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Mission | |
|---|---|
Launch date | 22 October 2001 |
Launch site | Sriharikota, India |
Launcher | Antrix/ISRO PSLV-C3 |
Orbit | LEO Sun-synchronous |
Orbital parameters | 681x561 km |
Orbital plane inclination | 97.9 degrees |
Orbital period | 96.97 minutes |
Mission duration | One year (planned) |
Number of instruments | Eight |
Number of technological payloads | Six |
Mission operations and ground station | ESA/REDU dedicated 2.4 m dish, average of 4 contacts of 10 m/day, automated evening & weekend passes |
Spacecraft | |
|---|---|
Spacecraft mass | 94 kg |
Instrument mass | 25 kg |
Technological payload mass | 30 kg |
Shape | 60x60x80 cm box shaped aluminium honeycomb structure |
9 Ah Li-Ion battery
Passive thermal-control system
1 Mbit/s S-band downlink
4 kbit/s uplink
1.2 Gbit data storage
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