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JPL Small-Body Database Browser
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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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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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3749961477036146 5.8154e-07  
a 1.313770539701431 2.0183e-07 au
q .8211116483468958 6.5113e-07 au
i 4.568748178167898 5.2695e-05 deg
node 344.9103293197835 1.6369e-05 deg
peri 71.0902826765238 9.4854e-05 deg
M 155.4417208948479 0.002367 deg
tp 2459159.011382037487
(2020-Nov-05.51138204)
0.0035616 TDB
period 550.0190166084197
1.51
0.00012675
3.47e-07
d
yr
n .6545228239922806 1.5083e-07 deg/d
Q 1.806429431055966 2.7752e-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      3  
   norm. resid. RMS      .34789  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 11:08:29  

Additional Information
 Earth MOID = .000296735 au 
 Jupiter MOID = 3.56506 au 
 T_jup = 4.889 
[ 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. 2020-October); Warner et al., 2009 Incomplete or inconclusive result.
Published Reference List:
[NASA/JPL NEO Program Office (2014) https://web.archive.org/web/20141011215227/http://neo.jpl.nasa.gov/ news/news185.html]

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