Date:
December 7th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 25 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 3278)
---------------------------------------
Vector Time (GMT): 2009/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1331445
00 A = 6716848
99 meter
Y = 4816509
09 meter E =
0014636
Z = -4499828
12 I = 51
79354
XDOT = -6931
811486 Wp = 83
50453
YDOT = 1039
671221 meter/sec RA = 150
58763 deg
ZDOT = 3174
278464 TA = 218
11144
MA = 218
21504
Ha = 188
956 n
mi
Hp = 178
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4368257
86 X = -1363345
55
Y = 15802195
17 feet Y = 4801442
42 meter
Z = -14763215
62 Z = -4506373
07
XDOT = -22742
163668 XDOT = -6958
342284
YDOT = 3410
994821 feet/sec YDOT = 962
006781 meter/sec
ZDOT = 10414
299424 ZDOT = 3140
539144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13808221
49 X = -4208745
91
Y = -8795731
49 feet Y = -2680938
96 meter
Z = -14788905
00 Z = -4507658
25
XDOT = 2896
769659 XDOT = 882
935392
YDOT = -21776
450581 feet/sec YDOT = -6637
462137 meter/sec
ZDOT = 10280
969537 ZDOT = 3133
639515
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 09338
51035670
00016717 00000-0 10270-3 0 9007
2 25544 51
6401 151
5565 0007375 44
8617 315
3143 15
76280128 32790
Satellite: ISS
Catalog Number: 25544
Epoch time: 09338
51035670 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 151
5565 deg
Eccentricity:
0007375
Arg of perigee: 44
8617 deg
Mean anomaly: 315
3143 deg
Mean motion: 15
76280128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 301
Coasting Arc #2 (Orbit 3294)
---------------------------------------
Vector Time (GMT): 2009/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5752250
64 A = 6720593
83 meter
Y = -692295
17 meter E =
0011642
Z = -3419721
24 I = 51
83260
XDOT = -2041
236373 Wp = 64
72189
YDOT = 5805
937206 meter/sec RA = 145
49627 deg
ZDOT = -4616
190420 TA = 155
55822
MA = 155
50298
Ha = 189
012 n
mi
Hp = 178
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18872213
40 X = 5776176
94
Y = -2271309
61 feet Y = -627835
87 meter
Z = -11219557
86 Z = -3391718
67
XDOT = -6696
969727 XDOT = -2083
582965
YDOT = 19048
350413 feet/sec YDOT = 5782
874752 meter/sec
ZDOT = -15144
981692 ZDOT = -4626
208857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3151259
48 X = -960503
89
Y = 18811172
59 feet Y = 5733645
41 meter
Z = -11108875
46 Z = -3385985
24
XDOT = -15045
721405 XDOT = -4585
935884
YDOT = -11473
266809 feet/sec YDOT = -3497
051723 meter/sec
ZDOT = -15184
370887 ZDOT = -4628
196246
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 09339
52471244
00016717 00000-0 10270-3 0 9011
2 25544 51
6407 146
3299 0007534 48
2715 311
9093 15
76318473 32955
Satellite: ISS
Catalog Number: 25544
Epoch time: 09339
52471244 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 146
3299 deg
Eccentricity:
0007534
Arg of perigee: 48
2715 deg
Mean anomaly: 311
9093 deg
Mean motion: 15
76318473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3295
Checksum: 320
Coasting Arc #3 (Orbit 3310)
---------------------------------------
Vector Time (GMT): 2009/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2152663
32 A = 6720334
53 meter
Y = -5329623
42 meter E =
0018802
Z = 3471132
19 I = 51
85563
XDOT = 6194
099526 Wp = 75
13745
YDOT = -485
520221 meter/sec RA = 140
30567 deg
ZDOT = -4561
691088 TA = 63
76781
MA = 63
57467
Ha = 188
995 n
mi
Hp = 177
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7062543
70 X = 2195237
95
Y = -17485641
13 feet Y = -5305313
40 meter
Z = 11388228
96 Z = 3481692
67
XDOT = 20321
848840 XDOT = 6221
228247
YDOT = -1592
914112 feet/sec YDOT = -416
101960 meter/sec
ZDOT = -14966
178111 ZDOT = -4531
534251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15006880
35 X = 4574097
13
Y = 11378598
07 feet Y = 3468196
69 meter
Z = 11429784
60 Z = 3483798
35
XDOT = -3041
433949 XDOT = -927
029068
YDOT = 19007
504417 feet/sec YDOT = 5793
487346 meter/sec
ZDOT = -14846
956152 ZDOT = -4525
352235
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 09340
53905572
00016717 00000-0 10270-3 0 9021
2 25544 51
6404 141
1024 0007364 52
3368 307
8464 15
76304081 33117
Satellite: ISS
Catalog Number: 25544
Epoch time: 09340
53905572 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 141
1024 deg
Eccentricity:
0007364
Arg of perigee: 52
3368 deg
Mean anomaly: 307
8464 deg
Mean motion: 15
76304081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3311
Checksum: 282
Coasting Arc #4 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2009/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5029198
51 A = 6716956
21 meter
Y = 81865
52 meter E =
0014722
Z = 4438810
64 I = 51
86761
XDOT = 2795
584162 Wp = 87
35282
YDOT = -6398
514512 meter/sec RA = 135
21784 deg
ZDOT = 3276
830069 TA = 329
91473
MA = 329
99922
Ha = 189
091 n
mi
Hp = 177
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16499995
11 X = -5051303
16
Y = 268587
66 feet Y = 25502
08 meter
Z = 14563027
02 Z = 4414325
04
XDOT = 9171
864047 XDOT = 2851
007408
YDOT = -20992
501679 feet/sec YDOT = -6366
943031 meter/sec
ZDOT = 10750
754819 ZDOT = 3290
545131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3858028
16 X = 1175926
98
Y = -16132212
46 feet Y = -4917098
36 meter
Z = 14466204
54 Z = 4409299
14
XDOT = 16896
309759 XDOT = 5149
995215
YDOT = 13755
129000 feet/sec YDOT = 4192
563319 meter/sec
ZDOT = 10804
749665 ZDOT = 3293
287698
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 09341
55338502
00016717 00000-0 10270-3 0 9038
2 25544 51
6410 135
8754 0007329 56
2643 303
9219 15
76362847 33270
Satellite: ISS
Catalog Number: 25544
Epoch time: 09341
55338502 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 135
8754 deg
Eccentricity:
0007329
Arg of perigee: 56
2643 deg
Mean anomaly: 303
9219 deg
Mean motion: 15
76362847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 312
Coasting Arc #5 (Orbit 3341)
---------------------------------------
Vector Time (GMT): 2009/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2645273
21 A = 6723392
06 meter
Y = 5786832
55 meter E =
0013501
Z = -2165799
24 I = 51
91119
XDOT = -5343
386595 Wp = 52
44411
YDOT = -383
165783 meter/sec RA = 130
03936 deg
ZDOT = 5533
925479 TA = 283
38797
MA = 283
53844
Ha = 189
043 n
mi
Hp = 177
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8678717
88 X = -2699264
86
Y = 18985671
09 feet Y = 5756949
81 meter
Z = -7105640
55 Z = -2178780
80
XDOT = -17530
795914 XDOT = -5365
587790
YDOT = -1257
105587 feet/sec YDOT = -443
043200 meter/sec
ZDOT = 18155
923489 ZDOT = 5507
913209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16468578
60 X = -5019622
76
Y = -12799711
77 feet Y = -3901352
15 meter
Z = -7156764
36 Z = -2181381
78
XDOT = 4374
343009 XDOT = 1333
299749
YDOT = -15665
112864 feet/sec YDOT = -4774
726401 meter/sec
ZDOT = 18053
038886 ZDOT = 5502
566252
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 09342
50430868
00016717 00000-0 10270-3 0 9043
2 25544 51
6422 130
9755 0007475 60
4269 299
7639 15
76357826 33429
Satellite: ISS
Catalog Number: 25544
Epoch time: 09342
50430868 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 130
9755 deg
Eccentricity:
0007475
Arg of perigee: 60
4269 deg
Mean anomaly: 299
7639 deg
Mean motion: 15
76357826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3342
Checksum: 336
Coasting Arc #6 (Orbit 3357)
---------------------------------------
Vector Time (GMT): 2009/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4297497
73 A = 6714158
35 meter
Y = 842417
51 meter E =
0021118
Z = -5108060
67 I = 51
89880
XDOT = -3224
957896 Wp = 73
01844
YDOT = 6795
797752 meter/sec RA = 124
93830 deg
ZDOT = -1591
808735 TA = 181
72448
MA = 181
73178
Ha = 189
061 n
mi
Hp = 177
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14099401
99 X = 4312572
54
Y = 2763836
96 feet Y = 890559
27 meter
Z = -16758729
24 Z = -5087146
56
XDOT = -10580
570526 XDOT = -3292
977216
YDOT = 22295
924383 feet/sec YDOT = 6759
354154 meter/sec
ZDOT = -5222
469604 ZDOT = -1607
640522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5749358
83 X = -1752404
57
Y = 13271900
10 feet Y = 4045275
15 meter
Z = -16675985
07 Z = -5082840
25
XDOT = -18540
496618 XDOT = -5651
143369
YDOT = -14674
711567 feet/sec YDOT = -4472
852086 meter/sec
ZDOT = -5284
837705 ZDOT = -1610
818532
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 09343
51861327
00016717 00000-0 10270-3 0 9054
2 25544 51
6424 125
7493 0007555 63
7264 296
4676 15
76391726 33581
Satellite: ISS
Catalog Number: 25544
Epoch time: 09343
51861327 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 125
7493 deg
Eccentricity:
0007555
Arg of perigee: 63
7264 deg
Mean anomaly: 296
4676 deg
Mean motion: 15
76391726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3358
Checksum: 339
Coasting Arc #7 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2009/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2925800
50 A = 6725178
15 meter
Y = -6022270
08 meter E =
0018049
Z = 577776
58 I = 51
95181
XDOT = 4519
819684 Wp = 107
54901
YDOT = 1603
186719 meter/sec RA = 119
78446 deg
ZDOT = -6029
735110 TA = 66
18316
MA = 65
99406
Ha = 189
039 n
mi
Hp = 177
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9599083
00 X = 2990118
35
Y = -19758103
92 feet Y = -5989192
47 meter
Z = 1895592
45 Z = 592146
12
XDOT = 14828
804739 XDOT = 4530
848410
YDOT = 5259
798947 feet/sec YDOT = 1653
792099 meter/sec
ZDOT = -19782
595506 ZDOT = -6007
750620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17468071
63 X = 5324268
23
Y = 13310659
61 feet Y = 4057089
05 meter
Z = 1952216
73 Z = 595035
66
XDOT = -7143
991211 XDOT = -2177
488521
YDOT = 12333
073331 feet/sec YDOT = 3759
120751 meter/sec
ZDOT = -19695
587919 ZDOT = -6003
215198
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 09344
53290443
00016717 00000-0 10270-3 0 9063
2 25544 51
6417 120
5207 0007477 66
9634 293
2318 15
76408535 33741
Satellite: ISS
Catalog Number: 25544
Epoch time: 09344
53290443 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 120
5207 deg
Eccentricity:
0007477
Arg of perigee: 66
9634 deg
Mean anomaly: 293
2318 deg
Mean motion: 15
76408535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 318
Coasting Arc #8 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2009/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3635165
98 A = 6713217
35 meter
Y = -1985773
08 meter E =
0009970
Z = 5274959
79 I = 51
92659
XDOT = 3398
881636 Wp = 72
36282
YDOT = -6918
625679 meter/sec RA = 114
65574 deg
ZDOT = -258
886212 TA = 20
10054
MA = 20
06130
Ha = 189
187 n
mi
Hp = 177
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11926397
58 X = -3638315
77
Y = -6515003
53 feet Y = -2026441
71 meter
Z = 17306298
54 Z = 5257292
04
XDOT = 11151
186470 XDOT = 3477
251949
YDOT = -22698
903146 feet/sec YDOT = -6880
179164 meter/sec
ZDOT = -849
364212 ZDOT = -242
184396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8585494
87 X = 2616858
84
Y = -10648460
05 feet Y = -3245650
62 meter
Z = 17236350
41 Z = 5253639
61
XDOT = 19526
108643 XDOT = 5951
557914
YDOT = 14457
066390 feet/sec YDOT = 4406
513836 meter/sec
ZDOT = -783
530800 ZDOT = -238
820188
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 09345
54718339
00016717 00000-0 10270-3 0 9075
2 25544 51
6428 115
2938 0007538 70
3074 289
8901 15
76418986 33908
Satellite: ISS
Catalog Number: 25544
Epoch time: 09345
54718339 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 115
2938 deg
Eccentricity:
0007538
Arg of perigee: 70
3074 deg
Mean anomaly: 289
8901 deg
Mean motion: 15
76418986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 347
Coasting Arc #9 (Orbit 3405)
---------------------------------------
Vector Time (GMT): 2009/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2960180
72 A = 6724785
75 meter
Y = 5940122
12 meter E =
0021088
Z = 1027457
22 I = 51
97823
XDOT = -3883
690771 Wp = 62
52352
YDOT = -2979
828872 meter/sec RA = 109
53626 deg
ZDOT = 5955
474187 TA = 308
67465
MA = 308
86312
Ha = 189
070 n
mi
Hp = 177
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9711878
99 X = -3031375
48
Y = 19488589
62 feet Y = 5906621
45 meter
Z = 3370922
63 Z = 1012904
10
XDOT = -12741
767622 XDOT = -3879
012290
YDOT = -9776
341445 feet/sec YDOT = -3023
233072 meter/sec
ZDOT = 19538
957308 ZDOT = 5936
617923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17626276
10 X = -5372488
96
Y = -12799362
49 feet Y = -3901245
69 meter
Z = 3313540
26 Z = 1009967
07
XDOT = 10820
754032 XDOT = 3298
165829
YDOT = -9790
928868 feet/sec YDOT = -2984
275119 meter/sec
ZDOT = 19464
276161 ZDOT = 5932
711374
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 09346
56144814
00016717 00000-0 10270-3 0 9080
2 25544 51
6438 110
0669 0007575 74
4959 285
7041 15
76447140 34063
Satellite: ISS
Catalog Number: 25544
Epoch time: 09346
56144814 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 110
0669 deg
Eccentricity:
0007575
Arg of perigee: 74
4959 deg
Mean anomaly: 285
7041 deg
Mean motion: 15
76447140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3406
Checksum: 327
Coasting Arc #10 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2009/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3185917
47 A = 6714490
27 meter
Y = 3228915
85 meter E =
0019799
Z = -4967988
85 I = 51
95301
XDOT = -3387
327837 Wp = 95
21995
YDOT = 6574
732999 meter/sec RA = 104
37938 deg
ZDOT = 2106
335988 TA = 195
10383
MA = 195
16304
Ha = 189
022 n
mi
Hp = 177
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10452485
13 X = 3173708
38
Y = 10593555
94 feet Y = 3264475
03 meter
Z = -16299176
03 Z = -4952540
64
XDOT = -11113
280306 XDOT = -3470
828270
YDOT = 21570
646322 feet/sec YDOT = 6536
386755 meter/sec
ZDOT = 6910
551141 ZDOT = 2089
678080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12030437
27 X = -3666877
28
Y = 8873438
94 feet Y = 2704624
19 meter
Z = -16237970
08 Z = -4949333
28
XDOT = -19046
893412 XDOT = -5805
493112
YDOT = -13330
110387 feet/sec YDOT = -4063
017646 meter/sec
ZDOT = 6844
844127 ZDOT = 2086
308490
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 09347
51231018
00016717 00000-0 10270-3 0 9090
2 25544 51
6441 105
1673 0007563 77
5220 282
6790 15
76476893 34210
Satellite: ISS
Catalog Number: 25544
Epoch time: 09347
51231018 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 105
1673 deg
Eccentricity:
0007563
Arg of perigee: 77
5220 deg
Mean anomaly: 282
6790 deg
Mean motion: 15
76476893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 314
Coasting Arc #11 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2009/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2964253
76 A = 6722168
86 meter
Y = -5438218
59 meter E =
0011647
Z = -2619706
95 I = 51
98596
XDOT = 3455
913558 Wp = 99
38274
YDOT = 4414
182210 meter/sec RA = 99
28707 deg
ZDOT = -5274
508817 TA = 110
25055
MA = 110
12530
Ha = 189
037 n
mi
Hp = 177
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9725242
00 X = 3037570
81
Y = -17841924
50 feet Y = -5404660
23 meter
Z = -8594839
09 Z = -2605129
10
XDOT = 11338
299076 XDOT = 3431
919520
YDOT = 14482
225098 feet/sec YDOT = 4452
694883 meter/sec
ZDOT = -17304
818952 ZDOT = -5257
777387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16417867
72 X = 5004166
08
Y = 12014731
93 feet Y = 3662090
29 meter
Z = -8537312
03 Z = -2602172
71
XDOT = -14971
520367 XDOT = -4563
319408
YDOT = 8259
777727 feet/sec YDOT = 2517
580251 meter/sec
ZDOT = -17238
504973 ZDOT = -5254
296316
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 09348
52655040
00016717 00000-0 10270-3 0 9109
2 25544 51
6448 99
9394 0007558 81
1252 279
0768 15
76480650 34375
Satellite: ISS
Catalog Number: 25544
Epoch time: 09348
52655040 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 99
9394 deg
Eccentricity:
0007558
Arg of perigee: 81
1252 deg
Mean anomaly: 279
0768 deg
Mean motion: 15
76480650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 338
Coasting Arc #12 (Orbit 3452)
---------------------------------------
Vector Time (GMT): 2009/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2912390
84 A = 6717771
93 meter
Y = -4423090
42 meter E =
0018143
Z = 4120191
92 I = 51
97532
XDOT = 3394
356550 Wp = 79
40874
YDOT = -5789
861412 meter/sec RA = 94
10994 deg
ZDOT = -3798
903843 TA = 49
37573
MA = 49
21807
Ha = 189
154 n
mi
Hp = 177
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9555088
05 X = -2882729
96
Y = -14511451
50 feet Y = -4455493
29 meter
Z = 13517690
04 Z = 4106114
73
XDOT = 11136
340386 XDOT = 3477
302095
YDOT = -18995
608306 feet/sec YDOT = -5751
439346 meter/sec
ZDOT = -12463
595287 ZDOT = -3782
213315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15507583
95 X = 4726711
59
Y = -7931111
08 feet Y = -2417402
66 meter
Z = 13461879
26 Z = 4103180
80
XDOT = 17027
993318 XDOT = 5190
132363
YDOT = 12154
732812 feet/sec YDOT = 3704
762561 meter/sec
ZDOT = -12397
703075 ZDOT = -3778
819897
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 09349
54077856
00016717 00000-0 10270-3 0 9116
2 25544 51
6453 94
7129 0007693 84
4792 275
7250 15
76479076 34532
Satellite: ISS
Catalog Number: 25544
Epoch time: 09349
54077856 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 94
7129 deg
Eccentricity:
0007693
Arg of perigee: 84
4792 deg
Mean anomaly: 275
7250 deg
Mean motion: 15
76479076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3453
Checksum: 352
Coasting Arc #13 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2009/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2982279
88 A = 6718308
56 meter
Y = 4562825
43 meter E =
0018693
Z = 3912496
46 I = 51
97940
XDOT = -3285
654034 Wp = 94
98259
YDOT = -5660
899062 meter/sec RA = 89
03067 deg
ZDOT = 4079
243547 TA = 312
76401
MA = 312
92112
Ha = 189
016 n
mi
Hp = 177
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9784382
81 X = -3052086
85
Y = 14969899
71 feet Y = 4529084
88 meter
Z = 12836274
49 Z = 3897839
63
XDOT = -10779
704836 XDOT = -3241
925013
YDOT = -18572
503484 feet/sec YDOT = -5697
397339 meter/sec
ZDOT = 13383
344971 ZDOT = 4063
387048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13954714
07 X = -4253396
85
Y = -11250813
22 feet Y = -3429247
87 meter
Z = 12778385
82 Z = 3894852
00
XDOT = 18708
215547 XDOT = 5702
264099
YDOT = -8007
447230 feet/sec YDOT = -2440
669916 meter/sec
ZDOT = 13320
464868 ZDOT = 4060
077692
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 09350
55499109
00016717 00000-0 10270-3 0 9129
2 25544 51
6460 89
4856 0007586 87
9209 272
2825 15
76547338 34694
Satellite: ISS
Catalog Number: 25544
Epoch time: 09350
55499109 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 89
4856 deg
Eccentricity:
0007586
Arg of perigee: 87
9209 deg
Mean anomaly: 272
2825 deg
Mean motion: 15
76547338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 357
Coasting Arc #14 (Orbit 3483)
---------------------------------------
Vector Time (GMT): 2009/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2844609
41 A = 6721441
47 meter
Y = 5368077
56 meter E =
0011829
Z = -2882893
94 I = 51
98814
XDOT = -3509
114096 Wp = 79
85871
YDOT = 4583
510467 meter/sec RA = 83
85181 deg
ZDOT = 5091
772264 TA = 247
17580
MA = 247
30078
Ha = 188
977 n
mi
Hp = 177
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9332708
03 X = 2798375
80
Y = 17611803
01 feet Y = 5399629
61 meter
Z = -9458313
46 Z = -2869186
26
XDOT = -11512
841521 XDOT = -3584
841852
YDOT = 15037
763998 feet/sec YDOT = 4543
845260 meter/sec
ZDOT = 16705
289581 ZDOT = 5074
541740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18296986
42 X = -5576921
46
Y = 7969997
00 feet Y = 2429255
09 meter
Z = -9403944
57 Z = -2866322
31
XDOT = -13494
670232 XDOT = -4113
175487
YDOT = -11425
870407 feet/sec YDOT = -3482
605300 meter/sec
ZDOT = 16637
205859 ZDOT = 5071
020346
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 09351
50580676
00016717 00000-0 10270-3 0 9136
2 25544 51
6462 84
5862 0007499 89
7738 270
4286 15
76514660 34849
Satellite: ISS
Catalog Number: 25544
Epoch time: 09351
50580676 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 84
5862 deg
Eccentricity:
0007499
Arg of perigee: 89
7738 deg
Mean anomaly: 270
4286 deg
Mean motion: 15
76514660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3484
Checksum: 349
Coasting Arc #15 (Orbit 3499)
---------------------------------------
Vector Time (GMT): 2009/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 743802
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3211909
00 A = 6714763
25 meter
Y = -3359749
77 meter E =
0019283
Z = -4863379
81 I = 51
96108
XDOT = 3221
559692 Wp = 80
83917
YDOT = 6555
363498 meter/sec RA = 78
76365 deg
ZDOT = -2406
057796 TA = 165
78171
MA = 165
72736
Ha = 188
931 n
mi
Hp = 177
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10537759
18 X = 3272864
96
Y = -11022801
07 feet Y = -3323490
76 meter
Z = -15955970
50 Z = -4847628
82
XDOT = 10569
421563 XDOT = 3159
705202
YDOT = 21507
098092 feet/sec YDOT = 6591
043392 meter/sec
ZDOT = -7893
890408 ZDOT = -2390
556756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10346349
48 X = 3153567
32
Y = 11290821
78 feet Y = 3441442
48 meter
Z = -15893706
39 Z = -4844401
71
XDOT = -21297
490159 XDOT = -6491
475000
YDOT = 8513
966339 feet/sec YDOT = 2595
056940 meter/sec
ZDOT = -7832
398209 ZDOT = -2387
314974
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 09352
51999703
00016717 00000-0 10270-3 0 9144
2 25544 51
6459 79
3589 0007513 94
2696 265
9327 15
76537784 35000
Satellite: ISS
Catalog Number: 25544
Epoch time: 09352
51999703 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 79
3589 deg
Eccentricity:
0007513
Arg of perigee: 94
2696 deg
Mean anomaly: 265
9327 deg
Mean motion: 15
76537784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3500
Checksum: 358
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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