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JPL Small-Body Database Browser
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97820 (2000 OZ49)
Classification: Main-belt Asteroid          SPK-ID: 2097820
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1746641623936563 4.8543e-08  
a 2.239859341167481 8.5691e-09 au
q 1.848636185462856 1.0667e-07 au
i 4.404037552005034 4.2558e-06 deg
node 164.4514484435049 5.934e-05 deg
peri 207.7961318883 6.0581e-05 deg
M 187.0987482375391 1.3083e-05 deg
tp 2459188.564798125117
(2020-Dec-05.06479813)
4.5852e-05 TDB
period 1224.417551446587
3.35
7.0264e-06
1.924e-08
d
yr
n .2940173469211368 1.6872e-09 deg/d
Q 2.631082496872106 1.0066e-08 au
  Orbit Determination Parameters
   # obs. used (total)      836  
   data-arc span      9889 days (27.07 yr)  
   first obs. used      1992-04-09  
   last obs. used      2019-05-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52481  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 06:30:01  

Additional Information
 Earth MOID = .848989 au 
 Jupiter MOID = 2.82893 au 
 T_jup = 3.611 
[ 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 16.1   n/a MPO337972  
diameter diameter 1.677 km 0.367 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.274   0.148 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97820 (2000 OZ49)          Discovered 2000-Jul-31 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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