Date:
May 20th 2009
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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 127)
---------------------------------------
Vector Time (GMT): 2009/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1847138
15 A = 6730584
14 meter
Y = 5526828
65 meter E =
0011868
Z = -3364537
54 I = 51
96953
XDOT = -4338
646868 Wp = 38
36639
YDOT = 4293
917363 meter/sec RA = 98
36527 deg
ZDOT = 4689
419519 TA = 282
22912
MA = 282
36201
Ha = 194
475 n
mi
Hp = 183
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6060164
52 X = 1801543
39
Y = 18132639
92 feet Y = 5547229
70 meter
Z = -11038508
99 Z = -3355674
47
XDOT = -14234
405734 XDOT = -4409
120274
YDOT = 14087
655389 feet/sec YDOT = 4245
005752 meter/sec
ZDOT = 15385
234643 ZDOT = 4668
171265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18415963
95 X = 5613185
81
Y = 5209882
35 feet Y = 1587972
14 meter
Z = -11003467
76 Z = -3353856
97
XDOT = 3891
783189 XDOT = 1186
215516
YDOT = 18438
197901 feet/sec YDOT = 5619
962720 meter/sec
ZDOT = 15302
293189 ZDOT = 4664
138964
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 09138
50696387
00010596 00000-0 82463-4 0 9005
2 25544 51
6372 99
1545 0009539 15
4625 344
6827 15
72841106 1288
Satellite: ISS
Catalog Number: 25544
Epoch time: 09138
50696387 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 99
1545 deg
Eccentricity:
0009539
Arg of perigee: 15
4625 deg
Mean anomaly: 344
6827 deg
Mean motion: 15
72841106 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 128
Checksum: 323
Coasting Arc #2 (Orbit 143)
---------------------------------------
Vector Time (GMT): 2009/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3292229
53 A = 6728863
70 meter
Y = -4421306
80 meter E =
0014227
Z = -3875448
64 I = 51
96813
XDOT = 2905
215148 Wp = 40
93132
YDOT = 5790
142734 meter/sec RA = 93
31191 deg
ZDOT = -4135
699012 TA = 185
96917
MA = 185
98615
Ha = 194
425 n
mi
Hp = 183
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10801277
98 X = 3360251
12
Y = -14505599
73 feet Y = -4384110
61 meter
Z = -12714726
50 Z = -3859289
81
XDOT = 9531
545760 XDOT = 2860
343612
YDOT = 18996
531281 feet/sec YDOT = 5822
379899 meter/sec
ZDOT = -13568
566311 ZDOT = -4121
693947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6102204
45 X = -1859951
92
Y = -17071658
02 feet Y = -5203441
36 meter
Z = -12651715
03 Z = -3856242
74
XDOT = 19901
199908 XDOT = 6065
885732
YDOT = 2905
917792 feet/sec YDOT = 885
723743 meter/sec
ZDOT = -13513
379883 ZDOT = -4118
878188
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 09139
52352214
00010596 00000-0 82463-4 0 9017
2 25544 51
6380 93
9419 0009539 19
1677 340
9843 15
72902011 1445
Satellite: ISS
Catalog Number: 25544
Epoch time: 09139
52352214 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 93
9419 deg
Eccentricity:
0009539
Arg of perigee: 19
1677 deg
Mean anomaly: 340
9843 deg
Mean motion: 15
72902011 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 144
Checksum: 302
Coasting Arc #3 (Orbit 159)
---------------------------------------
Vector Time (GMT): 2009/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3161364
92 A = 6728828
08 meter
Y = -4516227
06 meter E =
0018212
Z = 3854017
54 I = 51
96910
XDOT = 3066
645212 Wp = 54
82267
YDOT = -5711
731783 meter/sec RA = 88
15643 deg
ZDOT = -4153
666023 TA = 78
50694
MA = 78
30249
Ha = 194
488 n
mi
Hp = 183
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10371932
16 X = -3129351
20
Y = -14817017
91 feet Y = -4551400
54 meter
Z = 12644414
49 Z = 3838736
83
XDOT = 10061
171954 XDOT = 3150
464952
YDOT = -18739
277504 feet/sec YDOT = -5676
969840 meter/sec
ZDOT = -13627
513200 ZDOT = -4138
564760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18108305
78 X = -5519411
60
Y = 852348
97 feet Y = 259795
97 meter
Z = 12584314
73 Z = 3835699
13
XDOT = -10298
654213 XDOT = -3139
029804
YDOT = -17297
807413 feet/sec YDOT = -5272
371699 meter/sec
ZDOT = -13568
710161 ZDOT = -4135
742857
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 09140
54006051
00010596 00000-0 82463-4 0 9027
2 25544 51
6383 88
7298 0009516 22
4711 337
6866 15
72932842 1607
Satellite: ISS
Catalog Number: 25544
Epoch time: 09140
54006051 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 88
7298 deg
Eccentricity:
0009516
Arg of perigee: 22
4711 deg
Mean anomaly: 337
6866 deg
Mean motion: 15
72932842 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 160
Checksum: 304
Coasting Arc #4 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2009/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1987749
84 A = 6730244
50 meter
Y = 5466391
58 meter E =
0018836
Z = 3362616
75 I = 51
97254
XDOT = -4227
205984 Wp = 62
94087
YDOT = -4427
051134 meter/sec RA = 83
10340 deg
ZDOT = 4686
392512 TA = 336
50672
MA = 336
59266
Ha = 194
521 n
mi
Hp = 183
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6521488
99 X = -2065063
56
Y = 17934355
59 feet Y = 5443730
85 meter
Z = 11032207
18 Z = 3352772
69
XDOT = -13868
786036 XDOT = -4200
153914
YDOT = -14524
445978 feet/sec YDOT = -4474
171339 meter/sec
ZDOT = 15375
303516 ZDOT = 4665
921654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11850571
75 X = 3612054
27
Y = 14985899
91 feet Y = 4567702
29 meter
Z = 10993965
51 Z = 3350960
69
XDOT = -18584
084462 XDOT = -5664
428944
YDOT = 3447
414218 feet/sec YDOT = 1050
771854 meter/sec
ZDOT = 15294
891753 ZDOT = 4661
883006
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 09141
55657888
00010596 00000-0 82463-4 0 9030
2 25544 51
6389 83
5177 0009418 26
5239 333
6404 15
72962552 1765
Satellite: ISS
Catalog Number: 25544
Epoch time: 09141
55657888 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 83
5177 deg
Eccentricity:
0009418
Arg of perigee: 26
5239 deg
Mean anomaly: 333
6404 deg
Mean motion: 15
72962552 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 176
Checksum: 335
Coasting Arc #5 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2009/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4112163
26 A = 6727148
48 meter
Y = 3151433
53 meter E =
0013721
Z = -4298628
45 I = 51
95783
XDOT = -1416
854124 Wp = 67
49580
YDOT = 6674
218094 meter/sec RA = 77
94869 deg
ZDOT = 3551
722604 TA = 238
33171
MA = 238
46561
Ha = 194
565 n
mi
Hp = 183
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13491349
28 X = 4097500
24
Y = 10339348
85 feet Y = 3197336
61 meter
Z = -14103111
72 Z = -4278686
36
XDOT = -4648
471535 XDOT = -1508
635096
YDOT = 21897
040992 feet/sec YDOT = 6657
860453 meter/sec
ZDOT = 11652
633215 ZDOT = 3544
617126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15798994
09 X = 4815533
40
Y = -6442969
36 feet Y = -1963817
06 meter
Z = -14024846
95 Z = -4274773
35
XDOT = 15999
821024 XDOT = 4876
745448
YDOT = 14029
442599 feet/sec YDOT = 4276
174104 meter/sec
ZDOT = 11625
168179 ZDOT = 3543
351261
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 09142
50954720
00010596 00000-0 82463-4 0 9042
2 25544 51
6393 78
6311 0009468 29
5790 330
5906 15
72980116 1911
Satellite: ISS
Catalog Number: 25544
Epoch time: 09142
50954720 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 78
6311 deg
Eccentricity:
0009468
Arg of perigee: 29
5790 deg
Mean anomaly: 330
5906 deg
Mean motion: 15
72980116 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 191
Checksum: 313
Coasting Arc #6 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2009/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 470842
44 A = 6731402
55 meter
Y = -6081661
62 meter E =
0011041
Z = -2862515
88 I = 51
96639
XDOT = 5031
970352 Wp = 57
89305
YDOT = 2786
185139 meter/sec RA = 72
89126 deg
ZDOT = -5100
335952 TA = 154
74680
MA = 154
69278
Ha = 194
528 n
mi
Hp = 182
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1544758
65 X = 552719
53
Y = -19952958
08 feet Y = -6075938
19 meter
Z = -9391456
29 Z = -2860030
42
XDOT = 16509
089082 XDOT = 5025
217874
YDOT = 9141
027360 feet/sec YDOT = 2842
418518 meter/sec
ZDOT = -16733
385670 ZDOT = -5075
906064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16572969
58 X = -5051441
13
Y = -11225877
46 feet Y = -3421647
45 meter
Z = -9382037
16 Z = -2859644
93
XDOT = 15319
396840 XDOT = 4669
352157
YDOT = -8734
862714 feet/sec YDOT = -2662
386155 meter/sec
ZDOT = -16637
568061 ZDOT = -5071
130745
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 09143
52602702
00010596 00000-0 82463-4 0 9056
2 25544 51
6404 73
4185 0009501 33
5092 326
6670 15
73024916 2074
Satellite: ISS
Catalog Number: 25544
Epoch time: 09143
52602702 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 73
4185 deg
Eccentricity:
0009501
Arg of perigee: 33
5092 deg
Mean anomaly: 326
6670 deg
Mean motion: 15
73024916 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 207
Checksum: 280
Coasting Arc #7 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2009/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4591344
81 A = 6725764
79 meter
Y = -1688747
66 meter E =
0017345
Z = 4609558
49 I = 51
93764
XDOT = -390
909196 Wp = 50
07569
YDOT = -7096
354571 meter/sec RA = 67
74019 deg
ZDOT = -2970
949207 TA = 69
34832
MA = 69
16242
Ha = 194
648 n
mi
Hp = 182
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15063467
24 X = -4594512
57
Y = -5540510
69 feet Y = -1740109
24 meter
Z = 15123223
38 Z = 4587245
29
XDOT = -1282
510486 XDOT = -297
094877
YDOT = -23282
003185 feet/sec YDOT = -7100
200903 meter/sec
ZDOT = -9747
208685 ZDOT = -2972
621596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12106507
48 X = -3690063
48
Y = 10661889
53 feet Y = 3249743
93 meter
Z = 15035749
98 Z = 4582896
59
XDOT = -20260
508273 XDOT = -6175
402922
YDOT = -9165
317814 feet/sec YDOT = -2793
588870 meter/sec
ZDOT = -9754
110126 ZDOT = -2973
052767
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 09144
54248715
00010596 00000-0 82463-4 0 9060
2 25544 51
6405 68
2066 0009449 37
2571 322
9246 15
73043314 2238
Satellite: ISS
Catalog Number: 25544
Epoch time: 09144
54248715 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 68
2066 deg
Eccentricity:
0009449
Arg of perigee: 37
2571 deg
Mean anomaly: 322
9246 deg
Mean motion: 15
73043314 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 223
Checksum: 298
Coasting Arc #8 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2009/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1164599
44 A = 6732504
85 meter
Y = 6200372
87 meter E =
0022538
Z = 2314317
49 I = 51
94866
XDOT = -5345
525743 Wp = 59
79981
YDOT = -1042
830049 meter/sec RA = 62
67564 deg
ZDOT = 5455
773741 TA = 326
13534
MA = 326
27905
Ha = 194
592 n
mi
Hp = 182
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3820864
32 X = 1083936
57
Y = 20342430
68 feet Y = 6212944
66 meter
Z = 7592905
16 Z = 2319780
43
XDOT = -17537
814118 XDOT = -5359
970894
YDOT = -3421
358429 feet/sec YDOT = -1102
688629 meter/sec
ZDOT = 17899
520147 ZDOT = 5429
769507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19781788
57 X = 6029489
16
Y = 6063367
78 feet Y = 1848114
50 meter
Z = 7614598
53 Z = 2320929
63
XDOT = -10752
624684 XDOT = -3277
400004
YDOT = 12614
350946 feet/sec YDOT = 3844
854168 meter/sec
ZDOT = 17797
616323 ZDOT = 5424
713455
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 09145
55892740
00010596 00000-0 82463-4 0 9076
2 25544 51
6409 62
9940 0009463 40
8429 319
3441 15
73064582 2396
Satellite: ISS
Catalog Number: 25544
Epoch time: 09145
55892740 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 62
9940 deg
Eccentricity:
0009463
Arg of perigee: 40
8429 deg
Mean anomaly: 319
3441 deg
Mean motion: 15
73064582 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 239
Checksum: 322
Coasting Arc #9 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2009/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4634124
79 A = 6724502
26 meter
Y = 150074
25 meter E =
0018409
Z = -4884758
18 I = 51
90792
XDOT = 2244
842819 Wp = 79
79590
YDOT = 6965
002718 meter/sec RA = 57
52854 deg
ZDOT = 2354
303564 TA = 213
04757
MA = 213
16274
Ha = 194
586 n
mi
Hp = 182
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15203821
48 X = 4655831
66
Y = 492369
59 feet Y = 202018
05 meter
Z = -16026109
51 Z = -4862192
67
XDOT = 7364
969880 XDOT = 2155
355275
YDOT = 22851
058785 feet/sec YDOT = 6989
605055 meter/sec
ZDOT = 7724
093059 ZDOT = 2364
993071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7282838
87 X = 2219809
29
Y = -13460477
81 feet Y = -4102753
64 meter
Z = -15937709
89 Z = -4857813
97
XDOT = 22730
285338 XDOT = 6928
190971
YDOT = 3144
349708 feet/sec YDOT = 958
397791 meter/sec
ZDOT = 7766
289167 ZDOT = 2367
164938
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 09146
51182107
00010596 00000-0 82463-4 0 9083
2 25544 51
6416 58
1072 0009408 44
1084 316
0828 15
73104527 2544
Satellite: ISS
Catalog Number: 25544
Epoch time: 09146
51182107 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 58
1072 deg
Eccentricity:
0009408
Arg of perigee: 44
1084 deg
Mean anomaly: 316
0828 deg
Mean motion: 15
73104527 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 254
Checksum: 287
Coasting Arc #10 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2009/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2720211
71 A = 6733202
38 meter
Y = -5886012
13 meter E =
0011407
Z = -1825312
64 I = 51
92084
XDOT = 5140
957329 Wp = 87
06361
YDOT = -621
846693 meter/sec RA = 52
45409 deg
ZDOT = -5685
978950 TA = 113
07170
MA = 112
95140
Ha = 194
532 n
mi
Hp = 182
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8924579
11 X = -2645324
11
Y = -19311063
41 feet Y = -5916012
07 meter
Z = -5988558
52 Z = -1838346
61
XDOT = 16866
657905 XDOT = 5175
150333
YDOT = -2040
179439 feet/sec YDOT = -564
165293 meter/sec
ZDOT = -18654
786583 ZDOT = -5660
921193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21256620
73 X = -6479018
00
Y = -322406
27 feet Y = -98269
43 meter
Z = -6039887
81 Z = -1840957
80
XDOT = 5467
235491 XDOT = 1666
413378
YDOT = -14640
986865 feet/sec YDOT = -4462
572796 meter/sec
ZDOT = -18556
652311 ZDOT = -5656
067624
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 09147
52822241
00010596 00000-0 82463-4 0 9096
2 25544 51
6419 52
8940 0009275 47
9764 312
2187 15
73119978 2700
Satellite: ISS
Catalog Number: 25544
Epoch time: 09147
52822241 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 52
8940 deg
Eccentricity:
0009275
Arg of perigee: 47
9764 deg
Mean anomaly: 312
2187 deg
Mean motion: 15
73119978 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 270
Checksum: 326
Coasting Arc #11 (Orbit 285)
---------------------------------------
Vector Time (GMT): 2009/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4263137
92 A = 6723449
74 meter
Y = 1220542
77 meter E =
0014740
Z = 5046270
71 I = 51
86920
XDOT = -3957
699876 Wp = 51
90512
YDOT = -6364
866610 meter/sec RA = 47
31147 deg
ZDOT = -1791
601098 TA = 55
35553
MA = 55
21665
Ha = 194
569 n
mi
Hp = 182
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13986672
95 X = -4300983
20
Y = 4004405
42 feet Y = 1172657
47 meter
Z = 16556006
28 Z = 5025468
70
XDOT = -12984
579645 XDOT = -3877
529462
YDOT = -20882
108302 feet/sec YDOT = -6408
675379 meter/sec
ZDOT = -5877
956359 ZDOT = -1810
633849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2221529
46 X = -677122
18
Y = 14471250
83 feet Y = 4410837
25 meter
Z = 16474566
26 Z = 5021447
79
XDOT = -23322
647072 XDOT = -7108
742828
YDOT = 3243
200470 feet/sec YDOT = 988
527503 meter/sec
ZDOT = -5952
809597 ZDOT = -1814
416365
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 09148
54460235
00010596 00000-0 82463-4 0 9102
2 25544 51
6415 47
6809 0009283 50
7023 309
4962 15
73206304 2867
Satellite: ISS
Catalog Number: 25544
Epoch time: 09148
54460235 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 47
6809 deg
Eccentricity:
0009283
Arg of perigee: 50
7023 deg
Mean anomaly: 309
4962 deg
Mean motion: 15
73206304 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 286
Checksum: 299
Coasting Arc #12 (Orbit 301)
---------------------------------------
Vector Time (GMT): 2009/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4140938
89 A = 6733749
66 meter
Y = 5133778
21 meter E =
0023291
Z = 1298350
26 I = 51
88307
XDOT = -4507
830112 Wp = 57
19221
YDOT = 2134
105721 meter/sec RA = 42
22564 deg
ZDOT = 5875
532459 TA = 317
01874
MA = 317
20046
Ha = 194
543 n
mi
Hp = 182
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13585757
50 X = 4076917
21
Y = 16843104
35 feet Y = 5179726
47 meter
Z = 4259679
32 Z = 1318312
06
XDOT = -14789
468872 XDOT = -4559
901202
YDOT = 7001
659188 feet/sec YDOT = 2083
404604 meter/sec
ZDOT = 19276
681297 ZDOT = 5853
507283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20865133
40 X = 6359692
66
Y = -5677568
10 feet Y = -1730522
76 meter
Z = 4338117
98 Z = 1322258
36
XDOT = 32
052982 XDOT = 9
769749
YDOT = 14936
566152 feet/sec YDOT = 4552
665363 meter/sec
ZDOT = 19190
488018 ZDOT = 5849
260748
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 09149
56096558
00010596 00000-0 82463-4 0 9119
2 25544 51
6419 42
4674 0009343 54
5786 305
6248 15
73184104 3026
Satellite: ISS
Catalog Number: 25544
Epoch time: 09149
56096558 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 42
4674 deg
Eccentricity:
0009343
Arg of perigee: 54
5786 deg
Mean anomaly: 305
6248 deg
Mean motion: 15
73184104 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 302
Checksum: 315
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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