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(2014 RJ11)
Classification: Apollo [NEO]          SPK-ID: 3685819
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3185440868089247 0.00039562  
a 1.329790554727124 0.0005278 au
q .9061936368244391 0.00016642 au
i 2.015648531968358 0.0014693 deg
node 336.0156823455256 0.11335 deg
peri 65.25218210528153 0.13747 deg
M 235.9851327570615 1.0007 deg
tp 2459193.449894151756
(2020-Dec-09.94989415)
1.6718 TDB
period 560.1099564825546
1.53
0.33347
0.000913
d
yr
n .6427309420828207 0.00038266 deg/d
Q 1.753387472629809 0.00069593 au
  Orbit Determination Parameters
   # obs. used (total)      28  
   data-arc span      4 days  
   first obs. used      2014-09-03  
   last obs. used      2014-09-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48215  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:38:47  

Additional Information
 Earth MOID = .00681305 au 
 Jupiter MOID = 3.65702 au 
 T_jup = 4.871 
[ 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 27.3   n/a MPO311498  

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