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JPL Small-Body Database Browser
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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.


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Orbital Elements at Epoch 2456454.5 (2013-Jun-11.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4819772830301848 2.1328e-06  
a .7641479732114038 9.0702e-09 au
q .395846009249949 1.6254e-06 au
i 7.707299198842776 7.3097e-05 deg
node 25.35979129171799 3.595e-05 deg
peri 13.66060437185652 0.000106 deg
M 43.92836566276836 0.00044341 deg
tp 2456424.728057589712
(2013-May-12.22805759)
0.0003001 TDB
period 243.9858416309731
0.67
4.3441e-06
1.189e-08
d
yr
n 1.475495453316088 2.6271e-08 deg/d
Q 1.132449937172859 1.3442e-08 au

Additional Model Parameters
 Parameter Value Uncertainty (1-sigma) 
A2 [EST] 1.526047548322902E-13 4.475E-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)      57  
   data-arc span      2924 days (8.01 yr)  
   first obs. used      2010-04-12  
   last obs. used      2018-04-14  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .46977  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jan-14 15:58:55  

Additional Information
 Earth MOID = .0384376 au 
 Jupiter MOID = 4.29472 au 
 T_jup = 7.475 
 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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