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39070 (2000 VS11)
Classification: Main-belt Asteroid          SPK-ID: 2039070
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06366154169440717 3.8678e-08  
a 2.461739349966027 1.1706e-08 au
q 2.305021227697402 9.9048e-08 au
i .6711804511146929 3.9852e-06 deg
node 134.9211408917324 0.00037195 deg
peri 283.6806383211576 0.00037367 deg
M 12.60478599308328 3.5453e-05 deg
tp 2458951.103690370584
(2020-Apr-11.60369037)
0.00013893 TDB
period 1410.787257819978
3.86
1.0063e-05
2.755e-08
d
yr
n .2551766738780238 1.8201e-09 deg/d
Q 2.618457472234652 1.2451e-08 au
  Orbit Determination Parameters
   # obs. used (total)      810  
   data-arc span      9481 days (25.96 yr)  
   first obs. used      1994-02-10  
   last obs. used      2020-01-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54583  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 05:05:13  

Additional Information
 Earth MOID = 1.31717 au 
 Jupiter MOID = 2.56681 au 
 T_jup = 3.486 
[ 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 15.7   n/a MPO493122  
diameter diameter 2.332 km 0.485 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.169   0.082 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

39070 (2000 VS11)          Discovered 2000-Nov-01 by LINEAR at Socorro
Reference: 20020328/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 VS11 = 1994 CP4 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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