Date:
August 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6200 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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
235/17:58:05
000 0
0 0
0 0
0
014/19:21:23
047 0
0 0
0 184
7
000/00:00:00
000 0
0 0
0 183
8
Coasting Arc #1 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2007/225/17:58:05
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6410785
16 A = 6725676
40 meter
Y = 1979537
79 meter E =
0004474
Z = -421530
96 I = 51
73235
XDOT = -1771
649398 Wp =
58837
YDOT = -4455
040286 meter/sec RA = 165
68096 deg
ZDOT = 6027
621223 TA = 354
83092
MA = 354
83554
Ha = 185
979 n
mi
Hp = 182
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21032759
71 X = -6430396
51
Y = 6494546
56 feet Y = 1907739
14 meter
Z = -1382975
60 Z = -452721
42
XDOT = -5812
498025 XDOT = -1750
981233
YDOT = -14616
273903 feet/sec YDOT = -4474
736495 meter/sec
ZDOT = 19775
660182 ZDOT = 6019
064809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8335815
50 X = 2540756
57
Y = -20364920
37 feet Y = -6207227
73 meter
Z = -1500978
17 Z = -457498
15
XDOT = 13567
140084 XDOT = 4135
264298
YDOT = 4099
321506 feet/sec YDOT = 1249
473195 meter/sec
ZDOT = 19742
640955 ZDOT = 6017
556963
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 07225
74954961
00020000 00000-0 20000-3 0 9000
2 25544 51
6331 166
6653 0008449 241
9279 118
1032 15
76252900 19860
Satellite: ISS
Catalog Number: 25544
Epoch time: 07225
74954961 = yrday
fracday
Element set: 900
Inclination: 51
6331 deg
RA of node: 166
6653 deg
Eccentricity:
0008449
Arg of perigee: 241
9279 deg
Mean anomaly: 118
1032 deg
Mean motion: 15
76252900 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1986
Checksum: 302
Coasting Arc #2 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2007/226/18:02:51
596
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1160160
55 A = 6715346
77 meter
Y = 4485121
93 meter E =
0008182
Z = -4867455
87 I = 51
72466
XDOT = -7311
110149 Wp = 150
18250
YDOT = 640
478991 meter/sec RA = 160
50203 deg
ZDOT = 2327
478483 TA = 142
49412
MA = 142
43701
Ha = 185
752 n
mi
Hp = 183
091
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3806301
02 X = -1186582
85
Y = 14714966
97 feet Y = 4472000
69 meter
Z = -15969343
40 Z = -4873155
94
XDOT = -23986
581854 XDOT = -7329
034960
YDOT = 2101
309024 feet/sec YDOT = 558
621782 meter/sec
ZDOT = 7636
084261 ZDOT = 2291
918257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9464956
66 X = -2884918
79
Y = -11864260
84 feet Y = -3616226
70 meter
Z = -15990372
71 Z = -4873865
60
XDOT = 12004
517203 XDOT = 3658
976844
YDOT = -19710
366381 feet/sec YDOT = -6007
719673 meter/sec
ZDOT = 7501
332402 ZDOT = 2286
406116
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 07226
76392237
00020000 00000-0 20000-3 0 9016
2 25544 51
6322 161
4367 0008466 245
3482 114
6801 15
76279298 20022
Satellite: ISS
Catalog Number: 25544
Epoch time: 07226
76392237 = yrday
fracday
Element set: 901
Inclination: 51
6322 deg
RA of node: 161
4367 deg
Eccentricity:
0008466
Arg of perigee: 245
3482 deg
Mean anomaly: 114
6801 deg
Mean motion: 15
76279298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2002
Checksum: 290
Coasting Arc #3 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2007/227/18:07:53
868
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5193034
51 A = 6718452
86 meter
Y = 1172122
62 meter E =
0000956
Z = -4097262
91 I = 51
76114
XDOT = -4186
802278 Wp = 237
66009
YDOT = 5222
817454 meter/sec RA = 155
38330 deg
ZDOT = -3812
264018 TA = 353
28322
MA = 353
28450
Ha = 185
666 n
mi
Hp = 183
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17037514
81 X = 5199445
18
Y = 3845546
65 feet Y = 1230229
91 meter
Z = -13442463
60 Z = -4072019
94
XDOT = -13736
227947 XDOT = -4226
374406
YDOT = 17135
227868 feet/sec YDOT = 5175
777020 meter/sec
ZDOT = -12507
427881 ZDOT = -3832
699315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12964529
13 X = -3951588
48
Y = 11813316
81 feet Y = 3600698
96 meter
Z = -13346591
25 Z = -4068041
01
XDOT = -5338
493015 XDOT = -1627
172671
YDOT = -20076
827759 feet/sec YDOT = -6119
417101 meter/sec
ZDOT = -12584
235972 ZDOT = -3835
675124
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 07227
77828581
00020000 00000-0 20000-3 0 9025
2 25544 51
6314 156
2094 0008440 249
3760 110
6500 15
76288570 20189
Satellite: ISS
Catalog Number: 25544
Epoch time: 07227
77828581 = yrday
fracday
Element set: 902
Inclination: 51
6314 deg
RA of node: 156
2094 deg
Eccentricity:
0008440
Arg of perigee: 249
3760 deg
Mean anomaly: 110
6500 deg
Mean motion: 15
76288570 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2018
Checksum: 286
Coasting Arc #4 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2007/228/18:12:25
858
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5230929
89 A = 6724897
75 meter
Y = -4051762
00 meter E =
0010309
Z = 1162935
31 I = 51
80982
XDOT = 3784
339645 Wp = 159
91241
YDOT = 3188
199557 meter/sec RA = 150
18666 deg
ZDOT = -5908
286945 TA = 7
36399
MA = 7
34886
Ha = 185
203 n
mi
Hp = 183
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17161843
46 X = 5270199
24
Y = -13293182
40 feet Y = -3993047
22 meter
Z = 3815404
55 Z = 1188442
30
XDOT = 12415
812482 XDOT = 3777
108568
YDOT = 10459
972300 feet/sec YDOT = 3230
477744 meter/sec
ZDOT = -19384
143520 ZDOT = -5889
920373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1861397
57 X = 567353
98
Y = 21610864
17 feet Y = 6586991
40 meter
Z = 3911601
95 Z = 1192256
27
XDOT = -14007
262497 XDOT = -4269
413609
YDOT = 4705
764633 feet/sec YDOT = 1434
317060 meter/sec
ZDOT = -19314
080492 ZDOT = -5886
931734
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 07228
79263825
00020000 00000-0 20000-3 0 9033
2 25544 51
6318 150
9812 0008503 254
5131 105
5095 15
76344632 20344
Satellite: ISS
Catalog Number: 25544
Epoch time: 07228
79263825 = yrday
fracday
Element set: 903
Inclination: 51
6318 deg
RA of node: 150
9812 deg
Eccentricity:
0008503
Arg of perigee: 254
5131 deg
Mean anomaly: 105
5095 deg
Mean motion: 15
76344632 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2034
Checksum: 279
Coasting Arc #5 (Orbit 2049)
---------------------------------------
Vector Time (GMT): 2007/229/18:17:18
367
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -875135
81 A = 6714362
21 meter
Y = -4284858
91 meter E =
0004399
Z = 5098657
21 I = 51
79706
XDOT = 6802
371622 Wp = 280
01789
YDOT = -3253
527111 meter/sec RA = 145
02514 deg
ZDOT = -1567
056645 TA = 184
98650
MA = 184
99088
Ha = 185
250 n
mi
Hp = 183
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2871180
49 X = -851925
05
Y = -14057936
04 feet Y = -4294515
42 meter
Z = 16727878
00 Z = 5094462
19
XDOT = 22317
492197 XDOT = 6845
859910
YDOT = -10674
301544 feet/sec YDOT = -3177
215993 meter/sec
ZDOT = -5141
261960 ZDOT = -1533
905307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13604429
97 X = 4146630
25
Y = 4619446
08 feet Y = 1408007
17 meter
Z = 16711413
72 Z = 5093638
90
XDOT = -1878
409009 XDOT = -572
539066
YDOT = 23673
237598 feet/sec YDOT = 7215
602820 meter/sec
ZDOT = -5015
964824 ZDOT = -1528
866078
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 07229
80698417
00020000 00000-0 20000-3 0 9046
2 25544 51
6307 145
7524 0008467 256
2134 103
8088 15
76288387 20500
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
80698417 = yrday
fracday
Element set: 904
Inclination: 51
6307 deg
RA of node: 145
7524 deg
Eccentricity:
0008467
Arg of perigee: 256
2134 deg
Mean anomaly: 103
8088 deg
Mean motion: 15
76288387 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2050
Checksum: 308
Coasting Arc #6 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2007/230/18:21:44
463
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5632379
61 A = 6720352
39 meter
Y = 1177360
84 meter E =
0004451
Z = 3470108
17 I = 51
84004
XDOT = 1561
528587 Wp = 114
29991
YDOT = -6003
982875 meter/sec RA = 139
90655 deg
ZDOT = 4565
251975 TA = 286
75539
MA = 286
80423
Ha = 184
944 n
mi
Hp = 183
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18478935
71 X = -5661983
52
Y = 3862732
40 feet Y = 1114210
81 meter
Z = 11384869
32 Z = 3442674
26
XDOT = 5123
125285 XDOT = 1606
372858
YDOT = -19698
106544 feet/sec YDOT = -5986
270319 meter/sec
ZDOT = 14977
860812 ZDOT = 4572
946687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5474594
91 X = 1668656
53
Y = -18132163
43 feet Y = -5526683
41 meter
Z = 11280978
50 Z = 3438442
25
XDOT = 13568
155943 XDOT = 4135
573932
YDOT = 13445
885226 feet/sec YDOT = 4098
305817 meter/sec
ZDOT = 15006
269335 ZDOT = 4573
910893
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 07230
82131728
00020000 00000-0 20000-3 0 9058
2 25544 51
6300 140
5232 0008522 259
5406 100
4798 15
76348913 20662
Satellite: ISS
Catalog Number: 25544
Epoch time: 07230
82131728 = yrday
fracday
Element set: 905
Inclination: 51
6300 deg
RA of node: 140
5232 deg
Eccentricity:
0008522
Arg of perigee: 259
5406 deg
Mean anomaly: 100
4798 deg
Mean motion: 15
76348913 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2066
Checksum: 272
Coasting Arc #7 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2007/231/18:26:19
917
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3264427
62 A = 6723749
08 meter
Y = 5524610
98 meter E =
0005713
Z = -1995754
93 I = 51
87337
XDOT = -5176
892766 Wp = 316
01489
YDOT = -1029
981916 meter/sec RA = 134
70683 deg
ZDOT = 5611
091089 TA = 21
80466
MA = 21
78035
Ha = 184
688 n
mi
Hp = 183
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10710064
38 X = -3316267
02
Y = 18125364
10 feet Y = 5487816
52 meter
Z = -6547752
39 Z = -2011739
24
XDOT = -16984
556319 XDOT = -5192
248224
YDOT = -3379
205761 feet/sec YDOT = -1087
958883 meter/sec
ZDOT = 18409
091500 ZDOT = 5585
904450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11479879
93 X = -3499067
40
Y = -17625504
62 feet Y = -5372253
81 meter
Z = -6607670
36 Z = -2014017
93
XDOT = 9346
899095 XDOT = 2848
934844
YDOT = -12960
116752 feet/sec YDOT = -3950
243586 meter/sec
ZDOT = 18313
433903 ZDOT = 5581
934654
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 07231
77224801
00020000 00000-0 20000-3 0 9069
2 25544 51
6304 135
6213 0008358 262
7251 97
2964 15
76341772 20812
Satellite: ISS
Catalog Number: 25544
Epoch time: 07231
77224801 = yrday
fracday
Element set: 906
Inclination: 51
6304 deg
RA of node: 135
6213 deg
Eccentricity:
0008358
Arg of perigee: 262
7251 deg
Mean anomaly: 97
2964 deg
Mean motion: 15
76341772 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2081
Checksum: 283
Coasting Arc #8 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2007/232/18:31:05
354
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2792967
19 A = 6713454
97 meter
Y = 3106194
81 meter E =
0006857
Z = -5261417
70 I = 51
85859
XDOT = -5219
738984 Wp = 103
76462
YDOT = 5633
834482 meter/sec RA = 129
56657 deg
ZDOT = 554
218707 TA = 171
49191
MA = 171
48028
Ha = 184
263 n
mi
Hp = 183
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9163278
18 X = 2783584
66
Y = 10190927
86 feet Y = 3137375
14 meter
Z = -17261869
09 Z = -5247872
12
XDOT = -17125
127900 XDOT = -5285
041706
YDOT = 18483
708930 feet/sec YDOT = 5575
099265 meter/sec
ZDOT = 1818
302846 ZDOT = 528
702900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13095288
31 X = -3991443
88
Y = 4256616
97 feet Y = 1297416
85 meter
Z = -17210096
99 Z = -5245637
56
XDOT = -9503
413815 XDOT = -2896
640531
YDOT = -22260
303016 feet/sec YDOT = -6784
940359 meter/sec
ZDOT = 1722
235061 ZDOT = 524
937247
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 07232
78656388
00020000 00000-0 20000-3 0 9071
2 25544 51
6308 130
3937 0008240 266
2770 93
7452 15
76366221 20972
Satellite: ISS
Catalog Number: 25544
Epoch time: 07232
78656388 = yrday
fracday
Element set: 907
Inclination: 51
6308 deg
RA of node: 130
3937 deg
Eccentricity:
0008240
Arg of perigee: 266
2770 deg
Mean anomaly: 93
7452 deg
Mean motion: 15
76366221 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2097
Checksum: 305
Coasting Arc #9 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2007/233/18:35:59
550
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5053304
22 A = 6721780
83 meter
Y = -3343590
49 meter E =
0004531
Z = -2903861
33 I = 51
90459
XDOT = 881
900925 Wp = 246
03691
YDOT = 5736
254291 meter/sec RA = 124
44070 deg
ZDOT = -5065
839411 TA = 327
27181
MA = 327
29988
Ha = 183
456 n
mi
Hp = 183
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16579082
08 X = 5104423
56
Y = -10969785
08 feet Y = -3286795
59 meter
Z = -9527104
11 Z = -2879188
49
XDOT = 2893
375739 XDOT = 842
300594
YDOT = 18819
731925 feet/sec YDOT = 5745
895106 meter/sec
ZDOT = -16620
208040 ZDOT = -5061
650976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3927348
32 X = 1197055
77
Y = 19533169
83 feet Y = 5953710
17 meter
Z = -9433931
91 Z = -2875462
45
XDOT = -17141
008604 XDOT = -5224
579423
YDOT = -4579
643661 feet/sec YDOT = -1395
875388 meter/sec
ZDOT = -16603
598810 ZDOT = -5060
776917
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 07233
80086928
00020000 00000-0 20000-3 0 9083
2 25544 51
6311 125
1649 0008280 271
0717 88
9499 15
76389311 21138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07233
80086928 = yrday
fracday
Element set: 908
Inclination: 51
6311 deg
RA of node: 125
1649 deg
Eccentricity:
0008280
Arg of perigee: 271
0717 deg
Mean anomaly: 88
9499 deg
Mean motion: 15
76389311 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2113
Checksum: 303
Coasting Arc #10 (Orbit 2128)
---------------------------------------
Vector Time (GMT): 2007/234/18:40:47
990
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1123882
62 A = 6722562
58 meter
Y = -6110713
58 meter E =
0005755
Z = 2558424
11 I = 51
92238
XDOT = 5449
228159 Wp = 117
59191
YDOT = -1222
296531 meter/sec RA = 119
24226 deg
ZDOT = -5306
771296 TA = 33
48088
MA = 33
44452
Ha = 184
202 n
mi
Hp = 183
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3687278
93 X = 1179701
71
Y = -20048272
89 feet Y = -6097833
77 meter
Z = 8393779
87 Z = 2564019
04
XDOT = 17878
045141 XDOT = 5488
270246
YDOT = -4010
159222 feet/sec YDOT = -1161
141511 meter/sec
ZDOT = -17410
666982 ZDOT = -5280
204354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17621562
47 X = 5371052
24
Y = 10230634
00 feet Y = 3118297
24 meter
Z = 8414242
47 Z = 2564661
11
XDOT = -1585
118164 XDOT = -483
144016
YDOT = 16984
271740 feet/sec YDOT = 5176
806026 meter/sec
ZDOT = -17310
032400 ZDOT = -5276
097876
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 07234
81516603
00020000 00000-0 20000-3 0 9094
2 25544 51
6310 119
9363 0008334 273
9621 86
0591 15
76374557 21291
Satellite: ISS
Catalog Number: 25544
Epoch time: 07234
81516603 = yrday
fracday
Element set: 909
Inclination: 51
6310 deg
RA of node: 119
9363 deg
Eccentricity:
0008334
Arg of perigee: 273
9621 deg
Mean anomaly: 86
0591 deg
Mean motion: 15
76374557 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2129
Checksum: 297
Coasting Arc #11 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2007/235/17:58:05
000
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4148083
50 A = 6713484
17 meter
Y = 771711
74 meter E =
0007093
Z = -5227817
54 I = 51
90565
XDOT = -2486
609936 Wp = 64
98140
YDOT = 7231
371348 meter/sec RA = 114
29130 deg
ZDOT = -903
578824 TA = 196
43200
MA = 196
45500
Ha = 184
698 n
mi
Hp = 183
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13609197
83 X = 4164541
35
Y = 2531862
67 feet Y = 818190
36 meter
Z = -17151632
34 Z = -5207626
31
XDOT = -8158
169083 XDOT = -2562
898015
YDOT = 23724
971613 feet/sec YDOT = 7203
138192 meter/sec
ZDOT = -2964
497453 ZDOT = -915
843429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8965603
90 X = -2732716
07
Y = 10670699
00 feet Y = 3252429
06 meter
Z = -17074929
44 Z = -5204438
49
XDOT = -15839
015608 XDOT = -4827
731957
YDOT = -18135
261723 feet/sec YDOT = -5527
627773 meter/sec
ZDOT = -3010
131477 ZDOT = -917
488074
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 07235
76605992
00020000 00000-0 20000-3 0 9101
2 25544 51
6319 115
0362 0008190 278
5750 81
4487 15
76422171 21446
Satellite: ISS
Catalog Number: 25544
Epoch time: 07235
76605992 = yrday
fracday
Element set: 910
Inclination: 51
6319 deg
RA of node: 115
0362 deg
Eccentricity:
0008190
Arg of perigee: 278
5750 deg
Mean anomaly: 81
4487 deg
Mean motion: 15
76422171 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2144
Checksum: 289
Coasting Arc #12 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2007/236/18:03:04
586
Vector Time (MET): N/A
Weight (LBS) : 515214
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3409564
35 A = 6723860
84 meter
Y = -5501345
35 meter E =
0005344
Z = -1809817
55 I = 51
95141
XDOT = 3349
858894 Wp = 221
55106
YDOT = 3953
191110 meter/sec RA = 109
14779 deg
ZDOT = -5700
105501 TA = 338
44588
MA = 338
46837
Ha = 184
869 n
mi
Hp = 183
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11186234
74 X = 3479619
45
Y = -18049033
31 feet Y = -5462825
87 meter
Z = -5937721
61 Z = -1793084
31
XDOT = 10990
350702 XDOT = 3333
094452
YDOT = 12969
787106 feet/sec YDOT = 3990
557754 meter/sec
ZDOT = -18701
133533 ZDOT = -5683
872577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10882380
17 X = 3316949
48
Y = 18254183
54 feet Y = 5563875
14 meter
Z = -5874910
56 Z = -1790672
74
XDOT = -15285
206433 XDOT = -4658
930921
YDOT = 3107
634686 feet/sec YDOT = 947
207052 meter/sec
ZDOT = -18639
048291 ZDOT = -5681
181919
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 07236
78033727
00020000 00000-0 20000-3 0 9116
2 25544 51
6318 109
8068 0008311 282
8834 77
1402 15
76434376 21602
Satellite: ISS
Catalog Number: 25544
Epoch time: 07236
78033727 = yrday
fracday
Element set: 911
Inclination: 51
6318 deg
RA of node: 109
8068 deg
Eccentricity:
0008311
Arg of perigee: 282
8834 deg
Mean anomaly: 77
1402 deg
Mean motion: 15
76434376 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2160
Checksum: 290
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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