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59969 (1999 RV246)
Classification: Main-belt Asteroid          SPK-ID: 2059969
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07963576671926005 1.0689e-07  
a 3.118582710042368 2.6769e-08 au
q 2.870231984850716 3.3246e-07 au
i 15.40013920848027 1.1776e-05 deg
node 187.3832145617503 2.1361e-05 deg
peri 187.1851866381143 3.8512e-05 deg
M 171.3797744979141 3.2461e-05 deg
tp 2457642.884000952207
(2016-Sep-11.38400095)
0.00017772 TDB
period 2011.566187825748
5.51
2.59e-05
7.091e-08
d
yr
n .1789650284334492 2.3042e-09 deg/d
Q 3.366933435234019 2.89e-08 au
  Orbit Determination Parameters
   # obs. used (total)      436  
   data-arc span      8973 days (24.57 yr)  
   first obs. used      1994-10-06  
   last obs. used      2019-05-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58387  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 03:41:12  

Additional Information
 Earth MOID = 1.87012 au 
 Jupiter MOID = 2.08554 au 
 T_jup = 3.157 
[ 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 14.7   n/a MPO296573  
diameter diameter 5.723 km 0.351 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.085   0.028 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

59969 (1999 RV246)          Discovered 1999-Sep-04 by CSS at Catalina
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 RV246 = 2000 WA175 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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