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 CP13)
Classification: Apollo [NEO]          SPK-ID: 3661504
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4666512128307199 0.00025158  
a 1.891365783145916 0.00091053 au
q 1.00875764653435 9.8069e-06 au
i 4.257463912726358 0.0017617 deg
node 226.0423676489596 0.004866 deg
peri 317.6787855542555 0.0025488 deg
M 137.5292259636073 0.61944 deg
tp 2458637.543802262367
(2019-Jun-03.04380226)
1.3727 TDB
period 950.0833751520115
2.60
0.68608
0.001878
d
yr
n .378914113661236 0.00027362 deg/d
Q 2.773973919757482 0.0013354 au
  Orbit Determination Parameters
   # obs. used (total)      46  
   data-arc span      38 days  
   first obs. used      2014-02-10  
   last obs. used      2014-03-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .43427  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:30  

Additional Information
 Earth MOID = .0381203 au 
 Jupiter MOID = 2.19936 au 
 T_jup = 3.815 
[ 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 23.1   n/a E2014D50  

[ 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-Oct-21 09:54 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin