Official name CERISE
Alternative name Cerise
Cospar ID 1995-033B
Norad ID 23606
Launch date 1995-07-07
Launch site FRGUI
Launch vehicle Ariane-40 H10-3
Country/Organization France
Type application ELINT
Operator Alcatel, DGA
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 95.6
Inclination (deg) 98.28
Perigee (km) 541
Apogee (km) 554
Eccentricity 0.0118721461187215
Mean motion (revs. per day) 15.0627615062762
Semi-Major axis (km) 6925.635
Raan (deg) 248.583
Arg of perigee (deg) 13.0689
Shape Box + 1 Ant + 2 Pan
Mass (kg) 50
Height (m) 0.6
Width (m) 0.4
Depth (m) 0.4
Span (m^2) 6.5
Contractors Alcatel Espace (prime), SSTL (bus)
Propulsion None
Configuration Microsat-70
Power Solar cells, batteries

The 50 kg Cerise (Caractérisation de l'Environement Radioélectrique par un Instrument Spatial Embarque) was built by Alcatel Espace and based on the Surrey UOSAT bus. It carried equipment to catalog wideband radio interference and develop technology for an electronic intelligence satellite.

Its main purpose was to intercept HF radio signals for French intelligence services. Based on the SSTL-70 satellite platform and with a mass of 50 kg, it was launched by an Ariane-40 H10-3 rocket from Kourou in French Guiana on 7 July 1995.

In July 1996 it collided with a piece of orbital debris. Independent analyst B. Gimle suggests the debris piece may have been 18208 1986-19RF. The satellite was observed to suddenly tumble end over end; the debris impacted the 6 m long stabilization boom. The collision tore off a 4.2-metre (13-foot) portion of Cerise's gravity-gradient stabilisation boom, which left the satellite severely damaged. SSTL controllers at Guildford regained control of the satellite using electromagnetic stabilization.

Satellite COSPAR Date LS Launch Vehicle Remarks
CERISE 1995-033B 1995-07-07 FRGUI Ariane-40 H10-3 with Helios 1A, UPM-LBSat