[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 27th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 788)
---------------------------------------
Vector Time (GMT): 2012/361/11:45:21
748
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4766066
40 A = 6789177
56 meter
Y = 2632337
43 meter E =
0026615
Z = 4034747
80 I = 51
32318
XDOT = -361
841062 Wp = 83
82659
YDOT = 6621
107377 meter/sec RA = 245
29635 deg
ZDOT = -3867
459729 TA = 46
47543
MA = 46
25459
Ha = 230
490 n
mi
Hp = 212
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15636700
77 X = 4716677
00
Y = 8636277
65 feet Y = 2685357
94 meter
Z = 13237361
55 Z = 4057781
39
XDOT = -1187
142593 XDOT = -417
065613
YDOT = 21722
793233 feet/sec YDOT = 6616
752715 meter/sec
ZDOT = -12688
516170 ZDOT = -3869
350901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8389226
32 X = -2557036
18
Y = 15690196
42 feet Y = 4782371
87 meter
Z = 13332593
96 Z = 4063774
64
XDOT = -20592
592827 XDOT = -6276
622294
YDOT = -152
409579 feet/sec YDOT = -46
454440 meter/sec
ZDOT = -12697
152691 ZDOT = -3870
092140
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
53104715
00016717 00000-0 10270-3 0 9006
2 25544 51
6485 246
0374 0016068 87
8280 272
4711 15
51774892 7898
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
53104715 = yrday
fracday
Element set: 900
Inclination: 51
6485 deg
RA of node: 246
0374 deg
Eccentricity:
0016068
Arg of perigee: 87
8280 deg
Mean anomaly: 272
4711 deg
Mean motion: 15
51774892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 789
Checksum: 318
Coasting Arc #2 (Orbit 803)
---------------------------------------
Vector Time (GMT): 2012/362/11:45:21
748
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4952532
04 A = 6791169
62 meter
Y = -3172600
20 meter E =
0020861
Z = -3413834
32 I = 51
34362
XDOT = 752
616077 Wp = 91
45005
YDOT = -6080
060463 meter/sec RA = 240
30769 deg
ZDOT = 4582
443778 TA = 228
54627
MA = 228
72562
Ha = 230
516 n
mi
Hp = 212
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16248464
71 X = -4900103
76
Y = -10408793
31 feet Y = -3227688
96 meter
Z = -11200243
84 Z = -3437766
36
XDOT = 2469
212850 XDOT = 798
288347
YDOT = -19947
704931 feet/sec YDOT = -6071
389414 meter/sec
ZDOT = 15034
264364 ZDOT = 4586
210142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9868846
05 X = 3008024
28
Y = -16514722
69 feet Y = -5033687
48 meter
Z = -11299152
97 Z = -3443981
82
XDOT = 18810
029257 XDOT = 5733
296917
YDOT = 996
138449 feet/sec YDOT = 303
622999 meter/sec
ZDOT = 15050
609578 ZDOT = 4587
425799
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
49704748
00016717 00000-0 10270-3 0 9015
2 25544 51
6486 241
2394 0015939 91
3018 268
9960 15
51775408 8041
Satellite: ISS
Catalog Number: 25544
Epoch time: 12362
49704748 = yrday
fracday
Element set: 901
Inclination: 51
6486 deg
RA of node: 241
2394 deg
Eccentricity:
0015939
Arg of perigee: 91
3018 deg
Mean anomaly: 268
9960 deg
Mean motion: 15
51775408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 804
Checksum: 330
Coasting Arc #3 (Orbit 819)
---------------------------------------
Vector Time (GMT): 2012/363/11:45:21
748
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5070436
41 A = 6793237
33 meter
Y = 3674714
25 meter E =
0029548
Z = 2601198
30 I = 51
36594
XDOT = -1274
862439 Wp = 98
78737
YDOT = 5483
499047 meter/sec RA = 235
32282 deg
ZDOT = -5215
123998 TA = 51
80052
MA = 51
53480
Ha = 230
504 n
mi
Hp = 212
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16635290
06 X = 5016332
24
Y = 12056149
13 feet Y = 3731112
23 meter
Z = 8534115
14 Z = 2625698
98
XDOT = -4182
619551 XDOT = -1310
751717
YDOT = 17990
482439 feet/sec YDOT = 5469
042668 meter/sec
ZDOT = -17109
986869 ZDOT = -5221
403699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11208126
50 X = -3416236
96
Y = 17167513
64 feet Y = 5232658
16 meter
Z = 8635340
43 Z = 2632051
76
XDOT = -16919
549551 XDOT = -5157
078703
YDOT = -2350
783016 feet/sec YDOT = -716
518663 meter/sec
ZDOT = -17136
684044 ZDOT = -5223
261297
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
52743867
00016717 00000-0 10270-3 0 9026
2 25544 51
6481 236
1210 0016042 95
1877 265
1105 15
51781066 8202
Satellite: ISS
Catalog Number: 25544
Epoch time: 12363
52743867 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 236
1210 deg
Eccentricity:
0016042
Arg of perigee: 95
1877 deg
Mean anomaly: 265
1105 deg
Mean motion: 15
51781066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 820
Checksum: 292
Coasting Arc #4 (Orbit 834)
---------------------------------------
Vector Time (GMT): 2012/364/11:45:21
748
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5185043
91 A = 6794667
87 meter
Y = -4013727
79 meter E =
0020501
Z = -1790806
15 I = 51
38878
XDOT = 1827
120746 Wp = 80
80766
YDOT = -4848
986550 meter/sec RA = 230
34141 deg
ZDOT = 5636
427125 TA = 259
48787
MA = 259
71891
Ha = 230
409 n
mi
Hp = 212
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17011298
91 X = -5131076
99
Y = -13168398
27 feet Y = -4071408
26 meter
Z = -5875348
27 Z = -1815863
84
XDOT = 5994
490636 XDOT = 1853
827239
YDOT = -15908
748525 feet/sec YDOT = -4828
405804 meter/sec
ZDOT = 18492
214976 ZDOT = 5645
367435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11994232
45 X = 3655842
05
Y = -17824205
67 feet Y = -5432817
89 meter
Z = -5978862
84 Z = -1822357
39
XDOT = 14967
974387 XDOT = 4562
238593
YDOT = 3920
024744 feet/sec YDOT = 1194
823542 meter/sec
ZDOT = 18529
874067 ZDOT = 5647
905616
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
49341922
00016717 00000-0 10270-3 0 9030
2 25544 51
6476 231
3226 0015826 98
4227 261
8719 15
51808213 8358
Satellite: ISS
Catalog Number: 25544
Epoch time: 12364
49341922 = yrday
fracday
Element set: 903
Inclination: 51
6476 deg
RA of node: 231
3226 deg
Eccentricity:
0015826
Arg of perigee: 98
4227 deg
Mean anomaly: 261
8719 deg
Mean motion: 15
51808213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 835
Checksum: 312
Coasting Arc #5 (Orbit 850)
---------------------------------------
Vector Time (GMT): 2012/365/11:45:21
748
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5177532
43 A = 6795843
04 meter
Y = 4307494
69 meter E =
0028705
Z = 824335
11 I = 51
41219
XDOT = -2511
143799 Wp = 113
48481
YDOT = 4180
594026 meter/sec RA = 225
36370 deg
ZDOT = -5920
465682 TA = 57
57381
MA = 57
29648
Ha = 230
467 n
mi
Hp = 212
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16986654
96 X = 5124975
94
Y = 14132200
44 feet Y = 4365099
17 meter
Z = 2704511
52 Z = 849359
64
XDOT = -8238
660759 XDOT = -2528
945635
YDOT = 13715
859665 feet/sec YDOT = 4152
413828 meter/sec
ZDOT = -19424
100006 ZDOT = -5932
707380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12646411
91 X = -3854626
35
Y = 18104254
57 feet Y = 5518176
79 meter
Z = 2807872
99 Z = 855839
69
XDOT = -13031
853850 XDOT = -3972
109053
YDOT = -6007
787235 feet/sec YDOT = -1831
173549 meter/sec
ZDOT = -19475
380278 ZDOT = -5936
095909
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
52379071
00016717 00000-0 10270-3 0 9042
2 25544 51
6472 226
2038 0015906 102
7251 257
5679 15
51786835 8513
Satellite: ISS
Catalog Number: 25544
Epoch time: 12365
52379071 = yrday
fracday
Element set: 904
Inclination: 51
6472 deg
RA of node: 226
2038 deg
Eccentricity:
0015906
Arg of perigee: 102
7251 deg
Mean anomaly: 257
5679 deg
Mean motion: 15
51786835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 851
Checksum: 319
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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