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JPL Small-Body Database Browser
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(2017 UV7)
Classification: Apollo [NEO]          SPK-ID: 3788086
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 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4460730923696458 0.00021497  
a 1.548755573518413 0.0005399 au
q .8578973855143299 3.3935e-05 au
i 13.20236091850305 0.0051078 deg
node 32.86124042269986 2.5521e-05 deg
peri 60.87325191402673 0.0023981 deg
M 256.3970436266178 0.13102 deg
tp 2458803.101379433057
(2019-Nov-15.60137943)
0.36215 TDB
period 704.0001477664343
1.93
0.36812
0.001008
d
yr
n .511363529030731 0.00026739 deg/d
Q 2.239613761522496 0.00078073 au
  Orbit Determination Parameters
   # obs. used (total)      37  
   data-arc span      3 days  
   first obs. used      2017-10-27  
   last obs. used      2017-10-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .29205  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-31 06:19:37  

Additional Information
 Earth MOID = .0152299 au 
 Jupiter MOID = 3.05936 au 
 T_jup = 4.310 
[ hide covariance matrix ]
Orbital Elements at Epoch 2458054.5 (2017-Oct-28.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .446174518250158 0.00021431  
q .8588644954448011 3.3304e-05 au
tp 2458098.864150840067
(2017-Dec-11.36415084)
0.0062406 TDB
node 32.89818008671712 1.6904e-05 deg
peri 60.73120433432949 0.0023444 deg
i 13.24025934020968 0.0050852 deg
  Orbit Determination Parameters
   # obs. used (total)      37  
   data-arc span      3 days  
   first obs. used      2017-10-27  
   last obs. used      2017-10-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .29205  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Oct-31 06:19:37  

Additional Information
 Jupiter MOID = 3.05936 au 
 T_jup = 4.310 
Orbit Covariance (6×6)
  e q tp node peri i
e 4.59268284717019E-8 -7.125575802721459E-9 -1.336455672869423E-6 -1.504409141095394E-10 -4.941745653027692E-7 1.089417439746838E-6
q -7.125575802721459E-9 1.1091466318339E-9 2.06907125927648E-7 4.65059904264419E-11 7.586856115479039E-8 -1.688472021289821E-7
tp -1.336455672869423E-6 2.06907125927648E-7 3.894533258704372E-5 1.524865944007108E-9 1.447937757316547E-5 -3.172300023932101E-5
node -1.504409141095394E-10 4.65059904264419E-11 1.524865944007108E-9 2.857429967497734E-10 -3.664982188906753E-9 -1.58667946558666E-9
peri -4.941745653027692E-7 7.586856115479039E-8 1.447937757316547E-5 -3.664982188906753E-9 5.496215293524116E-6 -1.176174479780126E-5
i 1.089417439746838E-6 -1.688472021289821E-7 -3.172300023932101E-5 -1.58667946558666E-9 -1.176174479780126E-5 2.585879580536987E-5

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 26.5   n/a MPO421551  

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