Explorer 59 (ISEE 3)

Launch Success

Liftoff Time (GMT)

15:12:00

Saturday August 12, 1978

Watch Replay

24/7 Coverage

Mission Details

Explorer 59 (ISEE 3)

Wiki

The Explorer-class heliocentric spacecraft, International Sun-Earth Explorer 3, was part of the mother/daughter/heliocentric mission (ISEE 1, 2, and 3). The purposes of the mission were: (1) to investigate solar-terrestrial relationships at the outermost boundaries of the Earth's magnetosphere; (2) to examine in detail the structure of the solar wind near the Earth and the shock wave that forms the interface between the solar wind and Earth's magnetosphere; (3) to investigate motions of and mechanisms operating in the plasma sheets; and, (4) to continue the investigation of cosmic rays and solar flare emissions in the interplanetary region near 1 AU. The three spacecraft carried a number of complementary instruments for making measurements of plasmas, energetic particles, waves, and fields. The mission thus extended the investigations of previous IMP spacecraft. The launch of three coordinated spacecraft in this mission permitted the separation of spatial and temporal effects. Termination of operations of ICE/ISEE3 was authorized May 5, 1997.

Heliocentric Orbit

1 Payload

390 kilograms

Rocket

Retired
Delta 2914

Active 1974 to 1979


Payload to Orbit

GTO: 724 kg

Stages

3

Strap-ons

9

Launch Site

SLC-17B

Cape Canaveral SFS, Florida, USA

Fastest Turnaround

20 days 2 hours

Stats

Delta 2000 Series


39th

Mission

6th

Mission of 1978

1978


81st

Orbital launch attempt