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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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456901.5 (2014-Sep-01.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .400392203155666 7.6523e-07  
q .8344230022028795 2.3399e-07 au
tp 2456957.926729793454
(2014-Oct-27.42672979)
2.9542e-05 TDB
node 345.4784092898041 1.5414e-05 deg
peri 65.87901333988067 3.0684e-05 deg
i 1.439537958921252 5.8297e-06 deg
  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
 Jupiter MOID = 3.56506 au 
 T_jup = 4.889 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.855708921901961E-13 -1.602399049327185E-13 -2.091174398379309E-11 1.899156959479711E-12 -6.044142862314613E-12 1.352242294773711E-12
q -1.602399049327185E-13 5.474968004596341E-14 4.611534161448068E-12 1.588972448127423E-13 -1.221098279140308E-12 -5.475147208941998E-13
tp -2.091174398379309E-11 4.611534161448068E-12 8.727363830998026E-10 -9.615686250820475E-11 4.805009432322048E-10 -3.778733215753606E-11
node 1.899156959479711E-12 1.588972448127423E-13 -9.615686250820475E-11 2.376049938026464E-10 -3.47491147187409E-10 -5.853506457755118E-11
peri -6.044142862314613E-12 -1.221098279140308E-12 4.805009432322048E-10 -3.47491147187409E-10 9.415319265712607E-10 7.718381006893713E-11
i 1.352242294773711E-12 -5.475147208941998E-13 -3.778733215753606E-11 -5.853506457755118E-11 7.718381006893713E-11 3.398515064423232E-11

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]

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