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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 ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3750978202095532 6.5106e-07  
a 1.313411503398626 5.0409e-07 au
q .8207537114356489 5.7362e-07 au
i 4.569761909750696 5.3234e-05 deg
node 344.9462644101025 1.4716e-05 deg
peri 71.12603178367776 7.4887e-05 deg
M 354.2733817916506 0.0021119 deg
tp 2458609.245716183065
(2019-May-05.74571618)
0.0032304 TDB
period 549.7935625100922
1.51
0.00031652
8.666e-07
d
yr
n .6547912244668956 3.7696e-07 deg/d
Q 1.806069295361602 6.9317e-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 = .000400416 au 
 Jupiter MOID = 3.56265 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-January); Warner et al., 2009 Incomplete or inconclusive result.
Published Reference List:
[NASA/JPL NEO Program Office (2014) 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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