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JPL Small-Body Database Browser
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(2016 NK33)
Classification: Apollo [NEO]          SPK-ID: 3755348
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 2457582.5 (2016-Jul-13.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5332702137490133 0.0029529  
a 2.102485117713985 0.013057 au
q .9812924295865287 0.00011614 au
i 3.562325229825313 0.014233 deg
node 105.3150454511056 0.0012144 deg
peri 221.2834095505417 0.0098029 deg
M 350.5346502678761 0.096354 deg
tp 2457611.777364983314
(2016-Aug-11.27736498)
0.025619 TDB
period 1113.519488690679
3.05
10.373
0.0284
d
yr
n .323299236031605 0.0030117 deg/d
Q 3.223677805841441 0.02002 au
  Orbit Determination Parameters
   # obs. used (total)      18  
   data-arc span      2 days  
   first obs. used      2016-07-12  
   last obs. used      2016-07-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .61228  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-19 05:26:11  

Additional Information
 Earth MOID = .0160614 au 
 Jupiter MOID = 2.1372 au 
 T_jup = 3.548 
[ 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 25.9   n/a MPO384683  

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