Date:
June 4th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14800 38 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 348)
---------------------------------------
Vector Time (GMT): 2009/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2501368
36 A = 6722233
54 meter
Y = 3364715
96 meter E =
0012181
Z = 5245638
56 I = 51
77253
XDOT = -6611
231603 Wp = 64
26311
YDOT = -3912
139975 meter/sec RA = 26
87040 deg
ZDOT = -636
849670 TA = 31
81065
MA = 31
73713
Ha = 194
510 n
mi
Hp = 181
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8206589
12 X = -2564289
82
Y = 11039094
37 feet Y = 3336391
89 meter
Z = 17210100
25 Z = 5233334
30
XDOT = -21690
392399 XDOT = -6563
900306
YDOT = -12835
104906 feet/sec YDOT = -3985
805925 meter/sec
ZDOT = -2089
401805 ZDOT = -668
852675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7398920
16 X = 2255190
86
Y = 11666938
49 feet Y = 3556082
85 meter
Z = 17162044
95 Z = 5230991
30
XDOT = -18807
232189 XDOT = -5732
444371
YDOT = 15215
960314 feet/sec YDOT = 4637
824704 meter/sec
ZDOT = -2214
950164 ZDOT = -675
116810
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 09152
54654961
00010596 00000-0 82463-4 0 9007
2 25544 51
6419 27
1645 0009188 65
2935 294
9183 15
73299920 3498
Satellite: ISS
Catalog Number: 25544
Epoch time: 09152
54654961 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 27
1645 deg
Eccentricity:
0009188
Arg of perigee: 65
2935 deg
Mean anomaly: 294
9183 deg
Mean motion: 15
73299920 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 349
Checksum: 335
Coasting Arc #2 (Orbit 364)
---------------------------------------
Vector Time (GMT): 2009/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6141726
71 A = 6734046
04 meter
Y = 2721514
72 meter E =
0021709
Z = 318634
45 I = 51
78519
XDOT = -2207
031468 Wp = 56
56288
YDOT = 4240
376342 meter/sec RA = 21
75881 deg
ZDOT = 6041
102479 TA = 306
89425
MA = 307
09301
Ha = 194
394 n
mi
Hp = 181
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20150022
00 X = 6109289
91
Y = 8928854
08 feet Y = 2790013
70 meter
Z = 1045388
60 Z = 348392
80
XDOT = -7240
916891 XDOT = -2283
630960
YDOT = 13911
995872 feet/sec YDOT = 4215
267103 meter/sec
ZDOT = 19819
890022 ZDOT = 6030
194977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15189296
01 X = 4629697
42
Y = -15961688
65 feet Y = -4865122
70 meter
Z = 1162084
97 Z = 354203
50
XDOT = 9459
810214 XDOT = 2883
350153
YDOT = 10502
508839 feet/sec YDOT = 3201
164694 meter/sec
ZDOT = 19777
342198 ZDOT = 6028
133902
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 09153
56284067
00010596 00000-0 82463-4 0 9017
2 25544 51
6416 21
9505 0009130 68
8272 291
3865 15
73326493 3654
Satellite: ISS
Catalog Number: 25544
Epoch time: 09153
56284067 = yrday
fracday
Element set: 901
Inclination: 51
6416 deg
RA of node: 21
9505 deg
Eccentricity:
0009130
Arg of perigee: 68
8272 deg
Mean anomaly: 291
3865 deg
Mean motion: 15
73326493 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 365
Checksum: 311
Coasting Arc #3 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2009/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1350468
78 A = 6721959
96 meter
Y = -3952071
06 meter E =
0023772
Z = -5287271
69 I = 51
71586
XDOT = 7325
478284 Wp = 83
67102
YDOT = 2309
786849 meter/sec RA = 16
63085 deg
ZDOT = 147
702722 TA = 187
71416
MA = 187
75079
Ha = 194
336 n
mi
Hp = 181
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4430671
85 X = 1420246
12
Y = -12966112
39 feet Y = -3936578
53 meter
Z = -17346691
90 Z = -5280542
01
XDOT = 24033
721404 XDOT = 7298
387884
YDOT = 7578
040842 feet/sec YDOT = 2391
553137 meter/sec
ZDOT = 484
588984 ZDOT = 183
224896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10830878
92 X = -3301251
90
Y = -8446962
83 feet Y = -2574634
27 meter
Z = -17320494
34 Z = -5279286
67
XDOT = 14262
350832 XDOT = 4347
164534
YDOT = -19545
585617 feet/sec YDOT = -5957
494496 meter/sec
ZDOT = 623
842026 ZDOT = 190
147050
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 09154
51559414
00010596 00000-0 82463-4 0 9025
2 25544 51
6408 17
0619 0009077 71
8399 288
3751 15
73355193 3807
Satellite: ISS
Catalog Number: 25544
Epoch time: 09154
51559414 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 17
0619 deg
Eccentricity:
0009077
Arg of perigee: 71
8399 deg
Mean anomaly: 288
3751 deg
Mean motion: 15
73355193 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 380
Checksum: 322
Coasting Arc #4 (Orbit 395)
---------------------------------------
Vector Time (GMT): 2009/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6601166
39 A = 6734036
33 meter
Y = -1307942
59 meter E =
0018653
Z = 44738
78 I = 51
72773
XDOT = 874
219040 Wp = 109
88020
YDOT = -4688
122820 meter/sec RA = 11
50785 deg
ZDOT = -6043
710892 TA = 69
63461
MA = 69
43432
Ha = 194
340 n
mi
Hp = 181
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21657370
06 X = -6586267
48
Y = -4291150
24 feet Y = -1381677
39 meter
Z = 146780
79 Z = 12705
81
XDOT = 2868
172702 XDOT = 955
937159
YDOT = -15380
980380 feet/sec YDOT = -4677
889010 meter/sec
ZDOT = -19828
447809 ZDOT = -6039
266049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10673591
11 X = -3253310
57
Y = 19327472
53 feet Y = 5891013
63 meter
Z = 21241
12 Z = 6474
29
XDOT = -12336
488706 XDOT = -3760
161758
YDOT = -6740
624701 feet/sec YDOT = -2054
542409 meter/sec
ZDOT = -19811
226043 ZDOT = -6038
461698
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 09155
53184394
00010596 00000-0 82463-4 0 9030
2 25544 51
6408 11
8485 0009015 76
3401 283
8765 15
73346162 3964
Satellite: ISS
Catalog Number: 25544
Epoch time: 09155
53184394 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 11
8485 deg
Eccentricity:
0009015
Arg of perigee: 76
3401 deg
Mean anomaly: 283
8765 deg
Mean motion: 15
73346162 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 396
Checksum: 314
Coasting Arc #5 (Orbit 411)
---------------------------------------
Vector Time (GMT): 2009/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -153016
12 A = 6721834
42 meter
Y = 4169660
60 meter E =
0011289
Z = 5260403
84 I = 51
65703
XDOT = -7677
932035 Wp = 83
49635
YDOT = -635
255164 meter/sec RA = 6
38260 deg
ZDOT = 280
941344 TA = 3
84486
MA = 3
83619
Ha = 194
298 n
mi
Hp = 181
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -502021
38 X = -225185
06
Y = 13679988
83 feet Y = 4167545
09 meter
Z = 17258542
80 Z = 5259485
87
XDOT = -25190
065730 XDOT = -7671
622641
YDOT = -2084
170486 feet/sec YDOT = -721
079052 meter/sec
ZDOT = 921
723569 ZDOT = 243
656606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12928917
95 X = 3940734
19
Y = 4511721
61 feet Y = 1375172
75 meter
Z = 17255111
36 Z = 5259357
94
XDOT = -8914
270352 XDOT = -2717
069603
YDOT = 22587
892489 feet/sec YDOT = 6884
789631 meter/sec
ZDOT = 775
637729 ZDOT = 236
414380
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 09156
54807056
00010596 00000-0 82463-4 0 9040
2 25544 51
6401 6
6336 0008977 79
4156 280
8017 15
73392589 4121
Satellite: ISS
Catalog Number: 25544
Epoch time: 09156
54807056 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 6
6336 deg
Eccentricity:
0008977
Arg of perigee: 79
4156 deg
Mean anomaly: 280
8017 deg
Mean motion: 15
73392589 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 412
Checksum: 321
Coasting Arc #6 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2009/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6711051
26 A = 6733733
33 meter
Y = -198260
34 meter E =
0019042
Z = -435231
68 I = 51
66652
XDOT = 518
255710 Wp = 59
16331
YDOT = 4772
794285 meter/sec RA = 1
24594 deg
ZDOT = 6020
471381 TA = 296
10626
MA = 296
30208
Ha = 194
214 n
mi
Hp = 181
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22017884
73 X = 6714883
76
Y = -650460
44 feet Y = -123191
94 meter
Z = -1427925
47 Z = -402619
70
XDOT = 1700
314008 XDOT = 435
600272
YDOT = 15658
773900 feet/sec YDOT = 4778
126467 meter/sec
ZDOT = 19752
202693 ZDOT = 6022
789203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5345679
18 X = 1629363
01
Y = -21377150
80 feet Y = -6515755
57 meter
Z = -1300175
11 Z = -396293
38
XDOT = 13943
657863 XDOT = 4250
026917
YDOT = 2329
483626 feet/sec YDOT = 710
026609 meter/sec
ZDOT = 19761
466656 ZDOT = 6023
295037
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 09157
50076295
00010596 00000-0 82463-4 0 9051
2 25544 51
6390 1
7443 0008863 82
4622 277
7547 15
73428044 4274
Satellite: ISS
Catalog Number: 25544
Epoch time: 09157
50076295 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 1
7443 deg
Eccentricity:
0008863
Arg of perigee: 82
4622 deg
Mean anomaly: 277
7547 deg
Mean motion: 15
73428044 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 427
Checksum: 315
Coasting Arc #7 (Orbit 442)
---------------------------------------
Vector Time (GMT): 2009/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1014141
56 A = 6721742
25 meter
Y = -4101357
49 meter E =
0023714
Z = -5248491
64 I = 51
59566
XDOT = 7583
910196 Wp = 85
31479
YDOT = -1035
772795 meter/sec RA = 356
12242 deg
ZDOT = -656
657514 TA = 178
42703
MA = 178
41955
Ha = 194
132 n
mi
Hp = 181
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3327236
09 X = -942707
66
Y = -13455897
28 feet Y = -4112297
78 meter
Z = -17219460
76 Z = -5253245
67
XDOT = 24881
595131 XDOT = 7598
118679
YDOT = -3398
204707 feet/sec YDOT = -950
885512 meter/sec
ZDOT = -2154
388169 ZDOT = -619
780219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13834454
60 X = -4216741
76
Y = -304009
54 feet Y = -92662
11 meter
Z = -17238240
76 Z = -5254215
78
XDOT = 3027
706698 XDOT = 922
845001
YDOT = -23929
926572 feet/sec YDOT = -7293
841619 meter/sec
ZDOT = -2009
955655 ZDOT = -612
634484
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 09158
51694768
00010596 00000-0 82463-4 0 9065
2 25544 51
6378 356
5286 0008867 86
6321 273
5856 15
73471393 4432
Satellite: ISS
Catalog Number: 25544
Epoch time: 09158
51694768 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 356
5286 deg
Eccentricity:
0008867
Arg of perigee: 86
6321 deg
Mean anomaly: 273
5856 deg
Mean motion: 15
73471393 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 443
Checksum: 357
Coasting Arc #8 (Orbit 458)
---------------------------------------
Vector Time (GMT): 2009/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6495759
71 A = 6733288
02 meter
Y = 1597093
58 meter E =
0020908
Z = 704775
38 I = 51
60628
XDOT = -1773
950720 Wp = 112
25338
YDOT = -4517
051510 meter/sec RA = 350
97595 deg
ZDOT = -5980
962393 TA = 60
06383
MA = 59
85636
Ha = 193
985 n
mi
Hp = 181
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21311547
59 X = -6516559
58
Y = 5239808
33 feet Y = 1524337
76 meter
Z = 2312255
17 Z = 673168
60
XDOT = -5820
048295 XDOT = -1694
253861
YDOT = -14819
722802 feet/sec YDOT = -4536
442060 meter/sec
ZDOT = -19622
580029 ZDOT = -5989
387610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17239
58 X = 5254
62
Y = 21958925
37 feet Y = 6693080
45 meter
Z = 2188487
06 Z = 667050
86
XDOT = -14150
699900 XDOT = -4313
133330
YDOT = 2016
020396 feet/sec YDOT = 614
483017 meter/sec
ZDOT = -19655
758059 ZDOT = -5991
075056
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 09159
53310934
00010596 00000-0 82463-4 0 9079
2 25544 51
6385 351
3138 0008767 89
0854 271
1313 15
73542797 4592
Satellite: ISS
Catalog Number: 25544
Epoch time: 09159
53310934 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 351
3138 deg
Eccentricity:
0008767
Arg of perigee: 89
0854 deg
Mean anomaly: 271
1313 deg
Mean motion: 15
73542797 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 459
Checksum: 331
Coasting Arc #9 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2009/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2072272
19 A = 6721821
67 meter
Y = 3726551
31 meter E =
0012060
Z = 5186469
02 I = 51
53718
XDOT = -7183
999998 Wp = 101
24895
YDOT = 2617
826227 meter/sec RA = 345
85328 deg
ZDOT = 985
204491 TA = 339
33352
MA = 339
38225
Ha = 194
045 n
mi
Hp = 181
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6798793
29 X = 2005252
29
Y = 12226218
20 feet Y = 3749348
91 meter
Z = 17015974
48 Z = 5196374
08
XDOT = -23569
553799 XDOT = -7217
524992
YDOT = 8588
668725 feet/sec YDOT = 2537
302902 meter/sec
ZDOT = 3232
298198 ZDOT = 950
223652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13405340
01 X = 4085947
63
Y = -3830648
88 feet Y = -1167581
78 meter
Z = 17054922
39 Z = 5198340
34
XDOT = 2881
157352 XDOT = 878
176761
YDOT = 23925
619051 feet/sec YDOT = 7292
528687 meter/sec
ZDOT = 3095
345031 ZDOT = 943
461166
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 09160
54925235
00010596 00000-0 82463-4 0 9089
2 25544 51
6375 346
0979 0008875 94
0022 266
2156 15
73494915 4754
Satellite: ISS
Catalog Number: 25544
Epoch time: 09160
54925235 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 346
0979 deg
Eccentricity:
0008875
Arg of perigee: 94
0022 deg
Mean anomaly: 266
2156 deg
Mean motion: 15
73494915 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 475
Checksum: 333
Coasting Arc #10 (Orbit 489)
---------------------------------------
Vector Time (GMT): 2009/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5974375
63 A = 6732987
01 meter
Y = -2933771
30 meter E =
0016251
Z = -999598
35 I = 51
54677
XDOT = 2920
541816 Wp = 65
91856
YDOT = 3958
255777 meter/sec RA = 340
69572 deg
ZDOT = 5920
125963 TA = 283
14907
MA = 283
33037
Ha = 193
966 n
mi
Hp = 181
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19600969
91 X = 6011593
38
Y = -9625233
93 feet Y = -2866754
06 meter
Z = -3279522
13 Z = -970485
03
XDOT = 9581
830104 XDOT = 2847
304029
YDOT = 12986
403469 feet/sec YDOT = 3990
504367 meter/sec
ZDOT = 19422
985444 ZDOT = 5934
136785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5413832
58 X = -1650136
17
Y = -21172340
83 feet Y = -6453329
49 meter
Z = -3165567
13 Z = -964864
86
XDOT = 13103
472166 XDOT = 3993
938316
YDOT = -6221
178099 feet/sec YDOT = -1896
215084 meter/sec
ZDOT = 19478
031710 ZDOT = 5936
904065
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 09161
50186263
00010596 00000-0 82463-4 0 9097
2 25544 51
6374 341
2080 0008792 98
2374 261
9786 15
73570494 4902
Satellite: ISS
Catalog Number: 25544
Epoch time: 09161
50186263 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 341
2080 deg
Eccentricity:
0008792
Arg of perigee: 98
2374 deg
Mean anomaly: 261
9786 deg
Mean motion: 15
73570494 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 490
Checksum: 329
Coasting Arc #11 (Orbit 505)
---------------------------------------
Vector Time (GMT): 2009/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2965260
98 A = 6721700
16 meter
Y = -3161634
27 meter E =
0022831
Z = -5157104
47 I = 51
48170
XDOT = 6434
285486 Wp = 88
40366
YDOT = -4010
578096 meter/sec RA = 335
57432 deg
ZDOT = -1245
000785 TA = 169
66736
MA = 169
62036
Ha = 193
911 n
mi
Hp = 181
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9728546
51 X = -2904634
49
Y = -10372815
85 feet Y = -3194453
67 meter
Z = -16919634
09 Z = -5171362
95
XDOT = 21109
860519 XDOT = 6484
702202
YDOT = -13158
064618 feet/sec YDOT = -3938
344045 meter/sec
ZDOT = -4084
648244 ZDOT = -1213
621388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11994324
50 X = -3655870
11
Y = 7515205
36 feet Y = 2290634
59 meter
Z = -16975624
05 Z = -5174170
21
XDOT = -8415
741586 XDOT = -2565
118035
YDOT = -22350
345498 feet/sec YDOT = -6812
385308 meter/sec
ZDOT = -3961
855878 ZDOT = -1207
573672
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 09162
51796045
00010596 00000-0 82463-4 0 9106
2 25544 51
6376 335
9928 0008915 101
8353 258
3810 15
73610908 5061
Satellite: ISS
Catalog Number: 25544
Epoch time: 09162
51796045 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 335
9928 deg
Eccentricity:
0008915
Arg of perigee: 101
8353 deg
Mean anomaly: 258
3810 deg
Mean motion: 15
73610908 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 506
Checksum: 317
Coasting Arc #12 (Orbit 521)
---------------------------------------
Vector Time (GMT): 2009/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5236966
84 A = 6732535
33 meter
Y = 4049178
68 meter E =
0022203
Z = 1175067
36 I = 51
49211
XDOT = -3816
067905 Wp = 115
26356
YDOT = -3208
334459 meter/sec RA = 330
40850 deg
ZDOT = -5874
726012 TA = 51
83060
MA = 51
63078
Ha = 193
693 n
mi
Hp = 181
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17181649
75 X = -5287564
46
Y = 13284706
95 feet Y = 3990332
77 meter
Z = 3855207
86 Z = 1149504
03
XDOT = -12519
907826 XDOT = -3751
369927
YDOT = -10526
031689 feet/sec YDOT = -3250
645284 meter/sec
ZDOT = -19274
035472 ZDOT = -5893
107744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10156746
63 X = 3095776
37
Y = 19217025
48 feet Y = 5857349
37 meter
Z = 3755207
62 Z = 1144587
28
XDOT = -11086
587218 XDOT = -3379
191784
YDOT = 9690
605709 feet/sec YDOT = 2953
696620 meter/sec
ZDOT = -19346
186696 ZDOT = -5896
717705
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 09163
53403370
00010596 00000-0 82463-4 0 9116
2 25544 51
6375 330
7765 0008613 104
6047 255
6071 15
73676114 5226
Satellite: ISS
Catalog Number: 25544
Epoch time: 09163
53403370 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 330
7765 deg
Eccentricity:
0008613
Arg of perigee: 104
6047 deg
Mean anomaly: 255
6071 deg
Mean motion: 15
73676114 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 522
Checksum: 292
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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