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JPL Small-Body Database Browser
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193219 (2000 RG29)
Classification: Main-belt Asteroid          SPK-ID: 2193219
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1488024005401845 4.8044e-08  
a 2.409725643753634 9.8899e-09 au
q 2.051152683319851 1.1406e-07 au
i 6.569431322837183 5.1509e-06 deg
node 238.7310503876589 3.638e-05 deg
peri 148.5774265514869 3.9314e-05 deg
M 329.2511975453457 1.3226e-05 deg
tp 2458717.201256353702
(2019-Aug-21.70125635)
5.0275e-05 TDB
period 1366.31182138847
3.74
8.4113e-06
2.303e-08
d
yr
n .2634830456448527 1.6221e-09 deg/d
Q 2.768298604187416 1.1361e-08 au
  Orbit Determination Parameters
   # obs. used (total)      627  
   data-arc span      7027 days (19.24 yr)  
   first obs. used      2000-09-01  
   last obs. used      2019-11-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48481  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-04 15:35:44  

Additional Information
 Earth MOID = 1.05887 au 
 Jupiter MOID = 2.67373 au 
 T_jup = 3.496 
[ 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 15.7   n/a MPO454341  

193219 (2000 RG29)          Discovered 2000-Sep-01 by LINEAR at Socorro
Reference: 20081113/Numbers.arcLast Updated: 2008-11-17

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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
2129-Sep-13 09:20 00:03 Iris 0.00411280001582076 0.00409627732896376 0.00412941720578767 2.02711272735615 2.02711203781908 2498916.888715129 3.09527642775034 1284.21323292763 68.225885049333 -50.1460024678509 6913.86675809174 T 16 CATAB v2.0f-lin.ifort 2019-Dec-04 15:35:47 2019-Dec-04 15:36
2147-Aug-07 08:29 00:03 Hebe 0.0419029613971953 0.0418801321199172 0.0419258093914691 5.91497028189154 5.91497025680965 2505453.853245961 3.25492367000436 1802.19716646814 40.3098501622382 -50.8374467658938 120559.110122916 T 16 CATAB v2.0f-lin.ifort 2019-Dec-04 15:35:47 2019-Dec-04 15:36
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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