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61135 (2000 NT2)
Classification: Main-belt Asteroid          SPK-ID: 2061135
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 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1215947455572949 7.7752e-08  
a 2.513962718643791 9.009e-09 au
q 2.208278061529774 1.954e-07 au
i 3.194383739089615 5.5537e-06 deg
node 113.1224977660274 7.9108e-05 deg
peri 199.0146620498376 8.1648e-05 deg
M 84.46930256050292 1.7936e-05 deg
tp 2459054.888026857281
(2020-Jul-24.38802686)
7.2733e-05 TDB
period 1455.917198360806
3.99
7.8261e-06
2.143e-08
d
yr
n .2472668091326335 1.3292e-09 deg/d
Q 2.819647375757809 1.0104e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1130  
   data-arc span      10928 days (29.92 yr)  
   first obs. used      1991-03-12  
   last obs. used      2021-02-10  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .53897  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 11:49:08  

Additional Information
 Earth MOID = 1.1937 au 
 Jupiter MOID = 2.41279 au 
 T_jup = 3.447 
[ 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 15.28   n/a E2021B10  

61135 (2000 NT2)          Discovered 2000-Jul-05 by Kusnirak, P., Pravec, P. at Ondrejov
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 NT2 = 1995 FP19 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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