Official name JASON
Alternative name Jason
Cospar ID 2001-055A
Norad ID 26997
Launch date 2001-12-07
Launch site AFWTR
Launch vehicle Delta-7920-10C
Country/Organization USA, France
Type application Altimetry, Radar
Operator NASA, CNES
RCS size LARGE
Decay date ON ORBIT
Period (min) 112.15
Inclination (deg) 66.04
Perigee (km) 1318
Apogee (km) 1332
Eccentricity 0.00528301886792453
Mean motion (revs. per day) 12.8399465002229
Semi-Major axis (km) 7703.135
Raan (deg) 237.9621
Arg of perigee (deg) 278.1946
Shape Box + 2 Pan
Mass (kg) 500
Height (m) 3.3
Width (m) 1.9
Depth (m) 1.9
Span (m^2) 6
Lifetime 3 years; 11.5 years (achieved)
Contractors Alcatel Space
Equipment JMR, TRSR, LRA, Poseidon-2, DORIS
Configuration Proteus Bus
Power 2 deployable solar arrays, batteries

Jason-1 is the first follow-on to the highly successful TOPEX/Poseidon mission that measured ocean surface topography to an accuracy of 4.2 cm, enabled scientists to forecast the 1997-1998 El Niño, and improved understanding of ocean circulation and its effect of global climate. The joint NASA-CNES program will launch a French spacecraft on an American Delta-7920-10C from Vandenberg AFB. Like TOPEX/Poseidon, the payload will include both American and French instruments. Jason-1 altimeter data will be part of a suite of data provided by other JPL-managed ocean missions - the GRACE mission will use two satellites to accurately measure Earth's mass distribution, and the QuikSCAT scatterometer mission will measure ocean-surface winds.

Jason 1 features following instruments:

  • JMR: Microwave radiometer
  • TRSR: GPS tracking receiver
  • LRA: Laser retroreflector array
  • Poseidon-2: A solid state radar altimeter
  • DORIS: Doppler tracking system receiver

Jason 1 was retired in July 2013 after 11.5 years in orbit, surpassing its 3 years design life. Its mission was continued by the Jason 2 and 3 satellites.

Satellite COSPAR Date LS Launch Vehicle Remarks
JASON 2001-055A 2001-12-07 AFWTR Delta-7920-10C with TIMED