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(2015 FL35)
Classification: Apollo [NEO]          SPK-ID: 3713996
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2206014518108191 0.00041847  
a 1.284195397584211 0.00072051 au
q 1.000900028468362 3.4705e-05 au
i 24.393161376508 0.021893 deg
node 3.822325710867004 0.00030621 deg
peri 208.5398635208833 0.025595 deg
M 184.7480122181372 1.0524 deg
tp 2459259.265004869276
(2021-Feb-13.76500487)
1.7717 TDB
period 531.5511848509831
1.46
0.44735
0.001225
d
yr
n .6772630938654076 0.00056998 deg/d
Q 1.56749076670006 0.00087945 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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .651  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:55  

Additional Information
 Earth MOID = .0252917 au 
 Jupiter MOID = 3.41861 au 
 T_jup = 4.934 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457104.5 (2015-Mar-23.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2208176321202195 0.00042013  
q 1.001167895756094 3.4978e-05 au
tp 2457132.694128498076
(2015-Apr-20.19412850)
0.026457 TDB
node 3.843700161126105 0.00037658 deg
peri 208.3803982893561 0.025516 deg
i 24.40521444653163 0.021845 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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .651  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:55  

Additional Information
 Jupiter MOID = 3.41861 au 
 T_jup = 4.934 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.765063800005823E-7 1.012800556283054E-8 -9.703845580678624E-6 1.493751928800864E-7 -8.802428395252943E-6 9.17725585321957E-6
q 1.012800556283054E-8 1.22344928795136E-9 -8.837720942749689E-7 1.16950960363832E-8 -8.741331343258631E-7 5.249239127351467E-7
tp -9.703845580678624E-6 -8.837720942749689E-7 .0006999633228567186 -9.800957014528637E-6 .0006718288538778481 -.0005036602817071799
node 1.493751928800864E-7 1.16950960363832E-8 -9.800957014528637E-6 1.41813192889862E-7 -9.2429127114268E-6 7.758169204859606E-6
peri -8.802428395252943E-6 -8.741331343258631E-7 .0006718288538778481 -9.2429127114268E-6 .000651055503196823 -.0004566811931184418
i 9.17725585321957E-6 5.249239127351467E-7 -.0005036602817071799 7.758169204859606E-6 -.0004566811931184418 .0004772149876690921

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  

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