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(2016 LT1)
Classification: Apollo [NEO]          SPK-ID: 3753700
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 .2905852729528419 4.4267e-05  
a 1.323366739253503 8.6336e-05 au
q .9388158541108113 2.7305e-06 au
i 3.969740781856844 0.0004665 deg
node 76.86195678483941 0.0018972 deg
peri 228.6907784384231 0.0014424 deg
M 194.2209027398811 0.076874 deg
tp 2459256.562522339973
(2021-Feb-11.06252234)
0.1438 TDB
period 556.0562795063929
1.52
0.054415
0.000149
d
yr
n .6474164815107732 6.3356e-05 deg/d
Q 1.707917624396194 0.00011142 au
  Orbit Determination Parameters
   # obs. used (total)      64  
   data-arc span      3 days  
   first obs. used      2016-06-04  
   last obs. used      2016-06-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .30292  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:25:34  

Additional Information
 Earth MOID = .000624752 au 
 Jupiter MOID = 3.52923 au 
 T_jup = 4.895 
[ 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 29.0   n/a MPO381212  

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