Date:
November 4th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6673 62 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
There are no maneuvers
Coasting Arc #1 (Orbit 1514)
---------------------------------------
Vector Time (GMT): 2006/307/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6586752
88 A = 6721288
69 meter
Y = -40187
03 meter E =
0023765
Z = 1261032
44 I = 51
60655
XDOT = 1160
797210 Wp = 143
87298
YDOT = 4873
312410 meter/sec RA = 188
37605 deg
ZDOT = -5871
042133 TA = 22
24591
MA = 22
14298
Ha = 187
843 n
mi
Hp = 176
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21610081
64 X = 6580586
67
Y = -131847
20 feet Y = 33435
25 meter
Z = 4137245
55 Z = 1293016
81
XDOT = 3808
389796 XDOT = 1134
738145
YDOT = 15988
557774 feet/sec YDOT = 4886
147250 meter/sec
ZDOT = -19261
949256 ZDOT = -5865
466233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11671671
57 X = -3557525
50
Y = 18159945
36 feet Y = 5535151
35 meter
Z = 4256557
29 Z = 1297398
66
XDOT = -14209
618104 XDOT = -4331
091598
YDOT = -4595
372091 feet/sec YDOT = -1400
669413 meter/sec
ZDOT = -19240
463609 ZDOT = -5864
493308
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 06307
57589314
00020000 00000-0 20000-3 0 9007
2 25544 51
6350 189
1879 0012137 170
0893 190
0513 15
77579121 15153
Satellite: ISS
Catalog Number: 25544
Epoch time: 06307
57589314 = yrday
fracday
Element set: 900
Inclination: 51
6350 deg
RA of node: 189
1879 deg
Eccentricity:
0012137
Arg of perigee: 170
0893 deg
Mean anomaly: 190
0513 deg
Mean motion: 15
77579121 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1515
Checksum: 292
Coasting Arc #2 (Orbit 1530)
---------------------------------------
Vector Time (GMT): 2006/308/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 139984
00 A = 6709724
51 meter
Y = -4165039
50 meter E =
0012675
Z = 5255811
78 I = 51
59587
XDOT = 7700
727671 Wp = 164
17862
YDOT = 371
992243 meter/sec RA = 183
22302 deg
ZDOT = 77
646395 TA = 285
01493
MA = 285
15518
Ha = 187
616 n
mi
Hp = 176
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 459265
08 X = 161015
02
Y = -13664827
75 feet Y = -4163356
54 meter
Z = 17243476
96 Z = 5256542
92
XDOT = 25264
854565 XDOT = 7695
618458
YDOT = 1220
446992 feet/sec YDOT = 458
077485 meter/sec
ZDOT = 254
745389 ZDOT = 115
045349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11383286
58 X = 3469625
75
Y = 7568698
59 feet Y = 2306939
33 meter
Z = 17245623
43 Z = 5256466
02
XDOT = -13904
494710 XDOT = -4238
089988
YDOT = 19923
806375 feet/sec YDOT = 6072
776183 meter/sec
ZDOT = 394
321875 ZDOT = 120
189308
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 06308
58938482
00020000 00000-0 20000-3 0 9014
2 25544 51
6343 183
9541 0011967 174
6056 185
5240 15
77647664 15316
Satellite: ISS
Catalog Number: 25544
Epoch time: 06308
58938482 = yrday
fracday
Element set: 901
Inclination: 51
6343 deg
RA of node: 183
9541 deg
Eccentricity:
0011967
Arg of perigee: 174
6056 deg
Mean anomaly: 185
5240 deg
Mean motion: 15
77647664 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1531
Checksum: 312
Coasting Arc #3 (Orbit 1546)
---------------------------------------
Vector Time (GMT): 2006/309/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6586545
64 A = 6721089
30 meter
Y = -690413
61 meter E =
0012654
Z = 1153340
90 I = 51
66201
XDOT = 1535
546211 Wp = 110
95745
YDOT = -4713
563126 meter/sec RA = 178
06782 deg
ZDOT = 5891
421095 TA = 261
67737
MA = 261
82087
Ha = 187
361 n
mi
Hp = 176
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21609401
72 X = -6583938
73
Y = -2265136
50 feet Y = -764053
48 meter
Z = 3783926
83 Z = 1121348
66
XDOT = 5037
881271 XDOT = 1559
519358
YDOT = -15464
445950 feet/sec YDOT = -4696
257972 meter/sec
ZDOT = 19328
809367 ZDOT = 5898
939096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13114705
70 X = 3997362
30
Y = -17349102
49 feet Y = -5288006
44 meter
Z = 3664467
99 Z = 1116929
84
XDOT = 9427
922397 XDOT = 2873
630747
YDOT = 11255
472694 feet/sec YDOT = 3430
668077 meter/sec
ZDOT = 19356
207549 ZDOT = 5899
772061
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 06309
60285190
00020000 00000-0 20000-3 0 9020
2 25544 51
6330 178
7194 0011973 179
2499 180
8686 15
77713628 15470
Satellite: ISS
Catalog Number: 25544
Epoch time: 06309
60285190 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 178
7194 deg
Eccentricity:
0011973
Arg of perigee: 179
2499 deg
Mean anomaly: 180
8686 deg
Mean motion: 15
77713628 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1547
Checksum: 322
Coasting Arc #4 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2006/310/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2505596
71 A = 6711822
41 meter
Y = 4076904
19 meter E =
0018577
Z = -4721592
53 I = 51
65811
XDOT = -7103
002235 Wp = 147
06840
YDOT = -1248
640904 meter/sec RA = 172
87223 deg
ZDOT = 2680
795189 TA = 149
36039
MA = 149
25177
Ha = 187
157 n
mi
Hp = 176
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8220461
64 X = -2528061
60
Y = 13375669
90 feet Y = 4048759
94 meter
Z = -15490789
16 Z = -4733819
41
XDOT = -23303
813107 XDOT = -7101
535086
YDOT = -4096
590892 feet/sec YDOT = -1328
062597 meter/sec
ZDOT = 8795
259807 ZDOT = 2646
291153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7486987
18 X = -2282033
69
Y = -13748866
21 feet Y = -4190654
42 meter
Z = -15535854
80 Z = -4735328
54
XDOT = 14260
140332 XDOT = 4346
490773
YDOT = -17596
536721 feet/sec YDOT = -5363
424393 meter/sec
ZDOT = 8666
340158 ZDOT = 2641
500480
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 06310
55295732
00020000 00000-0 20000-3 0 9030
2 25544 51
6316 173
8113 0011892 182
9236 177
1861 15
77728977 15625
Satellite: ISS
Catalog Number: 25544
Epoch time: 06310
55295732 = yrday
fracday
Element set: 903
Inclination: 51
6316 deg
RA of node: 173
8113 deg
Eccentricity:
0011892
Arg of perigee: 182
9236 deg
Mean anomaly: 177
1861 deg
Mean motion: 15
77728977 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1562
Checksum: 307
Coasting Arc #5 (Orbit 1577)
---------------------------------------
Vector Time (GMT): 2006/311/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5580796
12 A = 6716554
56 meter
Y = 1535170
96 meter E =
0012279
Z = -3398216
89 I = 51
70122
XDOT = -4079
645138 Wp = 164
28148
YDOT = 4623
837747 meter/sec RA = 167
75787 deg
ZDOT = -4626
501766 TA = 55
89435
MA = 55
77790
Ha = 187
057 n
mi
Hp = 176
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18309698
55 X = 5579723
23
Y = 5036650
13 feet Y = 1597572
83 meter
Z = -11149005
53 Z = -3371107
08
XDOT = -13384
662525 XDOT = -4108
570989
YDOT = 15170
071348 feet/sec YDOT = 4578
055592 meter/sec
ZDOT = -15178
811569 ZDOT = -4646
391069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13344240
64 X = -4067324
55
Y = 13593911
16 feet Y = 4143424
12 meter
Z = -11047626
51 Z = -3367316
56
XDOT = -5783
171546 XDOT = -1762
710687
YDOT = -18030
799865 feet/sec YDOT = -5495
787799 meter/sec
ZDOT = -15252
409061 ZDOT = -4648
934282
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 06311
56637866
00020000 00000-0 20000-3 0 9041
2 25544 51
6306 168
5775 0011854 187
1314 172
9684 15
77753478 15788
Satellite: ISS
Catalog Number: 25544
Epoch time: 06311
56637866 = yrday
fracday
Element set: 904
Inclination: 51
6306 deg
RA of node: 168
5775 deg
Eccentricity:
0011854
Arg of perigee: 187
1314 deg
Mean anomaly: 172
9684 deg
Mean motion: 15
77753478 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1578
Checksum: 331
Coasting Arc #6 (Orbit 1593)
---------------------------------------
Vector Time (GMT): 2006/312/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4431665
36 A = 6717004
69 meter
Y = -3960961
28 meter E =
0016393
Z = 3105127
29 I = 51
73180
XDOT = 5499
159654 Wp = 139
95899
YDOT = 2316
300940 meter/sec RA = 162
54735 deg
ZDOT = -4891
875460 TA = 3
90073
MA = 3
88796
Ha = 186
597 n
mi
Hp = 177
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14539584
51 X = 4460543
53
Y = -12995279
78 feet Y = -3911242
79 meter
Z = 10187425
50 Z = 3126726
54
XDOT = 18041
862382 XDOT = 5496
614112
YDOT = 7599
412532 feet/sec YDOT = 2377
781864 meter/sec
ZDOT = -16049
460172 ZDOT = -4865
165894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4624887
62 X = 1409665
75
Y = 18901035
20 feet Y = 5761035
53 meter
Z = 10267508
73 Z = 3129536
66
XDOT = -13876
191784 XDOT = -4229
463256
YDOT = 12062
779883 feet/sec YDOT = 3676
735308 meter/sec
ZDOT = -15949
456960 ZDOT = -4861
394481
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 06312
57977430
00020000 00000-0 20000-3 0 9058
2 25544 51
6311 163
3423 0011752 191
8515 168
2375 15
77833614 15943
Satellite: ISS
Catalog Number: 25544
Epoch time: 06312
57977430 = yrday
fracday
Element set: 905
Inclination: 51
6311 deg
RA of node: 163
3423 deg
Eccentricity:
0011752
Arg of perigee: 191
8515 deg
Mean anomaly: 168
2375 deg
Mean motion: 15
77833614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1594
Checksum: 293
Coasting Arc #7 (Orbit 1609)
---------------------------------------
Vector Time (GMT): 2006/313/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3830669
70 A = 6711110
47 meter
Y = -2572595
19 meter E =
0015178
Z = 4875993
27 I = 51
73687
XDOT = 5892
113061 Wp = 169
82645
YDOT = -4404
282602 meter/sec RA = 157
43191 deg
ZDOT = 2289
489923 TA = 257
84920
MA = 258
01927
Ha = 186
660 n
mi
Hp = 177
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12567813
96 X = -3825304
96
Y = -8440272
93 feet Y = -2615402
36 meter
Z = 15997353
23 Z = 4857396
33
XDOT = 19331
079598 XDOT = 5929
802335
YDOT = -14449
746071 feet/sec YDOT = -4338
183226 meter/sec
ZDOT = 7511
449879 ZDOT = 2318
205394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13287662
70 X = 4050079
59
Y = -7406312
34 feet Y = -2257444
00 meter
Z = 15927586
85 Z = 4854728
47
XDOT = 3508
894291 XDOT = 1069
510980
YDOT = 22789
811294 feet/sec YDOT = 6946
334482 meter/sec
ZDOT = 7618
050593 ZDOT = 2321
981821
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 06313
59314979
00020000 00000-0 20000-3 0 9065
2 25544 51
6299 158
1067 0011742 194
8551 165
2270 15
77795088 16108
Satellite: ISS
Catalog Number: 25544
Epoch time: 06313
59314979 = yrday
fracday
Element set: 906
Inclination: 51
6299 deg
RA of node: 158
1067 deg
Eccentricity:
0011742
Arg of perigee: 194
8551 deg
Mean anomaly: 165
2270 deg
Mean motion: 15
77795088 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1610
Checksum: 315
Coasting Arc #8 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2006/314/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5617291
63 A = 6720925
54 meter
Y = 3618458
51 meter E =
0004251
Z = -745409
66 I = 51
79629
XDOT = -3154
483181 Wp = 138
33300
YDOT = -3666
587190 meter/sec RA = 152
24879 deg
ZDOT = 5989
222102 TA = 213
55618
MA = 213
58311
Ha = 186
372 n
mi
Hp = 177
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18429434
50 X = -5653715
14
Y = 11871583
02 feet Y = 3555439
25 meter
Z = -2445569
75 Z = -772786
96
XDOT = -10349
354267 XDOT = -3142
343363
YDOT = -12029
485533 feet/sec YDOT = -3701
795019 meter/sec
ZDOT = 19649
678813 ZDOT = 5973
926596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2528792
36 X = -770775
91
Y = -21764095
49 feet Y = -6633696
31 meter
Z = -2547294
10 Z = -776415
24
XDOT = 13822
407721 XDOT = 4213
069873
YDOT = -3893
102102 feet/sec YDOT = -1186
617521 meter/sec
ZDOT = 19592
082714 ZDOT = 5971
666811
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 06314
54316335
00020000 00000-0 20000-3 0 9070
2 25544 51
6295 153
1980 0011886 198
6265 161
4467 15
77865037 16250
Satellite: ISS
Catalog Number: 25544
Epoch time: 06314
54316335 = yrday
fracday
Element set: 907
Inclination: 51
6295 deg
RA of node: 153
1980 deg
Eccentricity:
0011886
Arg of perigee: 198
6265 deg
Mean anomaly: 161
4467 deg
Mean motion: 15
77865037 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1625
Checksum: 312
Coasting Arc #9 (Orbit 1640)
---------------------------------------
Vector Time (GMT): 2006/315/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1627968
22 A = 6709116
43 meter
Y = 3866563
60 meter E =
0016083
Z = -5245602
66 I = 51
78129
XDOT = -6705
734574 Wp = 139
92908
YDOT = 3725
486557 meter/sec RA = 147
09549 deg
ZDOT = 653
999926 TA = 136
34168
MA = 136
21434
Ha = 186
173 n
mi
Hp = 177
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5341103
07 X = 1610093
22
Y = 12685576
10 feet Y = 3884668
86 meter
Z = -17209982
49 Z = -5237737
06
XDOT = -22000
441516 XDOT = -6750
072144
YDOT = 12222
724924 feet/sec YDOT = 3650
251364 meter/sec
ZDOT = 2145
669047 ZDOT = 621
315696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13793022
03 X = -4204113
11
Y = -481248
75 feet Y = -146684
62 meter
Z = -17180094
98 Z = -5236492
95
XDOT = -1724
649467 XDOT = -525
673158
YDOT = -24115
236173 feet/sec YDOT = -7350
323986 meter/sec
ZDOT = 2024
133203 ZDOT = 616
955800
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 06315
55648934
00020000 00000-0 20000-3 0 9086
2 25544 51
6294 147
9625 0011847 201
8627 158
2034 15
77908097 16418
Satellite: ISS
Catalog Number: 25544
Epoch time: 06315
55648934 = yrday
fracday
Element set: 908
Inclination: 51
6294 deg
RA of node: 147
9625 deg
Eccentricity:
0011847
Arg of perigee: 201
8627 deg
Mean anomaly: 158
2034 deg
Mean motion: 15
77908097 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1641
Checksum: 316
Coasting Arc #10 (Orbit 1656)
---------------------------------------
Vector Time (GMT): 2006/316/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5844872
66 A = 6719457
16 meter
Y = -2722254
62 meter E =
0016218
Z = -1854388
07 I = 51
84042
XDOT = 616
788420 Wp = 182
50666
YDOT = 5183
472156 meter/sec RA = 141
96492 deg
ZDOT = -5679
329516 TA = 18
07376
MA = 18
01617
Ha = 185
894 n
mi
Hp = 177
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19176091
40 X = 5883887
26
Y = -8931281
56 feet Y = -2656675
77 meter
Z = -6083950
36 Z = -1825898
77
XDOT = 2023
584054 XDOT = 586
369700
YDOT = 17006
142244 feet/sec YDOT = 5190
199640 meter/sec
ZDOT = -18632
970854 ZDOT = -5676
406749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 268638
71 X = 81881
08
Y = 21182466
04 feet Y = 6456415
65 meter
Z = -5977933
54 Z = -1822074
14
XDOT = -14838
064102 XDOT = -4522
641938
YDOT = -5053
770436 feet/sec YDOT = -1540
389229 meter/sec
ZDOT = -18621
360739 ZDOT = -5675
790753
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 06316
56978978
00020000 00000-0 20000-3 0 9093
2 25544 51
6299 142
7275 0011652 206
3141 153
7434 15
77969279 16572
Satellite: ISS
Catalog Number: 25544
Epoch time: 06316
56978978 = yrday
fracday
Element set: 909
Inclination: 51
6299 deg
RA of node: 142
7275 deg
Eccentricity:
0011652
Arg of perigee: 206
3141 deg
Mean anomaly: 153
7434 deg
Mean motion: 15
77969279 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1657
Checksum: 337
Coasting Arc #11 (Orbit 1672)
---------------------------------------
Vector Time (GMT): 2006/317/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 471736
80 A = 6712733
16 meter
Y = -5106939
26 meter E =
0007778
Z = 4324042
96 I = 51
83891
XDOT = 6474
412742 Wp = 155
94157
YDOT = -2339
316989 meter/sec RA = 136
77108 deg
ZDOT = -3473
989482 TA = 328
99422
MA = 329
04010
Ha = 185
748 n
mi
Hp = 178
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1547692
92 X = 507802
59
Y = -16755050
06 feet Y = -5101462
53 meter
Z = 14186492
66 Z = 4326422
11
XDOT = 21241
511622 XDOT = 6516
966326
YDOT = -7674
924506 feet/sec YDOT = -2266
678461 meter/sec
ZDOT = -11397
603287 ZDOT = -3442
433139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14818220
37 X = 4516593
57
Y = 7957053
58 feet Y = 2425309
93 meter
Z = 14194691
72 Z = 4326542
04
XDOT = -767
399095 XDOT = -233
903244
YDOT = 21523
762006 feet/sec YDOT = 6560
442659 meter/sec
ZDOT = -11280
073962 ZDOT = -3438
166544
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 06317
58306694
00020000 00000-0 20000-3 0 9108
2 25544 51
6293 137
4917 0011813 209
9536 150
0954 15
77961520 16732
Satellite: ISS
Catalog Number: 25544
Epoch time: 06317
58306694 = yrday
fracday
Element set: 910
Inclination: 51
6293 deg
RA of node: 137
4917 deg
Eccentricity:
0011813
Arg of perigee: 209
9536 deg
Mean anomaly: 150
0954 deg
Mean motion: 15
77961520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1673
Checksum: 302
Coasting Arc #12 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2006/318/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5255909
39 A = 6713757
51 meter
Y = 1159834
56 meter E =
0012757
Z = 4018402
28 I = 51
86299
XDOT = 1595
203236 Wp = 161
43901
YDOT = -6430
169065 meter/sec RA = 131
66955 deg
ZDOT = 3927
164255 TA = 248
07912
MA = 248
21478
Ha = 185
458 n
mi
Hp = 178
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17243797
22 X = -5288009
15
Y = 3805231
50 feet Y = 1100880
49 meter
Z = 13183734
52 Z = 3992790
76
XDOT = 5233
606417 XDOT = 1647
909990
YDOT = -21096
355201 feet/sec YDOT = -6412
036015 meter/sec
ZDOT = 12884
397163 ZDOT = 3935
041736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3031317
61 X = 923945
61
Y = -17468492
53 feet Y = -5324396
52 meter
Z = 13088241
58 Z = 3989296
03
XDOT = 16299
831552 XDOT = 4968
188657
YDOT = 12541
272732 feet/sec YDOT = 3822
579929 meter/sec
ZDOT = 12912
954733 ZDOT = 3935
868603
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 06318
59631720
00020000 00000-0 20000-3 0 9112
2 25544 51
6295 132
2555 0011842 213
9655 146
0753 15
78043300 16891
Satellite: ISS
Catalog Number: 25544
Epoch time: 06318
59631720 = yrday
fracday
Element set: 911
Inclination: 51
6295 deg
RA of node: 132
2555 deg
Eccentricity:
0011842
Arg of perigee: 213
9655 deg
Mean anomaly: 146
0753 deg
Mean motion: 15
78043300 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1689
Checksum: 285
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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