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35082 (1990 RJ3)
Classification: Main-belt Asteroid          SPK-ID: 2035082
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07942270496999121 3.3756e-08  
a 2.238634391302329 8.0077e-09 au
q 2.060835992506248 7.6006e-08 au
i 6.284660036477637 5.236e-06 deg
node 352.0404459700678 3.3965e-05 deg
peri 319.0806857454793 4.8627e-05 deg
M 351.9474841282338 3.6105e-05 deg
tp 2459027.865429745438
(2020-Jun-27.36542975)
0.00012273 TDB
period 1223.413261798018
3.35
6.5643e-06
1.797e-08
d
yr
n .2942587032863429 1.5789e-09 deg/d
Q 2.416432790098409 8.6437e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1436  
   data-arc span      10852 days (29.71 yr)  
   first obs. used      1990-09-14  
   last obs. used      2020-05-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52016  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-23 20:27:42  

Additional Information
 Earth MOID = 1.05173 au 
 Jupiter MOID = 2.771 au 
 T_jup = 3.624 
[ 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 15.0   n/a MPO333131  
diameter diameter 2.144 km 0.298 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.350   0.099 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35082 (1990 RJ3)          Discovered 1990-Sep-14 by Holt, H. E. at Palomar
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1990 RJ3 = 1999 AG25 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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