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(2014 YC42)
Classification: Apollo [NEO]          SPK-ID: 3703246
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5353383994181822 0.00063451  
a 1.939860721045051 0.0025877 au
q .9013787875465925 2.8553e-05 au
i 27.5513616737803 0.017326 deg
node 98.51679069957569 0.00047552 deg
peri 42.09133585021626 0.011765 deg
M 350.4941471410551 1.4073 deg
tp 2459026.558105481930
(2020-Jun-26.05810548)
3.9101 TDB
period 986.8570566677229
2.70
1.9746
0.005406
d
yr
n .3647944730877198 0.00072993 deg/d
Q 2.978342654543509 0.003973 au
  Orbit Determination Parameters
   # obs. used (total)      47  
   data-arc span      2 days  
   first obs. used      2014-12-29  
   last obs. used      2014-12-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .41426  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:36:34  

Additional Information
 Earth MOID = .00642309 au 
 Jupiter MOID = 2.3447 au 
 T_jup = 3.597 
[ 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 24.8   n/a MPO319078  

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