DECAYED

DELTA 1 DEB (ADAPTER), 2631 (Decayed)

Orbit data source: Public

DELTA 1 DEB (ADAPTER), 2631 was space debris originally from a launch on Wed, 14 Dec 1966 UTC via a THOR DELTA G launch vehicle 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.

Not visible in the next 10 days

DELTA 1 DEB (ADAPTER) details

Identifier	2631, 1966-114C
Orbit	Decayed
Last TLE update	Unknown
Origin	ARC (US)
Manufacturer	GE/RSD
Mission	Decayed spacecraft
Bus & Motor	BIOSATELLITE, Unknown motor
Mass	241 kg wet, 241 kg dry
Launch date (UTC)	1966-12-14 (58 years ago)
Launch vehicle	THOR DELTA G
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl + 1 Frust, 2.1 m
Radar Cross Section	3.079 m²

Expand to show TLE details & history

Historical TLE search

Definitive object data

Latitude	Unknown
Longitude	Unknown
Altitude	Unknown
Speed	Unknown
True Right ascension	Unknown
True Declination	Unknown
Sunlit	N/A

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.

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.

Orbital elements

Apogee altitude	Unknown
Perigee altitude	Unknown
Semi-major axis	Unknown
Eccentricity	Unknown
Inclination	Unknown
RAAN	Unknown
Arg. of periapsis	Unknown
True anomaly	Unknown
Mean anomaly	Unknown
Eccentric anomaly	Unknown
Mean motion	Unknown
BSTAR	Unknown
Orbital period	Unknown