Date:
October 30th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5920 15 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3180)
---------------------------------------
Vector Time (GMT): 2007/301/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2894768
79 A = 6714824
90 meter
Y = 2981862
02 meter E =
0016736
Z = -5288441
31 I = 51
83887
XDOT = -5498
379451 Wp = 97
19144
YDOT = 5378
826076 meter/sec RA = 135
50593 deg
ZDOT = 21
148259 TA = 173
02059
MA = 172
99725
Ha = 187
925 n
mi
Hp = 180
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9497272
92 X = 2886901
09
Y = 9783011
89 feet Y = 3014189
30 meter
Z = -17350529
24 Z = -5274397
02
XDOT = -18039
302662 XDOT = -5558
220376
YDOT = 17647
067180 feet/sec YDOT = 5317
005497 meter/sec
ZDOT = 69
384051 ZDOT = -5
708724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13539234
22 X = -4126758
59
Y = -2111405
55 feet Y = -643556
41 meter
Z = -17296747
76 Z = -5272048
72
XDOT = 3766
331414 XDOT = 1147
977815
YDOT = -23942
012927 feet/sec YDOT = -7297
525540 meter/sec
ZDOT = -32
109022 ZDOT = -9
786830
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 07301
51860703
00020000 00000-0 20000-3 0 9000
2 25544 51
6333 136
3465 0002555 142
7217 217
4124 15
75854970 31817
Satellite: ISS
Catalog Number: 25544
Epoch time: 07301
51860703 = yrday
fracday
Element set: 900
Inclination: 51
6333 deg
RA of node: 136
3465 deg
Eccentricity:
0002555
Arg of perigee: 142
7217 deg
Mean anomaly: 217
4124 deg
Mean motion: 15
75854970 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3181
Checksum: 269
Coasting Arc #2 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2007/302/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4717165
45 A = 6726584
14 meter
Y = -4740063
37 meter E =
0013216
Z = -666485
96 I = 51
89941
XDOT = 2968
901914 Wp = 141
07975
YDOT = 3789
995531 meter/sec RA = 130
37912 deg
ZDOT = -6015
626334 TA = 46
16024
MA = 46
05109
Ha = 187
810 n
mi
Hp = 180
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15476264
62 X = 4773056
71
Y = -15551389
00 feet Y = -4687000
80 meter
Z = -2186633
72 Z = -643433
99
XDOT = 9740
491845 XDOT = 2955
524498
YDOT = 12434
368541 feet/sec YDOT = 3823
121117 meter/sec
ZDOT = -19736
306869 ZDOT = -6001
235270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2752792
56 X = -839051
17
Y = 21775123
31 feet Y = 6637057
58 meter
Z = -2099516
93 Z = -639932
76
XDOT = -13809
408423 XDOT = -4209
107687
YDOT = -3619
012829 feet/sec YDOT = -1103
075110 meter/sec
ZDOT = -19681
105953 ZDOT = -5998
801095
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 07302
53323267
00020000 00000-0 20000-3 0 9013
2 25544 51
6340 131
1212 0002403 145
4878 214
6443 15
75905349 31970
Satellite: ISS
Catalog Number: 25544
Epoch time: 07302
53323267 = yrday
fracday
Element set: 901
Inclination: 51
6340 deg
RA of node: 131
1212 deg
Eccentricity:
0002403
Arg of perigee: 145
4878 deg
Mean anomaly: 214
6443 deg
Mean motion: 15
75905349 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3197
Checksum: 265
Coasting Arc #3 (Orbit 3212)
---------------------------------------
Vector Time (GMT): 2007/303/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2331925
43 A = 6715393
61 meter
Y = -3661800
40 meter E =
0004984
Z = 5119319
52 I = 51
87905
XDOT = 5263
103872 Wp = 84
90885
YDOT = -5431
687432 meter/sec RA = 125
22722 deg
ZDOT = -1486
149951 TA = 19
28723
MA = 19
26838
Ha = 187
857 n
mi
Hp = 180
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7650673
98 X = -2315674
50
Y = -12013780
83 feet Y = -3687786
80 meter
Z = 16795667
70 Z = 5108030
03
XDOT = 17267
401154 XDOT = 5330
670232
YDOT = -17820
496824 feet/sec YDOT = -5372
454540 meter/sec
ZDOT = -4875
820049 ZDOT = -1460
417574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13553260
89 X = 4131033
92
Y = 4541858
21 feet Y = 1384358
38 meter
Z = 16752278
63 Z = 5106094
53
XDOT = -2039
357205 XDOT = -621
596076
YDOT = 23731
158414 feet/sec YDOT = 7233
257084 meter/sec
ZDOT = -4778
572819 ZDOT = -1456
508995
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 07303
54783665
00020000 00000-0 20000-3 0 9028
2 25544 51
6336 125
8946 0002531 151
3153 208
8151 15
75898087 32133
Satellite: ISS
Catalog Number: 25544
Epoch time: 07303
54783665 = yrday
fracday
Element set: 902
Inclination: 51
6336 deg
RA of node: 125
8946 deg
Eccentricity:
0002531
Arg of perigee: 151
3153 deg
Mean anomaly: 208
8151 deg
Mean motion: 15
75898087 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3213
Checksum: 293
Coasting Arc #4 (Orbit 3228)
---------------------------------------
Vector Time (GMT): 2007/304/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4442180
44 A = 6725058
59 meter
Y = 4663034
01 meter E =
0014473
Z = 1917375
43 I = 51
92753
XDOT = -2422
422200 Wp = 77
29122
YDOT = -4644
420261 meter/sec RA = 120
12443 deg
ZDOT = 5650
510986 TA = 303
96016
MA = 304
09763
Ha = 187
669 n
mi
Hp = 180
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14574082
81 X = -4503307
43
Y = 15298668
01 feet Y = 4613017
15 meter
Z = 6290601
80 Z = 1895646
79
XDOT = -7947
579396 XDOT = -2397
757097
YDOT = -15237
599281 feet/sec YDOT = -4671
371559 meter/sec
ZDOT = 18538
421871 ZDOT = 5638
802350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1486585
10 X = 453111
14
Y = -21101412
61 feet Y = -6431710
56 meter
Z = 6208482
47 Z = 1892345
46
XDOT = 14383
907217 XDOT = 4384
214920
YDOT = 6486
144156 feet/sec YDOT = 1976
976739 meter/sec
ZDOT = 18493
317835 ZDOT = 5636
763276
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 07304
56241612
00020000 00000-0 20000-3 0 9033
2 25544 51
6334 120
6677 0002546 154
7671 205
3617 15
75958598 32293
Satellite: ISS
Catalog Number: 25544
Epoch time: 07304
56241612 = yrday
fracday
Element set: 903
Inclination: 51
6334 deg
RA of node: 120
6677 deg
Eccentricity:
0002546
Arg of perigee: 154
7671 deg
Mean anomaly: 205
3617 deg
Mean motion: 15
75958598 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3229
Checksum: 298
Coasting Arc #5 (Orbit 3243)
---------------------------------------
Vector Time (GMT): 2007/305/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1938944
84 A = 6717169
17 meter
Y = 4461050
03 meter E =
0012675
Z = -4644818
48 I = 51
91528
XDOT = -4912
025098 Wp = 118
45061
YDOT = 5159
705002 meter/sec RA = 114
95382 deg
ZDOT = 2905
131006 TA = 180
21787
MA = 180
21842
Ha = 187
583 n
mi
Hp = 180
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6361367
58 X = 1911480
55
Y = 14635990
92 feet Y = 4482579
02 meter
Z = -15238905
76 Z = -4635465
53
XDOT = -16115
567908 XDOT = -4983
469388
YDOT = 16928
166018 feet/sec YDOT = 5104
376389 meter/sec
ZDOT = 9531
269704 ZDOT = 2881
094753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14424121
63 X = -4396472
27
Y = -6908221
46 feet Y = -2105625
90 meter
Z = -15202784
88 Z = -4633808
83
XDOT = 742
064986 XDOT = 226
181408
YDOT = -22324
357812 feet/sec YDOT = -6804
464261 meter/sec
ZDOT = 9440
419051 ZDOT = 2877
439727
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 07305
51356371
00020000 00000-0 20000-3 0 9049
2 25544 51
6339 115
7678 0002617 156
2582 203
8703 15
75994051 32441
Satellite: ISS
Catalog Number: 25544
Epoch time: 07305
51356371 = yrday
fracday
Element set: 904
Inclination: 51
6339 deg
RA of node: 115
7678 deg
Eccentricity:
0002617
Arg of perigee: 156
2582 deg
Mean anomaly: 203
8703 deg
Mean motion: 15
75994051 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3244
Checksum: 292
Coasting Arc #6 (Orbit 3259)
---------------------------------------
Vector Time (GMT): 2007/306/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4146401
18 A = 6722148
57 meter
Y = -4267559
56 meter E =
0006293
Z = -3128311
65 I = 51
94388
XDOT = 2057
237575 Wp = 122
40132
YDOT = 5578
161290 meter/sec RA = 109
87020 deg
ZDOT = -4893
216679 TA = 93
82638
MA = 93
75443
Ha = 187
483 n
mi
Hp = 180
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13603678
40 X = 4209010
45
Y = -14001179
67 feet Y = -4220842
05 meter
Z = -10263489
66 Z = -3108016
19
XDOT = 6749
467110 XDOT = 2018
479467
YDOT = 18301
054100 feet/sec YDOT = 5600
949852 meter/sec
ZDOT = -16053
860494 ZDOT = -4883
316565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -912982
53 X = -278277
07
Y = 19540437
06 feet Y = 5955925
22 meter
Z = -10186761
05 Z = -3104924
77
XDOT = -15843
801844 XDOT = -4829
190802
YDOT = -9071
524865 feet/sec YDOT = -2765
000779 meter/sec
ZDOT = -16015
523482 ZDOT = -4881
531557
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 07306
52809733
00020000 00000-0 20000-3 0 9057
2 25544 51
6342 110
5418 0002451 157
8305 202
2965 15
76049105 32609
Satellite: ISS
Catalog Number: 25544
Epoch time: 07306
52809733 = yrday
fracday
Element set: 905
Inclination: 51
6342 deg
RA of node: 110
5418 deg
Eccentricity:
0002451
Arg of perigee: 157
8305 deg
Mean anomaly: 202
2965 deg
Mean motion: 15
76049105 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3260
Checksum: 268
Coasting Arc #7 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2007/307/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1712581
76 A = 6720031
81 meter
Y = -5250945
69 meter E =
0012091
Z = 3817003
78 I = 51
94470
XDOT = 4590
073707 Wp = 94
00002
YDOT = -4555
010500 meter/sec RA = 104
68906 deg
ZDOT = -4196
284611 TA = 39
77824
MA = 39
68965
Ha = 187
450 n
mi
Hp = 180
336
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5618706
57 X = -1672280
17
Y = -17227512
10 feet Y = -5269871
40 meter
Z = 12522978
30 Z = 3808781
86
XDOT = 15059
296940 XDOT = 4661
052436
YDOT = -14944
260170 feet/sec YDOT = -4503
284842 meter/sec
ZDOT = -13767
337962 ZDOT = -4173
813322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15849708
52 X = 4830991
16
Y = 8828476
95 feet Y = 2690919
77 meter
Z = 12491067
07 Z = 3807277
24
XDOT = -380
396919 XDOT = -115
944981
YDOT = 20090
328485 feet/sec YDOT = 6123
532122 meter/sec
ZDOT = -13682
357396 ZDOT = -4170
382534
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 07307
54260772
00020000 00000-0 20000-3 0 9065
2 25544 51
6335 105
3146 0002535 164
0789 196
0455 15
76047403 32760
Satellite: ISS
Catalog Number: 25544
Epoch time: 07307
54260772 = yrday
fracday
Element set: 906
Inclination: 51
6335 deg
RA of node: 105
3146 deg
Eccentricity:
0002535
Arg of perigee: 164
0789 deg
Mean anomaly: 196
0455 deg
Mean motion: 15
76047403 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3276
Checksum: 287
Coasting Arc #8 (Orbit 3291)
---------------------------------------
Vector Time (GMT): 2007/308/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3886597
98 A = 6718776
68 meter
Y = 3598314
32 meter E =
0011804
Z = 4128177
07 I = 51
94786
XDOT = -1917
726784 Wp = 115
44312
YDOT = -6431
653280 meter/sec RA = 99
61015 deg
ZDOT = 3787
324527 TA = 295
87914
MA = 296
00079
Ha = 187
276 n
mi
Hp = 180
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12751305
70 X = -3946600
28
Y = 11805493
18 feet Y = 3554516
75 meter
Z = 13543888
04 Z = 4109149
87
XDOT = -6291
754540 XDOT = -1864
062981
YDOT = -21101
224671 feet/sec YDOT = -6452
798286 meter/sec
ZDOT = 12425
605402 ZDOT = 3778
138494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1150331
33 X = 350620
99
Y = -17395030
70 feet Y = -5302005
36 meter
Z = 13471897
20 Z = 4106234
27
XDOT = 17888
828375 XDOT = 5452
514889
YDOT = 10812
550741 feet/sec YDOT = 3295
665466 meter/sec
ZDOT = 12389
888358 ZDOT = 3776
437972
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 07308
55709205
00020000 00000-0 20000-3 0 9077
2 25544 51
6341 100
0876 0002521 169
0987 191
0232 15
76128009 32927
Satellite: ISS
Catalog Number: 25544
Epoch time: 07308
55709205 = yrday
fracday
Element set: 907
Inclination: 51
6341 deg
RA of node: 100
0876 deg
Eccentricity:
0002521
Arg of perigee: 169
0987 deg
Mean anomaly: 191
0232 deg
Mean motion: 15
76128009 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3292
Checksum: 276
Coasting Arc #9 (Orbit 3306)
---------------------------------------
Vector Time (GMT): 2007/309/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1668448
22 A = 6722895
92 meter
Y = 5922749
42 meter E =
0004515
Z = -2711754
33 I = 51
96665
XDOT = -4367
485988 Wp = 86
90441
YDOT = 3612
177240 meter/sec RA = 94
43252 deg
ZDOT = 5209
836457 TA = 242
29858
MA = 242
34440
Ha = 187
161 n
mi
Hp = 180
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5473911
48 X = 1615268
63
Y = 19431592
59 feet Y = 5941109
56 meter
Z = -8896831
79 Z = -2703778
11
XDOT = -14329
022270 XDOT = -4432
862273
YDOT = 11850
975197 feet/sec YDOT = 3562
972089 meter/sec
ZDOT = 17092
639296 ZDOT = 5188
459900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17573310
33 X = -5356344
99
Y = -9963972
71 feet Y = -3037018
88 meter
Z = -8865783
95 Z = -2702290
95
XDOT = 1230
469994 XDOT = 375
047254
YDOT = -17284
542505 feet/sec YDOT = -5268
328556 meter/sec
ZDOT = 17011
704088 ZDOT = 5185
167406
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 07309
50815062
00020000 00000-0 20000-3 0 9083
2 25544 51
6352 95
1877 0002479 169
3979 190
7238 15
76143727 33073
Satellite: ISS
Catalog Number: 25544
Epoch time: 07309
50815062 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 95
1877 deg
Eccentricity:
0002479
Arg of perigee: 169
3979 deg
Mean anomaly: 190
7238 deg
Mean motion: 15
76143727 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3307
Checksum: 318
Coasting Arc #10 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2007/310/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3793812
03 A = 6715665
02 meter
Y = -2637228
52 meter E =
0012045
Z = -4884289
59 I = 51
94387
XDOT = 1912
528306 Wp = 84
01355
YDOT = 7077
183092 meter/sec RA = 89
34447 deg
ZDOT = -2339
400627 TA = 163
29526
MA = 163
25555
Ha = 187
031 n
mi
Hp = 180
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12446889
85 X = 3846747
55
Y = -8652324
55 feet Y = -2594508
05 meter
Z = -16024572
13 Z = -4865730
16
XDOT = 6274
699167 XDOT = 1844
612709
YDOT = 23219
104633 feet/sec YDOT = 7098
190304 meter/sec
ZDOT = -7675
198907 ZDOT = -2330
274384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2599414
22 X = -792301
45
Y = 15009328
62 feet Y = 4574843
36 meter
Z = -15954240
79 Z = -4862852
59
XDOT = -19907
805957 XDOT = -6067
899256
YDOT = -11555
505281 feet/sec YDOT = -3522
118010 meter/sec
ZDOT = -7639
647847 ZDOT = -2328
564664
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 07310
52258782
00020000 00000-0 20000-3 0 9098
2 25544 51
6355 89
9612 0002324 173
2185 186
9011 15
76188435 33235
Satellite: ISS
Catalog Number: 25544
Epoch time: 07310
52258782 = yrday
fracday
Element set: 909
Inclination: 51
6355 deg
RA of node: 89
9612 deg
Eccentricity:
0002324
Arg of perigee: 173
2185 deg
Mean anomaly: 186
9011 deg
Mean motion: 15
76188435 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3323
Checksum: 295
Coasting Arc #11 (Orbit 3338)
---------------------------------------
Vector Time (GMT): 2007/311/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1691726
03 A = 6725131
37 meter
Y = -6363465
18 meter E =
0015352
Z = 1327357
37 I = 51
97425
XDOT = 4374
969558 Wp = 127
77367
YDOT = -2396
458453 meter/sec RA = 84
18246 deg
ZDOT = -5876
326429 TA = 37
69777
MA = 37
59030
Ha = 186
928 n
mi
Hp = 180
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5550282
25 X = -1626891
32
Y = -20877510
42 feet Y = -6382020
51 meter
Z = 4354847
02 Z = 1319296
21
XDOT = 14353
574665 XDOT = 4429
988933
YDOT = -7862
396498 feet/sec YDOT = -2347
227433 meter/sec
ZDOT = -19279
286183 ZDOT = -5854
938554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18990245
47 X = 5788226
82
Y = 10311120
12 feet Y = 3142829
41 meter
Z = 4323441
43 Z = 1317784
95
XDOT = -3486
294216 XDOT = -1062
622477
YDOT = 14521
237549 feet/sec YDOT = 4426
073205 meter/sec
ZDOT = -19198
157465 ZDOT = -5851
598395
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 07311
53700029
00020000 00000-0 20000-3 0 9108
2 25544 51
6354 84
7331 0002320 178
4050 181
7122 15
76214865 33399
Satellite: ISS
Catalog Number: 25544
Epoch time: 07311
53700029 = yrday
fracday
Element set: 910
Inclination: 51
6354 deg
RA of node: 84
7331 deg
Eccentricity:
0002320
Arg of perigee: 178
4050 deg
Mean anomaly: 181
7122 deg
Mean motion: 15
76214865 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3339
Checksum: 259
Coasting Arc #12 (Orbit 3354)
---------------------------------------
Vector Time (GMT): 2007/312/12:03:54
251
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3896284
95 A = 6713747
42 meter
Y = 1514811
54 meter E =
0004291
Z = 5251634
58 I = 51
93370
XDOT = -1970
786283 Wp = 144
11815
YDOT = -7420
043504 meter/sec RA = 79
07047 deg
ZDOT = 674
437754 TA = 299
47862
MA = 299
52142
Ha = 186
822 n
mi
Hp = 180
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12783087
09 X = -3938446
53
Y = 4969854
13 feet Y = 1471005
24 meter
Z = 17229772
24 Z = 5232603
43
XDOT = -6465
834261 XDOT = -1890
944164
YDOT = -24343
974752 feet/sec YDOT = -7441
635545 meter/sec
ZDOT = 2212
722290 ZDOT = 665
057174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5029659
99 X = 1533040
36
Y = -12856680
28 feet Y = -3918716
15 meter
Z = 17157508
85 Z = 5229608
70
XDOT = 21394
406765 XDOT = 6521
015182
YDOT = 11290
046610 feet/sec YDOT = 3441
206207 meter/sec
ZDOT = 2176
187029 ZDOT = 663
301806
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 07312
55138682
00020000 00000-0 20000-3 0 9112
2 25544 51
6368 79
5062 0002152 184
1903 175
9244 15
76281795 33555
Satellite: ISS
Catalog Number: 25544
Epoch time: 07312
55138682 = yrday
fracday
Element set: 911
Inclination: 51
6368 deg
RA of node: 79
5062 deg
Eccentricity:
0002152
Arg of perigee: 184
1903 deg
Mean anomaly: 175
9244 deg
Mean motion: 15
76281795 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3355
Checksum: 299
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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