Date:
November 29th 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 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1403)
---------------------------------------
Vector Time (GMT): 2008/331/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3303362
32 A = 6730298
49 meter
Y = -3725033
33 meter E =
0011646
Z = 4517668
22 I = 51
30287
XDOT = 3023
680831 Wp = 78
75941
YDOT = 6393
171706 meter/sec RA = 264
94115 deg
ZDOT = 3056
116481 TA = 340
67028
MA = 340
71441
Ha = 195
764 n
mi
Hp = 186
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10837802
90 X = 3322824
11
Y = -12221237
96 feet Y = -3687984
85 meter
Z = 14821746
11 Z = 4533763
31
XDOT = 9920
212699 XDOT = 2937
120137
YDOT = 20974
972790 feet/sec YDOT = 6426
499967 meter/sec
ZDOT = 10026
628875 ZDOT = 3070
596303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15022245
82 X = -4578780
53
Y = 6269222
93 feet Y = 1910859
15 meter
Z = 14883875
87 Z = 4536605
37
XDOT = 789
952915 XDOT = 240
777648
YDOT = -22080
206955 feet/sec YDOT = -6730
047080 meter/sec
ZDOT = 10083
255992 ZDOT = 3073
376426
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 08331
30093300
00020000 00000-0 20000-3 0 9002
2 25544 51
6407 265
4238 0006761 31
4027 328
7537 15
71520441 14046
Satellite: ISS
Catalog Number: 25544
Epoch time: 08331
30093300 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 265
4238 deg
Eccentricity:
0006761
Arg of perigee: 31
4027 deg
Mean anomaly: 328
7537 deg
Mean motion: 15
71520441 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1404
Checksum: 250
Coasting Arc #2 (Orbit 1418)
---------------------------------------
Vector Time (GMT): 2008/332/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3551395
24 A = 6734258
22 meter
Y = -4652632
69 meter E =
0010372
Z = -3331726
19 I = 51
32178
XDOT = 2796
842124 Wp = 56
57219
YDOT = -5453
005181 meter/sec RA = 259
75359 deg
ZDOT = 4649
721654 TA = 264
10594
MA = 264
22418
Ha = 195
819 n
mi
Hp = 185
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11651559
20 X = -3482919
45
Y = -15264542
93 feet Y = -4691963
18 meter
Z = -10930860
21 Z = -3348813
53
XDOT = 9175
991222 XDOT = 2835
022554
YDOT = -17890
436946 feet/sec YDOT = -5421
516340 meter/sec
ZDOT = 15254
992304 ZDOT = 4663
401176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4045175
41 X = 1232969
47
Y = 18733418
56 feet Y = 5709945
98 meter
Z = -10997472
11 Z = -3352029
50
XDOT = -14435
707698 XDOT = -4400
003706
YDOT = 12072
796567 feet/sec YDOT = 3679
788394 meter/sec
ZDOT = 15307
629817 ZDOT = 4665
765568
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 08332
25477313
00020000 00000-0 20000-3 0 9018
2 25544 51
6420 260
5441 0006782 34
5410 325
6191 15
71558611 14194
Satellite: ISS
Catalog Number: 25544
Epoch time: 08332
25477313 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 260
5441 deg
Eccentricity:
0006782
Arg of perigee: 34
5410 deg
Mean anomaly: 325
6191 deg
Mean motion: 15
71558611 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1419
Checksum: 264
Coasting Arc #3 (Orbit 1434)
---------------------------------------
Vector Time (GMT): 2008/333/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1416889
46 A = 6733654
09 meter
Y = 5556799
53 meter E =
0011107
Z = -3543114
45 I = 51
32529
XDOT = -4793
641454 Wp = 57
69441
YDOT = -4049
160722 meter/sec RA = 254
66504 deg
ZDOT = -4437
786989 TA = 164
62465
MA = 164
59088
Ha = 195
895 n
mi
Hp = 185
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4648587
48 X = -1461708
99
Y = 18230969
58 feet Y = 5540704
91 meter
Z = -11624391
25 Z = -3550106
01
XDOT = -15727
170126 XDOT = -4726
448342
YDOT = -13284
648038 feet/sec YDOT = -4102
389717 meter/sec
ZDOT = -14559
668598 ZDOT = -4460
912348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11609624
41 X = 3538613
52
Y = -14784209
98 feet Y = -4506227
20 meter
Z = -11651087
74 Z = -3551251
54
XDOT = 7798
252901 XDOT = 2376
907484
YDOT = 17657
679840 feet/sec YDOT = 5382
060815 meter/sec
ZDOT = -14649
658389 ZDOT = -4465
215877
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 08333
27218828
00020000 00000-0 20000-3 0 9026
2 25544 51
6411 255
3378 0006739 37
8094 322
3540 15
71566750 14354
Satellite: ISS
Catalog Number: 25544
Epoch time: 08333
27218828 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 255
3378 deg
Eccentricity:
0006739
Arg of perigee: 37
8094 deg
Mean anomaly: 322
3540 deg
Mean motion: 15
71566750 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1435
Checksum: 292
Coasting Arc #4 (Orbit 1450)
---------------------------------------
Vector Time (GMT): 2008/334/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4582647
03 A = 6730649
51 meter
Y = 2293445
29 meter E =
0015683
Z = 4356982
69 I = 51
32356
XDOT = -267
995673 Wp = 57
85853
YDOT = 6929
153226 meter/sec RA = 249
47564 deg
ZDOT = -3348
487117 TA = 66
07201
MA = 65
90781
Ha = 195
808 n
mi
Hp = 185
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15034931
21 X = 4535494
92
Y = 7524426
81 feet Y = 2344426
86 meter
Z = 14294562
65 Z = 4379131
40
XDOT = -879
250896 XDOT = -329
192024
YDOT = 22733
442342 feet/sec YDOT = 6925
814641 meter/sec
ZDOT = -10985
850121 ZDOT = -3349
936753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10812949
91 X = -3295787
13
Y = -12778024
76 feet Y = -3894741
95 meter
Z = 14380642
34 Z = 4383219
79
XDOT = 8719
579523 XDOT = 2657
727839
YDOT = -19810
573617 feet/sec YDOT = -6038
262838 meter/sec
ZDOT = -10990
948539 ZDOT = -3350
041115
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 08334
28958831
00020000 00000-0 20000-3 0 9034
2 25544 51
6400 250
1316 0006791 41
0337 319
1335 15
71610249 14519
Satellite: ISS
Catalog Number: 25544
Epoch time: 08334
28958831 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 250
1316 deg
Eccentricity:
0006791
Arg of perigee: 41
0337 deg
Mean anomaly: 319
1335 deg
Mean motion: 15
71610249 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1451
Checksum: 265
Coasting Arc #5 (Orbit 1466)
---------------------------------------
Vector Time (GMT): 2008/335/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1013571
57 A = 6736782
83 meter
Y = -6259831
67 meter E =
0020216
Z = 2242009
32 I = 51
35529
XDOT = 5346
485464 Wp = 63
16311
YDOT = 1092
466165 meter/sec RA = 244
38186 deg
ZDOT = 5438
627252 TA = 322
10060
MA = 322
24273
Ha = 195
880 n
mi
Hp = 185
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3325366
04 X = -954389
22
Y = -20537505
48 feet Y = -6270835
42 meter
Z = 7355673
63 Z = 2237228
19
XDOT = 17540
962808 XDOT = 5307
451701
YDOT = 3584
206579 feet/sec YDOT = 1152
034642 meter/sec
ZDOT = 17843
265264 ZDOT = 5464
506213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4593444
53 X = -1400081
89
Y = 20298447
22 feet Y = 6186966
71 meter
Z = 7336650
01 Z = 2236210
92
XDOT = -13334
576125 XDOT = -4064
378803
YDOT = -9537
186613 feet/sec YDOT = -2906
934480 meter/sec
ZDOT = 17943
733809 ZDOT = 5469
250065
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 08335
30697429
00020000 00000-0 20000-3 0 9042
2 25544 51
6396 244
9263 0006721 44
7128 315
4575 15
71626117 14679
Satellite: ISS
Catalog Number: 25544
Epoch time: 08335
30697429 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 244
9263 deg
Eccentricity:
0006721
Arg of perigee: 44
7128 deg
Mean anomaly: 315
4575 deg
Mean motion: 15
71626117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1467
Checksum: 303
Coasting Arc #6 (Orbit 1481)
---------------------------------------
Vector Time (GMT): 2008/336/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466531
39 A = 6727939
73 meter
Y = 370518
23 meter E =
0018157
Z = -5032984
69 I = 51
33868
XDOT = -2554
364761 Wp = 85
40304
YDOT = -7031
151318 meter/sec RA = 239
20910 deg
ZDOT = 1756
138601 TA = 201
57718
MA = 201
65380
Ha = 195
961 n
mi
Hp = 185
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14653974
39 X = -4445893
02
Y = 1215610
98 feet Y = 320686
97 meter
Z = -16512416
97 Z = -5054633
17
XDOT = -8380
461813 XDOT = -2484
082533
YDOT = -23068
081753 feet/sec YDOT = -7059
322972 meter/sec
ZDOT = 5761
609583 ZDOT = 1743
899114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14021886
68 X = 4273871
06
Y = 4101670
15 feet Y = 1250189
06 meter
Z = -16596372
66 Z = -5058574
39
XDOT = -146
321511 XDOT = -44
598797
YDOT = 23527
889413 feet/sec YDOT = 7171
300693 meter/sec
ZDOT = 5713
584551 ZDOT = 1741
500571
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 08336
26076114
00020000 00000-0 20000-3 0 9051
2 25544 51
6390 240
0453 0006770 47
5891 312
5843 15
71605669 14825
Satellite: ISS
Catalog Number: 25544
Epoch time: 08336
26076114 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 240
0453 deg
Eccentricity:
0006770
Arg of perigee: 47
5891 deg
Mean anomaly: 312
5843 deg
Mean motion: 15
71605669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1482
Checksum: 288
Coasting Arc #7 (Orbit 1497)
---------------------------------------
Vector Time (GMT): 2008/337/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3371801
86 A = 6738579
37 meter
Y = 5774786
26 meter E =
0012517
Z = -820992
63 I = 51
39021
XDOT = -4539
252374 Wp = 107
61423
YDOT = 1817
210705 meter/sec RA = 234
09359 deg
ZDOT = -5938
636089 TA = 81
35739
MA = 81
21561
Ha = 196
001 n
mi
Hp = 185
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11062342
06 X = 3310964
92
Y = 18946149
15 feet Y = 5812151
65 meter
Z = -2693545
39 Z = -804759
33
XDOT = -14892
560282 XDOT = -4530
386279
YDOT = 5961
977380 feet/sec YDOT = 1766
500473 meter/sec
ZDOT = -19483
714204 ZDOT = -5960
666213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3894996
40 X = -1187194
90
Y = -21598580
67 feet Y = -6583247
39 meter
Z = -2630110
72 Z = -801657
75
XDOT = 14353
882816 XDOT = 4375
063482
YDOT = -237
504034 feet/sec YDOT = -72
391230 meter/sec
ZDOT = -19569
045795 ZDOT = -5964
645158
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 08337
27811962
00020000 00000-0 20000-3 0 9062
2 25544 51
6382 234
8381 0006878 51
4999 308
6779 15
71653835 14988
Satellite: ISS
Catalog Number: 25544
Epoch time: 08337
27811962 = yrday
fracday
Element set: 906
Inclination: 51
6382 deg
RA of node: 234
8381 deg
Eccentricity:
0006878
Arg of perigee: 51
4999 deg
Mean anomaly: 308
6779 deg
Mean motion: 15
71653835 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1498
Checksum: 342
Coasting Arc #8 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2008/338/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3218248
86 A = 6726754
03 meter
Y = -2693713
99 meter E =
0008857
Z = 5250244
23 I = 51
36807
XDOT = 5016
174296 Wp = 62
97226
YDOT = 5846
534252 meter/sec RA = 228
94887 deg
ZDOT = -71
060526 TA = 27
72790
MA = 27
68070
Ha = 195
868 n
mi
Hp = 185
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10558559
24 X = 3222626
29
Y = -8837644
32 feet Y = -2657701
76 meter
Z = 17225210
72 Z = 5265888
94
XDOT = 16457
264752 XDOT = 4950
769783
YDOT = 19181
542821 feet/sec YDOT = 5902
262326 meter/sec
ZDOT = -233
138209 ZDOT = -46
850000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12775894
93 X = -3894092
77
Y = 4927070
78 feet Y = 1501771
17 meter
Z = 17285702
09 Z = 5268682
00
XDOT = -8913
886849 XDOT = -2716
952712
YDOT = -22580
416906 feet/sec YDOT = -6882
511073 meter/sec
ZDOT = -138
731563 ZDOT = -42
285381
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 08338
29546384
00020000 00000-0 20000-3 0 9079
2 25544 51
6374 229
6313 0006782 54
2941 305
8851 15
71666181 15145
Satellite: ISS
Catalog Number: 25544
Epoch time: 08338
29546384 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 229
6313 deg
Eccentricity:
0006782
Arg of perigee: 54
2941 deg
Mean anomaly: 305
8851 deg
Mean motion: 15
71666181 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1514
Checksum: 306
Coasting Arc #9 (Orbit 1528)
---------------------------------------
Vector Time (GMT): 2008/339/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5200158
69 A = 6738448
51 meter
Y = -4217834
07 meter E =
0017174
Z = -697087
84 I = 51
42800
XDOT = 2566
086573 Wp = 47
66338
YDOT = -4132
586142 meter/sec RA = 223
80799 deg
ZDOT = 5967
093125 TA = 304
72558
MA = 304
88721
Ha = 195
921 n
mi
Hp = 185
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17060888
09 X = -5149221
34
Y = -13838038
28 feet Y = -4275700
38 meter
Z = -2287033
60 Z = -722227
07
XDOT = 8418
919202 XDOT = 2583
119825
YDOT = -13558
353483 feet/sec YDOT = -4103
795984 meter/sec
ZDOT = 19577
077183 ZDOT = 5979
600269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11898072
57 X = 3626532
52
Y = 18453826
63 feet Y = 5624726
36 meter
Z = -2384927
77 Z = -726925
98
XDOT = -10765
459446 XDOT = -3281
312039
YDOT = 9434
706294 feet/sec YDOT = 2875
698478 meter/sec
ZDOT = 19625
279352 ZDOT = 5981
785146
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 08339
24921139
00020000 00000-0 20000-3 0 9081
2 25544 51
6372 224
7507 0006836 59
1971 300
9863 15
71717499 15295
Satellite: ISS
Catalog Number: 25544
Epoch time: 08339
24921139 = yrday
fracday
Element set: 908
Inclination: 51
6372 deg
RA of node: 224
7507 deg
Eccentricity:
0006836
Arg of perigee: 59
1971 deg
Mean anomaly: 300
9863 deg
Mean motion: 15
71717499 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1529
Checksum: 318
Coasting Arc #10 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2008/340/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1130118
74 A = 6727564
32 meter
Y = 4286591
13 meter E =
0020251
Z = -5078529
74 I = 51
41349
XDOT = -6577
138336 Wp = 72
44146
YDOT = -3631
528833 meter/sec RA = 218
69376 deg
ZDOT = -1600
876049 TA = 182
09173
MA = 182
10021
Ha = 195
999 n
mi
Hp = 184
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3707738
65 X = -1153297
29
Y = 14063619
19 feet Y = 4273824
28 meter
Z = -16661842
97 Z = -5084075
88
XDOT = -21578
537848 XDOT = -6528
264316
YDOT = -11914
464676 feet/sec YDOT = -3704
804809 meter/sec
ZDOT = -5252
218008 ZDOT = -1632
709659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7595018
76 X = 2314961
72
Y = -12375068
99 feet Y = -3771921
03 meter
Z = -16683017
69 Z = -5084983
79
XDOT = 16178
826900 XDOT = 4931
306439
YDOT = 17180
398343 feet/sec YDOT = 5236
585415 meter/sec
ZDOT = -5376
056004 ZDOT = -1638
621870
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 08340
26652933
00020000 00000-0 20000-3 0 9099
2 25544 51
6376 219
5427 0006818 61
2062 298
9784 15
71700466 15459
Satellite: ISS
Catalog Number: 25544
Epoch time: 08340
26652933 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 219
5427 deg
Eccentricity:
0006818
Arg of perigee: 61
2062 deg
Mean anomaly: 298
9784 deg
Mean motion: 15
71700466 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1545
Checksum: 310
Coasting Arc #11 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2008/341/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6069015
51 A = 6736685
68 meter
Y = 2036240
31 meter E =
0019375
Z = 2078125
58 I = 51
46863
XDOT = 110
936606 Wp = 95
61328
YDOT = 5356
115520 meter/sec RA = 213
52920 deg
ZDOT = -5529
872341 TA = 61
13884
MA = 60
94454
Ha = 195
917 n
mi
Hp = 184
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19911468
20 X = 6035699
58
Y = 6680578
45 feet Y = 2103921
14 meter
Z = 6817997
31 Z = 2107528
45
XDOT = 363
965244 XDOT = 77
898870
YDOT = 17572
557479 feet/sec YDOT = 5357
171720 meter/sec
ZDOT = -18142
625791 ZDOT = -5529
413299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17229615
32 X = -5251586
75
Y = -11944271
18 feet Y = -3640613
86 meter
Z = 6932281
27 Z = 2112959
33
XDOT = 3566
873079 XDOT = 1087
182914
YDOT = -15752
806523 feet/sec YDOT = -4801
455428 meter/sec
ZDOT = -18140
404269 ZDOT = -5529
195221
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 08341
28383334
00020000 00000-0 20000-3 0 9100
2 25544 51
6377 214
3358 0006803 63
6119 296
5741 15
71740668 15612
Satellite: ISS
Catalog Number: 25544
Epoch time: 08341
28383334 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 214
3358 deg
Eccentricity:
0006803
Arg of perigee: 63
6119 deg
Mean anomaly: 296
5741 deg
Mean motion: 15
71740668 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1561
Checksum: 294
Coasting Arc #12 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2008/342/05:56:50
867
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1375965
47 A = 6729740
47 meter
Y = -4810282
59 meter E =
0014383
Z = 4488995
58 I = 51
47141
XDOT = 6975
534635 Wp = 93
98692
YDOT = 939
282435 meter/sec RA = 208
44173 deg
ZDOT = 3135
052183 TA = 324
62594
MA = 324
72127
Ha = 195
855 n
mi
Hp = 184
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4514322
39 X = -1343880
93
Y = -15781767
01 feet Y = -4825490
32 meter
Z = 14727675
79 Z = 4482388
65
XDOT = 22885
612321 XDOT = 6949
283208
YDOT = 3081
635286 feet/sec YDOT = 1017
139919 meter/sec
ZDOT = 10285
604274 ZDOT = 3168
876206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 310638
65 X = 94682
66
Y = 16435118
88 feet Y = 5009424
24 meter
Z = 14701635
35 Z = 4481058
45
XDOT = -20026
757878 XDOT = -6104
155801
YDOT = -8967
929752 feet/sec YDOT = -2733
424989 meter/sec
ZDOT = 10416
966258 ZDOT = 3175
091316
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 08342
30112312
00020000 00000-0 20000-3 0 9111
2 25544 51
6384 209
1296 0006608 67
7833 292
4030 15
71791654 15778
Satellite: ISS
Catalog Number: 25544
Epoch time: 08342
30112312 = yrday
fracday
Element set: 911
Inclination: 51
6384 deg
RA of node: 209
1296 deg
Eccentricity:
0006608
Arg of perigee: 67
7833 deg
Mean anomaly: 292
4030 deg
Mean motion: 15
71791654 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1577
Checksum: 281
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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