Date:
February 25th 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 2808)
---------------------------------------
Vector Time (GMT): 2009/054/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6241150
55 A = 6738075
78 meter
Y = -607239
86 meter E =
0022679
Z = 2433782
19 I = 51
72211
XDOT = 2579
685749 Wp = 67
50781
YDOT = -4892
944506 meter/sec RA = 167
72203 deg
ZDOT = 5363
463220 TA = 319
93850
MA = 320
10555
Ha = 197
797 n
mi
Hp = 185
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20476215
73 X = -6245718
99
Y = -1992256
75 feet Y = -677057
46 meter
Z = 7984849
71 Z = 2403452
46
XDOT = 8463
535922 XDOT = 2608
153729
YDOT = -16052
967541 feet/sec YDOT = -4863
937534 meter/sec
ZDOT = 17596
664108 ZDOT = 5376
064361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20606628
25 X = -6280900
29
Y = 698334
21 feet Y = 212852
27 meter
Z = 7866481
05 Z = 2397703
42
XDOT = 6250
120425 XDOT = 1905
036706
YDOT = -15502
691209 feet/sec YDOT = -4725
220281 meter/sec
ZDOT = 17645
390690 ZDOT = 5378
315082
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 09054
65506418
00010596 00000-0 82463-4 0 9003
2 25544 51
6410 168
4135 0009038 56
5380 303
6644 15
71058027 28095
Satellite: ISS
Catalog Number: 25544
Epoch time: 09054
65506418 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 168
4135 deg
Eccentricity:
0009038
Arg of perigee: 56
5380 deg
Mean anomaly: 303
6644 deg
Mean motion: 15
71058027 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2809
Checksum: 298
Coasting Arc #2 (Orbit 2823)
---------------------------------------
Vector Time (GMT): 2009/055/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -698872
07 A = 6729466
23 meter
Y = 4403034
03 meter E =
0021012
Z = -5058469
16 I = 51
72142
XDOT = -7422
877601 Wp = 85
89857
YDOT = 857
241530 meter/sec RA = 162
58001 deg
ZDOT = 1779
506040 TA = 201
22243
MA = 201
30972
Ha = 197
783 n
mi
Hp = 185
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2292887
36 X = -723483
08
Y = 14445649
70 feet Y = 4395080
88 meter
Z = -16596027
43 Z = -5061924
27
XDOT = -24353
272968 XDOT = -7440
556035
YDOT = 2812
472210 feet/sec YDOT = 774
135868 meter/sec
ZDOT = 5838
274409 ZDOT = 1743
403626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -45029
80 X = -13725
08
Y = 14611552
04 feet Y = 4453601
06 meter
Z = -16609117
19 Z = -5062458
92
XDOT = -22640
716289 XDOT = -6900
890325
YDOT = 6377
568398 feet/sec YDOT = 1943
882848 meter/sec
ZDOT = 5697
505807 ZDOT = 1736
599770
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 09055
60918967
00010596 00000-0 82463-4 0 9016
2 25544 51
6405 163
5356 0009138 59
1530 301
0529 15
71069737 28248
Satellite: ISS
Catalog Number: 25544
Epoch time: 09055
60918967 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 163
5356 deg
Eccentricity:
0009138
Arg of perigee: 59
1530 deg
Mean anomaly: 301
0529 deg
Mean motion: 15
71069737 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2824
Checksum: 314
Coasting Arc #3 (Orbit 2839)
---------------------------------------
Vector Time (GMT): 2009/056/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6375018
09 A = 6740280
39 meter
Y = -2083779
49 meter E =
0015812
Z = -654138
10 I = 51
78578
XDOT = 940
752776 Wp = 105
20725
YDOT = 4722
155850 meter/sec RA = 157
49515 deg
ZDOT = -5998
333935 TA = 81
88958
MA = 81
71023
Ha = 197
842 n
mi
Hp = 185
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20915413
69 X = 6401023
08
Y = -6836546
88 feet Y = -2012344
98 meter
Z = -2146122
37 Z = -623105
59
XDOT = 3086
459240 XDOT = 917
017124
YDOT = 15492
637302 feet/sec YDOT = 4732
542674 meter/sec
ZDOT = -19679
573276 ZDOT = -5993
821909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19519771
75 X = 5949626
43
Y = -10182125
46 feet Y = -3103511
84 meter
Z = -2025234
91 Z = -617291
60
XDOT = 4959
562376 XDOT = 1511
674612
YDOT = 13332
735070 feet/sec YDOT = 4063
817649 meter/sec
ZDOT = -19661
550569 ZDOT = -5992
840613
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 09056
62691109
00010596 00000-0 82463-4 0 9026
2 25544 51
6405 158
3315 0009258 63
0364 297
1743 15
71096645 28406
Satellite: ISS
Catalog Number: 25544
Epoch time: 09056
62691109 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 158
3315 deg
Eccentricity:
0009258
Arg of perigee: 63
0364 deg
Mean anomaly: 297
1743 deg
Mean motion: 15
71096645 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2840
Checksum: 312
Coasting Arc #4 (Orbit 2855)
---------------------------------------
Vector Time (GMT): 2009/057/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2266543
56 A = 6728318
23 meter
Y = -3500041
22 meter E =
0011222
Z = 5270977
74 I = 51
77279
XDOT = 6688
971213 Wp = 75
30833
YDOT = -3808
995745 meter/sec RA = 152
38881 deg
ZDOT = 349
209218 TA = 11
39705
MA = 11
37166
Ha = 197
827 n
mi
Hp = 185
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7436166
52 X = -2252842
10
Y = -11483074
87 feet Y = -3525309
93 meter
Z = 17293234
05 Z = 5260000
66
XDOT = 21945
443611 XDOT = 6729
370531
YDOT = -12496
705199 feet/sec YDOT = -3733
969857 meter/sec
ZDOT = 1145
699534 ZDOT = 381
802182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9492357
44 X = -2893270
55
Y = -9926877
54 feet Y = -3025712
27 meter
Z = 17250095
00 Z = 5257828
96
XDOT = 18586
229787 XDOT = 5665
082839
YDOT = -15573
817572 feet/sec YDOT = -4746
899596 meter/sec
ZDOT = 1272
528362 ZDOT = 387
866645
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 09057
64461761
00010596 00000-0 82463-4 0 9039
2 25544 51
6406 153
1277 0009146 66
3212 293
8909 15
71133300 28565
Satellite: ISS
Catalog Number: 25544
Epoch time: 09057
64461761 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 153
1277 deg
Eccentricity:
0009146
Arg of perigee: 66
3212 deg
Mean anomaly: 293
8909 deg
Mean motion: 15
71133300 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2856
Checksum: 304
Coasting Arc #5 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2009/058/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4972351
72 A = 6739723
06 meter
Y = 4366560
84 meter E =
0017678
Z = -1253363
17 I = 51
83578
XDOT = -4020
906838 Wp = 53
75791
YDOT = -2910
037931 meter/sec RA = 147
27189 deg
ZDOT = 5881
032276 TA = 292
55102
MA = 292
73801
Ha = 197
870 n
mi
Hp = 184
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16313489
90 X = -5014721
23
Y = 14325986
99 feet Y = 4310720
09 meter
Z = -4112083
90 Z = -1277621
90
XDOT = -13191
951568 XDOT = -4016
636140
YDOT = -9547
368541 feet/sec YDOT = -2954
977636 meter/sec
ZDOT = 19294
725316 ZDOT = 5861
509574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13128014
52 X = -4001418
83
Y = 17269479
51 feet Y = 5263737
36 meter
Z = -4206352
59 Z = -1282096
27
XDOT = -13671
768536 XDOT = -4167
155050
YDOT = -5764
764972 feet/sec YDOT = -1757
100364 meter/sec
ZDOT = 19218
294670 ZDOT = 5857
736215
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 09058
59870779
00010596 00000-0 82463-4 0 9048
2 25544 51
6399 148
2491 0009353 68
7561 291
4599 15
71100331 28716
Satellite: ISS
Catalog Number: 25544
Epoch time: 09058
59870779 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 148
2491 deg
Eccentricity:
0009353
Arg of perigee: 68
7561 deg
Mean anomaly: 291
4599 deg
Mean motion: 15
71100331 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2871
Checksum: 344
Coasting Arc #6 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2009/059/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4471131
59 A = 6730256
82 meter
Y = 1367822
92 meter E =
0021308
Z = -4860690
18 I = 51
82840
XDOT = -4399
367483 Wp = 73
17296
YDOT = 5813
389532 meter/sec RA = 142
20201 deg
ZDOT = -2413
527575 TA = 173
27785
MA = 173
24922
Ha = 197
888 n
mi
Hp = 184
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14669066
91 X = 4479116
26
Y = 4487608
00 feet Y = 1417865
97 meter
Z = -15947146
27 Z = -4838950
29
XDOT = -14433
620351 XDOT = -4452
322398
YDOT = 19072
800301 feet/sec YDOT = 5763
896965 meter/sec
ZDOT = -7918
397556 ZDOT = -2435
028643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15380493
63 X = 4687974
46
Y = 1209431
31 feet Y = 368634
66 meter
Z = -15862197
68 Z = -4834797
85
XDOT = -9863
055043 XDOT = -3006
259177
YDOT = 20598
155039 feet/sec YDOT = 6278
317656 meter/sec
ZDOT = -8001
788711 ZDOT = -2438
945199
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 09059
61639057
00010596 00000-0 82463-4 0 9055
2 25544 51
6401 143
0443 0009398 73
4256 286
7937 15
71135385 28870
Satellite: ISS
Catalog Number: 25544
Epoch time: 09059
61639057 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 143
0443 deg
Eccentricity:
0009398
Arg of perigee: 73
4256 deg
Mean anomaly: 286
7937 deg
Mean motion: 15
71135385 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2887
Checksum: 335
Coasting Arc #7 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2009/060/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2551767
98 A = 6736447
55 meter
Y = -5500659
17 meter E =
0022429
Z = 2915734
32 I = 51
87198
XDOT = 5814
938996 Wp = 89
00987
YDOT = 3
020234 meter/sec RA = 137
06024 deg
ZDOT = -5049
771410 TA = 57
56167
MA = 57
34495
Ha = 197
821 n
mi
Hp = 184
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8371942
18 X = 2598923
55
Y = -18046782
05 feet Y = -5471859
98 meter
Z = 9566057
48 Z = 2928245
62
XDOT = 19077
883845 XDOT = 5839
003823
YDOT = 9
908904 feet/sec YDOT = 68
180521 meter/sec
ZDOT = -16567
491503 ZDOT = -5021
464101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3908104
29 X = 1191190
19
Y = -19482687
06 feet Y = -5938323
01 meter
Z = 9614407
94 Z = 2930471
54
XDOT = 17232
897430 XDOT = 5252
587137
YDOT = -4718
608320 feet/sec YDOT = -1438
231816 meter/sec
ZDOT = -16457
028876 ZDOT = -5016
102401
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 09060
63405866
00010596 00000-0 82463-4 0 9069
2 25544 51
6395 137
8398 0009485 76
1120 284
1097 15
71196467 29035
Satellite: ISS
Catalog Number: 25544
Epoch time: 09060
63405866 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 137
8398 deg
Eccentricity:
0009485
Arg of perigee: 76
1120 deg
Mean anomaly: 284
1097 deg
Mean motion: 15
71196467 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2903
Checksum: 334
Coasting Arc #8 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2009/061/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5339030
18 A = 6733964
80 meter
Y = 1446112
66 meter E =
0020971
Z = 3822555
18 I = 51
88347
XDOT = 1292
580495 Wp = 89
84708
YDOT = -6339
889483 meter/sec RA = 132
01217 deg
ZDOT = 4184
253623 TA = 316
42325
MA = 316
58871
Ha = 198
067 n
mi
Hp = 184
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17516503
22 X = -5373373
26
Y = 4744464
10 feet Y = 1386216
63 meter
Z = 12541191
52 Z = 3796534
80
XDOT = 4240
749657 XDOT = 1343
051855
YDOT = -20800
162346 feet/sec YDOT = -6325
152751 meter/sec
ZDOT = 13727
866217 ZDOT = 4190
655769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15858505
00 X = -4833672
32
Y = 8965451
13 feet Y = 2732669
51 meter
Z = 12439767
47 Z = 3791641
13
XDOT = -482
749843 XDOT = -147
142152
YDOT = -20025
343685 feet/sec YDOT = -6103
724755 meter/sec
ZDOT = 13752
316562 ZDOT = 4191
706088
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 09061
65171601
00010596 00000-0 82463-4 0 9070
2 25544 51
6390 132
6353 0009710 80
1611 280
0647 15
71182361 29196
Satellite: ISS
Catalog Number: 25544
Epoch time: 09061
65171601 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 132
6353 deg
Eccentricity:
0009710
Arg of perigee: 80
1611 deg
Mean anomaly: 280
0647 deg
Mean motion: 15
71182361 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2919
Checksum: 286
Coasting Arc #9 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2009/062/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 279304
30 A = 6732265
17 meter
Y = 5209830
63 meter E =
0017589
Z = -4270914
81 I = 51
89826
XDOT = -5961
032205 Wp = 96
07405
YDOT = 3255
003398 meter/sec RA = 126
86549 deg
ZDOT = 3591
535522 TA = 210
31987
MA = 210
42174
Ha = 197
900 n
mi
Hp = 184
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 916352
70 X = 241773
56
Y = 17092620
17 feet Y = 5212744
08 meter
Z = -14012187
70 Z = -4269649
18
XDOT = -19557
192273 XDOT = -6014
434080
YDOT = 10679
145007 feet/sec YDOT = 3188
045124 meter/sec
ZDOT = 11783
253026 ZDOT = 3562
447257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5492134
27 X = 1674002
53
Y = 16216791
33 feet Y = 4942878
00 meter
Z = -14006816
58 Z = -4269277
69
XDOT = -14909
798071 XDOT = -4544
506452
YDOT = 15098
560172 feet/sec YDOT = 4602
041140 meter/sec
ZDOT = 11669
993356 ZDOT = 3557
013975
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 09062
60575646
00010596 00000-0 82463-4 0 9084
2 25544 51
6403 127
7562 0009625 82
9553 277
2703 15
71204680 29345
Satellite: ISS
Catalog Number: 25544
Epoch time: 09062
60575646 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 127
7562 deg
Eccentricity:
0009625
Arg of perigee: 82
9553 deg
Mean anomaly: 277
2703 deg
Mean motion: 15
71204680 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2934
Checksum: 319
Coasting Arc #10 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2009/063/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4765326
26 A = 6737639
40 meter
Y = -4118919
29 meter E =
0014098
Z = -2397859
65 I = 51
93277
XDOT = 1769
524622 Wp = 104
25545
YDOT = 5175
884858 meter/sec RA = 121
81505 deg
ZDOT = -5403
989012 TA = 102
61069
MA = 102
45300
Ha = 197
902 n
mi
Hp = 184
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15634272
51 X = 4822678
78
Y = -13513514
72 feet Y = -4065309
95 meter
Z = -7866993
60 Z = -2374570
65
XDOT = 5805
526976 XDOT = 1737
766824
YDOT = 16981
249534 feet/sec YDOT = 5195
495161 meter/sec
ZDOT = -17729
622742 ZDOT = -5395
469876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11239393
93 X = 3425767
27
Y = -17382128
38 feet Y = -5298072
73 meter
Z = -7776424
79 Z = -2370254
28
XDOT = 9183
216243 XDOT = 2799
044311
YDOT = 13810
583447 feet/sec YDOT = 4209
465835 meter/sec
ZDOT = -17695
947312 ZDOT = -5393
724741
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 09063
62338757
00010596 00000-0 82463-4 0 9098
2 25544 51
6399 122
5510 0009630 87
0738 273
1526 15
71226811 29508
Satellite: ISS
Catalog Number: 25544
Epoch time: 09063
62338757 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 122
5510 deg
Eccentricity:
0009630
Arg of perigee: 87
0738 deg
Mean anomaly: 273
1526 deg
Mean motion: 15
71226811 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2950
Checksum: 316
Coasting Arc #11 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2009/064/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2659585
78 A = 6728908
06 meter
Y = -3535558
92 meter E =
0014319
Z = 5058777
69 I = 51
91745
XDOT = 4549
001365 Wp = 78
00900
YDOT = -5963
423353 meter/sec RA = 116
68567 deg
ZDOT = -1769
138925 TA = 28
98814
MA = 28
90870
Ha = 197
935 n
mi
Hp = 184
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8725675
15 X = -2644427
14
Y = -11599602
76 feet Y = -3565215
22 meter
Z = 16597039
66 Z = 5045894
44
XDOT = 14924
545161 XDOT = 4623
941284
YDOT = -19565
037247 feet/sec YDOT = -5912
134754 meter/sec
ZDOT = -5804
261566 ZDOT = -1746
858236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11877874
30 X = -3620376
09
Y = -8442786
82 feet Y = -2573361
42 meter
Z = 16546460
93 Z = 5043361
29
XDOT = 7830
479437 XDOT = 2386
730132
YDOT = -22268
071458 feet/sec YDOT = -6787
308180 meter/sec
ZDOT = -5717
764200 ZDOT = -1742
774528
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 09064
64100568
00010596 00000-0 82463-4 0 9100
2 25544 51
6391 117
3463 0009682 90
3217 269
9054 15
71263007 29669
Satellite: ISS
Catalog Number: 25544
Epoch time: 09064
64100568 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 117
3463 deg
Eccentricity:
0009682
Arg of perigee: 90
3217 deg
Mean anomaly: 269
9054 deg
Mean motion: 15
71263007 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2966
Checksum: 309
Coasting Arc #12 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2009/065/14:18:33
646
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2933145
20 A = 6739723
13 meter
Y = 6025740
71 meter E =
0021414
Z = 648617
34 I = 51
96673
XDOT = -4023
155877 Wp = 69
47247
YDOT = -2622
279397 meter/sec RA = 111
61358 deg
ZDOT = 6016
441401 TA = 297
55267
MA = 297
77007
Ha = 197
781 n
mi
Hp = 184
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9623179
79 X = -3003458
84
Y = 19769490
51 feet Y = 5992547
43 meter
Z = 2128009
65 Z = 634197
58
XDOT = -13199
330306 XDOT = -4022
760265
YDOT = -8603
278861 feet/sec YDOT = -2667
266402 meter/sec
ZDOT = 19738
980976 ZDOT = 5996
898313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2930137
01 X = -893105
76
Y = 21796492
15 feet Y = 6643570
81 meter
Z = 2072196
03 Z = 631605
35
XDOT = -13753
629793 XDOT = -4192
106361
YDOT = -3766
784212 feet/sec YDOT = -1148
115828 meter/sec
ZDOT = 19662
470608 ZDOT = 5993
121041
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
65861079
00010596 00000-0 82463-4 0 9114
2 25544 51
6396 112
1424 0009633 94
2894 265
9368 15
71292994 29823
Satellite: ISS
Catalog Number: 25544
Epoch time: 09065
65861079 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 112
1424 deg
Eccentricity:
0009633
Arg of perigee: 94
2894 deg
Mean anomaly: 265
9368 deg
Mean motion: 15
71292994 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2982
Checksum: 347
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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