Date:
October 4th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2285)
---------------------------------------
Vector Time (GMT): 2009/275/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1024987
36 A = 6728554
81 meter
Y = 6285084
59 meter E =
0008251
Z = -2185164
61 I = 51
95260
XDOT = -5250
921048 Wp = 112
38575
YDOT = 1058
367389 meter/sec RA = 114
84034 deg
ZDOT = 5520
575022 TA = 223
27457
MA = 223
33942
Ha = 191
650 n
mi
Hp = 181
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3362819
41 X = -1084576
82
Y = 20620356
27 feet Y = 6273289
17 meter
Z = -7169175
24 Z = -2190289
46
XDOT = -17227
431260 XDOT = -5289
183913
YDOT = 3472
333953 feet/sec YDOT = 999
435131 meter/sec
ZDOT = 18112
122777 ZDOT = 5494
972694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4029704
45 X = -1228253
92
Y = -20493521
94 feet Y = -6246425
49 meter
Z = -7189002
79 Z = -2191208
05
XDOT = 13561
363858 XDOT = 4133
503704
YDOT = -8969
456866 feet/sec YDOT = -2733
890453 meter/sec
ZDOT = 18011
253493 ZDOT = 5489
830065
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 09275
53121376
00020000 00000-0 20000-3 0 9000
2 25544 51
6364 115
7147 0008434 155
6070 204
5494 15
74536572 22867
Satellite: ISS
Catalog Number: 25544
Epoch time: 09275
53121376 = yrday
fracday
Element set: 900
Inclination: 51
6364 deg
RA of node: 115
7147 deg
Eccentricity:
0008434
Arg of perigee: 155
6070 deg
Mean anomaly: 204
5494 deg
Mean motion: 15
74536572 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2286
Checksum: 289
Coasting Arc #2 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2009/276/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4471772
54 A = 6720225
96 meter
Y = -1069765
62 meter E =
0015543
Z = -4912271
45 I = 51
93531
XDOT = -735
787589 Wp = 106
34324
YDOT = 7311
933121 meter/sec RA = 109
75925 deg
ZDOT = -2272
325011 TA = 141
67479
MA = 141
56423
Ha = 191
611 n
mi
Hp = 181
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14671169
75 X = 4507265
83
Y = -3509729
71 feet Y = -1019561
68 meter
Z = -16116376
16 Z = -4890460
89
XDOT = -2414
001275 XDOT = -806
457471
YDOT = 23989
281892 feet/sec YDOT = 7303
309736 meter/sec
ZDOT = -7455
134549 ZDOT = -2276
071953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12487537
51 X = -3806201
43
Y = 8624672
73 feet Y = 2628800
25 meter
Z = -16030453
29 Z = -4886082
16
XDOT = -5860
012342 XDOT = -1786
131762
YDOT = -22305
611336 feet/sec YDOT = -6798
750335 meter/sec
ZDOT = -7469
477409 ZDOT = -2276
696714
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 09276
54669456
00020000 00000-0 20000-3 0 9019
2 25544 51
6357 110
4948 0008451 158
6371 201
5147 15
74556223 23022
Satellite: ISS
Catalog Number: 25544
Epoch time: 09276
54669456 = yrday
fracday
Element set: 901
Inclination: 51
6357 deg
RA of node: 110
4948 deg
Eccentricity:
0008451
Arg of perigee: 158
6371 deg
Mean anomaly: 201
5147 deg
Mean motion: 15
74556223 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2302
Checksum: 293
Coasting Arc #3 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2009/277/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 237729
32 A = 6729047
38 meter
Y = -6469091
76 meter E =
0020442
Z = 1791971
21 I = 51
97487
XDOT = 4983
300078 Wp = 132
11607
YDOT = -1407
056466 meter/sec RA = 104
60635 deg
ZDOT = -5712
869921 TA = 28
08798
MA = 27
97784
Ha = 191
302 n
mi
Hp = 181
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 779951
84 X = 301344
89
Y = -21224054
32 feet Y = -6466077
46 meter
Z = 5879170
65 Z = 1793281
27
XDOT = 16349
409704 XDOT = 5026
416355
YDOT = -4616
326988 feet/sec YDOT = -1351
089735 meter/sec
ZDOT = -18743
011551 ZDOT = -5688
555656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7344425
70 X = 2238580
95
Y = 19926660
75 feet Y = 6073646
20 meter
Z = 5883966
08 Z = 1793432
86
XDOT = -12032
823141 XDOT = -3667
604493
YDOT = 9968
024010 feet/sec YDOT = 3038
253718 meter/sec
ZDOT = -18647
234218 ZDOT = -5683
676990
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 09277
56216133
00020000 00000-0 20000-3 0 9023
2 25544 51
6360 105
2743 0008187 163
6595 196
4833 15
74611124 23184
Satellite: ISS
Catalog Number: 25544
Epoch time: 09277
56216133 = yrday
fracday
Element set: 902
Inclination: 51
6360 deg
RA of node: 105
2743 deg
Eccentricity:
0008187
Arg of perigee: 163
6595 deg
Mean anomaly: 196
4833 deg
Mean motion: 15
74611124 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2318
Checksum: 289
Coasting Arc #4 (Orbit 2333)
---------------------------------------
Vector Time (GMT): 2009/278/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4227941
03 A = 6719625
18 meter
Y = 1367244
27 meter E =
0013048
Z = 5038179
80 I = 51
94827
XDOT = -207
791794 Wp = 149
94364
YDOT = -7477
741336 meter/sec RA = 99
51983 deg
ZDOT = 1841
817520 TA = 282
30933
MA = 282
45538
Ha = 191
450 n
mi
Hp = 181
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13871197
59 X = -4267390
75
Y = 4485709
55 feet Y = 1319744
75 meter
Z = 16529461
27 Z = 5017544
00
XDOT = -681
731609 XDOT = -133
106398
YDOT = -24533
272099 feet/sec YDOT = -7479
647258 meter/sec
ZDOT = 6042
708399 ZDOT = 1840
990028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11065634
34 X = 3372805
35
Y = -9631403
04 feet Y = -2935651
65 meter
Z = 16448179
68 Z = 5013405
17
XDOT = 9633
048243 XDOT = 2936
153105
YDOT = 21454
493891 feet/sec YDOT = 6539
329738 meter/sec
ZDOT = 6039
033227 ZDOT = 1840
697328
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 09278
57762040
00020000 00000-0 20000-3 0 9039
2 25544 51
6353 100
0538 0008359 166
3186 193
8206 15
74563517 23343
Satellite: ISS
Catalog Number: 25544
Epoch time: 09278
57762040 = yrday
fracday
Element set: 903
Inclination: 51
6353 deg
RA of node: 100
0538 deg
Eccentricity:
0008359
Arg of perigee: 166
3186 deg
Mean anomaly: 193
8206 deg
Mean motion: 15
74563517 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2334
Checksum: 294
Coasting Arc #5 (Orbit 2348)
---------------------------------------
Vector Time (GMT): 2009/279/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 599161
34 A = 6729577
18 meter
Y = 6556396
02 meter E =
0006905
Z = -1403969
19 I = 51
98685
XDOT = -4711
509141 Wp = 102
55806
YDOT = 1677
669157 meter/sec RA = 94
37373 deg
ZDOT = 5846
369412 TA = 242
09204
MA = 242
16198
Ha = 191
233 n
mi
Hp = 181
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1965752
41 X = 532622
46
Y = 21510485
62 feet Y = 6562724
08 meter
Z = -4606198
14 Z = -1401220
35
XDOT = -15457
707156 XDOT = -4758
320341
YDOT = 5504
163902 feet/sec YDOT = 1624
720855 meter/sec
ZDOT = 19181
002007 ZDOT = 5823
366480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10640289
10 X = -3243160
12
Y = -18800328
30 feet Y = -5730340
07 meter
Z = -4595012
42 Z = -1400559
78
XDOT = 10570
611808 XDOT = 3221
922479
YDOT = -10630
383597 feet/sec YDOT = -3240
140920 meter/sec
ZDOT = 19090
398558 ZDOT = 5818
753481
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 09279
52959898
00020000 00000-0 20000-3 0 9045
2 25544 51
6360 95
1595 0008525 169
8434 190
2903 15
74610404 23496
Satellite: ISS
Catalog Number: 25544
Epoch time: 09279
52959898 = yrday
fracday
Element set: 904
Inclination: 51
6360 deg
RA of node: 95
1595 deg
Eccentricity:
0008525
Arg of perigee: 169
8434 deg
Mean anomaly: 190
2903 deg
Mean motion: 15
74610404 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2349
Checksum: 323
Coasting Arc #6 (Orbit 2364)
---------------------------------------
Vector Time (GMT): 2009/280/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4025396
96 A = 6718861
71 meter
Y = -1534407
20 meter E =
0016108
Z = -5167697
07 I = 51
95272
XDOT = 1143
728025 Wp = 111
50972
YDOT = 7487
364018 meter/sec RA = 89
28160 deg
ZDOT = -1341
348900 TA = 145
74896
MA = 145
64496
Ha = 191
140 n
mi
Hp = 181
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13206682
95 X = 4067360
21
Y = -5034144
35 feet Y = -1489158
35 meter
Z = -16954386
72 Z = -5148039
20
XDOT = 3752
388535 XDOT = 1066
434225
YDOT = 24564
842578 feet/sec YDOT = 7499
721650 meter/sec
ZDOT = -4400
750983 ZDOT = -1335
980469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9895253
06 X = -3016073
13
Y = 10220694
39 feet Y = 3115267
65 meter
Z = -16876957
25 Z = -5144096
57
XDOT = -13132
819536 XDOT = -4002
883394
YDOT = -19896
350204 feet/sec YDOT = -6064
407542 meter/sec
ZDOT = -4379
202804 ZDOT = -1334
781015
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 09280
54503184
00020000 00000-0 20000-3 0 9053
2 25544 51
6368 89
9401 0008476 172
7729 187
3558 15
74641046 23653
Satellite: ISS
Catalog Number: 25544
Epoch time: 09280
54503184 = yrday
fracday
Element set: 905
Inclination: 51
6368 deg
RA of node: 89
9401 deg
Eccentricity:
0008476
Arg of perigee: 172
7729 deg
Mean anomaly: 187
3558 deg
Mean motion: 15
74641046 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2365
Checksum: 318
Coasting Arc #7 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2009/281/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1409018
12 A = 6729913
67 meter
Y = -6500113
26 meter E =
0019839
Z = 944687
38 I = 51
98824
XDOT = 4505
479436 Wp = 144
50145
YDOT = -1851
882111 meter/sec RA = 84
14327 deg
ZDOT = -5975
990076 TA = 25
21714
MA = 25
12041
Ha = 190
897 n
mi
Hp = 181
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4622762
87 X = -1340817
24
Y = -21325830
90 feet Y = -6515488
39 meter
Z = 3099368
05 Z = 938007
90
XDOT = 14781
756681 XDOT = 4554
883623
YDOT = -6075
728711 feet/sec YDOT = -1801
222982 meter/sec
ZDOT = -19606
266652 ZDOT = -5953
981915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13575562
09 X = 4137831
32
Y = 17088874
62 feet Y = 5208688
98 meter
Z = 3072712
27 Z = 936562
70
XDOT = -9439
434174 XDOT = -2877
139536
YDOT = 11036
071454 feet/sec YDOT = 3363
794579 meter/sec
ZDOT = -19519
577635 ZDOT = -5949
567263
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 09281
56045094
00020000 00000-0 20000-3 0 9068
2 25544 51
6365 84
7192 0008325 178
0074 182
1124 15
74665197 23818
Satellite: ISS
Catalog Number: 25544
Epoch time: 09281
56045094 = yrday
fracday
Element set: 906
Inclination: 51
6365 deg
RA of node: 84
7192 deg
Eccentricity:
0008325
Arg of perigee: 178
0074 deg
Mean anomaly: 182
1124 deg
Mean motion: 15
74665197 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2381
Checksum: 298
Coasting Arc #8 (Orbit 2396)
---------------------------------------
Vector Time (GMT): 2009/282/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3850130
25 A = 6718450
95 meter
Y = 1689656
56 meter E =
0010313
Z = 5239031
50 I = 51
94615
XDOT = -2089
139454 Wp = 164
91358
YDOT = -7368
152861 meter/sec RA = 79
04206 deg
ZDOT = 830
924531 TA = 277
15465
MA = 277
27191
Ha = 190
888 n
mi
Hp = 182
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12631660
91 X = -3894188
89
Y = 5543492
66 feet Y = 1646355
75 meter
Z = 17188423
57 Z = 5220220
20
XDOT = -6854
132068 XDOT = -2010
628782
YDOT = -24173
729860 feet/sec YDOT = -7391
075879 meter/sec
ZDOT = 2726
130350 ZDOT = 820
965939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8794894
99 X = 2680683
99
Y = -10746199
40 feet Y = -3275441
58 meter
Z = 17114324
23 Z = 5216446
03
XDOT = 16367
575043 XDOT = 4988
836873
YDOT = 17727
093157 feet/sec YDOT = 5403
217994 meter/sec
ZDOT = 2686
511880 ZDOT = 818
848821
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 09282
57585985
00020000 00000-0 20000-3 0 9079
2 25544 51
6373 79
4993 0008333 181
2080 178
9064 15
74657335 23977
Satellite: ISS
Catalog Number: 25544
Epoch time: 09282
57585985 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 79
4993 deg
Eccentricity:
0008333
Arg of perigee: 181
2080 deg
Mean anomaly: 178
9064 deg
Mean motion: 15
74657335 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2397
Checksum: 338
Coasting Arc #9 (Orbit 2411)
---------------------------------------
Vector Time (GMT): 2009/283/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2223431
01 A = 6730107
83 meter
Y = 6333878
99 meter E =
0006759
Z = -487608
57 I = 51
98026
XDOT = -4340
576097 Wp = 89
52030
YDOT = 1982
962857 meter/sec RA = 73
91268 deg
ZDOT = 6037
143601 TA = 265
20319
MA = 265
28038
Ha = 190
657 n
mi
Hp = 182
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7294721
16 X = 2154807
98
Y = 20780442
88 feet Y = 6358359
02 meter
Z = -1599765
65 Z = -476973
62
XDOT = -14240
735227 XDOT = -4391
755106
YDOT = 6505
783651 feet/sec YDOT = 1934
137773 meter/sec
ZDOT = 19806
901577 ZDOT = 6015
932476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16245954
69 X = -4951766
99
Y = -14874207
80 feet Y = -4533658
54 meter
Z = -1557533
96 Z = -474736
35
XDOT = 8502
055513 XDOT = 2591
426520
YDOT = -11326
200496 feet/sec YDOT = -3452
225911 meter/sec
ZDOT = 19723
344611 ZDOT = 6011
675437
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 09283
52779218
00020000 00000-0 20000-3 0 9080
2 25544 51
6387 74
6059 0008406 184
5425 175
5664 15
74689389 24123
Satellite: ISS
Catalog Number: 25544
Epoch time: 09283
52779218 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 74
6059 deg
Eccentricity:
0008406
Arg of perigee: 184
5425 deg
Mean anomaly: 175
5664 deg
Mean motion: 15
74689389 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2412
Checksum: 335
Coasting Arc #10 (Orbit 2427)
---------------------------------------
Vector Time (GMT): 2009/284/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3762025
33 A = 6718055
07 meter
Y = -1761469
50 meter E =
0015832
Z = -5291380
21 I = 51
93062
XDOT = 2967
975981 Wp = 118
95739
YDOT = 7092
020293 meter/sec RA = 68
80183 deg
ZDOT = -258
811276 TA = 148
64050
MA = 148
54599
Ha = 190
487 n
mi
Hp = 182
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12342602
80 X = 3807147
61
Y = -5779099
40 feet Y = -1719148
05 meter
Z = -17360171
28 Z = -5272994
49
XDOT = 9737
454005 XDOT = 2889
708464
YDOT = 23267
783112 feet/sec YDOT = 7124
772330 meter/sec
ZDOT = -849
118360 ZDOT = -244
582857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8053733
40 X = -2454777
94
Y = 11107869
94 feet Y = 3385678
76 meter
Z = -17287740
87 Z = -5269303
42
XDOT = -19030
380534 XDOT = -5800
459987
YDOT = -14990
252416 feet/sec YDOT = -4569
028936 meter/sec
ZDOT = -792
683020 ZDOT = -241
609784
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 09284
54317438
00020000 00000-0 20000-3 0 9096
2 25544 51
6389 69
3868 0008277 188
3402 171
7625 15
74725271 24280
Satellite: ISS
Catalog Number: 25544
Epoch time: 09284
54317438 = yrday
fracday
Element set: 909
Inclination: 51
6389 deg
RA of node: 69
3868 deg
Eccentricity:
0008277
Arg of perigee: 188
3402 deg
Mean anomaly: 171
7625 deg
Mean motion: 15
74725271 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2428
Checksum: 328
Coasting Arc #11 (Orbit 2443)
---------------------------------------
Vector Time (GMT): 2009/285/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2956212
56 A = 6730099
65 meter
Y = -6033549
77 meter E =
0017976
Z = -32581
34 I = 51
95909
XDOT = 4276
419041 Wp = 157
75966
YDOT = -2068
419467 meter/sec RA = 63
67949 deg
ZDOT = -6071
030772 TA = 22
59312
MA = 22
51408
Ha = 190
291 n
mi
Hp = 182
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9698860
11 X = -2888366
37
Y = -19795110
78 feet Y = -6066228
53 meter
Z = -106894
17 Z = -46777
75
XDOT = 14030
246199 XDOT = 4328
722829
YDOT = -6786
153108 feet/sec YDOT = -2020
305763 meter/sec
ZDOT = -19918
079961 ZDOT = -6050
128663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18324072
81 X = 5585177
39
Y = 12252651
18 feet Y = 3734608
08 meter
Z = -163154
58 Z = -49729
51
XDOT = -7934
999746 XDOT = -2418
587923
YDOT = 11634
184637 feet/sec YDOT = 3546
099477 meter/sec
ZDOT = -19835
734946 ZDOT = -6045
932012
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 09285
55854327
00020000 00000-0 20000-3 0 9103
2 25544 51
6387 64
1656 0008239 192
9707 167
1246 15
74733150 24444
Satellite: ISS
Catalog Number: 25544
Epoch time: 09285
55854327 = yrday
fracday
Element set: 910
Inclination: 51
6387 deg
RA of node: 64
1656 deg
Eccentricity:
0008239
Arg of perigee: 192
9707 deg
Mean anomaly: 167
1246 deg
Mean motion: 15
74733150 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2444
Checksum: 309
Coasting Arc #12 (Orbit 2459)
---------------------------------------
Vector Time (GMT): 2009/286/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3716534
49 A = 6717979
57 meter
Y = 1855560
80 meter E =
0007057
Z = 5279310
71 I = 51
90514
XDOT = -3795
150372 Wp = 179
12040
YDOT = -6695
536780 meter/sec RA = 58
55590 deg
ZDOT = -325
281202 TA = 273
91501
MA = 273
99568
Ha = 190
149 n
mi
Hp = 182
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12193354
62 X = -3762653
61
Y = 6087797
89 feet Y = 1813742
75 meter
Z = 17320573
20 Z = 5261143
52
XDOT = -12451
280747 XDOT = -3718
417482
YDOT = -21966
984186 feet/sec YDOT = -6737
547370 meter/sec
ZDOT = -1067
195545 ZDOT = -343
531425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7379400
49 X = 2249241
27
Y = -11565369
07 feet Y = -3525124
49 meter
Z = 17249003
54 Z = 5257496
28
XDOT = 21162
701074 XDOT = 6450
391287
YDOT = 11837
529861 feet/sec YDOT = 3608
079102 meter/sec
ZDOT = -1139
472308 ZDOT = -347
311159
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 09286
57389901
00020000 00000-0 20000-3 0 9118
2 25544 51
6398 58
9455 0008106 197
1592 162
9298 15
74756716 24607
Satellite: ISS
Catalog Number: 25544
Epoch time: 09286
57389901 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 58
9455 deg
Eccentricity:
0008106
Arg of perigee: 197
1592 deg
Mean anomaly: 162
9298 deg
Mean motion: 15
74756716 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2460
Checksum: 337
Coasting Arc #13 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2009/287/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639837
03 A = 6729847
25 meter
Y = 5632494
87 meter E =
0007506
Z = 550467
34 I = 51
92924
XDOT = -4271
409736 Wp = 83
76351
YDOT = 2164
566987 meter/sec RA = 53
44230 deg
ZDOT = 6026
387598 TA = 282
20121
MA = 282
28528
Ha = 189
905 n
mi
Hp = 182
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11941722
53 X = 3573908
87
Y = 18479313
86 feet Y = 5672829
09 meter
Z = 1805995
22 Z = 567989
28
XDOT = -14013
811469 XDOT = -4324
572260
YDOT = 7101
597727 feet/sec YDOT = 2116
504786 meter/sec
ZDOT = 19771
612853 ZDOT = 6005
507565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19927008
75 X = -6073752
27
Y = -9313902
74 feet Y = -2838877
56 meter
Z = 1875349
14 Z = 571606
42
XDOT = 7515
656015 XDOT = 2290
771953
YDOT = -12071
327220 feet/sec YDOT = -3679
340537 meter/sec
ZDOT = 19689
357231 ZDOT = 6001
316084
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 09287
58924113
00020000 00000-0 20000-3 0 9121
2 25544 51
6404 53
7251 0008056 200
7014 159
3825 15
74770233 24769
Satellite: ISS
Catalog Number: 25544
Epoch time: 09287
58924113 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 53
7251 deg
Eccentricity:
0008056
Arg of perigee: 200
7014 deg
Mean anomaly: 159
3825 deg
Mean motion: 15
74770233 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2476
Checksum: 282
Coasting Arc #14 (Orbit 2490)
---------------------------------------
Vector Time (GMT): 2009/288/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3771020
62 A = 6718108
38 meter
Y = -1931554
74 meter E =
0014414
Z = -5224370
10 I = 51
87147
XDOT = 4493
466814 Wp = 129
24081
YDOT = 6171
050052 meter/sec RA = 48
30619 deg
ZDOT = 954
709408 TA = 149
87761
MA = 149
79464
Ha = 189
705 n
mi
Hp = 183
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12372114
88 X = 3817718
78
Y = -6337121
86 feet Y = -1889124
32 meter
Z = -17140321
84 Z = -5205936
59
XDOT = 14742
345191 XDOT = 4419
489214
YDOT = 20246
227205 feet/sec YDOT = 6220
885100 meter/sec
ZDOT = 3132
248713 ZDOT = 976
358779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6990002
14 X = -2130552
65
Y = 12118261
26 feet Y = 3693646
03 meter
Z = -17067705
97 Z = -5202236
78
XDOT = -22505
141461 XDOT = -6859
567117
YDOT = -8415
846427 feet/sec YDOT = -2565
149991 meter/sec
ZDOT = 3217
897775 ZDOT = 980
815242
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 09288
54111200
00020000 00000-0 20000-3 0 9134
2 25544 51
6408 48
8318 0007974 204
5691 155
5094 15
74812708 24910
Satellite: ISS
Catalog Number: 25544
Epoch time: 09288
54111200 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 48
8318 deg
Eccentricity:
0007974
Arg of perigee: 204
5691 deg
Mean anomaly: 155
5094 deg
Mean motion: 15
74812708 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2491
Checksum: 296
Coasting Arc #15 (Orbit 2506)
---------------------------------------
Vector Time (GMT): 2009/289/12:38:42
240
Vector Time (MET): N/A
Weight (LBS) : 855902
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4188997
42 A = 6729312
70 meter
Y = -5134792
88 meter E =
0014609
Z = -1116098
92 I = 51
88884
XDOT = 4366
253664 Wp = 172
06800
YDOT = -2278
588580 meter/sec RA = 43
20046 deg
ZDOT = -5927
909460 TA = 20
11790
MA = 20
06038
Ha = 189
511 n
mi
Hp = 183
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13743429
84 X = -4125846
01
Y = -16846433
33 feet Y = -5181283
71 meter
Z = -3661741
87 Z = -1136295
68
XDOT = 14324
979214 XDOT = 4420
206062
YDOT = -7475
684319 feet/sec YDOT = -2229
461396 meter/sec
ZDOT = -19448
521852 ZDOT = -5906
566499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20804234
62 X = 6341130
71
Y = 6267114
32 feet Y = 1910216
44 meter
Z = -3741608
38 Z = -1140442
23
XDOT = -7314
386668 XDOT = -2229
425056
YDOT = 12764
371497 feet/sec YDOT = 3890
580432 meter/sec
ZDOT = -19364
447344 ZDOT = -5902
283551
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 09289
55642819
00020000 00000-0 20000-3 0 9142
2 25544 51
6412 43
6113 0007992 208
7534 151
3190 15
74809591 25078
Satellite: ISS
Catalog Number: 25544
Epoch time: 09289
55642819 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 43
6113 deg
Eccentricity:
0007992
Arg of perigee: 208
7534 deg
Mean anomaly: 151
3190 deg
Mean motion: 15
74809591 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2507
Checksum: 302
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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