[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 25th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2012/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2597300
78 A = 6795769
76 meter
Y = 6160408
30 meter E =
0027903
Z = 1176741
77 I = 51
32436
XDOT = -4076
095957 Wp = 100
14905
YDOT = 2854
363205 meter/sec RA = 255
23848 deg
ZDOT = -5832
750365 TA = 67
02191
MA = 66
72778
Ha = 230
650 n
mi
Hp = 212
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8521328
01 X = 2522504
40
Y = 20211313
33 feet Y = 6189034
62 meter
Z = 3860701
35 Z = 1189178
28
XDOT = -13373
018231 XDOT = -4079
376879
YDOT = 9364
708677 feet/sec YDOT = 2808
763968 meter/sec
ZDOT = -19136
320096 ZDOT = -5852
559579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19804045
11 X = -6036272
95
Y = 9408237
86 feet Y = 2867630
90 meter
Z = 3911532
95 Z = 1192235
24
XDOT = -9270
649737 XDOT = -2825
694040
YDOT = -11371
283077 feet/sec YDOT = -3465
967082 meter/sec
ZDOT = -19218
823153 ZDOT = -5857
897297
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 12359
53461980
00016717 00000-0 10270-3 0 9003
2 25544 51
6481 255
9524 0016027 81
6058 278
6910 15
51711379 7586
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
53461980 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 255
9524 deg
Eccentricity:
0016027
Arg of perigee: 81
6058 deg
Mean anomaly: 278
6910 deg
Mean motion: 15
51711379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 758
Checksum: 323
Coasting Arc #2 (Orbit 772)
---------------------------------------
Vector Time (GMT): 2012/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2525049
79 A = 6796179
55 meter
Y = -6295751
65 meter E =
0025620
Z = -312287
57 I = 51
33516
XDOT = 4353
774926 Wp = 67
46748
YDOT = -2022
577488 meter/sec RA = 250
25675 deg
ZDOT = 5975
274260 TA = 289
15589
MA = 289
43304
Ha = 230
543 n
mi
Hp = 212
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8284284
09 X = -2452944
68
Y = -20655353
18 feet Y = -6323585
14 meter
Z = -1024565
52 Z = -324379
68
XDOT = 14284
038472 XDOT = 4347
041721
YDOT = -6635
752912 feet/sec YDOT = -1973
929147 meter/sec
ZDOT = 19603
918175 ZDOT = 5996
408115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20096006
73 X = 6125262
85
Y = -9556141
05 feet Y = -2912711
79 meter
Z = -1073961
88 Z = -327343
58
XDOT = 6812
122644 XDOT = 2076
334982
YDOT = 12254
204821 feet/sec YDOT = 3735
081629 meter/sec
ZDOT = 19691
819970 ZDOT = 6002
066727
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 12360
50063333
00016717 00000-0 10270-3 0 9013
2 25544 51
6483 251
1548 0015939 84
5583 275
7387 15
51758500 7738
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
50063333 = yrday
fracday
Element set: 901
Inclination: 51
6483 deg
RA of node: 251
1548 deg
Eccentricity:
0015939
Arg of perigee: 84
5583 deg
Mean anomaly: 275
7387 deg
Mean motion: 15
51758500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 773
Checksum: 315
Coasting Arc #3 (Orbit 788)
---------------------------------------
Vector Time (GMT): 2012/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2330624
17 A = 6796086
83 meter
Y = 6345003
65 meter E =
0024065
Z = -671116
33 I = 51
34585
XDOT = -4711
541868 Wp = 108
95181
YDOT = 1121
952016 meter/sec RA = 245
27613 deg
ZDOT = -5937
334075 TA = 78
31642
MA = 78
04646
Ha = 230
571 n
mi
Hp = 212
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7646404
77 X = 2262759
91
Y = 20816941
10 feet Y = 6370686
77 meter
Z = -2201825
23 Z = -659958
41
XDOT = -15457
814528 XDOT = -4694
895483
YDOT = 3680
944933 feet/sec YDOT = 1069
358371 meter/sec
ZDOT = -19479
442503 ZDOT = -5960
181885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20138833
30 X = -6138316
39
Y = 9297222
47 feet Y = 2833793
41 meter
Z = -2156298
88 Z = -657239
90
XDOT = -4214
283165 XDOT = -1284
513509
YDOT = -13526
541636 feet/sec YDOT = -4122
889891 meter/sec
ZDOT = -19574
353150 ZDOT = -5966
262840
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 12361
53103545
00016717 00000-0 10270-3 0 9028
2 25544 51
6483 246
0364 0015873 88
8854 271
4116 15
51742316 7890
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
53103545 = yrday
fracday
Element set: 902
Inclination: 51
6483 deg
RA of node: 246
0364 deg
Eccentricity:
0015873
Arg of perigee: 88
8854 deg
Mean anomaly: 271
4116 deg
Mean motion: 15
51742316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 789
Checksum: 312
Coasting Arc #4 (Orbit 804)
---------------------------------------
Vector Time (GMT): 2012/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2149099
04 A = 6795154
03 meter
Y = -6249739
30 meter E =
0028756
Z = 1538708
10 I = 51
35636
XDOT = 5090
411874 Wp = 78
02786
YDOT = -319
261781 meter/sec RA = 240
29522 deg
ZDOT = 5727
920560 TA = 298
84964
MA = 299
13796
Ha = 230
475 n
mi
Hp = 212
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7050849
85 X = -2086528
05
Y = -20504394
03 feet Y = -6273422
20 meter
Z = 5048254
92 Z = 1528419
19
XDOT = 16700
826359 XDOT = 5065
778860
YDOT = -1047
446788 feet/sec YDOT = -262
476021 meter/sec
ZDOT = 18792
390289 ZDOT = 5752
589500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19720700
47 X = 6010869
50
Y = -9036612
58 feet Y = -2754359
51 meter
Z = 5006310
23 Z = 1525923
36
XDOT = 1990
398401 XDOT = 606
673433
YDOT = 14967
346563 feet/sec YDOT = 4562
047232 meter/sec
ZDOT = 18894
770131 ZDOT = 5759
125936
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 12362
56142250
00016717 00000-0 10270-3 0 9039
2 25544 51
6479 240
9184 0015841 91
7218 268
5748 15
51792115 8059
Satellite: ISS
Catalog Number: 25544
Epoch time: 12362
56142250 = yrday
fracday
Element set: 903
Inclination: 51
6479 deg
RA of node: 240
9184 deg
Eccentricity:
0015841
Arg of perigee: 91
7218 deg
Mean anomaly: 268
5748 deg
Mean motion: 15
51792115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 805
Checksum: 312
Coasting Arc #5 (Orbit 819)
---------------------------------------
Vector Time (GMT): 2012/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1808466
48 A = 6793591
95 meter
Y = 6071221
03 meter E =
0020330
Z = -2462303
54 I = 51
36673
XDOT = -5499
093483 Wp = 105
11209
YDOT = -496
199997 meter/sec RA = 235
31359 deg
ZDOT = -5304
296438 TA = 102
51931
MA = 102
29181
Ha = 230
425 n
mi
Hp = 212
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5933288
97 X = 1752403
58
Y = 19918704
18 feet Y = 6091131
25 meter
Z = -8078423
67 Z = -2453653
66
XDOT = -18041
645284 XDOT = -5467
369378
YDOT = -1627
952746 feet/sec YDOT = -557
516314 meter/sec
ZDOT = -17402
547369 ZDOT = -5330
933494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19105612
15 X = -5823390
58
Y = 8215924
19 feet Y = 2504213
69 meter
Z = -8043245
44 Z = -2451581
21
XDOT = 171
864731 XDOT = 52
384370
YDOT = -16609
902746 feet/sec YDOT = -5062
698357 meter/sec
ZDOT = -17513
008939 ZDOT = -5337
965125
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 12363
52739814
00016717 00000-0 10270-3 0 9045
2 25544 51
6475 236
1197 0015679 95
8440 264
4499 15
51788380 8201
Satellite: ISS
Catalog Number: 25544
Epoch time: 12363
52739814 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 236
1197 deg
Eccentricity:
0015679
Arg of perigee: 95
8440 deg
Mean anomaly: 264
4499 deg
Mean motion: 15
51788380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 820
Checksum: 340
Coasting Arc #6 (Orbit 835)
---------------------------------------
Vector Time (GMT): 2012/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1456484
14 A = 6791688
16 meter
Y = -5786777
06 meter E =
0028377
Z = 3220572
55 I = 51
37805
XDOT = 5908
702828 Wp = 93
43304
YDOT = 1178
278156 meter/sec RA = 230
33000 deg
ZDOT = 4751
379274 TA = 304
00557
MA = 304
27482
Ha = 230
399 n
mi
Hp = 212
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4778491
27 X = -1407311
52
Y = -18985489
05 feet Y = -5802789
77 meter
Z = 10566182
91 Z = 3213615
95
XDOT = 19385
507967 XDOT = 5872
007127
YDOT = 3865
741983 feet/sec YDOT = 1244
147298 meter/sec
ZDOT = 15588
514678 ZDOT = 4779
994072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18185564
87 X = 5542960
17
Y = -7291302
78 feet Y = -2222389
09 meter
Z = 10537985
04 Z = 3211977
84
XDOT = -1835
455313 XDOT = -559
446779
YDOT = 18303
720079 feet/sec YDOT = 5578
973880 meter/sec
ZDOT = 15707
117692 ZDOT = 4787
529472
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 12364
55775944
00016717 00000-0 10270-3 0 9054
2 25544 51
6468 231
0011 0015742 98
6996 261
5940 15
51819515 8361
Satellite: ISS
Catalog Number: 25544
Epoch time: 12364
55775944 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 231
0011 deg
Eccentricity:
0015742
Arg of perigee: 98
6996 deg
Mean anomaly: 261
5940 deg
Mean motion: 15
51819515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 836
Checksum: 329
Coasting Arc #7 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2012/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 929728
44 A = 6789375
07 meter
Y = 5445418
65 meter E =
0021625
Z = -3964482
86 I = 51
38994
XDOT = -6271
651928 Wp = 94
21077
YDOT = -1817
172430 meter/sec RA = 225
34409 deg
ZDOT = -3987
198282 TA = 134
04716
MA = 133
86884
Ha = 230
264 n
mi
Hp = 212
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3050290
15 X = 888025
76
Y = 17865546
75 feet Y = 5455582
63 meter
Z = -13006833
54 Z = -3960067
18
XDOT = -20576
285852 XDOT = -6231
497208
YDOT = -5961
851803 feet/sec YDOT = -1887
081100 meter/sec
ZDOT = -13081
359193 ZDOT = -4017
567815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17203556
22 X = -5243643
94
Y = 5742814
93 feet Y = 1750409
99 meter
Z = -12989129
27 Z = -3959086
60
XDOT = 3278
745250 XDOT = 999
361552
YDOT = -19898
273260 feet/sec YDOT = -6064
993690 meter/sec
ZDOT = -13207
186780 ZDOT = -4025
550531
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 12365
52370940
00016717 00000-0 10270-3 0 9060
2 25544 51
6459 226
2018 0015541 102
7389 257
5501 15
51840893 8512
Satellite: ISS
Catalog Number: 25544
Epoch time: 12365
52370940 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 226
2018 deg
Eccentricity:
0015541
Arg of perigee: 102
7389 deg
Mean anomaly: 257
5501 deg
Mean motion: 15
51840893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 306
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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