Solar System Dynamics Group |
2008 AF4 |
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 |
20080623 20990102 |
1.382541284 -7.99 1.386106525 |
0.410729606 -7.94 0.411537082 |
8.9198490 -7.29 8.9291090 |
109.4301821 -4.46 108.7135967 |
293.3347742 -0.57 294.4453396 |
130.7439128 8.00 23.5630140 |
0″.35 |
Impact date: 2099 01 09.970 (UT) Vimpact= 15.930 km/sec Ψimpact = 0°.54
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 |
20080623 21000103 |
1.382526173 -1.96 1.359046662 |
0.410721421 -1.98 0.404247977 |
8.9197146 -2.05 9.0690084 |
109.4301448 -0.91 108.6974362 |
293.3347456 0.60 292.6430110 |
130.7462217 1.94 24.8410565 |
0″.34 |
Impact date: 2100 01 10.213 (UT) Vimpact= 15.919 km/sec Ψimpact = 6°.70