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(2014 RC)
Classification: Apollo [NEO]          SPK-ID: 3685273
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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Orbit Diagram
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Note: This Java-based orbit viewer will eventually be retired.

Note: Make sure you have Java enabled on your browser to see the applet. This applet is provided as a 3D orbit visualization tool. The applet 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. For accurate long-term ephemerides, please instead use our Horizons system.

Note: If the applet is not working, here are some notes that might help.
Orbit Viewer

Additional Notes: the orbits shown in the applet are color coded. The planets are white lines, and the asteroid/comet is a blue line. The bright white line indicates the portion of the orbit that is above the ecliptic plane, and the darker portion is below the ecliptic plane. Likewise for the asteroid/comet orbit, the light blue indicates the portion above the ecliptic plane, and the dark blue the portion below the ecliptic plane.

Orbit Viewer applet originally written and kindly provided by Osamu Ajiki (AstroArts), and further modified by Ron Baalke (JPL).

Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3748952013517531 6.5276e-07  
a 1.313528775870401 5.021e-07 au
q .8210931409591454 5.7656e-07 au
i 4.569592517408262 5.325e-05 deg
node 344.9305304456344 1.4971e-05 deg
peri 71.13276019668754 7.4484e-05 deg
M 256.1959339716835 0.0022612 deg
tp 2459159.051253002441
0.0035447 TDB
period 549.8671994727878
n .6547035363178013 3.754e-07 deg/d
Q 1.805964410781657 6.9034e-07 au
  Orbit Determination Parameters
   # obs. used (total)      247  
   # delay obs. used      0  
   # Doppler obs. used      2  
   data-arc span      18 days  
   first obs. used      2014-08-20  
   last obs. used      2014-09-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .34772  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:38:48  

Additional Information
 Earth MOID = 4.67311E-5 au 
 Jupiter MOID = 3.56353 au 
 T_jup = 4.890 
[ 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 26.8   n/a MPO311496  
rotation period rot_per 0.004389 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Incomplete or inconclusive result.
Published Reference List:
[NASA/JPL NEO Program Office (2014) news/news185.html]

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