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// geodesy · 1966

SECOR 6

American military geodetic satellite. SECOR 6 was launched on June 9, 1966 aboard a Atlas SLV-3 Agena D from Vandenberg. Latest status in GCAT: reentered (orbital decay) (Jul 6, 1967).

COSPAR 1966-051BNORAD 2205United States

Identity

Name in GCAT
EGRS VI
Common name
SECOR 6
Payload designation
Secor II S/N 7 (TR-30A)
International designator
1966-051B
NORAD catalog number
2205
GCAT identifier
S02205
UN registration
A/AC.105/INF.141

Mission

Mission type
Geodesy
Use
Defense
Program
Secor II
Owner
USA ACE
Country
United States
Builder
ITT Federal Laboratories
Platform (bus)
Secor

Launch

Date
June 9, 1966 · 20:15 UTC
Launch record
1966-051Success
Spaceport
Vandenberg · pad PALC1-2

Orbit and fate

Orbit class (GCAT)
LEO/P
Perigee
171 km
Apogee
3,479 km
Inclination
90.05°
Status
Reentered (orbital decay)
Status date
July 6, 1967
Last known active
July 1967
End of operations
July 1967

Size

Mass
18 kg
Dry mass
18 kg
Length
0.2 m
Diameter
0.40 m
Span
0.5 m

Source: GCAT payload, deep-space and lander catalogs, Jonathan C. McDowell (CC BY 4.0); Wikidata Q52376243 (CC0).