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JPL Small-Body Database Browser
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330233 (2006 KV86)
Classification: Apollo [NEO, PHA]          SPK-ID: 2330233
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 39 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3740229502804048 9.6522e-08  
a 1.543041912681489 3.2898e-08 au
q .9659088240940397 1.5096e-07 au
i 37.07864190712159 2.2496e-05 deg
node 220.0616343700478 1.9126e-05 deg
peri 153.8370241201039 3.1057e-05 deg
M 142.4609856928533 3.2615e-05 deg
tp 2458323.449808260758
(2018-Jul-23.94980826)
5.5652e-05 TDB
period 700.1079526514212
1.92
2.239e-05
6.13e-08
d
yr
n .5142064143631311 1.6445e-08 deg/d
Q 2.120175001268938 4.5203e-08 au
  Orbit Determination Parameters
   # obs. used (total)      131  
   data-arc span      3122 days (8.55 yr)  
   first obs. used      2006-05-26  
   last obs. used      2014-12-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .65728  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:23:34  

Additional Information
 Earth MOID = .0014489 au 
 Jupiter MOID = 3.39848 au 
 T_jup = 4.178 
[ 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 18.7   n/a MPO258248  

330233 (2006 KV86)          Discovered 2006-May-26 by Mt. Lemmon Survey at Mount Lemmon
Reference: 20120604/Numbers.arcLast Updated: 2012-06-06

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