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(2016 VR)
Classification: Apollo [NEO]          SPK-ID: 3763268
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3281014455269979 1.8442e-05  
a 1.161144259955771 2.4279e-05 au
q .780171149798906 5.4651e-06 au
i 3.493548600003657 0.00023624 deg
node 45.29225174231737 5.9852e-05 deg
peri 87.95054464943695 0.00089015 deg
M 253.6559786578085 0.029607 deg
tp 2459135.501400669307
(2020-Oct-13.00140067)
0.041819 TDB
period 457.0120974132142
1.25
0.014334
3.924e-05
d
yr
n .7877253185149292 2.4707e-05 deg/d
Q 1.542117370112635 3.2246e-05 au
  Orbit Determination Parameters
   # obs. used (total)      25  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      9 days  
   first obs. used      2016-11-04  
   last obs. used      2016-11-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .47966  
   source      ORB  
   producer      OSOD/JPL  
   solution date      2017-Jul-21 16:08:36  

Additional Information
 Earth MOID = .00654841 au 
 Jupiter MOID = 3.50032 au 
 T_jup = 5.372 
[ 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 26.2   n/a MPO397900  

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