Date:
January 15th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 2182)
---------------------------------------
Vector Time (GMT): 2009/014/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -413441
30 A = 6730907
19 meter
Y = -4270447
46 meter E =
0006228
Z = -5191691
36 I = 51
68995
XDOT = 7580
808229 Wp = 73
88926
YDOT = 637
418102 meter/sec RA = 11
53006 deg
ZDOT = -1127
431408 TA = 185
33970
MA = 185
34635
Ha = 193
302 n
mi
Hp = 192
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1356434
72 X = -340437
95
Y = -14010654
41 feet Y = -4274662
38 meter
Z = -17033108
14 Z = -5193522
69
XDOT = 24871
418074 XDOT = 7578
593839
YDOT = 2091
266738 feet/sec YDOT = 722
178767 meter/sec
ZDOT = -3698
921942 ZDOT = -1090
609954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10822159
06 X = -3298594
08
Y = -8987077
09 feet Y = -2739261
10 meter
Z = -17040494
24 Z = -5193942
64
XDOT = 18379
532226 XDOT = 5602
081422
YDOT = -15387
188048 feet/sec YDOT = -4690
014917 meter/sec
ZDOT = -3555
533187 ZDOT = -1083
726515
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 09014
82754867
00010596 00000-0 82463-4 0 9001
2 25544 51
6430 11
9306 0008276 267
2702 92
7512 15
70351054 21831
Satellite: ISS
Catalog Number: 25544
Epoch time: 09014
82754867 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 11
9306 deg
Eccentricity:
0008276
Arg of perigee: 267
2702 deg
Mean anomaly: 92
7512 deg
Mean motion: 15
70351054 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2183
Checksum: 292
Coasting Arc #2 (Orbit 2198)
---------------------------------------
Vector Time (GMT): 2009/015/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6314969
55 A = 6740742
29 meter
Y = 984047
45 meter E =
0006948
Z = 2128887
05 I = 51
69379
XDOT = -2595
001391 Wp = 133
59757
YDOT = -4683
637288 meter/sec RA = 6
39843 deg
ZDOT = -5526
160238 TA = 22
65343
MA = 22
62278
Ha = 192
828 n
mi
Hp = 192
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20718404
04 X = -6335845
57
Y = 3228502
13 feet Y = 913312
99 meter
Z = 6984537
56 Z = 2098158
75
XDOT = -8513
784090 XDOT = -2515
590671
YDOT = -15366
264068 feet/sec YDOT = -4712
211875 meter/sec
ZDOT = -18130
446974 ZDOT = -5538
573847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12053515
71 X = -3673911
59
Y = 17205934
60 feet Y = 5244368
87 meter
Z = 6864971
25 Z = 2092443
24
XDOT = -15652
286829 XDOT = -4770
817026
YDOT = -3703
209465 feet/sec YDOT = -1128
738245 meter/sec
ZDOT = -18179
055109 ZDOT = -5540
975997
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 09015
84575404
00010596 00000-0 82463-4 0 9013
2 25544 51
6432 6
7305 0008177 270
5165 89
5059 15
70331164 21991
Satellite: ISS
Catalog Number: 25544
Epoch time: 09015
84575404 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 6
7305 deg
Eccentricity:
0008177
Arg of perigee: 270
5165 deg
Mean anomaly: 89
5059 deg
Mean motion: 15
70331164 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2199
Checksum: 304
Coasting Arc #3 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2009/016/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3943292
91 A = 6734734
64 meter
Y = 3444795
19 meter E =
0002537
Z = 4235887
66 I = 51
64456
XDOT = -6236
080251 Wp = 148
99134
YDOT = 2705
662264 meter/sec RA = 1
33537 deg
ZDOT = 3601
879352 TA = 264
33461
MA = 264
36354
Ha = 193
641 n
mi
Hp = 193
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12937312
69 X = 3883902
65
Y = 11301821
48 feet Y = 3488559
13 meter
Z = 13897269
22 Z = 4254899
83
XDOT = -20459
580876 XDOT = -6283
368995
YDOT = 8876
844698 feet/sec YDOT = 2635
662236 meter/sec
ZDOT = 11817
189476 ZDOT = 3571
470103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17030230
21 X = 5190814
17
Y = -1734385
19 feet Y = -528640
61 meter
Z = 13971488
38 Z = 4258509
66
XDOT = -7585
263543 XDOT = -2311
988328
YDOT = 19842
236586 feet/sec YDOT = 6047
913712 meter/sec
ZDOT = 11698
971760 ZDOT = 3565
846592
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 09016
86394331
00010596 00000-0 82463-4 0 9025
2 25544 51
6431 1
5291 0008236 275
5542 84
4680 15
70349758 22158
Satellite: ISS
Catalog Number: 25544
Epoch time: 09016
86394331 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 1
5291 deg
Eccentricity:
0008236
Arg of perigee: 275
5542 deg
Mean anomaly: 84
4680 deg
Mean motion: 15
70349758 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2215
Checksum: 303
Coasting Arc #4 (Orbit 2229)
---------------------------------------
Vector Time (GMT): 2009/017/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4153324
73 A = 6735543
66 meter
Y = -3464098
77 meter E =
0001860
Z = -4013949
92 I = 51
61749
XDOT = 6043
778823 Wp = 240
12188
YDOT = 2705
329856 meter/sec RA = 356
17638 deg
ZDOT = 3916
632533 TA = 70
38899
MA = 70
36891
Ha = 194
057 n
mi
Hp = 193
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13626393
46 X = 4211251
02
Y = -11365153
45 feet Y = -3417329
78 meter
Z = -13169127
03 Z = -3993632
75
XDOT = 19828
670678 XDOT = 5994
052085
YDOT = 8875
754122 feet/sec YDOT = 2772
636645 meter/sec
ZDOT = 12849
844269 ZDOT = 3945
872290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 685842
60 X = 209044
83
Y = -17788939
95 feet Y = -5422068
90 meter
Z = -13090242
70 Z = -3989905
97
XDOT = 18499
057133 XDOT = 5638
512614
YDOT = -8831
890833 feet/sec YDOT = -2691
960326 meter/sec
ZDOT = 12963
830517 ZDOT = 3951
375542
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 09017
81848120
00010596 00000-0 82463-4 0 9032
2 25544 51
6425 356
6531 0008429 278
6754 81
3453 15
70401143 22303
Satellite: ISS
Catalog Number: 25544
Epoch time: 09017
81848120 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 356
6531 deg
Eccentricity:
0008429
Arg of perigee: 278
6754 deg
Mean anomaly: 81
3453 deg
Mean motion: 15
70401143 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2230
Checksum: 295
Coasting Arc #5 (Orbit 2245)
---------------------------------------
Vector Time (GMT): 2009/018/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6191352
22 A = 6739753
81 meter
Y = -1004928
70 meter E =
0004590
Z = -2459574
04 I = 51
60210
XDOT = 2889
417248 Wp = 247
53676
YDOT = -4730
738204 meter/sec RA = 351
11353 deg
ZDOT = -5334
309676 TA = 320
22600
MA = 320
25965
Ha = 194
165 n
mi
Hp = 192
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20312835
35 X = -6167706
72
Y = -3297010
17 feet Y = -1074031
61 meter
Z = -8069468
65 Z = -2489594
01
XDOT = 9479
715381 XDOT = 2968
015281
YDOT = -15520
794631 feet/sec YDOT = -4697
987220 meter/sec
ZDOT = -17501
015998 ZDOT = -5320
082432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15760302
97 X = -4803740
35
Y = 13160310
06 feet Y = 4011262
51 meter
Z = -8186389
30 Z = -2495211
46
XDOT = -4500
259618 XDOT = -1371
679132
YDOT = -16254
044592 feet/sec YDOT = -4954
232792 meter/sec
ZDOT = -17445
912500 ZDOT = -5317
514130
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 09018
83664205
00010596 00000-0 82463-4 0 9046
2 25544 51
6420 351
4528 0008462 281
9979 78
0233 15
70396936 22469
Satellite: ISS
Catalog Number: 25544
Epoch time: 09018
83664205 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 351
4528 deg
Eccentricity:
0008462
Arg of perigee: 281
9979 deg
Mean anomaly: 78
0233 deg
Mean motion: 15
70396936 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2246
Checksum: 325
Coasting Arc #6 (Orbit 2261)
---------------------------------------
Vector Time (GMT): 2009/019/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -728570
49 A = 6731110
39 meter
Y = 4349049
15 meter E =
0006600
Z = 5090265
88 I = 51
54442
XDOT = -7505
609704 Wp = 321
78095
YDOT = 588
472951 meter/sec RA = 345
96531 deg
ZDOT = -1573
053386 TA = 143
38157
MA = 143
33644
Ha = 194
320 n
mi
Hp = 192
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2390323
13 X = -801875
48
Y = 14268533
96 feet Y = 4340491
54 meter
Z = 16700347
37 Z = 5086548
84
XDOT = -24624
703753 XDOT = -7503
990735
YDOT = 1930
685535 feet/sec YDOT = 504
550060 meter/sec
ZDOT = -5160
936307 ZDOT = -1609
511318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9349346
19 X = 2849680
72
Y = 11062051
34 feet Y = 3371713
25 meter
Z = 16686133
59 Z = 5085933
52
XDOT = -13492
240304 XDOT = -4112
434845
YDOT = 19421
976128 feet/sec YDOT = 5919
818324 meter/sec
ZDOT = -5302
825206 ZDOT = -1616
301123
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 09019
85478695
00010596 00000-0 82463-4 0 9056
2 25544 51
6420 346
2511 0008433 286
1492 73
8741 15
70447932 22626
Satellite: ISS
Catalog Number: 25544
Epoch time: 09019
85478695 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 346
2511 deg
Eccentricity:
0008433
Arg of perigee: 286
1492 deg
Mean anomaly: 73
8741 deg
Mean motion: 15
70447932 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2262
Checksum: 322
Coasting Arc #7 (Orbit 2277)
---------------------------------------
Vector Time (GMT): 2009/020/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6417347
37 A = 6742229
18 meter
Y = -2028762
76 meter E =
0011484
Z = 235427
00 I = 51
55264
XDOT = 1242
110576 Wp = 7
23451
YDOT = 4630
313745 meter/sec RA = 340
86491 deg
ZDOT = 6022
695167 TA = 355
32381
MA = 355
33453
Ha = 194
445 n
mi
Hp = 192
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21054289
26 X = 6438412
73
Y = -6656045
82 feet Y = -1956882
51 meter
Z = 772398
31 Z = 266653
09
XDOT = 4075
165932 XDOT = 1160
984502
YDOT = 15191
318061 feet/sec YDOT = 4643
749538 meter/sec
ZDOT = 19759
498579 ZDOT = 6028
532686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8047382
22 X = 2452842
10
Y = -20557804
68 feet Y = -6266018
87 meter
Z = 893838
65 Z = 272442
02
XDOT = 12808
230174 XDOT = 3903
948557
YDOT = 5876
467237 feet/sec YDOT = 1791
147214 meter/sec
ZDOT = 19782
494923 ZDOT = 6029
704452
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 09020
87291739
00010596 00000-0 82463-4 0 9063
2 25544 51
6408 341
0488 0008426 290
0232 70
0022 15
70464374 22783
Satellite: ISS
Catalog Number: 25544
Epoch time: 09020
87291739 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 341
0488 deg
Eccentricity:
0008426
Arg of perigee: 290
0232 deg
Mean anomaly: 70
0022 deg
Mean motion: 15
70464374 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2278
Checksum: 296
Coasting Arc #8 (Orbit 2292)
---------------------------------------
Vector Time (GMT): 2009/021/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2757612
03 A = 6730456
99 meter
Y = -3288938
54 meter E =
0008528
Z = -5190886
94 I = 51
48479
XDOT = 6567
642787 Wp = 51
37220
YDOT = -3863
333239 meter/sec RA = 335
75317 deg
ZDOT = -1037
111904 TA = 208
67893
MA = 208
72585
Ha = 194
547 n
mi
Hp = 191
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9047283
56 X = -2695413
61
Y = -10790480
79 feet Y = -3319427
43 meter
Z = -17030468
96 Z = -5204132
50
XDOT = 21547
384473 XDOT = 6615
393124
YDOT = -12674
977819 feet/sec YDOT = -3789
622950 meter/sec
ZDOT = -3402
598109 ZDOT = -1005
091197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14012248
26 X = -4270933
27
Y = 423201
12 feet Y = 128991
70 meter
Z = -17082227
26 Z = -5206662
87
XDOT = 3294
480749 XDOT = 1004
157732
YDOT = -23779
922491 feet/sec YDOT = -7248
120375 meter/sec
ZDOT = -3278
168579 ZDOT = -999
185783
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 09021
82740075
00010596 00000-0 82463-4 0 9072
2 25544 51
6397 336
1720 0008365 293
5531 66
4751 15
70489386 22931
Satellite: ISS
Catalog Number: 25544
Epoch time: 09021
82740075 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 336
1720 deg
Eccentricity:
0008365
Arg of perigee: 293
5531 deg
Mean anomaly: 66
4751 deg
Mean motion: 15
70489386 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2293
Checksum: 323
Coasting Arc #9 (Orbit 2308)
---------------------------------------
Vector Time (GMT): 2009/022/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4653316
60 A = 6740313
60 meter
Y = 4445185
47 meter E =
0005624
Z = 1997359
42 I = 51
49309
XDOT = -4716
755425 Wp = 102
78197
YDOT = -2429
457876 meter/sec RA = 330
60724 deg
ZDOT = -5570
007971 TA = 54
95846
MA = 54
90571
Ha = 194
766 n
mi
Hp = 191
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15266786
76 X = -4712380
19
Y = 14583941
83 feet Y = 4392818
92 meter
Z = 6553016
47 Z = 1974611
05
XDOT = -15474
919372 XDOT = -4662
180679
YDOT = -7970
662324 feet/sec YDOT = -2481
897618 meter/sec
ZDOT = -18274
304366 ZDOT = -5592
789254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2453755
85 X = 747904
78
Y = 20997492
20 feet Y = 6400035
62 meter
Z = 6464716
97 Z = 1970445
73
XDOT = -14078
136383 XDOT = -4291
015969
YDOT = 7311
044874 feet/sec YDOT = 2228
406477 meter/sec
ZDOT = -18363
139137 ZDOT = -5597
084809
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 09022
84549994
00010596 00000-0 82463-4 0 9083
2 25544 51
6406 330
9708 0008569 297
9676 62
0617 15
70556089 23090
Satellite: ISS
Catalog Number: 25544
Epoch time: 09022
84549994 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 330
9708 deg
Eccentricity:
0008569
Arg of perigee: 297
9676 deg
Mean anomaly: 62
0617 deg
Mean motion: 15
70556089 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2309
Checksum: 353
Coasting Arc #10 (Orbit 2324)
---------------------------------------
Vector Time (GMT): 2009/023/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5105481
99 A = 6733839
23 meter
Y = 685422
33 meter E =
0002027
Z = 4334796
68 I = 51
44506
XDOT = -3682
564626 Wp = 57
00164
YDOT = 5830
253590 meter/sec RA = 325
52709 deg
ZDOT = 3415
337039 TA = 358
41930
MA = 358
41994
Ha = 194
815 n
mi
Hp = 191
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16750268
98 X = 5076380
85
Y = 2248760
92 feet Y = 742351
63 meter
Z = 14221773
89 Z = 4359527
95
XDOT = -12081
904942 XDOT = -3764
076506
YDOT = 19128
128576 feet/sec YDOT = 5788
616905 meter/sec
ZDOT = 11205
174012 ZDOT = 3397
250155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11609922
51 X = 3538704
38
Y = -12169180
62 feet Y = -3709166
25 meter
Z = 14318101
54 Z = 4364157
35
XDOT = 7459
841298 XDOT = 2273
759628
YDOT = 20218
689123 feet/sec YDOT = 6162
656445 meter/sec
ZDOT = 11135
106264 ZDOT = 3393
980389
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 09023
86358692
00010596 00000-0 82463-4 0 9090
2 25544 51
6395 325
7682 0008408 300
8992 59
1342 15
70522394 23259
Satellite: ISS
Catalog Number: 25544
Epoch time: 09023
86358692 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 325
7682 deg
Eccentricity:
0008408
Arg of perigee: 300
8992 deg
Mean anomaly: 59
1342 deg
Mean motion: 15
70522394 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2325
Checksum: 329
Coasting Arc #11 (Orbit 2339)
---------------------------------------
Vector Time (GMT): 2009/024/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1591189
93 A = 6735635
52 meter
Y = -5297085
26 meter E =
0002990
Z = -3841246
09 I = 51
42735
XDOT = 6415
932178 Wp = 346
67582
YDOT = -1054
898071 meter/sec RA = 320
35289 deg
ZDOT = 4114
656410 TA = 326
46973
MA = 326
48865
Ha = 194
973 n
mi
Hp = 191
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5220439
40 X = 1668964
15
Y = -17378888
65 feet Y = -5278856
44 meter
Z = -12602513
43 Z = -3833327
87
XDOT = 21049
646253 XDOT = 6407
263638
YDOT = -3460
951676 feet/sec YDOT = -983
200242 meter/sec
ZDOT = 13499
528905 ZDOT = 4145
803056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11204375
86 X = -3415093
76
Y = -14300652
75 feet Y = -4358838
96 meter
Z = -12572008
41 Z = -3831948
16
XDOT = 8145
264336 XDOT = 2482
676570
YDOT = -18349
544909 feet/sec YDOT = -5592
941288 meter/sec
ZDOT = 13620
732588 ZDOT = 4151
599293
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 09024
81802774
00010596 00000-0 82463-4 0 9103
2 25544 51
6392 320
8910 0008190 303
9532 56
0850 15
70554691 23400
Satellite: ISS
Catalog Number: 25544
Epoch time: 09024
81802774 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 320
8910 deg
Eccentricity:
0008190
Arg of perigee: 303
9532 deg
Mean anomaly: 56
0850 deg
Mean motion: 15
70554691 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2340
Checksum: 293
Coasting Arc #12 (Orbit 2355)
---------------------------------------
Vector Time (GMT): 2009/025/19:26:07
092
Vector Time (MET): N/A
Weight (LBS) : 639525
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5627782
88 A = 6738603
78 meter
Y = 2523211
15 meter E =
0003506
Z = -2716548
35 I = 51
41627
XDOT = -71
805570 Wp = 318
20860
YDOT = -5711
124200 meter/sec RA = 315
27744 deg
ZDOT = -5149
513612 TA = 252
83301
MA = 252
87141
Ha = 195
131 n
mi
Hp = 190
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18463854
59 X = -5642383
45
Y = 8278251
81 feet Y = 2460196
59 meter
Z = -8912560
20 Z = -2743922
63
XDOT = -235
582578 XDOT = 17
077202
YDOT = -18737
284120 feet/sec YDOT = -5711
429817 meter/sec
ZDOT = -16894
729698 ZDOT = -5149
646970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3432098
77 X = -1046103
70
Y = 19893609
34 feet Y = 6063572
13 meter
Z = -9018986
32 Z = -2748987
03
XDOT = -14161
136194 XDOT = -4316
314312
YDOT = -10112
320964 feet/sec YDOT = -3082
235430 meter/sec
ZDOT = -16895
606774 ZDOT = -5149
780945
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 09025
83608289
00010596 00000-0 82463-4 0 9112
2 25544 51
6393 315
6900 0008200 308
9007 51
1423 15
70598091 23567
Satellite: ISS
Catalog Number: 25544
Epoch time: 09025
83608289 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 315
6900 deg
Eccentricity:
0008200
Arg of perigee: 308
9007 deg
Mean anomaly: 51
1423 deg
Mean motion: 15
70598091 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2356
Checksum: 299
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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