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101629 (1999 CV24)
Classification: Main-belt Asteroid          SPK-ID: 2101629
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 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0584967443023721 3.8439e-08  
a 2.209104353524587 7.926e-09 au
q 2.079878941019202 8.3719e-08 au
i 7.45450405382176 4.5981e-06 deg
node 31.69175096739056 2.619e-05 deg
peri 112.1948895869679 4.7185e-05 deg
M 226.922799866584 4.0969e-05 deg
tp 2459643.826741117279
(2022-Mar-05.32674112)
0.00013758 TDB
period 1199.286028276944
3.28
6.4543e-06
1.767e-08
d
yr
n .3001785991930753 1.6155e-09 deg/d
Q 2.338329766029972 8.3896e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1229  
   data-arc span      9548 days (26.14 yr)  
   first obs. used      1994-11-05  
   last obs. used      2020-12-26  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .49554  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 15:37:44  

Additional Information
 Earth MOID = 1.10293 au 
 Jupiter MOID = 2.65255 au 
 T_jup = 3.645 
[ 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 15.74   n/a E2021B55  
diameter diameter 2.378 km 0.660 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.216   0.156 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

101629 (1999 CV24)          Discovered 1999-Feb-10 by LINEAR at Socorro
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

Alternate Designations
 1999 CV24 = 2001 YY136 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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