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JPL Small-Body Database Browser
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(2007 EV)
Classification: Apollo [NEO]          SPK-ID: 3370286
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3078942774757539 0.00032686  
a 1.090895375201528 0.00016028 au
q .755014931852212 0.00024565 au
i 8.171411852456968 0.0088629 deg
node 357.3600450101798 0.0014622 deg
peri 268.6082636510102 0.00109 deg
M 170.1298442070632 1.0978 deg
tp 2458403.824129394944
(2018-Oct-12.32412939)
1.2258 TDB
period 416.1722109828437
1.14
0.091722
0.0002511
d
yr
n .8650265214724793 0.00019065 deg/d
Q 1.426775818550844 0.00020964 au
  Orbit Determination Parameters
   # obs. used (total)      53  
   data-arc span      5 days  
   first obs. used      2007-03-10  
   last obs. used      2007-03-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .67863  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:06:50  

Additional Information
 Earth MOID = .00379779 au 
 Jupiter MOID = 3.66998 au 
 T_jup = 5.632 
[ 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 25.0   n/a MPO118216  
rotation period rot_per 0.12874 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Result based on fragmentary lightcurve(s), may be completely wrong.
Published Reference List:
[Statler, T.S.; Cotto-Figueroa, D.; Riethmiller, D.A.; Sweeney, K.M. (2013) Icarus 225, 141-155.]

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