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 ]  
(2010 FV9)
Classification: Apollo [NEO]          SPK-ID: 3512702
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2873641198871723 7.4392e-07  
a 1.147519732160975 4.9293e-08 au
q .8177637342753727 8.8861e-07 au
i .6393058657433917 2.3444e-05 deg
node 30.47983792358752 0.0012057 deg
peri 64.80545189306032 0.0012852 deg
M 201.7314693226552 0.00027896 deg
tp 2458797.892541999500
(2019-Nov-10.39254200)
0.00036051 TDB
period 448.9920694638247
1.23
2.893e-05
7.921e-08
d
yr
n .8017958990453955 5.1663e-08 deg/d
Q 1.477275730046578 6.3458e-08 au
  Orbit Determination Parameters
   # obs. used (total)      71  
   data-arc span      1644 days (4.50 yr)  
   first obs. used      2010-03-21  
   last obs. used      2014-09-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .47809  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:58:01  

Additional Information
 Earth MOID = .00276238 au 
 Jupiter MOID = 3.68565 au 
 T_jup = 5.434 
[ 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 25.4   n/a MPO190720  

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