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 ]  
(2016 JM6)
Classification: Apollo [NEO]          SPK-ID: 3752801
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5461287278344482 1.6248e-05  
a 2.137127816560292 7.3332e-05 au
q .9699809208826079 1.4403e-06 au
i 7.426577440709811 0.000203 deg
node 35.35018992420157 0.00010159 deg
peri 249.6853079771675 0.00011922 deg
M 89.99385369801442 0.023311 deg
tp 2458715.231038447740
(2019-Aug-19.73103845)
0.059211 TDB
period 1141.153778161623
3.12
0.058735
0.0001608
d
yr
n .3154701906871423 1.6237e-05 deg/d
Q 3.304274712237977 0.00011338 au
  Orbit Determination Parameters
   # obs. used (total)      111  
   data-arc span      180 days  
   first obs. used      2016-04-09  
   last obs. used      2016-10-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .53993  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:26:06  

Additional Information
 Earth MOID = .0781618 au 
 Jupiter MOID = 1.95204 au 
 T_jup = 3.499 
[ 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 21.9   n/a E2016T48  

[ 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-31 06:11 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin