The Senate passed a resolution (S Res 256) creating a special Committee on Space and Astronautics to frame legislation for a national program for space exploration.

Following industry-wide competition, a formal contract for research and development of the Mercury spacecraft was negotiated with the McDonnell Aircraft Corporation. The contract called for design and construction of 12 Mercury spacecraft, but it did not include details on changes and ground support equipment which were to be negotiated as the project developed. Later, orders were placed with the company for eight additional spacecraft, two procedural trainers, an environmental trainer, and seven checkout trainers. McDonnell had been engaged in studying the development of a manned spacecraft since the NACA presentation in mid-March of 1958.

First test launch of USAF Titan ICBM (A-3) from Cape Canaveral. Dummy second stage (500 km range).

NASA Aerobee-Hi successfully reached 96 miles above Wallops Station in test of behavior of liquid hydrogen in zero gravity for Lewis Research Center hydrogen propulsion development.

John C. Houbolt of Langley Research Center and Charles W. Mathews of MSC made a presentation of lunar orbit rendezvous versus earth orbit rendezvous to the Manned Space Flight Management Council.

Tsien tutors Mao on science. This is one of only six times that Tsien actually met Mao.

The final medical report rejects Feoktistov's fitness to be a cosmonaut. Mishin accepts the findings of the report, but in classic manner ignores it and advocates Feoktistov be appointed as commander of the active spacecraft in the first Soyuz docking mission after return to flight. Kamanin is livid. Feoktistov has had years of training for EVA, but he has not had one day of training as a spacecraft commander, and now he wants him to command a mission due to launch in only two to three months! However agreement is finally reached on L1 commander assignments: Leonov, Bykovskiy, Popovich, Voloshin. Agreement is not reached on the second (civilian) crew member position for the flights. According to Mishin, the Soyuz and L1 flights planned from March 1 to the end of 1968 will require 16 to 18 crew members total.

High resolution photo reconnaissance satellite; returned film capsule

Meetings are held at the cosmonaut centre to plan for the big visit to the base by Marshal Grechko. N F Kuznetsov briefs plans for the centre with the general staff. Kamanin discusses the situation with Leonov. Leonov notes the saying from Lenin on a banner at the centre: "Know how to work!" Unfortunately, they have left out the second part: "Don't hurry!" Leonov states he is not assigning Volynov to any future flights.

Stationed at 63 deg E. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Pacific Ocean at 174 deg E in 1969; over the Indian Ocean 062 deg E in 1969-1975. Last known longitude (24 May 1979) 66.72 deg E drifting at 0.017 deg E per day.

A statement of agreements was reached between NASA Hq. and the Centers covering the requirements for a lunar roving vehicle (LRV). Appropriate portions of the agreements were being incorporated in a revised Apollo Program Specification and in Apollo Program Directive No. 4.

Robotic lunar soil return mission.

Threw excess equipment out of LM before lift-off.

The training session at KIS yesterday was subverted by Shonin's drunkenness. Kamanin investigates the matter all day. Shonin is said to have brought vodka to the KIS and consumed vodka during the session. Kamanin confronted him, but of course he is sober now. Kamanin cannot understand the man, He has known him for eleven years and thought him a competent person.

Attempted to reach rim of Cone Crater on moonwalk with ''golf cart'' for hauling equipment.

Replaced Cosmos 479. Possible ELINT satellite.

Decay date suspect Operation of the long-range telephone and telegraph radiocommunications system in the USSR; transmission of television programmes to stations in the Orbita network.

Geodesic satellite.

Synchronous Meteorological Satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Americas at (GOES W) 115 deg W in 1975-1976; over the Pacific Ocean (GOES W) 135 deg W in 1976-1978; over the Atlantic Ocean (GOES E) 75 deg W in 1979-1981; over the Americas at 106 deg W in 1982 As of 29 August 2001 located at 123.04 deg W drifting at 2.760 deg W per day. As of 2007 Feb 27 located at 127.44E drifting at 2.742W degrees per day.

Second generation geosynchronous ballistic missile launch detection satellite, remained in service for nearly seven years. Positioned in geosynchronous orbit over the Pacific Ocean at 135 deg W in 1977-1979; over the Indian Ocean 70 deg E in 1979-1984.

Experimental Communications Satellite. Experimental Communications Satellite (ECS). Launch time 0846 GMT. ECS was injected into the planned transfer orbit. On 9 Feb, however, ECS ceased radio transmissions about 10 seconds after the apogee kick motor was fired. Communicat ions and propagation experiments of satellite-communication systems. Operation and control experiment for geostationary satellites. Mass at launch 260 kg. Configuration - cylindrical. Height 1.9m including antenna. Diameter 1.4m. Spin stabilized. Last known longitude (13 June 1995) 146.23 deg W drifting at 33.817 deg E per day.

Oceanographic, terrestrial studies. Development of methods for comprehensive study of the oceans and the surface of the earth, and testing of the experimental system of automatic gathering of scientific information from sea and land stations. Launched under the INTERCOSMOS programme by the USSR together with the Czechoslovak Socialist Republic, the German Democratic Republic, the Hungarian People's Republic and the Socialist Republic of Romania.

Area survey photo reconnaissance; film capsule; also performed earth resources tasks. Returned in less than usual 30 day full duration.

Military cartographic satellite; returned film capsule.

Gathering meteorological information and data on penetrating radiation fluxes in circumterrestrial space.

Released 10 Romb radar calibration subsatellites.

Successful first launch of the prototype of the three-stage version of the Taurus launch vehicle being developed by Orbital Sciences for Boeing for use in the Ground-based Midcourse Defense (GMD) system. The vehicle launched the dummy payload on a trajectory over the Pacific Ocean, reaching an altitude of 2100 km and traveling 6500 km down range.