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 PF3)
Classification: Apollo [NEO]          SPK-ID: 54051063
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6014761599174628 0.00054611  
a 2.490623128550169 0.0033962 au
q .9925726933881958 6.6742e-06 au
i 5.91592872363641 0.0037665 deg
node 328.2836987400351 0.00052525 deg
peri 28.45075407422167 0.00027427 deg
M 333.3756318591838 0.055343 deg
tp 2459106.678665090107
(2020-Sep-14.17866509)		 0.0035321 TDB
period 1435.689261441631
3.93		 2.9366
0.00804		 d
yr
n .2507506392006514 0.00051289 deg/d
Q 3.988673563712141 0.005439 au
   Orbit Determination Parameters
   # obs. used (total)      87  
   data-arc span      12 days  
   first obs. used      2020-08-14  
   last obs. used      2020-08-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .50564  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-26 09:35:24  

Additional Information
 Earth MOID = .0159531 au 
 Jupiter MOID = 1.49744 au 
 T_jup = 3.189 
[ 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 25.806   .37121 12 autocmod 2.8

[ 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
2020-Aug-26 15:07 < 00:01 Earth 0.0165000127033372 0.0164615300081174 0.0165384947643983 9.57614713860485 9.55926917062281 2459088.129628584 0.0267007985187139 1912.15719062308 3.53879970579499 0.176259109094532 814.058474934198 T 12 CATAB v2.0f-lin.ifort 2020-Oct-26 09:35:28 2020-Oct-26 09:35
2024-Jul-15 12:51 8_09:18 Earth 0.463508893213162 0.315117530952005 0.611929863248112 22.9631201603406 22.9628698229307 2460507.035579061 12078.3629716302 7402720.79150952 14.4322583142728 1.38476438345324 104584.84303883 T 12 CATAB v2.0f-lin.ifort 2020-Oct-26 09:35:28 2020-Oct-26 09:35
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2021-Jan-16 05:44 UT
(server date/time)   		NASA Home Page
Site Manager:   Ryan S. Park
Webmaster:   Alan B. Chamberlin