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48156 (2001 GT5)
Classification: Main-belt Asteroid          SPK-ID: 2048156
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .155947832940168 4.53e-08  
a 2.264543717632843 7.1636e-09 au
q 1.911393032269729 1.0387e-07 au
i 4.342141274663672 4.7309e-06 deg
node 211.1949845239722 5.3858e-05 deg
peri 163.0691514613865 5.5266e-05 deg
M 305.0948012012484 1.1805e-05 deg
tp 2458790.336823527239
(2019-Nov-02.83682353)
4.0891e-05 TDB
period 1244.713760536643
3.41
5.9062e-06
1.617e-08
d
yr
n .2892231221456012 1.3724e-09 deg/d
Q 2.617694402995956 8.2807e-09 au
  Orbit Determination Parameters
   # obs. used (total)      781  
   data-arc span      9837 days (26.93 yr)  
   first obs. used      1992-11-21  
   last obs. used      2019-10-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55244  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 06:35:54  

Additional Information
 Earth MOID = .912019 au 
 Jupiter MOID = 2.84578 au 
 T_jup = 3.597 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.7   n/a MPO432039  
diameter diameter 1.530 km 0.261 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.329   0.115 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

48156 (2001 GT5)          Discovered 2001-Apr-13 by Spacewatch at Kitt Peak
Reference: 20020921/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2001 GT5 = 2000 AQ77 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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