Tiros 10

USA



Launch data:

Designation01430 / 65051A
Launch date02 Jul 1965 - 04:07 UT
Launch siteCC, LC17B
Launch vehicle Delta-C ( #415/D32)
MissionMeteorology
Earth orbit:
Perigee/Apogee 721 x 807 km
Inclination 98.8°
Period 100.1 min

Test satellite for the Tiros Operational Satellite (TOS)

Specifications

Prime contractor  
Platform  
Mass at launch  
Dry mass 127 kg
Dimension was in the form of an 18-sided right prism, 107 cm across opposite corners and 56 cm high
Solar array  
Stabilization spin-stabilized (between 8 and 12 rpm)
DC power  
Design lifetime  

Can be heard at 136.235 MHz

The satellite was equipped with two identical wide-angle TV cameras with 1.27 cm vidicon for taking earth cloudcover pictures. The pictures could be transmitted directly to either of two ground receiving stations or stored in a tape recorder on board for subsequent playback if the spacecraft was beyond the communication range of the station.

End of life

Out of service 31 Jul 1966
Cause desactivated, still in orbite

External links:


Ref: #7, #228 - update: 05.10.20