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JPL Small-Body Database Browser
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(2014 UL115)
Classification: Apollo [NEO]          SPK-ID: 3694784
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 2456961.5 (2014-Oct-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4832886931080471 0.0014049  
a 1.838838452432773 0.0049291 au
q .9501486199197142 3.6464e-05 au
i 4.143634838555061 0.010365 deg
node 23.90110642742384 0.00896 deg
peri 70.00814850328383 0.0076231 deg
M 341.6933246859319 0.081082 deg
tp 2457007.814904226492
(2014-Dec-16.31490423)
0.018911 TDB
period 910.7806434259635
2.49
3.6621
0.01003
d
yr
n .3952653172841217 0.0015893 deg/d
Q 2.727528284945832 0.0073113 au
  Orbit Determination Parameters
   # obs. used (total)      24  
   data-arc span      23 days  
   first obs. used      2014-10-26  
   last obs. used      2014-11-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .50226  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:47  

Additional Information
 Earth MOID = .0459507 au 
 Jupiter MOID = 2.51327 au 
 T_jup = 3.868 
[ 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 24.2   n/a MPO322373  

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