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249105 (2007 VV292)
Classification: Main-belt Asteroid          SPK-ID: 2249105
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2187446208779021 5.4865e-08  
a 2.777816353508935 2.5197e-08 au
q 2.170183968392187 1.5186e-07 au
i 10.1375183915122 4.3323e-06 deg
node 100.8553720554143 3.4701e-05 deg
peri 290.2755598297151 3.598e-05 deg
M 267.3493590075861 1.2318e-05 deg
tp 2459435.710785796644
(2021-Aug-09.21078580)
6.136e-05 TDB
period 1691.039384170263
4.63
2.3009e-05
6.3e-08
d
yr
n .2128868217795175 2.8966e-09 deg/d
Q 3.385448738625684 3.0709e-08 au
  Orbit Determination Parameters
   # obs. used (total)      262  
   data-arc span      6120 days (16.76 yr)  
   first obs. used      2002-08-20  
   last obs. used      2019-05-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .60105  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-25 10:19:47  

Additional Information
 Earth MOID = 1.20115 au 
 Jupiter MOID = 2.12967 au 
 T_jup = 3.277 
[ 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 16.0   n/a MPO476001  
diameter diameter 4.347 km 0.536 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.037   0.013 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

249105 (2007 VV292)          Discovered 2007-Nov-15 by CSS at Catalina
Reference: 20100824/Numbers.arcLast Updated: 2010-08-27

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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