Date:
April 8th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8503 49 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 3467)
---------------------------------------
Vector Time (GMT): 2009/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5109212
63 A = 6737574
51 meter
Y = -4298889
71 meter E =
0006998
Z = 895308
37 I = 51
42065
XDOT = 2503
964559 Wp = 91
84120
YDOT = 4218
322598 meter/sec RA = 313
78267 deg
ZDOT = 5925
223369 TA = 277
94655
MA = 278
02597
Ha = 194
258 n
mi
Hp = 187
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16762508
62 X = 5152554
57
Y = -14103968
85 feet Y = -4241513
10 meter
Z = 2937363
43 Z = 920234
45
XDOT = 8215
106820 XDOT = 2427
824925
YDOT = 13839
641069 feet/sec YDOT = 4245
898165 meter/sec
ZDOT = 19439
709215 ZDOT = 5937
202281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12790456
74 X = 3898531
21
Y = -17768746
72 feet Y = -5415914
00 meter
Z = 3034401
52 Z = 924885
58
XDOT = 9943
536282 XDOT = 3030
789859
YDOT = 10507
191525 feet/sec YDOT = 3202
591977 meter/sec
ZDOT = 19486
767677 ZDOT = 5939
566788
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 09096
56179075
00010596 00000-0 82463-4 0 9004
2 25544 51
6408 314
0343 0009109 207
4235 152
6447 15
71974178 34686
Satellite: ISS
Catalog Number: 25544
Epoch time: 09096
56179075 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 314
0343 deg
Eccentricity:
0009109
Arg of perigee: 207
4235 deg
Mean anomaly: 152
6447 deg
Mean motion: 15
71974178 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3468
Checksum: 320
Coasting Arc #2 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2009/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3071923
48 A = 6725888
55 meter
Y = -2882229
14 meter E =
0013278
Z = -5252695
68 I = 51
36037
XDOT = 4978
270549 Wp = 128
83455
YDOT = -5853
846159 meter/sec RA = 308
63229 deg
ZDOT = 292
956500 TA = 144
00577
MA = 143
91628
Ha = 194
016 n
mi
Hp = 187
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10078489
10 X = -3013948
92
Y = -9456132
36 feet Y = -2916257
50 meter
Z = -17233253
54 Z = -5267478
02
XDOT = 16332
908626 XDOT = 5041
936109
YDOT = -19205
532018 feet/sec YDOT = -5797
820234 meter/sec
ZDOT = 961
143372 ZDOT = 317
296131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12101149
73 X = -3688430
44
Y = -6523577
97 feet Y = -1988386
56 meter
Z = -17291168
71 Z = -5270348
22
XDOT = 10271
820567 XDOT = 3130
850909
YDOT = -21919
240060 feet/sec YDOT = -6680
984370 meter/sec
ZDOT = 1055
778781 ZDOT = 321
801372
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 09097
51537093
00010596 00000-0 82463-4 0 9019
2 25544 51
6394 309
1509 0009015 211
2116 148
8512 15
71984104 34833
Satellite: ISS
Catalog Number: 25544
Epoch time: 09097
51537093 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 309
1509 deg
Eccentricity:
0009015
Arg of perigee: 211
2116 deg
Mean anomaly: 148
8512 deg
Mean motion: 15
71984104 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3483
Checksum: 302
Coasting Arc #3 (Orbit 3498)
---------------------------------------
Vector Time (GMT): 2009/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443153
78 A = 6737846
42 meter
Y = 5765943
29 meter E =
0016466
Z = 388583
72 I = 51
38337
XDOT = -4314
344697 Wp = 163
82391
YDOT = -2168
730909 meter/sec RA = 303
49271 deg
ZDOT = -6002
701854 TA = 11
93632
MA = 11
89734
Ha = 193
832 n
mi
Hp = 187
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11296436
30 X = -3509261
31
Y = 18917136
77 feet Y = 5727070
34 meter
Z = 1274880
97 Z = 371695
70
XDOT = -14154
674202 XDOT = -4260
612690
YDOT = -7115
258889 feet/sec YDOT = -2216
676509 meter/sec
ZDOT = -19693
903721 ZDOT = -6023
530379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5607768
17 X = -1709247
74
Y = 21311576
48 feet Y = 6495768
51 meter
Z = 1209339
41 Z = 368606
65
XDOT = -13909
899534 XDOT = -4239
737378
YDOT = -2529
080088 feet/sec YDOT = -770
863611 meter/sec
ZDOT = -19775
375887 ZDOT = -6027
534570
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 09098
53250909
00010596 00000-0 82463-4 0 9021
2 25544 51
6395 303
9436 0009000 215
4171 144
6395 15
71991258 34994
Satellite: ISS
Catalog Number: 25544
Epoch time: 09098
53250909 = yrday
fracday
Element set: 902
Inclination: 51
6395 deg
RA of node: 303
9436 deg
Eccentricity:
0009000
Arg of perigee: 215
4171 deg
Mean anomaly: 144
6395 deg
Mean motion: 15
71991258 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3499
Checksum: 325
Coasting Arc #4 (Orbit 3514)
---------------------------------------
Vector Time (GMT): 2009/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4255156
91 A = 6726333
31 meter
Y = 797206
69 meter E =
0009486
Z = 5151571
58 I = 51
32813
XDOT = -2758
818406 Wp = 194
28534
YDOT = 7086
828442 meter/sec RA = 298
36436 deg
ZDOT = 1173
471367 TA = 244
40171
MA = 244
49978
Ha = 193
656 n
mi
Hp = 188
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13960488
56 X = 4220900
47
Y = 2615507
50 feet Y = 844599
16 meter
Z = 16901481
56 Z = 5172160
10
XDOT = -9051
241491 XDOT = -2843
560044
YDOT = 23250
749483 feet/sec YDOT = 7055
503994 meter/sec
ZDOT = 3849
971677 ZDOT = 1159
862530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14018705
50 X = 4272901
44
Y = -1576853
77 feet Y = -480625
03 meter
Z = 16981920
60 Z = 5176089
40
XDOT = -1949
212840 XDOT = -594
120074
YDOT = 23868
712746 feet/sec YDOT = 7275
183645 meter/sec
ZDOT = 3797
326199 ZDOT = 1157
425026
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 09099
54963407
00010596 00000-0 82463-4 0 9038
2 25544 51
6385 298
7340 0008958 219
1483 140
9031 15
71972043 35152
Satellite: ISS
Catalog Number: 25544
Epoch time: 09099
54963407 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 298
7340 deg
Eccentricity:
0008958
Arg of perigee: 219
1483 deg
Mean anomaly: 140
9031 deg
Mean motion: 15
71972043 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3515
Checksum: 330
Coasting Arc #5 (Orbit 3529)
---------------------------------------
Vector Time (GMT): 2009/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1321323
26 A = 6736633
09 meter
Y = -6400510
02 meter E =
0001419
Z = -1633632
37 I = 51
34950
XDOT = 5138
678777 Wp = 256
56487
YDOT = -397
752983 meter/sec RA = 293
19567 deg
ZDOT = 5710
188823 TA = 85
34488
MA = 85
32868
Ha = 193
492 n
mi
Hp = 188
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4335050
08 X = 1400732
64
Y = -20999048
61 feet Y = -6385290
29 meter
Z = -5359686
26 Z = -1627020
08
XDOT = 16859
182338 XDOT = 5115
005129
YDOT = -1304
963856 feet/sec YDOT = -340
421354 meter/sec
ZDOT = 18734
215298 ZDOT = 5735
095399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2369803
96 X = -722316
25
Y = -21316850
29 feet Y = -6497375
97 meter
Z = -5334309
82 Z = -1625897
63
XDOT = 13963
106527 XDOT = 4255
954870
YDOT = -6268
345936 feet/sec YDOT = -1910
591841 meter/sec
ZDOT = 18831
430374 ZDOT = 5739
819978
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 09100
50317337
00010596 00000-0 82463-4 0 9043
2 25544 51
6375 293
8498 0009085 223
1513 136
8937 15
72031245 35309
Satellite: ISS
Catalog Number: 25544
Epoch time: 09100
50317337 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 293
8498 deg
Eccentricity:
0009085
Arg of perigee: 223
1513 deg
Mean anomaly: 136
8937 deg
Mean motion: 15
72031245 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3530
Checksum: 302
Coasting Arc #6 (Orbit 3545)
---------------------------------------
Vector Time (GMT): 2009/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4506760
29 A = 6727727
29 meter
Y = 1499707
32 meter E =
0005309
Z = -4767700
27 I = 51
30891
XDOT = 246
907930 Wp = 118
55228
YDOT = -7265
115383 meter/sec RA = 288
08766 deg
ZDOT = -2523
306998 TA = 126
62929
MA = 126
58046
Ha = 193
153 n
mi
Hp = 188
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14785958
97 X = -4500034
33
Y = 4920299
61 feet Y = 1449347
58 meter
Z = -15642061
27 Z = -4789578
16
XDOT = 810
065387 XDOT = 340
387275
YDOT = -23835
680389 feet/sec YDOT = -7261
831713 meter/sec
ZDOT = -8278
566267 ZDOT = -2521
880238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12280521
61 X = -3743102
99
Y = 9452323
05 feet Y = 2881068
07 meter
Z = -15727377
07 Z = -4793704
53
XDOT = -6289
297541 XDOT = -1916
977891
YDOT = -21911
931151 feet/sec YDOT = -6678
756615 meter/sec
ZDOT = -8273
493737 ZDOT = -2521
760891
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 09101
52027005
00010596 00000-0 82463-4 0 9057
2 25544 51
6371 288
6412 0008954 226
5501 133
4917 15
72061705 35463
Satellite: ISS
Catalog Number: 25544
Epoch time: 09101
52027005 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 288
6412 deg
Eccentricity:
0008954
Arg of perigee: 226
5501 deg
Mean anomaly: 133
4917 deg
Mean motion: 15
72061705 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3546
Checksum: 290
Coasting Arc #7 (Orbit 3561)
---------------------------------------
Vector Time (GMT): 2009/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 868020
04 A = 6734294
92 meter
Y = 6077169
53 meter E =
0010197
Z = 2751969
45 I = 51
32384
XDOT = -4896
439021 Wp = 142
43967
YDOT = 3019
052093 meter/sec RA = 282
90023 deg
ZDOT = -5120
552227 TA = 5
96084
MA = 5
94871
Ha = 192
940 n
mi
Hp = 188
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2847834
77 X = 786630
83
Y = 19938220
25 feet Y = 6086421
18 meter
Z = 9028771
15 Z = 2755988
63
XDOT = -16064
432483 XDOT = -4904
959573
YDOT = 9905
026553 feet/sec YDOT = 2964
249595 meter/sec
ZDOT = -16799
712031 ZDOT = -5144
360181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9464874
28 X = 2884893
68
Y = 17769856
48 feet Y = 5416252
26 meter
Z = 9044879
96 Z = 2756879
41
XDOT = -10305
141286 XDOT = -3141
007064
YDOT = 14090
499758 feet/sec YDOT = 4294
784326 meter/sec
ZDOT = -16892
462490 ZDOT = -5148
822567
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 09102
53735073
00010596 00000-0 82463-4 0 9061
2 25544 51
6376 283
4320 0009091 231
9141 128
1201 15
72097972 35622
Satellite: ISS
Catalog Number: 25544
Epoch time: 09102
53735073 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 283
4320 deg
Eccentricity:
0009091
Arg of perigee: 231
9141 deg
Mean anomaly: 128
1201 deg
Mean motion: 15
72097972 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3562
Checksum: 293
Coasting Arc #8 (Orbit 3577)
---------------------------------------
Vector Time (GMT): 2009/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3839103
52 A = 6730096
88 meter
Y = -3684555
40 meter E =
0008353
Z = 4123750
95 I = 51
30397
XDOT = 2129
743250 Wp = 161
67080
YDOT = 6390
518236 meter/sec RA = 277
80349 deg
ZDOT = 3717
304778 TA = 250
03643
MA = 250
12642
Ha = 192
816 n
mi
Hp = 188
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12595484
00 X = 3859986
83
Y = -12088436
34 feet Y = -3641507
60 meter
Z = 13529366
62 Z = 4142452
21
XDOT = 6987
346622 XDOT = 2040
066904
YDOT = 20966
267180 feet/sec YDOT = 6413
832808 meter/sec
ZDOT = 12195
881816 ZDOT = 3727
433459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7341032
18 X = 2237546
61
Y = -15776926
76 feet Y = -4808807
28 meter
Z = 13602135
87 Z = 4145931
01
XDOT = 12834
082639 XDOT = 3911
828388
YDOT = 16548
671799 feet/sec YDOT = 5044
035164 meter/sec
ZDOT = 12235
868976 ZDOT = 3729
492864
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 09103
55441893
00010596 00000-0 82463-4 0 9079
2 25544 51
6370 278
2225 0009093 234
7772 125
2539 15
72114875 35786
Satellite: ISS
Catalog Number: 25544
Epoch time: 09103
55441893 = yrday
fracday
Element set: 907
Inclination: 51
6370 deg
RA of node: 278
2225 deg
Eccentricity:
0009093
Arg of perigee: 234
7772 deg
Mean anomaly: 125
2539 deg
Mean motion: 15
72114875 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3578
Checksum: 325
Coasting Arc #9 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2009/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2742052
49 A = 6731541
67 meter
Y = -4913288
59 meter E =
0006323
Z = -3698912
13 I = 51
30679
XDOT = 3657
315492 Wp = 196
50093
YDOT = -5256
304663 meter/sec RA = 272
60666 deg
ZDOT = 4263
001916 TA = 118
76603
MA = 118
70250
Ha = 192
644 n
mi
Hp = 188
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8996235
21 X = -2668938
67
Y = -16119713
23 feet Y = -4943542
93 meter
Z = -12135538
48 Z = -3712055
66
XDOT = 11999
066575 XDOT = 3695
111474
YDOT = -17245
094040 feet/sec YDOT = -5215
195206 meter/sec
ZDOT = 13986
226760 ZDOT = 4280
860991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14320844
13 X = -4364993
29
Y = -11594578
18 feet Y = -3534027
43 meter
Z = -12187201
35 Z = -3714658
97
XDOT = 3733
442446 XDOT = 1137
953258
YDOT = -19411
974026 feet/sec YDOT = -5916
769683 meter/sec
ZDOT = 14055
601941 ZDOT = 4284
147472
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 09104
50790754
00010596 00000-0 82463-4 0 9089
2 25544 51
6376 273
3388 0008944 237
4158 122
6141 15
72122830 35937
Satellite: ISS
Catalog Number: 25544
Epoch time: 09104
50790754 = yrday
fracday
Element set: 908
Inclination: 51
6376 deg
RA of node: 273
3388 deg
Eccentricity:
0008944
Arg of perigee: 237
4158 deg
Mean anomaly: 122
6141 deg
Mean motion: 15
72122830 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3593
Checksum: 316
Coasting Arc #10 (Orbit 3608)
---------------------------------------
Vector Time (GMT): 2009/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2404729
16 A = 6732675
13 meter
Y = 5354721
57 meter E =
0005398
Z = -3290036
85 I = 51
31114
XDOT = -3957
005594 Wp = 214
73710
YDOT = -4654
789278 meter/sec RA = 267
51358 deg
ZDOT = -4684
308198 TA = 4
04723
MA = 4
04287
Ha = 192
256 n
mi
Hp = 189
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7889531
35 X = -2448445
33
Y = 17567984
14 feet Y = 5327586
14 meter
Z = -10794084
15 Z = -3301825
14
XDOT = -12982
301816 XDOT = -3881
905214
YDOT = -15271
618365 feet/sec YDOT = -4698
618791 meter/sec
ZDOT = -15368
465218 ZDOT = -4703
349142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -334796
46 X = -102045
96
Y = 19229634
30 feet Y = 5861192
53 meter
Z = -10839746
32 Z = -3303954
68
XDOT = -16435
785154 XDOT = -5009
627315
YDOT = -8990
353250 feet/sec YDOT = -2740
259671 meter/sec
ZDOT = -15443
147132 ZDOT = -4707
071246
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 09105
52494643
00010596 00000-0 82463-4 0 9091
2 25544 51
6379 268
1306 0008814 242
2063 117
8206 15
72160809 36091
Satellite: ISS
Catalog Number: 25544
Epoch time: 09105
52494643 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 268
1306 deg
Eccentricity:
0008814
Arg of perigee: 242
2063 deg
Mean anomaly: 117
8206 deg
Mean motion: 15
72160809 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3609
Checksum: 312
Coasting Arc #11 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2009/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4003342
62 A = 6728845
18 meter
Y = 3093127
06 meter E =
0000469
Z = 4436105
98 I = 51
29993
XDOT = -1683
017990 Wp = 135
44911
YDOT = 6788
097302 meter/sec RA = 262
31894 deg
ZDOT = -3214
373141 TA = 346
90173
MA = 346
90295
Ha = 192
123 n
mi
Hp = 189
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13134326
17 X = 3946907
35
Y = 10148054
66 feet Y = 3137579
14 meter
Z = 14554153
47 Z = 4455417
25
XDOT = -5521
712567 XDOT = -1743
183657
YDOT = 22270
660438 feet/sec YDOT = 6768
940474 meter/sec
ZDOT = -10545
843640 ZDOT = -3222
695272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16049492
83 X = 4891885
42
Y = 3962313
54 feet Y = 1207713
17 meter
Z = 14629790
56 Z = 4459160
16
XDOT = 4359
622212 XDOT = 1328
812850
YDOT = 21395
660473 feet/sec YDOT = 6521
397312 meter/sec
ZDOT = -10577
865848 ZDOT = -3224
133511
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 09106
54197166
00010596 00000-0 82463-4 0 9106
2 25544 51
6372 262
9213 0008887 245
4195 114
6041 15
72139443 36254
Satellite: ISS
Catalog Number: 25544
Epoch time: 09106
54197166 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 262
9213 deg
Eccentricity:
0008887
Arg of perigee: 245
4195 deg
Mean anomaly: 114
6041 deg
Mean motion: 15
72139443 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3625
Checksum: 310
Coasting Arc #12 (Orbit 3640)
---------------------------------------
Vector Time (GMT): 2009/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 685930
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 462544
26 A = 6734958
66 meter
Y = -6308256
72 meter E =
0005081
Z = 2307389
96 I = 51
32732
XDOT = 4960
691604 Wp = 79
32037
YDOT = 2341
236979 meter/sec RA = 257
21773 deg
ZDOT = 5397
218300 TA = 306
71673
MA = 306
76340
Ha = 191
930 n
mi
Hp = 189
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1517533
67 X = 521840
97
Y = -20696380
32 feet Y = -6302752
76 meter
Z = 7570177
03 Z = 2309780
98
XDOT = 16275
234921 XDOT = 4907
924068
YDOT = 7681
223684 feet/sec YDOT = 2396
415238 meter/sec
ZDOT = 17707
409122 ZDOT = 5421
189216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7406950
17 X = -2257638
41
Y = -19381577
38 feet Y = -5907504
78 meter
Z = 7579062
90 Z = 2310098
37
XDOT = 16490
220540 XDOT = 5026
219221
YDOT = 670
805034 feet/sec YDOT = 204
461374 meter/sec
ZDOT = 17801
199869 ZDOT = 5425
805720
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 09107
55897962
00010596 00000-0 82463-4 0 9110
2 25544 51
6381 257
7121 0008938 249
3264 110
6941 15
72210982 36412
Satellite: ISS
Catalog Number: 25544
Epoch time: 09107
55897962 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 257
7121 deg
Eccentricity:
0008938
Arg of perigee: 249
3264 deg
Mean anomaly: 110
6941 deg
Mean motion: 15
72210982 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3641
Checksum: 322
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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