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Artist's rendering of theSakigake spacecraft | |
| Mission type | Halley flyby |
|---|---|
| Operator | ISAS |
| COSPAR ID | 1985-001A |
| SATCATno. | 15464 |
| Mission duration | 14 years and 1 day |
| Spacecraft properties | |
| Launch mass | 138.1 kilograms (304 lb)[1] |
| Start of mission | |
| Launch date | January 7, 1985, 19:27 (1985-01-07UTC19:27Z) UTC |
| Rocket | Mu-3SII |
| Launch site | Kagoshima |
| End of mission | |
| Last contact | Data: November 15, 1995 (1995-11-16) Beacon: January 8, 1999 |
| Orbital parameters | |
| Reference system | Heliocentric |
| Perihelion altitude | 0.92 AU |
| Aphelion altitude | 1.15 AU |
| Inclination | 0.07 degrees |
| Period | 382.8 days |
| Flyby of1P/Halley | |
| Closest approach | March 11, 1986, 04:18 UTC |
| Distance | 6,990,000 kilometres (4,340,000 mi) |
Sakigake (さきがけ;lit. 'pioneer', 'pathfinder'), known before launch asMS-T5, was Japan's firstinterplanetary spacecraft and the firstdeep space probe to be launched by any country other than the US or the Soviet Union. It aimed to demonstrate the performance of the newlaunch vehicle, test its ability to escape fromEarth gravity, and observe theinterplanetary medium andmagnetic field.Sakigake also served as a reference probe forHalley's Comet. Early measurements would be used to improve the mission of theSuisei probe launched several months later.
Sakigake was developed by theInstitute of Space and Astronautical Science for theNational Space Development Agency (both of which are now part of theJapanese Aerospace Exploration Agency, or JAXA). It became a part of theHalley Armada together with Suisei, the SovietVega probes, theESAGiotto and theNASAInternational Cometary Explorer, to explore Halley's Comet during its 1986 sojourn through the inner Solar System.
Unlike its twinSuisei, it carried no imaging instruments in itsinstrument payload.
Sakigake was launched January 7, 1985, fromKagoshima Space Center byM-3SII launch vehicle on M-3SII-1 mission.
It carried out a flyby of Halley's Comet on March 11, 1986, at a distance of 6.99 million km.
There were plans for thespacecraft to go on to an encounter with21P/Giacobini-Zinner in 1998, but the flyby had to be abandoned because of a lack ofpropellant.
Telemetry contact was lost on November 15, 1995, though a beacon signal continued to be received until January 7, 1999.[2][3]