1. REORIENTATION & LAPAN TUBSAT-1 SEPARATION REORIENTATION & SEPARATION OF DLA-U WITH PEHUENSAT-1 REORIENTATION & SRE SEPARATION CARTOSAT-2 SEPARATION LAPAN- TUBSAT SEPARATION SATELLITE SEPARATION SEQUENCE PSLV- C7 CARTOSAT-2 / SRE MISSION

2. SRE – MISSION PROFILE SRE will be in orbit for nearly 10 days during which it will perform Micro- Gravity experiments Subsequently it will be moved from Circular orbit to Repeating Elliptical Orbit (REO) It will de-boosted from REO and will be made to Re-enter and impact nearly 140 km off the coast of SHAR SRE will be recovered from the Sea T0 + 35 min Velocity: 8000 m/s T0 + 44 min Velocity: 47 m/s T0 + 46 min Velocity: 12 m/s 20 th Jan Deboost 22 nd Jan Velocity: 7350 m/s T0 PSLV- C7 CARTOSAT-2 / SRE MISSION 10 th Jan

3. Typical visibility: Prior & Post De-boost Saskatoon, Svalbard, Lucknow, Air- Borne Telemetry (ABT), Ship Borne Telemetry (SBT), SHAR PSLV- C7 CARTOSAT-2 / SRE MISSION De- Boost START Altitude : 638 km Latitude : 4 deg Longitude : - 92 deg De- Boost END Altitude : 635 km Latitude : 52 deg Longitude : - 105 deg RE- ENTRY Altitude : 100 km Latitude : 27 deg Longitude : 84 deg Data down load regions

4. SHAR CHENNAI 140 km 50x15 km – Stay out zone for ship Air borne Telemetry from SHAR Ship borne Telemetry Dornier aircraft from Chennai Chetak Helicopter from Sarang ICG Ship - Sarang DEPLOYMENT OF RECOVERY SYSTEMS Probable impact zone 30x5 km Reentry ground trace 50 km 15 km PSLV- C7 CARTOSAT-2 / SRE MISSION

5. EDUSAT