Date:
September 8th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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 117)
---------------------------------------
Vector Time (GMT): 2008/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5684041
13 A = 6737942
86 meter
Y = -3551807
36 meter E =
0019113
Z = 612604
61 I = 51
46816
XDOT = 2078
646331 Wp = 61
18588
YDOT = 4380
835296 meter/sec RA = 323
82585 deg
ZDOT = 5981
376402 TA = 305
49589
MA = 305
67405
Ha = 195
625 n
mi
Hp = 184
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18648428
92 X = 5720359
62
Y = -11652911
29 feet Y = -3488042
06 meter
Z = 2009857
66 Z = 640306
10
XDOT = 6819
705812 XDOT = 2000
448035
YDOT = 14372
819214 feet/sec YDOT = 4403
642765 meter/sec
ZDOT = 19623
938326 ZDOT = 5991
284519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21104180
29 X = -6432554
15
Y = 6142255
62 feet Y = 1872159
51 meter
Z = 2116610
65 Z = 645142
93
XDOT = -2095
463419 XDOT = -638
697250
YDOT = -14116
670912 feet/sec YDOT = -4302
761294 meter/sec
ZDOT = 19662
613950 ZDOT = 5993
164732
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 08249
56233711
00020000 00000-0 20000-3 0 9000
2 25544 51
6425 324
0421 0006399 82
3294 277
8595 15
71916473 1183
Satellite: ISS
Catalog Number: 25544
Epoch time: 08249
56233711 = yrday
fracday
Element set: 900
Inclination: 51
6425 deg
RA of node: 324
0421 deg
Eccentricity:
0006399
Arg of perigee: 82
3294 deg
Mean anomaly: 277
8595 deg
Mean motion: 15
71916473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 118
Checksum: 295
Coasting Arc #2 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2008/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2803261
08 A = 6726008
94 meter
Y = -3134100
84 meter E =
0021312
Z = -5267951
97 I = 51
40430
XDOT = 5752
784979 Wp = 88
38438
YDOT = -5090
679087 meter/sec RA = 318
68553 deg
ZDOT = -32
144567 TA = 181
30606
MA = 181
31164
Ha = 195
568 n
mi
Hp = 184
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9197050
79 X = -2742415
85
Y = -10282483
08 feet Y = -3165108
31 meter
Z = -17283306
97 Z = -5281422
48
XDOT = 18873
966465 XDOT = 5809
438362
YDOT = -16701
703041 feet/sec YDOT = -5026
031365 meter/sec
ZDOT = -105
461179 ZDOT = -4
059819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6168735
07 X = 1880230
45
Y = 12265810
18 feet Y = 3738618
94 meter
Z = -17335642
75 Z = -5283903
91
XDOT = -21620
714613 XDOT = -6589
993814
YDOT = 10875
033301 feet/sec YDOT = 3314
710150 meter/sec
ZDOT = 2
639939 ZDOT =
804653
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 08250
51592465
00020000 00000-0 20000-3 0 9012
2 25544 51
6415 319
1600 0006291 85
6567 274
5314 15
71932703 1330
Satellite: ISS
Catalog Number: 25544
Epoch time: 08250
51592465 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 319
1600 deg
Eccentricity:
0006291
Arg of perigee: 85
6567 deg
Mean anomaly: 274
5314 deg
Mean motion: 15
71932703 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 133
Checksum: 274
Coasting Arc #3 (Orbit 148)
---------------------------------------
Vector Time (GMT): 2008/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4218453
14 A = 6737735
70 meter
Y = 5203295
99 meter E =
0018738
Z = 660403
71 I = 51
42334
XDOT = -4125
788717 Wp = 115
17981
YDOT = -2571
394577 meter/sec RA = 313
54288 deg
ZDOT = -5970
293784 TA = 57
61043
MA = 57
42925
Ha = 195
545 n
mi
Hp = 184
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13840069
37 X = -4279531
84
Y = 17071181
07 feet Y = 5155781
30 meter
Z = 2166678
82 Z = 639762
12
XDOT = -13536
052221 XDOT = -4067
725659
YDOT = -8436
333915 feet/sec YDOT = -2617
206801 meter/sec
ZDOT = -19587
578031 ZDOT = -5990
195907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17528588
88 X = 5342713
89
Y = -13268713
75 feet Y = -4044303
95 meter
Z = 2087354
25 Z = 636225
58
XDOT = 10052
711804 XDOT = 3064
066558
YDOT = 10120
112673 feet/sec YDOT = 3084
610343 meter/sec
ZDOT = -19664
724792 ZDOT = -5993
808116
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 08251
53307237
00020000 00000-0 20000-3 0 9027
2 25544 51
6417 313
9521 0006484 88
4779 271
7126 15
71989013 1499
Satellite: ISS
Catalog Number: 25544
Epoch time: 08251
53307237 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 313
9521 deg
Eccentricity:
0006484
Arg of perigee: 88
4779 deg
Mean anomaly: 271
7126 deg
Mean motion: 15
71989013 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 149
Checksum: 298
Coasting Arc #4 (Orbit 164)
---------------------------------------
Vector Time (GMT): 2008/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224606
79 A = 6726481
45 meter
Y = 1212523
58 meter E =
0010586
Z = 5083839
79 I = 51
36649
XDOT = -3700
201227 Wp = 105
96019
YDOT = 6590
345555 meter/sec RA = 308
42416 deg
ZDOT = 1497
536595 TA = 329
60202
MA = 329
66336
Ha = 195
360 n
mi
Hp = 184
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13860258
51 X = 4186037
81
Y = 3978095
74 feet Y = 1259549
83 meter
Z = 16679264
41 Z = 5104269
26
XDOT = -12139
767804 XDOT = -3780
895281
YDOT = 21621
868618 feet/sec YDOT = 6548
516565 meter/sec
ZDOT = 4913
177804 ZDOT = 1479
365128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12537217
96 X = -3821344
03
Y = -6935869
49 feet Y = -2114053
02 meter
Z = 16758333
84 Z = 5107940
15
XDOT = 16160
209901 XDOT = 4925
631978
YDOT = -17465
211917 feet/sec YDOT = -5323
396592 meter/sec
ZDOT = 4843
523173 ZDOT = 1476
305863
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 08252
55020541
00020000 00000-0 20000-3 0 9031
2 25544 51
6416 308
7444 0006389 92
4338 267
7556 15
72014438 1655
Satellite: ISS
Catalog Number: 25544
Epoch time: 08252
55020541 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 308
7444 deg
Eccentricity:
0006389
Arg of perigee: 92
4338 deg
Mean anomaly: 267
7556 deg
Mean motion: 15
72014438 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 165
Checksum: 288
Coasting Arc #5 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2008/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2150884
09 A = 6736256
74 meter
Y = -6085655
99 meter E =
0011948
Z = -1925993
05 I = 51
38161
XDOT = 5277
442863 Wp = 65
32642
YDOT = 104
278385 meter/sec RA = 303
25496 deg
ZDOT = 5596
268872 TA = 273
20675
MA = 273
34344
Ha = 195
524 n
mi
Hp = 184
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7056706
33 X = 2228131
11
Y = -19966062
97 feet Y = -6061171
63 meter
Z = -6318874
83 Z = -1915356
53
XDOT = 17314
445089 XDOT = 5248
699006
YDOT = 342
120686 feet/sec YDOT = 163
133006 meter/sec
ZDOT = 18360
462179 ZDOT = 5621
836783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11040605
53 X = -3365176
57
Y = 18084714
24 feet Y = 5512220
90 meter
Z = -6278303
47 Z = -1913626
90
XDOT = -15453
483718 XDOT = -4710
221837
YDOT = -3062
699822 feet/sec YDOT = -933
510906 meter/sec
ZDOT = 18459
298518 ZDOT = 5626
394188
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 08253
50375691
00020000 00000-0 20000-3 0 9047
2 25544 51
6411 303
8621 0006471 94
6125 265
5776 15
72007569 1807
Satellite: ISS
Catalog Number: 25544
Epoch time: 08253
50375691 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 303
8621 deg
Eccentricity:
0006471
Arg of perigee: 94
6125 deg
Mean anomaly: 265
5776 deg
Mean motion: 15
72007569 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 180
Checksum: 286
Coasting Arc #6 (Orbit 195)
---------------------------------------
Vector Time (GMT): 2008/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4771674
30 A = 6728367
33 meter
Y = 1044717
50 meter E =
0016967
Z = -4642844
87 I = 51
34076
XDOT = 1203
408129 Wp = 80
86283
YDOT = -7043
247899 meter/sec RA = 298
15326 deg
ZDOT = -2827
803294 TA = 161
05339
MA = 160
99018
Ha = 195
503 n
mi
Hp = 184
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15655099
42 X = -4760447
90
Y = 3427550
87 feet Y = 991420
67 meter
Z = -15232430
66 Z = -4665998
25
XDOT = 3948
189399 XDOT = 1295
814292
YDOT = -23107
768699 feet/sec YDOT = -7029
274024 meter/sec
ZDOT = -9277
569863 ZDOT = -2821
732728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15934595
57 X = 4856864
73
Y = -432729
10 feet Y = -131895
83 meter
Z = -15321833
97 Z = -4670094
99
XDOT = -8315
289932 XDOT = -2534
500371
YDOT = 20777
948793 feet/sec YDOT = 6333
118792 meter/sec
ZDOT = -9254
740319 ZDOT = -2820
844849
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 08254
52086464
00020000 00000-0 20000-3 0 9058
2 25544 51
6416 298
6537 0006575 98
6952 261
4955 15
72026799 1963
Satellite: ISS
Catalog Number: 25544
Epoch time: 08254
52086464 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 298
6537 deg
Eccentricity:
0006575
Arg of perigee: 98
6952 deg
Mean anomaly: 261
4955 deg
Mean motion: 15
72026799 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 196
Checksum: 333
Coasting Arc #7 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2008/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 51757
79 A = 6733738
86 meter
Y = 6020036
85 meter E =
0019799
Z = 2996341
97 I = 51
34598
XDOT = -5353
768893 Wp = 97
81333
YDOT = 2515
332932 meter/sec RA = 292
96595 deg
ZDOT = -4935
984385 TA = 47
39702
MA = 47
23019
Ha = 195
404 n
mi
Hp = 184
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 169809
02 X = -30118
65
Y = 19750777
08 feet Y = 6020157
90 meter
Z = 9830518
28 Z = 2996394
42
XDOT = -17564
858572 XDOT = -5357
519917
YDOT = 8252
404631 feet/sec YDOT = 2455
442940 meter/sec
ZDOT = -16194
174491 ZDOT = -4962
001942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3275572
59 X = 998394
53
Y = -19477623
16 feet Y = -5936779
54 meter
Z = 9831273
57 Z = 2996572
18
XDOT = 17207
961538 XDOT = 5244
986677
YDOT = -5372
396689 feet/sec YDOT = -1637
506511 meter/sec
ZDOT = -16294
515648 ZDOT = -4966
568369
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 08255
53795697
00020000 00000-0 20000-3 0 9066
2 25544 51
6409 293
4458 0006565 100
8707 259
3194 15
72085068 2127
Satellite: ISS
Catalog Number: 25544
Epoch time: 08255
53795697 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 293
4458 deg
Eccentricity:
0006565
Arg of perigee: 100
8707 deg
Mean anomaly: 259
3194 deg
Mean motion: 15
72085068 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 212
Checksum: 315
Coasting Arc #8 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2008/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4357109
26 A = 6730917
71 meter
Y = -3301157
54 meter E =
0017825
Z = 3914999
14 I = 51
32554
XDOT = 1281
543388 Wp = 101
82442
YDOT = 6457
757886 meter/sec RA = 287
87348 deg
ZDOT = 4000
005446 TA = 306
40438
MA = 306
56865
Ha = 195
414 n
mi
Hp = 184
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14294977
87 X = 4374681
30
Y = -10830569
35 feet Y = -3252335
41 meter
Z = 12844485
36 Z = 3936208
62
XDOT = 4204
538674 XDOT = 1189
805308
YDOT = 21186
869705 feet/sec YDOT = 6471
576077 meter/sec
ZDOT = 13123
377446 ZDOT = 4006
008030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15724052
56 X = -4792691
22
Y = 8502756
01 feet Y = 2591640
03 meter
Z = 12926164
94 Z = 3939895
07
XDOT = -185
557926 XDOT = -56
558056
YDOT = -20423
900715 feet/sec YDOT = -6225
204938 meter/sec
ZDOT = 13147
184628 ZDOT = 4007
261875
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 08256
55503733
00020000 00000-0 20000-3 0 9078
2 25544 51
6402 288
2375 0006767 104
3094 255
8820 15
72076600 2288
Satellite: ISS
Catalog Number: 25544
Epoch time: 08256
55503733 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 288
2375 deg
Eccentricity:
0006767
Arg of perigee: 104
3094 deg
Mean anomaly: 255
8820 deg
Mean motion: 15
72076600 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 228
Checksum: 288
Coasting Arc #9 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2008/257/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086231
07 A = 6730839
38 meter
Y = -5061592
61 meter E =
0013504
Z = -3929820
71 I = 51
31874
XDOT = 4377
162732 Wp = 107
16316
YDOT = -4897
325553 meter/sec RA = 282
67836 deg
ZDOT = 3991
413873 TA = 204
50540
MA = 204
56964
Ha = 195
393 n
mi
Hp = 184
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6844590
14 X = -2010386
24
Y = -16606274
96 feet Y = -5084498
24 meter
Z = -12893112
56 Z = -3939770
99
XDOT = 14360
770117 XDOT = 4412
210648
YDOT = -16067
341052 feet/sec YDOT = -4848
181366 meter/sec
ZDOT = 13095
189872 ZDOT = 4012
763449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4422655
02 X = 1348025
25
Y = 17379617
92 feet Y = 5297307
54 meter
Z = -12932058
50 Z = -3941691
43
XDOT = -15092
017020 XDOT = -4600
046788
YDOT = 13627
638591 feet/sec YDOT = 4153
704243 meter/sec
ZDOT = 13177
254506 ZDOT = 4016
427173
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 08257
50853589
00020000 00000-0 20000-3 0 9082
2 25544 51
6412 283
3548 0006682 107
3049 252
8844 15
72108074 2437
Satellite: ISS
Catalog Number: 25544
Epoch time: 08257
50853589 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 283
3548 deg
Eccentricity:
0006682
Arg of perigee: 107
3049 deg
Mean anomaly: 252
8844 deg
Mean motion: 15
72108074 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 243
Checksum: 301
Coasting Arc #10 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2008/258/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3139815
00 A = 6733448
70 meter
Y = 5123233
92 meter E =
0011159
Z = -3043226
90 I = 51
32179
XDOT = -3302
005557 Wp = 109
32133
YDOT = -4923
712944 meter/sec RA = 277
58403 deg
ZDOT = -4900
464145 TA = 106
04189
MA = 105
91897
Ha = 195
307 n
mi
Hp = 184
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10301230
32 X = -3182087
06
Y = 16808510
22 feet Y = 5087886
08 meter
Z = -9984340
23 Z = -3058583
20
XDOT = -10833
351565 XDOT = -3222
896879
YDOT = -16153
913858 feet/sec YDOT = -4960
195977 meter/sec
ZDOT = -16077
638272 ZDOT = -4916
312670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12194030
78 X = 3716740
58
Y = -15452119
74 feet Y = -4709806
10 meter
Z = -10043207
68 Z = -3061169
70
XDOT = 7590
203439 XDOT = 2313
494008
YDOT = 16440
985465 feet/sec YDOT = 5011
212370 meter/sec
ZDOT = -16139
379050 ZDOT = -4919
282734
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 08258
52558729
00020000 00000-0 20000-3 0 9094
2 25544 51
6404 278
1457 0006652 111
4202 248
7671 15
72126145 2591
Satellite: ISS
Catalog Number: 25544
Epoch time: 08258
52558729 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 278
1457 deg
Eccentricity:
0006652
Arg of perigee: 111
4202 deg
Mean anomaly: 248
7671 deg
Mean motion: 15
72126145 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 259
Checksum: 297
Coasting Arc #11 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2008/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3542713
55 A = 6728125
63 meter
Y = 3391215
50 meter E =
0013501
Z = 4594934
90 I = 51
30040
XDOT = -2599
878769 Wp = 86
33371
YDOT = 6650
841741 meter/sec RA = 272
39237 deg
ZDOT = -2895
861537 TA = 32
49325
MA = 32
41021
Ha = 195
147 n
mi
Hp = 184
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11623075
96 X = 3482207
70
Y = 11126035
11 feet Y = 3430494
30 meter
Z = 15075245
74 Z = 4611998
16
XDOT = -8529
785989 XDOT = -2659
988705
YDOT = 21820
346918 feet/sec YDOT = 6621
432027 meter/sec
ZDOT = -9500
858062 ZDOT = -2908
638431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10324703
12 X = -3146969
51
Y = -12258952
84 feet Y = -3736528
83 meter
Z = 15141537
80 Z = 4615140
72
XDOT = 9791
371432 XDOT = 2984
410012
YDOT = -20074
507219 feet/sec YDOT = -6118
709800 meter/sec
ZDOT = -9549
598627 ZDOT = -2910
717662
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 08259
54262382
00020000 00000-0 20000-3 0 9106
2 25544 51
6391 272
9366 0006640 114
4080 245
7776 15
72169181 2759
Satellite: ISS
Catalog Number: 25544
Epoch time: 08259
54262382 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 272
9366 deg
Eccentricity:
0006640
Arg of perigee: 114
4080 deg
Mean anomaly: 245
7776 deg
Mean motion: 15
72169181 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 275
Checksum: 297
Coasting Arc #12 (Orbit 290)
---------------------------------------
Vector Time (GMT): 2008/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 643009
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293052
23 A = 6735646
92 meter
Y = -6298412
82 meter E =
0019036
Z = 1986025
07 I = 51
32583
XDOT = 4584
727242 Wp = 83
70336
YDOT = 2708
620515 meter/sec RA = 267
28782 deg
ZDOT = 5561
420072 TA = 298
50749
MA = 298
69905
Ha = 195
179 n
mi
Hp = 184
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4242297
36 X = 1353738
16
Y = -20664084
07 feet Y = -6283613
67 meter
Z = 6515830
28 Z = 1992454
77
XDOT = 15041
756042 XDOT = 4527
081637
YDOT = 8886
550247 feet/sec YDOT = 2759
567786 meter/sec
ZDOT = 18246
128844 ZDOT = 5583
552603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5971338
09 X = -1820063
85
Y = 20224445
08 feet Y = 6164410
86 meter
Z = 6540064
55 Z = 1993411
67
XDOT = -12640
186620 XDOT = -3852
728882
YDOT = -9706
229998 feet/sec YDOT = -2958
458903 meter/sec
ZDOT = 18331
951655 ZDOT = 5587
578865
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 08260
55964621
00020000 00000-0 20000-3 0 9115
2 25544 51
6391 267
7280 0006601 118
3539 241
8289 15
72180452 2913
Satellite: ISS
Catalog Number: 25544
Epoch time: 08260
55964621 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 267
7280 deg
Eccentricity:
0006601
Arg of perigee: 118
3539 deg
Mean anomaly: 241
8289 deg
Mean motion: 15
72180452 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 291
Checksum: 290
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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