Date:
December 11th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8342 03 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
352/04:02:44
529 1
4 1
7 1
7
N/A -0
9 0
2 196
4
000/00:09:29
058 0
1 0
2 184
7
Coasting Arc #1 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2008/343/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6077013
16 A = 6738436
37 meter
Y = 2859544
43 meter E =
0014751
Z = -501665
76 I = 51
53643
XDOT = -2439
446111 Wp = 116
27791
YDOT = 4156
807094 meter/sec RA = 201
79758 deg
ZDOT = -5998
802096 TA = 69
18092
MA = 69
02298
Ha = 195
741 n
mi
Hp = 185
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19937707
21 X = 6047022
66
Y = 9381707
45 feet Y = 2927333
46 meter
Z = -1645885
03 Z = -472215
59
XDOT = -8003
432123 XDOT = -2456
605158
YDOT = 13637
818550 feet/sec YDOT = 4129
432330 meter/sec
ZDOT = -19681
109240 ZDOT = -6010
694541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8715372
95 X = -2656445
68
Y = 20246847
63 feet Y = 6171239
16 meter
Z = -1531331
59 Z = -466749
87
XDOT = -12415
232936 XDOT = -3784
162999
YDOT = -6798
247379 feet/sec YDOT = -2072
105801 meter/sec
ZDOT = -19726
931935 ZDOT = -6012
768854
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 08343
57262224
00020000 00000-0 20000-3 0 9007
2 25544 51
6400 202
6317 0006156 71
4671 288
7159 15
71769521 15979
Satellite: ISS
Catalog Number: 25544
Epoch time: 08343
57262224 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 202
6317 deg
Eccentricity:
0006156
Arg of perigee: 71
4671 deg
Mean anomaly: 288
7159 deg
Mean motion: 15
71769521 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1597
Checksum: 288
Coasting Arc #2 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2008/344/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 927979
39 A = 6726450
18 meter
Y = -4083373
15 meter E =
0008457
Z = 5256781
03 I = 51
52312
XDOT = 7432
036268 Wp = 83
52134
YDOT = 2014
759765 meter/sec RA = 196
66798 deg
ZDOT = 253
643127 TA = 4
07193
MA = 4
06505
Ha = 195
703 n
mi
Hp = 185
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3044551
79 X = 948034
24
Y = -13396893
54 feet Y = -4072884
37 meter
Z = 17246656
93 Z = 5261337
56
XDOT = 24383
321089 XDOT = 7407
722341
YDOT = 6610
104217 feet/sec YDOT = 2097
733122 meter/sec
ZDOT = 832
162490 ZDOT = 289
690007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13527983
49 X = 4123329
37
Y = 2267313
15 feet Y = 691077
05 meter
Z = 17264014
05 Z = 5262071
48
XDOT = -5209
369324 XDOT = -1587
815770
YDOT = 23693
466590 feet/sec YDOT = 7221
768617 meter/sec
ZDOT = 972
264975 ZDOT = 296
346364
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 08344
58988147
00020000 00000-0 20000-3 0 9019
2 25544 51
6392 197
4238 0006180 75
0248 285
1598 15
71782073 16133
Satellite: ISS
Catalog Number: 25544
Epoch time: 08344
58988147 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 197
4238 deg
Eccentricity:
0006180
Arg of perigee: 75
0248 deg
Mean anomaly: 285
1598 deg
Mean motion: 15
71782073 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1613
Checksum: 314
Coasting Arc #3 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2008/345/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6641300
04 A = 6737987
32 meter
Y = -597139
29 meter E =
0015094
Z = -936419
27 I = 51
58951
XDOT = -387
417224 Wp = 53
81373
YDOT = -4882
980654 meter/sec RA = 191
53083 deg
ZDOT = 5936
504756 TA = 295
96336
MA = 296
11880
Ha = 195
626 n
mi
Hp = 184
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21789042
11 X = -6629580
06
Y = -1959118
40 feet Y = -671340
49 meter
Z = -3072241
69 Z = -968655
11
XDOT = -1271
053885 XDOT = -361
625311
YDOT = -16020
277737 feet/sec YDOT = -4887
169588 meter/sec
ZDOT = 19476
721642 ZDOT = 5934
684613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 485023
15 X = 147835
06
Y = -21853609
50 feet Y = -6660980
18 meter
Z = -3197448
07 Z = -974582
17
XDOT = 14296
575356 XDOT = 4357
596168
YDOT = -2496
670294 feet/sec YDOT = -760
985106 meter/sec
ZDOT = 19469
262676 ZDOT = 5934
231264
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 08345
54354845
00020000 00000-0 20000-3 0 9029
2 25544 51
6378 192
5412 0006090 78
2578 281
9267 15
71814199 16286
Satellite: ISS
Catalog Number: 25544
Epoch time: 08345
54354845 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 192
5412 deg
Eccentricity:
0006090
Arg of perigee: 78
2578 deg
Mean anomaly: 281
9267 deg
Mean motion: 15
71814199 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1628
Checksum: 317
Coasting Arc #4 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2008/346/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1577215
62 A = 6727405
52 meter
Y = 4195619
34 meter E =
0019383
Z = -5034058
66 I = 51
58195
XDOT = -7438
440415 Wp = 78
58689
YDOT = 614
478255 meter/sec RA = 186
43190 deg
ZDOT = -1820
545617 TA = 173
82020
MA = 173
79625
Ha = 195
664 n
mi
Hp = 184
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5174591
94 X = 1554637
34
Y = 13765155
30 feet Y = 4213131
29 meter
Z = -16515940
47 Z = -5026450
51
XDOT = -24404
332069 XDOT = -7435
914703
YDOT = 2016
004773 feet/sec YDOT = 531
311746 meter/sec
ZDOT = -5972
918691 ZDOT = -1856
676070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13269459
05 X = -4044531
12
Y = 6415865
94 feet Y = 1955555
94 meter
Z = -16486064
19 Z = -5024952
37
XDOT = -3603
915443 XDOT = -1098
473427
YDOT = -23143
811199 feet/sec YDOT = -7054
233654 meter/sec
ZDOT = -6113
169818 ZDOT = -1863
294160
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 08346
56078105
00020000 00000-0 20000-3 0 9035
2 25544 51
6367 187
3333 0006200 82
7957 277
3910 15
71846267 16445
Satellite: ISS
Catalog Number: 25544
Epoch time: 08346
56078105 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 187
3333 deg
Eccentricity:
0006200
Arg of perigee: 82
7957 deg
Mean anomaly: 277
3910 deg
Mean motion: 15
71846267 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 302
Coasting Arc #5 (Orbit 1659)
---------------------------------------
Vector Time (GMT): 2008/347/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6137266
67 A = 6735930
82 meter
Y = -1625914
80 meter E =
0019631
Z = 2226499
80 I = 51
64105
XDOT = 3164
091354 Wp = 101
41555
YDOT = 4401
303573 meter/sec RA = 181
27531 deg
ZDOT = -5470
886074 TA = 53
62188
MA = 53
44092
Ha = 195
457 n
mi
Hp = 184
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20135389
34 X = 6144175
70
Y = -5334366
15 feet Y = -1557246
14 meter
Z = 7304789
39 Z = 2256331
53
XDOT = 10380
877146 XDOT = 3141
217024
YDOT = 14439
972353 feet/sec YDOT = 4436
559423 meter/sec
ZDOT = -17949
101294 ZDOT = -5455
569427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7351740
52 X = 2240810
51
Y = 19445747
12 feet Y = 5927063
72 meter
Z = 7420521
83 Z = 2261775
06
XDOT = -11879
670836 XDOT = -3620
923671
YDOT = 11363
125443 feet/sec YDOT = 3463
480635 meter/sec
ZDOT = -17889
268537 ZDOT = -5452
649050
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 08347
57799771
00020000 00000-0 20000-3 0 9047
2 25544 51
6369 182
1251 0005983 84
7642 275
4202 15
71906076 16605
Satellite: ISS
Catalog Number: 25544
Epoch time: 08347
57799771 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 182
1251 deg
Eccentricity:
0005983
Arg of perigee: 84
7642 deg
Mean anomaly: 275
4202 deg
Mean motion: 15
71906076 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1660
Checksum: 314
Coasting Arc #6 (Orbit 1675)
---------------------------------------
Vector Time (GMT): 2008/348/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3852539
96 A = 6729698
93 meter
Y = -3263632
10 meter E =
0015076
Z = 4438499
68 I = 51
64822
XDOT = 6305
690968 Wp = 103
17029
YDOT = -2999
872888 meter/sec RA = 176
19915 deg
ZDOT = 3254
815481 TA = 314
17129
MA = 314
29511
Ha = 195
645 n
mi
Hp = 184
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12639566
80 X = -3837320
70
Y = -10707454
40 feet Y = -3306629
19 meter
Z = 14562006
81 Z = 4419820
28
XDOT = 20687
962493 XDOT = 6322
955999
YDOT = -9842
102651 feet/sec YDOT = -2929
263100 meter/sec
ZDOT = 10678
528481 ZDOT = 3285
490050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9118817
89 X = 2779415
69
Y = -13905781
74 feet Y = -4238482
28 meter
Z = 14489191
34 Z = 4416305
52
XDOT = 11210
233499 XDOT = 3416
879171
YDOT = 18644
948291 feet/sec YDOT = 5682
980239 meter/sec
ZDOT = 10797
447973 ZDOT = 3291
062142
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 08348
59520371
00020000 00000-0 20000-3 0 9059
2 25544 51
6360 176
9167 0006085 90
3162 269
8698 15
71895213 16760
Satellite: ISS
Catalog Number: 25544
Epoch time: 08348
59520371 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 176
9167 deg
Eccentricity:
0006085
Arg of perigee: 90
3162 deg
Mean anomaly: 269
8698 deg
Mean motion: 15
71895213 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1676
Checksum: 321
Coasting Arc #7 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2008/349/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4678048
27 A = 6733045
51 meter
Y = 3457960
33 meter E =
0011233
Z = -3400409
15 I = 51
68977
XDOT = -5448
651217 Wp = 93
81193
YDOT = -2837
486786 meter/sec RA = 171
03207 deg
ZDOT = 4622
720978 TA = 226
16259
MA = 226
25549
Ha = 195
580 n
mi
Hp = 184
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15347927
39 X = -4699849
52
Y = 11345014
21 feet Y = 3405526
39 meter
Z = -11156197
99 Z = -3423187
41
XDOT = -17876
152287 XDOT = -5438
973315
YDOT = -9309
339849 feet/sec YDOT = -2898
363455 meter/sec
ZDOT = 15166
407408 ZDOT = 4596
274485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13317257
79 X = -4059100
17
Y = -13599359
44 feet Y = -4145084
76 meter
Z = -11244422
79 Z = -3427300
07
XDOT = 5789
108728 XDOT = 1764
520340
YDOT = -18090
745414 feet/sec YDOT = -5514
059202 meter/sec
ZDOT = 15063
436223 ZDOT = 4591
335361
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 08349
54882114
00020000 00000-0 20000-3 0 9062
2 25544 51
6365 172
0337 0006273 94
7469 265
4410 15
71907825 16912
Satellite: ISS
Catalog Number: 25544
Epoch time: 08349
54882114 = yrday
fracday
Element set: 906
Inclination: 51
6365 deg
RA of node: 172
0337 deg
Eccentricity:
0006273
Arg of perigee: 94
7469 deg
Mean anomaly: 265
4410 deg
Mean motion: 15
71907825 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1691
Checksum: 306
Coasting Arc #8 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2008/350/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5475502
60 A = 6732502
33 meter
Y = 1562083
82 meter E =
0011597
Z = -3602200
95 I = 51
71750
XDOT = -4229
301861 Wp = 90
78910
YDOT = 4654
846056 meter/sec RA = 165
96826 deg
ZDOT = -4422
539762 TA = 132
13963
MA = 132
04103
Ha = 195
586 n
mi
Hp = 184
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17964247
38 X = 5475126
91
Y = 5124946
91 feet Y = 1623312
48 meter
Z = -11818244
57 Z = -3575601
79
XDOT = -13875
662275 XDOT = -4259
555013
YDOT = 15271
804647 feet/sec YDOT = 4607
383053 meter/sec
ZDOT = -14509
644890 ZDOT = -4443
158391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2306256
42 X = -702946
96
Y = 18603646
03 feet Y = 5670391
31 meter
Z = -11714764
42 Z = -3570660
20
XDOT = -15845
006492 XDOT = -4829
557979
YDOT = -11125
457790 feet/sec YDOT = -3391
039534 meter/sec
ZDOT = -14589
394620 ZDOT = -4446
847480
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 08350
56599879
00020000 00000-0 20000-3 0 9070
2 25544 51
6372 166
8258 0006336 97
1657 263
0225 15
71946797 17076
Satellite: ISS
Catalog Number: 25544
Epoch time: 08350
56599879 = yrday
fracday
Element set: 907
Inclination: 51
6372 deg
RA of node: 166
8258 deg
Eccentricity:
0006336
Arg of perigee: 97
1657 deg
Mean anomaly: 263
0225 deg
Mean motion: 15
71946797 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1707
Checksum: 338
Coasting Arc #9 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2008/351/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2592627
87 A = 6730033
06 meter
Y = -4482482
50 meter E =
0015494
Z = 4286538
78 I = 51
73715
XDOT = 6827
814525 Wp = 83
83108
YDOT = 566
504525 meter/sec RA = 160
80397 deg
ZDOT = -3524
788154 TA = 41
86478
MA = 41
74639
Ha = 195
516 n
mi
Hp = 184
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8505996
94 X = 2621735
94
Y = -14706307
40 feet Y = -4453327
98 meter
Z = 14063447
43 Z = 4299203
86
XDOT = 22400
966291 XDOT = 6838
094991
YDOT = 1858
610645 feet/sec YDOT = 642
914993 meter/sec
ZDOT = -11564
265597 ZDOT = -3491
593807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15923986
54 X = 4853631
10
Y = 5803222
74 feet Y = 1768822
29 meter
Z = 14112309
28 Z = 4301431
87
XDOT = 2409
810094 XDOT = 734
510117
YDOT = 21294
961255 feet/sec YDOT = 6490
704191 meter/sec
ZDOT = -11435
221094 ZDOT = -3485
455390
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 08351
58316332
00020000 00000-0 20000-3 0 9085
2 25544 51
6368 161
6172 0006295 102
0838 258
1029 15
71929751 17236
Satellite: ISS
Catalog Number: 25544
Epoch time: 08351
58316332 = yrday
fracday
Element set: 908
Inclination: 51
6368 deg
RA of node: 161
6172 deg
Eccentricity:
0006295
Arg of perigee: 102
0838 deg
Mean anomaly: 258
1029 deg
Mean motion: 15
71929751 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1723
Checksum: 293
Coasting Arc #10 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2008/352/04:07:29
058
Vector Time (MET): N/A
Weight (LBS) : 640263
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1113587
03 A = 6726810
68 meter
Y = -4028839
84 meter E =
0009747
Z = 5262172
41 I = 51
74387
XDOT = 7240
626626 Wp = 89
78163
YDOT = -2595
711008 meter/sec RA = 157
60825 deg
ZDOT = -454
309391 TA = 4
52892
MA = 4
52011
Ha = 196
396 n
mi
Hp = 184
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3653500
76 X = -1094015
66
Y = -13217978
47 feet Y = -4041183
72 meter
Z = 17264345
18 Z = 5256809
76
XDOT = 23755
336700 XDOT = 7271
321093
YDOT = -8516
112230 feet/sec YDOT = -2514
570462 meter/sec
ZDOT = -1490
516376 ZDOT = -419
060326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3988163
56 X = -1215592
25
Y = 13148683
19 feet Y = 4007718
64 meter
Z = 17243181
81 Z = 5255721
82
XDOT = -23636
876345 XDOT = -7204
519910
YDOT = -5390
824833 feet/sec YDOT = -1643
123409 meter/sec
ZDOT = -1353
730604 ZDOT = -412
617088
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 08352
21889572
00020000 00000-0 20000-3 0 9098
2 25544 51
6397 158
3673 0007299 95
9092 264
2902 15
71665069 17332
Satellite: ISS
Catalog Number: 25544
Epoch time: 08352
21889572 = yrday
fracday
Element set: 909
Inclination: 51
6397 deg
RA of node: 158
3673 deg
Eccentricity:
0007299
Arg of perigee: 95
9092 deg
Mean anomaly: 264
2902 deg
Mean motion: 15
71665069 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1733
Checksum: 332
Coasting Arc #11 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2008/353/04:07:29
058
Vector Time (MET): N/A
Weight (LBS) : 640263
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5818688
71 A = 6738808
98 meter
Y = 3369179
32 meter E =
0016559
Z = -383570
05 I = 51
81086
XDOT = -2675
604747 Wp = 64
10061
YDOT = -3957
631229 meter/sec RA = 152
49996 deg
ZDOT = 6033
340964 TA = 291
74388
MA = 291
92005
Ha = 196
378 n
mi
Hp = 184
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19090186
05 X = -5854067
66
Y = 11053737
94 feet Y = 3303913
60 meter
Z = -1258431
92 Z = -411922
82
XDOT = -8778
230798 XDOT = -2660
459816
YDOT = -12984
354427 feet/sec YDOT = -3987
467226 meter/sec
ZDOT = 19794
425736 ZDOT = 6020
379356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22043716
11 X = 6718924
67
Y = 637290
68 feet Y = 194246
20 meter
Z = -1368363
03 Z = -417077
05
XDOT = 778
691494 XDOT = 237
345167
YDOT = 14112
567312 feet/sec YDOT = 4301
510517 meter/sec
ZDOT = 19743
730573 ZDOT = 6017
889079
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 08353
17266745
00020000 00000-0 20000-3 0 9107
2 25544 51
6398 153
4860 0007359 98
7485 261
4511 15
71644220 17488
Satellite: ISS
Catalog Number: 25544
Epoch time: 08353
17266745 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 153
4860 deg
Eccentricity:
0007359
Arg of perigee: 98
7485 deg
Mean anomaly: 261
4511 deg
Mean motion: 15
71644220 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1748
Checksum: 307
Coasting Arc #12 (Orbit 1763)
---------------------------------------
Vector Time (GMT): 2008/354/04:07:29
058
Vector Time (MET): N/A
Weight (LBS) : 640263
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3388949
86 A = 6727263
78 meter
Y = 2671073
92 meter E =
0021178
Z = -5179320
29 I = 51
79867
XDOT = -5788
263385 Wp = 87
97921
YDOT = 4887
388158 meter/sec RA = 147
40814 deg
ZDOT = -1270
600777 TA = 169
89112
MA = 169
84846
Ha = 196
329 n
mi
Hp = 184
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11118601
92 X = 3383989
84
Y = 8763365
87 feet Y = 2708943
80 meter
Z = -16992520
65 Z = -5162868
59
XDOT = -18990
365437 XDOT = -5836
312405
YDOT = 16034
738050 feet/sec YDOT = 4822
391890 meter/sec
ZDOT = -4168
637720 ZDOT = -1298
836525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5158201
26 X = -1572219
75
Y = -13266093
98 feet Y = -4043505
44 meter
Z = -16928359
59 Z = -5159764
00
XDOT = 23530
762996 XDOT = 7172
176561
YDOT = -3706
024892 feet/sec YDOT = -1129
596387 meter/sec
ZDOT = -4278
002345 ZDOT = -1303
935115
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 08354
19000917
00020000 00000-0 20000-3 0 9118
2 25544 51
6406 148
2791 0007401 102
3488 257
8503 15
71690065 17642
Satellite: ISS
Catalog Number: 25544
Epoch time: 08354
19000917 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 148
2791 deg
Eccentricity:
0007401
Arg of perigee: 102
3488 deg
Mean anomaly: 257
8503 deg
Mean motion: 15
71690065 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1764
Checksum: 282
Coasting Arc #13 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2008/355/04:07:29
058
Vector Time (MET): N/A
Weight (LBS) : 640263
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4120264
93 A = 6737302
45 meter
Y = -4996490
76 meter E =
0021437
Z = 1822220
28 I = 51
85642
XDOT = 4838
627483 Wp = 111
41960
YDOT = 1900
522250 meter/sec RA = 142
27601 deg
ZDOT = -5683
992504 TA = 48
43565
MA = 48
25205
Ha = 196
296 n
mi
Hp = 184
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13517929
56 X = 4166978
22
Y = -16392686
23 feet Y = -4950154
54 meter
Z = 5978413
00 Z = 1842349
69
XDOT = 15874
762084 XDOT = 4844
627864
YDOT = 6235
309218 feet/sec YDOT = 1954
664607 meter/sec
ZDOT = -18648
269371 ZDOT = -5660
471594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19842660
54 X = -6048042
93
Y = 7535677
58 feet Y = 2296874
53 meter
Z = 6056268
63 Z = 1845950
68
XDOT = -10228
043713 XDOT = -3117
507724
YDOT = -11899
915802 feet/sec YDOT = -3627
094336 meter/sec
ZDOT = -18556
686533 ZDOT = -5656
078055
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 08355
20733713
00020000 00000-0 20000-3 0 9129
2 25544 51
6404 143
0725 0007375 106
2587 253
9386 15
71685605 17801
Satellite: ISS
Catalog Number: 25544
Epoch time: 08355
20733713 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 143
0725 deg
Eccentricity:
0007375
Arg of perigee: 106
2587 deg
Mean anomaly: 253
9386 deg
Mean motion: 15
71685605 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1780
Checksum: 292
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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