| Solar System Dynamics Group |
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2011 AG5 older result |
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| Solar System Dynamics Group |
|
2011 AG5 older result |
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Asteroid 2011 AG5 was discovered on January 8, 2011 by Mt. Lemmon Survey. It has a diameter of about 100—230 meters. The asteroid 2011 AG5 will make a close pass (36.6 lunar distances, 0.0941 AU), travelling at 7.73 km/second, to the Earth-Moon system on the 24th February, 2011.
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110608 20360129 |
1.430709792 -18.22 1.382492165 |
0.390614488 -18.22 0.375772679 |
3.6811444 -18.57 3.9073511 |
135.7111821 18.76 135.4768369 |
53.4804526 -18.80 56.9824246 |
43.5949282 18.22 329.3453705 |
0″.41 |
Impact date: 2036 02 05.120 (UT) Vimpact= 14.413 km/sec Ψimpact = 31°.61
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110608 20400129 |
1.430571674 -3.26 1.424993780 |
0.390541039 -3.27 0.388827212 |
3.6804661 -3.37 3.6976143 |
135.7128317 3.56 135.4885149 |
53.4782966 -3.53 54.2206045 |
43.6009329 3.25 331.8469405 |
0″.27 |
Impact date: 2040 02 05.158 (UT) Vimpact= 14.380 km/sec Ψimpact = 17°.89
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110608 20450129 |
1.430572711 -3.37 1.406252224 |
0.390541588 -3.38 0.383204089 |
3.6804697 -3.45 3.7319013 |
135.7128340 3.54 135.4283194 |
53.4782979 -3.54 55.4732938 |
43.6008878 3.36 331.2002866 |
0″.27 |
Impact date: 2045 02 04.423 (UT) Vimpact= 14.406 km/sec Ψimpact =31°.47
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110608 20460129 |
1.430704381 -17.63 1.392621771 |
0.390611734 -17.66 0.379291889 |
3.6811072 -17.74 3.8432969 |
135.7113379 17.32 135.3220177 |
53.4802747 -17.54 56.4066926 |
43.5951799 17.59 330.2939028 |
0″.40 |
Impact date: 2046 02 04.530 (UT) Vimpact= 14.382 km/sec Ψimpact = 21°.45
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110608 20470129 |
1.430570999 -3.19 1.452390156 |
0.390540660 -3.19 0.397053437 |
3.6804526 -3.06 3.6517927 |
135.7129419 2.55 135.4080491 |
53.4781820 -2.71 52.5936077 |
43.6009616 3.18 333.4626378 |
0″.27 |
Impact date: 2047 02 04.918 (UT) Vimpact= 14.435 km/sec Ψimpact = 35°.39
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110608 20510129 |
1.430702607 -17.44 1.395054294 |
0.390610820 -17.47 0.379780241 |
3.6810835 -17.21 3.8224351 |
135.7115033 15.80 135.3656773 |
53.4800990 -16.29 56.2320406 |
43.5952636 17.38 330.2346391 |
0″.41 |
Impact date: 2051 02 04.920 (UT) Vimpact= 14.668 km/sec Ψimpact = 67°.28
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110208 20360129 |
1.430621216 -3.72 1.382492160 |
0.390613620 -3.71 0.375773843 |
3.6829372 -3.73 3.9076730 |
135.7325101 3.77 135.4773829 |
53.5079123 -3.70 56.9821195 |
334.4593186 -3.72 329.3453174 |
0″.38 |
Impact date: 2036 02 05.120 (UT) Vimpact= 14.418 km/sec Ψimpact = 32°.37
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110208 20400129 |
1.430483056 -2.13 1.424993780 |
0.390539005 -2.16 0.388828030 |
3.6823024 -2.23 3.6976200 |
135.7337084 2.32 135.4886724 |
53.5059705 -2.49 54.2207058 |
334.4553863 -2.05 331.8468571 |
0″.38 |
Impact date: 2040 02 05.158 (UT) Vimpact= 14.380 km/sec Ψimpact =18°.04
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110208 20460129 |
1.430615802 -3.65 1.392621767 |
0.390610397 -3.65 0.379293060 |
3.6829080 -3.66 3.8434291 |
135.7325588 3.71 135.3225110 |
53.5077542 -3.60 56.4065057 |
334.4591968 -3.66 330.2938249 |
0″.38 |
Impact date: 2046 02 04.530 (UT) Vimpact= 14.383 km/sec Ψimpact =22°.03
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110208 20510129 |
1.430614032 -3.63 1.395054287 |
0.390608890 -3.62 0.379780932 |
3.6828859 -3.61 3.8225109 |
135.7326212 3.63 135.3660657 |
53.5075350 -3.46 56.2318612 |
334.4592056 -3.67 330.2346219 |
0″.38 |
Impact date: 2051 02 04.920 (UT) Vimpact= 14.655 km/sec Ψimpact =66°.26
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110208 20520129 |
1.430268246 0.34 1.427971642 |
0.390417607 0.37 0.389705634 |
3.6811921 0.38 3.6894318 |
135.7359277 -0.36 135.3927048 |
53.5011605 0.52 54.0695984 |
334.4498487 0.30 332.0026951 |
0″.37 |
Impact date: 2052 02 05.179 (UT) Vimpact= 14.443 km/sec Ψimpact =39°.35
Orbital elements of impact orbit for two dates (equ. J2000)
| Epoch [TT] | a [AU] | e | i [deg] | Ω [deg] | ω [deg] | M [deg] | rms | |
|---|---|---|---|---|---|---|---|---|
| dev/σ |
20110208 20570129 |
1.430271671 0.30 1.406194039 |
0.390421398 0.29 0.383227199 |
3.6812500 0.24 3.7230140 |
135.7357851 -0.19 135.3339839 |
53.5018404 0.10 55.5015664 |
334.4497376 0.34 331.1947150 |
0″.37 |
Impact date: 2057 02 04.415 (UT) Vimpact= 14.534 km/sec Ψimpact =52°.51