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15063 (1999 AQ3)
Classification: Main-belt Asteroid          SPK-ID: 2015063
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06863774447645178 3.1631e-08  
a 2.898794666028951 1.3116e-08 au
q 2.699827938452354 9.604e-08 au
i 3.521591538122818 4.1626e-06 deg
node 68.57669490382963 5.4831e-05 deg
peri 276.0229389173072 6.262e-05 deg
M 261.470159459334 3.0838e-05 deg
tp 2459493.889481183818
(2021-Oct-06.38948118)
0.00015517 TDB
period 1802.704766916431
4.94
1.2235e-05
3.35e-08
d
yr
n .1996999212554302 1.3554e-09 deg/d
Q 3.097761393605547 1.4016e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1726  
   data-arc span      17418 days (47.69 yr)  
   first obs. used      1972-10-09  
   last obs. used      2020-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52874  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-23 17:47:41  

Additional Information
 Earth MOID = 1.69507 au 
 Jupiter MOID = 2.19071 au 
 T_jup = 3.281 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.0   n/a MPO473970  
diameter diameter 5.254 km 0.303 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.193   0.026 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

15063 (1999 AQ3)          Discovered 1999-Jan-10 by Kobayashi, T. at Oizumi
Reference: 20000523/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1999 AQ3 = 1972 TY8 = 1997 XB7 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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