Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
JPL Small-Body Database Browser
Search: [ help ]  
(2014 RC)
Classification: Apollo [NEO]          SPK-ID: 3685273
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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.


[ revert to old Java-based viewer ]

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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456901.5 (2014-Sep-01.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4003922289884987 7.6522e-07  
q .8344229778536755 2.3398e-07 au
tp 2456957.926731168211
(2014-Oct-27.42673117)
2.9541e-05 TDB
node 345.4784154273938 1.5416e-05 deg
peri 65.87901109754158 3.0678e-05 deg
i 1.439530497214282 5.8299e-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.      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
 Jupiter MOID = 3.56353 au 
 T_jup = 4.890 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.855651131743075E-13 -1.602451367369532E-13 -2.091088778922554E-11 1.898912431454907E-12 -6.042538895628309E-12 1.352237008382672E-12
q -1.602451367369532E-13 5.474803723247635E-14 4.611875664960811E-12 1.582700092977812E-13 -1.219971578961283E-12 -5.47412715180426E-13
tp -2.091088778922554E-11 4.611875664960811E-12 8.726704979665692E-10 -9.606339936900516E-11 4.803087539081754E-10 -3.780116585163085E-11
node 1.898912431454907E-12 1.582700092977812E-13 -9.606339936900516E-11 2.376484682372041E-10 -3.473808027478697E-10 -5.854786478609397E-11
peri -6.042538895628309E-12 -1.219971578961283E-12 4.803087539081754E-10 -3.473808027478697E-10 9.411210073957173E-10 7.717294119146918E-11
i 1.352237008382672E-12 -5.47412715180426E-13 -3.780116585163085E-11 -5.854786478609397E-11 7.717294119146918E-11 3.398812458684119E-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. 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 ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Dec-05 00:03 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin