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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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .37472235938184 6.3371e-05  
a 1.705561166198299 0.0001904 au
q 1.06644926193043 1.0967e-05 au
i 1.480139955717954 0.00019961 deg
node 340.9355461053011 0.00010605 deg
peri 182.1644262227747 0.00036148 deg
M 17.1397202038215 0.18312 deg
tp 2459161.765263789974
(2020-Nov-08.26526379)
0.40735 TDB
period 813.5783355728348
2.23
0.13623
0.000373
d
yr
n .4424896586590233 7.4094e-05 deg/d
Q 2.344673070466168 0.00026174 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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .33463  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:21:57  

Additional Information
 Earth MOID = .074179 au 
 Jupiter MOID = 2.63565 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. 2020-October); 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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