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85879 (1999 CO10)
Classification: Main-belt Asteroid          SPK-ID: 2085879
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .08288330788705113 5.6634e-08  
a 2.319090976361885 1.0622e-08 au
q 2.126877044950001 1.3233e-07 au
i 23.93898244008223 6.3241e-06 deg
node 307.4138234957995 1.0307e-05 deg
peri 177.0216784104252 2.8048e-05 deg
M 17.31493545996112 2.5353e-05 deg
tp 2458938.456901008002
(2020-Mar-29.95690101)
9.0818e-05 TDB
period 1289.956620904976
3.53
8.8624e-06
2.426e-08
d
yr
n .2790791520938433 1.9174e-09 deg/d
Q 2.511304907773769 1.1502e-08 au
  Orbit Determination Parameters
   # obs. used (total)      665  
   data-arc span      8215 days (22.49 yr)  
   first obs. used      1997-08-05  
   last obs. used      2020-02-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52088  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 20:40:22  

Additional Information
 Earth MOID = 1.14233 au 
 Jupiter MOID = 2.56658 au 
 T_jup = 3.460 
[ 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 15.2   n/a MPO259850  
diameter diameter 2.653 km 0.222 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.181   0.046 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

85879 (1999 CO10)          Discovered 1999-Feb-12 by LINEAR at Socorro
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

Alternate Designations
 1999 CO10 = 1997 PW5 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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