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(2015 VP105)
Classification: Apollo [NEO]          SPK-ID: 3734563
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4250581359165433 0.00023786  
a 1.435060460626673 0.000554 au
q .8250763363051633 2.3364e-05 au
i 25.98714351144347 0.0094169 deg
node 48.70947191649248 7.8951e-05 deg
peri 294.6890778805151 0.0091324 deg
M 260.2450467766663 0.57546 deg
tp 2459174.494569376788
(2020-Nov-20.99456938)
1.1045 TDB
period 627.9191453822667
1.72
0.36361
0.0009955
d
yr
n .5733222225304788 0.00033199 deg/d
Q 2.045044584948182 0.00078948 au
  Orbit Determination Parameters
   # obs. used (total)      64  
   data-arc span      2 days  
   first obs. used      2015-11-12  
   last obs. used      2015-11-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34646  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:40  

Additional Information
 Earth MOID = .00707721 au 
 Jupiter MOID = 3.6139 au 
 T_jup = 4.480 
[ 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 25.6   n/a MPO355073  

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