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JPL Small-Body Database Browser
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(2015 VY105)
Classification: Apollo [NEO]          SPK-ID: 3734615
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7085639180967019 0.00049583  
a 2.702078546048178 0.0040549 au
q .7874831844552413 0.00015812 au
i 8.734906713401468 0.0079459 deg
node 52.12273469434291 0.00019672 deg
peri 59.42371594022009 0.011244 deg
M 271.0784383050868 0.60954 deg
tp 2459001.228251499115
(2020-May-31.72825150)
3.649 TDB
period 1622.35309175788
4.44
3.6519
0.009998
d
yr
n .2218999068876717 0.00049949 deg/d
Q 4.616673907641115 0.006928 au
  Orbit Determination Parameters
   # obs. used (total)      34  
   data-arc span      1 day  
   first obs. used      2015-11-14  
   last obs. used      2015-11-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .37309  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:39  

Additional Information
 Earth MOID = 1.6419E-5 au 
 Jupiter MOID = .822478 au 
 T_jup = 2.931 
[ 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 29.0   n/a MPO355074  
rotation period rot_per 0.0384 h n/a LCDB (Rev. 2019-January); Warner et al., 2009 Published Reference List:
[Carbognani, A.; Buzzi, L. (2016) Minor Planet Bull. 43, 115-118.]

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