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(2014 DG23)
Classification: Aten [NEO]          SPK-ID: 3662637
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2153918861823517 0.00050262  
a .9143140704108992 6.299e-05 au
q .7173782382220321 0.00050868 au
i 11.8327250810119 0.037837 deg
node 157.1821082328398 0.003244 deg
peri 215.268731753323 0.007594 deg
M 183.8297366866534 0.22071 deg
tp 2459156.768568693682
(2020-Nov-03.26856869)
0.21192 TDB
period 319.3313313590503
0.87
0.033
9.035e-05
d
yr
n 1.127355710659104 0.0001165 deg/d
Q 1.111249902599766 7.6557e-05 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   data-arc span      7 days  
   first obs. used      2014-02-27  
   last obs. used      2014-03-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .56767  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:18  

Additional Information
 Earth MOID = .0534356 au 
 Jupiter MOID = 4.24039 au 
 T_jup = 6.492 
[ 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 25.1   n/a E2014E17  

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