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Mission type | Navigation |
---|---|
Operator | ISRO |
COSPAR ID | 2015-018A |
SATCAT no. | 40547 |
Website | http://www.isro.gov.in/Spacecraft/irnss-1d |
Mission duration | 12 years |
Spacecraft properties | |
Spacecraft | IRNSS-1D |
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 | 1,660 W |
Start of mission | |
Launch date | 11:49,March 28, 2015(UTC) [1] |
Rocket | PSLV-XL C27 [2] |
Launch site | Satish Dhawan SLP [1] |
Contractor | ISRO |
Orbital parameters | |
Reference system | Geocentric |
Regime | Geosynchronous |
Longitude | 111.75° East |
Perigee altitude | 35,750.0 km (22,214.0 mi) [3] |
Apogee altitude | 35,884.1 km (22,297.3 mi) [3] |
Inclination | 30.43 degrees [3] |
Period | 1436.1 minutes [3] |
Epoch | 5 May 2015, 20:43:00 UTC [3] |
IRNSS-1D is a satellite in the Indian Regional Navigational Satellite System (IRNSS) constellation. The satellite is the fourth of seven in the constellation, launched after IRNSS-1A, IRNSS-1B and IRNSS-1C. The satellite is the only satellite in the constellation slated to provide navigational services to the region. The satellite will be placed in geosynchronous orbit. [4] It was launched successfully on 28 March 2015 onboard ISRO's PSLV-C27 from Satish Dhawan Space Centre, Sriharikota. [5] [6] [7]
The satellite will help in augmenting the satellite based navigation system of India which is currently under development. The navigational system so developed will be a regional one targeted towards South Asia. The satellite will provide navigation, tracking and mapping services. [8]
IRNSS-1D satellite has two payloads: a navigation payload and CDMA ranging payload in addition with a laser retro-reflector. The payload generates navigation signals at L5 and S-band. The design of the payload makes the IRNSS system inter-operable and compatible with Global Positioning System (GPS) and Galileo. [4] The satellite is powered by two solar arrays, which generate power up to 1,660 watts, and has a life-time of ten years.
The total cost of the mission was estimated at ₹14 billion. [9]