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58365 Robmedrano (1995 OQ)
Classification: Main-belt Asteroid          SPK-ID: 2058365
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .114059905490345 4.433e-08  
a 2.584873921430699 1.3041e-08 au
q 2.290043446247856 1.1703e-07 au
i 6.977759241495636 5.6789e-06 deg
node 170.5509555345318 3.2871e-05 deg
peri 127.7255142671359 4.0119e-05 deg
M 30.90132521279016 2.2176e-05 deg
tp 2459070.203701505383
(2020-Aug-08.70370151)
9.3389e-05 TDB
period 1517.950027549216
4.16
1.1487e-05
3.145e-08
d
yr
n .2371619575522079 1.7947e-09 deg/d
Q 2.879704396613542 1.4528e-08 au
  Orbit Determination Parameters
   # obs. used (total)      903  
   data-arc span      10217 days (27.97 yr)  
   first obs. used      1992-11-18  
   last obs. used      2020-11-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .59952  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 03:57:04  

Additional Information
 Earth MOID = 1.28064 au 
 Jupiter MOID = 2.33113 au 
 T_jup = 3.403 
[ 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 15.20   n/a E2021B10  

58365 Robmedrano           Discovered 1995 July 27 by AMOS at Haleakala.
Rob Medrano (b. 1969), a key member of the Air Force Maui Optical and Supercomputing (AMOS) team, provides technical support to the AMOS visiting observer programs ensuring their success, as well as supporting the annual AMOS Technical Conference.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: 20050125/MPCPages.arcLast Updated: 2005-06-01

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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
1987-Oct-02 14:56 < 00:01 Juno 0.0486163830223457 0.0486137139333856 0.0486190523982039 6.32681983921326 6.3268197996604 2447071.122360605 0.393963282058602 238.086283192982 44.3512792146625 -57.5732142743691 139324.410423895 T 25 CATAB v2.0f-lin.ifort 2020-Dec-18 03:57:06 2020-Dec-18 03:57
2087-Mar-29 21:56 00:02 Iris 0.00757739748205569 0.00756327677098193 0.00759152516294628 6.0405402290749 6.0405401034785 2483409.413810753 1.75594383743629 792.359519371238 52.4637060465842 27.3571929126308 10005.7405319409 T 25 CATAB v2.0f-lin.ifort 2020-Dec-18 03:57:06 2020-Dec-18 03:57

Alternate Designations
 1995 OQ = 2000 UK17 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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