[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 30th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2011/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3043932
24 A = 6769200
16 meter
Y = -4497101
67 meter E =
0023949
Z = -4054254
64 I = 51
29336
XDOT = 3339
052258 Wp = 191
45406
YDOT = -5738
079283 meter/sec RA = 272
65320 deg
ZDOT = 3830
894286 TA = 118
49372
MA = 118
25232
Ha = 219
604 n
mi
Hp = 203
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9986654
32 X = -2973724
04
Y = -14754270
56 feet Y = -4530747
72 meter
Z = -13301360
36 Z = -4068871
83
XDOT = 10954
895859 XDOT = 3384
358976
YDOT = -18825
719434 feet/sec YDOT = -5700
487107 meter/sec
ZDOT = 12568
550808 ZDOT = 3847
224447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14057579
28 X = 4284750
17
Y = -10873050
74 feet Y = -3314105
87 meter
Z = -13360732
92 Z = -4072351
39
XDOT = 18719
218645 XDOT = 5705
617843
YDOT = 8566
691473 feet/sec YDOT = 2611
127561 meter/sec
ZDOT = 12635
732920 ZDOT = 3851
371394
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 11360
50894568
00016717 00000-0 10270-3 0 9003
2 25544 51
6433 273
4121 0024150 208
9692 151
0124 15
58639518 30932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11360
50894568 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 273
4121 deg
Eccentricity:
0024150
Arg of perigee: 208
9692 deg
Mean anomaly: 151
0124 deg
Mean motion: 15
58639518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 299
Coasting Arc #2 (Orbit 3108)
---------------------------------------
Vector Time (GMT): 2011/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1396751
96 A = 6775410
27 meter
Y = 6460230
87 meter E =
0027183
Z = 1408131
01 I = 51
31363
XDOT = -4544
432234 Wp = 181
95968
YDOT = 2237
206119 meter/sec RA = 267
62266 deg
ZDOT = -5786
149925 TA = 342
55788
MA = 342
65107
Ha = 219
347 n
mi
Hp = 204
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4582519
56 X = 1317568
25
Y = 21194983
18 feet Y = 6475407
33 meter
Z = 4619852
40 Z = 1414724
63
XDOT = -14909
554575 XDOT = -4541
003840
YDOT = 7339
915089 feet/sec YDOT = 2186
407250 meter/sec
ZDOT = -18983
431514 ZDOT = -5808
217797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20736443
44 X = -6320467
96
Y = 6323105
32 feet Y = 1927282
50 meter
Z = 4646298
13 Z = 1416191
67
XDOT = -8097
474033 XDOT = -2468
110085
YDOT = -12611
671630 feet/sec YDOT = -3844
037513 meter/sec
ZDOT = -19073
783484 ZDOT = -5813
689206
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 11361
53479316
00016717 00000-0 10270-3 0 9018
2 25544 51
6432 268
2640 0024199 212
7284 147
2373 15
58636218 31097
Satellite: ISS
Catalog Number: 25544
Epoch time: 11361
53479316 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 268
2640 deg
Eccentricity:
0024199
Arg of perigee: 212
7284 deg
Mean anomaly: 147
2373 deg
Mean motion: 15
58636218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3109
Checksum: 309
Coasting Arc #3 (Orbit 3124)
---------------------------------------
Vector Time (GMT): 2011/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 588234
48 A = 6774772
49 meter
Y = -6520636
46 meter E =
0013601
Z = 1776167
96 I = 51
31401
XDOT = 4803
581386 Wp = 187
06688
YDOT = 1969
936347 meter/sec RA = 262
60806 deg
ZDOT = 5632
491314 TA = 192
53143
MA = 192
56528
Ha = 219
058 n
mi
Hp = 204
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1929903
14 X = 652477
67
Y = -21393164
25 feet Y = -6513699
40 meter
Z = 5827322
71 Z = 1779181
08
XDOT = 15759
781451 XDOT = 4753
835046
YDOT = 6463
045759 feet/sec YDOT = 2023
374348 meter/sec
ZDOT = 18479
302210 ZDOT = 5655
705999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21474694
25 X = 6545486
81
Y = -283041
35 feet Y = -86271
00 meter
Z = 5840127
32 Z = 1780070
81
XDOT = -4865
804709 XDOT = -1483
097275
YDOT = 14656
132346 feet/sec YDOT = 4467
189139 meter/sec
ZDOT = 18574
024777 ZDOT = 5661
362752
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 11362
56062073
00016717 00000-0 10270-3 0 9021
2 25544 51
6429 263
1144 0024091 216
8599 143
0901 15
58680625 31251
Satellite: ISS
Catalog Number: 25544
Epoch time: 11362
56062073 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 263
1144 deg
Eccentricity:
0024091
Arg of perigee: 216
8599 deg
Mean anomaly: 143
0901 deg
Mean motion: 15
58680625 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3125
Checksum: 296
Coasting Arc #4 (Orbit 3139)
---------------------------------------
Vector Time (GMT): 2011/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2535425
56 A = 6767975
44 meter
Y = 4544884
42 meter E =
0016990
Z = -4310956
70 I = 51
29710
XDOT = -4057
787881 Wp = 206
36026
YDOT = -5535
427466 meter/sec RA = 257
57265 deg
ZDOT = -3459
014035 TA = 28
46756
MA = 28
37486
Ha = 218
626 n
mi
Hp = 204
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8318325
33 X = -2565117
43
Y = 14911038
11 feet Y = 4516365
98 meter
Z = -14143558
74 Z = -4323345
43
XDOT = -13312
952364 XDOT = -3978
785066
YDOT = -18160
851266 feet/sec YDOT = -5580
362200 meter/sec
ZDOT = -11348
471242 ZDOT = -3478
534881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15780298
80 X = -4809835
08
Y = -6408705
01 feet Y = -1953373
29 meter
Z = -14194524
21 Z = -4326490
98
XDOT = 15997
813128 XDOT = 4876
133441
YDOT = -14150
997173 feet/sec YDOT = -4313
223938 meter/sec
ZDOT = -11427
843281 ZDOT = -3483
206632
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 11363
52231681
00016717 00000-0 10270-3 0 9032
2 25544 51
6434 258
2872 0024085 220
6855 139
2502 15
58727912 31403
Satellite: ISS
Catalog Number: 25544
Epoch time: 11363
52231681 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 258
2872 deg
Eccentricity:
0024085
Arg of perigee: 220
6855 deg
Mean anomaly: 139
2502 deg
Mean motion: 15
58727912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3140
Checksum: 299
Coasting Arc #5 (Orbit 3155)
---------------------------------------
Vector Time (GMT): 2011/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4029765
83 A = 6763894
53 meter
Y = -1306122
26 meter E =
0022598
Z = 5285715
17 I = 51
29106
XDOT = 2319
600203 Wp = 219
98004
YDOT = 7306
034053 meter/sec RA = 252
50535 deg
ZDOT = 19
953090 TA = 229
72989
MA = 229
92770
Ha = 218
380 n
mi
Hp = 204
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13221016
52 X = 4018394
97
Y = -4285178
03 feet Y = -1261122
80 meter
Z = 17341585
20 Z = 5305263
80
XDOT = 7610
236885 XDOT = 2237
633350
YDOT = 23969
927996 feet/sec YDOT = 7331
514945 meter/sec
ZDOT = 65
462895 ZDOT = 31
022831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6021816
69 X = 1835449
73
Y = 12414307
42 feet Y = 3783880
90 meter
Z = 17421575
72 Z = 5310096
28
XDOT = -21812
522670 XDOT = -6648
456910
YDOT = 10348
254256 feet/sec YDOT = 3154
147897 meter/sec
ZDOT = 110
179031 ZDOT = 33
582569
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 11364
54810850
00016717 00000-0 10270-3 0 9047
2 25544 51
6431 253
1378 0024151 224
5403 135
3812 15
58763813 31569
Satellite: ISS
Catalog Number: 25544
Epoch time: 11364
54810850 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 253
1378 deg
Eccentricity:
0024151
Arg of perigee: 224
5403 deg
Mean anomaly: 135
3812 deg
Mean motion: 15
58763813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3156
Checksum: 290
Coasting Arc #6 (Orbit 3170)
---------------------------------------
Vector Time (GMT): 2011/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4689820
86 A = 6767854
24 meter
Y = -2300412
28 meter E =
0021478
Z = -4306292
92 I = 51
31466
XDOT = 156
491204 Wp = 207
52514
YDOT = -6845
485916 meter/sec RA = 247
43692 deg
ZDOT = 3460
747877 TA = 97
89760
MA = 97
65376
Ha = 218
086 n
mi
Hp = 204
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15386551
39 X = -4642829
68
Y = -7547284
39 feet Y = -2352593
78 meter
Z = -14128257
61 Z = -4328961
79
XDOT = 513
422586 XDOT = 216
215665
YDOT = -22458
943294 feet/sec YDOT = -6843
402174 meter/sec
ZDOT = 11354
159702 ZDOT = 3461
652822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5126131
71 X = 1562444
95
Y = -16272929
38 feet Y = -4959988
87 meter
Z = -14220747
92 Z = -4334483
97
XDOT = 21076
720501 XDOT = 6424
184409
YDOT = -3359
679720 feet/sec YDOT = -1024
030379 meter/sec
ZDOT = 11358
343534 ZDOT = 3462
023109
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 11365
50977235
00016717 00000-0 10270-3 0 9056
2 25544 51
6432 248
3093 0024120 228
3805 131
5284 15
58774604 31712
Satellite: ISS
Catalog Number: 25544
Epoch time: 11365
50977235 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 248
3093 deg
Eccentricity:
0024120
Arg of perigee: 228
3805 deg
Mean anomaly: 131
5284 deg
Mean motion: 15
58774604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3171
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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