Date:
October 27th 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
9
000/00:00:00
000 0
0 0
0 175
2
Coasting Arc #1 (Orbit 1339)
---------------------------------------
Vector Time (GMT): 2006/296/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2356876
87 A = 6723086
83 meter
Y = 6263722
92 meter E =
0023452
Z = -531471
93 I = 51
36294
XDOT = -4682
803438 Wp = 132
99530
YDOT = 1268
922161 meter/sec RA = 245
74045 deg
ZDOT = -5993
181857 TA = 52
82147
MA = 52
60757
Ha = 189
507 n
mi
Hp = 174
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7732535
67 X = 2289241
76
Y = 20550272
03 feet Y = 6289700
65 meter
Z = -1743674
30 Z = -520186
21
XDOT = -15363
528339 XDOT = -4667
529940
YDOT = 4163
130449 feet/sec YDOT = 1216
641799 meter/sec
ZDOT = -19662
670134 ZDOT = -6015
894551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13105515
57 X = -3994561
15
Y = -17620984
79 feet Y = -5370876
16 meter
Z = -1700748
41 Z = -518388
11
XDOT = 12231
770568 XDOT = 3728
243669
YDOT = -7250
358405 feet/sec YDOT = -2209
909242 meter/sec
ZDOT = -19747
147447 ZDOT = -6018
930542
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
48909882
00020000 00000-0 20000-3 0 9000
2 25544 51
6313 246
4079 0012436 127
4403 232
7895 15
77160426 13403
Satellite: ISS
Catalog Number: 25544
Epoch time: 06296
48909882 = yrday
fracday
Element set: 900
Inclination: 51
6313 deg
RA of node: 246
4079 deg
Eccentricity:
0012436
Arg of perigee: 127
4403 deg
Mean anomaly: 232
7895 deg
Mean motion: 15
77160426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1340
Checksum: 295
Coasting Arc #2 (Orbit 1355)
---------------------------------------
Vector Time (GMT): 2006/297/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4461117
15 A = 6712024
68 meter
Y = -229988
55 meter E =
0014587
Z = 4996568
91 I = 51
33906
XDOT = 2374
504157 Wp = 110
65519
YDOT = 7120
784461 meter/sec RA = 240
54039 deg
ZDOT = -1793
159217 TA = 356
65098
MA = 356
66074
Ha = 189
264 n
mi
Hp = 175
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14636211
13 X = 4439084
15
Y = -754555
61 feet Y = -180225
13 meter
Z = 16392942
62 Z = 5018188
18
XDOT = 7790
367970 XDOT = 2303
413196
YDOT = 23362
153744 feet/sec YDOT = 7146
940019 meter/sec
ZDOT = -5883
068297 ZDOT = -1781
796096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13690797
27 X = -4172955
01
Y = 4970180
32 feet Y = 1514910
96 meter
Z = 16473493
13 Z = 5021120
71
XDOT = -13942
709319 XDOT = -4249
737800
YDOT = -19060
339843 feet/sec YDOT = -5809
591584 meter/sec
ZDOT = -5839
736278 ZDOT = -1779
951617
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
50287818
00020000 00000-0 20000-3 0 9013
2 25544 51
6314 241
1769 0012385 131
6000 228
6228 15
77201467 13567
Satellite: ISS
Catalog Number: 25544
Epoch time: 06297
50287818 = yrday
fracday
Element set: 901
Inclination: 51
6314 deg
RA of node: 241
1769 deg
Eccentricity:
0012385
Arg of perigee: 131
6000 deg
Mean anomaly: 228
6228 deg
Mean motion: 15
77201467 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1356
Checksum: 282
Coasting Arc #3 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2006/298/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1664060
25 A = 6720082
69 meter
Y = -5989219
31 meter E =
0022796
Z = 2543138
93 I = 51
38228
XDOT = 5587
810554 Wp = 104
44939
YDOT = 700
103380 meter/sec RA = 235
39749 deg
ZDOT = 5260
187734 TA = 284
53905
MA = 284
79179
Ha = 189
232 n
mi
Hp = 175
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5459515
26 X = -1609318
77
Y = -19649669
65 feet Y = -6007521
77 meter
Z = 8343631
66 Z = 2535187
44
XDOT = 18332
711790 XDOT = 5554
012796
YDOT = 2296
927101 feet/sec YDOT = 762
400213 meter/sec
ZDOT = 17257
833774 ZDOT = 5287
252056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11298611
05 X = 3443816
65
Y = 16993074
73 feet Y = 5179489
18 meter
Z = 8313171
06 Z = 2533854
54
XDOT = -16817
072945 XDOT = -5125
843834
YDOT = 2617
195106 feet/sec YDOT = 797
721068 meter/sec
ZDOT = 17358
815663 ZDOT = 5290
967014
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
51662640
00020000 00000-0 20000-3 0 9026
2 25544 51
6317 235
9453 0012423 136
0754 224
1401 15
77275372 13727
Satellite: ISS
Catalog Number: 25544
Epoch time: 06298
51662640 = yrday
fracday
Element set: 902
Inclination: 51
6317 deg
RA of node: 235
9453 deg
Eccentricity:
0012423
Arg of perigee: 136
0754 deg
Mean anomaly: 224
1401 deg
Mean motion: 15
77275372 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1372
Checksum: 275
Coasting Arc #4 (Orbit 1386)
---------------------------------------
Vector Time (GMT): 2006/299/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5265902
10 A = 6715962
05 meter
Y = -1384386
15 meter E =
0018649
Z = -3952979
39 I = 51
38577
XDOT = -1273
003471 Wp = 128
22607
YDOT = -6466
431446 meter/sec RA = 230
17006 deg
ZDOT = 3961
731265 TA = 183
01961
MA = 183
03089
Ha = 189
094 n
mi
Hp = 175
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17276581
70 X = -5230826
96
Y = -4541949
31 feet Y = -1443076
06 meter
Z = -12969092
50 Z = -3978476
69
XDOT = -4176
520574 XDOT = -1219
846203
YDOT = -21215
326265 feet/sec YDOT = -6480
369866 meter/sec
ZDOT = 12997
805986 ZDOT = 3955
675635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17747098
14 X = 5409315
51
Y = -1292503
79 feet Y = -393955
15 meter
Z = -13064336
20 Z = -3982009
67
XDOT = 10814
424434 XDOT = 3296
236568
YDOT = 17391
243288 feet/sec YDOT = 5300
850954 meter/sec
ZDOT = 12974
345893 ZDOT = 3954
580628
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
46699006
00020000 00000-0 20000-3 0 9038
2 25544 51
6316 231
0402 0012260 139
3180 220
8902 15
77279211 13876
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
46699006 = yrday
fracday
Element set: 903
Inclination: 51
6316 deg
RA of node: 231
0402 deg
Eccentricity:
0012260
Arg of perigee: 139
3180 deg
Mean anomaly: 220
8902 deg
Mean motion: 15
77279211 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1387
Checksum: 276
Coasting Arc #5 (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 = 5042530
63 A = 6714155
03 meter
Y = 493813
37 meter E =
0017497
Z = 4388081
39 I = 51
38563
XDOT = 2218
813173 Wp = 110
19076
YDOT = 6619
832410 meter/sec RA = 229
36042 deg
ZDOT = -3290
100972 TA = 12
89445
MA = 12
84977
Ha = 188
862 n
mi
Hp = 175
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16543735
67 X = 5015316
92
Y = 1620122
61 feet Y = 550049
35 meter
Z = 14396592
48 Z = 4412512
55
XDOT = 7279
570777 XDOT = 2160
607504
YDOT = 21718
610270 feet/sec YDOT = 6644
319143 meter/sec
ZDOT = -10794
294529 ZDOT = -3279
462728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5661312
07 X = -1725567
92
Y = 15544669
79 feet Y = 4738015
35 meter
Z = 14487741
33 Z = 4415863
56
XDOT = -21727
751488 XDOT = -6622
618654
YDOT = 2123
345539 feet/sec YDOT = 647
195720 meter/sec
ZDOT = -10753
728734 ZDOT = -3277
736518
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
65705865
00020000 00000-0 20000-3 0 9041
2 25544 51
6342 230
0602 0012205 139
9033 220
3035 15
77334890 13909
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
65705865 = yrday
fracday
Element set: 904
Inclination: 51
6342 deg
RA of node: 230
0602 deg
Eccentricity:
0012205
Arg of perigee: 139
9033 deg
Mean anomaly: 220
3035 deg
Mean motion: 15
77334890 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1390
Checksum: 272
Coasting Arc #6 (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 = -1327870
10 A = 6716695
26 meter
Y = -5430727
73 meter E =
0021990
Z = 3715928
21 I = 51
41359
XDOT = 6281
940680 Wp = 120
65757
YDOT = 1388
788160 meter/sec RA = 224
23213 deg
ZDOT = 4244
861284 TA = 284
42753
MA = 284
67146
Ha = 188
945 n
mi
Hp = 175
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4356529
20 X = -1285095
94
Y = -17817348
20 feet Y = -5445337
77 meter
Z = 12191365
52 Z = 3709580
86
XDOT = 20610
041600 XDOT = 6245
322966
YDOT = 4556
391602 feet/sec YDOT = 1458
831309 meter/sec
ZDOT = 13926
710250 ZDOT = 4275
290731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18357619
11 X = 5595402
31
Y = -172191
07 feet Y = -52483
84 meter
Z = 12166955
55 Z = 3708488
05
XDOT = -9205
279948 XDOT = -2805
769328
YDOT = 17578
264845 feet/sec YDOT = 5357
855125 meter/sec
ZDOT = 14040
356602 ZDOT = 4279
500692
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
67074563
00020000 00000-0 20000-3 0 9051
2 25544 51
6342 224
8277 0012243 143
7880 216
4116 15
77338986 14067
Satellite: ISS
Catalog Number: 25544
Epoch time: 06300
67074563 = yrday
fracday
Element set: 905
Inclination: 51
6342 deg
RA of node: 224
8277 deg
Eccentricity:
0012243
Arg of perigee: 143
7880 deg
Mean anomaly: 216
4116 deg
Mean motion: 15
77338986 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1406
Checksum: 290
Coasting Arc #7 (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 = -5828470
65 A = 6718994
73 meter
Y = -1832347
19 meter E =
0013316
Z = -2815967
99 I = 51
44327
XDOT = -647
793768 Wp = 128
08255
YDOT = -5737
864203 meter/sec RA = 219
00508 deg
ZDOT = 5082
622246 TA = 199
55489
MA = 199
60601
Ha = 188
697 n
mi
Hp = 175
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19122279
03 X = -5793868
21
Y = -6011637
77 feet Y = -1897330
76 meter
Z = -9238740
14 Z = -2844199
22
XDOT = -2125
307639 XDOT = -608
274894
YDOT = -18825
013791 feet/sec YDOT = -5744
887508 meter/sec
ZDOT = 16675
269836 ZDOT = 5079
570892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9972769
35 X = 3039700
10
Y = -17331597
18 feet Y = -5282670
82 meter
Z = -9344264
23 Z = -2848131
74
XDOT = 17597
650808 XDOT = 5363
763966
YDOT = 1156
354702 feet/sec YDOT = 352
456913 meter/sec
ZDOT = 16663
102620 ZDOT = 5078
913679
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
62104901
00020000 00000-0 20000-3 0 9068
2 25544 51
6339 219
9221 0012107 148
1104 212
0796 15
77393746 14212
Satellite: ISS
Catalog Number: 25544
Epoch time: 06301
62104901 = yrday
fracday
Element set: 906
Inclination: 51
6339 deg
RA of node: 219
9221 deg
Eccentricity:
0012107
Arg of perigee: 148
1104 deg
Mean anomaly: 212
0796 deg
Mean motion: 15
77393746 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1421
Checksum: 262
Coasting Arc #8 (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 = -330777
87 A = 6711682
38 meter
Y = 4532292
68 meter E =
0019427
Z = -4952353
53 I = 51
44133
XDOT = -6916
278627 Wp = 112
33052
YDOT = -2700
214016 meter/sec RA = 213
86901 deg
ZDOT = -2022
797517 TA = 138
10129
MA = 137
95246
Ha = 188
484 n
mi
Hp = 175
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1085229
22 X = -357376
06
Y = 14869726
63 feet Y = 4528445
21 meter
Z = -16247879
05 Z = -4954024
90
XDOT = -22691
202844 XDOT = -6875
743910
YDOT = -8858
969868 feet/sec YDOT = -2777
328958 meter/sec
ZDOT = -6636
474794 ZDOT = -2056
298886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14377355
67 X = -4382218
01
Y = -3923763
95 feet Y = -1195963
25 meter
Z = -16253485
36 Z = -4954062
34
XDOT = 12888
278568 XDOT = 3928
347308
YDOT = -19399
769098 feet/sec YDOT = -5913
049621 meter/sec
ZDOT = -6761
785796 ZDOT = -2060
992311
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
63467847
00020000 00000-0 20000-3 0 9072
2 25544 51
6334 214
6887 0012043 152
3662 207
8146 15
77450489 14378
Satellite: ISS
Catalog Number: 25544
Epoch time: 06302
63467847 = yrday
fracday
Element set: 907
Inclination: 51
6334 deg
RA of node: 214
6887 deg
Eccentricity:
0012043
Arg of perigee: 152
3662 deg
Mean anomaly: 207
8146 deg
Mean motion: 15
77450489 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1437
Checksum: 302
Coasting Arc #9 (Orbit 1452)
---------------------------------------
Vector Time (GMT): 2006/303/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6082936
97 A = 6722218
42 meter
Y = 2756580
42 meter E =
0024876
Z = 628615
52 I = 51
50147
XDOT = -1468
471282 Wp = 141
90084
YDOT = 4631
736188 meter/sec RA = 208
67205 deg
ZDOT = -5994
966867 TA = 31
22197
MA = 31
07445
Ha = 188
470 n
mi
Hp = 175
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19957142
28 X = 6048606
67
Y = 9043899
01 feet Y = 2824411
23 meter
Z = 2062386
88 Z = 658083
44
XDOT = -4817
819166 XDOT = -1491
032049
YDOT = 15195
984868 feet/sec YDOT = 4615
188882 meter/sec
ZDOT = -19668
526465 ZDOT = -6002
155509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12511343
05 X = -3813457
36
Y = 17974394
24 feet Y = 5478595
37 meter
Z = 2172676
52 Z = 662231
80
XDOT = -12779
359033 XDOT = -3895
148633
YDOT = -6474
755577 feet/sec YDOT = -1973
505500 meter/sec
ZDOT = -19694
692747 ZDOT = -6002
942349
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 06303
64828118
00020000 00000-0 20000-3 0 9087
2 25544 51
6336 209
4561 0012265 156
3939 203
7791 15
77443454 14531
Satellite: ISS
Catalog Number: 25544
Epoch time: 06303
64828118 = yrday
fracday
Element set: 908
Inclination: 51
6336 deg
RA of node: 209
4561 deg
Eccentricity:
0012265
Arg of perigee: 156
3939 deg
Mean anomaly: 203
7791 deg
Mean motion: 15
77443454 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1453
Checksum: 300
Coasting Arc #10 (Orbit 1468)
---------------------------------------
Vector Time (GMT): 2006/304/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2271313
50 A = 6710145
37 meter
Y = -3542400
36 meter E =
0012173
Z = 5220219
03 I = 51
48703
XDOT = 6843
970591 Wp = 147
50218
YDOT = 3504
476010 meter/sec RA = 203
50010 deg
ZDOT = -609
161463 TA = 308
23601
MA = 308
34552
Ha = 188
151 n
mi
Hp = 175
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7451815
96 X = 2285397
09
Y = -11622048
44 feet Y = -3516922
49 meter
Z = 17126702
87 Z = 5231287
46
XDOT = 22453
971755 XDOT = 6807
233628
YDOT = 11497
624705 feet/sec YDOT = 3580
803674 meter/sec
ZDOT = -1998
561231 ZDOT = -576
002282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10254345
69 X = 3125524
57
Y = 9167942
36 feet Y = 2794388
83 meter
Z = 17167491
06 Z = 5232651
28
XDOT = -14366
361634 XDOT = -4378
867026
YDOT = 19520
664146 feet/sec YDOT = 5949
898432 meter/sec
ZDOT = -1874
387796 ZDOT = -571
313400
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 06304
66185228
00020000 00000-0 20000-3 0 9099
2 25544 51
6334 204
2226 0012057 160
6554 199
5070 15
77533333 14695
Satellite: ISS
Catalog Number: 25544
Epoch time: 06304
66185228 = yrday
fracday
Element set: 909
Inclination: 51
6334 deg
RA of node: 204
2226 deg
Eccentricity:
0012057
Arg of perigee: 160
6554 deg
Mean anomaly: 199
5070 deg
Mean motion: 15
77533333 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1469
Checksum: 286
Coasting Arc #11 (Orbit 1484)
---------------------------------------
Vector Time (GMT): 2006/305/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5620811
33 A = 6720766
70 meter
Y = -3275640
72 meter E =
0016698
Z = 1687191
82 I = 51
54926
XDOT = 3781
824243 Wp = 109
26804
YDOT = -3522
161174 meter/sec RA = 198
34859 deg
ZDOT = 5709
583625 TA = 269
42827
MA = 269
61961
Ha = 187
984 n
mi
Hp = 175
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18440982
05 X = -5591961
12
Y = -10746852
74 feet Y = -3338334
39 meter
Z = 5535406
22 Z = 1659955
62
XDOT = 12407
559851 XDOT = 3793
191868
YDOT = -11555
646895 feet/sec YDOT = -3479
807003 meter/sec
ZDOT = 18732
229742 ZDOT = 5727
983745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13352739
83 X = 4069915
10
Y = -16684976
38 feet Y = -5085580
80 meter
Z = 5433349
54 Z = 1656084
94
XDOT = 8398
862093 XDOT = 2559
973166
YDOT = 12899
451900 feet/sec YDOT = 3931
752939 meter/sec
ZDOT = 18800
369283 ZDOT = 5730
352557
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 06305
67539551
00020000 00000-0 20000-3 0 9105
2 25544 51
6326 198
9884 0012050 165
2834 194
8684 15
77598578 14859
Satellite: ISS
Catalog Number: 25544
Epoch time: 06305
67539551 = yrday
fracday
Element set: 910
Inclination: 51
6326 deg
RA of node: 198
9884 deg
Eccentricity:
0012050
Arg of perigee: 165
2834 deg
Mean anomaly: 194
8684 deg
Mean motion: 15
77598578 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1485
Checksum: 336
Coasting Arc #12 (Orbit 1499)
---------------------------------------
Vector Time (GMT): 2006/306/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4286222
86 A = 6713147
98 meter
Y = 2636901
79 meter E =
0019104
Z = -4461183
21 I = 51
55058
XDOT = -5770
227312 Wp = 143
19770
YDOT = -3954
665826 meter/sec RA = 193
13849 deg
ZDOT = 3198
432737 TA = 158
91163
MA = 158
83275
Ha = 187
813 n
mi
Hp = 175
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14062410
97 X = -4293718
39
Y = 8651252
58 feet Y = 2588928
81 meter
Z = -14636427
85 Z = -4482024
44
XDOT = -18931
191968 XDOT = -5741
114589
YDOT = -12974
625413 feet/sec YDOT = -4019
028828 meter/sec
ZDOT = 10493
545724 ZDOT = 3170
471187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6754392
01 X = -2058738
68
Y = -14990091
47 feet Y = -4568979
88 meter
Z = -14713801
01 Z = -4484766
55
XDOT = 14246
957816 XDOT = 4342
472742
YDOT = -16642
324070 feet/sec YDOT = -5072
580377 meter/sec
ZDOT = 10388
682498 ZDOT = 3166
470425
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 06306
62556870
00020000 00000-0 20000-3 0 9115
2 25544 51
6318 194
0808 0012008 168
7404 191
4031 15
77618120 15000
Satellite: ISS
Catalog Number: 25544
Epoch time: 06306
62556870 = yrday
fracday
Element set: 911
Inclination: 51
6318 deg
RA of node: 194
0808 deg
Eccentricity:
0012008
Arg of perigee: 168
7404 deg
Mean anomaly: 191
4031 deg
Mean motion: 15
77618120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1500
Checksum: 267
Coasting Arc #13 (Orbit 1515)
---------------------------------------
Vector Time (GMT): 2006/307/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4240836
56 A = 6715711
09 meter
Y = 3604750
77 meter E =
0012838
Z = -3755230
88 I = 51
58650
XDOT = -5908
310087 Wp = 145
46573
YDOT = 2558
194076 meter/sec RA = 188
02021 deg
ZDOT = -4234
078423 TA = 80
07918
MA = 79
93429
Ha = 187
688 n
mi
Hp = 176
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13913505
76 X = 4218455
30
Y = 11826610
15 feet Y = 3652048
94 meter
Z = -12320311
27 Z = -3734682
75
XDOT = -19384
219446 XDOT = -5915
908071
YDOT = 8393
025184 feet/sec YDOT = 2492
081500 meter/sec
ZDOT = -13891
333409 ZDOT = -4262
800324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13334964
40 X = -4064497
15
Y = 12551032
66 feet Y = 3825554
76 meter
Z = -12243150
08 Z = -3731712
14
XDOT = -5235
887195 XDOT = -1595
898417
YDOT = -19161
557104 feet/sec YDOT = -5840
442605 meter/sec
ZDOT = -13998
121243 ZDOT = -4266
627355
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
63905865
00020000 00000-0 20000-3 0 9120
2 25544 51
6309 188
8474 0011975 172
7869 187
3470 15
77653004 15160
Satellite: ISS
Catalog Number: 25544
Epoch time: 06307
63905865 = yrday
fracday
Element set: 912
Inclination: 51
6309 deg
RA of node: 188
8474 deg
Eccentricity:
0011975
Arg of perigee: 172
7869 deg
Mean anomaly: 187
3470 deg
Mean motion: 15
77653004 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1516
Checksum: 322
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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