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(2016 LP10)
Classification: Apollo [NEO]          SPK-ID: 3753859
[ 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 2457548.5 (2016-Jun-09.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .622228404087478 0.0014165  
a 2.083278623027174 0.0069896 au
q .7870034901514169 0.00031045 au
i .6694925940730656 0.0011718 deg
node 79.30212768104998 0.00084048 deg
peri 245.3235309075902 0.0011241 deg
M 345.433057315906 0.08439 deg
tp 2457592.941158713464
(2016-Jul-23.44115871)		 0.033801 TDB
period 1098.296154780403
3.01		 5.5273
0.01513		 d
yr
n .3277804428551236 0.0016496 deg/d
Q 3.379553755902931 0.011339 au
   Orbit Determination Parameters
   # obs. used (total)      13  
   data-arc span      1 day  
   first obs. used      2016-06-08  
   last obs. used      2016-06-09  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .54642  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 17:09:17  

Additional Information
 Earth MOID = 8.52318E-6 au 
 Jupiter MOID = 1.97439 au 
 T_jup = 3.488 
[ 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 29.3   n/a MPO381224  

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