Date:
November 30th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 1932)
---------------------------------------
Vector Time (GMT): 2006/334/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -61947
19 A = 6712338
49 meter
Y = -5309444
76 meter E =
0006554
Z = -4104979
78 I = 51
87951
XDOT = 6047
646096 Wp = 310
73579
YDOT = 2881
703776 meter/sec RA = 51
98532 deg
ZDOT = -3810
379523 TA = 280
29169
MA = 280
36558
Ha = 181
807 n
mi
Hp = 178
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -203238
82 X = 17369
94
Y = -17419438
19 feet Y = -5309693
79 meter
Z = -13467781
42 Z = -4105088
33
XDOT = 19841
358582 XDOT = 6033
483440
YDOT = 9454
408714 feet/sec YDOT = 2949
252920 meter/sec
ZDOT = -12501
245154 ZDOT = -3781
033834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16935426
50 X = -5161918
00
Y = -4079384
36 feet Y = -1243396
35 meter
Z = -13468824
07 Z = -4105297
58
XDOT = 13683
005728 XDOT = 4170
580146
YDOT = -15804
728532 feet/sec YDOT = -4817
281257 meter/sec
ZDOT = -12391
207219 ZDOT = -3776
839960
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 06334
04488403
00020000 00000-0 20000-3 0 9006
2 25544 51
6346 52
4176 0012343 278
0203 81
9562 15
78391709 19334
Satellite: ISS
Catalog Number: 25544
Epoch time: 06334
04488403 = yrday
fracday
Element set: 900
Inclination: 51
6346 deg
RA of node: 52
4176 deg
Eccentricity:
0012343
Arg of perigee: 278
0203 deg
Mean anomaly: 81
9562 deg
Mean motion: 15
78391709 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1933
Checksum: 282
Coasting Arc #2 (Orbit 1948)
---------------------------------------
Vector Time (GMT): 2006/335/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5410927
69 A = 6717886
83 meter
Y = -3407883
20 meter E =
0002956
Z = 2052204
85 I = 51
87954
XDOT = 1145
278447 Wp = 154
60145
YDOT = -5182
351196 meter/sec RA = 46
78868 deg
ZDOT = -5585
772947 TA = 2
54247
MA = 2
54097
Ha = 182
024 n
mi
Hp = 179
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17752387
43 X = -5382387
56
Y = -11180719
17 feet Y = -3468231
75 meter
Z = 6732955
55 Z = 2025987
12
XDOT = 3757
475219 XDOT = 1230
278354
YDOT = -17002
464553 feet/sec YDOT = -5169
068450 meter/sec
ZDOT = -18326
026729 ZDOT = -5580
002920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14891051
32 X = -4538792
44
Y = 14823217
03 feet Y = 4518116
55 meter
Z = 6634550
38 Z = 2022210
95
XDOT = -14620
098481 XDOT = -4456
206017
YDOT = -6493
556267 feet/sec YDOT = -1979
235950 meter/sec
ZDOT = -18305
074789 ZDOT = -5579
386796
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 06335
05787991
00020000 00000-0 20000-3 0 9013
2 25544 51
6345 47
1805 0012162 281
7654 78
2147 15
78404224 19495
Satellite: ISS
Catalog Number: 25544
Epoch time: 06335
05787991 = yrday
fracday
Element set: 901
Inclination: 51
6345 deg
RA of node: 47
1805 deg
Eccentricity:
0012162
Arg of perigee: 281
7654 deg
Mean anomaly: 78
2147 deg
Mean motion: 15
78404224 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1949
Checksum: 300
Coasting Arc #3 (Orbit 1964)
---------------------------------------
Vector Time (GMT): 2006/336/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2167616
70 A = 6707499
82 meter
Y = 3588994
78 meter E =
0009369
Z = 5243165
46 I = 51
82537
XDOT = -6078
593443 Wp = 282
58043
YDOT = -4678
866923 meter/sec RA = 41
65813 deg
ZDOT = 692
761063 TA = 160
86727
MA = 160
83206
Ha = 182
365 n
mi
Hp = 179
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7111603
33 X = -2233059
22
Y = 11774917
26 feet Y = 3564388
92 meter
Z = 17201986
41 Z = 5232476
26
XDOT = -19942
891874 XDOT = -6029
187312
YDOT = -15350
613263 feet/sec YDOT = -4746
564946 meter/sec
ZDOT = 2272
838134 ZDOT = 663
350124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10019890
11 X = 3054062
50
Y = 9496523
53 feet Y = 2894540
37 meter
Z = 17162451
98 Z = 5231115
36
XDOT = -18470
307621 XDOT = -5629
749763
YDOT = 15598
367283 feet/sec YDOT = 4754
382348 meter/sec
ZDOT = 2162
351667 ZDOT = 659
084788
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 06336
07084366
00020000 00000-0 20000-3 0 9023
2 25544 51
6352 41
9429 0012271 286
3299 73
6516 15
78483207 19659
Satellite: ISS
Catalog Number: 25544
Epoch time: 06336
07084366 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 41
9429 deg
Eccentricity:
0012271
Arg of perigee: 286
3299 deg
Mean anomaly: 73
6516 deg
Mean motion: 15
78483207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1965
Checksum: 304
Coasting Arc #4 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2006/337/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4892404
68 A = 6718936
68 meter
Y = 4503871
57 meter E =
0012182
Z = 903389
23 I = 51
84210
XDOT = -3852
171014 Wp = 357
82820
YDOT = 2989
060338 meter/sec RA = 36
50460 deg
ZDOT = 5974
344871 TA = 12
02926
MA = 12
00019
Ha = 182
595 n
mi
Hp = 178
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16051196
45 X = 4837289
53
Y = 14776481
53 feet Y = 4558272
88 meter
Z = 2963875
43 Z = 927023
80
XDOT = -12638
356346 XDOT = -3914
331830
YDOT = 9806
628405 feet/sec YDOT = 2945
634954 meter/sec
ZDOT = 19600
868999 ZDOT = 5955
479905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17566739
58 X = 5354342
23
Y = -12917441
01 feet Y = -3937236
02 meter
Z = 3052744
60 Z = 930476
55
XDOT = 6249
726341 XDOT = 1904
916589
YDOT = 13103
855914 feet/sec YDOT = 3994
055282 meter/sec
ZDOT = 19530
696336 ZDOT = 5952
956243
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 06337
08377899
00020000 00000-0 20000-3 0 9032
2 25544 51
6350 36
7050 0012373 290
5822 69
4015 15
78534468 19812
Satellite: ISS
Catalog Number: 25544
Epoch time: 06337
08377899 = yrday
fracday
Element set: 903
Inclination: 51
6350 deg
RA of node: 36
7050 deg
Eccentricity:
0012373
Arg of perigee: 290
5822 deg
Mean anomaly: 69
4015 deg
Mean motion: 15
78534468 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1981
Checksum: 306
Coasting Arc #5 (Orbit 1995)
---------------------------------------
Vector Time (GMT): 2006/338/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4478017
20 A = 6709516
12 meter
Y = -1627853
15 meter E =
0001612
Z = -4722684
58 I = 51
78638
XDOT = 4799
128445 Wp = 335
14974
YDOT = 5399
316919 meter/sec RA = 31
31646 deg
ZDOT = 2690
525887 TA = 321
21785
MA = 321
22942
Ha = 182
940 n
mi
Hp = 178
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14691657
47 X = 4518829
74
Y = -5340725
55 feet Y = -1577548
57 meter
Z = -15494371
98 Z = -4700830
97
XDOT = 15745
172063 XDOT = 4725
325452
YDOT = 17714
294354 feet/sec YDOT = 5452
570381 meter/sec
ZDOT = 8827
184668 ZDOT = 2713
662135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2686910
77 X = -818970
40
Y = -15481210
22 feet Y = -4718672
88 meter
Z = -15412863
20 Z = -4697840
70
XDOT = 19047
050710 XDOT = 5805
541056
YDOT = -12177
101906 feet/sec YDOT = -3711
580661 meter/sec
ZDOT = 8914
290581 ZDOT = 2717
075769
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 06338
03338027
00020000 00000-0 20000-3 0 9049
2 25544 51
6345 31
7947 0012399 294
4118 65
5753 15
78577890 19963
Satellite: ISS
Catalog Number: 25544
Epoch time: 06338
03338027 = yrday
fracday
Element set: 904
Inclination: 51
6345 deg
RA of node: 31
7947 deg
Eccentricity:
0012399
Arg of perigee: 294
4118 deg
Mean anomaly: 65
5753 deg
Mean motion: 15
78577890 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1996
Checksum: 324
Coasting Arc #6 (Orbit 2011)
---------------------------------------
Vector Time (GMT): 2006/339/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3148979
13 A = 6713412
16 meter
Y = -4711165
96 meter E =
0008754
Z = -3601264
55 I = 51
77409
XDOT = 6260
970077 Wp = 320
65256
YDOT = -797
728115 meter/sec RA = 26
20335 deg
ZDOT = -4418
599144 TA = 262
40774
MA = 262
50718
Ha = 183
097 n
mi
Hp = 178
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10331296
37 X = -3078569
57
Y = -15456581
22 feet Y = -4745985
29 meter
Z = -11815172
41 Z = -3616392
35
XDOT = 20541
240410 XDOT = 6290
890198
YDOT = -2617
218226 feet/sec YDOT = -727
546424 meter/sec
ZDOT = -14496
716351 ZDOT = -4388
110250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16877338
52 X = -5144212
78
Y = 7710043
65 feet Y = 2350021
31 meter
Z = -11872260
02 Z = -3618664
86
XDOT = 1217
186430 XDOT = 370
998424
YDOT = -19545
536162 feet/sec YDOT = -5957
479422 meter/sec
ZDOT = -14382
822707 ZDOT = -4383
884361
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 06339
04626024
00020000 00000-0 20000-3 0 9059
2 25544 51
6338 26
5573 0012457 298
2085 61
7822 15
78594671 20123
Satellite: ISS
Catalog Number: 25544
Epoch time: 06339
04626024 = yrday
fracday
Element set: 905
Inclination: 51
6338 deg
RA of node: 26
5573 deg
Eccentricity:
0012457
Arg of perigee: 298
2085 deg
Mean anomaly: 61
7822 deg
Mean motion: 15
78594671 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2012
Checksum: 294
Coasting Arc #7 (Orbit 2027)
---------------------------------------
Vector Time (GMT): 2006/340/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6178066
62 A = 6715924
21 meter
Y = -148514
55 meter E =
0004758
Z = 2632256
80 I = 51
75724
XDOT = -2111
071002 Wp = 38
58914
YDOT = -5234
642951 meter/sec RA = 20
99207 deg
ZDOT = -5241
450676 TA = 111
48018
MA = 111
42943
Ha = 183
304 n
mi
Hp = 178
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20269247
46 X = -6188733
92
Y = -487252
47 feet Y = -217661
24 meter
Z = 8636013
12 Z = 2602217
45
XDOT = -6926
085966 XDOT = -2026
917274
YDOT = -17174
025431 feet/sec YDOT = -5257
778642 meter/sec
ZDOT = -17196
360486 ZDOT = -5251
502920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3328661
09 X = -1014575
90
Y = 20048125
80 feet Y = 6110668
75 meter
Z = 8523684
48 Z = 2598019
03
XDOT = -16499
564759 XDOT = -5029
067338
YDOT = 4600
274679 feet/sec YDOT = 1402
163722 meter/sec
ZDOT = -17234
530805 ZDOT = -5253
084989
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 06340
05911085
00020000 00000-0 20000-3 0 9067
2 25544 51
6341 21
3188 0012453 303
1119 56
8850 15
78687190 20284
Satellite: ISS
Catalog Number: 25544
Epoch time: 06340
05911085 = yrday
fracday
Element set: 906
Inclination: 51
6341 deg
RA of node: 21
3188 deg
Eccentricity:
0012453
Arg of perigee: 303
1119 deg
Mean anomaly: 56
8850 deg
Mean motion: 15
78687190 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2028
Checksum: 273
Coasting Arc #8 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2006/341/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 323672
63 A = 6707391
74 meter
Y = 4308061
81 meter E =
0008050
Z = 5135329
80 I = 51
70016
XDOT = -7516
206289 Wp = 307
04835
YDOT = -1031
124173 meter/sec RA = 15
85968 deg
ZDOT = 1344
952926 TA = 130
13513
MA = 130
06458
Ha = 183
544 n
mi
Hp = 178
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1061918
08 X = 250528
58
Y = 14134061
05 feet Y = 4311271
41 meter
Z = 16848194
88 Z = 5136725
31
XDOT = -24659
469453 XDOT = -7510
651067
YDOT = -3382
953324 feet/sec YDOT = -1115
143741 meter/sec
ZDOT = 4412
575217 ZDOT = 1308
452293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14145755
49 X = 4311626
27
Y = 777730
17 feet Y = 237052
15 meter
Z = 16853894
50 Z = 5137067
04
XDOT = -6337
553476 XDOT = -1931
686299
YDOT = 23048
217360 feet/sec YDOT = 7025
096651 meter/sec
ZDOT = 4275
979651 ZDOT = 1303
318598
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 06341
07193516
00020000 00000-0 20000-3 0 9072
2 25544 51
6330 16
0793 0012298 306
8948 53
1090 15
78667100 20445
Satellite: ISS
Catalog Number: 25544
Epoch time: 06341
07193516 = yrday
fracday
Element set: 907
Inclination: 51
6330 deg
RA of node: 16
0793 deg
Eccentricity:
0012298
Arg of perigee: 306
8948 deg
Mean anomaly: 53
1090 deg
Mean motion: 15
78667100 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2044
Checksum: 279
Coasting Arc #9 (Orbit 2059)
---------------------------------------
Vector Time (GMT): 2006/342/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6514038
29 A = 6718652
97 meter
Y = 1549279
19 meter E =
0016477
Z = 398635
31 I = 51
70993
XDOT = -1457
193900 Wp = 1
35055
YDOT = 4576
096001 meter/sec RA = 10
68450 deg
ZDOT = 6038
124986 TA = 2
99197
MA = 2
98212
Ha = 183
631 n
mi
Hp = 177
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21371516
70 X = 6494293
40
Y = 5082936
96 feet Y = 1622012
31 meter
Z = 1307858
61 Z = 430232
83
XDOT = -4780
819882 XDOT = -1537
588285
YDOT = 15013
438323 feet/sec YDOT = 4559
350356 meter/sec
ZDOT = 19810
121344 ZDOT = 6030
851400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7317797
11 X = 2230464
56
Y = -20705175
80 feet Y = -6310937
58 meter
Z = 1426186
87 Z = 434701
76
XDOT = 12900
847434 XDOT = 3932
178298
YDOT = 5919
912688 feet/sec YDOT = 1804
389387 meter/sec
ZDOT = 19783
434998 ZDOT = 6029
990987
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 06342
08472824
00020000 00000-0 20000-3 0 9087
2 25544 51
6320 10
8397 0012355 310
4770 49
5318 15
78740760 20608
Satellite: ISS
Catalog Number: 25544
Epoch time: 06342
08472824 = yrday
fracday
Element set: 908
Inclination: 51
6320 deg
RA of node: 10
8397 deg
Eccentricity:
0012355
Arg of perigee: 310
4770 deg
Mean anomaly: 49
5318 deg
Mean motion: 15
78740760 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2060
Checksum: 277
Coasting Arc #10 (Orbit 2074)
---------------------------------------
Vector Time (GMT): 2006/343/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2832278
36 A = 6708174
22 meter
Y = -3615309
01 meter E =
0005875
Z = -4890447
76 I = 51
64571
XDOT = 6961
254775 Wp = 31
61781
YDOT = 2443
217198 meter/sec RA = 5
49181 deg
ZDOT = 2231
523166 TA = 260
01513
MA = 260
08144
Ha = 183
796 n
mi
Hp = 177
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9292251
84 X = 2896251
61
Y = -11861250
04 feet Y = -3583278
51 meter
Z = -16044776
12 Z = -4876533
70
XDOT = 22838
762385 XDOT = 6922
576689
YDOT = 8015
804455 feet/sec YDOT = 2520
845235 meter/sec
ZDOT = 7321
270230 ZDOT = 2265
247280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10980976
19 X = -3347001
54
Y = -10397468
26 feet Y = -3169148
33 meter
Z = -15993150
19 Z = -4874712
18
XDOT = 9250
974302 XDOT = 2819
696967
YDOT = -21194
983692 feet/sec YDOT = -6460
231029 meter/sec
ZDOT = 7447
657975 ZDOT = 2270
046151
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 06343
03419711
00020000 00000-0 20000-3 0 9090
2 25544 51
6311 5
9273 0012225 314
1693 45
8467 15
78789997 20752
Satellite: ISS
Catalog Number: 25544
Epoch time: 06343
03419711 = yrday
fracday
Element set: 909
Inclination: 51
6311 deg
RA of node: 5
9273 deg
Eccentricity:
0012225
Arg of perigee: 314
1693 deg
Mean anomaly: 45
8467 deg
Mean motion: 15
78789997 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2075
Checksum: 304
Coasting Arc #11 (Orbit 2090)
---------------------------------------
Vector Time (GMT): 2006/344/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5189061
54 A = 6713528
05 meter
Y = -2667290
91 meter E =
0009643
Z = -3327871
88 I = 51
63563
XDOT = 4894
972092 Wp = 339
69603
YDOT = -3671
294527 meter/sec RA =
36400 deg
ZDOT = -4677
134013 TA = 239
49388
MA = 239
58912
Ha = 183
911 n
mi
Hp = 177
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17024480
10 X = -5142683
70
Y = -8750954
44 feet Y = -2725058
17 meter
Z = -10918214
85 Z = -3352967
95
XDOT = 16059
619723 XDOT = 4958
381829
YDOT = -12044
929550 feet/sec YDOT = -3616
201127 meter/sec
ZDOT = -15344
927863 ZDOT = -4653
200715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9944369
70 X = -3031043
88
Y = 16292845
73 feet Y = 4966059
38 meter
Z = -11012367
19 Z = -3356569
52
XDOT = -9668
505368 XDOT = -2946
960436
YDOT = -16241
050732 feet/sec YDOT = -4950
272263 meter/sec
ZDOT = -15255
840252 ZDOT = -4649
980109
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 06344
04693625
00020000 00000-0 20000-3 0 9102
2 25544 51
6308
6887 0012226 318
5512 41
4725 15
78836714 20917
Satellite: ISS
Catalog Number: 25544
Epoch time: 06344
04693625 = yrday
fracday
Element set: 910
Inclination: 51
6308 deg
RA of node:
6887 deg
Eccentricity:
0012226
Arg of perigee: 318
5512 deg
Mean anomaly: 41
4725 deg
Mean motion: 15
78836714 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2091
Checksum: 281
Coasting Arc #12 (Orbit 2106)
---------------------------------------
Vector Time (GMT): 2006/345/00:32:03
171
Vector Time (MET): N/A
Weight (LBS) : 470269
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5424431
51 A = 6714754
94 meter
Y = 2737771
73 meter E =
0009416
Z = 2863121
96 I = 51
61199
XDOT = -4519
067042 Wp = 36
76289
YDOT = -3641
742451 meter/sec RA = 355
13943 deg
ZDOT = -5063
494922 TA = 110
29349
MA = 110
19226
Ha = 184
026 n
mi
Hp = 177
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17796691
30 X = -5468551
01
Y = 8982190
73 feet Y = 2676865
76 meter
Z = 9393444
76 Z = 2836663
21
XDOT = -14826
335439 XDOT = -4453
411189
YDOT = -11947
973920 feet/sec YDOT = -3691
909557 meter/sec
ZDOT = -16612
516149 ZDOT = -5085
289415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7995786
19 X = 2437115
63
Y = 18311546
32 feet Y = 5581359
32 meter
Z = 9294807
71 Z = 2833057
39
XDOT = -11398
022589 XDOT = -3474
117285
YDOT = 13477
818424 feet/sec YDOT = 4108
039056 meter/sec
ZDOT = -16694
434997 ZDOT = -5088
463787
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 06345
05964537
00020000 00000-0 20000-3 0 9118
2 25544 51
6313 355
4485 0012337 321
7617 38
2673 15
78903735 21075
Satellite: ISS
Catalog Number: 25544
Epoch time: 06345
05964537 = yrday
fracday
Element set: 911
Inclination: 51
6313 deg
RA of node: 355
4485 deg
Eccentricity:
0012337
Arg of perigee: 321
7617 deg
Mean anomaly: 38
2673 deg
Mean motion: 15
78903735 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2107
Checksum: 295
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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