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(2016 LT10)
Classification: Apollo [NEO]          SPK-ID: 3753871
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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .280560376782462 0.0001849  
a 1.406158329008241 0.00035661 au
q 1.011646018405892 3.4408e-06 au
i .9802977058674108 0.00057627 deg
node 191.5153128493996 0.0062857 deg
peri 89.50718657116815 0.0055185 deg
M 125.8129619061001 0.32136 deg
tp 2458787.650493178883
(2019-Oct-31.15049318)
0.46271 TDB
period 609.0455331048588
1.67
0.23169
0.0006343
d
yr
n .5910888109871731 0.00022486 deg/d
Q 1.80067063961059 0.00045667 au
  Orbit Determination Parameters
   # obs. used (total)      22  
   data-arc span      10 days  
   first obs. used      2016-06-05  
   last obs. used      2016-06-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .63859  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:25  

Additional Information
 Earth MOID = .0169244 au 
 Jupiter MOID = 3.33553 au 
 T_jup = 4.698 
[ 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 26.9   n/a MPO386983  

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