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(2015 VT64)
Classification: Apollo [NEO]          SPK-ID: 3733861
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 .1707380589764022 0.00019346  
a 1.165821727230475 0.00028427 au
q .9667715884106272 1.0389e-05 au
i 17.98218373130928 0.01407 deg
node 45.22433619004102 0.00024696 deg
peri 47.94377515107089 0.02042 deg
M 189.4815882524618 0.44829 deg
tp 2459218.278710706205
(2021-Jan-03.77871071)
0.65218 TDB
period 459.7763669668113
1.26
0.16817
0.0004604
d
yr
n .7829893527911286 0.00028638 deg/d
Q 1.364871866050323 0.00033281 au
  Orbit Determination Parameters
   # obs. used (total)      97  
   data-arc span      4 days  
   first obs. used      2015-11-08  
   last obs. used      2015-11-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .44472  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:50  

Additional Information
 Earth MOID = .0240976 au 
 Jupiter MOID = 3.82526 au 
 T_jup = 5.350 
[ 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 26.0   n/a MPO361299  

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