Date:
May 3rd 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 3860)
---------------------------------------
Vector Time (GMT): 2009/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4470846
59 A = 6728794
91 meter
Y = -2874420
95 meter E =
0008931
Z = 4129404
60 I = 51
60351
XDOT = 5729
338134 Wp = 19
63214
YDOT = 3511
103214 meter/sec RA = 185
26453 deg
ZDOT = -3748
438609 TA = 108
84903
MA = 108
75216
Ha = 192
299 n
mi
Hp = 187
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14668131
86 X = 4482596
66
Y = -9430514
93 feet Y = -2824359
86 meter
Z = 13547915
34 Z = 4151152
36
XDOT = 18797
041122 XDOT = 5707
859812
YDOT = 11519
367500 feet/sec YDOT = 3575
052129 meter/sec
ZDOT = -12298
026932 ZDOT = -3720
657451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5464878
24 X = 1665694
89
Y = -16489945
35 feet Y = -5026135
34 meter
Z = 13632737
15 Z = 4155258
28
XDOT = 20720
676975 XDOT = 6315
662342
YDOT = -3238
734199 feet/sec YDOT = -987
166184 meter/sec
ZDOT = -12189
132824 ZDOT = -3715
247685
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 09121
54096204
00010596 00000-0 82463-4 0 9003
2 25544 51
6403 186
1014 0009090 309
3540 50
6817 15
72558114 38618
Satellite: ISS
Catalog Number: 25544
Epoch time: 09121
54096204 = yrday
fracday
Element set: 900
Inclination: 51
6403 deg
RA of node: 186
1014 deg
Eccentricity:
0009090
Arg of perigee: 309
3540 deg
Mean anomaly: 50
6817 deg
Mean motion: 15
72558114 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3861
Checksum: 281
Coasting Arc #2 (Orbit 3876)
---------------------------------------
Vector Time (GMT): 2009/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5610122
36 A = 6732763
41 meter
Y = -2313128
02 meter E =
0010714
Z = 2899946
94 I = 51
64560
XDOT = 4249
091445 Wp = 40
26316
YDOT = -3978
002774 meter/sec RA = 180
18793 deg
ZDOT = 5044
790884 TA = 353
09310
MA = 353
10785
Ha = 192
611 n
mi
Hp = 187
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18405913
27 X = -5597927
05
Y = -7589002
68 feet Y = -2375795
58 meter
Z = 9514261
62 Z = 2872722
50
XDOT = 13940
588729 XDOT = 4268
751640
YDOT = -13051
190205 feet/sec YDOT = -3930
377179 meter/sec
ZDOT = 16551
151195 ZDOT = 5065
480620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19043667
66 X = -5804509
90
Y = 5977218
18 feet Y = 1821856
10 meter
Z = 9407622
65 Z = 2867443
38
XDOT = 2727
485589 XDOT = 831
337607
YDOT = -17499
068162 feet/sec YDOT = -5333
715976 meter/sec
ZDOT = 16631
758772 ZDOT = 5069
360074
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 09122
55774369
00010596 00000-0 82463-4 0 9011
2 25544 51
6399 180
8909 0008917 314
2022 45
8407 15
72540059 38770
Satellite: ISS
Catalog Number: 25544
Epoch time: 09122
55774369 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 180
8909 deg
Eccentricity:
0008917
Arg of perigee: 314
2022 deg
Mean anomaly: 45
8407 deg
Mean motion: 15
72540059 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3877
Checksum: 331
Coasting Arc #3 (Orbit 3891)
---------------------------------------
Vector Time (GMT): 2009/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2857110
17 A = 6726824
87 meter
Y = 3938752
10 meter E =
0005338
Z = -4647011
90 I = 51
65574
XDOT = -6946
331111 Wp = 54
59269
YDOT = -1667
609624 meter/sec RA = 175
01923 deg
ZDOT = 2862
682081 TA = 243
69210
MA = 243
74695
Ha = 192
681 n
mi
Hp = 187
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9373721
01 X = -2878367
18
Y = 12922415
02 feet Y = 3906683
42 meter
Z = -15246102
04 Z = -4660943
38
XDOT = -22789
800234 XDOT = -6941
073792
YDOT = -5471
160184 feet/sec YDOT = -1745
258188 meter/sec
ZDOT = 9392
001578 ZDOT = 2828
949439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1403065
16 X = 427654
26
Y = 15850290
37 feet Y = 4831168
51 meter
Z = -15300287
13 Z = -4663527
52
XDOT = -19719
651060 XDOT = -6010
549643
YDOT = 10667
378915 feet/sec YDOT = 3251
417093 meter/sec
ZDOT = 9259
949456 ZDOT = 2822
432594
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 09123
51096402
00010596 00000-0 82463-4 0 9024
2 25544 51
6399 176
0062 0008992 318
6365 41
4116 15
72562887 38927
Satellite: ISS
Catalog Number: 25544
Epoch time: 09123
51096402 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 176
0062 deg
Eccentricity:
0008992
Arg of perigee: 318
6365 deg
Mean anomaly: 41
4116 deg
Mean motion: 15
72562887 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3892
Checksum: 321
Coasting Arc #4 (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 = 6375032
78 A = 6734323
82 meter
Y = 553942
50 meter E =
0002474
Z = -2101791
72 I = 51
71117
XDOT = -2248
463705 Wp = 333
03637
YDOT = 4840
364342 meter/sec RA = 169
93799 deg
ZDOT = -5539
496780 TA = 230
39003
MA = 230
41188
Ha = 192
862 n
mi
Hp = 187
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20915461
88 X = 6378574
90
Y = 1817396
67 feet Y = 625251
65 meter
Z = -6895642
12 Z = -2070812
95
XDOT = -7376
849426 XDOT = -2275
512269
YDOT = 15880
460441 feet/sec YDOT = 4815
069484 meter/sec
ZDOT = -18174
202034 ZDOT = -5550
485596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16845221
56 X = 5134423
53
Y = -12595827
53 feet Y = -3839208
23 meter
Z = -6774436
95 Z = -2064848
38
XDOT = 4228
992466 XDOT = 1288
996904
YDOT = 15461
730671 feet/sec YDOT = 4712
735508 meter/sec
ZDOT = -18216
813389 ZDOT = -5552
484721
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
52772018
00010596 00000-0 82463-4 0 9031
2 25544 51
6406 170
7957 0008979 323
1743 36
8802 15
72595317 39088
Satellite: ISS
Catalog Number: 25544
Epoch time: 09124
52772018 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 170
7957 deg
Eccentricity:
0008979
Arg of perigee: 323
1743 deg
Mean anomaly: 36
8802 deg
Mean motion: 15
72595317 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3908
Checksum: 329
Coasting Arc #5 (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 = 1042470
90 A = 6725208
66 meter
Y = -4376310
69 meter E =
0010767
Z = 5002272
07 I = 51
70892
XDOT = 7436
995803 Wp = 358
73381
YDOT = -444
862638 meter/sec RA = 164
78418 deg
ZDOT = -1928
580821 TA = 109
94402
MA = 109
82801
Ha = 192
958 n
mi
Hp = 186
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3420180
11 X = 1067029
61
Y = -14357974
72 feet Y = -4364515
89 meter
Z = 16411653
79 Z = 5007396
09
XDOT = 24399
592530 XDOT = 7450
786416
YDOT = -1459
523091 feet/sec YDOT = -361
620690 meter/sec
ZDOT = -6327
364898 ZDOT = -1892
417921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7299692
29 X = -2224946
21
Y = -12802974
34 feet Y = -3902346
58 meter
Z = 16431366
07 Z = 5008280
38
XDOT = 16025
846612 XDOT = 4884
678047
YDOT = -17120
369058 feet/sec YDOT = -5218
288489 meter/sec
ZDOT = -6185
950802 ZDOT = -1885
477805
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
54446276
00010596 00000-0 82463-4 0 9049
2 25544 51
6396 165
5852 0009036 326
8603 33
1992 15
72623966 39242
Satellite: ISS
Catalog Number: 25544
Epoch time: 09125
54446276 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 165
5852 deg
Eccentricity:
0009036
Arg of perigee: 326
8603 deg
Mean anomaly: 33
1992 deg
Mean motion: 15
72623966 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3924
Checksum: 331
Coasting Arc #6 (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 = -6468894
92 A = 6735570
89 meter
Y = 1339323
99 meter E =
0017148
Z = 1255372
62 I = 51
77137
XDOT = 112
942336 Wp = 26
63038
YDOT = -4979
898911 meter/sec RA = 159
69348 deg
ZDOT = 5879
158057 TA = 347
11797
MA = 347
16172
Ha = 193
342 n
mi
Hp = 186
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21223408
53 X = -6489489
16
Y = 4394107
57 feet Y = 1266869
86 meter
Z = 4118676
57 Z = 1223896
17
XDOT = 370
545721 XDOT = 140
059615
YDOT = -16338
251020 feet/sec YDOT = -4978
484422 meter/sec
ZDOT = 19288
576301 ZDOT = 5879
772509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12320397
95 X = -3755257
29
Y = 17859096
04 feet Y = 5443452
47 meter
Z = 3995651
45 Z = 1217874
56
XDOT = -9801
262878 XDOT = -2987
424925
YDOT = -11089
412334 feet/sec YDOT = -3380
052879 meter/sec
ZDOT = 19290
609663 ZDOT = 5879
777825
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
56119608
00010596 00000-0 82463-4 0 9059
2 25544 51
6394 160
3742 0009134 332
5306 27
5373 15
72584698 39400
Satellite: ISS
Catalog Number: 25544
Epoch time: 09126
56119608 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 160
3742 deg
Eccentricity:
0009134
Arg of perigee: 332
5306 deg
Mean anomaly: 27
5373 deg
Mean motion: 15
72584698 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3940
Checksum: 319
Coasting Arc #7 (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 = 821445
66 A = 6724291
41 meter
Y = 4166199
92 meter E =
0012461
Z = -5222134
47 I = 51
76182
XDOT = -7180
361794 Wp = 59
18168
YDOT = 2590
920598 meter/sec RA = 154
55787 deg
ZDOT = 945
461931 TA = 219
77607
MA = 219
86749
Ha = 193
351 n
mi
Hp = 186
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2695031
69 X = 800166
17
Y = 13668634
92 feet Y = 4175267
04 meter
Z = -17132987
10 Z = -5218195
32
XDOT = -23557
617433 XDOT = -7213
393217
YDOT = 8500
395664 feet/sec YDOT = 2510
440875 meter/sec
ZDOT = 3101
909221 ZDOT = 910
498880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11600439
64 X = 3535814
00
Y = 7750017
05 feet Y = 2362205
20 meter
Z = -17117273
71 Z = -5217345
03
XDOT = -10212
822809 XDOT = -3112
868392
YDOT = 21778
897849 feet/sec YDOT = 6638
208064 meter/sec
ZDOT = 2965
325387 ZDOT = 903
831178
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
51436794
00010596 00000-0 82463-4 0 9064
2 25544 51
6400 155
4891 0009083 334
9298 25
1414 15
72623854 39551
Satellite: ISS
Catalog Number: 25544
Epoch time: 09127
51436794 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 155
4891 deg
Eccentricity:
0009083
Arg of perigee: 334
9298 deg
Mean anomaly: 25
1414 deg
Mean motion: 15
72623854 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3955
Checksum: 325
Coasting Arc #8 (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 = 5948092
08 A = 6735926
22 meter
Y = -3134752
61 meter E =
0004518
Z = -411093
68 I = 51
82627
XDOT = 1897
666185 Wp = 90
55371
YDOT = 4383
983018 meter/sec RA = 149
45476 deg
ZDOT = -6029
201598 TA = 93
89865
MA = 93
84699
Ha = 193
435 n
mi
Hp = 186
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19514737
80 X = 5984700
39
Y = -10284621
42 feet Y = -3068032
86 meter
Z = -1348732
53 Z = -382108
49
XDOT = 6225
938926 XDOT = 1877
792119
YDOT = 14383
146386 feet/sec YDOT = 4405
093096 meter/sec
ZDOT = -19780
845138 ZDOT = -6020
030526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6279190
37 X = 1913897
23
Y = -21153313
49 feet Y = -6447529
95 meter
Z = -1235558
72 Z = -376598
30
XDOT = 13178
063968 XDOT = 4016
673897
YDOT = 5053
195616 feet/sec YDOT = 1540
214024 meter/sec
ZDOT = -19744
653001 ZDOT = -6018
170235
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
53107421
00010596 00000-0 82463-4 0 9070
2 25544 51
6387 150
2777 0009040 339
6397 20
4404 15
72659191 39714
Satellite: ISS
Catalog Number: 25544
Epoch time: 09128
53107421 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 150
2777 deg
Eccentricity:
0009040
Arg of perigee: 339
6397 deg
Mean anomaly: 20
4404 deg
Mean motion: 15
72659191 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3971
Checksum: 314
Coasting Arc #9 (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 = -2432632
80 A = 6723852
94 meter
Y = -3371188
12 meter E =
0008634
Z = 5284757
17 I = 51
80986
XDOT = 6248
529765 Wp = 359
07006
YDOT = -4498
424530 meter/sec RA = 144
33789 deg
ZDOT = 15
144993 TA = 90
83601
MA = 90
73708
Ha = 193
608 n
mi
Hp = 185
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7981078
75 X = -2420427
75
Y = -11060328
48 feet Y = -3398323
46 meter
Z = 17338442
16 Z = 5272968
54
XDOT = 20500
425738 XDOT = 6298
293923
YDOT = -14758
610663 feet/sec YDOT = -4428
271580 meter/sec
ZDOT = 49
688296 ZDOT = 45
621482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13590726
21 X = -4142453
35
Y = -1710581
49 feet Y = -521385
24 meter
Z = 17292082
95 Z = 5270626
88
XDOT = 3205
943478 XDOT = 977
171572
YDOT = -24048
210658 feet/sec YDOT = -7329
894609 meter/sec
ZDOT = 168
618388 ZDOT = 51
394885
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
54776738
00010596 00000-0 82463-4 0 9086
2 25544 51
6379 145
0661 0009101 343
7791 16
3079 15
72682549 39873
Satellite: ISS
Catalog Number: 25544
Epoch time: 09129
54776738 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 145
0661 deg
Eccentricity:
0009101
Arg of perigee: 343
7791 deg
Mean anomaly: 16
3079 deg
Mean motion: 15
72682549 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3987
Checksum: 349
Coasting Arc #10 (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 = -4847346
10 A = 6735678
36 meter
Y = 4639561
01 meter E =
0018042
Z = -442671
07 I = 51
87416
XDOT = -3580
664199 Wp = 17
75000
YDOT = -3172
384770 meter/sec RA = 139
22268 deg
ZDOT = 6040
689036 TA = 337
44968
MA = 337
52887
Ha = 193
571 n
mi
Hp = 185
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15903366
47 X = -4896715
73
Y = 15221656
84 feet Y = 4585079
16 meter
Z = -1452332
91 Z = -466339
35
XDOT = -11747
585956 XDOT = -3574
269059
YDOT = -10408
086516 feet/sec YDOT = -3212
390732 meter/sec
ZDOT = 19818
533582 ZDOT = 6023
309036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 544599
08 X = 165993
80
Y = 22000970
31 feet Y = 6705895
75 meter
Z = -1544632
65 Z = -470804
03
XDOT = -14078
313061 XDOT = -4291
069821
YDOT = 1717
594380 feet/sec YDOT = 523
522767 meter/sec
ZDOT = 19750
308889 ZDOT = 6019
894149
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
50090564
00010596 00000-0 82463-4 0 9091
2 25544 51
6385 140
1814 0009029 347
0444 13
0485 15
72737881 40021
Satellite: ISS
Catalog Number: 25544
Epoch time: 09130
50090564 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 140
1814 deg
Eccentricity:
0009029
Arg of perigee: 347
0444 deg
Mean anomaly: 13
0485 deg
Mean motion: 15
72737881 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4002
Checksum: 292
Coasting Arc #11 (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 = 3701365
77 A = 6724130
07 meter
Y = 2079759
30 meter E =
0016969
Z = -5226860
22 I = 51
85575
XDOT = -4737
788868 Wp = 49
80607
YDOT = 5976
860256 meter/sec RA = 134
12514 deg
ZDOT = -968
198992 TA = 210
92951
MA = 211
02956
Ha = 193
837 n
mi
Hp = 185
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12143588
48 X = 3703225
98
Y = 6823357
30 feet Y = 2121161
16 meter
Z = -17148491
53 Z = -5208873
94
XDOT = -15543
926732 XDOT = -4799
567592
YDOT = 19609
121575 feet/sec YDOT = 5923
534230 meter/sec
ZDOT = -3176
505879 ZDOT = -991
364878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13210856
60 X = 4026669
09
Y = -4681039
56 feet Y = -1426780
86 meter
Z = -17077963
70 Z = -5205363
34
XDOT = 4118
942896 XDOT = 1255
453795
YDOT = 23646
719041 feet/sec YDOT = 7207
519964 meter/sec
ZDOT = -3266
767725 ZDOT = -995
710803
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
51757399
00010596 00000-0 82463-4 0 9101
2 25544 51
6377 134
9696 0009192 350
7960 9
3032 15
72705324 40186
Satellite: ISS
Catalog Number: 25544
Epoch time: 09131
51757399 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 134
9696 deg
Eccentricity:
0009192
Arg of perigee: 350
7960 deg
Mean anomaly: 9
3032 deg
Mean motion: 15
72705324 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4018
Checksum: 317
Coasting Arc #12 (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 = 3371388
60 A = 6735040
58 meter
Y = -5698358
71 meter E =
0011272
Z = 1231975
92 I = 51
91245
XDOT = 4716
977249 Wp = 79
55311
YDOT = 1507
568798 meter/sec RA = 128
99587 deg
ZDOT = -5887
918756 TA = 87
00725
MA = 86
87826
Ha = 193
918 n
mi
Hp = 185
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11060986
22 X = 3428873
25
Y = -18695402
59 feet Y = -5660336
62 meter
Z = 4041915
74 Z = 1248493
24
XDOT = 15475
647141 XDOT = 4728
371557
YDOT = 4946
091857 feet/sec YDOT = 1560
381233 meter/sec
ZDOT = -19317
318754 ZDOT = -5864
975546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7093815
43 X = -2162194
94
Y = -20518712
26 feet Y = -6254103
50 meter
Z = 4106191
29 Z = 1251567
11
XDOT = 12368
322408 XDOT = 3769
864670
YDOT = -8154
402250 feet/sec YDOT = -2485
461806 meter/sec
ZDOT = -19227
421420 ZDOT = -5860
518049
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
53422899
00010596 00000-0 82463-4 0 9119
2 25544 51
6373 129
7575 0009357 355
0978 5
0091 15
72754621 40340
Satellite: ISS
Catalog Number: 25544
Epoch time: 09132
53422899 = yrday
fracday
Element set: 911
Inclination: 51
6373 deg
RA of node: 129
7575 deg
Eccentricity:
0009357
Arg of perigee: 355
0978 deg
Mean anomaly: 5
0091 deg
Mean motion: 15
72754621 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 4034
Checksum: 319
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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