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24319 (2000 AY15)
Classification: Main-belt Asteroid          SPK-ID: 2024319
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2307422817158978 3.9043e-08  
a 2.461730054297738 1.0039e-08 au
q 1.893704844600477 9.8036e-08 au
i 6.067064405434754 4.2536e-06 deg
node 274.1095632510786 3.3093e-05 deg
peri 359.8545863203076 3.3984e-05 deg
M 328.6113334165249 9.9746e-06 deg
tp 2459323.506888986068
(2021-Apr-19.00688899)
3.9497e-05 TDB
period 1410.779267007712
3.86
8.6295e-06
2.363e-08
d
yr
n .2551781192273731 1.5609e-09 deg/d
Q 3.029755263994999 1.2355e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1438  
   data-arc span      10893 days (29.82 yr)  
   first obs. used      1990-07-25  
   last obs. used      2020-05-21  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .53991  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 04:39:37  

Additional Information
 Earth MOID = .875535 au 
 Jupiter MOID = 2.09696 au 
 T_jup = 3.445 
[ 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 14.49   n/a E2021B10  
diameter diameter 3.528 km 0.608 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  
geometric albedo albedo 0.270   0.063 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  

24319 (2000 AY15)          Discovered 2000-Jan-03 by LINEAR at Socorro
Reference: 20010408/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 AY15 = 1990 OM4 = 1998 QR76 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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