Date:
August 4th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 2421 88 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 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 1796)
---------------------------------------
Vector Time (GMT): 2007/213/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3775055
52 A = 6725976
77 meter
Y = 5444676
51 meter E =
0016509
Z = -1099367
00 I = 51
41233
XDOT = -4559
770265 Wp = 166
45069
YDOT = 1978
278928 meter/sec RA = 227
65604 deg
ZDOT = -5893
598521 TA = 25
63771
MA = 25
55595
Ha = 188
435 n
mi
Hp = 180
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12385352
76 X = 3719232
20
Y = 17863111
91 feet Y = 5486579
24 meter
Z = -3606847
11 Z = -1081163
44
XDOT = -14959
876199 XDOT = -4552
923297
YDOT = 6490
416430 feet/sec YDOT = 1927
327597 meter/sec
ZDOT = -19335
953152 ZDOT = -5915
732727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20326387
26 X = -6195482
84
Y = -7734537
72 feet Y = -2357487
10 meter
Z = -3537228
19 Z = -1078147
15
XDOT = 8025
719683 XDOT = 2446
239359
YDOT = -12261
895010 feet/sec YDOT = -3737
425599 meter/sec
ZDOT = -19419
531668 ZDOT = -5919
073252
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 07213
76625360
00020000 00000-0 20000-3 0 9007
2 25544 51
6314 228
4024 0008660 193
2113 166
8825 15
76004757 17976
Satellite: ISS
Catalog Number: 25544
Epoch time: 07213
76625360 = yrday
fracday
Element set: 900
Inclination: 51
6314 deg
RA of node: 228
4024 deg
Eccentricity:
0008660
Arg of perigee: 193
2113 deg
Mean anomaly: 166
8825 deg
Mean motion: 15
76004757 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1797
Checksum: 285
Coasting Arc #2 (Orbit 1812)
---------------------------------------
Vector Time (GMT): 2007/214/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4316506
63 A = 6715615
50 meter
Y = -1402629
85 meter E =
0005411
Z = 4946269
21 I = 51
39815
XDOT = 4276
759252 Wp = 154
80674
YDOT = 6088
497853 meter/sec RA = 222
46155 deg
ZDOT = -2009
727648 TA = 314
66288
MA = 314
70697
Ha = 188
138 n
mi
Hp = 180
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14161767
16 X = 4307842
48
Y = -4601803
97 feet Y = -1354408
88 meter
Z = 16227917
35 Z = 4967217
41
XDOT = 14031
362374 XDOT = 4218
121671
YDOT = 19975
386658 feet/sec YDOT = 6135
995203 meter/sec
ZDOT = -6593
594646 ZDOT = -1989
093627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8808848
89 X = -2684937
14
Y = 11897938
16 feet Y = 3626491
55 meter
Z = 16307078
19 Z = 4970397
43
XDOT = -22167
424514 XDOT = -6756
630992
YDOT = -7501
157958 feet/sec YDOT = -2286
352946 meter/sec
ZDOT = -6514
681151 ZDOT = -1985
674815
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 07214
78078226
00020000 00000-0 20000-3 0 9014
2 25544 51
6314 223
1761 0008573 197
3201 162
7671 15
76030752 18139
Satellite: ISS
Catalog Number: 25544
Epoch time: 07214
78078226 = yrday
fracday
Element set: 901
Inclination: 51
6314 deg
RA of node: 223
1761 deg
Eccentricity:
0008573
Arg of perigee: 197
3201 deg
Mean anomaly: 162
7671 deg
Mean motion: 15
76030752 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1813
Checksum: 275
Coasting Arc #3 (Orbit 1828)
---------------------------------------
Vector Time (GMT): 2007/215/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3611114
10 A = 6723979
78 meter
Y = -5144993
05 meter E =
0011097
Z = 2385647
47 I = 51
44873
XDOT = 5375
954402 Wp = 111
61783
YDOT = -1275
190048 meter/sec RA = 217
33151 deg
ZDOT = 5363
386584 TA = 275
36495
MA = 275
49155
Ha = 188
105 n
mi
Hp = 181
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11847487
20 X = -3564902
59
Y = -16879898
46 feet Y = -5185116
28 meter
Z = 7826927
39 Z = 2368216
85
XDOT = 17637
645677 XDOT = 5363
760063
YDOT = -4183
694383 feet/sec YDOT = -1215
141500 meter/sec
ZDOT = 17596
412677 ZDOT = 5389
473088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19583442
05 X = 5969033
14
Y = 6543843
63 feet Y = 1994563
54 meter
Z = 7760259
35 Z = 2365327
05
XDOT = -11166
507437 XDOT = -3403
551467
YDOT = 12339
054774 feet/sec YDOT = 3760
943895 meter/sec
ZDOT = 17695
053632 ZDOT = 5393
452347
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 07215
79530509
00020000 00000-0 20000-3 0 9024
2 25544 51
6317 217
9486 0008537 201
2226 158
8585 15
76029047 18291
Satellite: ISS
Catalog Number: 25544
Epoch time: 07215
79530509 = yrday
fracday
Element set: 902
Inclination: 51
6317 deg
RA of node: 217
9486 deg
Eccentricity:
0008537
Arg of perigee: 201
2226 deg
Mean anomaly: 158
8585 deg
Mean motion: 15
76029047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1829
Checksum: 307
Coasting Arc #4 (Orbit 1843)
---------------------------------------
Vector Time (GMT): 2007/216/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5076598
01 A = 6718119
92 meter
Y = 878922
07 meter E =
0011938
Z = -4322104
48 I = 51
45384
XDOT = -3906
166130 Wp = 156
33314
YDOT = -5675
693886 meter/sec RA = 212
12086 deg
ZDOT = 3426
373467 TA = 148
40636
MA = 148
33464
Ha = 187
891 n
mi
Hp = 181
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16655505
27 X = -5065053
02
Y = 2883602
59 feet Y = 822217
49 meter
Z = -14180132
79 Z = -4346738
40
XDOT = -12815
505676 XDOT = -3859
054006
YDOT = -18621
042933 feet/sec YDOT = -5719
111615 meter/sec
ZDOT = 11241
382767 ZDOT = 3407
511493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11428278
42 X = 3483339
26
Y = -12347621
52 feet Y = -3763555
04 meter
Z = -14273327
60 Z = -4350510
25
XDOT = 20633
708759 XDOT = 6289
154430
YDOT = 6158
033522 feet/sec YDOT = 1876
968617 meter/sec
ZDOT = 11169
222175 ZDOT = 3404
378919
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 07216
74641371
00020000 00000-0 20000-3 0 9031
2 25544 51
6324 213
0483 0008506 204
9362 155
1392 15
76048206 18441
Satellite: ISS
Catalog Number: 25544
Epoch time: 07216
74641371 = yrday
fracday
Element set: 903
Inclination: 51
6324 deg
RA of node: 213
0483 deg
Eccentricity:
0008506
Arg of perigee: 204
9362 deg
Mean anomaly: 155
1392 deg
Mean motion: 15
76048206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1844
Checksum: 274
Coasting Arc #5 (Orbit 1859)
---------------------------------------
Vector Time (GMT): 2007/217/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3138651
59 A = 6720891
65 meter
Y = 4765914
22 meter E =
0006923
Z = -3544850
46 I = 51
48874
XDOT = -6235
643348 Wp = 171
37199
YDOT = 799
671663 meter/sec RA = 207
00813 deg
ZDOT = -4453
838314 TA = 51
03152
MA = 50
96986
Ha = 187
750 n
mi
Hp = 181
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10297413
36 X = 3102345
37
Y = 15636201
52 feet Y = 4800809
69 meter
Z = -11630086
80 Z = -3529690
71
XDOT = -20458
147467 XDOT = -6222
486053
YDOT = 2623
594695 feet/sec YDOT = 730
015125 meter/sec
ZDOT = -14612
330425 ZDOT = -4484
098983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17826426
73 X = -5433494
87
Y = -5838865
74 feet Y = -1779686
28 meter
Z = -11572061
01 Z = -3527164
19
XDOT = 13930
670121 XDOT = 4246
068253
YDOT = -13395
360272 feet/sec YDOT = -4082
905811 meter/sec
ZDOT = -14726
856820 ZDOT = -4488
745959
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 07217
76092329
00020000 00000-0 20000-3 0 9048
2 25544 51
6330 207
8218 0008494 209
2972 150
7717 15
76060134 18600
Satellite: ISS
Catalog Number: 25544
Epoch time: 07217
76092329 = yrday
fracday
Element set: 904
Inclination: 51
6330 deg
RA of node: 207
8218 deg
Eccentricity:
0008494
Arg of perigee: 209
2972 deg
Mean anomaly: 150
7717 deg
Mean motion: 15
76060134 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1860
Checksum: 290
Coasting Arc #6 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2007/218/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5771864
17 A = 6721259
10 meter
Y = -585744
99 meter E =
0010583
Z = 3379826
14 I = 51
51574
XDOT = 3240
017436 Wp = 131
75788
YDOT = 5251
750035 meter/sec RA = 201
79530 deg
ZDOT = -4620
631188 TA = 8
22084
MA = 8
20352
Ha = 187
487 n
mi
Hp = 181
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18936562
24 X = 5761566
55
Y = -1921735
53 feet Y = -521258
70 meter
Z = 11088668
43 Z = 3407840
69
XDOT = 10629
978465 XDOT = 3203
496901
YDOT = 17230
151035 feet/sec YDOT = 5287
778047 meter/sec
ZDOT = -15159
551142 ZDOT = -4604
979363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13384382
32 X = -4079559
73
Y = 13445500
16 feet Y = 4098188
45 meter
Z = 11194724
65 Z = 3412152
07
XDOT = -18226
317312 XDOT = -5555
381517
YDOT = -5565
279026 feet/sec YDOT = -1696
297047 meter/sec
ZDOT = -15099
596016 ZDOT = -4602
356866
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 07218
77542710
00020000 00000-0 20000-3 0 9055
2 25544 51
6322 202
5952 0008456 212
6750 147
3892 15
76053493 18761
Satellite: ISS
Catalog Number: 25544
Epoch time: 07218
77542710 = yrday
fracday
Element set: 905
Inclination: 51
6322 deg
RA of node: 202
5952 deg
Eccentricity:
0008456
Arg of perigee: 212
6750 deg
Mean anomaly: 147
3892 deg
Mean motion: 15
76053493 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1876
Checksum: 298
Coasting Arc #7 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2007/219/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2436922
94 A = 6717754
43 meter
Y = -4414341
66 meter E =
0010665
Z = 4441383
54 I = 51
53149
XDOT = 6967
704105 Wp = 161
26658
YDOT = -587
976090 meter/sec RA = 196
68454 deg
ZDOT = 3226
606352 TA = 256
32091
MA = 256
43967
Ha = 187
405 n
mi
Hp = 181
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7995154
00 X = -2408955
28
Y = -14482748
21 feet Y = -4441436
90 meter
Z = 14571468
30 Z = 4429612
41
XDOT = 22859
921603 XDOT = 6958
086929
YDOT = -1929
055414 feet/sec YDOT = -510
113491 meter/sec
ZDOT = 10585
978846 ZDOT = 3260
431787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15527468
75 X = 4732772
48
Y = 5821000
05 feet Y = 1774240
82 meter
Z = 14526315
58 Z = 4427620
99
XDOT = -15716
139059 XDOT = -4790
279185
YDOT = 15086
524452 feet/sec YDOT = 4598
372653 meter/sec
ZDOT = 10714
064624 ZDOT = 3265
646897
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 07219
78992270
00020000 00000-0 20000-3 0 9068
2 25544 51
6326 197
3679 0008419 217
2098 142
8483 15
76070834 18929
Satellite: ISS
Catalog Number: 25544
Epoch time: 07219
78992270 = yrday
fracday
Element set: 906
Inclination: 51
6326 deg
RA of node: 197
3679 deg
Eccentricity:
0008419
Arg of perigee: 217
2098 deg
Mean anomaly: 142
8483 deg
Mean motion: 15
76070834 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1892
Checksum: 329
Coasting Arc #8 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2007/220/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6339375
13 A = 6724048
21 meter
Y = 485230
14 meter E =
0002405
Z = -2190767
41 I = 51
58146
XDOT = -2272
399740 Wp = 218
74246
YDOT = -4900
762185 meter/sec RA = 191
48293 deg
ZDOT = 5485
051667 TA = 116
68787
MA = 116
66325
Ha = 187
146 n
mi
Hp = 181
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20798474
82 X = -6333687
67
Y = 1591962
40 feet Y = 414371
77 meter
Z = -7187557
10 Z = -2221549
83
XDOT = -7455
379726 XDOT = -2244
074855
YDOT = -16078
616093 feet/sec YDOT = -4926
015809 meter/sec
ZDOT = 17995
576336 ZDOT = 5474
080623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14547047
47 X = 4433940
07
Y = -14893112
21 feet Y = -4539420
60 meter
Z = -7304142
30 Z = -2226302
57
XDOT = 15201
168213 XDOT = 4633
316071
YDOT = 6034
888573 feet/sec YDOT = 1839
434037 meter/sec
ZDOT = 17953
387916 ZDOT = 5472
192637
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 07220
74100581
00020000 00000-0 20000-3 0 9073
2 25544 51
6328 192
4673 0008459 221
6244 138
4277 15
76098218 19072
Satellite: ISS
Catalog Number: 25544
Epoch time: 07220
74100581 = yrday
fracday
Element set: 907
Inclination: 51
6328 deg
RA of node: 192
4673 deg
Eccentricity:
0008459
Arg of perigee: 221
6244 deg
Mean anomaly: 138
4277 deg
Mean motion: 15
76098218 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1907
Checksum: 297
Coasting Arc #9 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2007/221/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1480101
84 A = 6715111
61 meter
Y = 4188254
71 meter E =
0007470
Z = -5041152
14 I = 51
57971
XDOT = -7480
228574 Wp = 111
82960
YDOT = 554
795586 meter/sec RA = 186
36129 deg
ZDOT = -1740
075042 TA = 141
43254
MA = 141
37915
Ha = 186
912 n
mi
Hp = 182
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4855977
15 X = 1457646
71
Y = 13740993
15 feet Y = 4204681
13 meter
Z = -16539213
05 Z = -5034015
94
XDOT = -24541
432331 XDOT = -7477
423622
YDOT = 1820
195491 feet/sec YDOT = 471
163364 meter/sec
ZDOT = -5708
907618 ZDOT = -1776
406452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12904965
28 X = -3933433
42
Y = -6838756
23 feet Y = -2084452
90 meter
Z = -16511640
12 Z = -5032747
91
XDOT = 16412
171014 XDOT = 5002
429725
YDOT = -16892
280655 feet/sec YDOT = -5148
767144 meter/sec
ZDOT = -5846
530407 ZDOT = -1782
022468
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 07221
75548780
00020000 00000-0 20000-3 0 9083
2 25544 51
6326 187
2402 0008436 226
3213 133
7253 15
76119667 19237
Satellite: ISS
Catalog Number: 25544
Epoch time: 07221
75548780 = yrday
fracday
Element set: 908
Inclination: 51
6326 deg
RA of node: 187
2402 deg
Eccentricity:
0008436
Arg of perigee: 226
3213 deg
Mean anomaly: 133
7253 deg
Mean motion: 15
76119667 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1923
Checksum: 292
Coasting Arc #10 (Orbit 1938)
---------------------------------------
Vector Time (GMT): 2007/222/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6646194
45 A = 6725979
81 meter
Y = -513092
79 meter E =
0014347
Z = 821970
51 I = 51
64508
XDOT = 1106
902965 Wp = 161
69190
YDOT = 4748
881370 meter/sec RA = 181
18502 deg
ZDOT = -5971
077774 TA = 9
32966
MA = 9
30304
Ha = 186
858 n
mi
Hp = 182
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21805099
90 X = 6647445
08
Y = -1683375
30 feet Y = -438764
40 meter
Z = 2696753
63 Z = 854259
97
XDOT = 3631
571408 XDOT = 1082
723761
YDOT = 15580
319455 feet/sec YDOT = 4761
124834 meter/sec
ZDOT = -19590
150178 ZDOT = -5965
758778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14714945
40 X = -4485115
36
Y = 16158334
99 feet Y = 4925060
50 meter
Z = 2819079
01 Z = 859255
28
XDOT = -12223
706674 XDOT = -3725
785794
YDOT = -7709
586657 feet/sec YDOT = -2349
882013 meter/sec
ZDOT = -19569
387214 ZDOT = -5964
749223
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 07222
76996480
00020000 00000-0 20000-3 0 9090
2 25544 51
6329 182
0134 0008523 228
9289 131
1139 15
76069515 19391
Satellite: ISS
Catalog Number: 25544
Epoch time: 07222
76996480 = yrday
fracday
Element set: 909
Inclination: 51
6329 deg
RA of node: 182
0134 deg
Eccentricity:
0008523
Arg of perigee: 228
9289 deg
Mean anomaly: 131
1139 deg
Mean motion: 15
76069515 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1939
Checksum: 313
Coasting Arc #11 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2007/223/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -429194
39 A = 6714063
44 meter
Y = -4148518
20 meter E =
0006944
Z = 5265530
67 I = 51
63450
XDOT = 7674
721195 Wp = 220
41873
YDOT = -629
672073 meter/sec RA = 176
04224 deg
ZDOT = 124
370387 TA = 228
37135
MA = 228
43085
Ha = 186
580 n
mi
Hp = 182
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1408118
09 X = -408351
51
Y = -13610624
01 feet Y = -4153201
58 meter
Z = 17275363
09 Z = 5263495
98
XDOT = 25179
531479 XDOT = 7680
587730
YDOT = -2065
853258 feet/sec YDOT = -543
816227 meter/sec
ZDOT = 408
039329 ZDOT = 161
667452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10574688
55 X = 3223165
07
Y = 8700148
10 feet Y = 2651805
14 meter
Z = 17267120
12 Z = 5263018
21
XDOT = -15960
036411 XDOT = -4864
619098
YDOT = 18275
275575 feet/sec YDOT = 5570
303995 meter/sec
ZDOT = 549
346739 ZDOT = 167
440886
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 07223
78443172
00020000 00000-0 20000-3 0 9100
2 25544 51
6331 176
7859 0008468 234
2484 125
7893 15
76124743 19552
Satellite: ISS
Catalog Number: 25544
Epoch time: 07223
78443172 = yrday
fracday
Element set: 910
Inclination: 51
6331 deg
RA of node: 176
7859 deg
Eccentricity:
0008468
Arg of perigee: 234
2484 deg
Mean anomaly: 125
7893 deg
Mean motion: 15
76124743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1955
Checksum: 314
Coasting Arc #12 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2007/224/17:40:42
002
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6669992
46 A = 6725907
19 meter
Y = 576191
01 meter E =
0004887
Z = 615989
93 I = 51
70314
XDOT = 139
725187 Wp = 38
47967
YDOT = -4822
963865 meter/sec RA = 170
89613 deg
ZDOT = 6002
686531 TA = 328
22462
MA = 328
25410
Ha = 186
327 n
mi
Hp = 182
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21883177
38 X = -6678932
09
Y = 1890390
44 feet Y = 501553
37 meter
Z = 2020964
35 Z = 583566
24
XDOT = 458
415969 XDOT = 164
486662
YDOT = -15823
372262 feet/sec YDOT = -4821
263264 meter/sec
ZDOT = 19693
853449 ZDOT = 6003
425176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14077111
10 X = 4290703
46
Y = -16874935
11 feet Y = -5143480
22 meter
Z = 1898113
03 Z = 578544
85
XDOT = 9758
237357 XDOT = 2974
310746
YDOT = 10364
274647 feet/sec YDOT = 3159
030913 meter/sec
ZDOT = 19696
032953 ZDOT = 6003
350844
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 07224
79889187
00020000 00000-0 20000-3 0 9113
2 25544 51
6328 171
5580 0008561 238
6282 121
4045 15
76156338 19715
Satellite: ISS
Catalog Number: 25544
Epoch time: 07224
79889187 = yrday
fracday
Element set: 911
Inclination: 51
6328 deg
RA of node: 171
5580 deg
Eccentricity:
0008561
Arg of perigee: 238
6282 deg
Mean anomaly: 121
4045 deg
Mean motion: 15
76156338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1971
Checksum: 310
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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