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 HT1)
Classification: Apollo [NEO]          SPK-ID: 54016607
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 2458958.5 (2020-Apr-19.0) TDB
Reference: JPL 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5725023703176165 0.0015199  
a 2.308987151819554 0.0081142 au
q .9870865343699371 4.0768e-05 au
i 3.166232106926236 0.0062692 deg
node 22.30550824960108 0.0023 deg
peri 222.6519033179055 0.0099735 deg
M 351.4716106970483 0.046577 deg
tp 2458988.859542124961
(2020-May-19.35954212)
0.0058077 TDB
period 1281.535677692763
3.51
6.7553
0.0185
d
yr
n .2809129751644002 0.0014808 deg/d
Q 3.630887769269171 0.01276 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      5 days  
   first obs. used      2020-04-18  
   last obs. used      2020-04-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .36289  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-23 07:00:52  

Additional Information
 Earth MOID = .0205381 au 
 Jupiter MOID = 1.4256 au 
 T_jup = 3.344 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 2.310013550494481E-6 -6.165263827658032E-8 -8.772690930729717E-6 -3.475730397710416E-6 1.506312068993455E-5 9.526035027669745E-6
q -6.165263827658032E-8 1.662006593037016E-9 2.31534922465035E-7 9.358610785230653E-8 -4.065256109382117E-7 -2.537312552960015E-7
tp -8.772690930729717E-6 2.31534922465035E-7 3.372917932872249E-5 1.307104367873728E-5 -5.649307951137633E-5 -3.625601886343593E-5
node -3.475730397710416E-6 9.358610785230653E-8 1.307104367873728E-5 5.290076907968562E-6 -2.290702599250694E-5 -1.429925343237995E-5
peri 1.506312068993455E-5 -4.065256109382117E-7 -5.649307951137633E-5 -2.290702599250694E-5 9.947143882449127E-5 6.197087374107883E-5
i 9.526035027669745E-6 -2.537312552960015E-7 -3.625601886343593E-5 -1.429925343237995E-5 6.197087374107883E-5 3.930341968876166E-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 25.852   .60789 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 2020-Oct-31 17:23 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin