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(2015 KF)
Classification: Aten [NEO]          SPK-ID: 3719245
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .145379633445982 2.0046e-06  
a .9794643756766384 2.6128e-07 au
q .8370702037673711 2.1852e-06 au
i 7.470330859950306 7.9617e-05 deg
node 58.35085002629321 1.1663e-05 deg
peri 39.82022322664871 0.00022024 deg
M 194.8583278412238 0.00043006 deg
tp 2459162.918528340203
(2020-Nov-09.41852834)
0.00048219 TDB
period 354.0636923323392
0.97
0.00014167
3.879e-07
d
yr
n 1.016766214091471 4.0684e-07 deg/d
Q 1.121858547585906 2.9926e-07 au
  Orbit Determination Parameters
   # obs. used (total)      56  
   data-arc span      390 days (1.07 yr)  
   first obs. used      2015-05-18  
   last obs. used      2016-06-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      2  
   norm. resid. RMS      .5448  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:33:43  

Additional Information
 Earth MOID = .0513081 au 
 Jupiter MOID = 3.96272 au 
 T_jup = 6.164 
[ show covariance matrix ]

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 25.1   n/a E2015L36  

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