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306367 Nut (5025 P-L)
Classification: Apollo [NEO]          SPK-ID: 2306367
Ephemeris | Orbit Diagram | Orbital Elements | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2457400.5 (2016-Jan-13.0) TDB
Reference: JPL 38 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7429979419339142 1.3966e-07  
a 2.531680854764024 1.4516e-07 au
q .6506471900408614 3.412e-07 au
i 3.77452486331405 2.2724e-05 deg
node 346.2200009340074 0.00014343 deg
peri 152.8278191238943 0.00015789 deg
M 310.0810993758521 0.00015094 deg
tp 2457604.520766264821
(2016-Aug-04.02076626)
0.00060734 JED
period 1471.336005741402
4.03
0.00012655
3.465e-07
d
yr
n .2446755864025749 2.1044e-08 deg/d
Q 4.412714519487186 2.5302e-07 au
  Orbit Determination Parameters
   # obs. used (total)      96  
   data-arc span      20136 days (55.13 yr)  
   first obs. used      1960-10-22  
   last obs. used      2015-12-09  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-BIG16  
   condition code      1  
   fit RMS      .54005  
   data source      ORB  
   producer      Otto Matic  
   solution date      2016-Jan-04 22:51:22  

Additional Information
 Earth MOID = .0529373 au 
 Jupiter MOID = .646769 au 
 T_jup = 2.987 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.7 mag n/a MPO266780  

306367 Nut           Discovered 1960 Oct. 22 by C. J. van Houten and I. van Houten-Groeneveld on Palomar Schmidt plates taken by T. Gehrels.
Nut was a goddess of the heavens in the old Egyptian religion. With Geb, the god of Earth, she gave birth to the god Osiris.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: 20120406/MPCPages.arcLast Updated: 2012-04-09

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