Date:
March 13th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 3058)
---------------------------------------
Vector Time (GMT): 2009/070/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -486668
35 A = 6739632
78 meter
Y = -6712885
19 meter E =
0021646
Z = 100576
15 I = 51
98911
XDOT = 4722
315151 Wp = 123
86279
YDOT = -446
914725 meter/sec RA = 86
52265 deg
ZDOT = -6065
477345 TA = 55
05058
MA = 54
84747
Ha = 197
572 n
mi
Hp = 184
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1596680
94 X = -412056
15
Y = -22023901
53 feet Y = -6717910
21 meter
Z = 329974
26 Z = 98393
95
XDOT = 15493
159943 XDOT = 4756
426281
YDOT = -1466
255659 feet/sec YDOT = -393
917015 meter/sec
ZDOT = -19899
860055 ZDOT = -6042
453723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -420541
54 X = -128181
06
Y = -22077831
97 feet Y = -6729323
19 meter
Z = 320923
33 Z = 97817
43
XDOT = 14053
977415 XDOT = 4283
652316
YDOT = -600
437803 feet/sec YDOT = -183
013442 meter/sec
ZDOT = -19809
990169 ZDOT = -6038
085004
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 09070
55538322
00010596 00000-0 82463-4 0 9009
2 25544 51
6383 87
1024 0009632 111
2562 248
9630 15
71383304 30592
Satellite: ISS
Catalog Number: 25544
Epoch time: 09070
55538322 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 87
1024 deg
Eccentricity:
0009632
Arg of perigee: 111
2562 deg
Mean anomaly: 248
9630 deg
Mean motion: 15
71383304 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3059
Checksum: 291
Coasting Arc #2 (Orbit 3074)
---------------------------------------
Vector Time (GMT): 2009/071/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3843726
54 A = 6727903
43 meter
Y = 1824667
82 meter E =
0013276
Z = 5202499
31 I = 51
94620
XDOT = -1984
988247 Wp = 117
18910
YDOT = -7362
313523 meter/sec RA = 81
43961 deg
ZDOT = 1107
539559 TA = 322
24656
MA = 322
33964
Ha = 197
588 n
mi
Hp = 184
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12610651
39 X = -3889117
24
Y = 5986442
99 feet Y = 1781431
82 meter
Z = 17068567
31 Z = 5183716
17
XDOT = -6512
428633 XDOT = -1907
894292
YDOT = -24154
571927 feet/sec YDOT = -7384
079641 meter/sec
ZDOT = 3633
659970 ZDOT = 1098
084634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12917454
46 X = -3937240
12
Y = 5522591
17 feet Y = 1683285
79 meter
Z = 16995363
34 Z = 5180186
75
XDOT = -5251
925605 XDOT = -1600
786924
YDOT = -23433
261010 feet/sec YDOT = -7142
457956 meter/sec
ZDOT = 3596
167866 ZDOT = 1096
111966
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 09071
57289769
00010596 00000-0 82463-4 0 9011
2 25544 51
6377 81
8964 0009507 114
8518 245
3633 15
71402289 30756
Satellite: ISS
Catalog Number: 25544
Epoch time: 09071
57289769 = yrday
fracday
Element set: 901
Inclination: 51
6377 deg
RA of node: 81
8964 deg
Eccentricity:
0009507
Arg of perigee: 114
8518 deg
Mean anomaly: 245
3633 deg
Mean motion: 15
71402289 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3075
Checksum: 337
Coasting Arc #3 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/072/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2863923
77 A = 6738061
66 meter
Y = 5831454
97 meter E =
0013143
Z = -1795056
25 I = 51
97550
XDOT = -3720
488704 Wp = 84
21506
YDOT = 3571
331244 meter/sec RA = 76
32129 deg
ZDOT = 5702
874810 TA = 256
02502
MA = 256
17121
Ha = 197
409 n
mi
Hp = 184
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9396075
35 X = 2807222
65
Y = 19132070
12 feet Y = 5863163
83 meter
Z = -5889292
17 Z = -1781281
65
XDOT = -12206
327770 XDOT = -3787
850870
YDOT = 11716
966023 feet/sec YDOT = 3529
350487 meter/sec
ZDOT = 18710
219194 ZDOT = 5684
636759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9064649
62 X = 2762905
21
Y = 19307778
13 feet Y = 5885010
77 meter
Z = -5835060
61 Z = -1778526
47
XDOT = -11126
750114 XDOT = -3391
433435
YDOT = 10819
975106 feet/sec YDOT = 3297
928412 meter/sec
ZDOT = 18639
274227 ZDOT = 5681
250784
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 09072
52680587
00010596 00000-0 82463-4 0 9021
2 25544 51
6380 77
0169 0009627 118
3451 241
8683 15
71450322 30906
Satellite: ISS
Catalog Number: 25544
Epoch time: 09072
52680587 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 77
0169 deg
Eccentricity:
0009627
Arg of perigee: 118
3451 deg
Mean anomaly: 241
8683 deg
Mean motion: 15
71450322 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3090
Checksum: 307
Coasting Arc #4 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2009/073/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2423960
89 A = 6730148
23 meter
Y = -4220475
74 meter E =
0018211
Z = -4663228
07 I = 51
94015
XDOT = 4313
301763 Wp = 94
20830
YDOT = 5662
666247 meter/sec RA = 71
26399 deg
ZDOT = -2893
905990 TA = 147
27269
MA = 147
15974
Ha = 197
347 n
mi
Hp = 184
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7952627
60 X = 2493627
91
Y = -13846705
18 feet Y = -4192980
43 meter
Z = -15299304
70 Z = -4651282
93
XDOT = 14151
252502 XDOT = 4263
718374
YDOT = 18578
301335 feet/sec YDOT = 5710
622641 meter/sec
ZDOT = -9494
442226 ZDOT = -2873
072864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8065863
72 X = 2458475
26
Y = -13832312
29 feet Y = -4216088
79 meter
Z = -15252974
59 Z = -4649106
65
XDOT = 13163
681915 XDOT = 4012
290248
YDOT = 18015
639029 feet/sec YDOT = 5491
166776 meter/sec
ZDOT = -9412
670587 ZDOT = -2868
981995
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 09073
54429592
00010596 00000-0 82463-4 0 9032
2 25544 51
6376 71
8098 0009461 121
8778 238
3306 15
71432888 31069
Satellite: ISS
Catalog Number: 25544
Epoch time: 09073
54429592 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 71
8098 deg
Eccentricity:
0009461
Arg of perigee: 121
8778 deg
Mean anomaly: 238
3306 deg
Mean motion: 15
71432888 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3106
Checksum: 331
Coasting Arc #5 (Orbit 3121)
---------------------------------------
Vector Time (GMT): 2009/074/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4466171
02 A = 6734921
59 meter
Y = -3855666
84 meter E =
0021331
Z = 3223357
44 I = 51
94599
XDOT = 1540
120757 Wp = 106
35274
YDOT = -5821
367368 meter/sec RA = 66
12295 deg
ZDOT = -4809
190408 TA = 36
14055
MA = 35
99657
Ha = 197
237 n
mi
Hp = 184
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14652792
05 X = -4438382
85
Y = -12649825
59 feet Y = -3905454
62 meter
Z = 10575319
68 Z = 3201728
50
XDOT = 5052
889623 XDOT = 1628
463960
YDOT = -19098
974303 feet/sec YDOT = -5803
651153 meter/sec
ZDOT = -15778
183753 ZDOT = -4801
493599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14906695
67 X = -4543560
84
Y = -12421671
97 feet Y = -3786125
62 meter
Z = 10490580
48 Z = 3197528
93
XDOT = 3943
483194 XDOT = 1201
973678
YDOT = -18089
043445 feet/sec YDOT = -5513
540442 meter/sec
ZDOT = -15748
551234 ZDOT = -4800
158416
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 09074
56177195
00010596 00000-0 82463-4 0 9045
2 25544 51
6378 66
6041 0009262 125
3527 234
8502 15
71479240 31221
Satellite: ISS
Catalog Number: 25544
Epoch time: 09074
56177195 = yrday
fracday
Element set: 904
Inclination: 51
6378 deg
RA of node: 66
6041 deg
Eccentricity:
0009262
Arg of perigee: 125
3527 deg
Mean anomaly: 234
8502 deg
Mean motion: 15
71479240 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3122
Checksum: 306
Coasting Arc #6 (Orbit 3137)
---------------------------------------
Vector Time (GMT): 2009/075/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -120472
03 A = 6733525
70 meter
Y = 5662904
66 meter E =
0020245
Z = 3630965
18 I = 51
92916
XDOT = -5578
309803 Wp = 109
78663
YDOT = -2960
515262 meter/sec RA = 61
07887 deg
ZDOT = 4405
707173 TA = 293
48982
MA = 293
70246
Ha = 197
043 n
mi
Hp = 184
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -395249
44 X = -201425
16
Y = 18579083
53 feet Y = 5661104
97 meter
Z = 11912615
42 Z = 3630183
09
XDOT = -18301
541350 XDOT = -5566
192323
YDOT = -9712
976580 feet/sec YDOT = -3022
827260 meter/sec
ZDOT = 14454
419860 ZDOT = 4378
637340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 141749
26 X = 43205
17
Y = 18584446
31 feet Y = 5664539
24 meter
Z = 11909963
71 Z = 3630156
94
XDOT = -17336
390290 XDOT = -5284
131760
YDOT = -9118
770313 feet/sec YDOT = -2779
401191 meter/sec
ZDOT = 14348
501614 ZDOT = 4373
423292
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 09075
57923433
00010596 00000-0 82463-4 0 9052
2 25544 51
6382 61
3992 0009282 130
3292 229
8682 15
71521740 31383
Satellite: ISS
Catalog Number: 25544
Epoch time: 09075
57923433 = yrday
fracday
Element set: 905
Inclination: 51
6382 deg
RA of node: 61
3992 deg
Eccentricity:
0009282
Arg of perigee: 130
3292 deg
Mean anomaly: 229
8682 deg
Mean motion: 15
71521740 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3138
Checksum: 315
Coasting Arc #7 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2009/076/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4981847
52 A = 6731218
81 meter
Y = 1254349
32 meter E =
0017787
Z = -4367860
17 I = 51
90562
XDOT = 1311
475322 Wp = 121
54324
YDOT = 6744
974514 meter/sec RA = 55
93163 deg
ZDOT = 3433
960256 TA = 183
06436
MA = 183
07527
Ha = 197
046 n
mi
Hp = 184
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16344644
11 X = 4988669
10
Y = 4115319
29 feet Y = 1310097
28 meter
Z = -14330249
89 Z = -4343641
92
XDOT = 4302
740558 XDOT = 1219
272937
YDOT = 22129
181477 feet/sec YDOT = 6759
124747 meter/sec
ZDOT = 11266
273807 ZDOT = 3440
107253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16611686
07 X = 5063241
91
Y = 3292301
15 feet Y = 1003493
39 meter
Z = -14235587
27 Z = -4339007
00
XDOT = 5574
029573 XDOT = 1698
964214
YDOT = 20679
548280 feet/sec YDOT = 6303
126316 meter/sec
ZDOT = 11290
748704 ZDOT = 3441
420205
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 09076
53309519
00010596 00000-0 82463-4 0 9063
2 25544 51
6383 56
5182 0009241 132
4788 227
7156 15
71482232 31531
Satellite: ISS
Catalog Number: 25544
Epoch time: 09076
53309519 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 56
5182 deg
Eccentricity:
0009241
Arg of perigee: 132
4788 deg
Mean anomaly: 227
7156 deg
Mean motion: 15
71482232 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3153
Checksum: 314
Coasting Arc #8 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2009/077/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2400320
34 A = 6736824
13 meter
Y = -5844268
29 meter E =
0014902
Z = -2328736
99 I = 51
90833
XDOT = 5438
583577 Wp = 135
32143
YDOT = -76
754878 meter/sec RA = 50
87785 deg
ZDOT = -5444
425766 TA = 70
74619
MA = 70
58503
Ha = 196
883 n
mi
Hp = 184
919
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7875066
72 X = -2323477
86
Y = -19174108
57 feet Y = -5870680
47 meter
Z = -7640213
21 Z = -2340210
88
XDOT = 17843
121971 XDOT = 5465
485493
YDOT = -251
820466 feet/sec YDOT = -15
787165 meter/sec
ZDOT = -17862
289258 ZDOT = -5417
939982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9097012
26 X = -2772769
34
Y = -18606843
22 feet Y = -5671365
81 meter
Z = -7685422
98 Z = -2342516
92
XDOT = 16532
087127 XDOT = 5038
980156
YDOT = -789
633998 feet/sec YDOT = -240
680443 meter/sec
ZDOT = -17758
861022 ZDOT = -5412
900840
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 09077
55053175
00010596 00000-0 82463-4 0 9071
2 25544 51
6391 51
3118 0009182 136
2788 223
9103 15
71531979 31698
Satellite: ISS
Catalog Number: 25544
Epoch time: 09077
55053175 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 51
3118 deg
Eccentricity:
0009182
Arg of perigee: 136
2788 deg
Mean anomaly: 223
9103 deg
Mean motion: 15
71531979 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3169
Checksum: 319
Coasting Arc #9 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2009/078/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4226545
41 A = 6728180
52 meter
Y = 1344053
55 meter E =
0011030
Z = 5049613
32 I = 51
85970
XDOT = -4129
060463 Wp = 110
40800
YDOT = -6254
085952 meter/sec RA = 45
74396 deg
ZDOT = -1792
024807 TA = 356
78778
MA = 356
79486
Ha = 196
926 n
mi
Hp = 185
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13866618
79 X = -4265790
57
Y = 4409624
52 feet Y = 1296570
56 meter
Z = 16566972
85 Z = 5028985
62
XDOT = -13546
786297 XDOT = -4050
114108
YDOT = -20518
654699 feet/sec YDOT = -6299
818144 meter/sec
ZDOT = -5879
346481 ZDOT = -1811
891658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13541775
20 X = -4127533
08
Y = 5568477
78 feet Y = 1697272
03 meter
Z = 16486505
82 Z = 5025086
97
XDOT = -14784
421976 XDOT = -4506
291818
YDOT = -18322
009720 feet/sec YDOT = -5584
548563 meter/sec
ZDOT = -5957
358760 ZDOT = -1815
802950
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 09078
56795461
00010596 00000-0 82463-4 0 9085
2 25544 51
6392 46
1064 0009145 140
3872 219
7960 15
71545657 31850
Satellite: ISS
Catalog Number: 25544
Epoch time: 09078
56795461 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 46
1064 deg
Eccentricity:
0009145
Arg of perigee: 140
3872 deg
Mean anomaly: 219
7960 deg
Mean motion: 15
71545657 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3185
Checksum: 335
Coasting Arc #10 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2009/079/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4656303
29 A = 6738773
62 meter
Y = 4805812
48 meter E =
0016225
Z = 778686
42 I = 51
87432
XDOT = -3927
439418 Wp = 87
69496
YDOT = 2818
343023 meter/sec RA = 40
66519 deg
ZDOT = 5984
865387 TA = 280
75444
MA = 280
93706
Ha = 196
680 n
mi
Hp = 185
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15276585
58 X = 4598435
15
Y = 15767101
30 feet Y = 4857558
44 meter
Z = 2554745
47 Z = 801165
72
XDOT = -12885
299927 XDOT = -3987
735732
YDOT = 9246
532228 feet/sec YDOT = 2774
087185 meter/sec
ZDOT = 19635
385129 ZDOT = 5965
639572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16779353
30 X = 5114346
89
Y = 14141105
31 feet Y = 4310208
90 meter
Z = 2642861
77 Z = 805544
27
XDOT = -10964
519522 XDOT = -3341
985550
YDOT = 9291
558575 feet/sec YDOT = 2832
067054 meter/sec
ZDOT = 19560
490645 ZDOT = 5962
037549
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 09079
58536205
00010596 00000-0 82463-4 0 9098
2 25544 51
6392 40
9002 0009180 144
5944 215
5828 15
71586033 32018
Satellite: ISS
Catalog Number: 25544
Epoch time: 09079
58536205 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 40
9002 deg
Eccentricity:
0009180
Arg of perigee: 144
5944 deg
Mean anomaly: 215
5828 deg
Mean motion: 15
71586033 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3201
Checksum: 306
Coasting Arc #11 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2009/080/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2442356
73 A = 6727002
96 meter
Y = -3376483
81 meter E =
0021277
Z = -5297813
36 I = 51
81211
XDOT = 6242
502104 Wp = 111
11583
YDOT = 4477
690536 meter/sec RA = 35
55391 deg
ZDOT = 16
640675 TA = 159
08567
MA = 158
99851
Ha = 196
570 n
mi
Hp = 185
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8012981
40 X = 2505667
08
Y = -11077702
79 feet Y = -3348818
23 meter
Z = -17381277
44 Z = -5285794
61
XDOT = 20480
649947 XDOT = 6191
887029
YDOT = 14690
585749 feet/sec YDOT = 4547
214830 meter/sec
ZDOT = 54
595390 ZDOT = 46
843157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6745432
11 X = 2056007
71
Y = -11960105
21 feet Y = -3645440
07 meter
Z = -17334566
75 Z = -5283575
95
XDOT = 21202
344897 XDOT = 6462
474725
YDOT = 11672
010513 feet/sec YDOT = 3557
628804 meter/sec
ZDOT = 172
852170 ZDOT = 52
685341
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 09080
53916962
00010596 00000-0 82463-4 0 9109
2 25544 51
6400 36
0189 0009035 148
1743 211
9966 15
71584544 32160
Satellite: ISS
Catalog Number: 25544
Epoch time: 09080
53916962 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 36
0189 deg
Eccentricity:
0009035
Arg of perigee: 148
1743 deg
Mean anomaly: 211
9966 deg
Mean motion: 15
71584544 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3216
Checksum: 309
Coasting Arc #12 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2009/081/12:33:35
153
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6039877
91 A = 6738792
83 meter
Y = -2863896
74 meter E =
0022002
Z = 752037
46 I = 51
82792
XDOT = 1434
800554 Wp = 136
85029
YDOT = -4622
857487 meter/sec RA = 30
44277 deg
ZDOT = -5994
543019 TA = 34
97393
MA = 34
82961
Ha = 196
488 n
mi
Hp = 185
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19815872
42 X = -6011057
66
Y = -9395986
68 feet Y = -2931276
98 meter
Z = 2467314
51 Z = 722766
35
XDOT = 4707
350899 XDOT = 1515
507485
YDOT = -15166
855271 feet/sec YDOT = -4606
361862 meter/sec
ZDOT = -19667
135889 ZDOT = -5987
376507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20919383
89 X = -6376228
21
Y = -6624552
32 feet Y = -2019163
55 meter
Z = 2352804
83 Z = 717134
91
XDOT = 2239
934424 XDOT = 682
732012
YDOT = -14154
641044 feet/sec YDOT = -4314
334590 meter/sec
ZDOT = -19639
460003 ZDOT = -5986
107409
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 09081
55655029
00010596 00000-0 82463-4 0 9117
2 25544 51
6407 30
8128 0009086 151
8636 208
3018 15
71602736 32320
Satellite: ISS
Catalog Number: 25544
Epoch time: 09081
55655029 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 30
8128 deg
Eccentricity:
0009086
Arg of perigee: 151
8636 deg
Mean anomaly: 208
3018 deg
Mean motion: 15
71602736 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3232
Checksum: 297
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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