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486898 (2014 KF93)
Classification: Main-belt Asteroid          SPK-ID: 2486898
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .01841099267948218 6.4535e-08  
a 3.079718766158674 5.3676e-08 au
q 3.023018086500063 2.0802e-07 au
i 9.753978969616053 6.1718e-06 deg
node 171.5825250516382 4.1222e-05 deg
peri 284.670285088002 0.00018197 deg
M 265.2709016710935 0.00017876 deg
tp 2459915.952593246815
(2022-Dec-02.45259325)
0.00097993 TDB
period 1974.081215463124
5.40
5.1609e-05
1.413e-07
d
yr
n .1823633177703599 4.7676e-09 deg/d
Q 3.136419445817285 5.4664e-08 au
  Orbit Determination Parameters
   # obs. used (total)      113  
   data-arc span      7601 days (20.81 yr)  
   first obs. used      1999-09-05  
   last obs. used      2020-06-27  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .60399  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 17:19:30  

Additional Information
 Earth MOID = 2.0568 au 
 Jupiter MOID = 1.87369 au 
 T_jup = 3.206 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.74   n/a E2021B25  

486898 (2014 KF93)          Discovered 2013-Mar-08 by Pan-STARRS 1 at Haleakala
Reference: Last Updated: 2017-03-14

[ show close-approach data ]
Alternate Designations
 2014 KF93 = 2013 EC65 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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