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(2010 GU6)
Classification: Apollo [NEO]          SPK-ID: 3514957
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6794564941830454 0.0003569  
a 2.684075299763968 0.0026435 au
q .8603629064630356 0.00011059 au
i 10.32859827368118 0.0037011 deg
node 195.5873576456432 0.0014612 deg
peri 84.42957775918579 0.00034471 deg
M 95.98775819978599 1.0661 deg
tp 2458572.243643170436
(2019-Mar-29.74364317)
4.124 TDB
period 1606.166154414749
4.40
2.3729
0.006497
d
yr
n .2241362134362593 0.00033113 deg/d
Q 4.507787693064901 0.0044397 au
  Orbit Determination Parameters
   # obs. used (total)      157  
   data-arc span      29 days  
   first obs. used      2010-04-05  
   last obs. used      2010-05-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .43566  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:57:56  

Additional Information
 Earth MOID = .0954474 au 
 Jupiter MOID = 1.08432 au 
 T_jup = 2.975 
[ 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 20.7   n/a MPO190721  
diameter diameter 0.252 km 0.022 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2014ApJ...784..110M)  
geometric albedo albedo 0.147   0.030 urn:nasa:pds:neowise_diameters_albedos::2.0[neos] (http://adsabs.harvard.edu/abs/2014ApJ...784..110M)  

[ 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
2001-Sep-16 22:27 9_14:20 Earth 0.346825734195305 0.159125170042632 0.555596668581973 24.7316903493997 24.7313797146985 2452169.435191740 13820.0674964044 10777990.5787016 184.557253946387 -19.0879309788398 88115.6762740271 T 25 CATAB v2.0e-lin.ifort 2017-Nov-28 17:16:12 2018-Dec-11 15:28
2010-May-01 01:34 < 00:01 Earth 0.127854407733657 0.127729525173614 0.127979290268017 17.8008726483644 17.7997018836067 2455317.565478580 0.267162573072351 6226.73227868341 26.8916985539984 -0.405987686488362 4366.21359986848 T 25 CATAB v2.0e-lin.ifort 2017-Nov-28 17:16:12 2018-Dec-11 15:28
2025-Jul-08 00:43 8_19:30 Jupiter 1.08486517976578 1.06955178077518 1.1019401101528 5.52505047011253 5.38188227652709 2460864.530136674 12689.7690145379 2354235.50753123 355.954340743462 72.9029931574126 226008.189089776 T 25 CATAB v2.0e-lin.ifort 2017-Nov-28 17:16:12 2018-Dec-11 15:28
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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