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JPL Small-Body Database Browser
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32436 (2000 RQ97)
Classification: Main-belt Asteroid          SPK-ID: 2032436
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 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04606227963430433 4.439e-08  
a 2.677963344453651 1.4379e-08 au
q 2.55461024803101 1.1771e-07 au
i 21.11388034165178 5.577e-06 deg
node 295.2918216853469 1.3417e-05 deg
peri 151.6738947739367 6.3906e-05 deg
M 98.15277408534432 6.1743e-05 deg
tp 2458564.079194149730
(2019-Mar-21.57919415)
0.00027387 TDB
period 1600.683134737364
4.38
1.2892e-05
3.53e-08
d
yr
n .2249039751762412 1.8114e-09 deg/d
Q 2.801316440876292 1.5042e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1576  
   data-arc span      11406 days (31.23 yr)  
   first obs. used      1989-02-04  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .45252  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 07:26:41  

Additional Information
 Earth MOID = 1.58029 au 
 Jupiter MOID = 2.34247 au 
 T_jup = 3.280 
[ 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 13.2   n/a MPO431865  
diameter diameter 5.864 km 0.150 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.355   0.084 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

32436 (2000 RQ97)          Discovered 2000-Sep-05 by LONEOS at Anderson Mesa
Reference: 20011130/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 RQ97 = 1989 CN2 = 1994 FT 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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