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(2013 YD48)
Classification: Apollo [NEO]          SPK-ID: 3655555
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5962507994955405 2.5344e-06  
a 1.922034987508344 1.0086e-05 au
q .7760200895480925 8.0676e-07 au
i 3.162293095573354 2.8166e-05 deg
node 248.1900301663933 0.0002077 deg
peri 287.526378833357 0.00018882 deg
M 125.7932987365025 0.0066308 deg
tp 2458660.408822637037
(2019-Jun-25.90882264)
0.01525 TDB
period 973.2857400228048
2.66
0.0076611
2.097e-05
d
yr
n .3698810998623743 2.9115e-06 deg/d
Q 3.068049885468594 1.61e-05 au
  Orbit Determination Parameters
   # obs. used (total)      142  
   data-arc span      183 days  
   first obs. used      2013-12-29  
   last obs. used      2014-06-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .31992  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:43:07  

Additional Information
 Earth MOID = .00432694 au 
 Jupiter MOID = 1.91823 au 
 T_jup = 3.682 
[ 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 22.6   n/a MPO279495  

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