Date:
October 30th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20989 63 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 ET - UTC (sec) : 66 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 2695)
---------------------------------------
Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 387025
59 A = 6715931
16 meter
Y = 4230292
98 meter E =
0003536
Z = 5204849
50 I = 51
51930
XDOT = -7450
883357 Wp = 279
38209
YDOT = 1745
429462 meter/sec RA = 341
66377 deg
ZDOT = -864
507669 TA = 178
86289
MA = 178
86208
Ha = 185
669 n
mi
Hp = 183
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1269769
00 X = 314408
28
Y = 13878913
99 feet Y = 4234215
11 meter
Z = 17076277
89 Z = 5206553
15
XDOT = -24445
155370 XDOT = -7465
647584
YDOT = 5726
474612 feet/sec YDOT = 1662
026706 meter/sec
ZDOT = -2836
311251 ZDOT = -900
740639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9140730
75 X = -2786094
73
Y = -10509480
02 feet Y = -3203289
51 meter
Z = 17083140
94 Z = 5206941
36
XDOT = 15565
210893 XDOT = 4744
276280
YDOT = -18380
947559 feet/sec YDOT = -5602
512816 meter/sec
ZDOT = -2979
129564 ZDOT = -908
038691
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 09301
54605251
00016717 00000-0 10270-3 0 9008
2 25544 51
6436 341
9487 0006503 259
6970 100
3461 15
75557748 26967
Satellite: ISS
Catalog Number: 25544
Epoch time: 09301
54605251 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 341
9487 deg
Eccentricity:
0006503
Arg of perigee: 259
6970 deg
Mean anomaly: 100
3461 deg
Mean motion: 15
75557748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 319
Coasting Arc #2 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2009/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6385554
98 A = 6726993
24 meter
Y = -1661845
88 meter E =
0008791
Z = 1282407
02 I = 51
52848
XDOT = 126
507912 Wp = 41
18074
YDOT = 5012
048096 meter/sec RA = 336
52803 deg
ZDOT = 5848
942399 TA = 332
92341
MA = 332
96923
Ha = 185
510 n
mi
Hp = 183
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20949983
52 X = 6397433
60
Y = -5452250
25 feet Y = -1590372
36 meter
Z = 4207372
12 Z = 1313457
65
XDOT = 415
052206 XDOT = 42
039196
YDOT = 16443
727350 feet/sec YDOT = 5012
990774 meter/sec
ZDOT = 19189
443566 ZDOT = 5849
351567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13376270
38 X = -4077087
21
Y = 16989981
15 feet Y = 5178546
25 meter
Z = 4329752
17 Z = 1319708
46
XDOT = -8940
519503 XDOT = -2725
070345
YDOT = -11942
740046 feet/sec YDOT = -3640
147166 meter/sec
ZDOT = 19191
230579 ZDOT = 5849
487081
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 09302
56087458
00016717 00000-0 10270-3 0 9015
2 25544 51
6435 336
7249 0006246 265
5682 94
4768 15
75557294 27122
Satellite: ISS
Catalog Number: 25544
Epoch time: 09302
56087458 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 336
7249 deg
Eccentricity:
0006246
Arg of perigee: 265
5682 deg
Mean anomaly: 94
4768 deg
Mean motion: 15
75557294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 341
Coasting Arc #3 (Orbit 2726)
---------------------------------------
Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 153578
17 A = 6716953
29 meter
Y = -4561694
99 meter E =
0006888
Z = -4934153
41 I = 51
46894
XDOT = 7133
723489 Wp = 121
07504
YDOT = -2011
283437 meter/sec RA = 331
34071 deg
ZDOT = 2080
139307 TA = 169
13979
MA = 169
12491
Ha = 185
299 n
mi
Hp = 183
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 503865
40 X = 228546
28
Y = -14966190
91 feet Y = -4559558
67 meter
Z = -16188167
37 Z = -4933224
98
XDOT = 23404
604624 XDOT = 7145
578606
YDOT = -6598
698939 feet/sec YDOT = -1931
443543 meter/sec
ZDOT = 6824
604025 ZDOT = 2114
824732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8778381
96 X = 2675650
82
Y = 12136479
26 feet Y = 3699198
88 meter
Z = -16184665
43 Z = -4933086
02
XDOT = -13406
372780 XDOT = -4086
262423
YDOT = 18986
137982 feet/sec YDOT = 5786
974857 meter/sec
ZDOT = 6961
298215 ZDOT = 2121
803696
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 09303
51223613
00016717 00000-0 10270-3 0 9027
2 25544 51
6444 331
8279 0006370 268
5599 91
4835 15
75626907 27275
Satellite: ISS
Catalog Number: 25544
Epoch time: 09303
51223613 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 331
8279 deg
Eccentricity:
0006370
Arg of perigee: 268
5599 deg
Mean anomaly: 91
4835 deg
Mean motion: 15
75626907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2727
Checksum: 326
Coasting Arc #4 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2009/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6038992
09 A = 6724889
14 meter
Y = 1792441
81 meter E =
0004267
Z = -2345930
58 I = 51
47012
XDOT = 468
612239 Wp = 210
87188
YDOT = -5479
581160 meter/sec RA = 326
21845 deg
ZDOT = -5392
355125 TA = 355
62308
MA = 355
62681
Ha = 185
222 n
mi
Hp = 183
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19812966
17 X = -6047190
19
Y = 5880714
59 feet Y = 1724864
30 meter
Z = -7696622
65 Z = -2375288
89
XDOT = 1537
441728 XDOT = 556
046931
YDOT = -17977
628477 feet/sec YDOT = -5473
852213 meter/sec
ZDOT = -17691
453823 ZDOT = -5389
865923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11615956
07 X = 3540543
41
Y = -17041470
87 feet Y = -5194240
32 meter
Z = -7812315
16 Z = -2381193
66
XDOT = 8836
323179 XDOT = 2693
311305
YDOT = 14130
030689 feet/sec YDOT = 4306
833354 meter/sec
ZDOT = -17681
829630 ZDOT = -5389
421671
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 09304
52699080
00016717 00000-0 10270-3 0 9035
2 25544 51
6437 326
6039 0006265 272
2259 87
8187 15
75693557 27433
Satellite: ISS
Catalog Number: 25544
Epoch time: 09304
52699080 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 326
6039 deg
Eccentricity:
0006265
Arg of perigee: 272
2259 deg
Mean anomaly: 87
8187 deg
Mean motion: 15
75693557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2743
Checksum: 342
Coasting Arc #5 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2009/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -630455
66 A = 6718691
81 meter
Y = 5032365
80 meter E =
0004787
Z = 4406771
33 I = 51
42423
XDOT = -6667
434028 Wp = 31
62383
YDOT = 2036
986834 meter/sec RA = 321
01106 deg
ZDOT = -3274
419435 TA = 91
34513
MA = 91
29029
Ha = 185
285 n
mi
Hp = 183
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2068424
09 X = -708089
63
Y = 16510386
49 feet Y = 5024881
70 meter
Z = 14457911
20 Z = 4403519
78
XDOT = -21874
783557 XDOT = -6673
809337
YDOT = 6683
027671 feet/sec YDOT = 1962
391935 meter/sec
ZDOT = -10742
845915 ZDOT = -3306
826477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8997767
26 X = -2742519
46
Y = -14009887
80 feet Y = -4270213
80 meter
Z = 14445264
44 Z = 4402916
60
XDOT = 11344
904476 XDOT = 3457
926884
YDOT = -18513
590656 feet/sec YDOT = -5642
942432 meter/sec
ZDOT = -10870
547349 ZDOT = -3313
342832
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 09305
54171125
00016717 00000-0 10270-3 0 9044
2 25544 51
6425 321
3795 0006208 277
1472 82
8986 15
75770962 27594
Satellite: ISS
Catalog Number: 25544
Epoch time: 09305
54171125 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 321
3795 deg
Eccentricity:
0006208
Arg of perigee: 277
1472 deg
Mean anomaly: 82
8986 deg
Mean motion: 15
75770962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2759
Checksum: 332
Coasting Arc #6 (Orbit 2774)
---------------------------------------
Vector Time (GMT): 2009/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5577002
79 A = 6722106
12 meter
Y = -1689202
12 meter E =
0006641
Z = 3344265
69 I = 51
41312
XDOT = -947
087199 Wp = 79
17024
YDOT = 6075
771223 meter/sec RA = 315
89567 deg
ZDOT = 4641
738320 TA = 320
38282
MA = 320
43132
Ha = 185
301 n
mi
Hp = 183
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18297253
25 X = 5579230
81
Y = -5542001
70 feet Y = -1626824
34 meter
Z = 10972000
28 Z = 3371365
16
XDOT = -3107
241467 XDOT = -1037
506691
YDOT = 19933
632621 feet/sec YDOT = 6064
674751 meter/sec
ZDOT = 15228
800261 ZDOT = 4636
917594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10089569
06 X = -3075300
65
Y = 16166295
86 feet Y = 4927486
98 meter
Z = 11078787
12 Z = 3376814
31
XDOT = -9524
151080 XDOT = -2902
961249
YDOT = -16382
153345 feet/sec YDOT = -4993
280339 meter/sec
ZDOT = 15209
999674 ZDOT = 4636
007901
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 09306
55639912
00016717 00000-0 10270-3 0 9050
2 25544 51
6420 316
1547 0006164 281
4844 78
5627 15
75794115 27756
Satellite: ISS
Catalog Number: 25544
Epoch time: 09306
55639912 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 316
1547 deg
Eccentricity:
0006164
Arg of perigee: 281
4844 deg
Mean anomaly: 78
5627 deg
Mean motion: 15
75794115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2775
Checksum: 330
Coasting Arc #7 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2009/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 978227
92 A = 6721241
40 meter
Y = -5575896
11 meter E =
0000894
Z = -3622097
69 I = 51
39018
XDOT = 6101
400745 Wp = 326
68713
YDOT = -1760
197039 meter/sec RA = 310
67756 deg
ZDOT = 4357
713293 TA = 349
70554
MA = 349
70737
Ha = 185
557 n
mi
Hp = 183
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3209409
20 X = 1058101
99
Y = -18293622
42 feet Y = -5564510
27 meter
Z = -11883522
61 Z = -3617151
46
XDOT = 20017
718979 XDOT = 6099
460347
YDOT = -5774
924668 feet/sec YDOT = -1691
978578 meter/sec
ZDOT = 14296
959624 ZDOT = 4387
350200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9834812
31 X = 2997650
79
Y = 15769974
46 feet Y = 4806688
22 meter
Z = -11864207
12 Z = -3616210
33
XDOT = -9765
789903 XDOT = -2976
612763
YDOT = 16933
669276 feet/sec YDOT = 5161
382395 meter/sec
ZDOT = 14413
750512 ZDOT = 4393
311156
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 09307
50763659
00016717 00000-0 10270-3 0 9063
2 25544 51
6424 311
2568 0006182 285
5825 74
4657 15
75840457 27909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09307
50763659 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 311
2568 deg
Eccentricity:
0006182
Arg of perigee: 285
5825 deg
Mean anomaly: 74
4657 deg
Mean motion: 15
75840457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2790
Checksum: 336
Coasting Arc #8 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2009/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5071223
29 A = 6718928
57 meter
Y = 1297389
84 meter E =
0005399
Z = -4217263
94 I = 51
36333
XDOT = 1267
914801 Wp = 22
55680
YDOT = -6696
069560 meter/sec RA = 305
55933 deg
ZDOT = -3581
219015 TA = 210
87777
MA = 210
90953
Ha = 185
663 n
mi
Hp = 182
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16637871
68 X = -5064866
63
Y = 4256528
34 feet Y = 1240716
23 meter
Z = -13836167
79 Z = -4241885
25
XDOT = 4159
825464 XDOT = 1360
094676
YDOT = -21968
732151 feet/sec YDOT = -6681
375369 meter/sec
ZDOT = -11749
406216 ZDOT = -3574
835769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9181931
86 X = 2798652
83
Y = -14419928
06 feet Y = -4395194
07 meter
Z = -13933203
11 Z = -4246840
31
XDOT = 10870
605844 XDOT = 3313
360661
YDOT = 18261
314993 feet/sec YDOT = 5566
048810 meter/sec
ZDOT = -11724
459024 ZDOT = -3573
615110
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 09308
52225719
00016717 00000-0 10270-3 0 9077
2 25544 51
6413 306
0310 0006162 289
2167 70
8330 15
75896760 28066
Satellite: ISS
Catalog Number: 25544
Epoch time: 09308
52225719 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 306
0310 deg
Eccentricity:
0006162
Arg of perigee: 289
2167 deg
Mean anomaly: 70
8330 deg
Mean motion: 15
75896760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 307
Coasting Arc #9 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2009/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1190265
12 A = 6723681
39 meter
Y = 6095960
79 meter E =
0007741
Z = 2567367
72 I = 51
36344
XDOT = -5524
347580 Wp = 94
60350
YDOT = 1136
363016 meter/sec RA = 300
34178 deg
ZDOT = -5246
388544 TA = 56
11861
MA = 56
04499
Ha = 185
793 n
mi
Hp = 182
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3905069
28 X = -1270814
91
Y = 19999871
35 feet Y = 6082199
97 meter
Z = 8423122
45 Z = 2561390
06
XDOT = -18124
499935 XDOT = -5511
157270
YDOT = 3728
225118 feet/sec YDOT = 1074
660660 meter/sec
ZDOT = -17212
560841 ZDOT = -5273
194464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11073201
04 X = -3375111
68
Y = -17117878
81 feet Y = -5217529
46 meter
Z = 8399753
29 Z = 2560244
80
XDOT = 9105
584594 XDOT = 2775
382184
YDOT = -14409
185755 feet/sec YDOT = -4391
919818 meter/sec
ZDOT = -17318
220985 ZDOT = -5278
593756
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 09309
53684213
00016717 00000-0 10270-3 0 9088
2 25544 51
6411 300
8055 0006264 294
3446 65
7064 15
75983713 28222
Satellite: ISS
Catalog Number: 25544
Epoch time: 09309
53684213 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 300
8055 deg
Eccentricity:
0006264
Arg of perigee: 294
3446 deg
Mean anomaly: 65
7064 deg
Mean motion: 15
75983713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 314
Coasting Arc #10 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2009/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4590439
67 A = 6716028
71 meter
Y = -608260
91 meter E =
0000625
Z = 4864731
05 I = 51
32344
XDOT = -1419
782942 Wp = 186
52290
YDOT = 7231
778558 meter/sec RA = 295
21033 deg
ZDOT = 2243
370022 TA = 241
57235
MA = 241
57865
Ha = 185
777 n
mi
Hp = 182
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15060497
60 X = 4573267
65
Y = -1995606
67 feet Y = -557024
32 meter
Z = 15960403
72 Z = 4886990
16
XDOT = -4658
080518 XDOT = -1511
442560
YDOT = 23726
307605 feet/sec YDOT = 7215
389031 meter/sec
ZDOT = 7360
137866 ZDOT = 2236
250498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9158296
55 X = -2791448
79
Y = 12004904
36 feet Y = 3659094
85 meter
Z = 16048158
66 Z = 4891478
76
XDOT = -12601
227650 XDOT = -3840
854188
YDOT = -19417
596883 feet/sec YDOT = -5918
483530 meter/sec
ZDOT = 7332
305219 ZDOT = 2234
886631
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 09310
55139330
00016717 00000-0 10270-3 0 9098
2 25544 51
6407 295
5800 0006267 297
6246 62
4282 15
76008566 28380
Satellite: ISS
Catalog Number: 25544
Epoch time: 09310
55139330 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 295
5800 deg
Eccentricity:
0006267
Arg of perigee: 297
6246 deg
Mean anomaly: 62
4282 deg
Mean motion: 15
76008566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 322
Coasting Arc #11 (Orbit 2852)
---------------------------------------
Vector Time (GMT): 2009/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1250609
10 A = 6725530
17 meter
Y = -6472316
41 meter E =
0010301
Z = -1299317
13 I = 51
34432
XDOT = 5034
676520 Wp = 1
46113
YDOT = -195
469495 meter/sec RA = 290
00727 deg
ZDOT = 5830
800429 TA = 344
20112
MA = 344
23323
Ha = 185
913 n
mi
Hp = 182
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4103048
21 X = 1329202
67
Y = -21234633
89 feet Y = -6457891
83 meter
Z = -4262851
49 Z = -1293051
13
XDOT = 16517
967584 XDOT = 5008
162632
YDOT = -641
304118 feet/sec YDOT = -139
317443 meter/sec
ZDOT = 19129
922667 ZDOT = 5855
194901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12423875
31 X = 3786797
19
Y = 17708759
99 feet Y = 5397630
05 meter
Z = -4238363
56 Z = -1291853
21
XDOT = -9632
818646 XDOT = -2936
083123
YDOT = 11350
770662 feet/sec YDOT = 3459
714898 meter/sec
ZDOT = 19226
118347 ZDOT = 5860
120872
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 09311
50250185
00016717 00000-0 10270-3 0 9108
2 25544 51
6406 290
6814 0006043 301
3776 58
6797 15
76081469 28531
Satellite: ISS
Catalog Number: 25544
Epoch time: 09311
50250185 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 290
6814 deg
Eccentricity:
0006043
Arg of perigee: 301
3776 deg
Mean anomaly: 58
6797 deg
Mean motion: 15
76081469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2853
Checksum: 313
Coasting Arc #12 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2009/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4231472
04 A = 6714239
06 meter
Y = -332678
56 meter E =
0010934
Z = -5211274
76 I = 51
29750
XDOT = 1433
795466 Wp = 63
03478
YDOT = -7531
754224 meter/sec RA = 284
85087 deg
ZDOT = -679
609341 TA = 200
44698
MA = 200
49078
Ha = 186
045 n
mi
Hp = 182
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13882782
27 X = -4202121
68
Y = -1091465
09 feet Y = -379832
99 meter
Z = -17097358
14 Z = -5231760
27
XDOT = 4704
053366 XDOT = 1521
211756
YDOT = -24710
479736 feet/sec YDOT = -7515
231871 meter/sec
ZDOT = -2229
689440 ZDOT = -672
431924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10191966
73 X = 3106511
46
Y = -9342224
59 feet Y = -2847510
06 meter
Z = -17178161
97 Z = -5235903
77
XDOT = 14187
554379 XDOT = 4324
366575
YDOT = 19549
127346 feet/sec YDOT = 5958
574015 meter/sec
ZDOT = -2201
651857 ZDOT = -671
063486
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 09312
51698315
00016717 00000-0 10270-3 0 9112
2 25544 51
6407 285
4550 0006174 305
6283 54
4306 15
76110686 28697
Satellite: ISS
Catalog Number: 25544
Epoch time: 09312
51698315 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 285
4550 deg
Eccentricity:
0006174
Arg of perigee: 305
6283 deg
Mean anomaly: 54
4306 deg
Mean motion: 15
76110686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 313
Coasting Arc #13 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2009/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1243305
49 A = 6725950
66 meter
Y = 6605371
04 meter E =
0005773
Z = -144893
67 I = 51
33145
XDOT = -4706
740911 Wp = 142
74086
YDOT = -1014
953571 meter/sec RA = 279
67139 deg
ZDOT = -6011
063444 TA = 38
84091
MA = 38
79944
Ha = 186
176 n
mi
Hp = 182
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4079086
26 X = -1316371
62
Y = 21671164
82 feet Y = 6591059
13 meter
Z = -475372
95 Z = -151111
03
XDOT = -15442
063356 XDOT = -4665
840663
YDOT = -3329
900168 feet/sec YDOT = -1067
358269 meter/sec
ZDOT = -19721
336760 ZDOT = -6033
829772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13384658
61 X = -4079643
94
Y = -17524427
92 feet Y = -5341445
63 meter
Z = -499648
64 Z = -152292
91
XDOT = 11448
607987 XDOT = 3489
535715
YDOT = -8190
782098 feet/sec YDOT = -2496
550384 meter/sec
ZDOT = -19811
165777 ZDOT = -6038
443329
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 09313
53142761
00016717 00000-0 10270-3 0 9125
2 25544 51
6409 280
2288 0006270 309
9662 50
0951 15
76185813 28855
Satellite: ISS
Catalog Number: 25544
Epoch time: 09313
53142761 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 280
2288 deg
Eccentricity:
0006270
Arg of perigee: 309
9662 deg
Mean anomaly: 50
0951 deg
Mean motion: 15
76185813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 314
Coasting Arc #14 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2009/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4036306
94 A = 6714113
08 meter
Y = 1465684
08 meter E =
0006451
Z = 5163546
81 I = 51
28791
XDOT = -1410
077095 Wp = 346
59693
YDOT = 7503
675207 meter/sec RA = 274
48544 deg
ZDOT = -1021
747043 TA = 113
22416
MA = 113
15622
Ha = 186
160 n
mi
Hp = 181
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13242476
84 X = 3994533
47
Y = 4808674
80 feet Y = 1510586
85 meter
Z = 16940770
39 Z = 5183054
02
XDOT = -4626
237187 XDOT = -1488
916162
YDOT = 24618
356978 feet/sec YDOT = 7487
466087 meter/sec
ZDOT = -3352
188462 ZDOT = -1028
788757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12251015
32 X = -3734109
47
Y = 6766423
84 feet Y = 2062405
98 meter
Z = 17017766
59 Z = 5187015
26
XDOT = -15067
405491 XDOT = -4592
545194
YDOT = -18731
661763 feet/sec YDOT = -5709
410505 meter/sec
ZDOT = -3379
672269 ZDOT = -1030
124107
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 09314
54583612
00016717 00000-0 10270-3 0 9132
2 25544 51
6407 275
0027 0006248 313
2992 46
7651 15
76225482 29010
Satellite: ISS
Catalog Number: 25544
Epoch time: 09314
54583612 = yrday
fracday
Element set: 913
Inclination: 51
6407 deg
RA of node: 275
0027 deg
Eccentricity:
0006248
Arg of perigee: 313
2992 deg
Mean anomaly: 46
7651 deg
Mean motion: 15
76225482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 306
Coasting Arc #15 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2009/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1232882
79 A = 6724439
81 meter
Y = -6396531
28 meter E =
0013596
Z = 1633057
26 I = 51
32250
XDOT = 4604
944587 Wp = 37
98686
YDOT = 2351
111860 meter/sec RA = 269
33290 deg
ZDOT = 5717
954275 TA = 340
16159
MA = 340
21441
Ha = 186
156 n
mi
Hp = 181
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4044891
04 X = 1296385
04
Y = -20985995
01 feet Y = -6382389
39 meter
Z = 5357799
41 Z = 1639201
01
XDOT = 15108
085914 XDOT = 4550
534483
YDOT = 7713
621588 feet/sec YDOT = 2402
302883 meter/sec
ZDOT = 18759
692502 ZDOT = 5740
193332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13494947
67 X = 4113260
05
Y = 16565083
89 feet Y = 5049037
57 meter
Z = 5381777
38 Z = 1640365
75
XDOT = -14342
513154 XDOT = -4371
598009
YDOT = 5545
496254 feet/sec YDOT = 1690
267258 meter/sec
ZDOT = 18847
502071 ZDOT = 5744
718631
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 09315
56020602
00016717 00000-0 10270-3 0 9141
2 25544 51
6408 269
7758 0006172 316
2573 43
8102 15
76311220 29178
Satellite: ISS
Catalog Number: 25544
Epoch time: 09315
56020602 = yrday
fracday
Element set: 914
Inclination: 51
6408 deg
RA of node: 269
7758 deg
Eccentricity:
0006172
Arg of perigee: 316
2573 deg
Mean anomaly: 43
8102 deg
Mean motion: 15
76311220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2917
Checksum: 293
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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