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(2019 VT3)
Classification: Apollo [NEO]          SPK-ID: 3892702
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 .1317033963841947 0.00010827  
a 1.037217258968097 6.6069e-05 au
q .900612223173694 5.617e-05 au
i 7.814222112002813 0.0071416 deg
node 40.73350685890624 0.00064147 deg
peri 92.13657582212186 0.0051542 deg
M 305.0755171705863 0.020139 deg
tp 2459259.366268148439
(2021-Feb-13.86626815)
0.027207 TDB
period 385.8362508256348
1.06
0.036866
0.0001009
d
yr
n .9330383011696053 8.915e-05 deg/d
Q 1.173822294762501 7.4771e-05 au
  Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      3 days  
   first obs. used      2019-11-05  
   last obs. used      2019-11-08  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .6386  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 22:07:31  

Additional Information
 Earth MOID = .00411163 au 
 Jupiter MOID = 3.83528 au 
 T_jup = 5.894 
[ 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 28.2   .32818 E2019-VC6 autocmod 2.8

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