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16633 (1993 OV5)
Classification: Main-belt Asteroid          SPK-ID: 2016633
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08616453547403748 3.6531e-08  
a 2.257376199197334 9.4304e-09 au
q 2.062870427603348 8.2468e-08 au
i 3.733138753414107 3.87e-06 deg
node 123.0283537411857 6.3285e-05 deg
peri 97.45565909714011 6.7748e-05 deg
M 98.40909363484982 2.4936e-05 deg
tp 2458861.860923912742
(2020-Jan-13.36092391)
8.5399e-05 TDB
period 1238.808964583743
3.39
7.7629e-06
2.125e-08
d
yr
n .2906017071978205 1.821e-09 deg/d
Q 2.45188197079132 1.0243e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1130  
   data-arc span      10408 days (28.50 yr)  
   first obs. used      1992-02-23  
   last obs. used      2020-08-22  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .56028  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 01:37:20  

Additional Information
 Earth MOID = 1.05732 au 
 Jupiter MOID = 2.5192 au 
 T_jup = 3.615 
[ 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 15.51   n/a E2021B10  
diameter diameter 1.841 km 0.332 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.395   0.148 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

16633 (1993 OV5)          Discovered 1993-Jul-20 by Elst, E. W. at La Silla
Reference: 20000913/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1993 OV5 = 1996 KA4 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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