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JPL Small-Body Database Browser
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(2010 AF30)
Classification: Apollo [NEO, PHA]          SPK-ID: 3485260
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3716194524828897 7.6151e-08  
a 1.324695768276134 1.8773e-08 au
q .8324130521629559 9.4007e-08 au
i 3.058944699981754 1.6378e-05 deg
node 62.43135572774963 0.00025539 deg
peri 162.8006757101111 0.0002693 deg
M 318.5372042703646 4.539e-05 deg
tp 2458664.639966927645
(2019-Jun-30.13996693)
7.1442e-05 TDB
period 556.8941429930757
1.52
1.1838e-05
3.241e-08
d
yr
n .6464424245246124 1.3742e-08 deg/d
Q 1.816978484389312 2.5749e-08 au
  Orbit Determination Parameters
   # obs. used (total)      95  
   data-arc span      2143 days (5.87 yr)  
   first obs. used      2010-01-10  
   last obs. used      2015-11-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .4972  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:58:37  

Additional Information
 Earth MOID = .0433459 au 
 Jupiter MOID = 3.16656 au 
 T_jup = 4.863 
[ 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 21.7   n/a E2013Q36  
rotation period rot_per 2.60 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:
[Thirouin, A.; Moskovitz, N.; Binzel, R.P.; Christensen, E.; et al. (2016) Astron. J. 152, A163.]

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