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(2010 GD35)
Classification: Aten [NEO]          SPK-ID: 3515692
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4816375881246107 1.5448e-06  
a .7640701558499076 7.986e-09 au
q .3960652488283627 1.1819e-06 au
i 7.785087205730937 5.5783e-05 deg
node 25.12927220471758 2.9758e-05 deg
peri 13.79771300807585 5.3069e-05 deg
M 202.1736340090424 0.00028711 deg
tp 2459107.448657665375
(2020-Sep-14.94865767)
0.00019392 TDB
period 243.9485729636632
0.67
3.8246e-06
1.047e-08
d
yr
n 1.475720868650553 2.3136e-08 deg/d
Q 1.132075062871452 1.1832e-08 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] 1.867295566370109E-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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .48824  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Sep-11 07:31:32  

Additional Information
 Earth MOID = .0385483 au 
 Jupiter MOID = 4.28657 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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