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(2010 UQ7)
Classification: Apollo [NEO, PHA]          SPK-ID: 3550082
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6786671410052514 1.2185e-07  
a 2.454547855660329 6.7224e-08 au
q .788726879998763 3.1925e-07 au
i 4.512945715167717 1.238e-05 deg
node 236.8975245515451 4.7162e-05 deg
peri 76.50126251340632 7.9494e-05 deg
M 193.3972560398567 1.9155e-05 deg
tp 2459650.532890704136
(2022-Mar-12.03289070)
0.00010115 TDB
period 1404.609762666766
3.85
5.7703e-05
1.58e-07
d
yr
n .256298944780585 1.0529e-08 deg/d
Q 4.120368831321894 1.1285e-07 au
  Orbit Determination Parameters
   # obs. used (total)      178  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      1305 days (3.57 yr)  
   first obs. used      2010-10-29  
   last obs. used      2014-05-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .40468  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:07  

Additional Information
 Earth MOID = .0180755 au 
 Jupiter MOID = 1.27131 au 
 T_jup = 3.126 
[ 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
absolute magnitude H 20.1   n/a MPO297901  

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