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 ]  
(2019 SB6)
Classification: Apollo [NEO]          SPK-ID: 3869331
[ 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 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2661192231499635 0.00092903  
a 1.001151258014096 0.00026739 au
q .7347256629757762 0.00073523 au
i 7.197628819716624 0.029185 deg
node 193.4886046771696 0.0044471 deg
peri 285.8572728127368 0.0061601 deg
M 156.5688557327374 0.016872 deg
tp 2458841.370444440038
(2019-Dec-23.87044444)		 0.080409 TDB
period 365.8878372297399
1.00		 0.14658
0.0004013		 d
yr
n .9839080815740727 0.00039417 deg/d
Q 1.267576853052416 0.00033854 au
   Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      5 days  
   first obs. used      2019-09-28  
   last obs. used      2019-10-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .29596  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Oct-03 06:13:51  

Additional Information
 Earth MOID = .00184237 au 
 Jupiter MOID = 3.80828 au 
 T_jup = 6.036 
[ 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 26.8   .32125 MPO492721 autocmod 2.8

[ 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-Aug-08 19:19 UT
(server date/time)   		NASA Home Page
Site Manager:   Ryan S. Park
Webmaster:   Alan B. Chamberlin