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(2013 VJ11)
Classification: Apollo [NEO]          SPK-ID: 3653605
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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4040942994326659 2.6806e-06  
a 1.507373084479473 6.4735e-06 au
q .8982522139230839 1.098e-06 au
i .1982361511962228 5.2931e-05 deg
node 82.37764775233747 0.010637 deg
peri 276.2640631729601 0.010704 deg
M 215.1716171518868 0.008502 deg
tp 2459272.444789385087
(2021-Feb-26.94478938)
0.017716 TDB
period 675.9733296290599
1.85
0.0043545
1.192e-05
d
yr
n .5325653901131718 3.4307e-06 deg/d
Q 2.116493955035863 9.0895e-06 au
  Orbit Determination Parameters
   # obs. used (total)      24  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      2 days  
   first obs. used      2013-11-09  
   last obs. used      2013-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .24699  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:43:45  

Additional Information
 Earth MOID = .00199841 au 
 Jupiter MOID = 3.3355 au 
 T_jup = 4.437 
[ 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 27.9   n/a MPO275431  

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