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JPL Small-Body Database Browser
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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2905520090102858 3.9118e-05  
a 1.323192165900588 7.1821e-05 au
q .938736023791501 9.8672e-07 au
i 3.970026227223959 0.00040298 deg
node 77.11202624148765 3.6062e-05 deg
peri 228.4814780263203 0.0024508 deg
M 295.2232610818139 0.051554 deg
tp 2458700.534403742008
(2019-Aug-05.03440374)
0.087759 TDB
period 555.9462539879783
1.52
0.045264
0.0001239
d
yr
n .6475446096049864 5.2722e-05 deg/d
Q 1.707648308009676 9.2689e-05 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 = .000274248 au 
 Jupiter MOID = 3.5278 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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