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(2014 QY33)
Classification: Apollo [NEO]          SPK-ID: 3682527
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 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5855398387027961 5.0608e-06  
a 1.939539049786754 1.9225e-05 au
q .8038616674168437 1.9234e-06 au
i .834968781825268 3.2476e-05 deg
node 166.1317481024172 0.00059662 deg
peri 235.7322515605133 0.0006329 deg
M 30.60290630757028 0.011122 deg
tp 2458916.630048738971
(2020-Mar-08.13004874)
0.029233 TDB
period 986.6116031764475
2.70
0.014669
4.016e-05
d
yr
n .3648852282306038 5.4251e-06 deg/d
Q 3.075216432156665 3.0482e-05 au
  Orbit Determination Parameters
   # obs. used (total)      33  
   # delay obs. used      4  
   # Doppler obs. used      2  
   data-arc span      7 days  
   first obs. used      2014-08-22  
   last obs. used      2014-08-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .48077  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:39:14  

Additional Information
 Earth MOID = .00190828 au 
 Jupiter MOID = 2.34927 au 
 T_jup = 3.673 
[ 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 26.2   n/a MPO305358  

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