Globalstar 31

USA



Launch data:

Designation: 25943 / 99058A
Launch date18 Oct 1999
Launch site Baikonur, LC-1
Launch vehicle  Soyuz-U/Ikar
Mission Telecommunications
Perigee/Apogee 1400 km
Inclination 52°
Period 110 min


Spacecraft data:

Prime contractor  Space Systems/Loral
Platform  LS-400
Operator 
Mass at launch  450 kg
Dry Mass 400 kg
Basic shape  trapezoidal shape
Dimension (m) 
Solar array  10.75m span (2 panels)
Stabilization  3-axis
DC power  1100 W
Design lifetime  7.5 yrs


Globalstar's payload

Capacity 2800 phone circuits
Voice 9600 bps
Fax yes
Data 9600 bps
Mobile uplink 2483.5 - 2500 MHz via 91-element phased-array antenna
Mobile downlink 1610 - 1626.5 MHz via 61-element phased-array antenna
Gateway uplink 5091 - 5250 MHz
Gateway downlink 6875 - 7055 MHz

Compatible with GSM, CDMA and AMPS.

Ref: #15 - update: 06.01.11