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JPL Small-Body Database Browser
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(2013 AV60)
Classification: Apollo [NEO]          SPK-ID: 3623952
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.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 35 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7320589414506204 6.3344e-08  
a 2.064659909774923 9.7849e-09 au
q .5532071617695593 1.3083e-07 au
i 7.371428138582302 6.8231e-06 deg
node 197.6602965244189 0.00011623 deg
peri 150.7150770813208 0.0001156 deg
M 62.4955486979358 5.8781e-06 deg
tp 2458412.387437693227
(2018-Oct-20.88743769)
1.6728e-05 TDB
period 1083.605534175827
2.97
7.7032e-06
2.109e-08
d
yr
n .3322242168814781 2.3617e-09 deg/d
Q 3.576112657780286 1.6948e-08 au
  Orbit Determination Parameters
   # obs. used (total)      194  
   data-arc span      2209 days (6.05 yr)  
   first obs. used      2013-01-09  
   last obs. used      2019-01-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .40485  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Feb-01 07:37:59  

Additional Information
 Earth MOID = .108381 au 
 Jupiter MOID = 1.89443 au 
 T_jup = 3.371 
[ 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 18.6   n/a MPO369170  
rotation period rot_per 3.2 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Vaduvescu, O.; Aznar Macias, A.; Tudor, V.; Predatu, M.; et al. (2017) Earth, Moon, and Planets 120, 41-100.]

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