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(2020 UO6)
Classification: Apollo [NEO]          SPK-ID: 54081197
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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .584125376918762 0.00024285  
a 2.348470912256575 0.0013574 au
q .9766694554519542 5.8297e-06 au
i 6.467523565832265 0.0020114 deg
node 214.836876027431 4.6517e-05 deg
peri 158.5818111418194 0.00085448 deg
M 323.628757453529 0.031364 deg
tp 2459133.310325883181
(2020-Oct-10.81032588)
0.00063544 TDB
period 1314.547262355875
3.60
1.1397
0.00312
d
yr
n .2738585445416572 0.00023744 deg/d
Q 3.720272369061195 0.0021504 au
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      3 days  
   first obs. used      2020-10-27  
   last obs. used      2020-10-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .44745  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-30 07:14:59  

Additional Information
 Earth MOID = .00565707 au 
 Jupiter MOID = 1.76568 au 
 T_jup = 3.299 
[ hide covariance matrix ]
Orbital Elements at Epoch 2459151.5 (2020-Oct-29.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5856603376582602 0.00024194  
q .9773586520153318 6.2932e-06 au
tp 2459133.539760489547
(2020-Oct-11.03976049)
0.00038783 TDB
node 214.764777409305 0.00011524 deg
peri 158.9494435734473 0.0012249 deg
i 6.585661486996922 0.0019152 deg
  Orbit Determination Parameters
   # obs. used (total)      45  
   data-arc span      3 days  
   first obs. used      2020-10-27  
   last obs. used      2020-10-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .44745  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Oct-30 07:14:59  

Additional Information
 Jupiter MOID = 1.76568 au 
 T_jup = 3.299 
Orbit Covariance (6×6)
  e q tp node peri i
e 5.853438262220525E-8 -1.517481206632875E-9 8.886069171169681E-8 2.78347429804401E-8 -2.935325365645109E-7 4.631620125808233E-7
q -1.517481206632875E-9 3.960425692019253E-11 -2.240588740512419E-9 -7.194439156794664E-10 7.695387001315468E-9 -1.198472672203758E-8
tp 8.886069171169681E-8 -2.240588740512419E-9 1.504116163420508E-7 4.2741859845134E-8 -4.246307820387708E-7 7.081003759759106E-7
node 2.78347429804401E-8 -7.194439156794664E-10 4.2741859845134E-8 1.327935049684548E-8 -1.389408170346407E-7 2.205431008731798E-7
peri -2.935325365645109E-7 7.695387001315468E-9 -4.246307820387708E-7 -1.389408170346407E-7 1.500390586160571E-6 -2.315865426270957E-6
i 4.631620125808233E-7 -1.198472672203758E-8 7.081003759759106E-7 2.205431008731798E-7 -2.315865426270957E-6 3.668049498558743E-6

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 27.33   .27173 4 autocmod 2.8

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