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6.8. Details to take into account in the observation of moving targets
6.8. Details to take into account in the observation of moving targets

Sunspot positions and sizes for 1825–1867 from the observations by Samuel  Heinrich Schwabe
Sunspot positions and sizes for 1825–1867 from the observations by Samuel Heinrich Schwabe

ENiM – Égyptologie on Twitter: "Kyle Andrew Weyburne, « Determining the  Dates of the Illumination of the Great Temple at Abu Simbel and their  Relation to Khoiak », ENiM 14, 2021, p.
ENiM – Égyptologie on Twitter: "Kyle Andrew Weyburne, « Determining the Dates of the Illumination of the Great Temple at Abu Simbel and their Relation to Khoiak », ENiM 14, 2021, p.

Using the JPL Horizons Ephemeris Website http://ssd.jpl.nasa.gov/?horizons
Using the JPL Horizons Ephemeris Website http://ssd.jpl.nasa.gov/?horizons

Orbital parameters of asteroids using analytical propagation
Orbital parameters of asteroids using analytical propagation

Giant Peanut-Shaped Asteroid to Pass Harmlessly by Earth Wednesday | Space
Giant Peanut-Shaped Asteroid to Pass Harmlessly by Earth Wednesday | Space

Ryan Haecker (@rhackerrr) / Twitter
Ryan Haecker (@rhackerrr) / Twitter

Asteroid 2012 DA14's Friday Flyby: A Skywatcher's Guide | Space
Asteroid 2012 DA14's Friday Flyby: A Skywatcher's Guide | Space

SPICE Files
SPICE Files

Horizons System
Horizons System

ToughSF on Twitter: "Catch an asteroid! @HopDavid41 expands on just how  easy it is to relocate Near-Earth Asteroids into a closed orbit around our  planet. There are hundreds to thousands of 100-1000
ToughSF on Twitter: "Catch an asteroid! @HopDavid41 expands on just how easy it is to relocate Near-Earth Asteroids into a closed orbit around our planet. There are hundreds to thousands of 100-1000

Final project. Earth to Neptune via Gravity assist flyby Jupiter
Final project. Earth to Neptune via Gravity assist flyby Jupiter

טוויטר \ ToughSF בטוויטר: "He uses the example of 2008HU4, a ~500 ton  asteroid that would only need 250m/s deltaV to move it into the Earth-Moon  Lagrange point 2. Propellant can come
טוויטר \ ToughSF בטוויטר: "He uses the example of 2008HU4, a ~500 ton asteroid that would only need 250m/s deltaV to move it into the Earth-Moon Lagrange point 2. Propellant can come

65803 Didymos (@AsteroidDidymos) / Twitter
65803 Didymos (@AsteroidDidymos) / Twitter

Horizons System
Horizons System

Asteroid Series 3: Generating an Ephemeris for Asteroids – Stone Edge  Observatory
Asteroid Series 3: Generating an Ephemeris for Asteroids – Stone Edge Observatory

HORIZONS Web-Interface http://ssd.jpl.nasa.gov/horizons.cgi#results 1 of 16  7/28/10 5:34 PM
HORIZONS Web-Interface http://ssd.jpl.nasa.gov/horizons.cgi#results 1 of 16 7/28/10 5:34 PM

Minor Revision Topical Editor Decision: Publish subject to technical  corrections (20 Sep 2020) by Margit Haberreiter Comments
Minor Revision Topical Editor Decision: Publish subject to technical corrections (20 Sep 2020) by Margit Haberreiter Comments

Ephemerides and Finding Charts
Ephemerides and Finding Charts

The argument of pericenter (top) and orbital eccentricity (bottom) of... |  Download Scientific Diagram
The argument of pericenter (top) and orbital eccentricity (bottom) of... | Download Scientific Diagram

11 Lab 5 - JPL Ephemeris, Binary Maker 3 In Lab 5 we'll look at another  ephemeris generating tool; Horizons Web-Interfac
11 Lab 5 - JPL Ephemeris, Binary Maker 3 In Lab 5 we'll look at another ephemeris generating tool; Horizons Web-Interfac