Oct 15, 1994
IRS-P2
First Spacecraft successfully orbited onboard the second developmental flight of PSLV.
Mission completed during 1997 after serving for 3 years.
| Mission | Operational Remote Sensing |
| Weight | 804 kg |
| onboard power | 510 Watts |
| Communication | S-band, X-band |
| Stabilization | Three axis body stabilized with 4 Reaction Wheels, Magnetic torquers |
| RCS | 4 tanks containing Monopropellant Hydrazine based with sixteen 1 N thrusters and one 11 N thruster |
| Payload | Two solid state Push Broom Cameras operating in four spectral bands in the visible and near-IR range using CCD arrays: LlSS-2A & LlSS-2B (Resolution: 32.74 metre) |
| Launch date | October 15, 1994 |
| Launch site | SHAR Centre, Sriharikota, India |
| Launch vehicle | PSLV-D2 |
| Inclination | 98.68o |
| Repetivity | 24 days |
| Mission completed on | 1997 |
प्रमोचन भार / Launch Mass:
804 kg
शक्ति / Power:
510 W
प्रमोचक राकेट / Launch Vehicle:
PSLV-D2
उपग्रह का प्रकार / Type of Satellite:
Earth Observation
निर्माता / Manufacturer:
ISRO
स्वामी / Owner:
ISRO
अनुप्रयोग / Application:
Earth Observation
कक्षा का प्रकार / Orbit Type:
SSPO