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(2015 VU65)
Classification: Apollo [NEO]          SPK-ID: 3734102
[ 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.


Orbital Elements at Epoch 2457337.5 (2015-Nov-11.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5791027403431084 0.00081937  
a 1.971809248417109 0.0034932 au
q .8299291092248762 0.00014538 au
i 2.961435392672305 0.003389 deg
node 230.6437489718854 0.00067675 deg
peri 238.6676266137477 0.00092705 deg
M 344.6625519712895 0.046097 deg
tp 2457380.587012144669
(2015-Dec-24.08701214)		 0.015004 TDB
period 1011.336719318943
2.77		 2.6875
0.007358		 d
yr
n .3559645300354883 0.00094591 deg/d
Q 3.113689387609341 0.0055161 au
   Orbit Determination Parameters
   # obs. used (total)      64  
   data-arc span      6 days  
   first obs. used      2015-11-09  
   last obs. used      2015-11-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .37993  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Aug-10 06:19:27  

Additional Information
 Earth MOID = .00244891 au 
 Jupiter MOID = 2.06139 au 
 T_jup = 3.641 
[ 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 26.4   n/a MPO361300  
diameter diameter 0.047 km 0.015 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  
geometric albedo albedo 0.022   0.025 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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