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35135 (1992 RO1)
Classification: Main-belt Asteroid          SPK-ID: 2035135
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2580561023998943 3.485e-08  
a 2.405568959557205 1.1533e-08 au
q 1.784797209799704 8.4756e-08 au
i 12.79210370846002 4.0989e-06 deg
node 135.7462090521689 2.3032e-05 deg
peri 181.7984941620004 2.5004e-05 deg
M 164.703747855325 1.1334e-05 deg
tp 2458377.014834857367
(2018-Sep-15.51483486)
4.1186e-05 TDB
period 1362.778093237489
3.73
9.8008e-06
2.683e-08
d
yr
n .2641662657966307 1.8998e-09 deg/d
Q 3.026340709314706 1.451e-08 au
  Orbit Determination Parameters
   # obs. used (total)      949  
   data-arc span      10050 days (27.52 yr)  
   first obs. used      1992-07-24  
   last obs. used      2020-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5924  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 03:43:27  

Additional Information
 Earth MOID = .771472 au 
 Jupiter MOID = 2.297 au 
 T_jup = 3.444 
[ 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 14.9   n/a MPO351075  
diameter diameter 6.228 km 0.081 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.067   0.004 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35135 (1992 RO1)          Discovered 1992-Sep-01 by Helin, E. F. at Palomar
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1992 RO1 = 1999 JK82 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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