CALIPSO
CALIPSO
Mission typeEarth observation
OperatorNASA / CNES
COSPAR ID2006-016A
SATCAT no.29108
Websitewww-calipso.larc.nasa.gov
Mission durationElapsed: 15 years, 10 months, 25 days
Spacecraft properties
Launch mass587 kilograms (1,294 lb)
Dimensions1.49 m × 1.84 m × 2.31 m (4.9 ft × 6.0 ft × 7.6 ft)
Power562 W
Start of mission
Launch dateApril 28, 2006, 10:02:16 (2006-04-28UTC10:02:16Z) UTC
RocketDelta 7420-10C D314
Launch siteVandenberg AFB SLC-2W
Orbital parameters
Reference systemGeocentric
RegimeSun-synchronous
Semi-major axis7,080.7 kilometres (4,399.7 mi)
Eccentricity0.0001111
Perigee altitude701 kilometers (436 mi)
Apogee altitude703 kilometers (437 mi)
Inclination98.2176 degrees
Period98.50 minutes
RAAN285.6451 degrees
Argument of perigee80.3481 degrees
Mean anomaly279.7840 degrees
Mean motion14.57093780
Revolution no.40530
 

CALIPSO is a joint NASA (USA) and CNES (France) environmental satellite, built in the Cannes Mandelieu Space Center, which was launched atop a Delta II rocket on April 28, 2006. Its name stands for Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observations. CALIPSO Launched Alongside CloudSat.

Passive and active remote sensing Instruments on board the CALIPSO satellite monitor aerosols and clouds 24 hours a day. CALIPSO is part of the "A Train", flying in formation with several other satellites (Aqua, Aura and CloudSat).

Mission

Three instruments:

In February 2009, CALIPSO switched over to the redundant laser as scheduled. The primary laser achieved its mission goal of three years of successful operation, and the redundant laser has been performing beyond expectations.

The CALIPSO mission was granted extended mission status in June 2009.[1]

The Delta II rocket with CALIPSO and CloudSat on Launch Pad SLC-2W, VAFB.
The Delta II rocket with CALIPSO and CloudSat on Launch Pad SLC-2W, VAFB.

See also

References

  1. ^ "CALIPSO - INSTRUMENT UPDATE". NASA LARC. Archived from the original on 2010-03-16.