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 ]  
(2012 SJ32)
Classification: Apollo [NEO]          SPK-ID: 3609119
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 2456194.5 (2012-Sep-24.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3679001711989628 0.00090972  
a 1.474380126167183 0.001955 au
q .9319554253379282 0.00010607 au
i 2.097166547206646 0.0043523 deg
node 175.6697165933235 0.0015401 deg
peri 236.9301728238152 0.0044294 deg
M 336.8092430137132 0.056829 deg
tp 2456236.623558610953
(2012-Nov-05.12355861)
0.019516 TDB
period 653.9019450253453
1.79
1.3006
0.003561
d
yr
n .5505412588825476 0.001095 deg/d
Q 2.016804826996438 0.0026743 au
  Orbit Determination Parameters
   # obs. used (total)      22  
   data-arc span      4 days  
   first obs. used      2012-09-22  
   last obs. used      2012-09-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .31551  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:48:52  

Additional Information
 Earth MOID = .00939769 au 
 Jupiter MOID = 3.37084 au 
 T_jup = 4.518 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 8.27589994317365E-7 -9.601412250895112E-8 -1.765263558304355E-5 1.361051468625254E-6 -2.819559915210552E-6 3.958286092822238E-6
q -9.601412250895112E-8 1.124988856191131E-8 2.026135328756451E-6 -1.555525900410905E-7 2.939702544839429E-7 -4.586672039436072E-7
tp -1.765263558304355E-5 2.026135328756451E-6 .0003808552867464808 -2.949560784841149E-5 6.669234337339109E-5 -8.454065942641466E-5
node 1.361051468625254E-6 -1.555525900410905E-7 -2.949560784841149E-5 2.371765141015391E-6 -5.424209573614111E-6 6.546533256656941E-6
peri -2.819559915210552E-6 2.939702544839429E-7 6.669234337339109E-5 -5.424209573614111E-6 1.961942196110905E-5 -1.367714841712575E-5
i 3.958286092822238E-6 -4.586672039436072E-7 -8.454065942641466E-5 6.546533256656941E-6 -1.367714841712575E-5 1.894280963513086E-5

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 25.1   n/a MPO240112  

[ 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-10 00:45 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin