Date:
October 20th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7620 85 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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
299/14:46:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
8
000/00:00:00
000 0
0 0
0 175
1
Coasting Arc #1 (Orbit 1259)
---------------------------------------
Vector Time (GMT): 2006/291/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1072234
18 A = 6722473
26 meter
Y = -6443223
00 meter E =
0017207
Z = -1598310
25 I = 51
33319
XDOT = 4656
390186 Wp = 82
65398
YDOT = -2182
241683 meter/sec RA = 271
84362 deg
ZDOT = 5728
280507 TA = 259
62317
MA = 259
81717
Ha = 190
077 n
mi
Hp = 174
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3517828
67 X = -992341
07
Y = -21139183
08 feet Y = -6454766
71 meter
Z = -5243800
03 Z = -1603324
80
XDOT = 15276
870688 XDOT = 4652
618928
YDOT = -7159
585573 feet/sec YDOT = -2130
192105 meter/sec
ZDOT = 18793
571217 ZDOT = 5750
892504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2015968
69 X = 614467
26
Y = 21330035
14 feet Y = 6501394
71 meter
Z = -5263372
46 Z = -1604275
93
XDOT = -14077
040656 XDOT = -4290
681992
YDOT = 5944
436909 feet/sec YDOT = 1811
864370 meter/sec
ZDOT = 18877
540640 ZDOT = 5753
874387
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 06291
41979277
00020000 00000-0 20000-3 0 9003
2 25544 51
6328 272
5626 0012894 108
9552 251
3011 15
77015876 12600
Satellite: ISS
Catalog Number: 25544
Epoch time: 06291
41979277 = yrday
fracday
Element set: 900
Inclination: 51
6328 deg
RA of node: 272
5626 deg
Eccentricity:
0012894
Arg of perigee: 108
9552 deg
Mean anomaly: 251
3011 deg
Mean motion: 15
77015876 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1260
Checksum: 295
Coasting Arc #2 (Orbit 1275)
---------------------------------------
Vector Time (GMT): 2006/292/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4131364
65 A = 6711736
48 meter
Y = 988379
97 meter E =
0026733
Z = -5218847
69 I = 51
29623
XDOT = -978
273925 Wp = 97
55321
YDOT = -7594
406084 meter/sec RA = 266
68167 deg
ZDOT = -670
249590 TA = 166
06826
MA = 165
99436
Ha = 190
009 n
mi
Hp = 174
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13554345
96 X = -4116757
13
Y = 3242716
43 feet Y = 942262
12 meter
Z = -17122203
71 Z = -5238882
79
XDOT = -3209
560121 XDOT = -890
023506
YDOT = -24916
030460 feet/sec YDOT = -7604
852294 meter/sec
ZDOT = -2198
981593 ZDOT = -674
787304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13610312
31 X = 4148423
19
Y = -2537149
65 feet Y = -773323
21 meter
Z = -17196733
25 Z = -5241564
30
XDOT = 1709
699456 XDOT = 521
116394
YDOT = 24056
285098 feet/sec YDOT = 7332
355698 meter/sec
ZDOT = -2216
940206 ZDOT = -675
723375
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 06292
43369393
00020000 00000-0 20000-3 0 9019
2 25544 51
6319 267
3306 0012696 112
5547 247
6962 15
76996379 12767
Satellite: ISS
Catalog Number: 25544
Epoch time: 06292
43369393 = yrday
fracday
Element set: 901
Inclination: 51
6319 deg
RA of node: 267
3306 deg
Eccentricity:
0012696
Arg of perigee: 112
5547 deg
Mean anomaly: 247
6962 deg
Mean motion: 15
76996379 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1276
Checksum: 328
Coasting Arc #3 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2006/293/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 628123
67 A = 6723417
88 meter
Y = 6670051
61 meter E =
0023615
Z = -456192
14 I = 51
33844
XDOT = -4842
837804 Wp = 126
57260
YDOT = 61
421213 meter/sec RA = 261
49739 deg
ZDOT = -5997
989019 TA = 58
41856
MA = 58
18824
Ha = 189
915 n
mi
Hp = 174
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2060773
19 X = 555707
69
Y = 21883371
41 feet Y = 6676670
71 meter
Z = -1496693
38 Z = -453316
93
XDOT = -15888
575472 XDOT = -4814
026891
YDOT = 201
513165 feet/sec YDOT = 7
426662 meter/sec
ZDOT = -19678
441665 ZDOT = -6021
446070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1303529
08 X = -397315
66
Y = -21942293
49 feet Y = -6688011
06 meter
Z = -1485055
52 Z = -452644
92
XDOT = 14177
061292 XDOT = 4321
168282
YDOT = 444
508943 feet/sec YDOT = 135
486326 meter/sec
ZDOT = -19765
852246 ZDOT = -6024
631764
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 06293
44756693
00020000 00000-0 20000-3 0 9025
2 25544 51
6311 262
0986 0012781 116
0577 244
1905 15
77053097 12921
Satellite: ISS
Catalog Number: 25544
Epoch time: 06293
44756693 = yrday
fracday
Element set: 902
Inclination: 51
6311 deg
RA of node: 262
0986 deg
Eccentricity:
0012781
Arg of perigee: 116
0577 deg
Mean anomaly: 244
1905 deg
Mean motion: 15
77053097 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1292
Checksum: 298
Coasting Arc #4 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2006/294/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4351276
23 A = 6712161
86 meter
Y = 855450
99 meter E =
0015435
Z = 5024841
04 I = 51
30621
XDOT = 454
571743 Wp = 102
45339
YDOT = 7520
805625 meter/sec RA = 256
29653 deg
ZDOT = -1672
995375 TA = 3
67679
MA = 3
66546
Ha = 189
622 n
mi
Hp = 174
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14275840
64 X = 4316976
63
Y = 2806597
73 feet Y = 903917
83 meter
Z = 16485698
96 Z = 5045896
75
XDOT = 1491
377110 XDOT = 378
566593
YDOT = 24674
559138 feet/sec YDOT = 7525
463854 meter/sec
ZDOT = -5488
829971 ZDOT = -1670
971982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14132637
70 X = -4307627
97
Y = -3057416
41 feet Y = -931900
52 meter
Z = 16564288
20 Z = 5048795
04
XDOT = -1306
983105 XDOT = -398
368450
YDOT = -23667
145837 feet/sec YDOT = -7213
746051 meter/sec
ZDOT = -5480
248385 ZDOT = -1670
379708
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 06294
46141015
00020000 00000-0 20000-3 0 9035
2 25544 51
6308 256
8670 0012598 120
0161 240
2255 15
77109561 13089
Satellite: ISS
Catalog Number: 25544
Epoch time: 06294
46141015 = yrday
fracday
Element set: 903
Inclination: 51
6308 deg
RA of node: 256
8670 deg
Eccentricity:
0012598
Arg of perigee: 120
0161 deg
Mean anomaly: 240
2255 deg
Mean motion: 15
77109561 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1308
Checksum: 266
Coasting Arc #5 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2006/295/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -97702
53 A = 6720586
58 meter
Y = -6265200
00 meter E =
0024060
Z = 2414940
47 I = 51
34346
XDOT = 5191
388921 Wp = 98
17698
YDOT = 1994
679142 meter/sec RA = 251
15043 deg
ZDOT = 5336
279845 TA = 289
24366
MA = 289
50381
Ha = 189
576 n
mi
Hp = 174
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -320546
35 X = -39368
63
Y = -20555118
13 feet Y = -6265966
33 meter
Z = 7923033
04 Z = 2414607
71
XDOT = 17032
115881 XDOT = 5142
774839
YDOT = 6544
222906 feet/sec YDOT = 2052
460483 meter/sec
ZDOT = 17507
479807 ZDOT = 5361
382220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 353494
04 X = 107744
98
Y = 20555389
54 feet Y = 6265282
73 meter
Z = 7920927
14 Z = 2414298
59
XDOT = -15432
844391 XDOT = -4703
930970
YDOT = -6578
702420 feet/sec YDOT = -2005
188498 meter/sec
ZDOT = 17601
309867 ZDOT = 5364
879247
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 06295
47522359
00020000 00000-0 20000-3 0 9042
2 25544 51
6309 251
6361 0012603 124
6518 235
5836 15
77188893 13248
Satellite: ISS
Catalog Number: 25544
Epoch time: 06295
47522359 = yrday
fracday
Element set: 904
Inclination: 51
6309 deg
RA of node: 251
6361 deg
Eccentricity:
0012603
Arg of perigee: 124
6518 deg
Mean anomaly: 235
5836 deg
Mean motion: 15
77188893 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1324
Checksum: 302
Coasting Arc #6 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2006/296/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4708949
06 A = 6715896
56 meter
Y = -2564059
81 meter E =
0019923
Z = -4066016
28 I = 51
33796
XDOT = 351
813347 Wp = 120
61017
YDOT = -6672
561898 meter/sec RA = 245
92105 deg
ZDOT = 3804
161631 TA = 188
69067
MA = 188
72522
Ha = 189
552 n
mi
Hp = 174
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15449307
94 X = -4660174
80
Y = -8412269
71 feet Y = -2616445
22 meter
Z = -13339948
42 Z = -4088774
58
XDOT = 1154
243264 XDOT = 407
920195
YDOT = -21891
607276 feet/sec YDOT = -6668
313978 meter/sec
ZDOT = 12480
845245 ZDOT = 3806
007151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15513572
63 X = 4728536
94
Y = 8154553
23 feet Y = 2485507
82 meter
Z = -13425123
73 Z = -4091977
71
XDOT = -125
451273 XDOT = -38
237548
YDOT = 20775
522157 feet/sec YDOT = 6332
379153 meter/sec
ZDOT = 12486
804135 ZDOT = 3805
977900
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 06296
42564981
00020000 00000-0 20000-3 0 9056
2 25544 51
6308 246
7307 0012554 127
1554 233
0759 15
77166960 13399
Satellite: ISS
Catalog Number: 25544
Epoch time: 06296
42564981 = yrday
fracday
Element set: 905
Inclination: 51
6308 deg
RA of node: 246
7307 deg
Eccentricity:
0012554
Arg of perigee: 127
1554 deg
Mean anomaly: 233
0759 deg
Mean motion: 15
77166960 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1339
Checksum: 307
Coasting Arc #7 (Orbit 1354)
---------------------------------------
Vector Time (GMT): 2006/297/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -817580
02 A = 6715641
76 meter
Y = 5261354
66 meter E =
0017657
Z = -4103032
26 I = 51
35060
XDOT = -5554
520007 Wp = 108
94336
YDOT = -3778
245600 meter/sec RA = 240
79019 deg
ZDOT = -3756
874603 TA = 122
46085
MA = 122
29002
Ha = 189
385 n
mi
Hp = 174
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2682349
15 X = -856420
03
Y = 17261662
25 feet Y = 5251994
91 meter
Z = -13461391
92 Z = -4107098
46
XDOT = -18223
490835 XDOT = -5493
607514
YDOT = -12395
818897 feet/sec YDOT = -3840
018694 meter/sec
ZDOT = -12325
704079 ZDOT = -3783
711406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2021780
33 X = 616238
64
Y = -17340230
40 feet Y = -5285302
23 meter
Z = -13475825
28 Z = -4107431
55
XDOT = 17300
154133 XDOT = 5273
086980
YDOT = 11626
180943 feet/sec YDOT = 3543
659952 meter/sec
ZDOT = -12426
252237 ZDOT = -3787
521682
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 06297
43940760
00020000 00000-0 20000-3 0 9062
2 25544 51
6310 241
4980 0012561 131
1939 229
0311 15
77230549 13553
Satellite: ISS
Catalog Number: 25544
Epoch time: 06297
43940760 = yrday
fracday
Element set: 906
Inclination: 51
6310 deg
RA of node: 241
4980 deg
Eccentricity:
0012561
Arg of perigee: 131
1939 deg
Mean anomaly: 229
0311 deg
Mean motion: 15
77230549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1355
Checksum: 277
Coasting Arc #8 (Orbit 1370)
---------------------------------------
Vector Time (GMT): 2006/298/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4937122
51 A = 6720375
65 meter
Y = 3883451
49 meter E =
0025525
Z = 2348342
22 I = 51
38217
XDOT = -1587
349098 Wp = 119
93239
YDOT = 5294
172383 meter/sec RA = 235
56358 deg
ZDOT = -5386
813031 TA = 33
43999
MA = 33
27906
Ha = 189
123 n
mi
Hp = 174
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16197908
49 X = 4881922
11
Y = 12740982
58 feet Y = 3938352
41 meter
Z = 7704534
83 Z = 2372193
53
XDOT = -5207
838247 XDOT = -1620
262346
YDOT = 17369
331965 feet/sec YDOT = 5276
237928 meter/sec
ZDOT = -17673
271098 ZDOT = -5394
604366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16784593
64 X = -5115944
14
Y = -11899415
75 feet Y = -3626941
92 meter
Z = 7793975
53 Z = 2375603
74
XDOT = 3348
914225 XDOT = 1020
749056
YDOT = -16383
817182 feet/sec YDOT = -4993
787477 meter/sec
ZDOT = -17701
589052 ZDOT = -5395
444343
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 06298
45313498
00020000 00000-0 20000-3 0 9078
2 25544 51
6309 236
2662 0012387 135
1173 225
0996 15
77289158 13713
Satellite: ISS
Catalog Number: 25544
Epoch time: 06298
45313498 = yrday
fracday
Element set: 907
Inclination: 51
6309 deg
RA of node: 236
2662 deg
Eccentricity:
0012387
Arg of perigee: 135
1173 deg
Mean anomaly: 225
0996 deg
Mean motion: 15
77289158 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1371
Checksum: 313
Coasting Arc #9 (Orbit 1386)
---------------------------------------
Vector Time (GMT): 2006/299/10:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2032460
96 A = 6711378
72 meter
Y = -3895250
86 meter E =
0017074
Z = 5065858
43 I = 51
36975
XDOT = 5693
945806 Wp = 135
79552
YDOT = 4974
368888 meter/sec RA = 230
41886 deg
ZDOT = 1525
281556 TA = 299
45586
MA = 299
62611
Ha = 188
971 n
mi
Hp = 175
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6668178
99 X = 2051257
46
Y = -12779694
43 feet Y = -3872417
92 meter
Z = 16620270
43 Z = 5075777
84
XDOT = 18680
924559 XDOT = 5630
488794
YDOT = 16320
107901 feet/sec YDOT = 5037
686861 meter/sec
ZDOT = 5004
204579 ZDOT = 1552
789594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5688997
18 X = -1734006
34
Y = 13198775
53 feet Y = 4022986
78 meter
Z = 16656717
13 Z = 5076967
38
XDOT = -18760
599395 XDOT = -5718
230696
YDOT = -14594
467978 feet/sec YDOT = -4448
393840 meter/sec
ZDOT = 5107
434982 ZDOT = 1556
746183
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 06299
46683221
00020000 00000-0 20000-3 0 9085
2 25544 51
6312 231
0349 0012319 139
6025 220
6057 15
77348882 13878
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
46683221 = yrday
fracday
Element set: 908
Inclination: 51
6312 deg
RA of node: 231
0349 deg
Eccentricity:
0012319
Arg of perigee: 139
6025 deg
Mean anomaly: 220
6057 deg
Mean motion: 15
77348882 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1387
Checksum: 295
Coasting Arc #10 (Orbit 1389)
---------------------------------------
Vector Time (GMT): 2006/299/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5072639
39 A = 6714232
76 meter
Y = 585194
53 meter E =
0017811
Z = 4341771
67 I = 51
38646
XDOT = 2126
660721 Wp = 110
17959
YDOT = 6609
801077 meter/sec RA = 229
35398 deg
ZDOT = -3370
473581 TA = 13
82241
MA = 13
77371
Ha = 188
823 n
mi
Hp = 175
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16642517
69 X = 5044626
57
Y = 1919929
55 feet Y = 641762
73 meter
Z = 14244657
72 Z = 4366347
17
XDOT = 6977
233337 XDOT = 2068
964518
YDOT = 21685
699073 feet/sec YDOT = 6633
260163 meter/sec
ZDOT = -11057
984190 ZDOT = -3360
281788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5976472
65 X = -1821628
86
Y = 15566644
97 feet Y = 4744713
39 meter
Z = 14336357
18 Z = 4369721
67
XDOT = -21619
489417 XDOT = -6589
620374
YDOT = 1863
072168 feet/sec YDOT = 567
864397 meter/sec
ZDOT = -11019
084166 ZDOT = -3358
616854
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 06299
65689710
00020000 00000-0 20000-3 0 9096
2 25544 51
6343 230
0547 0012242 139
8123 220
3949 15
77370174 13907
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
65689710 = yrday
fracday
Element set: 909
Inclination: 51
6343 deg
RA of node: 230
0547 deg
Eccentricity:
0012242
Arg of perigee: 139
8123 deg
Mean anomaly: 220
3949 deg
Mean motion: 15
77370174 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1390
Checksum: 295
Coasting Arc #11 (Orbit 1405)
---------------------------------------
Vector Time (GMT): 2006/300/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1228272
77 A = 6716368
43 meter
Y = -5407525
80 meter E =
0021961
Z = 3782747
31 I = 51
41309
XDOT = 6308
880540 Wp = 121
50077
YDOT = 1501
691963 meter/sec RA = 224
22575 deg
ZDOT = 4166
173936 TA = 284
63097
MA = 284
87436
Ha = 188
900 n
mi
Hp = 175
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4029766
29 X = -1186090
06
Y = -17741226
38 feet Y = -5421025
40 meter
Z = 12410588
29 Z = 3776882
38
XDOT = 20698
426969 XDOT = 6271
380576
YDOT = 4926
810901 feet/sec YDOT = 1572
031440 meter/sec
ZDOT = 13668
549658 ZDOT = 4196
732123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18208094
10 X = 5549827
08
Y = 126836
57 feet Y = 38659
79 meter
Z = 12387980
19 Z = 3775856
36
XDOT = -9564
625166 XDOT = -2915
297751
YDOT = 17590
647015 feet/sec YDOT = 5361
629210 meter/sec
ZDOT = 13782
691488 ZDOT = 4200
964365
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 06300
67056027
00020000 00000-0 20000-3 0 9102
2 25544 51
6343 224
8221 0012276 143
7246 216
4754 15
77376231 14062
Satellite: ISS
Catalog Number: 25544
Epoch time: 06300
67056027 = yrday
fracday
Element set: 910
Inclination: 51
6343 deg
RA of node: 224
8221 deg
Eccentricity:
0012276
Arg of perigee: 143
7246 deg
Mean anomaly: 216
4754 deg
Mean motion: 15
77376231 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1406
Checksum: 266
Coasting Arc #12 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2006/301/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5838965
49 A = 6719111
01 meter
Y = -1934258
41 meter E =
0013094
Z = -2724218
33 I = 51
44427
XDOT = -511
373807 Wp = 126
97048
YDOT = -5693
592677 meter/sec RA = 218
99892 deg
ZDOT = 5147
904382 TA = 201
84212
MA = 201
89800
Ha = 188
653 n
mi
Hp = 175
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19156710
92 X = -5803668
40
Y = -6345992
16 feet Y = -1999355
46 meter
Z = -8937724
18 Z = -2752498
86
XDOT = -1677
735586 XDOT = -472
677255
YDOT = -18679
766000 feet/sec YDOT = -5699
095059 meter/sec
ZDOT = 16889
450071 ZDOT = 5145
513772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10307064
18 X = 3141593
16
Y = -17294930
28 feet Y = -5271494
75 meter
Z = -9043446
14 Z = -2756442
38
XDOT = 17362
467204 XDOT = 5292
080004
YDOT = 1536
671735 feet/sec YDOT = 468
377545 meter/sec
ZDOT = 16879
752804 ZDOT = 5144
948655
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 06301
62084136
00020000 00000-0 20000-3 0 9111
2 25544 51
6341 219
9163 0012140 148
0298 212
1606 15
77431350 14215
Satellite: ISS
Catalog Number: 25544
Epoch time: 06301
62084136 = yrday
fracday
Element set: 911
Inclination: 51
6341 deg
RA of node: 219
9163 deg
Eccentricity:
0012140
Arg of perigee: 148
0298 deg
Mean anomaly: 212
1606 deg
Mean motion: 15
77431350 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1421
Checksum: 248
Coasting Arc #13 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2006/302/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -468350
08 A = 6711402
12 meter
Y = 4477151
95 meter E =
0019799
Z = -4991401
23 I = 51
44100
XDOT = -6906
137783 Wp = 112
32832
YDOT = -2817
336709 meter/sec RA = 213
86118 deg
ZDOT = -1892
430085 TA = 139
41492
MA = 139
26715
Ha = 188
438 n
mi
Hp = 175
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1536581
61 X = -494131
76
Y = 14688818
73 feet Y = 4471770
64 meter
Z = -16375988
29 Z = -4993738
95
XDOT = -22657
932359 XDOT = -6864
927448
YDOT = -9243
230671 feet/sec YDOT = -2894
334478 meter/sec
ZDOT = -6208
760123 ZDOT = -1925
880553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14110698
02 X = -4300940
76
Y = -4329590
83 feet Y = -1319659
29 meter
Z = -16384087
27 Z = -4993869
80
XDOT = 13229
194793 XDOT = 4032
258573
YDOT = -19312
736936 feet/sec YDOT = -5886
522218 meter/sec
ZDOT = -6333
897502 ZDOT = -1930
571959
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 06302
63444695
00020000 00000-0 20000-3 0 9124
2 25544 51
6336 214
6828 0012076 152
2726 207
9086 15
77488845 14372
Satellite: ISS
Catalog Number: 25544
Epoch time: 06302
63444695 = yrday
fracday
Element set: 912
Inclination: 51
6336 deg
RA of node: 214
6828 deg
Eccentricity:
0012076
Arg of perigee: 152
2726 deg
Mean anomaly: 207
9086 deg
Mean motion: 15
77488845 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1437
Checksum: 308
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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