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IRNSS R1A

NORAD 39199 Payload GEO 2013-034A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
35713 km
Apogee
35860 km
Inclination
35.7°
Period
1436.1 min
Mean Motion
1.00275723 rev/day
TLE Epoch
2026-06-18 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude35,787 km
Orbital Velocity11,070 km/h
Velocity3.07 km/s
Orbital Period~24 hours (geosynchronous)
Orbits / Day1.00
Eccentricity0.0017
Semi-Major Axis42,158 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇮🇳 Indian Space Research Organization (ISRO) (India)
Launch Date
2013-07-01
Launch Site
SRI
Int'l Designator
2013-034A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
IRNSS R1A is an active satellite operated by Indian Space Research Organization (ISRO) (India), launched on 2013-07-01 from SRI. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Geostationary Orbit (GEO) at altitudes between 35,713 km and 35,860 km with an inclination of 35.7°. It travels at approximately 11,070 km/h (3.07 km/s), completing one full orbit every ~24 hours (geosynchronous) — that’s roughly 1.00 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks IRNSS R1A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
IRNSS R1A occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 35.7°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of IRNSS R1A’s average altitude, there are currently 713 active payloads and 58 tracked debris or rocket body fragments — notable neighbours include ASTRA 1N, GOES 16, TDRS 13. India operates approximately 108 active satellites in total, of which 36 share a similar altitude band with IRNSS R1A.
❓ Frequently Asked Questions
IRNSS R1A orbits at approximately 35,787 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 11,070 km/h — it just keeps pace with the ground below. With an inclination of 35.7°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
IRNSS R1A is operated by Indian Space Research Organization (ISRO) (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39199. You can track IRNSS R1A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
IRNSS R1A was launched on 2013-07-01 from SRI. View the full satellite launch log.
Yes — Orbital Radar tracks IRNSS R1A (NORAD ID 39199) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
IRNSS R1A travels at approximately 11,070 km/h (6,878 mph) — roughly 3.07 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.