Date:
August 26th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 3866)
---------------------------------------
Vector Time (GMT): 2008/233/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1666202
79 A = 6729260
65 meter
Y = 4031735
26 meter E =
0009573
Z = 5115318
34 I = 51
85441
XDOT = -6091
011011 Wp = 65
35706
YDOT = -4460
347614 meter/sec RA = 45
39248 deg
ZDOT = 1533
174785 TA = 9
99359
MA = 9
97457
Ha = 197
287 n
mi
Hp = 186
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5466544
57 X = -1736011
68
Y = 13227477
89 feet Y = 4012712
62 meter
Z = 16782540
50 Z = 5107054
30
XDOT = -19983
631927 XDOT = -6048
129857
YDOT = -14633
686398 feet/sec YDOT = -4528
221010 meter/sec
ZDOT = 5030
101002 ZDOT = 1503
689003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8426428
13 X = 2568375
29
Y = -11614808
24 feet Y = -3540193
55 meter
Z = 16750954
74 Z = 5105691
00
XDOT = 15310
292121 XDOT = 4666
577039
YDOT = 18189
012796 feet/sec YDOT = 5544
011100 meter/sec
ZDOT = 4915
740384 ZDOT = 1498
317669
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 08233
60126787
00020000 00000-0 20000-3 0 9002
2 25544 51
6390 45
6923 0008287 36
4855 323
6870 15
71047972 38677
Satellite: ISS
Catalog Number: 25544
Epoch time: 08233
60126787 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 45
6923 deg
Eccentricity:
0008287
Arg of perigee: 36
4855 deg
Mean anomaly: 323
6870 deg
Mean motion: 15
71047972 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3867
Checksum: 311
Coasting Arc #2 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2008/234/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5794533
19 A = 6738385
99 meter
Y = 2582970
86 meter E =
0014326
Z = -2259609
89 I = 51
86533
XDOT = -281
543330 Wp = 41
42456
YDOT = 5397
478281 meter/sec RA = 40
26307 deg
ZDOT = 5478
050842 TA = 293
32525
MA = 293
47593
Ha = 197
309 n
mi
Hp = 186
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19010935
65 X = 5776196
12
Y = 8474313
83 feet Y = 2647666
12 meter
Z = -7413418
28 Z = -2231504
57
XDOT = -923
698590 XDOT = -368
489288
YDOT = 17708
262076 feet/sec YDOT = 5393
843805 meter/sec
ZDOT = 17972
607748 ZDOT = 5476
471868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16838980
39 X = -5132521
22
Y = -12299614
61 feet Y = -3748922
53 meter
Z = -7304564
31 Z = -2226431
20
XDOT = 3838
804163 XDOT = 1170
067509
YDOT = -15866
270498 feet/sec YDOT = -4836
039248 meter/sec
ZDOT = 17966
975420 ZDOT = 5476
334108
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 08234
55539571
00020000 00000-0 20000-3 0 9017
2 25544 51
6406 40
8142 0008269 40
8167 319
3613 15
71065571 38829
Satellite: ISS
Catalog Number: 25544
Epoch time: 08234
55539571 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 40
8142 deg
Eccentricity:
0008269
Arg of perigee: 40
8167 deg
Mean anomaly: 319
3613 deg
Mean motion: 15
71065571 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3882
Checksum: 288
Coasting Arc #3 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2008/235/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1232033
57 A = 6732383
65 meter
Y = -5028171
91 meter E =
0016721
Z = -4321593
56 I = 51
82278
XDOT = 6701
991449 Wp = 56
68065
YDOT = 1363
353593 meter/sec RA = 35
20856 deg
ZDOT = -3497
643145 TA = 177
92770
MA = 177
92076
Ha = 197
279 n
mi
Hp = 185
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4042104
88 X = -1154722
59
Y = -16496627
01 feet Y = -5041516
89 meter
Z = -14178456
55 Z = -4327391
09
XDOT = 21988
160923 XDOT = 6703
239077
YDOT = 4472
944860 feet/sec YDOT = 1438
306152 meter/sec
ZDOT = -11475
207169 ZDOT = -3465
081712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 686749
11 X = 209321
13
Y = 16951622
61 feet Y = 5166854
57 meter
Z = -14201296
12 Z = -4328555
06
XDOT = -19531
325197 XDOT = -5953
147920
YDOT = -8714
623623 feet/sec YDOT = -2656
217280 meter/sec
ZDOT = -11349
238861 ZDOT = -3459
248005
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 08235
57312074
00020000 00000-0 20000-3 0 9028
2 25544 51
6410 35
6107 0008330 44
0774 316
1050 15
71089505 38986
Satellite: ISS
Catalog Number: 25544
Epoch time: 08235
57312074 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 35
6107 deg
Eccentricity:
0008330
Arg of perigee: 44
0774 deg
Mean anomaly: 316
1050 deg
Mean motion: 15
71089505 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3898
Checksum: 266
Coasting Arc #4 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2008/236/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5568082
91 A = 6734420
59 meter
Y = 207636
55 meter E =
0019044
Z = 3772985
62 I = 51
80465
XDOT = -3094
476313 Wp = 68
42557
YDOT = -5638
253104 meter/sec RA = 30
05699 deg
ZDOT = -4232
585735 TA = 66
05983
MA = 65
86050
Ha = 197
414 n
mi
Hp = 185
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18267988
54 X = -5588319
42
Y = 681222
27 feet Y = 145257
73 meter
Z = 12378561
76 Z = 3745886
67
XDOT = -10152
481341 XDOT = -3010
637289
YDOT = -18498
205721 feet/sec YDOT = -5672
388370 meter/sec
ZDOT = -13886
436140 ZDOT = -4247
415334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18169510
15 X = 5538066
69
Y = 2575660
29 feet Y = 785061
26 meter
Z = 12273839
47 Z = 3741066
27
XDOT = 6827
176527 XDOT = 2080
923406
YDOT = 18664
229702 feet/sec YDOT = 5688
857213 meter/sec
ZDOT = -13944
230992 ZDOT = -4250
201606
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 08236
59083479
00020000 00000-0 20000-3 0 9036
2 25544 51
6409 30
4061 0008296 48
1779 312
0090 15
71085603 39140
Satellite: ISS
Catalog Number: 25544
Epoch time: 08236
59083479 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 30
4061 deg
Eccentricity:
0008296
Arg of perigee: 48
1779 deg
Mean anomaly: 312
0090 deg
Mean motion: 15
71085603 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3914
Checksum: 288
Coasting Arc #5 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2008/237/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4070978
41 A = 6736450
18 meter
Y = 4464515
54 meter E =
0020745
Z = 2953634
26 I = 51
78773
XDOT = -5579
432661 Wp = 70
64853
YDOT = 1754
899930 meter/sec RA = 25
00463 deg
ZDOT = 5015
816824 TA = 323
33524
MA = 323
47702
Ha = 197
212 n
mi
Hp = 185
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13356228
38 X = 4006404
72
Y = 14647360
69 feet Y = 4509678
32 meter
Z = 9690401
12 Z = 2973254
49
XDOT = -18305
225266 XDOT = -5623
007458
YDOT = 5757
545702 feet/sec YDOT = 1692
263544 meter/sec
ZDOT = 16456
091943 ZDOT = 4988
606240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10784659
06 X = -3287164
08
Y = -16587414
75 feet Y = -5055844
02 meter
Z = 9766610
79 Z = 2976862
97
XDOT = 17873
851643 XDOT = 5447
949981
YDOT = -1952
029848 feet/sec YDOT = -594
978698 meter/sec
ZDOT = 16351
064028 ZDOT = 4983
804316
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 08237
60853460
00020000 00000-0 20000-3 0 9045
2 25544 51
6422 25
2026 0008245 51
6205 308
5696 15
71154411 39309
Satellite: ISS
Catalog Number: 25544
Epoch time: 08237
60853460 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 25
2026 deg
Eccentricity:
0008245
Arg of perigee: 51
6205 deg
Mean anomaly: 308
5696 deg
Mean motion: 15
71154411 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3930
Checksum: 266
Coasting Arc #6 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2008/238/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3860784
02 A = 6730275
20 meter
Y = -2664712
32 meter E =
0018105
Z = -4840955
49 I = 51
73968
XDOT = 5952
008569 Wp = 85
64440
YDOT = 4199
322677 meter/sec RA = 19
85767 deg
ZDOT = 2444
523784 TA = 208
20907
MA = 208
30726
Ha = 197
353 n
mi
Hp = 185
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12666614
23 X = 3913810
65
Y = -8742494
47 feet Y = -2621241
97 meter
Z = -15882399
91 Z = -4822071
32
XDOT = 19527
587168 XDOT = 5892
733728
YDOT = 13777
305370 feet/sec YDOT = 4265
549863 meter/sec
ZDOT = 8020
091155 ZDOT = 2473
294777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13876739
81 X = -4229630
29
Y = 6827645
69 feet Y = 2081066
41 meter
Z = -15809626
79 Z = -4818774
25
XDOT = -16812
215536 XDOT = -5124
363295
YDOT = -15410
623064 feet/sec YDOT = -4697
157910 meter/sec
ZDOT = 8131
650785 ZDOT = 2478
527159
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 08238
56262010
00020000 00000-0 20000-3 0 9057
2 25544 51
6422 20
3249 0008356 54
5137 305
6803 15
71147166 39454
Satellite: ISS
Catalog Number: 25544
Epoch time: 08238
56262010 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 20
3249 deg
Eccentricity:
0008356
Arg of perigee: 54
5137 deg
Mean anomaly: 305
6803 deg
Mean motion: 15
71147166 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3945
Checksum: 273
Coasting Arc #7 (Orbit 3960)
---------------------------------------
Vector Time (GMT): 2008/239/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6062946
43 A = 6739482
17 meter
Y = -2648346
58 meter E =
0012780
Z = -1285742
76 I = 51
74339
XDOT = 2975
986406 Wp = 101
23509
YDOT = -3993
263799 meter/sec RA = 14
78152 deg
ZDOT = -5859
538979 TA = 92
82492
MA = 92
67865
Ha = 197
343 n
mi
Hp = 185
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19891556
53 X = -6026635
76
Y = -8688801
12 feet Y = -2715942
83 meter
Z = -4218316
13 Z = -1315108
16
XDOT = 9763
734928 XDOT = 3048
882766
YDOT = -13101
259182 feet/sec YDOT = -3959
576646 meter/sec
ZDOT = -19224
209250 ZDOT = -5844
905009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18613863
71 X = 5673505
66
Y = 11122989
71 feet Y = 3390287
26 meter
Z = -4332049
71 Z = -1320408
75
XDOT = -10634
671457 XDOT = -3241
447860
YDOT = 10395
393761 feet/sec YDOT = 3168
516018 meter/sec
ZDOT = -19167
972438 ZDOT = -5842
397999
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 08239
58029807
00020000 00000-0 20000-3 0 9066
2 25544 51
6425 15
1198 0008417 57
9120 302
2858 15
71169786 39612
Satellite: ISS
Catalog Number: 25544
Epoch time: 08239
58029807 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 15
1198 deg
Eccentricity:
0008417
Arg of perigee: 57
9120 deg
Mean anomaly: 302
2858 deg
Mean motion: 15
71169786 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3961
Checksum: 310
Coasting Arc #8 (Orbit 3976)
---------------------------------------
Vector Time (GMT): 2008/240/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1156143
66 A = 6728138
95 meter
Y = 4021122
54 meter E =
0011076
Z = 5260836
19 I = 51
67771
XDOT = -7522
186683 Wp = 62
33138
YDOT = -1612
546003 meter/sec RA = 9
65675 deg
ZDOT = -414
843890 TA = 31
63742
MA = 31
57090
Ha = 197
386 n
mi
Hp = 185
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3793122
24 X = -1226578
32
Y = 13192659
25 feet Y = 4007799
83 meter
Z = 17259961
24 Z = 5255048
82
XDOT = -24679
090168 XDOT = -7501
580670
YDOT = -5290
505258 feet/sec YDOT = -1696
548193 meter/sec
ZDOT = -1361
036386 ZDOT = -451
336068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5305715
58 X = 1617182
11
Y = -12690296
21 feet Y = -3868002
28 meter
Z = 17237925
07 Z = 5254119
56
XDOT = 23022
435667 XDOT = 7017
238391
YDOT = 7559
435694 feet/sec YDOT = 2304
116000 meter/sec
ZDOT = -1502
238820 ZDOT = -457
882392
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 08240
59796333
00020000 00000-0 20000-3 0 9075
2 25544 51
6433 9
9158 0008425 60
6944 299
5058 15
71205013 39773
Satellite: ISS
Catalog Number: 25544
Epoch time: 08240
59796333 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 9
9158 deg
Eccentricity:
0008425
Arg of perigee: 60
6944 deg
Mean anomaly: 299
5058 deg
Mean motion: 15
71205013 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3977
Checksum: 310
Coasting Arc #9 (Orbit 3991)
---------------------------------------
Vector Time (GMT): 2008/241/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6708206
87 A = 6740088
89 meter
Y = 80433
28 meter E =
0019218
Z = -571288
06 I = 51
68910
XDOT = 441
597139 Wp = 50
54380
YDOT = 4795
300535 meter/sec RA = 4
54467 deg
ZDOT = 6006
157723 TA = 303
24836
MA = 303
43239
Ha = 197
468 n
mi
Hp = 185
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22008552
71 X = 6709584
04
Y = 263888
71 feet Y = 155456
02 meter
Z = -1874304
64 Z = -538696
87
XDOT = 1448
809511 XDOT = 358
766232
YDOT = 15732
613305 feet/sec YDOT = 4799
775522 meter/sec
ZDOT = 19705
241873 ZDOT = 6008
101828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21901694
59 X = -6675636
51
Y = -2284346
93 feet Y = -696268
94 meter
Z = -1748307
97 Z = -532884
27
XDOT = -52
504582 XDOT = -16
003397
YDOT = -14191
790219 feet/sec YDOT = -4325
657659 meter/sec
ZDOT = 19713
162156 ZDOT = 6008
571825
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 08241
55201468
00020000 00000-0 20000-3 0 9083
2 25544 51
6438 5
0374 0008533 63
8711 296
3327 15
71180086 39925
Satellite: ISS
Catalog Number: 25544
Epoch time: 08241
55201468 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 5
0374 deg
Eccentricity:
0008533
Arg of perigee: 63
8711 deg
Mean anomaly: 296
3327 deg
Mean motion: 15
71180086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3992
Checksum: 290
Coasting Arc #10 (Orbit 4007)
---------------------------------------
Vector Time (GMT): 2008/242/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1882357
79 A = 6728958
28 meter
Y = -4009372
17 meter E =
0021992
Z = -5085263
90 I = 51
62284
XDOT = 7374
221080 Wp = 73
49512
YDOT = -1374
215195 meter/sec RA = 359
45080 deg
ZDOT = -1645
915103 TA = 180
63733
MA = 180
64014
Ha = 197
389 n
mi
Hp = 185
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6175714
55 X = -1812681
61
Y = -13154108
17 feet Y = -4030032
29 meter
Z = -16683936
68 Z = -5094238
92
XDOT = 24193
638715 XDOT = 7397
035120
YDOT = -4508
580035 feet/sec YDOT = -1291
624875 meter/sec
ZDOT = -5399
983935 ZDOT = -1610
036364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5080941
08 X = 1548670
84
Y = 13571429
05 feet Y = 4136571
57 meter
Z = -16718974
44 Z = -5095943
41
XDOT = -23503
533227 XDOT = -7163
876928
YDOT = 2316
714927 feet/sec YDOT = 706
134710 meter/sec
ZDOT = -5261
403345 ZDOT = -1603
675740
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 08242
56965681
00020000 00000-0 20000-3 0 9090
2 25544 51
6440 359
8336 0008397 67
5941 292
6109 15
71199298 40081
Satellite: ISS
Catalog Number: 25544
Epoch time: 08242
56965681 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 359
8336 deg
Eccentricity:
0008397
Arg of perigee: 67
5941 deg
Mean anomaly: 292
6109 deg
Mean motion: 15
71199298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4008
Checksum: 333
Coasting Arc #11 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2008/243/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5868397
73 A = 6737943
76 meter
Y = 2391137
66 meter E =
0021511
Z = 2268836
28 I = 51
62358
XDOT = -3735
313209 Wp = 94
09829
YDOT = -3960
544490 meter/sec RA = 354
30255 deg
ZDOT = -5444
745516 TA = 60
43527
MA = 60
22104
Ha = 197
490 n
mi
Hp = 185
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19253273
38 X = -5905721
09
Y = 7844939
84 feet Y = 2325305
27 meter
Z = 7443688
59 Z = 2240237
28
XDOT = -12254
964595 XDOT = -3664
298957
YDOT = -12993
912368 feet/sec YDOT = -4001
918076 meter/sec
ZDOT = -17863
338308 ZDOT = -5462
718739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19714755
10 X = 6009057
35
Y = -6722398
79 feet Y = -2048987
15 meter
Z = 7333341
86 Z = 2235202
60
XDOT = 10894
991953 XDOT = 3320
793547
YDOT = 12233
657004 feet/sec YDOT = 3728
818655 meter/sec
ZDOT = -17933
158482 ZDOT = -5466
026705
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 08243
58728741
00020000 00000-0 20000-3 0 9109
2 25544 51
6437 354
6297 0008587 71
7867 288
4229 15
71219642 40241
Satellite: ISS
Catalog Number: 25544
Epoch time: 08243
58728741 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 354
6297 deg
Eccentricity:
0008587
Arg of perigee: 71
7867 deg
Mean anomaly: 288
4229 deg
Mean motion: 15
71219642 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4024
Checksum: 322
Coasting Arc #12 (Orbit 4039)
---------------------------------------
Vector Time (GMT): 2008/244/13:13:25
434
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4468949
17 A = 6731852
01 meter
Y = 2613114
52 meter E =
0017397
Z = 4288758
96 I = 51
57544
XDOT = -5650
219187 Wp = 92
38349
YDOT = 3899
937058 meter/sec RA = 349
22943 deg
ZDOT = 3498
523242 TA = 322
13684
MA = 322
25907
Ha = 197
267 n
mi
Hp = 184
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14661906
74 X = 4418562
96
Y = 8573210
36 feet Y = 2662807
40 meter
Z = 14070731
50 Z = 4310346
36
XDOT = -18537
464523 XDOT = -5710
403996
YDOT = 12795
069088 feet/sec YDOT = 3836
416736 meter/sec
ZDOT = 11478
094626 ZDOT = 3470
928352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14223568
32 X = -4335343
62
Y = -9154226
44 feet Y = -2790208
22 meter
Z = 14154404
70 Z = 4314262
55
XDOT = 18436
131094 XDOT = 5619
332758
YDOT = -10997
369080 feet/sec YDOT = -3351
998096 meter/sec
ZDOT = 11371
767114 ZDOT = 3466
114616
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 08244
60490338
00020000 00000-0 20000-3 0 9112
2 25544 51
6441 349
4253 0008513 74
8354 285
3749 15
71276829 40405
Satellite: ISS
Catalog Number: 25544
Epoch time: 08244
60490338 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 349
4253 deg
Eccentricity:
0008513
Arg of perigee: 74
8354 deg
Mean anomaly: 285
3749 deg
Mean motion: 15
71276829 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4040
Checksum: 299
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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