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(2010 GD35)
Classification: Aten [NEO]          SPK-ID: 3515692
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4816164202425491 1.5448e-06  
a .7640676140330941 8.926e-09 au
q .3960801049392097 1.1824e-06 au
i 7.784891266893727 5.5783e-05 deg
node 25.12541379415072 2.9764e-05 deg
peri 13.79319948875765 5.3103e-05 deg
M 137.3197512309645 0.00028515 deg
tp 2459107.447805021675
(2020-Sep-14.94780502)
0.00019393 TDB
period 243.9473556564619
0.67
4.2748e-06
1.17e-08
d
yr
n 1.475728232557556 2.586e-08 deg/d
Q 1.132055123126978 1.3225e-08 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] 1.867210355093094E-13 2.544E-14
ALN [SET] 1. n/a
NK [SET] 0. n/a
NM [SET] 2. n/a
R0 [SET] 1. n/a
  Orbit Determination Parameters
   # obs. used (total)      65  
   data-arc span      3641 days (9.97 yr)  
   first obs. used      2010-04-12  
   last obs. used      2020-03-31  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      1  
   norm. resid. RMS      .48828  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 03:40:31  

Additional Information
 Earth MOID = .0383692 au 
 Jupiter MOID = 4.28762 au 
 T_jup = 7.476 
 Nongravitational accels. using nonstandard g(r) = (1 au/ r)^2 
[ 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 24.6   n/a MPO446909  

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