Date:
December 12th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9256 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2111)
---------------------------------------
Vector Time (GMT): 2006/345/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 498899
59 A = 6715614
02 meter
Y = -4211809
84 meter E =
0017110
Z = -5204402
30 I = 51
57789
XDOT = 7653
594405 Wp = 358
94229
YDOT = -165
917536 meter/sec RA = 353
49830 deg
ZDOT = 884
731949 TA = 279
38736
MA = 279
58076
Ha = 192
545 n
mi
Hp = 178
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1636809
69 X = 571241
60
Y = -13818273
75 feet Y = -4205825
88 meter
Z = -17074810
69 Z = -5201803
33
XDOT = 25110
217865 XDOT = 7650
583021
YDOT = -544
348872 feet/sec YDOT = -80
347714 meter/sec
ZDOT = 2902
663874 ZDOT = 921
905770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6337058
84 X = 1931535
53
Y = 12400846
01 feet Y = 3779777
87 meter
Z = -17065570
57 Z = -5201585
91
XDOT = -19541
888881 XDOT = -5956
367731
YDOT = 14096
297654 feet/sec YDOT = 4296
551525 meter/sec
ZDOT = 3041
664695 ZDOT = 927
099399
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
38927283
00020000 00000-0 20000-3 0 9009
2 25544 51
6343 353
9122 0023964 322
1656 37
7823 15
75669038 21124
Satellite: ISS
Catalog Number: 25544
Epoch time: 06345
38927283 = yrday
fracday
Element set: 900
Inclination: 51
6343 deg
RA of node: 353
9122 deg
Eccentricity:
0023964
Arg of perigee: 322
1656 deg
Mean anomaly: 37
7823 deg
Mean motion: 15
75669038 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2112
Checksum: 295
Coasting Arc #2 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2006/346/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6591555
21 A = 6726358
30 meter
Y = 265133
80 meter E =
0015205
Z = -1348810
97 I = 51
58747
XDOT = 1002
431254 Wp = 328
10863
YDOT = -4921
057810 meter/sec RA = 348
36623 deg
ZDOT = -5823
617035 TA = 226
70355
MA = 226
83046
Ha = 192
681 n
mi
Hp = 177
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21625837
30 X = -6587477
78
Y = 869861
54 feet Y = 191446
28 meter
Z = -4425232
85 Z = -1380822
91
XDOT = 3288
816451 XDOT = 1085
674867
YDOT = -16145
202788 feet/sec YDOT = -4909
382133 meter/sec
ZDOT = -19106
355101 ZDOT = -5818
545429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17150842
04 X = 5227576
65
Y = -13160870
91 feet Y = -4011433
45 meter
Z = -4544917
86 Z = -1385290
96
XDOT = 5571
686247 XDOT = 1698
249968
YDOT = 13899
513971 feet/sec YDOT = 4236
571858 meter/sec
ZDOT = -19087
950742 ZDOT = -5818
007386
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 06346
40400392
00020000 00000-0 20000-3 0 9011
2 25544 51
6349 348
6871 0023878 326
5588 33
4067 15
75750546 21283
Satellite: ISS
Catalog Number: 25544
Epoch time: 06346
40400392 = yrday
fracday
Element set: 901
Inclination: 51
6349 deg
RA of node: 348
6871 deg
Eccentricity:
0023878
Arg of perigee: 326
5588 deg
Mean anomaly: 33
4067 deg
Mean motion: 15
75750546 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2128
Checksum: 306
Coasting Arc #3 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2006/347/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1256363
86 A = 6716683
86 meter
Y = 4441810
62 meter E =
0025019
Z = 4892893
29 I = 51
52690
XDOT = -7355
924218 Wp = 344
99168
YDOT = 383
920334 meter/sec RA = 343
17999 deg
ZDOT = -2216
089587 TA = 126
71517
MA = 126
48509
Ha = 192
837 n
mi
Hp = 177
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4121928
69 X = -1329708
38
Y = 14572869
49 feet Y = 4427350
77 meter
Z = 16052799
50 Z = 4886612
04
XDOT = -24133
609639 XDOT = -7348
905128
YDOT = 1259
581149 feet/sec YDOT = 301
701731 meter/sec
ZDOT = -7270
635129 ZDOT = -2251
807822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5204041
36 X = -1586191
81
Y = -14248301
20 feet Y = -4342882
20 meter
Z = 16029817
83 Z = 4885888
47
XDOT = 17664
263094 XDOT = 5384
067391
YDOT = -14860
134031 feet/sec YDOT = -4529
368853 meter/sec
ZDOT = -7404
165742 ZDOT = -2256
789718
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 06347
41870493
00020000 00000-0 20000-3 0 9027
2 25544 51
6343 343
4617 0023871 330
2512 29
7293 15
75804023 21447
Satellite: ISS
Catalog Number: 25544
Epoch time: 06347
41870493 = yrday
fracday
Element set: 902
Inclination: 51
6343 deg
RA of node: 343
4617 deg
Eccentricity:
0023871
Arg of perigee: 330
2512 deg
Mean anomaly: 29
7293 deg
Mean motion: 15
75804023 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2144
Checksum: 276
Coasting Arc #4 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2006/348/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6217101
35 A = 6724294
28 meter
Y = -367798
61 meter E =
0025074
Z = 2493451
13 I = 51
52548
XDOT = -1813
267399 Wp = 7
12757
YDOT = 5288
224541 meter/sec RA = 338
06192 deg
ZDOT = 5319
990674 TA = 21
21607
MA = 21
11227
Ha = 192
991 n
mi
Hp = 177
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20397314
15 X = 6208639
20
Y = -1206688
35 feet Y = -298323
06 meter
Z = 8180613
95 Z = 2523633
53
XDOT = -5949
040024 XDOT = -1898
110117
YDOT = 17349
818048 feet/sec YDOT = 5267
472731 meter/sec
ZDOT = 17454
037645 ZDOT = 5310
976110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15488937
81 X = -4721028
25
Y = 13256717
88 feet Y = 4040647
61 meter
Z = 8293443
35 Z = 2527841
53
XDOT = -4697
139516 XDOT = -1431
688124
YDOT = -16348
595976 feet/sec YDOT = -4983
052053 meter/sec
ZDOT = 17420
931065 ZDOT = 5309
899789
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 06348
43338002
00020000 00000-0 20000-3 0 9036
2 25544 51
6340 338
2356 0023804 334
9959 25
0050 15
75793321 21604
Satellite: ISS
Catalog Number: 25544
Epoch time: 06348
43338002 = yrday
fracday
Element set: 903
Inclination: 51
6340 deg
RA of node: 338
2356 deg
Eccentricity:
0023804
Arg of perigee: 334
9959 deg
Mean anomaly: 25
0050 deg
Mean motion: 15
75793321 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2160
Checksum: 272
Coasting Arc #5 (Orbit 2174)
---------------------------------------
Vector Time (GMT): 2006/349/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1855069
11 A = 6718806
08 meter
Y = -4802097
64 meter E =
0019020
Z = -4305491
90 I = 51
48253
XDOT = 6877
351163 Wp = 357
84364
YDOT = -430
142200 meter/sec RA = 332
85621 deg
ZDOT = 3461
157427 TA = 307
07590
MA = 307
24964
Ha = 193
184 n
mi
Hp = 177
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6086184
75 X = 1929544
54
Y = -15754913
50 feet Y = -4780936
38 meter
Z = -14125629
59 Z = -4296299
43
XDOT = 22563
488067 XDOT = 6864
836035
YDOT = -1411
227691 feet/sec YDOT = -353
306162 meter/sec
ZDOT = 11355
503370 ZDOT = 3494
537600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4885053
76 X = 1488964
39
Y = 16197214
29 feet Y = 4936910
92 meter
Z = -14091800
96 Z = -4295180
93
XDOT = -15640
699753 XDOT = -4767
285285
YDOT = 14653
089553 feet/sec YDOT = 4466
261696 meter/sec
ZDOT = 11480
284182 ZDOT = 3499
190619
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 06349
38460750
00020000 00000-0 20000-3 0 9048
2 25544 51
6350 333
3369 0023787 338
3286 21
6869 15
75863404 21752
Satellite: ISS
Catalog Number: 25544
Epoch time: 06349
38460750 = yrday
fracday
Element set: 904
Inclination: 51
6350 deg
RA of node: 333
3369 deg
Eccentricity:
0023787
Arg of perigee: 338
3286 deg
Mean anomaly: 21
6869 deg
Mean motion: 15
75863404 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2175
Checksum: 312
Coasting Arc #6 (Orbit 2190)
---------------------------------------
Vector Time (GMT): 2006/350/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5728197
31 A = 6721214
55 meter
Y = 296455
27 meter E =
0023312
Z = -3523875
24 I = 51
46642
XDOT = 2462
766147 Wp = 354
85814
YDOT = -5756
611083 meter/sec RA = 327
74471 deg
ZDOT = -4462
470990 TA = 227
14582
MA = 227
34188
Ha = 193
253 n
mi
Hp = 176
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18793298
27 X = -5713967
98
Y = 972622
28 feet Y = 232479
37 meter
Z = -11561270
47 Z = -3551668
64
XDOT = 8079
941426 XDOT = 2548
632540
YDOT = -18886
519300 feet/sec YDOT = -5728
590429 meter/sec
ZDOT = -14640
652854 ZDOT = -4450
298805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13912866
66 X = 4240641
76
Y = -12575883
74 feet Y = -3833129
36 meter
Z = -11665175
45 Z = -3555545
48
XDOT = 4673
901398 XDOT = 1424
605146
YDOT = 18785
434134 feet/sec YDOT = 5725
800324 meter/sec
ZDOT = -14595
787109 ZDOT = -4448
795911
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 06350
39922235
00020000 00000-0 20000-3 0 9053
2 25544 51
6347 328
1108 0023700 342
3451 17
6887 15
75926302 21915
Satellite: ISS
Catalog Number: 25544
Epoch time: 06350
39922235 = yrday
fracday
Element set: 905
Inclination: 51
6347 deg
RA of node: 328
1108 deg
Eccentricity:
0023700
Arg of perigee: 342
3451 deg
Mean anomaly: 17
6887 deg
Mean motion: 15
75926302 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2191
Checksum: 280
Coasting Arc #7 (Orbit 2206)
---------------------------------------
Vector Time (GMT): 2006/351/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2415551
81 A = 6721516
62 meter
Y = 5276036
48 meter E =
0024097
Z = 3409805
23 I = 51
44314
XDOT = -6181
382893 Wp = 16
26141
YDOT = 145
363025 meter/sec RA = 322
52843 deg
ZDOT = -4573
302735 TA = 123
35739
MA = 123
12652
Ha = 193
397 n
mi
Hp = 176
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7925038
76 X = -2490934
13
Y = 17309830
98 feet Y = 5248602
47 meter
Z = 11187025
03 Z = 3397887
94
XDOT = -20280
127602 XDOT = -6160
332340
YDOT = 476
912811 feet/sec YDOT = 76
357714 meter/sec
ZDOT = -15004
274065 ZDOT = -4603
281194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5047723
18 X = -1538546
03
Y = -18383113
21 feet Y = -5603172
91 meter
Z = 11143054
17 Z = 3396402
91
XDOT = 13795
726759 XDOT = 4204
937516
YDOT = -13012
074521 feet/sec YDOT = -3966
080314 meter/sec
ZDOT = -15116
371023 ZDOT = -4607
469888
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 06351
41380671
00020000 00000-0 20000-3 0 9060
2 25544 51
6334 322
8839 0023739 346
3270 13
7248 15
75989343 22078
Satellite: ISS
Catalog Number: 25544
Epoch time: 06351
41380671 = yrday
fracday
Element set: 906
Inclination: 51
6334 deg
RA of node: 322
8839 deg
Eccentricity:
0023739
Arg of perigee: 346
3270 deg
Mean anomaly: 13
7248 deg
Mean motion: 15
75989343 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2207
Checksum: 300
Coasting Arc #8 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2006/352/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5064727
86 A = 6717929
00 meter
Y = 110870
31 meter E =
0020444
Z = 4397202
04 I = 51
40916
XDOT = -2980
999976 Wp = 12
37267
YDOT = 6307
736731 meter/sec RA = 317
41121 deg
ZDOT = 3291
370046 TA = 44
62470
MA = 44
46031
Ha = 193
428 n
mi
Hp = 176
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16616561
22 X = 5041750
58
Y = 363747
72 feet Y = 167377
71 meter
Z = 14426515
88 Z = 4421751
02
XDOT = -9780
183648 XDOT = -3067
301506
YDOT = 20694
674314 feet/sec YDOT = 6273
918460 meter/sec
ZDOT = 10798
458157 ZDOT = 3276
679559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12698666
98 X = -3870553
70
Y = 10598509
56 feet Y = 3230425
72 meter
Z = 14518341
21 Z = 4425190
40
XDOT = -5419
697173 XDOT = -1651
923698
YDOT = -21136
230941 feet/sec YDOT = -6442
323191 meter/sec
ZDOT = 10744
227760 ZDOT = 3274
840621
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 06352
42836236
00020000 00000-0 20000-3 0 9076
2 25544 51
6330 317
6568 0023659 350
3675 9
7032 15
75997440 22231
Satellite: ISS
Catalog Number: 25544
Epoch time: 06352
42836236 = yrday
fracday
Element set: 907
Inclination: 51
6330 deg
RA of node: 317
6568 deg
Eccentricity:
0023659
Arg of perigee: 350
3675 deg
Mean anomaly: 9
7032 deg
Mean motion: 15
75997440 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2223
Checksum: 299
Coasting Arc #9 (Orbit 2237)
---------------------------------------
Vector Time (GMT): 2006/353/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2708829
15 A = 6724040
13 meter
Y = -5696789
50 meter E =
0027778
Z = -2280726
14 I = 51
41106
XDOT = 5462
208292 Wp = 3
09505
YDOT = 433
289531 meter/sec RA = 312
20020 deg
ZDOT = 5435
601624 TA = 331
11935
MA = 331
27281
Ha = 193
556 n
mi
Hp = 175
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8887234
75 X = 2783409
58
Y = -18690254
26 feet Y = -5666080
45 meter
Z = -7482697
30 Z = -2267386
40
XDOT = 17920
630878 XDOT = 5430
551816
YDOT = 1421
553578 feet/sec YDOT = 494
192993 meter/sec
ZDOT = 17833
338663 ZDOT = 5462
060465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5903699
95 X = 1799447
75
Y = 19854206
64 feet Y = 6051562
18 meter
Z = -7433445
39 Z = -2265714
16
XDOT = -12729
431084 XDOT = -3879
930594
YDOT = 10461
463894 feet/sec YDOT = 3188
654195 meter/sec
ZDOT = 17932
349890 ZDOT = 5465
780247
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 06353
37947912
00020000 00000-0 20000-3 0 9086
2 25544 51
6339 312
7579 0023577 353
9921 6
0957 15
76072769 22381
Satellite: ISS
Catalog Number: 25544
Epoch time: 06353
37947912 = yrday
fracday
Element set: 908
Inclination: 51
6339 deg
RA of node: 312
7579 deg
Eccentricity:
0023577
Arg of perigee: 353
9921 deg
Mean anomaly: 6
0957 deg
Mean motion: 15
76072769 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2238
Checksum: 329
Coasting Arc #10 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2006/354/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4446799
85 A = 6715291
88 meter
Y = -737820
92 meter E =
0029273
Z = -4995260
63 I = 51
36262
XDOT = 3225
257688 Wp = 23
74192
YDOT = -6729
388340 meter/sec RA = 307
06586 deg
ZDOT = -1854
550470 TA = 228
14782
MA = 228
39805
Ha = 193
663 n
mi
Hp = 175
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14589238
36 X = -4413952
78
Y = -2420672
30 feet Y = -787362
89 meter
Z = -16388650
35 Z = -5016783
62
XDOT = 10581
554096 XDOT = 3309
276051
YDOT = -22078
045735 feet/sec YDOT = -6692
851595 meter/sec
ZDOT = -6084
483170 ZDOT = -1838
679303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12242815
94 X = 3731610
30
Y = -8134551
66 feet Y = -2479411
35 meter
Z = -16469241
56 Z = -5019824
83
XDOT = 6733
236480 XDOT = 2052
290479
YDOT = 22483
354854 feet/sec YDOT = 6852
926559 meter/sec
ZDOT = -6025
875712 ZDOT = -1836
686917
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 06354
39397486
00020000 00000-0 20000-3 0 9095
2 25544 51
6329 307
5307 0023589 357
6874 2
4177 15
76092190 22544
Satellite: ISS
Catalog Number: 25544
Epoch time: 06354
39397486 = yrday
fracday
Element set: 909
Inclination: 51
6329 deg
RA of node: 307
5307 deg
Eccentricity:
0023589
Arg of perigee: 357
6874 deg
Mean anomaly: 2
4177 deg
Mean motion: 15
76092190 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2254
Checksum: 321
Coasting Arc #11 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2006/355/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2896050
88 A = 6725670
58 meter
Y = 6013929
08 meter E =
0019625
Z = 896150
22 I = 51
38178
XDOT = -4711
380479 Wp = 36
34868
YDOT = -1374
804669 meter/sec RA = 301
87003 deg
ZDOT = -5917
573904 TA = 133
84580
MA = 133
68344
Ha = 193
796 n
mi
Hp = 175
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9501479
28 X = -2967437
57
Y = 19730738
45 feet Y = 5981144
52 meter
Z = 2940125
38 Z = 881908
96
XDOT = -15457
285037 XDOT = -4666
910617
YDOT = -4510
514006 feet/sec YDOT = -1427
240180 meter/sec
ZDOT = -19414
612545 ZDOT = -5940
353993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6883521
81 X = -2098097
45
Y = -20796724
92 feet Y = -6338841
75 meter
Z = 2887532
79 Z = 880119
99
XDOT = 12649
659135 XDOT = 3855
616104
YDOT = -6932
387754 feet/sec YDOT = -2112
991787 meter/sec
ZDOT = -19499
986463 ZDOT = -5943
595874
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 06355
40843959
00020000 00000-0 20000-3 0 9101
2 25544 51
6324 302
3030 0023711 1
6289 358
4949 15
76166630 22708
Satellite: ISS
Catalog Number: 25544
Epoch time: 06355
40843959 = yrday
fracday
Element set: 910
Inclination: 51
6324 deg
RA of node: 302
3030 deg
Eccentricity:
0023711
Arg of perigee: 1
6289 deg
Mean anomaly: 358
4949 deg
Mean motion: 15
76166630 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2270
Checksum: 281
Coasting Arc #12 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2006/356/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 469410
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3829106
01 A = 6713877
99 meter
Y = 1715232
38 meter E =
0023615
Z = 5236996
44 I = 51
32765
XDOT = -3332
188835 Wp = 10
72470
YDOT = 6949
332350 meter/sec RA = 296
70711 deg
ZDOT = 183
095004 TA = 77
66416
MA = 77
39990
Ha = 193
783 n
mi
Hp = 175
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12562683
75 X = 3784201
26
Y = 5627402
82 feet Y = 1757799
57 meter
Z = 17181746
85 Z = 5255489
33
XDOT = -10932
378067 XDOT = -3410
539028
YDOT = 22799
646816 feet/sec YDOT = 6911
631853 meter/sec
ZDOT = 600
705395 ZDOT = 166
718262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12790478
84 X = -3898537
95
Y = 4848019
17 feet Y = 1477676
24 meter
Z = 17251129
56 Z = 5258144
29
XDOT = -8056
984398 XDOT = -2455
768844
YDOT = -22914
172204 feet/sec YDOT = -6984
239688 meter/sec
ZDOT = 540
232107 ZDOT = 164
662746
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 06356
42287441
00020000 00000-0 20000-3 0 9113
2 25544 51
6318 297
0754 0023600 5
2471 354
8936 15
76186423 22869
Satellite: ISS
Catalog Number: 25544
Epoch time: 06356
42287441 = yrday
fracday
Element set: 911
Inclination: 51
6318 deg
RA of node: 297
0754 deg
Eccentricity:
0023600
Arg of perigee: 5
2471 deg
Mean anomaly: 354
8936 deg
Mean motion: 15
76186423 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2286
Checksum: 294
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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