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13153 (1995 QC3)
Classification: Mars-crossing Asteroid          SPK-ID: 2013153
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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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 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3671465453649698 4.3586e-08  
a 2.415610266509444 1.2352e-08 au
q 1.528727302212348 1.0559e-07 au
i 5.639020808834518 5.3666e-06 deg
node 336.8042544837524 4.4756e-05 deg
peri 345.1539784216919 4.548e-05 deg
M 278.5532614059206 1.3676e-05 deg
tp 2459510.748667240204
(2021-Oct-23.24866724)
5.3995e-05 TDB
period 1371.319737713749
3.75
1.0518e-05
2.88e-08
d
yr
n .2625208331064996 2.0136e-09 deg/d
Q 3.302493230806541 1.6887e-08 au
  Orbit Determination Parameters
   # obs. used (total)      626  
   data-arc span      14771 days (40.44 yr)  
   first obs. used      1980-10-08  
   last obs. used      2021-03-18  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .58676  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 01:25:20  

Additional Information
 Earth MOID = .515343 au 
 Jupiter MOID = 2.04666 au 
 T_jup = 3.415 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.43   n/a E2021B10  

13153 (1995 QC3)          Discovered 1995-Aug-31 by Kobayashi, T. at Oizumi
Reference: 20000124/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1995 QC3 = 1980 TL6 = 1980 TZ6 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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