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JPL Small-Body Database Browser
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(2015 HD10)
Classification: Apollo [NEO]          SPK-ID: 3717037
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5772784305187872 1.6787e-06  
a 2.071360912283692 7.3341e-06 au
q .8756089358025988 4.6174e-07 au
i 4.449987646759945 1.8714e-05 deg
node 215.8011035146302 1.4116e-05 deg
peri 52.09180024768424 5.7537e-05 deg
M 110.1057011949104 0.0029183 deg
tp 2458267.465367807096
(2018-May-28.96536781)
0.0070581 TDB
period 1088.885192032066
2.98
0.0057831
1.583e-05
d
yr
n .3306133673543413 1.7559e-06 deg/d
Q 3.267112888764784 1.1568e-05 au
  Orbit Determination Parameters
   # obs. used (total)      66  
   # delay obs. used      1  
   # Doppler obs. used      2  
   data-arc span      11 days  
   first obs. used      2015-04-18  
   last obs. used      2015-04-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .30714  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-10 07:06:36  

Additional Information
 Earth MOID = .00285758 au 
 Jupiter MOID = 1.866 au 
 T_jup = 3.539 
[ 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 26.5   n/a MPO337075  

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