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301P/LINEAR-NEAT
Classification: Jupiter-family Comet          SPK-ID: 1000334
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2452666.5 (2003-Jan-27.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5874165458554789 1.092e-06  
a 5.686867070697107 9.5374e-07 au
q 2.346307259288947 6.5804e-06 au
i 10.61823651060052 5.2435e-05 deg
node 355.7835584400734 0.00022598 deg
peri 189.399728846603 0.00052655 deg
M 52.78658437563432 0.00010971 deg
tp 2451940.178161044884
(2001-Jan-30.67816105)
0.0014641 TDB
period 4953.452948634729
13.56
0.0012461
3.412e-06
d
yr
n .07267657606381892 1.8283e-08 deg/d
Q 9.027426882105267 1.514e-06 au
  Orbit Determination Parameters
   # obs. used (total)      126  
   data-arc span      4904 days (13.43 yr)  
   first obs. used      2001-01-21  
   last obs. used      2014-06-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-BIG16  
   condition code      0  
   norm. resid. RMS      .5129  
   source      ORB  
   producer      Otto Matic  
   solution date      2015-Oct-05 13:18:20  

Additional Information
 Earth MOID = 1.3491 au 
 T_jup = 2.578 
[ 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 11.0   0.8 4 2 parameter fit from 60 observations, autocmod 2.6
comet total magnitude slope K1 16.   n/a 4 autocmod 2.6
comet nuclear magnitude M2 16.0   0.6 4 from 28 observations, autocmod 2.6
comet nuclear magnitude slope K2 5.   n/a 4 autocmod 2.6
comet nuclear phase coefficient PC 0.03   n/a 4 autocmod 2.6

[ show close-approach data ]
Alternate Designations
 Perihelion 
Year
(est.)
 New-Style 
Desig
Roman
 Numeral 
Year/
 Letter 
 2014.6   301P/2014 K1       
 2001.1   301P/2001 BB50       
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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