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JPL Small-Body Database Browser
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48615 (1995 FG16)
Classification: Main-belt Asteroid          SPK-ID: 2048615
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 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1791017207500493 7.8326e-08  
a 3.000740051922486 2.0706e-08 au
q 2.463302345099576 2.295e-07 au
i 14.99721461261668 6.839e-06 deg
node 9.432372986348563 1.9449e-05 deg
peri 344.1329430028022 2.5297e-05 deg
M 70.22783349001807 1.9046e-05 deg
tp 2458230.119802142741
(2018-Apr-21.61980214)
9.9033e-05 TDB
period 1898.632844021384
5.20
1.9652e-05
5.38e-08
d
yr
n .189610119267454 1.9626e-09 deg/d
Q 3.538177758745396 2.4415e-08 au
  Orbit Determination Parameters
   # obs. used (total)      673  
   data-arc span      9011 days (24.67 yr)  
   first obs. used      1995-03-28  
   last obs. used      2019-11-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53223  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-04 03:36:24  

Additional Information
 Earth MOID = 1.46186 au 
 Jupiter MOID = 1.91761 au 
 T_jup = 3.177 
[ 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 14.4   n/a MPO337646  

48615 (1995 FG16)          Discovered 1995-Mar-28 by Spacewatch at Kitt Peak
Reference: 20021120/Numbers.arcLast Updated: 2004-04-19

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Alternate Designations
 1995 FG16 = 1997 TO25 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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