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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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3885083585781531 6.003e-07  
a .8306231441757416 1.1674e-08 au
q .5079191098349995 4.9162e-07 au
i 5.063503830209114 1.7188e-05 deg
node 165.9960366321144 7.4967e-06 deg
peri 319.946962376179 1.8097e-05 deg
M 100.9665443118387 2.684e-05 deg
tp 2459122.950418160333
(2020-Sep-30.45041816)		 1.9547e-05 TDB
period 276.5059421668921
0.76		 5.8295e-06
1.596e-08		 d
yr
n 1.301961170088392 2.7449e-08 deg/d
Q 1.153327178516484 1.621e-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.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      1  
   norm. resid. RMS      .50019  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 04:07:31  

Additional Information
 Earth MOID = .00122519 au 
 Jupiter MOID = 3.90591 au 
 T_jup = 6.998 
[ 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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