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

Significant website upgrade scheduled for September 27. More details available here.

JPL Small-Body Database Browser
Search: [ help ]  
(2020 MX3)
Classification: Apollo [NEO]          SPK-ID: 54017684
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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2580083430023044 2.2611e-05  
a 1.169210764154891 2.609e-05 au
q .8675446322748294 7.0837e-06 au
i 8.216285873690378 0.00066739 deg
node 300.9878300418856 8.1134e-05 deg
peri 82.24723108251719 0.00089808 deg
M 213.5446338751406 0.0058566 deg
tp 2459584.362640565700
(2022-Jan-04.86264057)
0.0138 TDB
period 461.7826740878455
1.26
0.015456
4.232e-05
d
yr
n .7795874990570061 2.6093e-05 deg/d
Q 1.470876896034952 3.2821e-05 au
  Orbit Determination Parameters
   # obs. used (total)      142  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      32 days  
   first obs. used      2020-06-28  
   last obs. used      2020-07-30  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      5  
   norm. resid. RMS      .2879  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 22:36:58  

Additional Information
 Earth MOID = .0197396 au 
 Jupiter MOID = 4.00391 au 
 T_jup = 5.357 
[ 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 23.7   .37575 E2021-DA1 autocmod 2.8

[ 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 2021-Sep-19 22:53 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin