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85780 (1998 VK2)
Classification: Main-belt Asteroid          SPK-ID: 2085780
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 .1793883107983945 4.2874e-08  
a 2.781241899100421 1.9016e-08 au
q 2.282319612899078 1.2099e-07 au
i 3.459414234349527 4.9426e-06 deg
node 30.8902956932577 8.3209e-05 deg
peri 356.4588897587088 8.4369e-05 deg
M 247.4439921035292 1.6233e-05 deg
tp 2459530.191193352876
(2021-Nov-11.69119335)
7.9439e-05 TDB
period 1694.168380442485
4.64
1.7375e-05
4.757e-08
d
yr
n .2124936364979109 2.1793e-09 deg/d
Q 3.280164185301765 2.2427e-08 au
  Orbit Determination Parameters
   # obs. used (total)      472  
   data-arc span      9391 days (25.71 yr)  
   first obs. used      1993-08-15  
   last obs. used      2019-05-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58275  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 12:28:30  

Additional Information
 Earth MOID = 1.28695 au 
 Jupiter MOID = 2.17042 au 
 T_jup = 3.307 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456888.5 (2014-Aug-19.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1806175020096105 4.2716e-08  
q 2.276687996750813 1.2022e-07 au
tp 2456147.863979382252
(2012-Aug-08.36397938)
6.5843e-05 TDB
node 30.92086383652333 8.3127e-05 deg
peri 356.9629903648039 8.4274e-05 deg
i 3.462531800356263 4.9465e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      472  
   data-arc span      9391 days (25.71 yr)  
   first obs. used      1993-08-15  
   last obs. used      2019-05-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58275  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 12:28:30  

Additional Information
 Jupiter MOID = 2.17042 au 
 T_jup = 3.307 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.824657307339781E-15 -5.091035025776926E-15 -2.188456791298245E-13 -2.728119564777152E-15 -7.980048933024848E-14 -6.332921731188673E-16
q -5.091035025776926E-15 1.445189438719564E-14 7.466318382062913E-13 7.677390503547809E-15 2.767406222890308E-13 2.065772871572763E-15
tp -2.188456791298245E-13 7.466318382062913E-13 4.335357950552439E-9 1.849561145446281E-11 9.356104086399345E-10 -3.3454792356322E-13
node -2.728119564777152E-15 7.677390503547809E-15 1.849561145446281E-11 6.910082333471595E-9 -6.893150090109396E-9 -3.917374870316921E-11
peri -7.980048933024848E-14 2.767406222890308E-13 9.356104086399345E-10 -6.893150090109396E-9 7.102067411602351E-9 3.908700831820921E-11
i -6.332921731188673E-16 2.065772871572763E-15 -3.3454792356322E-13 -3.917374870316921E-11 3.908700831820921E-11 2.446805742621236E-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 15.6   n/a MPO436375  
diameter diameter 4.924 km 1.622 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.046   0.023 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

85780 (1998 VK2)          Discovered 1998-Nov-10 by ODAS at Caussols
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

[ 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
2174-Mar-30 12:42 00:20 Amphi 0.0290581808909596 0.0290546193757899 0.0290617787599672 2.27567368937075 2.27567360243576 2515186.028941787 20.3354821083935 1740.27417760206 63.3114883157621 -84.4889689754027 68235.8445569085 T 16 CATAB v2.0e-lin.ifort 2019-Jul-13 12:28:33 2019-Jul-13 12:28
2189-Sep-30 00:27 00:01 David 0.0479705424373527 0.0479636582351674 0.0479774576145931 5.43844198925884 5.43844193135146 2520848.518649126 1.12061384777916 1963.80881905894 38.5430927099241 -79.9777745475625 183258.573891712 T 16 CATAB v2.0e-lin.ifort 2019-Jul-13 12:28:33 2019-Jul-13 12:28
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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