NVS-03 (IRNSS-1L)

Liftoff Time

No Earlier Than October, 2025

Mission Details

NVS-03 (IRNSS-1L)

Wiki

The NVS, previously IRNSS, constellation is not a global positioning constellation, like GPS, GLONASS, Galileo, or Beidou-3, but a regional one, similar to the Chinese Beidou-1 and 2, or the Japanese QZSS, serving only the Indian sub-continent. IRNSS satellites have two payloads: a navigation payload and CDMA ranging payload in addition to a laser retro-reflector. The payload generates navigation signals at L5 and S-band. The design of the payload makes the IRNSS system interoperable and compatible with Global Positioning System (GPS) and Galileo systems. The satellite is powered by two solar arrays, which generate up to 1,660 watts, and has a lifetime of ten years.

Manufacturer: ISRO

Operator: ISRO

Geostationary Transfer Orbit

1 Payload

2,250 kilograms

Rocket

Active
GSLV Mk II

Active Since 2010

Indian Space Research Organisation logo

Agency

ISRO

Price

$47.00 million

Rocket

Height: 51.7m

Payload to Orbit

LEO: 5,000 kg

GTO: 2,500 kg

Liftoff Thrust

7,887 Kilonewtons

Fairing

Diameter: 4m

Height: 7.8m

Stages

3

Strap-ons

4

Launch Site

Second Launch Pad

Satish Dhawan Space Centre, India

Fastest Turnaround

31 days