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JPL Small-Body Database Browser
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136002 (2002 VZ43)
Classification: Main-belt Asteroid          SPK-ID: 2136002
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 .2104527175277635 4.9126e-08  
a 2.680055182927259 1.6524e-08 au
q 2.11603028655585 1.3663e-07 au
i 10.59643914911921 4.7004e-06 deg
node 290.9165515858062 2.6575e-05 deg
peri 49.92566137901409 2.8965e-05 deg
M 323.7281150117732 9.7516e-06 deg
tp 2458761.966211809006
(2019-Oct-05.46621181)
4.3261e-05 TDB
period 1602.559014236766
4.39
1.4821e-05
4.058e-08
d
yr
n .2246407132603809 2.0776e-09 deg/d
Q 3.244080079298667 2.0002e-08 au
  Orbit Determination Parameters
   # obs. used (total)      693  
   data-arc span      6289 days (17.22 yr)  
   first obs. used      2002-08-10  
   last obs. used      2019-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .497  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 16:00:21  

Additional Information
 Earth MOID = 1.12301 au 
 Jupiter MOID = 2.19676 au 
 T_jup = 3.321 
[ 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 15.0   n/a MPO436668  
diameter diameter 6.213 km 0.047 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.055   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

136002 (2002 VZ43)          Discovered 2002-Nov-04 by NEAT at Palomar
Reference: 20060907/Numbers.arcLast Updated: 2006-09-10
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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