Date:
March 12th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11505 0 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 3050)
---------------------------------------
Vector Time (GMT): 2009/070/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3160306
02 A = 6732698
61 meter
Y = 4470912
55 meter E =
0016082
Z = -3935292
77 I = 51
96602
XDOT = -3076
826650 Wp = 108
80424
YDOT = 5746
813560 meter/sec RA = 88
95635 deg
ZDOT = 4066
507120 TA = 203
37932
MA = 203
45253
Ha = 197
323 n
mi
Hp = 184
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10368458
05 X = 3129193
29
Y = 14668348
27 feet Y = 4506078
53 meter
Z = -12911065
52 Z = -3920016
32
XDOT = -10094
575625 XDOT = -3160
613856
YDOT = 18854
375198 feet/sec YDOT = 5711
938670 meter/sec
ZDOT = 13341
558793 ZDOT = 4051
355968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10868812
70 X = -3312814
11
Y = -14355494
01 feet Y = -4375554
57 meter
Z = -12851057
50 Z = -3917002
32
XDOT = 8567
041803 XDOT = 2611
234342
YDOT = -18352
267650 feet/sec YDOT = -5593
771180 meter/sec
ZDOT = 13282
850648 ZDOT = 4048
612877
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
04629071
00010596 00000-0 82463-4 0 9005
2 25544 51
6369 89
6928 0009393 110
2960 249
9212 15
71488376 30515
Satellite: ISS
Catalog Number: 25544
Epoch time: 09070
04629071 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 89
6928 deg
Eccentricity:
0009393
Arg of perigee: 110
2960 deg
Mean anomaly: 249
9212 deg
Mean motion: 15
71488376 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3051
Checksum: 320
Coasting Arc #2 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2009/071/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1691330
00 A = 6735487
88 meter
Y = -5821096
97 meter E =
0013989
Z = -2940045
98 I = 51
97412
XDOT = 4376
542465 Wp = 113
19678
YDOT = 3809
121217 meter/sec RA = 83
91198 deg
ZDOT = -5048
352894 TA = 100
44396
MA = 100
28628
Ha = 197
265 n
mi
Hp = 184
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5548982
94 X = 1770578
85
Y = -19098087
18 feet Y = -5801740
77 meter
Z = -9645820
13 Z = -2931636
42
XDOT = 14358
735123 XDOT = 4358
146718
YDOT = 12497
116854 feet/sec YDOT = 3857
958832 meter/sec
ZDOT = -16562
837580 ZDOT = -5027
136976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4709857
51 X = -1435564
57
Y = 19338279
41 feet Y = 5894307
56 meter
Z = -9613437
64 Z = -2930175
79
XDOT = -13609
899461 XDOT = -4148
297356
YDOT = -11467
395139 feet/sec YDOT = -3495
262039 meter/sec
ZDOT = -16479
693470 ZDOT = -5023
010570
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
06373835
00010596 00000-0 82463-4 0 9013
2 25544 51
6370 84
4865 0009425 113
3238 246
8916 15
71530164 30675
Satellite: ISS
Catalog Number: 25544
Epoch time: 09071
06373835 = yrday
fracday
Element set: 901
Inclination: 51
6370 deg
RA of node: 84
4865 deg
Eccentricity:
0009425
Arg of perigee: 113
3238 deg
Mean anomaly: 246
8916 deg
Mean motion: 15
71530164 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3067
Checksum: 308
Coasting Arc #3 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2009/072/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4237029
32 A = 6729300
25 meter
Y = -2031353
84 meter E =
0014690
Z = 4804271
69 I = 51
94839
XDOT = 588
619430 Wp = 93
18591
YDOT = -7251
948286 meter/sec RA = 78
77366 deg
ZDOT = -2541
343636 TA = 21
60103
MA = 21
53913
Ha = 197
372 n
mi
Hp = 184
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13901014
82 X = -4237337
65
Y = -6664546
72 feet Y = -2078735
99 meter
Z = 15762046
24 Z = 4783687
77
XDOT = 1931
166110 XDOT = 682
013510
YDOT = -23792
481252 feet/sec YDOT = -7244
844075 meter/sec
ZDOT = -8337
741589 ZDOT = -2538
256519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14388021
63 X = 4385468
99
Y = 5759469
22 feet Y = 1755486
22 meter
Z = 15681512
85 Z = 4779725
12
XDOT = -39
504690 XDOT = -12
041030
YDOT = 22821
125626 feet/sec YDOT = 6955
879091 meter/sec
ZDOT = -8326
244526 ZDOT = -2537
839331
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
08116907
00010596 00000-0 82463-4 0 9022
2 25544 51
6366 79
2795 0009465 118
2263 241
9855 15
71519800 30830
Satellite: ISS
Catalog Number: 25544
Epoch time: 09072
08116907 = yrday
fracday
Element set: 902
Inclination: 51
6366 deg
RA of node: 79
2795 deg
Eccentricity:
0009465
Arg of perigee: 118
2263 deg
Mean anomaly: 241
9855 deg
Mean motion: 15
71519800 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3083
Checksum: 322
Coasting Arc #4 (Orbit 3098)
---------------------------------------
Vector Time (GMT): 2009/073/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 724707
21 A = 6738173
60 meter
Y = 6534364
33 meter E =
0020469
Z = 1453931
04 I = 51
97237
XDOT = -4970
267431 Wp = 85
22936
YDOT = -760
585634 meter/sec RA = 73
71182 deg
ZDOT = 5827
483359 TA = 290
68052
MA = 290
89985
Ha = 197
152 n
mi
Hp = 184
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2377648
34 X = 644522
08
Y = 21438203
17 feet Y = 6542020
21 meter
Z = 4770114
97 Z = 1457256
32
XDOT = -16306
651675 XDOT = -4989
701856
YDOT = -2495
359692 feet/sec YDOT = -816
274212 meter/sec
ZDOT = 19119
039891 ZDOT = 5803
290699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4075972
73 X = -1242356
49
Y = -21177994
82 feet Y = -6455052
82 meter
Z = 4783591
29 Z = 1458038
62
XDOT = 15020
546131 XDOT = 4578
262461
YDOT = 1456
684465 feet/sec YDOT = 443
997425 meter/sec
ZDOT = 19024
514009 ZDOT = 5798
671870
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
09858100
00010596 00000-0 82463-4 0 9033
2 25544 51
6372 74
0726 0009559 122
3132 237
8957 15
71573739 30994
Satellite: ISS
Catalog Number: 25544
Epoch time: 09073
09858100 = yrday
fracday
Element set: 903
Inclination: 51
6372 deg
RA of node: 74
0726 deg
Eccentricity:
0009559
Arg of perigee: 122
3132 deg
Mean anomaly: 237
8957 deg
Mean motion: 15
71573739 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3099
Checksum: 327
Coasting Arc #5 (Orbit 3113)
---------------------------------------
Vector Time (GMT): 2009/074/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4163887
73 A = 6727186
97 meter
Y = -669946
19 meter E =
0023608
Z = -5261068
69 I = 51
92702
XDOT = 2193
955010 Wp = 107
74036
YDOT = 7315
931919 meter/sec RA = 68
59616 deg
ZDOT = 800
712147 TA = 169
89431
MA = 169
84676
Ha = 197
117 n
mi
Hp = 184
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13661048
99 X = 4196627
03
Y = -2197986
17 feet Y = -623200
46 meter
Z = -17260724
04 Z = -5240760
96
XDOT = 7198
015124 XDOT = 2108
094266
YDOT = 24002
401308 feet/sec YDOT = 7339
985982 meter/sec
ZDOT = 2627
008356 ZDOT = 811
161337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13478913
14 X = -4108372
73
Y = 3536077
98 feet Y = 1077796
57 meter
Z = -17181474
04 Z = -5236913
29
XDOT = -9242
499502 XDOT = -2817
113848
YDOT = -22200
092553 feet/sec YDOT = -6766
588210 meter/sec
ZDOT = 2668
348750 ZDOT = 813
312699
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
05238891
00010596 00000-0 82463-4 0 9040
2 25544 51
6382 69
1919 0009687 125
6745 234
5320 15
71598254 31147
Satellite: ISS
Catalog Number: 25544
Epoch time: 09074
05238891 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 69
1919 deg
Eccentricity:
0009687
Arg of perigee: 125
6745 deg
Mean anomaly: 234
5320 deg
Mean motion: 15
71598254 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3114
Checksum: 327
Coasting Arc #6 (Orbit 3129)
---------------------------------------
Vector Time (GMT): 2009/075/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3043294
15 A = 6738867
58 meter
Y = -6001122
27 meter E =
0021799
Z = 59405
71 I = 51
95473
XDOT = 4203
836312 Wp = 131
78193
YDOT = -2205
769099 meter/sec RA = 63
50534 deg
ZDOT = -6065
176876 TA = 47
57575
MA = 47
39156
Ha = 196
922 n
mi
Hp = 184
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9984560
87 X = -2976251
00
Y = -19688721
36 feet Y = -6034779
30 meter
Z = 194900
63 Z = 44784
52
XDOT = 13792
113886 XDOT = 4257
652654
YDOT = -7236
775259 feet/sec YDOT = -2158
458721 meter/sec
ZDOT = -19898
874266 ZDOT = -6044
623845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12185383
93 X = 3714105
02
Y = 18408496
34 feet Y = 5610909
68 meter
Z = 137374
67 Z = 41871
80
XDOT = -11639
081554 XDOT = -3547
592058
YDOT = 7901
005055 feet/sec YDOT = 2408
226341 meter/sec
ZDOT = -19818
773874 ZDOT = -6040
762277
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
06976450
00010596 00000-0 82463-4 0 9053
2 25544 51
6379 63
9845 0009491 129
1148 231
0859 15
71653262 31300
Satellite: ISS
Catalog Number: 25544
Epoch time: 09075
06976450 = yrday
fracday
Element set: 905
Inclination: 51
6379 deg
RA of node: 63
9845 deg
Eccentricity:
0009491
Arg of perigee: 129
1148 deg
Mean anomaly: 231
0859 deg
Mean motion: 15
71653262 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3130
Checksum: 323
Coasting Arc #7 (Orbit 3145)
---------------------------------------
Vector Time (GMT): 2009/076/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2920869
92 A = 6727088
92 meter
Y = 3064466
29 meter E =
0013038
Z = 5220549
82 I = 51
90157
XDOT = -4630
291901 Wp = 129
95207
YDOT = -6080
759728 meter/sec RA = 58
41689 deg
ZDOT = 969
004462 TA = 310
79454
MA = 310
90757
Ha = 196
992 n
mi
Hp = 184
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9582906
58 X = -2980280
62
Y = 10054023
26 feet Y = 3031471
39 meter
Z = 17127788
11 Z = 5206215
88
XDOT = -15191
246394 XDOT = -4566
658931
YDOT = -19949
999107 feet/sec YDOT = -6132
182530 meter/sec
ZDOT = 3179
148496 ZDOT = 946
665317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8267898
74 X = 2520055
53
Y = -11245634
49 feet Y = -3427669
39 meter
Z = 17072028
67 Z = 5203554
34
XDOT = 16892
731924 XDOT = 5148
904691
YDOT = 17161
770462 feet/sec YDOT = 5230
907637 meter/sec
ZDOT = 3091
485126 ZDOT = 942
284666
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
08712379
00010596 00000-0 82463-4 0 9065
2 25544 51
6387 58
7783 0009596 133
3442 226
8521 15
71651474 31460
Satellite: ISS
Catalog Number: 25544
Epoch time: 09076
08712379 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 58
7783 deg
Eccentricity:
0009596
Arg of perigee: 133
3442 deg
Mean anomaly: 226
8521 deg
Mean motion: 15
71651474 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3146
Checksum: 335
Coasting Arc #8 (Orbit 3160)
---------------------------------------
Vector Time (GMT): 2009/077/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4844230
80 A = 6737701
19 meter
Y = 4407067
50 meter E =
0011568
Z = -1595153
14 I = 51
92235
XDOT = -2250
178397 Wp = 93
02182
YDOT = 4550
608510 meter/sec RA = 53
29593 deg
ZDOT = 5774
130611 TA = 249
48227
MA = 249
60645
Ha = 196
847 n
mi
Hp = 184
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15893145
68 X = 4802339
12
Y = 14458882
88 feet Y = 4461004
25 meter
Z = -5233442
06 Z = -1571721
86
XDOT = -7382
475056 XDOT = -2328
946336
YDOT = 14929
817947 feet/sec YDOT = 4525
005413 meter/sec
ZDOT = 18943
998066 ZDOT = 5763
007888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17902205
07 X = -5456592
11
Y = -11921197
25 feet Y = -3633580
92 meter
Z = -5141633
90 Z = -1567170
01
XDOT = 4311
058242 XDOT = 1314
010552
YDOT = -14575
235428 feet/sec YDOT = -4442
531759 meter/sec
ZDOT = 18900
876309 ZDOT = 5760
987099
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 09077
04087946
00010596 00000-0 82463-4 0 9078
2 25544 51
6401 53
8976 0009718 137
1322 223
0599 15
71683752 31617
Satellite: ISS
Catalog Number: 25544
Epoch time: 09077
04087946 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 53
8976 deg
Eccentricity:
0009718
Arg of perigee: 137
1322 deg
Mean anomaly: 223
0599 deg
Mean motion: 15
71683752 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3161
Checksum: 325
Coasting Arc #9 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2009/078/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 884712
38 A = 6728784
80 meter
Y = -4654408
83 meter E =
0017545
Z = -4791238
04 I = 51
87424
XDOT = 6142
755173 Wp = 102
39610
YDOT = 3823
879335 meter/sec RA = 48
23094 deg
ZDOT = -2592
021796 TA = 142
28034
MA = 142
15720
Ha = 196
711 n
mi
Hp = 184
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2902599
69 X = 959967
77
Y = -15270370
19 feet Y = -4644094
79 meter
Z = -15719284
90 Z = -4786757
25
XDOT = 20153
396236 XDOT = 6112
130833
YDOT = 12545
535877 feet/sec YDOT = 3892
399915 meter/sec
ZDOT = -8504
008518 ZDOT = -2562
255034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -413962
97 X = -126175
91
Y = 15555634
87 feet Y = 4741357
51 meter
Z = -15702103
89 Z = -4786001
27
XDOT = -20871
874860 XDOT = -6361
747457
YDOT = -8983
392243 feet/sec YDOT = -2738
137956 meter/sec
ZDOT = -8387
499191 ZDOT = -2556
509753
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 09078
05820014
00010596 00000-0 82463-4 0 9082
2 25544 51
6403 48
6913 0009630 141
0180 219
1678 15
71712415 31771
Satellite: ISS
Catalog Number: 25544
Epoch time: 09078
05820014 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 48
6913 deg
Eccentricity:
0009630
Arg of perigee: 141
0180 deg
Mean anomaly: 219
1678 deg
Mean motion: 15
71712415 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3177
Checksum: 293
Coasting Arc #10 (Orbit 3192)
---------------------------------------
Vector Time (GMT): 2009/079/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5659713
03 A = 6735069
07 meter
Y = -2168366
79 meter E =
0021327
Z = 2908260
06 I = 51
87471
XDOT = -387
545551 Wp = 117
54308
YDOT = -5800
442422 meter/sec RA = 43
08538 deg
ZDOT = -5060
500404 TA = 29
09420
MA = 28
97553
Ha = 196
735 n
mi
Hp = 184
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18568612
31 X = -5649172
99
Y = -7114064
26 feet Y = -2231597
98 meter
Z = 9541535
62 Z = 2880791
16
XDOT = -1271
474906 XDOT = -298
072522
YDOT = -19030
322906 feet/sec YDOT = -5804
276063 meter/sec
ZDOT = -16602
691613 ZDOT = -5062
165578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19611283
12 X = 5977519
10
Y = 3583194
72 feet Y = 1092157
75 meter
Z = 9434111
78 Z = 2875517
27
XDOT = 4901
914526 XDOT = 1494
103547
YDOT = 17063
310944 feet/sec YDOT = 5200
897176 meter/sec
ZDOT = -16609
587804 ZDOT = -5062
602363
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 09079
07550199
00010596 00000-0 82463-4 0 9090
2 25544 51
6403 43
4840 0009732 145
0819 215
0983 15
71725267 31930
Satellite: ISS
Catalog Number: 25544
Epoch time: 09079
07550199 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 43
4840 deg
Eccentricity:
0009732
Arg of perigee: 145
0819 deg
Mean anomaly: 215
0983 deg
Mean motion: 15
71725267 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3193
Checksum: 320
Coasting Arc #11 (Orbit 3208)
---------------------------------------
Vector Time (GMT): 2009/080/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1596774
35 A = 6731595
51 meter
Y = 5199511
59 meter E =
0018871
Z = 3960367
47 I = 51
84267
XDOT = -6485
866696 Wp = 123
22243
YDOT = -1077
357748 meter/sec RA = 38
03173 deg
ZDOT = 4005
672914 TA = 285
24486
MA = 285
45341
Ha = 196
400 n
mi
Hp = 184
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5238760
99 X = 1519275
38
Y = 17058765
07 feet Y = 5216934
50 meter
Z = 12993331
61 Z = 3967936
03
XDOT = -21279
090209 XDOT = -6492
796033
YDOT = -3534
638281 feet/sec YDOT = -1149
925062 meter/sec
ZDOT = 13141
971501 ZDOT = 3974
148215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8471200
88 X = -2582022
03
Y = -15681412
15 feet Y = -4779694
42 meter
Z = 13023241
43 Z = 3969483
99
XDOT = 20486
636936 XDOT = 6244
326938
YDOT = -190
356293 feet/sec YDOT = -58
020598 meter/sec
ZDOT = 13018
780630 ZDOT = 3968
124336
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 09080
09278167
00010596 00000-0 82463-4 0 9108
2 25544 51
6414 38
2773 0009667 149
3740 210
7989 15
71805694 32095
Satellite: ISS
Catalog Number: 25544
Epoch time: 09080
09278167 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 38
2773 deg
Eccentricity:
0009667
Arg of perigee: 149
3740 deg
Mean anomaly: 210
7989 deg
Mean motion: 15
71805694 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3209
Checksum: 333
Coasting Arc #12 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2009/081/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5415485
62 A = 6731636
43 meter
Y = -252513
36 meter E =
0015295
Z = -4007774
56 I = 51
81849
XDOT = 3193
550294 Wp = 133
54722
YDOT = 5763
829375 meter/sec RA = 32
87591 deg
ZDOT = 3951
187483 TA = 177
31799
MA = 177
30978
Ha = 196
326 n
mi
Hp = 185
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17767341
28 X = 5437375
55
Y = -828455
92 feet Y = -191832
09 meter
Z = -13148866
68 Z = -3981413
32
XDOT = 10477
527210 XDOT = 3109
666955
YDOT = 18910
201363 feet/sec YDOT = 5799
072734 meter/sec
ZDOT = 12963
213528 ZDOT = 3966
497439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17238870
62 X = -5254407
76
Y = 4677869
77 feet Y = 1425814
70 meter
Z = -13045931
34 Z = -3976399
87
XDOT = -13914
237601 XDOT = -4241
059621
YDOT = -14947
713718 feet/sec YDOT = -4556
063141 meter/sec
ZDOT = 13023
394968 ZDOT = 3969
530786
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 09081
04646600
00010596 00000-0 82463-4 0 9116
2 25544 51
6415 33
3963 0009541 152
7174 207
4490 15
71790041 32249
Satellite: ISS
Catalog Number: 25544
Epoch time: 09081
04646600 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 33
3963 deg
Eccentricity:
0009541
Arg of perigee: 152
7174 deg
Mean anomaly: 207
4490 deg
Mean motion: 15
71790041 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3224
Checksum: 285
Coasting Arc #13 (Orbit 3239)
---------------------------------------
Vector Time (GMT): 2009/082/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3902574
92 A = 6734622
09 meter
Y = -4648816
91 meter E =
0013335
Z = -2910996
78 I = 51
80419
XDOT = 5594
467830 Wp = 142
44687
YDOT = -1545
123913 meter/sec RA = 27
81797 deg
ZDOT = -5055
004906 TA = 70
93641
MA = 70
79203
Ha = 196
183 n
mi
Hp = 185
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12803723
50 X = -3836160
12
Y = -15252023
97 feet Y = -4692086
66 meter
Z = -9550514
38 Z = -2929793
56
XDOT = 18354
553249 XDOT = 5635
885848
YDOT = -5069
304176 feet/sec YDOT = -1482
332124 meter/sec
ZDOT = -16584
661765 ZDOT = -5027
726622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15958428
41 X = 4864128
98
Y = 11852194
39 feet Y = 3612548
85 meter
Z = -9624237
45 Z = -2933467
57
XDOT = -15891
199778 XDOT = -4843
637692
YDOT = 8075
357832 feet/sec YDOT = 2461
369067 meter/sec
ZDOT = -16478
234126 ZDOT = -5022
565762
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 09082
06370871
00010596 00000-0 82463-4 0 9124
2 25544 51
6420 28
1887 0009648 156
5251 203
6353 15
71829309 32402
Satellite: ISS
Catalog Number: 25544
Epoch time: 09082
06370871 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 28
1887 deg
Eccentricity:
0009648
Arg of perigee: 156
5251 deg
Mean anomaly: 203
6353 deg
Mean motion: 15
71829309 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3240
Checksum: 306
Coasting Arc #14 (Orbit 3255)
---------------------------------------
Vector Time (GMT): 2009/083/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4129501
68 A = 6728512
60 meter
Y = 2339701
35 meter E =
0011323
Z = 4758516
97 I = 51
75746
XDOT = -5614
169301 Wp = 117
59281
YDOT = -4581
859146 meter/sec RA = 22
66540 deg
ZDOT = -2619
624649 TA = 358
05426
MA = 358
05867
Ha = 196
179 n
mi
Hp = 185
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13548233
87 X = -4178473
47
Y = 7676185
53 feet Y = 2293249
49 meter
Z = 15611932
33 Z = 4738336
90
XDOT = -18419
190621 XDOT = -5549
791401
YDOT = -15032
346281 feet/sec YDOT = -4644
280353 meter/sec
ZDOT = -8594
569058 ZDOT = -2646
741183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11282899
60 X = 3439027
80
Y = -10845469
41 feet Y = -3305699
08 meter
Z = 15533282
53 Z = 4734544
52
XDOT = 20756
087650 XDOT = 6326
455516
YDOT = 9133
642678 feet/sec YDOT = 2783
934288 meter/sec
ZDOT = -8700
776399 ZDOT = -2651
996646
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 09083
08093145
00010596 00000-0 82463-4 0 9134
2 25544 51
6425 22
9820 0009559 159
5418 200
6128 15
71861615 32565
Satellite: ISS
Catalog Number: 25544
Epoch time: 09083
08093145 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 22
9820 deg
Eccentricity:
0009559
Arg of perigee: 159
5418 deg
Mean anomaly: 200
6128 deg
Mean motion: 15
71861615 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3256
Checksum: 309
Coasting Arc #15 (Orbit 3271)
---------------------------------------
Vector Time (GMT): 2009/084/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5712989
97 A = 6736946
36 meter
Y = 3167971
27 meter E =
0015671
Z = 1641143
35 I = 51
75907
XDOT = -3653
380523 Wp = 100
56680
YDOT = 3588
557870 meter/sec RA = 17
59009 deg
ZDOT = 5741
597653 TA = 277
50588
MA = 277
68388
Ha = 195
905 n
mi
Hp = 185
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18743405
40 X = 5669168
25
Y = 10393606
52 feet Y = 3231612
41 meter
Z = 5384328
57 Z = 1668790
09
XDOT = -11986
156571 XDOT = -3721
128319
YDOT = 11773
483824 feet/sec YDOT = 3547
325454 meter/sec
ZDOT = 18837
262640 ZDOT = 5723
684704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20807257
71 X = -6342052
15
Y = -5022320
70 feet Y = -1530803
35 meter
Z = 5492505
62 Z = 1674115
71
XDOT = 8147
435501 XDOT = 2483
338341
YDOT = -13057
404098 feet/sec YDOT = -3979
896769 meter/sec
ZDOT = 18767
554227 ZDOT = 5720
350529
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 09084
09813286
00010596 00000-0 82463-4 0 9143
2 25544 51
6429 17
7748 0009543 163
7246 196
4225 15
71900058 32722
Satellite: ISS
Catalog Number: 25544
Epoch time: 09084
09813286 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 17
7748 deg
Eccentricity:
0009543
Arg of perigee: 163
7246 deg
Mean anomaly: 196
4225 deg
Mean motion: 15
71900058 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3272
Checksum: 325
Coasting Arc #16 (Orbit 3286)
---------------------------------------
Vector Time (GMT): 2009/085/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2139731
70 A = 6726458
00 meter
Y = -3726408
28 meter E =
0019832
Z = -5190824
01 I = 51
69547
XDOT = 7171
396618 Wp = 125
03497
YDOT = 2510
486578 meter/sec RA = 12
45234 deg
ZDOT = 1145
842746 TA = 155
96578
MA = 155
87310
Ha = 195
731 n
mi
Hp = 185
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7020117
12 X = 2206458
05
Y = -12225748
95 feet Y = -3702108
04 meter
Z = -17030262
51 Z = -5180266
72
XDOT = 23528
204127 XDOT = 7137
224650
YDOT = 8236
504521 feet/sec YDOT = 2590
490378 meter/sec
ZDOT = 3759
326595 ZDOT = 1180
598070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3361200
26 X = -1024493
84
Y = 13742169
11 feet Y = 4188613
14 meter
Z = -16989289
10 Z = -5178335
32
XDOT = -23874
564252 XDOT = -7276
967184
YDOT = -991
062022 feet/sec YDOT = -302
075704 meter/sec
ZDOT = 3895
210436 ZDOT = 1187
260141
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 09085
05174132
00010596 00000-0 82463-4 0 9151
2 25544 51
6430 12
8937 0009456 167
5650 192
5747 15
71939214 32872
Satellite: ISS
Catalog Number: 25544
Epoch time: 09085
05174132 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 12
8937 deg
Eccentricity:
0009456
Arg of perigee: 167
5650 deg
Mean anomaly: 192
5747 deg
Mean motion: 15
71939214 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3287
Checksum: 323
Coasting Arc #17 (Orbit 3302)
---------------------------------------
Vector Time (GMT): 2009/086/00:54:28
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6620555
06 A = 6737979
35 meter
Y = -1134925
99 meter E =
0020080
Z = -352747
97 I = 51
70468
XDOT = 1112
274821 Wp = 152
75872
YDOT = -4660
320477 meter/sec RA = 7
35081 deg
ZDOT = -6033
698488 TA = 31
07266
MA = 30
95406
Ha = 195
609 n
mi
Hp = 185
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21720981
17 X = -6605658
48
Y = -3723510
48 feet Y = -1208877
65 meter
Z = -1157309
60 Z = -384874
46
XDOT = 3649
195607 XDOT = 1193
615389
YDOT = -15289
765344 feet/sec YDOT = -4647
428196 meter/sec
ZDOT = -19795
598714 ZDOT = -6028
096974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21831148
93 X = 6654134
19
Y = -2959764
85 feet Y = -902136
32 meter
Z = -1282827
83 Z = -391005
92
XDOT = 779
203420 XDOT = 237
501203
YDOT = 14122
900303 feet/sec YDOT = 4304
660012 meter/sec
ZDOT = -19774
038325 ZDOT = -6027
126882
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 09086
06890485
00010596 00000-0 82463-4 0 9160
2 25544 51
6424 7
6866 0009555 171
5790 188
5534 15
71942038 33034
Satellite: ISS
Catalog Number: 25544
Epoch time: 09086
06890485 = yrday
fracday
Element set: 916
Inclination: 51
6424 deg
RA of node: 7
6866 deg
Eccentricity:
0009555
Arg of perigee: 171
5790 deg
Mean anomaly: 188
5534 deg
Mean motion: 15
71942038 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3303
Checksum: 334
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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