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(2013 RE6)
Classification: Apollo [NEO]          SPK-ID: 3647027
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 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2000829129033005 2.3956e-07  
a 1.060310202360834 4.5808e-09 au
q .8481602484913906 2.5265e-07 au
i 10.43254645506419 1.9387e-05 deg
node 192.3583262194618 3.0267e-05 deg
peri 344.908029788145 5.901e-05 deg
M 227.6701306088372 7.3538e-05 deg
tp 2459147.089620428082
(2020-Oct-24.58962043)
8.19e-05 TDB
period 398.7932852719473
1.09
2.5843e-06
7.075e-09
d
yr
n .9027233238255424 5.85e-09 deg/d
Q 1.272460156230278 5.4973e-09 au
  Orbit Determination Parameters
   # obs. used (total)      73  
   data-arc span      4644 days (12.71 yr)  
   first obs. used      2001-10-17  
   last obs. used      2014-07-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .44582  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:44:54  

Additional Information
 Earth MOID = .143038 au 
 Jupiter MOID = 3.68876 au 
 T_jup = 5.777 
[ 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 21.4   n/a E2013U19  

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