Date:
July 11th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 962)
---------------------------------------
Vector Time (GMT): 2009/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6683162
92 A = 6731163
93 meter
Y = 172287
38 meter E =
0016209
Z = 689030
89 I = 51
61727
XDOT = 497
007903 Wp = 154
28824
YDOT = 4825
206958 meter/sec RA = 186
15944 deg
ZDOT = -5989
176967 TA = 18
19662
MA = 18
13869
Ha = 190
131 n
mi
Hp = 184
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21926387
52 X = 6677392
53
Y = 565247
30 feet Y = 246990
06 meter
Z = 2260600
05 Z = 721483
18
XDOT = 1630
603356 XDOT = 472
108537
YDOT = 15830
731488 feet/sec YDOT = 4830
626375 meter/sec
ZDOT = -19649
530731 ZDOT = -5986
822373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6152890
35 X = -1875400
98
Y = -21038907
43 feet Y = -6412658
98 meter
Z = 2388012
01 Z = 727866
06
XDOT = 13007
346266 XDOT = 3964
639142
YDOT = -6046
659938 feet/sec YDOT = -1843
021949 meter/sec
ZDOT = -19639
999291 ZDOT = -5986
271784
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 09191
53316125
00010596 00000-0 82463-4 0 9006
2 25544 51
6352 187
0208 0007318 209
0752 151
0004 15
74276931 9638
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191
53316125 = yrday
fracday
Element set: 900
Inclination: 51
6352 deg
RA of node: 187
0208 deg
Eccentricity:
0007318
Arg of perigee: 209
0752 deg
Mean anomaly: 151
0004 deg
Mean motion: 15
74276931 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 963
Checksum: 284
Coasting Arc #2 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2009/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -674741
34 A = 6719479
06 meter
Y = -4160849
98 meter E =
0007661
Z = 5234858
44 I = 51
60728
XDOT = 7661
117848 Wp = 190
69347
YDOT = -391
899483 meter/sec RA = 181
03257 deg
ZDOT = 668
735124 TA = 252
90282
MA = 252
98675
Ha = 190
018 n
mi
Hp = 184
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2213718
31 X = -653593
49
Y = -13651082
61 feet Y = -4168277
69 meter
Z = 17174732
43 Z = 5231631
49
XDOT = 25134
901076 XDOT = 7661
682197
YDOT = -1285
759458 feet/sec YDOT = -306
225301 meter/sec
ZDOT = 2194
012875 ZDOT = 705
953634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12180949
57 X = -3712753
43
Y = 6581848
13 feet Y = 2006147
31 meter
Z = 17161811
73 Z = 5230920
22
XDOT = -8818
788670 XDOT = -2687
966786
YDOT = -22484
541522 feet/sec YDOT = -6853
288256 meter/sec
ZDOT = 2340
115366 ZDOT = 713
267164
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 09192
54881126
00010596 00000-0 82463-4 0 9017
2 25544 51
6349 181
8021 0007347 213
9240 146
1454 15
74276727 9791
Satellite: ISS
Catalog Number: 25544
Epoch time: 09192
54881126 = yrday
fracday
Element set: 901
Inclination: 51
6349 deg
RA of node: 181
8021 deg
Eccentricity:
0007347
Arg of perigee: 213
9240 deg
Mean anomaly: 146
1454 deg
Mean motion: 15
74276727 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 979
Checksum: 318
Coasting Arc #3 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2009/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6659642
48 A = 6731081
81 meter
Y = 848564
77 meter E =
0003832
Z = -466176
31 I = 51
67706
XDOT = -1016
611557 Wp = 51
29236
YDOT = -4693
465952 meter/sec RA = 175
88480 deg
ZDOT = 6015
060449 TA = 303
64196
MA = 303
67851
Ha = 189
804 n
mi
Hp = 184
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21849220
75 X = -6666371
74
Y = 2784005
15 feet Y = 774055
17 meter
Z = -1529449
83 Z = -498544
76
XDOT = -3335
339754 XDOT = -993
272620
YDOT = -15398
510340 feet/sec YDOT = -4704
704414 meter/sec
ZDOT = 19734
450292 ZDOT = 6010
178016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10000531
57 X = 3048162
02
Y = 19614376
11 feet Y = 5978461
84 meter
Z = -1656492
40 Z = -504898
88
XDOT = -11896
167853 XDOT = -3625
951961
YDOT = 7721
271885 feet/sec YDOT = 2353
443670 meter/sec
ZDOT = 19714
994116 ZDOT = 6009
130207
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 09193
50097240
00010596 00000-0 82463-4 0 9021
2 25544 51
6350 176
9102 0007403 216
1688 143
8976 15
74343260 9949
Satellite: ISS
Catalog Number: 25544
Epoch time: 09193
50097240 = yrday
fracday
Element set: 902
Inclination: 51
6350 deg
RA of node: 176
9102 deg
Eccentricity:
0007403
Arg of perigee: 216
1688 deg
Mean anomaly: 143
8976 deg
Mean motion: 15
74343260 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 994
Checksum: 310
Coasting Arc #4 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2009/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1085989
99 A = 6719273
74 meter
Y = 4041382
45 meter E =
0011089
Z = -5265419
40 I = 51
66672
XDOT = -7530
799671 Wp = 114
73246
YDOT = 1532
010581 meter/sec RA = 170
75670 deg
ZDOT = -382
533060 TA = 151
66400
MA = 151
60364
Ha = 189
600 n
mi
Hp = 184
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3562959
29 X = 1066296
13
Y = 13259128
77 feet Y = 4053417
02 meter
Z = -17274998
03 Z = -5260191
14
XDOT = -24707
348003 XDOT = -7545
512905
YDOT = 5026
281434 feet/sec YDOT = 1447
714541 meter/sec
ZDOT = -1255
029725 ZDOT = -419
153030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11102857
43 X = 3384150
95
Y = -8120536
55 feet Y = -2475139
54 meter
Z = -17254221
94 Z = -5259086
85
XDOT = 12853
829224 XDOT = 3917
847147
YDOT = 20510
324522 feet/sec YDOT = 6251
546914 meter/sec
ZDOT = -1398
734771 ZDOT = -426
334358
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 09194
51660059
00010596 00000-0 82463-4 0 9038
2 25544 51
6351 171
6908 0007267 221
7573 138
3036 15
74310701 10109
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194
51660059 = yrday
fracday
Element set: 903
Inclination: 51
6351 deg
RA of node: 171
6908 deg
Eccentricity:
0007267
Arg of perigee: 221
7573 deg
Mean anomaly: 138
3036 deg
Mean motion: 15
74310701 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 287
Coasting Arc #5 (Orbit 1025)
---------------------------------------
Vector Time (GMT): 2009/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6466553
25 A = 6731168
72 meter
Y = -1823963
09 meter E =
0014140
Z = 203571
42 I = 51
73679
XDOT = 1474
954142 Wp = 163
39540
YDOT = 4544
461388 meter/sec RA = 165
61762 deg
ZDOT = -6045
823490 TA = 14
39412
MA = 14
35389
Ha = 189
329 n
mi
Hp = 184
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21215725
88 X = 6485479
59
Y = -5984130
86 feet Y = -1751544
50 meter
Z = 667885
25 Z = 235031
65
XDOT = 4839
088394 XDOT = 1453
397013
YDOT = 14909
650224 feet/sec YDOT = 4560
835261 meter/sec
ZDOT = -19835
378903 ZDOT = -6038
710089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13409602
85 X = -4087246
95
Y = -17490548
30 feet Y = -5331119
12 meter
Z = 791321
14 Z = 241194
68
XDOT = 10741
577833 XDOT = 3274
032923
YDOT = -9142
643178 feet/sec YDOT = -2786
677641 meter/sec
ZDOT = -19807
169128 ZDOT = -6037
225150
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 09195
53221678
00010596 00000-0 82463-4 0 9042
2 25544 51
6355 166
4723 0007211 226
8124 133
2437 15
74346876 10265
Satellite: ISS
Catalog Number: 25544
Epoch time: 09195
53221678 = yrday
fracday
Element set: 904
Inclination: 51
6355 deg
RA of node: 166
4723 deg
Eccentricity:
0007211
Arg of perigee: 226
8124 deg
Mean anomaly: 133
2437 deg
Mean motion: 15
74346876 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1026
Checksum: 307
Coasting Arc #6 (Orbit 1041)
---------------------------------------
Vector Time (GMT): 2009/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1481228
40 A = 6719098
79 meter
Y = -3891814
05 meter E =
0005820
Z = 5276000
63 I = 51
72467
XDOT = 7234
717147 Wp = 214
20462
YDOT = -2633
586065 meter/sec RA = 160
48957 deg
ZDOT = 83
807157 TA = 234
97363
MA = 235
02826
Ha = 189
196 n
mi
Hp = 185
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4859673
22 X = -1463229
25
Y = -12768418
79 feet Y = -3908277
96 meter
Z = 17309713
35 Z = 5268848
10
XDOT = 23735
948644 XDOT = 7263
221533
YDOT = -8640
374230 feet/sec YDOT = -2552
523856 meter/sec
ZDOT = 274
957863 ZDOT = 119
022373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9863645
08 X = -3006439
02
Y = 9504587
27 feet Y = 2896998
20 meter
Z = 17281390
14 Z = 5267367
71
XDOT = -16439
490826 XDOT = -5010
756804
YDOT = -17839
586727 feet/sec YDOT = -5437
506035 meter/sec
ZDOT = 413
103958 ZDOT = 125
914086
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 09196
54782178
00010596 00000-0 82463-4 0 9052
2 25544 51
6354 161
2540 0007250 231
0638 128
9879 15
74352257 10424
Satellite: ISS
Catalog Number: 25544
Epoch time: 09196
54782178 = yrday
fracday
Element set: 905
Inclination: 51
6354 deg
RA of node: 161
2540 deg
Eccentricity:
0007250
Arg of perigee: 231
0638 deg
Mean anomaly: 128
9879 deg
Mean motion: 15
74352257 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1042
Checksum: 316
Coasting Arc #7 (Orbit 1057)
---------------------------------------
Vector Time (GMT): 2009/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6137462
63 A = 6731054
67 meter
Y = 2755788
59 meter E =
0005237
Z = 68673
10 I = 51
79284
XDOT = -1892
201757 Wp = 34
26765
YDOT = -4370
325485 meter/sec RA = 155
35904 deg
ZDOT = 6048
944270 TA = 326
47662
MA = 326
50975
Ha = 188
951 n
mi
Hp = 185
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20136032
24 X = -6168155
78
Y = 9041301
16 feet Y = 2686984
27 meter
Z = 225305
43 Z = 38783
05
XDOT = -6208
011013 XDOT = -1872
576131
YDOT = -14338
338206 feet/sec YDOT = -4391
376255 meter/sec
ZDOT = 19845
617684 ZDOT = 6039
799031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16371030
16 X = 4989889
99
Y = 14806531
55 feet Y = 4513030
82 meter
Z = 108066
65 Z = 32938
71
XDOT = -9508
802321 XDOT = -2898
282947
YDOT = 10358
060618 feet/sec YDOT = 3157
136877 meter/sec
ZDOT = 19809
440978 ZDOT = 6037
917610
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 09197
56341342
00010596 00000-0 82463-4 0 9060
2 25544 51
6351 156
0349 0007280 234
2703 125
7784 15
74393790 10585
Satellite: ISS
Catalog Number: 25544
Epoch time: 09197
56341342 = yrday
fracday
Element set: 906
Inclination: 51
6351 deg
RA of node: 156
0349 deg
Eccentricity:
0007280
Arg of perigee: 234
2703 deg
Mean anomaly: 125
7784 deg
Mean motion: 15
74393790 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1058
Checksum: 315
Coasting Arc #8 (Orbit 1072)
---------------------------------------
Vector Time (GMT): 2009/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1816935
72 A = 6719007
51 meter
Y = 3749685
15 meter E =
0009710
Z = -5278656
20 I = 51
77946
XDOT = -6772
967863 Wp = 115
72810
YDOT = 3644
335219 meter/sec RA = 150
22813 deg
ZDOT = 253
694773 TA = 156
69890
MA = 156
65486
Ha = 188
729 n
mi
Hp = 185
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5961075
19 X = 1800513
85
Y = 12302116
62 feet Y = 3769912
18 meter
Z = -17318425
84 Z = -5269868
82
XDOT = -22221
023173 XDOT = -6814
448462
YDOT = 11956
480378 feet/sec YDOT = 3568
363959 meter/sec
ZDOT = 832
331934 ZDOT = 220
691453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8647269
17 X = 2635687
64
Y = -10644392
45 feet Y = -3244410
82 meter
Z = -17283692
01 Z = -5268069
32
XDOT = 19368
029522 XDOT = 5903
375398
YDOT = 14572
719205 feet/sec YDOT = 4441
764814 meter/sec
ZDOT = 702
898146 ZDOT = 214
243355
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 09198
51552107
00010596 00000-0 82463-4 0 9070
2 25544 51
6358 151
1419 0007276 239
3135 120
7312 15
74388554 10737
Satellite: ISS
Catalog Number: 25544
Epoch time: 09198
51552107 = yrday
fracday
Element set: 907
Inclination: 51
6358 deg
RA of node: 151
1419 deg
Eccentricity:
0007276
Arg of perigee: 239
3135 deg
Mean anomaly: 120
7312 deg
Mean motion: 15
74388554 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1073
Checksum: 307
Coasting Arc #9 (Orbit 1088)
---------------------------------------
Vector Time (GMT): 2009/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5669598
94 A = 6730964
28 meter
Y = -3593616
81 meter E =
0011863
Z = -376306
22 I = 51
84594
XDOT = 2267
273042 Wp = 174
20671
YDOT = 4206
918416 meter/sec RA = 145
10761 deg
ZDOT = -6043
082507 TA = 9
87502
MA = 9
85173
Ha = 188
524 n
mi
Hp = 185
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18601046
39 X = 5711190
02
Y = -11790081
38 feet Y = -3529983
42 meter
Z = -1234600
46 Z = -348662
96
XDOT = 7438
559850 XDOT = 2249
418200
YDOT = 13802
225773 feet/sec YDOT = 4232
173627 meter/sec
ZDOT = -19826
386177 ZDOT = -6032
110737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18686024
80 X = -5695500
36
Y = -11665904
75 feet Y = -3555767
77 meter
Z = -1126200
52 Z = -343265
92
XDOT = 8318
070517 XDOT = 2535
347894
YDOT = -11423
485527 feet/sec YDOT = -3481
878389 meter/sec
ZDOT = -19783
044718 ZDOT = -6029
872030
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 09199
53109041
00010596 00000-0 82463-4 0 9089
2 25544 51
6365 145
9232 0007281 243
3932 116
6486 15
74408933 10892
Satellite: ISS
Catalog Number: 25544
Epoch time: 09199
53109041 = yrday
fracday
Element set: 908
Inclination: 51
6365 deg
RA of node: 145
9232 deg
Eccentricity:
0007281
Arg of perigee: 243
3932 deg
Mean anomaly: 116
6486 deg
Mean motion: 15
74408933 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1089
Checksum: 321
Coasting Arc #10 (Orbit 1104)
---------------------------------------
Vector Time (GMT): 2009/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2141035
62 A = 6718942
45 meter
Y = -3599006
50 meter E =
0004476
Z = 5257698
81 I = 51
83006
XDOT = 6173
771640 Wp = 249
02166
YDOT = -4559
716616 meter/sec RA = 139
97501 deg
ZDOT = -609
127933 TA = 206
74242
MA = 206
76551
Ha = 188
278 n
mi
Hp = 185
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7024395
07 X = -2126172
55
Y = -11807764
12 feet Y = -3622866
71 meter
Z = 17249668
03 Z = 5247333
15
XDOT = 20255
156298 XDOT = 6227
259331
YDOT = -14959
700183 feet/sec YDOT = -4490
378707 meter/sec
ZDOT = -1998
451223 ZDOT = -579
006910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7357412
87 X = -2242539
44
Y = 11663799
86 feet Y = 3555126
20 meter
Z = 17208739
50 Z = 5245223
80
XDOT = -21610
205716 XDOT = -6586
790702
YDOT = -10866
869337 feet/sec YDOT = -3312
221774 meter/sec
ZDOT = -1880
349558 ZDOT = -573
130545
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 09200
54664706
00010596 00000-0 82463-4 0 9098
2 25544 51
6370 140
7049 0007308 247
8532 112
1856 15
74443086 11051
Satellite: ISS
Catalog Number: 25544
Epoch time: 09200
54664706 = yrday
fracday
Element set: 909
Inclination: 51
6370 deg
RA of node: 140
7049 deg
Eccentricity:
0007308
Arg of perigee: 247
8532 deg
Mean anomaly: 112
1856 deg
Mean motion: 15
74443086 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1105
Checksum: 299
Coasting Arc #11 (Orbit 1120)
---------------------------------------
Vector Time (GMT): 2009/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5091034
66 A = 6730698
47 meter
Y = 4340589
36 meter E =
0006919
Z = 696908
11 I = 51
89194
XDOT = -2622
188131 Wp = 31
53736
YDOT = -4043
202127 meter/sec RA = 134
86288 deg
ZDOT = 6006
069736 TA = 336
02896
MA = 336
06116
Ha = 187
976 n
mi
Hp = 185
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16702869
61 X = -5142578
90
Y = 14240778
73 feet Y = 4283370
10 meter
Z = 2286443
93 Z = 672051
83
XDOT = -8602
979434 XDOT = -2605
957452
YDOT = -13265
098843 feet/sec YDOT = -4072
435354 meter/sec
ZDOT = 19704
953201 ZDOT = 5993
369983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20369765
29 X = 6208704
46
Y = 8203316
43 feet Y = 2500370
85 meter
Z = 2188999
67 Z = 667207
10
XDOT = -7109
696520 XDOT = -2167
035499
YDOT = 12390
333297 feet/sec YDOT = 3776
573589 meter/sec
ZDOT = 19654
823341 ZDOT = 5990
790154
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 09201
56219213
00010596 00000-0 82463-4 0 9102
2 25544 51
6372 135
4852 0007313 251
8406 108
1961 15
74451757 11211
Satellite: ISS
Catalog Number: 25544
Epoch time: 09201
56219213 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 135
4852 deg
Eccentricity:
0007313
Arg of perigee: 251
8406 deg
Mean anomaly: 108
1961 deg
Mean motion: 15
74451757 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1121
Checksum: 283
Coasting Arc #12 (Orbit 1135)
---------------------------------------
Vector Time (GMT): 2009/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2441582
42 A = 6719067
94 meter
Y = 3468867
40 meter E =
0008236
Z = -5217518
74 I = 51
87416
XDOT = -5452
761513 Wp = 116
85776
YDOT = 5339
168250 meter/sec RA = 129
72610 deg
ZDOT = 995
637905 TA = 162
62183
MA = 162
59362
Ha = 187
719 n
mi
Hp = 186
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8010441
00 X = 2427956
72
Y = 11380798
57 feet Y = 3496095
31 meter
Z = -17117843
65 Z = -5205690
28
XDOT = -17889
637509 XDOT = -5516
896272
YDOT = 17516
956201 feet/sec YDOT = 5277
833514 meter/sec
ZDOT = 3266
528561 ZDOT = 968
994057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6105098
42 X = 1860834
00
Y = -12570341
15 feet Y = -3831439
98 meter
Z = -17071163
08 Z = -5203290
51
XDOT = 23038
281842 XDOT = 7022
068306
YDOT = 6883
913210 feet/sec YDOT = 2098
216746 meter/sec
ZDOT = 3162
098628 ZDOT = 963
807662
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 09202
51425432
00010596 00000-0 82463-4 0 9111
2 25544 51
6382 130
5924 0007311 255
7923 104
2429 15
74469664 11361
Satellite: ISS
Catalog Number: 25544
Epoch time: 09202
51425432 = yrday
fracday
Element set: 911
Inclination: 51
6382 deg
RA of node: 130
5924 deg
Eccentricity:
0007311
Arg of perigee: 255
7923 deg
Mean anomaly: 104
2429 deg
Mean motion: 15
74469664 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1136
Checksum: 292
Coasting Arc #13 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2009/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4419867
26 A = 6730360
99 meter
Y = -4958250
81 meter E =
0009134
Z = -1046780
57 I = 51
93124
XDOT = 2966
114690 Wp = 187
57232
YDOT = 3898
400855 meter/sec RA = 124
62419 deg
ZDOT = -5944
488741 TA = 3
83236
MA = 3
82537
Ha = 187
504 n
mi
Hp = 185
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14500876
84 X = 4480067
72
Y = -16267227
07 feet Y = -4908488
52 meter
Z = -3434319
46 Z = -1025163
84
XDOT = 9731
347408 XDOT = 2951
178206
YDOT = 12790
029052 feet/sec YDOT = 3931
486999 meter/sec
ZDOT = -19502
915817 ZDOT = -5930
115441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21317204
79 X = -6497484
02
Y = -4587972
66 feet Y = -1398414
07 meter
Z = -3349618
26 Z = -1020963
64
XDOT = 5921
562263 XDOT = 1804
892178
YDOT = -13323
490406 feet/sec YDOT = -4060
999876 meter/sec
ZDOT = -19446
201784 ZDOT = -5927
202304
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 09203
52977584
00010596 00000-0 82463-4 0 9124
2 25544 51
6391 125
3738 0007335 259
3666 100
6671 15
74478815 11521
Satellite: ISS
Catalog Number: 25544
Epoch time: 09203
52977584 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 125
3738 deg
Eccentricity:
0007335
Arg of perigee: 259
3666 deg
Mean anomaly: 100
6671 deg
Mean motion: 15
74478815 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1152
Checksum: 325
Coasting Arc #14 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2009/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2745802
04 A = 6719202
16 meter
Y = -3340094
01 meter E =
0004166
Z = 5146727
54 I = 51
90985
XDOT = 4643
151196 Wp = 295
54815
YDOT = -5979
063412 meter/sec RA = 119
48362 deg
ZDOT = -1402
233748 TA = 167
83722
MA = 167
82715
Ha = 187
047 n
mi
Hp = 185
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9008536
88 X = -2733249
73
Y = -10958313
67 feet Y = -3370729
53 meter
Z = 16885589
03 Z = 5133418
89
XDOT = 15233
435682 XDOT = 4716
476647
YDOT = -19616
349776 feet/sec YDOT = -5926
730843 meter/sec
ZDOT = -4600
504422 ZDOT = -1379
500394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4798159
93 X = -1462479
15
Y = 13415900
82 feet Y = 4089166
57 meter
Z = 16833085
23 Z = 5130724
38
XDOT = -23673
906406 XDOT = -7215
806673
YDOT = -2802
676014 feet/sec YDOT = -854
255649 meter/sec
ZDOT = -4511
463281 ZDOT = -1375
094008
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 09204
54528391
00010596 00000-0 82463-4 0 9136
2 25544 51
6388 120
1551 0007407 264
1443 95
8876 15
74533749 11687
Satellite: ISS
Catalog Number: 25544
Epoch time: 09204
54528391 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 120
1551 deg
Eccentricity:
0007407
Arg of perigee: 264
1443 deg
Mean anomaly: 95
8876 deg
Mean motion: 15
74533749 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1168
Checksum: 323
Coasting Arc #15 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2009/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3680732
23 A = 6729868
98 meter
Y = 5448728
47 meter E =
0008250
Z = 1408847
21 I = 51
95938
XDOT = -3319
570892 Wp = 36
20039
YDOT = -3757
002387 meter/sec RA = 114
38911 deg
ZDOT = 5846
830514 TA = 339
22670
MA = 339
26021
Ha = 186
685 n
mi
Hp = 185
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12075893
13 X = -3748231
06
Y = 17876405
74 feet Y = 5407190
85 meter
Z = 4622202
12 Z = 1390803
06
XDOT = -10890
980617 XDOT = -3305
714973
YDOT = -12326
123318 feet/sec YDOT = -3794
046761 meter/sec
ZDOT = 19182
514811 ZDOT = 5830
737741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21567101
51 X = 6573652
54
Y = 949339
61 feet Y = 289358
71 meter
Z = 4551561
97 Z = 1387316
09
XDOT = -4669
955009 XDOT = -1423
402287
YDOT = 14255
067388 feet/sec YDOT = 4344
944540 meter/sec
ZDOT = 19119
038955 ZDOT = 5827
483073
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 09205
56078182
00010596 00000-0 82463-4 0 9148
2 25544 51
6389 114
9352 0007336 268
2816 91
7507 15
74517491 11848
Satellite: ISS
Catalog Number: 25544
Epoch time: 09205
56078182 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 114
9352 deg
Eccentricity:
0007336
Arg of perigee: 268
2816 deg
Mean anomaly: 91
7507 deg
Mean motion: 15
74517491 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1184
Checksum: 326
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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