Date:
September 24th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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 164)
---------------------------------------
Vector Time (GMT): 2008/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4229537
26 A = 6726536
85 meter
Y = 1203800
29 meter E =
0010599
Z = 5081868
92 I = 51
36687
XDOT = -3692
988057 Wp = 105
78786
YDOT = 6592
315680 meter/sec RA = 308
42660 deg
ZDOT = 1506
556678 TA = 329
68577
MA = 329
74703
Ha = 195
387 n
mi
Hp = 184
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13876434
60 X = 4191075
04
Y = 3949476
03 feet Y = 1250882
28 meter
Z = 16672798
30 Z = 5102322
60
XDOT = -12116
102549 XDOT = -3773
748495
YDOT = 21628
332285 feet/sec YDOT = 6550
566981 meter/sec
ZDOT = 4942
771254 ZDOT = 1488
420092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12559382
26 X = -3828099
71
Y = -6911565
40 feet Y = -2106645
14 meter
Z = 16751960
54 Z = 5105997
57
XDOT = 16140
509154 XDOT = 4919
627190
YDOT = -17475
116286 feet/sec YDOT = -5326
415444 meter/sec
ZDOT = 4873
251610 ZDOT = 1485
367091
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 08252
55022161
00020000 00000-0 20000-3 0 9008
2 25544 51
6420 308
7468 0006392 92
0765 268
1130 15
71998112 1652
Satellite: ISS
Catalog Number: 25544
Epoch time: 08252
55022161 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 308
7468 deg
Eccentricity:
0006392
Arg of perigee: 92
0765 deg
Mean anomaly: 268
1130 deg
Mean motion: 15
71998112 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 165
Checksum: 272
Coasting Arc #2 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2008/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2138575
23 A = 6736292
99 meter
Y = -6085819
64 meter E =
0011937
Z = -1939344
74 I = 51
38188
XDOT = 5284
072388 Wp = 65
33370
YDOT = 85
560158 meter/sec RA = 303
25741 deg
ZDOT = 5590
262337 TA = 273
04347
MA = 273
18006
Ha = 195
558 n
mi
Hp = 184
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7016322
93 X = 2215889
85
Y = -19966599
86 feet Y = -6061472
54 meter
Z = -6362679
58 Z = -1928767
86
XDOT = 17336
195498 XDOT = 5255
566526
YDOT = 280
709179 feet/sec YDOT = 144
490245 meter/sec
ZDOT = 18340
755700 ZDOT = 5615
863032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11001438
64 X = -3353238
50
Y = 18093478
65 feet Y = 5514892
29 meter
Z = -6322338
73 Z = -1927048
84
XDOT = -15486
849221 XDOT = -4720
391643
YDOT = -3009
940696 feet/sec YDOT = -917
429924 meter/sec
ZDOT = 18439
717092 ZDOT = 5620
425770
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 08253
50378452
00020000 00000-0 20000-3 0 9012
2 25544 51
6415 303
8646 0006475 94
2900 265
9002 15
71987038 1802
Satellite: ISS
Catalog Number: 25544
Epoch time: 08253
50378452 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 303
8646 deg
Eccentricity:
0006475
Arg of perigee: 94
2900 deg
Mean anomaly: 265
9002 deg
Mean motion: 15
71987038 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 180
Checksum: 286
Coasting Arc #3 (Orbit 195)
---------------------------------------
Vector Time (GMT): 2008/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4776130
43 A = 6728481
50 meter
Y = 1070341
50 meter E =
0016914
Z = -4632521
91 I = 51
34125
XDOT = 1180
998121 Wp = 80
72955
YDOT = -7038
096462 meter/sec RA = 298
15615 deg
ZDOT = -2849
939791 TA = 160
94697
MA = 160
88362
Ha = 195
545 n
mi
Hp = 184
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15669719
27 X = -4765240
38
Y = 3511619
08 feet Y = 1016992
95 meter
Z = -15198562
71 Z = -4655697
76
XDOT = 3874
665752 XDOT = 1273
455880
YDOT = -23090
867659 feet/sec YDOT = -7024
372900 meter/sec
ZDOT = -9350
196164 ZDOT = -2843
977966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15964984
59 X = 4866127
30
Y = -512500
21 feet Y = -156210
06 meter
Z = -15288050
55 Z = -4659797
81
XDOT = -8246
125327 XDOT = -2513
419000
YDOT = 20772
910056 feet/sec YDOT = 6331
582985 meter/sec
ZDOT = -9327
786484 ZDOT = -2843
109320
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 08254
52090736
00020000 00000-0 20000-3 0 9022
2 25544 51
6420 298
6563 0006579 98
3722 261
8186 15
72001393 1966
Satellite: ISS
Catalog Number: 25544
Epoch time: 08254
52090736 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 298
6563 deg
Eccentricity:
0006579
Arg of perigee: 98
3722 deg
Mean anomaly: 261
8186 deg
Mean motion: 15
72001393 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 196
Checksum: 300
Coasting Arc #4 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2008/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 79257
69 A = 6733757
45 meter
Y = 6006957
28 meter E =
0019760
Z = 3021980
46 I = 51
34609
XDOT = -5353
368807 Wp = 97
42570
YDOT = 2556
017251 meter/sec RA = 292
96887 deg
ZDOT = -4915
412873 TA = 47
44366
MA = 47
27703
Ha = 195
452 n
mi
Hp = 184
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 260031
80 X = -2599
08
Y = 19707865
10 feet Y = 6007385
96 meter
Z = 9914634
06 Z = 3022166
55
XDOT = -17563
545954 XDOT = -5357
674731
YDOT = 8385
883369 feet/sec YDOT = 2496
128631 meter/sec
ZDOT = -16126
682655 ZDOT = -4941
429836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3179802
99 X = 969203
95
Y = -19450738
24 feet Y = -5928585
02 meter
Z = 9915904
74 Z = 3022367
76
XDOT = 17231
902213 XDOT = 5252
283795
YDOT = -5497
073050 feet/sec YDOT = -1675
507866 meter/sec
ZDOT = -16227
017780 ZDOT = -4945
995019
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 08255
53801787
00020000 00000-0 20000-3 0 9031
2 25544 51
6413 293
4486 0006567 100
5501 259
6401 15
72054904 2123
Satellite: ISS
Catalog Number: 25544
Epoch time: 08255
53801787 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 293
4486 deg
Eccentricity:
0006567
Arg of perigee: 100
5501 deg
Mean anomaly: 259
6401 deg
Mean motion: 15
72054904 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 212
Checksum: 276
Coasting Arc #5 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2008/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4348210
45 A = 6731114
99 meter
Y = -3346016
06 meter E =
0017916
Z = 3886978
51 I = 51
32620
XDOT = 1321
053348 Wp = 101
33698
YDOT = 6427
350979 meter/sec RA = 287
87684 deg
ZDOT = 4035
838775 TA = 306
43269
MA = 306
59773
Ha = 195
472 n
mi
Hp = 184
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14265782
32 X = 4366420
89
Y = -10977742
97 feet Y = -3297289
88 meter
Z = 12752554
16 Z = 3908146
31
XDOT = 4334
164529 XDOT = 1229
478276
YDOT = 21087
109511 feet/sec YDOT = 6441
611906 meter/sec
ZDOT = 13240
940862 ZDOT = 4042
033695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15718471
88 X = -4790990
23
Y = 8652592
22 feet Y = 2637310
11 meter
Z = 12834068
45 Z = 3911824
06
XDOT = -317
449559 XDOT = -96
758626
YDOT = -20345
673568 feet/sec YDOT = -6201
361304 meter/sec
ZDOT = 13265
488695 ZDOT = 4043
320954
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 08256
55511954
00020000 00000-0 20000-3 0 9049
2 25544 51
6406 288
2405 0006769 103
9801 256
2114 15
72041195 2281
Satellite: ISS
Catalog Number: 25544
Epoch time: 08256
55511954 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 288
2405 deg
Eccentricity:
0006769
Arg of perigee: 103
9801 deg
Mean anomaly: 256
2114 deg
Mean motion: 15
72041195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 228
Checksum: 282
Coasting Arc #6 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2008/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2125499
56 A = 6730832
80 meter
Y = -5017157
40 meter E =
0013668
Z = -3965837
66 I = 51
31866
XDOT = 4352
572848 Wp = 107
29558
YDOT = -4956
417790 meter/sec RA = 282
68206 deg
ZDOT = 3944
770833 TA = 203
78080
MA = 203
84402
Ha = 195
456 n
mi
Hp = 184
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6973423
75 X = -2049973
72
Y = -16460490
16 feet Y = -5040503
94 meter
Z = -13011278
43 Z = -3975979
49
XDOT = 14280
094645 XDOT = 4388
509953
YDOT = -16261
213223 feet/sec YDOT = -4907
543613 meter/sec
ZDOT = 12942
161525 ZDOT = 3966
003115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4569640
21 X = 1392826
33
Y = 17252842
02 feet Y = 5258666
25 meter
Z = -13050960
58 Z = -3977932
78
XDOT = -15048
882916 XDOT = -4586
899513
YDOT = 13819
924489 feet/sec YDOT = 4212
312984 meter/sec
ZDOT = 13023
767126 ZDOT = 3969
644220
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 08257
50864089
00020000 00000-0 20000-3 0 9056
2 25544 51
6415 283
3580 0006677 106
9715 253
2179 15
72067095 2438
Satellite: ISS
Catalog Number: 25544
Epoch time: 08257
50864089 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 283
3580 deg
Eccentricity:
0006677
Arg of perigee: 106
9715 deg
Mean anomaly: 253
2179 deg
Mean motion: 15
72067095 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 243
Checksum: 306
Coasting Arc #7 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2008/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3102342
83 A = 6733724
89 meter
Y = 5178749
28 meter E =
0011173
Z = -2987307
26 I = 51
32262
XDOT = -3347
960820 Wp = 110
31540
YDOT = -4847
410481 meter/sec RA = 277
58779 deg
ZDOT = -4945
291860 TA = 104
30325
MA = 104
17916
Ha = 195
378 n
mi
Hp = 184
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10178290
13 X = -3145510
10
Y = 16990647
24 feet Y = 5143815
47 meter
Z = -9800876
85 Z = -3002483
71
XDOT = -10984
123425 XDOT = -3269
484189
YDOT = -15903
577694 feet/sec YDOT = -4884
410950 meter/sec
ZDOT = -16224
710827 ZDOT = -4961
365176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12094971
01 X = 3686547
16
Y = -15647613
39 feet Y = -4769392
56 meter
Z = -9859043
66 Z = -3005036
51
XDOT = 7754
938533 XDOT = 2363
705265
YDOT = 16217
756212 feet/sec YDOT = 4943
172093 meter/sec
ZDOT = -16287
313201 ZDOT = -4964
373064
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 08258
52571970
00020000 00000-0 20000-3 0 9064
2 25544 51
6407 278
1491 0006650 111
1017 249
0857 15
72081046 2591
Satellite: ISS
Catalog Number: 25544
Epoch time: 08258
52571970 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 278
1491 deg
Eccentricity:
0006650
Arg of perigee: 111
1017 deg
Mean anomaly: 249
0857 deg
Mean motion: 15
72081046 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 259
Checksum: 287
Coasting Arc #8 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2008/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3578399
19 A = 6728107
14 meter
Y = 3298234
42 meter E =
0013262
Z = 4634892
17 I = 51
30019
XDOT = -2535
088769 Wp = 85
99874
YDOT = 6711
819050 meter/sec RA = 272
39723 deg
ZDOT = -2811
140011 TA = 31
91030
MA = 31
83004
Ha = 195
225 n
mi
Hp = 184
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11740154
83 X = 3518736
31
Y = 10820979
07 feet Y = 3337917
00 meter
Z = 15206339
14 Z = 4652130
85
XDOT = -8317
220370 XDOT = -2596
296941
YDOT = 22020
403708 feet/sec YDOT = 6683
127723 meter/sec
ZDOT = -9222
900299 ZDOT = -2823
604827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10471938
47 X = -3191846
85
Y = -11967555
26 feet Y = -3647710
84 meter
Z = 15273300
21 Z = 4655301
90
XDOT = 9623
459289 XDOT = 2933
230391
YDOT = -20284
563492 feet/sec YDOT = -6182
734952 meter/sec
ZDOT = -9270
428528 ZDOT = -2825
626615
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 08259
54278687
00020000 00000-0 20000-3 0 9077
2 25544 51
6394 272
9403 0006639 114
0719 246
1138 15
72118909 2756
Satellite: ISS
Catalog Number: 25544
Epoch time: 08259
54278687 = yrday
fracday
Element set: 907
Inclination: 51
6394 deg
RA of node: 272
9403 deg
Eccentricity:
0006639
Arg of perigee: 114
0719 deg
Mean anomaly: 246
1138 deg
Mean motion: 15
72118909 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 275
Checksum: 315
Coasting Arc #9 (Orbit 290)
---------------------------------------
Vector Time (GMT): 2008/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1216067
68 A = 6735959
38 meter
Y = -6342880
55 meter E =
0018982
Z = 1892076
19 I = 51
32672
XDOT = 4612
129899 Wp = 82
66965
YDOT = 2569
616051 meter/sec RA = 267
29195 deg
ZDOT = 5604
263782 TA = 298
43739
MA = 298
62853
Ha = 195
263 n
mi
Hp = 184
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3989723
36 X = 1277712
96
Y = -20809975
55 feet Y = -6328936
92 meter
Z = 6207599
06 Z = 1898134
23
XDOT = 15131
659773 XDOT = 4555
828499
YDOT = 8430
498856 feet/sec YDOT = 2620
877274 meter/sec
ZDOT = 18386
692197 ZDOT = 5626
532715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5734049
75 X = -1747738
36
Y = 20391423
36 feet Y = 6215305
84 meter
Z = 6230392
25 Z = 1899023
56
XDOT = -12756
106031 XDOT = -3888
061118
YDOT = -9276
865216 feet/sec YDOT = -2827
588518 meter/sec
ZDOT = 18473
028586 ZDOT = 5630
579113
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 08260
55984314
00020000 00000-0 20000-3 0 9082
2 25544 51
6394 267
7320 0006596 118
0186 242
1644 15
72126803 2918
Satellite: ISS
Catalog Number: 25544
Epoch time: 08260
55984314 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 267
7320 deg
Eccentricity:
0006596
Arg of perigee: 118
0186 deg
Mean anomaly: 242
1644 deg
Mean motion: 15
72126803 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 291
Checksum: 292
Coasting Arc #10 (Orbit 305)
---------------------------------------
Vector Time (GMT): 2008/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4272152
89 A = 6726282
47 meter
Y = -1144857
34 meter E =
0020052
Z = -5085492
31 I = 51
29660
XDOT = 194
965244 Wp = 107
94974
YDOT = -7526
364120 meter/sec RA = 262
11629 deg
ZDOT = 1529
438895 TA = 176
83599
MA = 176
82329
Ha = 195
235 n
mi
Hp = 184
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14016249
63 X = -4234328
63
Y = -3756093
65 feet Y = -1192419
94 meter
Z = -16684686
06 Z = -5106154
76
XDOT = 639
649751 XDOT = 271
681924
YDOT = -24692
795669 feet/sec YDOT = -7523
754841 meter/sec
ZDOT = 5017
844143 ZDOT = 1530
572987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13627688
11 X = 4153719
33
Y = 4708938
21 feet Y = 1435284
37 meter
Z = -16764672
98 Z = -5109872
32
XDOT = -1972
112640 XDOT = -601
099933
YDOT = 23597
822041 feet/sec YDOT = 7192
616158 meter/sec
ZDOT = 5021
484276 ZDOT = 1530
548407
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 08261
51332293
00020000 00000-0 20000-3 0 9093
2 25544 51
6394 262
8483 0006507 121
3286 238
8514 15
72108877 3060
Satellite: ISS
Catalog Number: 25544
Epoch time: 08261
51332293 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 262
8483 deg
Eccentricity:
0006507
Arg of perigee: 121
3286 deg
Mean anomaly: 238
8514 deg
Mean motion: 15
72108877 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 306
Checksum: 295
Coasting Arc #11 (Orbit 321)
---------------------------------------
Vector Time (GMT): 2008/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 892110
69 A = 6737200
43 meter
Y = 6625656
26 meter E =
0016883
Z = -777701
22 I = 51
33835
XDOT = -4890
023735 Wp = 134
35227
YDOT = -28
946960 meter/sec RA = 256
99140 deg
ZDOT = -5947
123663 TA = 54
15749
MA = 54
00078
Ha = 195
166 n
mi
Hp = 184
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2926872
33 X = 821733
23
Y = 21737717
38 feet Y = 6635238
81 meter
Z = -2551513
18 Z = -773538
58
XDOT = -16043
384958 XDOT = -4860
446050
YDOT = -94
970340 feet/sec YDOT = -83
464972 meter/sec
ZDOT = -19511
560573 ZDOT = -5970
807962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1808833
89 X = -551332
57
Y = -21861112
41 feet Y = -6663267
06 meter
Z = -2534766
66 Z = -772596
88
XDOT = 14310
819705 XDOT = 4361
937846
YDOT = 1053
963573 feet/sec YDOT = 321
248097 meter/sec
ZDOT = -19603
121074 ZDOT = -5975
031303
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 08262
53035667
00020000 00000-0 20000-3 0 9103
2 25544 51
6387 257
6388 0006590 124
3669 235
8117 15
72146195 3227
Satellite: ISS
Catalog Number: 25544
Epoch time: 08262
53035667 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 257
6388 deg
Eccentricity:
0006590
Arg of perigee: 124
3669 deg
Mean anomaly: 235
8117 deg
Mean motion: 15
72146195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 322
Checksum: 302
Coasting Arc #12 (Orbit 337)
---------------------------------------
Vector Time (GMT): 2008/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 609794
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060411
70 A = 6725338
38 meter
Y = -1093079
48 meter E =
0008272
Z = 5242140
91 I = 51
30607
XDOT = 2243
980236 Wp = 115
88727
YDOT = 7367
539309 meter/sec RA = 251
83781 deg
ZDOT = -205
173981 TA = 336
04883
MA = 336
08729
Ha = 194
931 n
mi
Hp = 184
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13321560
70 X = 4046867
09
Y = -3586218
78 feet Y = -1047749
21 meter
Z = 17198625
04 Z = 5261833
87
XDOT = 7362
139883 XDOT = 2162
425162
YDOT = 24171
716892 feet/sec YDOT = 7392
176787 meter/sec
ZDOT = -673
142981 ZDOT = -194
470830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13339427
10 X = -4065857
38
Y = 3124711
21 feet Y = 952411
98 meter
Z = 17274649
42 Z = 5265313
14
XDOT = -6293
971898 XDOT = -1918
402634
YDOT = -23440
254890 feet/sec YDOT = -7144
589690 meter/sec
ZDOT = -631
037850 ZDOT = -192
340337
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 08263
54737767
00020000 00000-0 20000-3 0 9116
2 25544 51
6383 252
4298 0006433 128
4129 231
7612 15
72165576 3384
Satellite: ISS
Catalog Number: 25544
Epoch time: 08263
54737767 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 252
4298 deg
Eccentricity:
0006433
Arg of perigee: 128
4129 deg
Mean anomaly: 231
7612 deg
Mean motion: 15
72165576 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 338
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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