Date:
May 6th 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 3907)
---------------------------------------
Vector Time (GMT): 2009/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6378125
61 A = 6734381
57 meter
Y = 547534
89 meter E =
0002422
Z = -2094187
56 I = 51
71108
XDOT = -2237
185169 Wp = 332
96413
YDOT = 4841
275683 meter/sec RA = 169
94011 deg
ZDOT = -5543
255008 TA = 230
37238
MA = 230
39376
Ha = 192
878 n
mi
Hp = 187
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20925608
96 X = 6381702
21
Y = 1796374
32 feet Y = 618878
82 meter
Z = -6870694
09 Z = -2063193
69
XDOT = -7339
846356 XDOT = -2264
226505
YDOT = 15883
450404 feet/sec YDOT = 4816
106988 meter/sec
ZDOT = -18186
532178 ZDOT = -5554
189015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16838688
34 X = 5132432
21
Y = -12618172
36 feet Y = -3846018
94 meter
Z = -6749430
32 Z = -2057226
36
XDOT = 4257
015708 XDOT = 1297
538388
YDOT = 15439
754255 feet/sec YDOT = 4706
037097 meter/sec
ZDOT = -18228
929095 ZDOT = -5556
177588
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 09124
52773644
00010596 00000-0 82463-4 0 9004
2 25544 51
6405 170
7979 0008952 323
1581 36
8966 15
72579841 39087
Satellite: ISS
Catalog Number: 25544
Epoch time: 09124
52773644 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 170
7979 deg
Eccentricity:
0008952
Arg of perigee: 323
1581 deg
Mean anomaly: 36
8966 deg
Mean motion: 15
72579841 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3908
Checksum: 341
Coasting Arc #2 (Orbit 3923)
---------------------------------------
Vector Time (GMT): 2009/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1025556
13 A = 6725241
16 meter
Y = -4375271
48 meter E =
0010729
Z = 5006703
37 I = 51
70872
XDOT = 7440
098035 Wp = 358
60909
YDOT = -457
688393 meter/sec RA = 164
78658 deg
ZDOT = -1913
535664 TA = 109
91808
MA = 109
80247
Ha = 192
978 n
mi
Hp = 186
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3364685
48 X = 1050082
95
Y = -14354565
22 feet Y = -4363666
01 meter
Z = 16426192
16 Z = 5011745
14
XDOT = 24409
770455 XDOT = 7453
958749
YDOT = -1501
602339 feet/sec YDOT = -374
411362 meter/sec
ZDOT = -6278
004146 ZDOT = -1877
357523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7338204
61 X = -2236684
76
Y = -12762758
30 feet Y = -3890088
73 meter
Z = 16445582
80 Z = 5012613
64
XDOT = 16007
493834 XDOT = 4879
084121
YDOT = -17155
182406 feet/sec YDOT = -5228
899597 meter/sec
ZDOT = -6136
531407 ZDOT = -1870
414773
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 09125
54448985
00010596 00000-0 82463-4 0 9015
2 25544 51
6395 165
5875 0009010 326
8429 33
2167 15
72605984 39249
Satellite: ISS
Catalog Number: 25544
Epoch time: 09125
54448985 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 165
5875 deg
Eccentricity:
0009010
Arg of perigee: 326
8429 deg
Mean anomaly: 33
2167 deg
Mean motion: 15
72605984 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3924
Checksum: 334
Coasting Arc #3 (Orbit 3939)
---------------------------------------
Vector Time (GMT): 2009/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6469347
30 A = 6735649
32 meter
Y = 1355723
28 meter E =
0017150
Z = 1235719
91 I = 51
77132
XDOT = 84
753276 Wp = 26
49992
YDOT = -4973
964302 meter/sec RA = 159
69572 deg
ZDOT = 5884
590096 TA = 347
02892
MA = 347
07298
Ha = 193
365 n
mi
Hp = 186
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21224892
73 X = -6490029
42
Y = 4447911
01 feet Y = 1283263
59 meter
Z = 4054199
17 Z = 1204241
05
XDOT = 278
061928 XDOT = 111
779900
YDOT = -16318
780519 feet/sec YDOT = -4972
865547 meter/sec
ZDOT = 19306
397953 ZDOT = 5885
067383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12284019
61 X = -3744169
18
Y = 17898751
69 feet Y = 5455539
52 meter
Z = 3931165
84 Z = 1198219
35
XDOT = -9851
835432 XDOT = -3002
839440
YDOT = -11014
009059 feet/sec YDOT = -3357
069961 meter/sec
ZDOT = 19307
895214 ZDOT = 5885
046461
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 09126
56123556
00010596 00000-0 82463-4 0 9023
2 25544 51
6394 160
3766 0009110 332
5081 27
5598 15
72564437 39408
Satellite: ISS
Catalog Number: 25544
Epoch time: 09126
56123556 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 160
3766 deg
Eccentricity:
0009110
Arg of perigee: 332
5081 deg
Mean anomaly: 27
5598 deg
Mean motion: 15
72564437 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3940
Checksum: 311
Coasting Arc #4 (Orbit 3954)
---------------------------------------
Vector Time (GMT): 2009/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 853709
81 A = 6724338
03 meter
Y = 4154531
90 meter E =
0012514
Z = -5226381
46 I = 51
76163
XDOT = -7175
493467 Wp = 59
15296
YDOT = 2615
115419 meter/sec RA = 154
56069 deg
ZDOT = 914
599970 TA = 219
50876
MA = 219
60005
Ha = 193
378 n
mi
Hp = 186
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2800885
20 X = 832579
03
Y = 13630354
00 feet Y = 4163960
65 meter
Z = -17146920
80 Z = -5222285
21
XDOT = -23541
645232 XDOT = -7208
645877
YDOT = 8579
774997 feet/sec YDOT = 2534
689461 meter/sec
ZDOT = 3000
656071 ZDOT = 879
660278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11648809
16 X = 3550557
03
Y = 7648294
33 feet Y = 2331200
11 meter
Z = -17130593
67 Z = -5221404
95
XDOT = -10152
636660 XDOT = -3094
523654
YDOT = 21820
145206 feet/sec YDOT = 6650
780259 meter/sec
ZDOT = 2864
165380 ZDOT = 872
997608
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 09127
51442051
00010596 00000-0 82463-4 0 9034
2 25544 51
6399 155
4916 0009059 334
9085 25
1629 15
72601246 39552
Satellite: ISS
Catalog Number: 25544
Epoch time: 09127
51442051 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 155
4916 deg
Eccentricity:
0009059
Arg of perigee: 334
9085 deg
Mean anomaly: 25
1629 deg
Mean motion: 15
72601246 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3955
Checksum: 316
Coasting Arc #5 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2009/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5937077
98 A = 6736008
27 meter
Y = -3160024
50 meter E =
0004619
Z = -375931
30 I = 51
82618
XDOT = 1942
741907 Wp = 91
08151
YDOT = 4360
089993 meter/sec RA = 149
45715 deg
ZDOT = -6032
176242 TA = 92
98933
MA = 92
93647
Ha = 193
467 n
mi
Hp = 186
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19478602
29 X = 5973798
89
Y = -10367534
45 feet Y = -3093427
29 meter
Z = -1233370
40 Z = -346999
35
XDOT = 6373
825153 XDOT = 1923
146118
YDOT = 14304
757194 feet/sec YDOT = 4381
705690 meter/sec
ZDOT = -19790
604467 ZDOT = -6022
785512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6194155
26 X = 1887978
52
Y = -21184901
46 feet Y = -6457157
96 meter
Z = -1120406
66 Z = -341499
95
XDOT = 13223
021203 XDOT = 4030
376863
YDOT = 4898
780051 feet/sec YDOT = 1493
148160 meter/sec
ZDOT = -19753
554680 ZDOT = -6020
883466
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 09128
53114224
00010596 00000-0 82463-4 0 9046
2 25544 51
6386 150
2803 0009019 339
6287 20
4515 15
72634258 39717
Satellite: ISS
Catalog Number: 25544
Epoch time: 09128
53114224 = yrday
fracday
Element set: 904
Inclination: 51
6386 deg
RA of node: 150
2803 deg
Eccentricity:
0009019
Arg of perigee: 339
6287 deg
Mean anomaly: 20
4515 deg
Mean motion: 15
72634258 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3971
Checksum: 303
Coasting Arc #6 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2009/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2477935
49 A = 6723934
28 meter
Y = -3338471
57 meter E =
0008512
Z = 5284515
25 I = 51
80975
XDOT = 6225
326538 Wp = 359
10661
YDOT = -4530
054483 meter/sec RA = 144
34124 deg
ZDOT = 65
581551 TA = 90
32121
MA = 90
22367
Ha = 193
646 n
mi
Hp = 185
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8129709
61 X = -2466091
73
Y = -10952990
72 feet Y = -3366115
53 meter
Z = 17337648
47 Z = 5272505
67
XDOT = 20424
299666 XDOT = 6275
201096
YDOT = -14862
383474 feet/sec YDOT = -4460
160392 meter/sec
ZDOT = 215
162569 ZDOT = 95
945582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13614628
08 X = -4149738
64
Y = -1528814
84 feet Y = -465982
76 meter
Z = 17290427
01 Z = 5270122
15
XDOT = 3090
819243 XDOT = 942
081705
YDOT = -24061
600316 feet/sec YDOT = -7333
975776 meter/sec
ZDOT = 333
650447 ZDOT = 101
696656
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 09129
54785248
00010596 00000-0 82463-4 0 9059
2 25544 51
6378 145
0687 0009082 343
7653 16
3217 15
72654861 39875
Satellite: ISS
Catalog Number: 25544
Epoch time: 09129
54785248 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 145
0687 deg
Eccentricity:
0009082
Arg of perigee: 343
7653 deg
Mean anomaly: 16
3217 deg
Mean motion: 15
72654861 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3987
Checksum: 344
Coasting Arc #7 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2009/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4815655
64 A = 6735739
35 meter
Y = 4667275
82 meter E =
0017938
Z = -496169
39 I = 51
87397
XDOT = -3636
687550 Wp = 17
39440
YDOT = -3118
414266 meter/sec RA = 139
22528 deg
ZDOT = 6035
155000 TA = 337
22363
MA = 337
30311
Ha = 193
610 n
mi
Hp = 185
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15799395
16 X = -4865077
65
Y = 15312584
71 feet Y = 4613148
07 meter
Z = -1627852
32 Z = -519683
84
XDOT = -11931
389600 XDOT = -3630
864870
YDOT = -10231
017932 feet/sec YDOT = -3159
049913 meter/sec
ZDOT = 19800
377298 ZDOT = 6017
501449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 682519
59 X = 208031
97
Y = 21984616
48 feet Y = 6700911
10 meter
Z = -1719548
22 Z = -524118
30
XDOT = -14072
360619 XDOT = -4289
255517
YDOT = 1962
578501 feet/sec YDOT = 598
193927 meter/sec
ZDOT = 19731
085855 ZDOT = 6014
034969
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 09130
50100822
00010596 00000-0 82463-4 0 9067
2 25544 51
6384 140
1841 0009010 347
0452 13
0477 15
72708326 40022
Satellite: ISS
Catalog Number: 25544
Epoch time: 09130
50100822 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 140
1841 deg
Eccentricity:
0009010
Arg of perigee: 347
0452 deg
Mean anomaly: 13
0477 deg
Mean motion: 15
72708326 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4002
Checksum: 259
Coasting Arc #8 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2009/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3751160
94 A = 6724270
95 meter
Y = 2016615
16 meter E =
0016969
Z = -5216302
43 I = 51
85580
XDOT = -4686
744298 Wp = 49
31658
YDOT = 6004
793791 meter/sec RA = 134
12907 deg
ZDOT = -1040
281438 TA = 210
72648
MA = 210
82594
Ha = 193
881 n
mi
Hp = 185
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12306958
45 X = 3753672
25
Y = 6616191
48 feet Y = 2058577
50 meter
Z = -17113853
12 Z = -5198072
67
XDOT = -15376
457671 XDOT = -4748
489005
YDOT = 19700
767032 feet/sec YDOT = 5952
038774 meter/sec
ZDOT = -3412
996843 ZDOT = -1063
199259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13163170
25 X = 4012134
29
Y = -4940398
02 feet Y = -1505833
32 meter
Z = -17042376
63 Z = -5194516
40
XDOT = 4280
375914 XDOT = 1304
658578
YDOT = 23584
020110 feet/sec YDOT = 7188
409329 meter/sec
ZDOT = -3502
286023 ZDOT = -1067
496780
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 09131
51769681
00010596 00000-0 82463-4 0 9074
2 25544 51
6376 134
9724 0009177 350
7949 9
3043 15
72673298 40183
Satellite: ISS
Catalog Number: 25544
Epoch time: 09131
51769681 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 134
9724 deg
Eccentricity:
0009177
Arg of perigee: 350
7949 deg
Mean anomaly: 9
3043 deg
Mean motion: 15
72673298 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4018
Checksum: 337
Coasting Arc #9 (Orbit 4033)
---------------------------------------
Vector Time (GMT): 2009/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3312719
73 A = 6735057
32 meter
Y = -5716445
78 meter E =
0011444
Z = 1305085
08 I = 51
91207
XDOT = 4771
181124 Wp = 78
93070
YDOT = 1415
073052 meter/sec RA = 128
99881 deg
ZDOT = -5867
200405 TA = 86
81563
MA = 86
68469
Ha = 193
967 n
mi
Hp = 185
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10868503
05 X = 3370055
84
Y = -18754743
38 feet Y = -5679080
60 meter
Z = 4281775
18 Z = 1321317
02
XDOT = 15653
481378 XDOT = 4783
505060
YDOT = 4642
628124 feet/sec YDOT = 1468
496821 meter/sec
ZDOT = -19249
345160 ZDOT = -5843
991622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7264599
67 X = -2214249
98
Y = -20409446
56 feet Y = -6220799
31 meter
Z = 4344932
59 Z = 1324335
45
XDOT = 12260
028433 XDOT = 3736
856666
YDOT = -8473
696719 feet/sec YDOT = -2582
782760 meter/sec
ZDOT = -19158
414437 ZDOT = -5839
484720
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 09132
53437367
00010596 00000-0 82463-4 0 9081
2 25544 51
6372 129
7606 0009349 355
0699 5
0369 15
72720324 40346
Satellite: ISS
Catalog Number: 25544
Epoch time: 09132
53437367 = yrday
fracday
Element set: 908
Inclination: 51
6372 deg
RA of node: 129
7606 deg
Eccentricity:
0009349
Arg of perigee: 355
0699 deg
Mean anomaly: 5
0369 deg
Mean motion: 15
72720324 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4034
Checksum: 317
Coasting Arc #10 (Orbit 4049)
---------------------------------------
Vector Time (GMT): 2009/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4464784
81 A = 6725038
90 meter
Y = -398187
55 meter E =
0007542
Z = 5007697
35 I = 51
89553
XDOT = 2799
908270 Wp = 36
80623
YDOT = -6906
277383 meter/sec RA = 123
91978 deg
ZDOT = 1951
607779 TA = 34
43729
MA = 34
38845
Ha = 194
202 n
mi
Hp = 184
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14648244
12 X = -4484327
06
Y = -1306389
59 feet Y = -448225
25 meter
Z = 16429453
25 Z = 4985959
73
XDOT = 9186
050755 XDOT = 2867
446696
YDOT = -22658
390363 feet/sec YDOT = -6874
589786 meter/sec
ZDOT = 6402
912661 ZDOT = 1965
373055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10364680
07 X = -3159154
49
Y = 10566014
48 feet Y = 3220521
21 meter
Z = 16344338
11 Z = 4981754
26
XDOT = -10936
534415 XDOT = -3333
455690
YDOT = -20692
847890 feet/sec YDOT = -6307
180037 meter/sec
ZDOT = 6456
350510 ZDOT = 1967
895635
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 09133
55103961
00010596 00000-0 82463-4 0 9095
2 25544 51
6369 124
5490 0009350 358
2263 1
8865 15
72712782 40502
Satellite: ISS
Catalog Number: 25544
Epoch time: 09133
55103961 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 124
5490 deg
Eccentricity:
0009350
Arg of perigee: 358
2263 deg
Mean anomaly: 1
8865 deg
Mean motion: 15
72712782 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4050
Checksum: 307
Coasting Arc #11 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2009/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1534122
17 A = 6733842
04 meter
Y = 6204048
40 meter E =
0014927
Z = -2097569
41 I = 51
94119
XDOT = -5288
333969 Wp = 18
38260
YDOT = 567
600335 meter/sec RA = 118
77968 deg
ZDOT = 5571
101684 TA = 318
28567
MA = 318
39939
Ha = 194
186 n
mi
Hp = 184
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5033209
22 X = -1593193
19
Y = 20354489
51 feet Y = 6186562
91 meter
Z = -6881789
39 Z = -2105165
00
XDOT = -17350
177064 XDOT = -5321
351483
YDOT = 1862
205823 feet/sec YDOT = 508
277859 meter/sec
ZDOT = 18277
892664 ZDOT = 5545
330675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12849922
96 X = 3916656
52
Y = 16556365
22 feet Y = 5046380
12 meter
Z = -6911129
73 Z = -2106512
34
XDOT = -8175
818925 XDOT = -2491
989608
YDOT = 13899
744299 feet/sec YDOT = 4236
642062 meter/sec
ZDOT = 18177
040866 ZDOT = 5540
362056
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 09134
50415261
00010596 00000-0 82463-4 0 9102
2 25544 51
6371 119
6641 0009356 2
6725 357
4486 15
72736809 40658
Satellite: ISS
Catalog Number: 25544
Epoch time: 09134
50415261 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 119
6641 deg
Eccentricity:
0009356
Arg of perigee: 2
6725 deg
Mean anomaly: 357
4486 deg
Mean motion: 15
72736809 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4065
Checksum: 310
Coasting Arc #12 (Orbit 4080)
---------------------------------------
Vector Time (GMT): 2009/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4625713
39 A = 6726295
68 meter
Y = -1374423
73 meter E =
0017178
Z = -4701246
82 I = 51
92906
XDOT = -734
463140 Wp = 41
15854
YDOT = 7120
737450 meter/sec RA = 113
71372 deg
ZDOT = -2797
558704 TA = 201
26610
MA = 201
33758
Ha = 194
285 n
mi
Hp = 184
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15176225
02 X = 4663576
53
Y = -4509264
20 feet Y = -1322484
13 meter
Z = -15424038
11 Z = -4678683
17
XDOT = -2409
655972 XDOT = -800
443748
YDOT = 23361
999507 feet/sec YDOT = 7112
155616 meter/sec
ZDOT = -9178
342205 ZDOT = -2801
286299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5693242
35 X = 1735300
27
Y = -14864484
51 feet Y = -4530694
88 meter
Z = -15335785
36 Z = -4674347
38
XDOT = 16039
670439 XDOT = 4888
891550
YDOT = 15650
698048 feet/sec YDOT = 4770
332765 meter/sec
ZDOT = -9192
487712 ZDOT = -2801
870255
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 09135
52079548
00010596 00000-0 82463-4 0 9110
2 25544 51
6372 114
4518 0009396 5
9720 354
1553 15
72745130 40814
Satellite: ISS
Catalog Number: 25544
Epoch time: 09135
52079548 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 114
4518 deg
Eccentricity:
0009396
Arg of perigee: 5
9720 deg
Mean anomaly: 354
1553 deg
Mean motion: 15
72745130 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4081
Checksum: 304
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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