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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5654293011663651 2.3231e-05  
a 2.186410594331402 0.00011102 au
q .9501499799158603 2.5475e-06 au
i 8.63425538623347 0.00029313 deg
node 231.1780901749854 9.0397e-05 deg
peri 224.6113045966381 6.8979e-05 deg
M 134.4197822149621 0.037878 deg
tp 2458559.583147883367
(2019-Mar-17.08314788)
0.090663 TDB
period 1180.853473695925
3.23
0.089943
0.0002463
d
yr
n .3048642427017168 2.3221e-05 deg/d
Q 3.422671208746944 0.0001738 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 = .0374416 au 
 Jupiter MOID = 1.85442 au 
 T_jup = 3.437 
[ 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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