CICERO 1, 2 & 3

USA

Spacecraft nº:

US spacecraft nº:

Launch data:

Type	CICERO 1	CICERO 2	CICERO 3
NORAD ID
Designation	17042	17042	17042
Launch date	14 Jul 2017 - 06:37 UT
Launch site	Baik, LC31/6
Launch vehicle	Soyuz-2-1a Fregat-M
Mission	Meteo
Earth orbit:
Perigee / Apogee	587 x 604 km	587 x 604 km	587 x 604
Eccentricity
Inclination	97.6°	97.6°	97.6°
Period	min	min
Decay	min	min

Launched together with: Kanopus-V-IK 1 - Flying Laptop - WNISAT 1R - TechnoSat - NORSAT 1 & 2 - Corvus-BC 1 & 2 - MKA-N 1 &: 2 - Flock-2k - Lemur-2 42-49 - NanoACE - Mayak - Iskra-MAI-85 - Ecuador-UTE-YuZGU -

Spacecraft data:

Prime manufacturer	Tyvak
Platform	6U cubesats
Operator	GeoOptics
Mass at launch	kg
Dry Mass	kg
Basic shape
Dimension (m)
Equipment
Solar array
Stabilization
Propulsion
DC power
Design lifetime

Description:

CICERO 1 to 3 are 6U cubesats for the US company GeoOptics built by Tyvak, with GPS-RO weather payloads.

Ref.: #7(JR740) - update: 13.08.17