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6336 Dodo (1992 UU)
Classification: Main-belt Asteroid          SPK-ID: 2006336
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 47 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09757577476452321 1.8211e-08  
a 2.472951516765065 7.9288e-09 au
q 2.231651356561611 4.4629e-08 au
i 9.493898888911621 1.3489e-06 deg
node 24.27454573248266 2.1612e-06 deg
peri 359.657346342284 1.0799e-05 deg
M 142.9339467013556 8.9447e-06 deg
tp 2458832.531672539965
(2019-Dec-15.03167254)
3.4963e-05 TDB
period 1420.436520302753
3.89
6.8313e-06
1.87e-08
d
yr
n .2534432161201187 1.2189e-09 deg/d
Q 2.714251676968519 8.7025e-09 au
  Orbit Determination Parameters
   # obs. used (total)      2737  
   data-arc span      24735 days (67.72 yr)  
   first obs. used      1953-10-08  
   last obs. used      2021-06-28  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .40598  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 00:30:36  

Additional Information
 Earth MOID = 1.23441 au 
 Jupiter MOID = 2.71342 au 
 T_jup = 3.458 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457498.5 (2016-Apr-20.0) TDB
Reference: JPL 47 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09800273971285878 1.8362e-08  
q 2.230177428519606 4.5012e-08 au
tp 2457408.093886862687
(2016-Jan-20.59388686)
3.4495e-05 TDB
node 24.32355979111179 2.159e-06 deg
peri 358.6562920146492 1.0674e-05 deg
i 9.502666641424099 1.3495e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      2737  
   data-arc span      24735 days (67.72 yr)  
   first obs. used      1953-10-08  
   last obs. used      2021-06-28  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .40598  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 00:30:36  

Additional Information
 Jupiter MOID = 2.71342 au 
 T_jup = 3.458 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.371728827040847E-16 -8.163397303320571E-16 -2.006832275028451E-13 2.106619112560459E-14 -6.652637142088243E-14 -7.944355388114787E-15
q -8.163397303320571E-16 2.026070034041787E-15 4.723111581545845E-13 -5.183749469751926E-14 1.570250999269622E-13 1.978979514144553E-14
tp -2.006832275028451E-13 4.723111581545845E-13 1.189933112824975E-9 -2.164147812980423E-11 3.638644410945259E-10 2.873618854170868E-11
node 2.106619112560459E-14 -5.183749469751926E-14 -2.164147812980423E-11 4.661400854150404E-12 -9.559272484259007E-12 1.057730189891287E-13
peri -6.652637142088243E-14 1.570250999269622E-13 3.638644410945259E-10 -9.559272484259007E-12 1.139248834232489E-10 8.146631308637381E-12
i -7.944355388114787E-15 1.978979514144553E-14 2.873618854170868E-11 1.057730189891287E-13 8.146631308637381E-12 1.821157010719143E-12

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 13.19   n/a MPO614063  
diameter diameter 8.704 km 0.215 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.161   0.042 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

6336 Dodo           Discovered 1992 Oct. 21 by S. Otomo at Kiyosato.
Named for a large, flightless bird first discovered in 1507 on the island of Mauritius and extinct since the seventeenth century.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: 19990728/MPCPages.arcLast Updated: 2010-06-11

Alternate Designations
 1992 UU = 1953 TN1 = 1975 GQ = 1982 BA6 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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