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67710 (2000 TO67)
Classification: Main-belt Asteroid          SPK-ID: 2067710
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1291996944917414 3.5628e-08  
a 2.284203918948372 8.6927e-09 au
q 1.989085470463404 8.3876e-08 au
i 3.070497454797319 4.2959e-06 deg
node 235.5125954000985 6.559e-05 deg
peri 56.28168352040799 6.7722e-05 deg
M 23.55374687415495 1.5534e-05 deg
tp 2459117.999185146989
(2020-Sep-25.49918515)
5.4422e-05 TDB
period 1260.958330993764
3.45
7.198e-06
1.971e-08
d
yr
n .2854971422539262 1.6297e-09 deg/d
Q 2.57932236743334 9.8158e-09 au
  Orbit Determination Parameters
   # obs. used (total)      752  
   data-arc span      7822 days (21.42 yr)  
   first obs. used      1999-04-11  
   last obs. used      2020-09-09  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .54938  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 12:31:46  

Additional Information
 Earth MOID = .972933 au 
 Jupiter MOID = 2.57013 au 
 T_jup = 3.590 
[ 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 16.32   n/a E2021B10  
diameter diameter 1.538 km 0.221 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.297   0.144 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67710 (2000 TO67)          Discovered 2000-Oct-02 by LINEAR at Socorro
Reference: 20030910/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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