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(2016 LV)
Classification: Apollo [NEO]          SPK-ID: 3753664
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5359729996547186 0.00020422  
a 2.005512331137758 0.00083477 au
q .9306118711733266 2.2211e-05 au
i 2.128157632885834 0.00064207 deg
node 83.73361991407415 0.00028679 deg
peri 126.7399476823511 0.00046284 deg
M 157.2913675694013 0.32694 deg
tp 2458547.248949343956
(2019-Mar-04.74894934)
0.65912 TDB
period 1037.37656272955
2.84
0.6477
0.001773
d
yr
n .3470292398478392 0.00021667 deg/d
Q 3.08041279110219 0.0012822 au
  Orbit Determination Parameters
   # obs. used (total)      188  
   data-arc span      14 days  
   first obs. used      2016-06-03  
   last obs. used      2016-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .3072  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:37  

Additional Information
 Earth MOID = .00839929 au 
 Jupiter MOID = 1.88461 au 
 T_jup = 3.642 
[ 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 23.1   n/a MPO386982  

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