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160284 (2003 AX67)
Classification: Main-belt Asteroid          SPK-ID: 2160284
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1788415419733137 4.9301e-08  
a 2.311587409574177 1.1801e-08 au
q 1.898179552839833 1.1648e-07 au
i 4.026140995566347 5.5724e-06 deg
node 122.2422282009075 7.8302e-05 deg
peri 347.2583850964817 8.067e-05 deg
M 229.3749573508242 2.2181e-05 deg
tp 2459066.287523987856
(2020-Aug-04.78752399)
8.1202e-05 TDB
period 1283.701082387254
3.51
9.8306e-06
2.691e-08
d
yr
n .2804391185294637 2.1476e-09 deg/d
Q 2.72499526630852 1.3912e-08 au
  Orbit Determination Parameters
   # obs. used (total)      249  
   data-arc span      8718 days (23.87 yr)  
   first obs. used      1995-12-18  
   last obs. used      2019-10-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59807  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 18:39:21  

Additional Information
 Earth MOID = .915345 au 
 Jupiter MOID = 2.39248 au 
 T_jup = 3.559 
[ 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 16.8   n/a MPO454060  
diameter diameter 1.242 km 0.173 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.199   0.043 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

160284 (2003 AX67)          Discovered 2003-Jan-08 by LINEAR at Socorro
Reference: 20070730/Numbers.arcLast Updated: 2007-08-06

Alternate Designations
 2003 AX67 = 1995 YM25 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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