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 MJ6)
Classification: Apollo [NEO, PHA]          SPK-ID: 3673921
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 .6417900311958251 5.819e-08  
a 1.842676462170246 7.473e-09 au
q .6600650780301912 1.0744e-07 au
i 4.489958410236512 1.5775e-05 deg
node 271.5333924509019 3.6677e-05 deg
peri 102.5020348144726 3.9324e-05 deg
M 105.9215982536591 8.5948e-06 deg
tp 2458731.684637949534
(2019-Sep-05.18463795)
2.0827e-05 TDB
period 913.6335925220479
2.50
5.5579e-06
1.522e-08
d
yr
n .394031045866248 2.397e-09 deg/d
Q 3.025287846310301 1.2269e-08 au
  Orbit Determination Parameters
   # obs. used (total)      65  
   data-arc span      1840 days (5.04 yr)  
   first obs. used      2014-06-21  
   last obs. used      2019-07-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47645  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-06 07:04:49  

Additional Information
 Earth MOID = .00440243 au 
 Jupiter MOID = 2.47076 au 
 T_jup = 3.734 
[ 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 21.6   n/a MPCxxxxx  

[ 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-06 15:27 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin