Date:
February 21st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 2759)
---------------------------------------
Vector Time (GMT): 2009/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5631918
65 A = 6736670
35 meter
Y = -2074396
59 meter E =
0020197
Z = 3048374
97 I = 51
62417
XDOT = 4212
520104 Wp = 76
56076
YDOT = 4160
538190 meter/sec RA = 183
49657 deg
ZDOT = -4919
634967 TA = 68
15428
MA = 67
93958
Ha = 197
650 n
mi
Hp = 185
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18477423
40 X = 5639888
23
Y = -6805763
08 feet Y = -2011372
67 meter
Z = 10001230
23 Z = 3075753
50
XDOT = 13820
604017 XDOT = 4189
581303
YDOT = 13650
059680 feet/sec YDOT = 4207
516829 meter/sec
ZDOT = -16140
534668 ZDOT = -4899
226726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19342409
56 X = 5895566
43
Y = 3385457
37 feet Y = 1031887
41 meter
Z = 10107821
90 Z = 3080864
11
XDOT = 5403
791077 XDOT = 1647
075520
YDOT = 17386
169019 feet/sec YDOT = 5299
304317 meter/sec
ZDOT = -16060
591408 ZDOT = -4895
268261
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 09051
53818306
00010596 00000-0 82463-4 0 9009
2 25544 51
6391 184
3449 0008912 47
4699 312
7214 15
70982036 27605
Satellite: ISS
Catalog Number: 25544
Epoch time: 09051
53818306 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 184
3449 deg
Eccentricity:
0008912
Arg of perigee: 47
4699 deg
Mean anomaly: 312
7214 deg
Mean motion: 15
70982036 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2760
Checksum: 314
Coasting Arc #2 (Orbit 2775)
---------------------------------------
Vector Time (GMT): 2009/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925692
96 A = 6734889
01 meter
Y = -2756948
33 meter E =
0019385
Z = 3653385
26 I = 51
64938
XDOT = 5248
515735 Wp = 76
35543
YDOT = -3588
984827 meter/sec RA = 178
43419 deg
ZDOT = 4353
237666 TA = 327
49997
MA = 327
61918
Ha = 197
721 n
mi
Hp = 185
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16160409
98 X = -4912245
23
Y = -9045106
08 feet Y = -2811955
09 meter
Z = 11986172
11 Z = 3629489
57
XDOT = 17219
539814 XDOT = 5267
111610
YDOT = -11774
884602 feet/sec YDOT = -3530
188876 meter/sec
ZDOT = 14282
275807 ZDOT = 4378
779450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9748573
90 X = -2971365
33
Y = -15816739
34 feet Y = -4820942
15 meter
Z = 11892736
45 Z = 3624906
07
XDOT = 19550
812846 XDOT = 5959
087756
YDOT = -1199
756204 feet/sec YDOT = -365
685691 meter/sec
ZDOT = 14381
583812 ZDOT = 4383
506746
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 09052
55595205
00010596 00000-0 82463-4 0 9013
2 25544 51
6405 179
1416 0008892 50
8416 309
3534 15
71046754 27762
Satellite: ISS
Catalog Number: 25544
Epoch time: 09052
55595205 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 179
1416 deg
Eccentricity:
0008892
Arg of perigee: 50
8416 deg
Mean anomaly: 309
3534 deg
Mean motion: 15
71046754 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2776
Checksum: 315
Coasting Arc #3 (Orbit 2790)
---------------------------------------
Vector Time (GMT): 2009/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3266179
52 A = 6732123
82 meter
Y = 3903305
90 meter E =
0016214
Z = -4419322
14 I = 51
66995
XDOT = -6681
596809 Wp = 83
35554
YDOT = -1851
288396 meter/sec RA = 173
27451 deg
ZDOT = 3315
246817 TA = 219
94599
MA = 220
06539
Ha = 197
712 n
mi
Hp = 185
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10715812
08 X = -3288116
53
Y = 12806121
72 feet Y = 3866658
82 meter
Z = -14499088
39 Z = -4435242
17
XDOT = -21921
249372 XDOT = -6676
503221
YDOT = -6073
780827 feet/sec YDOT = -1925
977341 meter/sec
ZDOT = 10876
794019 ZDOT = 3282
800956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15425239
19 X = -4701612
91
Y = 6252415
87 feet Y = 1905736
36 meter
Z = -14560846
05 Z = -4438145
88
XDOT = -16038
620176 XDOT = -4888
571430
YDOT = -14626
435086 feet/sec YDOT = -4458
137414 meter/sec
ZDOT = 10750
074743 ZDOT = 3276
622782
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 09053
51010280
00010596 00000-0 82463-4 0 9026
2 25544 51
6408 174
2642 0008992 53
6863 306
5128 15
71030204 27918
Satellite: ISS
Catalog Number: 25544
Epoch time: 09053
51010280 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 174
2642 deg
Eccentricity:
0008992
Arg of perigee: 53
6863 deg
Mean anomaly: 306
5128 deg
Mean motion: 15
71030204 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2791
Checksum: 284
Coasting Arc #4 (Orbit 2806)
---------------------------------------
Vector Time (GMT): 2009/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6404125
93 A = 6738754
00 meter
Y = 339102
76 meter E =
0011939
Z = -2079244
56 I = 51
72204
XDOT = -2053
375002 Wp = 91
27363
YDOT = 4904
574546 meter/sec RA = 168
20707 deg
ZDOT = -5552
195366 TA = 111
85995
MA = 111
73293
Ha = 197
786 n
mi
Hp = 185
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21010911
83 X = 6409958
37
Y = 1112541
86 feet Y = 410749
94 meter
Z = -6821668
51 Z = -2048120
04
XDOT = -6736
794625 XDOT = -2081
095350
YDOT = 16091
123838 feet/sec YDOT = 4881
457269 meter/sec
ZDOT = -18215
864062 ZDOT = -5562
237934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18204502
04 X = 5548732
22
Y = 10627061
28 feet Y = 3239128
28 meter
Z = -6700223
91 Z = -2042228
25
XDOT = -12488
084488 XDOT = -3806
368152
YDOT = 9941
396591 feet/sec YDOT = 3030
137681 meter/sec
ZDOT = -18254
608733 ZDOT = -5564
004742
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
52785114
00010596 00000-0 82463-4 0 9034
2 25544 51
6414 169
0599 0009073 57
6129 302
5910 15
71055984 28073
Satellite: ISS
Catalog Number: 25544
Epoch time: 09054
52785114 = yrday
fracday
Element set: 903
Inclination: 51
6414 deg
RA of node: 169
0599 deg
Eccentricity:
0009073
Arg of perigee: 57
6129 deg
Mean anomaly: 302
5910 deg
Mean motion: 15
71055984 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2807
Checksum: 317
Coasting Arc #5 (Orbit 2822)
---------------------------------------
Vector Time (GMT): 2009/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 230226
92 A = 6728943
99 meter
Y = -4317003
11 meter E =
0013340
Z = 5147987
30 I = 51
71885
XDOT = 7495
612969 Wp = 59
00887
YDOT = -1189
628744 meter/sec RA = 163
07076 deg
ZDOT = -1323
555896 TA = 43
68603
MA = 43
58052
Ha = 197
768 n
mi
Hp = 185
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 755337
66 X = 253475
91
Y = -14163396
02 feet Y = -4314298
24 meter
Z = 16889722
11 Z = 5149162
47
XDOT = 24591
906065 XDOT = 7514
787938
YDOT = -3902
981443 feet/sec YDOT = -1105
701312 meter/sec
ZDOT = -4342
374987 ZDOT = -1287
096498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6857185
44 X = 2090070
12
Y = -12410049
96 feet Y = -3782583
23 meter
Z = 16893925
02 Z = 5149268
35
XDOT = 22897
457788 XDOT = 6979
145134
YDOT = 6892
828822 feet/sec YDOT = 2100
934225 meter/sec
ZDOT = -4200
243936 ZDOT = -1280
234352
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
54558748
00010596 00000-0 82463-4 0 9049
2 25544 51
6421 163
8565 0009149 60
4365 299
7708 15
71089164 28231
Satellite: ISS
Catalog Number: 25544
Epoch time: 09055
54558748 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 163
8565 deg
Eccentricity:
0009149
Arg of perigee: 60
4365 deg
Mean anomaly: 299
7708 deg
Mean motion: 15
71089164 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2823
Checksum: 340
Coasting Arc #6 (Orbit 2838)
---------------------------------------
Vector Time (GMT): 2009/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6292930
47 A = 6740517
59 meter
Y = 2382657
63 meter E =
0021549
Z = 191407
03 I = 51
78570
XDOT = -1514
239367 Wp = 54
38203
YDOT = -4522
030999 meter/sec RA = 157
97881 deg
ZDOT = 6045
635710 TA = 307
69191
MA = 307
88712
Ha = 197
852 n
mi
Hp = 185
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20646097
35 X = -6320035
84
Y = 7817118
22 feet Y = 2312134
88 meter
Z = 627975
82 Z = 160770
61
XDOT = -4967
976925 XDOT = -1492
928687
YDOT = -14836
059708 feet/sec YDOT = -4538
844447 meter/sec
ZDOT = 19834
762827 ZDOT = 6038
331837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22010119
61 X = -6708684
46
Y = -1748978
48 feet Y = -533088
64 meter
Z = 508660
79 Z = 155039
81
XDOT = 1611
817768 XDOT = 491
282056
YDOT = -13980
554253 feet/sec YDOT = -4261
272936 meter/sec
ZDOT = 19805
865767 ZDOT = 6036
827886
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
56331380
00010596 00000-0 82463-4 0 9054
2 25544 51
6425 158
6535 0009242 63
9825 296
2287 15
71072045 28398
Satellite: ISS
Catalog Number: 25544
Epoch time: 09056
56331380 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 158
6535 deg
Eccentricity:
0009242
Arg of perigee: 63
9825 deg
Mean anomaly: 296
2287 deg
Mean motion: 15
71072045 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2839
Checksum: 322
Coasting Arc #7 (Orbit 2853)
---------------------------------------
Vector Time (GMT): 2009/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2721233
88 A = 6728681
88 meter
Y = 3249341
87 meter E =
0023518
Z = -5246366
29 I = 51
77255
XDOT = -6466
095136 Wp = 77
45883
YDOT = 4055
271722 meter/sec RA = 152
88148 deg
ZDOT = -840
423332 TA = 184
52166
MA = 184
54295
Ha = 197
820 n
mi
Hp = 185
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8927932
67 X = 2710182
42
Y = 10660570
43 feet Y = 3279710
01 meter
Z = -17212487
82 Z = -5233173
90
XDOT = -21214
222888 XDOT = -6506
878730
YDOT = 13304
697252 feet/sec YDOT = 3982
735971 meter/sec
ZDOT = -2757
294395 ZDOT = -871
934520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3842230
36 X = 1171111
81
Y = 13430270
62 feet Y = 4093546
48 meter
Z = -17160727
77 Z = -5230589
82
XDOT = -23815
149363 XDOT = -7258
857526
YDOT = 3125
689616 feet/sec YDOT = 952
710195 meter/sec
ZDOT = -2879
880027 ZDOT = -877
787432
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
51742015
00010596 00000-0 82463-4 0 9062
2 25544 51
6422 153
7756 0009113 67
2984 292
9140 15
71087360 28540
Satellite: ISS
Catalog Number: 25544
Epoch time: 09057
51742015 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 153
7756 deg
Eccentricity:
0009113
Arg of perigee: 67
2984 deg
Mean anomaly: 292
9140 deg
Mean motion: 15
71087360 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2854
Checksum: 312
Coasting Arc #8 (Orbit 2869)
---------------------------------------
Vector Time (GMT): 2009/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4729044
01 A = 6739223
58 meter
Y = -4503890
39 meter E =
0021703
Z = 1636673
69 I = 51
83325
XDOT = 4437
297841 Wp = 98
90818
YDOT = 2546
550750 meter/sec RA = 147
75733 deg
ZDOT = -5752
271849 TA = 63
08081
MA = 62
85922
Ha = 197
871 n
mi
Hp = 184
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15515236
26 X = 4771105
22
Y = -14776543
28 feet Y = -4450772
14 meter
Z = 5369664
35 Z = 1659749
69
XDOT = 14558
063782 XDOT = 4436
435269
YDOT = 8354
825294 feet/sec YDOT = 2596
165845 meter/sec
ZDOT = -18872
282968 ZDOT = -5730
718042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20066876
37 X = 6116383
92
Y = -7444362
94 feet Y = -2269041
83 meter
Z = 5459305
44 Z = 1663996
30
XDOT = 9621
539587 XDOT = 2932
645266
YDOT = 12012
646336 feet/sec YDOT = 3661
454603 meter/sec
ZDOT = -18787
959502 ZDOT = -5726
570056
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
53512381
00010596 00000-0 82463-4 0 9077
2 25544 51
6414 148
5720 0009296 71
5314 288
6858 15
71108399 28703
Satellite: ISS
Catalog Number: 25544
Epoch time: 09058
53512381 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 148
5720 deg
Eccentricity:
0009296
Arg of perigee: 71
5314 deg
Mean anomaly: 288
6858 deg
Mean motion: 15
71108399 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2870
Checksum: 330
Coasting Arc #9 (Orbit 2885)
---------------------------------------
Vector Time (GMT): 2009/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760801
36 A = 6730997
16 meter
Y = -964073
49 meter E =
0016319
Z = 4646215
62 I = 51
83033
XDOT = 4018
697277 Wp = 94
30652
YDOT = -5909
948374 meter/sec RA = 142
69382 deg
ZDOT = 2881
682636 TA = 327
24065
MA = 327
34173
Ha = 197
920 n
mi
Hp = 184
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15619427
05 X = -4772237
42
Y = -3162970
78 feet Y = -1017375
11 meter
Z = 15243489
57 Z = 4623060
12
XDOT = 13184
702352 XDOT = 4070
486029
YDOT = -19389
594402 feet/sec YDOT = -5864
719161 meter/sec
ZDOT = 9454
339356 ZDOT = 2901
331598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13328983
44 X = -4062674
15
Y = -8891459
51 feet Y = -2710116
86 meter
Z = 15153052
76 Z = 4618650
48
XDOT = 18861
817751 XDOT = 5749
082050
YDOT = -11977
912510 feet/sec YDOT = -3650
867733 meter/sec
ZDOT = 9530
494091 ZDOT = 2904
894599
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
55281369
00010596 00000-0 82463-4 0 9080
2 25544 51
6415 143
3676 0009211 74
7264 285
4910 15
71159024 28865
Satellite: ISS
Catalog Number: 25544
Epoch time: 09059
55281369 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 143
3676 deg
Eccentricity:
0009211
Arg of perigee: 74
7264 deg
Mean anomaly: 285
4910 deg
Mean motion: 15
71159024 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2886
Checksum: 325
Coasting Arc #10 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2009/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2131655
31 A = 6735489
90 meter
Y = 5471058
71 meter E =
0013992
Z = -3309560
48 I = 51
86752
XDOT = -6040
924911 Wp = 81
08077
YDOT = 495
202995 meter/sec RA = 137
54891 deg
ZDOT = 4728
564326 TA = 240
29244
MA = 240
43178
Ha = 197
818 n
mi
Hp = 184
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6993619
79 X = -2176597
99
Y = 17949667
68 feet Y = 5446969
81 meter
Z = -10858138
05 Z = -3320025
52
XDOT = -19819
307451 XDOT = -6068
983794
YDOT = 1624
681741 feet/sec YDOT = 427
493261 meter/sec
ZDOT = 15513
662487 ZDOT = 4699
149455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12986424
48 X = -3958262
18
Y = 14197739
89 feet Y = 4327471
12 meter
Z = -10898504
98 Z = -3321864
32
XDOT = -18099
975500 XDOT = -5516
872532
YDOT = -4782
946752 feet/sec YDOT = -1457
842170 meter/sec
ZDOT = 15398
921422 ZDOT = 4693
591249
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
50689001
00010596 00000-0 82463-4 0 9093
2 25544 51
6407 138
4896 0009284 77
7078 282
5123 15
71159611 29015
Satellite: ISS
Catalog Number: 25544
Epoch time: 09060
50689001 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 138
4896 deg
Eccentricity:
0009284
Arg of perigee: 77
7078 deg
Mean anomaly: 282
5123 deg
Mean motion: 15
71159611 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2901
Checksum: 318
Coasting Arc #11 (Orbit 2916)
---------------------------------------
Vector Time (GMT): 2009/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5442975
43 A = 6734999
23 meter
Y = -1847494
68 meter E =
0014476
Z = -3524119
42 I = 51
88574
XDOT = -829
448630 Wp = 83
06854
YDOT = 6157
096069 meter/sec RA = 132
50175 deg
ZDOT = -4522
991195 TA = 138
56292
MA = 138
45305
Ha = 197
893 n
mi
Hp = 184
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17857530
93 X = 5480349
36
Y = -6061334
25 feet Y = -1786419
32 meter
Z = -11562071
59 Z = -3497586
70
XDOT = -2721
288157 XDOT = -876
264862
YDOT = 20200
446422 feet/sec YDOT = 6147
558761 meter/sec
ZDOT = -14839
209956 ZDOT = -4527
134585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18913188
01 X = 5764739
71
Y = 550077
94 feet Y = 167663
76 meter
Z = -11458683
03 Z = -3492606
59
XDOT = -9455
712186 XDOT = -2882
101074
YDOT = 16643
815419 feet/sec YDOT = 5073
034940 meter/sec
ZDOT = -14854
859757 ZDOT = -4527
761254
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
52455992
00010596 00000-0 82463-4 0 9108
2 25544 51
6399 133
2848 0009363 81
3539 278
8683 15
71157285 29177
Satellite: ISS
Catalog Number: 25544
Epoch time: 09061
52455992 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 133
2848 deg
Eccentricity:
0009363
Arg of perigee: 81
3539 deg
Mean anomaly: 278
8683 deg
Mean motion: 15
71157285 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2917
Checksum: 345
Coasting Arc #12 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2009/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -666598
93 A = 6731291
30 meter
Y = -4947178
78 meter E =
0017916
Z = 4503123
77 I = 51
89376
XDOT = 5962
015138 Wp = 75
83077
YDOT = -3706
637290 meter/sec RA = 127
35677 deg
ZDOT = -3174
829629 TA = 45
82136
MA = 45
67426
Ha = 197
775 n
mi
Hp = 184
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2187004
36 X = -633104
44
Y = -16230901
52 feet Y = -4954445
74 meter
Z = 14774028
11 Z = 4499966
87
XDOT = 19560
417118 XDOT = 6018
442921
YDOT = -12160
883498 feet/sec YDOT = -3639
651107 meter/sec
ZDOT = -10416
107706 ZDOT = -3145
729217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3237995
81 X = 986941
12
Y = -16066006
36 feet Y = -4896918
74 meter
Z = 14761296
75 Z = 4499243
25
XDOT = 21371
051327 XDOT = 6513
896444
YDOT = -5203
496976 feet/sec YDOT = -1586
025878 meter/sec
ZDOT = -10302
839632 ZDOT = -3140
305520
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
54221635
00010596 00000-0 82463-4 0 9117
2 25544 51
6406 128
0803 0009267 83
8774 276
3444 15
71223461 29336
Satellite: ISS
Catalog Number: 25544
Epoch time: 09062
54221635 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 128
0803 deg
Eccentricity:
0009267
Arg of perigee: 83
8774 deg
Mean anomaly: 276
3444 deg
Mean motion: 15
71223461 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2933
Checksum: 303
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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