Date:
October 12th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 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 667)
---------------------------------------
Vector Time (GMT): 2008/284/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -263331
84 A = 6726893
41 meter
Y = -4576796
47 meter E =
0003374
Z = 4920036
41 I = 51
81867
XDOT = 6834
195047 Wp = 87
60123
YDOT = -2773
127115 meter/sec RA = 144
26936 deg
ZDOT = -2212
446171 TA = 23
84675
MA = 23
83112
Ha = 192
738 n
mi
Hp = 187
245
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -863949
61 X = -236034
68
Y = -15015736
46 feet Y = -4579588
29 meter
Z = 16141851
75 Z = 4918823
71
XDOT = 22421
899759 XDOT = 6875
444438
YDOT = -9098
186072 feet/sec YDOT = -2696
472690 meter/sec
ZDOT = -7258
681663 ZDOT = -2179
144971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3851451
44 X = 1173922
40
Y = 14544817
87 feet Y = 4433260
49 meter
Z = 16136688
74 Z = 4918462
73
XDOT = -19210
592350 XDOT = -5855
388548
YDOT = 13002
517279 feet/sec YDOT = 3963
167267 meter/sec
ZDOT = -7129
998873 ZDOT = -2173
223657
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 08284
52312925
00020000 00000-0 20000-3 0 9000
2 25544 51
6426 145
0254 0003829 210
8874 149
2064 15
72165478 6681
Satellite: ISS
Catalog Number: 25544
Epoch time: 08284
52312925 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 145
0254 deg
Eccentricity:
0003829
Arg of perigee: 210
8874 deg
Mean anomaly: 149
2064 deg
Mean motion: 15
72165478 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 668
Checksum: 293
Coasting Arc #2 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2008/285/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5621626
66 A = 6736628
86 meter
Y = 3447112
02 meter E =
0010569
Z = 1356621
59 I = 51
87358
XDOT = -1504
167895 Wp = 68
81070
YDOT = -4768
730345 meter/sec RA = 139
19210 deg
ZDOT = 5851
457147 TA = 306
03140
MA = 306
12930
Ha = 192
600 n
mi
Hp = 187
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18443657
03 X = -5666345
32
Y = 11309422
63 feet Y = 3383997
81 meter
Z = 4450858
24 Z = 1329202
50
XDOT = -4934
934040 XDOT = -1479
157071
YDOT = -15645
440763 feet/sec YDOT = -4785
410524 meter/sec
ZDOT = 19197
694053 ZDOT = 5844
210929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15669009
73 X = 4775914
17
Y = -14949402
05 feet Y = -4556577
75 meter
Z = 4345017
41 Z = 1324361
31
XDOT = 7140
236850 XDOT = 2176
344192
YDOT = 13087
290275 feet/sec YDOT = 3989
006076 meter/sec
ZDOT = 19169
144678 ZDOT = 5842
755298
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 08285
54016624
00020000 00000-0 20000-3 0 9011
2 25544 51
6418 139
8163 0003875 215
0119 145
0788 15
72172582 6841
Satellite: ISS
Catalog Number: 25544
Epoch time: 08285
54016624 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 139
8163 deg
Eccentricity:
0003875
Arg of perigee: 215
0119 deg
Mean anomaly: 145
0788 deg
Mean motion: 15
72172582 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 684
Checksum: 294
Coasting Arc #3 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2008/286/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2261438
66 A = 6725515
34 meter
Y = 3577783
12 meter E =
0012998
Z = -5237620
07 I = 51
85664
XDOT = -5793
285067 Wp = 111
28348
YDOT = 4975
404133 meter/sec RA = 134
06548 deg
ZDOT = 894
466337 TA = 167
23941
MA = 167
20648
Ha = 192
447 n
mi
Hp = 187
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7419418
17 X = 2246707
09
Y = 11738133
60 feet Y = 3602989
00 meter
Z = -17183792
89 Z = -5226669
92
XDOT = -19006
840770 XDOT = -5852
835500
YDOT = 16323
504372 feet/sec YDOT = 4910
287387 meter/sec
ZDOT = 2934
600842 ZDOT = 866
176982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9992450
18 X = -3045698
81
Y = -9718573
01 feet Y = -2962221
05 meter
Z = -17141019
89 Z = -5224582
86
XDOT = 14099
388536 XDOT = 4297
493626
YDOT = -19496
714932 feet/sec YDOT = -5942
598711 meter/sec
ZDOT = 2825
538269 ZDOT = 861
224064
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 08286
49362434
00020000 00000-0 20000-3 0 9020
2 25544 51
6406 134
9323 0003820 219
2826 140
8059 15
72189601 6993
Satellite: ISS
Catalog Number: 25544
Epoch time: 08286
49362434 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 134
9323 deg
Eccentricity:
0003820
Arg of perigee: 219
2826 deg
Mean anomaly: 140
8059 deg
Mean motion: 15
72189601 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 699
Checksum: 295
Coasting Arc #4 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2008/287/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4354232
23 A = 6737368
25 meter
Y = -5127252
30 meter E =
0012733
Z = -204907
24 I = 51
91562
XDOT = 3505
625518 Wp = 154
27156
YDOT = 3213
117064 meter/sec RA = 128
97113 deg
ZDOT = -6056
600977 TA = 27
94539
MA = 27
87707
Ha = 192
419 n
mi
Hp = 187
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14285538
82 X = 4412237
80
Y = -16821693
90 feet Y = -5078236
45 meter
Z = -672267
85 Z = -183612
54
XDOT = 11501
396057 XDOT = 3498
857932
YDOT = 10541
722652 feet/sec YDOT = 3252
280621 meter/sec
ZDOT = -19870
738114 ZDOT = -6039
586979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9745569
06 X = -2970449
45
Y = 19803367
75 feet Y = 6036066
49 meter
Z = -590303
98 Z = -179924
65
XDOT = -12394
820029 XDOT = -3777
941145
YDOT = -6673
248459 feet/sec YDOT = -2034
006130 meter/sec
ZDOT = -19804
517398 ZDOT = -6036
416903
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 08287
51063100
00020000 00000-0 20000-3 0 9033
2 25544 51
6404 129
7242 0003891 222
7207 137
3653 15
72174219 7152
Satellite: ISS
Catalog Number: 25544
Epoch time: 08287
51063100 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 129
7242 deg
Eccentricity:
0003891
Arg of perigee: 222
7207 deg
Mean anomaly: 137
3653 deg
Mean motion: 15
72174219 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 715
Checksum: 267
Coasting Arc #5 (Orbit 730)
---------------------------------------
Vector Time (GMT): 2008/288/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3708563
33 A = 6725305
97 meter
Y = -1903111
47 meter E =
0003517
Z = 5278210
88 I = 51
89176
XDOT = 3994
980799 Wp = 184
99542
YDOT = -6565
980686 meter/sec RA = 123
86860 deg
ZDOT = 436
107533 TA = 260
85599
MA = 260
89578
Ha = 192
337 n
mi
Hp = 187
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12167202
51 X = -3712648
13
Y = -6243804
03 feet Y = -1944605
22 meter
Z = 17316964
84 Z = 5260184
38
XDOT = 13106
892384 XDOT = 4065
987146
YDOT = -21541
931386 feet/sec YDOT = -6520
909454 meter/sec
ZDOT = 1430
798993 ZDOT = 455
688669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13470715
87 X = 4105874
20
Y = 2825870
87 feet Y = 861325
44 meter
Z = 17246954
65 Z = 5256871
78
XDOT = -6816
038900 XDOT = -2077
528657
YDOT = 23231
634947 feet/sec YDOT = 7081
002332 meter/sec
ZDOT = 1505
993575 ZDOT = 459
026842
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 08288
52762062
00020000 00000-0 20000-3 0 9049
2 25544 51
6395 124
5141 0003808 227
6859 132
3981 15
72199688 7311
Satellite: ISS
Catalog Number: 25544
Epoch time: 08288
52762062 = yrday
fracday
Element set: 904
Inclination: 51
6395 deg
RA of node: 124
5141 deg
Eccentricity:
0003808
Arg of perigee: 227
6859 deg
Mean anomaly: 132
3981 deg
Mean motion: 15
72199688 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 731
Checksum: 312
Coasting Arc #6 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2008/289/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2533204
96 A = 6736793
94 meter
Y = 6165878
79 meter E =
0006257
Z = -951647
64 I = 51
94488
XDOT = -4754
665336 Wp = 29
56442
YDOT = -1036
639942 meter/sec RA = 118
75168 deg
ZDOT = 5961
802147 TA = 320
09587
MA = 320
14185
Ha = 192
010 n
mi
Hp = 187
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8311039
91 X = -2597341
46
Y = 20229261
11 feet Y = 6137192
38 meter
Z = -3122203
55 Z = -964110
43
XDOT = -15599
295723 XDOT = -4771
682389
YDOT = -3401
049680 feet/sec YDOT = -1089
904227 meter/sec
ZDOT = 19559
718331 ZDOT = 5938
661939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2352254
36 X = 716967
13
Y = -21736221
04 feet Y = -6625200
17 meter
Z = -3169879
96 Z = -966179
41
XDOT = 14452
789799 XDOT = 4405
210331
YDOT = -1265
036034 feet/sec YDOT = -385
582983 meter/sec
ZDOT = 19469
985036 ZDOT = 5934
451439
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 08289
48103253
00020000 00000-0 20000-3 0 9057
2 25544 51
6382 119
6292 0003877 233
2047 126
8760 15
72235121 7469
Satellite: ISS
Catalog Number: 25544
Epoch time: 08289
48103253 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 119
6292 deg
Eccentricity:
0003877
Arg of perigee: 233
2047 deg
Mean anomaly: 126
8760 deg
Mean motion: 15
72235121 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 746
Checksum: 288
Coasting Arc #7 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2008/290/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4409685
02 A = 6726002
72 meter
Y = -134244
39 meter E =
0010038
Z = -5085744
65 I = 51
92093
XDOT = -1740
492752 Wp = 85
19451
YDOT = 7294
805372 meter/sec RA = 113
67251 deg
ZDOT = -1703
724814 TA = 168
47133
MA = 168
44832
Ha = 191
931 n
mi
Hp = 187
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14467470
55 X = 4435564
89
Y = -440434
35 feet Y = -84788
11 meter
Z = -16685513
93 Z = -5064258
81
XDOT = -5710
278057 XDOT = -1813
658421
YDOT = 23933
088491 feet/sec YDOT = 7274
933063 meter/sec
ZDOT = -5589
648339 ZDOT = -1712
358240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13789544
59 X = -4203053
19
Y = 4703217
50 feet Y = 1433540
70 meter
Z = -16602297
03 Z = -5060380
13
XDOT = -1267
384001 XDOT = -386
298643
YDOT = -23539
094860 feet/sec YDOT = -7174
716113 meter/sec
ZDOT = -5622
400081 ZDOT = -1713
707545
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 08290
49799047
00020000 00000-0 20000-3 0 9063
2 25544 51
6374 114
4192 0003822 235
8590 124
2210 15
72272324 7629
Satellite: ISS
Catalog Number: 25544
Epoch time: 08290
49799047 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 114
4192 deg
Eccentricity:
0003822
Arg of perigee: 235
8590 deg
Mean anomaly: 124
2210 deg
Mean motion: 15
72272324 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 762
Checksum: 284
Coasting Arc #8 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2008/291/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 487377
37 A = 6735139
02 meter
Y = -6402202
17 meter E =
0011810
Z = 2011373
12 I = 51
96404
XDOT = 5091
635256 Wp = 125
58743
YDOT = -1379
946213 meter/sec RA = 108
53896 deg
ZDOT = -5609
974529 TA = 32
10715
MA = 32
03527
Ha = 191
609 n
mi
Hp = 187
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1599007
12 X = 549160
42
Y = -21004600
29 feet Y = -6396406
62 meter
Z = 6598993
19 Z = 2013890
85
XDOT = 16704
840078 XDOT = 5133
940706
YDOT = -4527
382588 feet/sec YDOT = -1322
771975 meter/sec
ZDOT = -18405
428244 ZDOT = -5585
135850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5036750
76 X = 1535201
63
Y = 20451411
10 feet Y = 6233590
10 meter
Z = 6608153
61 Z = 2014165
22
XDOT = -13082
653400 XDOT = -3987
592756
YDOT = 9155
097290 feet/sec YDOT = 2790
473654 meter/sec
ZDOT = -18309
330686 ZDOT = -5580
683993
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 08291
51492977
00020000 00000-0 20000-3 0 9070
2 25544 51
6384 109
2095 0003889 244
0677 116
0085 15
72343563 7785
Satellite: ISS
Catalog Number: 25544
Epoch time: 08291
51492977 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 109
2095 deg
Eccentricity:
0003889
Arg of perigee: 244
0677 deg
Mean anomaly: 116
0085 deg
Mean motion: 15
72343563 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 778
Checksum: 317
Coasting Arc #9 (Orbit 793)
---------------------------------------
Vector Time (GMT): 2008/292/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4293536
41 A = 6727651
07 meter
Y = 2252622
55 meter E =
0006471
Z = 4663095
33 I = 51
94587
XDOT = -606
516360 Wp = 143
79997
YDOT = -7116
295081 meter/sec RA = 103
47723 deg
ZDOT = 2872
134865 TA = 277
88046
MA = 277
95390
Ha = 191
716 n
mi
Hp = 187
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14086405
54 X = -4341059
56
Y = 7390493
93 feet Y = 2204343
86 meter
Z = 15298869
19 Z = 4642121
42
XDOT = -1989
883070 XDOT = -540
848397
YDOT = -23347
424806 feet/sec YDOT = -7122
710432 meter/sec
ZDOT = 9423
014648 ZDOT = 2869
347585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10981024
04 X = 3347016
13
Y = -11616234
71 feet Y = -3540628
34 meter
Z = 15217812
66 Z = 4638389
30
XDOT = 8713
390376 XDOT = 2655
841387
YDOT = 20597
266412 feet/sec YDOT = 6278
046802 meter/sec
ZDOT = 9411
569328 ZDOT = 2868
646331
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 08292
53185600
00020000 00000-0 20000-3 0 9086
2 25544 51
6377 103
9991 0003829 245
3247 114
7517 15
72311072 7947
Satellite: ISS
Catalog Number: 25544
Epoch time: 08292
53185600 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 103
9991 deg
Eccentricity:
0003829
Arg of perigee: 245
3247 deg
Mean anomaly: 114
7517 deg
Mean motion: 15
72311072 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 794
Checksum: 295
Coasting Arc #10 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2008/293/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1493495
35 A = 6733063
55 meter
Y = 5853479
49 meter E =
0000778
Z = -2973752
26 I = 51
97051
XDOT = -4508
564971 Wp = 79
36101
YDOT = 3699
259527 meter/sec RA = 98
33060 deg
ZDOT = 5018
479920 TA = 246
53560
MA = 246
54378
Ha = 191
545 n
mi
Hp = 187
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4899919
14 X = 1442376
04
Y = 19204329
02 feet Y = 5869894
91 meter
Z = -9756405
06 Z = -2966620
64
XDOT = -14791
879827 XDOT = -4573
974968
YDOT = 12136
678239 feet/sec YDOT = 3648
476215 meter/sec
ZDOT = 16464
829135 ZDOT = 4996
418134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11241503
33 X = -3426410
21
Y = -16339910
94 feet Y = -4980404
86 meter
Z = -9728248
23 Z = -2965170
06
XDOT = 8629
272456 XDOT = 2630
202245
YDOT = -15686
238775 feet/sec YDOT = -4781
165579 meter/sec
ZDOT = 16379
675040 ZDOT = 4992
524952
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 08293
48520661
00020000 00000-0 20000-3 0 9092
2 25544 51
6380 99
1145 0003780 246
3386 113
7380 15
72348586 8093
Satellite: ISS
Catalog Number: 25544
Epoch time: 08293
48520661 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 99
1145 deg
Eccentricity:
0003780
Arg of perigee: 246
3386 deg
Mean anomaly: 113
7380 deg
Mean motion: 15
72348586 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 809
Checksum: 307
Coasting Arc #11 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2008/294/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3430294
27 A = 6729615
79 meter
Y = -4115202
99 meter E =
0003781
Z = -4076520
68 I = 51
96277
XDOT = 2688
366994 Wp = 70
62928
YDOT = 6078
132453 meter/sec RA = 93
28035 deg
ZDOT = -3875
285328 TA = 159
62025
MA = 159
60515
Ha = 191
456 n
mi
Hp = 187
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11254246
28 X = 3495859
48
Y = -13501322
16 feet Y = -4076476
73 meter
Z = -13374411
68 Z = -4059696
93
XDOT = 8820
101686 XDOT = 2639
026245
YDOT = 19941
379439 feet/sec YDOT = 6107
919574 meter/sec
ZDOT = -12714
190708 ZDOT = -3862
344694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5727232
67 X = -1745660
52
Y = 16669508
29 feet Y = 5080866
13 meter
Z = -13309581
00 Z = -4056760
29
XDOT = -14244
521329 XDOT = -4341
730101
YDOT = -15000
695538 feet/sec YDOT = -4572
212000 meter/sec
ZDOT = -12663
506096 ZDOT = -3859
836658
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 08294
50209728
00020000 00000-0 20000-3 0 9106
2 25544 51
6385 93
9053 0003618 251
6124 108
4645 15
72393241 8258
Satellite: ISS
Catalog Number: 25544
Epoch time: 08294
50209728 = yrday
fracday
Element set: 910
Inclination: 51
6385 deg
RA of node: 93
9053 deg
Eccentricity:
0003618
Arg of perigee: 251
6124 deg
Mean anomaly: 108
4645 deg
Mean motion: 15
72393241 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 825
Checksum: 286
Coasting Arc #12 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2008/295/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3101865
04 A = 6730663
95 meter
Y = -4628044
31 meter E =
0007942
Z = 3769993
77 I = 51
96608
XDOT = 3150
652739 Wp = 87
13524
YDOT = -5587
514149 meter/sec RA = 88
12814 deg
ZDOT = -4258
906042 TA = 47
50635
MA = 47
43927
Ha = 191
431 n
mi
Hp = 187
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10176722
56 X = -3068197
12
Y = -15183872
41 feet Y = -4662542
96 meter
Z = 12368745
96 Z = 3755006
45
XDOT = 10336
787203 XDOT = 3233
588297
YDOT = -18331
739333 feet/sec YDOT = -5551
817957 meter/sec
ZDOT = -13972
788851 ZDOT = -4243
398616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15194354
78 X = 4631239
34
Y = 10231847
45 feet Y = 3118667
10 meter
Z = 12310256
73 Z = 3752166
25
XDOT = -2034
513119 XDOT = -620
119599
YDOT = 19792
539818 feet/sec YDOT = 6032
766137 meter/sec
ZDOT = -13913
181329 ZDOT = -4240
737669
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 08295
51897043
00020000 00000-0 20000-3 0 9112
2 25544 51
6380 88
6948 0003753 254
7985 105
2762 15
72385762 8418
Satellite: ISS
Catalog Number: 25544
Epoch time: 08295
51897043 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 88
6948 deg
Eccentricity:
0003753
Arg of perigee: 254
7985 deg
Mean anomaly: 105
2762 deg
Mean motion: 15
72385762 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 841
Checksum: 322
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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