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160751 (2000 SC83)
Classification: Main-belt Asteroid          SPK-ID: 2160751
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 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2048929514239601 4.1944e-08  
a 2.350372430004008 1.2672e-08 au
q 1.868797685874981 9.7665e-08 au
i 5.066698002770051 6.1346e-06 deg
node 345.080535175341 4.8176e-05 deg
peri 287.4603819580645 5.1772e-05 deg
M 232.3922784572341 2.3294e-05 deg
tp 2459467.028206711148
(2021-Sep-09.52820671)
8.6959e-05 TDB
period 1316.144135993583
3.60
1.0644e-05
2.914e-08
d
yr
n .2735262728107123 2.212e-09 deg/d
Q 2.831947174133034 1.5268e-08 au
  Orbit Determination Parameters
   # obs. used (total)      520  
   data-arc span      9599 days (26.28 yr)  
   first obs. used      1993-10-12  
   last obs. used      2020-01-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .61372  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 13:24:34  

Additional Information
 Earth MOID = .860331 au 
 Jupiter MOID = 2.30894 au 
 T_jup = 3.524 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457171.5 (2015-May-29.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2053032682496444 4.1937e-08  
q 1.867387024694209 9.7696e-08 au
tp 2456835.388884377743
(2014-Jun-26.88888438)
7.869e-05 TDB
node 345.121554208117 4.814e-05 deg
peri 287.4824371334698 5.1738e-05 deg
i 5.069582602941763 6.1369e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      520  
   data-arc span      9599 days (26.28 yr)  
   first obs. used      1993-10-12  
   last obs. used      2020-01-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .61372  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 13:24:34  

Additional Information
 Jupiter MOID = 2.30894 au 
 T_jup = 3.524 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.758690442920547E-15 -4.075881561267763E-15 1.438821145715648E-12 1.424668561893451E-14 3.381465643654183E-13 1.690962626084653E-15
q -4.075881561267763E-15 9.544539938603837E-15 -3.17078716120977E-12 -3.218308448149405E-14 -7.400543669931405E-13 -3.608323889644736E-15
tp 1.438821145715648E-12 -3.17078716120977E-12 6.192188068153881E-9 4.07349356945491E-11 1.505829570385983E-9 -1.110169470115506E-12
node 1.424668561893451E-14 -3.218308448149405E-14 4.07349356945491E-11 2.317505219036966E-9 -2.297581231811593E-9 -5.528158039863422E-12
peri 3.381465643654183E-13 -7.400543669931405E-13 1.505829570385983E-9 -2.297581231811593E-9 2.676851762113159E-9 5.322226186897805E-12
i 1.690962626084653E-15 -3.608323889644736E-15 -1.110169470115506E-12 -5.528158039863422E-12 5.322226186897805E-12 3.766136144470823E-11

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 16.4   n/a MPO454064  
diameter diameter 1.401 km 0.240 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.206   0.054 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

160751 (2000 SC83)          Discovered 2000-Sep-24 by LINEAR at Socorro
Reference: 20070828/Numbers.arcLast Updated: 2007-08-30

[ 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
2121-Jun-26 14:21 00:02 Hebe 0.0447506275516689 0.0447291516452363 0.0447721134210376 8.80019708324977 8.80019706746399 2495916.097851296 2.31830043312841 1502.74683603828 53.1836725315555 -44.5786930111742 88395.3111311667 T 16 CATAB v2.0f-lin.ifort 2020-Feb-24 13:24:37 2020-Feb-24 13:24
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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