[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 28th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 2454)
---------------------------------------
Vector Time (GMT): 2013/360/14:10:32
749
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4746706
34 A = 6791082
13 meter
Y = 81925
72 meter E =
0007615
Z = -4862593
91 I = 51
34104
XDOT = -2568
253344 Wp = 89
15724
YDOT = -6802
763548 meter/sec RA = 234
03444 deg
ZDOT = 2395
806348 TA = 204
44956
MA = 204
48570
Ha = 226
776 n
mi
Hp = 222
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15573183
54 X = -4723648
49
Y = 268785
18 feet Y = 28974
14 meter
Z = -15953392
09 Z = -4885596
98
XDOT = -8426
028030 XDOT = -2503
630633
YDOT = -22318
778046 feet/sec YDOT = -6831
122165 meter/sec
ZDOT = 7860
257048 ZDOT = 2383
486692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9537052
56 X = -2906893
62
Y = -12187803
13 feet Y = -3714842
39 meter
Z = -16050205
40 Z = -4892102
61
XDOT = 11816
196795 XDOT = 3601
576783
YDOT = -19516
087976 feet/sec YDOT = -5948
503615 meter/sec
ZDOT = 7809
444378 ZDOT = 2380
318647
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 13360
60259745
00016717 00000-0 10270-3 0 9008
2 25544 51
6470 234
9769 0005251 314
2078 45
8641 15
50064565 24554
Satellite: ISS
Catalog Number: 25544
Epoch time: 13360
60259745 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 234
9769 deg
Eccentricity:
0005251
Arg of perigee: 314
2078 deg
Mean anomaly: 45
8641 deg
Mean motion: 15
50064565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2455
Checksum: 306
Coasting Arc #2 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2013/361/14:10:32
749
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4904824
71 A = 6791695
30 meter
Y = -76530
27 meter E =
0008172
Z = 4697689
12 I = 51
36242
XDOT = 2770
400944 Wp = 24
35903
YDOT = 6580
338197 meter/sec RA = 229
05871 deg
ZDOT = -2776
319250 TA = 93
33179
MA = 93
23830
Ha = 226
861 n
mi
Hp = 222
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16091944
58 X = 4882495
80
Y = -251083
56 feet Y = -21806
49 meter
Z = 15412365
89 Z = 4721462
13
XDOT = 9089
241941 XDOT = 2710
098869
YDOT = 21589
036078 feet/sec YDOT = 6610
981567 meter/sec
ZDOT = -9108
658956 ZDOT = -2763
006983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10053108
91 X = 3064187
60
Y = 12444049
44 feet Y = 3792946
27 meter
Z = 15512426
65 Z = 4728187
64
XDOT = -10459
683188 XDOT = -3188
111436
YDOT = 19772
742983 feet/sec YDOT = 6026
732061 meter/sec
ZDOT = -9053
626434 ZDOT = -2759
545337
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 13361
63412986
00016717 00000-0 10270-3 0 9011
2 25544 51
6474 229
8666 0005333 317
2191 42
8544 15
50078866 24713
Satellite: ISS
Catalog Number: 25544
Epoch time: 13361
63412986 = yrday
fracday
Element set: 901
Inclination: 51
6474 deg
RA of node: 229
8666 deg
Eccentricity:
0005333
Arg of perigee: 317
2191 deg
Mean anomaly: 42
8544 deg
Mean motion: 15
50078866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2471
Checksum: 318
Coasting Arc #3 (Orbit 2485)
---------------------------------------
Vector Time (GMT): 2013/362/14:10:32
749
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5069371
73 A = 6792333
19 meter
Y = 120750
74 meter E =
0006014
Z = -4524010
48 I = 51
38426
XDOT = -2943
831641 Wp = 84
00771
YDOT = -6335
695131 meter/sec RA = 224
08310 deg
ZDOT = 3133
817501 TA = 217
55963
MA = 217
60165
Ha = 226
965 n
mi
Hp = 221
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16631797
03 X = -5048368
76
Y = 396163
83 feet Y = 64179
55 meter
Z = -14842554
06 Z = -4548586
06
XDOT = -9658
240291 XDOT = -2887
988965
YDOT = -20786
401348 feet/sec YDOT = -6368
302928 meter/sec
ZDOT = 10281
553480 ZDOT = 3119
651776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10720567
34 X = -3267628
93
Y = -12600050
12 feet Y = -3840495
28 meter
Z = -14946009
57 Z = -4555543
72
XDOT = 9107
400505 XDOT = 2775
935674
YDOT = -19858
839405 feet/sec YDOT = -6052
974251 meter/sec
ZDOT = 10222
883385 ZDOT = 3115
934856
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 13362
60118183
00016717 00000-0 10270-3 0 9022
2 25544 51
6460 225
0742 0005204 321
4152 38
6626 15
50093825 24864
Satellite: ISS
Catalog Number: 25544
Epoch time: 13362
60118183 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 225
0742 deg
Eccentricity:
0005204
Arg of perigee: 321
4152 deg
Mean anomaly: 38
6626 deg
Mean motion: 15
50093825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2486
Checksum: 280
Coasting Arc #4 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2013/363/14:10:32
749
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5250430
11 A = 6793106
60 meter
Y = -160605
45 meter E =
0009503
Z = 4306584
34 I = 51
40973
XDOT = 3064
257301 Wp = 40
19696
YDOT = 6088
089513 meter/sec RA = 219
11078 deg
ZDOT = -3497
340163 TA = 85
59529
MA = 85
48672
Ha = 227
070 n
mi
Hp = 221
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17225820
57 X = 5230915
58
Y = -526920
77 feet Y = -102001
32 meter
Z = 14129213
72 Z = 4332043
05
XDOT = 10053
337601 XDOT = 3012
940322
YDOT = 19974
046960 feet/sec YDOT = 6122
069394 meter/sec
ZDOT = -11474
213132 ZDOT = -3482
578340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11420673
59 X = 3481021
31
Y = 12788049
04 feet Y = 3897797
35 meter
Z = 14236405
33 Z = 4339256
35
XDOT = -7856
079784 XDOT = -2394
533118
YDOT = 19763
161051 feet/sec YDOT = 6023
811488 meter/sec
ZDOT = -11412
987077 ZDOT = -3478
678461
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 13363
63269157
00016717 00000-0 10270-3 0 9035
2 25544 51
6459 219
9636 0005293 324
3469 35
7327 15
50105530 25029
Satellite: ISS
Catalog Number: 25544
Epoch time: 13363
63269157 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 219
9636 deg
Eccentricity:
0005293
Arg of perigee: 324
3469 deg
Mean anomaly: 35
7327 deg
Mean motion: 15
50105530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 308
Coasting Arc #5 (Orbit 2516)
---------------------------------------
Vector Time (GMT): 2013/364/14:10:32
749
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5424879
38 A = 6793838
70 meter
Y = 255880
42 meter E =
0004833
Z = -4084282
64 I = 51
43592
XDOT = -3155
934809 Wp = 66
29451
YDOT = -5831
069370 meter/sec RA = 214
13910 deg
ZDOT = 3832
010535 TA = 243
46940
MA = 243
51895
Ha = 227
149 n
mi
Hp = 221
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17798160
69 X = -5407497
24
Y = 839502
67 feet Y = 195313
60 meter
Z = -13399877
44 Z = -4110593
87
XDOT = -10354
116829 XDOT = -3109
110733
YDOT = -19130
805019 feet/sec YDOT = -5866
099665 meter/sec
ZDOT = 12572
213042 ZDOT = 3816
792427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12253352
88 X = -3734821
96
Y = -12820010
37 feet Y = -3907539
16 meter
Z = -13510687
67 Z = -4118057
60
XDOT = 6659
851474 XDOT = 2029
922729
YDOT = -19529
522251 feet/sec YDOT = -5952
598382 meter/sec
ZDOT = 12509
016005 ZDOT = 3812
748078
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 13364
59972239
00016717 00000-0 10270-3 0 9044
2 25544 51
6449 215
1711 0005126 329
0734 31
0114 15
50124890 25171
Satellite: ISS
Catalog Number: 25544
Epoch time: 13364
59972239 = yrday
fracday
Element set: 904
Inclination: 51
6449 deg
RA of node: 215
1711 deg
Eccentricity:
0005126
Arg of perigee: 329
0734 deg
Mean anomaly: 31
0114 deg
Mean motion: 15
50124890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2517
Checksum: 289
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