Date:
August 19th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11500 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
239/11:29:36
000 0
0 0
0 0
0
018/12:52:54
047 0
0 0
0 185
7
000/00:00:00
000 0
0 0
0 183
1
Coasting Arc #1 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2007/229/11:29:36
000
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -333803
56 A = 6716230
50 meter
Y = 4722521
40 meter E =
0006429
Z = -4768724
49 I = 51
79793
XDOT = -6926
710784 Wp = 151
94991
YDOT = 2136
688858 meter/sec RA = 146
48192 deg
ZDOT = 2596
693526 TA = 143
48556
MA = 143
44171
Ha = 185
410 n
mi
Hp = 183
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1095156
04 X = -363421
25
Y = 15493836
60 feet Y = 4718623
03 meter
Z = -15645421
56 Z = -4770418
03
XDOT = -22725
429083 XDOT = -6962
702928
YDOT = 7010
134048 feet/sec YDOT = 2059
029223 meter/sec
ZDOT = 8519
335716 ZDOT = 2562
956385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11279480
80 X = 3437985
75
Y = -10670044
47 feet Y = -3252229
56 meter
Z = -15651230
60 Z = -4770495
09
XDOT = 20681
264790 XDOT = 6303
649508
YDOT = 9533
299930 feet/sec YDOT = 2905
749819 meter/sec
ZDOT = 8391
674397 ZDOT = 2557
782356
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 07229
49032940
00020000 00000-0 20000-3 0 9000
2 25544 51
6336 147
3931 0008253 255
8500 104
1747 15
76120786 20455
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
49032940 = yrday
fracday
Element set: 900
Inclination: 51
6336 deg
RA of node: 147
3931 deg
Eccentricity:
0008253
Arg of perigee: 255
8500 deg
Mean anomaly: 104
1747 deg
Mean motion: 15
76120786 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2045
Checksum: 277
Coasting Arc #2 (Orbit 2060)
---------------------------------------
Vector Time (GMT): 2007/230/11:33:52
637
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5352188
93 A = 6718960
95 meter
Y = -194882
84 meter E =
0001480
Z = -4056800
07 I = 51
83124
XDOT = -2719
337145 Wp = 307
63086
YDOT = 6074
359840 meter/sec RA = 141
37351 deg
ZDOT = -3877
617626 TA = 282
54449
MA = 282
56104
Ha = 185
261 n
mi
Hp = 184
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17559674
95 X = 5373677
48
Y = -639379
40 feet Y = -134911
45 meter
Z = -13309711
50 Z = -4030747
04
XDOT = -8921
709792 XDOT = -2768
222737
YDOT = 19929
002099 feet/sec YDOT = 6043
677394 meter/sec
ZDOT = -12721
842605 ZDOT = -3890
946782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13764201
66 X = -4195328
67
Y = -11041622
18 feet Y = -3365486
44 meter
Z = -13210932
71 Z = -4026692
29
XDOT = 18918
503936 XDOT = 5766
360000
YDOT = -8295
229007 feet/sec YDOT = -2528
385801 meter/sec
ZDOT = -12771
608171 ZDOT = -3892
786171
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 07230
50478524
00020000 00000-0 20000-3 0 9017
2 25544 51
6340 142
1664 0008216 259
9698 100
0539 15
76162060 20611
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
50478524 = yrday
fracday
Element set: 901
Inclination: 51
6340 deg
RA of node: 142
1664 deg
Eccentricity:
0008216
Arg of perigee: 259
9698 deg
Mean anomaly: 100
0539 deg
Mean motion: 15
76162060 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2061
Checksum: 270
Coasting Arc #3 (Orbit 2076)
---------------------------------------
Vector Time (GMT): 2007/231/11:38:58
592
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4163485
87 A = 6725515
87 meter
Y = -5163550
97 meter E =
0009176
Z = 1074176
87 I = 51
87517
XDOT = 4355
568633 Wp = 158
77988
YDOT = 2275
817905 meter/sec RA = 136
18169 deg
ZDOT = -5934
978536 TA = 9
49519
MA = 9
47786
Ha = 184
869 n
mi
Hp = 184
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13659730
55 X = 4215697
88
Y = -16940784
03 feet Y = -5116700
62 meter
Z = 3524202
34 Z = 1094529
73
XDOT = 14289
923335 XDOT = 4358
627385
YDOT = 7466
594177 feet/sec YDOT = 2324
541592 meter/sec
ZDOT = -19471
714357 ZDOT = -5913
811730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21224524
10 X = -6469234
95
Y = 4748969
29 feet Y = 1447485
84 meter
Z = 3600732
11 Z = 1097503
15
XDOT = -6261
709097 XDOT = -1908
568933
YDOT = -13265
025214 feet/sec YDOT = -4043
179685 meter/sec
ZDOT = -19391
144502 ZDOT = -5910
420844
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 07231
51922404
00020000 00000-0 20000-3 0 9021
2 25544 51
6339 136
9392 0008272 263
3514 96
6708 15
76160023 20778
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
51922404 = yrday
fracday
Element set: 902
Inclination: 51
6339 deg
RA of node: 136
9392 deg
Eccentricity:
0008272
Arg of perigee: 263
3514 deg
Mean anomaly: 96
6708 deg
Mean motion: 15
76160023 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2077
Checksum: 281
Coasting Arc #4 (Orbit 2092)
---------------------------------------
Vector Time (GMT): 2007/232/11:43:54
685
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1809799
34 A = 6714607
39 meter
Y = -4001516
89 meter E =
0005082
Z = 5083563
09 I = 51
85903
XDOT = 5841
092975 Wp = 301
27572
YDOT = -4739
661684 meter/sec RA = 131
02474 deg
ZDOT = -1649
948809 TA = 164
54000
MA = 164
52447
Ha = 184
210 n
mi
Hp = 183
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5937661
89 X = -1789614
28
Y = -13128336
25 feet Y = -4021642
45 meter
Z = 16678356
58 Z = 5074819
95
XDOT = 19163
690864 XDOT = 5901
673596
YDOT = -15550
071141 feet/sec YDOT = -4674
004494 meter/sec
ZDOT = -5413
217876 ZDOT = -1621
425869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2917954
33 X = -889392
48
Y = 14149790
90 feet Y = 4312856
27 meter
Z = 16644686
23 Z = 5073300
36
XDOT = -23643
351242 XDOT = -7206
493458
YDOT = 1370
753233 feet/sec YDOT = 417
805585 meter/sec
ZDOT = -5305
634595 ZDOT = -1617
157425
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 07232
53364331
00020000 00000-0 20000-3 0 9034
2 25544 51
6339 131
7120 0008415 268
2373 91
7828 15
76234792 20938
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
53364331 = yrday
fracday
Element set: 903
Inclination: 51
6339 deg
RA of node: 131
7120 deg
Eccentricity:
0008415
Arg of perigee: 268
2373 deg
Mean anomaly: 91
7828 deg
Mean motion: 15
76234792 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2093
Checksum: 284
Coasting Arc #5 (Orbit 2108)
---------------------------------------
Vector Time (GMT): 2007/233/11:48:15
588
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177118
10 A = 6720685
89 meter
Y = 2499384
38 meter E =
0004104
Z = 3477602
63 I = 51
89789
XDOT = 73
896547 Wp = 89
92650
YDOT = -6204
728197 meter/sec RA = 125
91263 deg
ZDOT = 4564
809980 TA = 311
20161
MA = 311
23698
Ha = 184
281 n
mi
Hp = 183
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16985295
61 X = -5221575
34
Y = 8200079
98 feet Y = 2441242
15 meter
Z = 11409457
44 Z = 3452344
41
XDOT = 242
442741 XDOT = 121
098277
YDOT = -20356
719808 feet/sec YDOT = -6203
638196 meter/sec
ZDOT = 14976
410697 ZDOT = 4565
283255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18707584
26 X = 5702071
68
Y = 2817420
61 feet Y = 858749
80 meter
Z = 11313961
73 Z = 3448495
54
XDOT = -11382
500461 XDOT = -3469
386141
YDOT = 15373
320452 feet/sec YDOT = 4685
788074 meter/sec
ZDOT = 14977
424265 ZDOT = 4565
118916
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 07233
54804780
00020000 00000-0 20000-3 0 9044
2 25544 51
6345 126
4842 0008317 272
2416 87
7796 15
76220450 21094
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
54804780 = yrday
fracday
Element set: 904
Inclination: 51
6345 deg
RA of node: 126
4842 deg
Eccentricity:
0008317
Arg of perigee: 272
2416 deg
Mean anomaly: 87
7796 deg
Mean motion: 15
76220450 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2109
Checksum: 290
Coasting Arc #6 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2007/234/11:52:38
583
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1743641
76 A = 6723803
52 meter
Y = 6142551
14 meter E =
0007088
Z = -2091842
05 I = 51
92553
XDOT = -5308
568898 Wp = 324
03959
YDOT = 391
418285 meter/sec RA = 120
71808 deg
ZDOT = 5570
454005 TA = 12
66453
MA = 12
64674
Ha = 184
761 n
mi
Hp = 184
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5720609
44 X = -1802037
34
Y = 20152726
85 feet Y = 6122726
40 meter
Z = -6862998
86 Z = -2100454
03
XDOT = -17416
564626 XDOT = -5339
611377
YDOT = 1284
180726 feet/sec YDOT = 331
880916 meter/sec
ZDOT = 18275
767732 ZDOT = 5544
589727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15538679
65 X = 4736189
56
Y = -14034539
52 feet Y = -4277727
65 meter
Z = -6894901
03 Z = -2101565
83
XDOT = 14490
099900 XDOT = 4416
582450
YDOT = 7106
542962 feet/sec YDOT = 2166
074295 meter/sec
ZDOT = 18177
697927 ZDOT = 5540
562328
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 07234
49903417
00020000 00000-0 20000-3 0 9057
2 25544 51
6350 121
5834 0008447 275
8706 84
1495 15
76267357 21243
Satellite: ISS
Catalog Number: 25544
Epoch time: 07234
49903417 = yrday
fracday
Element set: 905
Inclination: 51
6350 deg
RA of node: 121
5834 deg
Eccentricity:
0008447
Arg of perigee: 275
8706 deg
Mean anomaly: 84
1495 deg
Mean motion: 15
76267357 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2124
Checksum: 302
Coasting Arc #7 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2007/235/11:57:24
672
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3534482
96 A = 6713589
40 meter
Y = 2193911
98 meter E =
0006609
Z = -5274958
01 I = 51
90510
XDOT = -3606
728116 Wp = 84
04820
YDOT = 6791
114506 meter/sec RA = 115
58320 deg
ZDOT = 408
916918 TA = 189
81444
MA = 189
82735
Ha = 185
089 n
mi
Hp = 183
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11596072
71 X = 3535312
19
Y = 7197873
96 feet Y = 2233441
59 meter
Z = -17306292
68 Z = -5257785
46
XDOT = -11833
097493 XDOT = -3684
385735
YDOT = 22280
559403 feet/sec YDOT = 6750
347803 meter/sec
ZDOT = 1341
590938 ZDOT = 391
207457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6530638
10 X = -1990538
49
Y = -12078464
82 feet Y = -3681516
08 meter
Z = -17240867
49 Z = -5255016
41
XDOT = 20510
160638 XDOT = 6251
496962
YDOT = -12904
622294 feet/sec YDOT = -3933
328875 meter/sec
ZDOT = 1275
246512 ZDOT = 388
695137
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 07235
51340309
00020000 00000-0 20000-3 0 9067
2 25544 51
6351 116
3559 0008536 280
1209 79
8992 15
76303696 21404
Satellite: ISS
Catalog Number: 25544
Epoch time: 07235
51340309 = yrday
fracday
Element set: 906
Inclination: 51
6351 deg
RA of node: 116
3559 deg
Eccentricity:
0008536
Arg of perigee: 280
1209 deg
Mean anomaly: 79
8992 deg
Mean motion: 15
76303696 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2140
Checksum: 293
Coasting Arc #8 (Orbit 2155)
---------------------------------------
Vector Time (GMT): 2007/236/12:02:09
803
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4015127
21 A = 6722487
55 meter
Y = -4646194
66 meter E =
0004481
Z = -2730868
73 I = 51
94625
XDOT = 2419
242665 Wp = 261
46847
YDOT = 5147
416196 meter/sec RA = 110
46028 deg
ZDOT = -5194
120733 TA = 309
59837
MA = 309
63793
Ha = 185
228 n
mi
Hp = 183
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13172989
54 X = 4080049
13
Y = -15243420
79 feet Y = -4600932
06 meter
Z = -8959543
06 Z = -2711206
11
XDOT = 7937
147850 XDOT = 2386
735463
YDOT = 16887
848411 feet/sec YDOT = 5174
288126 meter/sec
ZDOT = -17041
078520 ZDOT = -5182
446812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18807256
01 X = -5732451
63
Y = 7314214
29 feet Y = 2229372
52 meter
Z = -8885512
56 Z = -2708304
23
XDOT = 1306
772431 XDOT = 398
304237
YDOT = -17313
546946 feet/sec YDOT = -5277
169109 meter/sec
ZDOT = -16996
144909 ZDOT = -5180
424968
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 07236
52775521
00020000 00000-0 20000-3 0 9078
2 25544 51
6352 111
1287 0008705 283
2204 76
7989 15
76284207 21568
Satellite: ISS
Catalog Number: 25544
Epoch time: 07236
52775521 = yrday
fracday
Element set: 907
Inclination: 51
6352 deg
RA of node: 111
1287 deg
Eccentricity:
0008705
Arg of perigee: 283
2204 deg
Mean anomaly: 76
7989 deg
Mean motion: 15
76284207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2156
Checksum: 298
Coasting Arc #9 (Orbit 2171)
---------------------------------------
Vector Time (GMT): 2007/237/12:06:49
979
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -609554
52 A = 6722083
03 meter
Y = -6080263
95 meter E =
0005179
Z = 2797097
27 I = 51
95457
XDOT = 4958
987955 Wp = 85
39364
YDOT = -2869
258721 meter/sec RA = 105
26523 deg
ZDOT = -5147
929922 TA = 62
70228
MA = 62
64955
Ha = 185
379 n
mi
Hp = 183
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1999850
80 X = -555106
37
Y = -19948372
53 feet Y = -6086776
04 meter
Z = 9176828
30 Z = 2794268
04
XDOT = 16269
645523 XDOT = 5015
711166
YDOT = -9413
578482 feet/sec YDOT = -2813
487105 meter/sec
ZDOT = -16889
533865 ZDOT = -5123
701927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6786593
37 X = -2068553
66
Y = 18870343
81 feet Y = 5751680
79 meter
Z = 9165338
11 Z = 2793595
05
XDOT = -17450
468917 XDOT = -5318
902926
YDOT = 1896
416185 feet/sec YDOT = 578
027653 meter/sec
ZDOT = -16797
951783 ZDOT = -5120
015703
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 07237
54208929
00020000 00000-0 20000-3 0 9085
2 25544 51
6352 105
9009 0008641 288
6895 71
3331 15
76355430 21722
Satellite: ISS
Catalog Number: 25544
Epoch time: 07237
54208929 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 105
9009 deg
Eccentricity:
0008641
Arg of perigee: 288
6895 deg
Mean anomaly: 71
3331 deg
Mean motion: 15
76355430 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2172
Checksum: 299
Coasting Arc #10 (Orbit 2187)
---------------------------------------
Vector Time (GMT): 2007/238/12:11:57
720
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4133622
41 A = 6713425
19 meter
Y = -380879
58 meter E =
0006193
Z = 5280873
18 I = 51
93108
XDOT = 1107
108412 Wp = 294
65709
YDOT = -7614
482568 meter/sec RA = 100
14046 deg
ZDOT = 320
221971 TA = 152
33183
MA = 152
29886
Ha = 185
624 n
mi
Hp = 183
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13561753
30 X = -4154709
17
Y = -1249604
93 feet Y = -427222
11 meter
Z = 17325699
40 Z = 5260741
19
XDOT = 3632
245445 XDOT = 1190
616854
YDOT = -24981
898188 feet/sec YDOT = -7601
635346 meter/sec
ZDOT = 1050
597018 ZDOT = 325
802853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12041367
17 X = 3670208
71
Y = 6567444
00 feet Y = 2001756
93 meter
Z = 17249251
60 Z = 5257571
89
XDOT = -12763
394618 XDOT = -3890
282680
YDOT = 20613
486272 feet/sec YDOT = 6282
990616 meter/sec
ZDOT = 1070
830153 ZDOT = 326
389031
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 07238
55640621
00020000 00000-0 20000-3 0 9097
2 25544 51
6346 100
6724 0008699 292
0552 67
9688 15
76358053 21880
Satellite: ISS
Catalog Number: 25544
Epoch time: 07238
55640621 = yrday
fracday
Element set: 909
Inclination: 51
6346 deg
RA of node: 100
6724 deg
Eccentricity:
0008699
Arg of perigee: 292
0552 deg
Mean anomaly: 67
9688 deg
Mean motion: 15
76358053 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2188
Checksum: 319
Coasting Arc #11 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2007/239/11:29:36
000
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1892314
01 A = 6724234
81 meter
Y = -6224179
59 meter E =
0004103
Z = -1692156
00 I = 51
97117
XDOT = 4255
227221 Wp = 232
87323
YDOT = 2858
360196 meter/sec RA = 95
17287 deg
ZDOT = -5748
153946 TA = 325
76447
MA = 325
79092
Ha = 185
718 n
mi
Hp = 183
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6208379
29 X = 1969993
10
Y = -20420536
70 feet Y = -6202584
35 meter
Z = -5551692
90 Z = -1682774
60
XDOT = 13960
719228 XDOT = 4250
871318
YDOT = 9377
822165 feet/sec YDOT = 2905
920164 meter/sec
ZDOT = -18858
772788 ZDOT = -5727
493041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16358140
81 X = -4985961
32
Y = 13723666
55 feet Y = 4182973
57 meter
Z = -5516864
35 Z = -1681540
25
XDOT = -5684
812930 XDOT = -1732
730981
YDOT = -14334
967708 feet/sec YDOT = -4369
298157 meter/sec
ZDOT = -18780
004983 ZDOT = -5724
145519
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 07239
50731262
00020000 00000-0 20000-3 0 9107
2 25544 51
6345 95
7715 0008809 294
8230 65
2018 15
76360684 22038
Satellite: ISS
Catalog Number: 25544
Epoch time: 07239
50731262 = yrday
fracday
Element set: 910
Inclination: 51
6345 deg
RA of node: 95
7715 deg
Eccentricity:
0008809
Arg of perigee: 294
8230 deg
Mean anomaly: 65
2018 deg
Mean motion: 15
76360684 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2203
Checksum: 287
Coasting Arc #12 (Orbit 2218)
---------------------------------------
Vector Time (GMT): 2007/240/11:34:16
252
Vector Time (MET): N/A
Weight (LBS) : 522151
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2879386
19 A = 6719333
58 meter
Y = -4831512
06 meter E =
0006905
Z = 3677742
31 I = 51
95665
XDOT = 3408
801615 Wp = 36
04262
YDOT = -5356
436898 meter/sec RA = 89
98180 deg
ZDOT = -4358
443459 TA = 99
93736
MA = 99
85942
Ha = 185
870 n
mi
Hp = 182
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9446805
10 X = -2843011
03
Y = -15851417
52 feet Y = -4863507
48 meter
Z = 12066083
69 Z = 3663842
99
XDOT = 11183
732332 XDOT = 3489
616931
YDOT = -17573
611869 feet/sec YDOT = -5317
866037 meter/sec
ZDOT = -14299
355182 ZDOT = -4341
687295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 37145
43 X = 11321
93
Y = 18487641
86 feet Y = 5635033
24 meter
Z = 12012729
00 Z = 3661479
80
XDOT = -17334
903635 XDOT = -5283
678628
YDOT = 9305
739795 feet/sec YDOT = 2836
389490 meter/sec
ZDOT = -14236
429469 ZDOT = -4339
263702
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 07240
52159338
00020000 00000-0 20000-3 0 9110
2 25544 51
6342 90
5422 0008996 300
2124 59
8149 15
76464247 22195
Satellite: ISS
Catalog Number: 25544
Epoch time: 07240
52159338 = yrday
fracday
Element set: 911
Inclination: 51
6342 deg
RA of node: 90
5422 deg
Eccentricity:
0008996
Arg of perigee: 300
2124 deg
Mean anomaly: 59
8149 deg
Mean motion: 15
76464247 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2219
Checksum: 287
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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