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7092 Cadmus (1992 LC)
Classification: Apollo [NEO]          SPK-ID: 2007092
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 195 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6975311405776554 4.6371e-08  
a 2.53580088119983 6.8173e-09 au
q .767000800258689 1.1804e-07 au
i 17.8090746855259 8.8143e-06 deg
node 57.69916081528585 1.8583e-05 deg
peri 93.80597852906999 1.8335e-05 deg
M 1.502892490531936 6.2955e-06 deg
tp 2458994.342611401748
(2020-May-24.84261140)
2.5772e-05 TDB
period 1474.929117908006
4.04
5.9478e-06
1.628e-08
d
yr
n .2440795260118078 9.8428e-10 deg/d
Q 4.304600962140972 1.1573e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1117  
   data-arc span      14682 days (40.20 yr)  
   first obs. used      1980-06-02  
   last obs. used      2020-08-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54635  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-14 07:25:34  

Additional Information
 Earth MOID = .0978362 au 
 Jupiter MOID = 1.51346 au 
 T_jup = 3.004 
[ 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 15.1   n/a MPO347582  
diameter diameter 6.319 km 3.783 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  
geometric albedo albedo 0.046   0.086 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2017AJ....154..168M)  

7092 Cadmus (1992 LC)          Discovered 1992-Jun-04 by Shoemaker, C. S. at Palomar
Reference: DISCOVERY.DBLast Updated: 2003-08-29

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