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80595 (2000 AO145)
Classification: Main-belt Asteroid          SPK-ID: 2080595
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09366051285335784 3.7839e-08  
a 2.289046449732391 9.2811e-09 au
q 2.074653185305297 9.0138e-08 au
i 7.565512621204068 3.8253e-06 deg
node 99.3192038193131 3.3549e-05 deg
peri 344.9860372278291 4.1556e-05 deg
M 244.742194867983 2.569e-05 deg
tp 2459005.493617891633
(2020-Jun-04.99361789)
9.1069e-05 TDB
period 1264.970318270335
3.46
7.6933e-06
2.106e-08
d
yr
n .2845916578439945 1.7308e-09 deg/d
Q 2.503439714159485 1.015e-08 au
  Orbit Determination Parameters
   # obs. used (total)      980  
   data-arc span      7773 days (21.28 yr)  
   first obs. used      1998-08-19  
   last obs. used      2019-11-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53239  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 07:47:05  

Additional Information
 Earth MOID = 1.09185 au 
 Jupiter MOID = 2.65935 au 
 T_jup = 3.582 
[ 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 15.2   n/a MPO296688  
diameter diameter 1.941 km 0.310 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.469   0.176 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

80595 (2000 AO145)          Discovered 2000-Jan-06 by LINEAR at Socorro
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

Alternate Designations
 2000 AO145 = 2002 UM29 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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