NEE-02 Krysaor

NEE-02 Krysaor
Mission type Technology demonstration
Operator Ecuadorian Civilian Space Agency
COSPAR ID 2013-066AB
SATCAT № 39441
Website www.exa.ec/krysaor/
Mission duration Design: 1 year
Elapsed: 3 years, 25 days
Orbits completed 15,074[1]
Spacecraft properties
Spacecraft type 1U CubeSat
Manufacturer Ecuadorian Civilian Space Agency
Launch mass 1.2 kg (2.6 lb)
Dimensions 10×10 cm (3.9×3.9 in)[2]
Power 127 watts maximum
Start of mission
Launch date 21 November 2013, 07:10 (2013-11-21UTC07:10) UTC
Rocket Dnepr
Launch site Dombarovsky 370/13
Entered service 25 January 2014
Orbital parameters
Reference system Geocentric
Regime Sun-synchronous
Semi-major axis 7,024.99 km (4,365.13 mi)[1]
Eccentricity 0.0083597[1]
Perigee 588.13 km (365.45 mi)[1]
Apogee 705.58 km (438.43 mi)[1]
Inclination 97.6637 degrees[1]
Period 97.66 minutes[1]
Mean motion 14.74[1]
Epoch 10 September 2016, 08:01:29 UTC[1]

NEE-02 Krysaor is an Ecuadorian technology demonstration satellite, and Ecuador's second satellite launched to space. Built by the Ecuadorian Civilian Space Agency (EXA), it is a single-unit CubeSat nanosatellite.[3] Krysaor is a Pegasus-class spacecraft, a "twin" of Ecuador's first satellite, NEE-01 Pegaso.[4] Like Pegaso, this spacecraft's instruments include a dual visible and infrared camera which allows the spacecraft to take pictures and transmit live video from space.

See also

References

  1. 1 2 3 4 5 6 7 8 9 "NEE 02 Krysaor - Orbit". Heavens Above. 10 September 2016. Retrieved 10 September 2016.
  2. "Ecuador already has its second satellite in space, NEE-02 Krysaor". Agencia Pública de Noticias del Ecuador y Suramérica. 21 November 2013. Retrieved 9 March 2014.
  3. Graham, William (21 November 2013). "Russian Dnepr conducts record breaking 32 satellite haul". NASA Spaceflight. Retrieved 9 March 2014.
  4. "NEE-02 Krysaor". Ecuadorian Civilian Space Agency. Retrieved 9 March 2014.

Media related to NEE-01 Pegaso at Wikimedia Commons


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