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364690 (2007 UE2)
Classification: Main-belt Asteroid          SPK-ID: 2364690
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 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2012639120715141 7.6447e-08  
a 2.223642989725284 1.3022e-08 au
q 1.776103902562776 1.6963e-07 au
i 5.799565215947337 7.4826e-06 deg
node 70.86770835199049 6.399e-05 deg
peri 281.9724922722781 6.6389e-05 deg
M 308.7813955912614 1.7162e-05 deg
tp 2459172.814275889021
(2020-Nov-19.31427589)
5.7958e-05 TDB
period 1211.144661908513
3.32
1.0639e-05
2.913e-08
d
yr
n .2972394721475424 2.611e-09 deg/d
Q 2.671182076887793 1.5643e-08 au
  Orbit Determination Parameters
   # obs. used (total)      260  
   data-arc span      5746 days (15.73 yr)  
   first obs. used      2003-06-04  
   last obs. used      2019-02-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55316  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-26 01:17:25  

Additional Information
 Earth MOID = .782246 au 
 Jupiter MOID = 2.77939 au 
 T_jup = 3.614 
[ 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 17.3   n/a MPO266859  

364690 (2007 UE2)          Discovered 2007-Oct-18 by Lowe, A. at Mayhill
Reference: Last Updated: 2013-06-26

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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
2114-Sep-19 13:07 00:09 Amphi 0.0499368193370652 0.049875817105369 0.0499978216174629 3.65197083824238 3.65197080671958 2493444.046199548 8.55527192125404 3041.59177947006 74.6261808994933 -1.62860124052183 3754.5402063875 T 17 CATAB v2.0f-lin.ifort 2020-Feb-26 01:17:28 2020-Feb-26 01:17

Alternate Designations
 2007 UE2 = 2004 XZ152 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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