Date:
May 17th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9418 42 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 83)
---------------------------------------
Vector Time (GMT): 2009/135/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4389174
96 A = 6731228
32 meter
Y = -3988988
72 meter E =
0010194
Z = -3197593
05 I = 51
95186
XDOT = 1692
216046 Wp = 31
94689
YDOT = 5735
542818 meter/sec RA = 112
77721 deg
ZDOT = -4830
781980 TA = 185
11066
MA = 185
12108
Ha = 194
227 n
mi
Hp = 184
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14400180
31 X = 4448987
68
Y = -13087233
33 feet Y = -3939571
66 meter
Z = -10490790
85 Z = -3176125
45
XDOT = 5551
889915 XDOT = 1651
421631
YDOT = 18817
397696 feet/sec YDOT = 5754
238540 meter/sec
ZDOT = -15849
022243 ZDOT = -4822
659693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18538241
79 X = -5650456
10
Y = -6060170
41 feet Y = -1847139
94 meter
Z = -10406992
26 Z = -3172051
24
XDOT = 13094
335735 XDOT = 3991
153532
YDOT = -12885
665044 feet/sec YDOT = -3927
550706 meter/sec
ZDOT = -15816
861482 ZDOT = -4820
979380
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
71134528
00010596 00000-0 82463-4 0 9009
2 25544 51
6405 113
4852 0009558 5
4343 354
6921 15
72801104 844
Satellite: ISS
Catalog Number: 25544
Epoch time: 09135
71134528 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 113
4852 deg
Eccentricity:
0009558
Arg of perigee: 5
4343 deg
Mean anomaly: 354
6921 deg
Mean motion: 15
72801104 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 84
Checksum: 283
Coasting Arc #2 (Orbit 99)
---------------------------------------
Vector Time (GMT): 2009/136/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2198325
43 A = 6727017
50 meter
Y = -4551621
45 meter E =
0016310
Z = 4437225
21 I = 51
94781
XDOT = 4418
157687 Wp = 38
40523
YDOT = -5371
188828 meter/sec RA = 107
62429 deg
ZDOT = -3301
835584 TA = 84
68776
MA = 84
50168
Ha = 194
339 n
mi
Hp = 184
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7212353
78 X = -2168820
38
Y = -14933141
23 feet Y = -4576039
80 meter
Z = 14557825
50 Z = 4426616
99
XDOT = 14495
268003 XDOT = 4493
930650
YDOT = -17622
010590 feet/sec YDOT = -5321
358469 meter/sec
ZDOT = -10832
793912 ZDOT = -3280
188464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9105930
87 X = -2775487
73
Y = 13903762
65 feet Y = 4237866
86 meter
Z = 14516006
49 Z = 4424478
78
XDOT = -21573
224081 XDOT = -6575
518700
YDOT = -2842
095731 feet/sec YDOT = -866
270779 meter/sec
ZDOT = -10748
370377 ZDOT = -3276
103291
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
72795108
00010596 00000-0 82463-4 0 9019
2 25544 51
6400 108
2737 0009597 9
2202 350
9135 15
72826400 1003
Satellite: ISS
Catalog Number: 25544
Epoch time: 09136
72795108 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 108
2737 deg
Eccentricity:
0009597
Arg of perigee: 9
2202 deg
Mean anomaly: 350
9135 deg
Mean motion: 15
72826400 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 100
Checksum: 282
Coasting Arc #3 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2009/137/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3228676
32 A = 6732741
45 meter
Y = 5312654
40 meter E =
0020083
Z = 2551962
60 I = 51
97533
XDOT = -3249
522648 Wp = 50
87063
YDOT = -4536
772997 meter/sec RA = 102
56514 deg
ZDOT = 5318
128545 TA = 337
94974
MA = 338
03602
Ha = 194
494 n
mi
Hp = 184
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10592770
07 X = -3300240
40
Y = 17429968
51 feet Y = 5276149
14 meter
Z = 8372580
71 Z = 2536104
13
XDOT = -10661
163544 XDOT = -3224
384848
YDOT = -14884
425844 feet/sec YDOT = -4572
970874 meter/sec
ZDOT = 17447
928297 ZDOT = 5302
403006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20421268
71 X = 6224402
70
Y = -113489
24 feet Y = -34591
52 meter
Z = 8310811
76 Z = 2533135
42
XDOT = -7010
040482 XDOT = -2136
660339
YDOT = 15491
330636 feet/sec YDOT = 4721
757578 meter/sec
ZDOT = 17386
073969 ZDOT = 5299
275346
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
74454336
00010596 00000-0 82463-4 0 9028
2 25544 51
6405 103
0616 0009631 13
1474 346
9937 15
72823518 1160
Satellite: ISS
Catalog Number: 25544
Epoch time: 09137
74454336 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 103
0616 deg
Eccentricity:
0009631
Arg of perigee: 13
1474 deg
Mean anomaly: 346
9937 deg
Mean motion: 15
72823518 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 116
Checksum: 298
Coasting Arc #4 (Orbit 130)
---------------------------------------
Vector Time (GMT): 2009/138/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3370739
20 A = 6725442
93 meter
Y = 3284819
69 meter E =
0014857
Z = -4813682
31 I = 51
95676
XDOT = -2875
927499 Wp = 67
94529
YDOT = 6663
346562 meter/sec RA = 97
41989 deg
ZDOT = 2544
840844 TA = 226
83739
MA = 226
96167
Ha = 194
470 n
mi
Hp = 183
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11058855
64 X = 3357141
50
Y = 10776967
47 feet Y = 3322437
52 meter
Z = -15792920
97 Z = -4797339
93
XDOT = -9435
457674 XDOT = -2962
586914
YDOT = 21861
373236 feet/sec YDOT = 6630
701569 meter/sec
ZDOT = 8349
215366 ZDOT = 2530
659358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3042795
60 X = 927444
10
Y = -15205464
03 feet Y = -4634625
44 meter
Z = -15728729
36 Z = -4794116
71
XDOT = 22410
800136 XDOT = 6830
811882
YDOT = -4055
083422 feet/sec YDOT = -1235
989427 meter/sec
ZDOT = 8294
087888 ZDOT = 2528
037988
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 09138
69758406
00010596 00000-0 82463-4 0 9039
2 25544 51
6409 98
1756 0009581 15
9166 344
2296 15
72864199 1311
Satellite: ISS
Catalog Number: 25544
Epoch time: 09138
69758406 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 98
1756 deg
Eccentricity:
0009581
Arg of perigee: 15
9166 deg
Mean anomaly: 344
2296 deg
Mean motion: 15
72864199 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 131
Checksum: 340
Coasting Arc #5 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2009/139/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1751954
56 A = 6733862
36 meter
Y = -6218490
96 meter E =
0008284
Z = -1912917
69 I = 51
98773
XDOT = 4300
826477 Wp = 65
88705
YDOT = 2945
614436 meter/sec RA = 92
35278 deg
ZDOT = -5652
447263 TA = 135
23428
MA = 135
16740
Ha = 194
468 n
mi
Hp = 183
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5747882
40 X = 1830653
30
Y = -20401873
23 feet Y = -6198459
44 meter
Z = -6275976
69 Z = -1904215
78
XDOT = 14110
323086 XDOT = 4295
027419
YDOT = 9664
089356 feet/sec YDOT = 2993
676697 meter/sec
ZDOT = -18544
774485 ZDOT = -5631
567469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20183507
33 X = -6151933
03
Y = 6505578
93 feet Y = 1982900
46 meter
Z = -6242270
55 Z = -1902644
06
XDOT = 627
587961 XDOT = 191
288811
YDOT = -15718
444109 feet/sec YDOT = -4790
981764 meter/sec
ZDOT = -18462
837880 ZDOT = -5627
472986
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 09139
71414817
00010596 00000-0 82463-4 0 9049
2 25544 51
6410 92
9633 0009420 19
4743 340
6778 15
72853691 1478
Satellite: ISS
Catalog Number: 25544
Epoch time: 09139
71414817 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 92
9633 deg
Eccentricity:
0009420
Arg of perigee: 19
4743 deg
Mean anomaly: 340
6778 deg
Mean motion: 15
72853691 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 147
Checksum: 317
Coasting Arc #6 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2009/140/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4045890
32 A = 6724175
15 meter
Y = -1813265
91 meter E =
0014448
Z = 5051698
26 I = 51
95608
XDOT = 1052
745424 Wp = 34
08093
YDOT = -7413
911569 meter/sec RA = 87
21644 deg
ZDOT = -1803
845990 TA = 73
29802
MA = 73
13949
Ha = 194
546 n
mi
Hp = 183
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13273918
39 X = -4049854
07
Y = -5949035
13 feet Y = -1858531
91 meter
Z = 16573813
18 Z = 5032033
21
XDOT = 3453
889185 XDOT = 1144
333710
YDOT = -24323
856855 feet/sec YDOT = -7401
626939 meter/sec
ZDOT = -5918
129889 ZDOT = -1798
509676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2715182
76 X = 827587
71
Y = 14379353
60 feet Y = 4382826
98 meter
Z = 16496702
22 Z = 5028194
84
XDOT = -20938
889134 XDOT = -6382
173408
YDOT = 10773
483985 feet/sec YDOT = 3283
757919 meter/sec
ZDOT = -5897
661659 ZDOT = -1797
607274
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 09140
73069563
00010596 00000-0 82463-4 0 9058
2 25544 51
6411 87
7509 0009571 22
6057 337
5525 15
72946930 1636
Satellite: ISS
Catalog Number: 25544
Epoch time: 09140
73069563 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 87
7509 deg
Eccentricity:
0009571
Arg of perigee: 22
6057 deg
Mean anomaly: 337
5525 deg
Mean motion: 15
72946930 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 163
Checksum: 314
Coasting Arc #7 (Orbit 178)
---------------------------------------
Vector Time (GMT): 2009/141/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -54549
16 A = 6734568
43 meter
Y = 6608734
44 meter E =
0022592
Z = 1225644
19 I = 51
98822
XDOT = -4818
479866 Wp = 45
32263
YDOT = -1144
538888 meter/sec RA = 82
13840 deg
ZDOT = 5906
528902 TA = 328
05885
MA = 328
19561
Ha = 194
573 n
mi
Hp = 183
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -178967
07 X = -134399
18
Y = 21682199
61 feet Y = 6607677
87 meter
Z = 4021142
35 Z = 1225185
78
XDOT = -15808
660979 XDOT = -4834
016805
YDOT = -3755
048846 feet/sec YDOT = -1198
509313 meter/sec
ZDOT = 19378
375664 ZDOT = 5883
082365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17733457
91 X = 5405157
97
Y = -12477409
51 feet Y = -3803114
42 meter
Z = 4019716
07 Z = 1225209
46
XDOT = 5322
098937 XDOT = 1622
175756
YDOT = 13830
654204 feet/sec YDOT = 4215
583401 meter/sec
ZDOT = 19286
495783 ZDOT = 5878
523915
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 09141
74723114
00010596 00000-0 82463-4 0 9060
2 25544 51
6411 82
5384 0009574 26
4628 333
7022 15
72934685 1790
Satellite: ISS
Catalog Number: 25544
Epoch time: 09141
74723114 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 82
5384 deg
Eccentricity:
0009574
Arg of perigee: 26
4628 deg
Mean anomaly: 333
7022 deg
Mean motion: 15
72934685 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 179
Checksum: 310
Coasting Arc #8 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2009/142/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4243388
78 A = 6723411
85 meter
Y = 191545
26 meter E =
0020092
Z = -5227001
84 I = 51
94544
XDOT = 916
192724 Wp = 71
65948
YDOT = 7561
410222 meter/sec RA = 77
01307 deg
ZDOT = 1030
260345 TA = 208
08735
MA = 208
19590
Ha = 194
596 n
mi
Hp = 183
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13921879
19 X = 4266323
95
Y = 628429
32 feet Y = 239126
13 meter
Z = -17148956
16 Z = -5206331
22
XDOT = 3005
881639 XDOT = 826
566724
YDOT = 24807
776318 feet/sec YDOT = 7571
154383 meter/sec
ZDOT = 3380
119242 ZDOT = 1034
494458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7865653
41 X = -2397451
16
Y = -11623910
18 feet Y = -3542967
82 meter
Z = -17067997
81 Z = -5202325
73
XDOT = 17272
860998 XDOT = 5264
768032
YDOT = -16630
898281 feet/sec YDOT = -5069
097796 meter/sec
ZDOT = 3397
105633 ZDOT = 1035
437797
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 09142
70021907
00010596 00000-0 82463-4 0 9079
2 25544 51
6409 77
6516 0009549 29
7539 330
4165 15
72963353 1941
Satellite: ISS
Catalog Number: 25544
Epoch time: 09142
70021907 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 77
6516 deg
Eccentricity:
0009549
Arg of perigee: 29
7539 deg
Mean anomaly: 330
4165 deg
Mean motion: 15
72963353 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 194
Checksum: 320
Coasting Arc #9 (Orbit 209)
---------------------------------------
Vector Time (GMT): 2009/143/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1634277
12 A = 6735036
24 meter
Y = -6507199
10 meter E =
0012320
Z = -595365
30 I = 51
97686
XDOT = 4741
533017 Wp = 92
13994
YDOT = -649
613227 meter/sec RA = 71
92302 deg
ZDOT = -6022
312989 TA = 94
30246
MA = 94
16167
Ha = 194
633 n
mi
Hp = 183
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5361801
58 X = -1558498
81
Y = -21349078
42 feet Y = -6525050
76 meter
Z = -1953298
23 Z = -603121
68
XDOT = 15556
210686 XDOT = 4777
700696
YDOT = -2131
276991 feet/sec YDOT = -596
387546 meter/sec
ZDOT = -19758
244715 ZDOT = -5999
190312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13639239
39 X = -4157240
17
Y = 17273745
97 feet Y = 5265037
77 meter
Z = -1984008
21 Z = -604725
70
XDOT = -9997
492838 XDOT = -3047
235817
YDOT = -10113
260499 feet/sec YDOT = -3082
521800 meter/sec
ZDOT = -19667
722881 ZDOT = -5994
721934
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 09143
71672650
00010596 00000-0 82463-4 0 9089
2 25544 51
6412 72
4399 0009389 33
9827 326
1936 15
72937018 2102
Satellite: ISS
Catalog Number: 25544
Epoch time: 09143
71672650 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 72
4399 deg
Eccentricity:
0009389
Arg of perigee: 33
9827 deg
Mean anomaly: 326
1936 deg
Mean motion: 15
72937018 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 210
Checksum: 321
Coasting Arc #10 (Orbit 225)
---------------------------------------
Vector Time (GMT): 2009/144/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3937262
78 A = 6722998
42 meter
Y = 1316018
46 meter E =
0011572
Z = 5281576
61 I = 51
92637
XDOT = -2813
007419 Wp = 44
67150
YDOT = -7167
712916 meter/sec RA = 66
80823 deg
ZDOT = -302
572344 TA = 48
23692
MA = 48
13806
Ha = 194
770 n
mi
Hp = 182
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12917528
79 X = -3977343
53
Y = 4317645
88 feet Y = 1271764
68 meter
Z = 17328007
24 Z = 5262351
87
XDOT = -9229
026965 XDOT = -2731
177902
YDOT = -23516
118492 feet/sec YDOT = -7198
712022 meter/sec
ZDOT = -992
691416 ZDOT = -316
040676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11498900
65 X = 3504864
92
Y = 7475387
37 feet Y = 2278498
07 meter
Z = 17252777
12 Z = 5258646
47
XDOT = -12070
765677 XDOT = -3679
169378
YDOT = 21045
593114 feet/sec YDOT = 6414
696781 meter/sec
ZDOT = -1045
793389 ZDOT = -318
757825
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 09144
73321769
00010596 00000-0 82463-4 0 9095
2 25544 51
6412 67
2271 0009474 37
3101 322
8718 15
72991360 2269
Satellite: ISS
Catalog Number: 25544
Epoch time: 09144
73321769 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 67
2271 deg
Eccentricity:
0009474
Arg of perigee: 37
3101 deg
Mean anomaly: 322
8718 deg
Mean motion: 15
72991360 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 226
Checksum: 304
Coasting Arc #11 (Orbit 240)
---------------------------------------
Vector Time (GMT): 2009/145/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3236003
93 A = 6734997
76 meter
Y = 5894170
29 meter E =
0021601
Z = -70567
70 I = 51
95324
XDOT = -4137
718804 Wp = 42
73198
YDOT = 2331
273738 meter/sec RA = 61
70302 deg
ZDOT = 6067
451604 TA = 316
50448
MA = 316
67466
Ha = 194
684 n
mi
Hp = 182
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10616810
78 X = 3170196
62
Y = 19337829
04 feet Y = 5929989
24 meter
Z = -231521
31 Z = -55005
70
XDOT = -13575
192928 XDOT = -4192
954946
YDOT = 7648
535886 feet/sec YDOT = 2284
693358 meter/sec
ZDOT = 19906
337283 ZDOT = 6047
216566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8129227
20 X = 2477788
45
Y = -20508743
81 feet Y = -6251065
11 meter
Z = -170287
04 Z = -51903
49
XDOT = 13125
322235 XDOT = 4000
598217
YDOT = 5078
337835 feet/sec YDOT = 1547
877372 meter/sec
ZDOT = 19827
189528 ZDOT = 6043
327368
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 09145
68616560
00010596 00000-0 82463-4 0 9108
2 25544 51
6403 62
3401 0009461 40
4305 319
7559 15
73010024 2412
Satellite: ISS
Catalog Number: 25544
Epoch time: 09145
68616560 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 62
3401 deg
Eccentricity:
0009461
Arg of perigee: 40
4305 deg
Mean anomaly: 319
7559 deg
Mean motion: 15
73010024 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 241
Checksum: 270
Coasting Arc #12 (Orbit 256)
---------------------------------------
Vector Time (GMT): 2009/146/16:27:55
870
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3204888
11 A = 6722898
14 meter
Y = -2674137
36 meter E =
0022816
Z = -5289043
03 I = 51
89645
XDOT = 4492
141996 Wp = 70
52155
YDOT = 6219
097870 meter/sec RA = 56
59827 deg
ZDOT = -416
386804 TA = 195
49424
MA = 195
56420
Ha = 194
667 n
mi
Hp = 182
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10514724
78 X = 3260245
95
Y = -8773416
54 feet Y = -2637987
90 meter
Z = -17352503
38 Z = -5273339
63
XDOT = 14737
998676 XDOT = 4424
287871
YDOT = 20403
864403 feet/sec YDOT = 6268
952310 meter/sec
ZDOT = -1366
098438 ZDOT = -394
727461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13569394
26 X = -4135951
37
Y = -2351718
49 feet Y = -716803
80 meter
Z = -17291113
55 Z = -5270331
41
XDOT = 5727
417330 XDOT = 1745
716802
YDOT = -23484
051707 feet/sec YDOT = -7157
938960 meter/sec
ZDOT = -1280
966171 ZDOT = -390
438489
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 09146
70262953
00010596 00000-0 82463-4 0 9116
2 25544 51
6392 57
1267 0009421 44
5369 315
6549 15
73040239 2574
Satellite: ISS
Catalog Number: 25544
Epoch time: 09146
70262953 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 57
1267 deg
Eccentricity:
0009421
Arg of perigee: 44
5369 deg
Mean anomaly: 315
6549 deg
Mean motion: 15
73040239 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 257
Checksum: 310
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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