Hakuto-R Mission 2

Hakuto-R Mission 2
Resilience
Full-size model of Hakuto-R
Mission typeLunar landing, technology demonstration
Operatorispace
COSPAR ID2025-010B Edit this at Wikidata
SATCAT no.62717Edit this on Wikidata
Websiteispace-inc.com/m2
Mission duration3 months and 11 days (elapsed)
Spacecraft properties
SpacecraftHakuto-R Resilience
Spacecraft typeLunar lander
Manufacturerispace
Landing mass340 kg (750 lb)
DimensionsWidth: 2.5 m (8 ft 2 in)
Height: 2.3 m (7 ft 7 in)
Start of mission
Launch date15 January 2025 (2025-01-15), 06:11:39 UTC (1:11:39 am EST)
RocketFalcon 9 Block 5 (B1085.5), Flight 425
Launch siteKennedy, LC-39A
ContractorSpaceX
Resilience Lunar lander
Landing dateNET 6 June 2025 (2025-06-06) (planned)[1]
Landing siteMare Frigoris (60°30′N 4°36′W / 60.5°N 4.6°W / 60.5; -4.6)[1]
Tenacious Lunar rover
Landing dateNET 6 June 2025 (2025-06-06) (planned)[1]
Landing siteMare Frigoris (60°30′N 4°36′W / 60.5°N 4.6°W / 60.5; -4.6)[1]

Hakuto-R Mission 2, also called Resilience, is a robotic lunar landing mission launched on 15 January 2025 at 06:11:39 UTC (1:11:39 am EST, local time at the launch site). Developed by ispace, the lander will deliver a new micro rover manufactured by the company, as well as other payloads. Like Hakuto-R Mission 1, this mission will serve as a technology demonstration, with the final goal of providing reliable transportation and data services on the Moon. The lander is named Resilience.[2]

  1. ^ a b c d "ispace Announces Mission 2 Landing Date Set for June 6, 2025 (JST)". ispace, Inc. 4 March 2025. Retrieved 4 March 2025.
  2. ^ "ispace Announces Mission 2 with Unveiling of Micro Rover Design". ispace. Retrieved 22 June 2024.

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