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 FF)
Classification: Amor [NEO]          SPK-ID: 54016199
[ 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 2458923.5 (2020-Mar-15.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4175614445613319 0.001713  
a 1.77254581289875 0.0053967 au
q 1.032399022713608 0.00010954 au
i 2.563752375210283 0.0082559 deg
node 356.7725089871574 0.00011504 deg
peri 194.5189682438822 0.027791 deg
M 353.6439315418488 0.022795 deg
tp 2458938.718810006500
(2020-Mar-30.21881001)		 0.020149 TDB
period 861.9749202533957
2.36		 3.9365
0.01078		 d
yr
n .4176455620010039 0.0019073 deg/d
Q 2.512692603083893 0.0076501 au
   Orbit Determination Parameters
   # obs. used (total)      15  
   data-arc span      2 days  
   first obs. used      2020-03-14  
   last obs. used      2020-03-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .33816  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-17 07:48:26  

Additional Information
 Earth MOID = .0349964 au 
 Jupiter MOID = 2.44517 au 
 T_jup = 3.995 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 2.934388476582178E-6 1.828583090790426E-7 2.798139010273458E-5 -1.231223737894117E-7 4.160457827470894E-5 1.414095160943401E-5
q 1.828583090790426E-7 1.199799727136335E-8 1.454042140868371E-6 -6.61022520439237E-9 2.260979702162875E-6 8.831995908822991E-7
tp 2.798139010273458E-5 1.454042140868371E-6 .0004059845511197325 -1.68403750326515E-6 .0005560673476251248 .0001338883026881826
node -1.231223737894117E-7 -6.61022520439237E-9 -1.68403750326515E-6 1.323340122733849E-8 -2.335798036143976E-6 -5.954115130848385E-7
peri 4.160457827470894E-5 2.260979702162875E-6 .0005560673476251248 -2.335798036143976E-6 .0007723288135776596 .0001994058985459179
i 1.414095160943401E-5 8.831995908822991E-7 .0001338883026881826 -5.954115130848385E-7 .0001994058985459179 6.8159201585634E-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 26.805   .32937 1 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-25 01:54 UT
(server date/time)   		NASA Home Page
Site Manager:   Ryan S. Park
Webmaster:   Alan B. Chamberlin