ERS 6
- ERS 6 ERS 6
Object Name ERS 6
Object Full Name -
Norad ID 608
Cospar ID 1963-014C
Object Type Satellite
Object Status -
Object Class -
End of Life -

ERS 6 was a 31-cm-diameter balloon satellite. It was one of three spacecraft simultaneously placed into orbit by a single launch vehicle. The spacecraft carried only one experiment on board, a solar cell damage experiment. However, the satellite was also designed to investigate the effects of the solar radiation pressure on orbital characteristics (i.e. eccentricity and period) for a negligible atmospheric drag situation. The spacecraft returned solar cell damage data.

Launch Date 1963-05-09
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: 166.4 min
Inclination: 87.3°
Apogee: 3715.0 km
Perigee: 3573.0 km
Longitude of Geo -
ECT -
Payload -
Platform -
Propulsion -
Propulsion Type -
Life Time -
Power -
Budget -
Call Sign -
Beacon -
RCS 0.7286 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: -