Date:
March 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7104 18 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
075/02:53:16
462 -2
3 8
7 8
7
N/A 5
4 -0
3 186
2
000/00:12:32
924 -6
4 0
0 178
5
Coasting Arc #1 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2007/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5114696
53 A = 6709340
97 meter
Y = -1173158
84 meter E =
0014080
Z = -4166935
41 I = 51
37279
XDOT = -1445
777579 Wp = 331
55214
YDOT = -6643
337627 meter/sec RA = 232
30300 deg
ZDOT = 3652
164133 TA = 335
69700
MA = 335
76334
Ha = 185
498 n
mi
Hp = 173
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16780500
43 X = -5080956
10
Y = -3848946
31 feet Y = -1230165
64 meter
Z = -13671047
93 Z = -4191700
20
XDOT = -4743
364760 XDOT = -1389
124618
YDOT = -21795
727124 feet/sec YDOT = -6659
188302 meter/sec
ZDOT = 11982
165791 ZDOT = 3645
278378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15895793
33 X = -4845037
81
Y = -6416025
18 feet Y = -1955604
47 meter
Z = -13764283
83 Z = -4195353
71
XDOT = -1806
924698 XDOT = -550
750648
YDOT = -21120
932572 feet/sec YDOT = -6437
660248 meter/sec
ZDOT = 11955
368232 ZDOT = 3643
996237
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 07073
50929144
00020000 00000-0 20000-3 0 9000
2 25544 51
6307 233
1680 0021018 316
4053 43
5451 15
79321604 35829
Satellite: ISS
Catalog Number: 25544
Epoch time: 07073
50929144 = yrday
fracday
Element set: 900
Inclination: 51
6307 deg
RA of node: 233
1680 deg
Eccentricity:
0021018
Arg of perigee: 316
4053 deg
Mean anomaly: 43
5451 deg
Mean motion: 15
79321604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3582
Checksum: 261
Coasting Arc #2 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2007/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -57686
38 A = 6708519
49 meter
Y = 5084879
91 meter E =
0020148
Z = -4382548
62 I = 51
38921
XDOT = -6312
777045 Wp = 346
69963
YDOT = -2933
576996 meter/sec RA = 227
15822 deg
ZDOT = -3298
257813 TA = 249
96439
MA = 250
18141
Ha = 185
839 n
mi
Hp = 173
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -189259
79 X = -93252
75
Y = 16682676
88 feet Y = 5084035
82 meter
Z = -14378440
35 Z = -4382915
42
XDOT = -20711
210779 XDOT = -6263
482172
YDOT = -9624
596445 feet/sec YDOT = -3003
894491 meter/sec
ZDOT = -10821
055818 ZDOT = -3328
804829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2435642
49 X = -742383
83
Y = 16504422
16 feet Y = 5030547
88 meter
Z = -14379108
76 Z = -4382752
35
XDOT = -17902
406276 XDOT = -5456
653433
YDOT = -12233
821993 feet/sec YDOT = -3728
868944 meter/sec
ZDOT = -10936
281002 ZDOT = -3333
378450
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 07074
52168518
00020000 00000-0 20000-3 0 9014
2 25544 51
6310 227
9272 0021099 320
6748 39
2884 15
79379565 35986
Satellite: ISS
Catalog Number: 25544
Epoch time: 07074
52168518 = yrday
fracday
Element set: 901
Inclination: 51
6310 deg
RA of node: 227
9272 deg
Eccentricity:
0021099
Arg of perigee: 320
6748 deg
Mean anomaly: 39
2884 deg
Mean motion: 15
79379565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3598
Checksum: 322
Coasting Arc #3 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2007/075/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4198424
04 A = 6721335
03 meter
Y = 5153124
84 meter E =
0005661
Z = -1005069
12 I = 51
43031
XDOT = -4330
860188 Wp = 298
43526
YDOT = 2370
728042 meter/sec RA = 223
90372 deg
ZDOT = -5908
217667 TA = 252
58898
MA = 252
65089
Ha = 186
229 n
mi
Hp = 178
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13774357
07 X = 4145371
36
Y = 16906577
57 feet Y = 5199777
29 meter
Z = -3297470
87 Z = -984802
73
XDOT = -14208
858886 XDOT = -4328
347676
YDOT = 7777
979139 feet/sec YDOT = 2322
311690 meter/sec
ZDOT = -19383
916231 ZDOT = -5929
250563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21232939
43 X = -6471799
94
Y = -5022829
42 feet Y = -1530958
41 meter
Z = -3220568
25 Z = -981629
20
XDOT = 6089
883559 XDOT = 1856
196509
YDOT = -13204
584023 feet/sec YDOT = -4024
757210 meter/sec
ZDOT = -19462
641900 ZDOT = -5932
213251
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 07075
15445816
00020000 00000-0 20000-3 0 9024
2 25544 51
6325 224
6558 0015260 313
3331 46
6561 15
77667967 36083
Satellite: ISS
Catalog Number: 25544
Epoch time: 07075
15445816 = yrday
fracday
Element set: 902
Inclination: 51
6325 deg
RA of node: 224
6558 deg
Eccentricity:
0015260
Arg of perigee: 313
3331 deg
Mean anomaly: 46
6561 deg
Mean motion: 15
77667967 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3608
Checksum: 299
Coasting Arc #4 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2007/076/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4574893
71 A = 6711597
03 meter
Y = -1209755
10 meter E =
0015487
Z = 4768875
62 I = 51
41949
XDOT = 4205
047408 Wp = 344
65961
YDOT = 5938
481589 meter/sec RA = 218
69469 deg
ZDOT = -2514
682631 TA = 130
10610
MA = 129
97026
Ha = 186
388 n
mi
Hp = 178
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15009493
79 X = 4564915
46
Y = -3969012
78 feet Y = -1158651
49 meter
Z = 15645917
40 Z = 4791075
88
XDOT = 13796
087296 XDOT = 4150
545563
YDOT = 19483
207313 feet/sec YDOT = 5985
199847 meter/sec
ZDOT = -8250
271100 ZDOT = -2494
387768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9214095
99 X = -2808456
46
Y = 12390539
61 feet Y = 3776636
47 meter
Z = 15729197
71 Z = 4794259
46
XDOT = -22054
188464 XDOT = -6722
116644
YDOT = -5971
683953 feet/sec YDOT = -1820
169269 meter/sec
ZDOT = -8173
137483 ZDOT = -2491
172305
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 07076
16791058
00020000 00000-0 20000-3 0 9039
2 25544 51
6323 219
4217 0015347 317
5309 42
4668 15
77719211 36242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07076
16791058 = yrday
fracday
Element set: 903
Inclination: 51
6323 deg
RA of node: 219
4217 deg
Eccentricity:
0015347
Arg of perigee: 317
5309 deg
Mean anomaly: 42
4668 deg
Mean motion: 15
77719211 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3624
Checksum: 293
Coasting Arc #5 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2007/077/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2942378
56 A = 6716935
49 meter
Y = -5070439
06 meter E =
0012968
Z = 3262372
47 I = 51
46155
XDOT = 6074
428203 Wp = 14
85323
YDOT = -488
760368 meter/sec RA = 213
56080 deg
ZDOT = 4727
190109 TA = 23
58566
MA = 23
52625
Ha = 186
668 n
mi
Hp = 177
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9653472
96 X = -2901309
27
Y = -16635298
74 feet Y = -5103112
41 meter
Z = 10703321
74 Z = 3248178
89
XDOT = 19929
226389 XDOT = 6056
478642
YDOT = -1603
544514 feet/sec YDOT = -420
932584 meter/sec
ZDOT = 15509
153902 ZDOT = 4756
655678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18070832
57 X = 5507989
77
Y = 6672520
78 feet Y = 2033784
33 meter
Z = 10649238
34 Z = 3245887
84
XDOT = -13815
404838 XDOT = -4210
935395
YDOT = 12529
747958 feet/sec YDOT = 3819
067178 meter/sec
ZDOT = 15619
851581 ZDOT = 4760
930762
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 07077
18133772
00020000 00000-0 20000-3 0 9046
2 25544 51
6330 214
1867 0015392 321
7211 38
2860 15
77744817 36407
Satellite: ISS
Catalog Number: 25544
Epoch time: 07077
18133772 = yrday
fracday
Element set: 904
Inclination: 51
6330 deg
RA of node: 214
1867 deg
Eccentricity:
0015392
Arg of perigee: 321
7211 deg
Mean anomaly: 38
2860 deg
Mean motion: 15
77744817 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3640
Checksum: 285
Coasting Arc #6 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2007/078/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5878006
65 A = 6716734
51 meter
Y = -256354
00 meter E =
0013824
Z = -3221992
27 I = 51
48730
XDOT = -2364
845513 Wp = 342
85106
YDOT = -5584
494351 meter/sec RA = 208
33326 deg
ZDOT = 4766
447814 TA = 339
28071
MA = 339
33670
Ha = 186
683 n
mi
Hp = 177
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19284798
71 X = -5859051
47
Y = -841056
43 feet Y = -321979
55 meter
Z = -10570840
77 Z = -3250501
30
XDOT = -7758
679503 XDOT = -2325
377479
YDOT = -18321
831860 feet/sec YDOT = -5610
718156 meter/sec
ZDOT = 15637
952145 ZDOT = 4755
056001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15177853
99 X = 4626209
90
Y = -11830699
36 feet Y = -3605997
16 meter
Z = -10678052
85 Z = -3254670
51
XDOT = 16993
062842 XDOT = 5179
485554
YDOT = 7748
761023 feet/sec YDOT = 2361
822360 meter/sec
ZDOT = 15594
322489 ZDOT = 4753
149495
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 07078
13140106
00020000 00000-0 20000-3 0 9052
2 25544 51
6339 209
2795 0015462 325
3093 34
7062 15
77803066 36550
Satellite: ISS
Catalog Number: 25544
Epoch time: 07078
13140106 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 209
2795 deg
Eccentricity:
0015462
Arg of perigee: 325
3093 deg
Mean anomaly: 34
7062 deg
Mean motion: 15
77803066 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3655
Checksum: 284
Coasting Arc #7 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2007/079/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 999481
62 A = 6711176
97 meter
Y = 4587456
19 meter E =
0017359
Z = -4804864
29 I = 51
49533
XDOT = -7235
389198 Wp = 11
50291
YDOT = -992
109287 meter/sec RA = 203
20324 deg
ZDOT = -2437
046834 TA = 234
55643
MA = 234
71860
Ha = 186
981 n
mi
Hp = 177
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3279139
17 X = 971450
86
Y = 15050709
30 feet Y = 4598475
72 meter
Z = -15763990
44 Z = -4800077
39
XDOT = -23738
153538 XDOT = -7211
918828
YDOT = -3254
951728 feet/sec YDOT = -1072
888488 meter/sec
ZDOT = -7995
560478 ZDOT = -2472
139167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12482877
51 X = -3804781
07
Y = -9057716
69 feet Y = -2760792
05 meter
Z = -15745333
79 Z = -4799177
74
XDOT = 19258
664081 XDOT = 5870
040812
YDOT = -12325
752315 feet/sec YDOT = -3756
889306 meter/sec
ZDOT = -8127
631443 ZDOT = -2477
302064
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 07079
14477685
00020000 00000-0 20000-3 0 9060
2 25544 51
6346 204
0454 0015577 329
4896 30
5362 15
77858225 36718
Satellite: ISS
Catalog Number: 25544
Epoch time: 07079
14477685 = yrday
fracday
Element set: 906
Inclination: 51
6346 deg
RA of node: 204
0454 deg
Eccentricity:
0015577
Arg of perigee: 329
4896 deg
Mean anomaly: 30
5362 deg
Mean motion: 15
77858225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3671
Checksum: 320
Coasting Arc #8 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2007/080/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6521096
65 A = 6720869
10 meter
Y = 1385313
58 meter E =
0007230
Z = 878947
20 I = 51
55491
XDOT = -232
728170 Wp = 35
27987
YDOT = 4885
555853 meter/sec RA = 198
00133 deg
ZDOT = -5943
432324 TA = 135
11287
MA = 135
05439
Ha = 187
146 n
mi
Hp = 177
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21394674
06 X = 6500851
44
Y = 4544992
05 feet Y = 1458123
01 meter
Z = 2883685
03 Z = 910577
48
XDOT = -763
543866 XDOT = -258
469655
YDOT = 16028
726552 feet/sec YDOT = 4882
808939 meter/sec
ZDOT = -19499
449883 ZDOT = -5944
625850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18849431
14 X = -5745306
61
Y = 11062856
62 feet Y = 3371958
70 meter
Z = 3002801
90 Z = 915254
02
XDOT = -9520
356029 XDOT = -2901
804518
YDOT = -10901
754743 feet/sec YDOT = -3322
854846 meter/sec
ZDOT = -19503
236192 ZDOT = -5944
586391
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 07080
15812748
00020000 00000-0 20000-3 0 9077
2 25544 51
6344 198
8106 0015507 333
1810 26
8552 15
77851071 36879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07080
15812748 = yrday
fracday
Element set: 907
Inclination: 51
6344 deg
RA of node: 198
8106 deg
Eccentricity:
0015507
Arg of perigee: 333
1810 deg
Mean anomaly: 26
8552 deg
Mean motion: 15
77851071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3687
Checksum: 298
Coasting Arc #9 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2007/081/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1471025
48 A = 6708942
28 meter
Y = -3931314
73 meter E =
0015830
Z = 5237783
58 I = 51
54336
XDOT = 7399
098245 Wp = 346
88730
YDOT = 2088
995840 meter/sec RA = 192
83375 deg
ZDOT = -495
215216 TA = 107
90739
MA = 107
73472
Ha = 187
210 n
mi
Hp = 176
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4826199
07 X = 1489432
35
Y = -12898014
21 feet Y = -3914761
72 meter
Z = 17184329
33 Z = 5244974
76
XDOT = 24275
256710 XDOT = 7377
594553
YDOT = 6853
660891 feet/sec YDOT = 2171
616437 meter/sec
ZDOT = -1624
721836 ZDOT = -459
322581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5424450
91 X = 1653372
64
Y = 12622028
49 feet Y = 3847194
28 meter
Z = 17210806
82 Z = 5245853
92
XDOT = -21433
403646 XDOT = -6532
901431
YDOT = 11308
665941 feet/sec YDOT = 3446
881379 meter/sec
ZDOT = -1489
471548 ZDOT = -453
990928
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 07081
17144876
00020000 00000-0 20000-3 0 9081
2 25544 51
6345 193
5755 0015738 336
9444 23
1014 15
77948783 37031
Satellite: ISS
Catalog Number: 25544
Epoch time: 07081
17144876 = yrday
fracday
Element set: 908
Inclination: 51
6345 deg
RA of node: 193
5755 deg
Eccentricity:
0015738
Arg of perigee: 336
9444 deg
Mean anomaly: 23
1014 deg
Mean motion: 15
77948783 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3703
Checksum: 314
Coasting Arc #10 (Orbit 3718)
---------------------------------------
Vector Time (GMT): 2007/082/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6098273
06 A = 6719735
15 meter
Y = -2194922
63 meter E =
0022489
Z = 1716211
57 I = 51
60760
XDOT = 3104
429443 Wp = 20
00035
YDOT = -4153
228409 meter/sec RA = 187
68341 deg
ZDOT = 5718
258659 TA = 359
06165
MA = 359
06586
Ha = 187
531 n
mi
Hp = 176
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20007457
55 X = -6081612
95
Y = -7201189
72 feet Y = -2263023
74 meter
Z = 5630615
40 Z = 1686626
60
XDOT = 10185
135967 XDOT = 3122
862365
YDOT = -13626
077457 feet/sec YDOT = -4118
409751 meter/sec
ZDOT = 18760
691140 ZDOT = 5733
384886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19358130
22 X = 5900358
09
Y = -8869166
76 feet Y = -2703322
03 meter
Z = 5519057
54 Z = 1682208
74
XDOT = 1679
631407 XDOT = 511
951653
YDOT = 15377
655913 feet/sec YDOT = 4687
109522 meter/sec
ZDOT = 18816
981000 ZDOT = 5735
415809
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 07082
18474653
00020000 00000-0 20000-3 0 9093
2 25544 51
6341 188
3403 0015896 341
1766 18
8810 15
77950749 37196
Satellite: ISS
Catalog Number: 25544
Epoch time: 07082
18474653 = yrday
fracday
Element set: 909
Inclination: 51
6341 deg
RA of node: 188
3403 deg
Eccentricity:
0015896
Arg of perigee: 341
1766 deg
Mean anomaly: 18
8810 deg
Mean motion: 15
77950749 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3719
Checksum: 321
Coasting Arc #11 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2007/083/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3846515
54 A = 6712286
11 meter
Y = 3313481
87 meter E =
0012838
Z = -4388061
10 I = 51
61149
XDOT = -6305
215316 Wp = 21
12014
YDOT = -2919
206680 meter/sec RA = 182
47508 deg
ZDOT = 3337
515698 TA = 282
33991
MA = 282
48360
Ha = 187
518 n
mi
Hp = 175
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12619801
63 X = -3861965
10
Y = 10871003
50 feet Y = 3270381
58 meter
Z = -14396525
93 Z = -4406785
00
XDOT = -20686
401956 XDOT = -6288
316746
YDOT = -9577
449737 feet/sec YDOT = -2989
620628 meter/sec
ZDOT = 10949
854653 ZDOT = 3306
926045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1073317
82 X = 327147
27
Y = -16561014
68 feet Y = -5047797
27 meter
Z = -14466473
34 Z = -4409381
07
XDOT = 20183
914294 XDOT = 6152
057077
YDOT = -8113
863483 feet/sec YDOT = -2473
105589 meter/sec
ZDOT = 10834
405203 ZDOT = 3302
326706
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 07083
13468714
00020000 00000-0 20000-3 0 9102
2 25544 51
6337 183
4324 0015932 344
4301 15
6372 15
78006514 37349
Satellite: ISS
Catalog Number: 25544
Epoch time: 07083
13468714 = yrday
fracday
Element set: 910
Inclination: 51
6337 deg
RA of node: 183
4324 deg
Eccentricity:
0015932
Arg of perigee: 344
4301 deg
Mean anomaly: 15
6372 deg
Mean motion: 15
78006514 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3734
Checksum: 273
Coasting Arc #12 (Orbit 3749)
---------------------------------------
Vector Time (GMT): 2007/084/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4616909
43 A = 6714090
08 meter
Y = 2902276
03 meter E =
0017841
Z = -3932797
83 I = 51
64560
XDOT = -5592
267784 Wp = 10
36534
YDOT = 3437
544770 meter/sec RA = 177
35805 deg
ZDOT = -4013
822323 TA = 217
87161
MA = 217
99724
Ha = 187
729 n
mi
Hp = 175
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15147340
66 X = 4603217
35
Y = 9521902
98 feet Y = 2953828
35 meter
Z = -12902880
02 Z = -3910402
25
XDOT = -18347
335248 XDOT = -5610
792956
YDOT = 11278
034021 feet/sec YDOT = 3374
905337 meter/sec
ZDOT = -13168
708409 ZDOT = -4041
034399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17394471
72 X = -5301834
98
Y = 4440493
53 feet Y = 1353462
43 meter
Z = -12818238
93 Z = -3906999
23
XDOT = 4775
398261 XDOT = 1455
541390
YDOT = -19738
927313 feet/sec YDOT = -6016
425045 meter/sec
ZDOT = -13270
573515 ZDOT = -4044
870807
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 07084
14793212
00020000 00000-0 20000-3 0 9119
2 25544 51
6330 178
1970 0015977 348
0424 12
0360 15
78028527 37509
Satellite: ISS
Catalog Number: 25544
Epoch time: 07084
14793212 = yrday
fracday
Element set: 911
Inclination: 51
6330 deg
RA of node: 178
1970 deg
Eccentricity:
0015977
Arg of perigee: 348
0424 deg
Mean anomaly: 12
0360 deg
Mean motion: 15
78028527 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3750
Checksum: 280
Coasting Arc #13 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2007/085/02:59:32
924
Vector Time (MET): N/A
Weight (LBS) : 478706
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5696376
04 A = 6718027
23 meter
Y = -2672123
42 meter E =
0016576
Z = 2365142
83 I = 51
68876
XDOT = 4012
899798 Wp = 43
36262
YDOT = 3749
227379 meter/sec RA = 172
14580 deg
ZDOT = -5394
996577 TA = 109
99456
MA = 109
81599
Ha = 187
822 n
mi
Hp = 175
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18688897
78 X = 5714343
42
Y = -8766809
13 feet Y = -2608322
89 meter
Z = 7759654
96 Z = 2392859
20
XDOT = 13165
681752 XDOT = 3996
884811
YDOT = 12300
614759 feet/sec YDOT = 3794
012315 meter/sec
ZDOT = -17700
120003 ZDOT = -5375
541010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6188186
24 X = -1886159
17
Y = 19652359
17 feet Y = 5990039
08 meter
Z = 7863537
21 Z = 2396806
14
XDOT = -16601
127814 XDOT = -5060
023758
YDOT = 1869
656676 feet/sec YDOT = 569
871355 meter/sec
ZDOT = -17626
408664 ZDOT = -5372
529361
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 07085
16115068
00020000 00000-0 20000-3 0 9120
2 25544 51
6333 172
9611 0016104 352
5528 7
5395 15
78101589 37668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07085
16115068 = yrday
fracday
Element set: 912
Inclination: 51
6333 deg
RA of node: 172
9611 deg
Eccentricity:
0016104
Arg of perigee: 352
5528 deg
Mean anomaly: 7
5395 deg
Mean motion: 15
78101589 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3766
Checksum: 290
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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