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71751 (2000 RS10)
Classification: Main-belt Asteroid          SPK-ID: 2071751
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06390243795393538 3.4067e-08  
a 2.31116663839405 9.9756e-09 au
q 2.163477455682869 7.8591e-08 au
i 7.567721093803521 3.8656e-06 deg
node 95.63635329438191 3.1936e-05 deg
peri 6.625776841779764 4.6836e-05 deg
M 65.87491803199453 3.397e-05 deg
tp 2458365.664957437670
(2018-Sep-04.16495744)
0.00012092 TDB
period 1283.350596070249
3.51
8.3089e-06
2.275e-08
d
yr
n .2805157071671271 1.8162e-09 deg/d
Q 2.458855821105232 1.0613e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1068  
   data-arc span      7741 days (21.19 yr)  
   first obs. used      1998-02-26  
   last obs. used      2019-05-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52496  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 05:37:20  

Additional Information
 Earth MOID = 1.18067 au 
 Jupiter MOID = 2.62937 au 
 T_jup = 3.570 
[ 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 15.1   n/a MPO324929  
diameter diameter 2.416 km 0.549 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.364   0.123 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

71751 (2000 RS10)          Discovered 2000-Sep-01 by LINEAR at Socorro
Reference: 20031109/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 RS10 = 1998 FW89 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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