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 ]  
(2020 SU5)
Classification: Apollo [NEO]          SPK-ID: 54054686
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 2459119.5 (2020-Sep-27.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5733628888363815 0.0021918  
a 2.324738043788001 0.011946 au
q .9918195232138745 1.1798e-05 au
i 8.004810815121035 0.021369 deg
node 187.4549682405075 0.00073731 deg
peri 200.7093015051512 0.0065964 deg
M 354.414224822542 0.047335 deg
tp 2459139.588171712490
(2020-Oct-17.08817171)
0.015593 TDB
period 1294.671122046024
3.54
9.9795
0.02732
d
yr
n .278062894792213 0.0021434 deg/d
Q 3.657656564362128 0.018796 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      1 day  
   first obs. used      2020-09-26  
   last obs. used      2020-09-27  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .32336  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-27 17:42:07  

Additional Information
 Earth MOID = .0114272 au 
 Jupiter MOID = 1.80031 au 
 T_jup = 3.323 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 4.803814657150776E-6 3.181291686939045E-9 -3.366752058447157E-5 1.424411001480562E-6 -1.160470079529082E-5 4.683422641010001E-5
q 3.181291686939045E-9 1.391840065915488E-10 -5.363822557227848E-8 4.980665919705812E-9 -5.374042003598167E-8 2.97364434620014E-8
tp -3.366752058447157E-5 -5.363822557227848E-8 .000243129495592694 -1.090501053134893E-5 9.18657499352608E-5 -.0003279430687336864
node 1.424411001480562E-6 4.980665919705812E-9 -1.090501053134893E-5 5.436197593262029E-7 -4.798580425751556E-6 1.384600400174476E-5
peri -1.160470079529082E-5 -5.374042003598167E-8 9.18657499352608E-5 -4.798580425751556E-6 4.35128415127849E-5 -.0001127032936899415
i 4.683422641010001E-5 2.97364434620014E-8 -.0003279430687336864 1.384600400174476E-5 -.0001127032936899415 .0004566254236067675

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 26.8   .2773 E2020-SN0 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-Mar-05 23:43 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin