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JPL Small-Body Database Browser
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6132 Danielson (1990 QY3)
Classification: Main-belt Asteroid          SPK-ID: 2006132
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.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1615936700418701 3.4225e-08  
a 2.466468167575656 8.8564e-09 au
q 2.067902524335659 8.4136e-08 au
i 2.957372250418365 4.3367e-06 deg
node 338.6317628859646 6.5486e-05 deg
peri 295.9178384442583 6.682e-05 deg
M 195.344043121358 1.3893e-05 deg
tp 2459247.622716379975
(2021-Feb-02.12271638)
5.5056e-05 TDB
period 1414.854234933601
3.87
7.6205e-06
2.086e-08
d
yr
n .2544431723858075 1.3704e-09 deg/d
Q 2.865033810815652 1.0287e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1809  
   data-arc span      11929 days (32.66 yr)  
   first obs. used      1986-08-02  
   last obs. used      2019-03-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48227  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-12 18:42:46  

Additional Information
 Earth MOID = 1.05317 au 
 Jupiter MOID = 2.25487 au 
 T_jup = 3.467 
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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 13.8   n/a MPO332877  

6132 Danielson (1990 QY3)          Discovered 1990-Aug-22 by Holt, H. E. at Palomar
Reference: DISCOVERY.DBLast Updated: 2003-08-29

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Alternate Designations
 1990 QY3 = 1986 PO = 1989 EF2 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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