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JPL Small-Body Database Browser
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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5353170367907629 0.00063127  
a 1.939608396028127 0.002587 au
q .9013029769318655 2.2414e-05 au
i 27.55122283699492 0.017316 deg
node 98.51679222705373 0.00045403 deg
peri 42.10813142318007 0.011783 deg
M 204.5307660507313 1.1162 deg
tp 2459026.599934885487
(2020-Jun-26.09993489)
3.9118 TDB
period 986.6645165874439
2.70
1.974
0.005405
d
yr
n .3648656599561567 0.00072996 deg/d
Q 2.977913815124388 0.0039718 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 = .00653368 au 
 Jupiter MOID = 2.34637 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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