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134180 Nirajinamdar (2005 CN22)
Classification: Main-belt Asteroid          SPK-ID: 2134180
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0814402773842203 3.4857e-08  
a 2.435309820633556 1.3903e-08 au
q 2.236977513324644 8.5191e-08 au
i 13.23594222622306 4.8825e-06 deg
node 104.488636667121 1.709e-05 deg
peri 272.0150107675401 3.7595e-05 deg
M 225.6000685477087 3.5837e-05 deg
tp 2459914.734478435912
(2022-Dec-01.23447844)
0.00014041 TDB
period 1388.128775223031
3.80
1.1887e-05
3.254e-08
d
yr
n .2593419331302016 2.2208e-09 deg/d
Q 2.633642127942469 1.5035e-08 au
  Orbit Determination Parameters
   # obs. used (total)      542  
   data-arc span      7481 days (20.48 yr)  
   first obs. used      2000-12-20  
   last obs. used      2021-06-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .50999  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 09:16:30  

Additional Information
 Earth MOID = 1.28398 au 
 Jupiter MOID = 2.75016 au 
 T_jup = 3.464 
[ 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 16.02   n/a MPO637654  

134180 Nirajinamdar           Discovered 2005 Feb. 1 by the Catalina Sky Survey.
Niraj K. Inamdar (b. 1986) worked as a student engineer at the Massachusetts Institute of Technology where he conducted the preliminary performance modeling in the development of the student-built Regolith X-ray Imaging Spectrometer aboard the OSIRIS-REx Asteroid Sample Return Mission.
NOTE: some special characters may not display properly (any characters within {} are an attempt to place the proper accent above a character)
Reference: MPC batch dated 2016-08-18Last Updated: 2016-08-22

Alternate Designations
 2005 CN22 = 2003 QL106 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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