This article will address the topic of IRNSS-1F, a matter of great relevance and interest today. IRNSS-1F has captured the attention of experts and the general public due to its impact on various areas of society. Along these lines, different aspects related to IRNSS-1F will be examined, from its origin and evolution, to its implications in the contemporary world. The opinions and positions of specialists in the matter will also be analyzed, as well as the possible solutions or measures to be taken regarding this issue. Without a doubt, IRNSS-1F is a topic that leaves no one indifferent, so it is essential to deepen its study and understanding to achieve a more complete and clarifying vision.
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Mission type | Navigation |
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Operator | ISRO |
COSPAR ID | 2016-015A |
SATCAT no. | 41384 [1] |
Website | http://www.isro.gov.in/Spacecraft/irnss-1f |
Mission duration | 12 years |
Spacecraft properties | |
Spacecraft | IRNSS-1F |
Spacecraft type | Satellite |
Bus | I-1K |
Manufacturer | ISRO Satellite Centre Space Applications Centre |
Launch mass | 1,425 kilograms (3,142 lb) |
Dry mass | 598 kilograms (1,318 lb) |
Power | 1660 W |
Start of mission | |
Launch date | 10:31, March 10, 2016 (UTC) |
Rocket | PSLV-XL C32 |
Launch site | Satish Dhawan Second |
Contractor | ISRO |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sub-Geosynchronous Transfer Orbit (sub-GTO)[2] |
Perigee altitude | 35,708 km (22,188 mi)[3] |
Apogee altitude | 35,862 km (22,284 mi)[3] |
Inclination | 32.5 deg E |
IRNSS-1F is the sixth navigation satellite out of seven in the Indian Regional Navigational Satellite System (IRNSS) series of satellites after IRNSS-1A, IRNSS-1B, IRNSS-1C, IRNSS-1D and IRNSS-1E. The satellite is one among the seven of the IRNSS constellation of satellites launched to provide navigational services to the region.[4]
It was launched aboard a PSLV-XL rocket bearing flight number C32 and was successfully put into geosynchronous orbit at 1601 hrs IST on 10 March 2016.[5][6]
The satellite carries two types of payloads. The navigation payload transmit navigation service signals to users and ranging payload consists of C-band transponder that facilitates accurate determination of the range of the satellite.[4]
It carries Corner Cube Retro Reflectors for laser ranging.[7]
IRNSS-1F has a 12-year mission life.[2]