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(2010 AG30)
Classification: Apollo [NEO]          SPK-ID: 3485261
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 2455207.5 (2010-Jan-11.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6946757784588594 0.0038728  
a 2.2605174757767 0.025265 au
q .6901907385716651 0.0010405 au
i 2.087632930228903 0.011232 deg
node 103.581220662242 0.0010351 deg
peri 84.62426697411047 0.009487 deg
M 346.5349781548394 0.25224 deg
tp 2455253.931722128636
(2010-Feb-26.43172213)
0.091353 TDB
period 1241.395681234382
3.40
20.812
0.05698
d
yr
n .2899961756287358 0.0048618 deg/d
Q 3.830844212981735 0.042816 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   data-arc span      4 days  
   first obs. used      2010-01-10  
   last obs. used      2010-01-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      9  
   norm. resid. RMS      .39137  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 03:22:02  

Additional Information
 Earth MOID = .0064875 au 
 Jupiter MOID = 1.12112 au 
 T_jup = 3.249 
[ 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 27.1   n/a MPO170308  

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