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47808 (2000 EG67)
Classification: Main-belt Asteroid          SPK-ID: 2047808
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 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1179920951888216 4.01e-08  
a 3.061113352302718 1.8557e-08 au
q 2.699926174254043 1.2744e-07 au
i 2.024346546701956 4.6162e-06 deg
node 296.4052510246985 0.00015716 deg
peri 149.7217470146628 0.00015916 deg
M 3.115434736156579 2.463e-05 deg
tp 2458983.570906581726
(2020-May-14.07090658)
0.00013381 TDB
period 1956.219323052589
5.36
1.7789e-05
4.87e-08
d
yr
n .1840284449487171 1.6735e-09 deg/d
Q 3.422300530351393 2.0747e-08 au
  Orbit Determination Parameters
   # obs. used (total)      873  
   data-arc span      10247 days (28.05 yr)  
   first obs. used      1992-10-25  
   last obs. used      2020-11-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50638  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-17 21:25:10  

Additional Information
 Earth MOID = 1.71646 au 
 Jupiter MOID = 1.77362 au 
 T_jup = 3.222 
[ 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 14.6   n/a MPO502474  
diameter diameter 6.955 km 0.145 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.070   0.014 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

47808 (2000 EG67)          Discovered 2000-Mar-10 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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