India’s Aditya-L1 Completes First Halo Orbit Around Sun-Earth L1 Point

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India’s Aditya-L1 Completes First Halo Orbit Around Sun-Earth L1 Point
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India’s Aditya-L1 Completes First Halo Orbit Around Sun-Earth L1 Point

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ISRO announced a significant milestone for India’s first solar mission, Aditya-L1, as it completed its first halo orbit around the Sun-Earth L1 point

The spacecraft, launched on September 2, 2023, achieved insertion into its initial halo orbit on January 6, 2024.

 

Aditya-L1 Mission

  • India’s first solar mission.
  • Launched via PSLV-C57 from the Satish Dhawan Space Centre at Sriharikota.
  • Objective: It intends to investigate the Sun’s corona and atmosphere from the L1 (Lagrange point).

〈 L1, which lies between the Sun and Earth. This unique location allows it to observe the Sun continuously without Earth’s interference. 〉

 

India's Aditya-L1 Completes First Halo Orbit Around Sun-Earth L1 Point

About Halo Orbit:

  • It is a three-dimensional, periodic orbit around Lagrange points in a two-body system like Earth-Sun or Earth-Moon. 
  • It is commonly linked with L1, L2, and L3 Lagrange points, where the gravitational forces of two large bodies and centrifugal force balance each other.
  • The spacecraft’s halo orbit takes 178 days to complete one revolution around the L1 point.
  • During this journey, perturbing forces (such as gravitational interactions) can cause the spacecraft to deviate from its intended path.

 

India's Aditya-L1 Completes First Halo Orbit Around Sun-Earth L1 Point

 

Lagrange Points

  • Positions in space where the gravitational pull of two large masses balances with the centripetal force required for a small object to move with them.
  • There are five Lagrange points in a two-body system:
  1. Three unstable points: L1, L2, L3 (lie along the line connecting the two large masses).
  2. Two stable points: L4 and L5 (form the apex of two equilateral triangles with the large masses at their vertices).

 

Benefits of placing Aditya-L1 in a halo orbit around the L1 point are:

  • Ensuring a mission lifetime of 5 years: It is selected to minimise station-keeping manoeuvres and fuel consumption, thus extending the mission life.
  • A satellite in a halo orbit around L1 has the major advantage of continuously viewing the Sun without any occultation or eclipses. 
  • It provides an unobstructed view of the Sun crucial for studying the solar atmosphere, including the photosphere, chromosphere, and corona.

 

The orbit provides a stable line of sight to Earth and the Sun, which is beneficial for continuous communication and solar power.

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