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JPL Small-Body Database Browser
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(2016 VR)
Classification: Apollo [NEO]          SPK-ID: 3763268
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3280157737503651 1.8504e-05  
a 1.161228264075851 2.4352e-05 au
q .7803270765342174 5.4854e-06 au
i 3.493831486905632 0.00023639 deg
node 45.30253166512199 6.1804e-05 deg
peri 87.92832007860919 0.00089413 deg
M 298.609560367321 0.019714 deg
tp 2458678.442272943886
(2019-Jul-13.94227294)
0.027482 TDB
period 457.0616927926795
1.25
0.014378
3.936e-05
d
yr
n .7876398431038366 2.4777e-05 deg/d
Q 1.542129451617484 3.234e-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 = .0064822 au 
 Jupiter MOID = 3.50185 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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