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56130 (1999 CM45)
Classification: Main-belt Asteroid          SPK-ID: 2056130
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 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1756230955962362 3.5003e-08  
a 2.441175442758548 9.1511e-09 au
q 2.01244865460778 8.7051e-08 au
i 3.424070851433604 4.2097e-06 deg
node 27.08506869039761 6.9666e-05 deg
peri 10.54293213580293 7.1064e-05 deg
M 200.6306588644628 1.6298e-05 deg
tp 2459217.235847029828
(2021-Jan-02.73584703)
6.5421e-05 TDB
period 1393.146908613462
3.81
7.8336e-06
2.145e-08
d
yr
n .2584077800942703 1.453e-09 deg/d
Q 2.869902230909316 1.0758e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1134  
   data-arc span      10375 days (28.41 yr)  
   first obs. used      1990-12-09  
   last obs. used      2019-05-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52186  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 05:08:53  

Additional Information
 Earth MOID = 1.01925 au 
 Jupiter MOID = 2.55049 au 
 T_jup = 3.478 
[ 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 14.8   n/a MPO436175  
diameter diameter 3.257 km 0.061 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.152   0.023 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

56130 (1999 CM45)          Discovered 1999-Feb-10 by LINEAR at Socorro
Reference: 20030318/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 CM45 = 2001 OM73 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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