Date:
May 8th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 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 3943)
---------------------------------------
Vector Time (GMT): 2009/126/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6333856
08 A = 6736094
77 meter
Y = 2236065
66 meter E =
0017492
Z = 321038
09 I = 51
77955
XDOT = -1313
539966 Wp = 17
05923
YDOT = -4597
743962 meter/sec RA = 158
39820 deg
ZDOT = 6042
416529 TA = 346
42459
MA = 346
47158
Ha = 193
289 n
mi
Hp = 186
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20780367
73 X = -6359948
97
Y = 7336173
41 feet Y = 2165090
88 meter
Z = 1053274
58 Z = 290204
32
XDOT = -4309
514323 XDOT = -1291
383108
YDOT = -15084
461818 feet/sec YDOT = -4612
308998 meter/sec
ZDOT = 19824
201211 ZDOT = 6036
088938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19858085
94 X = 6052744
59
Y = 9567589
39 feet Y = 2916201
25 meter
Z = 932827
25 Z = 284325
75
XDOT = -6879
626130 XDOT = -2096
910044
YDOT = 12324
781635 feet/sec YDOT = 3756
593442 meter/sec
ZDOT = 19799
109251 ZDOT = 6034
768500
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 09126
81542616
00010596 00000-0 82463-4 0 9001
2 25544 51
6386 159
0767 0009358 331
6239 28
4412 15
72615019 39446
Satellite: ISS
Catalog Number: 25544
Epoch time: 09126
81542616 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 159
0767 deg
Eccentricity:
0009358
Arg of perigee: 331
6239 deg
Mean anomaly: 28
4412 deg
Mean motion: 15
72615019 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3944
Checksum: 317
Coasting Arc #2 (Orbit 3958)
---------------------------------------
Vector Time (GMT): 2009/127/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2011018
96 A = 6724024
63 meter
Y = 3650508
21 meter E =
0014220
Z = -5286272
99 I = 51
76646
XDOT = -6820
328880 Wp = 51
60857
YDOT = 3551
195199 meter/sec RA = 153
28097 deg
ZDOT = -133
878065 TA = 217
07238
MA = 217
17069
Ha = 193
461 n
mi
Hp = 186
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6597831
23 X = 1995729
20
Y = 11976732
97 feet Y = 3672911
36 meter
Z = -17343415
32 Z = -5276540
22
XDOT = -22376
407085 XDOT = -6858
881666
YDOT = 11650
902885 feet/sec YDOT = 3474
710747 meter/sec
ZDOT = -439
232498 ZDOT = -167
105407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3542734
89 X = 1079825
60
Y = -13257108
96 feet Y = -4040766
81 meter
Z = -17305076
02 Z = -5274587
17
XDOT = 23198
334207 XDOT = 7070
852266
YDOT = 6978
117399 feet/sec YDOT = 2126
930183 meter/sec
ZDOT = -568
960323 ZDOT = -173
419107
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 09127
76860376
00010596 00000-0 82463-4 0 9013
2 25544 51
6389 154
1915 0009406 335
3228 24
7484 15
72628278 39598
Satellite: ISS
Catalog Number: 25544
Epoch time: 09127
76860376 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 154
1915 deg
Eccentricity:
0009406
Arg of perigee: 335
3228 deg
Mean anomaly: 24
7484 deg
Mean motion: 15
72628278 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3959
Checksum: 341
Coasting Arc #3 (Orbit 3974)
---------------------------------------
Vector Time (GMT): 2009/128/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5468501
06 A = 6735914
42 meter
Y = -3895360
08 meter E =
0006966
Z = 539889
94 I = 51
83283
XDOT = 3165
383094 Wp = 86
58216
YDOT = 3600
629063 meter/sec RA = 148
16042 deg
ZDOT = -6016
212212 TA = 87
56643
MA = 87
48668
Ha = 193
563 n
mi
Hp = 186
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17941276
45 X = 5509030
45
Y = -12780052
74 feet Y = -3833981
53 meter
Z = 1771292
47 Z = 566554
68
XDOT = 10385
115139 XDOT = 3154
111302
YDOT = 11813
087476 feet/sec YDOT = 3635
963624 meter/sec
ZDOT = -19738
229043 ZDOT = -6000
861570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21819808
76 X = -6650677
71
Y = -2955618
16 feet Y = -900872
42 meter
Z = 1875337
95 Z = 571603
01
XDOT = 215
425119 XDOT = 65
661576
YDOT = -14207
330240 feet/sec YDOT = -4330
394257 meter/sec
ZDOT = -19677
916857 ZDOT = -5997
829058
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 09128
78531821
00010596 00000-0 82463-4 0 9027
2 25544 51
6391 148
9805 0009382 339
4241 20
6543 15
72635754 39759
Satellite: ISS
Catalog Number: 25544
Epoch time: 09128
78531821 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 148
9805 deg
Eccentricity:
0009382
Arg of perigee: 339
4241 deg
Mean anomaly: 20
6543 deg
Mean motion: 15
72635754 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3975
Checksum: 326
Coasting Arc #4 (Orbit 3990)
---------------------------------------
Vector Time (GMT): 2009/129/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3434800
40 A = 6724249
17 meter
Y = -2530111
96 meter E =
0006808
Z = 5196298
92 I = 51
81825
XDOT = 5528
140588 Wp = 3
26306
YDOT = -5245
183173 meter/sec RA = 143
06313 deg
ZDOT = 1106
824159 TA = 76
23868
MA = 76
16291
Ha = 193
675 n
mi
Hp = 185
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11269030
18 X = -3431496
18
Y = -8300892
25 feet Y = -2568503
91 meter
Z = 17048224
81 Z = 5179620
11
XDOT = 18136
944185 XDOT = 5581
005379
YDOT = -17208
606212 feet/sec YDOT = -5183
068800 meter/sec
ZDOT = 3631
312859 ZDOT = 1133
808351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2843589
41 X = 866726
05
Y = 13785378
71 feet Y = 4201783
43 meter
Z = 16982789
99 Z = 5176354
39
XDOT = -23974
298264 XDOT = -7307
366111
YDOT = 368
852945 feet/sec YDOT = 112
426378 meter/sec
ZDOT = 3736
531852 ZDOT = 1138
894908
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 09129
80202168
00010596 00000-0 82463-4 0 9031
2 25544 51
6389 143
7696 0009425 342
4777 17
6059 15
72691993 39916
Satellite: ISS
Catalog Number: 25544
Epoch time: 09129
80202168 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 143
7696 deg
Eccentricity:
0009425
Arg of perigee: 342
4777 deg
Mean anomaly: 17
6059 deg
Mean motion: 15
72691993 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3991
Checksum: 347
Coasting Arc #5 (Orbit 4005)
---------------------------------------
Vector Time (GMT): 2009/130/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4082138
43 A = 6735116
33 meter
Y = 5159326
23 meter E =
0016391
Z = -1394959
81 I = 51
87776
XDOT = -4578
634910 Wp = 10
91071
YDOT = -2048
875666 meter/sec RA = 137
92951 deg
ZDOT = 5847
653682 TA = 333
80176
MA = 333
88459
Ha = 193
820 n
mi
Hp = 185
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13392842
62 X = -4132750
91
Y = 16926923
33 feet Y = 5113394
54 meter
Z = -4576639
81 Z = -1414913
57
XDOT = -15021
768077 XDOT = -4583
791095
YDOT = -6722
033026 feet/sec YDOT = -2100
106108 meter/sec
ZDOT = 19185
215491 ZDOT = 5825
397518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21207914
47 X = 6464172
33
Y = -3923744
67 feet Y = -1195957
37 meter
Z = -4654373
27 Z = -1418652
97
XDOT = 6666
561252 XDOT = 2031
967870
YDOT = 13481
431174 feet/sec YDOT = 4109
140222 meter/sec
ZDOT = 19097
984807 ZDOT = 5821
065769
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 09130
75517578
00010596 00000-0 82463-4 0 9042
2 25544 51
6390 138
8840 0009528 346
7516 13
3395 15
72660821 40066
Satellite: ISS
Catalog Number: 25544
Epoch time: 09130
75517578 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 138
8840 deg
Eccentricity:
0009528
Arg of perigee: 346
7516 deg
Mean anomaly: 13
3395 deg
Mean motion: 15
72660821 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4006
Checksum: 318
Coasting Arc #6 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2009/131/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4422249
40 A = 6725224
89 meter
Y = 985173
96 meter E =
0016771
Z = -4983354
10 I = 51
86686
XDOT = -3741
304023 Wp = 40
62677
YDOT = 6396
038985 meter/sec RA = 132
85017 deg
ZDOT = -2046
993891 TA = 209
53866
MA = 209
63352
Ha = 193
943 n
mi
Hp = 185
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14508692
25 X = 4435112
93
Y = 3232198
04 feet Y = 1034698
67 meter
Z = -16349586
94 Z = -4961839
13
XDOT = -12274
619499 XDOT = -3802
603475
YDOT = 20984
379873 feet/sec YDOT = 6353
859047 meter/sec
ZDOT = -6715
859224 ZDOT = -2065
317533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9060168
05 X = -2761539
22
Y = -11900040
26 feet Y = -3627132
27 meter
Z = -16265320
31 Z = -4957669
63
XDOT = 22027
302845 XDOT = 6713
921907
YDOT = -7454
971533 feet/sec YDOT = -2272
275323 meter/sec
ZDOT = -6787
147196 ZDOT = -2068
722465
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 09131
77186309
00010596 00000-0 82463-4 0 9050
2 25544 51
6400 133
6728 0009517 351
1446 8
9547 15
72704782 40228
Satellite: ISS
Catalog Number: 25544
Epoch time: 09131
77186309 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 133
6728 deg
Eccentricity:
0009517
Arg of perigee: 351
1446 deg
Mean anomaly: 8
9547 deg
Mean motion: 15
72704782 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4022
Checksum: 308
Coasting Arc #7 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2009/132/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2414812
28 A = 6733856
58 meter
Y = -5900135
48 meter E =
0013296
Z = 2166853
31 I = 51
91508
XDOT = 5354
404084 Wp = 68
95448
YDOT = 151
244243 meter/sec RA = 127
70628 deg
ZDOT = -5523
557217 TA = 86
91261
MA = 86
76047
Ha = 194
045 n
mi
Hp = 185
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7922612
48 X = 2470082
82
Y = -19357399
86 feet Y = -5872822
88 meter
Z = 7109098
78 Z = 2178718
11
XDOT = 17566
942534 XDOT = 5379
147619
YDOT = 496
208146 feet/sec YDOT = 211
259351 meter/sec
ZDOT = -18121
906880 ZDOT = -5497
485118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18350826
62 X = -5593331
96
Y = 10003346
08 feet Y = 3049019
88 meter
Z = 7155154
29 Z = 2180891
03
XDOT = -12641
366582 XDOT = -3853
088534
YDOT = -10227
015353 feet/sec YDOT = -3117
194279 meter/sec
ZDOT = -18019
849005 ZDOT = -5492
449977
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 09132
78854185
00010596 00000-0 82463-4 0 9067
2 25544 51
6399 128
4615 0009463 354
7956 5
3106 15
72685810 40386
Satellite: ISS
Catalog Number: 25544
Epoch time: 09132
78854185 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 128
4615 deg
Eccentricity:
0009463
Arg of perigee: 354
7956 deg
Mean anomaly: 5
3106 deg
Mean motion: 15
72685810 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4038
Checksum: 333
Coasting Arc #8 (Orbit 4053)
---------------------------------------
Vector Time (GMT): 2009/133/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4802767
30 A = 6726582
00 meter
Y = 755317
06 meter E =
0009329
Z = 4639711
03 I = 51
90860
XDOT = 1722
892198 Wp = 50
56059
YDOT = -6922
180843 meter/sec RA = 122
64062 deg
ZDOT = 2912
270103 TA = 10
74731
MA = 10
72739
Ha = 194
289 n
mi
Hp = 184
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15757110
56 X = -4833395
47
Y = 2478074
33 feet Y = 701437
90 meter
Z = 15222149
06 Z = 4616304
71
XDOT = 5652
533459 XDOT = 1786
021755
YDOT = -22710
567070 feet/sec YDOT = -6902
561832 meter/sec
ZDOT = 9554
691940 ZDOT = 2920
792486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13975580
81 X = 4259757
03
Y = 7867025
41 feet Y = 2397869
35 meter
Z = 15130573
68 Z = 4611798
86
XDOT = -17885
515542 XDOT = -5451
505137
YDOT = 13345
746886 feet/sec YDOT = 4067
783651 meter/sec
ZDOT = 9587
608374 ZDOT = 2922
303033
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 09133
80521024
00010596 00000-0 82463-4 0 9075
2 25544 51
6406 123
2501 0009549 358
6196 1
4938 15
72712783 40544
Satellite: ISS
Catalog Number: 25544
Epoch time: 09133
80521024 = yrday
fracday
Element set: 907
Inclination: 51
6406 deg
RA of node: 123
2501 deg
Eccentricity:
0009549
Arg of perigee: 358
6196 deg
Mean anomaly: 1
4938 deg
Mean motion: 15
72712783 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4054
Checksum: 299
Coasting Arc #9 (Orbit 4068)
---------------------------------------
Vector Time (GMT): 2009/134/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -577273
06 A = 6732089
25 meter
Y = 6039395
17 meter E =
0012318
Z = -2906691
54 I = 51
94309
XDOT = -5469
955634 Wp = 21
39063
YDOT = 1909
689326 meter/sec RA = 117
48955 deg
ZDOT = 5072
105513 TA = 305
32897
MA = 305
44406
Ha = 194
252 n
mi
Hp = 184
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1893940
47 X = -630643
43
Y = 19814288
63 feet Y = 6032641
68 meter
Z = -9536389
58 Z = -2909624
92
XDOT = -17946
048669 XDOT = -5515
543057
YDOT = 6265
384927 feet/sec YDOT = 1848
265640 meter/sec
ZDOT = 16640
766119 ZDOT = 5045
421807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13464531
77 X = 4103989
28
Y = -14652221
21 feet Y = -4465997
02 meter
Z = -9547490
16 Z = -2910075
00
XDOT = 17082
614529 XDOT = 5206
780908
YDOT = 4960
885810 feet/sec YDOT = 1512
077995 meter/sec
ZDOT = 16536
423957 ZDOT = 5040
302022
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 09134
75832818
00010596 00000-0 82463-4 0 9087
2 25544 51
6413 118
3648 0009619 1
6377 358
4815 15
72736528 40691
Satellite: ISS
Catalog Number: 25544
Epoch time: 09134
75832818 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 118
3648 deg
Eccentricity:
0009619
Arg of perigee: 1
6377 deg
Mean anomaly: 358
4815 deg
Mean motion: 15
72736528 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4069
Checksum: 338
Coasting Arc #10 (Orbit 4084)
---------------------------------------
Vector Time (GMT): 2009/135/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4610828
04 A = 6728177
92 meter
Y = -2537659
40 meter E =
0014900
Z = -4206783
13 I = 51
94263
XDOT = 340
085527 Wp = 34
09881
YDOT = 6736
497083 meter/sec RA = 112
43361 deg
ZDOT = -3685
123700 TA = 198
36346
MA = 198
41730
Ha = 194
322 n
mi
Hp = 184
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15127388
59 X = 4659297
76
Y = -8325654
18 feet Y = -2485827
01 meter
Z = -13801781
91 Z = -4184266
14
XDOT = 1115
766164 XDOT = 282
633342
YDOT = 22101
368382 feet/sec YDOT = 6739
979240 meter/sec
ZDOT = -12090
300854 ZDOT = -3683
610463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17185087
99 X = -5238014
82
Y = -2290959
01 feet Y = -698284
31 meter
Z = -13713783
02 Z = -4179961
06
XDOT = 11959
525869 XDOT = 3645
263485
YDOT = -17262
102264 feet/sec YDOT = -5261
488770 meter/sec
ZDOT = -12083
953001 ZDOT = -3683
188875
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 09135
77497799
00010596 00000-0 82463-4 0 9096
2 25544 51
6414 113
1537 0009645 4
7530 355
3723 15
72748418 40859
Satellite: ISS
Catalog Number: 25544
Epoch time: 09135
77497799 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 113
1537 deg
Eccentricity:
0009645
Arg of perigee: 4
7530 deg
Mean anomaly: 355
3723 deg
Mean motion: 15
72748418 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4085
Checksum: 335
Coasting Arc #11 (Orbit 4100)
---------------------------------------
Vector Time (GMT): 2009/136/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1137503
95 A = 6730291
01 meter
Y = -5620059
25 meter E =
0017083
Z = 3521772
03 I = 51
96023
XDOT = 4901
351112 Wp = 53
80430
YDOT = -3842
131657 meter/sec RA = 107
27881 deg
ZDOT = -4523
186686 TA = 84
55082
MA = 84
35597
Ha = 194
433 n
mi
Hp = 184
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3731968
35 X = -1091683
17
Y = -18438514
59 feet Y = -5632523
57 meter
Z = 11554370
17 Z = 3516356
85
XDOT = 16080
548269 XDOT = 4965
923119
YDOT = -12605
418822 feet/sec YDOT = -3786
960478 meter/sec
ZDOT = -14839
851332 ZDOT = -4499
219277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7556871
61 X = -2303334
47
Y = 17242322
42 feet Y = 5255459
88 meter
Z = 11532817
83 Z = 3515202
87
XDOT = -19220
963039 XDOT = -5858
549534
YDOT = 1494
195384 feet/sec YDOT = 455
430753 meter/sec
ZDOT = -14746
247168 ZDOT = -4494
656137
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 09136
79161847
00010596 00000-0 82463-4 0 9103
2 25544 51
6414 107
9422 0009734 9
1187 351
0151 15
72780096 41014
Satellite: ISS
Catalog Number: 25544
Epoch time: 09136
79161847 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 107
9422 deg
Eccentricity:
0009734
Arg of perigee: 9
1187 deg
Mean anomaly: 351
0151 deg
Mean motion: 15
72780096 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4101
Checksum: 297
Coasting Arc #12 (Orbit 4116)
---------------------------------------
Vector Time (GMT): 2009/137/18:03:29
295
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3830948
29 A = 6729932
06 meter
Y = 4123523
67 meter E =
0016389
Z = 3670014
43 I = 51
96612
XDOT = -2210
430369 Wp = 58
80046
YDOT = -5950
620238 meter/sec RA = 102
22605 deg
ZDOT = 4372
650974 TA = 345
10325
MA = 345
15147
Ha = 194
679 n
mi
Hp = 184
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12568727
97 X = -3894601
88
Y = 13528620
95 feet Y = 4080327
61 meter
Z = 12040729
75 Z = 3651249
22
XDOT = -7252
068141 XDOT = -2164
966934
YDOT = -19523
032276 feet/sec YDOT = -5975
084662 meter/sec
ZDOT = 14345
967764 ZDOT = 4362
022654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18065902
01 X = 5506486
93
Y = -4046934
05 feet Y = -1233505
50 meter
Z = 11967505
58 Z = 3647695
70
XDOT = -5245
284970 XDOT = -1598
762859
YDOT = 18941
927813 feet/sec YDOT = 5773
499597 meter/sec
ZDOT = 14303
985465 ZDOT = 4359
854770
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 09137
80824967
00010596 00000-0 82463-4 0 9116
2 25544 51
6411 102
7302 0009774 12
8519 347
2891 15
72754342 41175
Satellite: ISS
Catalog Number: 25544
Epoch time: 09137
80824967 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 102
7302 deg
Eccentricity:
0009774
Arg of perigee: 12
8519 deg
Mean anomaly: 347
2891 deg
Mean motion: 15
72754342 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4117
Checksum: 311
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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