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Muses
Country: Japan. Spacecraft: Hagoromo, Hiten, Haruka. Launch Vehicles: Mu-3S-II, M-V. Launch Sites: Kagoshima. Agency: ISAS, NEC.
1990 January 24 - . 11:46 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. Launch Pad: M1. LV Family: Mu. Launch Vehicle: Mu-3S-II.
- Hiten - .
Payload: Muses A. Mass: 185 kg (407 lb). Nation: Japan.
Agency: ISAS.
Program: Muses.
Class: Moon.
Type: Lunar probe. Spacecraft: Hiten.
Decay Date: 1993-04-11 . USAF Sat Cat: 20448 . COSPAR: 1990-007A. Apogee: 286,183 km (177,825 mi). Perigee: 262 km (162 mi). Inclination: 30.60 deg. Period: 9,597.60 min.
MUSES-A was renamed Hiten after launch. It developed of lunar swingby techniques for future missions and ejected a lunar orbiter. Launching organization ISAS. On 1990 Jan 25: Period 6.665 days, inclination 30.63 deg, 262.49 x 286182.72 km. On 1992 Feb 17: Period 4.53 days, inclination 38.90 deg, perilune 2289.67 km, apolune 49013.93 km.
- Hagoromo - . Payload: Muses A. Mass: 12 kg (26 lb). Nation: Japan. Agency: ISAS. Program: Muses. Class: Moon. Type: Lunar probe. Spacecraft: Hagoromo. USAF Sat Cat: 20618 . COSPAR: 1990-007B. Lunar orbiter ejected from Muses A 3/19/90; contact lost after release; engineering test. Lunar Orbit (Selenocentric). .
1997 February 12 - . 04:50 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M-V. Launch Vehicle: M-V.
- Haruka - . Payload: MUSES B. Nation: Japan. Agency: ISAS. Manufacturer: NEC. Program: Muses. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Haruka. USAF Sat Cat: 24720 . COSPAR: 1997-005A. Apogee: 21,415 km (13,306 mi). Perigee: 569 km (353 mi). Inclination: 31.40 deg. Period: 379.30 min.
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