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(2010 RX30)
Classification: Aten [NEO]          SPK-ID: 3545558
[ 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 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3885010267914889 6.0038e-07  
a .8307164075347253 1.2968e-08 au
q .5079822302349476 4.9098e-07 au
i 5.063286351496716 1.7188e-05 deg
node 165.9978059721241 7.4867e-06 deg
peri 319.9301926362774 1.8285e-05 deg
M 200.6016617059585 2.324e-05 deg
tp 2459122.950030664564
(2020-Sep-30.45003066)		 1.9532e-05 TDB
period 276.5525131003882
0.76		 6.4757e-06
1.773e-08		 d
yr
n 1.301741922226975 3.0481e-08 deg/d
Q 1.153450584834503 1.8006e-08 au
   Orbit Determination Parameters
   # obs. used (total)      101  
   data-arc span      1073 days (2.94 yr)  
   first obs. used      2010-09-05  
   last obs. used      2013-08-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      1  
   norm. resid. RMS      .50711  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:50  

Additional Information
 Earth MOID = .000743995 au 
 Jupiter MOID = 3.9064 au 
 T_jup = 6.997 
[ 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 MPO279189  

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