Date:
January 2nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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) : 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 1965)
---------------------------------------
Vector Time (GMT): 2009/001/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4096735
47 A = 6729446
27 meter
Y = -2908049
91 meter E =
0011976
Z = 4465779
46 I = 51
95809
XDOT = 1313
352829 Wp = 103
07988
YDOT = -6858
283467 meter/sec RA = 79
43851 deg
ZDOT = -3256
585391 TA = 19
40025
MA = 19
35470
Ha = 195
310 n
mi
Hp = 185
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13440733
17 X = -4085606
41
Y = -9540846
17 feet Y = -2953800
13 meter
Z = 14651507
43 Z = 4445904
53
XDOT = 4308
900356 XDOT = 1405
765399
YDOT = -22500
930011 feet/sec YDOT = -6843
079820 meter/sec
ZDOT = -10684
335273 ZDOT = -3249
981292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6911673
28 X = 2106678
02
Y = -15039145
82 feet Y = -4583931
65 meter
Z = 14573969
58 Z = 4442145
93
XDOT = 21824
084991 XDOT = 6651
981105
YDOT = -314
243457 feet/sec YDOT = -95
781406 meter/sec
ZDOT = -10659
098946 ZDOT = -3248
893359
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 09001
54197331
00010596 00000-0 82463-4 0 9003
2 25544 51
6421 79
9558 0006875 152
5003 207
6524 15
71945191 19667
Satellite: ISS
Catalog Number: 25544
Epoch time: 09001
54197331 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 79
9558 deg
Eccentricity:
0006875
Arg of perigee: 152
5003 deg
Mean anomaly: 207
6524 deg
Mean motion: 15
71945191 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1966
Checksum: 310
Coasting Arc #2 (Orbit 1989)
---------------------------------------
Vector Time (GMT): 2009/002/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -46083
83 A = 6735877
39 meter
Y = 6348066
00 meter E =
0016325
Z = 2241674
04 I = 51
97252
XDOT = -5014
000593 Wp = 96
64150
YDOT = -1987
868296 meter/sec RA = 74
38485 deg
ZDOT = 5490
457075 TA = 288
36374
MA = 288
54121
Ha = 195
165 n
mi
Hp = 185
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -151193
67 X = -127955
09
Y = 20826988
19 feet Y = 6347092
74 meter
Z = 7354573
61 Z = 2241251
75
XDOT = -16450
133180 XDOT = -5018
070713
YDOT = -6521
877612 feet/sec YDOT = -2043
960900 meter/sec
ZDOT = 18013
310615 ZDOT = 5466
089221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20447343
63 X = -6232350
34
Y = 3963628
87 feet Y = 1208114
08 meter
Z = 7353355
32 Z = 2241302
70
XDOT = 3378
645470 XDOT = 1029
811139
YDOT = -16030
603964 feet/sec YDOT = -4886
128088 meter/sec
ZDOT = 17918
350305 ZDOT = 5461
513173
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 09002
55914702
00010596 00000-0 82463-4 0 9015
2 25544 51
6415 74
7484 0006936 155
4610 204
6883 15
71937958 19909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09002
55914702 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 74
7484 deg
Eccentricity:
0006936
Arg of perigee: 155
4610 deg
Mean anomaly: 204
6883 deg
Mean motion: 15
71937958 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1990
Checksum: 324
Coasting Arc #3 (Orbit 2004)
---------------------------------------
Vector Time (GMT): 2009/003/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4432966
42 A = 6727118
87 meter
Y = 546427
46 meter E =
0018006
Z = -5046070
86 I = 51
93327
XDOT = 1222
775510 Wp = 121
66235
YDOT = 7353
121440 meter/sec RA = 69
25185 deg
ZDOT = 1866
084313 TA = 166
32857
MA = 166
27974
Ha = 195
027 n
mi
Hp = 185
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14543853
08 X = 4451039
52
Y = 1792741
01 feet Y = 596100
84 meter
Z = -16555350
59 Z = -5024491
65
XDOT = 4011
730676 XDOT = 1131
395752
YDOT = 24124
414174 feet/sec YDOT = 7366
284170 meter/sec
ZDOT = 6122
323860 ZDOT = 1871
803060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1415436
44 X = 431425
03
Y = 14680216
72 feet Y = 4474530
06 meter
Z = -16471338
52 Z = -5020463
98
XDOT = -21623
307352 XDOT = -6590
784081
YDOT = 8995
881268 feet/sec YDOT = 2741
944611 meter/sec
ZDOT = 6145
064595 ZDOT = 1873
015689
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 09003
51273332
00010596 00000-0 82463-4 0 9020
2 25544 51
6409 69
8661 0006773 158
3540 201
7909 15
71951113 20051
Satellite: ISS
Catalog Number: 25544
Epoch time: 09003
51273332 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 69
8661 deg
Eccentricity:
0006773
Arg of perigee: 158
3540 deg
Mean anomaly: 201
7909 deg
Mean motion: 15
71951113 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2005
Checksum: 291
Coasting Arc #4 (Orbit 2020)
---------------------------------------
Vector Time (GMT): 2009/004/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2168009
74 A = 6737461
73 meter
Y = -6290240
05 meter E =
0016322
Z = -1007508
82 I = 51
95744
XDOT = 4829
020590 Wp = 149
40529
YDOT = -719
374020 meter/sec RA = 64
17789 deg
ZDOT = -5955
648150 TA = 41
55389
MA = 41
42993
Ha = 194
915 n
mi
Hp = 185
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7112892
86 X = -2092615
82
Y = -20637270
51 feet Y = -6314062
37 meter
Z = -3305475
14 Z = -1017858
34
XDOT = 15843
243404 XDOT = 4865
637310
YDOT = -2360
150985 feet/sec YDOT = -665
167952 meter/sec
ZDOT = -19539
528050 ZDOT = -5932
099871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18416383
27 X = 5613313
62
Y = -11707108
55 feet Y = -3568326
69 meter
Z = -3346159
26 Z = -1019909
34
XDOT = 5159
434197 XDOT = 1572
595543
YDOT = 13623
415250 feet/sec YDOT = 4152
416968 meter/sec
ZDOT = -19447
935429 ZDOT = -5927
730719
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 09004
52987797
00010596 00000-0 82463-4 0 9030
2 25544 51
6414 64
6581 0006770 161
0096 199
1320 15
71986648 20211
Satellite: ISS
Catalog Number: 25544
Epoch time: 09004
52987797 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 64
6581 deg
Eccentricity:
0006770
Arg of perigee: 161
0096 deg
Mean anomaly: 199
1320 deg
Mean motion: 15
71986648 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2021
Checksum: 321
Coasting Arc #5 (Orbit 2036)
---------------------------------------
Vector Time (GMT): 2009/005/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3774397
60 A = 6725786
91 meter
Y = 1753681
87 meter E =
0007032
Z = 5279531
12 I = 51
90456
XDOT = -3684
201634 Wp = 143
28003
YDOT = -6751
904002 meter/sec RA = 59
06536 deg
ZDOT = -396
370305 TA = 310
43881
MA = 310
50012
Ha = 194
849 n
mi
Hp = 185
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12383194
23 X = -3819374
12
Y = 5753549
45 feet Y = 1711222
44 meter
Z = 17321296
34 Z = 5261085
95
XDOT = -12087
275701 XDOT = -3606
501413
YDOT = -22151
916016 feet/sec YDOT = -6792
668401 meter/sec
ZDOT = -1300
427509 ZDOT = -414
080064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8688420
14 X = -2648230
46
Y = -10650628
26 feet Y = -3246311
49 meter
Z = 17249626
39 Z = 5257686
12
XDOT = 17657
305615 XDOT = 5381
946751
YDOT = -16594
706593 feet/sec YDOT = -5058
066570 meter/sec
ZDOT = -1369
775348 ZDOT = -417
507526
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 09005
54700649
00010596 00000-0 82463-4 0 9043
2 25544 51
6415 59
4506 0006709 165
5375 194
5981 15
72023129 20378
Satellite: ISS
Catalog Number: 25544
Epoch time: 09005
54700649 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 59
4506 deg
Eccentricity:
0006709
Arg of perigee: 165
5375 deg
Mean anomaly: 194
5981 deg
Mean motion: 15
72023129 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2037
Checksum: 311
Coasting Arc #6 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2009/006/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4149506
01 A = 6737867
24 meter
Y = 5298303
89 meter E =
0009641
Z = -304641
32 I = 51
92871
XDOT = -3574
205265 Wp = 76
47882
YDOT = 3137
610188 meter/sec RA = 53
96479 deg
ZDOT = 6046
412538 TA = 280
22816
MA = 280
33687
Ha = 194
686 n
mi
Hp = 186
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13613864
86 X = 4091431
00
Y = 17382886
77 feet Y = 5344381
39 meter
Z = -999479
39 Z = -284623
42
XDOT = -11726
395225 XDOT = -3638
397384
YDOT = 10293
996681 feet/sec YDOT = 3097
281767 meter/sec
ZDOT = 19837
311477 ZDOT = 6028
893404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13127984
14 X = -4001409
56
Y = 17756924
36 feet Y = 5412310
54 meter
Z = -921248
03 Z = -280796
40
XDOT = -11780
929486 XDOT = -3590
827307
YDOT = -7713
980494 feet/sec YDOT = -2351
221255 meter/sec
ZDOT = 19769
325997 ZDOT = 6025
690564
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 09006
50055330
00010596 00000-0 82463-4 0 9051
2 25544 51
6415 54
5680 0006484 167
1704 192
9625 15
71987722 20522
Satellite: ISS
Catalog Number: 25544
Epoch time: 09006
50055330 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 54
5680 deg
Eccentricity:
0006484
Arg of perigee: 167
1704 deg
Mean anomaly: 192
9625 deg
Mean motion: 15
71987722 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2052
Checksum: 303
Coasting Arc #7 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2009/007/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2317742
26 A = 6726060
78 meter
Y = -3572986
88 meter E =
0016043
Z = -5218424
53 I = 51
87196
XDOT = 5600
789527 Wp = 106
28211
YDOT = 5159
129806 meter/sec RA = 48
87381 deg
ZDOT = -1051
873298 TA = 153
74099
MA = 153
65957
Ha = 194
588 n
mi
Hp = 186
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7604141
27 X = 2382873
94
Y = -11722397
90 feet Y = -3546703
65 meter
Z = -17120815
40 Z = -5207007
21
XDOT = 18375
293724 XDOT = 5547
792845
YDOT = 16926
278892 feet/sec YDOT = 5221
464906 meter/sec
ZDOT = -3451
027881 ZDOT = -1024
792616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13422624
91 X = 4091216
07
Y = 4072213
96 feet Y = 1241210
81 meter
Z = -17076595
41 Z = -5204946
28
XDOT = -10734
871239 XDOT = -3271
988754
YDOT = 21452
605658 feet/sec YDOT = 6538
754205 meter/sec
ZDOT = -3345
322233 ZDOT = -1019
654217
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 09007
51765507
00010596 00000-0 82463-4 0 9068
2 25544 51
6424 49
3597 0006628 171
2723 188
8556 15
72031320 20687
Satellite: ISS
Catalog Number: 25544
Epoch time: 09007
51765507 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 49
3597 deg
Eccentricity:
0006628
Arg of perigee: 171
2723 deg
Mean anomaly: 188
8556 deg
Mean motion: 15
72031320 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2068
Checksum: 315
Coasting Arc #8 (Orbit 2083)
---------------------------------------
Vector Time (GMT): 2009/008/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5480363
43 A = 6736674
11 meter
Y = -3587111
36 meter E =
0018527
Z = 1527482
01 I = 51
88723
XDOT = 1536
180461 Wp = 134
78674
YDOT = -4830
512292 meter/sec RA = 43
74738 deg
ZDOT = -5802
435806 TA = 28
43593
MA = 28
33496
Ha = 194
436 n
mi
Hp = 186
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17980194
99 X = -5447264
66
Y = -11768738
06 feet Y = -3648211
14 meter
Z = 5011423
91 Z = 1500938
28
XDOT = 5039
962144 XDOT = 1618
268972
YDOT = -15848
137441 feet/sec YDOT = -4812
873907 meter/sec
ZDOT = -19036
862879 ZDOT = -5794
774455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5838801
45 X = 1779666
68
Y = -20705696
96 feet Y = -6311096
43 meter
Z = 4907900
60 Z = 1495928
10
XDOT = 15153
234518 XDOT = 4618
705881
YDOT = -255
998830 feet/sec YDOT = -78
028443 meter/sec
ZDOT = -19007
327793 ZDOT = -5793
433511
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 09008
53474162
00010596 00000-0 82463-4 0 9076
2 25544 51
6419 44
1517 0006518 173
8931 186
2311 15
72082412 20840
Satellite: ISS
Catalog Number: 25544
Epoch time: 09008
53474162 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 44
1517 deg
Eccentricity:
0006518
Arg of perigee: 173
8931 deg
Mean anomaly: 186
2311 deg
Mean motion: 15
72082412 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2084
Checksum: 296
Coasting Arc #9 (Orbit 2099)
---------------------------------------
Vector Time (GMT): 2009/009/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -267284
97 A = 6727435
52 meter
Y = 4660905
99 meter E =
0011884
Z = 4842158
49 I = 51
83357
XDOT = -6698
189560 Wp = 147
59139
YDOT = -2918
308476 meter/sec RA = 38
67500 deg
ZDOT = 2426
772748 TA = 278
70533
MA = 278
83992
Ha = 194
303 n
mi
Hp = 186
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -876919
19 X = -342906
21
Y = 15291686
33 feet Y = 4657493
40 meter
Z = 15886346
74 Z = 4840677
15
XDOT = -21975
687532 XDOT = -6676
847433
YDOT = -9574
502873 feet/sec YDOT = -2993
092602 meter/sec
ZDOT = 7961
852849 ZDOT = 2394
284600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14815626
21 X = -4515802
87
Y = 3908511
96 feet Y = 1191314
45 meter
Z = 15880850
90 Z = 4840483
35
XDOT = 2418
056858 XDOT = 737
023730
YDOT = -22837
245005 feet/sec YDOT = -6960
792278 meter/sec
ZDOT = 7835
224634 ZDOT = 2388
176468
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 09009
55181443
00010596 00000-0 82463-4 0 9087
2 25544 51
6412 38
9434 0006506 176
7159 183
4047 15
72093005 21007
Satellite: ISS
Catalog Number: 25544
Epoch time: 09009
55181443 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 38
9434 deg
Eccentricity:
0006506
Arg of perigee: 176
7159 deg
Mean anomaly: 183
4047 deg
Mean motion: 15
72093005 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2100
Checksum: 294
Coasting Arc #10 (Orbit 2114)
---------------------------------------
Vector Time (GMT): 2009/010/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6010385
39 A = 6734435
61 meter
Y = 1465244
84 meter E =
0005378
Z = -2669679
89 I = 51
83475
XDOT = 962
430416 Wp = 131
13401
YDOT = 5561
319131 meter/sec RA = 33
52661 deg
ZDOT = 5222
411197 TA = 198
60442
MA = 198
62409
Ha = 194
124 n
mi
Hp = 186
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19719112
18 X = 6006522
67
Y = 4807233
72 feet Y = 1532435
29 meter
Z = -8758792
28 Z = -2640491
09
XDOT = 3157
580106 XDOT = 874
802231
YDOT = 18245
797673 feet/sec YDOT = 5571
590767 meter/sec
ZDOT = 17133
895002 ZDOT = 5226
874675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2028072
99 X = 618156
65
Y = 20243981
70 feet Y = 6170365
62 meter
Z = -8645082
32 Z = -2635021
09
XDOT = -14719
712135 XDOT = -4486
568259
YDOT = 8794
407873 feet/sec YDOT = 2680
535520 meter/sec
ZDOT = 17151
591292 ZDOT = 5227
805026
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 09010
50530654
00010596 00000-0 82463-4 0 9097
2 25544 51
6422 34
0609 0006511 180
0571 180
0592 15
72148754 21157
Satellite: ISS
Catalog Number: 25544
Epoch time: 09010
50530654 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 34
0609 deg
Eccentricity:
0006511
Arg of perigee: 180
0571 deg
Mean anomaly: 180
0592 deg
Mean motion: 15
72148754 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2115
Checksum: 274
Coasting Arc #11 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2009/011/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1943066
43 A = 6729629
95 meter
Y = -4852381
32 meter E =
0008143
Z = -4242914
70 I = 51
79263
XDOT = 6777
292889 Wp = 114
50424
YDOT = 438
502637 meter/sec RA = 28
46405 deg
ZDOT = -3613
901469 TA = 118
82241
MA = 118
74064
Ha = 193
967 n
mi
Hp = 186
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6374889
85 X = -1868051
07
Y = -15919886
21 feet Y = -4873689
78 meter
Z = -13920323
80 Z = -4252172
36
XDOT = 22235
212892 XDOT = 6789
441036
YDOT = 1438
656945 feet/sec YDOT = 514
358684 meter/sec
ZDOT = -11856
632116 ZDOT = -3580
948598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12732772
29 X = 3880948
99
Y = -11443162
24 feet Y = -3487875
85 meter
Z = -13956645
74 Z = -4253985
62
XDOT = 5581
580112 XDOT = 1701
265618
YDOT = 20480
276823 feet/sec YDOT = 6242
388376 meter/sec
ZDOT = -11728
320349 ZDOT = -3574
792042
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 09011
52235056
00010596 00000-0 82463-4 0 9100
2 25544 51
6414 28
8517 0006398 184
7567 175
3535 15
72138248 21315
Satellite: ISS
Catalog Number: 25544
Epoch time: 09011
52235056 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 28
8517 deg
Eccentricity:
0006398
Arg of perigee: 184
7567 deg
Mean anomaly: 175
3535 deg
Mean motion: 15
72138248 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2131
Checksum: 305
Coasting Arc #12 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2009/012/12:00:01
000
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5627418
11 A = 6731765
67 meter
Y = 678517
09 meter E =
0012365
Z = 3617184
46 I = 51
77257
XDOT = -3473
944601 Wp = 115
55504
YDOT = -5277
048883 meter/sec RA = 23
30196 deg
ZDOT = -4408
292873 TA = 21
22519
MA = 21
17394
Ha = 193
875 n
mi
Hp = 186
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18462657
83 X = -5652158
31
Y = 2226105
94 feet Y = 615449
32 meter
Z = 11867403
08 Z = 3589787
17
XDOT = -11397
456040 XDOT = -3393
263465
YDOT = -17313
152502 feet/sec YDOT = -5315
444965 meter/sec
ZDOT = -14462
903126 ZDOT = -4424
973439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8822431
42 X = -2689077
10
Y = -16447166
37 feet Y = -5013096
31 meter
Z = 11760780
58 Z = 3584685
92
XDOT = 10804
176495 XDOT = 3293
112996
YDOT = -16199
194413 feet/sec YDOT = -4937
514457 meter/sec
ZDOT = -14528
153111 ZDOT = -4428
181068
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 09012
53937965
00010596 00000-0 82463-4 0 9111
2 25544 51
6405 23
6427 0006257 188
6886 171
4169 15
72183546 21477
Satellite: ISS
Catalog Number: 25544
Epoch time: 09012
53937965 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 23
6427 deg
Eccentricity:
0006257
Arg of perigee: 188
6886 deg
Mean anomaly: 171
4169 deg
Mean motion: 15
72183546 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2147
Checksum: 328
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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