MOS-1 was equipped with three types of sensors: MESSR,( a spectrometer for measuring visible near infrared radiation), VTIR, (a device for measuring visible thermal infrared radiation), MSR, (for measuring microwave radiation).These seusor finished their rolls oe seuding wave onNovember 29,1995. MOS-1b, which has the same functions as MOS-1, was launched subsequently as a follow-up.and finished its opration on April 17,1996
Main Characteristics
Sbape
Box type with expanding type solar paddle (one wing)
Body 1.26x1.48x2.4(m)
Solar paddle 2.0x5.28(m)
Weight
Approx 7.40kg (at lift off)
Attitude Contrel
Three-axis stabilized (controled bias momentum)
Mission life
2 years
Reliability
0.5 (after 2 years in orbit)
Launch vehicle
MOS-1 : N-II rocket, MOS-1b : H-I rocket
Altitude : Approx. 909km
Inclination : Approx. 99deg.
Period : Approx. 103min.
Recurrent period : 17 days (west-ward shift)
Descending Node Time : 10:00-11:00 a.m.
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