Date:
August 5th 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 1824)
---------------------------------------
Vector Time (GMT): 2007/215/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 912554
60 A = 6715425
10 meter
Y = -4383145
98 meter E =
0011595
Z = 5006822
24 I = 51
41291
XDOT = 6642
022862 Wp = 171
38699
YDOT = 3458
320384 meter/sec RA = 218
59420 deg
ZDOT = 1805
104255 TA = 261
10188
MA = 261
23317
Ha = 188
218 n
mi
Hp = 180
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2993945
53 X = 937177
75
Y = -14380400
20 feet Y = -4372803
80 meter
Z = 16426582
16 Z = 5011315
03
XDOT = 21791
413588 XDOT = 6594
088976
YDOT = 11346
195487 feet/sec YDOT = 3532
327143 meter/sec
ZDOT = 5922
258055 ZDOT = 1837
254604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13153509
37 X = -4009189
66
Y = 6496436
40 feet Y = 1980113
81 meter
Z = 16443044
92 Z = 5011840
09
XDOT = -3851
342746 XDOT = -1173
889269
YDOT = -23195
193789 feet/sec YDOT = -7069
895067 meter/sec
ZDOT = 6044
461998 ZDOT = 1842
352017
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
54166254
00020000 00000-0 20000-3 0 9007
2 25544 51
6303 219
2552 0008723 198
5727 161
5120 15
76041243 18250
Satellite: ISS
Catalog Number: 25544
Epoch time: 07215
54166254 = yrday
fracday
Element set: 900
Inclination: 51
6303 deg
RA of node: 219
2552 deg
Eccentricity:
0008723
Arg of perigee: 198
5727 deg
Mean anomaly: 161
5120 deg
Mean motion: 15
76041243 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1825
Checksum: 269
Coasting Arc #2 (Orbit 1839)
---------------------------------------
Vector Time (GMT): 2007/216/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5925513
36 A = 6725807
12 meter
Y = -3054960
55 meter E =
0003005
Z = -894321
58 I = 51
47264
XDOT = 1511
235460 Wp = 96
94930
YDOT = -4663
704364 meter/sec RA = 213
40535 deg
ZDOT = 5934
655865 TA = 253
26553
MA = 253
29852
Ha = 188
031 n
mi
Hp = 180
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19440660
63 X = -5886567
51
Y = -10022836
46 feet Y = -3121005
18 meter
Z = -2934125
92 Z = -923013
15
XDOT = 4958
121589 XDOT = 1534
444025
YDOT = -15300
867335 feet/sec YDOT = -4646
675422 meter/sec
ZDOT = 19470
655725 ZDOT = 5942
053543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4314411
40 X = 1315032
60
Y = 21427330
89 feet Y = 6531050
46 meter
Z = -3043185
27 Z = -927562
87
XDOT = -13412
712817 XDOT = -4088
194866
YDOT = 5462
361407 feet/sec YDOT = 1664
927757 meter/sec
ZDOT = 19498
085994 ZDOT = 5943
016611
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
49276264
00020000 00000-0 20000-3 0 9016
2 25544 51
6308 214
3558 0008842 201
7886 158
2903 15
76105660 18405
Satellite: ISS
Catalog Number: 25544
Epoch time: 07216
49276264 = yrday
fracday
Element set: 901
Inclination: 51
6308 deg
RA of node: 214
3558 deg
Eccentricity:
0008842
Arg of perigee: 201
7886 deg
Mean anomaly: 158
2903 deg
Mean motion: 15
76105660 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1840
Checksum: 293
Coasting Arc #3 (Orbit 1855)
---------------------------------------
Vector Time (GMT): 2007/217/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1777382
68 A = 6714285
50 meter
Y = 3796664
22 meter E =
0013253
Z = -5254076
84 I = 51
45709
XDOT = -6855
493193 Wp = 123
39297
YDOT = -3492
169062 meter/sec RA = 208
25159 deg
ZDOT = -211
927844 TA = 144
63352
MA = 144
54555
Ha = 187
833 n
mi
Hp = 181
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5831308
00 X = -1794182
14
Y = 12456247
45 feet Y = 3776695
00 meter
Z = -17237784
91 Z = -5262751
86
XDOT = -22491
775568 XDOT = -6814
904223
YDOT = -11457
247579 feet/sec YDOT = -3568
604087 meter/sec
ZDOT = -695
301324 ZDOT = -245
133434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13249150
02 X = 4038340
92
Y = -3536221
81 feet Y = -1077840
41 meter
Z = -17270166
22 Z = -5263946
66
XDOT = 5275
724899 XDOT = 1608
040949
YDOT = 23657
755991 feet/sec YDOT = 7210
884026 meter/sec
ZDOT = -821
521720 ZDOT = -250
399820
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
50726361
00020000 00000-0 20000-3 0 9028
2 25544 51
6299 209
1282 0008667 206
9275 153
1441 15
76050291 18561
Satellite: ISS
Catalog Number: 25544
Epoch time: 07217
50726361 = yrday
fracday
Element set: 902
Inclination: 51
6299 deg
RA of node: 209
1282 deg
Eccentricity:
0008667
Arg of perigee: 206
9275 deg
Mean anomaly: 153
1441 deg
Mean motion: 15
76050291 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1856
Checksum: 291
Coasting Arc #4 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2007/218/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5984141
73 A = 6726178
21 meter
Y = 3003151
24 meter E =
0016043
Z = -522743
76 I = 51
52307
XDOT = -2574
284957 Wp = 169
55907
YDOT = 4091
785509 meter/sec RA = 203
09225 deg
ZDOT = -6006
195293 TA = 16
14714
MA = 16
09607
Ha = 187
647 n
mi
Hp = 181
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19633010
94 X = 5952654
69
Y = 9852858
39 feet Y = 3069893
28 meter
Z = -1715038
59 Z = -493749
05
XDOT = -8445
816788 XDOT = -2590
671651
YDOT = 13424
493139 feet/sec YDOT = 4062
907407 meter/sec
ZDOT = -19705
365136 ZDOT = -6018
740516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5320143
80 X = -1621579
83
Y = -21321254
99 feet Y = -6498718
52 meter
Z = -1604820
86 Z = -489149
40
XDOT = 14060
335120 XDOT = 4285
590144
YDOT = -2033
288336 feet/sec YDOT = -619
746285 meter/sec
ZDOT = -19752
375301 ZDOT = -6020
523992
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
52175796
00020000 00000-0 20000-3 0 9032
2 25544 51
6295 203
9009 0008536 210
8977 149
1686 15
76076367 18720
Satellite: ISS
Catalog Number: 25544
Epoch time: 07218
52175796 = yrday
fracday
Element set: 903
Inclination: 51
6295 deg
RA of node: 203
9009 deg
Eccentricity:
0008536
Arg of perigee: 210
8977 deg
Mean anomaly: 149
1686 deg
Mean motion: 15
76076367 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1872
Checksum: 324
Coasting Arc #5 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2007/219/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2725010
57 A = 6714772
08 meter
Y = -3392708
12 meter E =
0004663
Z = 5114261
46 I = 51
51112
XDOT = 6791
261687 Wp = 198
35568
YDOT = 3360
419519 meter/sec RA = 197
91535 deg
ZDOT = -1394
017005 TA = 264
98334
MA = 265
03657
Ha = 187
405 n
mi
Hp = 181
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8940323
40 X = 2737901
80
Y = -11130932
16 feet Y = -3362164
08 meter
Z = 16779073
02 Z = 5127530
37
XDOT = 22281
042281 XDOT = 6759
952080
YDOT = 11024
998422 feet/sec YDOT = 3436
188344 meter/sec
ZDOT = -4573
546604 ZDOT = -1361
100876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14196387
52 X = -4327058
92
Y = 783816
17 feet Y = 238907
17 meter
Z = 16828919
70 Z = 5129454
72
XDOT = -6522
836535 XDOT = -1988
160576
YDOT = -22961
200702 feet/sec YDOT = -6998
573974 meter/sec
ZDOT = -4448
414657 ZDOT = -1355
876788
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
53624507
00020000 00000-0 20000-3 0 9044
2 25544 51
6288 198
6738 0008571 215
8469 144
2121 15
76084172 18881
Satellite: ISS
Catalog Number: 25544
Epoch time: 07219
53624507 = yrday
fracday
Element set: 904
Inclination: 51
6288 deg
RA of node: 198
6738 deg
Eccentricity:
0008571
Arg of perigee: 215
8469 deg
Mean anomaly: 144
2121 deg
Mean motion: 15
76084172 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1888
Checksum: 317
Coasting Arc #6 (Orbit 1903)
---------------------------------------
Vector Time (GMT): 2007/220/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5783265
22 A = 6724563
96 meter
Y = -2856274
41 meter E =
0007581
Z = 1897653
43 I = 51
57242
XDOT = 3698
411572 Wp = 99
19521
YDOT = -3737
395982 meter/sec RA = 192
78603 deg
ZDOT = 5625
617358 TA = 281
92220
MA = 282
00718
Ha = 187
260 n
mi
Hp = 181
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18973967
27 X = -5760114
47
Y = -9370979
03 feet Y = -2920816
95 meter
Z = 6225897
09 Z = 1869614
49
XDOT = 12133
896235 XDOT = 3712
600890
YDOT = -12261
797841 feet/sec YDOT = -3695
959687 meter/sec
ZDOT = 18456
749861 ZDOT = 5643
618002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5975853
28 X = 1821440
08
Y = 20333025
21 feet Y = 6197506
08 meter
Z = 6119292
44 Z = 1865160
33
XDOT = -15686
340427 XDOT = -4781
196562
YDOT = -985
135057 feet/sec YDOT = -300
269165 meter/sec
ZDOT = 18524
489812 ZDOT = 5646
264495
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
55072353
00020000 00000-0 20000-3 0 9055
2 25544 51
6287 193
4469 0008720 219
2004 140
8529 15
76147256 19049
Satellite: ISS
Catalog Number: 25544
Epoch time: 07220
55072353 = yrday
fracday
Element set: 905
Inclination: 51
6287 deg
RA of node: 193
4469 deg
Eccentricity:
0008720
Arg of perigee: 219
2004 deg
Mean anomaly: 140
8529 deg
Mean motion: 15
76147256 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1904
Checksum: 286
Coasting Arc #7 (Orbit 1918)
---------------------------------------
Vector Time (GMT): 2007/221/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3719531
29 A = 6716941
69 meter
Y = 3188542
11 meter E =
0010567
Z = -4603342
63 I = 51
57481
XDOT = -6364
614606 Wp = 157
02479
YDOT = -3189
716822 meter/sec RA = 187
58942 deg
ZDOT = 2925
955699 TA = 142
04030
MA = 141
96577
Ha = 187
041 n
mi
Hp = 182
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12203186
64 X = -3732547
77
Y = 10461096
16 feet Y = 3146876
04 meter
Z = -15102830
15 Z = -4621443
01
XDOT = -20881
281517 XDOT = -6342
687213
YDOT = -10464
950204 feet/sec YDOT = -3260
767305 meter/sec
ZDOT = 9599
592188 ZDOT = 2895
089763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15932830
44 X = 4856326
72
Y = 1559703
58 feet Y = 475397
65 meter
Z = -15171025
49 Z = -4624128
57
XDOT = 6974
821819 XDOT = 2125
925691
YDOT = 21214
672899 feet/sec YDOT = 6466
232300 meter/sec
ZDOT = 9482
215923 ZDOT = 2890
179413
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
50179453
00020000 00000-0 20000-3 0 9061
2 25544 51
6287 188
5459 0008461 223
9324 136
1168 15
76084801 19191
Satellite: ISS
Catalog Number: 25544
Epoch time: 07221
50179453 = yrday
fracday
Element set: 906
Inclination: 51
6287 deg
RA of node: 188
5459 deg
Eccentricity:
0008461
Arg of perigee: 223
9324 deg
Mean anomaly: 136
1168 deg
Mean motion: 15
76084801 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1919
Checksum: 304
Coasting Arc #8 (Orbit 1934)
---------------------------------------
Vector Time (GMT): 2007/222/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5257342
46 A = 6721850
44 meter
Y = 2735249
29 meter E =
0006827
Z = -3162980
87 I = 51
62109
XDOT = -4788
008952 Wp = 195
92397
YDOT = 3621
732507 meter/sec RA = 182
48156 deg
ZDOT = -4830
415812 TA = 20
99154
MA = 20
96352
Ha = 186
881 n
mi
Hp = 182
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17248498
87 X = 5241730
61
Y = 8973915
00 feet Y = 2793952
92 meter
Z = -10377233
83 Z = -3137478
86
XDOT = -15708
690786 XDOT = -4804
687073
YDOT = 11882
324498 feet/sec YDOT = 3568
097591 meter/sec
ZDOT = -15847
820906 ZDOT = -4853
715556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5759477
47 X = -1755488
73
Y = -18624558
57 feet Y = -5676765
45 meter
Z = -10280227
77 Z = -3133413
43
XDOT = 18069
344465 XDOT = 5507
536193
YDOT = 3200
946447 feet/sec YDOT = 975
648477 meter/sec
ZDOT = -15935
675600 ZDOT = -4857
193923
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
51626125
00020000 00000-0 20000-3 0 9077
2 25544 51
6295 183
3184 0008405 228
2510 131
7936 15
76125713 19351
Satellite: ISS
Catalog Number: 25544
Epoch time: 07222
51626125 = yrday
fracday
Element set: 907
Inclination: 51
6295 deg
RA of node: 183
3184 deg
Eccentricity:
0008405
Arg of perigee: 228
2510 deg
Mean anomaly: 131
7936 deg
Mean motion: 15
76125713 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1935
Checksum: 280
Coasting Arc #9 (Orbit 1950)
---------------------------------------
Vector Time (GMT): 2007/223/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4581759
96 A = 6719911
99 meter
Y = -3181122
12 meter E =
0006022
Z = 3740480
48 I = 51
64413
XDOT = 5627
482638 Wp = 127
67432
YDOT = 3102
394466 meter/sec RA = 177
27843 deg
ZDOT = -4253
690129 TA = 7
07027
MA = 7
06178
Ha = 186
520 n
mi
Hp = 182
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15032020
88 X = 4598821
09
Y = -10436752
37 feet Y = -3129791
24 meter
Z = 12271917
58 Z = 3762779
28
XDOT = 18462
869547 XDOT = 5613
036108
YDOT = 10178
459535 feet/sec YDOT = 3165
243750 meter/sec
ZDOT = -13955
676276 ZDOT = -4226
387303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17991662
97 X = -5483858
87
Y = -3019224
44 feet Y = -920259
61 meter
Z = 12356041
44 Z = 3766121
43
XDOT = -6337
666800 XDOT = -1931
720841
YDOT = -18935
095808 feet/sec YDOT = -5771
417202 meter/sec
ZDOT = -13851
782556 ZDOT = -4222
023323
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
53072093
00020000 00000-0 20000-3 0 9080
2 25544 51
6298 178
0915 0008437 232
8656 127
1738 15
76137907 19519
Satellite: ISS
Catalog Number: 25544
Epoch time: 07223
53072093 = yrday
fracday
Element set: 908
Inclination: 51
6298 deg
RA of node: 178
0915 deg
Eccentricity:
0008437
Arg of perigee: 232
8656 deg
Mean anomaly: 127
1738 deg
Mean motion: 15
76137907 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1951
Checksum: 311
Coasting Arc #10 (Orbit 1966)
---------------------------------------
Vector Time (GMT): 2007/224/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4492160
79 A = 6718440
58 meter
Y = -2726072
45 meter E =
0008014
Z = 4189047
88 I = 51
66914
XDOT = 5671
951638 Wp = 160
08316
YDOT = -3702
616768 meter/sec RA = 172
17936 deg
ZDOT = 3663
396749 TA = 252
54004
MA = 252
62766
Ha = 186
429 n
mi
Hp = 182
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14738060
33 X = -4481692
70
Y = -8943807
24 feet Y = -2776248
05 meter
Z = 13743595
40 Z = 4167250
77
XDOT = 18608
765215 XDOT = 5695
137628
YDOT = -12147
692810 feet/sec YDOT = -3639
060397 meter/sec
ZDOT = 12019
018205 ZDOT = 3691
006486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4608235
99 X = 1404590
33
Y = 16680540
78 feet Y = 5084228
83 meter
Z = 13660609
26 Z = 4163753
70
XDOT = -20599
116493 XDOT = -6278
610707
YDOT = -4263
103371 feet/sec YDOT = -1299
393908 meter/sec
ZDOT = 12123
214879 ZDOT = 3695
155895
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
54517226
00020000 00000-0 20000-3 0 9095
2 25544 51
6309 172
8646 0008594 236
4548 123
5796 15
76177068 19672
Satellite: ISS
Catalog Number: 25544
Epoch time: 07224
54517226 = yrday
fracday
Element set: 909
Inclination: 51
6309 deg
RA of node: 172
8646 deg
Eccentricity:
0008594
Arg of perigee: 236
4548 deg
Mean anomaly: 123
5796 deg
Mean motion: 15
76177068 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1967
Checksum: 329
Coasting Arc #11 (Orbit 1981)
---------------------------------------
Vector Time (GMT): 2007/225/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5251112
80 A = 6723116
75 meter
Y = 3307717
01 meter E =
0003520
Z = -2584267
20 I = 51
71326
XDOT = -4613
400949 Wp = 252
78307
YDOT = -3202
172435 meter/sec RA = 166
98302 deg
ZDOT = 5268
725231 TA = 77
89285
MA = 77
85341
Ha = 186
188 n
mi
Hp = 183
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17228060
37 X = -5275156
30
Y = 10852089
93 feet Y = 3248861
77 meter
Z = -8478566
94 Z = -2609834
79
XDOT = -15135
829886 XDOT = -4602
844820
YDOT = -10505
815075 feet/sec YDOT = -3253
703257 meter/sec
ZDOT = 17285
843935 ZDOT = 5246
339378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20001231
18 X = 6096375
26
Y = 3588707
46 feet Y = 1093838
03 meter
Z = -8575077
11 Z = -2613683
50
XDOT = 4410
026131 XDOT = 1344
175965
YDOT = 16574
738274 feet/sec YDOT = 5051
980226 meter/sec
ZDOT = 17200
554707 ZDOT = 5242
729075
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
49621627
00020000 00000-0 20000-3 0 9103
2 25544 51
6309 167
9638 0008437 241
0522 118
9796 15
76138916 19822
Satellite: ISS
Catalog Number: 25544
Epoch time: 07225
49621627 = yrday
fracday
Element set: 910
Inclination: 51
6309 deg
RA of node: 167
9638 deg
Eccentricity:
0008437
Arg of perigee: 241
0522 deg
Mean anomaly: 118
9796 deg
Mean motion: 15
76138916 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1982
Checksum: 317
Coasting Arc #12 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2007/226/11:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3526258
87 A = 6715559
92 meter
Y = 2926066
48 meter E =
0004334
Z = -4913093
12 I = 51
71670
XDOT = -6278
846842 Wp = 91
23564
YDOT = 3880
033631 meter/sec RA = 161
87641 deg
ZDOT = -2197
434786 TA = 157
45798
MA = 157
43894
Ha = 186
011 n
mi
Hp = 183
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11569090
79 X = 3517143
52
Y = 9599955
66 feet Y = 2965448
22 meter
Z = -16119071
90 Z = -4895984
99
XDOT = -20599
891215 XDOT = -6311
092773
YDOT = 12729
769129 feet/sec YDOT = 3809
639767 meter/sec
ZDOT = -7209
431714 ZDOT = -2228
015067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2380138
16 X = -725466
11
Y = -14914329
05 feet Y = -4545887
50 meter
Z = -16053822
61 Z = -4893205
13
XDOT = 22747
763071 XDOT = 6933
518184
YDOT = 4248
056769 feet/sec YDOT = 1294
807703 meter/sec
ZDOT = -7324
877929 ZDOT = -2232
622793
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
51065493
00020000 00000-0 20000-3 0 9111
2 25544 51
6319 162
7366 0008420 244
9870 115
0420 15
76173144 19985
Satellite: ISS
Catalog Number: 25544
Epoch time: 07226
51065493 = yrday
fracday
Element set: 911
Inclination: 51
6319 deg
RA of node: 162
7366 deg
Eccentricity:
0008420
Arg of perigee: 244
9870 deg
Mean anomaly: 115
0420 deg
Mean motion: 15
76173144 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1998
Checksum: 288
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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