Names | ISEE-3 International Sun-Earth Explorer-C Explorer 59 | ||||||||||||||||||||||||||||
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Mission type | Magnetospheric research ISEE-3: Sun/Earth L1 orbiter ICE: 21P/G-Z and Halley fly-by | ||||||||||||||||||||||||||||
Operator | NASA | ||||||||||||||||||||||||||||
COSPAR ID | 1978-079A | ||||||||||||||||||||||||||||
SATCAT no. | 11004 | ||||||||||||||||||||||||||||
Mission duration | Launch to last routine contact: 18 years, 8 months, 22 days Launch to last contact: 36 years, 1 month, 3 days | ||||||||||||||||||||||||||||
Spacecraft properties | |||||||||||||||||||||||||||||
Spacecraft | Explorer LIX | ||||||||||||||||||||||||||||
Spacecraft type | International Sun-Earth Explorer | ||||||||||||||||||||||||||||
Bus | ISEE | ||||||||||||||||||||||||||||
Manufacturer | Fairchild Industries | ||||||||||||||||||||||||||||
Launch mass | 479 kg (1,056 lb)[1] | ||||||||||||||||||||||||||||
Dry mass | 390 kg (860 lb) | ||||||||||||||||||||||||||||
Dimensions | 1.77 × 1.58 m (5 ft 10 in × 5 ft 2 in) | ||||||||||||||||||||||||||||
Power | 173 watts | ||||||||||||||||||||||||||||
Start of mission | |||||||||||||||||||||||||||||
Launch date | 12 August 1978, 15:12 UTC | ||||||||||||||||||||||||||||
Rocket | Thor-Delta 2914 (Thor 633 / Delta 144) | ||||||||||||||||||||||||||||
Launch site | Cape Canaveral, SLC-17B | ||||||||||||||||||||||||||||
Contractor | Douglas Aircraft Company | ||||||||||||||||||||||||||||
Entered service | 12 August 1978 | ||||||||||||||||||||||||||||
End of mission | |||||||||||||||||||||||||||||
Deactivated | 5 May 1997 | ||||||||||||||||||||||||||||
Last contact | 16 September 2014 | ||||||||||||||||||||||||||||
Orbital parameters | |||||||||||||||||||||||||||||
Reference system | Heliocentric orbit | ||||||||||||||||||||||||||||
Perihelion altitude | 0.93 AU (139,000,000 km; 86,000,000 mi) | ||||||||||||||||||||||||||||
Aphelion altitude | 1.03 AU (154,000,000 km; 96,000,000 mi) | ||||||||||||||||||||||||||||
Inclination | 0.10° | ||||||||||||||||||||||||||||
Period | 355 days | ||||||||||||||||||||||||||||
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The International Cometary Explorer (ICE) spacecraft, designed and launched as the International Sun-Earth Explorer-3 (ISEE-3) satellite, was launched on 12 August 1978 into a heliocentric orbit. It was one of three spacecraft, along with the mother/daughter pair of ISEE-1 and ISEE-2, built for the International Sun-Earth Explorer (ISEE) program, a joint effort by NASA and ESRO/ESA to study the interaction between the Earth's magnetic field and the solar wind.
ISEE-3 was the first spacecraft to be placed in a halo orbit at the L1 Earth-Sun Lagrange point.[2] Renamed ICE, it became the first spacecraft to visit a comet,[3] passing through the plasma tail of comet Giacobini-Zinner within about 7,800 km (4,800 mi) of the nucleus on 11 September 1985.[4]
NASA suspended routine contact with ISEE-3 in 1997 and made brief status checks in 1999 and 2008.[5][6]
On 29 May 2014, two-way communication with the spacecraft was reestablished by the ISEE-3 Reboot Project, an unofficial group,[7] with support from the Skycorp company and SpaceRef Interactive.[8][9][10] On 2 July 2014, they fired the thrusters for the first time since 1987. However, later firings of the thrusters failed, apparently due to a lack of nitrogen pressure in the fuel tanks.[11][12] The project team initiated an alternative plan to use the spacecraft to "collect scientific data and send it back to Earth",[13] but on 16 September 2014, contact with the probe was lost.[14]
The ground stations listening to ISEE-3 have not been able to obtain a signal since the 16 September 2014