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376P/LONEOS
Classification: Jupiter-family Comet          SPK-ID: 1000562
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2455276.5 (2010-Mar-21.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5151083318382463 1.4808e-07  
a 5.857509729881561 8.1892e-08 au
q 2.840257664195973 8.7512e-07 au
i 1.188832251073736 1.1424e-05 deg
node 315.1471425146397 0.0012754 deg
peri 285.5154539897699 0.0012794 deg
M 116.6617033987685 3.3642e-05 deg
tp 2453598.493002856115
(2005-Aug-15.99300286)		 0.00046567 TDB
period 5178.070449622594
14.18		 0.00010859
2.973e-07		 d
yr
n .06952396718090979 1.458e-09 deg/d
Q 8.874761795567149 1.2408e-07 au
   Orbit Determination Parameters
   # obs. used (total)      393  
   data-arc span      5637 days (15.43 yr)  
   first obs. used      2005-04-02  
   last obs. used      2020-09-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .73183  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-30 21:15:58  

Additional Information
 Earth MOID = 1.82833 au 
 Jupiter MOID = .0461472 au 
 T_jup = 2.707 
[ 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
comet total magnitude M1 9.1   0.5 28 2 parameter fit from 235 observations, autocmod 2.8
comet total magnitude slope K1 15.5   n/a 28 autocmod 2.8
comet nuclear magnitude M2 14.2   0.9 28 from 109 observations, autocmod 2.8
comet nuclear magnitude slope K2 5.   n/a 28 autocmod 2.8
comet nuclear phase coefficient PC 0.03   n/a 28 autocmod 2.8

[ show close-approach data ]
Alternate Designations
 Perihelion 
Year (est.)		  New-Style 
Desig		 Roman
 Numeral 		 Year/
 Letter 
 2019.8   376P/2018 X1       
 2005.6   376P/2005 GF8       
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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