This article needs to be updated.(August 2015) |
Mission type | Ultraviolet astronomy |
---|---|
Operator | JAXA |
COSPAR ID | 2013-049A |
SATCAT no. | 39253 |
Website | www |
Mission duration | ~1 year planned (science phase) 10 years, 9 months and 17 days (achieved) |
Spacecraft properties | |
Bus | NEXTAR NX-300L |
Manufacturer | NEC |
Launch mass | 348 kg (767 lb) |
Dimensions | 4×1×1 m (13.1×3.3×3.3 ft) |
Power | 900 watts |
Start of mission | |
Launch date | 14 September 2013, 05:00 UTC |
Rocket | Epsilon |
Launch site | Uchinoura |
End of mission | |
Disposal | Decommissioned [1] |
Deactivated | 8 December 2023 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Semi-major axis | 7,431.52 kilometres (4,617.73 mi) [2] |
Eccentricity | 0.0136807 [2] |
Perigee altitude | 957.9 kilometres (595.2 mi) [2] |
Apogee altitude | 1,161.8 kilometres (721.9 mi) [2] |
Inclination | 29.72 degrees [2] |
Period | 106.27 minutes [2] |
Epoch | 23 January 2015, 18:21:14 UTC [2] |
Hisaki, also known as the Spectroscopic Planet Observatory for Recognition of Interaction of Atmosphere (SPRINT-A) was a Japanese ultraviolet astronomy satellite operated by the Japan Aerospace Exploration Agency (JAXA). The first mission of the Small Scientific Satellite program, [3] it was launched in September 2013 on the maiden flight of the Epsilon rocket. It was used for extreme ultraviolet observations of the Solar System planets.
Hisaki was decommissioned by deactivation on 8 December 2023. [1]
Hisaki was launched with an Epsilon rocket, which was its first flight. The four-stage Epsilon rocket [4] flew from the Mu rocket launch complex at the Uchinoura Space Center. The launch occurred at 05:00 UTC on 14 September 2013, following a scrubbed launch attempt on 27 August 2013. [5] Following its successful insertion into orbit and deployment of its solar arrays, the satellite was renamed Hisaki, having been designated SPRINT-A until that point. [6]
Hisaki was named after a cape Hisaki (火崎, literally Cape Fire) used by local fishermen to pray for safe travels in the eastern part of Kimotsuki, Kagoshima near the Uchinoura Space Center, but has the additional meaning of "beyond the Sun". [7] [8] An old name for the mission was EXCEED (Extreme Ultraviolet Spectroscope for Exospheric Dynamics). [9]
Hisaki carries an extreme ultraviolet spectrometer, which is used to study the composition of the atmospheres and the behavior of the magnetospheres of the planets of the Solar System. [10] Designed for a one-year mission, Hisaki was operated in a low Earth orbit with a perigee of 950 km (590 mi), an apogee of 1,150 km (710 mi), 31 degrees of inclination and a period of 106 minutes. [11]
In October 2020, it performed joint observation with the BepiColombo probe which performed a flyby of Venus en route to Mercury. [12]
In 2023, Hisaki performed joint observations with Juno orbiter. [13]
It was decommissioned on 8 December 2023 due to accuracy issues. [14]
BepiColombo is a joint mission of the European Space Agency (ESA) and the Japan Aerospace Exploration Agency (JAXA) to the planet Mercury. The mission comprises two satellites launched together: the Mercury Planetary Orbiter (MPO) and Mio. The mission will perform a comprehensive study of Mercury, including characterization of its magnetic field, magnetosphere, and both interior and surface structure. It was launched on an Ariane 5 rocket on 20 October 2018 at 01:45 UTC, with an arrival at Mercury planned for on 5 December 2025, after a flyby of Earth, two flybys of Venus, and six flybys of Mercury. The mission was approved in November 2009, after years in proposal and planning as part of the European Space Agency's Horizon 2000+ programme; it is the last mission of the programme to be launched.
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The Uchinoura Space Center is a space launch facility in the Japanese town of Kimotsuki, Kagoshima Prefecture. Before the establishment of the JAXA space agency in 2003, it was simply called the Kagoshima Space Center (鹿児島宇宙空間観測所) (KSC). All of Japan's scientific satellites were launched from Uchinoura prior to the M-V launch vehicles being decommissioned in 2006. It continues to be used for suborbital launches, stratospheric balloons and has also been used for the Epsilon orbital launch vehicle. Additionally, the center has antennas for communication with interplanetary space probes.
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