Date:
July 10th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7803 84 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 930)
---------------------------------------
Vector Time (GMT): 2009/189/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3691419
76 A = 6721247
26 meter
Y = -2888580
98 meter E =
0004805
Z = 4812970
40 I = 51
52542
XDOT = 6200
164306 Wp = 136
64069
YDOT = 3872
134531 meter/sec RA = 196
64514 deg
ZDOT = -2433
443575 TA = 337
14251
MA = 337
16389
Ha = 190
471 n
mi
Hp = 183
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12110957
22 X = 3700065
85
Y = -9476971
72 feet Y = -2847253
86 meter
Z = 15790585
30 Z = 4830923
53
XDOT = 20341
746411 XDOT = 6168
225667
YDOT = 12703
853448 feet/sec YDOT = 3941
290240 meter/sec
ZDOT = -7983
738763 ZDOT = -2403
400559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9636759
01 X = -2937284
15
Y = -11891009
32 feet Y = -3624379
64 meter
Z = 15860883
80 Z = 4834397
38
XDOT = 11562
492218 XDOT = 3524
247628
YDOT = -19853
347880 feet/sec YDOT = -6051
300434 meter/sec
ZDOT = -7865
598311 ZDOT = -2397
434365
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 09189
50182921
00010596 00000-0 82463-4 0 9005
2 25544 51
6365 197
4559 0007515 200
3691 159
7174 15
74260862 9315
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189
50182921 = yrday
fracday
Element set: 900
Inclination: 51
6365 deg
RA of node: 197
4559 deg
Eccentricity:
0007515
Arg of perigee: 200
3691 deg
Mean anomaly: 159
7174 deg
Mean motion: 15
74260862 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 931
Checksum: 320
Coasting Arc #2 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2009/190/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5629487
37 A = 6729390
62 meter
Y = -2943230
25 meter E =
0010475
Z = 2215968
06 I = 51
58166
XDOT = 4045
631419 Wp = 102
46787
YDOT = -3601
714025 meter/sec RA = 191
54031 deg
ZDOT = 5469
925122 TA = 282
39119
MA = 282
50841
Ha = 190
411 n
mi
Hp = 184
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18469446
74 X = -5606921
86
Y = -9656267
21 feet Y = -3006056
64 meter
Z = 7270236
42 Z = 2188674
82
XDOT = 13273
068960 XDOT = 4059
034268
YDOT = -11816
647065 feet/sec YDOT = -3556
399320 meter/sec
ZDOT = 17945
948562 ZDOT = 5489
610462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9085414
96 X = -2769234
48
Y = 18798085
24 feet Y = 5729656
38 meter
Z = 7162927
01 Z = 2183260
15
XDOT = -10842
802971 XDOT = -3304
886345
YDOT = -12138
423493 feet/sec YDOT = -3699
791481 meter/sec
ZDOT = 18023
010014 ZDOT = 5493
413452
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 09190
51749930
00010596 00000-0 82463-4 0 9018
2 25544 51
6366 192
2375 0007420 204
4043 155
6770 15
74251556 9470
Satellite: ISS
Catalog Number: 25544
Epoch time: 09190
51749930 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 192
2375 deg
Eccentricity:
0007420
Arg of perigee: 204
4043 deg
Mean anomaly: 155
6770 deg
Mean motion: 15
74251556 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 947
Checksum: 308
Coasting Arc #3 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2009/191/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3368611
53 A = 6721656
96 meter
Y = 3399115
15 meter E =
0012480
Z = -4730550
70 I = 51
58598
XDOT = -6627
770871 Wp = 144
87310
YDOT = -2859
608739 meter/sec RA = 186
35846 deg
ZDOT = 2658
300054 TA = 151
33206
MA = 151
26340
Ha = 190
207 n
mi
Hp = 184
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11051875
08 X = -3383390
87
Y = 11151952
60 feet Y = 3361363
37 meter
Z = -15520179
45 Z = -4746950
58
XDOT = -21744
655090 XDOT = -6608
214977
YDOT = -9381
918435 feet/sec YDOT = -2933
615368 meter/sec
ZDOT = 8721
456870 ZDOT = 2626
149983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11662634
63 X = 3554771
04
Y = 10416172
47 feet Y = 3174849
37 meter
Z = -15584359
61 Z = -4750112
81
XDOT = -7570
224304 XDOT = -2307
404368
YDOT = 21367
865737 feet/sec YDOT = 6512
925477 meter/sec
ZDOT = 8595
071698 ZDOT = 2619
777853
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 09191
46967903
00010596 00000-0 82463-4 0 9026
2 25544 51
6373 187
3452 0007448 208
9865 151
0886 15
74254418 9625
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191
46967903 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 187
3452 deg
Eccentricity:
0007448
Arg of perigee: 208
9865 deg
Mean anomaly: 151
0886 deg
Mean motion: 15
74254418 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 962
Checksum: 341
Coasting Arc #4 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2009/192/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5920850
24 A = 6728889
38 meter
Y = 2055586
14 meter E =
0010131
Z = -2432009
55 I = 51
63916
XDOT = -3643
265442 Wp = 180
00720
YDOT = 4163
599027 meter/sec RA = 181
26011 deg
ZDOT = -5360
492911 TA = 27
46710
MA = 27
41359
Ha = 190
146 n
mi
Hp = 184
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19425361
68 X = 5909238
37
Y = 6744049
01 feet Y = 2121731
91 meter
Z = -7979033
94 Z = -2403274
43
XDOT = -11952
970610 XDOT = -3663
512812
YDOT = 13660
101796 feet/sec YDOT = 4122
745314 meter/sec
ZDOT = -17586
919000 ZDOT = -5378
240339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5464997
60 X = 1665731
27
Y = -19868323
10 feet Y = -6055864
88 meter
Z = -7866091
42 Z = -2397584
67
XDOT = 12951
824825 XDOT = 3947
716207
YDOT = 10539
786728 feet/sec YDOT = 3212
526995 meter/sec
ZDOT = -17656
346911 ZDOT = -5381
654539
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 09192
48532804
00010596 00000-0 82463-4 0 9038
2 25544 51
6363 182
1264 0007457 212
2896 147
7812 15
74275236 9789
Satellite: ISS
Catalog Number: 25544
Epoch time: 09192
48532804 = yrday
fracday
Element set: 903
Inclination: 51
6363 deg
RA of node: 182
1264 deg
Eccentricity:
0007457
Arg of perigee: 212
2896 deg
Mean anomaly: 147
7812 deg
Mean motion: 15
74275236 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 978
Checksum: 327
Coasting Arc #5 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2009/193/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2967294
79 A = 6721897
47 meter
Y = -3869927
30 meter E =
0003620
Z = 4622834
13 I = 51
64584
XDOT = 6898
945174 Wp = 129
45447
YDOT = 1827
003079 meter/sec RA = 176
07958 deg
ZDOT = -2899
592809 TA = 349
22683
MA = 349
23458
Ha = 189
761 n
mi
Hp = 184
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9735219
11 X = 2987891
79
Y = -12696611
88 feet Y = -3836630
58 meter
Z = 15166778
63 Z = 4637298
72
XDOT = 22634
334562 XDOT = 6892
088111
YDOT = 5994
104591 feet/sec YDOT = 1904
113079 meter/sec
ZDOT = -9513
099766 ZDOT = -2866
094570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13445543
96 X = -4098201
80
Y = -8571869
09 feet Y = -2612705
70 meter
Z = 15223338
22 Z = 4640073
49
XDOT = 3485
716460 XDOT = 1062
446377
YDOT = -22124
321054 feet/sec YDOT = -6743
493057 meter/sec
ZDOT = -9381
458865 ZDOT = -2859
468662
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 09193
50096532
00010596 00000-0 82463-4 0 9046
2 25544 51
6361 176
9078 0007385 217
2270 142
8382 15
74315725 9946
Satellite: ISS
Catalog Number: 25544
Epoch time: 09193
50096532 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 176
9078 deg
Eccentricity:
0007385
Arg of perigee: 217
2270 deg
Mean anomaly: 142
8382 deg
Mean motion: 15
74315725 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 994
Checksum: 322
Coasting Arc #6 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2009/194/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6080821
11 A = 6728221
05 meter
Y = -1145778
13 meter E =
0008873
Z = 2638596
36 I = 51
69683
XDOT = 3159
188381 Wp = 107
40052
YDOT = -4683
394414 meter/sec RA = 170
98866 deg
ZDOT = 5229
861132 TA = 282
58882
MA = 282
68804
Ha = 189
625 n
mi
Hp = 184
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19950200
48 X = -6080374
61
Y = -3759114
59 feet Y = -1213775
19 meter
Z = 8656812
22 Z = 2609056
91
XDOT = 10364
791276 XDOT = 3185
918557
YDOT = -15365
467238 feet/sec YDOT = -4647
917567 meter/sec
ZDOT = 17158
337048 ZDOT = 5245
272840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1755657
15 X = -535124
30
Y = 20274494
53 feet Y = 6179665
93 meter
Z = 8540748
15 Z = 2603220
04
XDOT = -14829
536993 XDOT = -4520
042875
YDOT = -8561
380539 feet/sec YDOT = -2609
508788 meter/sec
ZDOT = 17218
570045 ZDOT = 5248
220150
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 09194
51659128
00010596 00000-0 82463-4 0 9055
2 25544 51
6360 171
6898 0007498 221
3097 138
7499 15
74355328 10101
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194
51659128 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 171
6898 deg
Eccentricity:
0007498
Arg of perigee: 221
3097 deg
Mean anomaly: 138
7499 deg
Mean motion: 15
74355328 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 336
Coasting Arc #7 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2009/195/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2539765
01 A = 6722419
41 meter
Y = 4307740
72 meter E =
0009551
Z = -4500697
45 I = 51
70612
XDOT = -6970
827691 Wp = 154
54046
YDOT = -807
028845 meter/sec RA = 165
80912 deg
ZDOT = 3155
252793 TA = 146
99003
MA = 146
93037
Ha = 189
428 n
mi
Hp = 184
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8332562
36 X = -2565882
63
Y = 14133007
61 feet Y = 4279194
00 meter
Z = -14766067
74 Z = -4513098
60
XDOT = -22870
169589 XDOT = -6976
612870
YDOT = -2647
732431 feet/sec YDOT = -885
013383 meter/sec
ZDOT = 10351
879241 ZDOT = 3121
374474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14996178
20 X = 4570835
11
Y = 6546394
31 feet Y = 1995340
99 meter
Z = -14814506
97 Z = -4515461
73
XDOT = 515
432028 XDOT = 157
103682
YDOT = 21988
737308 feet/sec YDOT = 6702
167131 meter/sec
ZDOT = 10218
788528 ZDOT = 3114
686743
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 09195
46873254
00010596 00000-0 82463-4 0 9069
2 25544 51
6356 166
7969 0007287 225
4581 134
5981 15
74316110 10251
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195
46873254 = yrday
fracday
Element set: 906
Inclination: 51
6356 deg
RA of node: 166
7969 deg
Eccentricity:
0007287
Arg of perigee: 225
4581 deg
Mean anomaly: 134
5981 deg
Mean motion: 15
74316110 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1025
Checksum: 330
Coasting Arc #8 (Orbit 1040)
---------------------------------------
Vector Time (GMT): 2009/196/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6070090
57 A = 6727643
67 meter
Y = 279787
61 meter E =
0006978
Z = -2877167
17 I = 51
75237
XDOT = -2640
129526 Wp = 191
66277
YDOT = 5159
586526 meter/sec RA = 160
72372 deg
ZDOT = -5072
832709 TA = 21
35579
MA = 21
32669
Ha = 189
302 n
mi
Hp = 185
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19914995
32 X = 6080487
56
Y = 917938
36 feet Y = 347725
37 meter
Z = -9439524
85 Z = -2847653
38
XDOT = -8661
842277 XDOT = -2672
985771
YDOT = 16927
777317 feet/sec YDOT = 5129
879909 meter/sec
ZDOT = -16643
151932 ZDOT = -5085
737696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1754481
46 X = -534765
95
Y = -19913478
30 feet Y = -6069628
19 meter
Z = -9323596
71 Z = -2841832
28
XDOT = 16466
677515 XDOT = 5019
043307
YDOT = 6358
089097 feet/sec YDOT = 1937
945557 meter/sec
ZDOT = -16693
525964 ZDOT = -5088
186714
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 09196
48433800
00010596 00000-0 82463-4 0 9072
2 25544 51
6355 161
5778 0007232 229
4611 130
5923 15
74356888 10415
Satellite: ISS
Catalog Number: 25544
Epoch time: 09196
48433800 = yrday
fracday
Element set: 907
Inclination: 51
6355 deg
RA of node: 161
5778 deg
Eccentricity:
0007232
Arg of perigee: 229
4611 deg
Mean anomaly: 130
5923 deg
Mean motion: 15
74356888 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1041
Checksum: 317
Coasting Arc #9 (Orbit 1056)
---------------------------------------
Vector Time (GMT): 2009/197/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2045908
07 A = 6722807
52 meter
Y = -4696262
23 meter E =
0003135
Z = 4350649
06 I = 51
76385
XDOT = 6896
334570 Wp = 109
56776
YDOT = -170
500243 meter/sec RA = 155
54631 deg
ZDOT = -3426
109733 TA = 14
92964
MA = 14
92039
Ha = 188
944 n
mi
Hp = 185
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6712296
82 X = 2077135
71
Y = -15407684
50 feet Y = -4673209
66 meter
Z = 14273783
02 Z = 4360663
35
XDOT = 22625
769585 XDOT = 6914
372032
YDOT = -559
384000 feet/sec YDOT = -93
280093 meter/sec
ZDOT = -11240
517497 ZDOT = -3392
563479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16229350
53 X = -4946706
04
Y = -4235956
49 feet Y = -1291119
54 meter
Z = 14312840
59 Z = 4362553
81
XDOT = -4275
555007 XDOT = -1303
189166
YDOT = -21164
880793 feet/sec YDOT = -6451
055666 meter/sec
ZDOT = -11108
766878 ZDOT = -3385
952145
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 09197
49993123
00010596 00000-0 82463-4 0 9084
2 25544 51
6351 156
3592 0007317 234
6650 125
3830 15
74379630 10578
Satellite: ISS
Catalog Number: 25544
Epoch time: 09197
49993123 = yrday
fracday
Element set: 908
Inclination: 51
6351 deg
RA of node: 156
3592 deg
Eccentricity:
0007317
Arg of perigee: 234
6650 deg
Mean anomaly: 125
3830 deg
Mean motion: 15
74379630 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1057
Checksum: 322
Coasting Arc #10 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2009/198/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5937618
42 A = 6726835
31 meter
Y = 550974
03 meter E =
0007344
Z = 3110621
37 I = 51
80476
XDOT = 2049
728030 Wp = 112
63657
YDOT = -5582
718614 meter/sec RA = 150
46714 deg
ZDOT = 4889
521587 TA = 283
41332
MA = 283
49517
Ha = 188
775 n
mi
Hp = 185
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19480375
39 X = -5958449
06
Y = 1807657
57 feet Y = 484459
15 meter
Z = 10205450
68 Z = 3081725
86
XDOT = 6724
829495 XDOT = 2088
250158
YDOT = -18316
005951 feet/sec YDOT = -5559
582719 meter/sec
ZDOT = 16041
737491 ZDOT = 4899
571894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5053548
11 X = 1540321
46
Y = 18960947
92 feet Y = 5779296
93 meter
Z = 10091976
04 Z = 3076034
30
XDOT = -17784
775272 XDOT = -5420
799503
YDOT = -3839
992924 feet/sec YDOT = -1170
429843 meter/sec
ZDOT = 16080
895707 ZDOT = 4901
457012
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 09198
51551186
00010596 00000-0 82463-4 0 9098
2 25544 51
6355 151
1405 0007450 237
7878 122
2563 15
74431616 10732
Satellite: ISS
Catalog Number: 25544
Epoch time: 09198
51551186 = yrday
fracday
Element set: 909
Inclination: 51
6355 deg
RA of node: 151
1405 deg
Eccentricity:
0007450
Arg of perigee: 237
7878 deg
Mean anomaly: 122
2563 deg
Mean motion: 15
74431616 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1073
Checksum: 310
Coasting Arc #11 (Orbit 1087)
---------------------------------------
Vector Time (GMT): 2009/199/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1518327
34 A = 6723445
52 meter
Y = 5048402
37 meter E =
0006219
Z = -4177888
97 I = 51
81859
XDOT = -6660
038038 Wp = 169
88510
YDOT = 1068
104627 meter/sec RA = 145
29053 deg
ZDOT = 3705
879346 TA = 137
91523
MA = 137
86745
Ha = 188
530 n
mi
Hp = 185
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4981388
92 X = -1554371
20
Y = 16562999
90 feet Y = 5031222
75 meter
Z = -13706984
80 Z = -4185351
65
XDOT = -21850
518496 XDOT = -6689
489236
YDOT = 3504
280273 feet/sec YDOT = 993
462862 meter/sec
ZDOT = 12158
396803 ZDOT = 3673
453577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17182488
22 X = 5237222
41
Y = 1764230
84 feet Y = 537737
56 meter
Z = -13736019
13 Z = -4186738
63
XDOT = 7614
208214 XDOT = 2320
810664
YDOT = 19646
114601 feet/sec YDOT = 5988
135730 meter/sec
ZDOT = 12031
066515 ZDOT = 3667
069074
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 09199
46761071
00010596 00000-0 82463-4 0 9101
2 25544 51
6356 146
2473 0007281 242
8276 117
2146 15
74390247 10885
Satellite: ISS
Catalog Number: 25544
Epoch time: 09199
46761071 = yrday
fracday
Element set: 910
Inclination: 51
6356 deg
RA of node: 146
2473 deg
Eccentricity:
0007281
Arg of perigee: 242
8276 deg
Mean anomaly: 117
2146 deg
Mean motion: 15
74390247 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1088
Checksum: 316
Coasting Arc #12 (Orbit 1103)
---------------------------------------
Vector Time (GMT): 2009/200/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5676777
19 A = 6726096
26 meter
Y = -1287437
38 meter E =
0003587
Z = -3365241
87 I = 51
85260
XDOT = -1418
241779 Wp = 212
79506
YDOT = 5955
643917 meter/sec RA = 140
21611 deg
ZDOT = -4671
502919 TA = 6
73110
MA = 6
72629
Ha = 188
378 n
mi
Hp = 185
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18624597
09 X = 5707099
25
Y = -4223875
93 feet Y = -1223786
16 meter
Z = -11040819
78 Z = -3337590
86
XDOT = -4653
024210 XDOT = -1462
040244
YDOT = 19539
514162 feet/sec YDOT = 5939
540306 meter/sec
ZDOT = -15326
453146 ZDOT = -4678
497943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7898352
37 X = -2407417
80
Y = -17456188
94 feet Y = -5320646
39 meter
Z = -10932243
30 Z = -3332147
76
XDOT = 18784
991938 XDOT = 5725
665543
YDOT = 1114
531876 feet/sec YDOT = 339
709316 meter/sec
ZDOT = -15353
608801 ZDOT = -4679
779962
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 09200
48316979
00010596 00000-0 82463-4 0 9110
2 25544 51
6366 141
0282 0007275 247
1816 112
8579 15
74437923 11041
Satellite: ISS
Catalog Number: 25544
Epoch time: 09200
48316979 = yrday
fracday
Element set: 911
Inclination: 51
6366 deg
RA of node: 141
0282 deg
Eccentricity:
0007275
Arg of perigee: 247
1816 deg
Mean anomaly: 112
8579 deg
Mean motion: 15
74437923 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1104
Checksum: 311
Coasting Arc #13 (Orbit 1119)
---------------------------------------
Vector Time (GMT): 2009/201/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 935260
43 A = 6723989
58 meter
Y = -5341042
76 meter E =
0003791
Z = 3972865
26 I = 51
86863
XDOT = 6312
479162 Wp = 93
05685
YDOT = -1869
699401 meter/sec RA = 135
04235 deg
ZDOT = -3996
564876 TA = 38
23396
MA = 38
20708
Ha = 188
022 n
mi
Hp = 185
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3068439
74 X = 975616
18
Y = -17523106
16 feet Y = -5330359
24 meter
Z = 13034334
83 Z = 3977505
70
XDOT = 20710
233471 XDOT = 6352
331620
YDOT = -6134
184388 feet/sec YDOT = -1798
885982 meter/sec
ZDOT = -13112
089489 ZDOT = -3965
802825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17753759
16 X = -5411345
79
Y = 900287
60 feet Y = 274407
66 meter
Z = 13052278
53 Z = 3978334
49
XDOT = -10453
574455 XDOT = -3186
249494
YDOT = -17653
749389 feet/sec YDOT = -5380
862814 meter/sec
ZDOT = -12991
301731 ZDOT = -3959
748767
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 09201
49871724
00010596 00000-0 82463-4 0 9127
2 25544 51
6372 135
8097 0007334 251
4023 108
6344 15
74455607 11207
Satellite: ISS
Catalog Number: 25544
Epoch time: 09201
49871724 = yrday
fracday
Element set: 912
Inclination: 51
6372 deg
RA of node: 135
8097 deg
Eccentricity:
0007334
Arg of perigee: 251
4023 deg
Mean anomaly: 108
6344 deg
Mean motion: 15
74455607 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1120
Checksum: 294
Coasting Arc #14 (Orbit 1135)
---------------------------------------
Vector Time (GMT): 2009/202/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5327101
13 A = 6725216
24 meter
Y = 1941445
64 meter E =
0005662
Z = 3615127
14 I = 51
89388
XDOT = 723
972332 Wp = 119
37895
YDOT = -6261
769658 meter/sec RA = 129
97216 deg
ZDOT = 4421
721746 TA = 283
71840
MA = 283
78142
Ha = 187
759 n
mi
Hp = 185
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17477365
90 X = -5365976
06
Y = 6369572
29 feet Y = 1881656
89 meter
Z = 11860653
36 Z = 3589154
51
XDOT = 2375
237310 XDOT = 772
459216
YDOT = -20543
863706 feet/sec YDOT = -6253
403428 meter/sec
ZDOT = 14506
961110 ZDOT = 4425
355433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10311601
05 X = 3142976
00
Y = 15559861
19 feet Y = 4742645
69 meter
Z = 11758676
43 Z = 3584044
58
XDOT = -19372
506950 XDOT = -5904
740118
YDOT = 1845
036459 feet/sec YDOT = 562
367113 meter/sec
ZDOT = 14520
900641 ZDOT = 4425
970515
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 09202
51425236
00010596 00000-0 82463-4 0 9135
2 25544 51
6380 130
5908 0007391 254
7168 105
3178 15
74482721 11361
Satellite: ISS
Catalog Number: 25544
Epoch time: 09202
51425236 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 130
5908 deg
Eccentricity:
0007391
Arg of perigee: 254
7168 deg
Mean anomaly: 105
3178 deg
Mean motion: 15
74482721 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1136
Checksum: 296
Coasting Arc #15 (Orbit 1150)
---------------------------------------
Vector Time (GMT): 2009/203/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -310609
30 A = 6724730
09 meter
Y = 5581666
53 meter E =
0003073
Z = -3738796
91 I = 51
91073
XDOT = -5863
834000 Wp = 208
12902
YDOT = 2548
448030 meter/sec RA = 124
79981 deg
ZDOT = 4287
670064 TA = 106
93284
MA = 106
89916
Ha = 187
418 n
mi
Hp = 186
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1019059
39 X = -354839
41
Y = 18312554
25 feet Y = 5577946
34 meter
Z = -12266394
08 Z = -3740412
47
XDOT = -19238
300524 XDOT = -5912
723589
YDOT = 8361
049967 feet/sec YDOT = 2482
601246 meter/sec
ZDOT = 14067
159003 ZDOT = 4259
065852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17962108
08 X = 5474850
54
Y = -3688153
64 feet Y = -1124149
23 meter
Z = -12272438
42 Z = -3740639
23
XDOT = 12682
367411 XDOT = 3865
585587
YDOT = 15286
259098 feet/sec YDOT = 4659
251773 meter/sec
ZDOT = 13954
858875 ZDOT = 4253
440985
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 09203
46630694
00010596 00000-0 82463-4 0 9147
2 25544 51
6381 125
6980 0007400 259
4327 100
6003 15
74477418 11516
Satellite: ISS
Catalog Number: 25544
Epoch time: 09203
46630694 = yrday
fracday
Element set: 914
Inclination: 51
6381 deg
RA of node: 125
6980 deg
Eccentricity:
0007400
Arg of perigee: 259
4327 deg
Mean anomaly: 100
6003 deg
Mean motion: 15
74477418 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1151
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 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
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