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JPL Small-Body Database Browser
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(2014 YN)
Classification: Aten [NEO]          SPK-ID: 3702671
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 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1341493703949256 1.1513e-05  
a .8923135137909213 6.4255e-06 au
q .7726102177209855 1.5837e-05 au
i 1.208753509347485 9.9414e-05 deg
node 239.360399656247 0.00050374 deg
peri 15.89117553002407 0.00023018 deg
M 1.647863932900981 0.028023 deg
tp 2458999.090732359236
(2020-May-29.59073236)
0.02395 TDB
period 307.875147059061
0.84
0.0033255
9.105e-06
d
yr
n 1.169305166197581 1.263e-05 deg/d
Q 1.012016809860857 7.2875e-06 au
  Orbit Determination Parameters
   # obs. used (total)      83  
   data-arc span      51 days  
   first obs. used      2014-12-03  
   last obs. used      2015-01-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .46671  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:10:29  

Additional Information
 Earth MOID = .00524875 au 
 Jupiter MOID = 3.99277 au 
 T_jup = 6.652 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457022.5 (2014-Dec-31.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1355568939879209 1.1252e-05  
q .7703502616481159 1.6139e-05 au
tp 2457152.070775631227
(2015-May-09.57077563)
0.0015751 TDB
node 240.1097955506016 0.0002951 deg
peri 15.53600876240218 5.8611e-05 deg
i 1.218115572136759 0.00010167 deg
  Orbit Determination Parameters
   # obs. used (total)      83  
   data-arc span      51 days  
   first obs. used      2014-12-03  
   last obs. used      2015-01-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .46671  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:10:29  

Additional Information
 Jupiter MOID = 3.99277 au 
 T_jup = 6.652 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.266165388138981E-10 -1.81600281891788E-10 -1.772271043323497E-8 3.257555151867344E-9 2.685644013747704E-10 1.143885649426374E-9
q -1.81600281891788E-10 2.60461478205567E-10 2.541851706515743E-8 -4.672652066480004E-9 -3.851545513596465E-10 -1.640626773788554E-9
tp -1.772271043323497E-8 2.541851706515743E-8 2.480997475569584E-6 -4.556197313704531E-7 -3.755649139125455E-8 -1.60105376618278E-7
node 3.257555151867344E-9 -4.672652066480004E-9 -4.556197313704531E-7 8.708484880014072E-8 4.068482001115631E-9 2.951617100167448E-8
peri 2.685644013747704E-10 -3.851545513596465E-10 -3.755649139125455E-8 4.068482001115631E-9 3.435269867153281E-9 2.34595865536412E-9
i 1.143885649426374E-9 -1.640626773788554E-9 -1.60105376618278E-7 2.951617100167448E-8 2.34595865536412E-9 1.033742010893447E-8

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 25.7   n/a MPCxxxxx  

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