Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
JPL Small-Body Database Browser
Search: [ help ]  
241555 (2010 GT5)
Classification: Main-belt Asteroid          SPK-ID: 2241555
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ hide orbit diagram ]

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 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .009790887253405435 3.4794e-08  
a 2.914321718323421 2.6085e-08 au
q 2.885787922959165 1.004e-07 au
i 6.432184689707729 5.9483e-06 deg
node 44.29545072858435 3.7585e-05 deg
peri 75.73816907074524 0.00035299 deg
M 132.5241076112342 0.00034933 deg
tp 2458531.544769559299
(2019-Feb-17.04476956)
0.0017634 TDB
period 1817.208108770072
4.98
2.4398e-05
6.68e-08
d
yr
n .1981060937724168 2.6598e-09 deg/d
Q 2.942855513687676 2.6341e-08 au
  Orbit Determination Parameters
   # obs. used (total)      316  
   data-arc span      9163 days (25.09 yr)  
   first obs. used      1995-04-24  
   last obs. used      2020-05-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51309  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 01:07:42  

Additional Information
 Earth MOID = 1.90752 au 
 Jupiter MOID = 2.03566 au 
 T_jup = 3.273 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457591.5 (2016-Jul-22.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .01105496005319808 3.4924e-08  
q 2.882480740834307 1.0111e-07 au
tp 2456719.827078100870
(2014-Mar-03.32707810)
0.0015582 TDB
node 44.31202185217953 3.7579e-05 deg
peri 76.95020379119417 0.00031237 deg
i 6.432689515802381 5.9485e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      316  
   data-arc span      9163 days (25.09 yr)  
   first obs. used      1995-04-24  
   last obs. used      2020-05-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51309  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 01:07:42  

Additional Information
 Jupiter MOID = 2.03566 au 
 T_jup = 3.273 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.219651747220602E-15 -3.415439733629874E-15 5.720207112048343E-12 8.574358146492538E-15 1.125074818431264E-12 -2.073132477078583E-15
q -3.415439733629874E-15 1.022417175241647E-14 -1.82636245068754E-11 -2.472097117134663E-14 -3.540399147246808E-12 6.645046794140994E-15
tp 5.720207112048343E-12 -1.82636245068754E-11 2.427836686933779E-6 -2.349360299589254E-11 4.831840991199703E-7 8.676100701440581E-12
node 8.574358146492538E-15 -2.472097117134663E-14 -2.349360299589254E-11 1.412202763247582E-9 -1.407900739029326E-9 -7.049200474962557E-11
peri 1.125074818431264E-12 -3.540399147246808E-12 4.831840991199703E-7 -1.407900739029326E-9 9.757261201366352E-8 7.191830096787907E-11
i -2.073132477078583E-15 6.645046794140994E-15 8.676100701440581E-12 -7.049200474962557E-11 7.191830096787907E-11 3.538498938435773E-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 16.06   n/a E2021B55  

241555 (2010 GT5)          Discovered 2010-Apr-03 by Mayhill at Mayhill
Reference: 20100527/Numbers.arcLast Updated: 2010-06-03

[ 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
2038-May-07 20:48 00:02 Thisb 0.0493252681370693 0.0493134472354795 0.0493370892856317 4.52203577231825 4.52203574174995 2465551.366743729 1.60183223271139 614.822445161703 75.7830214970641 -16.717642125441 30261.306412364 T 15 CATAB v2.0f-lin.ifort 2020-Nov-12 01:07:43 2020-Nov-12 01:07
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2021-Mar-08 16:45 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin