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34029 (2000 OX25)
Classification: Main-belt Asteroid          SPK-ID: 2034029
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .005956436164635226 3.7038e-08  
a 2.795175104938425 1.4192e-08 au
q 2.778525822856881 1.0279e-07 au
i 6.063489478196356 4.64e-06 deg
node 339.9366333785819 3.2475e-05 deg
peri 213.9771631619907 0.00037084 deg
M 199.8631663198595 0.0003708 deg
tp 2459759.777783675233
(2022-Jun-29.27778368)
0.0017588 TDB
period 1706.915241430693
4.67
1.3e-05
3.559e-08
d
yr
n .2109067815800023 1.6063e-09 deg/d
Q 2.811824387019968 1.4277e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1349  
   data-arc span      10297 days (28.19 yr)  
   first obs. used      1991-09-07  
   last obs. used      2019-11-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53502  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-14 02:38:22  

Additional Information
 Earth MOID = 1.77925 au 
 Jupiter MOID = 2.15976 au 
 T_jup = 3.319 
[ 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 14.2   n/a MPO395328  
diameter diameter 5.018 km 0.327 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.176   0.022 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

34029 (2000 OX25)          Discovered 2000-Jul-23 by LINEAR at Socorro
Reference: 20020128/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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