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 RX30)
Classification: Aten [NEO]          SPK-ID: 3545558
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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .388472644459659 5.9966e-07  
a .830679859062849 1.3842e-08 au
q .5079834575133273 4.8977e-07 au
i 5.059852497810464 1.721e-05 deg
node 166.1471900850443 8.247e-06 deg
peri 319.7944249319988 1.6832e-05 deg
M 39.86584782642909 1.9643e-05 deg
tp 2458569.877019938967
(2019-Mar-27.37701994)
1.5135e-05 TDB
period 276.5342623583525
0.76
6.9122e-06
1.892e-08
d
yr
n 1.301827834749413 3.254e-08 deg/d
Q 1.153376260612371 1.922e-08 au
  Orbit Determination Parameters
   # obs. used (total)      101  
   data-arc span      1073 days (2.94 yr)  
   first obs. used      2010-09-05  
   last obs. used      2013-08-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .50711  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:50  

Additional Information
 Earth MOID = .00116191 au 
 Jupiter MOID = 3.90794 au 
 T_jup = 6.997 
[ 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 27.1   n/a MPO279189  

[ 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 2019-Dec-11 20:53 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin