Date:
July 26th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 1164)
---------------------------------------
Vector Time (GMT): 2009/204/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2455237
20 A = 6731451
56 meter
Y = 6138072
27 meter E =
0007281
Z = -1242324
30 I = 51
94394
XDOT = -4895
567808 Wp = 356
46765
YDOT = -766
264232 meter/sec RA = 120
26130 deg
ZDOT = 5894
564144 TA = 349
96718
MA = 349
98170
Ha = 187
898 n
mi
Hp = 185
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8055240
15 X = -2517656
85
Y = 20138032
40 feet Y = 6110267
50 meter
Z = -4075867
14 Z = -1254402
49
XDOT = -16061
574174 XDOT = -4915
269483
YDOT = -2513
990264 feet/sec YDOT = -821
120146 meter/sec
ZDOT = 19339
121208 ZDOT = 5870
734120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15649545
77 X = 4769981
55
Y = 15004413
82 feet Y = 4573345
33 meter
Z = -4123010
89 Z = -1256693
72
XDOT = -7307
882789 XDOT = -2227
442674
YDOT = 12905
759954 feet/sec YDOT = 3933
675634 meter/sec
ZDOT = 19245
398028 ZDOT = 5865
997319
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 09204
35660096
00010596 00000-0 82463-4 0 9000
2 25544 51
6386 121
1570 0005998 270
4448 89
6028 15
74012378 11652
Satellite: ISS
Catalog Number: 25544
Epoch time: 09204
35660096 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 121
1570 deg
Eccentricity:
0005998
Arg of perigee: 270
4448 deg
Mean anomaly: 89
6028 deg
Mean motion: 15
74012378 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1165
Checksum: 312
Coasting Arc #2 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2009/205/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4311668
81 A = 6720710
98 meter
Y = 316888
24 meter E =
0008295
Z = -5152775
14 I = 51
92226
XDOT = -2197
741124 Wp = 67
72056
YDOT = 7241
790707 meter/sec RA = 115
16960 deg
ZDOT = -1392
334086 TA = 188
98308
MA = 188
99793
Ha = 187
928 n
mi
Hp = 186
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14145895
06 X = 4332835
57
Y = 1039659
60 feet Y = 365222
62 meter
Z = -16905430
26 Z = -5131778
07
XDOT = -7210
436760 XDOT = -2271
793165
YDOT = 23759
155862 feet/sec YDOT = 7216
800345 meter/sec
ZDOT = -4568
025216 ZDOT = -1403
189756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6089752
24 X = 1856156
48
Y = -12918474
88 feet Y = -3937551
14 meter
Z = -16822863
49 Z = -5127608
79
XDOT = 18647
088065 XDOT = 5683
632442
YDOT = 14799
493555 feet/sec YDOT = 4510
885635 meter/sec
ZDOT = -4610
304525 ZDOT = -1405
220819
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 09205
37242327
00010596 00000-0 82463-4 0 9017
2 25544 51
6392 115
9398 0006137 275
3155 84
7308 15
74014705 11814
Satellite: ISS
Catalog Number: 25544
Epoch time: 09205
37242327 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 115
9398 deg
Eccentricity:
0006137
Arg of perigee: 275
3155 deg
Mean anomaly: 84
7308 deg
Mean motion: 15
74014705 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1181
Checksum: 301
Coasting Arc #3 (Orbit 1196)
---------------------------------------
Vector Time (GMT): 2009/206/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1373458
60 A = 6731444
12 meter
Y = -6476871
59 meter E =
0008477
Z = 1186953
69 I = 51
97044
XDOT = 4935
514784 Wp = 138
12023
YDOT = -39
953520 meter/sec RA = 110
03273 deg
ZDOT = -5911
157023 TA = 28
93439
MA = 28
88742
Ha = 188
041 n
mi
Hp = 186
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4506097
78 X = 1440016
10
Y = -21249578
70 feet Y = -6461140
70 meter
Z = 3894205
02 Z = 1193787
08
XDOT = 16192
633805 XDOT = 4964
309571
YDOT = -131
081104 feet/sec YDOT = 15
399685 meter/sec
ZDOT = -19393
559786 ZDOT = -5887
110764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18418540
87 X = -5613971
26
Y = -11506505
95 feet Y = -3507183
01 meter
Z = 3920716
49 Z = 1195034
39
XDOT = 4635
629079 XDOT = 1412
939743
YDOT = -14016
072738 feet/sec YDOT = -4272
098971 meter/sec
ZDOT = -19299
020810 ZDOT = -5882
341543
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 09206
38823425
00010596 00000-0 82463-4 0 9024
2 25544 51
6394 110
7230 0006199 279
9173 80
1290 15
74039233 11972
Satellite: ISS
Catalog Number: 25544
Epoch time: 09206
38823425 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 110
7230 deg
Eccentricity:
0006199
Arg of perigee: 279
9173 deg
Mean anomaly: 80
1290 deg
Mean motion: 15
74039233 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1197
Checksum: 306
Coasting Arc #4 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2009/207/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4285595
22 A = 6720443
18 meter
Y = 374840
97 meter E =
0002850
Z = 5165558
31 I = 51
94316
XDOT = 936
702771 Wp = 248
97599
YDOT = -7526
670828 meter/sec RA = 104
94213 deg
ZDOT = 1322
891609 TA = 188
41750
MA = 188
42228
Ha = 188
260 n
mi
Hp = 186
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14060351
78 X = -4314561
29
Y = 1229793
20 feet Y = 326754
65 meter
Z = 16947369
77 Z = 5144668
80
XDOT = 3073
171822 XDOT = 1014
371383
YDOT = -24693
801930 feet/sec YDOT = -7515
761883 meter/sec
ZDOT = 4340
195567 ZDOT = 1327
630245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3469296
73 X = -1057441
64
Y = 13782100
43 feet Y = 4200784
21 meter
Z = 16865257
60 Z = 5140530
52
XDOT = -21333
042706 XDOT = -6502
311417
YDOT = -10705
174339 feet/sec YDOT = -3262
937138 meter/sec
ZDOT = 4358
420535 ZDOT = 1328
446579
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 09207
40403295
00010596 00000-0 82463-4 0 9038
2 25544 51
6397 105
5064 0006349 283
5153 76
5302 15
74083139 12134
Satellite: ISS
Catalog Number: 25544
Epoch time: 09207
40403295 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 105
5064 deg
Eccentricity:
0006349
Arg of perigee: 283
5153 deg
Mean anomaly: 76
5302 deg
Mean motion: 15
74083139 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1213
Checksum: 292
Coasting Arc #5 (Orbit 1227)
---------------------------------------
Vector Time (GMT): 2009/208/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -256484
23 A = 6731426
19 meter
Y = 6626237
65 meter E =
0009428
Z = -1120498
74 I = 51
98615
XDOT = -4845
790923 Wp = 358
99987
YDOT = 813
984579 meter/sec RA = 99
80662 deg
ZDOT = 5931
294371 TA = 348
79141
MA = 348
81239
Ha = 188
432 n
mi
Hp = 185
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -841483
68 X = -325117
75
Y = 21739624
83 feet Y = 6622985
82 meter
Z = -3676176
98 Z = -1121910
99
XDOT = -15898
264184 XDOT = -4883
345806
YDOT = 2670
553082 feet/sec YDOT = 759
585720 meter/sec
ZDOT = 19459
627203 ZDOT = 5907
662546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20407849
28 X = 6220312
46
Y = 7536629
56 feet Y = 2297164
69 meter
Z = -3681380
49 Z = -1122084
77
XDOT = -1888
497007 XDOT = -575
613888
YDOT = 14560
151274 feet/sec YDOT = 4437
934108 meter/sec
ZDOT = 19366
752742 ZDOT = 5902
986236
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 09208
35633574
00010596 00000-0 82463-4 0 9049
2 25544 51
6393 100
6149 0006292 287
8401 72
2075 15
74070622 12289
Satellite: ISS
Catalog Number: 25544
Epoch time: 09208
35633574 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 100
6149 deg
Eccentricity:
0006292
Arg of perigee: 287
8401 deg
Mean anomaly: 72
2075 deg
Mean motion: 15
74070622 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1228
Checksum: 298
Coasting Arc #6 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2009/209/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4157639
87 A = 6720328
92 meter
Y = -1026995
80 meter E =
0009442
Z = -5186833
33 I = 51
95363
XDOT = 338
597875 Wp = 60
21376
YDOT = 7588
363449 meter/sec RA = 94
71451 deg
ZDOT = -1228
162181 TA = 198
07561
MA = 198
10921
Ha = 188
609 n
mi
Hp = 186
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13640550
75 X = 4194011
46
Y = -3369408
79 feet Y = -980298
85 meter
Z = -17017169
71 Z = -5166547
36
XDOT = 1110
885416 XDOT = 259
684489
YDOT = 24896
205542 feet/sec YDOT = 7591
708721 meter/sec
ZDOT = -4029
403482 ZDOT = -1226
708347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 824916
25 X = 251434
47
Y = -14122451
88 feet Y = -4304523
33 meter
Z = -16937457
64 Z = -5162537
09
XDOT = 23096
727464 XDOT = 7039
882531
YDOT = 6185
942674 feet/sec YDOT = 1885
475327 meter/sec
ZDOT = -4023
298630 ZDOT = -1226
301423
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 09209
37211393
00010596 00000-0 82463-4 0 9054
2 25544 51
6401 95
3974 0006341 291
9496 68
0993 15
74094451 12446
Satellite: ISS
Catalog Number: 25544
Epoch time: 09209
37211393 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 95
3974 deg
Eccentricity:
0006341
Arg of perigee: 291
9496 deg
Mean anomaly: 68
0993 deg
Mean motion: 15
74094451 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1244
Checksum: 320
Coasting Arc #7 (Orbit 1259)
---------------------------------------
Vector Time (GMT): 2009/210/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -844886
86 A = 6731440
46 meter
Y = -6595843
03 meter E =
0007529
Z = 1019518
82 I = 51
99307
XDOT = 4641
241358 Wp = 131
08149
YDOT = -1518
301994 meter/sec RA = 89
58190 deg
ZDOT = -5953
057204 TA = 37
82952
MA = 37
77663
Ha = 188
746 n
mi
Hp = 185
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2771938
52 X = -776020
84
Y = -21639904
94 feet Y = -6604906
09 meter
Z = 3344878
02 Z = 1015581
02
XDOT = 15227
169809 XDOT = 4686
793057
YDOT = -4981
305754 feet/sec YDOT = -1466
145645 meter/sec
ZDOT = -19531
027573 ZDOT = -5930
399662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21563012
00 X = -6572406
06
Y = -3333341
22 feet Y = -1016002
40 meter
Z = 3329067
11 Z = 1014699
66
XDOT = -764
575570 XDOT = -233
042634
YDOT = -14548
315690 feet/sec YDOT = -4434
326622 meter/sec
ZDOT = -19442
009027 ZDOT = -5925
924352
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 09210
38788145
00010596 00000-0 82463-4 0 9062
2 25544 51
6408 90
1804 0006335 295
8933 64
1576 15
74101038 12602
Satellite: ISS
Catalog Number: 25544
Epoch time: 09210
38788145 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 90
1804 deg
Eccentricity:
0006335
Arg of perigee: 295
8933 deg
Mean anomaly: 64
1576 deg
Mean motion: 15
74101038 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1260
Checksum: 304
Coasting Arc #8 (Orbit 1275)
---------------------------------------
Vector Time (GMT): 2009/211/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3936776
25 A = 6720033
10 meter
Y = 1609788
65 meter E =
0002734
Z = 5204809
35 I = 51
95389
XDOT = -1588
149573 Wp = 292
02055
YDOT = -7452
788115 meter/sec RA = 84
48836 deg
ZDOT = 1105
291497 TA = 147
48539
MA = 147
46855
Ha = 188
939 n
mi
Hp = 185
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12915932
57 X = -3979768
47
Y = 5281458
81 feet Y = 1565524
34 meter
Z = 17076146
17 Z = 5185580
35
XDOT = -5210
464478 XDOT = -1510
062462
YDOT = -24451
404578 feet/sec YDOT = -7470
111250 meter/sec
ZDOT = 3626
284439 ZDOT = 1097
765149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1696241
20 X = 517014
32
Y = 13943170
66 feet Y = 4249878
42 meter
Z = 17000607
26 Z = 5181785
09
XDOT = -23951
964629 XDOT = -7300
558819
YDOT = -1465
205373 feet/sec YDOT = -446
594598 meter/sec
ZDOT = 3596
330511 ZDOT = 1096
161540
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 09211
40363597
00010596 00000-0 82463-4 0 9077
2 25544 51
6409 84
9635 0006499 299
0784 60
9728 15
74160865 12760
Satellite: ISS
Catalog Number: 25544
Epoch time: 09211
40363597 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 84
9635 deg
Eccentricity:
0006499
Arg of perigee: 299
0784 deg
Mean anomaly: 60
9728 deg
Mean motion: 15
74160865 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1276
Checksum: 347
Coasting Arc #9 (Orbit 1290)
---------------------------------------
Vector Time (GMT): 2009/212/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1922085
61 A = 6731456
15 meter
Y = 6378808
17 meter E =
0011588
Z = -909541
04 I = 51
98810
XDOT = -4349
671128 Wp = 4
59850
YDOT = 2160
958189 meter/sec RA = 79
35692 deg
ZDOT = 5979
822637 TA = 345
51554
MA = 345
54872
Ha = 189
168 n
mi
Hp = 185
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6306055
15 X = 1855032
18
Y = 20927848
34 feet Y = 6399927
26 meter
Z = -2984058
54 Z = -900365
71
XDOT = -14270
574568 XDOT = -4402
560711
YDOT = 7089
757837 feet/sec YDOT = 2112
021159 meter/sec
ZDOT = 19618
840674 ZDOT = 5958
563905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21838922
97 X = 6656503
72
Y = -1009162
15 feet Y = -307592
62 meter
Z = -2947678
49 Z = -898452
40
XDOT = 3280
442305 XDOT = 999
878814
YDOT = 14089
760615 feet/sec YDOT = 4294
559035 meter/sec
ZDOT = 19535
338224 ZDOT = 5954
371091
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 09212
35589881
00010596 00000-0 82463-4 0 9089
2 25544 51
6411 80
0721 0006510 304
1190 55
9356 15
74129604 12913
Satellite: ISS
Catalog Number: 25544
Epoch time: 09212
35589881 = yrday
fracday
Element set: 908
Inclination: 51
6411 deg
RA of node: 80
0721 deg
Eccentricity:
0006510
Arg of perigee: 304
1190 deg
Mean anomaly: 55
9356 deg
Mean motion: 15
74129604 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1291
Checksum: 292
Coasting Arc #10 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2009/213/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3650066
80 A = 6719898
89 meter
Y = -2140341
30 meter E =
0011066
Z = -5229254
52 I = 51
94377
XDOT = 2784
833729 Wp = 57
97075
YDOT = 7107
517566 meter/sec RA = 74
26009 deg
ZDOT = -961
015908 TA = 202
87715
MA = 202
92649
Ha = 189
255 n
mi
Hp = 185
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11975284
77 X = 3699131
65
Y = -7022117
12 feet Y = -2099249
11 meter
Z = -17156346
84 Z = -5211403
80
XDOT = 9136
593599 XDOT = 2709
817664
YDOT = 23318
627184 feet/sec YDOT = 7138
239895 meter/sec
ZDOT = -3152
939330 ZDOT = -947
668640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4084031
51 X = -1244812
80
Y = -13358103
66 feet Y = -4071550
00 meter
Z = -17086239
04 Z = -5207885
66
XDOT = 23817
682851 XDOT = 7259
629733
YDOT = -3298
583198 feet/sec YDOT = -1005
408159 meter/sec
ZDOT = -3100
123466 ZDOT = -944
917633
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 09213
37163384
00010596 00000-0 82463-4 0 9099
2 25544 51
6420 74
8547 0006462 308
2619 51
7963 15
74174514 13073
Satellite: ISS
Catalog Number: 25544
Epoch time: 09213
37163384 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 74
8547 deg
Eccentricity:
0006462
Arg of perigee: 308
2619 deg
Mean anomaly: 51
7963 deg
Mean motion: 15
74174514 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1307
Checksum: 312
Coasting Arc #11 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2009/214/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2928402
86 A = 6731476
94 meter
Y = -6009627
38 meter E =
0007005
Z = 761359
37 I = 51
97341
XDOT = 3989
746123 Wp = 123
08527
YDOT = -2708
950062 meter/sec RA = 69
13049 deg
ZDOT = -6001
067640 TA = 48
65561
MA = 48
59537
Ha = 189
377 n
mi
Hp = 185
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9607620
94 X = -2864683
03
Y = -19716625
25 feet Y = -6042018
31 meter
Z = 2497898
19 Z = 747287
42
XDOT = 13089
718252 XDOT = 4048
893193
YDOT = -8887
631437 feet/sec YDOT = -2664
002918 meter/sec
ZDOT = -19688
542125 ZDOT = -5981
542422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21304228
46 X = -6493528
83
Y = 5239874
72 feet Y = 1597113
82 meter
Z = 2442283
68 Z = 744408
07
XDOT = -5516
038712 XDOT = -1681
288599
YDOT = -13230
112434 feet/sec YDOT = -4032
538270 meter/sec
ZDOT = -19611
867432 ZDOT = -5977
697193
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 09214
38735837
00010596 00000-0 82463-4 0 9101
2 25544 51
6421 69
6374 0006481 311
5068 48
5538 15
74160439 13231
Satellite: ISS
Catalog Number: 25544
Epoch time: 09214
38735837 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 69
6374 deg
Eccentricity:
0006481
Arg of perigee: 311
5068 deg
Mean anomaly: 48
5538 deg
Mean motion: 15
74160439 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1323
Checksum: 312
Coasting Arc #12 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2009/215/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3315629
11 A = 6719658
23 meter
Y = 2579083
67 meter E =
0003713
Z = 5246181
55 I = 51
92237
XDOT = -3895
980545 Wp = 328
49060
YDOT = -6596
036846 meter/sec RA = 64
02901 deg
ZDOT = 783
741274 TA = 114
10015
MA = 114
06131
Ha = 189
564 n
mi
Hp = 184
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10878048
25 X = -3369706
96
Y = 8461560
60 feet Y = 2541703
39 meter
Z = 17211881
73 Z = 5229943
47
XDOT = -12782
088403 XDOT = -3825
740178
YDOT = -21640
540833 feet/sec YDOT = -6639
211340 meter/sec
ZDOT = 2571
329639 ZDOT = 764
984792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6166313
86 X = 1879492
46
Y = 12413588
82 feet Y = 3783661
87 meter
Z = 17148125
26 Z = 5226748
58
XDOT = -22810
126606 XDOT = -6952
526589
YDOT = 7896
174237 feet/sec YDOT = 2406
753908 meter/sec
ZDOT = 2497
263536 ZDOT = 761
165926
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 09215
40307000
00010596 00000-0 82463-4 0 9113
2 25544 51
6421 64
4197 0006622 315
1928 44
8700 15
74219548 13392
Satellite: ISS
Catalog Number: 25544
Epoch time: 09215
40307000 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 64
4197 deg
Eccentricity:
0006622
Arg of perigee: 315
1928 deg
Mean anomaly: 44
8700 deg
Mean motion: 15
74219548 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1339
Checksum: 285
Coasting Arc #13 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2009/216/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3856470
74 A = 6731420
90 meter
Y = 5472945
44 meter E =
0013692
Z = -607126
96 I = 51
94806
XDOT = -3585
235232 Wp = 11
44516
YDOT = 3190
970746 meter/sec RA = 58
90014 deg
ZDOT = 6027
697518 TA = 341
96926
MA = 342
01778
Ha = 189
712 n
mi
Hp = 184
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12652463
07 X = 3797933
96
Y = 17955857
73 feet Y = 5515743
52 meter
Z = -1991886
36 Z = -588534
24
XDOT = -11762
582782 XDOT = -3649
931598
YDOT = 10469
064127 feet/sec YDOT = 3150
516194 meter/sec
ZDOT = 19775
910492 ZDOT = 6010
123990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19918500
18 X = 6071158
85
Y = -9275662
87 feet Y = -2827222
04 meter
Z = -1918512
09 Z = -584762
48
XDOT = 7518
557785 XDOT = 2291
656413
YDOT = 12094
705036 feet/sec YDOT = 3686
466095 meter/sec
ZDOT = 19706
924402 ZDOT = 6006
670558
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 09216
35529167
00010596 00000-0 82463-4 0 9129
2 25544 51
6424 59
5281 0006706 319
4313 40
6350 15
74213642 13543
Satellite: ISS
Catalog Number: 25544
Epoch time: 09216
35529167 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 59
5281 deg
Eccentricity:
0006706
Arg of perigee: 319
4313 deg
Mean anomaly: 40
6350 deg
Mean motion: 15
74213642 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1354
Checksum: 292
Coasting Arc #14 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2009/217/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2945744
96 A = 6719491
59 meter
Y = -2970859
79 meter E =
0012656
Z = -5267915
84 I = 51
89186
XDOT = 4894
983821 Wp = 58
44358
YDOT = 5905
818025 meter/sec RA = 53
79328 deg
ZDOT = -587
953471 TA = 205
95082
MA = 206
01434
Ha = 189
806 n
mi
Hp = 184
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9664517
59 X = 3004336
71
Y = -9746915
31 feet Y = -2937590
70 meter
Z = -17283188
45 Z = -5253463
66
XDOT = 16059
658204 XDOT = 4831
436256
YDOT = 19376
043390 feet/sec YDOT = 5960
201340 meter/sec
ZDOT = -1928
981204 ZDOT = -564
328026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8053089
62 X = -2454581
72
Y = -11203141
26 feet Y = -3414717
46 meter
Z = -17226469
02 Z = -5250627
76
XDOT = 20887
749965 XDOT = 6366
586189
YDOT = -12164
257362 feet/sec YDOT = -3707
665644 meter/sec
ZDOT = -1835
789442 ZDOT = -559
548622
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 09217
37098276
00010596 00000-0 82463-4 0 9135
2 25544 51
6425 54
3102 0006778 323
4914 36
5787 15
74250107 13703
Satellite: ISS
Catalog Number: 25544
Epoch time: 09217
37098276 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 54
3102 deg
Eccentricity:
0006778
Arg of perigee: 323
4914 deg
Mean anomaly: 36
5787 deg
Mean motion: 15
74250107 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1370
Checksum: 308
Coasting Arc #15 (Orbit 1385)
---------------------------------------
Vector Time (GMT): 2009/218/08:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4672033
64 A = 6731509
77 meter
Y = -4825677
55 meter E =
0006740
Z = 409504
90 I = 51
91326
XDOT = 3158
493588 Wp = 115
45683
YDOT = -3576
774096 meter/sec RA = 48
66553 deg
ZDOT = -6040
247586 TA = 60
10881
MA = 60
04186
Ha = 189
929 n
mi
Hp = 184
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15328194
36 X = -4619714
11
Y = -15832275
44 feet Y = -4877630
47 meter
Z = 1343520
00 Z = 386935
43
XDOT = 10362
511773 XDOT = 3227
596736
YDOT = -11734
823151 feet/sec YDOT = -3541
067217 meter/sec
ZDOT = -19817
085255 ZDOT = -6024
736331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17869599
74 X = -5446654
00
Y = 12904382
91 feet Y = 3933255
91 meter
Z = 1254528
15 Z = 382380
18
XDOT = -9168
658028 XDOT = -2794
606967
YDOT = -10750
595444 feet/sec YDOT = -3276
781491 meter/sec
ZDOT = -19756
225947 ZDOT = -6021
697669
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 09218
38666410
00010596 00000-0 82463-4 0 9149
2 25544 51
6424 49
0923 0006681 326
5028 33
5712 15
74210718 13863
Satellite: ISS
Catalog Number: 25544
Epoch time: 09218
38666410 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 49
0923 deg
Eccentricity:
0006681
Arg of perigee: 326
5028 deg
Mean anomaly: 33
5712 deg
Mean motion: 15
74210718 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1386
Checksum: 302
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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