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(2010 VQ)
Classification: Aten [NEO]          SPK-ID: 3550139
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 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1979692839806231 3.6973e-05  
a .8604985611119356 8.2328e-05 au
q .6901462771022493 9.7843e-05 au
i .3563218924229223 0.00023843 deg
node 28.91482863724816 0.031961 deg
peri 198.2730641079776 0.11407 deg
M 48.32324806729059 0.050782 deg
tp 2459161.363925087338
(2020-Nov-07.86392509)
0.046741 TDB
period 291.5571186137863
0.80
0.041842
0.0001146
d
yr
n 1.234749477946643 0.0001772 deg/d
Q 1.030850845121622 9.8626e-05 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      10 days  
   first obs. used      2010-11-01  
   last obs. used      2010-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .57484  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:55:59  

Additional Information
 Earth MOID = .00115531 au 
 Jupiter MOID = 3.94277 au 
 T_jup = 6.844 
[ hide covariance matrix ]
Orbital Elements at Epoch 2455504.5 (2010-Nov-04.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1979356835519674 0.0003115  
q .6909998837772684 0.00040343 au
tp 2455367.553181866664
(2010-Jun-20.05318187)
0.05173 TDB
node 27.8419813614951 0.0028137 deg
peri 200.6724773290768 0.0025485 deg
i .3885848768698802 0.00067785 deg
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      10 days  
   first obs. used      2010-11-01  
   last obs. used      2010-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .57484  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:55:59  

Additional Information
 Jupiter MOID = 3.94277 au 
 T_jup = 6.844 
Orbit Covariance (6×6)
  e q tp node peri i
e 9.703524505512114E-8 -1.256718214777212E-7 1.610818713066534E-5 7.765596781735229E-7 6.602677228422317E-7 2.108283323777649E-7
q -1.256718214777212E-7 1.627595166908851E-7 -2.086193928095087E-5 -1.005731614179516E-6 -8.55102329398436E-7 -2.730465982642448E-7
tp 1.610818713066534E-5 -2.086193928095087E-5 .002675972050290333 .0001295717977723223 .0001106145150849556 3.50083664101009E-5
node 7.765596781735229E-7 -1.005731614179516E-6 .0001295717977723223 7.917132878159949E-6 4.143396642439482E-6 1.734784106824564E-6
peri 6.602677228422317E-7 -8.55102329398436E-7 .0001106145150849556 4.143396642439482E-6 6.494800176062358E-6 1.395712299121985E-6
i 2.108283323777649E-7 -2.730465982642448E-7 3.50083664101009E-5 1.734784106824564E-6 1.395712299121985E-6 4.594829970137972E-7

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 27.7   n/a MPO186458  

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