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(2015 VU64)
Classification: Aten [NEO]          SPK-ID: 3733862
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1080104860282808 1.8718e-05  
a .9348575379049574 7.7562e-06 au
q .833883120868641 2.4411e-05 au
i 2.483961550600128 0.00036162 deg
node 224.5283879418883 0.00016087 deg
peri 49.78821051700524 0.00038833 deg
M 137.1739864961001 0.020436 deg
tp 2458874.698494784952
(2020-Jan-26.19849478)
0.017177 TDB
period 330.1540112250439
0.90
0.0041087
1.125e-05
d
yr
n 1.090400200391968 1.357e-05 deg/d
Q 1.035831954941274 8.5939e-06 au
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      2 days  
   first obs. used      2015-11-08  
   last obs. used      2015-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .42701  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:50  

Additional Information
 Earth MOID = .00107975 au 
 Jupiter MOID = 3.99067 au 
 T_jup = 6.408 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457335.5 (2015-Nov-09.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1145389158878248 1.6952e-05  
q .8250209029239866 2.1733e-05 au
tp 2457225.129732042486
(2015-Jul-21.62973204)
0.0030294 TDB
node 224.8561789464617 2.1798e-05 deg
peri 49.71875580967704 0.00042065 deg
i 2.571646681820772 0.00033987 deg
  Orbit Determination Parameters
   # obs. used (total)      30  
   data-arc span      2 days  
   first obs. used      2015-11-08  
   last obs. used      2015-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      5  
   norm. resid. RMS      .42701  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:50  

Additional Information
 Jupiter MOID = 3.99067 au 
 T_jup = 6.408 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.873569347380959E-10 -3.683655207561083E-10 5.118983593510472E-8 1.564631549077547E-10 5.189941580844158E-9 5.662551238674719E-9
q -3.683655207561083E-10 4.723433589495698E-10 -6.554230096507851E-8 -2.000937345510474E-10 -6.553194118815947E-9 -7.25925342160767E-9
tp 5.118983593510472E-8 -6.554230096507851E-8 9.177160040094726E-6 3.015494552406895E-8 9.932840172291993E-7 1.002083106547818E-6
node 1.564631549077547E-10 -2.000937345510474E-10 3.015494552406895E-8 4.751338619303846E-10 4.772019943959094E-9 2.09337289137333E-9
peri 5.189941580844158E-9 -6.553194118815947E-9 9.932840172291993E-7 4.772019943959094E-9 1.769495637304309E-7 9.663651302956946E-8
i 5.662551238674719E-9 -7.25925342160767E-9 1.002083106547818E-6 2.09337289137333E-9 9.663651302956946E-8 1.155108529060902E-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 30.6   n/a MPO355052  

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