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26019 (2768 P-L)
Classification: Main-belt Asteroid          SPK-ID: 2026019
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 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .123373293085947 4.2819e-08  
a 2.612499512291735 1.1386e-08 au
q 2.290186844274873 1.1035e-07 au
i 2.777494490223712 3.8491e-06 deg
node 126.3035333852775 0.00011026 deg
peri 112.4542015556854 0.00011182 deg
M 163.6132016229196 1.9919e-05 deg
tp 2458299.531348090546
(2018-Jun-30.03134809)
8.5045e-05 TDB
period 1542.349347022699
4.22
1.0083e-05
2.761e-08
d
yr
n .2334101549009842 1.5259e-09 deg/d
Q 2.934812180308597 1.2791e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1139  
   data-arc span      21963 days (60.13 yr)  
   first obs. used      1960-09-24  
   last obs. used      2020-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53591  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 03:28:33  

Additional Information
 Earth MOID = 1.27971 au 
 Jupiter MOID = 2.06877 au 
 T_jup = 3.396 
[ 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 14.9   n/a MPO351005  
diameter diameter 5.552 km 0.177 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.057   0.011 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

26019 (2768 P-L)          Discovered 1960-Sep-24 by van Houten, C. J., van Houten-Groeneveld, I., Gehrels, T. at Palomar
Reference: 20010606/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2768 P-L = 1997 LT17 = 3188 T-3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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