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(2014 DH10)
Classification: Amor [NEO]          SPK-ID: 3662290
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 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3747557184449533 6.8621e-05  
a 1.7055115791868 0.00020569 au
q 1.066361362012464 1.157e-05 au
i 1.480179223190915 0.00021759 deg
node 340.9370796975351 0.00011136 deg
peri 182.171861890277 0.00036799 deg
M 288.6468533812372 0.1831 deg
tp 2459161.746785078022
(2020-Nov-08.24678508)
0.44295 TDB
period 813.54285520498
2.23
0.14717
0.0004029
d
yr
n .442508956592452 8.005e-05 deg/d
Q 2.344661796361136 0.00028277 au
  Orbit Determination Parameters
   # obs. used (total)      35  
   data-arc span      61 days  
   first obs. used      2014-02-22  
   last obs. used      2014-04-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .31448  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:22  

Additional Information
 Earth MOID = .0743594 au 
 Jupiter MOID = 2.63651 au 
 T_jup = 4.112 
[ 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 25.8   n/a MPO297947  
rotation period rot_per 0.2662 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Published Reference List:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

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