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(2015 FC35)
Classification: Apollo [NEO]          SPK-ID: 3713989
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .394702991955775 3.8941e-08  
a 1.39234988877898 6.9184e-09 au
q .8427852218286258 5.7225e-08 au
i 15.45400338027812 1.1101e-05 deg
node 12.31641225323309 5.4199e-06 deg
peri 249.7956473354156 1.0551e-05 deg
M 241.4206271777915 5.131e-06 deg
tp 2459594.164032829335
(2022-Jan-14.66403283)
9.095e-06 TDB
period 600.0963753219759
1.64
4.4727e-06
1.225e-08
d
yr
n .5999036401558758 4.4713e-09 deg/d
Q 1.941914555729333 9.6491e-09 au
  Orbit Determination Parameters
   # obs. used (total)      217  
   data-arc span      1843 days (5.05 yr)  
   first obs. used      2015-03-17  
   last obs. used      2020-04-02  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .4913  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 13:12:50  

Additional Information
 Earth MOID = .0218573 au 
 Jupiter MOID = 3.22294 au 
 T_jup = 4.653 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457953.5 (2017-Jul-19.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3950046261185041 3.8895e-08  
q .843297928133227 5.7027e-08 au
tp 2457791.895063244693
(2017-Feb-07.39506324)
1.4307e-05 TDB
node 12.35009394141161 5.4213e-06 deg
peri 249.6354055613226 1.0684e-05 deg
i 15.46612141525418 1.1098e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      217  
   data-arc span      1843 days (5.05 yr)  
   first obs. used      2015-03-17  
   last obs. used      2020-04-02  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .4913  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 13:12:50  

Additional Information
 Jupiter MOID = 3.22294 au 
 T_jup = 4.653 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.512822988441524E-15 -2.214198370847323E-15 2.051920885147627E-13 -6.034825121775676E-14 2.408648225336353E-13 8.379038007912167E-14
q -2.214198370847323E-15 3.252025783384256E-15 -3.377554109308841E-13 8.800512664755307E-14 -3.67797650629871E-13 -1.362407850088422E-13
tp 2.051920885147627E-13 -3.377554109308841E-13 2.046855874536813E-10 6.579198937793009E-12 1.243469152501392E-10 7.088019947587257E-11
node -6.034825121775676E-14 8.800512664755307E-14 6.579198937793009E-12 2.939004426625345E-11 -2.112598957889674E-11 -2.205271049124829E-11
peri 2.408648225336353E-13 -3.67797650629871E-13 1.243469152501392E-10 -2.112598957889674E-11 1.141506074649377E-10 6.507055999477536E-11
i 8.379038007912167E-14 -1.362407850088422E-13 7.088019947587257E-11 -2.205271049124829E-11 6.507055999477536E-11 1.231751186712316E-10

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 22.1   n/a E2020-PA3  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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