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JPL Small-Body Database Browser
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(2015 FF36)
Classification: Apollo [NEO]          SPK-ID: 3714122
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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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.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5337041410159989 0.00018884  
a 2.087254141879355 0.00071119 au
q .9732779630055476 6.2535e-05 au
i .1772053069360129 5.1957e-05 deg
node 6.1016314008362 0.12787 deg
peri 205.4709182867212 0.13238 deg
M 120.8835633655799 0.4372 deg
tp 2458230.649528324064
(2018-Apr-22.14952832)
1.1486 TDB
period 1101.44147058829
3.02
0.56294
0.001541
d
yr
n .3268444212543773 0.00016705 deg/d
Q 3.201230320753162 0.0010908 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      12 days  
   first obs. used      2015-03-14  
   last obs. used      2015-03-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .40095  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:52  

Additional Information
 Earth MOID = .000183162 au 
 Jupiter MOID = 1.7679 au 
 T_jup = 3.564 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457102.5 (2015-Mar-21.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5368252448720708 0.00032634  
q .9744805706286928 1.3447e-05 au
tp 2457128.991799982079
(2015-Apr-16.49179998)
0.0006291 TDB
node 6.331491013879691 0.00024205 deg
peri 204.9979614083043 0.00236 deg
i .1800471893384812 8.3375e-05 deg
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      12 days  
   first obs. used      2015-03-14  
   last obs. used      2015-03-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .40095  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:52  

Additional Information
 Jupiter MOID = 1.7679 au 
 T_jup = 3.564 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.065009900299914E-7 -4.387833787393904E-9 -2.048946560835304E-7 -6.145578438954044E-8 7.683153154931905E-7 2.708643556548409E-8
q -4.387833787393904E-9 1.808231235932652E-10 8.433518553487202E-9 2.533715316424804E-9 -3.166770336489276E-8 -1.115982273565665E-9
tp -2.048946560835304E-7 8.433518553487202E-9 3.957722991091115E-7 1.180074569866854E-7 -1.475726321377774E-6 -5.210748634953294E-8
node -6.145578438954044E-8 2.533715316424804E-9 1.180074569866854E-7 5.85867170728566E-8 -4.668252869393361E-7 -1.644622448275869E-8
peri 7.683153154931905E-7 -3.166770336489276E-8 -1.475726321377774E-6 -4.668252869393361E-7 5.569619236740595E-6 1.962272016696034E-7
i 2.708643556548409E-8 -1.115982273565665E-9 -5.210748634953294E-8 -1.644622448275869E-8 1.962272016696034E-7 6.951384840757224E-9

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 26.6   n/a MPO332802  

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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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