Failed · Failure
3MV-1A was a deep-space return technology experiment. Its planned route extended 12–16 million km from Earth, outside the ecliptic, before returning after roughly six months. The actual spacecraft remained in Earth orbit after Blok L failed and reentered on November 14, 1963.
- Destinations
- Launch vehicle
- Molniya
- Launch site
- Tyuratam (Baikonur Cosmodrome), U.S.S.R
- Countries
- Soviet Union
- Mission types
- Technology demonstrator, Flyby
Chronology
Mission timeline
Loss of contact
Telemetry from the Blok L upper stage lost
The master catalog records that after launch and insertion into Earth orbit, telemetry from the Blok L upper stage was lost at about 6:45:44 UT, and that it is thought the main engine turbopump exploded upon ignition, destroying the spacecraft. Recorded at day precision because the page hedges the time itself with the word about.
EarthLaunch
Launched into Earth orbit on a Molniya
NSSDCA's launch/orbital information page gives the launch date and time as 1963-11-11T06:28:00Z, recorded at minute precision because the page prints a whole minute with zero seconds, and an Earth orbit with a periapsis of 182.00 km, an apoapsis of 216.00 km, a period of 88.50 minutes and an inclination of 64.800°. The master catalog prints the same time as 6:28 UT on 11 November 1963. Source review: The NSSDCA introduction is uncertain about a Venus flyby versus Earth-orbit test; its technical description and NASA history identify a deep-space return experiment. The planned route did not occur. NSSDCA launch 06:28 UTC conflicts with 06:23:34 UT in the history. Blok L telemetry loss at about 06:45:44 UT is approximate and does not resolve liftoff.
EarthMission end
Orbit decayed three days after launch
The master catalog records that the orbit decayed on 14 November, three days after launch, and the launch/orbital information page gives a decay date of 1963-11-14.
Earth
Mission architecture
Vehicles
Cosmos 21 · Spacecraft
Destinations: Venus
3MV-1 No. 1 SA · Other
Trajectory record
Trajectory dataset not yet available
Known dates and encounters do not uniquely determine a flight path. This mission’s sourced timeline is available above; no verified trajectory is currently published here.
What is needed to reconstruct this path?
- A frame-qualified position and vector velocity at an epoch, or equivalent complete orbital elements.
- Separate state histories and release epochs for the listed vehicles; a parent mission trajectory cannot be assigned to every component.
- Finer event-time constraints where required by an orbital reconstruction; the stored day/month/year precision is retained.
- The actual failed-flight state history. Intended destinations are not evidence that the spacecraft reached them.
Provenance
Sources
Each source is listed once and labeled with the mission, event, trajectory, or destination/body context it supports.
Data verified through September 14, 2026
- Cosmos 21 - NSSDCA Master Catalog (spacecraft 1963-044A), archived snapshot — NSSDCAArchive · Supports: mission claims · event claims
- Cosmos 21 - NSSDCA launch/orbital information (1963-044A), archived snapshot — NSSDCAArchive · Supports: mission claims · event claims
- GCAT: General Catalog of Artificial Space Objects (auxiliary catalog), J. McDowell — OTHEROther · Supports: mission claims
- Siddiqi (2018): Beyond Earth, a chronicle of deep space exploration 1958–2016 — NASAMission page · Supports: mission claims · event claims
- Cosmos 21: mission, orbit and collection records inspected September 2026 — NSSDCAMission page · Supports: mission claims · event claims
- Planet Sizes and Locations in Our Solar System — NASAOther · Supports: destination/body context