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
IMPORTANT: The SSD Announcement email list is now available. Major changes are coming in the near future, including possible hostname and/or URL changes. To be notified of such changes, subscribe to this email list.

Please visit this page for more details.


JPL Small-Body Database Browser
Search: [ help ]  
(2020 FN)
Classification: Apollo [NEO]          SPK-ID: 54016205
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5241006931822789 0.00029876  
a 2.115821605383424 0.0013397 au
q 1.006918035351929 5.4224e-06 au
i 1.548338423862435 0.00068256 deg
node 353.7652209162239 0.00022645 deg
peri 188.4723873422064 0.0012228 deg
M 22.40006774877736 0.021448 deg
tp 2458930.553847683821
(2020-Mar-22.05384768)
0.00059529 TDB
period 1124.131190862081
3.08
1.0676
0.002923
d
yr
n .3202473189307386 0.00030415 deg/d
Q 3.224725175414918 0.0020418 au
  Orbit Determination Parameters
   # obs. used (total)      55  
   data-arc span      3 days  
   first obs. used      2020-03-16  
   last obs. used      2020-03-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .53466  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-20 06:06:22  

Additional Information
 Earth MOID = .0107935 au 
 Jupiter MOID = 1.73689 au 
 T_jup = 3.545 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458925.5 (2020-Mar-17.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5264815399892262 0.0002965  
q 1.006937745240131 5.4029e-06 au
tp 2458930.378825011385
(2020-Mar-21.87882501)
0.00084764 TDB
node 353.8985342718053 0.00042431 deg
peri 188.1202393905968 0.0017252 deg
i 1.569694982438182 0.00065809 deg
  Orbit Determination Parameters
   # obs. used (total)      55  
   data-arc span      3 days  
   first obs. used      2020-03-16  
   last obs. used      2020-03-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .53466  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Mar-20 06:06:22  

Additional Information
 Jupiter MOID = 1.73689 au 
 T_jup = 3.545 
Orbit Covariance (6×6)
  e q tp node peri i
e 8.791223960200342E-8 1.600730959734766E-9 2.405694016362994E-7 -1.248518693084881E-7 5.0265426108383E-7 1.949014005950985E-7
q 1.600730959734766E-9 2.919103223314873E-11 4.32969146827312E-9 -2.269449538234789E-9 9.087237491399277E-9 3.552744561650442E-9
tp 2.405694016362994E-7 4.32969146827312E-9 7.184919425160714E-7 -3.464294630125106E-7 1.45307451899821E-6 5.288695052285501E-7
node -1.248518693084881E-7 -2.269449538234789E-9 -3.464294630125106E-7 1.800368684765573E-7 -7.223590008365905E-7 -2.753458090634595E-7
peri 5.0265426108383E-7 9.087237491399277E-9 1.45307451899821E-6 -7.223590008365905E-7 2.976351343464177E-6 1.1075186840475E-6
i 1.949014005950985E-7 3.552744561650442E-9 5.288695052285501E-7 -2.753458090634595E-7 1.1075186840475E-6 4.330821030791319E-7

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 27.621   .49876 4 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-May-26 17:17 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin