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 HB1)
Classification: Apollo [NEO]          SPK-ID: 54016577
[ 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 2458956.5 (2020-Apr-17.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5722722149215944 0.00097136  
a 2.37699001432797 0.005439 au
q 1.01670467398199 1.7521e-05 au
i 1.371157494234314 0.0018008 deg
node 64.95513854648316 0.0071844 deg
peri 147.6786032947543 0.0036578 deg
M 358.7385438627272 0.0037656 deg
tp 2458961.190391736658
(2020-Apr-21.69039174)		 0.0021038 TDB
period 1338.564992713469
3.66		 4.5944
0.01258		 d
yr
n .2689447295870385 0.0009231 deg/d
Q 3.737275354673949 0.0085517 au
   Orbit Determination Parameters
   # obs. used (total)      23  
   data-arc span      5 days  
   first obs. used      2020-04-16  
   last obs. used      2020-04-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .49287  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-21 06:33:40  

Additional Information
 Earth MOID = .0157981 au 
 Jupiter MOID = 1.23091 au 
 T_jup = 3.297 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 9.435379831246053E-7 1.70185863769474E-8 2.038180541935258E-6 6.784675829258971E-6 -3.068204513706639E-6 1.748436570724088E-6
q 1.70185863769474E-8 3.069715812378062E-10 3.675113647178633E-8 1.2248553724563E-7 -5.54653841793834E-8 3.153303252739919E-8
tp 2.038180541935258E-6 3.675113647178633E-8 4.425795403575225E-6 1.443068663748093E-5 -6.374963198971987E-6 3.784336036984485E-6
node 6.784675829258971E-6 1.2248553724563E-7 1.443068663748093E-5 5.16161379277642E-5 -2.516185393991583E-5 1.247994044792447E-5
peri -3.068204513706639E-6 -5.54653841793834E-8 -6.374963198971987E-6 -2.516185393991583E-5 1.337934195670102E-5 -5.584152492702451E-6
i 1.748436570724088E-6 3.153303252739919E-8 3.784336036984485E-6 1.247994044792447E-5 -5.584152492702451E-6 3.243006566047484E-6

[ 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 27.018   .26353 2 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-Jan-19 10:02 UT
(server date/time)   		NASA Home Page
Site Manager:   Ryan S. Park
Webmaster:   Alan B. Chamberlin