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(2010 UC)
Classification: Aten [NEO]          SPK-ID: 3549617
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06615326771355276 0.0001498  
a .9418957366523812 0.00014321 au
q .8795862558273623 0.00027483 au
i 4.852566045424788 0.005138 deg
node 21.28130344554391 0.026 deg
peri 177.3311507469032 0.010665 deg
M 248.8791608712586 0.15152 deg
tp 2459303.561316334656
(2021-Mar-30.06131633)
0.11703 TDB
period 333.8894321837408
0.91
0.076148
0.0002085
d
yr
n 1.078201240588802 0.0002459 deg/d
Q 1.0042052174774 0.00015268 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      7 days  
   first obs. used      2010-10-17  
   last obs. used      2010-10-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .33925  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:12  

Additional Information
 Earth MOID = .00608441 au 
 Jupiter MOID = 3.94979 au 
 T_jup = 6.370 
[ hide covariance matrix ]
Orbital Elements at Epoch 2455487.5 (2010-Oct-18.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07228312790096622 2.6377e-05  
q .8677982457943906 4.3817e-05 au
tp 2455649.205183308554
(2011-Mar-28.70518331)
0.0015627 TDB
node 22.35096232742994 7.4201e-05 deg
peri 178.5015981903876 0.0041011 deg
i 5.004968126343329 0.0021831 deg
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      7 days  
   first obs. used      2010-10-17  
   last obs. used      2010-10-24  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .33925  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:12  

Additional Information
 Jupiter MOID = 3.94979 au 
 T_jup = 6.370 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.957496889862737E-10 -1.155758522974616E-9 -3.381085322258283E-8 -1.72221286813193E-9 1.05666257220378E-7 5.75477733617397E-8
q -1.155758522974616E-9 1.919971871813908E-9 5.59601983383965E-8 2.852520265347189E-9 -1.757327533436582E-7 -9.558000553765124E-8
tp -3.381085322258283E-8 5.59601983383965E-8 2.442141892063802E-6 1.130876684892087E-7 -4.350246013073855E-6 -2.843535406240828E-6
node -1.72221286813193E-9 2.852520265347189E-9 1.130876684892087E-7 5.505849224087578E-9 -2.326142711650218E-7 -1.444712455568998E-7
peri 1.05666257220378E-7 -1.757327533436582E-7 -4.350246013073855E-6 -2.326142711650218E-7 1.681897706805503E-5 8.692877436763937E-6
i 5.75477733617397E-8 -9.558000553765124E-8 -2.843535406240828E-6 -1.444712455568998E-7 8.692877436763937E-6 4.766098328243299E-6

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 27.4   n/a MPO186431  

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