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16764 (1996 TV14)
Classification: Main-belt Asteroid          SPK-ID: 2016764
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06779045469483878 2.9785e-08  
a 2.867327669008819 1.0998e-08 au
q 2.672950222567618 8.5922e-08 au
i 1.488138869711541 3.6861e-06 deg
node 340.5876401675629 0.0001151 deg
peri 334.9921474690278 0.00011852 deg
M 53.39288138969548 2.6764e-05 deg
tp 2458937.476063670267
(2020-Mar-28.97606367)
0.0001322 TDB
period 1773.431487759682
4.86
1.0203e-05
2.793e-08
d
yr
n .202996282903929 1.1679e-09 deg/d
Q 3.061705115450018 1.1744e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1961  
   data-arc span      10720 days (29.35 yr)  
   first obs. used      1991-10-08  
   last obs. used      2021-02-12  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .51412  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 01:41:11  

Additional Information
 Earth MOID = 1.6573 au 
 Jupiter MOID = 2.12727 au 
 T_jup = 3.295 
[ 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 14.04   n/a E2021B10  
diameter diameter 4.126 km 0.137 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.313   0.059 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

16764 (1996 TV14)          Discovered 1996-Oct-09 by Okuni, T. at Nanyo
Reference: 20000913/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1996 TV14 = 1998 BE12 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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