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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 18 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2351894037461908 3.0992e-08  
a 2.275105508741074 9.5155e-09 au
q 1.740024800680587 6.9378e-08 au
i 4.220528254994895 4.5421e-06 deg
node 31.04937934125737 4.963e-05 deg
peri 267.3818132115842 5.0869e-05 deg
M 235.4693614269666 1.3018e-05 deg
tp 2459434.085204625498
(2021-Aug-07.58520463)
4.7068e-05 TDB
period 1253.431889965271
3.43
7.8636e-06
2.153e-08
d
yr
n .2872114575048627 1.8019e-09 deg/d
Q 2.810186216801561 1.1753e-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 = .730834 au 
 Jupiter MOID = 2.42641 au 
 T_jup = 3.569 
[ 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 16.1   n/a MPO493484  

86800 (2000 GG113)          Discovered 2000-Apr-06 by LINEAR at Socorro
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

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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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