Satellite description
ATLAS CENTAUR R/B(2), 6425 is space debris originally from a launch on Fri, 06 Apr 1973 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
Satellite metadata
Identifier
Orbit
Last TLE update
Unknown
Origin
LERC (US)Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 37, Unknown motor
Mass
~70 kg wet, ~70 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Domed Cyl + 1 Nozzle, 8.59 m
Radar Cross Section
6.614 m²
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.