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 FS3)
Classification: Apollo [NEO]          SPK-ID: 54016331
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 2458932.5 (2020-Mar-24.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6912138362513264 0.0015499  
a 3.043467475617238 0.01511 au
q .9397806462897067 5.1406e-05 au
i 17.43378100818735 0.025313 deg
node 1.068380632967961 0.0015383 deg
peri 226.1961961711216 0.0018902 deg
M 353.5960818513383 0.050743 deg
tp 2458966.998061806664
(2020-Apr-27.49806181)
0.016442 TDB
period 1939.328698789573
5.31
14.443
0.03954
d
yr
n .1856312445768957 0.0013824 deg/d
Q 5.147154304944769 0.025554 au
  Orbit Determination Parameters
   # obs. used (total)      105  
   data-arc span      9 days  
   first obs. used      2020-03-23  
   last obs. used      2020-04-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .48908  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-02 06:06:07  

Additional Information
 Earth MOID = .0522182 au 
 Jupiter MOID = .845816 au 
 T_jup = 2.764 
[ hide covariance matrix ]
Orbit Covariance (6×6)
  e q tp node peri i
e 2.402323800263068E-6 -7.966121988495485E-8 -2.548360420145092E-5 -2.384133936499625E-6 -2.910733730521779E-6 3.923393529636658E-5
q -7.966121988495485E-8 2.642561195880323E-9 8.449090764516778E-7 7.907046907911519E-8 9.630794085092689E-8 -1.300909055484293E-6
tp -2.548360420145092E-5 8.449090764516778E-7 .0002703445870329222 2.528899542176046E-5 3.090478672095079E-5 -.0004162009308147652
node -2.384133936499625E-6 7.907046907911519E-8 2.528899542176046E-5 2.36634006552555E-6 2.885897803484606E-6 -3.893517386639385E-5
peri -2.910733730521779E-6 9.630794085092689E-8 3.090478672095079E-5 2.885897803484606E-6 3.5727503964478E-6 -4.755662314681482E-5
i 3.923393529636658E-5 -1.300909055484293E-6 -.0004162009308147652 -3.893517386639385E-5 -4.755662314681482E-5 .0006407696890187827

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 23.643   .35385 6 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-Mar-29 00:35 < 00:01 Earth 0.0527921039947711 0.052520825481896 0.0530633813857059 15.8386581795461 15.8354712776534 2458937.524309398 0.193857919262224 13522.0887159222 24.4415237050439 -0.000553987577064224 438.29489935622 T 6 CATAB v2.0f-lin.ifort 2020-Apr-02 06:06:38 2020-Apr-02 06:06
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2020-Dec-04 18:10 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin