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
IMPORTANT: The SSD Announcement email list is now available. Major changes are coming in the near future, including possible hostname and/or URL changes. To be notified of such changes, subscribe to this email list.

Please visit this page for more details.


JPL Small-Body Database Browser
Search: [ help ]  
(2014 KS76)
Classification: Aten [NEO]          SPK-ID: 3672909
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2704984561733025 7.8472e-07  
a .9281843505406973 9.8634e-08 au
q .6771119166752192 8.0031e-07 au
i 1.096120578885502 2.3753e-06 deg
node 62.28560407924166 4.0903e-05 deg
peri 51.33940977976424 4.5012e-05 deg
M 4.172347834121491 0.00047644 deg
tp 2458996.714460381976
(2020-May-27.21446038)
0.00043167 TDB
period 326.6252759042582
0.89
5.2063e-05
1.425e-07
d
yr
n 1.102180469663116 1.7568e-07 deg/d
Q 1.179256784406175 1.2531e-07 au
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      473 days (1.30 yr)  
   first obs. used      2014-05-27  
   last obs. used      2015-09-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .44955  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:40:17  

Additional Information
 Earth MOID = .00167147 au 
 Jupiter MOID = 3.90092 au 
 T_jup = 6.419 
[ 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 26.6   n/a MPO347317  

[ 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-Jun-01 23:58 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin