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 ]  
(2013 VA10)
Classification: Apollo [NEO]          SPK-ID: 3653602
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 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7664373719313529 4.729e-08  
a 1.168265293038163 2.0986e-08 au
q .2728631121233814 5.9872e-08 au
i 1.029833475951179 3.6029e-06 deg
node 104.9538207397383 0.00013192 deg
peri 164.3429974717265 0.00013524 deg
M 112.3903860478992 3.5411e-05 deg
tp 2458856.508352329115
(2020-Jan-08.00835233)
4.1533e-05 TDB
period 461.2226631148545
1.26
1.2428e-05
3.403e-08
d
yr
n .7805340647589821 2.1032e-08 deg/d
Q 2.063667473952944 3.7071e-08 au
  Orbit Determination Parameters
   # obs. used (total)      204  
   data-arc span      1844 days (5.05 yr)  
   first obs. used      2013-11-08  
   last obs. used      2018-11-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .43796  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Nov-26 06:29:01  

Additional Information
 Earth MOID = .00954864 au 
 Jupiter MOID = 3.06201 au 
 T_jup = 5.063 
[ 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 22.2   n/a MPO363954  
rotation period rot_per 6.23 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Warner, B.D. (2016) Minor Planet Bull. 43, 240-250.]

[ 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-Apr-03 20:47 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin