Mission type | Lunar orbiter |
---|---|
Operator | NASA |
COSPAR ID | 1967-041A |
SATCAT no. | 2772 |
Mission duration | 180 days |
Spacecraft properties | |
Manufacturer | Langley Research Center |
Launch mass | 385.6 kilograms (850 lb)[1] |
Start of mission | |
Launch date | May 4, 1967, 22:25:00[1] | UTC
Rocket | Atlas SLV-3 Agena-D |
Launch site | Cape Canaveral LC-13 |
End of mission | |
Last contact | July 17, 1967[1] |
Decay date | October 6, 1967[1] |
Orbital parameters | |
Reference system | Selenocentric |
Semi-major axis | 6,152.5 kilometers (3,823.0 mi) |
Eccentricity | 0.28 |
Periselene altitude | 4,449 kilometers (2,764 mi) |
Aposelene altitude | 7,856 kilometers (4,881 mi) |
Inclination | 85.5 degrees |
Period | 721 minutes |
Epoch | March 7, 1967, 20:00:00 UTC[2] |
Lunar orbiter | |
Orbital insertion | May 8, 1967, 21:54 UTC |
Orbits | 360 |
Lunar Orbiter 4 was a robotic U.S. spacecraft, part of the Lunar Orbiter Program,[3] designed to orbit the Moon, after the three previous orbiters had completed the required needs for Apollo mapping and site selection. It was given a more general objective, to "perform a broad systematic photographic survey of lunar surface features in order to increase the scientific knowledge of their nature, origin, and processes, and to serve as a basis for selecting sites for more detailed scientific study by subsequent orbital and landing missions".[2] It was also equipped to collect selenodetic, radiation intensity, and micrometeoroid impact data.