NEXT SPACEFLIGHT

Status

Success

Okean-O n°1

Launch Time
Sat Jul 17, 1999 05:37 UTC

Rocket

Zenit-2
VKS RF
Status: Retired
Liftoff Thrust: 7,257 kN
Payload to LEO: 13,500 kg
Payload to GTO: 4,500 kg
Stages: 2
Strap-ons: 0
Rocket Height: 57.0 m
Fairing Diameter: 3.9 m
Fairing Height: 13.65 m

Mission Details

Okean-O n°1

The Okean-O series, a joint Ukrainian/Russian remote sensing program, represents a new generation spacecraft over the Okean-O1 series with regard to the sensor complement. All the scientific assets of the spacecraft, scientific data downloaded from each instrument are mutually divided between Russia and Ukraine on an equal basis.

The satellite is three-axis stabilized with an attitude pointing accuracy of ±10 arcmin and an angular stabilization velocity of ±0.0015º/s. Solar power of up to 3.5 kW is provided. The spacecraft mass is 6150 kg, the mass of the onboard special complex (BSC) is 1520 kg. The spacecraft bus, a cylinder, has a diameter of 1.9 m and a length of 6.6 m. The S/C design life is three years. Note: The Okean-O-1 spacecraft is also being referred to as Sich-2.

Okean-O n°1 stopped all operations in the fall of 2000 (after a year of operations) due to attitude control problems of the spacecraft. At the time, both space agencies, NKAU and RKA (Russian Space Agency or Rosaviakosmos), did not provide any funding for the development of a further Okean-O spacecraft due to the tight economic situation in the Ukraine and in Russia.

Payloads: 1
Total Mass: 6,150.0 kg
Sun-Synchronous Orbit

Location

Site 45/1, Baikonur Cosmodrome, Kazakhstan

Stats

1999

41st orbital launch attempt

Zenit

33rd mission
2nd mission of 1999
24th successful mission
2nd consecutive successful mission