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(2013 RQ5)
Classification: Apollo [NEO]          SPK-ID: 3647014
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 2456537.5 (2013-Sep-02.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7424010601485501 0.0020589  
a 2.071807670711158 0.01379 au
q .533695459551296 0.00071332 au
i .6493558479111134 0.002149 deg
node 337.3600017913554 0.0051011 deg
peri 102.9317102024172 0.0086777 deg
M 343.0834015260061 0.19348 deg
tp 2456588.683870307310
(2013-Oct-23.18387031)
0.074373 TDB
period 1089.237492924977
2.98
10.875
0.02977
d
yr
n .3305064343986878 0.0032998 deg/d
Q 3.60991988187102 0.024028 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      4 days  
   first obs. used      2013-09-01  
   last obs. used      2013-09-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .47684  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:44:57  

Additional Information
 Earth MOID = .00137216 au 
 Jupiter MOID = 1.69229 au 
 T_jup = 3.357 
[ 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 26.0   n/a E2013R56  

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