The Constellation

GeoOptics is developing a constellation of small satellites to collect data about Earth’s climate and environment from low Earth orbit (LEO). The constellation is called CICERO, for Community Initiative for Continuous Earth Remote Observation.  The first CICERO satellite is scheduled to be launched in late 2014.

Artist’s rendering of the LASP design for the CICERO Pathfinder spacecraft.

CICERO will initially perform GPS and Galileo radio occultation (GNSS-RO) of Earth’s atmosphere as described under the Science tab above.  The sensors will deliver critical data on the state of the earth’s atmosphere and ionosphere to scientists and decision makers worldwide. Products will include high-accuracy profiles of atmospheric density, pressure, temperature, moisture, and winds, as well as 3D maps of the electron distribution in the ionosphere.  Principal applications will be weather forecasting, climate research, and space weather monitoring.

CICERO will be built up over time, starting with the launch of a first spacecraft in late 2014.  The initial operational constellation (CICERO-I) will consist of 12 LEOs in multiple orbit planes for broad global coverage. CICERO-I is expected to be fully operational in 2017.

 

SPACE BASED SENSOR NETWORK

Typical space based Earth sensors are sizable instruments carried on large spacecraft, typically costing hundreds of millions of dollars each for the instrument alone.  The average cost of a focused, single-purpose mission on NASA’s Earth science “Decadal Survey” list is approaching $1 billion.  The cost of multi-sensor super-platforms, such as the next-generation weather satellites of NOAA’s Joint Polar Satellite System, now exceeds $5 billion each.  Despite these extraordinary costs, sensors on a single platform have limited coverage and can take a full day or many days to cover most of the earth.

CICERO introduces an altogether different approach.  It will comprise many small spacecraft, each equipped with one or more small, low-cost, high-performance sensors, exploiting the same micro-technologies found in modern cell phones and notebook computers.  The spacecraft design is modular for low-cost expandability and versatility. Deployed as a distributed network, the system will provide global coverage in less than one hour and deliver improved measurement quality, all at a substantially lower cost than traditional systems.


DEVELOPMENT & DEPLOYMENT TIMELINE

GeoOptics was founded in 2006 just as the first dedicated GPS Radio Occultation constellation, COSMIC (see www.cosmic.ucar.edu), was launched.  At that time, following multiple experimental missions, it was clear that GPS RO was the atmospheric sensing technique of the future, delivering unprecedented measurement accuracy and vertical resolution at a tiny fraction of the cost of conventional sensors.  Since then, GeoOptics and its partners have been working meticulously – raising financing and advancing the technology – towards the deployment of the first operational constellation.  Major events and milestones include:

2006 Company created
2008 NOAA Issues RFQ for the provision of key environmental data products by commercial means
2010 Preliminary system design is completed, identifying major needed technology development needs
GeoOptics completes first round of financing, raising multiple millions of dollars
Prototype spacecraft design presented to investors and stakeholders
GeoOptics signs MOU with University of Colorado Laboratory for Atmospheric and Space Physics (LASP) to collaborate on CICERO
2011 Development of key technologies continues for CICERO system
Second round of financing complete, bringing total raised to more than $10 million
GeoOptics signs long term teaming agreement with CU/LASP
GeoOptics moves into new Boulder facility, collocated with CU/LASP
2012 Initial engineering model spacecraft to be completed at LASP
2014 Launch of the first CICERO Pathfinder spacecraft
2015 Launch of the second CICERO Pathfinder spacecraft
2016 Completion of six-satellite operational CICERO constellation
2017
Completion of twelve-satellite operational CICERO constellation

 

 

GeoOptics (C)2013