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13299 (1998 RU15)
Classification: Main-belt Asteroid          SPK-ID: 2013299
[ 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 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1133062189538955 3.3557e-08  
a 2.299168291737272 7.2824e-09 au
q 2.038658225861834 7.6542e-08 au
i 5.055810318674713 4.1957e-06 deg
node 175.5045207453956 3.9905e-05 deg
peri 78.57196703008658 4.3864e-05 deg
M 186.6515733519464 1.8961e-05 deg
tp 2459613.657397815100
(2022-Feb-03.15739782)		 6.7747e-05 TDB
period 1273.369868314953
3.49		 6.0499e-06
1.656e-08		 d
yr
n .282714401336029 1.3432e-09 deg/d
Q 2.559678357612709 8.1075e-09 au
   Orbit Determination Parameters
   # obs. used (total)      2061  
   data-arc span      13719 days (37.56 yr)  
   first obs. used      1983-04-05  
   last obs. used      2020-10-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49527  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 02:47:17  

Additional Information
 Earth MOID = 1.03156 au 
 Jupiter MOID = 2.47515 au 
 T_jup = 3.579 
[ 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 14.2   n/a MPO347630  
diameter diameter 4.119 km 0.310 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.287   0.103 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

13299 (1998 RU15)          Discovered 1998-Sep-04 by Beijing Schmidt CCD Asteroid Program at Xinglong
Reference: 20000124/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1998 RU15 = 1983 GE 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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