Date:
December 22nd 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2256)
---------------------------------------
Vector Time (GMT): 2006/354/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5006459
25 A = 6717589
39 meter
Y = -927253
85 meter E =
0021845
Z = 4363984
41 I = 51
37013
XDOT = -1647
388843 Wp = 19
28500
YDOT = 6757
619195 meter/sec RA = 306
27608 deg
ZDOT = 3341
378978 TA = 37
12773
MA = 36
97683
Ha = 193
560 n
mi
Hp = 175
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16425391
25 X = 4995256
34
Y = -3042171
44 feet Y = -871332
32 meter
Z = 14317534
16 Z = 4388278
48
XDOT = -5404
819040 XDOT = -1739
062915
YDOT = 22170
666650 feet/sec YDOT = 6738
683965 meter/sec
ZDOT = 10962
529457 ZDOT = 3333
154551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5625593
68 X = 1714680
95
Y = 15645879
36 feet Y = 4768864
03 meter
Z = 14408303
99 Z = 4391651
06
XDOT = -21619
397116 XDOT = -6589
592241
YDOT = -2247
498620 feet/sec YDOT = -685
037579 meter/sec
ZDOT = 10932
528221 ZDOT = 3332
234602
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 06354
58402864
00020000 00000-0 20000-3 0 9004
2 25544 51
6347 306
5574 0023937 356
8370 3
2639 15
76160268 22575
Satellite: ISS
Catalog Number: 25544
Epoch time: 06354
58402864 = yrday
fracday
Element set: 900
Inclination: 51
6347 deg
RA of node: 306
5574 deg
Eccentricity:
0023937
Arg of perigee: 356
8370 deg
Mean anomaly: 3
2639 deg
Mean motion: 15
76160268 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2257
Checksum: 301
Coasting Arc #2 (Orbit 2271)
---------------------------------------
Vector Time (GMT): 2006/355/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1543547
52 A = 6723760
37 meter
Y = -6112256
55 meter E =
0028628
Z = -2291967
21 I = 51
37467
XDOT = 5449
894436 Wp = 8
44146
YDOT = -644
865006 meter/sec RA = 301
06027 deg
ZDOT = 5426
445900 TA = 325
62307
MA = 325
80797
Ha = 193
864 n
mi
Hp = 175
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5064132
28 X = 1622914
84
Y = -20053335
13 feet Y = -6094551
55 meter
Z = -7519577
46 Z = -2284277
04
XDOT = 17880
231089 XDOT = 5430
339746
YDOT = -2115
698839 feet/sec YDOT = -584
031615 meter/sec
ZDOT = 17803
300196 ZDOT = 5452
873798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20640997
63 X = 6291376
08
Y = 1467080
38 feet Y = 447166
10 meter
Z = -7491503
36 Z = -2283410
22
XDOT = 5343
784883 XDOT = 1628
785632
YDOT = 15618
716264 feet/sec YDOT = 4760
584717 meter/sec
ZDOT = 17902
092336 ZDOT = 5456
557744
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 06355
53507177
00020000 00000-0 20000-3 0 9014
2 25544 51
6344 301
6573 0024082
5129 359
6055 15
76158446 22726
Satellite: ISS
Catalog Number: 25544
Epoch time: 06355
53507177 = yrday
fracday
Element set: 901
Inclination: 51
6344 deg
RA of node: 301
6573 deg
Eccentricity:
0024082
Arg of perigee:
5129 deg
Mean anomaly: 359
6055 deg
Mean motion: 15
76158446 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2272
Checksum: 282
Coasting Arc #3 (Orbit 2287)
---------------------------------------
Vector Time (GMT): 2006/356/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4498633
66 A = 6714835
89 meter
Y = 94741
89 meter E =
0030847
Z = -5004335
35 I = 51
33246
XDOT = 1894
552814 Wp = 28
58107
YDOT = -7225
205666 meter/sec RA = 295
92297 deg
ZDOT = -1817
822244 TA = 223
66741
MA = 223
91189
Ha = 193
854 n
mi
Hp = 174
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14759296
79 X = -4475048
77
Y = 310832
97 feet Y = 44568
41 meter
Z = -16418423
05 Z = -5026132
23
XDOT = 6215
724456 XDOT = 1984
035853
YDOT = -23704
742998 feet/sec YDOT = -7203
519084 meter/sec
ZDOT = -5963
983741 ZDOT = -1808
402481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3155176
73 X = -961697
87
Y = -14328092
56 feet Y = -4367202
61 meter
Z = -16499960
54 Z = -5029187
97
XDOT = 23422
267142 XDOT = 7139
107025
YDOT = 1753
549511 feet/sec YDOT = 534
481891 meter/sec
ZDOT = -5929
570693 ZDOT = -1807
333147
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 06356
54948402
00020000 00000-0 20000-3 0 9027
2 25544 51
6351 296
4302 0023972 4
5997 355
5383 15
76240366 22888
Satellite: ISS
Catalog Number: 25544
Epoch time: 06356
54948402 = yrday
fracday
Element set: 902
Inclination: 51
6351 deg
RA of node: 296
4302 deg
Eccentricity:
0023972
Arg of perigee: 4
5997 deg
Mean anomaly: 355
5383 deg
Mean motion: 15
76240366 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2288
Checksum: 307
Coasting Arc #4 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2006/357/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1743334
68 A = 6725396
73 meter
Y = 6453189
19 meter E =
0021201
Z = 817034
37 I = 51
35741
XDOT = -4861
848569 Wp = 42
47721
YDOT = -549
243351 meter/sec RA = 290
72564 deg
ZDOT = -5930
642703 TA = 128
58661
MA = 128
39651
Ha = 193
946 n
mi
Hp = 174
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5719601
98 X = -1819334
55
Y = 21171880
54 feet Y = 6433269
19 meter
Z = 2680558
95 Z = 808381
72
XDOT = -15950
946749 XDOT = -4826
535853
YDOT = -1801
979499 feet/sec YDOT = -603
412906 meter/sec
ZDOT = -19457
489184 ZDOT = -5954
175608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21905338
21 X = -6676747
09
Y = -1134493
03 feet Y = -345793
48 meter
Z = 2648934
17 Z = 807395
13
XDOT = -1666
809856 XDOT = -508
043644
YDOT = -14268
758774 feet/sec YDOT = -4349
117674 meter/sec
ZDOT = -19545
603091 ZDOT = -5957
499822
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 06357
56386272
00020000 00000-0 20000-3 0 9032
2 25544 51
6352 291
2027 0023903 8
4598 351
6964 15
76281935 23048
Satellite: ISS
Catalog Number: 25544
Epoch time: 06357
56386272 = yrday
fracday
Element set: 903
Inclination: 51
6352 deg
RA of node: 291
2027 deg
Eccentricity:
0023903
Arg of perigee: 8
4598 deg
Mean anomaly: 351
6964 deg
Mean motion: 15
76281935 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2304
Checksum: 302
Coasting Arc #5 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2006/358/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4048310
14 A = 6713334
98 meter
Y = 1094663
17 meter E =
0024362
Z = 5235990
41 I = 51
30825
XDOT = -2035
812105 Wp = 17
14335
YDOT = 7437
434166 meter/sec RA = 285
55867 deg
ZDOT = 42
069219 TA = 72
58925
MA = 72
32302
Ha = 193
800 n
mi
Hp = 174
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13281857
43 X = 4010333
41
Y = 3591414
59 feet Y = 1139720
64 meter
Z = 17178446
23 Z = 5255564
75
XDOT = -6679
173572 XDOT = -2119
031597
YDOT = 24401
030727 feet/sec YDOT = 7414
203275 meter/sec
ZDOT = 138
022372 ZDOT = 31
978141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -491074
01 X = -149679
36
Y = 13657914
02 feet Y = 4162932
19 meter
Z = 17251818
49 Z = 5258354
28
XDOT = -24285
327334 XDOT = -7402
167771
YDOT = -906
239248 feet/sec YDOT = -276
221723 meter/sec
ZDOT = 101
139555 ZDOT = 30
827336
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 06358
57820632
00020000 00000-0 20000-3 0 9048
2 25544 51
6347 285
9752 0023812 11
9522 348
2202 15
76373913 23205
Satellite: ISS
Catalog Number: 25544
Epoch time: 06358
57820632 = yrday
fracday
Element set: 904
Inclination: 51
6347 deg
RA of node: 285
9752 deg
Eccentricity:
0023812
Arg of perigee: 11
9522 deg
Mean anomaly: 348
2202 deg
Mean motion: 15
76373913 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2320
Checksum: 285
Coasting Arc #6 (Orbit 2335)
---------------------------------------
Vector Time (GMT): 2006/359/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1776788
39 A = 6725236
76 meter
Y = -6420890
92 meter E =
0035601
Z = 737202
57 I = 51
34181
XDOT = 4499
968774 Wp = 28
98020
YDOT = 1940
934942 meter/sec RA = 280
38944 deg
ZDOT = 5970
613701 TA = 339
11650
MA = 339
26156
Ha = 194
003 n
mi
Hp = 174
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5829358
22 X = 1844874
48
Y = -21065915
08 feet Y = -6400641
26 meter
Z = 2418643
60 Z = 745998
87
XDOT = 14763
677079 XDOT = 4448
926665
YDOT = 6367
896790 feet/sec YDOT = 1990
970124 meter/sec
ZDOT = 19588
627627 ZDOT = 5992
350529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21848619
27 X = 6659459
15
Y = 485264
65 feet Y = 147908
66 meter
Z = 2450793
05 Z = 747001
72
XDOT = -2553
512404 XDOT = -778
310581
YDOT = 14174
193621 feet/sec YDOT = 4320
294216 meter/sec
ZDOT = 19670
197533 ZDOT = 5995
476208
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 06359
59252061
00020000 00000-0 20000-3 0 9057
2 25544 51
6347 280
7472 0023893 16
1128 344
0791 15
76366188 23365
Satellite: ISS
Catalog Number: 25544
Epoch time: 06359
59252061 = yrday
fracday
Element set: 905
Inclination: 51
6347 deg
RA of node: 280
7472 deg
Eccentricity:
0023893
Arg of perigee: 16
1128 deg
Mean anomaly: 344
0791 deg
Mean motion: 15
76366188 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2336
Checksum: 304
Coasting Arc #7 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2006/360/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3829280
13 A = 6714191
08 meter
Y = -2309682
66 meter E =
0028585
Z = -5021261
06 I = 51
30182
XDOT = 2068
811223 Wp = 47
48785
YDOT = -7198
697566 meter/sec RA = 275
19043 deg
ZDOT = 1758
945182 TA = 239
40444
MA = 239
68670
Ha = 193
965 n
mi
Hp = 173
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12563255
03 X = -3778776
12
Y = -7577699
02 feet Y = -2352221
02 meter
Z = -16473953
62 Z = -5039741
10
XDOT = 6787
438397 XDOT = 2140
609735
YDOT = -23617
774166 feet/sec YDOT = -7175
161663 meter/sec
ZDOT = 5770
817527 ZDOT = 1769
169226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4055525
24 X = 1236124
09
Y = -14018457
64 feet Y = -4272825
89 meter
Z = -16543385
62 Z = -5042423
94
XDOT = 23540
199322 XDOT = 7175
052753
YDOT = 53
682500 feet/sec YDOT = 16
362426 meter/sec
ZDOT = 5808
209071 ZDOT = 1770
342125
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 06360
54340720
00020000 00000-0 20000-3 0 9065
2 25544 51
6351 275
8459 0023768 19
6802 340
5274 15
76434178 23517
Satellite: ISS
Catalog Number: 25544
Epoch time: 06360
54340720 = yrday
fracday
Element set: 906
Inclination: 51
6351 deg
RA of node: 275
8459 deg
Eccentricity:
0023768
Arg of perigee: 19
6802 deg
Mean anomaly: 340
5274 deg
Mean motion: 15
76434178 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2351
Checksum: 294
Coasting Arc #8 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2006/361/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1875747
33 A = 6722738
40 meter
Y = 6034049
62 meter E =
0022203
Z = -2337591
10 I = 51
32999
XDOT = -4298
796738 Wp = 37
23007
YDOT = -3415
033630 meter/sec RA = 270
04739 deg
ZDOT = -5375
063256 TA = 169
15399
MA = 169
10603
Ha = 194
027 n
mi
Hp = 173
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6154026
66 X = -1931725
94
Y = 19796750
73 feet Y = 6012761
16 meter
Z = -7669262
14 Z = -2346838
98
XDOT = -14103
663838 XDOT = -4234
178817
YDOT = -11204
178576 feet/sec YDOT = -3462
743459 meter/sec
ZDOT = -17634
721969 ZDOT = -5395
790079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20715350
39 X = -6314038
80
Y = -369998
75 feet Y = -112775
62 meter
Z = -7703137
30 Z = -2347916
25
XDOT = 6844
250062 XDOT = 2086
127419
YDOT = -15056
755225 feet/sec YDOT = -4589
298992 meter/sec
ZDOT = -17712
699465 ZDOT = -5398
830797
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 06361
55765575
00020000 00000-0 20000-3 0 9077
2 25544 51
6352 270
6168 0023635 23
4708 336
7530 15
76474639 23674
Satellite: ISS
Catalog Number: 25544
Epoch time: 06361
55765575 = yrday
fracday
Element set: 907
Inclination: 51
6352 deg
RA of node: 270
6168 deg
Eccentricity:
0023635
Arg of perigee: 23
4708 deg
Mean anomaly: 336
7530 deg
Mean motion: 15
76474639 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2367
Checksum: 313
Coasting Arc #9 (Orbit 2382)
---------------------------------------
Vector Time (GMT): 2006/362/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3739539
54 A = 6716995
28 meter
Y = 3621084
11 meter E =
0031478
Z = 4242710
04 I = 51
31224
XDOT = -2240
721890 Wp = 40
02985
YDOT = 6479
318085 meter/sec RA = 264
82328 deg
ZDOT = -3516
728405 TA = 85
93319
MA = 85
57345
Ha = 193
986 n
mi
Hp = 173
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12268830
52 X = 3678159
77
Y = 11880197
23 feet Y = 3662558
16 meter
Z = 13919652
35 Z = 4260728
00
XDOT = -7351
449771 XDOT = -2295
924328
YDOT = 21257
605267 feet/sec YDOT = 6453
952745 meter/sec
ZDOT = -11537
822851 ZDOT = -3527
747378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7765330
62 X = -2366872
77
Y = 15148230
89 feet Y = 4617180
77 meter
Z = 13987521
27 Z = 4263396
48
XDOT = -21356
319083 XDOT = -6509
406056
YDOT = -141
217724 feet/sec YDOT = -43
043162 meter/sec
ZDOT = -11578
270923 ZDOT = -3529
056977
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 06362
57187180
00020000 00000-0 20000-3 0 9081
2 25544 51
6349 265
3878 0023718 27
2491 332
9912 15
76555107 23832
Satellite: ISS
Catalog Number: 25544
Epoch time: 06362
57187180 = yrday
fracday
Element set: 908
Inclination: 51
6349 deg
RA of node: 265
3878 deg
Eccentricity:
0023718
Arg of perigee: 27
2491 deg
Mean anomaly: 332
9912 deg
Mean motion: 15
76555107 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2383
Checksum: 315
Coasting Arc #10 (Orbit 2398)
---------------------------------------
Vector Time (GMT): 2006/363/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2070962
67 A = 6718823
34 meter
Y = -5183078
07 meter E =
0030471
Z = 3703572
59 I = 51
32294
XDOT = 4331
448219 Wp = 51
55696
YDOT = 4775
624894 meter/sec RA = 259
69573 deg
ZDOT = 4256
556011 TA = 353
53371
MA = 353
57294
Ha = 194
016 n
mi
Hp = 172
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6794496
94 X = 2110775
28
Y = -17004849
31 feet Y = -5159697
22 meter
Z = 12150828
69 Z = 3713729
50
XDOT = 14210
788120 XDOT = 4257
046899
YDOT = 15668
060675 feet/sec YDOT = 4823
645082 meter/sec
ZDOT = 13965
078777 ZDOT = 4277
418111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18253447
92 X = 5563650
93
Y = 1109905
84 feet Y = 338299
30 meter
Z = 12188210
49 Z = 3714966
56
XDOT = -10419
669366 XDOT = -3175
915223
YDOT = 16971
091488 feet/sec YDOT = 5172
788686 meter/sec
ZDOT = 14043
735480 ZDOT = 4280
530574
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 06363
58605743
00020000 00000-0 20000-3 0 9094
2 25544 51
6354 260
1587 0023676 31
2214 329
0351 15
76570307 23999
Satellite: ISS
Catalog Number: 25544
Epoch time: 06363
58605743 = yrday
fracday
Element set: 909
Inclination: 51
6354 deg
RA of node: 260
1587 deg
Eccentricity:
0023676
Arg of perigee: 31
2214 deg
Mean anomaly: 329
0351 deg
Mean motion: 15
76570307 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2399
Checksum: 295
Coasting Arc #11 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2006/364/12:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3814319
05 A = 6720588
70 meter
Y = -4610347
17 meter E =
0027191
Z = -3050007
69 I = 51
33607
XDOT = 2584
736106 Wp = 40
58026
YDOT = -5353
213174 meter/sec RA = 254
46679 deg
ZDOT = 4904
156162 TA = 283
85638
MA = 284
15876
Ha = 193
968 n
mi
Hp = 172
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12514170
11 X = -3747665
55
Y = -15125810
93 feet Y = -4652627
90 meter
Z = -10006586
91 Z = -3068376
49
XDOT = 8480
105334 XDOT = 2620
580763
YDOT = -17563
035349 feet/sec YDOT = -5324
109488 meter/sec
ZDOT = 16089
751187 ZDOT = 4916
799194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10219506
68 X = 3114905
64
Y = -16720178
89 feet Y = -5096310
53 meter
Z = -10075896
61 Z = -3071133
29
XDOT = 18122
208753 XDOT = 5523
649228
YDOT = 1440
232472 feet/sec YDOT = 438
982858 meter/sec
ZDOT = 16136
421145 ZDOT = 4918
381165
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 06364
53682648
00020000 00000-0 20000-3 0 9101
2 25544 51
6355 255
2567 0023570 34
3380 325
9302 15
76624257 24147
Satellite: ISS
Catalog Number: 25544
Epoch time: 06364
53682648 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 255
2567 deg
Eccentricity:
0023570
Arg of perigee: 34
3380 deg
Mean anomaly: 325
9302 deg
Mean motion: 15
76624257 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2414
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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