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(2018 GU1)
Classification: Apollo [NEO]          SPK-ID: 3802429
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | 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 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4162752176919718 0.00050383  
a 1.548512969213153 0.0012885 au
q .903905395855106 2.8058e-05 au
i 23.09698352610983 0.017525 deg
node 198.5477526320451 9.9603e-05 deg
peri 311.3289977204219 0.014313 deg
M 60.379273224729 0.5356 deg
tp 2458882.452694675388
(2020-Feb-02.95269468)		 0.89981 TDB
period 703.8347374385951
1.93		 0.87849
0.002405		 d
yr
n .5114837061184517 0.00063841 deg/d
Q 2.193120542571199 0.0018249 au
   Orbit Determination Parameters
   # obs. used (total)      64  
   data-arc span      7 days  
   first obs. used      2018-04-10  
   last obs. used      2018-04-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .33384  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Apr-18 06:25:05  

Additional Information
 Earth MOID = .00221776 au 
 Jupiter MOID = 2.9412 au 
 T_jup = 4.273 
[ show covariance matrix ]

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 24.3   n/a MPO445229  

[ 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
2016-Apr-27 11:14 2_10:28 Earth 0.32688398227393 0.282161065712931 0.371690894707005 21.9184232415959 21.9180513528019 2457505.968121524 3508.19730090109 2247487.32901437 27.9260245760888 -6.61912046698179 208684.195032153 T 6 CATAB v2.0e-lin.ifort 2018-Apr-18 06:25:10 2018-Dec-11 17:20
2018-Apr-08 07:20 < 00:01 Earth 0.00436872897510513 0.00435682202407654 0.00438063560465633 15.2889530371297 15.2490094382059 2458216.805898352 0.471753049233986 590.78723870318 7.24826059902056 -0.612601357218295 821.300527781175 T 6 CATAB v2.0e-lin.ifort 2018-Apr-18 06:25:10 2018-Dec-11 17:20
2018-Apr-08 07:49 < 00:01 Moon 0.00265221948230941 0.00264262909779042 0.00266182729429978 15.8582058428244 15.8574266123482 2458216.825503386 0.490603354972598 586.607448309805 9.38480604303047 -35.324665428293 23539.6175619858 T 6 CATAB v2.0e-lin.ifort 2018-Apr-18 06:25:10 2018-Dec-11 17:20
2019-Dec-09 07:16 1_00:56 Earth 0.402050996325824 0.395299995954198 0.414040817132133 13.8543645732946 13.8538862163317 2458826.802478695 1495.701055364 2339458.74205153 290.941534799374 78.4054227415725 150236.542232915 T 6 CATAB v2.0e-lin.ifort 2018-Apr-18 06:25:10 2018-Dec-11 17:20
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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