Date:
January 22nd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 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 2776)
---------------------------------------
Vector Time (GMT): 2007/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 654396
00 A = 6715018
71 meter
Y = -5197335
05 meter E =
0030773
Z = 4170347
35 I = 51
84979
XDOT = 6422
796474 Wp = 106
81626
YDOT = -2174
465182 meter/sec RA = 135
88507 deg
ZDOT = -3704
266869 TA = 20
80901
MA = 20
68401
Ha = 193
097 n
mi
Hp = 170
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2146968
52 X = 692206
42
Y = -17051624
18 feet Y = -5189805
94 meter
Z = 13682241
97 Z = 4173618
03
XDOT = 21072
166910 XDOT = 6464
628509
YDOT = -7134
072118 feet/sec YDOT = -2102
407897 meter/sec
ZDOT = -12153
106524 ZDOT = -3672
964156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15715840
90 X = 4790188
31
Y = -6932708
95 feet Y = -2113089
69 meter
Z = 13693830
64 Z = 4173879
58
XDOT = 16428
368506 XDOT = 5007
366721
YDOT = 13380
086818 feet/sec YDOT = 4078
250462 meter/sec
ZDOT = -12035
954796 ZDOT = -3668
559022
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 07022
54102421
00020000 00000-0 20000-3 0 9009
2 25544 51
6337 136
6096 0022838 120
5622 239
7801 15
77346637 27771
Satellite: ISS
Catalog Number: 25544
Epoch time: 07022
54102421 = yrday
fracday
Element set: 900
Inclination: 51
6337 deg
RA of node: 136
6096 deg
Eccentricity:
0022838
Arg of perigee: 120
5622 deg
Mean anomaly: 239
7801 deg
Mean motion: 15
77346637 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2777
Checksum: 282
Coasting Arc #2 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2007/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5226939
35 A = 6715434
45 meter
Y = 1229046
91 meter E =
0033013
Z = 4018922
24 I = 51
87190
XDOT = 1520
987710 Wp = 117
29434
YDOT = -6469
004033 meter/sec RA = 130
79026 deg
ZDOT = 3917
223801 TA = 292
32441
MA = 292
67403
Ha = 192
915 n
mi
Hp = 170
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17148751
15 X = -5259817
06
Y = 4032306
12 feet Y = 1170412
46 meter
Z = 13185440
41 Z = 3993450
43
XDOT = 4990
117158 XDOT = 1574
183199
YDOT = -21223
766511 feet/sec YDOT = -6451
698138 meter/sec
ZDOT = 12851
784125 ZDOT = 3924
741710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12483232
72 X = -3804889
33
Y = -12530557
16 feet Y = -3819313
82 meter
Z = 13090035
73 Z = 3989842
89
XDOT = 19726
672186 XDOT = 6012
689682
YDOT = -6062
431582 feet/sec YDOT = -1847
829146 meter/sec
ZDOT = 12879
141837 ZDOT = 3925
562432
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 07023
55466639
00020000 00000-0 20000-3 0 9016
2 25544 51
6341 131
3771 0022671 124
4587 235
8724 15
77446193 27933
Satellite: ISS
Catalog Number: 25544
Epoch time: 07023
55466639 = yrday
fracday
Element set: 901
Inclination: 51
6341 deg
RA of node: 131
3771 deg
Eccentricity:
0022671
Arg of perigee: 124
4587 deg
Mean anomaly: 235
8724 deg
Mean motion: 15
77446193 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2793
Checksum: 301
Coasting Arc #3 (Orbit 2807)
---------------------------------------
Vector Time (GMT): 2007/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1902478
90 A = 6719768
33 meter
Y = 5971174
70 meter E =
0024057
Z = -2460448
67 I = 51
90423
XDOT = -5490
128921 Wp = 115
06480
YDOT = 447
509859 meter/sec RA = 125
59898 deg
ZDOT = 5361
845902 TA = 217
26560
MA = 217
43276
Ha = 192
721 n
mi
Hp = 171
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6241728
67 X = -1957155
79
Y = 19590468
19 feet Y = 5949594
47 meter
Z = -8072338
15 Z = -2469823
44
XDOT = -18012
233993 XDOT = -5520
771499
YDOT = 1468
208198 feet/sec YDOT = 385
944724 meter/sec
ZDOT = 17591
357947 ZDOT = 5335
100829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19833439
00 X = -6045232
21
Y = 5368784
05 feet Y = 1636405
38 meter
Z = -8106732
95 Z = -2470932
20
XDOT = -10627
373331 XDOT = -3239
223391
YDOT = -13000
143295 feet/sec YDOT = -3962
443676 meter/sec
ZDOT = 17491
068985 ZDOT = 5331
277827
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 07024
50493443
00020000 00000-0 20000-3 0 9026
2 25544 51
6340 126
4720 0022448 127
5421 232
7788 15
77427292 28086
Satellite: ISS
Catalog Number: 25544
Epoch time: 07024
50493443 = yrday
fracday
Element set: 902
Inclination: 51
6340 deg
RA of node: 126
4720 deg
Eccentricity:
0022448
Arg of perigee: 127
5421 deg
Mean anomaly: 232
7788 deg
Mean motion: 15
77427292 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2808
Checksum: 284
Coasting Arc #4 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2007/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4320576
24 A = 6711007
24 meter
Y = 584783
13 meter E =
0032651
Z = -5124932
08 I = 51
89030
XDOT = -2739
949303 Wp = 111
87927
YDOT = 7017
086960 meter/sec RA = 120
48890 deg
ZDOT = -1528
836750 TA = 143
58993
MA = 143
36741
Ha = 192
608 n
mi
Hp = 171
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14175118
90 X = 4338611
71
Y = 1918579
83 feet Y = 633199
27 meter
Z = -16814081
64 Z = -5103899
13
XDOT = -8989
334983 XDOT = -2810
784997
YDOT = 23021
938845 feet/sec YDOT = 6986
051321 meter/sec
ZDOT = -5015
868603 ZDOT = -1542
319044
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6317069
81 X = 1925442
88
Y = 12936761
68 feet Y = 3943124
96 meter
Z = -16735086
26 Z = -5100854
29
XDOT = -23183
383473 XDOT = -7066
295283
YDOT = 4851
324139 feet/sec YDOT = 1478
683598 meter/sec
ZDOT = -5065
548253 ZDOT = -1543
979108
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 07025
51852607
00020000 00000-0 20000-3 0 9030
2 25544 51
6338 121
2387 0022425 131
5973 228
7118 15
77473423 28244
Satellite: ISS
Catalog Number: 25544
Epoch time: 07025
51852607 = yrday
fracday
Element set: 903
Inclination: 51
6338 deg
RA of node: 121
2387 deg
Eccentricity:
0022425
Arg of perigee: 131
5973 deg
Mean anomaly: 228
7118 deg
Mean motion: 15
77473423 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2824
Checksum: 286
Coasting Arc #5 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2007/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2761875
46 A = 6722192
08 meter
Y = -6108059
60 meter E =
0035133
Z = 149543
67 I = 51
94128
XDOT = 4401
058053 Wp = 134
51006
YDOT = 1820
691007 meter/sec RA = 115
33180 deg
ZDOT = -6075
676948 TA = 43
86680
MA = 43
58834
Ha = 192
511 n
mi
Hp = 171
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9061271
18 X = 2829244
93
Y = -20039565
62 feet Y = -6076798
10 meter
Z = 490628
83 Z = 163123
96
XDOT = 14439
166839 XDOT = 4409
885970
YDOT = 5973
395691 feet/sec YDOT = 1869
955851 meter/sec
ZDOT = -19933
323321 ZDOT = -6054
275262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21634190
65 X = 6594101
31
Y = -3949793
29 feet Y = -1203896
99 meter
Z = 540805
30 Z = 164837
46
XDOT = 3075
870517 XDOT = 937
525334
YDOT = 13786
643427 feet/sec YDOT = 4202
168917 meter/sec
ZDOT = -19852
781147 ZDOT = -6051
127694
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 07026
53209142
00020000 00000-0 20000-3 0 9044
2 25544 51
6332 116
0058 0022527 135
1091 225
1900 15
77517275 28401
Satellite: ISS
Catalog Number: 25544
Epoch time: 07026
53209142 = yrday
fracday
Element set: 904
Inclination: 51
6332 deg
RA of node: 116
0058 deg
Eccentricity:
0022527
Arg of perigee: 135
1091 deg
Mean anomaly: 225
1900 deg
Mean motion: 15
77517275 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2840
Checksum: 257
Coasting Arc #6 (Orbit 2855)
---------------------------------------
Vector Time (GMT): 2007/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3366249
38 A = 6710214
62 meter
Y = -2595986
61 meter E =
0023039
Z = 5174310
12 I = 51
91377
XDOT = 3471
316234 Wp = 129
20940
YDOT = -6799
904225 meter/sec RA = 110
18107 deg
ZDOT = -1164
095462 TA = 331
76904
MA = 331
89373
Ha = 192
306 n
mi
Hp = 171
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11044125
28 X = -3362106
07
Y = -8517016
43 feet Y = -2633607
18 meter
Z = 16976083
09 Z = 5157966
91
XDOT = 11388
832790 XDOT = 3552
750631
YDOT = -22309
397064 feet/sec YDOT = -6760
630606 meter/sec
ZDOT = -3819
210832 ZDOT = -1147
034819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 427649
67 X = 130347
62
Y = -14014961
15 feet Y = -4271760
16 meter
Z = 16914421
32 Z = 5155515
62
XDOT = 23756
059902 XDOT = 7240
847058
YDOT = -3765
025334 feet/sec YDOT = -1147
579722 meter/sec
ZDOT = -3756
048692 ZDOT = -1144
843641
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 07027
54562740
00020000 00000-0 20000-3 0 9053
2 25544 51
6340 110
7724 0022241 138
8623 221
4223 15
77618481 28560
Satellite: ISS
Catalog Number: 25544
Epoch time: 07027
54562740 = yrday
fracday
Element set: 905
Inclination: 51
6340 deg
RA of node: 110
7724 deg
Eccentricity:
0022241
Arg of perigee: 138
8623 deg
Mean anomaly: 221
4223 deg
Mean motion: 15
77618481 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2856
Checksum: 275
Coasting Arc #7 (Orbit 2871)
---------------------------------------
Vector Time (GMT): 2007/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3219780
63 A = 6719914
13 meter
Y = 5493980
21 meter E =
0029860
Z = 2147834
43 I = 51
95493
XDOT = -3364
999730 Wp = 115
54866
YDOT = -4164
302581 meter/sec RA = 105
06837 deg
ZDOT = 5535
595842 TA = 268
39423
MA = 268
73628
Ha = 192
140 n
mi
Hp = 171
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10563584
74 X = -3291409
42
Y = 18024869
44 feet Y = 5457574
10 meter
Z = 7046700
87 Z = 2132019
58
XDOT = -11040
025360 XDOT = -3345
074305
YDOT = -13662
410043 feet/sec YDOT = -4201
821063 meter/sec
ZDOT = 18161
403682 ZDOT = 5519
296889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20790508
21 X = -6336946
90
Y = 2250189
64 feet Y = 685857
80 meter
Z = 6988036
12 Z = 2129953
41
XDOT = 4477
672561 XDOT = 1364
794597
YDOT = -15577
023099 feet/sec YDOT = -4747
876641 meter/sec
ZDOT = 18099
707456 ZDOT = 5516
790833
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 07028
55913998
00020000 00000-0 20000-3 0 9061
2 25544 51
6338 105
5395 0022292 142
3524 217
9206 15
77625060 28729
Satellite: ISS
Catalog Number: 25544
Epoch time: 07028
55913998 = yrday
fracday
Element set: 906
Inclination: 51
6338 deg
RA of node: 105
5395 deg
Eccentricity:
0022292
Arg of perigee: 142
3524 deg
Mean anomaly: 217
9206 deg
Mean motion: 15
77625060 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2872
Checksum: 302
Coasting Arc #8 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2007/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2535069
73 A = 6714110
36 meter
Y = 4611589
99 meter E =
0029216
Z = -4200788
39 I = 51
94157
XDOT = -3890
102727 Wp = 136
36308
YDOT = 5503
419439 meter/sec RA = 99
88232 deg
ZDOT = 3688
529161 TA = 171
23341
MA = 171
18228
Ha = 191
942 n
mi
Hp = 171
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8317157
91 X = 2503720
10
Y = 15129888
42 feet Y = 4639763
74 meter
Z = -13782114
14 Z = -4188548
92
XDOT = -12762
804222 XDOT = -3969
271448
YDOT = 18055
838055 feet/sec YDOT = 5459
475078 meter/sec
ZDOT = 12101
473624 ZDOT = 3669
439761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6858343
65 X = -2090423
14
Y = 15884956
09 feet Y = 4841734
62 meter
Z = -13735596
16 Z = -4186609
71
XDOT = -20974
687015 XDOT = -6393
084602
YDOT = 1362
500190 feet/sec YDOT = 415
290058 meter/sec
ZDOT = 12030
508087 ZDOT = 3666
898865
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 07029
50928356
00020000 00000-0 20000-3 0 9072
2 25544 51
6333 100
6333 0022251 145
5407 214
7206 15
77681746 28876
Satellite: ISS
Catalog Number: 25544
Epoch time: 07029
50928356 = yrday
fracday
Element set: 907
Inclination: 51
6333 deg
RA of node: 100
6333 deg
Eccentricity:
0022251
Arg of perigee: 145
5407 deg
Mean anomaly: 214
7206 deg
Mean motion: 15
77681746 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2887
Checksum: 290
Coasting Arc #9 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2007/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3571190
82 A = 6714353
23 meter
Y = -3914301
69 meter E =
0024816
Z = -4128522
43 I = 51
94588
XDOT = 2465
198648 Wp = 131
57135
YDOT = 6227
370943 meter/sec RA = 94
79025 deg
ZDOT = -3802
497827 TA = 99
73940
MA = 99
45904
Ha = 191
883 n
mi
Hp = 171
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11716505
32 X = 3634750
76
Y = -12842197
16 feet Y = -3874010
84 meter
Z = -13545021
10 Z = -4111020
08
XDOT = 8087
922072 XDOT = 2413
851435
YDOT = 20431
007030 feet/sec YDOT = 6254
651469 meter/sec
ZDOT = -12475
386571 ZDOT = -3790
646279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17393171
36 X = 5301438
63
Y = 1199396
04 feet Y = 365575
91 meter
Z = -13479805
67 Z = -4108644
77
XDOT = -10786
365509 XDOT = -3287
684207
YDOT = 17855
681002 feet/sec YDOT = 5442
411569 meter/sec
ZDOT = -12430
120333 ZDOT = -3788
700677
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 07030
52274503
00020000 00000-0 20000-3 0 9085
2 25544 51
6332 95
3990 0022152 149
4254 210
8207 15
77677594 29030
Satellite: ISS
Catalog Number: 25544
Epoch time: 07030
52274503 = yrday
fracday
Element set: 908
Inclination: 51
6332 deg
RA of node: 95
3990 deg
Eccentricity:
0022152
Arg of perigee: 149
4254 deg
Mean anomaly: 210
8207 deg
Mean motion: 15
77677594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2903
Checksum: 287
Coasting Arc #10 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2007/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1805500
66 A = 6719302
76 meter
Y = -6043346
46 meter E =
0033399
Z = 2254466
39 I = 51
96497
XDOT = 4278
755456 Wp = 135
54209
YDOT = -3339
103881 meter/sec RA = 89
60319 deg
ZDOT = -5499
091014 TA = 19
15939
MA = 19
03408
Ha = 191
571 n
mi
Hp = 171
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5923558
60 X = -1748740
37
Y = -19827252
17 feet Y = -6063219
41 meter
Z = 7396543
28 Z = 2245832
88
XDOT = 14037
911602 XDOT = 4342
488543
YDOT = -10955
065228 feet/sec YDOT = -3290
899622 meter/sec
ZDOT = -18041
637185 ZDOT = -5478
150957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11475573
02 X = 3497754
66
Y = -17233955
60 feet Y = -5252909
67 meter
Z = 7363377
34 Z = 2244357
41
XDOT = 16195
992338 XDOT = 4936
538465
YDOT = 3074
049049 feet/sec YDOT = 936
970150 meter/sec
ZDOT = -17963
437601 ZDOT = -5475
255781
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 07031
53617918
00020000 00000-0 20000-3 0 9099
2 25544 51
6338 90
1653 0021920 152
8751 207
3564 15
77760921 29198
Satellite: ISS
Catalog Number: 25544
Epoch time: 07031
53617918 = yrday
fracday
Element set: 909
Inclination: 51
6338 deg
RA of node: 90
1653 deg
Eccentricity:
0021920
Arg of perigee: 152
8751 deg
Mean anomaly: 207
3564 deg
Mean motion: 15
77760921 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2919
Checksum: 299
Coasting Arc #11 (Orbit 2934)
---------------------------------------
Vector Time (GMT): 2007/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3892800
01 A = 6709832
73 meter
Y = 1770069
22 meter E =
0025557
Z = 5164231
47 I = 51
93123
XDOT = -1693
502770 Wp = 151
63997
YDOT = -7421
575436 meter/sec RA = 84
49181 deg
ZDOT = 1242
690484 TA = 286
41072
MA = 286
69150
Ha = 191
502 n
mi
Hp = 172
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12771653
58 X = -3937389
91
Y = 5807313
73 feet Y = 1726288
12 meter
Z = 16943016
63 Z = 5145212
69
XDOT = -5556
111449 XDOT = -1616
424357
YDOT = -24349
000775 feet/sec YDOT = -7440
082241 meter/sec
ZDOT = 4077
068517 ZDOT = 1234
650464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12780217
14 X = -3895410
18
Y = -5992766
60 feet Y = -1826595
26 meter
Z = 16871829
74 Z = 5142533
71
XDOT = 14425
484789 XDOT = 4396
887764
YDOT = -19145
489767 feet/sec YDOT = -5835
545281 meter/sec
ZDOT = 4045
954782 ZDOT = 1233
207018
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 07032
54958835
00020000 00000-0 20000-3 0 9109
2 25544 51
6332 84
9316 0021955 156
7170 203
4994 15
77789567 29354
Satellite: ISS
Catalog Number: 25544
Epoch time: 07032
54958835 = yrday
fracday
Element set: 910
Inclination: 51
6332 deg
RA of node: 84
9316 deg
Eccentricity:
0021955
Arg of perigee: 156
7170 deg
Mean anomaly: 203
4994 deg
Mean motion: 15
77789567 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2935
Checksum: 325
Coasting Arc #12 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2007/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1102145
02 A = 6721417
13 meter
Y = 6635462
33 meter E =
0020532
Z = 184525
44 I = 51
96587
XDOT = -4706
536188 Wp = 124
94259
YDOT = 599
920626 meter/sec RA = 79
33969 deg
ZDOT = 6054
728044 TA = 237
05264
MA = 237
25025
Ha = 191
263 n
mi
Hp = 172
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3615961
36 X = 1026968
07
Y = 21769889
53 feet Y = 6647366
79 meter
Z = 605398
42 Z = 189697
13
XDOT = -15441
391693 XDOT = -4742
306553
YDOT = 1968
243525 feet/sec YDOT = 547
089279 meter/sec
ZDOT = 19864
593321 ZDOT = 6031
777616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13889958
79 X = -4233659
44
Y = 17147809
86 feet Y = 5226652
45 meter
Z = 625648
10 Z = 190697
54
XDOT = -10540
990680 XDOT = -3212
893959
YDOT = -9316
020122 feet/sec YDOT = -2839
522933 meter/sec
ZDOT = 19778
494089 ZDOT = 6028
484998
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 07033
56297412
00020000 00000-0 20000-3 0 9110
2 25544 51
6328 79
6967 0021746 159
9391 200
2634 15
77781007 29515
Satellite: ISS
Catalog Number: 25544
Epoch time: 07033
56297412 = yrday
fracday
Element set: 911
Inclination: 51
6328 deg
RA of node: 79
6967 deg
Eccentricity:
0021746
Arg of perigee: 159
9391 deg
Mean anomaly: 200
2634 deg
Mean motion: 15
77781007 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2951
Checksum: 307
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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