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(2017 LV)
Classification: Apollo [NEO]          SPK-ID: 3775204
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 2457919.5 (2017-Jun-15.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4848707161818678 0.00079331  
a 1.77861678021124 0.0025307 au
q .9162175881771287 0.00010737 au
i 4.431056818653816 0.0057144 deg
node 256.3298360989754 0.00069016 deg
peri 58.33611603211295 0.00088649 deg
M 343.1166980244906 0.041619 deg
tp 2457960.132813276251
(2017-Jul-25.63281328)
0.013443 TDB
period 866.4071045266635
2.37
1.8491
0.005063
d
yr
n .4155090581773052 0.00088681 deg/d
Q 2.641015972245352 0.0037578 au
  Orbit Determination Parameters
   # obs. used (total)      65  
   data-arc span      6 days  
   first obs. used      2017-06-13  
   last obs. used      2017-06-19  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .4274  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 19:07:34  

Additional Information
 Earth MOID = .0165443 au 
 Jupiter MOID = 2.68045 au 
 T_jup = 3.945 
[ 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 26.1   n/a MPO412131  

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