Date:
February 12th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6673 62 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3107)
---------------------------------------
Vector Time (GMT): 2007/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6038815
37 A = 6716739
41 meter
Y = 608877
47 meter E =
0018183
Z = -2898391
32 I = 51
78750
XDOT = 1880
665016 Wp = 187
56329
YDOT = 5489
813450 meter/sec RA = 27
84086 deg
ZDOT = 5050
395767 TA = 139
17631
MA = 139
03996
Ha = 188
921 n
mi
Hp = 174
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19812386
38 X = 6045637
62
Y = 1997629
48 feet Y = 676445
17 meter
Z = -9509157
86 Z = -2869038
65
XDOT = 6170
160814 XDOT = 1794
603874
YDOT = 18011
198983 feet/sec YDOT = 5510
362636 meter/sec
ZDOT = 16569
539918 ZDOT = 5059
323134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14284924
54 X = 4354045
00
Y = 13948034
40 feet Y = 4251360
89 meter
Z = -9398857
81 Z = -2864771
86
XDOT = -5461
396453 XDOT = -1664
633639
YDOT = 16829
227408 feet/sec YDOT = 5129
548514 meter/sec
ZDOT = 16603
726578 ZDOT = 5060
815861
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 07043
50581447
00020000 00000-0 20000-3 0 9007
2 25544 51
6313 28
3435 0021135 198
3350 161
7056 15
78175894 31080
Satellite: ISS
Catalog Number: 25544
Epoch time: 07043
50581447 = yrday
fracday
Element set: 900
Inclination: 51
6313 deg
RA of node: 28
3435 deg
Eccentricity:
0021135
Arg of perigee: 198
3350 deg
Mean anomaly: 161
7056 deg
Mean motion: 15
78175894 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3108
Checksum: 279
Coasting Arc #2 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2007/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -364726
53 A = 6709211
23 meter
Y = -4441217
58 meter E =
0017115
Z = -5015404
95 I = 51
73662
XDOT = 7332
336588 Wp = 162
76011
YDOT = 1479
176880 meter/sec RA = 22
72002 deg
ZDOT = -1860
696642 TA = 89
43257
MA = 89
23646
Ha = 188
661 n
mi
Hp = 174
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1196609
35 X = -290673
69
Y = -14570923
81 feet Y = -4444881
82 meter
Z = -16454740
63 Z = -5016997
13
XDOT = 24056
222401 XDOT = 7324
290003
YDOT = 4852
942520 feet/sec YDOT = 1561
126272 meter/sec
ZDOT = -6104
647776 ZDOT = -1825
096376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8012200
17 X = 2442118
61
Y = -12220225
99 feet Y = -3724724
88 meter
Z = -16461254
79 Z = -5017390
46
XDOT = 15237
789074 XDOT = 4644
478110
YDOT = 17955
643510 feet/sec YDOT = 5472
880142 meter/sec
ZDOT = -5970
774766 ZDOT = -1819
892149
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 07044
51893718
00020000 00000-0 20000-3 0 9017
2 25544 51
6314 23
1063 0021115 202
4404 157
5840 15
78206410 31247
Satellite: ISS
Catalog Number: 25544
Epoch time: 07044
51893718 = yrday
fracday
Element set: 901
Inclination: 51
6314 deg
RA of node: 23
1063 deg
Eccentricity:
0021115
Arg of perigee: 202
4404 deg
Mean anomaly: 157
5840 deg
Mean motion: 15
78206410 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3124
Checksum: 246
Coasting Arc #3 (Orbit 3139)
---------------------------------------
Vector Time (GMT): 2007/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6439333
38 A = 6720107
77 meter
Y = -1841918
04 meter E =
0027446
Z = 234156
46 I = 51
74715
XDOT = 1112
936714 Wp = 179
80785
YDOT = -4657
862202 meter/sec RA = 17
54225 deg
ZDOT = -6058
590719 TA = 357
64203
MA = 357
65494
Ha = 188
322 n
mi
Hp = 174
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21126421
86 X = -6419395
67
Y = -6043038
19 feet Y = -1913814
79 meter
Z = 768229
84 Z = 202923
34
XDOT = 3651
367171 XDOT = 1194
369634
YDOT = -15281
700138 feet/sec YDOT = -4644
961105 meter/sec
ZDOT = -19877
266137 ZDOT = -6052
986653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13360046
63 X = -4072142
21
Y = -17450499
21 feet Y = -5318912
16 meter
Z = 650706
98 Z = 198335
49
XDOT = 10859
225578 XDOT = 3309
891956
YDOT = -9050
627702 feet/sec YDOT = -2758
631324 meter/sec
ZDOT = -19856
781174 ZDOT = -6052
346902
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 07045
53203852
00020000 00000-0 20000-3 0 9025
2 25544 51
6319 17
8701 0021026 206
5948 153
4141 15
78251199 31401
Satellite: ISS
Catalog Number: 25544
Epoch time: 07045
53203852 = yrday
fracday
Element set: 902
Inclination: 51
6319 deg
RA of node: 17
8701 deg
Eccentricity:
0021026
Arg of perigee: 206
5948 deg
Mean anomaly: 153
4141 deg
Mean motion: 15
78251199 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3140
Checksum: 268
Coasting Arc #4 (Orbit 3155)
---------------------------------------
Vector Time (GMT): 2007/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2328467
95 A = 6708580
34 meter
Y = 3642248
33 meter E =
0017071
Z = 5132887
98 I = 51
68075
XDOT = -7105
497632 Wp = 203
92284
YDOT = -2655
434778 meter/sec RA = 12
37024 deg
ZDOT = -1355
930107 TA = 258
94178
MA = 259
13382
Ha = 188
095 n
mi
Hp = 174
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7639330
54 X = -2393956
90
Y = 11949633
62 feet Y = 3615843
77 meter
Z = 16840183
67 Z = 5121417
68
XDOT = -23312
000105 XDOT = -7068
689432
YDOT = -8712
056358 feet/sec YDOT = -2734
686569 meter/sec
ZDOT = -4448
589591 ZDOT = -1390
358225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13245199
89 X = -4037136
93
Y = 5210763
34 feet Y = 1588240
67 meter
Z = 16797545
23 Z = 5119891
79
XDOT = -13477
066401 XDOT = -4107
809839
YDOT = -19677
825499 feet/sec YDOT = -5997
801212 meter/sec
ZDOT = -4578
217742 ZDOT = -1395
440768
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 07046
54511901
00020000 00000-0 20000-3 0 9035
2 25544 51
6320 12
6338 0021033 210
5753 149
4187 15
78273632 31567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07046
54511901 = yrday
fracday
Element set: 903
Inclination: 51
6320 deg
RA of node: 12
6338 deg
Eccentricity:
0021033
Arg of perigee: 210
5753 deg
Mean anomaly: 149
4187 deg
Mean motion: 15
78273632 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3156
Checksum: 264
Coasting Arc #5 (Orbit 3171)
---------------------------------------
Vector Time (GMT): 2007/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5598291
52 A = 6716956
69 meter
Y = 2730515
33 meter E =
0014380
Z = 2535130
02 I = 51
68223
XDOT = -4200
029170 Wp = 173
46099
YDOT = 3682
160935 meter/sec RA = 7
23819 deg
ZDOT = 5291
953369 TA = 215
25601
MA = 215
35121
Ha = 187
762 n
mi
Hp = 174
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18367098
18 X = 5555027
65
Y = 8958383
64 feet Y = 2792876
65 meter
Z = 8317355
69 Z = 2562220
53
XDOT = -13779
623261 XDOT = -4266
597960
YDOT = 12080
580494 feet/sec YDOT = 3634
821643 meter/sec
ZDOT = 17362
051735 ZDOT = 5271
388632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9983689
05 X = 3043028
42
Y = 17782584
75 feet Y = 5420131
83 meter
Z = 8419440
08 Z = 2566245
34
XDOT = -16986
000053 XDOT = -5177
332816
YDOT = 1326
457984 feet/sec YDOT = 404
304393 meter/sec
ZDOT = 17285
262568 ZDOT = 5268
548031
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 07047
55817596
00020000 00000-0 20000-3 0 9047
2 25544 51
6325 7
3968 0021170 214
4630 145
5164 15
78350892 31725
Satellite: ISS
Catalog Number: 25544
Epoch time: 07047
55817596 = yrday
fracday
Element set: 904
Inclination: 51
6325 deg
RA of node: 7
3968 deg
Eccentricity:
0021170
Arg of perigee: 214
4630 deg
Mean anomaly: 145
5164 deg
Mean motion: 15
78350892 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3172
Checksum: 294
Coasting Arc #6 (Orbit 3186)
---------------------------------------
Vector Time (GMT): 2007/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4837537
80 A = 6713870
25 meter
Y = -2788438
86 meter E =
0019133
Z = -3737067
03 I = 51
64296
XDOT = 5348
790333 Wp = 201
95255
YDOT = 3552
984372 meter/sec RA = 2
02220 deg
ZDOT = 4248
365877 TA = 112
86914
MA = 112
66701
Ha = 187
490 n
mi
Hp = 175
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15871187
02 X = 4886512
39
Y = -9148421
47 feet Y = -2734069
09 meter
Z = -12260718
60 Z = -3713448
01
XDOT = 17548
524716 XDOT = 5288
025710
YDOT = 11656
772875 feet/sec YDOT = 3612
457905 meter/sec
ZDOT = 13938
208258 ZDOT = 4274
201748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18337670
06 X = 5589321
83
Y = 1215375
31 feet Y = 370446
39 meter
Z = -12172351
17 Z = -3710132
64
XDOT = 8174
236278 XDOT = 2491
507217
YDOT = 18046
478946 feet/sec YDOT = 5500
566783 meter/sec
ZDOT = 14035
685714 ZDOT = 4278
077006
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 07048
50790011
00020000 00000-0 20000-3 0 9056
2 25544 51
6328 2
4871 0020974 218
4323 141
5349 15
78332853 31875
Satellite: ISS
Catalog Number: 25544
Epoch time: 07048
50790011 = yrday
fracday
Element set: 905
Inclination: 51
6328 deg
RA of node: 2
4871 deg
Eccentricity:
0020974
Arg of perigee: 218
4323 deg
Mean anomaly: 141
5349 deg
Mean motion: 15
78332853 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3187
Checksum: 283
Coasting Arc #7 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2007/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3469425
51 A = 6710410
54 meter
Y = -3449729
47 meter E =
0012563
Z = -4583484
43 I = 51
60434
XDOT = 6589
541253 Wp = 198
44950
YDOT = -2706
335185 meter/sec RA = 356
90076 deg
ZDOT = -2960
513805 TA = 42
28051
MA = 42
18372
Ha = 187
051 n
mi
Hp = 175
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11382629
64 X = -3408327
20
Y = -11318010
06 feet Y = -3488185
17 meter
Z = -15037678
58 Z = -4600189
81
XDOT = 21619
229833 XDOT = 6633
695359
YDOT = -8879
052443 feet/sec YDOT = -2632
400545 meter/sec
ZDOT = -9712
971802 ZDOT = -2928
395346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3404604
45 X = -1037723
44
Y = -15625822
22 feet Y = -4762750
61 meter
Z = -15100852
12 Z = -4602739
73
XDOT = 21898
256293 XDOT = 6674
588518
YDOT = 4469
051805 feet/sec YDOT = 1362
166990 meter/sec
ZDOT = -9592
675661 ZDOT = -2923
847541
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 07049
52091691
00020000 00000-0 20000-3 0 9068
2 25544 51
6337 357
2503 0020939 222
3285 137
6265 15
78393210 32036
Satellite: ISS
Catalog Number: 25544
Epoch time: 07049
52091691 = yrday
fracday
Element set: 906
Inclination: 51
6337 deg
RA of node: 357
2503 deg
Eccentricity:
0020939
Arg of perigee: 222
3285 deg
Mean anomaly: 137
6265 deg
Mean motion: 15
78393210 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3203
Checksum: 286
Coasting Arc #8 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6315140
98 A = 6719071
91 meter
Y = 1896539
27 meter E =
0022215
Z = 1217210
17 I = 51
60546
XDOT = -2436
515904 Wp = 188
13418
YDOT = -4357
858670 meter/sec RA = 351
69574 deg
ZDOT = -5885
745571 TA = 338
47336
MA = 338
56662
Ha = 186
879 n
mi
Hp = 175
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20718966
46 X = -6341791
85
Y = 6222241
71 feet Y = 1825770
91 meter
Z = 3993471
70 Z = 1186467
06
XDOT = -7993
818584 XDOT = -2359
013391
YDOT = -14297
436583 feet/sec YDOT = -4384
672239 meter/sec
ZDOT = -19310
188882 ZDOT = -5897
393327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20918638
22 X = -6376000
93
Y = -5595486
23 feet Y = -1705504
20 meter
Z = 3878245
52 Z = 1182089
24
XDOT = 387
745671 XDOT = 118
184881
YDOT = -14783
237478 feet/sec YDOT = -4505
930783 meter/sec
ZDOT = -19354
481238 ZDOT = -5899
245881
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 07050
53391264
00020000 00000-0 20000-3 0 9071
2 25544 51
6343 352
0140 0020965 226
1194 133
8240 15
78404094 32194
Satellite: ISS
Catalog Number: 25544
Epoch time: 07050
53391264 = yrday
fracday
Element set: 907
Inclination: 51
6343 deg
RA of node: 352
0140 deg
Eccentricity:
0020965
Arg of perigee: 226
1194 deg
Mean anomaly: 133
8240 deg
Mean motion: 15
78404094 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3219
Checksum: 267
Coasting Arc #9 (Orbit 3234)
---------------------------------------
Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 655533
66 A = 6707432
68 meter
Y = 4133430
49 meter E =
0018715
Z = 5252740
10 I = 51
53868
XDOT = -7533
385635 Wp = 226
63865
YDOT = 1559
181261 meter/sec RA = 346
53107 deg
ZDOT = -300
079505 TA = 226
13714
MA = 226
29192
Ha = 186
453 n
mi
Hp = 175
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2150700
99 X = 583747
90
Y = 13561123
65 feet Y = 4140360
03 meter
Z = 17233399
28 Z = 5255749
97
XDOT = -24715
832135 XDOT = -7548
803020
YDOT = 5115
424085 feet/sec YDOT = 1474
852511 meter/sec
ZDOT = -984
512811 ZDOT = -336
713628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5154130
00 X = -1570978
82
Y = 12710503
35 feet Y = 3874161
42 meter
Z = 17245222
20 Z = 5256343
73
XDOT = -22933
311205 XDOT = -6990
073255
YDOT = -7836
495534 feet/sec YDOT = -2388
563839 meter/sec
ZDOT = -1121
901056 ZDOT = -341
955442
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 07051
54688480
00020000 00000-0 20000-3 0 9083
2 25544 51
6344 346
7776 0021001 230
3990 129
5321 15
78470500 32358
Satellite: ISS
Catalog Number: 25544
Epoch time: 07051
54688480 = yrday
fracday
Element set: 908
Inclination: 51
6344 deg
RA of node: 346
7776 deg
Eccentricity:
0021001
Arg of perigee: 230
3990 deg
Mean anomaly: 129
5321 deg
Mean motion: 15
78470500 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3235
Checksum: 283
Coasting Arc #10 (Orbit 3250)
---------------------------------------
Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6453979
80 A = 6718061
31 meter
Y = -716054
32 meter E =
0007614
Z = 1741492
73 I = 51
54697
XDOT = -968
528423 Wp = 212
14355
YDOT = 5093
600126 meter/sec RA = 341
37279 deg
ZDOT = 5688
747336 TA = 167
17206
MA = 167
15268
Ha = 186
179 n
mi
Hp = 175
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21174474
41 X = 6453047
40
Y = -2349259
57 feet Y = -643887
43 meter
Z = 5713558
82 Z = 1772843
55
XDOT = -3177
586690 XDOT = -1053
048376
YDOT = 16711
286501 feet/sec YDOT = 5082
297231 meter/sec
ZDOT = 18663
869211 ZDOT = 5683
836712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19528442
03 X = 5952269
13
Y = 8435585
85 feet Y = 2571166
57 meter
Z = 5831207
81 Z = 1777352
14
XDOT = -10515
530985 XDOT = -3205
133844
YDOT = 11465
367311 feet/sec YDOT = 3494
643956 meter/sec
ZDOT = 18646
065670 ZDOT = 5683
320816
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 07052
55983666
00020000 00000-0 20000-3 0 9090
2 25544 51
6341 341
5395 0020963 234
2586 125
6629 15
78486406 32513
Satellite: ISS
Catalog Number: 25544
Epoch time: 07052
55983666 = yrday
fracday
Element set: 909
Inclination: 51
6341 deg
RA of node: 341
5395 deg
Eccentricity:
0020963
Arg of perigee: 234
2586 deg
Mean anomaly: 125
6629 deg
Mean motion: 15
78486406 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3251
Checksum: 315
Coasting Arc #11 (Orbit 3265)
---------------------------------------
Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2234351
45 A = 6711462
38 meter
Y = -4686793
35 meter E =
0017166
Z = -4253138
53 I = 51
49839
XDOT = 6849
781444 Wp = 214
41750
YDOT = 42
718494 meter/sec RA = 336
15240 deg
ZDOT = 3530
532747 TA = 91
51312
MA = 91
31647
Ha = 185
866 n
mi
Hp = 175
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7330549
39 X = 2307254
56
Y = -15376618
60 feet Y = -4661400
08 meter
Z = -13953866
58 Z = -4242106
95
XDOT = 22473
036235 XDOT = 6831
644153
YDOT = 140
152540 feet/sec YDOT = 119
215266 meter/sec
ZDOT = 11583
112687 ZDOT = 3563
764593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13885140
89 X = 4232190
94
Y = -9925643
72 feet Y = -3025336
20 meter
Z = -13913022
88 Z = -4240689
37
XDOT = 18860
935774 XDOT = 5748
813224
YDOT = 9877
321024 feet/sec YDOT = 3010
607448 meter/sec
ZDOT = 11707
920113 ZDOT = 3568
574050
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 07053
50945854
00020000 00000-0 20000-3 0 9105
2 25544 51
6344 336
6292 0020930 237
8756 122
0378 15
78527225 32662
Satellite: ISS
Catalog Number: 25544
Epoch time: 07053
50945854 = yrday
fracday
Element set: 910
Inclination: 51
6344 deg
RA of node: 336
6292 deg
Eccentricity:
0020930
Arg of perigee: 237
8756 deg
Mean anomaly: 122
0378 deg
Mean motion: 15
78527225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3266
Checksum: 299
Coasting Arc #12 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5182385
70 A = 6711530
15 meter
Y = -909414
62 meter E =
0012836
Z = -4152734
96 I = 51
47411
XDOT = 3924
405091 Wp = 236
45660
YDOT = -5527
836307 meter/sec RA = 331
02189 deg
ZDOT = -3685
752886 TA = 355
90863
MA = 355
91911
Ha = 185
368 n
mi
Hp = 175
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17002577
77 X = -5151658
31
Y = -2983643
76 feet Y = -967195
16 meter
Z = -13624458
53 Z = -4177836
08
XDOT = 12875
344786 XDOT = 4003
831008
YDOT = -18135
945890 feet/sec YDOT = -5483
507338 meter/sec
ZDOT = -12092
365111 ZDOT = -3666
495388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13593908
72 X = -4143423
38
Y = -10517352
89 feet Y = -3205689
16 meter
Z = -13718840
52 Z = -4181502
59
XDOT = 19128
089322 XDOT = 5830
241625
YDOT = -9038
785327 feet/sec YDOT = -2755
021768 meter/sec
ZDOT = -12020
730380 ZDOT = -3663
918620
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 07054
52236730
00020000 00000-0 20000-3 0 9115
2 25544 51
6349 331
3919 0020875 241
9285 117
9770 15
78570824 32826
Satellite: ISS
Catalog Number: 25544
Epoch time: 07054
52236730 = yrday
fracday
Element set: 911
Inclination: 51
6349 deg
RA of node: 331
3919 deg
Eccentricity:
0020875
Arg of perigee: 241
9285 deg
Mean anomaly: 117
9770 deg
Mean motion: 15
78570824 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3282
Checksum: 303
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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