Date:
March 22nd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 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 1449)
---------------------------------------
Vector Time (GMT): 2008/081/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2273328
09 A = 6716741
84 meter
Y = -4399568
55 meter E =
0007964
Z = 4533618
89 I = 51
93792
XDOT = 4409
591160 Wp = 61
62527
YDOT = -5498
450010 meter/sec RA = 108
46869 deg
ZDOT = -3116
921285 TA = 59
32345
MA = 59
24498
Ha = 186
290 n
mi
Hp = 180
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7458425
48 X = -2245985
80
Y = -14434280
01 feet Y = -4424836
83 meter
Z = 14874077
73 Z = 4522642
04
XDOT = 14467
162600 XDOT = 4485
889279
YDOT = -18039
534155 feet/sec YDOT = -5448
713176 meter/sec
ZDOT = -10226
119703 ZDOT = -3095
313735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9668543
90 X = 2946972
18
Y = -13105785
78 feet Y = -3994643
51 meter
Z = 14831465
75 Z = 4520630
76
XDOT = 21624
818895 XDOT = 6591
244799
YDOT = 4444
618923 feet/sec YDOT = 1354
719848 meter/sec
ZDOT = -10143
903247 ZDOT = -3091
861710
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 08081
36863897
00020000 00000-0 20000-3 0 9006
2 25544 51
6392 109
1013 0001037 286
8736 73
2315 15
76292337 14500
Satellite: ISS
Catalog Number: 25544
Epoch time: 08081
36863897 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 109
1013 deg
Eccentricity:
0001037
Arg of perigee: 286
8736 deg
Mean anomaly: 73
2315 deg
Mean motion: 15
76292337 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1450
Checksum: 288
Coasting Arc #2 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2008/082/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3751211
38 A = 6720765
70 meter
Y = 4452784
42 meter E =
0011690
Z = 3346584
24 I = 51
95930
XDOT = -2445
051833 Wp = 87
62824
YDOT = -5600
090951 meter/sec RA = 103
38563 deg
ZDOT = 4696
997608 TA = 311
62481
MA = 311
72489
Ha = 186
251 n
mi
Hp = 180
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12307123
96 X = -3816981
37
Y = 14608872
77 feet Y = 4410468
84 meter
Z = 10979607
09 Z = 3328200
68
XDOT = -8021
823598 XDOT = -2405
066135
YDOT = -18373
001807 feet/sec YDOT = -5627
208855 meter/sec
ZDOT = 15410
097140 ZDOT = 4685
217288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18630460
09 X = -5678564
24
Y = -4395707
94 feet Y = -1339811
78 meter
Z = 10909626
21 Z = 3325254
07
XDOT = 12374
259591 XDOT = 3771
674323
YDOT = -14203
233938 feet/sec YDOT = -4329
145704 meter/sec
ZDOT = 15364
268344 ZDOT = 4683
028991
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 08082
38299455
00020000 00000-0 20000-3 0 9013
2 25544 51
6388 103
8740 0001046 286
7718 73
3332 15
76319864 14833
Satellite: ISS
Catalog Number: 25544
Epoch time: 08082
38299455 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 103
8740 deg
Eccentricity:
0001046
Arg of perigee: 286
7718 deg
Mean anomaly: 73
3332 deg
Mean motion: 15
76319864 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1483
Checksum: 308
Coasting Arc #3 (Orbit 1497)
---------------------------------------
Vector Time (GMT): 2008/083/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2042696
25 A = 6720043
94 meter
Y = 5326386
73 meter E =
0004324
Z = -3555779
28 I = 51
96205
XDOT = -4217
590540 Wp = 92
74421
YDOT = 4614
607915 meter/sec RA = 98
20419 deg
ZDOT = 4494
029302 TA = 225
06366
MA = 225
09875
Ha = 186
181 n
mi
Hp = 180
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6701759
35 X = 2000257
31
Y = 17475022
06 feet Y = 5348991
71 meter
Z = -11665942
51 Z = -3545959
42
XDOT = -13837
239304 XDOT = -4290
709566
YDOT = 15139
789748 feet/sec YDOT = 4567
035993 meter/sec
ZDOT = 14744
190624 ZDOT = 4473
362181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12261057
27 X = -3737170
26
Y = 14172082
93 feet Y = 4319650
88 meter
Z = -11627670
84 Z = -3544114
07
XDOT = -18866
302471 XDOT = -5750
448993
YDOT = -4301
851317 feet/sec YDOT = -1311
204281 meter/sec
ZDOT = 14665
464129 ZDOT = 4470
033467
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 08083
33393808
00020000 00000-0 20000-3 0 9027
2 25544 51
6382 98
9740 0001042 294
3702 65
7354 15
76341473 14981
Satellite: ISS
Catalog Number: 25544
Epoch time: 08083
33393808 = yrday
fracday
Element set: 902
Inclination: 51
6382 deg
RA of node: 98
9740 deg
Eccentricity:
0001042
Arg of perigee: 294
3702 deg
Mean anomaly: 65
7354 deg
Mean motion: 15
76341473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1498
Checksum: 300
Coasting Arc #4 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2008/084/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3653090
60 A = 6717113
78 meter
Y = -3513719
54 meter E =
0008677
Z = -4416561
67 I = 51
95444
XDOT = 2262
670391 Wp = 63
85702
YDOT = 6553
033450 meter/sec RA = 93
12275 deg
ZDOT = -3343
214137 TA = 172
67475
MA = 172
66207
Ha = 186
196 n
mi
Hp = 180
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11985205
37 X = 3713565
01
Y = -11527951
26 feet Y = -3472530
79 meter
Z = -14490031
74 Z = -4398667
72
XDOT = 7423
459287 XDOT = 2205
465995
YDOT = 21499
453576 feet/sec YDOT = 6578
015829 meter/sec
ZDOT = -10968
550319 ZDOT = -3332
361470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15928517
94 X = 4855012
27
Y = 4979320
44 feet Y = 1517696
87 meter
Z = -14421806
81 Z = -4395766
72
XDOT = -14826
497558 XDOT = -4519
116456
YDOT = 15795
419275 feet/sec YDOT = 4814
443795 meter/sec
ZDOT = -10926
186562 ZDOT = -3330
301664
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 08084
34826031
00020000 00000-0 20000-3 0 9039
2 25544 51
6377 93
7463 0001050 300
5921 59
5139 15
76339477 15144
Satellite: ISS
Catalog Number: 25544
Epoch time: 08084
34826031 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 93
7463 deg
Eccentricity:
0001050
Arg of perigee: 300
5921 deg
Mean anomaly: 59
5139 deg
Mean motion: 15
76339477 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1514
Checksum: 285
Coasting Arc #5 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2008/085/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1944787
58 A = 6723229
66 meter
Y = -6038355
14 meter E =
0013057
Z = 2209073
47 I = 51
97668
XDOT = 4193
483335 Wp = 106
57444
YDOT = -3376
277615 meter/sec RA = 87
94835 deg
ZDOT = -5514
055207 TA = 48
75137
MA = 48
63895
Ha = 186
161 n
mi
Hp = 180
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6380536
69 X = -1887852
56
Y = -19810876
45 feet Y = -6059784
41 meter
Z = 7247616
38 Z = 2199764
26
XDOT = 13758
147426 XDOT = 4257
712177
YDOT = -11077
026296 feet/sec YDOT = -3329
024862 meter/sec
ZDOT = -18090
732307 ZDOT = -5493
526949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13963332
24 X = 4256023
67
Y = -15450999
74 feet Y = -4709464
72 meter
Z = 7211239
66 Z = 2197985
85
XDOT = 15389
266732 XDOT = 4690
648500
YDOT = 5465
490927 feet/sec YDOT = 1665
881634 meter/sec
ZDOT = -18012
381261 ZDOT = -5490
173809
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 08085
36256349
00020000 00000-0 20000-3 0 9042
2 25544 51
6384 88
5187 0001128 315
4348 44
6725 15
76408671 15308
Satellite: ISS
Catalog Number: 25544
Epoch time: 08085
36256349 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 88
5187 deg
Eccentricity:
0001128
Arg of perigee: 315
4348 deg
Mean anomaly: 44
6725 deg
Mean motion: 15
76408671 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1530
Checksum: 302
Coasting Arc #6 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2008/086/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3717702
55 A = 6714094
54 meter
Y = 2326042
56 meter E =
0004004
Z = 5081691
06 I = 51
94376
XDOT = -2216
858317 Wp = 123
03180
YDOT = -7190
770319 meter/sec RA = 82
85054 deg
ZDOT = 1666
530139 TA = 311
01179
MA = 311
04641
Ha = 186
240 n
mi
Hp = 180
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12197186
86 X = -3768122
50
Y = 7631373
24 feet Y = 2284187
35 meter
Z = 16672214
77 Z = 5063507
81
XDOT = -7273
157207 XDOT = -2144
380994
YDOT = -23591
766137 feet/sec YDOT = -7215
155197 meter/sec
ZDOT = 5467
618566 ZDOT = 1655
936869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12862887
99 X = -3920608
26
Y = -6623241
51 feet Y = -2018764
01 meter
Z = 16602733
33 Z = 5060513
12
XDOT = 16002
556895 XDOT = 4877
579342
YDOT = -17450
843847 feet/sec YDOT = -5319
017205 meter/sec
ZDOT = 5426
199261 ZDOT = 1653
905535
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 08086
37684869
00020000 00000-0 20000-3 0 9057
2 25544 51
6384 83
2910 0001088 315
0582 45
0494 15
76427164 15468
Satellite: ISS
Catalog Number: 25544
Epoch time: 08086
37684869 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 83
2910 deg
Eccentricity:
0001088
Arg of perigee: 315
0582 deg
Mean anomaly: 45
0494 deg
Mean motion: 15
76427164 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1546
Checksum: 307
Coasting Arc #7 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2008/087/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1919705
54 A = 6725182
66 meter
Y = 6406187
25 meter E =
0011313
Z = -653234
42 I = 51
97573
XDOT = -4401
029109 Wp = 34
24105
YDOT = 1927
057298 meter/sec RA = 77
69898 deg
ZDOT = 6023
961127 TA = 318
67008
MA = 318
75564
Ha = 186
264 n
mi
Hp = 180
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6298246
53 X = 1851101
19
Y = 21017674
69 feet Y = 6427270
89 meter
Z = -2143157
54 Z = -644075
21
XDOT = -14439
071879 XDOT = -4451
514113
YDOT = 6322
366463 feet/sec YDOT = 1877
560310 meter/sec
ZDOT = 19763
651991 ZDOT = 6002
458171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14506847
57 X = -4421687
14
Y = 16465545
98 feet Y = 5018698
41 meter
Z = -2107332
92 Z = -642315
07
XDOT = -11857
179217 XDOT = -3614
068225
YDOT = -7953
035231 feet/sec YDOT = -2424
085138 meter/sec
ZDOT = 19681
388015 ZDOT = 5998
887067
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 08087
32772525
00020000 00000-0 20000-3 0 9061
2 25544 51
6383 78
3900 0001234 330
6850 29
4245 15
76396453 15618
Satellite: ISS
Catalog Number: 25544
Epoch time: 08087
32772525 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 78
3900 deg
Eccentricity:
0001234
Arg of perigee: 330
6850 deg
Mean anomaly: 29
4245 deg
Mean motion: 15
76396453 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1561
Checksum: 291
Coasting Arc #8 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2008/088/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4024093
41 A = 6713150
10 meter
Y = -1013815
38 meter E =
0014522
Z = -5289222
93 I = 51
92870
XDOT = 2142
452940 Wp = 87
89698
YDOT = 7387
013123 meter/sec RA = 72
57099 deg
ZDOT = 215
113653 TA = 184
13216
MA = 184
14416
Ha = 186
184 n
mi
Hp = 180
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13202406
21 X = 4060825
11
Y = -3326165
95 feet Y = -968610
34 meter
Z = -17353093
61 Z = -5269584
62
XDOT = 7029
045078 XDOT = 2058
645993
YDOT = 24235
607360 feet/sec YDOT = 7410
502669 meter/sec
ZDOT = 705
753455 ZDOT = 225
318079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10016049
87 X = 3052892
00
Y = 9362183
03 feet Y = 2853593
39 meter
Z = -17277877
22 Z = -5266296
98
XDOT = -15852
755870 XDOT = -4831
919989
YDOT = 18329
860508 feet/sec YDOT = 5586
941483 meter/sec
ZDOT = 745
685641 ZDOT = 227
284983
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 08088
34197483
00020000 00000-0 20000-3 0 9079
2 25544 51
6389 73
1620 0001097 331
2847 28
8257 15
76448457 15771
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
34197483 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 73
1620 deg
Eccentricity:
0001097
Arg of perigee: 331
2847 deg
Mean anomaly: 28
8257 deg
Mean motion: 15
76448457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1577
Checksum: 322
Coasting Arc #9 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2008/089/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1779467
60 A = 6724564
82 meter
Y = -6397882
06 meter E =
0008710
Z = -1035351
41 I = 51
95840
XDOT = 4875
759329 Wp = 139
18288
YDOT = -398
741521 meter/sec RA = 67
44987 deg
ZDOT = -5950
361619 TA = 52
09694
MA = 52
01822
Ha = 186
170 n
mi
Hp = 180
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5838148
29 X = -1702763
69
Y = -20990426
71 feet Y = -6417352
22 meter
Z = -3396822
20 Z = -1043809
70
XDOT = 15996
585724 XDOT = 4908
761490
YDOT = -1308
207089 feet/sec YDOT = -344
033507 meter/sec
ZDOT = -19522
183791 ZDOT = -5926
595044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14183254
63 X = 4323056
01
Y = -16531519
83 feet Y = -5038807
25 meter
Z = -3429946
07 Z = -1045447
56
XDOT = 8859
141196 XDOT = 2700
266236
YDOT = 11609
106667 feet/sec YDOT = 3538
455712 meter/sec
ZDOT = -19431
061920 ZDOT = -5922
587673
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 08089
35620462
00020000 00000-0 20000-3 0 9080
2 25544 51
6394 67
9340 0001096 343
6295 16
4834 15
76510544 15939
Satellite: ISS
Catalog Number: 25544
Epoch time: 08089
35620462 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 67
9340 deg
Eccentricity:
0001096
Arg of perigee: 343
6295 deg
Mean anomaly: 16
4834 deg
Mean motion: 15
76510544 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1593
Checksum: 301
Coasting Arc #10 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2008/090/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4526875
33 A = 6714335
54 meter
Y = -278031
01 meter E =
0006719
Z = 4948216
51 I = 51
91089
XDOT = -1885
606510 Wp = 47
52766
YDOT = -7165
612725 meter/sec RA = 62
28909 deg
ZDOT = -2121
413351 TA = 62
97686
MA = 62
90829
Ha = 186
256 n
mi
Hp = 179
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14851953
19 X = -4547467
34
Y = -912175
23 feet Y = -328768
20 meter
Z = 16234306
13 Z = 4926175
03
XDOT = -6186
373065 XDOT = -1795
033973
YDOT = -23509
228101 feet/sec YDOT = -7186
192260 meter/sec
ZDOT = -6960
017557 ZDOT = -2130
353511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7793823
88 X = -2375557
52
Y = -12783111
41 feet Y = -3896292
36 meter
Z = 16149725
84 Z = 4922436
44
XDOT = 14843
854322 XDOT = 4524
406797
YDOT = -17913
637216 feet/sec YDOT = -5460
076623 meter/sec
ZDOT = -6995
068021 ZDOT = -2132
096733
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 08090
37041444
00020000 00000-0 20000-3 0 9092
2 25544 51
6385 62
7061 0001115 346
8448 13
2687 15
76554009 16092
Satellite: ISS
Catalog Number: 25544
Epoch time: 08090
37041444 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 62
7061 deg
Eccentricity:
0001115
Arg of perigee: 346
8448 deg
Mean anomaly: 13
2687 deg
Mean motion: 15
76554009 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1609
Checksum: 286
Coasting Arc #11 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2008/091/07:50:08
675
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1433200
97 A = 6721952
41 meter
Y = 6013835
61 meter E =
0014058
Z = 2621302
38 I = 51
92173
XDOT = -5542
633761 Wp = 72
60442
YDOT = -982
793457 meter/sec RA = 57
19297 deg
ZDOT = 5266
316139 TA = 317
12527
MA = 317
23479
Ha = 186
260 n
mi
Hp = 179
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4702102
93 X = 1353113
08
Y = 19730431
79 feet Y = 6029414
75 meter
Z = 8600073
42 Z = 2628070
16
XDOT = -18184
493967 XDOT = -5556
814711
YDOT = -3224
387981 feet/sec YDOT = -1044
853526 meter/sec
ZDOT = 17277
940089 ZDOT = 5239
355785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13267528
89 X = -4043942
81
Y = 15326912
71 feet Y = 4671642
99 meter
Z = 8626667
81 Z = 2629408
35
XDOT = -6975
869895 XDOT = -2126
245144
YDOT = -15739
822725 feet/sec YDOT = -4797
497967 meter/sec
ZDOT = 17174
413185 ZDOT = 5234
761139
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 08091
38460698
00020000 00000-0 20000-3 0 9102
2 25544 51
6384 57
4775 0001202
5309 359
5856 15
76539390 16259
Satellite: ISS
Catalog Number: 25544
Epoch time: 08091
38460698 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 57
4775 deg
Eccentricity:
0001202
Arg of perigee:
5309 deg
Mean anomaly: 359
5856 deg
Mean motion: 15
76539390 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1625
Checksum: 303
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 may contain past, current and future orbital data 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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]
If you're still having trouble, please contact the list owner at:
<mailto:list
admin@aus-city
com>
The following physical address is associated with this mailing list:
http://www aus-city com
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list