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(2015 VE66)
Classification: Apollo [NEO]          SPK-ID: 3734183
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4998241075722297 8.681e-05  
a 2.011079043115284 0.00034659 au
q 1.005893255132973 1.2277e-06 au
i 6.116640160311341 0.0007991 deg
node 238.3194790009881 0.00013002 deg
peri 187.4860195074439 0.00045763 deg
M 278.6733493525017 0.16477 deg
tp 2459435.827414524715
(2021-Aug-09.32741452)
0.53762 TDB
period 1041.698736569125
2.85
0.26929
0.0007373
d
yr
n .3455893603036074 8.9337e-05 deg/d
Q 3.016264831097594 0.00051982 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 = .0200072 au 
 Jupiter MOID = 2.32711 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. 2020-October); 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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