[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 25th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
243/12:13:52
403 -5
8 6
7 6
7
N/A 2
5 0
1 215
0
000/00:17:44
807 2
0 -0
0 205
2
Coasting Arc #1 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2011/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4547889
69 A = 6765189
56 meter
Y = -3395358
53 meter E =
0024295
Z = 3664868
61 I = 51
59838
XDOT = 5659
891806 Wp = 99
76657
YDOT = -2867
088718 meter/sec RA = 185
95849 deg
ZDOT = 4338
863491 TA = 304
03834
MA = 304
26881
Ha = 215
601 n
mi
Hp = 200
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14920897
95 X = -4527387
24
Y = -11139627
74 feet Y = -3446101
25 meter
Z = 12023847
15 Z = 3642824
88
XDOT = 18569
198838 XDOT = 5670
454258
YDOT = -9406
459050 feet/sec YDOT = -2803
737382 meter/sec
ZDOT = 14235
116439 ZDOT = 4366
384610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7312297
90 X = 2228788
40
Y = 17187211
08 feet Y = 5238661
94 meter
Z = 11934298
32 Z = 3637574
13
XDOT = -19449
512661 XDOT = -5928
211459
YDOT = -1752
836421 feet/sec YDOT = -534
264541 meter/sec
ZDOT = 14347
152306 ZDOT = 4373
012023
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 11234
55633271
00016717 00000-0 10270-3 0 9000
2 25544 51
6366 186
7106 0012473 104
3006 255
9536 15
60507279 11277
Satellite: ISS
Catalog Number: 25544
Epoch time: 11234
55633271 = yrday
fracday
Element set: 900
Inclination: 51
6366 deg
RA of node: 186
7106 deg
Eccentricity:
0012473
Arg of perigee: 104
3006 deg
Mean anomaly: 255
9536 deg
Mean motion: 15
60507279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 291
Coasting Arc #2 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2011/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 456172
33 A = 6759010
70 meter
Y = 4203833
03 meter E =
0026748
Z = -5295707
02 I = 51
60788
XDOT = -7641
025689 Wp = 96
08345
YDOT = 248
750904 meter/sec RA = 180
90096 deg
ZDOT = -465
526511 TA = 169
49697
MA = 169
44099
Ha = 215
526 n
mi
Hp = 200
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1496628
39 X = 434855
64
Y = 13792103
12 feet Y = 4208815
18 meter
Z = -17374366
87 Z = -5293542
63
XDOT = -25068
981919 XDOT = -7640
977952
YDOT = 816
111891 feet/sec YDOT = 163
304570 meter/sec
ZDOT = -1527
317950 ZDOT = -502
646070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5365461
41 X = 1635392
64
Y = -12805266
23 feet Y = -3903045
15 meter
Z = -17365702
11 Z = -5293066
00
XDOT = 21307
616254 XDOT = 6494
561434
YDOT = 11182
695183 feet/sec YDOT = 3408
485492 meter/sec
ZDOT = -1678
327075 ZDOT = -511
554092
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 11235
51692989
00016717 00000-0 10270-3 0 9019
2 25544 51
6367 181
8745 0012412 107
1771 253
0745 15
60483616 11422
Satellite: ISS
Catalog Number: 25544
Epoch time: 11235
51692989 = yrday
fracday
Element set: 901
Inclination: 51
6367 deg
RA of node: 181
8745 deg
Eccentricity:
0012412
Arg of perigee: 107
1771 deg
Mean anomaly: 253
0745 deg
Mean motion: 15
60483616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 305
Coasting Arc #3 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2011/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3827922
54 A = 6763115
59 meter
Y = -3623941
56 meter E =
0021242
Z = 4217837
66 I = 51
65291
XDOT = 6324
842513 Wp = 94
56527
YDOT = 2427
437349 meter/sec RA = 175
83959 deg
ZDOT = -3640
434088 TA = 32
62511
MA = 32
49405
Ha = 215
385 n
mi
Hp = 200
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12558800
99 X = 3847672
48
Y = -11889572
05 feet Y = -3581025
08 meter
Z = 13838050
05 Z = 4236481
30
XDOT = 20750
795645 XDOT = 6314
912664
YDOT = 7964
033298 feet/sec YDOT = 2498
110174 meter/sec
ZDOT = -11943
681391 ZDOT = -3609
732518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16626166
29 X = -5067655
49
Y = 4532948
76 feet Y = 1381642
78 meter
Z = 13914021
88 Z = 4240993
87
XDOT = -14206
747921 XDOT = -4330
216766
YDOT = -15688
921060 feet/sec YDOT = -4781
983139 meter/sec
ZDOT = -11818
852614 ZDOT = -3602
386277
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 11236
54155536
00016717 00000-0 10270-3 0 9026
2 25544 51
6371 176
7174 0012409 110
8319 249
4167 15
60513514 11586
Satellite: ISS
Catalog Number: 25544
Epoch time: 11236
54155536 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 176
7174 deg
Eccentricity:
0012409
Arg of perigee: 110
8319 deg
Mean anomaly: 249
4167 deg
Mean motion: 15
60513514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 296
Coasting Arc #4 (Orbit 1172)
---------------------------------------
Vector Time (GMT): 2011/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6416410
86 A = 6770288
52 meter
Y = 1884820
20 meter E =
0017298
Z = -1060567
89 I = 51
70701
XDOT = -2241
940889 Wp = 82
51855
YDOT = -4358
491134 meter/sec RA = 170
82301 deg
ZDOT = 5902
395981 TA = 265
96972
MA = 266
16747
Ha = 215
383 n
mi
Hp = 200
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21051216
74 X = -6431858
46
Y = 6183793
30 feet Y = 1812981
62 meter
Z = -3479553
44 Z = -1091775
73
XDOT = -7355
449111 XDOT = -2221
709005
YDOT = -14299
511593 feet/sec YDOT = -4383
448854 meter/sec
ZDOT = 19364
816212 ZDOT = 5891
553910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21517411
68 X = 6558507
08
Y = 4182552
04 feet Y = 1274841
86 meter
Z = -3606601
06 Z = -1099292
00
XDOT = 362
629512 XDOT = 110
529475
YDOT = 14564
012352 feet/sec YDOT = 4439
110965 meter/sec
ZDOT = 19320
842618 ZDOT = 5888
992830
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 11237
50213191
00016717 00000-0 10270-3 0 9036
2 25544 51
6370 171
8822 0012360 114
3142 245
9306 15
60519606 11731
Satellite: ISS
Catalog Number: 25544
Epoch time: 11237
50213191 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 171
8822 deg
Eccentricity:
0012360
Arg of perigee: 114
3142 deg
Mean anomaly: 245
9306 deg
Mean motion: 15
60519606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1173
Checksum: 271
Coasting Arc #5 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2011/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6171234
23 A = 6767688
24 meter
Y = 640914
38 meter E =
0017272
Z = -2703123
77 I = 51
72946
XDOT = -2771
348614 Wp = 120
41731
YDOT = 4924
973567 meter/sec RA = 165
82595 deg
ZDOT = -5192
460016 TA = 90
16314
MA = 89
96522
Ha = 215
377 n
mi
Hp = 200
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20246831
46 X = 6176739
75
Y = 2102737
46 feet Y = 709955
66 meter
Z = -8868516
32 Z = -2673131
19
XDOT = -9092
351095 XDOT = -2800
991163
YDOT = 16158
049762 feet/sec YDOT = 4893
816888 meter/sec
ZDOT = -17035
629973 ZDOT = -5205
994964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17248124
81 X = -5257228
44
Y = -10909057
12 feet Y = -3325080
61 meter
Z = -8746481
25 Z = -2665927
48
XDOT = 14440
587641 XDOT = 4401
491113
YDOT = -9217
449206 feet/sec YDOT = -2809
478518 meter/sec
ZDOT = -17090
870313 ZDOT = -5209
297271
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 11238
52673650
00016717 00000-0 10270-3 0 9040
2 25544 51
6384 166
7239 0012354 118
0242 242
2165 15
60548078 11891
Satellite: ISS
Catalog Number: 25544
Epoch time: 11238
52673650 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 166
7239 deg
Eccentricity:
0012354
Arg of perigee: 118
0242 deg
Mean anomaly: 242
2165 deg
Mean motion: 15
60548078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 305
Coasting Arc #6 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2011/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3284936
73 A = 6759801
53 meter
Y = -3065736
84 meter E =
0017958
Z = 5040134
04 I = 51
73270
XDOT = 6421
488324 Wp = 123
38113
YDOT = -3793
594334 meter/sec RA = 160
79249 deg
ZDOT = 1863
285738 TA = 308
55707
MA = 308
71785
Ha = 215
291 n
mi
Hp = 200
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10777351
48 X = -3274894
43
Y = -10058191
72 feet Y = -3102414
69 meter
Z = 16535872
84 Z = 5024200
67
XDOT = 21067
875079 XDOT = 6454
380474
YDOT = -12446
175637 feet/sec YDOT = -3721
601359 meter/sec
ZDOT = 6113
142184 ZDOT = 1894
560643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5507997
98 X = 1678837
79
Y = 13752007
55 feet Y = 4191611
90 meter
Z = 16471122
09 Z = 5020398
01
XDOT = -23333
951959 XDOT = -7112
188557
YDOT = 1814
335194 feet/sec YDOT = 553
009367 meter/sec
ZDOT = 6240
550964 ZDOT = 1902
119934
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 11239
55132916
00016717 00000-0 10270-3 0 9050
2 25544 51
6385 161
5669 0012284 122
5386 237
6959 15
60589229 12054
Satellite: ISS
Catalog Number: 25544
Epoch time: 11239
55132916 = yrday
fracday
Element set: 905
Inclination: 51
6385 deg
RA of node: 161
5669 deg
Eccentricity:
0012284
Arg of perigee: 122
5386 deg
Mean anomaly: 237
6959 deg
Mean motion: 15
60589229 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 328
Coasting Arc #7 (Orbit 1219)
---------------------------------------
Vector Time (GMT): 2011/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -922490
89 A = 6760561
15 meter
Y = 4623334
25 meter E =
0023907
Z = -4868006
02 I = 51
76422
XDOT = -7174
824284 Wp = 116
81955
YDOT = 1131
676960 meter/sec RA = 155
73269 deg
ZDOT = 2433
112593 TA = 177
03993
MA = 177
02576
Ha = 215
170 n
mi
Hp = 200
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3026544
90 X = -950473
95
Y = 15168419
46 feet Y = 4612861
65 meter
Z = -15971148
36 Z = -4872555
63
XDOT = -23539
449750 XDOT = -7198
765044
YDOT = 3712
850920 feet/sec YDOT = 1051
309974 meter/sec
ZDOT = 7982
652864 ZDOT = 2398
199808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8940657
99 X = 2725112
55
Y = -12597977
89 feet Y = -3839863
66 meter
Z = -15989812
09 Z = -4873694
72
XDOT = 22092
515472 XDOT = 6733
798716
YDOT = 5721
885204 feet/sec YDOT = 1744
030610 meter/sec
ZDOT = 7840
510714 ZDOT = 2389
787666
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 11240
51187725
00016717 00000-0 10270-3 0 9067
2 25544 51
6392 156
7311 0012264 125
3718 234
8585 15
60572370 12200
Satellite: ISS
Catalog Number: 25544
Epoch time: 11240
51187725 = yrday
fracday
Element set: 906
Inclination: 51
6392 deg
RA of node: 156
7311 deg
Eccentricity:
0012264
Arg of perigee: 125
3718 deg
Mean anomaly: 234
8585 deg
Mean motion: 15
60572370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1220
Checksum: 291
Coasting Arc #8 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2011/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4539889
41 A = 6768586
13 meter
Y = -4505179
86 meter E =
0025836
Z = 2171985
37 I = 51
81838
XDOT = 4873
693256 Wp = 118
81761
YDOT = 2236
012605 meter/sec RA = 150
70901 deg
ZDOT = -5511
882495 TA = 37
03562
MA = 36
85757
Ha = 215
101 n
mi
Hp = 200
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14894650
30 X = 4579378
86
Y = -14780773
82 feet Y = -4454191
07 meter
Z = 7125936
26 Z = 2194136
05
XDOT = 15989
807270 XDOT = 4875
102784
YDOT = 7335
999360 feet/sec YDOT = 2290
520672 meter/sec
ZDOT = -18083
603987 ZDOT = -5488
203245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19505744
99 X = -5945351
07
Y = 7651965
84 feet Y = 2332319
19 meter
Z = 7216244
23 Z = 2199511
24
XDOT = -11293
470023 XDOT = -3442
249663
YDOT = -11711
849590 feet/sec YDOT = -3569
771755 meter/sec
ZDOT = -17987
285079 ZDOT = -5482
524492
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 11241
53645052
00016717 00000-0 10270-3 0 9073
2 25544 51
6393 151
5734 0012315 129
3989 230
8259 15
60577269 12367
Satellite: ISS
Catalog Number: 25544
Epoch time: 11241
53645052 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 151
5734 deg
Eccentricity:
0012315
Arg of perigee: 129
3989 deg
Mean anomaly: 230
8259 deg
Mean motion: 15
60577269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 314
Coasting Arc #9 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2011/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6038871
47 A = 6769566
80 meter
Y = 2607527
61 meter E =
0021414
Z = 1586863
00 I = 51
84766
XDOT = -643
354175 Wp = 95
19229
YDOT = -5036
046428 meter/sec RA = 145
72116 deg
ZDOT = 5758
406915 TA = 282
15893
MA = 282
39874
Ha = 215
025 n
mi
Hp = 200
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19812570
44 X = -6075289
14
Y = 8554880
60 feet Y = 2539793
77 meter
Z = 5206243
43 Z = 1557437
82
XDOT = -2110
742044 XDOT = -614
965290
YDOT = -16522
462033 feet/sec YDOT = -5043
081588 meter/sec
ZDOT = 18892
411138 ZDOT = 5755
350919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21606741
83 X = 6585734
91
Y = -326175
81 feet Y = -99418
39 meter
Z = 5086375
65 Z = 1550327
30
XDOT = -4279
122510 XDOT = -1304
276541
YDOT = 14542
815690 feet/sec YDOT = 4432
650222 meter/sec
ZDOT = 18880
130626 ZDOT = 5754
663815
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 11242
56101232
00016717 00000-0 10270-3 0 9085
2 25544 51
6393 146
4157 0012187 132
9145 227
3035 15
60597660 12528
Satellite: ISS
Catalog Number: 25544
Epoch time: 11242
56101232 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 146
4157 deg
Eccentricity:
0012187
Arg of perigee: 132
9145 deg
Mean anomaly: 227
3035 deg
Mean motion: 15
60597660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 287
Coasting Arc #10 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2011/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4930373
46 A = 6761571
24 meter
Y = 631502
63 meter E =
0018544
Z = -4596336
31 I = 51
84613
XDOT = -3602
681955 Wp = 107
02223
YDOT = 6043
488580 meter/sec RA = 140
70863 deg
ZDOT = -3049
593332 TA = 132
67579
MA = 132
51941
Ha = 214
898 n
mi
Hp = 200
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16175765
96 X = 4945273
48
Y = 2071859
01 feet Y = 686720
03 meter
Z = -15079843
52 Z = -4572348
56
XDOT = -11819
822687 XDOT = -3655
179381
YDOT = 19827
718439 feet/sec YDOT = 6002
907421 meter/sec
ZDOT = -10005
227466 ZDOT = -3067
223037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14379287
30 X = -4382806
77
Y = -7881572
94 feet Y = -2402303
43 meter
Z = -14982209
10 Z = -4566577
33
XDOT = 17626
083801 XDOT = 5372
430343
YDOT = -13098
232261 feet/sec YDOT = -3992
341193 meter/sec
ZDOT = -10077
196576 ZDOT = -3071
529516
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 11243
52152807
00016717 00000-0 10270-3 0 9097
2 25544 51
6398 141
5798 0012116 136
6445 223
5667 15
60639322 12673
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52152807 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 141
5798 deg
Eccentricity:
0012116
Arg of perigee: 136
6445 deg
Mean anomaly: 223
5667 deg
Mean motion: 15
60639322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 314
Coasting Arc #11 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2011/243/12:22:44
807
Vector Time (MET): N/A
Weight (LBS) : 900973
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3052146
02 A = 6771158
33 meter
Y = 5359891
60 meter E =
0008408
Z = -2805944
24 I = 51
86494
XDOT = -5672
634709 Wp = 121
33673
YDOT = -549
256307 meter/sec RA = 140
58446 deg
ZDOT = 5128
231264 TA = 206
89711
MA = 206
94072
Ha = 215
030 n
mi
Hp = 205
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10013602
44 X = -3098223
85
Y = 17584946
19 feet Y = 5325502
78 meter
Z = -9205853
81 Z = -2820883
81
XDOT = -18611
006264 XDOT = -5690
983085
YDOT = -1802
022003 feet/sec YDOT = -612
793368 meter/sec
ZDOT = 16824
905723 ZDOT = 5100
629250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14362066
05 X = 4377557
73
Y = -14216429
84 feet Y = -4333167
82 meter
Z = -9266849
10 Z = -2824535
60
XDOT = 16481
576758 XDOT = 5023
584596
YDOT = 5771
465685 feet/sec YDOT = 1759
142741 meter/sec
ZDOT = 16712
554608 ZDOT = 5093
986644
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 11243
52152831
00016717 00000-0 10270-3 0 9106
2 25544 51
6396 141
5803 0007281 154
7912 205
3600 15
59222268 12675
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52152831 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 141
5803 deg
Eccentricity:
0007281
Arg of perigee: 154
7912 deg
Mean anomaly: 205
3600 deg
Mean motion: 15
59222268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 285
Coasting Arc #12 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2011/244/12:22:44
807
Vector Time (MET): N/A
Weight (LBS) : 900973
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5084070
01 A = 6774573
94 meter
Y = -4435204
48 meter E =
0018233
Z = -494622
57 I = 51
89831
XDOT = 2798
356227 Wp = 147
04966
YDOT = 3865
814241 meter/sec RA = 135
60381 deg
ZDOT = -6019
238881 TA = 38
28167
MA = 38
15237
Ha = 215
060 n
mi
Hp = 205
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16680019
73 X = 5135690
26
Y = -14551195
81 feet Y = -4378062
71 meter
Z = -1622777
47 Z = -469798
57
XDOT = 9180
958749 XDOT = 2784
160257
YDOT = 12683
117589 feet/sec YDOT = 3897
027434 meter/sec
ZDOT = -19748
159060 ZDOT = -6005
679219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19850090
38 X = -6050307
55
Y = 9810837
42 feet Y = 2990343
25 meter
Z = -1521560
22 Z = -463771
56
XDOT = -5040
335864 XDOT = -1536
294371
YDOT = -13187
908436 feet/sec YDOT = -4019
674491 meter/sec
ZDOT = -19693
085953 ZDOT = -6002
452598
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 11244
54699977
00016717 00000-0 10270-3 0 9117
2 25544 51
6394 136
4283 0007385 159
6569 200
4882 15
59188140 12831
Satellite: ISS
Catalog Number: 25544
Epoch time: 11244
54699977 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 136
4283 deg
Eccentricity:
0007385
Arg of perigee: 159
6569 deg
Mean anomaly: 200
4882 deg
Mean motion: 15
59188140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 342
Coasting Arc #13 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2011/245/12:22:44
807
Vector Time (MET): N/A
Weight (LBS) : 900973
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5394155
03 A = 6769239
49 meter
Y = 1998705
64 meter E =
0016083
Z = 3562702
47 I = 51
90129
XDOT = 681
116101 Wp = 117
13192
YDOT = -6194
104535 meter/sec RA = 130
61749 deg
ZDOT = 4483
542050 TA = 284
86363
MA = 285
04170
Ha = 214
881 n
mi
Hp = 205
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17697359
04 X = -5433410
98
Y = 6557433
21 feet Y = 1938165
55 meter
Z = 11688656
41 Z = 3536402
28
XDOT = 2234
632876 XDOT = 728
548960
YDOT = -20321
865273 feet/sec YDOT = -6186
222493 meter/sec
ZDOT = 14709
783628 ZDOT = 4486
966361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18818827
60 X = 5735978
65
Y = -2131124
12 feet Y = -649566
63 meter
Z = 11581501
34 Z = 3530041
61
XDOT = -7086
111745 XDOT = -2159
846860
YDOT = 17850
616669 feet/sec YDOT = 5440
867961 meter/sec
ZDOT = 14723
948320 ZDOT = 4487
859448
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 11245
57246020
00016717 00000-0 10270-3 0 9129
2 25544 51
6391 131
2760 0007123 162
3746 197
7658 15
59225582 12997
Satellite: ISS
Catalog Number: 25544
Epoch time: 11245
57246020 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 131
2760 deg
Eccentricity:
0007123
Arg of perigee: 162
3746 deg
Mean anomaly: 197
7658 deg
Mean motion: 15
59225582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 310
Coasting Arc #14 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2011/246/12:22:44
807
Vector Time (MET): N/A
Weight (LBS) : 900973
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4073723
28 A = 6762846
43 meter
Y = 1362722
61 meter E =
0016321
Z = -5236036
12 I = 51
89903
XDOT = -3663
005369 Wp = 106
95709
YDOT = 6638
994039 meter/sec RA = 125
59544 deg
ZDOT = -1129
559910 TA = 152
29468
MA = 152
20763
Ha = 214
634 n
mi
Hp = 205
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13365233
87 X = 4083617
93
Y = 4470874
69 feet Y = 1408332
69 meter
Z = -17178596
19 Z = -5216222
02
XDOT = -12017
734149 XDOT = -3731
484469
YDOT = 21781
476506 feet/sec YDOT = 6597
649165 meter/sec
ZDOT = -3705
905215 ZDOT = -1147
521206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12141845
75 X = -3700834
58
Y = -7345577
52 feet Y = -2238932
03 meter
Z = -17097965
86 Z = -5211460
00
XDOT = 15991
161227 XDOT = 4874
105942
YDOT = -17693
459266 feet/sec YDOT = -5392
966384 meter/sec
ZDOT = -3779
292264 ZDOT = -1151
928282
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 11246
53381912
00016717 00000-0 10270-3 0 9137
2 25544 51
6388 126
4454 0007049 167
2346 192
8989 15
59275582 13142
Satellite: ISS
Catalog Number: 25544
Epoch time: 11246
53381912 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 126
4454 deg
Eccentricity:
0007049
Arg of perigee: 167
2346 deg
Mean anomaly: 192
8989 deg
Mean motion: 15
59275582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 333
Coasting Arc #15 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2011/247/12:22:44
807
Vector Time (MET): N/A
Weight (LBS) : 900973
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1703571
39 A = 6764589
99 meter
Y = -4471076
06 meter E =
0008270
Z = 4774035
10 I = 51
92247
XDOT = 5306
072154 Wp = 113
81807
YDOT = -4872
511962 meter/sec RA = 120
56159 deg
ZDOT = -2669
506606 TA = 2
37838
MA = 2
37445
Ha = 214
489 n
mi
Hp = 205
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5589144
99 X = -1676639
61
Y = -14668884
71 feet Y = -4489975
82 meter
Z = 15662844
83 Z = 4765824
65
XDOT = 17408
373208 XDOT = 5373
131083
YDOT = -15985
931633 feet/sec YDOT = -4812
801293 meter/sec
ZDOT = -8758
223773 ZDOT = -2643
566930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2556423
44 X = 779197
86
Y = 15521604
71 feet Y = 4730985
12 meter
Z = 15629584
61 Z = 4763897
39
XDOT = -19234
825703 XDOT = -5862
774874
YDOT = 11881
819843 feet/sec YDOT = 3621
578688 meter/sec
ZDOT = -8652
397919 ZDOT = -2637
250886
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 11247
55925945
00016717 00000-0 10270-3 0 9141
2 25544 51
6392 121
2934 0006973 172
0325 188
0942 15
59312395 13307
Satellite: ISS
Catalog Number: 25544
Epoch time: 11247
55925945 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 121
2934 deg
Eccentricity:
0006973
Arg of perigee: 172
0325 deg
Mean anomaly: 188
0942 deg
Mean motion: 15
59312395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 312
Coasting Arc #16 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2011/248/12:22:44
807
Vector Time (MET): N/A
Weight (LBS) : 900973
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -916376
35 A = 6771923
88 meter
Y = 6269196
00 meter E =
0005513
Z = -2400161
30 I = 51
96055
XDOT = -5295
111975 Wp = 124
64274
YDOT = 1289
205520 meter/sec RA = 115
55703 deg
ZDOT = 5394
773230 TA = 208
62637
MA = 208
65665
Ha = 214
343 n
mi
Hp = 205
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3006484
07 X = -974752
17
Y = 20568228
35 feet Y = 6258622
11 meter
Z = -7874544
96 Z = -2404754
84
XDOT = -17372
414616 XDOT = -5335
341167
YDOT = 4229
676902 feet/sec YDOT = 1229
767432 meter/sec
ZDOT = 17699
387239 ZDOT = 5368
952096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6774794
78 X = 2064957
45
Y = -19644187
97 feet Y = -5987548
49 meter
Z = -7893507
28 Z = -2405941
02
XDOT = 16530
038365 XDOT = 5038
355694
YDOT = -1361
437775 feet/sec YDOT = -414
966234 meter/sec
ZDOT = 17594
172620 ZDOT = 5362
703815
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 11248
52060253
00016717 00000-0 10270-3 0 9152
2 25544 51
6386 116
4627 0006942 175
9446 184
1767 15
59279564 13455
Satellite: ISS
Catalog Number: 25544
Epoch time: 11248
52060253 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 116
4627 deg
Eccentricity:
0006942
Arg of perigee: 175
9446 deg
Mean anomaly: 184
1767 deg
Mean motion: 15
59279564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 331
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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