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JPL Small-Body Database Browser
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(2015 VE66)
Classification: Apollo [NEO]          SPK-ID: 3734183
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5003353862531701 8.7262e-05  
a 2.010545714575235 0.00034368 au
q 1.004598547893579 3.7207e-06 au
i 6.122041303516222 0.000801 deg
node 238.3552858639667 4.4235e-05 deg
peri 187.4687098701768 0.00028464 deg
M 209.5601108541061 0.14724 deg
tp 2459435.640853506960
(2021-Aug-09.14085351)
0.53746 TDB
period 1041.284383761999
2.85
0.26699
0.000731
d
yr
n .3457268788564521 8.8647e-05 deg/d
Q 3.016492881256892 0.00051563 au
  Orbit Determination Parameters
   # obs. used (total)      258  
   data-arc span      68 days  
   first obs. used      2015-11-09  
   last obs. used      2016-01-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .36604  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-10 07:07:14  

Additional Information
 Earth MOID = .0193704 au 
 Jupiter MOID = 2.32601 au 
 T_jup = 3.658 
[ 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 24.1   n/a E2016A09  
rotation period rot_per 0.037 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Published Reference List:
[Thirouin, A.; Moskovitz, N.A.; Binzel, R.P.; Christensen, E.J.; et al. (2018) Astrophys. J. Supp. Series 2391, A4.]

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