Date:
September 24th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
276/12:05:13
167 -4
0 5
1 5
1
N/A -2
2 0
0 193
7
000/00:10:26
334 2
2 0
2 188
8
Coasting Arc #1 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2008/266/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4578694
63 A = 6726817
83 meter
Y = 296176
60 meter E =
0018362
Z = -4935925
50 I = 51
35337
XDOT = -2692
630149 Wp = 116
21022
YDOT = -6888
586682 meter/sec RA = 235
63929 deg
ZDOT = 2082
428082 TA = 174
10511
MA = 174
08347
Ha = 194
895 n
mi
Hp = 184
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15021964
03 X = -4557688
30
Y = 971708
00 feet Y = 245092
50 meter
Z = -16193981
30 Z = -4958117
86
XDOT = -8834
088415 XDOT = -2625
516838
YDOT = -22600
350006 feet/sec YDOT = -6918
321999 meter/sec
ZDOT = 6832
113130 ZDOT = 2069
510174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7755644
13 X = 2363920
33
Y = -12793264
99 feet Y = -3899387
17 meter
Z = -16279772
88 Z = -4962074
77
XDOT = 22674
625060 XDOT = 6911
225718
YDOT = 5108
173806 feet/sec YDOT = 1556
971376 meter/sec
ZDOT = 6781
470315 ZDOT = 2066
992152
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 08266
66220033
00020000 00000-0 20000-3 0 9003
2 25544 51
6402 236
4920 0006256 138
2664 221
8977 15
72145162 3873
Satellite: ISS
Catalog Number: 25544
Epoch time: 08266
66220033 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 236
4920 deg
Eccentricity:
0006256
Arg of perigee: 138
2664 deg
Mean anomaly: 221
8977 deg
Mean motion: 15
72145162 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 387
Checksum: 278
Coasting Arc #2 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2008/267/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3362055
33 A = 6736754
70 meter
Y = 5688331
67 meter E =
0015380
Z = -1278927
93 I = 51
40469
XDOT = -4781
846776 Wp = 142
92946
YDOT = 1524
403979 meter/sec RA = 230
52805 deg
ZDOT = -5838
891392 TA = 51
14215
MA = 51
00501
Ha = 194
843 n
mi
Hp = 185
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11030365
24 X = 3304410
40
Y = 18662505
50 feet Y = 5725605
80 meter
Z = -4195957
79 Z = -1262735
13
XDOT = -15688
473674 XDOT = -4770
173251
YDOT = 5001
325390 feet/sec YDOT = 1470
995850 meter/sec
ZDOT = -19156
467822 ZDOT = -5862
093238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21654151
55 X = -6600185
39
Y = -1257843
35 feet Y = -383390
65 meter
Z = -4132757
10 Z = -1259664
36
XDOT = 4463
452673 XDOT = 1360
460375
YDOT = -14135
651580 feet/sec YDOT = -4308
546602 meter/sec
ZDOT = -19246
048500 ZDOT = -5866
195583
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 08267
67922311
00020000 00000-0 20000-3 0 9014
2 25544 51
6405 231
2832 0006308 142
9356 217
2243 15
72151495 4039
Satellite: ISS
Catalog Number: 25544
Epoch time: 08267
67922311 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 231
2832 deg
Eccentricity:
0006308
Arg of perigee: 142
9356 deg
Mean anomaly: 217
2243 deg
Mean motion: 15
72151495 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 403
Checksum: 265
Coasting Arc #3 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2008/268/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3581730
16 A = 6725327
53 meter
Y = -2289853
16 meter E =
0007112
Z = 5205650
83 I = 51
38630
XDOT = 4912
151172 Wp = 121
01916
YDOT = 5880
773743 meter/sec RA = 225
37039 deg
ZDOT = -795
775257 TA = 336
56149
MA = 336
59389
Ha = 194
496 n
mi
Hp = 185
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11751083
19 X = 3581781
43
Y = -7512641
59 feet Y = -2249799
73 meter
Z = 17078906
94 Z = 5223051
02
XDOT = 16115
981537 XDOT = 4849
892050
YDOT = 19293
877108 feet/sec YDOT = 5935
356117 meter/sec
ZDOT = -2610
811212 ZDOT = -772
063516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -40807
75 X = -12438
20
Y = 13864727
41 feet Y = 4225968
91 meter
Z = 17145975
35 Z = 5226093
29
XDOT = -23954
406300 XDOT = -7301
303040
YDOT = 3032
657619 feet/sec YDOT = 924
354042 meter/sec
ZDOT = -2518
494355 ZDOT = -767
637079
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 08268
69622915
00020000 00000-0 20000-3 0 9025
2 25544 51
6401 226
0745 0006147 147
0888 213
0658 15
72233110 4193
Satellite: ISS
Catalog Number: 25544
Epoch time: 08268
69622915 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 226
0745 deg
Eccentricity:
0006147
Arg of perigee: 147
0888 deg
Mean anomaly: 213
0658 deg
Mean motion: 15
72233110 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 419
Checksum: 280
Coasting Arc #4 (Orbit 434)
---------------------------------------
Vector Time (GMT): 2008/269/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5080362
40 A = 6737263
14 meter
Y = -4419915
73 meter E =
0012479
Z = 115539
02 I = 51
44831
XDOT = 3232
792326 Wp = 75
11101
YDOT = -3544
546941 meter/sec RA = 220
23983 deg
ZDOT = 6015
818510 TA = 286
14595
MA = 286
28327
Ha = 194
574 n
mi
Hp = 185
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16667855
64 X = -5031121
87
Y = -14501035
85 feet Y = -4476451
95 meter
Z = 379065
02 Z = 90978
56
XDOT = 10606
274035 XDOT = 3242
964076
YDOT = -11629
091015 feet/sec YDOT = -3508
338764 meter/sec
ZDOT = 19736
937370 ZDOT = 6031
548285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21130349
85 X = 6440530
64
Y = -6455155
17 feet Y = -1967531
29 meter
Z = 283601
25 Z = 86441
66
XDOT = 3832
792765 XDOT = 1168
235235
YDOT = 13519
616199 feet/sec YDOT = 4120
779017 meter/sec
ZDOT = 19797
415965 ZDOT = 6034
252386
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 08269
71322318
00020000 00000-0 20000-3 0 9034
2 25544 51
6406 220
8651 0006157 150
1682 209
9833 15
72214526 4351
Satellite: ISS
Catalog Number: 25544
Epoch time: 08269
71322318 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 220
8651 deg
Eccentricity:
0006157
Arg of perigee: 150
1682 deg
Mean anomaly: 209
9833 deg
Mean motion: 15
72214526 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 435
Checksum: 277
Coasting Arc #5 (Orbit 449)
---------------------------------------
Vector Time (GMT): 2008/270/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1957893
63 A = 6725168
45 meter
Y = 3740410
56 meter E =
0018112
Z = -5249636
47 I = 51
43186
XDOT = -6492
534055 Wp = 104
53544
YDOT = -4083
009341 meter/sec RA = 215
10657 deg
ZDOT = -493
625305 TA = 160
78681
MA = 160
71842
Ha = 194
415 n
mi
Hp = 185
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6423535
52 X = -1974072
20
Y = 12271688
17 feet Y = 3718425
37 meter
Z = -17223216
75 Z = -5259187
52
XDOT = -21300
964746 XDOT = -6443
996702
YDOT = -13395
699937 feet/sec YDOT = -4155
341259 meter/sec
ZDOT = -1619
505593 ZDOT = -525
047805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7259960
75 X = -2212836
04
Y = -11742596
71 feet Y = -3579143
48 meter
Z = -17259771
92 Z = -5260778
48
XDOT = 21593
281851 XDOT = 6581
632308
YDOT = -10818
850358 feet/sec YDOT = -3297
585589 meter/sec
ZDOT = -1741
490522 ZDOT = -530
806311
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 08270
66663942
00020000 00000-0 20000-3 0 9042
2 25544 51
6413 215
9813 0006137 153
9154 206
2319 15
72257947 4507
Satellite: ISS
Catalog Number: 25544
Epoch time: 08270
66663942 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 215
9813 deg
Eccentricity:
0006137
Arg of perigee: 153
9154 deg
Mean anomaly: 206
2319 deg
Mean motion: 15
72257947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 450
Checksum: 291
Coasting Arc #6 (Orbit 465)
---------------------------------------
Vector Time (GMT): 2008/271/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6114314
72 A = 6736792
83 meter
Y = 2626821
25 meter E =
0019267
Z = 977185
97 I = 51
49570
XDOT = -1106
751807 Wp = 134
99586
YDOT = 4800
917128 meter/sec RA = 209
95791 deg
ZDOT = -5923
072017 TA = 34
30503
MA = 34
18075
Ha = 194
416 n
mi
Hp = 185
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20060087
65 X = 6079739
73
Y = 8618179
94 feet Y = 2695001
82 meter
Z = 3205990
71 Z = 1006805
22
XDOT = -3631
075482 XDOT = -1131
580822
YDOT = 15751
040447 feet/sec YDOT = 4788
401401 meter/sec
ZDOT = -19432
650976 ZDOT = -5928
509410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17489099
69 X = -5330677
59
Y = 13040775
88 feet Y = 3974828
49 meter
Z = 3320854
55 Z = 1012196
47
XDOT = -10925
923146 XDOT = -3330
221375
YDOT = -9652
698277 feet/sec YDOT = -2942
142435 meter/sec
ZDOT = -19453
177933 ZDOT = -5929
328634
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 08271
68360369
00020000 00000-0 20000-3 0 9053
2 25544 51
6415 210
7723 0006295 158
2391 201
9039 15
72226757 4661
Satellite: ISS
Catalog Number: 25544
Epoch time: 08271
68360369 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 210
7723 deg
Eccentricity:
0006295
Arg of perigee: 158
2391 deg
Mean anomaly: 201
9039 deg
Mean motion: 15
72226757 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 466
Checksum: 296
Coasting Arc #7 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2008/272/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -90341
70 A = 6726048
82 meter
Y = -4456592
59 meter E =
0010918
Z = 5033838
02 I = 51
48654
XDOT = 7271
982061 Wp = 144
97050
YDOT = 1836
582518 meter/sec RA = 204
84909 deg
ZDOT = 1745
816219 TA = 288
12808
MA = 288
24695
Ha = 194
232 n
mi
Hp = 185
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -296396
66 X = -64954
38
Y = -14621366
78 feet Y = -4457460
40 meter
Z = 16515216
62 Z = 5033461
25
XDOT = 23858
208861 XDOT = 7242
423677
YDOT = 6025
533195 feet/sec YDOT = 1917
736923 meter/sec
ZDOT = 5727
743501 ZDOT = 1781
071892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12973470
71 X = 3954313
87
Y = 6754633
05 feet Y = 2058812
15 meter
Z = 16513285
18 Z = 5033249
32
XDOT = -16339
233326 XDOT = -4980
198318
YDOT = 16960
066961 feet/sec YDOT = 5169
428410 meter/sec
ZDOT = 5864
335019 ZDOT = 1787
449314
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 08272
70055011
00020000 00000-0 20000-3 0 9063
2 25544 51
6420 205
5630 0006097 161
9910 198
1470 15
72287203 4821
Satellite: ISS
Catalog Number: 25544
Epoch time: 08272
70055011 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 205
5630 deg
Eccentricity:
0006097
Arg of perigee: 161
9910 deg
Mean anomaly: 198
1470 deg
Mean motion: 15
72287203 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 482
Checksum: 266
Coasting Arc #8 (Orbit 496)
---------------------------------------
Vector Time (GMT): 2008/273/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6395377
31 A = 6735101
82 meter
Y = -565978
98 meter E =
0005681
Z = -2041491
19 I = 51
54458
XDOT = -1312
986000 Wp = 99
20874
YDOT = -5154
673319 meter/sec RA = 199
68418 deg
ZDOT = 5554
495028 TA = 238
02613
MA = 238
08136
Ha = 194
025 n
mi
Hp = 185
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20982209
02 X = -6378655
77
Y = -1856886
43 feet Y = -637402
48 meter
Z = -6697805
75 Z = -2072519
75
XDOT = -4307
696850 XDOT = -1282
231182
YDOT = -16911
657870 feet/sec YDOT = -5169
183411 meter/sec
ZDOT = 18223
408883 ZDOT = 5548
191627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11487297
90 X = 3501328
40
Y = -17610217
73 feet Y = -5367594
37 meter
Z = -6817913
37 Z = -2078099
99
XDOT = 15715
698504 XDOT = 4790
144904
YDOT = 3221
091598 feet/sec YDOT = 981
788719 meter/sec
ZDOT = 18198
473422 ZDOT = 5546
894699
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 08273
65392371
00020000 00000-0 20000-3 0 9072
2 25544 51
6419 200
6791 0005966 166
7975 193
3345 15
72313090 4979
Satellite: ISS
Catalog Number: 25544
Epoch time: 08273
65392371 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 200
6791 deg
Eccentricity:
0005966
Arg of perigee: 166
7975 deg
Mean anomaly: 193
3345 deg
Mean motion: 15
72313090 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 497
Checksum: 313
Coasting Arc #9 (Orbit 512)
---------------------------------------
Vector Time (GMT): 2008/274/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2171780
31 A = 6727642
33 meter
Y = 4371396
89 meter E =
0011084
Z = -4638047
60 I = 51
54684
XDOT = -7118
033819 Wp = 102
28896
YDOT = 500
853694 meter/sec RA = 194
59497 deg
ZDOT = -2869
058908 TA = 139
30420
MA = 139
22133
Ha = 193
884 n
mi
Hp = 185
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7125263
47 X = 2145268
47
Y = 14341853
30 feet Y = 4395534
38 meter
Z = -15216691
59 Z = -4627561
63
XDOT = -23353
129328 XDOT = -7109
167770
YDOT = 1643
220781 feet/sec YDOT = 421
305073 meter/sec
ZDOT = -9412
922926 ZDOT = -2903
617492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16052871
79 X = -4892915
32
Y = -102851
47 feet Y = -31349
13 meter
Z = -15175657
06 Z = -4625540
27
XDOT = 9130
009868 XDOT = 2782
827008
YDOT = -20324
536637 feet/sec YDOT = -6194
918767 meter/sec
ZDOT = -9546
581478 ZDOT = -2909
798034
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 08274
67084038
00020000 00000-0 20000-3 0 9084
2 25544 51
6413 195
4695 0005939 171
9223 188
2036 15
72336344 5137
Satellite: ISS
Catalog Number: 25544
Epoch time: 08274
67084038 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 195
4695 deg
Eccentricity:
0005939
Arg of perigee: 171
9223 deg
Mean anomaly: 188
2036 deg
Mean motion: 15
72336344 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 513
Checksum: 303
Coasting Arc #10 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2008/275/15:35:44
821
Vector Time (MET): N/A
Weight (LBS) : 614388
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5871173
66 A = 6732875
05 meter
Y = -1404556
17 meter E =
0015539
Z = 2960197
00 I = 51
59411
XDOT = 3627
092174 Wp = 118
72676
YDOT = 4613
738882 meter/sec RA = 189
42171 deg
ZDOT = -4992
378880 TA = 27
09027
MA = 27
00927
Ha = 193
610 n
mi
Hp = 185
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19262380
78 X = 5872062
86
Y = -4608123
91 feet Y = -1338896
16 meter
Z = 9711932
42 Z = 2988722
03
XDOT = 11899
908707 XDOT = 3599
483632
YDOT = 15136
938590 feet/sec YDOT = 4654
144442 meter/sec
ZDOT = -16379
195801 ZDOT = -4974
825433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4304324
03 X = -1311957
96
Y = 19276766
95 feet Y = 5875558
57 meter
Z = 9822158
70 Z = 2993793
97
XDOT = -17462
573704 XDOT = -5322
592465
YDOT = 4432
103506 feet/sec YDOT = 1350
905149 meter/sec
ZDOT = -16310
789258 ZDOT = -4971
528566
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 08275
68774142
00020000 00000-0 20000-3 0 9099
2 25544 51
6415 190
2604 0005858 175
0569 185
0652 15
72389026 5291
Satellite: ISS
Catalog Number: 25544
Epoch time: 08275
68774142 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 190
2604 deg
Eccentricity:
0005858
Arg of perigee: 175
0569 deg
Mean anomaly: 185
0652 deg
Mean motion: 15
72389026 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 529
Checksum: 312
Coasting Arc #11 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2008/276/12:10:26
334
Vector Time (MET): N/A
Weight (LBS) : 614022
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5546188
63 A = 6735025
22 meter
Y = 2070090
97 meter E =
0003569
Z = -3216601
34 I = 51
61612
XDOT = -4334
733560 Wp = 156
29754
YDOT = -4182
836502 meter/sec RA = 185
02549 deg
ZDOT = 4780
816096 TA = 166
18045
MA = 166
17068
Ha = 193
745 n
mi
Hp = 188
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18196156
91 X = -5553298
49
Y = 6791637
06 feet Y = 2008030
39 meter
Z = -10553154
01 Z = -3243562
70
XDOT = -14221
566799 XDOT = -4310
863102
YDOT = -13723
216869 feet/sec YDOT = -4231
176309 meter/sec
ZDOT = 15685
092179 ZDOT = 4759
815662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16060316
19 X = 4895184
37
Y = -10820554
43 feet Y = -3298104
99 meter
Z = -10657268
21 Z = -3248335
35
XDOT = 16319
739286 XDOT = 4974
256534
YDOT = 8850
109731 feet/sec YDOT = 2697
513446 meter/sec
ZDOT = 15603
390691 ZDOT = 4755
913483
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 08276
51396328
00020000 00000-0 20000-3 0 9100
2 25544 51
6408 186
0275 0004940 219
6138 140
4664 15
71396245 5421
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51396328 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 186
0275 deg
Eccentricity:
0004940
Arg of perigee: 219
6138 deg
Mean anomaly: 140
4664 deg
Mean motion: 15
71396245 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 293
Coasting Arc #12 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2008/277/12:10:26
334
Vector Time (MET): N/A
Weight (LBS) : 614022
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4895412
87 A = 6733934
63 meter
Y = 2866988
19 meter E =
0003312
Z = -3626987
39 I = 51
64188
XDOT = -5281
105701 Wp = 145
18125
YDOT = 3474
754889 meter/sec RA = 179
96005 deg
ZDOT = -4385
984295 TA = 78
20589
MA = 78
16873
Ha = 193
617 n
mi
Hp = 189
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16061065
83 X = 4880609
53
Y = 9406129
23 feet Y = 2921648
65 meter
Z = -11899564
94 Z = -3603241
00
XDOT = -17326
462275 XDOT = -5298
261680
YDOT = 11400
114465 feet/sec YDOT = 3415
602473 meter/sec
ZDOT = -14389
712254 ZDOT = -4411
682232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17963679
66 X = -5475329
56
Y = -5091659
48 feet Y = -1551937
81 meter
Z = -11807369
11 Z = -3598886
11
XDOT = 13488
948604 XDOT = 4111
431535
YDOT = -14026
335913 feet/sec YDOT = -4275
227186 meter/sec
ZDOT = -14488
802527 ZDOT = -4416
187010
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 08277
53147991
00020000 00000-0 20000-3 0 9114
2 25544 51
6411 180
8224 0004953 224
7689 135
3074 15
71412942 5581
Satellite: ISS
Catalog Number: 25544
Epoch time: 08277
53147991 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 180
8224 deg
Eccentricity:
0004953
Arg of perigee: 224
7689 deg
Mean anomaly: 135
3074 deg
Mean motion: 15
71412942 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 558
Checksum: 297
Coasting Arc #13 (Orbit 573)
---------------------------------------
Vector Time (GMT): 2008/278/12:10:26
334
Vector Time (MET): N/A
Weight (LBS) : 614022
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3458610
25 A = 6731116
52 meter
Y = -3778955
31 meter E =
0005121
Z = 4362001
46 I = 51
66160
XDOT = 6581
937116 Wp = 90
06851
YDOT = 2098
434301 meter/sec RA = 174
79562 deg
ZDOT = -3397
423929 TA = 34
18598
MA = 34
15302
Ha = 193
283 n
mi
Hp = 189
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11347146
48 X = 3479419
85
Y = -12398147
35 feet Y = -3740162
73 meter
Z = 14311028
40 Z = 4378854
31
XDOT = 21594
281876 XDOT = 6574
487297
YDOT = 6884
626973 feet/sec YDOT = 2171
995624 meter/sec
ZDOT = -11146
403968 ZDOT = -3365
466365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7565359
26 X = -2305921
50
Y = 14945806
51 feet Y = 4555481
83 meter
Z = 14375866
29 Z = 4381764
05
XDOT = -21618
728170 XDOT = -6589
388346
YDOT = -330
200397 feet/sec YDOT = -100
645081 meter/sec
ZDOT = -11022
499406 ZDOT = -3359
657819
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 08278
54898170
00020000 00000-0 20000-3 0 9129
2 25544 51
6404 175
6171 0004902 229
2852 130
7884 15
71449124 5740
Satellite: ISS
Catalog Number: 25544
Epoch time: 08278
54898170 = yrday
fracday
Element set: 912
Inclination: 51
6404 deg
RA of node: 175
6171 deg
Eccentricity:
0004902
Arg of perigee: 229
2852 deg
Mean anomaly: 130
7884 deg
Mean motion: 15
71449124 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 574
Checksum: 301
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/plugins/scheduled_mailings pl/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list