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(2019 VL5)
Classification: Apollo [NEO]          SPK-ID: 3892813
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .279668928146707 0.00057442  
a 1.000561817337288 0.0003443 au
q .7207357663380475 0.00032753 au
i 1.623339295511856 0.0032215 deg
node 283.9013080611942 0.023965 deg
peri 232.9680336468202 0.046973 deg
M 319.8041801993142 0.019867 deg
tp 2459241.317152607752
(2021-Jan-26.81715261)
0.041199 TDB
period 365.5647530428039
1.00
0.18869
0.0005166
d
yr
n .9847776543102547 0.00050831 deg/d
Q 1.280387868336529 0.00044059 au
  Orbit Determination Parameters
   # obs. used (total)      22  
   data-arc span      4 days  
   first obs. used      2019-11-09  
   last obs. used      2019-11-13  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .48303  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 22:07:38  

Additional Information
 Earth MOID = .00866034 au 
 Jupiter MOID = 3.70342 au 
 T_jup = 6.042 
[ 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 25.9   .28213 E2019-VE8 autocmod 2.8

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