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160596 (1999 RT152)
Classification: Main-belt Asteroid          SPK-ID: 2160596
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1852520079126781 1.457e-07  
a 2.570831730598162 3.6872e-08 au
q 2.094579990499227 3.5315e-07 au
i 11.69688103376804 1.0633e-05 deg
node 327.6158392499304 3.1509e-05 deg
peri 1.263076052951202 4.8596e-05 deg
M 18.98352807410595 5.6973e-05 deg
tp 2458921.106795339042
(2020-Mar-12.60679534)
0.00023666 TDB
period 1505.597566815351
4.12
3.2391e-05
8.868e-08
d
yr
n .2391077190443886 5.144e-09 deg/d
Q 3.047083470697097 4.3702e-08 au
  Orbit Determination Parameters
   # obs. used (total)      285  
   data-arc span      6797 days (18.61 yr)  
   first obs. used      1999-08-08  
   last obs. used      2018-03-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .63608  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 11:14:55  

Additional Information
 Earth MOID = 1.0834 au 
 Jupiter MOID = 2.30899 au 
 T_jup = 3.377 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.4   n/a MPO436809  

160596 (1999 RT152)          Discovered 1999-Sep-09 by LINEAR at Socorro
Reference: 20070828/Numbers.arcLast Updated: 2007-08-30

[ show close-approach data ]
Alternate Designations
 1999 RT152 = 2002 GJ51 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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