Date:
September 14th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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 1950)
---------------------------------------
Vector Time (GMT): 2009/254/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2655463
38 A = 6728942
19 meter
Y = 5571274
40 meter E =
0012874
Z = -2690854
91 I = 51
41497
XDOT = -5690
183972 Wp = 93
85984
YDOT = 225
302640 meter/sec RA = 224
15920 deg
ZDOT = -5170
977490 TA = 116
88941
MA = 116
75778
Ha = 193
298 n
mi
Hp = 180
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8712150
19 X = 2606038
86
Y = 18278459
31 feet Y = 5600693
01 meter
Z = -8828264
14 Z = -2678074
61
XDOT = -18668
582585 XDOT = -5667
160560
YDOT = 739
181891 feet/sec YDOT = 161
800397 meter/sec
ZDOT = -16965
149244 ZDOT = -5198
564699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19867588
86 X = 6055641
08
Y = -4021708
37 feet Y = -1225816
71 meter
Z = -8777622
59 Z = -2675419
37
XDOT = -4123
160184 XDOT = -1256
739224
YDOT = 16736
373424 feet/sec YDOT = 5101
246620 meter/sec
ZDOT = -17073
699906 ZDOT = -5204
063731
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 09254
26591782
00020000 00000-0 20000-3 0 9009
2 25544 51
6389 224
9551 0009030 77
3566 282
8606 15
74042333 19518
Satellite: ISS
Catalog Number: 25544
Epoch time: 09254
26591782 = yrday
fracday
Element set: 900
Inclination: 51
6389 deg
RA of node: 224
9551 deg
Eccentricity:
0009030
Arg of perigee: 77
3566 deg
Mean anomaly: 282
8606 deg
Mean motion: 15
74042333 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1951
Checksum: 299
Coasting Arc #2 (Orbit 1966)
---------------------------------------
Vector Time (GMT): 2009/255/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4955989
68 A = 6722983
04 meter
Y = -599992
14 meter E =
0017476
Z = 4491113
50 I = 51
41831
XDOT = 3570
856514 Wp = 73
55875
YDOT = 6081
669200 meter/sec RA = 218
96164 deg
ZDOT = -3113
131143 TA = 47
61892
MA = 47
47112
Ha = 193
041 n
mi
Hp = 180
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16259808
67 X = 4940513
46
Y = -1968478
15 feet Y = -544657
94 meter
Z = 14734624
34 Z = 4515152
18
XDOT = 11715
408511 XDOT = 3517
707929
YDOT = 19952
982939 feet/sec YDOT = 6121
303486 meter/sec
ZDOT = -10213
684851 ZDOT = -3095
912882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1773096
23 X = 540439
73
Y = -16196186
56 feet Y = -4936597
66 meter
Z = 14829197
87 Z = 4519939
51
XDOT = 20931
695555 XDOT = 6379
980805
YDOT = -7042
073760 feet/sec YDOT = -2146
424082 meter/sec
ZDOT = -10145
536638 ZDOT = -3092
359567
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 09255
28171299
00020000 00000-0 20000-3 0 9010
2 25544 51
6392 219
7380 0008877 80
1011 280
1154 15
74100803 19672
Satellite: ISS
Catalog Number: 25544
Epoch time: 09255
28171299 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 219
7380 deg
Eccentricity:
0008877
Arg of perigee: 80
1011 deg
Mean anomaly: 280
1154 deg
Mean motion: 15
74100803 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1967
Checksum: 284
Coasting Arc #3 (Orbit 1982)
---------------------------------------
Vector Time (GMT): 2009/256/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3549031
59 A = 6728772
73 meter
Y = -5005935
29 meter E =
0022773
Z = 2736497
47 I = 51
46057
XDOT = 5624
298363 Wp = 81
29867
YDOT = -1158
707767 meter/sec RA = 213
85754 deg
ZDOT = 5141
715173 TA = 310
08084
MA = 310
28029
Ha = 193
340 n
mi
Hp = 180
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11643804
43 X = -3506083
98
Y = -16423672
20 feet Y = -5045382
54 meter
Z = 8978010
08 Z = 2719360
57
XDOT = 18452
422450 XDOT = 5611
859735
YDOT = -3801
534668 feet/sec YDOT = -1095
883154 meter/sec
ZDOT = 16869
144270 ZDOT = 5169
007750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18524327
38 X = -5646214
99
Y = 7960955
73 feet Y = 2426499
31 meter
Z = 8910237
58 Z = 2715840
42
XDOT = 743
870724 XDOT = 226
731797
YDOT = -17391
737550 feet/sec YDOT = -5301
001605 meter/sec
ZDOT = 16976
501967 ZDOT = 5174
437799
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 09256
29750030
00020000 00000-0 20000-3 0 9029
2 25544 51
6385 214
5209 0009158 84
1630 276
0577 15
74072198 19837
Satellite: ISS
Catalog Number: 25544
Epoch time: 09256
29750030 = yrday
fracday
Element set: 902
Inclination: 51
6385 deg
RA of node: 214
5209 deg
Eccentricity:
0009158
Arg of perigee: 84
1630 deg
Mean anomaly: 276
0577 deg
Mean motion: 15
74072198 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1983
Checksum: 298
Coasting Arc #4 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2009/257/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4839826
41 A = 6723136
68 meter
Y = 1408044
93 meter E =
0018593
Z = -4466491
10 I = 51
46785
XDOT = -4496
378879 Wp = 99
62526
YDOT = -5355
032833 meter/sec RA = 208
66215 deg
ZDOT = 3192
284036 TA = 202
40050
MA = 202
48179
Ha = 193
257 n
mi
Hp = 180
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15878695
56 X = -4833514
42
Y = 4619569
97 feet Y = 1353958
40 meter
Z = -14653842
20 Z = -4489987
52
XDOT = -14751
899210 XDOT = -4451
671245
YDOT = -17569
005357 feet/sec YDOT = -5405
063990 meter/sec
ZDOT = 10473
372823 ZDOT = 3170
549390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1459566
19 X = 444875
77
Y = 16389820
87 feet Y = 4995617
40 meter
Z = -14746251
36 Z = -4494657
41
XDOT = -18919
099337 XDOT = -5766
541478
YDOT = 11006
486878 feet/sec YDOT = 3354
777200 meter/sec
ZDOT = 10387
464079 ZDOT = 3166
099051
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 09257
24978855
00020000 00000-0 20000-3 0 9033
2 25544 51
6386 209
6294 0009158 87
1965 273
0246 15
74099143 19986
Satellite: ISS
Catalog Number: 25544
Epoch time: 09257
24978855 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 209
6294 deg
Eccentricity:
0009158
Arg of perigee: 87
1965 deg
Mean anomaly: 273
0246 deg
Mean motion: 15
74099143 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1998
Checksum: 341
Coasting Arc #5 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2009/258/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4269640
74 A = 6728305
18 meter
Y = 4345878
97 meter E =
0013536
Z = -2863704
58 I = 51
51294
XDOT = -5432
659055 Wp = 100
19780
YDOT = 2018
760672 meter/sec RA = 203
56165 deg
ZDOT = -5058
798613 TA = 112
72222
MA = 112
57909
Ha = 193
272 n
mi
Hp = 180
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14008007
67 X = 4234638
28
Y = 14258133
12 feet Y = 4393428
80 meter
Z = -9395356
22 Z = -2843048
01
XDOT = -17823
684564 XDOT = -5430
254896
YDOT = 6623
230552 feet/sec YDOT = 1958
022753 meter/sec
ZDOT = -16597
108312 ZDOT = -5085
184474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16528684
67 X = 5037943
09
Y = -11306995
58 feet Y = -3446372
25 meter
Z = -9313742
08 Z = -2838828
59
XDOT = 2545
156718 XDOT = 775
763768
YDOT = 17415
703041 feet/sec YDOT = 5308
306287 meter/sec
ZDOT = -16700
862096 ZDOT = -5090
422767
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 09258
26555158
00020000 00000-0 20000-3 0 9044
2 25544 51
6394 204
4114 0009219 91
0312 269
1907 15
74128462 20144
Satellite: ISS
Catalog Number: 25544
Epoch time: 09258
26555158 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 204
4114 deg
Eccentricity:
0009219
Arg of perigee: 91
0312 deg
Mean anomaly: 269
1907 deg
Mean motion: 15
74128462 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2014
Checksum: 280
Coasting Arc #6 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2009/259/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4620037
91 A = 6723238
81 meter
Y = -2133707
25 meter E =
0017959
Z = 4379840
31 I = 51
52361
XDOT = 5267
632839 Wp = 81
97784
YDOT = 4538
873809 meter/sec RA = 198
36916 deg
ZDOT = -3331
264626 TA = 41
58769
MA = 41
45122
Ha = 193
066 n
mi
Hp = 180
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15157604
69 X = 4622277
72
Y = -7000351
87 feet Y = -2082030
46 meter
Z = 14369554
84 Z = 4402289
85
XDOT = 17282
259972 XDOT = 5232
669416
YDOT = 14891
318272 feet/sec YDOT = 4597
583875 meter/sec
ZDOT = -10929
345887 ZDOT = -3305
759896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4487913
02 X = -1367915
89
Y = -16002263
16 feet Y = -4877489
81 meter
Z = 14457808
37 Z = 4406739
99
XDOT = 16317
163031 XDOT = 4973
471292
YDOT = -14401
176993 feet/sec YDOT = -4389
478747 meter/sec
ZDOT = -10828
615909 ZDOT = -3300
562129
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 09259
28130176
00020000 00000-0 20000-3 0 9057
2 25544 51
6386 199
1940 0009144 94
4188 265
8020 15
74164878 20305
Satellite: ISS
Catalog Number: 25544
Epoch time: 09259
28130176 = yrday
fracday
Element set: 905
Inclination: 51
6386 deg
RA of node: 199
1940 deg
Eccentricity:
0009144
Arg of perigee: 94
4188 deg
Mean anomaly: 265
8020 deg
Mean motion: 15
74164878 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2030
Checksum: 304
Coasting Arc #7 (Orbit 2045)
---------------------------------------
Vector Time (GMT): 2009/260/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4884507
82 A = 6728104
88 meter
Y = -3552743
10 meter E =
0022519
Z = 2944380
03 I = 51
56842
XDOT = 5118
038972 Wp = 88
85669
YDOT = -2867
471149 meter/sec RA = 193
27372 deg
ZDOT = 4998
163961 TA = 305
15648
MA = 305
36725
Ha = 193
330 n
mi
Hp = 180
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16025288
13 X = -4858720
60
Y = -11655981
30 feet Y = -3607220
10 meter
Z = 9660039
46 Z = 2920714
16
XDOT = 16791
466442 XDOT = 5125
443086
YDOT = -9407
713744 feet/sec YDOT = -2810
196383 meter/sec
ZDOT = 16398
175724 ZDOT = 5023
045505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13844761
31 X = -4219883
25
Y = 14240462
01 feet Y = 4340492
82 meter
Z = 9566605
90 Z = 2915901
48
XDOT = -5873
480251 XDOT = -1790
236781
YDOT = -16864
074319 feet/sec YDOT = -5140
169852 meter/sec
ZDOT = 16495
960149 ZDOT = 5027
968653
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 09260
29704282
00020000 00000-0 20000-3 0 9066
2 25544 51
6388 193
9762 0009336 97
7521 262
4703 15
74134348 20468
Satellite: ISS
Catalog Number: 25544
Epoch time: 09260
29704282 = yrday
fracday
Element set: 906
Inclination: 51
6388 deg
RA of node: 193
9762 deg
Eccentricity:
0009336
Arg of perigee: 97
7521 deg
Mean anomaly: 262
4703 deg
Mean motion: 15
74134348 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2046
Checksum: 306
Coasting Arc #8 (Orbit 2060)
---------------------------------------
Vector Time (GMT): 2009/261/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4300702
48 A = 6723517
73 meter
Y = 2854450
18 meter E =
0018075
Z = -4326293
45 I = 51
58441
XDOT = -5851
537306 Wp = 106
40440
YDOT = -3595
708973 meter/sec RA = 188
08435 deg
ZDOT = 3451
391877 TA = 198
52791
MA = 198
59381
Ha = 193
151 n
mi
Hp = 180
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14109916
28 X = -4311285
44
Y = 9364994
04 feet Y = 2806297
58 meter
Z = -14193876
16 Z = -4347212
27
XDOT = -19197
957041 XDOT = -5827
660814
YDOT = -11796
945448 feet/sec YDOT = -3661
010456 meter/sec
ZDOT = 11323
464163 ZDOT = 3423
023462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7513815
12 X = 2290210
85
Y = 15099525
52 feet Y = 4602335
38 meter
Z = -14276059
78 Z = -4351343
02
XDOT = -13039
329119 XDOT = -3974
387516
YDOT = 17067
461496 feet/sec YDOT = 5202
162264 meter/sec
ZDOT = 11211
501609 ZDOT = 3417
265690
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 09261
24928635
00020000 00000-0 20000-3 0 9073
2 25544 51
6403 189
0849 0009153 101
3790 258
8402 15
74158214 20615
Satellite: ISS
Catalog Number: 25544
Epoch time: 09261
24928635 = yrday
fracday
Element set: 907
Inclination: 51
6403 deg
RA of node: 189
0849 deg
Eccentricity:
0009153
Arg of perigee: 101
3790 deg
Mean anomaly: 258
8402 deg
Mean motion: 15
74158214 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2061
Checksum: 290
Coasting Arc #9 (Orbit 2076)
---------------------------------------
Vector Time (GMT): 2009/262/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5304691
42 A = 6727533
73 meter
Y = 2740665
88 meter E =
0013683
Z = -3106606
65 I = 51
62700
XDOT = -4717
216789 Wp = 106
03121
YDOT = 3622
857881 meter/sec RA = 182
99369 deg
ZDOT = -4880
223821 TA = 110
03602
MA = 109
88866
Ha = 193
139 n
mi
Hp = 180
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17403843
25 X = 5288742
00
Y = 8991685
95 feet Y = 2799896
56 meter
Z = -10192279
03 Z = -3080875
31
XDOT = -15476
433034 XDOT = -4733
670212
YDOT = 11886
016671 feet/sec YDOT = 3570
014692 meter/sec
ZDOT = -16011
233008 ZDOT = -4903
180542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10849747
38 X = 3307003
00
Y = -16373343
33 feet Y = -4990595
05 meter
Z = -10090755
07 Z = -3075662
14
XDOT = 8935
827864 XDOT = 2723
640333
YDOT = 15800
671821 feet/sec YDOT = 4816
044771 meter/sec
ZDOT = -16101
393535 ZDOT = -4907
704749
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 09262
26500200
00020000 00000-0 20000-3 0 9081
2 25544 51
6396 183
8668 0009164 105
6789 254
5385 15
74185605 20778
Satellite: ISS
Catalog Number: 25544
Epoch time: 09262
26500200 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 183
8668 deg
Eccentricity:
0009164
Arg of perigee: 105
6789 deg
Mean anomaly: 254
5385 deg
Mean motion: 15
74185605 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2077
Checksum: 311
Coasting Arc #10 (Orbit 2092)
---------------------------------------
Vector Time (GMT): 2009/263/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3904826
34 A = 6723707
32 meter
Y = -3481793
39 meter E =
0018203
Z = 4207782
69 I = 51
64377
XDOT = 6273
100111 Wp = 90
40731
YDOT = 2633
605047 meter/sec RA = 177
80692 deg
ZDOT = -3628
913248 TA = 36
53607
MA = 36
41202
Ha = 192
921 n
mi
Hp = 180
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12811110
04 X = 3923029
25
Y = -11423206
67 feet Y = -3438025
16 meter
Z = 13805061
32 Z = 4226797
09
XDOT = 20581
037110 XDOT = 6260
813264
YDOT = 8640
436507 feet/sec YDOT = 2703
685515 meter/sec
ZDOT = -11905
883361 ZDOT = -3598
468260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10197955
42 X = -3108336
81
Y = -13731322
68 feet Y = -4185307
15 meter
Z = 13879711
51 Z = 4230536
07
XDOT = 9509
883415 XDOT = 2898
612465
YDOT = -19019
859978 feet/sec YDOT = -5797
253321 meter/sec
ZDOT = -11785
798143 ZDOT = -3592
311274
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 09263
28070480
00020000 00000-0 20000-3 0 9097
2 25544 51
6386 178
6490 0009107 108
8110 251
4042 15
74233322 20936
Satellite: ISS
Catalog Number: 25544
Epoch time: 09263
28070480 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 178
6490 deg
Eccentricity:
0009107
Arg of perigee: 108
8110 deg
Mean anomaly: 251
4042 deg
Mean motion: 15
74233322 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2093
Checksum: 275
Coasting Arc #11 (Orbit 2108)
---------------------------------------
Vector Time (GMT): 2009/264/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5599617
09 A = 6727092
67 meter
Y = -1850852
05 meter E =
0021440
Z = 3221076
49 I = 51
68410
XDOT = 4202
549511 Wp = 97
72759
YDOT = -4344
331321 meter/sec RA = 172
72217 deg
ZDOT = 4779
718440 TA = 299
92896
MA = 300
14172
Ha = 193
014 n
mi
Hp = 180
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18371447
13 X = -5594152
00
Y = -6072349
26 feet Y = -1913439
48 meter
Z = 10567836
24 Z = 3193886
55
XDOT = 13787
892095 XDOT = 4227
596872
YDOT = -14253
055515 feet/sec YDOT = -4297
195540 meter/sec
ZDOT = 15681
490946 ZDOT = 4800
195888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7442030
13 X = -2268330
78
Y = 17923568
29 feet Y = 5463103
62 meter
Z = 10460618
79 Z = 3188396
61
XDOT = -11874
751097 XDOT = -3619
424134
YDOT = -14187
217924 feet/sec YDOT = -4324
264023 meter/sec
ZDOT = 15761
853671 ZDOT = 4804
212999
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 09264
29639612
00020000 00000-0 20000-3 0 9109
2 25544 51
6380 173
4317 0009045 112
8601 247
3518 15
74235270 21096
Satellite: ISS
Catalog Number: 25544
Epoch time: 09264
29639612 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 173
4317 deg
Eccentricity:
0009045
Arg of perigee: 112
8601 deg
Mean anomaly: 247
3518 deg
Mean motion: 15
74235270 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2109
Checksum: 277
Coasting Arc #12 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2009/265/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3423605
43 A = 6724121
72 meter
Y = 4085680
10 meter E =
0016768
Z = -4116578
94 I = 51
70357
XDOT = -6488
624509 Wp = 113
41651
YDOT = -1627
985368 meter/sec RA = 167
53841 deg
ZDOT = 3786
202015 TA = 195
43162
MA = 195
48281
Ha = 192
910 n
mi
Hp = 180
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11232301
28 X = -3449039
85
Y = 13404462
26 feet Y = 4047252
90 meter
Z = -13505836
42 Z = -4133273
08
XDOT = -21288
138152 XDOT = -6488
330819
YDOT = -5341
159344 feet/sec YDOT = -1700
543143 meter/sec
ZDOT = 12421
922623 ZDOT = 3754
680583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12733757
53 X = 3881249
30
Y = 11913117
70 feet Y = 3631118
27 meter
Z = -13571325
06 Z = -4136539
88
XDOT = -5703
958713 XDOT = -1738
566616
YDOT = 20085
355696 feet/sec YDOT = 6122
016416 meter/sec
ZDOT = 12297
651171 ZDOT = 3748
324077
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 09265
24859515
00020000 00000-0 20000-3 0 9112
2 25544 51
6377 168
5399 0008989 115
8766 244
3325 15
74222925 21241
Satellite: ISS
Catalog Number: 25544
Epoch time: 09265
24859515 = yrday
fracday
Element set: 911
Inclination: 51
6377 deg
RA of node: 168
5399 deg
Eccentricity:
0008989
Arg of perigee: 115
8766 deg
Mean anomaly: 244
3325 deg
Mean motion: 15
74222925 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2124
Checksum: 325
Coasting Arc #13 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2009/266/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5710395
87 A = 6726492
92 meter
Y = 1017201
24 meter E =
0013463
Z = -3412410
04 I = 51
73939
XDOT = -3632
998089 Wp = 109
91270
YDOT = 4967
919720 meter/sec RA = 162
45674 deg
ZDOT = -4617
817955 TA = 110
31194
MA = 110
16722
Ha = 192
891 n
mi
Hp = 180
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18734894
59 X = 5715174
05
Y = 3337274
39 feet Y = 1081084
84 meter
Z = -11195571
01 Z = -3384656
96
XDOT = -11919
285070 XDOT = -3665
847356
YDOT = 16298
949213 feet/sec YDOT = 4927
109569 meter/sec
ZDOT = -15150
321376 ZDOT = -4635
547280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4103314
45 X = 1250690
24
Y = -18647628
23 feet Y = -5683797
08 meter
Z = -11086174
17 Z = -3379065
89
XDOT = 14441
314462 XDOT = 4401
712648
YDOT = 12188
308912 feet/sec YDOT = 3714
996557 meter/sec
ZDOT = -15219
841547 ZDOT = -4639
007704
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 09266
26426217
00020000 00000-0 20000-3 0 9125
2 25544 51
6366 163
3207 0009016 119
8689 240
3372 15
74252297 21401
Satellite: ISS
Catalog Number: 25544
Epoch time: 09266
26426217 = yrday
fracday
Element set: 912
Inclination: 51
6366 deg
RA of node: 163
3207 deg
Eccentricity:
0009016
Arg of perigee: 119
8689 deg
Mean anomaly: 240
3372 deg
Mean motion: 15
74252297 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2140
Checksum: 288
Coasting Arc #14 (Orbit 2155)
---------------------------------------
Vector Time (GMT): 2009/267/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2886441
02 A = 6724447
25 meter
Y = -4590921
86 meter E =
0018262
Z = 3958660
96 I = 51
76086
XDOT = 6560
405668 Wp = 98
73300
YDOT = 667
199388 meter/sec RA = 157
27590 deg
ZDOT = -3996
876032 TA = 32
61829
MA = 32
50561
Ha = 192
625 n
mi
Hp = 180
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9469950
85 X = 2918332
28
Y = -15062079
59 feet Y = -4558465
58 meter
Z = 12987732
82 Z = 3972761
02
XDOT = 21523
640642 XDOT = 6571
873680
YDOT = 2188
974371 feet/sec YDOT = 740
625744 meter/sec
ZDOT = -13113
110341 ZDOT = -3964
977352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14834875
76 X = -4521670
13
Y = -9748551
87 feet Y = -2971358
61 meter
Z = 13042990
92 Z = 3975503
63
XDOT = 1989
448890 XDOT = 606
384022
YDOT = -20460
003416 feet/sec YDOT = -6236
209041 meter/sec
ZDOT = -12987
392179 ZDOT = -3958
557136
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 09267
27991552
00020000 00000-0 20000-3 0 9137
2 25544 51
6361 158
1025 0008793 123
4473 236
7532 15
74294614 21562
Satellite: ISS
Catalog Number: 25544
Epoch time: 09267
27991552 = yrday
fracday
Element set: 913
Inclination: 51
6361 deg
RA of node: 158
1025 deg
Eccentricity:
0008793
Arg of perigee: 123
4473 deg
Mean anomaly: 236
7532 deg
Mean motion: 15
74294614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2156
Checksum: 301
Coasting Arc #15 (Orbit 2171)
---------------------------------------
Vector Time (GMT): 2009/268/05:44:50
891
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5699501
63 A = 6725820
60 meter
Y = -159963
93 meter E =
0020035
Z = 3556813
58 I = 51
79278
XDOT = 2959
837511 Wp = 107
70485
YDOT = -5535
795697 meter/sec RA = 152
20012 deg
ZDOT = 4467
442202 TA = 294
63799
MA = 294
84654
Ha = 192
617 n
mi
Hp = 180
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18699152
33 X = -5714567
80
Y = -524816
04 feet Y = -223783
30 meter
Z = 11669335
90 Z = 3529088
56
XDOT = 9710
752989 XDOT = 2999
817529
YDOT = -18162
059372 feet/sec YDOT = -5502
473448 meter/sec
ZDOT = 14656
962606 ZDOT = 4481
918413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -646828
56 X = -197153
35
Y = 18763082
23 feet Y = 5718987
46 meter
Z = 11560081
68 Z = 3523512
89
XDOT = -16730
523627 XDOT = -5099
463602
YDOT = -9696
002939 feet/sec YDOT = -2955
341696 meter/sec
ZDOT = 14713
653014 ZDOT = 4484
721439
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 09268
29555605
00020000 00000-0 20000-3 0 9146
2 25544 51
6362 152
8847 0008770 128
3127 231
8826 15
74337775 21727
Satellite: ISS
Catalog Number: 25544
Epoch time: 09268
29555605 = yrday
fracday
Element set: 914
Inclination: 51
6362 deg
RA of node: 152
8847 deg
Eccentricity:
0008770
Arg of perigee: 128
3127 deg
Mean anomaly: 231
8826 deg
Mean motion: 15
74337775 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2172
Checksum: 315
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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