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47495 (2000 AD43)
Classification: Main-belt Asteroid          SPK-ID: 2047495
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1156616807200573 5.529e-08  
a 2.60493585010229 1.2955e-08 au
q 2.303644591511528 1.4553e-07 au
i 16.7824522839444 5.478e-06 deg
node 116.7552775457406 1.6266e-05 deg
peri 26.36730146903313 2.4063e-05 deg
M 275.2307924979248 1.8006e-05 deg
tp 2459362.100979459915
(2021-May-27.60097946)
7.7699e-05 TDB
period 1535.656123744963
4.20
1.1455e-05
3.136e-08
d
yr
n .2344274831021919 1.7487e-09 deg/d
Q 2.906227108693052 1.4453e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1346  
   data-arc span      8833 days (24.18 yr)  
   first obs. used      1995-11-18  
   last obs. used      2020-01-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47963  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 08:48:47  

Additional Information
 Earth MOID = 1.32736 au 
 Jupiter MOID = 2.17512 au 
 T_jup = 3.343 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 13.8   n/a MPO395451  
diameter diameter 5.724 km 0.182 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.215   0.026 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

47495 (2000 AD43)          Discovered 2000-Jan-05 by LINEAR at Socorro
Reference: 20020921/Numbers.arcLast Updated: 2004-04-19

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