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67182 (2000 BQ28)
Classification: Main-belt Asteroid          SPK-ID: 2067182
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 43 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04816789949332247 1.2665e-08  
a 3.076389840089642 1.769e-08 au
q 2.928206603469925 4.6529e-08 au
i 13.57203823771879 3.6893e-07 deg
node 17.25149575908861 9.1112e-07 deg
peri 230.1340043478358 3.0716e-05 deg
M 204.0698139771425 3.3197e-05 deg
tp 2460054.166375685201
(2023-Apr-19.66637569)
0.00018232 TDB
period 1970.88134815425
5.40
1.7e-05
4.654e-08
d
yr
n .1826593977040493 1.5755e-09 deg/d
Q 3.224573076709358 1.8543e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2017  
   data-arc span      8159 days (22.34 yr)  
   first obs. used      1998-11-16  
   last obs. used      2021-03-19  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .46883  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 07:03:27  

Additional Information
 Earth MOID = 1.93501 au 
 Jupiter MOID = 1.78734 au 
 T_jup = 3.185 
[ 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 13.06   n/a E2021B10  
diameter diameter 6.901 km 0.260 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.281   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67182 (2000 BQ28)          Discovered 2000-Jan-29 by LINEAR at Socorro
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

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