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35271 (1996 RR3)
Classification: Main-belt Asteroid          SPK-ID: 2035271
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0208052345644949 4.4232e-08  
a 2.42752309645105 9.8801e-09 au
q 2.377017909018657 1.0994e-07 au
i 3.27486057048185 4.6015e-06 deg
node 1.960327127710522 5.4449e-05 deg
peri 171.9007860871054 9.978e-05 deg
M 277.516155265004 8.552e-05 deg
tp 2459317.026356126993
(2021-Apr-12.52635613)
0.0003289 TDB
period 1381.476440287359
3.78
8.4339e-06
2.309e-08
d
yr
n .260590763259862 1.5909e-09 deg/d
Q 2.478028283883443 1.0086e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1409  
   data-arc span      10518 days (28.80 yr)  
   first obs. used      1991-04-13  
   last obs. used      2020-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5201  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 03:46:11  

Additional Information
 Earth MOID = 1.37976 au 
 Jupiter MOID = 2.48109 au 
 T_jup = 3.507 
[ show covariance matrix ]

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 14.9   n/a MPO351076  
diameter diameter 2.777 km 0.417 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.302   0.084 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35271 (1996 RR3)          Discovered 1996-Sep-13 by JPL/GEODSS NEAT at Haleakala
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1996 RR3 = 1998 BF15 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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