Globalstar FM5, 7, 9 to 13, 16 to 18, 20 & 21

Launch Failure

Liftoff Time (GMT)

20:29:00

Wednesday September 9, 1998

Mission Details

Launch Notes

Guidance system failure at T+272 seconds caused shutdown of 2nd stage engine. Following this failure, Globalstar cancelled its contract, which still included two other Zenit flights.

Globalstar FM5, 7, 9 to 13, 16 to 18, 20 & 21

Wiki

Globalstar, Inc. is an American satellite communications company that operates a low Earth orbit (LEO) satellite constellation for satellite phone and low-speed data communications, somewhat similar to the Iridium satellite constellation and Orbcomm satellite systems. The constellation operates in a 1410 km orbit inclined at 52 degrees, and will also have 8 spares. The satellites are based on the SS/Loral LS-400 platform, with the body is trapezoidal in shape with two deployed solar panels, in order to allow multiple satellites to be carried on the same launch. The satellite is 3-axis stabilized and employs magnetometers on a deployable boom, sun sensors, GPS as attitude sensors, and carries two deployable solar arrays delivering 1100 W for normal operations. The propulsion system employs hydrazine, and its primary use is station keeping. Each satellite weighs 450 kg, with a dry mass of 350 kg, and is designed for a 7.5 year lifetime. The payload antennas are phased arrays mounted on the satellite body. The Attitude control, orbit control and solar panels were delivered by Dornier.

Low Earth Orbit

12 Payloads

6,600 kilograms

Rocket

Retired
Zenit-2

Active 1985 to 2007

Yuzhmash logo

Manufacturer

Yuzhmash

Rocket

Height: 57m

Payload to Orbit

LEO: 13,500 kg

GTO: 4,500 kg

Liftoff Thrust

7,257 Kilonewtons

Fairing

Diameter: 3.9m

Height: 13.65m

Stages

2

Launch Site

Site 45/1

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

18 days 2 hours

Stats

Zenit


31st

Mission

3rd

Mission of 1998

1998


56th

Orbital launch attempt