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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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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
(2020-Nov-05.55125300)
0.0035447 TDB
period 549.8671994727878
1.51
0.00031528
8.632e-07
d
yr
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) 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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