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JPL Small-Body Database Browser
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(2015 VB65)
Classification: Apollo [NEO]          SPK-ID: 3733937
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5659138951888307 2.291e-05  
a 2.18519673417819 0.00011217 au
q .9485635385854986 1.3789e-06 au
i 8.641795760047639 0.00028603 deg
node 231.1937700307001 0.00011619 deg
peri 224.538655440713 0.00013373 deg
M 12.45541836970854 0.02861 deg
tp 2458559.678396502126
(2019-Mar-17.17839650)
0.090624 TDB
period 1179.870223787463
3.23
0.090844
0.0002487
d
yr
n .3051183026251614 2.3493e-05 deg/d
Q 3.421829929770882 0.00017564 au
  Orbit Determination Parameters
   # obs. used (total)      216  
   data-arc span      115 days  
   first obs. used      2015-11-06  
   last obs. used      2016-02-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .38261  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Aug-10 06:19:27  

Additional Information
 Earth MOID = .0361417 au 
 Jupiter MOID = 1.85569 au 
 T_jup = 3.438 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 22.9   n/a MPO361299  
diameter diameter 0.049 km 0.025 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  
geometric albedo albedo 0.519   0.166 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  

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