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115114 (2003 SB39)
Classification: Main-belt Asteroid          SPK-ID: 2115114
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1842618750163552 8.2625e-08  
a 2.885350215458058 2.1424e-08 au
q 2.353690174678912 2.3624e-07 au
i 19.64806327126353 7.2201e-06 deg
node 345.2608025165911 1.5896e-05 deg
peri 30.09519287708634 2.3094e-05 deg
M 180.2107990169534 1.8391e-05 deg
tp 2460094.540781657542
(2023-May-30.04078166)
9.7985e-05 TDB
period 1790.178050944588
4.90
1.9938e-05
5.459e-08
d
yr
n .2010973153257275 2.2397e-09 deg/d
Q 3.417010256237204 2.5371e-08 au
  Orbit Determination Parameters
   # obs. used (total)      594  
   data-arc span      10073 days (27.58 yr)  
   first obs. used      1993-08-20  
   last obs. used      2021-03-19  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .53604  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 08:56:12  

Additional Information
 Earth MOID = 1.36744 au 
 Jupiter MOID = 2.10561 au 
 T_jup = 3.182 
[ 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 14.9   n/a MPO469189  
diameter diameter 7.296 km 0.149 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.053   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

115114 (2003 SB39)          Discovered 2003-Sep-16 by NEAT at Palomar
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

Alternate Designations
 2003 SB39 = 1993 QU6 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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