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79627 (1998 RP67)
Classification: Main-belt Asteroid          SPK-ID: 2079627
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05231846641133292 9.3974e-08  
a 2.523094080881296 1.158e-08 au
q 2.391089667958075 2.3649e-07 au
i 11.19533823604051 6.7189e-06 deg
node 350.3206503204501 1.6963e-05 deg
peri 68.96683612960636 0.00041385 deg
M 100.723190057776 0.00039168 deg
tp 2458590.932426331715
(2019-Apr-17.43242633)
0.0015927 TDB
period 1463.856798379864
4.01
1.0077e-05
2.759e-08
d
yr
n .2459256946433784 1.693e-09 deg/d
Q 2.655098493804517 1.2185e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1022  
   data-arc span      7937 days (21.73 yr)  
   first obs. used      1998-09-14  
   last obs. used      2020-06-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51986  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 21:22:34  

Additional Information
 Earth MOID = 1.42429 au 
 Jupiter MOID = 2.4983 au 
 T_jup = 3.427 
[ 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 15.3   n/a MPO453218  
diameter diameter 2.237 km 0.796 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.322   0.261 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

79627 (1998 RP67)          Discovered 1998-Sep-14 by LINEAR at Socorro
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

[ hide close-approach data ]
Close-Approach Data   ...sorted by Date/Time (TDB)
Date/Time (TDB) Time Uncertainty
(days_HH:MM)
Body Nominal Distance (au) Minimum Distance (au) Maximum Distance (au) V-relative (km/s) V-infinity (km/s) JD (TDB) Time Uncertainty (minutes) Semi-major axis (km) Semi-minor axis (km) range-LOV angle (deg) N-sigma BP Orbit Ref. Reference Modified
1970-Jun-03 23:34 00:07 Amphi 0.0492661591393529 0.0492547849092324 0.0492775334328271 1.85507337927839 1.85507331637657 2440741.481611146 7.25835274396897 575.250151143008 278.841419711064 11.7349001661076 13615.2916401596 T 24 CATAB v2.0f-lin.ifort 2020-Nov-12 21:22:37 2020-Nov-12 21:22
2194-Dec-14 11:25 00:12 Amphi 0.0317803124602417 0.0317466953319764 0.0318139558142393 1.7079848666717 1.70798476076318 2522749.975580454 12.360435145397 2225.75655921767 355.332609788176 41.9552290014121 9059.55675979328 T 24 CATAB v2.0f-lin.ifort 2020-Nov-12 21:22:37 2020-Nov-12 21:22
2196-Oct-22 13:26 00:16 Amphi 0.0479554911614974 0.0479164206374461 0.0479945705185591 1.65699538354732 1.65699531120151 2523428.059428893 15.6583587939911 2203.40438664689 345.3738910164 28.5388978959894 10297.1652968929 T 24 CATAB v2.0f-lin.ifort 2020-Nov-12 21:22:37 2020-Nov-12 21:22

Alternate Designations
 1998 RP67 = 2000 DE82 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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