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JPL Small-Body Database Browser
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(2016 RL17)
Classification: Aten [NEO]          SPK-ID: 3759008
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3318615227455472 0.00027909  
a .8576300481907775 7.1789e-05 au
q .573015634445849 0.00028717 au
i 3.182281352622641 0.0035563 deg
node 166.3881035667391 0.0011849 deg
peri 318.3103366067581 0.0047509 deg
M 2.306660647295835 0.17418 deg
tp 2458598.641213046591
(2019-Apr-25.14121305)
0.14013 TDB
period 290.1004549636068
0.79
0.036425
9.973e-05
d
yr
n 1.240949449890253 0.00015581 deg/d
Q 1.142244461935706 9.5613e-05 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      3 days  
   first obs. used      2016-09-05  
   last obs. used      2016-09-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .8214  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:24:08  

Additional Information
 Earth MOID = .00139936 au 
 Jupiter MOID = 3.9157 au 
 T_jup = 6.832 
[ 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 26.5   n/a E2016-RA6  

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