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(2015 FL35)
Classification: Apollo [NEO]          SPK-ID: 3713996
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .220544983692626 0.00041784  
a 1.284294059787775 0.00072142 au
q 1.001049447315344 3.579e-05 au
i 24.39297355957676 0.021875 deg
node 3.819107129522754 0.00031833 deg
peri 208.5291576425503 0.025697 deg
M 320.1833859952512 1.1663 deg
tp 2459259.297242905524
(2021-Feb-13.79724291)
1.7718 TDB
period 531.6124430737383
1.46
0.44793
0.001226
d
yr
n .6771850521754352 0.00057058 deg/d
Q 1.567538672260207 0.00088052 au
  Orbit Determination Parameters
   # obs. used (total)      53  
   data-arc span      1 day  
   first obs. used      2015-03-22  
   last obs. used      2015-03-23  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .64025  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 13:12:53  

Additional Information
 Earth MOID = .0249507 au 
 Jupiter MOID = 3.41744 au 
 T_jup = 4.934 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457104.5 (2015-Mar-23.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2208226173853941 0.00042014  
q 1.001171176381245 3.4978e-05 au
tp 2457132.692283810610
(2015-Apr-20.19228381)
0.026456 TDB
node 3.843719849688649 0.0003766 deg
peri 208.3783805185329 0.025515 deg
i 24.40539450254978 0.021846 deg
  Orbit Determination Parameters
   # obs. used (total)      53  
   data-arc span      1 day  
   first obs. used      2015-03-22  
   last obs. used      2015-03-23  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .64025  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 13:12:53  

Additional Information
 Jupiter MOID = 3.41744 au 
 T_jup = 4.934 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.76521709981369E-7 1.012901154333344E-8 -9.703748323250491E-6 1.493878425212875E-7 -8.802299141508652E-6 9.177835246381255E-6
q 1.012901154333344E-8 1.223461240014673E-9 -8.837621581924197E-7 1.169581911436471E-8 -8.741169815655107E-7 5.249610715639933E-7
tp -9.703748323250491E-6 -8.837621581924197E-7 .0006999085370331768 -9.800877311229078E-6 .0006717762362082962 -.000503641864489388
node 1.493878425212875E-7 1.169581911436471E-8 -9.800877311229078E-6 1.418238139146145E-7 -9.242799121639968E-6 7.758629352461639E-6
peri -8.802299141508652E-6 -8.741169815655107E-7 .0006717762362082962 -9.242799121639968E-6 .0006510047187853386 -.0004566620503747589
i 9.177835246381255E-6 5.249610715639933E-7 -.000503641864489388 7.758629352461639E-6 -.0004566620503747589 .0004772338102872197

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 24.3   n/a MPO332800  

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