Date:
March 4th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 1186)
---------------------------------------
Vector Time (GMT): 2008/063/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -708117
47 A = 6716015
05 meter
Y = -4457981
74 meter E =
0007149
Z = 4971130
22 I = 51
51075
XDOT = 7384
315717 Wp = 145
17386
YDOT = 1013
903352 meter/sec RA = 199
84920 deg
ZDOT = 1953
953198 TA = 285
88348
MA = 285
96226
Ha = 187
167 n
mi
Hp = 181
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2323220
05 X = -682363
32
Y = -14625924
34 feet Y = -4465756
24 meter
Z = 16309482
34 Z = 4967752
88
XDOT = 24226
757601 XDOT = 7362
937536
YDOT = 3326
454567 feet/sec YDOT = 1096
359478 meter/sec
ZDOT = 6410
607606 ZDOT = 1989
773467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3576300
53 X = -1090056
40
Y = -14386254
74 feet Y = -4384930
45 meter
Z = 16296011
09 Z = 4967024
18
XDOT = 23329
364963 XDOT = 7110
790441
YDOT = 1644
276511 feet/sec YDOT = 501
175480 meter/sec
ZDOT = 6547
917166 ZDOT = 1995
805152
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
61661172
00020000 00000-0 20000-3 0 9006
2 25544 51
6375 200
5580 0002631 197
3086 162
7989 15
75899067 11871
Satellite: ISS
Catalog Number: 25544
Epoch time: 08063
61661172 = yrday
fracday
Element set: 900
Inclination: 51
6375 deg
RA of node: 200
5580 deg
Eccentricity:
0002631
Arg of perigee: 197
3086 deg
Mean anomaly: 162
7989 deg
Mean motion: 15
75899067 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1187
Checksum: 309
Coasting Arc #2 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2008/064/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6582723
69 A = 6726228
27 meter
Y = -831508
70 meter E =
0007255
Z = -1086784
28 I = 51
57361
XDOT = -346
998996 Wp = 43
39965
YDOT = -4932
564598 meter/sec RA = 194
66571 deg
ZDOT = 5904
155284 TA = 304
69295
MA = 304
76128
Ha = 187
045 n
mi
Hp = 181
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21596862
48 X = -6567657
11
Y = -2728046
93 feet Y = -905036
27 meter
Z = -3565565
23 Z = -1118725
75
XDOT = -1138
448151 XDOT = -320
497130
YDOT = -16182
954719 feet/sec YDOT = -4936
296555 meter/sec
ZDOT = 19370
588202 ZDOT = 5902
534146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21739175
22 X = -6626100
61
Y = -621934
30 feet Y = -189565
57 meter
Z = -3688010
74 Z = -1124105
67
XDOT = -2857
764843 XDOT = -871
046724
YDOT = -14400
314677 feet/sec YDOT = -4389
215914 meter/sec
ZDOT = 19363
779839 ZDOT = 5902
080095
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
56781217
00020000 00000-0 20000-3 0 9015
2 25544 51
6379 195
6595 0002363 201
4424 158
6642 15
75896593 12029
Satellite: ISS
Catalog Number: 25544
Epoch time: 08064
56781217 = yrday
fracday
Element set: 901
Inclination: 51
6379 deg
RA of node: 195
6595 deg
Eccentricity:
0002363
Arg of perigee: 201
4424 deg
Mean anomaly: 158
6642 deg
Mean motion: 15
75896593 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1202
Checksum: 306
Coasting Arc #3 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2008/065/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -161026
66 A = 6714605
74 meter
Y = 4197730
15 meter E =
0013847
Z = -5249989
57 I = 51
56379
XDOT = -7627
123439 Wp = 94
65429
YDOT = -892
268237 meter/sec RA = 189
52589 deg
ZDOT = -481
683241 TA = 170
77434
MA = 170
74888
Ha = 186
864 n
mi
Hp = 181
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -528302
70 X = -182451
49
Y = 13772080
53 feet Y = 4195809
35 meter
Z = -17224375
24 Z = -5250824
11
XDOT = -25023
370862 XDOT = -7614
239224
YDOT = -2927
389230 feet/sec YDOT = -977
487073 meter/sec
ZDOT = -1580
325593 ZDOT = -518
703547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1143912
45 X = 348664
51
Y = 13731291
25 feet Y = 4185297
57 meter
Z = -17227057
60 Z = -5250807
16
XDOT = -24183
358883 XDOT = -7371
087788
YDOT = -137
042767 feet/sec YDOT = -41
770636 meter/sec
ZDOT = -1722
245048 ZDOT = -524
940291
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
58239234
00020000 00000-0 20000-3 0 9026
2 25544 51
6382 190
4344 0002349 207
4395 152
6646 15
75962524 12188
Satellite: ISS
Catalog Number: 25544
Epoch time: 08065
58239234 = yrday
fracday
Element set: 902
Inclination: 51
6382 deg
RA of node: 190
4344 deg
Eccentricity:
0002349
Arg of perigee: 207
4395 deg
Mean anomaly: 152
6646 deg
Mean motion: 15
75962524 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1218
Checksum: 296
Coasting Arc #4 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2008/066/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6675378
38 A = 6726450
98 meter
Y = 721491
87 meter E =
0012684
Z = -266108
78 I = 51
63301
XDOT = -746
464997 Wp = 147
10170
YDOT = 4733
971370 meter/sec RA = 184
37073 deg
ZDOT = -6034
328164 TA = 35
79353
MA = 35
70859
Ha = 186
794 n
mi
Hp = 181
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21900847
71 X = 6668107
10
Y = 2367099
32 feet Y = 796099
08 meter
Z = -873060
31 Z = -233698
24
XDOT = -2449
032142 XDOT = -770
032492
YDOT = 15531
402134 feet/sec YDOT = 4725
491694 meter/sec
ZDOT = -19797
664581 ZDOT = -6038
012052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22026662
42 X = 6713726
71
Y = -527208
48 feet Y = -160693
14 meter
Z = -748810
71 Z = -228237
51
XDOT = -317
316754 XDOT = -96
718146
YDOT = 14097
568009 feet/sec YDOT = 4296
938729 meter/sec
ZDOT = -19811
192118 ZDOT = -6038
451357
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
59693969
00020000 00000-0 20000-3 0 9038
2 25544 51
6380 185
2088 0002303 209
3895 150
7140 15
76007724 12348
Satellite: ISS
Catalog Number: 25544
Epoch time: 08066
59693969 = yrday
fracday
Element set: 903
Inclination: 51
6380 deg
RA of node: 185
2088 deg
Eccentricity:
0002303
Arg of perigee: 209
3895 deg
Mean anomaly: 150
7140 deg
Mean motion: 15
76007724 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1234
Checksum: 298
Coasting Arc #5 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2008/067/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1155098
62 A = 6714460
18 meter
Y = -4115706
20 meter E =
0001786
Z = 5176451
39 I = 51
62365
XDOT = 7590
820377 Wp = 79
45518
YDOT = 758
396587 meter/sec RA = 179
20708 deg
ZDOT = -1090
226953 TA = 20
94531
MA = 20
93800
Ha = 186
484 n
mi
Hp = 181
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3789693
64 X = 1175889
41
Y = -13502973
09 feet Y = -4102672
45 meter
Z = 16983108
23 Z = 5182113
68
XDOT = 24904
266328 XDOT = 7587
071738
YDOT = 2488
177779 feet/sec YDOT = 843
260403 meter/sec
ZDOT = -3576
860081 ZDOT = -1053
360583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1650991
15 X = 503222
10
Y = -13901308
87 feet Y = -4237118
95 meter
Z = 17004289
61 Z = 5182907
47
XDOT = 24003
944587 XDOT = 7316
402310
YDOT = -1354
114153 feet/sec YDOT = -412
733994 meter/sec
ZDOT = -3435
528339 ZDOT = -1047
149038
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
61145149
00020000 00000-0 20000-3 0 9045
2 25544 51
6389 179
9825 0002151 218
4357 141
6654 15
76106977 12508
Satellite: ISS
Catalog Number: 25544
Epoch time: 08067
61145149 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 179
9825 deg
Eccentricity:
0002151
Arg of perigee: 218
4357 deg
Mean anomaly: 141
6654 deg
Mean motion: 15
76106977 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1250
Checksum: 305
Coasting Arc #6 (Orbit 1265)
---------------------------------------
Vector Time (GMT): 2008/068/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6486982
86 A = 6725041
98 meter
Y = -627490
15 meter E =
0012295
Z = 1636552
67 I = 51
68829
XDOT = 1917
519643 Wp = 66
95485
YDOT = -4762
437226 meter/sec RA = 174
08175 deg
ZDOT = 5745
385291 TA = 311
12803
MA = 311
23408
Ha = 186
488 n
mi
Hp = 181
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21282752
18 X = -6487434
03
Y = -2058694
73 feet Y = -700033
64 meter
Z = 5369267
30 Z = 1605038
25
XDOT = 6291
074943 XDOT = 1942
721710
YDOT = -15624
794048 feet/sec YDOT = -4740
852889 meter/sec
ZDOT = 18849
689274 ZDOT = 5754
762227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21360104
30 X = -6510559
79
Y = 1490808
37 feet Y = 454398
39 meter
Z = 5248450
26 Z = 1599727
64
XDOT = 3626
300722 XDOT = 1105
296460
YDOT = -14874
228737 feet/sec YDOT = -4533
664919 meter/sec
ZDOT = 18885
022030 ZDOT = 5756
154715
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
62593239
00020000 00000-0 20000-3 0 9055
2 25544 51
6387 174
7568 0001983 221
4503 138
6511 15
76121012 12664
Satellite: ISS
Catalog Number: 25544
Epoch time: 08068
62593239 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 174
7568 deg
Eccentricity:
0001983
Arg of perigee: 221
4503 deg
Mean anomaly: 138
6511 deg
Mean motion: 15
76121012 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1266
Checksum: 291
Coasting Arc #7 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2008/069/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2183682
85 A = 6716130
00 meter
Y = 4242435
67 meter E =
0010739
Z = -4736726
06 I = 51
68711
XDOT = -7185
000758 Wp = 117
53803
YDOT = -730
296809 meter/sec RA = 168
89821 deg
ZDOT = 2657
985005 TA = 178
57953
MA = 178
57648
Ha = 186
315 n
mi
Hp = 180
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7164313
82 X = -2207950
09
Y = 13918752
21 feet Y = 4217880
32 meter
Z = -15540439
82 Z = -4747393
71
XDOT = -23572
837131 XDOT = -7189
212406
YDOT = -2395
986905 feet/sec YDOT = -810
666868 meter/sec
ZDOT = 8720
423244 ZDOT = 2623
070304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4422260
66 X = -1347905
05
Y = 14974880
66 feet Y = 4564343
63 meter
Z = -15580785
77 Z = -4749023
50
XDOT = -22571
182100 XDOT = -6879
696304
YDOT = 2269
437423 feet/sec YDOT = 691
724527 meter/sec
ZDOT = 8586
560717 ZDOT = 2617
183707
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
57697652
00020000 00000-0 20000-3 0 9065
2 25544 51
6378 169
8577 0001831 226
7563 133
3449 15
76191760 12811
Satellite: ISS
Catalog Number: 25544
Epoch time: 08069
57697652 = yrday
fracday
Element set: 906
Inclination: 51
6378 deg
RA of node: 169
8577 deg
Eccentricity:
0001831
Arg of perigee: 226
7563 deg
Mean anomaly: 133
3449 deg
Mean motion: 15
76191760 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1281
Checksum: 328
Coasting Arc #8 (Orbit 1296)
---------------------------------------
Vector Time (GMT): 2008/070/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5985116
60 A = 6722109
13 meter
Y = 705635
48 meter E =
0003978
Z = -2976581
67 I = 51
73483
XDOT = -3069
270982 Wp = 135
81690
YDOT = 4994
272988 meter/sec RA = 163
79572 deg
ZDOT = -4994
315205 TA = 78
51718
MA = 78
47251
Ha = 186
287 n
mi
Hp = 180
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19636209
32 X = 5991240
93
Y = 2315077
05 feet Y = 772598
48 meter
Z = -9765687
88 Z = -2947491
18
XDOT = -10069
786687 XDOT = -3100
628137
YDOT = 16385
410066 feet/sec YDOT = 4959
774914 meter/sec
ZDOT = -16385
548572 ZDOT = -5009
302284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19758086
58 X = 6022264
79
Y = -1650634
66 feet Y = -503113
44 meter
Z = -9654137
86 Z = -2942581
22
XDOT = -6636
004954 XDOT = -2022
654310
YDOT = 16602
603454 feet/sec YDOT = 5060
473533 meter/sec
ZDOT = -16442
358298 ZDOT = -5011
630809
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
59139181
00020000 00000-0 20000-3 0 9078
2 25544 51
6370 164
6308 0001789 232
2373 127
8630 15
76213565 12976
Satellite: ISS
Catalog Number: 25544
Epoch time: 08070
59139181 = yrday
fracday
Element set: 907
Inclination: 51
6370 deg
RA of node: 164
6308 deg
Eccentricity:
0001789
Arg of perigee: 232
2373 deg
Mean anomaly: 127
8630 deg
Mean motion: 15
76213565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1297
Checksum: 296
Coasting Arc #9 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2008/071/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3120286
78 A = 6718992
81 meter
Y = -4506500
05 meter E =
0009547
Z = 3878657
06 I = 51
75352
XDOT = 6459
741316 Wp = 83
27333
YDOT = 937
595828 meter/sec RA = 158
60022 deg
ZDOT = -4097
679370 TA = 49
37736
MA = 49
29436
Ha = 185
966 n
mi
Hp = 180
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10237161
35 X = 3151605
42
Y = -14785105
14 feet Y = -4471431
90 meter
Z = 12725252
84 Z = 3893891
74
XDOT = 21193
377022 XDOT = 6468
682678
YDOT = 3076
101797 feet/sec YDOT = 1009
882117 meter/sec
ZDOT = -13443
829955 ZDOT = -4066
276252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6733463
51 X = 2052359
68
Y = -16630819
91 feet Y = -5069073
91 meter
Z = 12783081
17 Z = 3896283
14
XDOT = 20219
119108 XDOT = 6162
787504
YDOT = -2078
825675 feet/sec YDOT = -633
626066 meter/sec
ZDOT = -13323
382492 ZDOT = -4060
966984
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
60577153
00020000 00000-0 20000-3 0 9087
2 25544 51
6374 159
4036 0001734 244
9689 115
1295 15
76308346 13138
Satellite: ISS
Catalog Number: 25544
Epoch time: 08071
60577153 = yrday
fracday
Element set: 908
Inclination: 51
6374 deg
RA of node: 159
4036 deg
Eccentricity:
0001734
Arg of perigee: 244
9689 deg
Mean anomaly: 115
1295 deg
Mean motion: 15
76308346 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1313
Checksum: 297
Coasting Arc #10 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2008/072/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5221056
38 A = 6718300
58 meter
Y = -1006583
15 meter E =
0009401
Z = 4101090
70 I = 51
77712
XDOT = 4028
804160 Wp = 109
84914
YDOT = -5355
749688 meter/sec RA = 153
50756 deg
ZDOT = 3804
354023 TA = 301
17402
MA = 301
26616
Ha = 186
098 n
mi
Hp = 180
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17129450
06 X = -5229334
92
Y = -3302438
15 feet Y = -1065014
17 meter
Z = 13455021
99 Z = 4075706
74
XDOT = 13217
861418 XDOT = 4069
912696
YDOT = -17571
357245 feet/sec YDOT = -5310
467357 meter/sec
ZDOT = 12481
476455 ZDOT = 3824
025931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17501726
45 X = -5334526
22
Y = 790732
59 feet Y = 241015
29 meter
Z = 13357622
82 Z = 4071403
44
XDOT = 8756
095079 XDOT = 2668
857780
YDOT = -18871
466941 feet/sec YDOT = -5752
023124 meter/sec
ZDOT = 12556
218326 ZDOT = 3827
135346
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 08072
62011977
00020000 00000-0 20000-3 0 9098
2 25544 51
6366 154
1763 0001608 246
3160 113
7836 15
76338769 13292
Satellite: ISS
Catalog Number: 25544
Epoch time: 08072
62011977 = yrday
fracday
Element set: 909
Inclination: 51
6366 deg
RA of node: 154
1763 deg
Eccentricity:
0001608
Arg of perigee: 246
3160 deg
Mean anomaly: 113
7836 deg
Mean motion: 15
76338769 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1329
Checksum: 302
Coasting Arc #11 (Orbit 1343)
---------------------------------------
Vector Time (GMT): 2008/073/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3838708
43 A = 6722234
97 meter
Y = 4831881
52 meter E =
0003519
Z = -2664582
62 I = 51
81634
XDOT = -5462
436354 Wp = 49
44474
YDOT = -1460
306962 meter/sec RA = 148
31681 deg
ZDOT = 5228
058763 TA = 280
26937
MA = 280
30905
Ha = 185
919 n
mi
Hp = 180
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12594187
78 X = -3879509
98
Y = 15852629
65 feet Y = 4788726
75 meter
Z = -8742068
96 Z = -2683330
11
XDOT = -17921
379115 XDOT = -5471
097852
YDOT = -4791
033339 feet/sec YDOT = -1521
439450 meter/sec
ZDOT = 17152
423762 ZDOT = 5201
501328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8195684
60 X = -2498044
67
Y = 18479689
01 feet Y = 5632609
21 meter
Z = -8813345
01 Z = -2686307
56
XDOT = -17296
353275 XDOT = -5271
928478
YDOT = 450
398283 feet/sec YDOT = 137
281397 meter/sec
ZDOT = 17050
462788 ZDOT = 5196
981058
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 08073
57104145
00020000 00000-0 20000-3 0 9105
2 25544 51
6362 149
2754 0001454 252
5551 107
5455 15
76389257 13448
Satellite: ISS
Catalog Number: 25544
Epoch time: 08073
57104145 = yrday
fracday
Element set: 910
Inclination: 51
6362 deg
RA of node: 149
2754 deg
Eccentricity:
0001454
Arg of perigee: 252
5551 deg
Mean anomaly: 107
5455 deg
Mean motion: 15
76389257 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1344
Checksum: 285
Coasting Arc #12 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2008/074/13:34:31
211
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4276932
32 A = 6714880
07 meter
Y = 1635268
66 meter E =
0011097
Z = -4921703
06 I = 51
81635
XDOT = -4704
072663 Wp = 73
29777
YDOT = 5679
207237 meter/sec RA = 143
21568 deg
ZDOT = -2201
802313 TA = 175
36305
MA = 175
35277
Ha = 185
912 n
mi
Hp = 180
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14031930
19 X = 4282237
14
Y = 5365054
67 feet Y = 1683125
44 meter
Z = -16147319
76 Z = -4900913
03
XDOT = -15433
309261 XDOT = -4756
532967
YDOT = 18632
569676 feet/sec YDOT = 5626
310301 meter/sec
ZDOT = -7223
760870 ZDOT = -2224
781882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15041541
99 X = 4584662
00
Y = 1415764
20 feet Y = 431524
93 meter
Z = -16067434
08 Z = -4897353
91
XDOT = -9779
162812 XDOT = -2980
688825
YDOT = 20958
250727 feet/sec YDOT = 6388
074822 meter/sec
ZDOT = -7311
171146 ZDOT = -2228
444965
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 08074
58532546
00020000 00000-0 20000-3 0 9118
2 25544 51
6369 144
0472 0001381 259
3979 100
7030 15
76411998 13603
Satellite: ISS
Catalog Number: 25544
Epoch time: 08074
58532546 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 144
0472 deg
Eccentricity:
0001381
Arg of perigee: 259
3979 deg
Mean anomaly: 100
7030 deg
Mean motion: 15
76411998 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1360
Checksum: 293
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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