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JPL Small-Body Database Browser
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(2015 CG)
Classification: Apollo [NEO]          SPK-ID: 3709713
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5832754218011265 0.0005238  
a 2.163792315094526 0.0025907 au
q .9017054398177303 5.3947e-05 au
i 4.543631994566877 0.0033197 deg
node 134.4995326912644 0.00014675 deg
peri 50.41332174180808 0.0020825 deg
M 105.6380033439567 0.84204 deg
tp 2458259.354638059368
(2018-May-20.85463806)
2.1066 TDB
period 1162.577163625018
3.18
2.0879
0.005716
d
yr
n .3096568651645351 0.00055613 deg/d
Q 3.425879190371321 0.0041018 au
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      3 days  
   first obs. used      2015-02-07  
   last obs. used      2015-02-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48265  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:35:50  

Additional Information
 Earth MOID = .0135722 au 
 Jupiter MOID = 1.54053 au 
 T_jup = 3.449 
[ 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 25.6   n/a MPO335352  

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