CICERO 7

USA

Int. spacecraft nº:

US spacecraft nº:

CICERO= Community Initiative for Cellular Earth Remote Observation.

Launch data:

Designation	43143 / 18004AJ
Launch date	12 Jan 2018 - 03:59 UT
Launch site	Sriharikota, FLP
Launch vehicle	PSLV-XL
Mission	Weather, Earth observing
Earth orbit:
Perigee / Apogee	498 x 510 km
Eccentricity
Inclination	97.6 °
Period	94.6 min

Launched together with: Cartosat 2F - Microsat-TD - LEO Vantage 1 - Carbonite 2 - ICEYE X1 - INS 1C - Arkyd 6A - Landmapper-BC 3 v2 - Lemur-2 68/71 - Flock-3p′ 1/4 - MicroMAS 2a - PicSat - CANYVAL-X 1 & 2 - CNUSail 1 - KAUSAT 5 - SIGMA - DemoSat 2 - Tyvak 61C - FOX 1D - STEP Cube Lab - SpaceBEE 1/4

Spacecraft data:

Prime manufacturer	Tyvak Nano-Satellite Systems, Inc.
Platform	6U Cubesat
Operator	GeoOptics
Mass at launch	~10 kg
Dry Mass	kg
Basic shape
Dimension (m)
Equipment	Cion GPS radio occultation payload
Solar array	Solar cells
Stabilization
Propulsion
DC power
Design lifetime

Description:

CICERO 7, for GeoOptics, a Tyvak-built 6U cubesat for GNSS-RO meteorology.

External links:

Satellite tracking (n2ya.com): Real time satellite tracking

Ref.: #7(JR745), #228 - update: 15.02.18