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(2010 AE30)
Classification: Apollo [NEO]          SPK-ID: 3485259
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4167823035705714 2.0757e-08  
a 1.267555177814513 2.9725e-09 au
q .7392606109021751 2.5218e-08 au
i 5.966444236327102 1.1453e-05 deg
node 279.4269527072688 1.8179e-05 deg
peri 278.323108442299 2.2214e-05 deg
M 193.3310078381157 7.6714e-06 deg
tp 2459441.824294843619
(2021-Aug-15.32429484)		 1.1187e-05 TDB
period 521.2532038312207
1.43		 1.8336e-06
5.02e-09		 d
yr
n .6906432370180045 2.4294e-09 deg/d
Q 1.795849744726851 4.2114e-09 au
   Orbit Determination Parameters
   # obs. used (total)      88  
   data-arc span      3678 days (10.07 yr)  
   first obs. used      2009-12-18  
   last obs. used      2020-01-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .39465  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-26 07:26:14  

Additional Information
 Earth MOID = .00783576 au 
 Jupiter MOID = 3.18063 au 
 T_jup = 4.997 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 23.6   n/a MPO170308  
diameter diameter 0.050 km 0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2014ApJ...784..110M)  
geometric albedo albedo 0.259   0.147 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2014ApJ...784..110M)  

[ show close-approach data ]
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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