Date:
August 16th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 3786)
---------------------------------------
Vector Time (GMT): 2008/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4435825
35 A = 6730110
58 meter
Y = 875635
30 meter E =
0015397
Z = -4996198
66 I = 51
93412
XDOT = 833
423912 Wp = 72
31678
YDOT = 7363
740053 meter/sec RA = 71
09197 deg
ZDOT = 2040
210268 TA = 217
33221
MA = 217
43931
Ha = 196
956 n
mi
Hp = 187
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14553232
79 X = 4449974
30
Y = 2872819
23 feet Y = 925318
63 meter
Z = -16391727
90 Z = -4974615
46
XDOT = 2734
330420 XDOT = 741
108687
YDOT = 24159
252142 feet/sec YDOT = 7372
543608 meter/sec
ZDOT = 6693
603241 ZDOT = 2044
035124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10067616
08 X = -3068609
38
Y = -11019226
17 feet Y = -3358660
14 meter
Z = -16308224
30 Z = -4970746
77
XDOT = 11394
982924 XDOT = 3473
190795
YDOT = -20292
869707 feet/sec YDOT = -6185
266687 meter/sec
ZDOT = 6709
045541 ZDOT = 2044
917081
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 08228
51241078
00020000 00000-0 20000-3 0 9007
2 25544 51
6397 71
7123 0008313 15
9378 344
2043 15
70976771 37877
Satellite: ISS
Catalog Number: 25544
Epoch time: 08228
51241078 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 71
7123 deg
Eccentricity:
0008313
Arg of perigee: 15
9378 deg
Mean anomaly: 344
2043 deg
Mean motion: 15
70976771 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3787
Checksum: 296
Coasting Arc #2 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2008/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2099210
93 A = 6740442
14 meter
Y = -6350109
39 meter E =
0009206
Z = -846193
82 I = 51
95831
XDOT = 4769
790237 Wp = 90
13799
YDOT = -787
481235 meter/sec RA = 66
02571 deg
ZDOT = -5978
934810 TA = 99
03292
MA = 98
92872
Ha = 196
991 n
mi
Hp = 186
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6887174
98 X = -2023936
41
Y = -20833692
23 feet Y = -6373163
07 meter
Z = -2776226
45 Z = -856208
92
XDOT = 15648
918102 XDOT = 4807
285465
YDOT = -2583
599854 feet/sec YDOT = -733
932884 meter/sec
ZDOT = -19615
927854 ZDOT = -5955
672594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6504760
29 X = -1982650
94
Y = 20950998
97 feet Y = 6385864
49 meter
Z = -2815507
12 Z = -858166
57
XDOT = -12803
572902 XDOT = -3902
529021
YDOT = -6574
991842 feet/sec YDOT = -2004
057514 meter/sec
ZDOT = -19526
080788 ZDOT = -5951
549424
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 08229
53020114
00020000 00000-0 20000-3 0 9017
2 25544 51
6396 66
5091 0008365 19
4877 340
6603 15
70986248 38033
Satellite: ISS
Catalog Number: 25544
Epoch time: 08229
53020114 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 66
5091 deg
Eccentricity:
0008365
Arg of perigee: 19
4877 deg
Mean anomaly: 340
6603 deg
Mean motion: 15
70986248 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3803
Checksum: 292
Coasting Arc #3 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2008/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3538855
19 A = 6728757
58 meter
Y = 2170216
69 meter E =
0009315
Z = 5290508
82 I = 51
90510
XDOT = -3853
334747 Wp = 37
70290
YDOT = -6665
822248 meter/sec RA = 60
92529 deg
ZDOT = 163
924337 TA = 50
78857
MA = 50
70589
Ha = 197
224 n
mi
Hp = 186
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11610417
29 X = -3588559
75
Y = 7120133
51 feet Y = 2130365
25 meter
Z = 17357312
41 Z = 5273196
65
XDOT = -12642
174367 XDOT = -3779
306369
YDOT = -21869
495565 feet/sec YDOT = -6708
498542 meter/sec
ZDOT = 537
809504 ZDOT = 145
384970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13682830
31 X = 4170526
68
Y = 768176
48 feet Y = 234140
19 meter
Z = 17290588
32 Z = 5270171
32
XDOT = -1916
819024 XDOT = -584
246439
YDOT = 24187
145045 feet/sec YDOT = 7372
241810 meter/sec
ZDOT = 465
549957 ZDOT = 141
899627
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 08230
54798199
00020000 00000-0 20000-3 0 9026
2 25544 51
6390 61
3041 0008332 23
7778 336
3767 15
70967618 38197
Satellite: ISS
Catalog Number: 25544
Epoch time: 08230
54798199 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 61
3041 deg
Eccentricity:
0008332
Arg of perigee: 23
7778 deg
Mean anomaly: 336
3767 deg
Mean motion: 15
70967618 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3819
Checksum: 315
Coasting Arc #4 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2008/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4428487
37 A = 6740172
78 meter
Y = 4941825
67 meter E =
0017721
Z = -1132583
88 I = 51
92797
XDOT = -2919
004655 Wp = 32
59936
YDOT = 3960
157138 meter/sec RA = 55
81890 deg
ZDOT = 5923
119511 TA = 315
06034
MA = 315
20365
Ha = 197
138 n
mi
Hp = 186
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14529158
05 X = 4378399
76
Y = 16213338
80 feet Y = 4991067
49 meter
Z = -3715826
38 Z = -1111192
33
XDOT = -9576
786927 XDOT = -2991
843862
YDOT = 12992
641530 feet/sec YDOT = 3927
107979 meter/sec
ZDOT = 19432
806795 ZDOT = 5908
762198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3173109
39 X = -967163
74
Y = -21552518
09 feet Y = -6569207
52 meter
Z = -3632698
05 Z = -1107246
37
XDOT = 13680
919606 XDOT = 4169
944296
YDOT = -5247
960924 feet/sec YDOT = -1599
578490 meter/sec
ZDOT = 19377
665121 ZDOT = 5906
312329
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 08231
50214020
00020000 00000-0 20000-3 0 9030
2 25544 51
6384 56
4245 0008280 27
0062 333
1529 15
71007873 38343
Satellite: ISS
Catalog Number: 25544
Epoch time: 08231
50214020 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 56
4245 deg
Eccentricity:
0008280
Arg of perigee: 27
0062 deg
Mean anomaly: 333
1529 deg
Mean motion: 15
71007873 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3834
Checksum: 255
Coasting Arc #5 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2008/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1323291
56 A = 6730321
57 meter
Y = -4448126
43 meter E =
0019327
Z = -4892073
52 I = 51
87767
XDOT = 5901
044670 Wp = 56
34380
YDOT = 4327
490460 meter/sec RA = 50
75320 deg
ZDOT = -2334
683788 TA = 190
90685
MA = 190
94882
Ha = 197
166 n
mi
Hp = 186
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4341507
73 X = 1396697
47
Y = -14593590
66 feet Y = -4432918
32 meter
Z = -16050109
97 Z = -4885466
61
XDOT = 19360
382776 XDOT = 5863
556775
YDOT = 14197
803347 feet/sec YDOT = 4393
269673 meter/sec
ZDOT = -7659
723715 ZDOT = -2306
107932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11587836
67 X = -3531972
62
Y = 9917157
84 feet Y = 3022749
71 meter
Z = -16024968
94 Z = -4884410
53
XDOT = -7996
021707 XDOT = -2437
187416
YDOT = -21561
773575 feet/sec YDOT = -6572
028586 meter/sec
ZDOT = -7548
884985 ZDOT = -2300
900143
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 08232
51990012
00020000 00000-0 20000-3 0 9045
2 25544 51
6384 51
2205 0008363 31
9404 328
2263 15
71039419 38507
Satellite: ISS
Catalog Number: 25544
Epoch time: 08232
51990012 = yrday
fracday
Element set: 904
Inclination: 51
6384 deg
RA of node: 51
2205 deg
Eccentricity:
0008363
Arg of perigee: 31
9404 deg
Mean anomaly: 328
2263 deg
Mean motion: 15
71039419 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3850
Checksum: 264
Coasting Arc #6 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2008/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5567676
70 A = 6737033
76 meter
Y = -2450969
80 meter E =
0018534
Z = 2886094
03 I = 51
88114
XDOT = -97
251019 Wp = 74
82605
YDOT = -5788
223991 meter/sec RA = 45
61443 deg
ZDOT = -5071
508428 TA = 72
16073
MA = 71
95865
Ha = 197
190 n
mi
Hp = 186
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18266655
85 X = -5553875
84
Y = -8041239
51 feet Y = -2513153
54 meter
Z = 9468812
43 Z = 2859079
92
XDOT = -319
065024 XDOT = -7
882551
YDOT = -18990
236191 feet/sec YDOT = -5788
811942 meter/sec
ZDOT = -16638
807177 ZDOT = -5071
763661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11402391
31 X = 3475448
87
Y = 16440444
61 feet Y = 5011047
52 meter
Z = 9364182
37 Z = 2854202
79
XDOT = -8549
424674 XDOT = -2605
864640
YDOT = 15467
360309 feet/sec YDOT = 4714
451422 meter/sec
ZDOT = -16640
304969 ZDOT = -5071
964955
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 08233
53764776
00020000 00000-0 20000-3 0 9055
2 25544 51
6387 46
0156 0008274 34
1670 326
0023 15
71060260 38663
Satellite: ISS
Catalog Number: 25544
Epoch time: 08233
53764776 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 46
0156 deg
Eccentricity:
0008274
Arg of perigee: 34
1670 deg
Mean anomaly: 326
0023 deg
Mean motion: 15
71060260 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3866
Checksum: 280
Coasting Arc #7 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2008/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1574088
62 A = 6734108
78 meter
Y = 5301761
61 meter E =
0017105
Z = 3824145
83 I = 51
85042
XDOT = -6372
390365 Wp = 73
71116
YDOT = -1131
688853 meter/sec RA = 40
56593 deg
ZDOT = 4181
311094 TA = 332
60986
MA = 332
69993
Ha = 197
173 n
mi
Hp = 186
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5164332
74 X = 1496109
45
Y = 17394230
99 feet Y = 5318928
00 meter
Z = 12546410
21 Z = 3831603
31
XDOT = -20906
792535 XDOT = -6379
574105
YDOT = -3712
889938 feet/sec YDOT = -1202
988720 meter/sec
ZDOT = 13718
212250 ZDOT = 4150
336548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4462917
60 X = 1360297
28
Y = -17566338
29 feet Y = -5354219
91 meter
Z = 12575696
38 Z = 3833072
26
XDOT = 14898
121540 XDOT = 4540
947445
YDOT = 13545
028556 feet/sec YDOT = 4128
524704 meter/sec
ZDOT = 13598
394854 ZDOT = 4144
790751
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 08234
55538618
00020000 00000-0 20000-3 0 9063
2 25544 51
6387 40
8112 0008224 39
2509 320
9247 15
71084692 38823
Satellite: ISS
Catalog Number: 25544
Epoch time: 08234
55538618 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 40
8112 deg
Eccentricity:
0008224
Arg of perigee: 39
2509 deg
Mean anomaly: 320
9247 deg
Mean motion: 15
71084692 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3882
Checksum: 298
Coasting Arc #8 (Orbit 3896)
---------------------------------------
Vector Time (GMT): 2008/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5175192
07 A = 6732638
23 meter
Y = -460367
96 meter E =
0014036
Z = -4291555
33 I = 51
82335
XDOT = 3454
698498 Wp = 76
99069
YDOT = 5879
752829 meter/sec RA = 35
41653 deg
ZDOT = 3548
066440 TA = 228
90213
MA = 229
02342
Ha = 197
343 n
mi
Hp = 185
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16978976
62 X = 5200803
02
Y = -1510393
57 feet Y = -402352
72 meter
Z = -14079905
94 Z = -4266351
96
XDOT = 11334
312659 XDOT = 3371
457478
YDOT = 19290
527655 feet/sec YDOT = 5917
919780 meter/sec
ZDOT = 11640
637926 ZDOT = 3564
647313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15580526
70 X = -4748944
54
Y = -7109615
30 feet Y = -2167010
74 meter
Z = -13982533
57 Z = -4261876
23
XDOT = -791
878767 XDOT = -241
364648
YDOT = -21202
345927 feet/sec YDOT = -6462
475038 meter/sec
ZDOT = 11705
229004 ZDOT = 3567
753800
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 08235
50950690
00020000 00000-0 20000-3 0 9078
2 25544 51
6399 35
9327 0008350 43
7579 316
4243 15
71080238 38970
Satellite: ISS
Catalog Number: 25544
Epoch time: 08235
50950690 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 35
9327 deg
Eccentricity:
0008350
Arg of perigee: 43
7579 deg
Mean anomaly: 316
4243 deg
Mean motion: 15
71080238 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3897
Checksum: 310
Coasting Arc #9 (Orbit 3912)
---------------------------------------
Vector Time (GMT): 2008/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4316015
00 A = 6738014
21 meter
Y = -4635124
24 meter E =
0010391
Z = -2311711
00 I = 51
81761
XDOT = 5050
120103 Wp = 79
76913
YDOT = -1999
117672 meter/sec RA = 30
36055 deg
ZDOT = -5439
164538 TA = 126
09267
MA = 125
99641
Ha = 197
316 n
mi
Hp = 185
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14160154
21 X = -4252633
62
Y = -15207100
52 feet Y = -4683033
92 meter
Z = -7584353
68 Z = -2332524
49
XDOT = 16568
635509 XDOT = 5098
521764
YDOT = -6558
785013 feet/sec YDOT = -1942
373469 meter/sec
ZDOT = -17845
028013 ZDOT = -5414
513507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5113811
41 X = 1558689
72
Y = 20109253
00 feet Y = 6129300
32 meter
Z = -7665192
14 Z = -2336350
57
XDOT = -16309
576532 XDOT = -4971
158927
YDOT = -2595
012747 feet/sec YDOT = -790
959885 meter/sec
ZDOT = -17749
918971 ZDOT = -5410
175302
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 08236
52722314
00020000 00000-0 20000-3 0 9082
2 25544 51
6400 30
7285 0008487 46
7052 313
4816 15
71121184 39137
Satellite: ISS
Catalog Number: 25544
Epoch time: 08236
52722314 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 30
7285 deg
Eccentricity:
0008487
Arg of perigee: 46
7052 deg
Mean anomaly: 313
4816 deg
Mean motion: 15
71121184 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3913
Checksum: 271
Coasting Arc #10 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2008/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3347154
03 A = 6729363
56 meter
Y = 2853340
78 meter E =
0013543
Z = 5085878
69 I = 51
76185
XDOT = -6166
952143 Wp = 52
21564
YDOT = -4319
718078 meter/sec RA = 25
22368 deg
ZDOT = -1624
071730 TA = 53
41842
MA = 53
29388
Ha = 197
553 n
mi
Hp = 185
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10981476
48 X = -3403518
03
Y = 9361354
25 feet Y = 2815595
50 meter
Z = 16685953
70 Z = 5069481
50
XDOT = -20232
782623 XDOT = -6110
300583
YDOT = -14172
303407 feet/sec YDOT = -4388
363628 meter/sec
ZDOT = -5328
319325 ZDOT = -1653
893423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14154287
86 X = 4314226
94
Y = -3160224
62 feet Y = -963236
46 meter
Z = 16622814
01 Z = 5066633
71
XDOT = 11100
320370 XDOT = 3383
377649
YDOT = 20890
165943 feet/sec YDOT = 6367
322580 meter/sec
ZDOT = -5443
947630 ZDOT = -1659
315238
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 08237
54493062
00020000 00000-0 20000-3 0 9091
2 25544 51
6398 25
5242 0008461 51
5588 308
6332 15
71074539 39295
Satellite: ISS
Catalog Number: 25544
Epoch time: 08237
54493062 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 25
5242 deg
Eccentricity:
0008461
Arg of perigee: 51
5588 deg
Mean anomaly: 308
6332 deg
Mean motion: 15
71074539 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3929
Checksum: 308
Coasting Arc #11 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2008/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6163312
85 A = 6740212
49 meter
Y = 2661044
89 meter E =
0021504
Z = 477945
01 I = 51
77350
XDOT = -2298
577455 Wp = 51
75528
YDOT = 4211
381743 meter/sec RA = 20
13784 deg
ZDOT = 6024
442265 TA = 313
43127
MA = 313
61002
Ha = 197
369 n
mi
Hp = 185
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20220842
67 X = 6130776
79
Y = 8730462
25 feet Y = 2729784
65 meter
Z = 1568061
06 Z = 507807
36
XDOT = -7541
264615 XDOT = -2374
764430
YDOT = 13816
869235 feet/sec YDOT = 4185
251310 meter/sec
ZDOT = 19765
230527 ZDOT = 6013
091091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14154003
76 X = -4314140
35
Y = -16863912
92 feet Y = -5140120
66 meter
Z = 1683711
19 Z = 513195
17
XDOT = 11805
805025 XDOT = 3598
409372
YDOT = -7888
072838 feet/sec YDOT = -2404
284601 meter/sec
ZDOT = 19721
703906 ZDOT = 6011
175351
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 08238
56262307
00020000 00000-0 20000-3 0 9102
2 25544 51
6412 20
3205 0008395 55
1124 305
0825 15
71145130 39458
Satellite: ISS
Catalog Number: 25544
Epoch time: 08238
56262307 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 20
3205 deg
Eccentricity:
0008395
Arg of perigee: 55
1124 deg
Mean anomaly: 305
0825 deg
Mean motion: 15
71145130 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3945
Checksum: 252
Coasting Arc #12 (Orbit 3959)
---------------------------------------
Vector Time (GMT): 2008/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 537993
42 A = 6728272
90 meter
Y = -4167422
18 meter E =
0022738
Z = -5274095
97 I = 51
70584
XDOT = 7493
675495 Wp = 75
75787
YDOT = 1604
044769 meter/sec RA = 15
03133 deg
ZDOT = -499
378504 TA = 189
46810
MA = 189
51103
Ha = 197
390 n
mi
Hp = 185
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1765070
26 X = 610174
51
Y = -13672644
96 feet Y = -4161002
10 meter
Z = -17303464
47 Z = -5271307
38
XDOT = 24585
549525 XDOT = 7477
607725
YDOT = 5262
614072 feet/sec YDOT = 1687
753554 meter/sec
ZDOT = -1638
380918 ZDOT = -463
013593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7597955
62 X = -2315856
87
Y = 11519059
02 feet Y = 3511009
19 meter
Z = -17293031
13 Z = -5270915
89
XDOT = -19054
111277 XDOT = -5807
693117
YDOT = -14834
600566 feet/sec YDOT = -4521
586253 meter/sec
ZDOT = -1497
677412 ZDOT = -456
492075
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 08239
51670128
00020000 00000-0 20000-3 0 9113
2 25544 51
6414 15
4425 0008488 57
9640 302
2345 15
71165488 39606
Satellite: ISS
Catalog Number: 25544
Epoch time: 08239
51670128 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 15
4425 deg
Eccentricity:
0008488
Arg of perigee: 57
9640 deg
Mean anomaly: 302
2345 deg
Mean motion: 15
71165488 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3960
Checksum: 291
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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