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JPL Small-Body Database Browser
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(2019 UT7)
Classification: Apollo [NEO]          SPK-ID: 3883094
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.


Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5985635181610675 1.0549e-05  
a 2.423443784287826 6.3044e-05 au
q .9728587466989338 4.1397e-07 au
i 5.905190843711098 7.7441e-05 deg
node 33.85668966725227 8.0131e-06 deg
peri 335.631322607904 0.00010748 deg
M 164.947687668032 0.0064463 deg
tp 2458765.118892098437
(2019-Oct-08.61889210)
8.5513e-05 TDB
period 1377.995666735341
3.77
0.053771
0.0001472
d
yr
n .2612490073012267 1.0194e-05 deg/d
Q 3.874028821876718 0.00010078 au
  Orbit Determination Parameters
   # obs. used (total)      82  
   # delay obs. used      0  
   # Doppler obs. used      1  
   data-arc span      9 days  
   first obs. used      2019-10-26  
   last obs. used      2019-11-04  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      5  
   norm. resid. RMS      .37825  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 22:00:36  

Additional Information
 Earth MOID = .00659586 au 
 Jupiter MOID = 1.593 au 
 T_jup = 3.235 
[ 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 26.8   .3428 MPO502125 autocmod 2.8

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