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392818 (2012 TY286)
Classification: Main-belt Asteroid          SPK-ID: 2392818
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ hide orbit diagram ]

For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1434532953641299 8.7826e-08  
a 2.62809944507974 4.6576e-08 au
q 2.25108991913841 2.4865e-07 au
i 13.34915101142042 9.4324e-06 deg
node 49.49729884542999 3.6347e-05 deg
peri 34.26192168194025 6.5185e-05 deg
M 244.5596950000998 6.2407e-05 deg
tp 2459499.517853099878
(2021-Oct-12.01785310)
0.0002804 TDB
period 1556.184619540908
4.26
4.1368e-05
1.133e-07
d
yr
n .2313350199452581 6.1496e-09 deg/d
Q 3.00510897102107 5.3257e-08 au
  Orbit Determination Parameters
   # obs. used (total)      93  
   data-arc span      5244 days (14.36 yr)  
   first obs. used      2006-05-04  
   last obs. used      2020-09-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59629  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 16:22:14  

Additional Information
 Earth MOID = 1.27813 au 
 Jupiter MOID = 2.3299 au 
 T_jup = 3.349 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.95   n/a E2021B25  

392818 (2012 TY286)          Discovered 2006-May-04 by Spacewatch at Kitt Peak
Reference: Last Updated: 2014-04-17

Alternate Designations
 2012 TY286 = 2006 JC52 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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