Date:
March 1st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 1139)
---------------------------------------
Vector Time (GMT): 2008/060/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5965025
78 A = 6724293
52 meter
Y = 1661343
66 meter E =
0014472
Z = 2601611
68 I = 51
45976
XDOT = 728
125979 Wp = 114
50933
YDOT = 5610
489770 meter/sec RA = 215
11676 deg
ZDOT = -5235
392495 TA = 35
80593
MA = 35
70899
Ha = 187
624 n
mi
Hp = 181
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19570294
57 X = 5933367
05
Y = 5450602
56 feet Y = 1727870
97 meter
Z = 8535471
39 Z = 2630512
52
XDOT = 2388
864762 XDOT = 690
766779
YDOT = 18407
118668 feet/sec YDOT = 5618
423205 meter/sec
ZDOT = -17176
484565 ZDOT = -5231
946046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20256648
77 X = 6174226
54
Y = 684924
90 feet Y = 208765
11 meter
Z = 8646318
77 Z = 2635397
96
XDOT = 6813
964357 XDOT = 2076
896336
YDOT = 15821
782138 feet/sec YDOT = 4822
479196 meter/sec
ZDOT = -17162
625684 ZDOT = -5231
168308
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 08060
63602189
00020000 00000-0 20000-3 0 9008
2 25544 51
6369 215
9045 0003004 184
1180 175
9960 15
75709479 11405
Satellite: ISS
Catalog Number: 25544
Epoch time: 08060
63602189 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 215
9045 deg
Eccentricity:
0003004
Arg of perigee: 184
1180 deg
Mean anomaly: 175
9960 deg
Mean motion: 15
75709479 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1140
Checksum: 285
Coasting Arc #2 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2008/061/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -379947
01 A = 6716928
50 meter
Y = -4656163
58 meter E =
0008457
Z = 4823955
56 I = 51
46086
XDOT = 7078
676420 Wp = 139
69655
YDOT = 1897
241747 meter/sec RA = 209
99680 deg
ZDOT = 2380
111980 TA = 286
99678
MA = 287
08944
Ha = 187
462 n
mi
Hp = 181
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1246545
32 X = -351286
38
Y = -15276127
23 feet Y = -4660252
13 meter
Z = 15826625
84 Z = 4822179
40
XDOT = 23224
004004 XDOT = 7045
373094
YDOT = 6224
546414 feet/sec YDOT = 1976
213327 meter/sec
ZDOT = 7808
766337 ZDOT = 2414
418771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5156185
26 X = -1571605
27
Y = -14441620
79 feet Y = -4401806
02 meter
Z = 15819271
99 Z = 4821714
10
XDOT = 22946
927701 XDOT = 6994
223563
YDOT = 536
111839 feet/sec YDOT = 163
406889 meter/sec
ZDOT = 7940
354089 ZDOT = 2420
219926
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 08061
65072648
00020000 00000-0 20000-3 0 9013
2 25544 51
6376 210
6797 0002858 190
0418 170
0689 15
75796962 11569
Satellite: ISS
Catalog Number: 25544
Epoch time: 08061
65072648 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 210
6797 deg
Eccentricity:
0002858
Arg of perigee: 190
0418 deg
Mean anomaly: 170
0689 deg
Mean motion: 15
75796962 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1156
Checksum: 314
Coasting Arc #3 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2008/062/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6351073
47 A = 6726072
70 meter
Y = -1615378
38 meter E =
0005920
Z = -1507028
20 I = 51
51774
XDOT = -71
325485 Wp = 47
55973
YDOT = -5091
353842 meter/sec RA = 204
80370 deg
ZDOT = 5776
299032 TA = 295
80373
MA = 295
86479
Ha = 187
357 n
mi
Hp = 181
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20836855
21 X = -6325217
30
Y = -5299797
83 feet Y = -1686255
14 meter
Z = -4944318
23 Z = -1537818
32
XDOT = -234
007497 XDOT = -42
447563
YDOT = -16703
916806 feet/sec YDOT = -5091
989969 meter/sec
ZDOT = 18951
112309 ZDOT = 5776
022692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21466863
80 X = -6543100
09
Y = 504304
58 feet Y = 153712
04 meter
Z = -5062421
36 Z = -1543026
03
XDOT = -4793
874765 XDOT = -1461
173028
YDOT = -14428
472323 feet/sec YDOT = -4397
798364 meter/sec
ZDOT = 18949
445907 ZDOT = 5775
791113
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 08062
60199182
00020000 00000-0 20000-3 0 9023
2 25544 51
6376 205
7817 0002593 194
0443 166
0649 15
75779854 11714
Satellite: ISS
Catalog Number: 25544
Epoch time: 08062
60199182 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 205
7817 deg
Eccentricity:
0002593
Arg of perigee: 194
0443 deg
Mean anomaly: 166
0649 deg
Mean motion: 15
75779854 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1171
Checksum: 309
Coasting Arc #4 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2008/063/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -319516
30 A = 6715260
32 meter
Y = 4266376
95 meter E =
0013465
Z = -5187444
44 I = 51
50872
XDOT = -7413
516874 Wp = 92
13344
YDOT = -1789
987262 meter/sec RA = 199
66898 deg
ZDOT = -1018
294838 TA = 168
14766
MA = 168
11594
Ha = 187
197 n
mi
Hp = 181
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1048281
84 X = -342000
74
Y = 13997299
70 feet Y = 4262678
14 meter
Z = -17019174
68 Z = -5189051
29
XDOT = -24322
561923 XDOT = -7388
003392
YDOT = -5872
661622 feet/sec YDOT = -1872
746798 meter/sec
ZDOT = -3340
862328 ZDOT = -1054
246903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3091686
38 X = 942346
01
Y = 13684763
12 feet Y = 4171115
80 meter
Z = -17024815
24 Z = -5189163
69
XDOT = -23969
696210 XDOT = -7305
963405
YDOT = 1098
708922 feet/sec YDOT = 334
886479 meter/sec
ZDOT = -3478
770598 ZDOT = -1060
329278
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 08063
61664902
00020000 00000-0 20000-3 0 9033
2 25544 51
6377 200
5569 0002617 199
6326 160
4738 15
75830951 11870
Satellite: ISS
Catalog Number: 25544
Epoch time: 08063
61664902 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 200
5569 deg
Eccentricity:
0002617
Arg of perigee: 199
6326 deg
Mean anomaly: 160
4738 deg
Mean motion: 15
75830951 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1187
Checksum: 305
Coasting Arc #5 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2008/064/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6547496
57 A = 6726836
65 meter
Y = 1488116
61 meter E =
0013937
Z = 250577
85 I = 51
57578
XDOT = -836
759806 Wp = 142
28822
YDOT = 4724
840245 meter/sec RA = 194
50113 deg
ZDOT = -6030
469360 TA = 34
98334
MA = 34
89186
Ha = 187
126 n
mi
Hp = 181
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21481287
96 X = 6529152
37
Y = 4882272
36 feet Y = 1561231
90 meter
Z = 822105
82 Z = 282340
21
XDOT = -2745
274954 XDOT = -860
237292
YDOT = 15501
444374 feet/sec YDOT = 4715
351637 meter/sec
ZDOT = -19785
004462 ZDOT = -6034
591433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21947046
15 X = 6689459
67
Y = -1842364
28 feet Y = -561552
63 meter
Z = 943945
42 Z = 287714
56
XDOT = 2044
720553 XDOT = 623
230824
YDOT = 13971
387751 feet/sec YDOT = 4258
478987 meter/sec
ZDOT = -19800
219254 ZDOT = -6035
106829
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 08064
63128135
00020000 00000-0 20000-3 0 9040
2 25544 51
6374 195
3319 0002572 201
0157 159
0902 15
75867794 12032
Satellite: ISS
Catalog Number: 25544
Epoch time: 08064
63128135 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 195
3319 deg
Eccentricity:
0002572
Arg of perigee: 201
0157 deg
Mean anomaly: 159
0902 deg
Mean motion: 15
75867794 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1203
Checksum: 284
Coasting Arc #6 (Orbit 1218)
---------------------------------------
Vector Time (GMT): 2008/065/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1166315
79 A = 6714578
65 meter
Y = -4025989
76 meter E =
0001847
Z = 5244442
48 I = 51
56480
XDOT = 7524
944210 Wp = 135
61084
YDOT = 1598
351271 meter/sec RA = 189
34479 deg
ZDOT = -447
679770 TA = 318
63555
MA = 318
64954
Ha = 186
834 n
mi
Hp = 181
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3826495
38 X = 1185772
42
Y = -13208627
83 feet Y = -4012838
25 meter
Z = 17206176
11 Z = 5250155
80
XDOT = 24688
137171 XDOT = 7508
686626
YDOT = 5243
934616 feet/sec YDOT = 1682
408563 meter/sec
ZDOT = -1468
765648 ZDOT = -411
164074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -676961
22 X = -206337
78
Y = -13708210
41 feet Y = -4178262
53 meter
Z = 17227568
12 Z = 5250962
76
XDOT = 24079
563142 XDOT = 7339
450846
YDOT = -2853
989408 feet/sec YDOT = -869
895972 meter/sec
ZDOT = -1328
692194 ZDOT = -404
985381
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 08065
64588585
00020000 00000-0 20000-3 0 9052
2 25544 51
6383 190
1059 0002431 209
0787 151
0243 15
75956803 12194
Satellite: ISS
Catalog Number: 25544
Epoch time: 08065
64588585 = yrday
fracday
Element set: 905
Inclination: 51
6383 deg
RA of node: 190
1059 deg
Eccentricity:
0002431
Arg of perigee: 209
0787 deg
Mean anomaly: 151
0243 deg
Mean motion: 15
75956803 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1219
Checksum: 298
Coasting Arc #7 (Orbit 1234)
---------------------------------------
Vector Time (GMT): 2008/066/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6510533
25 A = 6726201
71 meter
Y = -1304770
77 meter E =
0011748
Z = 1040585
94 I = 51
63294
XDOT = 1867
626512 Wp = 60
59081
YDOT = -4562
184127 meter/sec RA = 184
20576 deg
ZDOT = 5920
343727 TA = 310
79816
MA = 310
90001
Ha = 186
834 n
mi
Hp = 181
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21360017
22 X = -6500514
09
Y = -4280743
98 feet Y = -1377519
16 meter
Z = 3413995
87 Z = 1008982
92
XDOT = 6127
383570 XDOT = 1889
743429
YDOT = -14967
795691 feet/sec YDOT = -4541
175098 meter/sec
ZDOT = 19423
699893 ZDOT = 5929
470562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21577511
63 X = -6576825
55
Y = 3130358
89 feet Y = 954133
39 meter
Z = 3292767
43 Z = 1003635
51
XDOT = 882
133275 XDOT = 268
874222
YDOT = -14545
310609 feet/sec YDOT = -4433
410674 meter/sec
ZDOT = 19458
099798 ZDOT = 5930
828818
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 08066
66046794
00020000 00000-0 20000-3 0 9067
2 25544 51
6384 184
8809 0002226 212
2108 147
8920 15
75950649 12358
Satellite: ISS
Catalog Number: 25544
Epoch time: 08066
66046794 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 184
8809 deg
Eccentricity:
0002226
Arg of perigee: 212
2108 deg
Mean anomaly: 147
8920 deg
Mean motion: 15
75950649 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1235
Checksum: 307
Coasting Arc #8 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2008/067/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2103829
46 A = 6715596
32 meter
Y = 3986765
67 meter E =
0012475
Z = -4989092
28 I = 51
62649
XDOT = -7307
806027 Wp = 113
59414
YDOT = -1418
261901 meter/sec RA = 179
02928 deg
ZDOT = 1947
196065 TA = 175
24342
MA = 175
23155
Ha = 186
668 n
mi
Hp = 181
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6902327
63 X = -2124018
04
Y = 13079939
85 feet Y = 3963126
05 meter
Z = -16368412
99 Z = -4999361
95
XDOT = -23975
741557 XDOT = -7300
862636
YDOT = -4653
090226 feet/sec YDOT = -1499
942938 meter/sec
ZDOT = 6388
438533 ZDOT = 1911
712376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1781370
71 X = -542961
79
Y = 14638319
01 feet Y = 4461759
63 meter
Z = -16407261
57 Z = -5000933
33
XDOT = -23048
641581 XDOT = -7025
225954
YDOT = 4206
971158 feet/sec YDOT = 1282
284809 meter/sec
ZDOT = 6252
321732 ZDOT = 1905
707664
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 08067
61161342
00020000 00000-0 20000-3 0 9071
2 25544 51
6379 179
9823 0002114 217
7212 142
3804 15
76005261 12505
Satellite: ISS
Catalog Number: 25544
Epoch time: 08067
61161342 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 179
9823 deg
Eccentricity:
0002114
Arg of perigee: 217
7212 deg
Mean anomaly: 142
3804 deg
Mean motion: 15
76005261 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1250
Checksum: 268
Coasting Arc #9 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2008/068/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6182651
45 A = 6724077
09 meter
Y = 1204874
66 meter E =
0006305
Z = -2345399
44 I = 51
68390
XDOT = -2949
418108 Wp = 154
78602
YDOT = 4616
825310 meter/sec RA = 173
91609 deg
ZDOT = -5414
048354 TA = 51
62060
MA = 51
56398
Ha = 186
645 n
mi
Hp = 181
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20284289
54 X = 6180112
25
Y = 3953000
85 feet Y = 1273998
15 meter
Z = -7694880
04 Z = -2315370
75
XDOT = -9676
568595 XDOT = -2974
524779
YDOT = 15147
064664 feet/sec YDOT = 4583
702265 meter/sec
ZDOT = -17762
625832 ZDOT = -5428
437950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20358754
97 X = 6205348
51
Y = -3789365
99 feet Y = -1154998
76 meter
Z = -7579683
26 Z = -2310287
46
XDOT = -3619
343411 XDOT = -1103
175872
YDOT = 16120
889635 feet/sec YDOT = 4913
647161 meter/sec
ZDOT = -17817
181450 ZDOT = -5430
676906
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 08068
62614483
00020000 00000-0 20000-3 0 9083
2 25544 51
6375 174
7564 0002054 221
1809 138
9201 15
76030445 12661
Satellite: ISS
Catalog Number: 25544
Epoch time: 08068
62614483 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 174
7564 deg
Eccentricity:
0002054
Arg of perigee: 221
1809 deg
Mean anomaly: 138
9201 deg
Mean motion: 15
76030445 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1266
Checksum: 286
Coasting Arc #10 (Orbit 1281)
---------------------------------------
Vector Time (GMT): 2008/069/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3008790
18 A = 6717784
38 meter
Y = -4117908
30 meter E =
0007477
Z = 4367468
89 I = 51
69311
XDOT = 6789
350746 Wp = 74
52412
YDOT = 1368
795977 meter/sec RA = 168
72365 deg
ZDOT = -3379
933685 TA = 49
48840
MA = 49
42328
Ha = 186
294 n
mi
Hp = 181
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9871358
85 X = 3033397
38
Y = -13510197
82 feet Y = -4084124
26 meter
Z = 14328966
18 Z = 4382145
71
XDOT = 22274
772789 XDOT = 6789
959084
YDOT = 4490
800448 feet/sec YDOT = 1444
721433 meter/sec
ZDOT = -11089
021276 ZDOT = -3346
949852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3864898
20 X = 1178020
97
Y = -16230580
49 feet Y = -4947080
93 meter
Z = 14384688
44 Z = 4384453
04
XDOT = 21169
381070 XDOT = 6452
427350
YDOT = -4694
273284 feet/sec YDOT = -1430
814497 meter/sec
ZDOT = -10962
477323 ZDOT = -3341
363088
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 08069
64064822
00020000 00000-0 20000-3 0 9093
2 25544 51
6380 169
5302 0002008 232
4685 127
6297 15
76112107 12829
Satellite: ISS
Catalog Number: 25544
Epoch time: 08069
64064822 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 169
5302 deg
Eccentricity:
0002008
Arg of perigee: 232
4685 deg
Mean anomaly: 127
6297 deg
Mean motion: 15
76112107 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1282
Checksum: 284
Coasting Arc #11 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2008/070/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5594134
54 A = 6720884
23 meter
Y = -1238575
85 meter E =
0010993
Z = 3505283
57 I = 51
73088
XDOT = 3915
187710 Wp = 98
16831
YDOT = -4863
611693 meter/sec RA = 163
62740 deg
ZDOT = 4516
242989 TA = 303
49151
MA = 303
59651
Ha = 186
443 n
mi
Hp = 181
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18353459
77 X = -5596896
85
Y = -4063569
06 feet Y = -1301147
82 meter
Z = 11500274
17 Z = 3478100
67
XDOT = 12845
104036 XDOT = 3947
343304
YDOT = -15956
731275 feet/sec YDOT = -4819
649673 meter/sec
ZDOT = 14817
070173 ZDOT = 4535
341454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18509889
90 X = -5641814
44
Y = 3624125
43 feet Y = 1104633
43 meter
Z = 11395967
52 Z = 3473490
90
XDOT = 5597
200303 XDOT = 1706
026652
YDOT = -18373
771390 feet/sec YDOT = -5600
325520 meter/sec
ZDOT = 14889
649514 ZDOT = 4538
365172
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 08070
65512836
00020000 00000-0 20000-3 0 9101
2 25544 51
6371 164
3039 0001838 232
9216 127
1780 15
76123918 12985
Satellite: ISS
Catalog Number: 25544
Epoch time: 08070
65512836 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 164
3039 deg
Eccentricity:
0001838
Arg of perigee: 232
9216 deg
Mean anomaly: 127
1780 deg
Mean motion: 15
76123918 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1298
Checksum: 288
Coasting Arc #12 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2008/071/14:22:32
614
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3770524
98 A = 6720809
49 meter
Y = 4390156
74 meter E =
0003806
Z = -3421732
80 I = 51
75858
XDOT = -5972
922520 Wp = 108
08923
YDOT = -1542
247031 meter/sec RA = 158
43138 deg
ZDOT = 4606
042971 TA = 211
51839
MA = 211
54120
Ha = 186
271 n
mi
Hp = 180
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12370488
78 X = -3802713
98
Y = 14403401
37 feet Y = 4347812
42 meter
Z = -11226157
47 Z = -3440128
44
XDOT = -19596
202492 XDOT = -5977
608300
YDOT = -5059
865588 feet/sec YDOT = -1609
065618 meter/sec
ZDOT = 15111
689539 ZDOT = 4577
015188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5223833
95 X = -1592224
59
Y = 18210518
09 feet Y = 5550565
91 meter
Z = -11296112
82 Z = -3443055
19
XDOT = -18679
548644 XDOT = -5693
526427
YDOT = 3940
305536 feet/sec YDOT = 1201
005127 meter/sec
ZDOT = 15000
270146 ZDOT = 4572
082340
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 08071
60617994
00020000 00000-0 20000-3 0 9119
2 25544 51
6366 159
4040 0001666 236
6302 123
4703 15
76180814 13132
Satellite: ISS
Catalog Number: 25544
Epoch time: 08071
60617994 = yrday
fracday
Element set: 911
Inclination: 51
6366 deg
RA of node: 159
4040 deg
Eccentricity:
0001666
Arg of perigee: 236
6302 deg
Mean anomaly: 123
4703 deg
Mean motion: 15
76180814 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1313
Checksum: 273
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 may contain past, current and future orbital data 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
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