Solar System
Dynamics
Group
2008 YC3
older results

Number of original observations: 35
Arc : 2008 12 22 - 2009 01 18
Nominal rms: 1″.54 (70 residuals)

Possible collisions in: 2088, 2090, 2092, 2105A, 2105B, 2106





Year: 2088


Orbital elements of impact orbit for two dates (equ. J2000)

Epoch [TT] a [AU] e i [deg] Ω [deg] ω [deg] M [deg] rms
20081130
20880615
1.011739947
1.039994459
0.044466798
0.049205985
11.9733798
11.8778771
91.7483333
90.6949080
82.3376385
115.0047442
259.1187967
53.1298245
1″.56
 

Impact date: 2088 06 22.207 (UT)   Vimpact= 12.890 km/sec   Ψimpact = 32°.25  

Vimpact
The velocity of the asteroid relative to the Earth at the moment of impact.
Ψimpact
The impact angle is measured from the vertical axis that goes through the impact point. Thus, the impact angle is 0 degrees for a vertical impact.
rms
Root mean square for the derived impact orbit.

Year: 2090


Orbital elements of impact orbit for two dates (equ. J2000)

Epoch [TT] a [AU] e i [deg] Ω [deg] ω [deg] M [deg] rms
20081130
20900615
1.011759414
1.037724678
0.044482145
0.048300343
11.9772631
11.8903108
91.7480005
90.6803300
82.3253990
112.7236478
259.1332775
54.9248609
1″.55
 

Impact date: 2090 06 22.696 (UT)   Vimpact= 12.801 km/sec   Ψimpact =25°.39  

Year: 2092


Orbital elements of impact orbit for two dates (equ. J2000)

Epoch [TT] a [AU] e i [deg] Ω [deg] ω [deg] M [deg] rms
20081130
20920615
1.011778846
1.035604190
0.044497448
0.047686801
11.9811205
11.9026429
91.7476695
90.6595041
82.3131513
110.4650357
259.1477599
57.6151218
1″.54
 

Impact date: 2092 06 22.188 (UT)   Vimpact= 12.816 km/sec   Ψimpact =6°.73  

Year: 2105


Orbital elements of impact orbit for two dates (equ. J2000)

Epoch [TT] a [AU] e i [deg] Ω [deg] ω [deg] M [deg] rms
20081130
21050615
1.011672582
1.040812628
0.044413691
0.050228760
11.9599673
11.8479973
91.7494841
90.5204397
82.3801064
115.5339098
259.0685705
51.4483753
1″.61
 

Impact date: 2105 06 23.365 (UT)   Vimpact= 12.813 km/sec   Ψimpact =48°.36  

Epoch [TT] a [AU] e i [deg] Ω [deg] ω [deg] M [deg] rms
20081130
21050615
1.011733213
1.040796673
0.044461495
0.049835759
11.9720298
11.8655510
91.7484490
90.5227072
82.3418615
115.7037185
259.1137986
51.3232196
1″.57
 

Impact date: 2105 06 23.359 (UT)   Vimpact= 12.822 km/sec   Ψimpact =3°.67  

Year: 2106


Orbital elements of impact orbit for two dates (equ. J2000)

Epoch [TT] a [AU] e i [deg] Ω [deg] ω [deg] M [deg] rms
20081130
21060615
1.011658506
1.039201936
0.044402582
0.049844096
11.9571617
11.8491368
91.7497248
90.4735562
82.3889824
113.7509954
259.0580715
52.9774786
1″.62
 

Impact date: 2106 06 23.569 (UT)   Vimpact= 12.818 km/sec   Ψimpact =23°.26  



External links:

2008 YC3 page (NASA JPL) and Impact Risk page NEO Program (NASA JPL)
2008 YC3 page and Impact Risk page at the NEO Dynamic Site (NEODyS)




Solar System Dynamics & Planetology Group, 2008. All rights reserved