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482562 (2012 VN82)
Classification: Apollo [NEO]          SPK-ID: 2482562
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 45 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5065912878451441 4.6335e-08  
a 1.55087577746669 2.4819e-08 au
q .7652156200720005 7.3659e-08 au
i 9.711760675974276 7.7988e-06 deg
node 228.6386931855147 5.4532e-05 deg
peri 331.2039762862263 5.4613e-05 deg
M 243.666946873328 2.1416e-05 deg
tp 2459228.463109198560
(2021-Jan-13.96310920)
4.7226e-05 TDB
period 705.4462777841939
1.93
1.6934e-05
4.636e-08
d
yr
n .5103152590594987 1.225e-08 deg/d
Q 2.336535934861379 3.7392e-08 au
  Orbit Determination Parameters
   # obs. used (total)      136  
   data-arc span      3954 days (10.83 yr)  
   first obs. used      2006-10-21  
   last obs. used      2017-08-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54127  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Jan-16 06:57:32  

Additional Information
 Earth MOID = .115763 au 
 Jupiter MOID = 2.64336 au 
 T_jup = 4.283 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 20.0   n/a E2015A31  

482562 (2012 VN82)          Discovered 2012-Nov-13 by Mt. Lemmon Survey at Mount Lemmon
Reference: Last Updated: 2017-01-17

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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