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215172 (2000 GQ67)
Classification: Main-belt Asteroid          SPK-ID: 2215172
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1196564905119531 4.6578e-08  
a 2.701023673723138 1.8356e-08 au
q 2.377828660135724 1.2903e-07 au
i 3.294207881570858 5.0163e-06 deg
node 182.9577766016866 9.0086e-05 deg
peri 3.027359975804459 9.2777e-05 deg
M 254.8462030742252 2.4022e-05 deg
tp 2459674.101938205961
(2022-Apr-04.60193821)
0.00011061 TDB
period 1621.403151752047
4.44
1.6529e-05
4.525e-08
d
yr
n .2220299125550565 2.2634e-09 deg/d
Q 3.024218687310551 2.0553e-08 au
  Orbit Determination Parameters
   # obs. used (total)      345  
   data-arc span      7586 days (20.77 yr)  
   first obs. used      2000-04-05  
   last obs. used      2021-01-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55983  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 12:45:44  

Additional Information
 Earth MOID = 1.37875 au 
 Jupiter MOID = 1.93158 au 
 T_jup = 3.355 
[ 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 16.1   n/a MPO450014  

215172 (2000 GQ67)          Discovered 2000-Apr-05 by LINEAR at Socorro
Reference: 20090607/Numbers.arcLast Updated: 2009-06-08

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