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JPL Small-Body Database Browser
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6696 Eubanks (1986 RC1)
Classification: Main-belt Asteroid          SPK-ID: 2006696
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1927767120257731 3.5879e-08  
a 2.676438332106658 1.2512e-08 au
q 2.160483350503392 9.5305e-08 au
i 1.73725561419216 4.0379e-06 deg
node 4.596029689003026 0.00012613 deg
peri 297.2925576531848 0.00012654 deg
M 291.3853302905191 1.3102e-05 deg
tp 2459305.323724403824
(2021-Mar-31.82372440)
5.9145e-05 TDB
period 1599.316024547062
4.38
1.1215e-05
3.07e-08
d
yr
n .2250962251828589 1.5785e-09 deg/d
Q 3.192393313709923 1.4924e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1855  
   data-arc span      13586 days (37.20 yr)  
   first obs. used      1982-10-25  
   last obs. used      2020-01-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .495  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jan-28 20:33:14  

Additional Information
 Earth MOID = 1.14575 au 
 Jupiter MOID = 2.04502 au 
 T_jup = 3.351 
[ 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 13.7   n/a MPO384815  
diameter diameter 8.967 km 0.193 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.167   0.037 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

6696 Eubanks (1986 RC1)          Discovered 1986-Sep-01 by Oak Ridge Observatory at Harvard
Reference: DISCOVERY.DBLast Updated: 2003-08-29

Alternate Designations
 1986 RC1 = 1982 UE11 = 1986 TE17 = 1990 HZ3 = 1990 MW1 = 1991 XS1 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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