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86058 (1999 RO15)
Classification: Main-belt Asteroid          SPK-ID: 2086058
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09425868760872132 7.1981e-08  
a 3.122329987762722 2.5889e-08 au
q 2.828023260834853 2.2202e-07 au
i 22.7868716023458 7.6661e-06 deg
node 345.9102944961314 1.2704e-05 deg
peri 335.130691158801 3.8252e-05 deg
M 291.301118368218 4.1294e-05 deg
tp 2459385.059720493917
(2021-Jun-19.55972049)
0.00023368 TDB
period 2015.192912744059
5.52
2.5064e-05
6.862e-08
d
yr
n .1786429466496055 2.2219e-09 deg/d
Q 3.416636714690591 2.833e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1009  
   data-arc span      7194 days (19.70 yr)  
   first obs. used      1999-08-12  
   last obs. used      2019-04-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5168  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 04:51:08  

Additional Information
 Earth MOID = 1.82923 au 
 Jupiter MOID = 2.01286 au 
 T_jup = 3.088 
[ 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 13.6   n/a MPO468831  
diameter diameter 10.709 km 0.113 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.056   0.006 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

86058 (1999 RO15)          Discovered 1999-Sep-07 by LINEAR at Socorro
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

Alternate Designations
 1999 RO15 = 2000 XF45 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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