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17659 (1996 VX5)
Classification: Main-belt Asteroid          SPK-ID: 2017659
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1890589887904756 5.9421e-08  
a 2.624040387881629 1.1745e-08 au
q 2.12794196560336 1.5548e-07 au
i 5.169249147587871 5.9916e-06 deg
node 233.4735406981212 5.7137e-05 deg
peri 180.6767283297018 5.958e-05 deg
M 196.363174570858 1.4652e-05 deg
tp 2459706.220518358127
(2022-May-06.72051836)
6.4406e-05 TDB
period 1552.580758900988
4.25
1.0424e-05
2.854e-08
d
yr
n .2318719963107298 1.5567e-09 deg/d
Q 3.120138810159897 1.3965e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1027  
   data-arc span      10997 days (30.11 yr)  
   first obs. used      1989-03-02  
   last obs. used      2019-04-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51651  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-12 22:22:37  

Additional Information
 Earth MOID = 1.13936 au 
 Jupiter MOID = 2.24204 au 
 T_jup = 3.372 
[ 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 15.0   n/a MPO467896  
diameter diameter 6.332 km 0.090 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.056   0.007 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17659 (1996 VX5)          Discovered 1996-Nov-15 by Kobayashi, T. at Oizumi
Reference: 20001013/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1996 VX5 = 1989 EO4 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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