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67247 (2000 EA82)
Classification: Main-belt Asteroid          SPK-ID: 2067247
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1215003835772595 5.7537e-08  
a 2.306272670762262 7.5582e-09 au
q 2.026059656630897 1.3226e-07 au
i 4.020835546841517 3.6676e-06 deg
node 55.85852653628606 7.0831e-05 deg
peri 110.3156964813135 7.1953e-05 deg
M 336.5163954091112 1.2406e-05 deg
tp 2459283.950062129236
(2021-Mar-10.45006213)
4.4074e-05 TDB
period 1279.276452226621
3.50
6.2887e-06
1.722e-08
d
yr
n .2814090725842788 1.3834e-09 deg/d
Q 2.586485684893628 8.4765e-09 au
  Orbit Determination Parameters
   # obs. used (total)      933  
   data-arc span      8224 days (22.52 yr)  
   first obs. used      1998-09-17  
   last obs. used      2021-03-24  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .52348  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 07:03:40  

Additional Information
 Earth MOID = 1.03663 au 
 Jupiter MOID = 2.38576 au 
 T_jup = 3.575 
[ 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 15.91   n/a MPCxxxxx  
diameter diameter 1.900 km 0.148 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.178   0.014 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67247 (2000 EA82)          Discovered 2000-Mar-05 by LINEAR at Socorro
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 EA82 = 1998 SV17 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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