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86800 (2000 GG113)
Classification: Main-belt Asteroid          SPK-ID: 2086800
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2352549544017979 3.0993e-08  
a 2.27474134954886 9.5033e-09 au
q 1.739597177084859 6.9371e-08 au
i 4.220890472834742 4.5426e-06 deg
node 31.04560902939498 4.9626e-05 deg
peri 267.4248600517687 5.0865e-05 deg
M 292.8789638915721 1.3245e-05 deg
tp 2459434.142912402777
(2021-Aug-07.64291240)
4.7053e-05 TDB
period 1253.130960748658
3.43
7.8529e-06
2.15e-08
d
yr
n .2872804290023487 1.8003e-09 deg/d
Q 2.809885522012861 1.1739e-08 au
  Orbit Determination Parameters
   # obs. used (total)      730  
   data-arc span      7354 days (20.13 yr)  
   first obs. used      2000-03-10  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54965  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 15:49:33  

Additional Information
 Earth MOID = .728459 au 
 Jupiter MOID = 2.42636 au 
 T_jup = 3.569 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457141.5 (2015-Apr-29.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2358035185110121 3.0992e-08  
q 1.738319629376744 6.9414e-08 au
tp 2456927.183005946885
(2014-Sep-26.68300595)
3.8461e-05 TDB
node 31.07191930906405 4.9633e-05 deg
peri 267.3737528100486 5.0867e-05 deg
i 4.221545029466079 4.5418e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      730  
   data-arc span      7354 days (20.13 yr)  
   first obs. used      2000-03-10  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .54965  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 15:49:33  

Additional Information
 Jupiter MOID = 2.42636 au 
 T_jup = 3.569 
Orbit Covariance (6×6)
  e q tp node peri i
e 9.605346552205677E-16 -2.140111127034775E-15 8.783720049728679E-14 2.556464812440936E-15 1.925248534330705E-14 7.629867010459356E-16
q -2.140111127034775E-15 4.818309929650304E-15 -9.052393627448829E-14 -7.433201420176736E-15 -1.299393658428984E-14 -1.377753929294582E-15
tp 8.783720049728679E-14 -9.052393627448829E-14 1.479229450983384E-9 -1.866271863314134E-11 4.384167421358969E-10 2.137482087153665E-12
node 2.556464812440936E-15 -7.433201420176736E-15 -1.866271863314134E-11 2.463481281002295E-9 -2.461639962725678E-9 -4.460998273210526E-12
peri 1.925248534330705E-14 -1.299393658428984E-14 4.384167421358969E-10 -2.461639962725678E-9 2.587491145237169E-9 5.047457718610804E-12
i 7.629867010459356E-16 -1.377753929294582E-15 2.137482087153665E-12 -4.460998273210526E-12 5.047457718610804E-12 2.062823243336033E-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 16.08   n/a E2021B10  

86800 (2000 GG113)          Discovered 2000-Apr-06 by LINEAR at Socorro
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
2140-Jun-26 18:10 < 00:01 Hebe 0.0122763820086587 0.0122599694354279 0.012292801765161 7.14548978800885 7.14548971714004 2502856.257281552 0.922604555015756 943.253747623654 45.830029102492 29.8485433069358 20009.8250050891 T 18 CATAB v2.0f-lin.ifort 2020-May-20 15:49:43 2020-May-20 15:49
2178-Apr-02 22:37 00:01 Hebe 0.0364818849412667 0.0364575442303024 0.0365062258441485 7.43313713676752 7.43313711384259 2516650.442218937 1.15441216847651 1220.7411596842 46.2137200317658 6.2181012189377 13537.0598304289 T 18 CATAB v2.0f-lin.ifort 2020-May-20 15:49:43 2020-May-20 15:49
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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