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47806 (2000 EV65)
Classification: Main-belt Asteroid          SPK-ID: 2047806
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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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 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .03867843914249862 4.0599e-08  
a 3.126089445360506 1.8063e-08 au
q 3.005177184994122 1.3113e-07 au
i .91745255404339 4.3686e-06 deg
node 42.24982521986437 0.00023598 deg
peri 358.1956845865348 0.00024168 deg
M 16.98180843703511 5.1035e-05 deg
tp 2458905.268206424339
(2020-Feb-25.76820642)
0.00028628 TDB
period 2018.833613295885
5.53
1.7497e-05
4.79e-08
d
yr
n .1783207876216581 1.5455e-09 deg/d
Q 3.247001705726889 1.8761e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1158  
   data-arc span      10375 days (28.41 yr)  
   first obs. used      1991-09-08  
   last obs. used      2020-02-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5588  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 09:40:51  

Additional Information
 Earth MOID = 2.01262 au 
 Jupiter MOID = 1.92618 au 
 T_jup = 3.213 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456786.5 (2014-May-09.0) TDB
Reference: JPL 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0358225742675702 4.1173e-08  
q 3.013332144882221 1.3211e-07 au
tp 2456851.332302044718
(2014-Jul-12.83230204)
0.00030791 TDB
node 42.15120679085254 0.000235 deg
peri 352.3062468243284 0.00024151 deg
i .9219129136911808 4.366e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1158  
   data-arc span      10375 days (28.41 yr)  
   first obs. used      1991-09-08  
   last obs. used      2020-02-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5588  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 09:40:51  

Additional Information
 Jupiter MOID = 1.92618 au 
 T_jup = 3.213 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.695209551147939E-15 -5.393547711488906E-15 -3.469357671765572E-12 -8.586947234385069E-16 -6.508866238803098E-13 -2.286847142636704E-17
q -5.393547711488906E-15 1.745375542743645E-14 9.986986531185032E-12 -2.292634532176041E-15 1.883510204000294E-12 1.453319341234299E-16
tp -3.469357671765572E-12 9.986986531185032E-12 9.480955123464601E-8 3.286239296790041E-11 1.717265854243737E-8 -1.376685356871614E-12
node -8.586947234385069E-16 -2.292634532176041E-15 3.286239296790041E-11 5.522407985055724E-8 -5.52107742118048E-8 -2.741767368534181E-10
peri -6.508866238803098E-13 1.883510204000294E-12 1.717265854243737E-8 -5.52107742118048E-8 5.832795620474551E-8 2.738985726425595E-10
i -2.286847142636704E-17 1.453319341234299E-16 -1.376685356871614E-12 -2.741767368534181E-10 2.738985726425595E-10 1.906153034281638E-11

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 14.3   n/a MPO502474  
diameter diameter 7.839 km 0.238 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.066   0.012 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

47806 (2000 EV65)          Discovered 2000-Mar-10 by LINEAR at Socorro
Reference: 20020921/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 2000 EV65 = 2000 GZ12 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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