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(2007 VE3)
Classification: Apollo [NEO]          SPK-ID: 3392303
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6971969228778284 1.3194e-07  
a 2.268680391052235 4.7364e-08 au
q .6869634034173484 3.1359e-07 au
i 1.395832943900845 1.9107e-05 deg
node 343.4583423524059 0.0011646 deg
peri 325.8738247381902 0.0011646 deg
M 263.6704779867417 1.9049e-05 deg
tp 2459334.476037293138
(2021-Apr-29.97603729)
7.6311e-05 TDB
period 1248.125921448895
3.42
3.9086e-05
1.07e-07
d
yr
n .2884324360334505 9.0325e-09 deg/d
Q 3.850397378687122 8.0386e-08 au
  Orbit Determination Parameters
   # obs. used (total)      81  
   data-arc span      2385 days (6.53 yr)  
   first obs. used      2007-11-02  
   last obs. used      2014-05-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5353  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:05:27  

Additional Information
 Earth MOID = .0161346 au 
 Jupiter MOID = 1.45678 au 
 T_jup = 3.240 
[ 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 23.1   n/a MPO322180  

[ show close-approach data ]
Alternate Designations
 2007 VE3 = 2014 HL132 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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