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58624 (1997 VC2)
Classification: Main-belt Asteroid          SPK-ID: 2058624
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09491462274867619 3.5742e-08  
a 3.015660191018876 1.8169e-08 au
q 2.729429941650118 1.072e-07 au
i 9.65384507561726 4.1125e-06 deg
node 235.3743640911193 3.1692e-05 deg
peri 195.3804392019065 4.2575e-05 deg
M 92.18212869664075 2.824e-05 deg
tp 2458510.702839127187
(2019-Jan-27.20283913)
0.00014936 TDB
period 1912.810871340164
5.24
1.7286e-05
4.733e-08
d
yr
n .1882047019880093 1.7008e-09 deg/d
Q 3.301890440387633 1.9893e-08 au
  Orbit Determination Parameters
   # obs. used (total)      932  
   data-arc span      8242 days (22.57 yr)  
   first obs. used      1997-10-29  
   last obs. used      2020-05-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54885  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 22:50:22  

Additional Information
 Earth MOID = 1.7448 au 
 Jupiter MOID = 2.0049 au 
 T_jup = 3.220 
[ 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 14.3   n/a MPO385193  
diameter diameter 4.952 km 0.172 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.104   0.019 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

58624 (1997 VC2)          Discovered 1997-Nov-01 by Kobayashi, T. at Oizumi
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1997 VC2 = 2000 JB14 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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