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(2014 QO295)
Classification: Apollo [NEO]          SPK-ID: 3683467
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .416692886571581 0.00069856  
a 1.491961756731928 0.0015361 au
q .8702719056648939 0.00014635 au
i 3.873309947728434 0.0060581 deg
node 148.8652809507277 0.00030595 deg
peri 247.9018777696486 0.0038187 deg
M 245.02047009209 2.0368 deg
tp 2459609.094973186609
(2022-Jan-29.59497319)
4.0944 TDB
period 665.6331819105322
1.82
1.028
0.002815
d
yr
n .5408384223976196 0.00083525 deg/d
Q 2.113651607798961 0.0021762 au
  Orbit Determination Parameters
   # obs. used (total)      11  
   data-arc span      3 days  
   first obs. used      2014-08-24  
   last obs. used      2014-08-27  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .45978  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 10:55:35  

Additional Information
 Earth MOID = .0115401 au 
 Jupiter MOID = 3.32334 au 
 T_jup = 4.459 
[ 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 26.8   n/a MPO305405  

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