Date:
August 21st 2009
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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 1592)
---------------------------------------
Vector Time (GMT): 2009/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5746035
44 A = 6732251
19 meter
Y = 3180442
64 meter E =
0011117
Z = 1474218
21 I = 51
55177
XDOT = -3518
855696 Wp = 83
84190
YDOT = -3658
090353 meter/sec RA = 341
30158 deg
ZDOT = -5785
054176 TA = 79
91819
MA = 79
79278
Ha = 192
002 n
mi
Hp = 184
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18851822
30 X = -5788333
96
Y = 10434523
11 feet Y = 3115950
57 meter
Z = 4836673
92 Z = 1446201
93
XDOT = -11544
802151 XDOT = -3449
586664
YDOT = -12001
608771 feet/sec YDOT = -3697
052841 meter/sec
ZDOT = -18979
836537 ZDOT = -5801
980214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21522234
79 X = 6559977
16
Y = 1454818
14 feet Y = 443428
57 meter
Z = 4726606
07 Z = 1440669
53
XDOT = 3216
746227 XDOT = 980
464250
YDOT = 14712
686880 feet/sec YDOT = 4484
426961 meter/sec
ZDOT = -19046
570808 ZDOT = -5805
394782
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 09231
53458337
00010596 00000-0 82463-4 0 9003
2 25544 51
6413 341
6510 0007998 351
3674 8
7350 15
73656498 15939
Satellite: ISS
Catalog Number: 25544
Epoch time: 09231
53458337 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 341
6510 deg
Eccentricity:
0007998
Arg of perigee: 351
3674 deg
Mean anomaly: 8
7350 deg
Mean motion: 15
73656498 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1593
Checksum: 322
Coasting Arc #2 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3435064
22 A = 6721921
44 meter
Y = 2851159
73 meter E =
0006174
Z = 5021074
97 I = 51
49053
XDOT = -6156
170749 Wp = 35
24277
YDOT = 4272
821104 meter/sec RA = 336
18852 deg
ZDOT = 1789
217938 TA = 37
51420
MA = 37
47113
Ha = 191
981 n
mi
Hp = 183
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11269895
74 X = 3378535
79
Y = 9354198
60 feet Y = 2889256
62 meter
Z = 16473343
08 Z = 5037624
83
XDOT = -20197
410593 XDOT = -6212
184147
YDOT = 14018
441941 feet/sec YDOT = 4203
666018 meter/sec
ZDOT = 5870
137592 ZDOT = 1759
175782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4564569
44 X = -1391280
76
Y = -13839188
52 feet Y = -4218184
66 meter
Z = 16538566
46 Z = 5040955
06
XDOT = 23572
609530 XDOT = 7184
931385
YDOT = -915
933600 feet/sec YDOT = -279
176561 meter/sec
ZDOT = 5752
155378 ZDOT = 1753
256959
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 09232
55062751
00010596 00000-0 82463-4 0 9018
2 25544 51
6420 336
4357 0008116 355
0274 5
0807 15
73712814 16098
Satellite: ISS
Catalog Number: 25544
Epoch time: 09232
55062751 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 336
4357 deg
Eccentricity:
0008116
Arg of perigee: 355
0274 deg
Mean anomaly: 5
0807 deg
Mean motion: 15
73712814 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1609
Checksum: 286
Coasting Arc #3 (Orbit 1623)
---------------------------------------
Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4946813
80 A = 6731992
79 meter
Y = -4243135
07 meter E =
0015405
Z = -1652567
53 I = 51
49697
XDOT = 4318
225171 Wp = 17
26032
YDOT = 2815
220097 meter/sec RA = 331
01604 deg
ZDOT = 5725
910268 TA = 324
43465
MA = 324
53723
Ha = 192
361 n
mi
Hp = 183
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16229704
06 X = 5001921
35
Y = -13921046
81 feet Y = -4187508
82 meter
Z = -5421809
48 Z = -1628402
31
XDOT = 14167
405418 XDOT = 4258
608960
YDOT = 9236
286407 feet/sec YDOT = 2863
175873 meter/sec
ZDOT = 18785
794843 ZDOT = 5746
742979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21097346
06 X = -6430471
08
Y = 3622214
30 feet Y = 1104050
92 meter
Z = -5326951
21 Z = -1623654
73
XDOT = -7074
802800 XDOT = -2156
399893
YDOT = -13596
753180 feet/sec YDOT = -4144
290369 meter/sec
ZDOT = 18867
863448 ZDOT = 5750
924779
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 09233
50316294
00010596 00000-0 82463-4 0 9029
2 25544 51
6420 331
5473 0008372 358
8518 1
2624 15
73661067 16244
Satellite: ISS
Catalog Number: 25544
Epoch time: 09233
50316294 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 331
5473 deg
Eccentricity:
0008372
Arg of perigee: 358
8518 deg
Mean anomaly: 1
2624 deg
Mean motion: 15
73661067 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1624
Checksum: 293
Coasting Arc #4 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4046943
36 A = 6722231
62 meter
Y = -2049917
70 meter E =
0017357
Z = -4975261
38 I = 51
43847
XDOT = 5140
713390 Wp = 48
16001
YDOT = -5369
259438 meter/sec RA = 325
90254 deg
ZDOT = -1962
275744 TA = 202
75016
MA = 202
82717
Ha = 192
332 n
mi
Hp = 183
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13277373
22 X = -3999551
37
Y = -6725451
77 feet Y = -2094908
20 meter
Z = -16323036
01 Z = -4994806
04
XDOT = 16865
857580 XDOT = 5209
903589
YDOT = -17615
680572 feet/sec YDOT = -5311
386173 meter/sec
ZDOT = -6437
912546 ZDOT = -1937
134144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8087950
10 X = 2465207
19
Y = 12393015
68 feet Y = 3777391
18 meter
Z = -16400002
17 Z = -4998720
66
XDOT = -22523
484303 XDOT = -6865
158016
YDOT = 6280
159996 feet/sec YDOT = 1914
192767 meter/sec
ZDOT = -6339
273450 ZDOT = -1932
210548
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 09234
51919058
00010596 00000-0 82463-4 0 9039
2 25544 51
6415 326
3325 0008241 2
3687 357
7513 15
73689894 16401
Satellite: ISS
Catalog Number: 25544
Epoch time: 09234
51919058 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 326
3325 deg
Eccentricity:
0008241
Arg of perigee: 2
3687 deg
Mean anomaly: 357
7513 deg
Mean motion: 15
73689894 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1640
Checksum: 320
Coasting Arc #5 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4012200
88 A = 6731662
20 meter
Y = 5104749
10 meter E =
0014052
Z = 1771129
10 I = 51
44556
XDOT = -4871
186764 Wp = 80
27621
YDOT = -1849
002898 meter/sec RA = 320
72315 deg
ZDOT = -5665
201088 TA = 80
05844
MA = 79
89986
Ha = 192
488 n
mi
Hp = 183
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13163388
71 X = -4077588
65
Y = 16747864
49 feet Y = 5059516
76 meter
Z = 5810791
00 Z = 1751478
93
XDOT = -15981
583870 XDOT = -4822
628467
YDOT = -6066
282474 feet/sec YDOT = -1903
204054 meter/sec
ZDOT = -18586
617742 ZDOT = -5688
747188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19640797
10 X = 5986514
96
Y = -8300260
86 feet Y = -2529919
51 meter
Z = 5733743
82 Z = 1747645
12
XDOT = 10369
652426 XDOT = 3160
670059
YDOT = 11541
117827 feet/sec YDOT = 3517
732714 meter/sec
ZDOT = -18679
309943 ZDOT = -5693
453671
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 09235
53520932
00010596 00000-0 82463-4 0 9042
2 25544 51
6408 321
1173 0008327 7
4991 352
6295 15
73714650 16563
Satellite: ISS
Catalog Number: 25544
Epoch time: 09235
53520932 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 321
1173 deg
Eccentricity:
0008327
Arg of perigee: 7
4991 deg
Mean anomaly: 352
6295 deg
Mean motion: 15
73714650 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1656
Checksum: 305
Coasting Arc #6 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4427108
98 A = 6722215
23 meter
Y = 1159901
03 meter E =
0008180
Z = 4916553
69 I = 51
39221
XDOT = -3978
959440 Wp = 53
42081
YDOT = 6253
425978 meter/sec RA = 315
60671 deg
ZDOT = 2109
943930 TA = 16
08238
MA = 16
05643
Ha = 192
385 n
mi
Hp = 182
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14524635
78 X = 4389926
04
Y = 3805449
59 feet Y = 1209199
76 meter
Z = 16130425
50 Z = 4937970
22
XDOT = -13054
328870 XDOT = -4058
840309
YDOT = 20516
489428 feet/sec YDOT = 6208
484320 meter/sec
ZDOT = 6922
388222 ZDOT = 2090
420020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10977952
57 X = -3346079
94
Y = -10109644
64 feet Y = -3081419
68 meter
Z = 16214708
15 Z = 4942243
05
XDOT = 20428
823646 XDOT = 6226
705447
YDOT = -11215
888096 feet/sec YDOT = -3418
602692 meter/sec
ZDOT = 6845
894160 ZDOT = 2086
628540
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 09236
55121681
00010596 00000-0 82463-4 0 9054
2 25544 51
6410 315
9010 0008369 10
4765 349
6571 15
73757949 16725
Satellite: ISS
Catalog Number: 25544
Epoch time: 09236
55121681 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 315
9010 deg
Eccentricity:
0008369
Arg of perigee: 10
4765 deg
Mean anomaly: 349
6571 deg
Mean motion: 15
73757949 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1672
Checksum: 319
Coasting Arc #7 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2009/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2897821
08 A = 6731419
12 meter
Y = -5758144
47 meter E =
0015320
Z = -1913650
94 I = 51
40152
XDOT = 5222
597485 Wp = 24
73414
YDOT = 773
970641 meter/sec RA = 310
42194 deg
ZDOT = 5609
501415 TA = 313
91117
MA = 314
03755
Ha = 192
736 n
mi
Hp = 182
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9507287
02 X = 2971290
44
Y = -18891550
11 feet Y = -5725328
55 meter
Z = -6278382
35 Z = -1899394
85
XDOT = 17134
506184 XDOT = 5186
304712
YDOT = 2539
273756 feet/sec YDOT = 832
169887 meter/sec
ZDOT = 18403
876033 ZDOT = 5634
784635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17054435
17 X = -5198191
84
Y = 12534869
16 feet Y = 3820628
12 meter
Z = -6222584
09 Z = -1896643
63
XDOT = -13124
650670 XDOT = -4000
393524
YDOT = -8720
441291 feet/sec YDOT = -2657
990505 meter/sec
ZDOT = 18503
347076 ZDOT = 5639
820189
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 09237
50371762
00010596 00000-0 82463-4 0 9068
2 25544 51
6403 311
0120 0008612 13
6706 346
4689 15
73715024 16876
Satellite: ISS
Catalog Number: 25544
Epoch time: 09237
50371762 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 311
0120 deg
Eccentricity:
0008612
Arg of perigee: 13
6706 deg
Mean anomaly: 346
4689 deg
Mean motion: 15
73715024 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1687
Checksum: 294
Coasting Arc #8 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4635685
95 A = 6722475
85 meter
Y = -207069
10 meter E =
0018665
Z = -4880655
36 I = 51
35252
XDOT = 2664
832261 Wp = 51
26433
YDOT = -6854
775582 meter/sec RA = 305
30483 deg
ZDOT = -2234
505805 TA = 196
85200
MA = 196
91409
Ha = 192
764 n
mi
Hp = 182
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15208943
42 X = -4609316
61
Y = -679360
57 feet Y = -258760
56 meter
Z = -16012648
83 Z = -4903111
47
XDOT = 8742
887997 XDOT = 2752
140304
YDOT = -22489
421202 feet/sec YDOT = -6824
487668 meter/sec
ZDOT = -7331
055790 ZDOT = -2221
348076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13300716
17 X = 4054058
29
Y = 7213039
69 feet Y = 2198534
50 meter
Z = -16100975
78 Z = -4907577
42
XDOT = -17199
584624 XDOT = -5242
433393
YDOT = 15424
235107 feet/sec YDOT = 4701
306861 meter/sec
ZDOT = -7279
629135 ZDOT = -2218
830960
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 09238
51970909
00010596 00000-0 82463-4 0 9079
2 25544 51
6395 305
7960 0008544 18
1417 342
0049 15
73743208 17037
Satellite: ISS
Catalog Number: 25544
Epoch time: 09238
51970909 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 305
7960 deg
Eccentricity:
0008544
Arg of perigee: 18
1417 deg
Mean anomaly: 342
0049 deg
Mean motion: 15
73743208 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1703
Checksum: 316
Coasting Arc #9 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2009/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1749765
72 A = 6731031
87 meter
Y = 6185260
31 meter E =
0016620
Z = 1989033
14 I = 51
36608
XDOT = -5313
132721 Wp = 79
71181
YDOT = 299
306378 meter/sec RA = 300
11463 deg
ZDOT = -5562
415900 TA = 78
05224
MA = 77
86596
Ha = 192
855 n
mi
Hp = 182
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5740701
17 X = -1828462
65
Y = 20292848
80 feet Y = 6165253
34 meter
Z = 6525699
27 Z = 1980341
80
XDOT = -17431
537797 XDOT = -5289
063586
YDOT = 981
976306 feet/sec YDOT = 240
026530 meter/sec
ZDOT = -18249
395997 ZDOT = -5588
168565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13788638
66 X = 4202777
06
Y = -15970910
36 feet Y = -4867933
48 meter
Z = 6491808
64 Z = 1978703
27
XDOT = 14961
914374 XDOT = 4560
391501
YDOT = 5401
641890 feet/sec YDOT = 1646
420448 meter/sec
ZDOT = -18350
666674 ZDOT = -5593
283202
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 09239
53568998
00010596 00000-0 82463-4 0 9084
2 25544 51
6400 300
5799 0008797 21
9579 338
1949 15
73805165 17191
Satellite: ISS
Catalog Number: 25544
Epoch time: 09239
53568998 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 300
5799 deg
Eccentricity:
0008797
Arg of perigee: 21
9579 deg
Mean anomaly: 338
1949 deg
Mean motion: 15
73805165 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1719
Checksum: 365
Coasting Arc #10 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2009/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4608062
05 A = 6722443
31 meter
Y = -735122
72 meter E =
0010468
Z = 4829293
46 I = 51
32303
XDOT = -1301
202044 Wp = 65
59319
YDOT = 7227
701925 meter/sec RA = 294
99646 deg
ZDOT = 2342
099980 TA = 1
50372
MA = 1
50058
Ha = 192
776 n
mi
Hp = 182
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15118313
83 X = 4592480
13
Y = -2411819
96 feet Y = -683679
95 meter
Z = 15844138
66 Z = 4851641
44
XDOT = -4269
035579 XDOT = -1393
304179
YDOT = 23712
932825 feet/sec YDOT = 7212
636073 meter/sec
ZDOT = 7684
055054 ZDOT = 2335
555296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14712628
72 X = -4484409
23
Y = -3889333
55 feet Y = -1185468
87 meter
Z = 15932001
11 Z = 4856073
94
XDOT = 13276
267487 XDOT = 4046
606330
YDOT = -18853
178091 feet/sec YDOT = -5746
448682 meter/sec
ZDOT = 7658
660378 ZDOT = 2334
359683
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 09240
55166247
00010596 00000-0 82463-4 0 9090
2 25544 51
6396 295
3639 0008722 26
0407 334
1194 15
73805152 17355
Satellite: ISS
Catalog Number: 25544
Epoch time: 09240
55166247 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 295
3639 deg
Eccentricity:
0008722
Arg of perigee: 26
0407 deg
Mean anomaly: 334
1194 deg
Mean motion: 15
73805152 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1735
Checksum: 315
Coasting Arc #11 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2009/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 509099
40 A = 6730825
45 meter
Y = -6369274
59 meter E =
0015257
Z = -2098458
32 I = 51
33936
XDOT = 5191
546078 Wp = 34
31712
YDOT = -1391
895288 meter/sec RA = 289
80282 deg
ZDOT = 5516
070181 TA = 302
13047
MA = 302
27843
Ha = 193
024 n
mi
Hp = 181
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1670273
64 X = 590477
73
Y = -20896570
18 feet Y = -6363126
46 meter
Z = -6884705
77 Z = -2095787
67
XDOT = 17032
631488 XDOT = 5179
928803
YDOT = -4566
585591 feet/sec YDOT = -1333
905502 meter/sec
ZDOT = 18097
343115 ZDOT = 5541
262232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9719911
87 X = -2962629
14
Y = 18577406
06 feet Y = 5662393
37 meter
Z = -6874513
06 Z = -2095351
58
XDOT = -16013
302544 XDOT = -4880
854615
YDOT = -1683
577516 feet/sec YDOT = -513
154427 meter/sec
ZDOT = 18196
363314 ZDOT = 5546
251538
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 09241
50412900
00010596 00000-0 82463-4 0 9108
2 25544 51
6393 290
4741 0008871 29
7486 330
4179 15
73801741 17503
Satellite: ISS
Catalog Number: 25544
Epoch time: 09241
50412900 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 290
4741 deg
Eccentricity:
0008871
Arg of perigee: 29
7486 deg
Mean anomaly: 330
4179 deg
Mean motion: 15
73801741 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1750
Checksum: 301
Coasting Arc #12 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2009/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4416144
18 A = 6722606
58 meter
Y = 1655274
28 meter E =
0019726
Z = -4809042
29 I = 51
30325
XDOT = -93
496233 Wp = 56
11318
YDOT = -7293
396255 meter/sec RA = 284
68386 deg
ZDOT = -2420
814803 TA = 190
06362
MA = 190
10318
Ha = 193
125 n
mi
Hp = 181
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14488662
02 X = -4410964
34
Y = 5430689
90 feet Y = 1605919
44 meter
Z = -15777697
81 Z = -4830483
05
XDOT = -306
746172 XDOT = -
173528
YDOT = -23928
465405 feet/sec YDOT = -7293
919933 meter/sec
ZDOT = -7942
305784 ZDOT = -2421
042498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15382730
85 X = 4688656
36
Y = 345740
67 feet Y = 105381
76 meter
Z = -15861952
05 Z = -4834722
99
XDOT = -8679
337501 XDOT = -2645
462070
YDOT = 21168
996241 feet/sec YDOT = 6452
310054 meter/sec
ZDOT = -7943
568116 ZDOT = -2421
199562
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 09242
52008361
00010596 00000-0 82463-4 0 9114
2 25544 51
6398 285
2577 0008896 34
1100 326
0633 15
73806389 17663
Satellite: ISS
Catalog Number: 25544
Epoch time: 09242
52008361 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 285
2577 deg
Eccentricity:
0008896
Arg of perigee: 34
1100 deg
Mean anomaly: 326
0633 deg
Mean motion: 15
73806389 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1766
Checksum: 317
Coasting Arc #13 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2009/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 670872
90 A = 6730601
28 meter
Y = 6344458
50 meter E =
0018923
Z = 2133092
43 I = 51
32363
XDOT = -4850
894489 Wp = 82
43337
YDOT = 2373
050840 meter/sec RA = 279
48765 deg
ZDOT = -5488
469338 TA = 73
60194
MA = 73
39400
Ha = 193
168 n
mi
Hp = 181
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2201026
56 X = 589516
17
Y = 20815152
55 feet Y = 6351505
68 meter
Z = 6998334
73 Z = 2136153
93
XDOT = -15915
008166 XDOT = -4850
408194
YDOT = 7785
599868 feet/sec YDOT = 2318
808061 meter/sec
ZDOT = -18006
789168 ZDOT = -5512
033457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5431763
36 X = 1655601
47
Y = -20209842
12 feet Y = -6159959
88 meter
Z = 7010706
85 Z = 2136863
45
XDOT = 16075
118333 XDOT = 4899
696068
YDOT = -2008
161346 feet/sec YDOT = -612
087578 meter/sec
ZDOT = -18099
360013 ZDOT = -5516
684932
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 09243
53602731
00010596 00000-0 82463-4 0 9128
2 25544 51
6391 280
0415 0009075 37
5627 322
6169 15
73857453 17823
Satellite: ISS
Catalog Number: 25544
Epoch time: 09243
53602731 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 280
0415 deg
Eccentricity:
0009075
Arg of perigee: 37
5627 deg
Mean anomaly: 322
6169 deg
Mean motion: 15
73857453 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1782
Checksum: 311
Coasting Arc #14 (Orbit 1797)
---------------------------------------
Vector Time (GMT): 2009/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4022337
51 A = 6722568
31 meter
Y = -2481726
90 meter E =
0012722
Z = 4768813
76 I = 51
29213
XDOT = 1455
586212 Wp = 75
53101
YDOT = 7149
790022 meter/sec RA = 274
36852 deg
ZDOT = 2490
671220 TA = 350
00094
MA = 350
02623
Ha = 193
150 n
mi
Hp = 181
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13196645
39 X = 4026623
96
Y = -8142148
61 feet Y = -2436722
75 meter
Z = 15645714
43 Z = 4788364
42
XDOT = 4775
545315 XDOT = 1363
428792
YDOT = 23457
316345 feet/sec YDOT = 7165
551984 meter/sec
ZDOT = 8171
493503 ZDOT = 2497
518449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15098650
70 X = -4602068
73
Y = 3173081
48 feet Y = 967155
23 meter
Z = 15722490
72 Z = 4792215
17
XDOT = 3804
607535 XDOT = 1159
644377
YDOT = -22559
850658 feet/sec YDOT = -6876
242481 meter/sec
ZDOT = 8198
812966 ZDOT = 2498
998192
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 09244
55196270
00010596 00000-0 82463-4 0 9138
2 25544 51
6383 274
8252 0009139 42
2397 317
9469 15
73854213 17980
Satellite: ISS
Catalog Number: 25544
Epoch time: 09244
55196270 = yrday
fracday
Element set: 913
Inclination: 51
6383 deg
RA of node: 274
8252 deg
Eccentricity:
0009139
Arg of perigee: 42
2397 deg
Mean anomaly: 317
9469 deg
Mean motion: 15
73854213 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1798
Checksum: 338
Coasting Arc #15 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2009/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1857592
34 A = 6730310
65 meter
Y = -6075655
29 meter E =
0015209
Z = -2210138
89 I = 51
31848
XDOT = 4321
000717 Wp = 44
73966
YDOT = -3293
703748 meter/sec RA = 269
17092 deg
ZDOT = 5456
019631 TA = 290
36953
MA = 290
53285
Ha = 193
225 n
mi
Hp = 181
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6094463
07 X = -1778778
95
Y = -19933252
27 feet Y = -6095987
37 meter
Z = -7251111
84 Z = -2218971
34
XDOT = 14176
511539 XDOT = 4331
006341
YDOT = -10806
114658 feet/sec YDOT = -3245
327677 meter/sec
ZDOT = 17900
326872 ZDOT = 5477
035158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -766384
38 X = -233593
96
Y = 20817772
66 feet Y = 6345257
11 meter
Z = -7286195
55 Z = -2220832
40
XDOT = -15305
013007 XDOT = -4664
967965
YDOT = 5692
363142 feet/sec YDOT = 1735
032286 meter/sec
ZDOT = 17982
818677 ZDOT = 5481
163133
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 09245
50439284
00010596 00000-0 82463-4 0 9140
2 25544 51
6391 269
9353 0009138 45
9662 314
2252 15
73899420 18137
Satellite: ISS
Catalog Number: 25544
Epoch time: 09245
50439284 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 269
9353 deg
Eccentricity:
0009138
Arg of perigee: 45
9662 deg
Mean anomaly: 314
2252 deg
Mean motion: 15
73899420 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1813
Checksum: 327
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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