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 ]  
357468 (2004 EA96)
Classification: Main-belt Asteroid          SPK-ID: 2357468
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2403529271497862 5.1792e-08  
a 2.701929616615142 3.2283e-08 au
q 2.052512924308993 1.3567e-07 au
i 15.96867537343082 7.8631e-06 deg
node 138.1490037848546 2.1608e-05 deg
peri 89.85361259278685 2.7833e-05 deg
M 206.0955587861546 2.0266e-05 deg
tp 2459694.018620665584
(2022-Apr-24.51862067)
9.9764e-05 TDB
period 1622.21896568083
4.44
2.9074e-05
7.96e-08
d
yr
n .221918253710535 3.9773e-09 deg/d
Q 3.351346308921291 4.0043e-08 au
  Orbit Determination Parameters
   # obs. used (total)      213  
   data-arc span      5708 days (15.63 yr)  
   first obs. used      2004-03-15  
   last obs. used      2019-10-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53606  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-08 11:08:37  

Additional Information
 Earth MOID = 1.11667 au 
 Jupiter MOID = 1.93129 au 
 T_jup = 3.271 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.3   n/a MPO450330  

357468 (2004 EA96)          Discovered 2004-Mar-15 by LINEAR at Socorro
Reference: 20130327/Numbers.arcLast Updated: 2013-03-29

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2012-Jul-18 00:45 < 00:01 Eunom 0.0437127738746532 0.0437091566116031 0.0437163911959437 11.4686876141836 11.4686875861827 2456126.530947306 0.791284951485634 218.88266304718 138.361027330431 46.9892937307066 40115.2700812529 T 9 CATAB v2.0f-lin.ifort 2019-Nov-08 11:08:38 2019-Nov-08 11:08
2163-Dec-15 08:57 00:11 Amphi 0.0439715590468229 0.0439135377084807 0.0440298042419586 8.92163178665136 8.92163177199734 2511427.872675632 11.194459461742 5736.36634135824 106.159880233537 -59.6658377965623 53477.164298906 T 9 CATAB v2.0f-lin.ifort 2019-Nov-08 11:08:38 2019-Nov-08 11:08
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Aug-04 09:47 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin