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(2015 YC10)
Classification: Apollo [NEO]          SPK-ID: 3739065
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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6373754316469242 0.00070849  
a 2.242311893353466 0.0041488 au
q .8131173824402687 8.4222e-05 au
i 5.324710558794571 0.0044277 deg
node 285.8550262892617 0.0014173 deg
peri 236.4317490463861 0.00096009 deg
M 100.8978291735405 1.2675 deg
tp 2458656.766564085040
(2019-Jun-22.26656409)
3.3641 TDB
period 1226.429130765047
3.36
3.4038
0.009319
d
yr
n .293535102004167 0.00081467 deg/d
Q 3.671506404266663 0.0067932 au
  Orbit Determination Parameters
   # obs. used (total)      62  
   data-arc span      5 days  
   first obs. used      2015-12-31  
   last obs. used      2016-01-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .56425  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:29:34  

Additional Information
 Earth MOID = .000255613 au 
 Jupiter MOID = 1.37952 au 
 T_jup = 3.328 
[ 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 24.9   n/a E2016A38  

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