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277823 (2006 GV50)
Classification: Outer Main-belt Asteroid          SPK-ID: 2277823
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05089397749110774 6.0819e-08  
a 3.20936442039104 5.7183e-08 au
q 3.046027099818897 2.0437e-07 au
i 18.19837340358742 8.3133e-06 deg
node 67.43274959771121 1.9394e-05 deg
peri 102.1139540861529 9.1139e-05 deg
M 118.5559409577356 8.7068e-05 deg
tp 2457908.911443779142
(2017-Jun-04.41144378)
0.00050503 TDB
period 2100.037148946132
5.75
5.6126e-05
1.537e-07
d
yr
n .1714255389151853 4.5816e-09 deg/d
Q 3.372701740963183 6.0093e-08 au
  Orbit Determination Parameters
   # obs. used (total)      354  
   data-arc span      5290 days (14.48 yr)  
   first obs. used      2005-01-07  
   last obs. used      2019-07-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58936  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 04:47:14  

Additional Information
 Earth MOID = 2.10315 au 
 Jupiter MOID = 1.74438 au 
 T_jup = 3.112 
[ 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 MPO450167  
diameter diameter 6.239 km 0.364 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.060   0.014 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

277823 (2006 GV50)          Discovered 2006-Apr-02 by LONEOS at Anderson Mesa
Reference: 20110517/Numbers.arcLast Updated: 2011-05-20

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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