Date:
March 8th 2009
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) : 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 2979)
---------------------------------------
Vector Time (GMT): 2009/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2786730
13 A = 6739763
92 meter
Y = -6120317
27 meter E =
0019610
Z = -356259
13 I = 51
96736
XDOT = 4194
586993 Wp = 118
07151
YDOT = 2246
890791 meter/sec RA = 112
10602 deg
ZDOT = -6049
311409 TA = 65
77957
MA = 65
57476
Ha = 197
725 n
mi
Hp = 184
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9142815
40 X = 2856692
03
Y = -20079781
06 feet Y = -6088763
25 meter
Z = -1168829
17 Z = -342551
50
XDOT = 13761
768351 XDOT = 4198
535984
YDOT = 7371
688947 feet/sec YDOT = 2293
819141 meter/sec
ZDOT = -19846
822207 ZDOT = -6028
924957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14448759
74 X = 4403981
97
Y = -16677624
70 feet Y = -5083340
01 meter
Z = -1115804
10 Z = -340097
09
XDOT = 10012
725525 XDOT = 3051
878740
YDOT = 9937
306516 feet/sec YDOT = 3028
891026 meter/sec
ZDOT = -19767
050016 ZDOT = -6024
996845
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 09065
53122336
00010596 00000-0 82463-4 0 9005
2 25544 51
6408 112
7996 0009571 94
1997 266
0259 15
71319588 29809
Satellite: ISS
Catalog Number: 25544
Epoch time: 09065
53122336 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 112
7996 deg
Eccentricity:
0009571
Arg of perigee: 94
1997 deg
Mean anomaly: 266
0259 deg
Mean motion: 15
71319588 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2980
Checksum: 334
Coasting Arc #2 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2009/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4142391
13 A = 6727817
61 meter
Y = -547250
23 meter E =
0012411
Z = 5262873
59 I = 51
93652
XDOT = 1779
257557 Wp = 102
11026
YDOT = -7472
411933 meter/sec RA = 107
01525 deg
ZDOT = 619
674991 TA = 342
00582
MA = 342
04971
Ha = 197
828 n
mi
Hp = 184
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13590522
09 X = -4161529
28
Y = -1795440
39 feet Y = -593679
70 meter
Z = 17266645
62 Z = 5242703
88
XDOT = 5837
459178 XDOT = 1859
672878
YDOT = -24515
787182 feet/sec YDOT = -7452
065595 meter/sec
ZDOT = 2033
054433 ZDOT = 628
513966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12719704
81 X = -3876966
03
Y = -5371209
78 feet Y = -1637144
74 meter
Z = 17187849
28 Z = 5238856
46
XDOT = 11743
598496 XDOT = 3579
448821
YDOT = -21156
301323 feet/sec YDOT = -6448
440643 meter/sec
ZDOT = 2066
967198 ZDOT = 630
011602
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 09066
54879216
00010596 00000-0 82463-4 0 9014
2 25544 51
6400 107
5952 0009595 98
0632 262
1619 15
71337356 29967
Satellite: ISS
Catalog Number: 25544
Epoch time: 09066
54879216 = yrday
fracday
Element set: 901
Inclination: 51
6400 deg
RA of node: 107
5952 deg
Eccentricity:
0009595
Arg of perigee: 98
0632 deg
Mean anomaly: 262
1619 deg
Mean motion: 15
71337356 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2996
Checksum: 331
Coasting Arc #3 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2009/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -257503
32 A = 6738831
12 meter
Y = 6583052
41 meter E =
0015465
Z = -1414586
39 I = 51
98178
XDOT = -4890
153392 Wp = 71
40805
YDOT = 1052
102578 meter/sec RA = 101
90385 deg
ZDOT = 5842
909737 TA = 273
13726
MA = 273
31419
Ha = 197
656 n
mi
Hp = 184
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -844827
17 X = -324225
34
Y = 21597940
99 feet Y = 6579799
71 meter
Z = -4641031
46 Z = -1415999
77
XDOT = -16043
810340 XDOT = -4929
937814
YDOT = 3451
780112 feet/sec YDOT = 997
195939 meter/sec
ZDOT = 19169
651369 ZDOT = 5819
057280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6176662
07 X = -1882646
60
Y = 20712008
10 feet Y = 6313020
07 meter
Z = -4646022
67 Z = -1416107
71
XDOT = -14994
478410 XDOT = -4570
317019
YDOT = -234
013256 feet/sec YDOT = -71
327241 meter/sec
ZDOT = 19076
597965 ZDOT = 5814
547060
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 09067
50275199
00010596 00000-0 82463-4 0 9022
2 25544 51
6406 102
7155 0009626 101
3187 258
9056 15
71356738 30115
Satellite: ISS
Catalog Number: 25544
Epoch time: 09067
50275199 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 102
7155 deg
Eccentricity:
0009626
Arg of perigee: 101
3187 deg
Mean anomaly: 258
9056 deg
Mean motion: 15
71356738 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3011
Checksum: 307
Coasting Arc #4 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2009/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4087124
47 A = 6729722
66 meter
Y = -2326852
41 meter E =
0020510
Z = -4831495
54 I = 51
95610
XDOT = 1120
602311 Wp = 86
94605
YDOT = 7171
403650 meter/sec RA = 96
84348 deg
ZDOT = -2513
856910 TA = 158
54284
MA = 158
45674
Ha = 197
649 n
mi
Hp = 184
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13409201
02 X = 4136309
95
Y = -7634030
21 feet Y = -2280873
21 meter
Z = -15851363
31 Z = -4811521
08
XDOT = 3676
516767 XDOT = 1052
538776
YDOT = 23528
227199 feet/sec YDOT = 7183
554096 meter/sec
ZDOT = -8247
562042 ZDOT = -2508
579098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14906040
25 X = 4543361
07
Y = -4284371
17 feet Y = -1305876
33 meter
Z = -15773551
78 Z = -4807778
58
XDOT = -2163
377088 XDOT = -659
397336
YDOT = 22662
080449 feet/sec YDOT = 6907
402121 meter/sec
ZDOT = -8226
378533 ZDOT = -2507
400177
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 09068
52029571
00010596 00000-0 82463-4 0 9037
2 25544 51
6407 97
5097 0009635 105
1459 255
0769 15
71358569 30276
Satellite: ISS
Catalog Number: 25544
Epoch time: 09068
52029571 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 97
5097 deg
Eccentricity:
0009635
Arg of perigee: 105
1459 deg
Mean anomaly: 255
0769 deg
Mean motion: 15
71358569 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3027
Checksum: 333
Coasting Arc #5 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2009/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2132364
85 A = 6735858
24 meter
Y = -5658893
47 meter E =
0022944
Z = 2941539
97 I = 51
97787
XDOT = 4069
081191 Wp = 101
95454
YDOT = -4169
276524 meter/sec RA = 91
70726 deg
ZDOT = -5042
870736 TA = 44
31693
MA = 44
13347
Ha = 197
618 n
mi
Hp = 184
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6995947
68 X = -2083216
89
Y = -18565923
45 feet Y = -5682463
70 meter
Z = 9650721
69 Z = 2931301
12
XDOT = 13350
003906 XDOT = 4139
897217
YDOT = -13678
728752 feet/sec YDOT = -4123
378270 meter/sec
ZDOT = -16544
851497 ZDOT = -5022
931057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2877981
32 X = -877208
71
Y = -19650262
12 feet Y = -5989399
89 meter
Z = 9610288
69 Z = 2929215
99
XDOT = 14648
064348 XDOT = 4464
730013
YDOT = -10244
398077 feet/sec YDOT = -3122
492534 meter/sec
ZDOT = -16467
320821 ZDOT = -5019
239386
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 09069
53782579
00010596 00000-0 82463-4 0 9044
2 25544 51
6392 92
3039 0009688 107
9139 252
3080 15
71402675 30433
Satellite: ISS
Catalog Number: 25544
Epoch time: 09069
53782579 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 92
3039 deg
Eccentricity:
0009688
Arg of perigee: 107
9139 deg
Mean anomaly: 252
3080 deg
Mean motion: 15
71402675 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3043
Checksum: 327
Coasting Arc #6 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2743484
97 A = 6733196
48 meter
Y = 4778198
72 meter E =
0020933
Z = 3857001
57 I = 51
96797
XDOT = -3568
450849 Wp = 104
44982
YDOT = -5418
985306 meter/sec RA = 86
66390 deg
ZDOT = 4151
257849 TA = 302
27504
MA = 302
47768
Ha = 197
620 n
mi
Hp = 184
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9000934
96 X = -2815448
07
Y = 15676504
99 feet Y = 4747117
55 meter
Z = 12654204
62 Z = 3843498
55
XDOT = -11707
515910 XDOT = -3527
755446
YDOT = -17778
823181 feet/sec YDOT = -5458
661787 meter/sec
ZDOT = 13619
612366 ZDOT = 4134
022007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12012339
06 X = -3661360
94
Y = 13557120
92 feet Y = 4132210
46 meter
Z = 12601853
68 Z = 3841045
00
XDOT = -7023
333817 XDOT = -2140
712148
YDOT = -18892
753153 feet/sec YDOT = -5758
511161 meter/sec
ZDOT = 13551
880296 ZDOT = 4130
613114
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 09070
55534353
00010596 00000-0 82463-4 0 9054
2 25544 51
6387 87
0981 0009690 111
5647 248
6548 15
71395682 30595
Satellite: ISS
Catalog Number: 25544
Epoch time: 09070
55534353 = yrday
fracday
Element set: 905
Inclination: 51
6387 deg
RA of node: 87
0981 deg
Eccentricity:
0009690
Arg of perigee: 111
5647 deg
Mean anomaly: 248
6548 deg
Mean motion: 15
71395682 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3059
Checksum: 339
Coasting Arc #7 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2009/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3859810
67 A = 6732017
41 meter
Y = 3593967
98 meter E =
0017527
Z = -4202243
69 I = 51
96188
XDOT = -1968
761942 Wp = 112
66244
YDOT = 6436
474196 meter/sec RA = 81
52037 deg
ZDOT = 3702
077400 TA = 195
03821
MA = 195
09039
Ha = 197
469 n
mi
Hp = 184
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12663420
83 X = 3839749
05
Y = 11791233
53 feet Y = 3637017
99 meter
Z = -13786888
75 Z = -4183542
00
XDOT = -6459
192722 XDOT = -2058
573244
YDOT = 21117
041325 feet/sec YDOT = 6413
956604 meter/sec
ZDOT = 12145
923228 ZDOT = 3692
294356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10382186
14 X = 3164490
34
Y = 13914797
92 feet Y = 4241230
41 meter
Z = -13713581
82 Z = -4179899
74
XDOT = -9251
503376 XDOT = -2819
858229
YDOT = 18817
658759 feet/sec YDOT = 5735
622390 meter/sec
ZDOT = 12108
221840 ZDOT = 3690
586017
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 09071
50925284
00010596 00000-0 82463-4 0 9068
2 25544 51
6395 82
2181 0009548 115
0365 245
1789 15
71406706 30747
Satellite: ISS
Catalog Number: 25544
Epoch time: 09071
50925284 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 82
2181 deg
Eccentricity:
0009548
Arg of perigee: 115
0365 deg
Mean anomaly: 245
1789 deg
Mean motion: 15
71406706 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3074
Checksum: 315
Coasting Arc #8 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 570890
63 A = 6736647
13 meter
Y = -6202460
96 meter E =
0014721
Z = -2564716
28 I = 51
97111
XDOT = 4904
453369 Wp = 122
34266
YDOT = 2634
426774 meter/sec RA = 76
47273 deg
ZDOT = -5309
032792 TA = 86
56265
MA = 86
39427
Ha = 197
428 n
mi
Hp = 184
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1873000
77 X = 652664
05
Y = -20349281
35 feet Y = -6195619
96 meter
Z = -8414423
49 Z = -2561743
67
XDOT = 16090
726275 XDOT = 4900
420509
YDOT = 8643
132461 feet/sec YDOT = 2689
248159 meter/sec
ZDOT = -17418
086587 ZDOT = -5285
217085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5256749
12 X = 1602257
13
Y = -19752347
74 feet Y = -6020515
59 meter
Z = -8403288
26 Z = -2561322
26
XDOT = 13100
544352 XDOT = 3993
045919
YDOT = 10815
562326 feet/sec YDOT = 3296
583397 meter/sec
ZDOT = -17324
889268 ZDOT = -5280
626249
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 09072
52674393
00010596 00000-0 82463-4 0 9074
2 25544 51
6384 77
0113 0009610 119
2088 241
0036 15
71431089 30900
Satellite: ISS
Catalog Number: 25544
Epoch time: 09072
52674393 = yrday
fracday
Element set: 907
Inclination: 51
6384 deg
RA of node: 77
0113 deg
Eccentricity:
0009610
Arg of perigee: 119
2088 deg
Mean anomaly: 241
0036 deg
Mean motion: 15
71431089 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3090
Checksum: 294
Coasting Arc #9 (Orbit 3105)
---------------------------------------
Vector Time (GMT): 2009/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4421072
99 A = 6728695
36 meter
Y = -904336
92 meter E =
0013125
Z = 4979515
93 I = 51
93633
XDOT = -800
497243 Wp = 97
45725
YDOT = -7385
873399 meter/sec RA = 71
34032 deg
ZDOT = -2049
178456 TA = 12
29714
MA = 12
26514
Ha = 197
411 n
mi
Hp = 184
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14504832
66 X = -4434821
54
Y = -2966984
65 feet Y = -953852
42 meter
Z = 16336994
52 Z = 4958005
05
XDOT = -2626
303291 XDOT = -707
893148
YDOT = -24231
868106 feet/sec YDOT = -7394
307409 meter/sec
ZDOT = -6723
026430 ZDOT = -2052
841757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13998082
90 X = -4266615
67
Y = -5097694
49 feet Y = -1553777
28 meter
Z = 16252930
33 Z = 4953893
16
XDOT = 660
674875 XDOT = 201
373702
YDOT = -23327
038003 feet/sec YDOT = -7110
081183 meter/sec
ZDOT = -6737
880778 ZDOT = -2053
706061
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 09073
54422037
00010596 00000-0 82463-4 0 9084
2 25544 51
6382 71
8055 0009471 122
7009 237
5067 15
71472865 31061
Satellite: ISS
Catalog Number: 25544
Epoch time: 09073
54422037 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 71
8055 deg
Eccentricity:
0009471
Arg of perigee: 122
7009 deg
Mean anomaly: 237
5067 deg
Mean motion: 15
71472865 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3106
Checksum: 305
Coasting Arc #10 (Orbit 3121)
---------------------------------------
Vector Time (GMT): 2009/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1962589
50 A = 6738766
18 meter
Y = 6368014
45 meter E =
0019034
Z = 978718
76 I = 51
96050
XDOT = -4841
821396 Wp = 84
01913
YDOT = 562
226454 meter/sec RA = 66
27224 deg
ZDOT = 5954
482672 TA = 286
61337
MA = 286
82229
Ha = 197
154 n
mi
Hp = 184
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6438941
94 X = 1886481
00
Y = 20892435
87 feet Y = 6389535
78 meter
Z = 3211019
54 Z = 988067
79
XDOT = -15885
240799 XDOT = -4876
674238
YDOT = 1844
574981 feet/sec YDOT = 507
887846 meter/sec
ZDOT = 19535
704305 ZDOT = 5930
876429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3624350
96 X = 1104702
17
Y = 21554098
00 feet Y = 6569689
07 meter
Z = 3247989
54 Z = 989987
21
XDOT = -14529
870275 XDOT = -4428
704460
YDOT = -533
916858 feet/sec YDOT = -162
737858 meter/sec
ZDOT = 19443
564825 ZDOT = 5926
398559
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 09074
56168157
00010596 00000-0 82463-4 0 9098
2 25544 51
6385 66
6004 0009581 127
5099 232
6935 15
71539241 31224
Satellite: ISS
Catalog Number: 25544
Epoch time: 09074
56168157 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 66
6004 deg
Eccentricity:
0009581
Arg of perigee: 127
5099 deg
Mean anomaly: 232
6935 deg
Mean motion: 15
71539241 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3122
Checksum: 322
Coasting Arc #11 (Orbit 3136)
---------------------------------------
Vector Time (GMT): 2009/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3758929
21 A = 6727297
85 meter
Y = -1791415
47 meter E =
0023184
Z = -5302979
05 I = 51
90818
XDOT = 3554
173989 Wp = 106
11518
YDOT = 6804
921461 meter/sec RA = 61
16418 deg
ZDOT = 215
020298 TA = 165
95574
MA = 165
89116
Ha = 197
149 n
mi
Hp = 184
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12332444
93 X = 3804442
61
Y = -5877347
35 feet Y = -1749126
65 meter
Z = -17398225
23 Z = -5284607
59
XDOT = 11660
675816 XDOT = 3476
771540
YDOT = 22325
857813 feet/sec YDOT = 6844
233533 meter/sec
ZDOT = 705
447171 ZDOT = 232
098182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13022200
53 X = 3969166
72
Y = -4420572
57 feet Y = -1347390
52 meter
Z = -17326611
98 Z = -5281151
33
XDOT = 8710
604689 XDOT = 2654
992309
YDOT = 22560
439586 feet/sec YDOT = 6876
421986 meter/sec
ZDOT = 772
620075 ZDOT = 235
494599
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 09075
51554239
00010596 00000-0 82463-4 0 9106
2 25544 51
6384 61
7191 0009437 129
7802 230
4192 15
71488576 31373
Satellite: ISS
Catalog Number: 25544
Epoch time: 09075
51554239 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 61
7191 deg
Eccentricity:
0009437
Arg of perigee: 129
7802 deg
Mean anomaly: 230
4192 deg
Mean motion: 15
71488576 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3137
Checksum: 319
Coasting Arc #12 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2009/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4124944
29 A = 6739044
82 meter
Y = -5280467
55 meter E =
0022529
Z = 605635
28 I = 51
93320
XDOT = 3415
840567 Wp = 130
30286
YDOT = -3374
361461 meter/sec RA = 56
06325 deg
ZDOT = -6024
015034 TA = 43
13167
MA = 42
95538
Ha = 196
989 n
mi
Hp = 184
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13533281
79 X = -4068532
70
Y = -17324368
62 feet Y = -5326279
66 meter
Z = 1986992
39 Z = 585733
55
XDOT = 11206
826008 XDOT = 3482
582813
YDOT = -11070
739701 feet/sec YDOT = -3335
790513 meter/sec
ZDOT = -19763
828852 ZDOT = -6007
258758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11800362
95 X = -3596750
63
Y = -18556376
72 feet Y = -5655983
62 meter
Z = 1908905
52 Z = 581834
40
XDOT = 10988
118962 XDOT = 3349
178660
YDOT = -9060
199585 feet/sec YDOT = -2761
548834 meter/sec
ZDOT = -19698
628832 ZDOT = -6004
142068
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 09076
53297728
00010596 00000-0 82463-4 0 9117
2 25544 51
6387 56
5128 0009318 133
0110 227
1834 15
71540785 31531
Satellite: ISS
Catalog Number: 25544
Epoch time: 09076
53297728 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 56
5128 deg
Eccentricity:
0009318
Arg of perigee: 133
0110 deg
Mean anomaly: 227
1834 deg
Mean motion: 15
71540785 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3153
Checksum: 308
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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