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35990 (1999 NG10)
Classification: Main-belt Asteroid          SPK-ID: 2035990
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1149211303788806 5.4618e-08  
a 2.555980613382645 1.3407e-08 au
q 2.262244432066207 1.4347e-07 au
i 11.48372828692996 6.5554e-06 deg
node 314.5458003525592 2.0963e-05 deg
peri 256.3385148356181 3.9797e-05 deg
M 127.0529524030078 3.7864e-05 deg
tp 2458473.734867241113
(2018-Dec-21.23486724)
0.00015495 TDB
period 1492.570178075688
4.09
1.1743e-05
3.215e-08
d
yr
n .2411946890591997 1.8977e-09 deg/d
Q 2.849716794699083 1.4947e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1381  
   data-arc span      7833 days (21.45 yr)  
   first obs. used      1998-01-25  
   last obs. used      2019-07-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5431  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 04:00:50  

Additional Information
 Earth MOID = 1.29088 au 
 Jupiter MOID = 2.24172 au 
 T_jup = 3.400 
[ 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 14.2   n/a MPO395344  
diameter diameter 3.793 km 0.207 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.308   0.058 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35990 (1999 NG10)          Discovered 1999-Jul-13 by LINEAR at Socorro
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 NG10 = 1998 FM95 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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