Date:
November 25th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 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 1368)
---------------------------------------
Vector Time (GMT): 2008/329/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3752661
26 A = 6731498
17 meter
Y = 3759096
05 meter E =
0012849
Z = -4149239
72 I = 51
30960
XDOT = -2278
760499 Wp = 49
38569
YDOT = -6345
982612 meter/sec RA = 276
22359 deg
ZDOT = -3687
574004 TA = 182
67772
MA = 182
68461
Ha = 195
353 n
mi
Hp = 186
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12311880
77 X = -3774260
38
Y = 12332992
30 feet Y = 3717011
08 meter
Z = -13612991
22 Z = -4167522
90
XDOT = -7476
248355 XDOT = -2189
715277
YDOT = -20820
152926 feet/sec YDOT = -6370
966954 meter/sec
ZDOT = -12098
339909 ZDOT = -3698
428563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10418453
63 X = 3175544
67
Y = 13900132
88 feet Y = 4236760
50 meter
Z = -13683594
81 Z = -4170759
70
XDOT = -20663
736148 XDOT = -6298
306778
YDOT = 3533
740233 feet/sec YDOT = 1077
084023 meter/sec
ZDOT = -12140
903610 ZDOT = -3700
547420
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 08329
07539891
00020000 00000-0 20000-3 0 9003
2 25544 51
6419 276
8084 0006082 22
1144 338
0279 15
71598832 13693
Satellite: ISS
Catalog Number: 25544
Epoch time: 08329
07539891 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 276
8084 deg
Eccentricity:
0006082
Arg of perigee: 22
1144 deg
Mean anomaly: 338
0279 deg
Mean motion: 15
71598832 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1369
Checksum: 308
Coasting Arc #2 (Orbit 1384)
---------------------------------------
Vector Time (GMT): 2008/330/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2946591
09 A = 6732696
74 meter
Y = 4719244
37 meter E =
0015884
Z = 3785069
47 I = 51
31203
XDOT = -3430
730271 Wp = 63
61677
YDOT = 5494
859201 meter/sec RA = 271
03197 deg
ZDOT = -4159
819350 TA = 70
27684
MA = 70
10556
Ha = 195
418 n
mi
Hp = 186
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9667293
61 X = 2875213
03
Y = 15483085
19 feet Y = 4751795
48 meter
Z = 12418206
94 Z = 3799211
38
XDOT = -11255
676741 XDOT = -3471
711479
YDOT = 18027
753285 feet/sec YDOT = 5456
265959 meter/sec
ZDOT = -13647
701279 ZDOT = -4176
585452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16589327
18 X = 5056426
92
Y = -7523496
15 feet Y = -2293161
63 meter
Z = 12473395
12 Z = 3801890
83
XDOT = 15890
741449 XDOT = 4843
497994
YDOT = 12194
398581 feet/sec YDOT = 3716
852687 meter/sec
ZDOT = -13712
294627 ZDOT = -4179
507402
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 08330
09276963
00020000 00000-0 20000-3 0 9016
2 25544 51
6420 271
6025 0006189 27
5104 332
6384 15
71619034 13859
Satellite: ISS
Catalog Number: 25544
Epoch time: 08330
09276963 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 271
6025 deg
Eccentricity:
0006189
Arg of perigee: 27
5104 deg
Mean anomaly: 332
6384 deg
Mean motion: 15
71619034 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1385
Checksum: 277
Coasting Arc #3 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2008/331/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2043733
51 A = 6734729
08 meter
Y = -5636880
65 meter E =
0017524
Z = 3044845
83 I = 51
32071
XDOT = 4226
701817 Wp = 67
83479
YDOT = 4185
916394 meter/sec RA = 265
94132 deg
ZDOT = 4896
373649 TA = 327
61583
MA = 327
72326
Ha = 195
354 n
mi
Hp = 185
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6705162
44 X = 2091822
41
Y = -18493702
91 feet Y = -5613757
85 meter
Z = 9989651
68 Z = 3054890
85
XDOT = 13867
131947 XDOT = 4155
793709
YDOT = 13733
321502 feet/sec YDOT = 4232
784887 meter/sec
ZDOT = 16064
218007 ZDOT = 4916
735702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17636104
30 X = -5375484
59
Y = -8670229
10 feet Y = -2642685
83 meter
Z = 10028177
49 Z = 3056588
50
XDOT = 14552
826522 XDOT = 4435
701524
YDOT = -10869
696663 feet/sec YDOT = -3313
083543 meter/sec
ZDOT = 16143
487009 ZDOT = 4920
534840
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 08331
11012070
00020000 00000-0 20000-3 0 9028
2 25544 51
6425 266
3959 0006189 30
6847 329
4676 15
71683203 14016
Satellite: ISS
Catalog Number: 25544
Epoch time: 08331
11012070 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 266
3959 deg
Eccentricity:
0006189
Arg of perigee: 30
6847 deg
Mean anomaly: 329
4676 deg
Mean motion: 15
71683203 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1401
Checksum: 276
Coasting Arc #4 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2008/332/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4190170
46 A = 6729135
96 meter
Y = -2450051
93 meter E =
0014034
Z = -4671926
86 I = 51
30562
XDOT = 1083
081589 Wp = 83
75323
YDOT = -7093
725307 meter/sec RA = 260
75577 deg
ZDOT = 2757
304449 TA = 213
56047
MA = 213
64945
Ha = 195
398 n
mi
Hp = 185
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13747278
42 X = -4139766
18
Y = -8038228
12 feet Y = -2496626
49 meter
Z = -15327844
03 Z = -4692161
09
XDOT = 3553
417286 XDOT = 1148
929443
YDOT = -23273
376990 feet/sec YDOT = -7081
245800 meter/sec
ZDOT = 9046
274438 ZDOT = 2762
725344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9293192
23 X = -2832564
99
Y = 12838229
96 feet Y = 3913092
49 meter
Z = -15406492
38 Z = -4695898
88
XDOT = -21902
072852 XDOT = -6675
751805
YDOT = -5007
399933 feet/sec YDOT = -1526
255500 meter/sec
ZDOT = 9066
762571 ZDOT = 2763
549232
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 08332
06387378
00020000 00000-0 20000-3 0 9030
2 25544 51
6425 261
5162 0006249 34
1791 325
9772 15
71717565 14166
Satellite: ISS
Catalog Number: 25544
Epoch time: 08332
06387378 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 261
5162 deg
Eccentricity:
0006249
Arg of perigee: 34
1791 deg
Mean anomaly: 325
9772 deg
Mean motion: 15
71717565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1416
Checksum: 298
Coasting Arc #5 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2008/333/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 212144
00 A = 6737358
73 meter
Y = 6502047
62 meter E =
0008492
Z = -1756996
05 I = 51
33846
XDOT = -5023
423712 Wp = 96
98014
YDOT = -1359
483024 meter/sec RA = 255
65260 deg
ZDOT = -5661
983429 TA = 102
52634
MA = 102
43132
Ha = 195
495 n
mi
Hp = 185
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 696010
51 X = 147956
65
Y = 21332177
24 feet Y = 6504061
27 meter
Z = -5764422
74 Z = -1756120
51
XDOT = -16481
048924 XDOT = -4980
342857
YDOT = -4460
246143 feet/sec YDOT = -1415
416250 meter/sec
ZDOT = -18576
061119 ZDOT = -5686
283330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21324595
10 X = 6499736
59
Y = 923379
38 feet Y = 281446
03 meter
Z = -5760538
17 Z = -1755812
04
XDOT = -5646
469887 XDOT = -1721
044021
YDOT = 14424
890885 feet/sec YDOT = 4396
706742 meter/sec
ZDOT = -18670
401746 ZDOT = -5690
738452
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 08333
08119354
00020000 00000-0 20000-3 0 9041
2 25544 51
6418 256
3098 0006216 37
7899 322
3698 15
71710701 14321
Satellite: ISS
Catalog Number: 25544
Epoch time: 08333
08119354 = yrday
fracday
Element set: 904
Inclination: 51
6418 deg
RA of node: 256
3098 deg
Eccentricity:
0006216
Arg of perigee: 37
7899 deg
Mean anomaly: 322
3698 deg
Mean motion: 15
71710701 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1432
Checksum: 294
Coasting Arc #6 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2008/334/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4330498
58 A = 6726899
97 meter
Y = -106075
04 meter E =
0010131
Z = 5141455
79 I = 51
31295
XDOT = 1615
956068 Wp = 46
17903
YDOT = 7434
611511 meter/sec RA = 250
48547 deg
ZDOT = -1199
295335 TA = 55
37532
MA = 55
27982
Ha = 195
298 n
mi
Hp = 185
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14207672
51 X = 4306386
12
Y = -348015
22 feet Y = -57784
43 meter
Z = 16868293
28 Z = 5162435
19
XDOT = 5301
693135 XDOT = 1538
527001
YDOT = 24391
770048 feet/sec YDOT = 7452
249302 meter/sec
ZDOT = -3934
695980 ZDOT = -1191
631920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 502260
04 X = 153088
86
Y = -14105861
84 feet Y = -4299466
69 meter
Z = 16949654
50 Z = 5166254
69
XDOT = 23639
400674 XDOT = 7205
289325
YDOT = -3882
762163 feet/sec YDOT = -1183
465907 meter/sec
ZDOT = -3904
411514 ZDOT = -1190
064629
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 08334
09849442
00020000 00000-0 20000-3 0 9052
2 25544 51
6423 251
1030 0006217 40
1325 320
0295 15
71780620 14481
Satellite: ISS
Catalog Number: 25544
Epoch time: 08334
09849442 = yrday
fracday
Element set: 905
Inclination: 51
6423 deg
RA of node: 251
1030 deg
Eccentricity:
0006217
Arg of perigee: 40
1325 deg
Mean anomaly: 320
0295 deg
Mean motion: 15
71780620 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1448
Checksum: 255
Coasting Arc #7 (Orbit 1463)
---------------------------------------
Vector Time (GMT): 2008/335/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2568591
40 A = 6738593
47 meter
Y = -6211484
62 meter E =
0019213
Z = 319000
99 I = 51
36216
XDOT = 4561
757952 Wp = 46
96030
YDOT = -1567
013381 meter/sec RA = 245
35961 deg
ZDOT = 6004
340225 TA = 316
51913
MA = 316
67046
Ha = 195
586 n
mi
Hp = 185
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8427137
15 X = -2500492
34
Y = -20378886
55 feet Y = -6239827
38 meter
Z = 1046591
17 Z = 306687
11
XDOT = 14966
397480 XDOT = 4549
773052
YDOT = -5141
120018 feet/sec YDOT = -1516
069024 meter/sec
ZDOT = 19699
278953 ZDOT = 6026
472266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20722817
25 X = -6316314
70
Y = 7548453
25 feet Y = 2300768
55 meter
Z = 998353
39 Z = 304298
11
XDOT = -3946
707335 XDOT = -1202
956396
YDOT = -13549
241562 feet/sec YDOT = -4129
808828 meter/sec
ZDOT = 19785
008616 ZDOT = 6030
470626
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 08335
11578255
00020000 00000-0 20000-3 0 9068
2 25544 51
6416 245
8971 0006422 44
0830 316
0843 15
71738130 14640
Satellite: ISS
Catalog Number: 25544
Epoch time: 08335
11578255 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 245
8971 deg
Eccentricity:
0006422
Arg of perigee: 44
0830 deg
Mean anomaly: 316
0843 deg
Mean motion: 15
71738130 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1464
Checksum: 280
Coasting Arc #8 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2008/336/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3402287
55 A = 6726552
65 meter
Y = 2510460
09 meter E =
0020202
Z = -5248663
16 I = 51
33414
XDOT = -4106
488963 Wp = 75
34573
YDOT = -6478
575782 meter/sec RA = 240
22124 deg
ZDOT = -433
188990 TA = 190
49194
MA = 190
53416
Ha = 195
562 n
mi
Hp = 185
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11162360
71 X = -3404609
69
Y = 8236417
62 feet Y = 2472401
48 meter
Z = -17220023
49 Z = -5265196
97
XDOT = -13472
732817 XDOT = -4031
634887
YDOT = -21255
169887 feet/sec YDOT = -6524
078325 meter/sec
ZDOT = -1421
223719 ZDOT = -452
957625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7947723
90 X = 2422466
25
Y = 11272271
72 feet Y = 3435788
42 meter
Z = -17283971
07 Z = -5268154
38
XDOT = -20773
899944 XDOT = -6331
884703
YDOT = 12331
255334 feet/sec YDOT = 3758
566626 meter/sec
ZDOT = -1498
412249 ZDOT = -456
716053
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 08336
06947176
00020000 00000-0 20000-3 0 9076
2 25544 51
6405 241
0159 0006289 47
5124 312
6569 15
71766710 14797
Satellite: ISS
Catalog Number: 25544
Epoch time: 08336
06947176 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 241
0159 deg
Eccentricity:
0006289
Arg of perigee: 47
5124 deg
Mean anomaly: 312
6569 deg
Mean motion: 15
71766710 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1479
Checksum: 305
Coasting Arc #9 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2008/337/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470180
34 A = 6737839
55 meter
Y = 4922509
78 meter E =
0016951
Z = 1059583
20 I = 51
38858
XDOT = -2961
534866 Wp = 102
11842
YDOT = 3973
364498 meter/sec RA = 235
06844 deg
ZDOT = -5889
081458 TA = 66
26325
MA = 66
08553
Ha = 195
571 n
mi
Hp = 185
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14665946
01 X = 4409656
49
Y = 16149966
49 feet Y = 4972159
38 meter
Z = 3476322
85 Z = 1081153
16
XDOT = -9716
321740 XDOT = -2977
137212
YDOT = 13035
972761 feet/sec YDOT = 3940
160414 meter/sec
ZDOT = -19321
133392 ZDOT = -5903
506123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16275812
90 X = 4960867
77
Y = -14505782
38 feet Y = -4421362
47 meter
Z = 3560393
56 Z = 1085207
96
XDOT = 11894
609423 XDOT = 3625
476952
YDOT = 8530
423756 feet/sec YDOT = 2600
073161 meter/sec
ZDOT = -19376
787953 ZDOT = -5906
044968
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 08337
08672522
00020000 00000-0 20000-3 0 9080
2 25544 51
6405 235
8088 0006493 51
3194 308
8548 15
71834704 14957
Satellite: ISS
Catalog Number: 25544
Epoch time: 08337
08672522 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 235
8088 deg
Eccentricity:
0006493
Arg of perigee: 51
3194 deg
Mean anomaly: 308
8548 deg
Mean motion: 15
71834704 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1495
Checksum: 309
Coasting Arc #10 (Orbit 1510)
---------------------------------------
Vector Time (GMT): 2008/338/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1595050
31 A = 6727576
68 meter
Y = -4253966
87 meter E =
0010211
Z = 4952972
27 I = 51
37161
XDOT = 5897
448837 Wp = 88
49864
YDOT = 4538
829782 meter/sec RA = 229
95768 deg
ZDOT = 1995
788236 TA = 342
11890
MA = 342
15480
Ha = 195
492 n
mi
Hp = 185
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5233104
68 X = 1618439
48
Y = -13956584
20 feet Y = -4235999
87 meter
Z = 16249909
01 Z = 4960777
42
XDOT = 19348
585424 XDOT = 5836
561336
YDOT = 14891
173825 feet/sec YDOT = 4604
437803 meter/sec
ZDOT = 6547
861668 ZDOT = 2024
290876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13999959
67 X = -4267187
71
Y = -5019814
33 feet Y = -1530039
41 meter
Z = 16279857
59 Z = 4962100
59
XDOT = 14359
138261 XDOT = 4376
665342
YDOT = -18416
655305 feet/sec YDOT = -5613
396537 meter/sec
ZDOT = 6658
815879 ZDOT = 2029
607080
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 08338
10396202
00020000 00000-0 20000-3 0 9093
2 25544 51
6401 230
6016 0006390 55
2583 304
9180 15
71855530 15116
Satellite: ISS
Catalog Number: 25544
Epoch time: 08338
10396202 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 230
6016 deg
Eccentricity:
0006390
Arg of perigee: 55
2583 deg
Mean anomaly: 304
9180 deg
Mean motion: 15
71855530 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1511
Checksum: 261
Coasting Arc #11 (Orbit 1525)
---------------------------------------
Vector Time (GMT): 2008/339/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5602057
91 A = 6735693
02 meter
Y = -2873051
92 meter E =
0011949
Z = -2390535
24 I = 51
41869
XDOT = 539
194342 Wp = 53
81393
YDOT = -5491
606221 meter/sec RA = 224
78371 deg
ZDOT = 5362
055300 TA = 279
17961
MA = 279
31477
Ha = 195
551 n
mi
Hp = 184
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18379455
09 X = -5557901
74
Y = -9426023
35 feet Y = -2935450
25 meter
Z = -7842963
40 Z = -2417643
26
XDOT = 1769
010307 XDOT = 574
514214
YDOT = -18017
080779 feet/sec YDOT = -5485
379662 meter/sec
ZDOT = 17592
044949 ZDOT = 5364
760000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8950501
01 X = -2728112
71
Y = 18570892
14 feet Y = 5660407
92 meter
Z = -7948387
08 Z = -2422668
38
XDOT = -16699
694501 XDOT = -5090
066884
YDOT = -550
329921 feet/sec YDOT = -167
740560 meter/sec
ZDOT = 17602
099587 ZDOT = 5365
119954
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 08339
05760842
00020000 00000-0 20000-3 0 9105
2 25544 51
6397 225
7197 0006504 58
8148 301
3651 15
71869990 15263
Satellite: ISS
Catalog Number: 25544
Epoch time: 08339
05760842 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 225
7197 deg
Eccentricity:
0006504
Arg of perigee: 58
8148 deg
Mean anomaly: 301
3651 deg
Mean motion: 15
71869990 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1526
Checksum: 310
Coasting Arc #12 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2008/340/01:16:00
357
Vector Time (MET): N/A
Weight (LBS) : 611774
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 695545
82 A = 6730016
17 meter
Y = 5094789
87 meter E =
0015520
Z = -4357810
62 I = 51
42184
XDOT = -6610
235674 Wp = 66
88809
YDOT = -1984
328104 meter/sec RA = 219
69336 deg
ZDOT = -3378
519350 TA = 168
90629
MA = 168
87203
Ha = 195
647 n
mi
Hp = 184
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2281974
47 X = 659693
00
Y = 16715189
86 feet Y = 5102367
74 meter
Z = -14297278
95 Z = -4354518
32
XDOT = -21687
124915 XDOT = -6571
142917
YDOT = -6510
262810 feet/sec YDOT = -2058
028739 meter/sec
ZDOT = -11084
381068 ZDOT = -3410
537371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16598051
00 X = 5059085
95
Y = -3080048
56 feet Y = -938798
80 meter
Z = -14284087
95 Z = -4353790
01
XDOT = -5799
995194 XDOT = -1767
838535
YDOT = 20672
434791 feet/sec YDOT = 6300
958124 meter/sec
ZDOT = -11208
798447 ZDOT = -3416
441767
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 08340
07481545
00020000 00000-0 20000-3 0 9110
2 25544 51
6403 220
5116 0006577 62
9376 297
2457 15
71881882 15423
Satellite: ISS
Catalog Number: 25544
Epoch time: 08340
07481545 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 220
5116 deg
Eccentricity:
0006577
Arg of perigee: 62
9376 deg
Mean anomaly: 297
2457 deg
Mean motion: 15
71881882 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1542
Checksum: 295
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/plugins/scheduled_mailings pl/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list