Date:
October 9th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6027 79 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 ET - UTC (sec) : 65 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 1039)
---------------------------------------
Vector Time (GMT): 2006/277/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2748041
94 A = 6713686
43 meter
Y = -3428943
56 meter E =
0025844
Z = -5098596
25 I = 51
53102
XDOT = 6819
998941 Wp = 68
27095
YDOT = -3200
745107 meter/sec RA = 344
08340 deg
ZDOT = -1520
016506 TA = 187
07903
MA = 187
11560
Ha = 190
547 n
mi
Hp = 175
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9015885
63 X = -2684726
65
Y = -11249814
82 feet Y = -3459320
04 meter
Z = -16727678
00 Z = -5111792
24
XDOT = 22375
324611 XDOT = 6862
667226
YDOT = -10501
132241 feet/sec YDOT = -3124
241640 meter/sec
ZDOT = -4986
930795 ZDOT = -1486
780987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8377512
74 X = 2553465
88
Y = 11661872
56 feet Y = 3554538
76 meter
Z = -16777298
57 Z = -5113720
61
XDOT = -22026
840060 XDOT = -6713
780850
YDOT = 8811
230853 feet/sec YDOT = 2685
663164 meter/sec
ZDOT = -4863
529098 ZDOT = -1482
403669
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 06277
47672869
00020000 00000-0 20000-3 0 9000
2 25544 51
6369 344
4623 0012384 57
4543 302
7816 15
76514597 10406
Satellite: ISS
Catalog Number: 25544
Epoch time: 06277
47672869 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 344
4623 deg
Eccentricity:
0012384
Arg of perigee: 57
4543 deg
Mean anomaly: 302
7816 deg
Mean motion: 15
76514597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1040
Checksum: 308
Coasting Arc #2 (Orbit 1055)
---------------------------------------
Vector Time (GMT): 2006/278/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6118121
63 A = 6724813
49 meter
Y = 2747288
89 meter E =
0021081
Z = 454607
07 I = 51
54141
XDOT = -2352
829967 Wp = 96
25345
YDOT = -4206
620279 meter/sec RA = 338
90416 deg
ZDOT = -6007
558104 TA = 78
79198
MA = 78
55508
Ha = 190
588 n
mi
Hp = 175
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20072577
52 X = -6150595
90
Y = 9013414
99 feet Y = 2678691
13 meter
Z = 1491493
02 Z = 424805
87
XDOT = -7719
258421 XDOT = -2276
432225
YDOT = -13801
247634 feet/sec YDOT = -4232
504326 meter/sec
ZDOT = -19709
836299 ZDOT = -6018
802277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20345571
97 X = 6201330
34
Y = -8397950
61 feet Y = -2559695
34 meter
Z = 1380831
68 Z = 420877
50
XDOT = 6574
364260 XDOT = 2003
866226
YDOT = 12542
661989 feet/sec YDOT = 3823
003374 meter/sec
ZDOT = -19752
290117 ZDOT = -6020
498028
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 06278
49091654
00020000 00000-0 20000-3 0 9011
2 25544 51
6362 339
2340 0012596 61
4375 298
8056 15
76564270 10561
Satellite: ISS
Catalog Number: 25544
Epoch time: 06278
49091654 = yrday
fracday
Element set: 901
Inclination: 51
6362 deg
RA of node: 339
2340 deg
Eccentricity:
0012596
Arg of perigee: 61
4375 deg
Mean anomaly: 298
8056 deg
Mean motion: 15
76564270 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1056
Checksum: 304
Coasting Arc #3 (Orbit 1071)
---------------------------------------
Vector Time (GMT): 2006/279/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1375775
48 A = 6712675
42 meter
Y = 3963233
67 meter E =
0015180
Z = 5228885
77 I = 51
47540
XDOT = -7062
513731 Wp = 64
73041
YDOT = 3072
979145 meter/sec RA = 333
73945 deg
ZDOT = -463
507618 TA = 29
71634
MA = 29
63020
Ha = 190
438 n
mi
Hp = 175
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4513699
07 X = 1305954
44
Y = 13002735
14 feet Y = 3978228
47 meter
Z = 17155137
05 Z = 5235399
41
XDOT = -23170
976808 XDOT = -7094
099636
YDOT = 10081
952574 feet/sec YDOT = 2993
825550 meter/sec
ZDOT = -1520
694284 ZDOT = -497
894828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4246398
43 X = -1294302
24
Y = -13059911
44 feet Y = -3980661
01 meter
Z = 17179934
26 Z = 5236443
96
XDOT = 22341
376111 XDOT = 6809
651439
YDOT = -9464
694876 feet/sec YDOT = -2884
838998 meter/sec
ZDOT = -1648
392146 ZDOT = -502
429926
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 06279
50508207
00020000 00000-0 20000-3 0 9022
2 25544 51
6365 334
0051 0012455 64
6063 295
6390 15
76633998 10727
Satellite: ISS
Catalog Number: 25544
Epoch time: 06279
50508207 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 334
0051 deg
Eccentricity:
0012455
Arg of perigee: 64
6063 deg
Mean anomaly: 295
6390 deg
Mean motion: 15
76633998 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1072
Checksum: 291
Coasting Arc #4 (Orbit 1087)
---------------------------------------
Vector Time (GMT): 2006/280/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6083017
54 A = 6724068
30 meter
Y = -2545713
20 meter E =
0026672
Z = 1253619
56 I = 51
48782
XDOT = 845
383377 Wp = 63
02532
YDOT = 4945
652517 meter/sec RA = 328
58950 deg
ZDOT = 5857
724417 TA = 310
78351
MA = 311
01464
Ha = 190
623 n
mi
Hp = 175
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19957406
62 X = 6104941
96
Y = -8352077
44 feet Y = -2477566
84 meter
Z = 4112925
08 Z = 1283224
95
XDOT = 2773
567509 XDOT = 761
561203
YDOT = 16225
894084 feet/sec YDOT = 4954
637865 meter/sec
ZDOT = 19218
255960 ZDOT = 5861
627365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19901191
31 X = -6065883
11
Y = 8430974
63 feet Y = 2569761
07 meter
Z = 4222875
82 Z = 1287132
55
XDOT = -2116
906087 XDOT = -645
232975
YDOT = -14763
763471 feet/sec YDOT = -4499
995106 meter/sec
ZDOT = 19233
456844 ZDOT = 5862
357646
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 06280
51923174
00020000 00000-0 20000-3 0 9030
2 25544 51
6357 328
7766 0012767 68
1855 292
0666 15
76605098 10889
Satellite: ISS
Catalog Number: 25544
Epoch time: 06280
51923174 = yrday
fracday
Element set: 903
Inclination: 51
6357 deg
RA of node: 328
7766 deg
Eccentricity:
0012767
Arg of perigee: 68
1855 deg
Mean anomaly: 292
0666 deg
Mean motion: 15
76605098 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1088
Checksum: 321
Coasting Arc #5 (Orbit 1102)
---------------------------------------
Vector Time (GMT): 2006/281/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -122396
78 A = 6714542
44 meter
Y = -4695377
93 meter E =
0023480
Z = -4818238
22 I = 51
43174
XDOT = 6800
125772 Wp = 88
60916
YDOT = -2648
944089 meter/sec RA = 323
38884 deg
ZDOT = 2419
360077 TA = 205
06624
MA = 205
18041
Ha = 190
595 n
mi
Hp = 175
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -401564
23 X = -46476
59
Y = -15404783
23 feet Y = -4696322
40 meter
Z = -15807868
18 Z = -4818648
18
XDOT = 22310
123923 XDOT = 6817
488117
YDOT = -8690
761448 feet/sec YDOT = -2572
804110 meter/sec
ZDOT = 7937
533061 ZDOT = 2452
438228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 640218
54 X = 195138
61
Y = 15394501
85 feet Y = 4692244
16 meter
Z = -15810019
91 Z = -4818894
07
XDOT = -20954
527860 XDOT = -6386
940092
YDOT = 9113
354205 feet/sec YDOT = 2777
750362 meter/sec
ZDOT = 8060
407232 ZDOT = 2456
812124
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 06281
46997560
00020000 00000-0 20000-3 0 9046
2 25544 51
6349 323
8741 0012780 71
5677 288
6876 15
76654695 11033
Satellite: ISS
Catalog Number: 25544
Epoch time: 06281
46997560 = yrday
fracday
Element set: 904
Inclination: 51
6349 deg
RA of node: 323
8741 deg
Eccentricity:
0012780
Arg of perigee: 71
5677 deg
Mean anomaly: 288
6876 deg
Mean motion: 15
76654695 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1103
Checksum: 331
Coasting Arc #6 (Orbit 1118)
---------------------------------------
Vector Time (GMT): 2006/282/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5724592
20 A = 6720690
25 meter
Y = 1974971
24 meter E =
0016784
Z = -2931313
64 I = 51
43131
XDOT = 539
073569 Wp = 84
34203
YDOT = -5822
798172 meter/sec RA = 318
26071 deg
ZDOT = -4998
753269 TA = 129
52430
MA = 129
37583
Ha = 190
583 n
mi
Hp = 174
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18781470
46 X = -5732010
97
Y = 6479564
42 feet Y = 1910914
14 meter
Z = -9617170
73 Z = -2959142
48
XDOT = 1768
614071 XDOT = 628
428502
YDOT = -19103
668542 feet/sec YDOT = -5816
270441 meter/sec
ZDOT = -16400
109149 ZDOT = -4995
917220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18465821
94 X = 5628382
53
Y = -7193195
83 feet Y = -2192486
09 meter
Z = -9720582
01 Z = -2962833
40
XDOT = -1649
558404 XDOT = -502
785401
YDOT = 17814
183527 feet/sec YDOT = 5429
763139 meter/sec
ZDOT = -16390
313650 ZDOT = -4995
767600
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 06282
48408402
00020000 00000-0 20000-3 0 9052
2 25544 51
6351 318
6440 0012899 75
5895 284
6700 15
76694955 11193
Satellite: ISS
Catalog Number: 25544
Epoch time: 06282
48408402 = yrday
fracday
Element set: 905
Inclination: 51
6351 deg
RA of node: 318
6440 deg
Eccentricity:
0012899
Arg of perigee: 75
5895 deg
Mean anomaly: 284
6700 deg
Mean motion: 15
76694955 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1119
Checksum: 317
Coasting Arc #7 (Orbit 1134)
---------------------------------------
Vector Time (GMT): 2006/283/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -971405
60 A = 6718139
00 meter
Y = 5458167
65 meter E =
0024375
Z = 3777262
01 I = 51
40248
XDOT = -6234
304890 Wp = 80
19156
YDOT = 1796
583400 meter/sec RA = 313
03769 deg
ZDOT = -4172
482238 TA = 53
71713
MA = 53
49221
Ha = 190
510 n
mi
Hp = 174
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3187026
26 X = -1050717
07
Y = 17907374
18 feet Y = 5446861
38 meter
Z = 12392591
91 Z = 3772350
20
XDOT = -20453
756202 XDOT = -6233
661553
YDOT = 5894
302494 feet/sec YDOT = 1726
871575 meter/sec
ZDOT = -13689
246189 ZDOT = -4202
767614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2255828
87 X = 687576
64
Y = -18060394
74 feet Y = -5504808
32 meter
Z = 12375011
05 Z = 3771903
37
XDOT = 18702
114728 XDOT = 5700
404569
YDOT = -7181
571894 feet/sec YDOT = -2188
943113 meter/sec
ZDOT = -13801
837910 ZDOT = -4206
800195
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 06283
49817026
00020000 00000-0 20000-3 0 9061
2 25544 51
6349 313
4144 0012815 78
7287 281
5317 15
76753047 11358
Satellite: ISS
Catalog Number: 25544
Epoch time: 06283
49817026 = yrday
fracday
Element set: 906
Inclination: 51
6349 deg
RA of node: 313
4144 deg
Eccentricity:
0012815
Arg of perigee: 78
7287 deg
Mean anomaly: 281
5317 deg
Mean motion: 15
76753047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1135
Checksum: 301
Coasting Arc #8 (Orbit 1150)
---------------------------------------
Vector Time (GMT): 2006/284/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5100296
32 A = 6716436
76 meter
Y = -1060314
84 meter E =
0022434
Z = 4221028
26 I = 51
37820
XDOT = -1579
018815 Wp = 93
21933
YDOT = 6660
394690 meter/sec RA = 307
91434 deg
ZDOT = 3563
544687 TA = 320
46765
MA = 320
63107
Ha = 190
476 n
mi
Hp = 174
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16733255
63 X = 5091268
46
Y = -3478723
21 feet Y = -1003331
06 meter
Z = 13848517
91 Z = 4245784
01
XDOT = -5180
507923 XDOT = -1670
690294
YDOT = 21851
688614 feet/sec YDOT = 6642
224590 meter/sec
ZDOT = 11691
419576 ZDOT = 3555
651137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16359574
34 X = -4986398
26
Y = 4680650
42 feet Y = 1426662
25 meter
Z = 13940611
40 Z = 4249098
36
XDOT = 3983
707766 XDOT = 1214
234127
YDOT = -20982
102816 feet/sec YDOT = -6395
344938 meter/sec
ZDOT = 11662
884835 ZDOT = 3554
847298
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 06284
51223817
00020000 00000-0 20000-3 0 9075
2 25544 51
6345 308
1848 0013029 83
0105 277
2541 15
76758788 11518
Satellite: ISS
Catalog Number: 25544
Epoch time: 06284
51223817 = yrday
fracday
Element set: 907
Inclination: 51
6345 deg
RA of node: 308
1848 deg
Eccentricity:
0013029
Arg of perigee: 83
0105 deg
Mean anomaly: 277
2541 deg
Mean motion: 15
76758788 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1151
Checksum: 295
Coasting Arc #9 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2006/285/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1703323
84 A = 6721854
45 meter
Y = -6078438
47 meter E =
0017811
Z = -2315573
45 I = 51
38138
XDOT = 5458
930928 Wp = 73
70400
YDOT = -513
843267 meter/sec RA = 302
69315 deg
ZDOT = 5403
652444 TA = 260
14307
MA = 260
34420
Ha = 190
516 n
mi
Hp = 174
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5588332
80 X = 1782415
98
Y = -19942383
42 feet Y = -6058948
68 meter
Z = -7597025
75 Z = -2307106
61
XDOT = 17909
878372 XDOT = 5438
020738
YDOT = -1685
837489 feet/sec YDOT = -452
915520 meter/sec
ZDOT = 17728
518516 ZDOT = 5430
121499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3815622
93 X = -1163001
87
Y = 20367508
04 feet Y = 6208016
45 meter
Z = -7566277
72 Z = -2306201
45
XDOT = -16103
015552 XDOT = -4908
199140
YDOT = 3557
799899 feet/sec YDOT = 1084
417409 meter/sec
ZDOT = 17827
073215 ZDOT = 5433
691916
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 06285
46290745
00020000 00000-0 20000-3 0 9085
2 25544 51
6354 303
2821 0013052 86
6120 273
6537 15
76812602 11664
Satellite: ISS
Catalog Number: 25544
Epoch time: 06285
46290745 = yrday
fracday
Element set: 908
Inclination: 51
6354 deg
RA of node: 303
2821 deg
Eccentricity:
0013052
Arg of perigee: 86
6120 deg
Mean anomaly: 273
6537 deg
Mean motion: 15
76812602 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1166
Checksum: 281
Coasting Arc #10 (Orbit 1181)
---------------------------------------
Vector Time (GMT): 2006/286/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4424989
90 A = 6712978
62 meter
Y = -277379
15 meter E =
0026565
Z = -5063916
02 I = 51
33742
XDOT = 2284
033348 Wp = 83
68357
YDOT = -7159
924585 meter/sec RA = 297
54964 deg
ZDOT = -1608
012907 TA = 170
79844
MA = 170
74967
Ha = 190
501 n
mi
Hp = 174
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14517683
40 X = -4396959
50
Y = -910036
57 feet Y = -326705
02 meter
Z = -16613897
69 Z = -5085344
75
XDOT = 7493
547730 XDOT = 2371
738376
YDOT = -23490
566223 feet/sec YDOT = -7133
892848 meter/sec
ZDOT = -5275
632898 ZDOT = -1596
704045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14440323
75 X = 4401410
68
Y = -638434
65 feet Y = -194594
88 meter
Z = -16693781
65 Z = -5088264
65
XDOT = -5013
244959 XDOT = -1528
037063
YDOT = 23107
394401 feet/sec YDOT = 7043
133813 meter/sec
ZDOT = -5234
439353 ZDOT = -1595
457115
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 06286
47693396
00020000 00000-0 20000-3 0 9097
2 25544 51
6357 298
0518 0012982 90
2717 269
9936 15
76802421 11822
Satellite: ISS
Catalog Number: 25544
Epoch time: 06286
47693396 = yrday
fracday
Element set: 909
Inclination: 51
6357 deg
RA of node: 298
0518 deg
Eccentricity:
0012982
Arg of perigee: 90
2717 deg
Mean anomaly: 269
9936 deg
Mean motion: 15
76802421 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1182
Checksum: 331
Coasting Arc #11 (Orbit 1197)
---------------------------------------
Vector Time (GMT): 2006/287/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2217101
24 A = 6724003
38 meter
Y = 6324413
76 meter E =
0024831
Z = 443817
46 I = 51
36192
XDOT = -4688
883286 Wp = 111
91218
YDOT = -1204
702971 meter/sec RA = 292
35328 deg
ZDOT = -5998
051947 TA = 63
23497
MA = 62
98113
Ha = 190
464 n
mi
Hp = 174
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7273954
19 X = -2289812
93
Y = 20749388
97 feet Y = 6299214
35 meter
Z = 1456094
03 Z = 432870
11
XDOT = -15383
475349 XDOT = -4645
925985
YDOT = -3952
437569 feet/sec YDOT = -1256
896456 meter/sec
ZDOT = -19678
648119 ZDOT = -6020
726361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4651599
56 X = 1417807
55
Y = -21492438
87 feet Y = -6550895
37 meter
Z = 1416140
86 Z = 431639
73
XDOT = 14079
667363 XDOT = 4291
482612
YDOT = 1687
630107 feet/sec YDOT = 514
389657 meter/sec
ZDOT = -19763
301825 ZDOT = -6023
854396
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 06287
49093909
00020000 00000-0 20000-3 0 9106
2 25544 51
6345 292
8215 0013118 93
8503 266
4162 15
76850356 11989
Satellite: ISS
Catalog Number: 25544
Epoch time: 06287
49093909 = yrday
fracday
Element set: 910
Inclination: 51
6345 deg
RA of node: 292
8215 deg
Eccentricity:
0013118
Arg of perigee: 93
8503 deg
Mean anomaly: 266
4162 deg
Mean motion: 15
76850356 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1198
Checksum: 307
Coasting Arc #12 (Orbit 1213)
---------------------------------------
Vector Time (GMT): 2006/288/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3794254
25 A = 6711965
08 meter
Y = 1844709
14 meter E =
0015587
Z = 5206837
00 I = 51
31138
XDOT = -2709
667943 Wp = 91
61418
YDOT = 7203
939052 meter/sec RA = 287
17333 deg
ZDOT = -576
655250 TA = 3
88451
MA = 3
87242
Ha = 190
286 n
mi
Hp = 174
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12448340
72 X = 3748050
44
Y = 6052195
34 feet Y = 1886880
33 meter
Z = 17082798
55 Z = 5225157
34
XDOT = -8889
986691 XDOT = -2787
220696
YDOT = 23634
970643 feet/sec YDOT = 7173
204416 meter/sec
ZDOT = -1891
913550 ZDOT = -590
007370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13084212
84 X = -3988068
07
Y = -4248287
52 feet Y = -1294878
04 meter
Z = 17151317
41 Z = 5227721
55
XDOT = 5145
795639 XDOT = 1568
438511
YDOT = -23697
319939 feet/sec YDOT = -7222
943117 meter/sec
ZDOT = -1940
704881 ZDOT = -591
526848
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 06288
50492231
00020000 00000-0 20000-3 0 9111
2 25544 51
6337 287
5914 0013091 97
4515 262
8138 15
76894310 12140
Satellite: ISS
Catalog Number: 25544
Epoch time: 06288
50492231 = yrday
fracday
Element set: 911
Inclination: 51
6337 deg
RA of node: 287
5914 deg
Eccentricity:
0013091
Arg of perigee: 97
4515 deg
Mean anomaly: 262
8138 deg
Mean motion: 15
76894310 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1214
Checksum: 293
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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