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30048 Sreyasmisra (2000 EB37)
Classification: Main-belt Asteroid          SPK-ID: 2030048
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 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1647743210429523 5.4851e-08  
a 2.405025569501935 9.2171e-09 au
q 2.008739114196314 1.3081e-07 au
i 2.025780850329304 5.9748e-06 deg
node 4.039601370497215 9.5291e-05 deg
peri 189.3284573278966 9.5857e-05 deg
M 243.728793301283 1.2739e-05 deg
tp 2459836.494910412783
(2022-Sep-13.99491041)
4.9747e-05 TDB
period 1362.316365727971
3.73
7.8315e-06
2.144e-08
d
yr
n .2642557992083061 1.5191e-09 deg/d
Q 2.801312024807555 1.0736e-08 au
  Orbit Determination Parameters
   # obs. used (total)      868  
   data-arc span      9175 days (25.12 yr)  
   first obs. used      1995-11-23  
   last obs. used      2021-01-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .5506  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 19:46:17  

Additional Information
 Earth MOID = 1.00893 au 
 Jupiter MOID = 2.15395 au 
 T_jup = 3.504 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457176.5 (2015-Jun-03.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1639820550820803 5.4981e-08  
q 2.011037073236249 1.3103e-07 au
tp 2457111.025999150506
(2015-Mar-29.52599915)
4.1973e-05 TDB
node 4.121671899025998 9.5254e-05 deg
peri 189.2890951402177 9.5824e-05 deg
i 2.026174772484283 5.9747e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      868  
   data-arc span      9175 days (25.12 yr)  
   first obs. used      1995-11-23  
   last obs. used      2021-01-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .5506  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 19:46:17  

Additional Information
 Jupiter MOID = 2.15395 au 
 T_jup = 3.504 
Orbit Covariance (6×6)
  e q tp node peri i
e 3.022888644712717E-15 -7.192018320955866E-15 2.978918263046445E-14 9.319642975909125E-15 -1.403317797256813E-14 -4.407831582390063E-16
q -7.192018320955866E-15 1.716951103730782E-14 4.60784764052595E-14 -2.242333413676133E-14 6.000876754150607E-14 1.063060726420836E-15
tp 2.978918263046445E-14 4.60784764052595E-14 1.761770602564992E-9 -2.200975557434421E-12 4.444354201697501E-10 1.02516882544368E-13
node 9.319642975909125E-15 -2.242333413676133E-14 -2.200975557434421E-12 9.073275832533581E-9 -9.067670693251665E-9 8.561991037780449E-11
peri -1.403317797256813E-14 6.000876754150607E-14 4.444354201697501E-10 -9.067670693251665E-9 9.182173664642047E-9 -8.555644836933409E-11
i -4.407831582390063E-16 1.063060726420836E-15 1.02516882544368E-13 8.561991037780449E-11 -8.555644836933409E-11 3.569719638684762E-11

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 15.68   n/a MPCxxxxx  

30048 Sreyasmisra           Discovered 2000 Mar. 8 by the Lincoln Laboratory Near-Earth Asteroid Research Team at Socorro.
Sreyas Misra (b. 1996) is a finalist in the 2014 Intel Science Talent Search, a science competition for high school seniors, for his bioengineering project. He attends the Harker School, San Jose, California.
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 2014-04-15Last Updated: 2014-04-17
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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