SECOR 4 (EGRS 4)
- SECOR 4 (EGRS 4) SECOR 4 (EGRS 4)
Object Name SECOR 4 (EGRS 4)
Object Full Name -
Norad ID 1315
Cospar ID 1965-027B
Object Type Satellite
Object Status -
Object Class -
End of Life -

SECOR 4 (EGRS 4) was launched from Vandenberg AFB via an Atlas Agena A launch vehicle. The small geodetic spacecraft was intended to be used to precisely determine points on the earth, but the mission failed.

Launch Date 1965-04-03
Decay Date -
Launch Vehicle -
Launch Site Air Force Western Test Range, California, USA
Launch Provider -
Launch Provider Country -
Launch Mass -
Dry Mass -
User -
Mission -
Mission Detail -
Country of Registry -
Programme -
Operator -
Country of Operator United States
Contractor -
Country of Contractor -
Payload Contractor -
Payload Contractor Country -
Orbit Status Earth Orbit
Orbit -
Orbit Type -
Period: 111.4 min
Inclination: 90.3°
Apogee: 1316.0 km
Perigee: 1266.0 km
Longitude of Geo -
ECT -
Payload -
Platform -
Propulsion -
Propulsion Type -
Life Time -
Power -
Budget -
Call Sign -
Beacon -
RCS 0.1720 m²
References -
Date
Rise
Heights
Set
Pass Time
Visible
Time
Altitude
Azimuth
Time
Altitude
Azimuth
Time
Altitude
Azimuth

					


Angular Momentum: -
Eccentricity: -
Inclination: -
RAAN: -
Argument of Perigee: -
True Anomaly: -
Period: -
Semi-Major Axis: -
Perigee: -
Apogee: -
Mean Motion: -
Mean Anomaly: -

Latitude: -
Longitude: -
Altitude: -
Speed: -
Azimuth: -
Elevation: -
Range: -