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243768 (2000 RS63)
Classification: Main-belt Asteroid          SPK-ID: 2243768
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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2161372416637793 4.4514e-08  
a 2.326192544294821 1.1322e-08 au
q 1.82341570419209 1.0176e-07 au
i 4.044615783027552 6.0461e-06 deg
node 227.329513358357 7.0858e-05 deg
peri 110.6406556033463 7.2319e-05 deg
M 208.9739692852073 1.6223e-05 deg
tp 2459544.146033364431
(2021-Nov-25.64603336)
6.0665e-05 TDB
period 1295.886352073912
3.55
9.4606e-06
2.59e-08
d
yr
n .2778021386087312 2.0281e-09 deg/d
Q 2.828969384397553 1.3769e-08 au
  Orbit Determination Parameters
   # obs. used (total)      212  
   data-arc span      7139 days (19.55 yr)  
   first obs. used      2000-09-03  
   last obs. used      2020-03-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .65288  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 00:54:27  

Additional Information
 Earth MOID = .819331 au 
 Jupiter MOID = 2.57963 au 
 T_jup = 3.539 
[ 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 17.5   n/a MPO454790  

243768 (2000 RS63)          Discovered 2000-Sep-03 by LINEAR at Socorro
Reference: 20100726/Numbers.arcLast Updated: 2010-07-28

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
2176-Oct-20 18:26 00:04 Amphi 0.0485113047460907 0.048471729568097 0.0485508831985235 4.38014279446271 4.38014276740806 2516121.267820694 3.83721910757546 2070.19700368619 60.5568481988009 17.6711928137399 36514.0441318379 T 11 CATAB v2.0f-lin.ifort 2020-Nov-12 00:54:27 2020-Nov-12 00:54
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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