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173424 (2000 GV23)
Classification: Main-belt Asteroid          SPK-ID: 2173424
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1439236448675842 3.7615e-08  
a 2.637422531546321 1.4516e-08 au
q 2.257835067750283 1.0205e-07 au
i 11.57101139580447 5.7465e-06 deg
node 12.97100534773502 2.0117e-05 deg
peri 98.24306428003375 2.9906e-05 deg
M 7.70587683926105 2.0084e-05 deg
tp 2459167.012127482423
(2020-Nov-13.51212748)		 8.7314e-05 TDB
period 1564.472720989358
4.28		 1.2916e-05
3.536e-08		 d
yr
n .2301094772508014 1.8997e-09 deg/d
Q 3.017009995342358 1.6605e-08 au
   Orbit Determination Parameters
   # obs. used (total)      593  
   data-arc span      7607 days (20.83 yr)  
   first obs. used      2000-03-27  
   last obs. used      2021-01-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57531  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 11:29:01  

Additional Information
 Earth MOID = 1.3082 au 
 Jupiter MOID = 2.15236 au 
 T_jup = 3.353 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457529.5 (2016-May-21.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1419767984011633 3.7849e-08  
q 2.262758696214205 1.0259e-07 au
tp 2457603.623878573591
(2016-Aug-03.12387857)		 9.1392e-05 TDB
node 13.01865051571932 2.0089e-05 deg
peri 98.46206020622309 3.0134e-05 deg
i 11.57929194599033 5.7502e-06 deg
   Orbit Determination Parameters
   # obs. used (total)      593  
   data-arc span      7607 days (20.83 yr)  
   first obs. used      2000-03-27  
   last obs. used      2021-01-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57531  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 11:29:01  

Additional Information
 Jupiter MOID = 2.15236 au 
 T_jup = 3.353 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.432579742339596E-15 -3.854973936110114E-15 1.386205919816522E-12 -7.95326110390619E-15 3.284370517821502E-13 -4.023680994288734E-15
q -3.854973936110114E-15 1.052521600388176E-14 -3.958297663474168E-12 2.144795104315497E-14 -9.414628971517283E-13 1.073517049557858E-14
tp 1.386205919816522E-12 -3.958297663474168E-12 8.352535881672961E-9 -2.884249285077229E-11 2.06548185830789E-9 -9.690359918473763E-12
node -7.95326110390619E-15 2.144795104315497E-14 -2.884249285077229E-11 4.035877063519163E-10 -4.020215351840991E-10 -2.830219387272503E-11
peri 3.284370517821502E-13 -9.414628971517283E-13 2.06548185830789E-9 -4.020215351840991E-10 9.080750223825679E-10 2.552080909246067E-11
i -4.023680994288734E-15 1.073517049557858E-14 -9.690359918473763E-12 -2.830219387272503E-11 2.552080909246067E-11 3.306451773900812E-11

[ 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 15.9   n/a MPO493969  

173424 (2000 GV23)          Discovered 2000-Apr-05 by LINEAR at Socorro
Reference: 20080122/Numbers.arcLast Updated: 2008-01-28

[ 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
2186-Feb-20 09:45 00:02 Ceres 0.00942016318383791 0.00937896992281802 0.00946136170530897 3.82875000597316 3.82873829273715 2519530.906142901 1.56437524076845 2064.94765133453 63.8712084269356 9.67213449496855 3726.38092523251 T 23 CATAB v2.0f-lin.ifort 2021-Feb-24 11:29:02 2021-Feb-24 11:29
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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