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308680 (2006 DY62)
Classification: Outer Main-belt Asteroid          SPK-ID: 2308680
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4271686769231644 9.223e-08  
a 3.261583539976479 2.6229e-08 au
q 1.868337214530356 2.9087e-07 au
i 24.03836815631236 9.2422e-06 deg
node 61.83354903594829 1.2481e-05 deg
peri 167.0660777758963 1.4085e-05 deg
M 127.5873767161411 4.8296e-06 deg
tp 2458237.988506431348
(2018-Apr-29.48850643)
2.4947e-05 TDB
period 2151.499190201527
5.89
2.5953e-05
7.106e-08
d
yr
n .1673251849870692 2.0184e-09 deg/d
Q 4.654829865422603 3.7433e-08 au
  Orbit Determination Parameters
   # obs. used (total)      721  
   data-arc span      9453 days (25.88 yr)  
   first obs. used      1994-01-11  
   last obs. used      2019-11-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .41401  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 18:56:54  

Additional Information
 Earth MOID = .862774 au 
 Jupiter MOID = .409745 au 
 T_jup = 2.903 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.5   n/a MPO455273  

308680 (2006 DY62)          Discovered 2006-Feb-25 by Lowe, A. at Mayhill
Reference: 20111210/Numbers.arcLast Updated: 2011-12-12

Alternate Designations
 2006 DY62 = 2000 HJ84 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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