LUNA 2
- LUNA 2 LUNA 2
Object Name LUNA 2
Object Full Name -
Norad ID 114
Cospar ID 1959-014A
Object Type Satellite
Object Status Decayed
Object Class -
End of Life -

Luna 2 was the second of a series of spacecraft launched in the direction of the Moon. The first spacecraft to land on the Moon, it impacted the lunar surface east of Mare Serenitatis near the Aristides, Archimedes, and Autolycus craters. Luna 2 was similar in design to Luna 1, a spherical spacecraft with protruding antennae and instrument parts. The instrumentation was also similar, including scintillation- and geiger- counters, a magnetometer, and micrometeorite detectors. The spacecraft also carried Soviet pennants. There were no propulsion systems on Luna 2 itself. After launch and attainment of escape velocity on 12 September 1959 (13 September Moscow time), Luna 2 separated from its third stage, which travelled along with it towards the Moon. On 13 September the spacecraft released a bright orange cloud of sodium gas which aided in spacecraft tracking and acted as an experiment on the behavior of gas in space. On 14 September, after 33.5 hours of flight, radio signals from Luna 2 abruptly ceased, indicating it had impacted on the Moon. The impact point, in the Palus Putredinus region, is roughly estimated to have occurred at 0 degrees longitude, 29.1 degrees N latitude. Some 30 minutes after Luna 2, the third stage of its rocket also impacted the Moon at an unknown location. The mission confirmed that the Moon had no appreciable magnetic field, and found no evidence of radiation belts at the Moon. Spacecraft image for illustrative purposes - not necessarily in the public domain.

Launch Date 1959-09-12
Decay Date 1959-09-13
Launch Vehicle -
Launch Site Baikonur Cosmodrome, Kazakhstan
Launch Provider -
Launch Provider Country -
Launch Mass -
Dry Mass -
User -
Mission -
Mission Detail -
Country of Registry -
Programme -
Operator -
Country of Operator USSR/Russia
Contractor -
Country of Contractor -
Payload Contractor -
Payload Contractor Country -
Orbit Status Moon Impact
Orbit -
Orbit Type -
Period: -
Inclination: -
Apogee: -
Perigee: -
Longitude of Geo -
ECT -
Payload -
Platform -
Propulsion -
Propulsion Type -
Life Time -
Power -
Budget -
Call Sign -
Beacon -
RCS -
References -
Date
Rise
Heights
Set
Pass Time
Visible
Time
Altitude
Azimuth
Time
Altitude
Azimuth
Time
Altitude
Azimuth

					


Angular Momentum: -
Eccentricity: -
Inclination: -
RAAN: -
Argument of Perigee: -
True Anomaly: -
Period: -
Semi-Major Axis: -
Perigee: -
Apogee: -
Mean Motion: -
Mean Anomaly: -

Latitude: -
Longitude: -
Altitude: -
Speed: -
Azimuth: -
Elevation: -
Range: -