329
9525 deg
Mean motion: 15
59719302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2329
Checksum: 331
Coasting Arc #5 (Orbit 2344)
---------------------------------------
Vector Time (GMT): 2011/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5235076
78 A = 6765752
54 meter
Y = -1017644
30 meter E =
0027255
Z = 4133424
08 I = 51
78540
XDOT = 4031
400185 Wp = 55
22098
YDOT = -5352
804035 meter/sec RA = 153
39450 deg
ZDOT = 3785
631222 TA = 356
01089
MA = 356
03257
Ha = 219
662 n
mi
Hp = 199
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17175448
74 X = -5243388
10
Y = -3338728
03 feet Y = -1076232
51 meter
Z = 13561102
62 Z = 4107971
30
XDOT = 13226
378559 XDOT = 4072
566316
YDOT = -17561
693029 feet/sec YDOT = -5307
492183 meter/sec
ZDOT = 12420
049942 ZDOT = 3805
316356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14293932
86 X = 4356790
73
Y = -10228921
19 feet Y = -3117775
18 meter
Z = 13457314
13 Z = 4101789
35
XDOT = 2953
180380 XDOT = 900
129380
YDOT = 20583
101052 feet/sec YDOT = 6273
729201 meter/sec
ZDOT = 12500
611659 ZDOT = 3810
186434
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 11312
55506739
00016717 00000-0 10270-3 0 9049
2 25544 51
6379 154
1303 0021827 33
8088 326
4455 15
59769847 23454
Satellite: ISS
Catalog Number: 25544
Epoch time: 11312
55506739 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 154
1303 deg
Eccentricity:
0021827
Arg of perigee: 33
8088 deg
Mean anomaly: 326
4455 deg
Mean motion: 15
59769847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2345
Checksum: 327
Coasting Arc #6 (Orbit 2359)
---------------------------------------
Vector Time (GMT): 2011/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2190200
87 A = 6760779
48 meter
Y = 3575757
67 meter E =
0033032
Z = -5327591
64 I = 51
79473
XDOT = -6526
637569 Wp = 58
80008
YDOT = 4003
602167 meter/sec RA = 148
35174 deg
ZDOT = 20
759602 TA = 211
29901
MA = 211
49607
Ha = 219
483 n
mi
Hp = 199
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7185698
38 X = 2175934
40
Y = 11731488
43 feet Y = 3600170
04 meter
Z = -17478975
18 Z = -5316986
05
XDOT = -21412
852917 XDOT = -6571
022407
YDOT = 13135
177713 feet/sec YDOT = 3930
369135 meter/sec
ZDOT = 68
108929 ZDOT = -11
055463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13575431
77 X = -4137791
60
Y = -2544477
72 feet Y = -775556
81 meter
Z = -17435880
85 Z = -5314456
48
XDOT = 4587
423537 XDOT = 1398
246694
YDOT = -23673
046903 feet/sec YDOT = -7215
544696 meter/sec
ZDOT = -61
890958 ZDOT = -18
864364
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 11313
51607866
00016717 00000-0 10270-3 0 9050
2 25544 51
6365 149
2971 0021730 37
5375 322
7293 15
59843352 23608
Satellite: ISS
Catalog Number: 25544
Epoch time: 11313
51607866 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 149
2971 deg
Eccentricity:
0021730
Arg of perigee: 37
5375 deg
Mean anomaly: 322
7293 deg
Mean motion: 15
59843352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2360
Checksum: 312
Coasting Arc #7 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2011/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1560090
61 A = 6765432
51 meter
Y = -5160539
01 meter E =
0030806
Z = 4079506
56 I = 51
83670
XDOT = 6550
315790 Wp = 52
75291
YDOT = -1099
698045 meter/sec RA = 143
31031 deg
ZDOT = -3857
887817 TA = 77
12133
MA = 76
77738
Ha = 219
372 n
mi
Hp = 198
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5118407
51 X = 1597862
80
Y = -16930902
26 feet Y = -5142881
97 meter
Z = 13384207
86 Z = 4087177
37
XDOT = 21490
537370 XDOT = 6580
867403
YDOT = -3607
933218 feet/sec YDOT = -1026
277529 meter/sec
ZDOT = -12657
112259 ZDOT = -3825
991350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9343786
62 X = 2847986
16
Y = 14990041
43 feet Y = 4568964
63 meter
Z = 13415769
69 Z = 4089126
60
XDOT = -10492
500248 XDOT = -3198
114076
YDOT = 17863
545096 feet/sec YDOT = 5444
808545 meter/sec
ZDOT = -12526
909024 ZDOT = -3818
201871
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 11314
54112197
00016717 00000-0 10270-3 0 9063
2 25544 51
6368 144
1416 0021624 40
8898 319
3875 15
59910427 23761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11314
54112197 = yrday
fracday
Element set: 906
Inclination: 51
6368 deg
RA of node: 144
1416 deg
Eccentricity:
0021624
Arg of perigee: 40
8898 deg
Mean anomaly: 319
3875 deg
Mean motion: 15
59910427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2376
Checksum: 318
Coasting Arc #8 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2011/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4406004
55 A = 6772005
05 meter
Y = 5019336
26 meter E =
0031183
Z = -1042339
00 I = 51
88164
XDOT = -4206
591810 Wp = 43
08718
YDOT = -2486
779645 meter/sec RA = 138
31052 deg
ZDOT = 5932
576338 TA = 305
60973
MA = 305
89984
Ha = 219
397 n
mi
Hp = 198
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14455395
49 X = -4456740
66
Y = 16467638
63 feet Y = 4969781
96 meter
Z = -3419747
39 Z = -1063867
00
XDOT = -13801
154231 XDOT = -4207
291609
YDOT = -8158
725869 feet/sec YDOT = -2533
824432 meter/sec
ZDOT = 19463
833130 ZDOT = 5912
138422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3144609
78 X = -958477
06
Y = -21671238
78 feet Y = -6605393
58 meter
Z = -3507861
48 Z = -1069196
18
XDOT = 13662
884649 XDOT = 4164
447241
YDOT = -5054
329025 feet/sec YDOT = -1540
559487 meter/sec
ZDOT = 19380
562816 ZDOT = 5907
195546
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 11315
50206888
00016717 00000-0 10270-3 0 9072
2 25544 51
6358 139
3081 0021643 44
7452 315
5445 15
59938849 23910
Satellite: ISS
Catalog Number: 25544
Epoch time: 11315
50206888 = yrday
fracday
Element set: 907
Inclination: 51
6358 deg
RA of node: 139
3081 deg
Eccentricity:
0021643
Arg of perigee: 44
7452 deg
Mean anomaly: 315
5445 deg
Mean motion: 15
59938849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 326
Coasting Arc #9 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2011/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5545208
85 A = 6769493
80 meter
Y = -2940208
67 meter E =
0023172
Z = -2571069
54 I = 51
89598
XDOT = 489
038144 Wp = 61
60847
YDOT = 5521
357527 meter/sec RA = 133
32830 deg
ZDOT = -5284
755169 TA = 147
18959
MA = 147
04550
Ha = 219
415 n
mi
Hp = 198
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18192942
44 X = 5590164
79
Y = -9646353
91 feet Y = -2877947
26 meter
Z = -8435267
51 Z = -2544021
24
XDOT = 1604
455854 XDOT = 452
933858
YDOT = 18114
690050 feet/sec YDOT = 5526
624636 meter/sec
ZDOT = -17338
435593 ZDOT = -5282
466800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4168397
56 X = -1270527
58
Y = 20211693
42 feet Y = 6160524
15 meter
Z = -8324719
02 Z = -2537374
36
XDOT = -13586
389248 XDOT = -4141
131443
YDOT = -9904
782587 feet/sec YDOT = -3018
977733 meter/sec
ZDOT = -17329
397071 ZDOT = -5282
000227
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 11316
52704222
00016717 00000-0 10270-3 0 9081
2 25544 51
6358 134
1522 0021793 48
5036 311
7986 15
60023732 24073
Satellite: ISS
Catalog Number: 25544
Epoch time: 11316
52704222 = yrday
fracday
Element set: 908
Inclination: 51
6358 deg
RA of node: 134
1522 deg
Eccentricity:
0021793
Arg of perigee: 48
5036 deg
Mean anomaly: 311
7986 deg
Mean motion: 15
60023732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 288
Coasting Arc #10 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2011/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4572094
95 A = 6761816
41 meter
Y = -460553
48 meter E =
0024642
Z = 4937717
11 I = 51
89021
XDOT = 3072
254169 Wp = 66
70448
YDOT = -6698
447824 meter/sec RA = 128
31127 deg
ZDOT = 2220
788307 TA = 1
78722
MA = 1
77843
Ha = 219
539 n
mi
Hp = 198
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15000311
53 X = -4590592
15
Y = -1511002
22 feet Y = -511785
16 meter
Z = 16199859
29 Z = 4915460
48
XDOT = 10079
574044 XDOT = 3136
140796
YDOT = -21976
534857 feet/sec YDOT = -6663
734917 meter/sec
ZDOT = 7286
050875 ZDOT = 2235
868399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10587414
12 X = 3227043
82
Y = -10868916
21 feet Y = -3312845
66 meter
Z = 16109042
10 Z = 4910036
03
XDOT = 10145
267155 XDOT = 3092
277429
YDOT = 20769
153393 feet/sec YDOT = 6330
437954 meter/sec
ZDOT = 7347
977832 ZDOT = 2239
663643
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 11317
55197970
00016717 00000-0 10270-3 0 9092
2 25544 51
6355 128
9956 0021675 52
2871 308
0245 15
60043776 24235
Satellite: ISS
Catalog Number: 25544
Epoch time: 11317
55197970 = yrday
fracday
Element set: 909
Inclination: 51
6355 deg
RA of node: 128
9956 deg
Eccentricity:
0021675
Arg of perigee: 52
2871 deg
Mean anomaly: 308
0245 deg
Mean motion: 15
60043776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 321
Coasting Arc #11 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2011/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2154385
86 A = 6761151
49 meter
Y = 3955808
19 meter E =
0032013
Z = -5066111
18 I = 51
90751
XDOT = -5231
906597 Wp = 74
08089
YDOT = 5259
263537 meter/sec RA = 123
26727 deg
ZDOT = 1900
222279 TA = 214
19410
MA = 214
40068
Ha = 219
358 n
mi
Hp = 197
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7068195
07 X = 2134601
75
Y = 12978373
31 feet Y = 3979789
54 meter
Z = -16621099
69 Z = -5055692
82
XDOT = -17165
047889 XDOT = -5299
558952
YDOT = 17254
801629 feet/sec YDOT = 5200
378768 meter/sec
ZDOT = 6234
325061 ZDOT = 1874
641264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14657645
51 X = -4467650
35
Y = -2226065
54 feet Y = -678504
78 meter
Z = -16578798
83 Z = -5053217
88
XDOT = -3358
167882 XDOT = -1023
569571
YDOT = -23085
825826 feet/sec YDOT = -7036
559712 meter/sec
ZDOT = 6129
598713 ZDOT = 1868
301688
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 11318
51282400
00016717 00000-0 10270-3 0 9104
2 25544 51
6364 124
1620 0021687 56
2165 304
1052 15
60108393 24380
Satellite: ISS
Catalog Number: 25544
Epoch time: 11318
51282400 = yrday
fracday
Element set: 910
Inclination: 51
6364 deg
RA of node: 124
1620 deg
Eccentricity:
0021687
Arg of perigee: 56
2165 deg
Mean anomaly: 304
1052 deg
Mean motion: 15
60108393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 268
Coasting Arc #12 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2011/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 857858
21 A = 6768630
97 meter
Y = -6123664
92 meter E =
0032969
Z = 2737347
49 I = 51
94866
XDOT = 5449
207899 Wp = 75
45260
YDOT = -1578
222259 meter/sec RA = 118
24833 deg
ZDOT = -5178
376314 TA = 73
61308
MA = 73
25089
Ha = 219
262 n
mi
Hp = 197
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2814495
45 X = 912972
78
Y = -20090764
17 feet Y = -6113763
81 meter
Z = 8980798
84 Z = 2741648
54
XDOT = 17877
978672 XDOT = 5491
606819
YDOT = -5177
894549 feet/sec YDOT = -1517
048518 meter/sec
ZDOT = -16989
423603 ZDOT = -5151
800832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14491750
20 X = 4417085
46
Y = 14185456
93 feet Y = 4323727
27 meter
Z = 8998717
98 Z = 2742809
24
XDOT = -5517
596496 XDOT = -1681
763412
YDOT = 16469
844188 feet/sec YDOT = 5020
008508 meter/sec
ZDOT = -16880
836072 ZDOT = -5145
278835
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 11319
53768775
00016717 00000-0 10270-3 0 9112
2 25544 51
6361 119
0050 0021590 59
6595 300
6692 15
60165900 24540
Satellite: ISS
Catalog Number: 25544
Epoch time: 11319
53768775 = yrday
fracday
Element set: 911
Inclination: 51
6361 deg
RA of node: 119
0050 deg
Eccentricity:
0021590
Arg of perigee: 59
6595 deg
Mean anomaly: 300
6692 deg
Mean motion: 15
60165900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 306
Coasting Arc #13 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2011/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3225132
56 A = 6771380
31 meter
Y = 5880397
99 meter E =
0034943
Z = 818014
87 I = 51
97311
XDOT = -3822
990266 Wp = 59
89425
YDOT = -2952
915759 meter/sec RA = 113
26932 deg
ZDOT = 5982
521881 TA = 308
94706
MA = 309
25797
Ha = 219
233 n
mi
Hp = 197
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10581143
57 X = -3294622
44
Y = 19292644
31 feet Y = 5843944
00 meter
Z = 2683775
83 Z = 802178
50
XDOT = -12542
618984 XDOT = -3818
748336
YDOT = -9688
043828 feet/sec YDOT = -2995
643328 meter/sec
ZDOT = 19627
696459 ZDOT = 5963
959784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9525194
53 X = -2903279
29
Y = -19843943
98 feet Y = -6048434
12 meter
Z = 2618765
54 Z = 798199
74
XDOT = 13798
037521 XDOT = 4205
641836
YDOT = -3966
462948 feet/sec YDOT = -1208
977907 meter/sec
ZDOT = 19552
086016 ZDOT = 5959
475818
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
56251484
00016717 00000-0 10270-3 0 9122
2 25544 51
6373 113
8493 0021663 63
7586 296
5793 15
60234697 24706
Satellite: ISS
Catalog Number: 25544
Epoch time: 11320
56251484 = yrday
fracday
Element set: 912
Inclination: 51
6373 deg
RA of node: 113
8493 deg
Eccentricity:
0021663
Arg of perigee: 63
7586 deg
Mean anomaly: 296
5793 deg
Mean motion: 15
60234697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 322
Coasting Arc #14 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2011/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4406002
65 A = 6764474
27 meter
Y = -3146109
47 meter E =
0028950
Z = -4086455
84 I = 51
96203
XDOT = 1053
209288 Wp = 68
15657
YDOT = 6509
843804 meter/sec RA = 108
27723 deg
ZDOT = -3887
834102 TA = 161
74294
MA = 161
63879
Ha = 219
198 n
mi
Hp = 197
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14455389
28 X = 4460707
04
Y = -10321881
45 feet Y = -3096532
86 meter
Z = -13407007
36 Z = -4064918
51
XDOT = 3455
411049 XDOT = 999
223207
YDOT = 21357
755261 feet/sec YDOT = 6521
319694 meter/sec
ZDOT = -12755
361227 ZDOT = -3882
848514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 244530
56 X = 74532
92
Y = 17826809
92 feet Y = 5433611
66 meter
Z = -13318874
39 Z = -4059592
91
XDOT = -18286
656221 XDOT = -5573
772816
YDOT = -9235
596912 feet/sec YDOT = -2815
009939 meter/sec
ZDOT = -12735
399992 ZDOT = -3881
749918
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
52325535
00016717 00000-0 10270-3 0 9139
2 25544 51
6378 109
0151 0021742 66
9481 293
3965 15
60289444 24858
Satellite: ISS
Catalog Number: 25544
Epoch time: 11321
52325535 = yrday
fracday
Element set: 913
Inclination: 51
6378 deg
RA of node: 109
0151 deg
Eccentricity:
0021742
Arg of perigee: 66
9481 deg
Mean anomaly: 293
3965 deg
Mean motion: 15
60289444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 311
Coasting Arc #15 (Orbit 2494)
---------------------------------------
Vector Time (GMT): 2011/322/03:30:47
682
Vector Time (MET): N/A
Weight (LBS) : 870468
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4223921
15 A = 6762727
59 meter
Y = 267483
11 meter E =
0031469
Z = -5301519
40 I = 51
95401
XDOT = -1409
453564 Wp = 73
87097
YDOT = 7486
045081 meter/sec RA = 105
02505 deg
ZDOT = -740
404044 TA = 189
04438
MA = 189
10120
Ha = 219
204 n
mi
Hp = 200
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13858009
02 X = 4246370
22
Y = 877569
25 feet Y = 314843
20 meter
Z = -17393436
36 Z = -5280944
88
XDOT = -4624
191484 XDOT = -1489
462465
YDOT = 24560
515357 feet/sec YDOT = 7469
836366 meter/sec
ZDOT = -2429
147126 ZDOT = -747
445440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3656155
04 X = -1114396
06
Y = -13504148
05 feet Y = -4116064
33 meter
Z = -17309439
21 Z = -5275917
07
XDOT = 23754
388075 XDOT = 7240
337485
YDOT = -3259
707571 feet/sec YDOT = -993
558868 meter/sec
ZDOT = -2458
360043 ZDOT = -749
308141
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
16373375
00016717 00000-0 10270-3 0 9146
2 25544 51
6401 105
7969 0017294 65
0212 295
2738 15
59235740 24952
Satellite: ISS
Catalog Number: 25544
Epoch time: 11322
16373375 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 105
7969 deg
Eccentricity:
0017294
Arg of perigee: 65
0212 deg
Mean anomaly: 295
2738 deg
Mean motion: 15
59235740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2495
Checksum: 312
Coasting Arc #16 (Orbit 2510)
---------------------------------------
Vector Time (GMT): 2011/323/03:30:47
682
Vector Time (MET): N/A
Weight (LBS) : 870468
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2952113
41 A = 6765370
39 meter
Y = -3970797
60 meter E =
0025777
Z = 4598363
01 I = 51
96986
XDOT = 3492
864987 Wp = 67
44911
YDOT = -6138
990539 meter/sec RA = 99
99572 deg
ZDOT = -3035
637728 TA = 52
75403
MA = 52
51916
Ha = 219
220 n
mi
Hp = 200
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9685411
44 X = -2929830
01
Y = -13027551
20 feet Y = -4003685
37 meter
Z = 15086492
82 Z = 4584075
60
XDOT = 11459
530798 XDOT = 3575
999533
YDOT = -20141
045077 feet/sec YDOT = -6099
466341 meter/sec
ZDOT = -9959
441366 ZDOT = -3018
467290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8962221
83 X = -2731685
21
Y = 13599720
28 feet Y = 4145194
74 meter
Z = 15028397
75 Z = 4580655
63
XDOT = -21856
097067 XDOT = -6661
738386
YDOT = -3391
178228 feet/sec YDOT = -1033
631124 meter/sec
ZDOT = -9888
940446 ZDOT = -3014
149048
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
18918102
00016717 00000-0 10270-3 0 9153
2 25544 51
6396 100
6450 0017287 68
3251 291
9743 15
59293522 25115
Satellite: ISS
Catalog Number: 25544
Epoch time: 11323
18918102 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 100
6450 deg
Eccentricity:
0017287
Arg of perigee: 68
3251 deg
Mean anomaly: 291
9743 deg
Mean motion: 15
59293522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2511
Checksum: 302
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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